formers OC X AC Generator EO DC Starter Generator EO Equipment & Furnishings, Chapter 25 May be determined by assigned inspector.
Fire Protection, Chapter 26 10,000 5 X X X Containers * X X * Detector Control 2,000 1 X Relay OC X Heat Sensing Units OC X * 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 10,000 5 X X X Speed Brake & Control- Actuator 2,000 2.5 X X X Flap Controls- Actuator 2,000 2.5 X X X Gust Lock and Controls OC X X X Stabilizer- Installation OC X X X Flap Torque Tube 10,000 5 X X X Note 1 Valve-Flap Control 10,000 5 X X X Note 1 Valve-Speed Brake 10,000 5 X X X Note 1 Trim Actuators 4,000 2 X X X BC 2,000 Fuel, Chapter 28 10,000 5 X X X Cells OC X X X R&R Boost-Pump AC 4,000 2 X X X Boost-Pump DC 8,000 4 X X X Note 2 Fuel Quantity Indication System OC X C 1,000 Compensator Fuel Temp. OC X C 1,000
Effective date _____________________ PAGE 5 of 11
OPERATIONS SPECIFICATIONS
AIRCRAFT MAINTENANCE JET COMMANDER 1121
OVERHAUL INSPECTION AND CHECK PERIOD HOURS or YRS. P.F. S.C. P.I. OTHER Hydraulic, Chapter 29 10,000 5 X X X Pump Emergency 2,000 2.5 X X X Pump Engine Driven EO X X X Regulator-Air- Pressure 4,000 4 X Valve-Reservoir Relief 4,000 4 X Accumulator- Emergency 4,000 4 X X Accumulator- Regulator 4,000 4 X X Primary Filters - Pressure OC X R&R 4-PI Valve-Thermal Relief-Emergency 4,000 4 X X X Reservoir Air Filters OC Note 3 Ice and Rain, Chapter 30 10,000 5 X X X Boots OC 2.5 X X X Regulator OC 2.5 X X Valve Distributor OC 2.5 X X Instruments, Chapter 31 May be determined by assigned inspector.
Landing Gear, Chapter 32 10,000 5 X X X Wheels OC X X X Zyglo wheels ea.
tire ch.
Brakes OC X X X Anti-Skid-Control Units OC 5 X Spin check at wheel or brake
change.
Tires OC X X X Cable-Emergency System OC X FC 4-PI Bottle-Nitrogen Pressure * * X X X * Doors and Linkage OC X X X Valve Assy. - Power Brake 4,000 2 X X X Lights, Chapter 33 May be determined by assigned inspector Navigation, Chapter 34 Overhaul times may be determined by assigned inspector. X X X * 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 6 of 11 PAGES
OPERATIONS SPECIFICATIONS
AIRCRAFT MAINTENANCE JET COMMANDER 1121
OVERHAUL INSPECTION AND CHECK PERIOD HOURS or YRS. P.F. S.C. P.I. OTHER Oxygen, Chapter 35 10,000 5 X X X Cylinders * X X X Regulators, Crew 2,500 2 X X X Passenger regulator control panel 2,500 2 X X X Masks, Crew OC X X X Masks, Passenger OC Drop Test 3-PI * 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.
Doors, Chapter 52 10,000 5 X X X Locking mechanism 10,000 5 Note 1 and pins Fuselage, 10,000 5 X X X Chapter 53 Connection of 10,000 5 Note 4 bottom frame carry thru structure between floor beams, FS 104 thru FS 270 - Z line .50 Fuselage splice 10,000 5 Note 4 attachment in "J" stringers, Z line 65 and FS 105.78 Splice at top of 10,000 5 Note 4 frames FS 105, FS 134.78 and FS 163.65, Z line 65 Splice at inner caps at lower centerline, FS 105, FS 134.78 and FS 163.65, Z line 10.5 Escape hatch 10,000 5 500 hrs.
retention blocks or 6 mo.
FS 196 and FS
216. - Z lines
32.45 and 59.45 Seat brace 10,000 5 Note 4 support. R/H side, FS 141 to FS 158. R/H and L/H sides FS 163 thru FS 259. Z line 10.5 Clips connecting 10,000 5 Note 4 window line fuselage frames to adjacent
fuselage frame.
R/H side FS
134.78, R/H and L/H side FS
163.65 thru FS 250 - Z lines
38.75 and 56.25.
Effective date _____________________
OPERATIONS SPECIFICATIONS AIRCRAFT MAINTENANCE Page 7 of 11 JET COMMANDER 1121
OVERHAUL INSPECTION AND CHECK PERIOD HOURS or YRS. P.F. S.C. P.I. OTHER Fuselage, Chapter 53 (Cont.)
Window frames 10,000 5 Note 4 connecting to fuselage frames R/H side FS
134.73, R/H and L/H side FS
163.65 thru FS
250. Z lines
38.75 and 56.25.
Splice bolts 10,000 5 Note 4 through pork chop fittings and members spanning floor beams. FS 196 and FS 216. -Z lines 1 and 9.
Control idler 10,000 5 Note 4 attachments between floor beams in forward fuselage and supported on frames in aft fuselage.
FS 76 thru FS 87, FS 125 thru
FS 150, FS 196 thru FS 223, FS 259 thru FS 269, FS 317 thru FS
328. Z line
10.5 Aft pressure 5,000 5 bulkhead mold line "U" cap channel used for skin splice. FS
269.87 "J" stringer 10,000 5 Note 4 attachment at pressure bulkhead FS 269.87 Z line 65.
Center fuel 5,000 5 separation panel floor to lower wing FS 270 to FS 316, Z lines
10.5 thru 38.
Angles to connect 5,000 5 centerfuel separation panel to pressure bulkhead. FS 270, Z lines
10.5 thru 38.
Angle under wing 5,000 5 rear spar FS 316, Z line 38.
Lower floor beam 10,000 5 Note 4 cap carry through fittings FS 270 and FS
316. Z line -
10.5.
Effective date _____________________
OPERATIONS SPECIFICATIONS
AIRCRAFT MAINTENANCE Page 8 of 11 JET COMMANDER 1121
OVERHAUL INSPECTION AND CHECK PERIOD HOURS or YRS. P.F. S.C. P.I. OTHER Fuselage, Chapter 53 (Cont.)
Engine nacelle 10,000 5 EC mount yoke to fuselage attachments FS 404 and FS 419 Nacelle/Pylons, 10,000 5 X X X Chapter 54 Engine mount 10,000 5 X EC structure (including nacelle internal skins) NS 47.83 thru 102.58 Engine attach OC X EC bolts Magnaflux Stabilizers, 10,000 5 X X X Chapter 55 Elevator hinge 10,000 5 X X X Note 5 bolts Elevator spar, 10,000 5 X X Note 6 external and internal Elevator ribs 10,000 5 X X Note 6 Elevator balance 10,000 5 X 2500 hrs weights or 2.5 yrs.
Horizontal 10,000 5 X X Note 6 stabilizer front spar and ribs Horizontal trim OC X Note 8 actuator bolts Forward surface 10,000 5 Note 1 of forward spar, vertical stabilizer
Rudder hinge 10,000 5 X X X Note 5 bolts Rudder balance 10,000 5 X 2500 hrs weights or 2.5 yrs.
Rudder tab hinge 10,000 5 X X X Note 4 pin Rudder tab 10,000 5 X 2500 hrs balance weight or 2.5 yr Forward surface 10,000 5 X 2500 of forward hrs. or rudder spar 2.5 yrs.
Effective date _____________________
OPERATIONS SPECIFICATIONS AIRCRAFT MAINTENANCE Page 9 of 11 JET COMMANDER 1121
OVERHAUL INSPECTION AND CHECK PERIOD HOURS or YRS. P.F. S.C. P.I. OTHER Windows, Chapter 10,000 5 X X X 56 All Glass OC X X X Note 7 Wing, Chapter 57 10,000 5 X X X Wing to fuselage 10,000 5 Note 4 attachments, WS 33 57 Spar - rear 10,000 5 Note 4 side Front spar, main 10,000 5 Note 4 Dagger fittings 10,000 5 Note 4 WS 0 WS 62 and WS 93 Rib, Center WS 0 10,000 5 Note 4 Ribs - WS 33 10,000 5 Note 4 thru WS 247 Stringers 10,000 5 Note 4
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 @