L/R 2E ---------------------------------------------------------------- ---------------------------------------------------------------- FIGURE 22. OPERATIONS SPECIFICATIONS AIRCRAFT MAINTENANCE
- DOUGLAS DC-8/F DC-8 INSPECTION AND MAINTENANCE PROGRAM [FIGURE NOT INCLUDED] ---------------------------------------------------------------- ---------------------------------------------------------------- FIGURE 23. OPERATIONS SPECIFICATIONS AIRCRAFT MAINTENANCE - LOCKHEED MODEL 382 Form Approved.
UNITED STATES OF AMERICA Budget Bureau FEDERAL AVIATION AGENCY No. 04-R075.
WASHINGTON PART D Page 1 of 12 Pages
OPERATIONS SPECIFICATIONS
AIRCRAFT MAINTENANCE LOCKHEED MODEL SERIES 382, 382B, D, E, F & G
INSPECTION/CHECK REQUIREMENTS The basic requirements for performing these inspections and checks are as specified in PART I of Lockheed Service Manual Publication SMP 515, revised June 1, 1970, and subsequent revisions thereto.
"A" INSPECTION/CHECK To be accomplished each service calendar day.
"B" INSPECTION/CHECK To be accomplished at intervals not exceeding 200 hours time in service after the preceding "B" or "C" inspection/check period.
"C" INSPECTION/CHECK To be accomplished at intervals not exceeding 600 hours time in service after the preceding "C" inspection/check period.
AIRFRAME STRUCTURAL INSPECTIONS The frequency and procedure for performing these inspections will
be accomplished as specified in PART I and PART III of Lockheed Service Manual Publication SMP 515, revised June 1, 1970, and subsequent thereto.
"SP" SPECIAL INSPECTIONS The frequency and procedure for performing these inspections will be accomplished as specified in PART IV of Lockheed Service Publication SMP 515, revised June 1, 1970, and subsequent revisions thereto.
Effective date _____________________ Page 2 of 12 Pages
OPERATIONS SPECIFICATIONS
AIRCRAFT MAINTENANCE LOCKHEED MODEL SERIES 382, 382B, D, E, F & G Overhaul Inspection & Period Check Period Air Conditioning, Chapter 21 OC A B C SP Condenser, Water Separator (Cargo Compt.) OC C Condenser, Water Separator (Flt.
Sta.) OC C Control Box, Temp. (Cargo Compt.) OC C Control Box, Temp. (Flt. Sta.) OC C Controller, Cabin Air Pressure 3,400 C Fan, Recirculation 6,300 C Heat Exchanger (Cargo Compt.) OC C Heat Exchanger (Flt. Sta.) OC C Indicator, Cabin Altitude 12,600 C Indicator, Cabin Rate of Climb 12,600 C Indicator, Differential Press. 12,600 C Separator, Water (Cargo Compt.) OC C Separator, Water (Flt. Sta.) OC C Switch, Differential Pressure 1,800 C Switch, Emergency Depressurization OC C Thermostat, Cabin Air Temp. 6,300 C Thermostat, Duct Anticipator (Cargo Compt.) OC C Thermostat, Duct Anticipator (Flt. Sta.) OC C Turbine, Cooling (Cargo Compt.) 1,800 C Turbine, Cooling (Flt. Sta.) 1,800 C Valve, Aux. Vent (Cargo Compt.) 12,600 C Valve, Aux. Vent (Flt. Sta.) 12,600 C Valve, Cargo Floor Heat 12,600 C
Valve, Cargo Floor Heat Diverter 12,600 C Valve, Flow Cont. & Shut-Off (Cargo Compt.) 12,600 C Valve, Flow Cont. & Shut-Off (Flt. Sta.) 12,600 C Valve, Outflow 6,300 C Valve, Safety OC C Valve, Temp. Cont. (Cargo Compt.
Dual Butterfly) 12,600 C Valve, Temp. Cont. (Flt. Sta. Dual Butterfly) 12,600 C Auto Flight, Chapter 22 OC A B C 2C Amplifier, Electronic Control, Approach and Nav. 3,400 C Amplifier, Electronic Control, Auto Pilot (Main) 3,400 C Control, Engage & Approach 6,300 C Control, Gyro, Roll & Pitch 3,400 C Control, Servo 3,400 C 2C Control, Trim Tab Adapter 6,300 C Controller, Flight 6,300 C Drum and Bracket Assembly OC C Motor and Drive Assembly 6,300 C Relay, Servo Engage 6,300 C Effective date _____________________ Page 3 of 12 Pages
OPERATIONS SPECIFICATIONS
AIRCRAFT MAINTENANCE LOCKHEED MODEL SERIES 382, 382B, D, E, F & G Overhaul Inspection & Period Check Period Communications, Chapter 23 OC A B C SP May be determined by assigned inspector.
Electrical Power, Chapter 24 OC A B C Battery OC A B C Control Panel, AC 3,400 C Frequency Meter OC C Generator, 20 KVA, ATM Driven 12,600 C Generator, 40 KVA, Engine Driven EO B C Indicator, Loadmeter (AC) OC C
Indicator, Loadmeter (DC) OC C Inverter, 250 VA 6,300 C Inverter, 2500 VA 6,300 C Regulator, Voltage, 20 KVA Generator 12,600 C Regulator, Voltage, 40 KVA Generator 3,400 C Relay, Battery OC C Relay, Bus 6,300 C Relay, Bus Off (AC) OC C Relay, Bus Off (DC) OC C Relay, External Power, AC OC C Relay, External Power, DC OC C Relay, Frequency Sensitive OC C Relay, Generator & Bus Tie (AC) 12,600 C Relay, Reverse Current 9,450 C Transformer, Instrument OC C Transformer, Instrument (Engine) OC C Transformer, Rectifier OC C Voltmeter, AC OC C Voltmeter, DC OC C Equipment & Furnishings, Chapter 25 OC A B C Kit, First Aid OC A B C Seat Belts and Harnesses OC A B C Seat, Flight Station, FAA Observer OC A B C Seats, Flight Station OC A B C Effective date _____________________ PAGE 4 of 12 PAGES
OPERATIONS SPECIFICATIONS
AIRCRAFT MAINTENANCE LOCKHEED MODEL SERIES 382B, D, E, & F Overhaul Inspection & Period Check Period Fire Protection, Chapter 26 OC A B C EC SP Amplifier, Control Unit OC C Amplifier, Control, Smoke Detection OC C Control Panel, Assembly OC C Control Relay (Unit) OC C Extinguisher, Portable * B C Flasher, Overheat OC C Inert Element, Fire Detection OC C Smoke Detector OC C Sensing Element, Fire Detection OC C EC
Sphere Assy., (Agent Container) * B C Squib, Fire Extinguisher OC C SP (Note 1) Valve, Directional OC C Note 1: Replace at 5 years from date of manufacture.
* 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 SP Actuator, Rudder Trim Tab 6,300 C Actuator, Aileron Trim Tab 6,300 C Actuator, Elevator Trim Tab 3,400 C Aileron & Trim Tab Assembly OC A B C Booster Assy. Rudder 8,000 B C Booster Assy. Elevator 8,000 B C Booster Assy. Aileron 8,000 B C Brake, Flap Asymmetry 12,600 C Control Column Assembly 12,600 B C Elevator & Trim Tab Assy. OC A B C Gear Box Assy., Flap Drive 12,600 C Gear Box, Wing Flap Jackscrew 6,300 B C Indicator, Flap Position 12,600 C Indicator, Aileron Trim Tab Position 12,600 C Indicator, Elevator Trim Tab Position 12,600 C Indicator, Rudder Trim Tab Position 12,600 C Motor, Wing Flap Drive 6,300 B C Relay, Trim Tab Control 12,600 C Effective date _____________________ Page 5 of 12 Pages
OPERATIONS SPECIFICATIONS
AIRCRAFT MAINTENANCE LOCKHEED MODEL SERIES 382, 382B, D, E, F & G Overhaul Inspection & Period Check Period Flight Controls, Chapter 27 continued Rudder Pedal Assembly 12,600 B C Rudder & Trim Tab Assy. OC B C Screw and Yoke Assy., Flap
Jackscrew OC B C SP Screwjack, Elevator Trim Tab 6,300 C Shaft, Flexible, Elevator Trim Tab 6,300 C Shaft, Flexible, Elevator Trim Tab Actuator 6,300 C Switch, Flap Asymmetry 12,600 C Switch, Flap Cable Failure Detection OC C (Note
1) Tension Regulator, Cable OC C Transmitter, Flap Position 12,600 C Valve, Flap Brake Control 12,600 C Valve, Flap Selector 12,600 C Valve, Pressure Reducer OC C Valve, Rudder System Relief OC C Wing Flap Assembly OC A B C Note 1: Perform operational check at 6300 hours.
Fuel System, Chapter 28 OC A B C SP Indicator, Fuel Quantity 12,600 C Indicator, Manifold Fuel Pressure 12,600 C Power Supply OC C Pump, Drain (SPR Manifold) 12,600 C Pump, Fuel Boost 6,300 C Pump, Fuel Jettison 12,600 C Relay, Fuel Quantity OC C Switch, Fuel Press. Warning OC C Tank Unit, Fuel Quantity OC C Transmitter, Manifold Fuel Pressure 12,600 C Valve, 1-inch Motor Operated Fuel Shut Off 12,600 C Valve, Dual Level Control 12,600 C Valve, Fuel Dump and Shut-Off 12,600 C Valve, Fuel Shut-Off 12,600 C Valve, Fuel Tank Vent 12,600 C Effective date _____________________ Page 6 of 12 Pages
OPERATIONS SPECIFICATIONS
AIRCRAFT MAINTENANCE LOCKHEED MODEL SERIES 382, 382B, D, E, F & G Overhaul Inspection &
Period Check Period Hydraulic Power, Chapter 29 OC A B C SP Accumulator 12,600 B C Filter Assy., High Pressure OC C Filter Assy., Low Pressure OC C Filter, Reservoir Vent Line OC C Heat Exchanger OC C Indicator, Remote Pressure 12,600 C Pump, Auxiliary Elec. Driven 6,300 B C Pump, Engine Driven EO B C Pump, Hand OC C Pump, Suction Boost 3,400 B C Reservoir OC A B C Switch, Low Pressure OC C Transmitter, Pressure 12,600 C Valve, Check OC C Valve, Firewall Shut-Off 6,300 C Valve, Pressure Shut-Off 12,600 C Valve, Relief 12,600 C Valve, Relief, In-Line OC C Valve, 9 Ported Manual 6,300 C Ice & Rain Protection, Chapter 30 OC A B C SP Ammeter, Propeller Anti-Icing OC C Boot, Propeller Blade Anti-Icing OC B C Control Box, NESA 12,600 C Converter, Windshield Wiper 12,600 B C Detector, Ice OC C Duct, Bleed Air OC C Duct, Wing & Empennage OC C Ejector, Wing & Empennage Anti-Icing OC C Indicator, Temperature, Anti-Icing OC C Interpreter, Ice Detector OC C Light Assy., Ice Warning OC C Motor, Windshield Wiper 12,600 B C Relay, Windshield, Anti-Icing 12,600 C Switch, Thermal Inlet Duct Anti-Ice OC C Temperature Bulb OC C Thermostat, Overheat Warning OC C Timer, Propeller De-Icing 12,600 C Effective date _____________________
Page 7 of 12 Pages
OPERATIONS SPECIFICATIONS
AIRCRAFT MAINTENANCE LOCKHEED MODEL SERIES 382, 382B, D, E, F & G Overhaul Inspection & Period Check Period Ice & Rain Protection, Chapter 30 continued Transformer, NESA OC C Valve, Pressure Regulator 12,600 C Valve, Pressure Relief (Radome) OC C Valve, Wing & Empennage Anti-Icing OC C Window, NESA OC B C Instruments, Chapter 31 OC A B C Accelerometer OC C Accelerometer, Vertical (Flight Recorder) 3,400 C Amplifier, Servo, Flight Recorder 3,400 C Clock OC C Control, Flight Recorder OC C Flight Recorder 3,400 C Landing Gear, Chapter 32 OC A B C SP Accumulator, Brake 12,600 B C SP Ball Screw Assy., MLG 3,400 B C Brake Assembly OC B C Control Box, Anti-Skid 6,300 C Cylinder, NLG Steering 12,600 A B C Cylinder, NLG Up-Lock 12,600 A B C Cylinder, NLG Drag Strut Actuating 12,600 A B C Detector, Anti-Skid 6,300 A B C (Note
1) Fuse, Brake, Hydraulic OC C Gear Box Assy., Manual Extension & Retraction MLG 6,300 C Gear Box Assy., Extension & Retraction, MLG (90 degrees) 12,600 C Indicator, Position OC C Limit Switch OC C Linkages, Landing Gear Door Actuating OC A B C Motor, Hydraulic, MLG Actuating 6,300 C
Relay, Touchdown OC C Strut, MLG, Oleo-pneumatic 12,600 A B C Strut, NLG, Oleo-pneumatic 12,600 A B C Tires, MLG OC A B C Tires, NLG OC A B C Torque Strut, MLG 12,600 A B C Valve, Brake Anti-Skid 6,300 C Valve, Control By-Pass, LG 12,600 C Effective date _____________________ PAGE 8 of 12 PAGES
OPERATIONS SPECIFICATIONS
AIRCRAFT MAINTENANCE LOCKHEED MODEL SERIES 382, 382B, D, E, F & G Overhaul Inspection & Period Check Period Landing Gear, Chapter 32 (continued) Valve, Dual Brake Control 6,300 C Valve, NLG Emerg. Extension 12,600 A B C Valve, NLG Steering Control 6,300 C Valve, Selector Emer. Brake 12,600 C Valve, Selector, Landing Gear 12,600 C Valve, Shuttle OC C Valve, Shuttle, NLG OC C Wheel, Main Landing Gear OC A B C (Note
2) Wheel, Nose Landing Gear OC A B C (Note
2) Note 1: Inspect at each wheel removal.
Note 2: Visually inspect at each tire change; perform non-destructive inspection each 5th tire change.
Lights, Chapter 33 OC A B C Light Assy., Anti-Collision OC B C Light Assy., Dome OC B C Light Assy., Instrument Edge OC B C Light Assy., Instrument Panel Floor OC B C Light Assy., Leading Edge Scanning OC B C Light Assy., Navigation OC B C Light Assy., Ramp Flood OC B C Light Assy., Retractable, Landing OC B C
Light Assy., Thunderstorm OC B C Rheostat OC B C Transformer, Instr. Lights OC C Navigation, Chapter 34 OC A B C May be determined by assigned inspector.
Oxygen, Chapter 35 OC A B C SP Cylinder Assy., Oxygen * A B C Cylinder, Portable Oxygen * A B C Mask, Crew OC A B C Regulator Assy., (Fixed System) 6,300 A B C Regulator Assy., Portable System 6,300 C * 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.
Effective date _____________________ Page 9 of 12 Pages
OPERATIONS SPECIFICATIONS
AIRCRAFT MAINTENANCE LOCKHEED MODEL SERIES 382, 382B, D, E, F & G Overhaul Inspection & Period Check Period Pneumatic, Chapter 36 OC A B C SP Indicator, Bleed Air Pressure OC C (Note 1) Valve, Bleed Air Check OC C Valve, Bleed Air Divider 12,600 C Valve, Bleed Air Shut-Off 12,600 C Valve, Wing Isolation 12,600 C Note 1: Bench Service to insure proper operation and calibration at 12,600 flight hours.
Auxiliary Power, Chapter 49 OC A B C SP Actuator, G.T.C. Door 12,600 C Air Turbine Motor ETI 800* B C Compressor, Gas Turbine ETI 1250* B C SP or 5,000 Starts
Fan, ATM 6,300 C Indicator, Elapsed Time OC C Valve, GTC Oil Shut-Off OC C * Airframe equivalent hours of 6,300 may be used.
Door System, Chapter 52 OC A B C Cylinder, Aft Cargo Door 12,600 A B C Cylinder, Ramp Actuating 9,450 C Cylinder, Ramp Uplock 12,600 C Uplock, Aft Cargo Door 12,600 C Valve, Ramp Manifold Control 12,600 C Fuselage, Chapter 53 See Structural Inspection Program Nacelles, Chapter 54 See Structural Inspection Program Stabilizers, Chapter 55 See Structural Inspection Program Windows, Chapter 56 See Structural Inspection Program Wings, Chapter 57 See Structural Inspection Program Effective date _____________________ Page 10 of 12 Pages
OPERATIONS SPECIFICATIONS
AIRCRAFT MAINTENANCE LOCKHEED MODEL SERIES 382, 382B, D, E, F & G Overhaul Inspection & Period Check Period Propeller, Chapter 61 OC A B C SP Hub, Dome & Blade Assy., Propeller 4,000 A B C SP (Note 1) Pump Housing, Propeller 4,000 A B C SP (Note 2) Relay, Prop., Feathering 12,600 C Spinner, Propeller OC A B C Synchrophaser OC C Trim Control, Manual Phase OC C Valve Housing, Propeller 4,000* A B C SP Note 1: This includes the Spinner Bulkhead.
Note 2: This includes the NTS Bracket and Anti-Rotation (Drive) Lug.
* The overhaul period for valve housings serial C8175 and up or having a part number with the suffix P4 or having
Hamilton-Standard Service Bulletin No. 36 incorporated is 4,000 hours. For other valve housings the overhaul period is 2,400 hours.
Power Plant, Chapter 71 OC A B C EC SP Cowling OC A B C EC Engine Dynafocal Mounts OC C EC Fire Seals OC C EC QEC Cone Mounts OC C EC QEC Structure OC C EC Engine, Turboprop, Chapter 72 OC A B C SP Engine Compressor Section 5,000 A B C (Note 2) Reduction Gear Assy. EO B C Torquemeter, Assy. EO B C Turbine Unit 501-D22 EO A B C (Note 1) Turbine Unit 501-D22A EO A B C (Note 3) Note 1: At intervals not to exceed 2,000 hours turbine operating time, perform turbine maintenance inspection in accordance with Allison Publication 4RC-2 and replace life limited parts on turbines not modified in accordance with Allison Commercial Engine Bulletin No.
72-1019.
Note 2: Operators of Allison D-22 engines having an approved engine overhaul period greater than 5,000 hours may have the same approved time for D-22A engines.
Effective date _____________________ Page 11 of 12 Pages
OPERATIONS SPECIFICATIONS
AIRCRAFT MAINTENANCE LOCKHEED MODEL SERIES 382, 382B, D, E, F & G Overhaul Inspection & Period Check Period Engine, Turboprop, Chapter 72 continued OC A B C SP Note 3: At an interval not to exceed 3,000 hours turbine section operating time, perform one hot section inspection in accordance with Allison Publication 4RC-2, Chapter