Production of the King Air C90A ended in 1992, with a total of 235 being built. It is powered by two Pratt & Whitney PT6A-21 turboprop engines with 550 shp each. The aircraft was equipped with improved C90-1 landing gear retraction and electrical systems.
The Model C90A featured the redesigned engine cowlings of the F90-1 and received an increase in takeoff weight in 1987, being certified to 10,100 lb. The Model C90A, a variant of the C90, was introduced in 1984. Several variants of the original design were created, including the Model A90, B90, and C90. Production is currently still active, giving the Beechcraft King Air the longest continual production run of any civilian aircraft of its class. Since production began in 1964, over 3,100 aircraft have been built. and other information needed to properly carry out basic maintenance activities such as patching a pothole or removing.
#Aircraft maintenance manual chapter 06 dimensions how to
The King Air line of aircraft is comprised of a number of models that have been divided into two families the Model 90 and 100 series are known as King Airs, while the Model 200 and 300 series were originally marketed as Super King Airs. The purpose of this manual is to provide maintenance personnel with guidance on how to conduct a wide variety of activities performed within the.
All aviation maintenance staff, technicians, mechanics, engineers and even pilots are familiar with this specification and that the aircraft they operate have similar systems, not the same when talking about the model system but the functional system or parts of the aircraft.The Beechcraft King Air family is part of a line of twin-turboprop aircraft produced by Beechcraft. So, the list has more numbers of chapters, but those are examples only. Source: ATA/ ATA Number ATA Chapter name ATA 20 STANDARD PRACTICES – AIRFRAME ATA 21 AIR CONDITIONING ATA 22 AUTO FLIGHT ATA 23 COMMUNICATION ATA 24 ELECTRICAL POWER ATA 25 EQUIPMENT /FURNISHINGS ATA 26 FIRE PROTECTION ATA 27 FLIGHT CONTROLS ATA 28 FUEL ATA 29 HYDRAULIC POWER ATA 30 ICE AND RAIN PROTECTION ATA 31 INDICATING / RECORDING SYSTEM ATA 32 LANDING GEAR ATA 33 LIGHTS ATA 34 NAVIGATION ATA 35 OXYGEN ATA 36 PNEUMATIC ATA 37 VACUUM ATA 38 WATER / WASTE ATA 39 ELECTRICAL – ELECTRONIC PANELS AND MULTIPURPOSE COMPONENTS ATA 40 MULTISYSTEM ATA 41 WATER BALLAST ATA 42 INTEGRATED MODULAR AVIONICS ATA 44 CABIN SYSTEMS ATA 45 ONBOARD MAINTENANCE SYSTEMS (OMS) ATA 46 INFORMATION SYSTEMS ATA 47 INERT GAS SYSTEM ATA 48 IN FLIGHT FUEL DISPENSING ATA 49 (AIRBORNE) AUXILIARY POWER UNIT Aircraft systems This operating and maintenance manual contains basic information related to the proper operation of the engine in various situations and under different conditions. ATA numbers ATA Number ATA Chapter name ATA 00 GENERAL ATA 01 MAINTENANCE POLICY ATA 02 OPERATIONS ATA 03 SUPPORT ATA 04 AIRWORTHINESS LIMITATIONS ATA 05 TIME LIMITS/MAINTENANCE CHECKS ATA 06 DIMENSIONS AND AREAS ATA 07 LIFTING AND SHORING ATA 08 LEVELING AND WEIGHING ATA 09 TOWING AND TAXIING ATA 10 PARKING, MOORING, STORAGE AND RETURN TO SERVICE ATA 11 PLACARDS AND MARKINGS ATA 12 SERVICING ATA 15 AIRCREW INFORMATION ATA 16 CHANGE OF ROLE ATA 18 VIBRATION AND NOISE ANALYSIS (HELICOPTERS ONLY) General Therefore, the aircraft technical documentation in most of the cases is arranged using this ATA chapters. In this way it is possible to observe the common chapter 28 dedicated to the fuel system information for the plane or the helicopter. Fuel system of the MD500 extracted from a Maintenance manual.
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