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RULES: Bombardier,
Published: 2002-02-20
This amendment adopts a new airworthiness directive (AD),
applicable to certain Bombardier Model CL6002B19 series airplanes,
that requires repetitive inspections for cracking of the left and right
lower wing planks, and repair, if necessary. The actions specified by
this AD are intended to find and fix such cracking, which could result
in reduced
RULES: Boeing,
Published: 2002-03-18
This amendment adopts a new airworthiness directive (AD),
applicable to certain Boeing Model 737100, 200, 200C, 300, 400,
and 500 series airplanes. For certain airplanes, this action requires
repetitive inspections for discrepancies of the rear spar attachments
and cracks in the upper flange of the inboard track at the rear spar
attachment of each
RULES: McDonnell Douglas,
Published: 2002-04-02
This amendment adopts a new airworthiness directive (AD)
applicable to certain McDonnell Douglas MD9030 airplanes. This action
requires inspection of the power feeder cables on the left and right
side of the aft cargo compartment between certain stations for minimum
clearance from the adjacent structure and for the presence of a grommet
in the
RULES: Enstrom Helicopter Corp.,
Published: 2002-04-17
This amendment supersedes an existing airworthiness directive
(AD) for Enstrom Helicopter Corporation (EHC) Model F28, F28A, F28C,
F28F, 280, 280C, 280F, and 280FX helicopters. That AD currently
requires determining the radius of the shaft fillet, performing certain
visual and dyepenetrant inspections before further flight, and
replacing certain
RULES: McDonnell Douglas,
Published: 2002-08-30
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 to
PROPOSED RULES: Eurocopter France,
Published: 2002-12-18
This document proposes adopting a new airworthiness directive
(AD) for Eurocopter France (ECF) Model SA365N, SA365N1, AS365N2, AS
365 N3, and SA366G1 helicopters. This proposal would require
inspecting the 9degree frame flange (frame) for the correct edge
distance of the four attachment holes for the stretcher support and for
a crack and repairing
PROPOSED RULES: Raytheon,
Published: 2002-12-02
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain Raytheon Model Hawker
800XP and 800 (including variant U125A) airplanes. This proposal would
require a onetime inspection to identify the bolts installed at
certain locations in the wing or fuselage, and corrective actions if
necessary. This
RULES: British Aerospace; correction,
Published: 2002-11-19
Correction
In rule document 0226370 beginning on page 64792 in the issue of Tuesday, October 22, 2002, make the following corrections:
Sec. 39.13 [Corrected]
1. On page 64794, in Sec. 39.13, in the table, in the second
column, in the first entry, in the third and fourth lines, ``June 23, 2002'' should read ``June 23, 2000''.
2. On the
RULES: MORAVAN a.s.,
Published: 2002-11-01
This amendment adopts a new airworthiness directive (AD) that
applies to certain MORAVAN a.s. (Moravan) Models Z143L and Z242L
airplanes. This AD requires you to modify the engine secondary vent
line. This AD is the result of mandatory continuing airworthiness
information (MCAI) issued by the airworthiness authority for the Czech
Republic. The
RULES: Agusta S.p.A.,
Published: 2002-10-16
This amendment supersedes an existing emergency airworthiness
directive (EAD) for Agusta S.p.A. (Agusta) Model A119 helicopters. EAD
20021752, which was issued on August 21, 2002, was sent to all known
U.S. owners and operators of Agusta Model A119 helicopters by
individual letters. That AD currently requires installing a placard in
the helicopter
PROPOSED RULES: Boeing,
Published: 2002-09-25
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
inspection of landing gear parts and/or their records to see that parts
have serial numbers and that each part's number of flight cycles has
been tracked;
PROPOSED RULES: Pilatus Britten-Norman Ltd.,
Published: 2002-08-22
This document proposes to adopt a new airworthiness directive
(AD) that would apply to all Pilatus BrittenNorman Limited (Pilatus BrittenNorman) BN2, BN2A, BN2B, BN2T, BN2A MK. III series
airplanes. This proposed AD would require you to repetitively inspect
the bottom corner of the engine mount bracket for cracks and replace
any cracked bracket
RULES: Bombardier,
Published: 2002-08-12
This amendment adopts a new airworthiness directive (AD) that
is applicable to all Bombardier Model CL6002B19 series airplanes.
This action requires revising the Airworthiness Limitations section of
the maintenance requirements manual to incorporate life limits for
certain horizontal stabilizer trim actuators (HSTAs), and replacing the
HSTAs with
RULES: Empresa Brasileira de Aeronautica S.A. (EMBRAER),
Published: 2002-07-24
This amendment supersedes an existing airworthiness directives
(AD), applicable to certain EMBRAER Model EMB135 and 145 series
airplanes, that currently requires repetitive inspections (tests) of
the actuator clutches of the primary and backup pitch trim systems of
the horizontal stabilizer for proper pitch trim indications, and
replacement of the
RULES: Rockwell Collins, Inc.,
Published: 2002-07-15
This amendment adopts a new airworthiness directive (AD) that
applies to certain Rockwell Collins, Inc. (Rockwell Collins) ADC85,
ADC85A, ADC850D, and ADC850F air data computers that are installed
on airplanes. This AD requires you to replace any affected air data
computer (ADC) with one that has a reprogrammed and tested central
processing unit
PROPOSED RULES: Air Tractor, Inc.,
Published: 2002-06-28
This document proposes to revise an earlier proposed
airworthiness directive (AD) that would apply to certain Air Tractor,
Inc. (Air Tractor) Model AT602 airplanes. The earlier NPRM would have
required you to repetitively inspect the left hand upper longeron and
upper diagonal tube of the fuselage frame for cracks and repair any
cracks found. The
RULES: Eurocopter France,
Published: 2002-06-12
This amendment adopts a new airworthiness directive (AD) for
Eurocopter France (Eurocopter) Model AS332L2 helicopters. This action
requires removing the main rotor shaft nonrotating scissors (non
rotating scissors) from the swashplate balljoint and inspecting for
friction or play in the hinges between the two links of the non
rotating scissors, or
RULES: Boeing,
Published: 2002-05-23
This amendment supersedes an existing airworthiness directive
(AD), applicable to certain Boeing Model 747 series airplanes, that
currently requires repetitive inspections to detect cracks in various
areas of the fuselage internal structure, and repair, if necessary.
This amendment adds new repetitive inspections for cracking of certain
areas of
RULES: Cessna,
Published: 2002-05-09
This amendment adopts a new airworthiness directive (AD) that
applies to certain Cessna Aircraft Company (Cessna) Model CESSNA 441
airplanes. This AD requires you to do a onetime inspection of the fuel
boost pump wiring inside and outside the boost pump reservoir, and
repair or replace the wiring as necessary. This AD is the result of
several
RULES: British Aerospace,
Published: 2002-01-17
This amendment adopts a new airworthiness directive (AD) that
applies to all British Aerospace Model HP.137 Jetstream Mk.1, Jetstream
Series 200, Jetstream Series 3101, and Jetstream Model 3201 airplanes
that are equipped with certain main landing gear (MLG) radius rods.
This AD requires you to inspect the MLG radius rod cylinders for the
required
PROPOSED RULES: McDonnell Douglas,
Published: 2002-01-09
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain McDonnell Douglas Model
DC981, 82, and 83 series airplanes, and Model MD88 airplanes. This
proposal would require an inspection to verify proper installation of
the support clamp of the alternating current (AC) power relay feeder
cables at the
PROPOSED RULES: Airbus,
Published: 2002-01-02
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain Airbus Model A330 and A340
series airplanes. This proposal would require a onetime inspection of
the hydraulically operated valve of the parking brake of the main
landing gear to identify the part and serial numbers, and followon
actions, if
RULES: General Electric Co.,
Published: 2002-01-30
This amendment supersedes an existing airworthiness directive
(AD), that is applicable to General Electric Company (GE) GE9076B,
77B, 85B, 90B, and 92B model turbofan engines. That AD currently
requires initial and repetitive eddy current inspections (ECI) for
cracks in the high pressure compressor (HPC) stage 26 spool, and, if
necessary,
RULES: BAE Systems (Operations) Ltd.,
Published: 2002-02-14
This amendment adopts a new airworthiness directive (AD),
applicable to certain BAE Systems (Operations) Limited Model BAe 146
and Avro 146RJ series airplanes, that requires repetitive inspections
to detect cracking of the oleo strut of the nose landing gear (NLG),
and corrective actions if necessary. This AD also provides for optional
terminating
RULES: Airbus,
Published: 2002-02-26
This amendment adopts a new airworthiness directive (AD),
applicable to certain Airbus Model A300 B2 and A300 B4 series
airplanes; certain Model A300 F4605R airplanes and Model A300 B4600
and A300 B4600R series airplanes; and certain Model A310 series
airplanes, that requires repetitive inspections to detect damage of the
fillet seals and feeder