1 RULES: Bombardier,
This amendment adopts a new airworthiness directive (AD), applicable to certain Bombardier Model CL6002B16 series airplanes, that requires modification of the wiring for the internal fuel/defuel panel. The actions specified by this AD are intended to prevent the loss of engine and fuel indications essential for safe flight and landing. This action
2 RULES: Airbus,
This amendment supersedes an existing airworthiness directive (AD), applicable to all Airbus Model A300 B2, A300 B4, A310, A319, A320, A321, A330, and A340 series airplanes; and Model A300 B4600, A300 B4600R, and A300 F4600R (collectively called A300600) series airplanes. That AD currently requires certain repetitive checks, and replacement of the
3 RULES: Boeing,
This amendment supersedes an existing airworthiness directive (AD), applicable to certain Boeing Model 747 series airplanes, that currently requires inspections to detect fatigue cracking of the vertical beam webs and chords of the nose wheel well (NWW) and of the inner chord and web of the fuselage frames at body station (BS) 300 and BS 320, and
4 PROPOSED RULES: Honeywell,
This document proposes to adopt a new airworthiness directive (AD) that is applicable to Honeywell International, Inc. (formerly AlliedSignal Inc. and Textron Lycoming) ALF502 and LF507 series turbofan engines. This proposal would require removing from service certain gas producer turbine (GPT) components prior to reaching new, lower cyclic life
5 RULES: Industrie Aeronautiche e Meccaniche,
This amendment removes Airworthiness Directive (AD) 2000-03- 19, which currently applies to all Industrie Aeronautiche e Meccaniche (I.A.M.) Model Piaggio P180 airplanes that are equipped with pneumatic deicing boots. AD 20000319 requires revising the Airplane Flight Manual (AFM) to include requirements for activating the airframe pneumatic deicing
6 RULES: Gulfstream,
This amendment adopts a new airworthiness directive (AD), applicable to certain Gulfstream Model G1159A (GIII) series airplanes, that requires modification of the master caution panel by installing an additional legend labeled ``BATT ON BUS'' and associated wiring to indicate when the airplane batteries are powering the direct current (DC)
7 RULES: BMW Rolls-Royce GmbH,
This amendment adopts a new airworthiness directive (AD) that is
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applicable to BMW RollsRoyce (RR) GmbH models BR700710A110 and
BR700710A220 turbofan engines with oil filter differential pressure
switch part number (P/N) 21SN04419 or P/N 21SN04431 installed. This
action requires inspections of oil filter differential pressure
8 RULES: Bell,
This document publishes in the Federal Register an amendment adopting Airworthiness Directive (AD) 20011952 which was sent previously to all known U.S. owners and operators of Bell Helicopter Textron Canada (BHTC) Model 222, 222B, 222U, and 230 helicopters by individual letters. This AD requires removing certain serialnumbered main rotor pendulum
9 PROPOSED RULES: General Electric Co.,
The Federal Aviation Administration (FAA) proposes to supersede an existing airworthiness directive (AD), that is applicable to General Electric Company CF34 series turbofan engines. That AD currently requires revisions to the Engine Maintenance Program specified in the manufacturer's Instructions for Continued Airworthiness (ICA) for General
10 Part V: Department of Transportation, Federal Aviation Administration,
This amendment rescinds Airworthiness Directive (AD) 2000-17- 09, which is applicable to certain McDonnell Douglas Model MD11 series airplanes. That AD requires an inspection of the upper avionics circuit breaker panel at the main observer's station to detect damage of the wires and to verify the correct routing of the wire bundles; corrective
Years: 20002001200220032004200520062007200820092010201120122013