Auto Flight, Chapter 22 OC A B C 2C S Actuator, Servo AFCS 6,000 C Actuator, Servo Yaw Damper 6,000 C Compensator, Mach Trim 3,000 C 2C S Computer, Aileron, AFCS 1,000 C Computer, Elevator, AFCS 1,000 C Computer, Yaw Damper 1,000 C Effective date ____________________ Page 4 of 12
OPERATIONS SPECIFICATIONS
AIRCRAFT MAINTENANCE LOCKHEED MODEL 300 (C-141A) Overhaul Inspection and Auto Flight, Chapter 22, Continued Period Check Period Control, Mach Trim OC A B C 2C Control Panel, Yaw Damper OC A B C Gyro-Rate, Single Axis 3,000 B C Gyro-Rate, Two Axis 3,000 B C Indicator, Trim, AFCS 6,000 A B C Mounts, Servo, Aileron and Elevator OC C Mounts, Servo, Yaw Damper OC C Panel, Control, AFCS 3,000 A B C Sensor, Control Wheel Force 12,000 C Transmitter, Mach Trim Compensator 12,000 C 2C Vertical Gyro, AFCS 1,000 C Communications, Chapter 23 OC A B C S ST Control, Intercommunications OC A B C S ST Requirements for additional equipment may be determined by assigned inspector.
Electrical Power, Chapter 24 OC A B C 2C S Battery OC A B C Constant Speed Drive (CSD) EO B C S Controller - Load 12,000 C Contractor 12,000 C Cooler - Oil CSD EO B C Frequency Meter 12,000 A B C Generator - Engine Driven 40 KVA EO B C Generator - APU Driven 40 KVA 6,000 B C Generator - Emergency Hydraulic
Driven OC B C 2C Indicator - Temperature CSD Oil 12,000 A B C S Loadmeter OC A B C Panel - Bus Protection OC C Panel - Generator Protection 9,000 C Panel - Protection Aux. Power 12,000 C Quick-Attach/Detach Assembly EO B C Regulator-Voltage 12,000 C Relay - "Bus Off" Indicator 12,000 C Relay - Emergency Bus Power 12,000 C 2C Relay - Essential Bus Power 12,000 C Relay - Frequency Sensitive 12,000 C 2C Relay - Isolated Bus 12,000 C 2C Relay - Isolated Bus Reverse Current 12,000 C 2C Relay - Main D-C Bus 12,000 C Tank, Oil, CSD EO B C Transformer - Rectifier Unit OC B C Sensor - Temperature CSD Oil 12,000 B C S Switch, Pressure, CSD Oil 12,000 B C Voltmeter 12,000 A B C Effective date ____________________ PAGE 5 of 12 PAGES
OPERATIONS SPECIFICATIONS
AIRCRAFT MAINTENANCE LOCKHEED MODEL 300 (C-141A) Overhaul Inspection & Period Check Period Equipment & Furnishings, Chapter 25 OC A B C ST Belt, Flight Crew Safety 6,000 A B C Belt, Passenger Type Safety 6,000 A B C Galley - Aircraft Type, Crew 12,000 A B C ST Goggles, Smoke OC A B C Harness, Aircraft Safety, Shoulder 6,000 A B C Kit, First Aid, Medical 6 months A B C Ladder Assy. - Emergency Exit OC A B C Lavatory - Crew 12,000 A B C ST Rope Assembly - Escape OC A B C Seats - Flight Station 12,000 A B C Winch - Cargo OC C Fire Protection, Chapter 26 OC A B C S ST Amplifier - Smoke Detection OC B C
Cable - Flex OC B C S ST Control Unit - Fire Warning OC A B C S Detector - Smoke OC B C Element - Sensing OC A B C S Extinguisher - Fire, Portable CO2 * A B C S Extinguisher - Fire, Dry Chemical, Portable * A B C S Generator - Fire Warning (Tone) OC A B C S Horn, APU Fire Warning SDU-1A OC A B C S Keyer, Engine Overheat OC A B C S Sphere-Charged, and Operating Head, APU and Engine * B C S Valve, Fire Extinguisher, Two-Way Check OC C S * Hydrostatic and life limits shall be entered here and shall not exceed those set forth in Part 173, Chapter I, Subtitle "B" of CFR Title 49.
Flight Controls, Chapter 27 OC A B C 2C S ST Actuator - Aileron Trim and Transmitter Assembly 6,000 B C Actuator - Aileron Artificial Feel (Cartridge) 6,000 B C Actuator - Elevator, Artificial Feel "Q" 3,000 B C Actuator - Rudder Artificial Feel (Cartridge) 6,000 B C Actuator - Flap Inboard and Outboard 6,000 A B C Actuator - Rudder Pedal, Bungee (Rudder Pedal Steering) 6,000 B C Actuator - Rudder Trim & Transmitter Assembly 6,000 B C Actuator - Spoiler Control, Cable Servo 6,000 B C Actuator - Spoiler Control Servo 6,000 B C Actuator Assembly - Stabilizer Trim (PITCH) 6,000 B C 2C Actuator Assembly - Aileron Tab Lockout 6,000 B C Actuator Assembly - Control Column Pusher 6,000 B C Effective date ____________________ Page 6 of 12
OPERATIONS SPECIFICATIONS
AIRCRAFT MAINTENANCE LOCKHEED MODEL 300 (C-141A)
Overhaul Inspection and Flight Controls - Chapter 27 Period Check Period Continued Actuator Assembly - Pitch Trim Arming 6,000 B C 2C Aileron Assembly OC A B C ST Brake Assembly - Flap Asymmetry 12,000 B C 2C Broken Cable Detector, Wing Flap OC B C 2C Carriage Assembly - Flap Inboard and Outboard 6,000 B C Chain and Cable Assembly - Flap Asymmetry OC B C 2C Computer Amplifier - Flap Asymmetry System 6,000 B C 2C Computer, Stall Warning and Prevention 3,000 B C Control Assembly - Aileron Power 6,000 B C Control Assembly - Elevator Power 6,000 B C Control Assembly - Rudder Power 6,000 B C Control Column Assembly OC B C ST Elevator Assembly OC A B C ST Flap Assembly - Inboard and Outboard OC A B C ST Gear Box Assembly - Flap Drive 6,000 B C Indicator - Aileron Trim 12,000 C Indicator - Flap Position 12,000 C Indicator - Pitch Trim 12,000 C 2C Indicator - Rudder Trim 12,000 C Indicator - Spoiler Position 6,000 C 2C Limit Switch - Flap Position 6,000 B C Regulator Assembly - Control Cable Tension (All Control Systems) OC B C ST Rudder Assembly OC A B C ST Shaker - Control Column 12,000 B C Spoiler Panels - Inboard, Outboard Upper and Lower OC A B C ST Transmitter, Angle of Attack 6,000 B C Transmitter - Flap Drive Sprocket, Position 12,000 C 2C Transmitter - Flap Position 6,000 C Transmitter - Pitch Trim Position 6,000 C 2C Transmitter - Spoiler Position 6,000 C 2C Valve, Flow Control, Pitch Trim 6,000 B C Valve, Spoiler, Shutoff, Manual OC C Fuel System, Chapter 28 OC A B C 3C S ST Actuator, Fuel Shut-Off Valve 12,000 C Control Unit, Fuel Sensing 12,000 C Indicator, Fuel Pressure 12,000 A B C Indicator, Fuel Tank Quantity 12,000 A B C 3C S Indicator, Total Fuel Quantity 12,000 A B C 3C S Pump, Fuel Boost 6,000 A B C Pump, Fuel, SPR Drain 12,000 A B C
Switch, Boost Pump Low Pressure Warning OC A B C Effective date ____________________ Page 7 of 12
OPERATIONS SPECIFICATIONS
AIRCRAFT MAINTENANCE LOCKHEED MODEL 300 (C-141A) Overhaul Inspection and Fuel System, Chapter 28 Continued Period Check Period Switch, Fuel Inlet Pressure OC A B C Tank Unit, Fuel Quantity OC A B C 3C S ST Transmitter, Fuel Pressure 12,000 A B C Valve, APU Fuel Shut-Off Supply OC A B C Valve, Fuel Level Control 12,000 A B C ST Valve, Fuel, Manual Shut-off OC C S ST Valve, Fuel Shut-Off 12,000 A B C S ST Hydraulic Power, Chapter 29 OC A B C 2C 3C 6C S ST Accumulator 12,000 A B C ST Filter-Air Vent Line OC B C 2C S Filter - Hydraulic OC B C 3C S Fuse - Hydraulic OC B C Gage - System Pressure, Direct Reading OC A B C S Indicator, Hydraulic Pressure 12,000 A B C S Pump - Suction Boost, Hydraulic Driven 6,000 B C S Pump - Hand Operated OC B C 6C Pump - Hydraulic, Engine Driven 4,000 B C S Pump - Hydraulic, Electric Driven 6,000 B C S Pump - Suction Boost, Electric Driven 6,000 B C S Pressure Transmitter 12,000 B C S Reservoir OC A B C S Snubber - Pressure Line OC C Switch - Low Pressure Warning OC C Valve - Interconnect OC C Valve - Inline Relief, Case Drain OC C Valve - Motor Operated, Shut-Off 12,000 C Valve - Pressure Relief (3560) 12,000 C Valve - Pressure Shut-Off 12,000 C S Valve - Solenoid Operated, 3-way 12,000 C Valve - Solenoid Operated, 4-way 12,000 C Valve - Drain Line Shut-Off OC C Ice and Rain Protection, Chapter 30 OC A B C S
Auto-Transformer, Windshield Heat OC C Box, Control, Windshield Heat OC C Control Box, Temperature Sensing Rain Removal 6,000 C Controller, Temperature, Empennage De-Icing System OC C Detector, Ice OC C Nozzle, Rain Removal OC C Sensor, Temperature Control, Wing Anti-Ice OC C Switch, Overheat, Wing Anti-Ice OC C Valve, Drain, Windshield Rain Removal OC C Valve, Modulating, Wing Anti-Ice 12,000 C Effective date ____________________ Page 8 of 12
OPERATIONS SPECIFICATIONS
AIRCRAFT MAINTENANCE LOCKHEED MODEL 300 (C-141A) Ice and Rain Protection, Overhaul Inspection and Chapter 30 Continued Period Check Period Valve, Pressure Regulating and Shut-Off, Rain Removal 12,000 C Valve, Pressure Relief, Rain Removal Duct OC C Valve, Shut-Off, Rain Removal 12,000 C Windshield, NESA OC A B C Instruments, Chapter 31 OC A B C S Accelerometer 12,000 A B C Accelerometer, Sensor, Flight Recorder 3,000 C Clock OC A B C Recorder, Flight 3,000 A B C Landing Gear, Chapter 32 OC A B C 6C S ST Actuator, MLG Downlock 12,000 A B C Actuator, NLG Steering 9,000 A B C Actuator, NLG Up-Down Lock 12,000 A B C Actuator, Uplock, MLG 12,000 A B C Assembly, MLG 9,000 A B C Assembly, NLG 9,000 A B C Brake Assembly, MLG OC A B C Control Box, Anti-Skid 3,000 B C Control Box, Touchdown 6,000 B C Control Panel, Landing Gear OC A B C
Cylinder, MLG Actuating 6,000 A B C Cylinder, NLG Actuating 12,000 A B C Detector, Anti-Skid 6,000 C Fuse, Hydraulic Brake 12,000 B C Horn, Warning OC A B C Indicator, Brake Pressure OC A B C Indicator, Panel, Bogie Position OC A B C Relay, MLG Up and Locked @ OC C Relay, Touchdown OC C Tire, MLG OC A B C Tire, NLG OC A B C Transmitter, Pressure, Brake 12,000 B C Uplock, MLG 12,000 A B C Valve, By Pass, Manual OC C Valve, Control, Dual Brake Anti-Skid 6,000 C Valve, Downlock Selector, MLG 12,000 B C Valve, Dual Metering Brake (Pilot) 12,000 B C Valve, Flow Regulation, MLG OC C Valve, Flow Regulation, NLG OC C Valve, Main Brake Metering 12,000 C Valve, Pressure Relief (1200) 12,000 C 6C Valve, Selector, Brake 12,000 C Valve, Selector, MLG 12,000 C Effective date ____________________ Page 9 of 12
OPERATIONS SPECIFICATIONS
AIRCRAFT MAINTENANCE LOCKHEED MODEL 300 (C-141A) Overhaul Inspection and Landing Gear, Chapter 32 Continued Period Check Period Valve, Selector, NLG 12,000 C Valve, Selector, NLG Emergency, Manual OC C Valve, Shutter, Brake OC C Wheel, MLG OC A B C Note (1) Wheel, NLG OC A B C Note (1) Note (1): Visually inspect at each tire change and perform non-destructive inspection at each 15th tire change.
Lights, Chapter 33 OC A B C ST Control - Master Caution, Annunciator OC A B C ST Light, Anti-Collision 3,000 A B C ST Light, Emergency Exit 6,000 A B C ST Light, Landing 3,000 A B C ST
Lights, Navigation OC A B C ST Navigation, Chapter 34 OC A B C 2C S Altimeter - Pressure 6,000 A B C 2C S Amplifier - Slaving, Gyro Compass 3,000 B C S Amplifier - Airspeed - Mach Number 3,000 B C S Amplifier - Altitude - Vertical Speed 3,000 B C S Amplifier - Servo Gyro Compass 3,000 B C S Amplifier - Audible Warning OC B C S Compass - Magnetic, Pilots Standby OC B C S Computer - Central Air Data 1,000 B C S Computer - Flight Director 3,000 B C S Controller - Gyro Compass 3,000 A B C S Flux Valve and Compensator 3,000 B C S Generator - Audible Warning OC B C S Gyro-Directional 2,000 B C S Gyro-Rate Switching 3,000 B C S Gyro-Vertical 2,000 B C S Indicator - Attitude Director 2,000 A B C S Indicator - Airspeed, Mach Number 3,000 A B C 2C S Indicator - Airspeed, Standby 6,000 A B C 2C S Indicator - Altitude, Vertical Speed 3,000 A B C S Indicator - BDHI 2,000 A B C S Indicator - Horizontal Situation 2,000 A B C S Indicator - Total Air Temperature OC A B C S Keyer, Audible Warning (Underspoiler Speed Warning) OC B C S Power Supply - Gyro Compass 3,000 B C S Probe - Total Air Temperature OC A B C S Rack - Gyro Compass OC B C S Sensor - Rate of Turn 2,000 B C S Tube - Pitot Static OC A B C 2C S Requirements for additional equipment may be determined by assigned inspector.
Effective date ____________________ PAGE 10 of 12 PAGES
OPERATIONS SPECIFICATIONS
AIRCRAFT MAINTENANCE LOCKHEED MODEL 300 (C-141A) Overhaul Inspection & Oxygen Chapter 35 Period Check Period Oxygen OC A B C S Cylinder Assembly * A B C S Pressure Reducer 5 years A B C S
Gage - Remote Pressure 6,000 A B C S Mask, Oxygen OC A B C Oxygen Cylinder - Portable * A B C S Regulator, Oxygen 6,000 A B C S * Hydrostatic and life limits shall be entered here and shall not exceed those set forth in Part 173, Chapter I, Subtitle "B" of CFR Title 49.
Pneumatic System, Chapter 36 OC A B C 2C Indicator-Pressure, Bleed Air Manifold 12,000 A B C 2C Transmitter-Pressure, Bleed Air Manifold 12,000 C 2C Valve - Shut-Off, Bleed Air 6,000 C 2C Auxiliary Power, Chapter 49 OC A B C S Auxiliary Power Plant ** E.T.I. 1250 A B C S or Note 1 5,000 Starts Tank, Oil, APU OC A B C ** Note 1: Whichever occurs first.
Doors, Chapter 52 OC A B C 2C 6C S ST Actuator, Cargo Ramp 12,000 A B C Actuator, Pedal Door and Ramp Lock 12,000 A B C Actuator, Pressure Door 12,000 A B C Actuator, Pressure Door Down Lock 12,000 A B C Actuator, Pressure Door Up Lock 12,000 A B C Central Gear Box Assy., Pedal Door Actuator 12,000 A B C Jack Screw Assembly, Pedal Door Actuator 12,000 A B C Valve, Flow Regulation 12,000 B C Valve, Pressure Door, Selector 12,000 B C Valve, Pressure Reducing, Cargo Ramp 12,000 B C Valve, Selector, Door Locks 12,000 B C Valve, Shuttle, Ramp Lock & Pressure Door 12,000 B C Fuselage, Chapter 53 Structural inspection Nacelles, Chapter 54 requirements are as specified Stabilizers, Chapter 55 in Parts I, III, and IV of Windows, Chapter 56 Lockheed Service Publication Wings, Chapter 57 SMP No. 231 dated June 1, 1967.
Power Plant, Chapter 71 OC A B C EC S Mount, Engine EC B C EC S
Cowling OC A B C EC Firewall OC B C EC Effective date ____________________ Page 11 of 12
OPERATIONS SPECIFICATIONS
AIRCRAFT MAINTENANCE LOCKHEED MODEL 300 (C-141A) Overhaul Inspection and Period Check Period Engine - Turbine, Chapter 72 OC A B C EO S Engine, Turbo Fan P&W TF-33-P7/ JT3D-5A 4,000 A B C EO S Note I Note I: Major Inspection at 2,000 hours.
Engine Fuel and Control, Chapter 73 A B C EO Actuator, Fuel Shut-Off EO B C Control, Fuel EO B C Filter Assembly, Fuel De-Icing OC B C EO Heater, Fuel De-Icing EO B C Indicator, Engine Fuel Inlet Temperature 12,000 A B C Indicator, Fuel Flow 2,000 A B C Pump, Fuel EO B C Switch, Differential Pressure OC B C EO/FC Switch, Inlet Pressure OC B C EO/FC Transmitter, Rate of Flow, Fuel 2 EO B C Valve Assembly, Fuel Pressurization and Dump EO B C Ignition, Chapter 74 A B C EO Cable, Exciter, Electrical Power EO B C Cable, Special Purpose EO B C Exciter, Ignition EO B C Plug, Igniter OC C EO Engine Air, Chapter 75 A B C EO Actuator, Compressor Bleed EO B C Regulator, Anti-Icing Air EO B C Regulator, Duct Seal Pressure OC B C EO/FC Regulator, Pressure, CSD Oil Tank OC B C EO/FC Valve and Actuator Assembly, Anti-Icing Air EO B C Valve Assembly, Breather Pressurizing EO B C
Valve, Bleed Air Shut-Off EO B C Valve, Check, Duct Seal Pressure OC B C EO/FC Valve, Compressor Bleed EO B C Valve and Control Assembly, Compressor Bleed EO B C Valve, Nacelle Preheat OC B C EO/FC Valve, Nose Cowl Anti-Ice OC B C EO/FC Valve, Shut-Off, Compartment Cooling (Zone I) OC B C EO/FC Valve, Shut-Off, Compartment Cooling (Zone II) OC B C EO/FC Engine Controls, Chapter 76 A B C EC ST Power Lever System, Cables, Pulley, Rods and Linkages OC B C EC ST Tension Regulator, Throttle OC EC Effective date ____________________ Page 12 of 12
OPERATIONS SPECIFICATIONS
AIRCRAFT MAINTENANCE LOCKHEED MODEL 300 (C-141A) Overhaul Inspection and Period Check Period Engine Indicating, Chapter 77 A B C 2C S Converter, Engine Instrument 3,000 B C Generator, Tachometer EO B C Indicator, Engine Pressure Ratio 2,000 A B C 2C Indicator, Engine Vibration 6,000 A B C Indicator, Exhaust Gas Temperature 2,000 A B C 2C Indicator, Tachometer 2,000 A B C Pick-Up, Engine Vibration EO C Transmitter, Pressure Ratio EO C 2C Exhaust, Chapter 78 A B C EO S Actuator, Thrust Reverser 2EO A B C EO Control, Thrust Reverser 2EO B C EO Door, Thrust Reverser OC A B C EO Filter, Thrust Reverser OC B C EO Nozzle Assembly, Primary Exhaust EO A B C Pump, Thrust Reverser 2EO B C EO Telescopic Unit, Thrust Reverser OC A B C EO Valve, Flow Regulator, Thrust Reverser OC B C EO Valve, Relief OC B C EO/FC Engine Oil, Chapter 79 A B C EO S
Bulb, Temperature OC C EO Cooler Assembly, Fuel Oil Coolant EO B C Heat Exchanger, Air-Oil EO B C Indicator, Engine Oil Temperature 6,000 A B C Indicator, Oil Pressure 6,000 A B C Pump Assembly, Oil EO C Strainer Assembly, Oil, Main OC C EO Switch, Low Oil Quantity OC C EO Switch, Oil Pressure OC C EO Tank Assy., Lubricating Oil EO B C Transmitter, Oil Pressure EO B C Valve, Oil Pressure Relief EO C Starting, Chapter 80 OC A B C EO Starter, Engine EO B C Valve, Pressure Regulating EO B C Effective date ____________________ ---------------------------------------------------------------- ---------------------------------------------------------------- FIGURE 31. OPERATIONS SPECIFICATIONS AIRCRAFT MAINTENANCE
- LOCKHEED JETSTAR - MODEL 1329 Form Approved.
UNITED STATES OF AMERICA Budget Bureau FEDERAL AVIATION AGENCY No. 04-R075.
WASHINGTON Page 1 of 11
OPERATIONS SPECIFICATIONS
AIRCRAFT MAINTENANCE - GENERAL LOCKHEED JETSTAR - MODEL 1329 Aircraft shall not be utilized in air carrier or commercial operations unless:
a. The aircraft and its component parts, accessories and appliances are maintained in an airworthy condition in accordance with the operator's maintenance manual. Such manual shall at least include the methods, procedures and limitations contained in the Lockheed JetStar Handbook of Operating and Maintenance Instructions.
b. The aircraft and its component parts, accessories, and appliances are maintained in an airworthy condition in accordance with the maximum time limits hereinafter set forth for the accomplishment of the overhaul, periodic inspection, and routine checks of the aircraft and its component parts, accessories, and appliances.