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Bell 206 Jet Ranger HB-XYA

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HB-XYA

BELL 206 JET RANGER CHECKLIST EMERGENCY CHECKLIST LIMITATIONS PERFORMANCES PREFLIGHT CHECKLIST ALERT CHECKLISTE SECURITY AROUND W&B COMPUTATION SAMPLES

The pilot is responsible for correct operation of the helicopter according the AFM. This summary is provided only as additional material for preflight preparation. Heli-Lausanne declines all responsability in case of non respect of any official manufacturer limitations(AFM).

ALLWAYS REFER TO AFM FOR MANUFACTURER PROCEDURES


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BELL 206 B III - NORMAL PROCEDURES / CHECKLISTS 0. Rotor blades ……………………………………………………… free

Cockpit Preparation 1. Frictions.......................................................................................... off 2. Flight Controls.................................................. freedom of movement 3. Frictions.......................................................................................... on 4. Throttle...................................... check freedom & idle stop operation 5. Rotor brake (if installed) ....................................................... secured 6. Circuit breakers ........................................................................... all in 7. Overhead switches......................................................................... off 8. Cabin heater .................................................................................. off 9. Generator........................................................................................ off 10. Altimeter......................................................................................... set 11. Engine gauges............................................................................. zero 12. Flight instruments............................................................... static/zero 13. Fuel valve switch............................................................................. on 14. Comm / Nav / Transponder (master switch)................................... off 15. Hydraulic switch ............................................................................. on 16. Engine Anti-Ice switch.................................................................... off 17. Landing light................................................................................... off

Engine Pre-Start 1. Battery switch (for battery and GPU start)......................................... on (for battery cart start........................................................................ off) (for GPU start…………………………………………………………… on) 2. Engine Out Horn ....................................................................... audible 3. Fuel pumps .................................................................................. check 4. Fuel pressure ............................................................................... check 5. Fuel quantity ................................................................................ check 6. Warning lights ................................................................... press to test 7. TOT instrument check .....................................OAT or residual temp if S/E or O/E digits = previous exceedance detected -> abort start 8. Rotor Low RPM............................................................. light and audio


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Engine Start 1. Anti-Collision light............................................................................... on 2. Collective...................................................................................... down

Caution !

3. Throttle........................................ .............................................. clos ed 4. Rotor ............................................................................................... free 5. Area .............................................................................................. clear

Caution ! Monitor TOT in case of inadvertent throttle opening ! TOT must stay steady or decrease when starter is en gaged! If TOT rise before throttle opening ……close throttl e immediately !

6. Starter....................................................................................... engage 7. Engine Oil Pressure ................................................................ increase 8. Throttle.......................... open to flight idle at 15% N1 and TOT <150°C N1 Starting Speed N1 RPM.......................................................................................................................... TEMP °C 15% ............................................................................................................................ Above 7°C 13% ........................................................................................................................ .. -18 to +7°C 12% ......................................................................................................................... Below –18°C If N1 remains below 12% …………………………………………………………………... abort start

Caution ! Abort start if TOT is about to reach either 927°C o r remains maximum 10 seconds between 810°C and 927°C TOT digits flash indicates TOT is passing red line, in transcient (max 10 seconds to return below red line)

9. TOT.......................................................................................... monit or 10. Rotor .................................................................... turning at 25% N1 11. Starter ................................................................. release at 58% N1


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12. Idle (60%-62% N1) (If more than 15 minutes shutdown)................ 1 minute 13. Engine gauges.................................................................. within limits 14. (GPU disconnect; Battery................................................................ on) 15. Throttle....................................................................... open to 70% N1 16. Generator Switch ............................................................................. on 17. Loadmeter..................................................................... below red line 18. Avionic master switch (if installed)................................................... on 19. Position lights..................................................................... as required 20. Standby horizon (if installed) ........................................................... on 21. Strobe light..................................................................................... on 22. Defog Blower .................................................... check, on as required 23. GPS (if installed).............................................................................. on 24. FLARM (if installed)......................................................................... on 25. COMM / NAV............................................................... set as required 26. Transponder................................................................ set as required 27. ELT ..................................................... check for inadvertent xmission

Engine Run-Up 1. Throttle........................................................... increase to full open psn

Caution ! Do not exceed 40% Torque during accelaration Avoid N 2 range 75 – 88 % when torque is greater th an 33 %

2. N2 Governor.........................................................check range 97-100% 3. Engine Anti-Ice.......................................... check for TOT rise, then off 4. Hydraulic system.......................................................................... check 5. Engine relight (if installed)....................................... test, reset, then on 6. Directional gyro (if installed).............................................................. set 7. LANDING LIGHT ON (for in-flight collision avoidance, keep light ON a ll flight duration)


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Check before Departure 1. Frictions............................................................................................. off 2. Throttle..................................................................................... full open 3. RRPM............................................................................................ 100% 4. All warning lights ............................................................................... off 5. Engine gauges.............................................................................. green 6. Fuel quantity ........................................................................... checked 7. Engine anti-ice (4,4°C and below + visble moisture =ON)………… as required 8. Heater ............................................................................................... off 9. Landing light...................................... ............................................. ON 10. Comm / Nav setting............................................................... checked Check in Ground Effect 1. RRPM........................................................................................... 100% 2. Torque/TOT/N1 .................................................................. within limits 3. Take-off axis ................................................................................. clear 4. Wind............................................................................................. check Climb check 1. Speed....................................................................................... adjusted 2. Vertical speed ........................................................................... positive 3. Engine Anti-Ice (4°C and below + visble moisture =ON).............. as required 4. Pitot heat.............................................................................. as required Check for Approach 1. Throttle..................................................................................... full open 2. RRPM............................................................................................ 100% 3. All warning lights ............................................................................... off 4. Engine gauges.............................................................................. green 5. Fuel quantity ........................................................................... checked 6. Engine Anti-Ice (4°C and below + visble moisture =ON).............. as required 7. Heater ............................................................................................... off 8. Landing light................................................................................ ON Final Check 1. Speed........................................................................................... 30 kt. 2. Vertical speed ..................................................................... <500ft/Min. 3. Decision ........................................................................ land/go around


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Engine Shut Down 1. Throttle............................................................................ idle for 2 min 2. Frictions.............................................................................................. on 3. Landing light...................................................................................... off 4. Avionics master switch (if installed)................................................... off 5. Position lights.................................................................................... off 6. Heater ............................................................................................... off 7. Strobe light (if installed)..................................................................... off 8. Gyro / standby horizon ...................................................................... off 9. GPS (if installed) .............................................................................. off 10. FLARM (if installed)......................................................................... off 11. Com/Nav/XPDR (if no master switch) ............................................ off 12. ELT (if installed).................................. check for inadvertent xmission After 2 minutes cool-down 13. Generator........................................................................................ off 14. Throttle........................................................................................ close 15. Rotor brake (if installed) ................................ apply 38%-30% RRPM 16. Beacon............................................................................................. off 17. Battery switch (if TOT stabilized and N1=0%)................................. off


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BELL 206 B III - EMERGENCY PROCEDURES ENGINE FAILURE

- Enter autorotation immediately TAIL ROTOR CONTROL FAILURE

• Complete Loss of Thrust - Close throttle - Enter autorotation - Maintain minimum airspeed 50 knots (58 mph)

• Fixed Pitch Failure - Adjust power to minimise excessive yawing - Adjust airspeed to minimise excessive yawing

FUEL CONTROL/GOVERNOR FAILURE - Control power with Throttle if engine overspeeds - Maintain RPM with collective pitch if engine underspeeds - Establish autorotation if power is too low or engine must be shut

down - Prepare for power-off landing

HYDRAULIC SYSTEM FAILURE

- Reduce airspeed to 61-69 knots (70-80 mph) - HYD BOOST c/b: ON (OFF if power is not restored) - Land as soon as practical and investigate - (A run-on landing at 10-15 knots (12-17 mph) is recommended

GENERATOR FAILURE

- Cycle GENerator switch. If power is not restored: OFF - All electrical equipment: OFF (to conserve battery) - Required electrical equipment: ON (only as needed) - Reduce altitude to below 6000 feet (1830 m)

BOOST PUMP FAILURE

- Descend to below 6000 feet (1830 m) CAUTION : UNUSABLE FUEL: 10 U.S. GALLS (38 LITERS)

ENGINE FIRE DURING FLIGHT - Close throttle - Enter autorotation immediately - FUEL VALVE switch: OFF - BATTery switch: OFF - GENerator switch: OFF - Execute autorotational landing


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ENGINE FIRE DURING START

- Close throttle - Continue to motor engine with starter

FUEL VALVE switch: OFF -

ENGINE AIR START - Establish steady autorotation - GENerator switch: OFF - Perform normal engine starting procedures

CAUTION:DO NOT ATTEMPT AIR-RESTART ABOVE 12'000 FEET (3660 M)

RED L I G H T S

ENG OUT (audio and light)

Engine failure. Enter autorotation

BATTERY HOT Land as soon as possible (Do not use helicopter battery for restart)

A M B E R L I G H T S

ROTOR LOW RPM (audio and light)

1. Reduce collective pitch 2. Check throttle full open

TRANS TEMP Land as soon as possible TRANS PRESS Land as soon as possible TRANS CHIP Land as soon as possible ENG CHIP Land as soon as possible T/R CHIP Land as soon as possible FUEL FILTER Land as soon as practical A/F FUEL FILTER Land as soon as practical FUEL PUMP

1. Descend to below 6000 feet (1830 m) CAUTION: UNUSABLE FUEL: 10 U.S. GALLS.

FUEL LOW Plan landing (approx. 20 Galls left) BATTERY TEMP

1. Move battery switch to OFF until battery cools and light extinguishes 2. BATTery switch: ON

GEN FAIL

1. Gen switch – RESET; then ON 2. If power not restored – Gen switch OFF 3. All unnecessary equipment off 4. Reduce altitude to below 6000 ft PA 5. Land as soon as practical


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BELL 206 BIII - LIMITATIONS (summary from AFM) MTOW Internal load Maximum 3200 lbs With external load 3350 lbs Cargo hook 1500 lbs

Speed (VNE) Power-on </= 3000 lbs MTOW

Maximum 130 kts

above 3000 ft -3.5 kts/1000 ft Alt

Power-on > 3000 lbs MTOW

Maximum 122 kts

above 3000 ft -7.0 kts/1000 ft Alt

Power-off Maximum 100 kts Aft Doors removed Maximum 87 kts Forward Doors removed Maximum 69 kts LH Sliding door opening Maximum 87 kts LH Sliding door closing Maximum 87 kts

Altitude </= 3000 lbs Maximum 20’000 ft PA > 3000 lbs 13’500 ft DA

Temperature OAT Below 4,4°C and visible Moist Anti Ice ON

Main Rotor Power-on In stabilized flight 97% – 100% RPM Maximum transient (5 sec) 95% -97% RPM Power-off Maximum 107% RPM Minimum 90% RPM Rotor brake Maximum 38% RPM

Torque Maximum continuous 85 % IAS < 80 kts Maximum take-off (5 min) 100 % Maximum transient (5 sec) 110 % (intentional

use prohibited)

Gas Producer (N1)

Flight Maximum continuous 60% -105%

Maximum 105% Maximum transient (15 sec) 106% Idle Minimum Ng = 60%-62%

TOT Engine start Maximum transient (10 sec) 810°C -927°C Take-off Maximum (5 min) 738°C – 810°C Power transient Maximum (6 sec) 810°C – 843°C

(intentional use prohibited)

In-flight Continuous 100°C – 738°C

Engine Oil Pressure Min. (N1 < 78.5%) 50 psi Min. (N1 < 78.5%) 90 psi Min. (N1 > 94.2%) 115 psi Maximum 130 psi Temperature Maximum 107°C

Xmsn Oil Pressure Minimum 30 psi Continious 30 psi -50 psi Maximum 70 psi Temperature Maximum 110°C

Fuel Pressure Minimum 4.0 psi Maximum 30.0 psi

Pilot & Pax Pilot Minimum 1 170 lbs< 75 usg 200 lbs> 75 usg Persons carried Maximum 5 (pilot included)

Heater Bleed Air Heater Switch OFF for T/O and landing


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PERFORMANCES HOGE


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BELL 206 B III - NORMAL PROCEDURES – PREFLIGHT CHEC K


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QUI QUAND QUOI COMMENT CONTACT

EQ

UIP

AG

E

Immédiat 1

Alerte

- REGA - Ambulance - Police - Pompiers

1414 canal K/R 144 117 118

Immédiat 2

Secours

- sécuriser le site de l’accident - actions pour sauver les vies - information aux sauveteurs

Immédiat 3

Information

Communication externe EXCLUSIVEMENT par le management de la COMPAGNIE. Aucune information aux médias ou tiers 021 / 636 35 35 piquet Heli-Lausanne

- Management compagnie - Responsable des opérations - Management technique

Protocole

- noter tous les appels et messages

Les principes les plus importants lors de l’alerte

Alerte Que s’est -il passé Où cela s’est -il passé (lieu, rue, montagne, altitude,

coordonnées, etc.) Quand cela s’est -il passé Qui est concerné ( nombres personnes, blessés, décès , etc. ) Hélicoptère et immatriculation Quelles mesures ont été prises Tous les appels, messages et mesures pr ises ont été

enregistrées jusqu’à ce que le management prenne le relais

Proches Les proches sont informées exclusivement par le management ou une personne autorisée par le managem ent

Information L’information à des tiers et aux médias est effectu ée exclusivement par le management ou une personne autorisée par le management


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