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RULES: Boeing,
Published: 2003-01-06
This amendment adopts a new airworthiness directive (AD),
applicable to certain Boeing Model 747 series airplanes, that requires
repetitive inspections to detect evidence of wear damage in the area at
the interface between the vertical stabilizer and fuselage skin, and
corrective actions, if necessary. This amendment also provides for an
optional
PROPOSED RULES: British Aerospace,
Published: 2003-01-27
This document proposes to adopt a new airworthiness directive
(AD) that would apply to all British Aerospace Model HP.137 Jetstream
Mk.1, Jetstream Series 200, Jetstream Series 3101, and Jetstream Model
3201 airplanes. This proposed AD would require you to inspect the
steering jack piston rod for cracks and replace if necessary; measure
the torque
RULES: Dornier,
Published: 2003-02-05
This amendment adopts a new airworthiness directive (AD),
applicable to certain Dornier Model 328100 and 300 series airplanes,
that requires replacement of the screws in the aileron, rudder, and
elevator trim tabs with new screws; and removal and reinstallation of
screws in the aileron, elevator, and rudder trim tabs and the rudder
spring tab; as
PROPOSED RULES: Boeing,
Published: 2003-02-24
This document revises an earlier proposed airworthiness
directive (AD), applicable to certain Boeing Model 767 series
airplanes, that would have required replacement of the aileron control
override quadrant with a modified unit. This new action revises the
applicability of the proposed rule. The actions specified by this new
proposed AD are
RULES: Rolls-Royce Deutschland Ltd. & Co. KG,
Published: 2003-03-11
This amendment supersedes an existing airworthiness directive
(AD) that is applicable to RollsRoyce Deutschland Ltd. & Co KG (RRD)
Model Tay 62015 and 65015 turbofan engines. That AD currently
requires initial and repetitive inspections of certain low pressure
(LP) fuel tubes. This amendment requires the same inspections and adds
two engine models
RULES: Saab,
Published: 2003-03-26
This amendment adopts a new airworthiness directive (AD),
applicable to certain Saab Model SAAB SF340A series airplanes, that
requires modifying the structure of the air recirculation fan support,
and replacing the air recirculation fans with two upgraded air
recirculation fans; or replacing the air recirculation fans with two
new air
RULES: Boeing,
Published: 2003-04-15
This amendment supersedes an existing airworthiness directive
(AD), applicable to certain Boeing Model 757 series airplanes, that
currently requires repetitive inspections for excessive wear of the
internal and external splines of the torque tube couplings of the
trailing edge flaps, and replacement of the couplings, if necessary.
That AD also
RULES: Boeing,
Published: 2003-04-25
This amendment adopts a new airworthiness directive (AD) that
is applicable to certain Boeing Model 737200, 200C, 300, 400, and
500 series airplanes. This action requires a onetime midfrequency
eddy current (MFEC), a lowfrequency eddy current (LFEC), and a
detailed inspection for damage or cracking of stringer S4L and S4R
lap joints and stringer
PROPOSED RULES: Cessna,
Published: 2003-05-15
This document proposes to supersede Airworthiness Directive
(AD) 20002301, which applies to all Cessna Aircraft Company (Cessna)
Model 402C airplanes. AD 20002301 currently requires repetitive
inspections of the forward, aft, and auxiliary wing spars for cracks,
and repair or replacement as necessary. Cessna has performed fatigue
and crack growth
RULES: BAE Systems (Operations) Ltd.,
Published: 2003-05-29
This amendment adopts a new airworthiness directive (AD),
applicable to all BAE Systems (Operations) Limited Model ATP airplanes,
that requires a onetime inspection of the fuel pipes within the fuel
``float switch'' test pipelines in the left and right inner wings for
evidence of damage, cracks, misalignment, or fuel leakage; followon
corrective
PROPOSED RULES: McDonnell Douglas,
Published: 2003-06-10
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain McDonnell Douglas Model DC1010, 10F, 15, 30, 30F (KC10A and KDC10), 40, and 40F
airplanes; and certain Model MD1010F and 30F airplanes. This
proposal would require inspections for cracking and corrosion of the
bolt assemblies and bushings on the
RULES: Airbus,
Published: 2003-06-23
This amendment adopts a new airworthiness directive (AD),
applicable to all Model A321131 series airplanes, equipped with
International Aero Engines (IAE) V25()()A5 series engines. This action
requires revising the Limitations section of the airplane flight manual
to incorporate new procedures to follow in the event of an oil filter
clog message.
PROPOSED RULES: Boeing,
Published: 2003-07-09
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain Boeing Model 747100, 747
100B, 747100B SUD, 747200B, 747200C, 747200F, 747300, 747SP, and
747SR series airplanes. This proposal would require a onetime
inspection of each emergency evacuation slide or slide/raft to
determine if a certain discrepant
RULES: Boeing,
Published: 2003-07-18
This amendment adopts a new airworthiness directive (AD),
applicable to certain Boeing Model 767200 and 300 series airplanes.
This action requires modification of the wire bundles of the video
control center (VCC) of the passenger address and entertainment system,
and an operational test if necessary. This action is necessary to
prevent chafing of
PROPOSED RULES: McDonnell Douglas,
Published: 2003-07-29
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain McDonnell Douglas airplane
models. This proposal would require a onetime inspection for chafing
of wiring in the lefthand tunnel area of the forward cargo
compartment, repair if necessary, and coiling and stowing of excess
wiring. This action is
RULES: Airbus,
Published: 2003-08-18
This amendment adopts a new airworthiness directive (AD),
applicable to certain Airbus Model A300 B4600, B4600R, and F4600R
(collectively called A300600) series airplanes, and Airbus Model A310
series airplanes. This AD requires replacement of Honeywell inertial
reference units (IRU) with new or modified Honeywell IRUs. For certain
airplanes, this
RULES: Airbus,
Published: 2003-09-02
This amendment adopts a new airworthiness directive (AD),
applicable to certain Airbus Model A300 B2 and B4; A300 B4600, A300
B4600R, and A300 F4600R (collectively called A300600); A310; A319;
A320; A321; A330; and A340 series airplanes; equipped with certain PPG
Aerospace windshields. This AD requires replacement of certain
windshields
RULES: Bombardier; correction,
Published: 2003-09-17
This document corrects typographical errors that appeared in
airworthiness directive (AD) 20031402 that was published as a final
rule; correction in the Federal Register on August 15, 2003 (68 FR
48783). The typographical errors resulted in an incorrect AD number and
effective date. This AD is applicable to certain Bombardier Model CL
6002B19
RULES: Rolls-Royce plc.; correction,
Published: 2003-09-29
This document makes a correction to Airworthiness Directive
(AD) 20031423 applicable to RollsRoyce plc RB211524G2, 524G2T,
524G3, 524G3T, 524H, 524HT, 524H2, and ``524H2T Series, and
Models RB211 Trent 76860, 77260, and 772B60 turbofan engines that
was published in the Federal Register on July 17, 2003. RB211 Trent
76860, 77260, and 772B60
PROPOSED RULES: Bombardier,
Published: 2003-10-09
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain Bombardier Model DHC8
400, 401, and 402 airplanes. This proposal would require a onetime
inspection of the forward engine mount assemblies on the left and right
engine nacelles for installation of preproduction engine mount
assemblies, and
RULES: Eurocopter France,
Published: 2003-10-24
This amendment adopts a new airworthiness directive (AD) for
the specified Eurocopter France (Eurocopter) model helicopters that
requires inspecting certain main rotor blades for disbonds, which may
be indicated by cracking, and repairing or replacing each main rotor
blade (MRB) as necessary. This amendment is prompted by the discovery
of
RULES: Cessna,
Published: 2003-11-13
This amendment adopts a new airworthiness directive (AD) that
is applicable to certain Cessna Model 560 airplanes. This action
requires disengaging and tiestrapping the pitch trim and autopilot
servo (servo 1) circuit breakers. This action also provides an optional
inspection and followon actions that, if accomplished, terminates the
requirement
RULES: MD Helicopters, Inc.,
Published: 2003-11-25
This amendment adopts a new airworthiness directive (AD) for
the specified model helicopters modified with a Helicopter Technology
Company, LLC, Supplemental Type Certificate (STC) No. SR09172RC,
SR09074RC, or SR09184RC. This action requires recording on the
component history card or equivalent record the number of torque events
(TEs) on each main
RULES: Boeing,
Published: 2003-12-23
This amendment adopts a new airworthiness directive (AD),
applicable to certain Boeing airplane models, that requires a onetime
inspection to identify all H11 steel bolts installed in the latch
fittings of the cargo doors, repetitive inspections for cracked or
broken H11 steel bolts, and followon and corrective actions if
necessary. This amendment
PROPOSED RULES: Empresa Brasileira de Aeronautica S.A. (EMBRAER),
Published: 2003-12-11
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain EMBRAER Model EMB120
series airplanes. This proposal would require a onetime inspection for
signs of overheating of wiring splices of the pitot/static 1, 2, and
auxiliary sensors; the angleofattack sensors; the side slip sensors;
and the current