* 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 _____________________ ---------------------------------------------------------------- ---------------------------------------------------------------- FIGURE 19. OPERATIONS SPECIFICATIONS AIRCRAFT MAINTENANCE
- LOCKHEED L-188 A & C Form Approved.
UNITED STATES OF AMERICA Budget Bureau FEDERAL AVIATION AGENCY No. 04-R075.
WASHINGTON
OPERATIONS SPECIFICATIONS PART D Page 1 of 5 pages
OPERATIONS SPECIFICATIONS
AIRCRAFT MAINTENANCE LOCKHEED L-188 A & C Overhaul Inspection & Period Check Period Air Conditioning System, Chapter 21 12,000 Air Cycle By-Pass Valve 4,000 Air Cycle Cooling Air Exit Door Actuator 4,000 Air Cycle Heat Exchange O.C.
Air Cycle Cooling Turbine 4,000 Altimeter, Cabin 7,000 Cabin Air Compressor 2,000 Cabin Air Flow Control Valve 2,000 Cabin Pressure Reg. Outflow Valve 5,000 BC 2500 Cabin Pressure Safety Valve 12,000 BC 4000 Cabin Air Duct Shut-Off Valve O.C.
Cabin Air Duct Check Valve O.C.
Cabin Air Pressure Outflow Valve Control 3,500 Cabin Air Pressure Outflow Valve Control Filter 1,500 Cabin Freon Evaporator O.C.
Cabin Aux. Vent Inlet Valve & System O.C.
Cabin Air Warmup Valve Actuator O.C.
Cabin Air Filter O.C.
Cabin Duct Heater O.C.
Cabin Recirculating Fan 4,000 Cooling Air Exit Door Actuator (tunnel) 4,000 Cooling Air Inlet Door Actuator (tunnel) 4,000 Flight Station Recirculating Fan 4,000 Flight Station Freon Evaporator O.C.
Flight Station Duct Heater O.C.
Flight Station Aux. Vent Inlet Valve O.C.
Flight Station Air Filter O.C.
Freon Suction Pressure Throttling Valve 4,000 Freon Condenser Fan 4,000 Freon Condenser O.C.
Freon Compressor 3,000 Lavatory Exhaust Fan O.C.
Manual Control Valve 5,000 Negative Pressure Relief Valve O.C.
Radio Rack Exhaust Fan 1,400 Rate of Climb 7,000 Radiant Heating Panel (floor and wall) O.C.
Radiant Heating Panel (cargo compt.) O.C.
Surge Control Valve 2,000 Temperature Control Box 2,500 Effective date April 1, 1964 PAGE 2 of 5 PAGES
OPERATIONS SPECIFICATIONS
AIRCRAFT MAINTENANCE LOCKHEED L-188 A & C Overhaul Inspection & Period Check Period Auto-Pilot System, Chapter 22 May be determined by the assigned inspector.
Communications System, Chapter 23 May be determined by the assigned inspector.
Electrical Power, Chapter 24 OC Battery OC Flight Station Electrical &
Instrument Panels OC Generator, AC 2,000 Generator Control and Protection Components 2,000 Inverter 2,000 Main & Flight Station Distribution Centers, including Wiring, Terminals, Relays, Circuit Breakers, Etc. OC Power Contactors and Reverse Current Relays 2,000 Secondary Electrical Centers, including Wiring, Terminals, Relays, Circuit Breakers, Etc. OC Transformer Rectifiers 2,000 Voltage Regulators 2,000 Equipment & Furnishings, Chapter 25 May be determined by the assigned inspector.
Fire Protection, Chapter 26 OC Cylinder * Discharge Valve Cartridges 3 years Transfer Valve 8,000 Valve, Drain 3,500 Flight Controls, Chapter 27 OC Aileron Trim Tab Control Unit 12,000 Aileron Trim Tab Actuator Unit 12,000 Aileron Push-Pull Tubes, Bellcranks Fittings, etc. 8,000 Asymmetry Detector Shut-Off Valve 6,000 Asymmetry Detector Actuated Flap Actuator Brake 12,000 * 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 3 of 5 pages
OPERATIONS SPECIFICATIONS
AIRCRAFT MAINTENANCE LOCKHEED L-188 A & C Overhaul Inspection & Period Check Period
Flight Controls, Chapter 27, continued Booster Actuators 8,000 Booster Valve Cluster 8,000 Booster Frame Disconnect Mechanism 8,000 Control Column 12,000 Control Cables, Pulleys, Fairleads, etc. O.C.
Elevator Trim Tab Control Unit 12,000 Elevator Trim Tab Actuator Unit 12,000 Elevator Push-Pull and Torque Tube 8,000 Flap Control System 5,000 Hydraulic Load Sensors 8,000 Rudder Pedals 12,000 Rudder Trim Tab Control Unit 12,000 Rudder Trim Tab Actuator & Linkage 12,000 Rudder Push-Pull and Torque Tube Installation 8,000 Wing Flap Main Drive Hydraulic Motor 12,000 Wing Flap Main Drive Gear Box 12,000 Wing Flap Actuators, Linkages, Tracks and Carriages @ 4,000 Fuel System, Chapter 28 Boost Pump, Main 5,000 Boost Pump, Scavange 5,000 Fuel Valves (Crossfeed-Elect.; Shut- Off-Manual) 8,000 Fuel Dump Valves 8,000 Fueling Valve 8,000 Fuel Quantity Tank Units O.C.
Fuel Quantity Indicators 5,000 Fuel Pressure Warning System O.C.
Misc. Valves, Pilot & Vent. 10,000 Overflow Valve 8,000 Transmitter, Fuel Crossfeed 8,000 Hydraulic System, Chapter 29 O.C.
Aux. Pump (DC) 4,000 Hydraulic Motor Pump (AC) 2,000 Heat Exchanger O.C.
Relief Valve, Main System 12,000 Reservoir 12,000 Pressure Switches O.C.
Effective date April 1, 1964 PAGE 4 of 5 PAGES
OPERATIONS SPECIFICATIONS
AIRCRAFT MAINTENANCE LOCKHEED L-188 A & C Overhaul Inspection & Period Check Period Ice & Rain Protection, Chapter 30 OC Airfoil Temperature Sensor Amplifier 4,000 Bleed Air Shut-Off Valve 3,000 Control Unit, Temperature 8,000 Fuselage Isolation Valve 8,000 Indicator, Airfoil Temperature 8,000 Indicator, Bleed Air Manifold 8,000 Leakage Detector Valve 3,000 Modulating Control Valves 8,000 Switch Temperature Selector 8,000 Transmitter, Bleed Air Manifold 8,000 Thermostats OC Universals OC Firewall Bleed Air Shut-Off Valve 3,500 Timer, Prop De-Ice 5,000 Windshield De-Fog 8,000 Windshield Wiper Accumulator 12,000 Windshield Wiper Control Unit 4,000 Window Units 12,000 Landing Gear, Chapter 32 Brake Accumulators 12,000 Brake System 12,000 Gear Up-and-Down Locks 10,000 Lockout Cylinder 12,000 Main and Nose Wheels OC Main Gear 12,000 Main Gear Door Actuating Cylinder 10,000 Nose Gear 12,000 Nose Gear Door Actuating Cylinder 10,000 Nose Wheel Steering 12,000 Valve, Shuttle 12,000 Valve, Priority 12,000 Lighting, Chapter 33 May be determined by assigned inspector.
Navigation, Chapter 34 May be determined by assigned inspector.
Oxygen System, Chapter 35 Oxygen Bottle *
* 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 5 of 5 pages
OPERATIONS SPECIFICATIONS
AIRCRAFT MAINTENANCE LOCKHEED L-188 A & C Overhaul Inspection & Period Check Period Doors, Chapter 52 Actuators 4,000 Cylinder, Stair Actuating 4,000 Doors and Emergency Exits 12,000 Valve, Stair Selector 8,000 Fuselage, Chapter 53 Crew Seats and Attachments 8,000 Exterior Covering 12,000 Floor Support Members 12,000 Interior O.C.
Nose Gear Well Area 12,000 Passenger Seats and Attachments 12,000 Structure Around Windows 12,000 Nacelles, Chapter 54 Attachments 12,000 4,000 Main Gear Support Structure 12,000 Skin and Structure Beneath Tail Pipe Shroud 12,000 4,000 Tail Pipe and Shroud 12,000 2,000 Stabilizers, Chapter 55 Attachments and Joints 6,000 Exterior Covering 6,000 Elevator and Tabs 12,000 * 500 Interior Structure 6,000 ** 2,000 Rudder and Tabs 12,000 Vertical, Horizontal and Installation 6,000 Windows, Chapter 56 Cabin 12,000 Windshield Structure 12,000
Wings, Chapter 57 Ailerons and Tabs 12,000 Attach Joints 12,000 Center Wing Section 8,000 Flaps, Structure 12,000 Interior Structure 12,000 Wing to Fuselage Fillets 8,000 * Counter weight bracket Effective date April 1, 1964 ** Inspection Rear Spar Web ---------------------------------------------------------------- ---------------------------------------------------------------- FIGURE 20. OPERATIONS SPECIFICATIONS AIRCRAFT MAINTENANCE
- ALLISON 501-D13 ENGINE AEROPRODUCTS PROPELLER Form Approved.
UNITED STATES OF AMERICA Budget Bureau FEDERAL AVIATION AGENCY No. 04-R075.
WASHINGTON
OPERATIONS SPECIFICATIONS
AIRCRAFT MAINTENANCE
ENGINE MAKE - ALLISON PROPELLER MAKE - AEROPRODUCTS ENGINE MODEL - 501-D13 PROPELLER MODEL - A6441FN606 Overhaul Inspection & Period Check Period Propellers, Chapter 61 Alternator 2000 Regulator 2000 Hub 2500 Blades 2500 Reservoir 2500 Spinner OC Power Plant General, Chapter 71 Engine Mounting System OC Vibration Isolators OC Engine Cowling OC Engine Fire Seal OC Engine, Chapter 72 Compressor/Gearbox 4000 Turbine Section 4000
Engine Fuel and Control, Chapter 73 Temperature Datum Control System 3000 Fuel Control 3000 Engine Fuel Pump 3000 Fuel Flow Meter 3000 Ignition System, Chapter 74 Exciter and Relay EO Ignitor EO Engine Air, Chapter 75 Ducts and Scoops OC Anti-ice System 3000 Speed-sensitive Control 3000 Engine Controls, Chapter 76 Power Lever System and Engine Coordinator Controls and Linkages OC Effective date _____________________
OPERATIONS SPECIFICATIONS
AIRCRAFT MAINTENANCE
ENGINE MAKE - ALLISON ENGINE MODEL - 501-D13 Overhaul Inspection & Period Check Period Engine Indicating, Chapter 77 Tachometer Generator 3,000 Tachometer Indicator 5,000 T. I. T. Indicator 5,000 Torquemeter Indicator 5,000 Torquemeter Phase Detector 5,000 Indicator Oil Temperature 5,000 Indicator Oil Quantity OC Indicator Oil Pressure Gearbox 5,000 Indicator Oil Pressure Engine 5,000 Engine Exhaust System, Chapter 78 Engine Exhaust System OC Engine Oil System, Chapter 79 Engine Oil System OC Actuator Oil Cooler Flap 3,000 Oil Quantity Transmitter OC Oil Pressure Warning Switch OC Oil Pressure Transmitters 5,000
Oil Cooler Flap Position Indicator OC Fuel Oil Heat Exchanger 3,000 Oil Cooler EO Starting, Chapter 80 Engine Starter EO Bleed Air Shutoff Valves 5,000 Isolation and Firewell Valves 5,000 Combustor Assembly 1,800 Air Storage Bottles * Corrosion Inspection 1 year Air Bottle Cooling Valve 5,000 Air Compressor OC Low Pressure Regulator Valve EO * 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 _____________________ ---------------------------------------------------------------- ---------------------------------------------------------------- FIGURE 21. OPERATIONS SPECIFICATIONS AIRCRAFT MAINTENANCE
- BOEING 707/720 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 BOEING 707/720 Overhaul Inspection & Period Check Period Air Conditioning, Chapter 21 O.C.
Ducting, Plumbing, Electrical Conduits O.C.
Turbo Compressor 3,000 Outflow Valves 2,500 Cabin Pressure Controller 5,000 Differential Pressure Indicator 8,000 Vapor Cycle Pack 5,000 Tachometer, Turbo Compressor 3,500 Actuator - Ram Air Damper 7,500 Controller, Cockpit Airflow 7,500
Valve - Pack Shutoff 5,000 Valve - Cabin Temp. Control 7,500 Valve - Cockpit Temp. Control (Hot) 10,000 Valve - Cockpit Temp. Control (Cold) 10,000 Valve - Ram Air Shutoff 12,500 Valve - Wing Shutoff 12,500 Blower - Recirculating 3,500 Controller - Cabin Pressure Manual 5,000 Fan Assembly - Condenser 4,000 Heat Exchanger O.C.
Heaters - Electric O.C.
Indicator - Cabin Temperature O.C.
Indicator - Cabin Rate of Climb 10,000 Pump - Jet O.C.
Relay - Compressor Discharge Overheat 10,000 Relay - Cabin Pressure Warning 10,000 Elements - Temperature Sensing O.C.
Switch - Duct Overheat O.C.
Switch - Pressure Altitude O.C.
Valve - Blower Shutoff 10,000 Valve - Cabin Air Check O.C.
Valve - Cockpit Air Check O.C.
Valve - Turbo Compressor Check O.C.
Electronic Equipment Blower 6,000 Valve - Cabin Pressure Bleed Air Shutoff O.C.
Air Cycle Machine 5,000 Condenser O.C.
Evaporator O.C.
Compressor 10,000 Auto Pilot - Chapter 22 O.C.
Auto Pilot Adapter O.C.
Box - Power Junction 5,000 Control Panel O.C.
Indicator - 3 Axis Trim (Eclipse Pioneer) 7,500 Sero - Stabilizer Trim 5,000 Effective date July 1, 1964 PAGE 2 of 12 PAGES
OPERATIONS SPECIFICATIONS
AIRCRAFT MAINTENANCE BOEING 707/720 Overhaul Inspection &
Period Check Period Auto Pilot, Chapter 22 (continued) Annunciator - Glide Scope OC Three Axis Rate Transmitter 5,000 Air Data Sensor 3,000 Amplifier and Computer 3,000 Servo - Aileron, Rudder, & Elevator 2,500 Unit - Comparison 2,500 Communications, Chapter 23 May be determined by assigned inspector. OC Electrical Power, Chapter 24 OC Constant Speed Drive Oil Temp.
Indicator 10,000 Resistance Bulb c/o Drive Oil Temp. OC Wattmeters 10,000 DC Voltmeters 10,000 DC Ammeters 10,000 Generator Control Unit OC Relay - Essential Power Failure 5,000 Relay - External Power 6,000 Relay External Power Control 5,000 Relay - External Power Interlock 7,500 Relay - Negative Sequence Aux #1 7,500 Relay - Negative Sequence Aux #2 7,500 Relay - Negative Sequence 6,000 Transformer Rectifier OC A/C Generator 3,000 Voltage Regulator 5,000 Load Controller 5,000 Reverse Current Relay 5,000 Battery OC A/C Voltmeter and Ammeter 10,000 Frequency Meter 10,000 C/S Drive & Disconnect 3,000 Equipment and Furnishings, Chapter 25 OC May be determined by assigned inspector.
Fire Protection, Chapter 26 OC Control Unit - Wheel Well Area Fire Detector 5,000 Valve - Double Tee 10,000 Bottle - Fire Extinguisher * Control - Fire Warning Bell OC Stop Valve & Solenoid 6,000
Portable CO2 Bottles * Wheel Well Fire Detector Sensing Elements OC Engine Fire Detector Thermo Switches OC * 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 3 of 12 Pages
OPERATIONS SPECIFICATIONS
AIRCRAFT MAINTENANCE BOEING 707/720 Overhaul Inspection & Period Check Period Flight Controls - Chapter 27 O.C.
Flasher - Speed Brake and Flap Warning 5,000 Gear Box - Angle Flap Drive 10,000 Gear Box - Double Angle Fillet Flap Drive 10,000 Indicator - Flap Position 10,000 Motor - Emery Flap Drive 10,000 Motor - Hydraulic Flap Drive 10,000 Motor - Stabilizer Trim Drive 5,000 Power Unit - Flap Drive Gearbox 10,000 Relay - Emergency Flap Drive 10,000 Relay - Stabilizer Trim Control 10,000 Relay - Stabilizer Trim Safety 10,000 Screw Assembly - Fillet Flap Drive 10,000 Screw Assembly - Main Flap Drive 10,000 Transmitter - Flap Position 10,000 Valve - Flap By Pass 10,000 Valve - Flap Metering 10,000 Flap Cables - Tension Check and Pressure Seal Inspection O.C.
Valve - Spoiler Metering 10,000 Control Column O.C.
Snubber - Aileron Gust O.C.
Snubber - Elevator Gust O.C.
Snubber - Rudder Gust 10,000 Damper - Rudder Control Tab 10,000 Actuator - Leading Edge Flap 12,000 Valve - Leading Edge Flap Actuator 12,000 Actuator - Stabilizer Trim 5,000 Aileron Control Surface Assembly 10,000