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PROPOSED RULES: Airbus,
Published: 2003-09-09
This document proposes the supersedure of an existing
airworthiness directive (AD), applicable to certain Airbus Model A300
B4600R and A300 F4600R series airplanes, that currently requires a
onetime visual inspection for damage of the center tank fuel pumps and
fuel pump canisters, and replacement of damaged fuel pumps and fuel
pump canisters with new
RULES: Bombardier,
Published: 2003-09-22
This amendment revises an existing airworthiness directive
(AD), applicable to certain Bombardier Model CL6002B19 (Regional Jet
series 100 & 440) airplanes, that currently requires revising the
airworthiness limitations section of the Instructions for Continued
Airworthiness by incorporating new structural inspection intervals for
the pressure
RULES: Bombardier,
Published: 2003-10-06
This amendment adopts a new airworthiness directive (AD),
applicable to certain Model CL6002B19 (Regional Jet Series 100 & 440)
airplanes, that requires revising the airworthiness limitations section
of the Instructions for Continued Airworthiness by incorporating new
structural inspection intervals for the vertical beams of the pressure
bulkheads
PROPOSED RULES: Bombardier,
Published: 2003-10-20
This document proposes the supersedure of an existing
airworthiness directive (AD), applicable to certain Bombardier Model
DHC8102, 103, 106, 201, 202, 301, 311, and 315 airplanes, that
currently requires a onetime inspection to detect chafing of
electrical wires in the cable trough below the cabin floor; repair, if
necessary; installation of
PROPOSED RULES: Airbus,
Published: 2003-11-04
This document proposes the supersedure of an existing
airworthiness directive (AD), applicable to certain Airbus Model A320
series airplanes, that currently requires an inspection to detect
moisture and migrated bushings of the guide fittings of the safety
locking pins of the passenger doors, removal of any moisture,
application of grease, and
PROPOSED RULES: General Electric Co.,
Published: 2003-11-18
The FAA proposes to adopt a new airworthiness directive (AD)
for GE CF680C2 turbofan engines with certain part number (P/N) high
pressure turbine stage 2 nozzle guide vanes (HPT S2 NGVs) installed.
This proposed AD would require flex borescope inspections of HPT S2
NGVs installed in CF680C2 turbofan engines. This proposed AD is
prompted by an
PROPOSED RULES: Empresa Brasileira de Aeronautica S.A.,
Published: 2003-12-31
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain EMBRAER Model EMB135 and
EMB145 series airplanes. This proposal would require inspection of the
housings of the main landing gear (MLG) leg strut bushings; repair of
the housings if necessary; and replacement of the MLG leg strut
bushings with
RULES: Rolls-Royce Corp.,
Published: 2003-12-17
The FAA is adopting a new airworthiness directive (AD) for
RollsRoyce Corporation (formerly Allison Engine Company) AE 3007A1, AE
3007A1/1, AE 3007A1/3, AE 3007A3, AE 3007A1E, and AE 3007A1P turbofan
engines, with 1st to 2nd stage turbine spacers, part number (P/N)
23069627, 23070989, 23072849, or 23075364 installed. This AD reduces
the life limit
RULES: McDonnell Douglas,
Published: 2003-12-04
This amendment supersedes an existing airworthiness directive
(AD), applicable to certain McDonnell Douglas Model MD11 airplanes,
that currently requires repetitive general visual inspections of the
power feeder cables, terminal strip, fuseholder, and fuses of the
galley load control unit (GLCU) within the No. 3 bay electrical power
center (EPC)
RULES: Empresa Brasileira de Aeronautica S.A. (EMBRAER),
Published: 2003-01-06
This document publishes in the Federal Register an amendment
adopting airworthiness directive (AD) 20022651 that was sent
previously to all known U.S. owners and operators of certain EMBRAER
Model EMB135 and 145 series airplanes by individual notices. This AD
requires revising the Limitations Section of the Airplane Flight Manual
to advise the
PROPOSED RULES: New Piper Aircraft, Inc.,
Published: 2003-01-27
This document proposes to adopt a new airworthiness directive
(AD) that would apply to certain The New Piper Aircraft, Inc. (Piper)
Models PA23, PA23160, PA23235, PA23250, and PAE23250 airplanes
that do not incorporate a certain design flap control torque tube or
torque tube assembly. This proposed AD would require you to
repetitively inspect the
RULES: Piaggio Aero Industries S.p.A.,
Published: 2003-02-05
This amendment adopts a new airworthiness directive (AD) that
applies to all Piaggio Aero Industries S.p.A. (Piaggio) Model P180
airplanes. This AD requires you to inspect and determine whether any
firewall shutoff or crossfeed valve with a serial number in a certain
range is installed and requires you to replace any valve that has a
serial number
PROPOSED RULES: Boeing,
Published: 2003-02-24
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to all Boeing Model 737600, 737700,
737700C, 737800, 737900, 757, and 767 series airplanes. This
proposal would require revising the Airplane Flight Manual (AFM) to
advise the flightcrew to don oxygen masks as a first and immediate step
when a cabin
PROPOSED RULES: Boeing,
Published: 2003-03-04
This document proposes the supersedure of 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 action would add one airplane to the applicability,
change certain
RULES: General Electric Aircraft Engines,
Published: 2003-03-20
This amendment adopts a new airworthiness directive (AD) that
is applicable to certain General Electric Aircraft Engines (GEAE) CT7
series turboprop engines. This amendment requires initial and
repetitive inspections of the propeller gearbox (PGB) oil filter
impending bypass button (IBB) for extension (popping), requires follow
on inspections,
PROPOSED RULES: Pratt & Whitney,
Published: 2003-04-07
The Federal Aviation Administration (FAA) proposes to
supersede an existing airworthiness directive (AD), that is applicable
to Pratt and Whitney (PW) model 4000 series turbofan engines. That AD
currently requires interim actions to address engine takeoff power loss
events until the highpressurecompressor (HPC) case is redesigned and
available for
RULES: Consolidated, Consolidated Vultee, and Convair,
Published: 2003-04-22
This amendment adopts a new airworthiness directive (AD) that
is applicable to various surplus military airplanes manufactured by
Consolidated, Consolidated Vultee, and Convair. This action requires
repetitive inspections to find fatigue cracks in the lower rear cap of
the wing front spar, front spar web, and lower skin of the wings;
repair or
PROPOSED RULES: Rolls-Royce Deutschland Ltd & Co KG Dart,
Published: 2003-05-05
The FAA proposes to adopt a new airworthiness directive (AD)
for RollsRoyce Deutschland Ltd & Co KG (RRD) (formerly RollsRoyce
plc) Dart 5287E, 5297H, 7E, 8E, 8H, 8X, 8Y, 8Z, 529D7E, 7H, 8E, 8H, 8X, 8Y, 8Z, 531, 5322L, 7, 7N, 7P, 7L, 7R, 5352,
7R, 5424, 4K, 10, 10J, 10K, 5522, 5527, and 7R turboprop
engines. This proposed AD would require removal
RULES: McDonnell Douglas,
Published: 2003-05-29
This amendment adopts a new airworthiness directive (AD),
applicable to all McDonnell Douglas Model MD9030 airplanes, that
requires replacement of the starter relay of the auxiliary power unit
(APU) with a new, improved relay. The actions specified by this AD are
intended to prevent failure of the APU starter relay, which could
result in depleted
RULES: Boeing,
Published: 2003-05-29
This amendment adopts a new airworthiness directive (AD),
applicable to certain Boeing Model 727, 737100, 737200, and 737200C
series airplanes, that requires onetime inspections to determine the
part numbers of hydraulic accumulators installed in various areas of
the airplane, and followon corrective actions if necessary. The
actions specified by
RULES: Boeing,
Published: 2003-06-11
This amendment adopts a new airworthiness directive (AD),
applicable to certain Boeing Model 727100 and 727200 series
airplanes, that requires, under certain conditions, replacement of the
installed autopilot pitch control computer with a modified computer,
testing of the modified system, and revision of the Airplane Flight
Manual (AFM). The
RULES: Empresa Brasileira de Aeronautica, S.A. (EMBRAER),
Published: 2003-06-23
This amendment adopts a new airworthiness directive (AD),
applicable to certain EMBRAER Model EMB120 series airplanes, that
requires either revising the Airplane Flight Manual (AFM) to require a
maximum operating altitude of 25,000 feet; or modifying the flight
attendant's seat or reworking the oxygen bottle kit, as applicable, and
revising the
PROPOSED RULES: Boeing,
Published: 2003-07-09
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain Boeing transport category
airplanes listed above. This proposal would require drilling witness
holes through the cowl skin at the cowl latch locations in the left
hand side of the cowl panel assembly of each engine. This action is
necessary to
RULES: Bombardier,
Published: 2003-07-18
This amendment adopts a new airworthiness directive (AD),
applicable to certain Bombardier Model CL6002B19 (Regional Jet Series
100 & 440) airplanes, that requires the installation of protective tape
on the fire and overheat control unit located in the flight
compartment. The actions specified by this AD are intended to prevent
fluid contamination
RULES: Honeywell International Inc.,
Published: 2003-07-30
This amendment adopts a new airworthiness directive (AD) that
is applicable to Honeywell International Inc. (formerly AlliedSignal)
model RE220 (RJ) auxiliary power units (APUs) part number (P/N)
WE38007702. This amendment requires replacing the existing fuel
nozzles with new design fuel nozzles, making reidentification updates
to the APU