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A/P Autopilot: AAE Above aerodrome elevation [1] In aviation, above aerodrome level (AAL), or above aerodrome elevation (AAE), denotes that an altitude is given above the nearest aerodrome or airport. AAIB Air Accidents Investigation Branch: United Kingdom AAIM Aircraft Autonomous Integrity Monitoring AAO Assumed adverse obstacle AAS
The FAA ATP flight test can be taken in a light piston aircraft with 1,500 hours of experience, however, the FAA additionally requires a 'Type Rating' to pilot any large or jet-powered aircraft. Most FAA-certified pilots earn their ATP certificate and Type Rating (aircraft specific) simultaneously via the successful completion of a part 121 ...
Title 14 CFR – Aeronautics and Space is one of the fifty titles that make up the United States Code of Federal Regulations (CFR). Title 14 is the principal set of rules and regulations (sometimes called administrative law) issued by the Department of Transportation and Federal Aviation Administration, federal agencies of the United States which oversee Aeronautics and Space.
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Applicants who attend an aviation maintenance school program certificated under Part 147 study an FAA-approved and supervised curriculum. Those applying for a mechanic certificate with a single rating—either airframe or powerplant—study a "general" set of subjects for at least 400 hours, as well as at least 750 hours of material appropriate ...
The applicant must accumulate and log specific aeronautical experience, and pass a three-part examination: a knowledge test (a computerized multiple-choice test, typically called the "written test"), an oral test, and a practical test carried out by either an FAA inspector or a Designated Pilot Examiner.
The FAA's Advisory Circular System is defined in FAA Order 1320.46D. [ 2 ] By writing advisory circulars, the FAA can provide guidance for compliance with airworthiness regulations , pilot certifications, operational standards, training standards, and any other rules within the 14 CFR Aeronautics and Space title, aka 14 CRF or FARs.
A 1976 study included an evaluation of the armor required to contain the energy from 1 blade, 2 blade, and 4 blade fragments of the compressor and turbine stages of General Electric CF6 and Pratt & Whitney JT9D engines; although the 4 blade fragment was unlikely to occur, containing it would have required a steel plate 1.212 inches (30.8 mm ...