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RULES: Boeing,
Published: 2001-01-22
This amendment adopts a new airworthiness directive (AD) that
is applicable to all Boeing Model 747400, 747400F, 767200, and 767
300 series airplanes equipped with Pratt & Whitney Model PW4000 series
engines. This action requires revising the Airplane Flight Manual
(AFM). This action is necessary to prevent reduced acceleration and
climb
RULES: Boeing,
Published: 2001-01-29
This amendment adopts a new airworthiness directive (AD),
applicable to certain Boeing Model 767 series airplanes powered by
Pratt & Whitney engines, that requires modification of the nacelle
strut and wing structure. The actions specified by this AD are intended
to prevent fatigue cracking in primary strut structure and consequent
reduced
PROPOSED RULES: McDonnell Douglas,
Published: 2001-10-05
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain McDonnell Douglas Model
MD11 series airplanes. This proposal would require an inspection of
the connector cables for signs of arcing and/or signs of moisture
penetration into the overhead decoder units (ODU), and replacement of
the affected
PROPOSED RULES: Pilatus Aircraft Ltd.,
Published: 2001-09-20
This document proposes to supersede Airworthiness Directive
(AD) 991932, which applies to certain Pilatus Aircraft Ltd. (Pilatus)
Models PC12 and PC12/45 airplanes. AD 991932 currently requires you
to inspect the flap actuator internal gear system for correct endplay
and backlash measurements and accomplish any corrective adjustments, as
RULES: Boeing,
Published: 2001-08-17
This amendment adopts a new airworthiness directive (AD),
applicable to all Boeing Model 767300 series airplanes modified by
supplemental type certificate ST00157SE, that requires modification of the electrical circuits that supply power to the inflight
entertainment (IFE) system. This action is necessary to prevent the
inability of the flight
RULES: Boeing,
Published: 2001-07-12
This amendment adopts a new airworthiness directive (AD),
applicable to all Boeing Model 767200 series airplanes modified by
Supplemental Type Certificate ST09022ACD, that requires modifying the
passenger entertainment system (PES) and revising the Airplane
Operations Manual. This action is necessary to ensure that the flight
crew is able to
RULES: Gulfstream; correction,
Published: 2001-06-29
This amendment corrects and clarifies information in an
existing airworthiness directive (AD), applicable to certain Gulfstream
Model G1159, G1159A, G1159B, GIV, and GV series airplanes, that
currently requires an inspection to determine if certain door control
valves of the landing gear are installed, and modification of the
valve, if necessary.
RULES: General Electric Co.,
Published: 2001-06-21
This amendment adopts a new airworthiness directive (AD) that
is applicable to General Electric Company (GE) CF650 turbofan engines.
This amendment requires removal of old high pressure compressor (HPC)
air ducts and mating hardware and replacement with newly designed air
ducts and reworked mating hardware. This amendment also requires the
PROPOSED RULES: Foker,
Published: 2001-06-11
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to all Fokker Model F.28 Mark 1000,
2000, 3000, and 4000 series airplanes. This proposal would require a
onetime inspection to detect the presence of filler plates of the
engine support fittings, and corrective action, if necessary. This
action is
RULES: Airbus,
Published: 2001-12-12
This amendment adopts a new airworthiness directive (AD),
applicable to certain Airbus Model A300 B2 and B4, A300 B4600 and B4
600R, and A310 series airplanes, that requires modification of the
terminal blocks of the starter feeder line of the auxiliary power unit
(APU). This action is necessary to prevent slackness and subsequent
overheat and
PROPOSED RULES: CFE Co.,
Published: 2001-12-04
The Federal Aviation Administration (FAA) proposes to adopt a
new airworthiness directive (AD) that is applicable to CFE Company
Model CFE73811B turbofan engines. This proposal would require
replacing the high pressure turbine (HPT) stage 1 aft cooling plate and
HPT stage 2 disk at or before they reach new reduced life cycle limits.
This proposal
RULES: Cessna,
Published: 2001-02-06
This amendment adopts a new airworthiness directive (AD) that
applies to certain The Cessna Aircraft Company (Cessna) Model 525
(CitationJet 1) airplanes. This AD requires you to replace certain
direct current (DC) power battery switches. This AD is the result of
reports of the potential for a certain 8pole battery switch to fail
during flight.
RULES: Rolls-Royce plc.,
Published: 2001-11-19
This amendment adopts a new airworthiness directive (AD), that
is applicable to RollsRoyce plc model RB211535E437, RB211535E4B
37, RB211535C37, RB211535E4B75 and RB21122B02 turbofan engines.
This amendment requires inspection of certain high pressure (HP)
turbine disks, manufactured between 1989 and 1999, for cracks in the
rim cooling air holes,
RULES: Airbus,
Published: 2001-02-16
This amendment adopts a new airworthiness directive (AD),
applicable to certain Airbus Model A330 and A340 series airplanes, that
requires identifying the part and serial numbers of the pressure
reducing valve on each air pressurization unit, testing pressure
reducing valves and air pressurization units having affected serial
numbers, and
PROPOSED RULES: McDonnell Douglas,
Published: 2001-06-06
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain McDonnell Douglas Model
DC910, 20, 30, 40, and 50 series airplanes; and C9 (military) airplanes.
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This proposal would require replacing the transformer ballast assembly
in the first officer's console with a new, improved ballast
RULES: Eurocopter France,
Published: 2001-03-05
This amendment adopts a new airworthiness directive (AD) for
Eurocopter France Model EC120B helicopters. This action requires
visually checking the engine to main gearbox coupling tube assembly
(tube) for a crack and replacing any cracked tube. This amendment is
prompted by a report of a crack detected on a tube. The actions
specified by this AD
PROPOSED RULES: General Electric Co.,
Published: 2001-05-17
The Federal Aviation Administration (FAA) proposes to adopt a
new airworthiness directive (AD) that is applicable to General Electric
Company CF650 and CF680C2 turbofan engines. This proposal would
require replacement of certain existing CF650 and CF680C2 shrouds
with new design shrouds. This proposal is prompted by 37 low pressure
turbine (LPT)
PROPOSED RULES: McDonnell Douglas,
Published: 2001-03-20
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain McDonnell Douglas Model
DC981, 82, 83, and 87 Series Airplanes, and MD88 airplanes. This
proposal would require revising the wiring of the selective calling
(SELCAL) system. This action is necessary to prevent inadvertent very
high frequency
PROPOSED RULES: GE Aircraft Engines,
Published: 2001-05-02
The Federal Aviation Administration (FAA) proposes to adopt a
new airworthiness directive (AD) that is applicable to GE Aircraft
Engines (GE) CT7 series turboprop engines. This proposal would require
removal of stage 2 turbine aft cooling plates of a certain part number
(P/N) and installation of cooling plates of a new design. This proposal
is
RULES: Pratt & Whitney,
Published: 2001-04-27
This amendment supersedes an emergency airworthiness directive
(AD) 20010852 that was sent previously to all known U.S. owners and
operators of Pratt and Whitney (PW) model PW4050, PW4052, PW4056,
PW4060, PW4060A, PW4060C, PW4062, PW4152, PW4156, PW4156A, PW4158,
PW4160, PW4460, PW4462, and PW4650 turbofan engines by individual
letters. That
RULES: Boeing,
Published: 2001-04-25
This amendment adopts a new airworthiness directive (AD) that
is applicable to all Boeing Model 737 series airplanes. This action
requires revising the Airplane Flight Manual to prohibit extended dry
operation of the center tank fuel pumps (with no fuel passing through
the pumps). This action is necessary to prevent ignition of fuel vapors
due to
PROPOSED RULES: Boeing,
Published: 2001-04-12
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain Boeing Model 737100,
200, and 200C series airplanes. This proposal would require a onetime
detailed visual inspection of the carriage spindles on the outboard
midflap for circumferential score marks; and rework of the carriage
spindles or
RULES: Airbus,
Published: 2001-08-06
This amendment adopts a new airworthiness directive (AD),
applicable to certain Airbus Model A300 B2 and B4; A310; and A300 B4
600, B4600R, and F4600R (collectively called A300600) series
airplanes; that requires modification of certain components related to
the fuel level sensors. This action is necessary to prevent the
possibility of overheating
PROPOSED RULES: Bombardier,
Published: 2001-09-04
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain Bombardier Model DHC8
100, 200, and 300 series airplanes. This proposal would require
installation of a backup pressure regulating valve on the oil pump of
the propeller control unit (PCU) on both engines. This action is
necessary to prevent a
RULES: McDonnell Douglas,
Published: 2001-08-29
This amendment revises an existing airworthiness directive
(AD), applicable to certain McDonnell Douglas Model MD11 series
airplanes, that requires a onetime inspection to identify the part
numbers of two dimmer controls for the overhead instrument panel light
and circuit breaker lightplate located in the flight compartment. For
airplanes on which