Rear spar, main 10,000 5 Note 4 Front spar 10,000 5 Note 4 splice, WS 15 RH side upper, WS 15 LH side lower Rear spar splice, 10,000 5 Note 4 WS 10 RH side upper, WS 10 RH side lower Flap hinge pin 2,500 2.5 X X X Aileron hinge 10,000 5 X X X Note 8 bolts Aileron tab hinge 10,000 5 X X X Note 4 pin Aileron and tab 10,000 5 X Note 4 balance weights Engine, Chapter 72 CJ 610-1 1,000 X X X Hot section 500 hrs.
Note 9 Effective date _____________________
OPERATIONS SPECIFICATIONS AIRCRAFT MAINTENANCE Page 10 of 11 JET COMMANDER 1121
OVERHAUL INSPECTION AND CHECK PERIOD HOURS or YRS. P.F. S.C. P.I. OTHER Engine Fuel and Control, Chapter 73 EO X X Ignition, Chapter 74 EO X X Ignitor plug OC Note 7 Engine Controls, Chapter 76 OC X X X EO
Engine Indicating, Chapter 77 EO X X Tachometer, Generator EO X X Exhaust Temperature Thermocouples EO X X Exhaust Pressure Ratio Transducer EO X X Fuel Flow Transm@ter EO X X Oil Pressure Transmitter EO X X Fuel Pressure Transmitter EO X X Exhaust, Chapter 78 OC X X X Tail cone EO X X X Oil, Chapter 79 EO X Oil tank EO X Oil pump EO X Starting, Chapter 80 EO X Starter-Generator (See Chapter 24) Note 1 Sample 1/3 of fleet at 2,500, 5,000 and 7,500 hours.
Note 2 Sample 1/3 of fleet at 4,000 and 6,000 hours.
Note 3 Inspect 1/3 of fleet at 2nd and 4th Periodic Inspection. If found satisfactory, increase time between inspections to each 8th Periodic Inspection.
Effective date _____________________
OPERATIONS SPECIFICATIONS AIRCRAFT MAINTENANCE Page 11 of 11 JET COMMANDER 1121 Note 4 Inspect at 5,000 hours or 2.5 years.
Note 5 Inspect and magnaflux center bolt at 1,000 and 5,000 hours.
Note 6 Xray 1/3 of fleet at 1,000, 3,000 and 5,000 hours.
Note 7 Inspect, repair and/or replace in accordance with factory recommendations.
Note 8 Inspect and magnaflux at intervals of 2,500 hours or
2.5 years.
Note 9 Serialized engines listed in CJ 610 Service Bulletin No. 9 require a combustion liner change at 400 hours unless Service Bulletin No. 9, Service Bulletin No. 47 or subsequent revisions are incorporated.
Effective date_____________________ ---------------------------------------------------------------- ---------------------------------------------------------------- FIGURE 28. OPERATIONS SPECIFICATIONS AIRCRAFT MAINTENANCE
- DOUGLAS DC-8-62/62F Form Approved.
UNITED STATES OF AMERICA Budget Bureau FEDERAL AVIATION AGENCY No. 04-R075.
WASHINGTON PART D PAGE 1 of 10 PAGES
OPERATIONS SPECIFICATIONS
AIRCRAFT MAINTENANCE DOUGLAS DC-8-62/62F Following are additional items and/or changes to the original Douglas DC-8/F aircraft specification listing which apply to the Douglas DC-8-62/62F aircraft.
Zone diagrams for the Douglas DC-8/F are also applicable to Douglas DC-8-62/62F aircraft; however, fuselage stations listed will only apply to the Douglas DC-8/F.
Overhaul Inspection & Air Conditioning, Chapter 21 Period Check Period Valve, Cold Air Bypass OC D,E Electrical Power, Chapter 24 Constant Speed Rive, 30 KVA 3,000 D - Oil Change Generator, 30 KVA 5,000 B,D - Oil Level check
Panel, Voltage Regulator and Generator Control OC F/C @ E Cooler, Air/Oil CSD EO D Fire Protection, Chapter 26 (62F) Pyrotector (Smoke Detector) OC A,B,D,E Container - Fire Extinguisher * B,D,E Cartridge - Dual Squib 4 years B,D,E * 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 Cylinder and Control Valve Rudder Power 2E D Fuel, Chapter 28 Pump, Residual Fuel Scavenge Center Wing OC D - F/C @ E Heater, Sump, Center Wing OC D - F/C @ E Valve, Fuel Scavenge Selector Center Wing OC D - F/C @ E Ice and Rain System, Chapter 30 Rain Repellent System OC A,B,D Tail, De-icing OC D,E Effective date ____________________ Page 2 of 10
OPERATIONS SPECIFICATIONS
AIRCRAFT MAINTENANCE DOUGLAS DC-8-62/62F Overhaul Inspection & Landing Gear, Chapter 32 Period Check Period Limiter, Brake Fluid Quantity 12,500 D Bogie Beam, Main Landing Gear, Non Swivel 12,500 D Valve, Nose Wheel Steering Bypass 12,500 D Pneumatic, Chapter 36 Heat Exchanger, Bleed Air O.C. D - E.C.
Valve, Bleed Air Temperature Control O.C. D - F/C @ E Valve, 16th Stage Shut-Off O.C. D - F/C @
E.O.
Valve, 12th Stage Check O.C. D - F/C @ E.O.
Amplifier, Pneumatic Manifold Rupture Warning O.C. D,E Sensing Element, Pneumatic Manifold Rupture Warning O.C. E Doors, Chapter 52 (62F) Main Cabin Cargo Door Hydraulic System O.C. See NOTE * (62F) Cylinder Assembly, Main Cabin Cargo Door Actuating O.C. See NOTE * NOTE:
* The design of the main cabin cargo door installation is such that in the normally latched and locked position, it can be structurally compared to any fixed portion of the fuselage.
It is only when the door is actuated open on the ground during cargo loading operations that the heaviest loads are incurred. These loads would be greatest at the upper door hinge and hydraulic actuating cylinder attach points. The door seal would also be subject to damage at this time.
Thus, door utilization established inspection frequency.
Under these conditions, Douglas suggests the following procedures for purposes of inspection: (1) Conduct a general visual area inspection of the upper cargo door hinge attachments, door jamb, door actuating cylinder attachments, door seal and latching mechanism at the scheduled "D" service following use of the aircraft in cargo configuration. (2) If the aircraft is operated solely in the passenger configuration, conduct a general visual area inspection (as above) no later than "E" frequency.
Effective date ____________________ Page 3 of 10
OPERATIONS SPECIFICATIONS
AIRCRAFT MAINTENANCE DOUGLAS DC-8-62/62F Overhaul Inspection & Powerplant, Chapter 71 Period Check Period Nose Cowl and Fan Duct Attach.,
Fireseal, Engine Mounts, Control Engine and Accessory Brackets Change D Engine Air, Chapter 75 Valve, Engine Nose Cowl Anti-ice Shut-off O.C. D - F/C @ E.O.
Thrust Reverser, Chapter 78 Thrust Reverser Assembly O.C. B,D (X-Ray Reverser Structure, on Aircraft at E Frequency) Pump Assembly, Electric Driven 5000 D Accumulator 16,000 D Cylinder, Thrust Reverser Actuator 12,000 D Valve, Thrust Reverser Control 12,000 D Cylinder, Stow Latch, Thrust Reverser 12,000 D Filter Assembly O.C. E Effective date ____________________ Page 4 of 10
OPERATIONS SPECIFICATIONS
AIRCRAFT MAINTENANCE DOUGLAS DC-8-62/62F
STRUCTURE INSPECTION PROGRAM E Check - 4000 Hours Overhaul Inspection & D Check - 500 Hours Period Check Period Wings Wing Tip, Zone 5 L/R 5E D Wing Outboard of Sta. Xw 408, Zone 9 L/R & Zone 6 L/R 5E Wing Leading Edge Sta. Xfs.
710 to Xw 736 Cant, Zone 7
L/R E Wing Leading Edge Sta. Xw 485
to Xfs. 710, Zone 8 L/R E * No. 1 & 4 Alternate Fuel Tanks, Zone 9 L/R and Zone 6 L/R 5E E-Sample One Tank Per Aircraft Wing Trailing Edge Sta. Xw 408 to Xw 736 Cant, Aft of Rear Spar, Zone 10 L/R E Aileron Hinge Brackets and Bolts 4D Aileron and Tab, Zone 11 L/R E Hinges & Attachments 4D Aileron Leading Edge Balance Weights 2E Wing Leading Edge at Outboard Pylon Sta. Xfs. 526 to Xw 485, Zone 12 L/R E Outboard Pylon, Apron and Nacelle Access Doors, Zone 13 L/R E 2D * Pylon Upper Spar and Pylon Leading Edge attachments, Zone 13 L/R E 2D Effective date ____________________ Page 5 of 10
OPERATIONS SPECIFICATIONS
AIRCRAFT MAINTENANCE DOUGLAS DC-8-62/62F
STRUCTURE INSPECTION PROGRAM Overhaul Inspection & Period Check Period Wings (Continued) * Pylon to Wing Front Spar and Pylon to Wing Attachments, Zone 13 L/R E 2D
Inboard Pylon, Apron and Nacelle Access Doors, Zone 14 L/R E 2D * Pylon Upper Spar and Pylon Leading Edge Attachments, Zone 14 L/R E 2D * Pylon to Wing Front Spar and Pylon to Wing Attachments, Zone 14 L/R E 2D Wing Leading Edge Sta. Xw 408 to Xfs. 526, Zone 15 L/R E Wing Leading Edge Sta. Xw 257 to Xw 408, Zone 16 L/R E * No. 1 & 4 Main Fuel Tanks, Zone 17 L/R 5E E-Sample One Tank Per Aircraft Wing Trailing Edge from Outboard Auxiliary Spar to Sta. Xw 408, Zone 18 L/R E Main Landing Gear Support Fittings and Auxiliary Spars, Zone 19 L/R 2E Wing Leading Edge at Inboard Pylon Sta. Xfs. 250 to Xw 257, Zone 20 L/R E Wing Leading Edge Sta. Xw0 to Xfs. 207, Zone 21 L/R & 22 L/R External Inspection E Wing Leading Edge Xfs Sta. 207 to Xs 250, Zone 20 & Zone 21 External Inspection E Wing Leading Edge Xfs Sta. 207 to Xs 250, Zone 20 & Zone 21 Including Forward Face of Wing Front Spar, as visible. E Effective date ____________________
Page 6 of 10
OPERATIONS SPECIFICATIONS
AIRCRAFT MAINTENANCE DOUGLAS DC-8-62/62F
STRUCTURE INSPECTION PROGRAM Overhaul Inspection & Period Check Period Wings (Continued) Leading Edge Fuel Tanks, Zone 21 L/R and Zone 22 L/R 5E No. 2 and 3 Main and Alternate Fuel Tanks, Zone 23 L/R and Zone 24 L/R 5E Outboard Wing Flap Interior Structure, Zone 25 L/R 3E Flap Hinge Support Fittings, Zone 25 L/R 2E Aft Side of Flap Spar, Zone 25 L/R 4E Inboard Wing Flap & Links at the Outboard End of the Flap, which Connect to the Inboard End of the Outboard Flap, Zone 26 L/R E Flap Hinge Support Fittings and Aft Side of Flap Spar, Zone 26 L/R 4E Interior of Center Wing Sta.
Xcw 0 to Xcw 69.5 (Front to Rear Spar, Zone 27 L/R 5E NOTE:
* Specified times for items identified by (*) applicable to all operators until satisfactory service experience accumulated.
Fuselage (All Stations are DC-8-62/62F)
Radome, Zone 51 E Effective date ____________________ Page 7 of 10
OPERATIONS SPECIFICATIONS
AIRCRAFT MAINTENANCE DOUGLAS DC-8-62/62F
STRUCTURE INSPECTION PROGRAM Overhaul Inspection & Period Check Period Fuselage (Continued) Fuselage Turbo Compressor Compartment, Zone 52 4E Navigation Antenna Compartment, Zone 53 4E Nose Gear Wheel Well, Zone 54 4E Nose Wheel Well Tunnel, Zone 55, L/R 4E Air Conditioning Accessory Compartment, Sta. 208 to 270, Zone 56 E Forward Cargo Compartment, Sta.
270 to 640, Zone 57 4E Forward Cargo Compartment Tunnel Sta. 270 to 640, Zone 57 L/R 4E Fuselage Accessory Compartment Sta. 640 to 680, Zone 58 E Upper and Lower Front Spar Cap, Forward Face of Front Spar Web Upper and Lower Front Spar Caps and Splice Plates at Sta. Xcw 0, Zone 58 4E Aft Cargo Compartment Sta. 980 to 1380, Zone 59 4E
Aft Cargo Compartment Tunnel, Sta. 980 to 1380, Zone 59 L/R 4E Fuselage Belly Compartment Sta.
1380 to Pressure Panel at Sta. 1606, Zone 60 E Effective date ____________________ Page 8 of 10
OPERATIONS SPECIFICATIONS
AIRCRAFT MAINTENANCE DOUGLAS DC-8-62/62F
STRUCTURE INSPECTION PROGRAM Overhaul Inspection & Period Check Period Fuselage (Continued) Aft Fuselage Sta. 1606 to 1730, Zone 61 E Aft Face and Periphery of Pressure Panel at Fuselage Sta. 1606, Zone 61 E Fuselage Tail Cone, Zone 62 E Fuselage Sta. 69 to 83 Above Cockpit Floor, Zone 63 4E Fuselage Cockpit Sta. 83 to 148, Zone 64 4E Fuselage Cockpit Sta. 148 to 225 Above Floor, Zone 65 L/R E Fuselage Sta. 208 to 69 Between Cockpit Floor and Horizontal Pressure Panel, Zone 66 E Forward and Aft Galley Areas Sta. 340 to 420 and Sta. 1440 to 1520 R. Side, Zone 67 E Scuff Plates at Forward and Aft Service Door Jambs, Internal Inspection of Door Jambs.
Intercostals and Frames at Fuselage Sta. 355, 391, 1460 and 1500. Inspection of Door Hinge Attachments and Door Snubber Attachments to Jambs, Zone 67 4E Forward and Aft Lavatory Areas, Zone 68 4E Vertical Stabilizer Front and Center Spar Attachments to Fuselage Longerons, Between Fuselage Sta.'s 1540 and 1606, Zone 68 4E Effective date ____________________ Page 9 of 10
OPERATIONS SPECIFICATIONS
AIRCRAFT MAINTENANCE DOUGLAS DC-8-62/62F
STRUCTURE INSPECTION PROGRAM Overhaul Inspection & Period Check Period Fuselage (Continued) Upper and Lower Attachments of Aft Pressure Panel Vertical Beam (Center Line-Forward Face Pressure Panel) Fuselage Sta. 1606, Zone 68 4E Fuselage Entrance Doors, Zone 69 4E (62F) Main Cabin Cargo Door, Zone 69 4E Emergency Exit Doors, Zone 69 4E Fuselage Sta. 680 to 980 Between Bottom of Floor and Top of Wing and Wheel Well, Zone 70 4E Upper Wing to Fuselage Fillet,