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RULES: Eurocopter France,
Published: 2002-03-20
This amendment adopts a new airworthiness directive (AD) for
specified Eurocopter France (ECF) helicopters that requires replacing
the tail rotor hub pitch change plate ``SNR'' bearing (bearing). This
amendment is prompted by fatigue cracks found in the bearings. The
actions specified by this AD are intended to prevent seizure of the
bearing, loss
PROPOSED RULES: Bombardier,
Published: 2002-04-04
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 inspection of
certain installed electrical relays to determine whether they have
certain manufacturing date codes, and replacement of the electrical
relays with those date
RULES: CFM International,
Published: 2002-09-09
This amendment revises an existing airworthiness directive
(AD) that is applicable to CFM International (CFMI) CFM565C series
turbofan engines. This action establishes new life limits for certain
low pressure turbine rotor (LPTR) stage 3 disks and all high pressure
turbine rotor (HPTR) disks listed in the existing AD. This amendment is
prompted by
PROPOSED RULES: McDonnell Douglas,
Published: 2002-08-29
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain McDonnell Douglas Model
MD11 and 11F airplanes. This proposal would require an inspection to
detect damage of the wiring/bundles routed to the wire support bar of
the circuit breaker panel and to the circuit breakers, and an
inspection of the
PROPOSED RULES: Boeing,
Published: 2002-12-11
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain Boeing Model 767200 and
767300 series airplanes. This proposal would require modification of
the installation of the aft pressure bulkheadtofloor insulation
blankets. This action is necessary to avoid interference with venting
during a rapid
PROPOSED RULES: Boeing,
Published: 2002-11-27
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain Boeing Model 747200B and
200F series airplanes powered by Pratt & Whitney JT9D70 series
engines. This proposal would require repetitive detailed inspections of
the pylon skin and internal structure of the nacelle struts adjacent to
and aft of
RULES: Gulfstream,
Published: 2002-11-13
This amendment adopts a new airworthiness directive (AD) that
is applicable to certain Gulfstream Aerospace LP Model Galaxy and
Gulfstream 200 airplanes. This action requires a onetime inspection
for evidence of damage to the forward engine cross spar assembly; and
repair if necessary. This action is necessary to detect and correct
damage to the
PROPOSED RULES: Brackett,
Published: 2002-10-25
This document proposes to adopt a new airworthiness directive
(AD) that would apply to Brackett Aircraft Company (Brackett) single
screen air filter assemblies that are installed on airplanes. This
proposed AD would require you to check the Brackett single screen air
filter assembly for correct installation. This proposed AD would also
require you
RULES: Breeze Eastern Aerospace,
Published: 2002-10-03
This amendment adopts a new airworthiness directive (AD), that
is applicable to certain Breeze Eastern Aerospace rescue hoists. This
amendment requires a onetime inspection of the mounting brackets for
cracks, and, if necessary, replacement with serviceable parts. This
amendment is prompted by reports of cracked mounting brackets. The
actions
PROPOSED RULES: Pratt & Whitney,
Published: 2002-09-20
The Federal Aviation Administration (FAA) proposes to adopt a
new airworthiness directive (AD) that is applicable to certain serial
number (SN) Pratt and Whitney (PW) models PW4164, PW4168, and PW4168A
turbofan engines. This proposal would require operators to initially
and repetitively borescopeinspect 14th and 15th stage rubstrips
located on the
PROPOSED RULES: McDonnell Douglas,
Published: 2002-08-16
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain McDonnell Douglas Model
DC910, DC920, DC930, DC940, and DC950 series airplanes; and Model DC981 (MD81), DC982 (MD82), DC983 (MD83), DC987 (MD
87), and MD88 airplanes. This proposal would require replacement of
the emergency power switch knob on
RULES: Bell,
Published: 2002-08-07
This document publishes in the Federal Register an amendment
adopting Emergency Airworthiness Directive (EAD) 20020951, sent
previously to all known U.S. owners and operators of specified Bell
Helicopter Textron, Inc. (Bell) model helicopters by individual
letters. This AD requires cleaning and inspecting the tail rotor (T/R)
grip to determine if
Part II: Transportation Department, Federal Aviation Administration,
Published: 2002-07-19
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: Pratt & Whitney,
Published: 2002-07-10
The Federal Aviation Administration (FAA) proposes to adopt a
new airworthiness directive (AD) that is applicable to certain Pratt &
Whitney (PW) JT8D200 series turbofan engines. This proposal would
require the installation of stops on the fan exit guide vane case. This
proposal is prompted by reports of the flange between the fan duct case
and
RULES: Pratt & Whitney,
Published: 2002-06-26
This amendment supersedes an existing airworthiness directive
(AD), that is applicable to Pratt & Whitney PW4000 series turbofan
engines. That AD requires operators to perform initial and repetitive
inspections for cracking of high pressure compressor (HPC) front drum
rotors based on cycle usage. That AD also requires the removal from
service of
RULES: Sikorsky,
Published: 2002-06-07
This amendment supersedes an existing airworthiness directive
(AD) for Sikorsky Model S70A and S70C helicopters. That AD currently
requires inspecting a certain partnumbered main landing gear drag beam
(beam) for a crack, removing any cracked beam before further flight,
and reducing the torque of the jackpad mounting bolt retention nut
(nut) of
PROPOSED RULES: Diamond Aircraft Industries GmbH,
Published: 2002-05-20
This document proposes to adopt a new airworthiness directive
(AD) that would apply to all Diamond Aircraft Industries GmbH (Diamond)
Models H36 ``Dimona'', HK 36 R ``Super Dimona'', HK 36 TC, HK 36 TS,
HK 36 TTC, HK 36 TTCECO, HK 36 TTCECO (Restricted Category), and HK
36 TTS sailplanes. This proposed AD would require you to inspect the
long
RULES: McDonnell Douglas,
Published: 2002-05-02
This amendment adopts a new airworthiness directive (AD),
applicable to certain McDonnell Douglas Model DC981 (MD81), DC982
(MD82), DC983 (MD83), and MD88 airplanes. This AD requires an
inspection to verify proper installation of the support clamp of the
alternating current (AC) power relay feeder cables at the aft inboard
side of the electrical
PROPOSED RULES: McDonnell Douglas,
Published: 2002-01-04
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain McDonnell Douglas MD9030
series airplanes. This proposal would require replacement of the
existing strake feedthru and internal electrical connectors with new,
moisture resistant connectors. This action is necessary to prevent
moisture from
RULES: McDonnell Douglas; correction,
Published: 2002-01-02
Correction
In final rule document 0130203 beginning on page 64109 in the
issue of Wednesday, December 12, 2001, make the following corrections: Sec. 39.13 [Corrected]
1. On page 64111, in the second column, under heading Restatement of Requirements of AD 960205:
a. In paragraph (a):
(1) In the second line,
RULES: Boeing,
Published: 2002-02-04
This amendment adopts a new airworthiness directive (AD),
applicable to certain Boeing Model 707 and 720 series airplanes, that
requires installation of a new support structure for the trailing edge
beam and main landing gear uplock mechanism. This action is necessary
to prevent cracking in the frame and adjacent structure near the attach
bolt of
PROPOSED RULES: Pratt & Whitney,
Published: 2002-02-14
The Federal Aviation Administration (FAA) proposes to
supersede an existing airworthiness directive (AD), that is applicable
to Pratt & Whitney JT8D models 209, 217, 217A, 217C and 219
turbofan engines. That AD currently requires initial and repetitive
fluorescent magnetic particle inspections or fluorescent penetrant
inspections of the combustion
PROPOSED RULES: de Havilland,
Published: 2002-03-04
This document proposes to adopt a new airworthiness directive
(AD) that would apply to certain de Havilland Inc. (de Havilland)
Models DHC2 Mk. I, DHC2 Mk. II, and DHC2 Mk. III airplanes. This
proposed AD would require you to modify the elevator tip rib on each
elevator; repetitively inspect underneath the mass balance weights at
each elevator tip
RULES: Pilatus Aircraft Ltd.,
Published: 2002-03-27
This amendment adopts a new airworthiness directive (AD) that
applies to certain Pilatus Aircraft Ltd. (Pilatus) Models PC12 and PC
12/45 airplanes. This AD requires you to replace the metered connector
and oxygen tubing and related components in the rear seat bench. This
AD is the result of mandatory continuing airworthiness information
(MCAI)
RULES: General Electric Co.,
Published: 2002-04-10
This amendment supersedes an existing airworthiness directive
(AD), that is applicable to General Electric Company (GE) CF680A, CF6
80C2, and CF680E1 series turbofan engines. That AD currently requires
revisions to the Life Limits Section of the manufacturer's Instructions
for Continued Airworthiness (ICA) to include required inspection of
selected
