FOUR DAY TURBOJET TRAINING SYLLABUS

Citation I, II, III, V, Ultra, Encore, CJ CJ1, 2, 3

Lear 24, 25, 35

Westwind's I, II - Saberliner's - Falcon 10

HS 125 Hawker Series

PURPOSE: Upon completion of this course of instruction, the customer will be able to

demonstrate a comprehensive knowledge of the aircraft listed and their associated

systems, by successfully achieving a passing grade on both oral and written examinations.

Ground Training20 HOURS TOTAL

SUBJECT

TIME

AIRCRAFT 1.0

A. General Description

B. Airframe and Engines

ENGINES 3.0

A. Engine Description

(1) Temperature Limitations

(2) Thrust Limitations

(3) Fuel Control

(4) Power and Compressor Modules

(5) Free Turbine Principal

(6) Accessory Section

B. Engine Controls

(1) Power Levers

(2) Reverse Levers

(3) Fuel Levers

C. Engine Instruments

(1) Fan N1%

(2) ITT Gauges

(3) Turbine N2%

(4) Fuel Flow Gauge

(5) Oil Pressure Gauge

(6) Oil Temperature Gauge

D. Starting Procedures and Limitations

(1) Hot Starts

(2) Hung Starts

(3) Starter Limitation

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(4) Engine Clearing Procedures

(5) Bypass Ratio

E. Ignition System

(1) Auto Igniters System

(2) ITT Probes

(3) Fuel Nozzles

F. Air Induction System

(1) Ice Protection System

(2) Air Flow

G. Engine Fuel System

(1) Oil-to-Fuel Heater

H. Engine Oil System

(1) Quantity

(2) Tank and Location

(3) Oil Reading Hot/Cold

I. Fire Detection and Extinguishing

J. Auto Ignition System

(1) Arming System

(2) Recommended Use of System

PREFLIGHT & NORMAL PROCEDURES 3.0

A. Aircraft Preflight

B. Before Engine Starting

C. Starting Engines

D. Before Taxiing

E. Taxiing

F. Engine Run-Up Systems Testing

G. Before Takeoff

H. Line Up and Takeoff

I. After Takeoff

J. Climb Power Set Limitations

K. Cruise Power Set

L. Descent Checklist

M. Before Landing Checklist

N. After Landing

O. Shutdown Checklist

LANDING GEAR & BRAKES 1.5

A. Landing Gear Hydraulic or Electrical

(1) Components

(2) Normal Operation and Safety Features

(3) Emergency Systems and Operations

B. Brake System

(1) Components

(2) Parking Brake

(3) Limitations

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FUEL SYSTEM 1.5

A. Tanks

(1) Location and Type

(2) Vent System

B. Indicating System

C. Pumps

(1) High Pressure Pump Orientation

(2) Boost Pumps and Standby Pumps Orientation

(3) Normal and Crossfeed Operation

(4) Fuel Additives Cold Weather Operations

ELECTRICAL SYSTEM 1.5

A. Battery

(1) Lead Acid or Nicad Description

(2) Maintenance and Precautions

(3) Hot Battery Bus

B. Starters/Generators

(1) Description and Limitations

(2) Power Distribution and Control

(3) Cross Generator Start Assist Procedures

C. Normal Operations

D. Emergency Operations

E. External Power Procedures

F. Monitoring System

(1) Annunciator Lights

(2) Volt/Ammeter

G. Avionics Emergency Busses

H. Lighting

(1) Internal

(2) External

(3)Annunciator Panel Lighting

ENVIRONMENTAL SYSTEMS 1.0

A. Air Distribution, Heating & Ventilation Systems

(1) Heating Electrical

(2) Heating Bleed Air

(3) Heating Combustion Heaters

(4) Operation and Limitations Heating System

B. Pressurization System

(1) Safety Valve Control

(2) Outflow Valve Operation and Tests

(3) High Altitude Physiological Operation

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(4) Air-Conditioning System

(5) Oxygen System and Operation

EMERGENCY PROCEDURES 2.0

A. Loss of Power Procedures

B. Electrical System Maintenance

C. Fuel System Control and Crossfeed Procedures

D. Avionics Bus Failure

E. Flight Instrument Failure and Procedure

F. Landing Gear System Failure

G. Pressurization System Emergency and Procedures

H. Split Flap System and Checks

I. Spins

J. Alternate Static System Operations and Procedures

FLIGHT CONTROLS 1.0

A. Ailerons

B. Aileron Trim

C. Elevator and Trim (Emergency)

D. Rudder and Rudder Trim

E. Flap System and Limitations

F. Nose Wheel Steering

G. Stall Warning System

H. Limitations

FLIGHT INSTRUMENT 1.0

A. Pilot Static System

B. Vacuum/ Pressure System

C. Engine Instruments

D. Flight

ANTI-ICE/DEICE SYSTEMS 1.0

A. Anti-Ice

(1) Pilot Heat

(2) Stall/Vent Heat

(3) Ice Vanes/Lip-Ice Boots

(4) Windshield Heat

B. Deice

(1) Surface Deice System

WEIGHT & BALANCE / PERFORMANCE 2.0

A. Weight & Balance

(1) Effects of Weight & Balance on C.G.

(2) Aircraft Forms

(3) Determining Weight & Balance

(4) Sample Problems

B. Performance

(1) Explanation of Tables

(2) Interpreting Charts

(3) Practical Exercise

(4) Single Engine Performance Charts

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(5) Review FAR 23.149

Flight Training10 HOURS TOTAL

FLIGHT #1 3.0

Pre-Flight Planning

High Altitude Climb above FL 290 to FL 410 RVSM

Vref + 10 kts

Flight Director/Autopilot Procedures (Climb & Descent)

Altitude Preselect (Climb & Descent)

A. Engagement Procedures

B. Disengagement Procedures

Normal Descent

A. Power Setting

B. Flap Positions

C. Drag Devices/Spoilers

Emergency Descent

A. Turbulent Air Vmo/Mmo minus 10 kts

B. Smooth Air

Stalls

A. Slow Flight Configuration

B. Clean Configuration

C. Landing Configuration

D. Power On

E. Accelerated

Emergency Procedures

A. Electrical Failure

B. Depressurization/Emergency Descent

C. Emergency Landing Gear Extension (when applicable)

D. Engine Failure (zero thrust fir twin/simulated for single)

E. Power Off Landing

F. No Flap Take-Off and Landing

G. Short Field Take-Off and Landing

H. Balked Landing

FLIGHT #2 3.0

Flight Planning/Preflight

Normal Take-Off/Landing

IFR Climb 1,000' AGL (all flight maneuvers above 1,000' AGL for

Flight #2 will be under the hood)

Steep Turns

Slow Flight

Stalls

A. Clean Configuration

B. Landing Configuration

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C. Power-On

Descents

A. Normal

(1) Power

(2) Flaps

(3) Gear

B. Rough Air Penetration

Unusual Attitudes

A. Nose Low (pitch 10 degrees down, roll 35 degrees,

airspeed increasing)

B. Nose High (pitch 10 degrees up, roll 40 degrees,

airspeed decreasing)

Instrument Approaches

A. ILS

B. VOR

C. NDB

Instrument Approaches (flight director engaged only)

FLIGHT #3 4.0

Flight Planning/Preflight

Normal Take-Off

IFR Cross Country (actual or simulated)

A. Cross Country 300 Miles Minimum

B. Multiple Approaches at Two Different Airports

C. Pressurized Flight above 15,000' MSL on at Least

One Leg of the Cross Country

Instrument Procedures

A. Partial Panel

B. Holding

C. Minimum Equipment Flight (i.e., Single Radio, CDL,

Stand-By, Compass, etc.)

D. Simulated Electrical Failure and Decompression

Instrument Approaches (Flight Director/Autopilot Coupled)

A. ILS

B. VOR/GPS

C. NDB/GPS

D. BC

E. DME ARC

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1903 Teepee Drive ~ Tampa, Florida 33618-1521 ~ Phone: (813) 264-5583 ~ Fax: (813) 269-9818

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