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RULES: Boeing,
Published: 2003-01-13
This amendment adopts a new airworthiness directive (AD),
applicable to certain Boeing Model 747400 and 400D series airplanes,
that requires repetitive inspections to detect discrepancies of the
drip shield and supports located above the rudder pedal mechanisms;
corrective action, if necessary; and eventual modification of the drip
shield, which
PROPOSED RULES: Bombardier,
Published: 2003-01-30
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain Bombardier Model CL600
2B19 series airplanes. This proposal would require a onetime general
visual inspection of the dust covers for the flight data recorder (FDR)
and cockpit voice recorder (CVR) equipment for the presence of markings
that
PROPOSED RULES: Turbomeca S.A.,
Published: 2003-02-12
The Federal Aviation Administration (FAA) proposes to adopt a
new airworthiness directive (AD) that is applicable to Turbomeca S.A.
Arriel 1 series turboshaft engines. This proposal would require initial
and repetitive visual inspections for ingestive erosion, and cleaning
if necessary, of M02 and M03 modules. This proposal is prompted by
reports
RULES: Bombardier,
Published: 2003-02-28
This amendment adopts a new airworthiness directive (AD),
applicable to certain Bombardier Model CL6002B19 (Regional Jet Series
440) series airplanes, that requires replacement of the overwing
emergency exit placards, door weight placards, and no baggage placards
with new placards. This action is necessary to prevent the inability of
a passenger
PROPOSED RULES: Rolls-Royce plc,
Published: 2003-03-11
The Federal Aviation Administration (FAA) proposes to adopt a
new airworthiness directive (AD) that is applicable to RollsRoyce plc
(RR) RB211 Trent 875, Trent 877, Trent 884, Trent 892, Trent 892B, and
Trent 895 turbofan engines with high pressure (HP) compressor rotor
rear stage 5 and 6 discs and cone shafts, part numbers (P/Ns) FK25230
and
RULES: Airbus,
Published: 2003-03-27
This amendment supersedes an existing airworthiness directive
(AD), applicable to all Airbus Model A300 B4600, B4600R, and F4600R (collectively called A300600) series
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airplanes, that currently requires repetitive inspections to detect
cracking of the upper radius of the forward fitting of frame 47, and
repair if necessary. This
RULES: Rolls-Royce Deutschland Ltd. & Co. KG,
Published: 2003-04-15
The FAA is adopting a new airworthiness directive (AD) for
certain serial numbers (SNs) of RollsRoyce Deutschland Ltd. & Co KG
(RRD) Model Tay 65015 turbofan engines. This action requires initial
and repetitive visual inspections of low pressure (LP) turbine stage 2
rotor discs and LP turbine stage 3 rotor discs on certain SNs of
engines, for
RULES: McDonnell Douglas,
Published: 2003-04-25
This amendment adopts a new airworthiness directive (AD),
applicable to certain McDonnell Douglas Model MD9030 airplanes, that
requires a onetime inspection for chafing of the RDB wire bundle
against the No. 2 automatic direction finder (ADF) receiver located at
the aft end of the forward right radio rack; repair or replacement, if
necessary; and
PROPOSED RULES: Dornier,
Published: 2003-05-15
This document proposes to adopt a new airworthiness directive
(AD) that would apply to certain Dornier Luftfahrt GMBH (Dornier) Models 228100, 228101, 228200, 228201, 228202, and 228212
airplanes that have electrical cabin/cockpit heater option P05 or
option P09 installed. This proposed AD would require you to modify the
cockpit and cabin
RULES: Boeing,
Published: 2003-05-29
This amendment supersedes an existing airworthiness directive
(AD), applicable to all Boeing Model 747 series airplanes, that
currently requires periodic inspections and cleaning of the drainage
system cavity of the canted pressure deck, aft of the wing center
section. This amendment adds new repetitive tests and inspections for
discrepancies of
RULES: Boeing,
Published: 2003-06-11
This amendment adopts a new airworthiness directive (AD),
applicable to certain Boeing transport category airplanes listed above.
This AD requires an initial inspection to identify all H11 steel bolts
on the outer chord of the body station (BS) 2360 aft pressure bulkhead
between stringers 12L and 12R, followon repetitive inspections to
identify
PROPOSED RULES: Boeing,
Published: 2003-06-23
This document revises an earlier proposed airworthiness
directive (AD), applicable to certain Boeing Model 737100, 200,
200C, 300, 400, and 500 series airplanes, that would have required
replacing the existing pressure relief valve on the potable water tank
with a new, improved pressure relief valve, which is made of stainless
steel and is
PROPOSED RULES: Boeing and McDonnell Douglas,
Published: 2003-07-09
This document proposes to revise an existing airworthiness
directive (AD), applicable to various Boeing and McDonnell Douglas
transport category airplanes, that currently requires revising the
Airplane Flight Manual (AFM) to advise the flightcrew to don oxygen
masks as a first and immediate step when the cabin altitude warning
horn sounds. The actions
RULES: Bombardier,
Published: 2003-07-18
This amendment adopts a new airworthiness directive (AD),
applicable to certain Bombardier Model DHC8102, 103, 106, 201,
202, 301, 311, and 315 airplanes. This AD requires modification of
the No. 3 electrical equipment panel behind the avionics rack, and
modification of the No. 2 propeller deice timer. This action is
necessary to prevent incorrect
RULES: Rolls-Royce plc,
Published: 2003-07-30
This amendment adopts a new airworthiness directive (AD) that
applies to RollsRoyce plc (RR) RB211 Trent 87517, Trent 87717, Trent
88417, Trent 89217, Trent 892B17, and Trent 89517 turbofan engines
with high pressure (HP) compressor rotor rear stage 5 and 6 discs and
cone shafts, part numbers (P/Ns) FK25230 and FK27899 installed. This
amendment
RULES: Boeing,
Published: 2003-08-18
This amendment supersedes an existing airworthiness directive
(AD), applicable to certain Boeing Model 747 series airplanes, that
currently requires inspections to detect cracking of the front spar web
of the wing, and corrective action if necessary. This amendment adds
one airplane to the applicability, changes certain compliance times,
adds
RULES: deHavilland,
Published: 2003-09-02
This amendment adopts a new airworthiness directive (AD) that
applies to certain Robert E. Rust (R.E. Rust) Models DeHavilland DH.C1
Chipmunk 21, 22, and 22A airplanes. This AD requires you to
repetitively inspect the tailplane attachment brackets and replace each
bracket at a specified time. This AD also requires you to repetitively
inspect each
PROPOSED RULES: International Aero Engines,
Published: 2003-09-17
The FAA proposes to supersede an existing airworthiness
directive (AD) for certain IAE V2522A5, V2524A5, V2527A5, V2527EA5,
V2527MA5, V2530A5, and V2533A5 turbofan engines. That AD currently
requires initial and repetitive inspections of the master magnetic chip
detector (MCD) or the No. 1, 2, 3 bearing chamber MCD. This proposed AD
would require
RULES: Dornier,
Published: 2003-09-30
This amendment adopts a new airworthiness directive (AD),
applicable to certain Dornier Model 328300 series airplanes, that
requires a onetime inspection of the antiice tubing in the engine
nacelle at the joint between the antiice tubing adapter and duct, and
also between the joint of the antiice shutoff valve and the same duct,
to detect any air
PROPOSED RULES: Dassault,
Published: 2003-10-09
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain Dassault Model Falcon
900EX series airplanes. This proposal would require modification of the
front attachment area of the No. 2 engine. This action is necessary to
prevent failure of the failsafe lugs of the hoisting plate of the
forward engine
PROPOSED RULES: Australia Pty Ltd.; AeroSpace Technologies,
Published: 2003-10-24
The FAA proposes to adopt a new airworthiness directive (AD)
for all AeroSpace Technologies of Australia Pty Ltd. (ASTA) Models
N22B, N22S, and N24A airplanes. This proposed AD would require you to
repetitively inspect wing fittings for fatigue defects, replace or
correct defective wing fittings, and replace the stub wing front spar
assembly and
PROPOSED RULES: Airbus,
Published: 2003-11-17
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain Airbus Model A320111,
211, 212, and 231 series airplanes. This proposal would require
repetitive inspections for fatigue cracking around the fasteners
attaching the pressure panel to the flexible bracket at frame 36,
adjacent to the longitudinal
PROPOSED RULES: McDonnell Douglas,
Published: 2003-11-28
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain McDonnell Douglas airplane
models. This proposal would require inspection of the captain's and
first officer's seat locking pins for minimum engagement with the
detent holes in the seat tracks; inspection of the seat lockpins for
excessive wear;
RULES: Boeing,
Published: 2003-12-18
This amendment adopts a new airworthiness directive (AD),
applicable to certain Boeing Model 777200 and 777300 series
airplanes, that requires application of hightemperature sealant in
designated areas of the strut aft dry bay. The actions specified by
this AD are intended to prevent leakage of hydraulic fluid into the
strut aft dry bay, where high
PROPOSED RULES: Bombardier,
Published: 2003-12-05
This document proposes the supersedure of an existing
airworthiness directive (AD), applicable to certain Bombardier Model
CL2151A10 and CL2156B11 series airplanes, that currently requires
repetitive inspections to detect cracking of main landing gear (MLG)
axles that have been reworked by chromium plating, and replacement of
cracked axles with
