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PROPOSED RULES: McDonnell Douglas; withdrawn,
Published: 2004-09-01
This action withdraws a notice of proposed rulemaking (NPRM)
that proposed a new airworthiness directive (AD), applicable to certain
McDonnell Douglas airplane models. That action would have superseded an
existing AD to require that the repetitive inspections of the numbers 1
and 2 electric motors of the auxiliary hydraulic pump for electrical
PROPOSED RULES: Raytheon,
Published: 2004-09-14
The FAA proposes to supersede Airworthiness Directive (AD) 93-
2507, which applies to Raytheon Aircraft Company (Raytheon) Beech 100,
200, and 300 series airplanes. AD 932507 currently requires you to
repetitively inspect the fuselage stringers for cracks and modify at
certain times depending on the number of cracked stringers. This
proposed AD is
RULES: Airbus,
Published: 2004-09-30
The FAA is adopting a new airworthiness directive (AD) for
certain Airbus Model A318, A319, A320, and A321 series airplanes. This
AD requires revising the airplane flight manual to provide procedures
for the flightcrew to follow in the event of the loss of all liquid
crystal display (LCD) units on airplanes equipped with a certain EIS2
standard of
RULES: de Havilland,
Published: 2004-10-21
The FAA adopts a new airworthiness directive (AD) for all
deHavilland Inc. Models DHC2 Mk. I and DHC2 Mk. II airplanes and for
all Bombardier Inc. Model (Otter) DHC3 airplanes powered by radial
engines. This AD requires you to visually inspect the firewall
connector plugs for proper lockwire security and replace or modify as
appropriate. This AD
PROPOSED RULES: Bombardier,
Published: 2004-11-03
The FAA proposes to adopt a new airworthiness directive (AD)
for certain Bombardier Model CL2156B11 (CL215T variant) and CL215
6B11 (CL415 variant) series airplanes. This proposed AD would require
replacing the mounting pad studs of the auxiliary feather pump with
new, longer studs, and installing a pressure relief valve. This
proposed AD is
RULES: Raytheon,
Published: 2004-11-09
The FAA supersedes Airworthiness Directive (AD) 87-22-01 R1,
which applies to certain Raytheon Aircraft Company (Raytheon) 65, 90,
99, 100, 200, and 1900 series airplanes, and Models 70 and 300
airplanes. AD 872201 R1 currently requires you to repetitively
inspect the nose landing gear (NLG) fork for cracks. If cracks are
found that exceed certain
PROPOSED RULES: Pacific Aerospace Corp., Ltd.,
Published: 2004-11-22
The FAA proposes to adopt a new airworthiness directive (AD)
for all Pacific Aerospace Corporation, Ltd. (Pacific Aerospace) Model
750XL airplanes. This proposed AD would require you to replace any type
TLPD or TLED rivets on the aileron pushrod ends and elevator control
pushrod ends. This proposed AD results from mandatory continuing
RULES: Boeing,
Published: 2004-12-07
The FAA is adopting a new airworthiness directive (AD) for
certain Boeing Model 747100, 747100B, 747100B SUD, 747200B, 747
200C, 747200F, and 747300 series airplanes; and Model 747SP and 747SR
series airplanes. This AD requires revising the airplane flight manual
to prohibit operation of the autopilot/flight director in command mode
with
PROPOSED RULES: Boeing,
Published: 2004-12-16
The FAA proposes to supersede an existing airworthiness
directive (AD) for certain Boeing Model 747, 757, 767, and 777 series
airplanes. That AD currently requires modifying certain drip shields
located on the flight deck, and followon actions. This proposed AD
would remove certain airplanes that are included in the applicability
statement of the
RULES: Raytheon,
Published: 2004-01-14
The FAA supersedes Airworthiness Directive (AD) 97-22-16,
which applies to certain Raytheon Model 1900, 1900C, and 1900D
airplanes. AD 972216 currently requires you to replace the bearings
on the vent blower assemblies with improved design bearings and install
a thermal protection device for the vent blowers. That AD resulted from
reports of vent
RULES: Airbus,
Published: 2004-02-03
This amendment adopts a new airworthiness directive (AD) that
is applicable to all Airbus Model A321 series airplanes. This action
requires revising the Limitations section of the airplane flight manual
to include an instruction to use Flap 3 for landing when performing an
approach in conditions of moderate to severe icing, significant
crosswind
RULES: Learjet,
Published: 2004-02-09
This amendment adopts a new airworthiness directive (AD),
applicable to certain Learjet Model 31, 31A, 35, 35A (C21A), 36, and
36A airplanes, that requires modification of the drag angles of the
fuselage and engine pylons to gain access to the shear webs of the
forward engine beams; repetitive inspections of the shear webs of the
forward engine
RULES: Boeing,
Published: 2004-02-18
This amendment adopts a new airworthiness directive (AD),
applicable to certain Boeing Model 737100, 200, 200C, 300, 400,
and 500 series airplanes, that requires replacing existing screw, nut,
and washers that attach the latch cable assembly to the latch block
assembly of the door mounted escape slides, with new, improved screw,
nut, and washers.
RULES: Airbus,
Published: 2004-03-03
This amendment adopts a new airworthiness directive (AD),
applicable to certain Airbus Model A300 B2 and B4 series airplanes;
Model A300 B4600, A300 B4600R, and A300 F4600R series airplanes
(collectively called A300600); Model A310 series airplanes; Model
A319, A320, and A321 series airplanes; Model A330301, 321, 322,
341, and 342 airplanes; and
RULES: Boeing,
Published: 2004-03-09
This amendment adopts a new airworthiness directive (AD), [[Page 10918]]
applicable to certain Boeing Model 767200 and 300 series airplanes,
that requires repetitive inspections of the aft pressure bulkhead web,
and corrective action, if necessary. This action is necessary to detect
and correct fatigue cracks in the aft pressure bulkhead web, which
PROPOSED RULES: Dornier,
Published: 2004-03-17
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to all Dornier Model 328300 series
airplanes. This proposal would require various onetime inspections for
discrepancies of the ground spoiler assemblies and the flap of each
wing, and related investigative and corrective actions. This action is
necessary to
RULES: Airbus,
Published: 2004-03-30
This amendment adopts a new airworthiness directive (AD) that
is applicable to all Airbus Model A318, A319, A320, and A321 series
airplanes. This action requires a onetime general visual inspection to
determine the part number and serial number of both main landing gear
(MLG) sliding tubes, and related investigative and corrective actions
if
PROPOSED RULES: Saab,
Published: 2004-04-01
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain Saab Model SAAB SF340A
series airplanes. This proposal would require replacing certain power
wires with a modification harness; and testing the new harness
installation. These actions are necessary to prevent a momentary loss
of data on the
PROPOSED RULES: Glaser-Dirks Flugzeugbau GmbH,
Published: 2004-04-12
The FAA proposes to adopt a new airworthiness directive (AD)
for all GlaserDirks Flugzeugbau GmbH (DG Flugzeugbau) Model DG800B
sailplanes equipped with engine SOLO 2625 or MidWest AE 50T. This
proposed AD would require you to modify the coolant pump and fuel pump
electrical circuits, replace the nonresettable circuit breaker with a
resettable
PROPOSED RULES: Valentin GmbH & Co.,
Published: 2004-04-22
The FAA proposes to adopt a new airworthiness directive (AD)
for all Valentin GmbH & Co. Taifun 17E sailplanes. This proposed AD
would require you to do an operational check of the front winglocking
mechanism left and right, inspect stop key movement, inspect wing and
fuselage side root ribs, inspect the wing side shear force fittings,
and take
RULES: Boeing; correction,
Published: 2004-05-05
This document corrects a typographical error that appeared in
airworthiness directive (AD) 20040510 that was published in the
Federal Register on March 5, 2004 (69 FR 10321). The typographical
error resulted in an incorrect reference to a previous AD. This AD is
applicable to certain Boeing Model 767 series airplanes. This AD
requires repetitive
RULES: Bombardier,
Published: 2004-05-11
This amendment adopts a new airworthiness directive (AD),
applicable to certain Bombardier Model DHC8101, 102, 103, 106,
201, 202, 301, 311, and 315 airplanes on which engine oil coolers
have been installed per LORI, Inc., STC SA8937SW. This amendment
requires an inspection or a review of the airplane maintenance records
to determine the part
PROPOSED RULES: Bombardier,
Published: 2004-05-19
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain Bombardier Model DHC8
101, 102, 103, 106, 201, 202, 301, 311, and 315 airplanes. This
proposal would require an inspection of the fuel tube assembly of the
auxiliary power unit (APU) for clearance from adjacent components; and
inspecting the fuel
RULES: Boeing,
Published: 2004-06-03
This document publishes in the Federal Register an amendment
adopting Airworthiness Directive (AD) 20040651, which was sent
previously to all known U.S. owners and operators of Boeing Defense and
Space Group (Boeing) Model 234 helicopters by individual letters. This
AD requires, before further flight, inspecting the upper shaft
extension for a
RULES: Empresa Brasileira de Aeronautica S.A. (EMBRAER),
Published: 2004-06-16
This amendment adopts a new airworthiness directive (AD),
applicable to certain EMBRAER Model EMB120 series airplanes. This
action requires repetitive inspections for cracks or evidence of
damage/distortion of the antiskid drive coupling clips for the hubcaps
of the main landing gear (MLG) wheels; repetitive measurement of the
gap and height