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- #AIRCRAFT MAINTENANCE MANUAL CHAPTER 06 DIMENSIONS CODE#
- #AIRCRAFT MAINTENANCE MANUAL CHAPTER 06 DIMENSIONS SIMULATOR#
Pressure shall be increased at a rate simulating a descent in altitude at the rate of 5,000 to 20,000 feet per minute until within 3,000 feet of the first test point (50 percent of maximum altitude). The hysteresis test shall begin not more than 15 minutes after the altimeter's initial exposure to the pressure corresponding to the upper limit of the scale error test prescribed in subparagraph (i) and while the altimeter is at this pressure, the hysteresis test shall commence. Scope and Detail of Items (as Applicable to the Particular Aircraft) To Be Included in Annual and 100-Hour Inspections Recording of Major Repairs and Major Alterations Major Alterations, Major Repairs, and Preventive Maintenance aeronautical products by certain Canadian persons. Maintenance, preventive maintenance, and alterations performed on U.S. Maintenance records: Falsification, reproduction, or alteration.Īdditional performance rules for inspections. Persons authorized to approve aircraft, airframes, aircraft engines, propellers, appliances, or component parts for return to service after maintenance, preventive maintenance, rebuilding, or alteration.Ĭontent, form, and disposition of maintenance, preventive maintenance, rebuilding, and alteration records (except inspections performed in accordance with part 91, part 125, § 135.411(a)(1), and § 135.419 of this chapter).ĭisposition of life-limited aircraft parts.Ĭontent, form, and disposition of records for inspections conducted under parts 91 and 125 and §§ 135.411(a)(1) and 135.419 of this chapter. Persons authorized to perform maintenance, preventive maintenance, rebuilding, and alterations.Īpproval for return to service after maintenance, preventive maintenance, rebuilding, or alteration. Air Transport Association of America.Maintenance, Preventive Maintenance, Rebuilding, and Alteration ATA Specification 100 - Specification for Manufacturers' Technical Data, Revision No.'From Paper to Interactive Electronic Technical Publications' (PDF).
#AIRCRAFT MAINTENANCE MANUAL CHAPTER 06 DIMENSIONS CODE#
'FEDERAL AVIATION ADMINISTRATION JOINT AIRCRAFT SYSTEM/COMPONENT CODE TABLE AND DEFINITIONS' (PDF).
#AIRCRAFT MAINTENANCE MANUAL CHAPTER 06 DIMENSIONS SIMULATOR#
STANDARD PRACTICES AND STRUCTURES - GENERALĮNGINE - TURBINE/TURBOPROP, DUCTED FAN/UNDUCTED FANġ15 FLIGHT SIMULATOR SYSTEMS/WORK SIMULATION Major Zones in Aircraft Zone 100 Fuselage Lower Zone 200 Fuselage Top Zone 300 Stabilizers / Empennage Zone 400 Nacelles-Pylons Zone 500 Left Wing Zone 600 Right Wing Zone 700 Landing Gear Compartment Zone 800 Doors Zone 900 Lavatories & Galleys Major sub Zones in Aircraft Zone 100 Fuselage Lower Zone 200 Fuselage Top Zone 300 Stabilizers / Empennage Zone 400 Nacelles-Pylons Zone 500 Left Wing Zone 600 Right Wing Zone 700 Landing Gear Compartment Zone 800 Doors See also External links References VIBRATION AND NOISE ANALYSIS (HELICOPTER ONLY)ĮLECTRICAL - ELECTRONIC PANELS AND MULTIPURPOSE COMPONENTS PARKING, MOORING, STORAGE AND RETURN TO SERVICE Examples of this include Oxygen (Chapter 35), Electrical Power (Chapter 24) and Doors (Chapter 52).ĪTA Chapters Aircraft General ATA Number
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Thus a chapter reference number for a Boeing 747 will be the same for other Boeing aircraft, a BAe 125 and Airbus Aircraft. The unique aspect of the chapter numbers is its relevance for all aircraft.
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