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Pilots' Checklist

Model 182TNAV Ill AVIONICS O PTION

THIS CHECKLIST IS CURRENT WITH MODEL 182T NAV Ill POH FAA APPROVED U.S.PILOT'S OPERATING HANDBOOK REVISION 3, DATED 19 JULY, 2005. (PART NUMBER182TPHAUS-03)

- COPYRIGHT@ 2004CESSNA AIRCRAFT COMPANY

WICHITA, KANSAS, USA

REVISION 1 19 JULY 2005

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Pilots' Checklist NAV Ill Avionics Model 182T -NOTICE

THE PILOT'S CHECKLIST SHOULD NOT BE USED UNTILTHE FLIGHT CREW HAS BECOME COMPLETELYFAMII-IAR WITH THE AIRPLANE AND SYSTEMS. ALLNORMAL AND EMERGENCY PROCEDURE ITEMS ANDCOMPLETE PERFORMANCE IN THE PILOT'SOPERATING HANDBOOK AND FAA APPROVEDAIRPLANE FLIGHT MANUAL SHALL TAKE PRECEDENCEIN CASE OF CONFLICT.

REVISIONSChanges and/or additions to this checklist will be covered by Owner Advisoryrevisions published by Cessna Aircraft Company. Owner Advisories aremailed automatically at no charge to owners of United States registeredairplanes according to FAA records at the time of the issuance. OwnerAdvisories are mailed automatically to owners of other than United Statesregistered airplanes, to the subscription address provided Cessna on anOwner Advisory Application.

NOTEIt is the responsibility of the owner to maintain this checklistin a current status when it is being used for operational -purposes.

Owners should contact a Cessna Service Station whenever the revisionstatus of their checklist is in question. -

1 REVISED MATERIAL INDICATORSA bar will extend the full lengin of deieted, new or revisedted--addebonnew -or presently existing pages. This bar will be located adjacent to the applicabletext in the outer margin of the page.A bar located adjacent to the figure number in the outer margin will be used -o indicate that the figure number only has changed.An asterisk located at the end of a figure number will be used to indicate thatan illustration has been revised or is all new material (Ex: Figure 4*). -A change bar in the footer will indicate a revision to the headerlfooter, a newpage, format or spellinglgrammar changes and/or that information hasslipped to or from that page.All revised pages will carry the revision number opposite the page number on -the applicable page. A list of revisions is located at the beginning of the Logof Effective Pages.

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- Model 182T. NAV I ll Avionics Pilots' ChecklistNORMAL PROCEDURESTABLE OF CO NTENTS

AIRSPEEDS FOR NORM AL OPERATIONS .............................................N-2PREFLIGHT INSPECTION .......................................................................N-3BEFORE STARTING ENGINE ................................................................ -10 1STARTING ENG INE (USING B ATTERY) .............................................. N-10STARTING ENG INE (USING EXTERNAL POWER) ..............................N-12BEFORE TAKEOFF ................................................................................N-14

...............................................................................................AKEOFF N - I7NORMAL TAKEOFF .........................................................................N-17SHORT FIELD TAKEOFF .................................................................N-17

..................................................................................NROUTE CI-IMB N - I8NORMAL CLIMB ............................................................................... N - I 8

...............................................AXIMUM PERFORMANCE CLIMB N-18...................................................................................................RUISE N-18

...............................................................................................ESCENT N-19................................................................................EFORE LANDING N-20

............................................................................................ANDING N-21..........................................................................ORMAL LANDING N-21

.................................................................HORT FIELD LANDING N-21...........................................................................ALKED LANDING N-2 I

................................................................................FTER LANDING N-22...........................................................................ECURING AIRPLANE N-22

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-ilots' Checklist NAV Il l Avionics Model 182TAIRSPEEDS FO R NORMAL OPERATIONSUnless otherwise noted, the following speeds are based on a maximumweight and may be used for any lesser weight.TAKEOFF:

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ormal Climb 70 - 80 KlAS! Short Field Takeoff, Flaps 20, Speed at 50 Feet . . . . . . . . . . . 58 KlAS

ENROUTE CLIMB, FLAPS UP:. . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ormal, Sea Level 85 - 95 KlAS. . . . . . . . . . . . . . . . . . . . . . . .Best Rate-of-Climb, Sea Level. 80 KlAS! . . . . . . . . . . . . . . . . . . . . . . .Best Rate-of-Climb, 10,000 Feet 74 KlAS. . . . . . . . . . . . . . . . . . . . . . . .Best Angle-of-Climb, Sea Level 65 KlAS. . . . . . . . . . . . . . . . . . . . . .est Angle-of-Climb, 10,000 Feet. 68 KlAS

LANDING APPROACH:. . . . . . . . . . . . . . . . . . . . . . .ormal Approach, Flaps Up 70 - 80 KlAS. . . . . . . . . . . . . . . . . . . . . .ormal Approach, Flaps Full 60 - 70 KlAS. . . . . . . . . . . . . . . . . . . . . .hort Field Approach, Flaps Full. .6 0 KlAS

BALKED LANDING:. . . . . . . . . . . . . . . . . . . . . . . . . . .aximum Power, Flaps 20" 55 KlAS

MAXIMUM RECOMMENDED TURBULENT AIR PENETRATION SPEED:. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .31 00 POUNDS. 110 KlAS2600 POUNDS 101 KlAS. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .100 POUNDS 91 KlAS

MAXIMUM DEMONSTRATED CROSSWIND VELOCITY:. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .akeoff or Landing 15 KNOTS

All references to Sections throughout this checklist refer to thecorresponding Section of the Pilot's Operating Handbook.

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- Model 182T NAV Ill Avionics- NORMAL PROCEDURES

PREFLIGHT INSPECTION

Pilots' Checklist

Figure 1NOTE

Visually check airplane for general condition during walk-around inspection. Airplane should be parked in a normalground attitude (refer to Figure 1-1 in the POH) to ensure thatfuel drain valves allow for accurate sampling. Use of therefueling steps and assist handles will simplify access to theupper wing surfaces for visual checks and refuelingoperations. In cold weather, remove even smallaccumulations of frost, ice or snow from wing, tail and controlsurfaces. Also, make sure that control surfaces contain nointernal accumulations of ice or debris. Prior to flight, checkthat pitot heater is warm to touch within 30 seconds withbattery and pitot heat switches on. If a night flight is planned,check operation of all lights, and make sure a flashlight isavailable.

(Continued Next Page)

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Pilots' Checklist NAV Ill Avionics Mod el 182TPREFLIGHT INSPECTION (Continued)@ CABIN

1. Pitot Tube Cove r . . . . . . . . . . REMO VE (Check for pitot blockage)2. Pilots' Operating Ha ndb ook . . . . . . . . . . . ACCESSIBLE TO PILOT3. Garmin G l OOOTM Cockpit. . . . . . . . . . . . . . . . .eference Guide ACCES SIBLE TO PILOT4. Airplane Weight and Balance. . . . . . . . . . . . . . . . . . . . .CHECKED5. Parking Brake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET6. Control Wheel Lo ck . . . . . . . . . . . . . . . . . . . . . . . . . . . . . REMOVE

I WARNING IWHEN THE MASTER SWITCH IS ON, USING ANEXTERNAL POWER SOURCE, OR MANUALLYROTATING THE PROPELLER, TREAT THE PROPELLERAS IF THE MAGNETOS SWITCH WERE ON. DO NOTSTAND, NOR ALLOW ANYONE ELSE TO STAND, WITHINTHE ARC OF THE PROPELLER SINCE A LOOSE ORBROKEN WIRE, OR A COMPONENT MALFUNCTION,COULD CAUSE THE ENGINE TO START.

MAGNETOS Switch. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFFAVIONICS Switch (BUS 1 and BUS 2). . . . . . . . . . . . . . . . . . .OFFMAST ER Switch (ALT and BAT) . . . . . . . . . . . . . . . . . . . . . . . . ONPrimary Flight D isplay (PFD) . . . . . . . . . . . . . . . . . . . .VERiF'i ONFUEL QTY (L and R) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK. . . . . .OW FUEL L and LO W FUEL R Annunciators VERIFY OFFOIL PRESSURE Annunciator. . . . . . . . . . . . . . . . . . . . VERIFY ONLOW VOLTS Annunciator. . . . . . . . . . . . . . . . . . . . . . . VERIFY ON

LOW VACUUM Annunc iator. . . . . . . . . . . . . . . . . . . . . VERIFY ONAVIONICS Switch (BUS 1) . . . . . . . . . . . . . . . . . . . . . . . . . . . . NForward Avionics Fan. . . . . . . CHECK AUDIBLY FOR OPERATIONAVIONICS Switch (BUS 1). . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFAVIONICS Switch (BUS 2) . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON(Continued Next Page)

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- Mod el 182T NAV Il l Avionics Pilots' ChecklistPREFLIGHT INSPECTION (Continued)@ CABIN (Continued)

. . . . . . . . . .f t Avionics F an . CHEC K AUDIBLY FOR OPERA-TION. . . . . . . . . . . . . . . . . . . . . . . . . . .VIONICS Switch (BUS 2). OFF

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .lTOT HEAT Switch ON(Carefully check that pitot tube is warmto the touch w ithin 30 seconds). . . . . . . . . . . . . . . . . . . . . . . . . . . . .ta ll Warning System CHEC K(Gently move the stall vane upward andverify that the stall warning horn is heard). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .lTOT HEAT Switch OFF

. . . . . . . . . . . . . . . . . . . . . . .ASTER Switch (ALT and BAT) OFF. . . . . . . . . . . . . . . . . . . . . . . . . .r im Controls. TAKEOFF posi tion. . . . . . . . . . . . . . . . . . . . . . . . . . .UEL SELECTOR Valve. BOTH

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . .LT STATIC AIR Valve. OF F. . . . . . . . . . . . . . . . . . . .ire Extinguisher VERIFY gage green arc

@ EMPENNAGE. . . . . .. Baggage Compartment Door CHEC K latched, lock with key. . . . . . . . . . . . . . . . . . . .. Rudder Gust Lock (if installed). REM OVE

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. Tail Tiedown. DISCO NNEC T4. Control Surface s. . . CHECK for freedom of movement and security. . . . . . . . . . . . . . . . . . . . . . . . . . . . .. Trim Tab. CHEC K for security. . . . . . . . . . . . . . . . . .. Antennas CH ECK for security of attachmentand gen eral condition

@ RIGHT WING TRAILING EDGE. . . . . . . . . .. Aileron CH EC K for freedom of movem ent and security

. . . . . . . . . . . . . . . . . . . . . .. Flap CH ECK for security and condition


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Pilots' Checklist NAV Il l Avionics -Model 182TPREFLIGHT INSPECTION (Continued)@ RIGHT WING

1. Wing Tiedown . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DISCONNECT2. Fuel Tank Vent Opening . . . . . . . . . . . . . . . . . CHECK for blockage3. Main Wheel Tire. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK

for proper inflation and general condition(weather checks, tread depth and wear, etc.). . . . . . . . . . . . . . . . . .. Fuel Tank Sump Quick Drain Valves DRAINI Drain at least a cupful of fuel (usirlg sampler cup) from eachsump location to check for water, sediment, and proper fuelgrade before each flight and after each refueling. If water isobserved, take further samples until clear and then gentlyrock wings and lower tail to the ground to move anyadditional contaminants to the sump locations. Takerepeated samples from all sump locations until allcontamination has been removed. If contaminants are stillpresent, refer to WARNING below and do not fly airplane.

NOTECollect all sampled fuel in a safe container. Dispose of thesampled fuel so that it does not cause a nuisance, hazard ordamage to the environment.

I WARNINGIF, AFTER REPEATED SAMPLES, EVIDENCE OFCONTAMINATION STILL EXISTS, THE AIRPLANESHOULD NOT BE FLOWN. TANKS SHOULD BEDRAINED AND SYSTEM PURGED BY QUALIFIEDMAINTENANCE PERSONNEL. ALL EVIDENCE OFCONTAMINATION MUST BE REMOVED BEFOREFLIGHT.

5. Fuel Quantity. . . . . . . . . . . . . . CHECK VISUALLY for desired level6. Fuel Filler Cap. . . . . . . . . . SECURE and VENT UNOBSTRUCTED


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- Model 182T NAV I l l Avionics Pilots' ChecklistPREFLIGHT INSPECTION (Continued).- @ NOSE

. . . . . . . . . .- 1. Static Source Ope ning (right side of fuselage ). CHE CKfor blockage2. Fue l Strainer Quick Drain Valve

. . . . . . . .Located on lower r ight s ide of engine cowling) DRAIN- Drain at least a cupful of fuel (using sampler cup) from valveto check for water, sediment, and proper fuel grade beforeeach fl ight and after ea ch refueling. If water is obse rved,take further samples until clear and then gently rock wingsand lower ta i l to the ground to move any addi t ionalcontaminants to the sump locations. Take repeated sam plesfrom all sum p locations, including the fuel return line and thefuel selector, until all contamination has been removed. Ifcontaminants are sti ll prese nt, refer to WA RNING below anddo not f ly airplane.NOTE

Collect all sampled fuel in a safe container. Dispos e of thesampled fuel so that it does not cause a n uisance, hazard ordamag e to the environment.

IF, AFTER REPEATED SAMPLES, EVIDENCE OFCONTAMINATION STILL EXISTS, THE AIRPLANESHOULD NOT BE FLOWN. TANKS SHOULD BEDRAINED AND SYSTEM PURGED BY QUALIFIEDMAINTENANCE PERSONNEL. ALL EVIDENCE OFCONTAMINATION MUST BE REMOVED BEFOREFLIGHT.3 . Engine Oil Dipst ickIFi ller Ca p . . . . . . . . . . . . . . CHECK O IL LEVELthen check dipsticklf i l ler cap SECURE.Do not operate with l ess than 4 quarts.Fill to 9 quarts for extended fl ight4. Eng ine Cooling Air Inlets . . . . . . . . . . . . . . . CLEAR of obstructions5. Propel ler and Spinner. . . . . . . . . . . . CHECK for nicks and security

(Cont inued Next Page)

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Pilots' Checklist NAV Ill Avionics -odel 182TPREFLIGHT INSPEC'TION (Continued) -

NOSE (Continued) -ir Filter. . . . CHECK for restrictions by dust or other foreign matterNosewheel Strut and Tire . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK

for proper inflation of strut and general condition of tire(weather checks, tread depth and wear, etc.) -. . . . . . . . . . .tatic Source Opening (left side of fuselage). CHECK

for blockage

LEFT WINGWing Tiedown . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DISCONNECT -Fuel Quantity. . . . . . . . . . . . . . CHECK VISUALLY for desired levelFuel Filler Cap. . . . . . . . . . SECURE and VENT UNOBSTRUCTEDFuel Tank Sump Quick Drain Valves . . . . . . . . . . . . . . . . . . DRAIN -Drain at least a cupful of fuel (using sampler cup) from eachsump location to check for water, sediment, and proper fuelgrade before each flight and after each refueling. If water isobserved, take further samples until clear and then gently -rock wings and lower tail to the ground to move anyadditional contaminants to the sump locations. Takerepeated samples from all sump locations until allcontamination has been removed. If contaminants are stillpresent, refer to WARNING below and do not fly airplane.

NOTECollect all sampled fuel in a safe container. Dispose of thesampled fuel so that it does not cause a nuisance, hazard ordamage to the environment.


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- Model 182T NAV Ill Avionics Pilots' Checklist- PREFLIGH T INSPECTION (Continued)

@ LEFT WlNG (Continued)- T i-IF, AFTER REPEATED SAMPLES, EVIDENCE OFCONTAMINATION STILL EXISTS, THE AIRPLANE- SHOULD NOT BE FLOWN. TANKS SHOULD BEDRAINED AND SYSTEM PURGED BY QUALIFIEDMAINTENANCE PERSONNEL. ALL EVIDENCE OFCONTAMINATION MUST BE REMOVED BEFORE- FLIGHT.

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. Main Wheel Tire. CHECK- for proper inflation and general condition(weather checks, tread depth and wear, etc.)- a EFT WlNG LEADING ED GE. . . . . . . . . . . . . . . . .. Fuel Tank Vent Opening CHECK for blockage. . . . . . . . . . . . . . . . . .. Stall Warning Opening CHECK for blockage

. . . . . . . . . . . . . . . .. LandinglTaxi Light(s) CHECK for condition and- cleanliness of cover@ LEFT WlNG TRAILING ED GE- . . . . . . . . . . . .. Aileron. CHECK freedom of movement and security. . . . . . . . . . . . . . . . . . . . . .. Flap CHECK for security and condition

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-ilots' Checklist NAV Il l Avior~ics Model 182TBEFORE STARTING ENGINE

1. Preflight Inspection . . . . . . . . . . . . . . . . . . . . . . . . . . . COMPLETE2. Passenger Briefing . . . . . . . . . . . . . . . . . . . . . . . . . . .COMPLETE3. Seats, Seat Belts, Shoulder Harnesses . . . . . . ADJUST and LOCK(Make sure inertia reel locks)4. Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . EST and SET5. Circuit Breakers. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK IN

.. Electrical Equipment . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFI CAUTION I

THE AVIONICS SWITCH (BUS 1 AND BUS 2) MUST BEOFF DURING ENGINE START TO PREVENT POSSIBLEDAMAGE TO AVIONICS.7. AVIONICS Switch (BUS 1 and BUS 2). . . . . . . . . . . . . . . . . . . OFF8. Cowl Flaps. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OPEN9. FUEL SELECTOR Valve. . . . . . . . . . . . . . . . . . . . . . . . . . . .BOTH

STARTING ENGINE (USING BATTERY)Throttle Control . . . . . . . . . . . . . . . . . . . . . . . . . . . OPEN 114 INCHPropeller Control. . . . . . . . . . . . . . . . . . . . . . . . . . . . . .HIGH RPMMixture Control. . . . . . . . . . . . . . . . . . . . . . . . . . . . DLE CUT OFFSTBY BATT Switcha. TEST - (Hold for 20 seconds, verify that green TEST lamp doesnot go out)b. ARM - (Verify that PFD comes on)Engine Indicating System. . . . . . . . . . . . . . CHECK PARAMETERS(Verify no red X's through ENGINE page indicators)BUS E Volts. . . . . . . . . . . . . . . . . . . . VERIFY 24 VOLTS minimumM BUS Volts . . . . . . . . . . . . . . . . . . . . . . . . . . . . VERIFY 0 VOLTSBATT S Amps. . . . . . . . . . . . . . . . VERIFY DISCHARGE (negative)STBY BATT Annunciator . . . . . . . . . . . . . . . . . . . . . . . VERIFY ONPropeller Area. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLEAR

. . . . . . . . . . . . . . . . . . . . . . . .ASTER Switch (ALT and BAT) ON(Continued Next Page)

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- Model 182T NAV Il l Avionics Pilots' ChecklistISTARTING E NGINE (USING BATTERY) (Continued)

NOTEIf engine is warm, omit priming procedure of steps 12, 13 and14 below.FUEL PUMP Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ONMixture Control . . . . . . . . . . . . . . . . . . . .ADVANCE to FULL RICHwait until fuel flow indication is stable,

then return to IDLE CUT OFF positionFUEL PUMP Switch. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFFMAGNETOS Switch . . . . . . . . . START release when engine startsMixture Control. . . . . . . . . . . . . ADVANCE smoothly to FULL RICH

when engine startsNOTE

If the engine floods, place the mixture control in the IDLECUT OFF position, open the throttle control 112 to full, andengage the starter motor (START). When the engine starts,advance the mixture control to the FULL RlCH position andretard the throttle control promptly.OIL Pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . HECKAMPS (M BATT and BATT S). . . . . . . . . . CHECK charge (positive)LOW VOLTS Annunciator. . . . . . . . . . . . . . . . . . . . . .VERIFY OFFBEACON Light Switch. . . . . . . . . . . . . . . . . . . . . . . ON as requiredNAV Lights Switch . . . . . . . . . . . . . . . . . . . . . . . . . ON as requiredAVlOhllCS Switch (BUS 1 and BUS 2). . . . . . . . . . . . . . . . . . . . ON

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Pilots' Checklist NAV Il l Avionics Model 182T -STARTING ENGINE (USING EXTERNALPOWER)

Throttle Control . ~ . ~ :. : .. . : - : ~ . ~ .. . . . . . . . . . . . . OPEN i i4 iNCH. . . . . . . . . . . . . . . . . . . . . . . . . . . . .ropeller Control. HIGH RPM

. . . . . . . . . . . . . . . . . . . . . . . . . . .ixture Control. IDLE CUT OFFSTBY BATT Switcha. TEST - (hold for 20 seconds, verify that green TEST lamp doesnot go out)b. ARM - (verify that PFD comes on)

. . . . . . . . . . . . .ngine Indication System. CHECK PARAMETERS(Verify no red X's through ENGINE page indicators)

. . . . . . . . . . . . . . . . . . .US E Volts. VERIFY 24 VOLTS minimum. . . . . . . . . . . . . . . . . . . . . . . . . . .BUS Volts. VERIFY 0 VOLTS. . . . . . . . . . . . . . . . . .ATT S Amps VERIFY discharge (negative)

. . . . . . . . . . . . . . . . . . . . . . .TBY BATT Annunciator VERIFY ON. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ropeller Area. CLEAR

. . . . . . . . . . . . . . . . . .VIONICS Switch (BUS 1 and BUS 2). OFF. . . . . . . . . . . . . . . . . . . . . . .ASTER Switch (AI-T and BAT) OFF

. . . . . . . . .xternal Power. CONNECT to ground power receptacle. . . . . . . . . . . . . . . . . . . . . . . .ASTER Switch (AI-T and BAT) ON. . . . . . . . . . . . . . . . .BUS VOLTS VERIFY external power volts

NOTEIf engine is warm, omit priming procedure of steps 16, 17 and18 below.

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .6. FUEL PUMP Switch OW. . . . . . . . . . . . . . . . . . . . .7. Mixture Control. Advance to FULL RICH

wait until indicated fuel flow stabilizes,then return to IDLE CUT OFF position

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .8. FUEL PUMP Switch. OFF

. . . . . . . . .9. MAGNETOS Switch START release when engine starts. . . . . . . . . . . .0. Mixture Control. ADVANCE smoothly to FULL RICHwhen engine starts


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- Model 182T NAV Il l Avionics Pilots' Checklist- STARTING ENGINE (USING EXTERNAL POWER)(Continued)- NOTE

If the engine floods, place the mixture control in the IDLECUT OFF position, open the throttle control 112 to full, andengage the starter motor (START). When the engine starts,advance the mixture control to the FULL RICH position andretard the throttle control promptly.OIL Pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKEngine RPM . . . . . . . . . . . . . . . . . . . . . . . . . . . . . REDUCE to idleExternal Power. . . . . . . . . . . . . . . . . . . DISCONNECT from ground

power receptacleEngine RPM . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .INCREASE

(to approximately 1500 RPM forseveral minutes to charge battery)

AMPS (M BATT and BATT S). . . . . . . . . . CHECK charge (positive)LOW VOLTS Annunciator. . . . . . . . . . . . . . . . . . . . . . VERIFY OFFInternal Power . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECKa. MASTER Switch (ALT) . . . . . . . . . . . . . . . . . . . . . . . . . . .OFFb. TAXI and LANDING Light Switches. . . . . . . . . . . . . . . . . . . ONc. Engine RPM . . . . . . . . . . . . . . . . . . . . . . . . . . REDUCE to idled. MASTER Switch (AI-T and BAT) . . . . . . . . . . . . . . . . . . . . . ONe. Engine RPM . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . INCREASE

(to approximately 1500 RPM). . . . . . . . . . . . . . . .. Main Battery (M BATT) Ammeter. CHECK,

(Battery charging, Amps positive). . . . . . . . . . . . . . . .. LOW VOLTAGE Annunciator VERIFY OFF

I WARNING bIF M BATT (MAIN BATTERY) DOES NOT SHOW + AMPS,- REMOVE THE MAIN BATTERY FROM THE AIRPLANEAND SERVICE OR REPLACE THE BATTERY BEFOREFLIGHT.

. . . . . . . . . . . . . . . . . . . . . .- 28. BEACON Light Switch. ON as required29. NAV Lights Switch . . . . . . . . . . . . . . . . . . . . . . . . . ON as required30 AVIONICS Switch (BUS 1 and BUS 2). . . . . . . . . . . . . . . . . . . . ON

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Pilots' Checklist NAV Il l Avionics Model 182T -BEFORE TAKEOFF

1. Parking Brake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET2. Passenger Seat Backs . . . . . . . . . . . . MOST UPRIGHT POSITION3. Seats and Seat Belts. . . . . . . . . . . . . . . . . . . . . .CHECK SECURE4. Cabin Doors. . . . . . . . . . . . . . . . . . . . . . . .CLOSED and LOCKED5. Flight Controls . . . . . . . . . . . . . . . . . . . . . . .FREE and CORRECT6. Flight Instruments (PFD) . . . . . . . . . . . . . . . . .CHECK (no red X's)7. Altimeters:

a. PFD (BARO) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .SETb. Standby Altimeter. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ETc. KAP 140 Autopilot (BARO). . . . . . . . . . . . . . . . . . . . . . . . .SET

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. GIOOOALTSEL SET. . . . . . . . . . . . . . . . . . . . . . . . . . .. KAP 140 Altitude Preselect SETNOTE

There is no connection between the GI000 ALT SEL featureand the KAP 140 autopilot altitude preselect or altitude holdfunctions. GI000 and KAP 140 altitudes are setindependently.

10. Standby Flight Instruments . . . . . . . . . . . . . . . . . . . . . . . . . CHECK11. Fuel Quantity . . . . . . . . . . . . . . . . . . . .CHECK, verify correct level

NOTEFlight is not recommended when both fuel quantity indicatorsare in the yellow arc range.

12. Mixture Control . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RICH13. FUEL SELECTOR Valve. . . . . . . . . . . . . . . . . . . RECHECK BOTH14. Elevator and Rudder Trim . . . . . . . . . . . . . . . . . . . . SET for takeoff15. Manual Electric Trim (MET) . . . . . . . . . . . . . . . . . . . . . . . . CHECK

(Refer to the POHIAFM, Supplement 3 for Manual Electric Trimcheck procedures)


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Model 182T NAV Il l Avionics Pilots' Checklist

BEFORE TAKEOFF (Continued) y k16. Throttle Control . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .1800 RPM 9 5a. MAGNETOS Switch. CHECK w Y. . . . . . . . . . . . . . . . . . . . . . . . . . m S(RPM drop should not exceed 175 RPM on either

magneto or 50 RPM differential between magnetos)b. Propeller Control . . . . . . . . . . . . CYCLE from high to low RPM;

return to high RPM (full in)c. VAC Indicator. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKd. Engine Indicators . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECKe. Ammeters and Voltmeters . . . . . . . . . . . . . . . . . . . . . . CHECKAnnunciators . . . . . . . . . . . . . . . . . . . . . . CHECK none illuminatedThrottle Control . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK IDLEThrottle Control . . . . . . . . . . . . . . . . . . . . . . . .1000 RPM or LESSThrottle Control Friction Lock. . . . . . . . . . . . . . . . . . . . . . . ADJUSTCOM Frequency(s) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .SETNAV Frequency(s) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETFMSlGPS Flight Plan. . . . . . . . . . . . . . . . . . . . . . . . .AS DESIRED

NOTE

Check GPS2 availability on AUX-GPS STATUS page. Noannunciation is provided for loss of GPS2.XPDR . . . . . . . . . . . . . . . .CDI Softkey. . . . . . . . . . . .

. . . . . . . . . . . . . SETSELECT NAV Source

I CAUTION ITHE GI000 HSI SHOWS A COURSE DEVIATIONINDICATOR FOR THE SELECTED GPS, NAV 1 OR NAV 2NAVIGATION SOURCE. THE GI000 HSI DOES NOTPROVIDE A WARNING "FLAG" WHEN A VALIDNAVIGATION SIGNAL IS NOT BEING SUPPLIED TO THEINDICATOR. WHEN AVALID NAVIGATION SIGNAL IS NOTBEING SUPPLIED, THE COURSE DEVIATION BAR (D-BAR) PART OF THE INDICATOR IS NOT SHOWN ON THEHSI COMPASS CARD. THE MISSING D-BAR ISCONSIDERED TO BE THE WARNING FLAG.


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Pilots' Checklist NAV Ill Avionics Model 182T -BEFORE TAKEOFF (Continued)

I WARNING bWHEN THE KAP 140 AUTOPILOT IS ENGAGED IN NAV,APR OR REV OPERATING MODES, IF THE HSINAVIGKTION SOURCE IS CHANGED FROM GPS TONAV1, AUTOMATICALLY OR MANUALLY (USING THECDI SOFTKEY), OR MANUALLY FROM NAV2 TO GPS,THE CHANGE WlLL INTERRUPT THE NAVIGATIONSIGNAL TO THE AUTOPILOT AND WlLL CAUSE THEAUTOPILOT TO REVERT TO ROL MODE OPERATION.NO WARNING CHIME OR PFD ANNUNCIATION WlLL BEPROVIDED. THE PREVIOUSLY SELECTED MODESYMBOL SHOWN ON THE AUTOPILOT DISPLAY WlLLBE FLASHING TO SHOW THE REVERSION TO ROLMODE OPERATION. IN ROL MODE, THE AUTOPILOTWlLL ONLY KEEP THE WINGS LEVEL AND WlLL NOTCORRECT THE AIRPLANE HEADING OR COURSE. SETTHE HDG BUG TO THE CORRECT HEADING ANDSELECT THE CORRECT NAVIGATION SOURCE ON THEHSI USING THE CDI SOFTKEY BEFORE ENGAGING THEAUTOPILOT IN ANY OTHER OPERATING MODE.

26. Autopilot . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF27. Wing Flaps . . . . . . . . . . . . . . . . . . . . . . . . . 0" - 20" (10" preferred)28. Cowl Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OPEN29. Cabin Windows . . . . . . . . . . . . . . . . . . . . . CLOSED and LOCKED30. STRO BE Lights Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON31. Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RELEASE

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Model 182T NAV Il l Avionics Pilots' Checklist

TAKEOFFNORMAL TAKEOFF

. . . . . . . . . . . . . . . . . . . . . . . . .. Wing Flaps 0" - 20" (10" preferred). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. Throttle Control FULL

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. Propeller Control 2400 RPM. . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. Mixture Control. FULL RICH(Above 5000 feet pressure altitude, lean for maximum RPM) 1. . . . . . . . . . .. Elevator Control LIFT NOSEWHEEL AT 50 - 60 KlAS

. . . . . . . . . . . . . . . . . . . . . . .. Climb Airspeed 70 KlAS (FLAPS 20")80 KlAS (FLAPS 0")

. . . . . . . . . . . . . . . . . . . . . .. Wing Flaps. RETRACT at safe altitude

SHORT FIELD TAKEOFF. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. Wing Flaps 20'

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. Brakes. . APPLY. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. Throttle Control FULL

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. Propeller Control 2400 RPM. . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. Mixture Control. FULL RICH(Above 5000 feet pressure altitude, lean for maximum RPM). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. Brakes RELEASE

. . . . . . . . . . . . . . . . . . . . . .. Elevator Control. SLIGHTLY TAIL LOW I. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. Climb Airspeed 58 KlAS

(Until all obstacles are cleared). . . . . . . . . . . . . . . . . . . . . . . . . . .. Wing Flaps RETRACT SLOWLY

(When airspeed is more than 70 KIAS)

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Pilots' Checklist NAV Ill Avionics Model 182T -ENROUTE CLIMBNORMAL CLIMB

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. Airspeed. 85 - 95 KlAS. . . . . . . . . . . . . . . . . . . . . . . . . .2. Throttle Control 23 in.hg. or FULL

I (if less than 23 in.hg.). . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. Propeller Control 2400 RPM. . . . . . . . . . . . . . . . . . . . . .. Mixture Control 15 GPH or FULL RICH

(if less than 15 GPH). . . . . . . . . . . . . . . . . . . . . . . . . . .. FUEL SELECTOR Valve. BOTH

. . . . . . . . . . . . . . . . . . . . . . . . . . . .. Cowl Flaps. OPEN as requiredMAXIMUM PERFORMANCE CLIMB

. . . . . . . . . . . . . . . . . . . . . . . . . .. Airspeed. 80 KlAS at Sea Level74 KlAS at 10,000 Feet

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. Throttle Control FULL. . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. Propeller Control 2400 RPM. . . . . . . . .. Mixture Control FULL RICH or SET to Maximum Power

Fuel Flow placard value for altitude. . . . . . . . . . . . . . . . . . . . . . . . . . .. FUEL SELECTOR Valve. BOTH. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. Cowl Flaps. OPEN

CRUISE. . . . . . . . . . . . . . . . . . . .I. ower 15 - 23 in.hg. at 2000 - 2400 RPM

(No more than 80% power recommended). . . . . . . . . . . . . . . . . . . . . . . . .. Elevator and Rudder Trim ADJUST. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. Mixture Control LEAN. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. Cowl Flaps. CLOSE

. . . . . . . . . . . .. FMSIGPS. REVIEW and BRIEF OBSISUSP softkeyoperation for hold pattern procedure (IFR)

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- Model 182T NAV Ill Avionics Pilots' Checklist.- DESCENT

Power. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS DESIREDMixture . . . . . . . . . . . . . . . . . . . . . . . . ENRICHEN AS REQUIRED(for smooth operation)Cowl Flaps. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CLOSEDAltimeters:a. PFD (BARO) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETb. Standby Altimeter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETc. KAP 140 Autopilot (BARO). . . . . . . . . . . . . . . . . . . . . . . . . SETGIOOOALTSEL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETKAP 140 Altitude Preselect . . . . . . . . . . . . . . . . . . . . . . . . . . . SETNOTE

There is no connection between the G I000 ALT SEL featureand the KAP 140 autopilot altitude preselect or altitude holdfunctions. GI0 00 and KAP 140 altitudes are setindependently.7. CDI Softkey. . . . . . . . . . . . . . . . . . . . . . . . . .SELECT NAV source8. FMSIGPS . . . . . . . . . . . . . REVIEW and BRIEF OBSISUSP softkeyoperation for holding pattern procedure (IFR)

I CAUTION ITHE GI000 HSI SHOWS A COURSE DEVIATIONINDICATOR FOR THE SELECTED GPS, NAV 1 OR NAV 2NAVIGATION SOURCE. THE GI000 HSI DOES NOTPROVIDE A WARNING "FLAG" WHEN A VALIDNAVIGATION SIGNAL IS NOT BEING SUPPLIED TO THEINDICATOR. WHEN AVALID NAVIGATION SIGNAL IS NOTBEING SUPPLIED, THE COURSE DEVIATION BAR (D-BAR) PART OF THE INDICATOR IS NOT SHOWN ON THEHSI COMPASS CARD. THE MISSING D-BAR ISCONSIDERED TO BE THE WARNING FLAG.


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Pilots' Checklist NAV Il l Avionics Model 182T -

DESCENT (Continued) -I WARNING 1 -

WHEN THE KAP 140 AUTOPILOT IS ENGAGED IN NAV,APR OR REV OPERATING MODES, IF THE HSI ,NAVIGATION SOURCE IS CHANGED FROM GPS TO -NAVI, AUTOMATICALLY OR MANUALLY (USING THECDI SOFTKEY), OR MANUALLY FROM NAV2 TO GPS,THE CHANGE WlLL INTERRUPT THE NAVIGATIONSIGNAL TO THE AUTOPILOT AND WlLL CAUSE THEAUTOPILOT TO REVERT TO ROL MODE OPERATION.NO WARNING CHIME OR PFD ANNUNCIATION WlLL BEPROVIDED. THE PREVIOUSLY SELECTED MODESYMBOL SHOWN ON THE AUTOPILOT DISPLAY WlLLBE FLASHING TO SHOW THE REVERSION TO ROLMODE OPERATION. IN ROL MODE, THE AUTOPILOTWlLL ONLY KEEP THE WINGS LEVEL AND WlLL NOTCORRECT THE AIRPLANE HEADING OR COURSE. SETTHE HDG BUG TO THE CORRECT HEADING ANDSELECT THE CORRECT NAVIGATION SOURCE ON THEHSI USING THE CDI SOFTKEY BEFORE ENGAGING THEAUTOPILOT IN ANY OTHER OPERATING MODE.

9. FUEL SELECTOR Valve. . . . . . . . . . . . . . . . . . . . . . . . . . . . BOTH -10. Wing Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS DESIRED

(0" - 10" below 140 KIAS)(10" - 20" below 120 KIAS) -

(20" - FULL below 100 KIAS)

BEFORE LANDING -1. Pilot and Passenger Seat Backs. . . . . MOST UPRIGHT POSITION2. Seats and Seat Belts. . . . . . . . . . . . . . . . SECURED and LOCKED -. . . . . . . . . . . . . . . . . . . . . . . . . . .. FUEL SELECTOR Valve. BOTH4. Mixture Control . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RICH5. Propeller Control.. . . . . . . . . . . . . . . . . . . . . . . . . . . . . HIGH RPM6. LANDING and TAXI Light Switches. . . . . . . . . . . . . . . . . . . . . . ON -7. Autopilot . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

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Model 182T NAV Ill Avionics Pilots' Checklist

LANDINGNORMAL LANDING

. . . . . . . . . . . . . . . . . . . . . . . . . .. Airspeed 70 - 80 KlAS (Flaps UP)2. Wing Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS DESIRED(0" - 10" below 140 KIAS)(10" - 20" below 120 KIAS)(20" - FULL below 100 KIAS). . . . . . . . . . . . . . . . . . . . . . . .. Airspeed 60 - 70 KlAS (Flaps FULL)4. Trim . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ADJUST5. Touchdown . . . . . . . . . . . . . . . . . . . . . . . . . MAIN WHEELS FIRST

6. Landing Roll. . . . . . . . . . . . . . . . . LOWER NOSEWHEEL GENTLY7. Braking. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIREDSHORT FIELD LANDING

. . . . . . . . . . . . . . . . . . . . . . . . . .. Airspeed 70 - 80 KlAS (Flaps UP). . . . . . . . . . . . . . . . . . . . . . . .. Wing Flaps. FULL (below 100 KIAS)

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. Power REDUCE TO IDLE(As obstacle is cleared). . . . . . . . . . . . . . . . . . . . . . . . . . . . .. Airspeed. 60 KlAS (until flare)

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. Trim ADJUST. . . . . . . . . . . . . . . . . . . . . . . . .. Touchdown MAIN WHEELS FIRST

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. Brakes APPLY HEAVILYBALKED LANDING

. . . . . . . . . . . . . . . . . . . .. Power. FULL THROTTLE and 2400 RPM. . . . . . . . . . . . . . . . . . . . . . . . . . . .. Wing Flaps. RETRACT TO 20". . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. Climb Speed 55 KlAS

. . . . . . . . . . . . . . . . . . . . . . . . . . .. Wing Flaps RETRACT SLOWLY(After reaching a safe altitude and 70 KIAS). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. Cowl Flaps . OPEN

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Pilots' Checklist NAV Ill Avionics Mo del 182T -AFTER LANDING

1. Wing Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP2. Cowl F laps. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OPENSECURING AIRPLANE

Parking Brake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETThrottle Control. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLEElectrical Equipment . . . . . . . . . . . . . . . . . . . . . . . . . . . . -. . . OFFAVIONICS Switch (BUS 1 and BUS 2). . . . . . . . . . . . . . . . . . . OFFMixture Control. . . . . . . . . . . . . . . . . . . . . . . . . . . . DLE CUT OFFMAGNETO S Switch. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFFMAS TER Switch (ALT and BAT) . . . . . . . . . . . . . . . . . . . . . . . OFFSTBY BATT Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFFControl Lock. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NSTALLFUEL SELECTOR Valve. . . . . . . . . . . . . . . . . . . . . LEFT or RIGHT(To prevent crossfeeding between tanks)

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- lblodel 182T NAV Ill Avionics Pilots' Checklist- EMERGENCY PROCEDURES

TABLE OF CONTE NTSAIRSPEEDS FOR EMERGENCY OPERATIONS ................................... E-3ENGINE FAILURES ..................................................................................E-4

ENGINE FAILURE DUR ING TAKEOFF RO LL ................................. E-4ENGIN E FAILURE IMMEDIATELY AFTER TAKEO FF ....................... E-4ENGINE FAILURE DURING FLIGHT (RESTART PROCEDURES) .. .E-5

FORCED LANDINGS . . . . . . . . . . . . . . . . . . . .. . . . . . . . . . . . . . . . . . . .. . . . . . . . . . . . . . . . . . . . .. . . . . . . . . . . . . . . . . . .-6EMERGENCY LANDING WITHOUT ENGINE POWER ................... E-6PRECAUTIOIVARY LANDING WITH ENGINE POW ER ....................E-6DITCHING ........................................................................................... E-7

FIRES ........................................................................................................ E-8DURING START ON G ROUND .......................................................... E-8ENGINE FIRE IN FLIGHT ..................................................................E-9ELECTRICAL FIRE IN FLIGHT ........................................................ E-10 iCABIN FIRE .................................................................................... E-11 ~WING FIRE ..................................................................................... E-11 ~

ICING ..................................................................................................... E-12 'INADVERTENT ICING ENCOUNTER DURING FLIGHT .................E-12STATIC SOURCE BLOCKAGE

(ERRONEOUS INSTRUMENT READING SUSPECTED) ...........E-13 I.....................................................................XCESSIVE FUEL VAPOR E - I3

.................................UEL FLOW STABILIZATION PROCEDUR ES E-13 'ABNORMAL LANDINGS ........................................................................ -14

LANDING W ITH A FLAT MAIN TIRE ................................................ E-14LANDING WITH A FLAT NOSE TIRE ...............................................E-14


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Pilots' Checklist NAV Ill Avionics Model 182T

TABLE OF CONTENTS (Continued) .ELECTRICAL POWER SUPPLY SYSTEM MALFU NCTIONS ..............E-14

M BUS VOLTS MORE 'THAN 32 OR....................................................BAT AMPS MORE THAN 40 E- I4

.....I ......................................LOW VOLTS ANNUNCIATOR COMES ON BELOW 1000 RPM E-16LOW VOLTS ANNUNCIATOR COMES ON OR................................................................DOES NOT GO OFF AT HIGHER RPM E-I6AIR DATA SYSTEM FAILURE E-I8I RED X - PFD AIRSPEED INDICATOR .............................................E-I8~ ..............................................ED X - PFD ALTITUDE IhlDlCATOR E-I8: ATTITUDE AND HEAD ING REFERENCE SYSTEMi (AHRS) FAILURE .................................................................................... - I8..............................................RED X - PFD ATTITUDE INDICATOR E-18...................ED X - HORIZONTAL SITUATION INDICATOR (HSI) E-181 DISPLAY COOLING ADVISORY ............................................................ E-19

PFDI COOLING OR MFDI COOLING ANNUNCIATOR(S) ............E-19.................................................................ACUUM SYSTEM FAILURE E-I91 LOW VACUUM ANNUNCIATOR COMES ON ............................E-191 MAXIMUM GLIDE ....................................................................................E-20

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- Model 182TAIRSPEEDS

NAV Ill Avionics Pilots' Checklist

AIRSPEEDS FOR EMERGENCY OPERATIONS

ENGINE FAILURE AFTER TAKEOFFWing Flaps Up . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 75 KlASWing Flaps 10" - FULL. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 70 KlAS

MANEUVERING SPEED3100 POUNDS. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 110 KlAS ~2600 POUNDS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 101 KlAS 12100 POLINDS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 91 KlAS ~MAXIMUM GLIDE3100 POUNDS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 76 KlAS ~2600 POUNDS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 70 KlAS ~2100 POUNDS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 58 KlAS IPRECAUTIONARY LANDING WITH ENGINE POWER . . . . . . . . . 70 KlASLANDING WITHOUT ENGINE POWERWing Flaps Up. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 75 KlASWing Flaps 10" - FULL. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 70 KlAS

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Pilots' Checklist NAV Il l Avionics Model 182T --

EMERGENCY PROCEDURESProcedures in the Emergency Procedures Checklist portion of this sectionshown in bold-faced type are immediate action items which should becommitted to memory.

ENGINE FAILURESENGINE FAILURE DURING TAKEOFF ROLL

1. Throttle Control . . . . . . . . . . . . . . . . . . . . . . . IDLE (pull full out)2. Brakes. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PPLY3. Wing Flaps. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RETRACT4. Mixture Control . . . . . . . . . . . . . . . . . . DLE CUT OFF (pull full out)5. MAGNETOS Switch. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF6. STBY BATT Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF7. MASTER Switch (ALT and BAT) . . . . . . . . . . . . . . . . . . . . . . . OFF

ENGINE FAILURE IMMEDIATELY AFTER TAKEOFF1 1. Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . 7 5 KlAS (Flaps UP)~ 70 KlAS (Flaps 10" - FULL)2 . Mixture Control . . . . . . . . . . . . . . . . . . DLE CUT OFF (pull full out)

3 . FUEL SELECTOR Valve . . . . PUSH DOWN and ROTATE TO OFF. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. MAGNETOS Switch. OFF5. Wing Flaps. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .AS REQUIRED

(FULL recommended)6. STBY BATT Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF7. MASTER Switch (ALT arid BAT j . . . . . . . . . . . . . . . . . . . . -:-.OFF

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. Cabin Door. UNLATCH9. Land. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .STRAIGHT AHEAD

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- Mo del 182 T NAV Ill Avionics Pilots' ChecklistENGINE FAILURE DURING FLIGHT- (RESTART PROCEDURES)

1. Airspeed . . . . . . . . . . . . . . . . . . . . . . 7 6 KlAS (best glide speed) 1- 2. FUEL SELECTOR Valve . . . . . . . . . . . . . . . . . . . . . . . . . . .BOTH3. FUEL PUMP Switch. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON4. Mixture Control . . . . . . . . . . . RICH (if restart has not occurred)

. . . . . . . . . . . . . . . . . . . . .5. MAG NETO S Switch BOTH (or START i fpropeller is stopped)- NOTEIf propeller is windmill ing, engine will restart automaticallywithin a few seconds. If propeller has stopped (possible at- low speeds), turn MAGNETOS switch to START, advancethrottle slowly from idle, and lean the mixture from full rich asrequired to obtain smooth operation.

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. 6. FUEL PUMP Swi tch. OFFNOTE

If the indicated fuel f low (FF LOW GP H) immediately drops tozero, a sign of failure of the engine-driven fuel pump, returnthe FUEL P UMP Sw i tch to the ON posit ion. I

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FORCED LANDINGSEMERGENCY LANDING WITHOUT ENGINE POWER

Passenger Seat Backs . . . . . . . . . . . . MOST UPRIGHT POSITIONSeats and Seat Belts . . . . . . . . . . . . . . . . . . . . . . . . . . . .SECUREAirspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5 KlAS (Flaps UP)70 KlAS (Flaps 10" - FULL)Mixture Control. . . . . . . . . . . . . . . . . . . . . . . . . . . . DLE CUT OFFFUEL SELECTOR Valve . . . . PUSH DOWN and ROTATE TO OFFMAGNETOS Switch. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFFWing Flaps. . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1AS REQUIRED(FULL recommended)STBY BATT Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFFMASTER Switch (ALT and BAT) . . . . . . . . . . . . . . . . . . . . . . .OFF(when landing is assured)Doors. . . . . . . . . . . . . . . . . . UNLATCH PRIOR TO TOUCHDOWN-ouchd down . . . . . . . . . . . . . . . . . . . . . . . . . . SilGHTiY TAi i iClWBrakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PPLY HEAVILY

PRECAUTIONARY LANDING WITH ENGINE POWER. . . . . . . . . . . .assenger Seat Backs MOST UPRIGHT POSITION

. . . . . . . . . . . . . . . . . . . . . . . . . . . .eats and Seat Belts SECUREAirspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 75KlAS. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ing Flaps .2 0

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .elected Field FLY OVER(noting terrain and obstructions). . . . . . . . . . . . . . . . . . . . . . .ing Flaps. FULL (on final approach). . . . . . . . . . . . . . . . . . . . . . . . . . . . . .irspeed . . . . 70 KlAS. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .TBY BATT Switch OFF

. . . . . . . . . . . . . . . . . . . . . . .ASTER Switch (ALT and BAT) OFFDoors . . . . . . . . . . . . . . . . . . UNLATCH PRIOR TO TOUCHDOWN. . . . . . . . . . . . . . . . . . . . . . . . . .ouchdown SLIGHTLY TAIL LOW. . . . . . . . . . . . . . . . . . . . . . . . . . .ixture Control. IDLE CUT OFF

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .AGNETOS Switch. OFF. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .rakes APPLY HEAVILY

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- Model 182T NAV Ill Avionics Pilots' Checklist- DITCHING

1. Radio. . . . . . . . . . . . . . . . . . . TRANSMIT MAYDAY on 121.5 MHz ,(Give Location, Intentions and SQUAWK 7700)- 2. Heavy Objects (in baggage ar ea ). . . . . . . SECURE OR JETTISON(if possible)3. Passenger Seat Backs . . . . . . . . . . . . MOST UPRIGHT POSITION. . . . . . . . . . . . . . . . . . . . . . . . . . . .4. Seats and Seat Belts SECURE5. Wing Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 0" - FULL6. Power. . . . . . . . . . ESTABLISH 300 FTIMIN DESCEN T AT 65 KlAS- NOTEIf no power is available, approach at 70 KlAS with Flaps UP- or at 65 KlAS with Flaps 10".

7. ApproachHigh Winds, Heavy Seas . . . . . . . . . . . . . . . . lVTO THE WINDLight Winds, Heavy Swells . . . . . . . . . PARALLEL TO SW ELLS8. Cabin Doors. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .UNLATCH9. Touchdown . . . . . . . . . . . . . . LEVEL ATTITUDE AT ESTABLISHEDRATE-OF-DESCENT10. Face . . . . . . . . . . . . . . . . CUSH ION at touchdown with folded coat11. ELT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ACTIVATE12. Airplane . . . . . . . . . . . . . . EVACUATE THROUG H CABIN DOORSIf necessary, open window and flood cabin to equalize pressure sodoors can be opened.

. . . . . .3. Life Vests and Raft INFLATE WHE N CLEAR OF AIRPLANE

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Pilots' Checklist NAV I l l Avionics -Model 182TDURING START ON GROUND

. . . . . . . . . . . . . . . . . . . . . . . . . . . . .. MAGNETOS Swi tch . START(Continue cranking to start the eng ine)IF ENGINE STARTS

. . . . . . . . . . . . . . . . . . . . . . . .. Power. 1700 RPM for a few minutes. . . . . . . . . . . . . . . .. Eng ine. SHUT DOW N and inspect for damageIF ENGINE FAILS TO START

. . . . . . . . . . . . . . . . . . . . . . . . . . . .. Throttle Control. FULL OPEN. . . . . . . . . . . . . . . . . . . . . . . . . .. Mixture Control. IDLE CUT OFF4. MAGNETOS Switch . . . . . . . . . . . . .START (continue cranking)

. .. . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . . . . . . . . . . . . . . . . . . . . . . . . .I . FUEL SELECTOR Valve.. PUSH DOWN and ROTATE TO OFF6. FUEL PUMP Sw it ch .. OFF. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .7. MAGNETOS Sw itch .. OFF8. STBY BATT Switch . . . . . . . . . . . . . . . . . . . . . .OFF9. MASTER Swi tch (ALT and BAT) OFF. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .0. Engin e. SECURE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .1. Parking Brake. RELE ASE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .2. Fire Extinguisher OBTAIN(Have ground attendants obtain if not installed). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .3. Airplane EVACUATE. . . . . . . . . . . . . . . . . . . .4. Fire EXTING UISH using fire extinguisher,wool blanket, or dirt. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .5. Fire Dam age . INSPECT(Repair damage or replace damaged componen tsor wiring before conducting anothe r flight)

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- Model 182T NAV Il l Avionics Pilots' Checklist- ENGINE FIRE IN FLIGHT. . . . . . . . . . . . . . . . . . . . . . . . . .ixture Con trol. IDLE CUT OFFFUEL SELECTOR Valve . . . . PUSH DO WN and ROTATE to OFF. . . . . . . . . . . . . . . . . . . . . . . . . . . . . .UEL PUMP Sw itch . . OFF. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .TBY BATT Switch OFF. . . . . . . . . . . . . . . . . . . . . .ASTER Sw itch (ALT and B AT) OFF. . . . . . . . . . . . . .abin He at and Air OFF (except overhead vents)

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .i rspeed 100KlAS(If fire is not extinguished, increase glide speed to find an airspeed,within airspeed limitations, which will provide an incom bustib lemixture) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .orced Landing EXECUTE(Refer to EMERGENCY LANDING WITHOUT ENGINE POWER,page E-6) I

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-Pilots' Checklist NAV Ill Avionics Mod el 182TELECTRICAL FlRE IN FLIGHT

1. STBY BATT Swi tch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF2. MASTER Switch (ALT and BAT) . . . . . . . . . . . . . . . . . . . . . . OFF3. VentslCabin AirlHeat . . . . . . . . . . . . . . . . . . . . . . . . . . . CLOSED4. Fire Extinguisher . . . . . . . . . . . . . . . . . . .ACTIVATE (if available)

. . . . . . . . . . . . . . . . . .. AVIONICS Switch (BUS 1 and BUS 2) . OFF. . . . . . . . . . .. All Other Switches (except MAGN ETOS switch). OFF

( WARNING 1AFTER THE FlRE EXTINGUISHER HAS BEEN USED,MAKE SURE THAT THE FlRE IS EXTINGUISHEDBEFORE EXTERIOR AIR IS USED TO REMOVE SMOKEFROM THE CABIN.

7. VentsICabin AirlHeat. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OPEN(When sure that fire is completely extinguished)

IF FlRE HAS BEEN EXTINGUISHED AND ELECTRICAL POWER ISNECESSARY FOR CONTINUED FLIGHT TO NEAREST SUITABLEAIRPORT OR LANDING AREA8. Circuit Breakers . . . . CHECK for O PEN circuit(s), DO N OT RESE T9. MASTER Switch (ALT and BAT) . . . . . . . . . . . . . . . . . . . . . . . .ON10. AVIONICS Switch (BUS 1). . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

I 11. AVIONICS Switch (BUS 2). . . . . . . . . . . . . . . . . . . . . . . . . . . . .O N

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- Model 182T NAV Ill Avionics Pilots' Checklist- CABIN FIRE

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. STBY BATT Switch OFF2. MASTER Switch (ALT and BAT) . . . . . . . . . . . . . . . . . . . . . .OFF- . . . . . . . . . . . . . . . . . . . . . . . . . . .. VentslCabin AirlHeat CLOSED(to avoid drafts). . . . . . . . . . . . . . . . . . . . . . . . . . . .. Fire Extinguisher. ACTIVATE- (if available)I WARNING 1

AFTER THE FlRE EXTINGUISHER HAS BEEN USED,MAKE SURE THAT THE FlRE IS EXTINGUISHEDBEFORE EXTERIOR AIR IS USED TO REMOVE SMOKEFROM THE CABIN.. . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. VentsICabin AirIHe at. OPE N(When sure that fire is completely extinguished)6. Land the airplane as soon as possible to inspect for damage.

- WING FlRE- 1. LAND and TAXI Light Switches. . . . . . . . . . . . . . . . . . . . . . .OFF. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. NAV Light Switch. OFF. . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. STROBE Light Switch OFF. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .- 4. PlTOT HEAT Switch. OFF

NOTE- Perform a sideslip to keep the flames aw ay from the fuel tankand cabin. Land as soon as possible using flaps only asrequired for final approach and touchdown.-

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ICING -INADVERTENT ICING ENCOUNTER DURING FLIGHT

1. PlTOT HEAT Switch. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON2. Turn back or change alti tude to obtain an outside air temperaturethat is less conducive to icing.3. Pull cabin heat control full out and rotate defroster controlclockwise to obtain maximum defroster airflow.4. Increase engine speed to minimize ice build-up on propeller blades.If excessive vibration is noted, momentarily reduce engine speed to2200 RPM with the propeller control, and then rapidly move thecontrol forward.

NOTE --Cycling the RPM flexes the propeller blades and high RPMincreases centrifugal force, causing ice to shed more rapidly. -Watch for signs of induction air filter icing. A loss of manifold pressurecould be caused by ice blocking the air intake filter. Adjust the throttleas necessary to hold manifold pressure. Adjust mixture, as -necessary, for any change in power settings.Plan a landing at the nearest airport. With an extremely rapid icebuild-up, select a suitable "off airport" landing site.With an ice accumulation of 0.25 inch or more on the wing leading -edges, be prepared for significantly higher power requirements,higher approach and stall speeds, and a longer landing roll.Leave wing flaps retracted. With a severe ice build-up on the -horizontal tail, the change in wing wake airflow direction caused bywing flap extension could result in a loss of elevator effectiveness.Open left window and, if practical, scrape ice from a portion of the -windshield for visibility in the landing approach.Perform a landing approach using a forward slip, if necessary, forimproved visibility.Approach at 80 to 90 KlAS depending upon the amount of the -accumulation.Perform a landing in level attitude.Missed approaches should be avoided whenever possible because -of severely reduced climb capability.

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-. Model 182T NAV Ill Avionics Pilots' Checklist

- STATIC SOURCE BLOCKAGE (ERRONEOUS INSTRUMENTREADING SUSPECTED)1. ALT STATIC AIR Valve. . . . . . . . . . . . . . . . . . . . . . . . . . ULL ON- 2. CABIN HT and CABIN AIR Knobs . . . . . . . . . . . . . . . . . . ULL ON3. V e n t s . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LOSED4. Airspeed. . . . . . . . . . . . . . . . . . . . . . . Refer to the P OH , Section 5,- Figure 5-1 (Sheet 2) Airspeed Calibration, Alternate Static Source.5. Altitude. . . . . . . . . . . . . . . . . . . . . . . . Refer to the POH, Section 5,Figure 5-2 Altimeter Correction, Alternate Static Source

- EXCESSIVE FU EL VAPORFUEL FLOW STABILIZATION PROCEDURES

- (If flow fluctuations of 1 GPH or more, or power surges occur.)1. FUEL PUMP Switch2. Mixture . . . . . . . . .3. Fuel Selector Valve. . . . .4. FUEL PUMP Switch.

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . N. . . . . . . . . . . ADJUST AS NECESSARY(for smooth engine operation)

. . . . . . . . . . . SELECT OPPOS ITE TANK(if vapor sy mptoms con tinue). . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF(after fuel flow has stabilized)

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ABNORMAL LANDINGSLANDING WlTH A FLAT MAlN TlRE

1. Approach.. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .NORMAL2. Wing Flaps. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ULL3. Touchdown. . . . . . . . . . . . . . . . . . . . . . .GOOD MAIN TIRE FIRST

(Hold airplane off flat tire as long as possible with aileron control)4. Directional Control . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MAINTAIN(Using brake on good wheel as required)

LANDING WlTH A FLAT NOSE TlRE1. Approach.. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .NORMAL2. Wing Flaps. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .AS REQUIRED

120 to 140 KlAS - Flaps UP - 10"100 to 120 KlAS - Flaps 10" - 20"Below 100 KlAS - Flaps FULL

3. Touchdown . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON MAINS(Hold nosewheel off the ground as long as possible)

4. When nosewheel touches down, maintain full up elevator as airplaneslows to stop.

ELECTRICAL POWER SUPPLY SYSTEMMALFUNCTIONSM BUS VOLTS MORE THAN 32 OR M BAT AMPS MORETHAN 40

1. MASTER Switch (ALT Only) . . . . . . . . . . . . . . . . . . . . . . . . . .OFFNOTE

The Main Battery supplies electrical power to the Main andEssential Buses until M BUS VOLTS decreases below 20volts. When M BUS VOLTS falls below 20 volts, the StandbyBattery System will automatically supply electrical power tothe Essential Bus for at least 30 minutes.


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- Model 182T NAV Il l Avionics Pilots' Checklist- M BUS VOLTS MORE THAN 32 OR M BAT AMPS MORETHAN 40 (Continued)

. . . . . . . . . . . .- 2. Electrical Load REDUCE IMMEDIATELY as follows:. . . . . . . . . . . . . . . . . . . . . . . .. AVIONICS Switch (BUS 1). OFFb. PlTOT HEAT. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFFc. BEACON Light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FFd. LANDLight . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF(use as required for landing)e. TAXI Light. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFFf. NAVLights . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FFg. STROBE Lights. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. CABIN PWR 12V OFF

NOTESelect COM l MIC and NAVl on the audio panel and tune tothe active frequency before setting AVIONICS BUS 2 to OFF.If COM2 MIC and NAV2 are selected when AVIONICS BUS2 is set to off, the COM and NAV radios cannot be tuned.i. CO Ml and NAV1. . . . . . . . . . TUNE TO ACTIVE FREQUENCYj . CO Ml MIC and NAVl . . . . . . . . . . . . . . . . . . . . . . . . .SELECT(COM2 MIC and NAV2 will be inoperative onceAVIONICS BUS 2 is selected to OFF)

NOTEWhen AVIONICS BUS 2 is set to OFF, the following items willnot operate:

KAP 140 Autopilot GMA 1347 Audio PanelCOMM 2 NAV 2GTX 33 Transponder GDU 1040 MFDk. AVIONICS Switch (BUS 2). . . . . . . . . . . . . . . . . . . . . . . . . OFF(KEEP ON if in clouds)


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-Pilots' Checklist NAV Ill Avionics Model 182TM BUS VOLTS MORE THAN 32 OR M BAT AMPS MORETHAN 40 (Continued)

3. Land as soon as practical. -NOTE

Ma ke sure a successful landing is possible before extendingflaps. The flap motor is a large electrical load during -operation.

LOW VOLTS ANNUNCIATOR COMES ON BELOW 1000 RPM -1. Throttle Control . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1000 RPM

. . . . . . . . . .. Low Voltage Annunciator (LOW VOLTS ). CHECK OFF -LOW VOLTS ANNUNCIATOR REMAINS ON AT 1000 RPM3. Authorized maintenance personnel m ust do electrical systeminspection prior to next flight. -

LOW VOLTS ANNUNCIATOR COMES ON OR DOES NOT GOOFF AT HIGHER RPM --

I. MAS TER S witch (AI-T Only) . . . . . . . . . . . . . . . . . . . . . . . . . . OFF2. Alternator Circuit Breaker (ALT FIE LD) . . . . . . . . . . . . . . CHECK IN -3. MAS TER Switch (AI-T and BAT) . . . . . . . . . . . . . . . . . . . . . . . .ON4. Low Voltage Annunciator (LOW VOLTS). . . . . . . . . . . CHECK OFF5. M BUS VOLTS. . . . . . . . . . . . . . . . . . . . .CHECK 27.5 V m inimum6. M BAT AMPS . . . . . . . . . . . . . . . . . . . . . . CHECK CHARGING (+) -IF LOW VOLTS ANNUNCIATOR REMAINS ON7. MAS TER Switch (AI-T Only) . . . . . . . . . . . . . . . . . . . . . . . . . . OFF -

NOTEThe Main Battery supplies electrical power to the Main and -Essential Buses until M BUS VOLTS decreases below 20volts. When M BUS VOLTS falls below 20 volts, the StandbyBattery System will automatically supply electrical power to -the Essential Bus for at least 30 minutes.1 (Continued Next Page) -

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- Model 182T NAV Il l Avionics Pilots' ChecklistIF LOW VOLTS ANNUNCIATOR REMAINS ON(Continued)8. Electrical Load . . . . . . . . . . . . REDUCE IMMEDIATELY as follows:a. AVIONICS Switch (BUS 1). . . . . . . . . . . . . . . . . . . . . . . . .OFFb. PlTOT HEAT. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFFc. BEACON Light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFd. LAND Light. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

(Use as required for landing)e. TAXI Light. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFf. NAVLights . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFFg. STROBE Lights. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFh. CABIN PWR 12V . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFFNOTE

Select COMl MIC and NAVI on the audio panel and tune tothe active frequency before setting AVIONICS BUS 2 to OFF.If COM2 MIC and NAV2 are selected when AVIONICS BUS2 is set to off, the COM and NAV radios cannot be tuned.i. COMl and NAVI . . . . . . . . . . TUNE TO ACTIVE FREQUENCYj. COM l MIC and NAVI . . . . . . . . . . . . . . . . . . . . . . . . . SELECT(COM2 MIC and NAV2 will be inoperative onceAVIONICS BUS 2 is selected to OFF)

NOTEWhen AVIONICS BUS 2 is set to OFF, the following items willnot operate:

KAP 140 Autopilot GMA 1347 Audio PanelCOMM 2 NAV 2GTX 33 Transponder GDU 1040 MFDk. AVIONICS Switch (BUS 2). . . . . . . . . . . . . . . . . . . . . . . . . OFF(KEEP ON if in clouds)

9. Land as soon as practical.NOTE

Make sure a successful landing is possible before extendingflaps. The flap motor is a large electrical load duringoperation.

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Pilots' Checklist NAV Il l Avionics IWodeI 182T

AIR DATA SYSTEM FAILURE -RED X - PFD AIRSPEED INDICATOR

1. ADCIAHRS Circuit Breakers . . . . . . . . . . . . . . . . . . . . .CHECK IN -(ESS BUS and AVN BUS 1)If open, reset (close) circuit breaker. If circuit breaker opens again,do not reset.. . . . . . . . . . . . . .. Standby Airspeed Indicator USE FOR AIRSPEEDINFORMATION

RED X - PFD ALTITUDE INDICATOR -1. ADCIAHRS Circuit Breakers . . . . . . . . . . . . . . . . . . . . .CHECK IN(ESS BUS and AVN BUS 1 -If open, reset (close) circuit breaker. If circuit breaker opens again,do not reset.2. Standby Altimeter . . . . . . CHECK current barometric pressure SET. --USE FOR ALTITUDE INFORMATION.

ATTITUDE AND HEADING REFERENCE -SYSTEM (AHRS) FAILURERED X - PFD ATTITUDE INDICATOR -

1. ADCIAHRS Circuit Breakers . . . . . . . . . . . . . . . . . . . . . CHECK IN(ESS BUS and AVN BUS 1If open, reset (close) circuit breaker. If circuit breaker opens again, --do not reset.2. Standby Attitude Indicator. . . . . . . . . . . . . . . . USE FOR ATTITUDEINFORMATION -

RED X - HORIZONTAL SITUATION INDICATOR (HSI)1. ADCIAHRS Circuit Breakers . . . . . . . . . . . . . . . . . . . . .CHECK IN -(ESS BUS and AVN BUS 1)If open, reset (close) circuit breaker. If circuit breaker opens again,do not reset. -2. Non-Stabilized Magnetic Compass . . . . . . . . . USE FOR HEADINGINFORMATION

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DISPLAY CO OLING ADVISORYPF DI COOLING OR M FD l COOLING ANNUNCIATOR(S)

1. Cab~nHeat (CABIN H i ) . . . . . . . . . . . . . . . . . . . . . . . REDUCE(minimum preferred!2. Forward Avionics Fa n. . . . . . . . . . . . . . . . . . . . . . . . . CHECK

(Feel for airflow from screen on glareshield)IF FORWA RD AVIONICS FAN HAS FAILED3 . STBY BATT Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

(Unless needed for emergency power)IF PFDI COOLING OR MFDI COOLING ANNUNCIATOR DOES NOTGO OFF WITHIN 3 MINUTES OR IF BOTH PFD I COOLING AND M FD lCOOLING ANNUNCIATORS COME ON3 STBY BATT Sw~t cil 1'3FF

(Land as soon d\ b r i - t , l 21

VACUUM SYSTEM FAILURELOW VACUUM ANNUNCIATOR COMES ON

1 CAUTION I- 5F 'JACUUILI F'(31NTER ! S (JUT OF THE GREEN 4:;DURING FLIGHT (R GYRO FLAG IS SHOWN OIJ T t ~ r5 4NDBY P TIT!JDE INDICATOR THE STAI

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Pilots' Checklist NAV I ll Avionics

MAXIMUM GLIDEModel 182T -

-

Ground Distance - Nautical MilesFigure 2*

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- Mo del 182T IVAV Ill Avionics Pilots' Chec klistPERFORMANCE

TABLE OF CONTE NTSCROSSWIND COMPONENT ..................................................................... -2- TAKEOFF

SHORT FIELD TAKEOFF DISTANCE AT 3100 POUNDS .............SHORT FIELD TAKEOFF DISTANCE AT 2700 PO UNDS .................4- SHORT F IELD TAKEOFF DISTANCE AT 2300 PO UNDS . . . . . . . . . . . . . . . . .

CRUISE. . . . . .CRU ISE PERFORMAN CE PRESSURE ALTITUDE SEA LEVEL P-6

CRUISE PER FORMANCE PRESSURE ALTITUDE 2000 FEET .......P-8CRUISE PER FORMANCE PRESSURE ALTITUDE 4000 FEET .....P-10- CRUISE PER FORMANCE PRESSURE ALTITUDE 6000 FEET .....P-12CRUISE PER FORMANCE PRESSURE ALTITUDE 8000 FEET .....P-13

- CRU ISE PERFOR MAN CE PRESSURE ALTITUDE 10,000 FEET ..P-14CRLllSE PERFO RMA NCE PRE SSUR E AI-TITLIDE 12,000 FEET ..P-15CRU ISE PERFOR MAN CE PRESSURE ALTITUDE 14,000 FEET ..P-16- LANDING

...............HORT FIELD LAND ING DISTANCE AT 2950 PO UNDS P-17...................................................................ENSITY AL1-ITUDE CHA RT P-18-

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Pilots' Checklist NAV Ill Avionics Model 182T -CROSSWIND COMPONENT

Crosswind Component - KnotsNoteMaximum demonstrated crosswind velocity is 15knots (not a limitation).

Figure 3

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- Model 182T NAV Il l Avionics Pilots' Checklist- SHORT FIELD TAKEOFF DISTANCEAT 3100 POUNDS- CONDITIONS:Flaps 20" Cowl Flaps Open

2400 RPM, Full Throttle and Lift Off: 49 KlASMixture Set Prior to Brake Release Speed at 50 Feet: 58 KlASPaved, Level, Dry Runway Zero Wind-

- NOTE

PressureAltitudeinFeet

S L10002000300040005000600070008000

Short field technique as specified in NORMAL PROCEDURES pageN-17.- Prior to takeoff, the mixture should be leaned to the Maximum PowerFuel Flow placard value in a full throttle, static runup.- Decrease distances 10% for each 9 knots headwind. For operationwith tail winds up to 10 knots, increase distances by 10% for each 2knots.

0C

- For operation on dry, grass runway, increase distances by 15% of the"ground roll" figure.

GrndRoll71577585092510151110122013401480

TotalFt toClear50 FtObst136514901635180019902210247027853175

10C

GrndRoll76583591599510901195131514451595


20C

GrndRoll825900980107011751290141515601720


30C

GrndRoll885965105511501260138515201675

---

40CTotalFt toClear50 FtObst16801845203522552515282032003685-..

GrndRoll945103011301235135514851635---...

TotalFt toClear50 FtObst1800198021902435272030703510......

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Pilots' Checklist NAV Ill Avionics Model 182T -SHORT FIELD TAKEOFF DISTANCE

AT 2700 POUNDSCONDITIONS:

Flaps 20" Cowl Flaps Open2400 RPM, Full Throttle and Lift Off: 45 KlASMixture Set Prior to Brake Release Speed at 50 Feet: 54 KlASPaved, Level, Dry Runway Zero Wind

NOTEShort field technique as specified in NORMAL PROCEDURES pageN-17.

PressureAltitudeinFeet

S L10002000300040005000600070008000

Prior to takeoff, the mixture should be leaned to the Maximum PowerFuel Flow placard value in a full throttle, static runup.Decrease distances 10% for each 9 knots headwind. For operationwith tail winds up to 10 knots, increase distances by 10% for each 2knots.For operation on dry, grass runway, increase distances by 15% of the"ground roll" figure.

0C

GrndRoll5205656156757358058809651060


10C

GrndRoll56061066572579086595010401145


20C

GrndRoll600655710775850930102011201230


30C

GrndRoll6457007658359101000109512001320

40CTotalFt toClear50 FtObst121513201445158517401920213523802675

GrndRoll6907508208959751070117512901420


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- Model 182T NAV Il l Avionics Pilots' Checklist- SHO RT FIELD TAKEOFF DISTANCE

AT 2300 POUNDS- CONDITIONS:Flaps 20" Cowl Flaps Open2400 RPM, Full Throttle and Lift Off: 42 KlASMixture Set Prior to Brake Release Speed at 50 Feet 50 KlASPaved, Level, Dry Runway- Zero Wind

- NOTE

PressureAltitudein Feet

S L10002000300040005000600070008000

Short field technique as specified in NORMAL PROCEDURES pageN-17.- Prior to takeoff, the mixture should be leaned to the Maximum PowerFuel Flow placard value in a full throttle, static runup.Decrease distances 10% for each 9 knots headwind. For operationwith tail winds up to 10 knots, increase distances by 10% for each 2knots.

0C

For operation on dry, grass runway, increase distances by 15% of the- "ground roll" figure.

GrndRoll365395430470510555610665730


10C

GrndRoll390

20C 30CTotalFt toClear50 FtObst750

425460505550600655715785

GrndRoll420

GrndRoll450

40C

81588596010451140125013701510

TotalFt toClearSO FtObst800


GrndRoll480

455 870 490 925 520 985495 1 940 1 530 1 1005 I 565 1 1070 1


540590640700770845

102511151220133514701620

580630690755825905

109011901305143015701735

620675735805885970

116512701390153016851865

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Pilots' Checklist NAV Ill Avionics Model 182T -CRUISE PERFORMANCE

PRESSURE ALTITUDE SEA LEVELCONDITIONS:3100 PoundsRecommended Lean MixtureCowl Flaps Closed

NOTEMaximum cruise power is 80% MCP. Those powers abovethat value in the table are for interpolation purposes only.

RPM2400

2300

2200

' For best economy, operate at peak EGT. -

MP2726252423222120

2726252423222120

2726252423222120

20C BELOWO h

BPH------847974696560------807671676258-- -82777369656056

STANDARDSTANDARD

KTAS.-----134132129126122118--.--.133130127124120116---133131129126122118114

BPH------817671676258...82787369656056

8379757166625854

20C ABOVETEMP

GPH------

14.513.612.812.111.410.7------

13.913.212.411.711.110.4...

14.213.412.712.011.410.810.2

%BPH.--82787469656056

8479757167625854

8076726864605652

TEMPERATUREKTAS------136133130127122118---137135132128124120116

137135133130126122119114

GPH.-.---

14.013.212.411.711.110.4--.

14.213.412.712.011.410.810.2

14.413.612.912.311.711.11 0 . 59.9

STANDARDKTAS--.140138135131127123118

141139136132129125121116

139136

TEMPGPH

---14.313.512.812.111.410.810.2

14.513.713.012.311.713.110.59.9

13.913.2

1 3 4 1 1 2 . 6 1130126123118 .114

11.911.310.8

-10~29.7 -

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- Mo del 182T NAV Ill Avionics Pilots' ChecklistCRUISE PERFORMANCE

PRESSURE ALTITUDE SEA LEVEL (Continued)CONDITIONS:3100 PoundsRecommended Lean MixtureCowl Flaps Closed

NOTE

RPM2100

2000

Maximu m cruise pow er is 80% MCP. Those powers abovethat value in the table are for interpolation purposes o nly.For best economy, operate at peak EGT.

MP2726252423222120

2726252423222120

20C BELOWYo

BPH8278747066615753

787470666 2585451-

STANDARDSTANDARDKTAS

13 313 112 912 612 311 911 511 1

13 112 912 612 312 011 611 310 8

%BPH7 975716763595551

757167646 0565349

20C ABOVESTANDARD TEMPEM PGPH14.213.412.812.111.510.910.49.8

13.412.812.211.611.010.510.09.4

%BPHTEMPERATURE

KTAS13 513 313 012 712 312 011 611 1

13 313 012 712 412 011 711 210 8

G PH13.713.012.411.811.210.610.19.6

13.012.411.811.310.710.29.79.2

KTAS GP H1 76 ( 13 6 1 13.2 1

73 1 13 4 1 12.6 112.011.410.910.49.99.3

12.612.011.511.010.510.09. 59.0

696561575450

7269656258545147

13 012 712 312 011 511 1

13 413 112 712 412 111 611 210 8

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P~lo ts ' heckl~st NAV I l l Avionics M ~ d e !82T

CRUISE PERFORMANCEPRESSURE ALTITUDE 2000 FEET

CONDITIONS:3100 PoundsRecommended Lean MixtureCowl Flaps Closed

NOTE

RPM2400

2300

2200

Maximum cruise power is 8O0/0 MCP. Those powers abovethat value in the table are for interpo lation purpose s only.For best economy, operate at peak EGT.

MP26252423222120

26252423222120

26252423222120

20C BELOW

YoBPH-- ----8177726762

---837874696560

---807571676258

STANDARDSTANDARD

KTAS......136133130126122

-..137134131128124120

---135132129126122118

20C ABOVETEMP

GPH....-.14.113.312.511.811.0

---14.413.612.812.111.410.7

---13.813.112.411.711.110.5

GPH---

14.413.612.812.111.410.7

...13.913.112.411.711.110.5

14.113.312.612.011.410.810.2

O/oBPH-.-807671676358

82777369656056

78747066625854

%BPH---837974696560

---807671676258

81777369646056

TEMPERATURE

KTAS---140138134131126122

---139136133128124120

139137134130126122118

STANDARD

KTAS---142139135131127122

143140137133129125120

140138134130127122118

TEMP

GPH---

13.913.212.411.711 110.5

14213.412.712.011.410.810.2

13.612.912.311.611.010.59.9

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- Mo del 182T NAV Il l Avionics Pilots' ChecklistCRUISE PERFORMANCE

PRESSURE ALTITUDE 2000 FEET (Continued)CONDITIONS:- 3100 PoundsRecommended Lean MixtureCowl Flaps Closed

- NOTEMaximu m cruise power is 80% MCP. Those powers abovethat value in the table are for interpolation purposes only.

RPM2100

2000

- For best economy, operate at peak EGT

~p26252423222120

26252423222120

20C BELOWYo

BPH80767268645955

76726864605652

STANDARDSTANDARDKTAS135133130127123119115

133130127124120116112

20C ABOVE

GPH13.412.712.111.510.910.49.8

12.712.111.511.010.510.09.4

TEMPGPH13.913.112.511.811.210.610.1

13.112.511.911.310.810.29.7

YoBPH77736965615753

73696662585451

YoBPH75716763595552

71676460565349

TEMPERATUREKTAS137134131127123119115

134131127124120116112

STANDARD TEMPKTAS138134131127124119115

134131128124120

GPH12.912.311.711.210.610.19.6

12.311.811.210.710.2

116 1 9>7 1111 9.2

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Pilots' Checklist NAV Ill Avionics Model 182 T -CRUISE PERFORMANCE

PRESSURE ALTITUDE 4000 FEETCONDITIONS:3100 PoundsRecommended Lean MixtureCowl Flaps Closed

NOTE

RpM2400

2300

2200

Ma ximu m cruise powe r is 80o MCP. Those pow ers above -that value in the table are for interpolation purposes only.For best economy, operate at peak EGT. -

MP252423222120

252423222120

252423222120

20C BELOWyo

BPH---8479747065---8176726762

827873696560

STANDARDyo

BPH---8176726762

837874696560

797571666258

STANDARDKTAS---140138134130126---138135132128124

139136133130126122

20C ABOVETEMP

GPH...14.613.712.912.111.4...

14.013.212.511.711.1

14.213.412.712.011.410.7

%BPH

7874696560

807571676258

777268646056

TEMPERATUREKTAS---142139135131126

143140137133128124

141138134130126122

GPH

14.013.212.511.711.1

14.313.512.812.111.410.7

13.713.012.311.711.010.4

STANDARDKTAS74 s143139135131126

144141137133129124

142138134130126121

TEMPGPHi 4 . 413.612.812.111.410.8

13.813.112.411.711.110.5

13.212.611.911.310.710.2

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Model 182T NAV Ill Avionics Pilots' ChecklistCRUISE PERFORMANCE

PRESSURE ALTITUDE 4000 FEET (Continued)CONDITIONS:3100 PoundsRecommended Lean MixtureCowl Flaps Closed

NOTEMaximum cruise power is 80% IVICP. Those powers abovethat value in the table are for interpolation purposes oniy.

R p M2100

2000

For best economy, operate at peak EGT

M p252423222120252423222120

20C B ELOWSTANDARD TEMPYoBPH787470666157747066625854

STANDARDTEMPERATURE

KTAS13 713 413 112 712 311 913 413 112 712 412 011 6

YoBPH757167635955716864605652

20C ABO VESTANDARD TEMP

GPH13.512.812.211.510.910.312.812.211.611.010.59. 9

O/oBP H736965615753696562585451

KTAS13 813 513 112 712 311 913 513 112 812 412 011 5

GPH13.012.411.811.210.610.112.411.811.310.710.29. 7

KTAS13 813 513 112 712 311 813 513 212 812 412 011 5

GPH12.612.011.410.910.39. 812.111.511.010.49 .99. 4

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PRESSURE ALTITUDE 6000 FEETCONDITIONS:3100 PoundsRecommended Lean MixtureCowl F l a ~ s losed

Maximum cruise power is 80% MCP. Those powers abovethat value in the table are for interpolation purposes only.

RPM2400

2300

2200

2100

2000

For best economy, operate at peak EGT.

~p23222120192322212019

232221201923222120192322212019

20C BELOW

%BPH82777267627974696560

767167625872686359556864605652

STANDARDSTANDARD

KTAS142138135130126140136132128124

137134130126121135131127123118131127124119115

%BPH7974696560

20C ABOVESTANDARD TEMPEMP

GPH14.213.312.511.711.013.612.812.111.410.7

13.112.411.711.010.412.511.811.210.610.011.911.310.710.29.6

7671676258

736964605669656157536662585450

NOTE

TEMPERATUREGPH13.212.411.711.110.4

YoBPH7672676258

KTAS143139135130126

KTAS144139135131125

I:: I :::I / :: 1 ::: ::::GPH13.612.812.111.410.7

133128123

138134130126121135131127122118132128123119114

11.711.010.4

12.612.011.310.710.112.111.510.910.39.811.511.010.49.99.4

646056

706662585467635955516360565248

133128123

138135130125120135131127122117132128123118113

11.410.710.1

12.311.611.010.49.911.711.110.610.09.511.210.710.29.79.1

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- Model 182T NAV Il l Avionics Pilots' Checklist- CRUISE PERFORMANCEPRESSURE ALTITUDE 8000 FEET

CONDITIONS:3100 PoundsRecommended Lean MixtureCowl Flaps Closed

- NOTE

RPM2400

2300

2200

2100

2000

Maximum cruise power is 80% MCP. Those powers abovethat value in the table are for interpolation purposes only.For best economy, operate at peak EGT.

Mp21201918212019182120191821201918212019

20C BELOWYo

BPH74696459726762576964605565615752

625854

STANDARDSTANDARDKTAS139134130125136132128122134130125120131127122

%BPH72676257696460556662575363

20 C ABOVETEMPGPH1 2 91 2 111 41 0 61 2 51 1 711 01 0 31 2 01 1 31 0 71 0 11 1 51 0 91 0 3

5955

%BPH69656055676258536460555161 .


5017

GPH1 2 51 1 711 010 31 2 01 1 31 0 710 11 1 61 1 01 0 49 81 1 2

126121116127123118

STANDARDKTAS140135130124137132127121134129124119131

9 7

TEMPGPH1 2 11 1 41 0 710 11 1 71 1 01 0 49 81131 0 710 19 51 0 8

57I 531 2 8 1 1 1 0 1 60

9 4 , 49107 58

126121115

127122117

1 0 19 6

5652

123118

I11 0 49 99 4

5450

1 0 49 9

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PRESSURE ALTITUDE 10,000 FEETCONDITIONS:3100 PoundsRecommended Lean MixtureCowl Flaps Closed

NOTE

RPM2400

2300

2200

2100

2000

Maximum cruise power is 80% MCP. Those powers abovethat value in the table are for interpolation purposes only.For best economy, operate at peak EGT.

MP201918

21201918

201918

201918

201918

20C BELOWTEMPGPH12.511.711.0

12.812.111.310.6

11.611.010.3

11.210.59.9

10.710.19.6

STANDARD%

BPH726762

74696459

666257

635954

605651

YoBPH696459

71666257

645955

615652

585450

20C ABOVESTANDARDKTAS139134129

141136132126

134129124

131126121

127122117


141137132126

134129123

130125120

127122116

TEMPGPH11.711.010.3

12.011.310 710.1

10.91 0 49.8

10.510.09.4

10.19.69.0

%BPH676257

69646055

625753

595450

555248

GPH12.111.310.6

12.411.711.010.3

11.310.610.0

10.810.29.7

10.49.89.3

STANDARDKTAS139134128

142136131125

133128123

130125119

126121115

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- Mo del 182T IVAV Ill Avionics Pilots' ChecklistCRUISE PERFORMANCE

PRESSURE ALTITUDE 12,000 FEETCONDl'fIONS:- 3100 PoundsRecommended Lean MixtureCowl Flaps Closed

NOTE

RPM2400

2300

2200

2100

2000

Maximum cruise power is 80% MCP. Those powers abovethat value in the table are for interpolation purposes only.For best economy, operate at peak EGT.

MP181716

181716

1817

1817

1918

20C BELOW 20C ABOVE%

BPH645953

615652

5954

5652

5753

STANDARDO h

BPH595450

575248

5550

5248

5349

YoBPH615651

595450

5752

5450

5551

STANDARD

KTAS133127121

131125118

128122

125119

126121

STANDARD

KTAS133126119

130123117

127121

123117

125119

TEMP

GPH11.310.59.8

10.910.29.6

10.69.9

10.29.6

10.49.8

TEMP

GPH10.610.09.3

10.39 79.0

10.09.4

9.69.1

9.89.3

TEMPERATURE

KTAS133127120

130124118

128121

124118

125120

GPH10.910.29.6

10.610.09.3

10.39.7

9.99.3

10.19.5

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g1000noroppoh_c182t

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