Inboard 95.4 Trailing Edge, Wing, 94.5 & 1,000 Inboard 95.5 Trailing Edge, Wing, 94.6 & 1,000 Inboard 95.6 Trailing Edge, Wing, 94.7 & 2,500 Inboard 95.7 Trailing Edge, Wing, 94.8 & 1,000 Inboard 95.8 Flap, Outboard 92.1 & 2,500 S
97.1 Flap, Inboard 94.1 & 2,500 S
95.1 Spoiler, Outboard 92.2 & 2,500 S
97.2 Spoiler, Inboard 94.2 & 2,500 S
95.2 Aileron 93.1 & 2,500 S
96.1 Anti-Shock Body, Outboard 100 & 2,500 S 103 Anti-Shock Body, Inboard 101 & 2,500 S 102 Effective date _____________________ ---------------------------------------------------------------- ---------------------------------------------------------------- FIGURE 27. OPERATIONS SPECIFICATIONS AIRCRAFT MAINTENANCE
- JET COMMANDER 1121 Form Approved.
UNITED STATES OF AMERICA Budget Bureau FEDERAL AVIATION AGENCY No. 04-R075.
WASHINGTON
OPERATIONS SPECIFICATIONS
AIRCRAFT MAINTENANCE - GENERAL JET COMMANDER 1121 Page 1 of 11 Thorough checks shall be accomplished in accordance with the applicable procedures as listed in ABC Airlines' Maintenance Manual.
Preflight (P.F.) shall be accomplished each service calendar day.
Inspection shall be in accordance with the applicable procedures listed in ABC Airlines' Maintenance Manual.
Station Check (S.C.) shall be accomplished at basic intervals of 90 hours time in service. Inspection shall be in accordance with applicable procedures listed in ABC Airlines' Maintenance Manual.
During initial operation, the basic intervals for station checks will be evaluated in the following manner:
Ten inspections at 75 hours.* Periodic Inspection (P.I.) shall be accomplished at intervals not to exceed 175 hours time in service. Inspection shall be in accordance with the applicable procedures listed in ABC Airlines' Maintenance Manual. During initial operation, the basic intervals for periodic inspections will be evaluated in the following manner:
Five inspections at 150 hours.* * Note - Upon termination of the evaluation period, the assigned FAA maintenance and avionics inspectors will review the maintenance inspection findings and the operating history. If satisfactory, the carrier will be authorized to continue at the time established for the subsequent stage, i.e., Station Check - 90 hours Periodic Inspection - 175 hours Overhaul times as listed in hours and years are maximum limits of whichever occurs first.
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 schedule of maintenance and inspection functions and procedures set forth in the operator's maintenance manual.
b. OC "On Condition" items will be maintained in continuous airworthiness condition by periodic and progressive inspections, checks, services, repair and/or preventive maintenance and are appropriately described in the operator's maintenance manual.
c. Parts or sub-components, not listed below, will be checked, inspected and/or overhauled at the same time limits specified for the component or accessory to which such parts or sub-components are related.
Effective date _____________________
OPERATIONS SPECIFICATIONS
AIRCRAFT MAINTENANCE - GENERAL JET COMMANDER 1121 Page 2 of 11 Abbreviations used in the Jet Commander maintenance specifications are defined as follows:
FC - Indicates "Functional Check" BC - Indicates "Bench Check" EO - Indicates "Engine Overhaul" EC - Indicates "Engine Change" OC - Indicates "On Condition" R&R - Indicates "Remove and Replace" in accordance with factory recommendations HYD - Indicates "Hydrostatic Test" C - Indicates "Calibration" Effective date _____________________
OPERATIONS SPECIFICATIONS Page 3 of 11
AIRCRAFT MAINTENANCE JET COMMANDER 1121
OVERHAUL INSPECTION AND CHECK PERIOD HOURS or YRS. P.F S.C. P.I. OTHER Air-Conditioning, Chapter 21 10,000 5 X X X Controller-Cabin Pressure 5,000 2.5 X Indicator-Rate of Climb 4,000 2 X C 2000/1yr Indicator-Alt. & Diff. Pressure 4,000 2 X C 2000/1yr Turbine-Cooling 5,000 2.5 X Separator-Water OC X Regulator- Absolute Pressure 5,000 2.5 X FC 4-PI Filter-Cabin Air OC -- X R&R 4-PI Valve-Bleed Air Flow Control 4,000 2 X Valve-Bleed Air Shutoff 5,000 2.5 X Valve-Bleed Air Check 5,000 2.5 4-PI Valve-Emer. Air Pressure Regulator Shutoff 5,000 2.5 X FC 4-PI Valve-Outflow 2,000 1 X
Auto-Pilot, Chapter 22* 10,000 5 X X X Pedestal Controller OC X BC/C 2,000 Computer Amplifier OC X BC 1,000 Servos 2,000 2 X Trim Coupler 5,000 2.5 X Sensing Unit 2,000 2 X Rate Gyro 2,000 2 X Emergency Disconnect 5,000 2.5 X Altitude Controller 2,000 2 X Servo Mount 2,000 2 X Vertical Reference 2,000 2 X Communications, Chapter 23 May be determined by assigned inspector.
* Applies to Collins auto pilot.
Effective date PAGE 4 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 Electrical, Chapter 24 10,000 5 X X X Ammeter, AC OC X C 2,000 Ammeter, DC OC X C 2,000 Volt Meters AC/DC OC C 2,000 Battery N/C OC X X X DC Bus & Contactor Box OC X F C 2,500 AC Control Panel 5,000 2.5 X DC Control Panel Regulator 5,000 2.5 X AC Converter Regulator 2,000 2 X Current Trans-
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