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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.
[[Page 30346]]
This proposal would require replacing the transformer ballast assembly
in the first officer's console with a new, improved ballast
Part III: Department of Transportation, Federal Aviation Administration,
Published: 2001-03-02
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to all Boeing Model 757200 series
airplanes modified by supplemental type certificate (STC) SA1727GL.
This proposal would require deactivation of the airtoground telephone
system approved by that STC. This action is necessary to prevent the
inability of
RULES: Bombardier,
Published: 2001-05-18
This amendment adopts a new airworthiness directive (AD),
applicable to certain Bombardier Model DHC8100, 200, and 300 series
airplanes, that requires removing certain foam filters from the cabin
ducting installation located below the dado panels on the left and
righthand sides of the airplane. The actions specified by this AD are
intended to
RULES: Airbus,
Published: 2001-05-10
This amendment adopts a new airworthiness directive (AD) that
is applicable to Airbus Model A330243, 341, 342, and 343 series
airplanes equipped with Rolls Royce Trent 700 series engines. This
action requires repetitive inspections of certain components, and
corrective action, if necessary. This action is necessary to detect and
correct fatigue
RULES: Airbus,
Published: 2001-05-04
This amendment adopts a new airworthiness directive (AD),
applicable to certain Airbus Model A330 and A340 series airplanes. This action requires a onetime inspection to verify the proper
configuration of the drive assemblies for the lowpressure and, for
certain airplanes, the crossfeed fuel valves; and corrective action,
if necessary. This action
PROPOSED RULES: Bombardier,
Published: 2001-03-29
This document proposes the supersedure of an existing
airworthiness directive (AD), applicable to certain Bombardier Model
DHC8200 and 300 series airplanes, that currently requires repetitive
inspections to detect chafing or arcing damage to the cable/wire and
fuel tube assemblies on the righthand side of each engine, and
replacement with new
RULES: Airbus,
Published: 2001-04-26
This amendment adopts a new airworthiness directive (AD) that
is applicable to certain Airbus Model A319 and A320 series airplanes.
This action requires revising the Airplane Flight Manual (AFM) to
specify procedures for landing under certain conditions of gusty winds
and turbulence. This action is prompted by a report of a recent hard
landing on
RULES: Boeing,
Published: 2001-04-10
This amendment adopts a new airworthiness directive (AD),
applicable to certain Boeing Model 767 series airplanes powered by
General Electric or Pratt & Whitney engines, that requires repetitive
inspections to detect discrepancies of the aftmost fastener holes in
the horizontal tangs of the midspar fitting of the strut, and
corrective actions, if
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
PROPOSED RULES: Dassault,
Published: 2001-07-25
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain Dassault Model Mystere
Falcon 50 series airplanes. This proposal would require repetitive
tests of doubleskin feeder tanks for fuel leaks, and corrective
actions, if necessary. It would also require modification of seals in
the feeder tanks,
PROPOSED RULES: McDonnell Douglas,
Published: 2001-07-23
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain McDonnell Douglas Model
DC910 and 30 series airplanes. This proposal would require an
inspection of the power feeder cable for evidence of chafing, and
repair of any chafed power feeder cable. This proposal also would
require replacement of the
PROPOSED RULES: Airbus,
Published: 2001-01-09
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain Airbus Model A300 B4620,
A310203, A310221, and A310222 series airplanes. This proposal would
require repetitive inspections of fuselage frame 07 in the upper frame
section assemblies of the lateral cockpit windows, and corrective
action, if
RULES: Honeywell,
Published: 2001-10-26
This amendment adopts a new airworthiness directive (AD), that
is applicable to certain Honeywell International, Inc. (formerly
AlliedSignal, Inc. and Textron Lycoming) LTP 101 series turboprop and
LTS101 series turboshaft engines. This amendment requires a new life
limitation and removal of rigid tube fuel manifold assemblies and
replacement with
RULES: Boeing,
Published: 2001-10-16
This amendment adopts a new airworthiness directive (AD),
applicable to certain Boeing Model 737 series airplanes, that requires
inspection of wire bundles in certain junction boxes in the main wheel
well to detect chafing or damage, and followon actions. The actions
specified by this AD are intended to prevent wire damage, which could
result in
RULES: Fokker,
Published: 2001-10-10
This amendment supersedes an existing airworthiness directive
(AD), applicable to all Fokker Model F.28 Mark 0100 series airplanes,
that currently requires replacement of the antiskid control boxes with
improved units. This amendment requires modification or replacement of
the antiskid control boxes with new, improved units, which render the
skid
RULES: Agusta S.p.A.,
Published: 2001-10-03
This amendment adopts a new airworthiness directive (AD) for
Agusta S.p.A. (Agusta) Model A109E helicopters that requires modifying
the passenger compartment sliding doors by installing certain locking
mechanism kits. This amendment is prompted by accidental opening of a
passenger compartment sliding door (door) in flight due to a door
locking
RULES: McDonnell Douglas,
Published: 2001-08-22
This amendment adopts a new airworthiness directive (AD), [[Page 44036]]
applicable to certain McDonnell Douglas Model MD11 series airplanes,
that requires an inspection to detect arcing damage of the electrical
cables leading to the hydraulic pump terminal strips and the
surrounding structure in the wheel well area of the right main landing
gear
RULES: McDonnell Douglas,
Published: 2001-07-23
This amendment adopts a new airworthiness directive (AD),
applicable to certain McDonnell Douglas Model DC1010, 15, 30, and
40 series airplanes, and Model MD1010F and 30F series airplanes,
that requires a general visual inspection to detect chafing or damage
of the feeder cables of the external ground power in the forward cargo
compartment between
RULES: Boeing,
Published: 2001-07-11
This amendment adopts a new airworthiness directive (AD) that
is applicable to all Boeing Model 737600, 700, 700C, and 800 series
airplanes. This action prohibits installation of repairs of the
elevator tab using previously approved repair procedures. This action
is necessary to prevent installation of repairs of the elevator tab
that are outside