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PROPOSED RULES: McDonnell Douglas,
Published: 2001-02-20
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain McDonnell Douglas Model
MD11 series airplanes. This proposal would require a onetime general
visual inspection of the electrical wiring of the right side of the
cockpit to determine if the electrical wiring is chafing against the
observer
PROPOSED RULES: Boeing,
Published: 2001-06-05
This document revises an earlier proposed airworthiness
directive (AD), applicable to certain Boeing Model 767 series
airplanes, that would have required a onetime detailed visual
inspection of certain wire bundles located in the aft section of the
strut forward fairing panel of both engine struts to detect chafing
damage, and repair or
PROPOSED RULES: Kaman Aerospace Corp.,
Published: 2001-03-05
This document proposes the adoption of a new airworthiness
directive (AD) for Kaman Aerospace Corporation (Kaman) Model K1200
helicopters. The AD would require reducing the life limit of the rotor
shaft and teeter pin assembly, and establishing a life limit for the
flap clevis. This proposal is prompted by the discovery of cracks in
parts that
RULES: Air Tractor, Inc.,
Published: 2001-05-16
This amendment supersedes Airworthiness Directive (AD) 2000-
1451, which requires inspection of the wing lower spar cap for cracks
on Air Tractor, Inc. (Air Tractor) Models AT501, AT502, and AT502A
airplanes, and modification or replacement of any cracked wing lower
spar cap. This AD lowers the safe life for the wing lower spar cap on
Air Tractor
PROPOSED RULES: Boeing,
Published: 2001-03-21
This document proposes the supersedure of an existing
airworthiness directive (AD), applicable to certain Boeing Model 747
series airplanes powered by Pratt & Whitney JT9D7 series engines, that
currently requires detailed visual inspections of the lugs on the
bulkhead fitting of the rear engine mount, and corrective action, if
necessary. The
PROPOSED RULES: Honeywell International, Inc.,
Published: 2001-05-02
The Federal Aviation Administration (FAA) proposes to
supersede two existing airworthiness directives (ADs), applicable to
Honeywell International Inc. (formerly AlliedSignal Inc. and Garrett
Turbine Engine Co.) TFE7312, 3, and 4 series turbofan engines. Those
AD's currently require removing certain fan rotor discs from service in
accordance with
RULES: Rolls-Royce Corp.,
Published: 2001-04-27
This amendment adopts a new airworthiness directive (AD) that
is applicable to RollsRoyce Corporation (formerly Allison Engine
Company) AE 3007A, AE 3007A1/1, AE 3007A1/2, AE 3007A1, AE 3007A1/3, AE
3007A1P, and AE 3007A3 turbofan engines. This action requires initial
and repetitive inspections for bearing material contamination of the
engine oil
RULES: Dornier,
Published: 2001-04-25
This amendment revises an existing airworthiness directive
(AD), applicable to all Dornier Model 328100 series airplanes, that
currently requires revising the Airworthiness Limitations Section of
the Instructions for Continued Airworthiness to incorporate life limits
for certain items and inspections to detect fatigue cracking in certain
PROPOSED RULES: Bombardier,
Published: 2001-04-12
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain Bombardier Model DHC8
102, 103, and 301 series airplanes. This proposal would require
repair of the flight deck angle. This action is necessary to prevent
the flight deck angle from interfering with the clevis of the roll
control disconnect
RULES: Airbus,
Published: 2001-08-06
This amendment adopts a new airworthiness directive (AD),
applicable to certain Airbus Model A319, A320, and A321 series
airplanes, that requires modifications of route segregation between the
low voltage wire bundles of the fuel quantity indicating system and the
high voltage wire bundles of the ground power control unit. This
amendment is
RULES: Rolls-Royce Corp.,
Published: 2001-08-31
This amendment adopts a new airworthiness directive (AD), that
is applicable to RollsRoyce Corporation (formerly Allison Engine
Company) AE 2100 turboprop and AE 3007 turbofan series engines. This
amendment requires a onetime acid etch inspection of the 2nd stage
high pressure turbine (HPT) wheel for evidence of damaged material
indicating that a
RULES: Raytheon,
Published: 2001-08-29
This amendment adopts a new airworthiness directive (AD),
applicable to certain Raytheon Model DH.125, HS.125, BH.125, and BAe.
125 (U125 and C29A) series airplanes; Model Hawker 800, Hawker 800
(U125A), Hawker 800XP, and Hawker 1000 airplanes, that requires an
inspection for cracking or corrosion of the cylinder head lugs of the
main landing gear
PROPOSED RULES: BAE Systems (Operations) Ltd.,
Published: 2001-08-23
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain BAe Systems (Operations)
Limited Model Avro 146RJ series airplanes. This proposal would require
a onetime inspection of the S4 and S5 static pipes of the pitot static
system for discrepancies, and followon corrective actions, if
necessary. This
RULES: McDonnell Douglas,
Published: 2001-11-13
This amendment adopts a new airworthiness directive (AD),
applicable to certain McDonnell Douglas Model DC981, 982, 983,
and 987 series airplanes; Model MD88 airplanes; and Model MD9030
series airplanes. This action requires repetitive inspections of the
electric motors (or motors) of the auxiliary hydraulic pump for
electrical resistance,
PROPOSED RULES: Airbus,
Published: 2001-01-09
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to all Airbus Model A300 B2 and A300
B4 series airplanes, and all A300 B4600, A300 B4600R, and A300 F4
600R (A300600) series airplanes. For certain airplanes, this proposal
would require modifying the frame 40 aft fittings. For all airplanes,
this proposal
PROPOSED RULES: Airbus,
Published: 2001-10-26
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain Airbus Model A319, A320,
and A321 series airplanes. This proposal would require a onetime
inspection of the forward and aft lower bogies of the left and right
hand sliding windows of the flightcrew compartment for the presence of
a lock pin. If
RULES: Boeing,
Published: 2001-01-24
This amendment adopts a new airworthiness directive (AD),
applicable to certain Boeing Model 737300, 400, and 500 series
airplanes, that requires repetitive inspections to detect cracking of
certain areas of the forward pressure bulkhead, and repair, if
necessary. This amendment also requires certain preventive
modifications, which, when
PROPOSED RULES: General Electric Co.,
Published: 2001-10-10
The FAA proposes to supersede an existing airworthiness
directive (AD), which is applicable to General Electric Company (GE)
GE90 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 enhanced inspection
of selected critical
RULES: Bell,
Published: 2001-10-03
This amendment adopts a new airworthiness directive (AD) for
Bell Helicopter Textron Canada (BHTC) Model 206L4 helicopters that
requires installing a high altitude tail rotor static stop yield
indicator (indicator) to allow operators to detect excessive bending
loads sustained by the tail rotor yoke. A preflight check of the
indicator is also
RULES: McDonnell Douglas,
Published: 2001-08-22
This amendment supersedes an existing airworthiness directive
(AD), applicable to certain McDonnell Douglas Model MD11 series
airplanes, that currently requires replacement of the air driven
generator (ADG) wire assembly with a new, increased length wire
assembly. This amendment requires, among other actions, replacement of
the existing ADG wire
RULES: McDonnell Douglas,
Published: 2001-07-23
This amendment adopts a new airworthiness directive (AD),
applicable to certain McDonnell Douglas Model DC910 and 30 series
airplanes. This action requires replacement of a certain circuit
breaker in the navigation transfer circuit located on the overhead
circuit breaker panel with a certain new circuit breaker; and
installation of a new
RULES: Boeing,
Published: 2001-07-11
This amendment adopts a new airworthiness directive (AD),
applicable to all Boeing Model 757200 series airplanes modified by
Supplemental Type Certificate (STC) SA1727GL, that requires
deactivation of the airtoground telephone system approved by that
STC. This action is necessary to prevent the inability of the flight
crew to remove power from the
RULES: Eurocopter France,
Published: 2001-06-27
This amendment adopts a new airworthiness directive (AD) for
Eurocopter France Model AS332L2 helicopters. This AD requires, at
specified time intervals, visually inspecting the main rotor blade
sleeve yoke (sleeve) for cracks, corrosion, fretting, or bonding
separation; the bearing surface of the metal bushing (bushing) for
fretting or cracks; and
RULES: Boeing,
Published: 2001-06-15
This amendment adopts a new airworthiness directive (AD),
applicable to certain Boeing Model 777200 series airplanes, that
requires repetitive detailed visual and ultrasonic inspections of the
lower flange of the flaperon inboard support to find cracking, and
corrective actions, if necessary. This AD also requires a modification,
which terminates
PROPOSED RULES: Pratt & Whitney,
Published: 2001-12-27
This action revises an earlier proposed airworthiness
directive (AD), applicable to certain Pratt & Whitney (PW) PW2000
series turbofan engines, that would supersede an existing airworthiness
directive (AD) by modifying the airworthiness limitations section of
the manufacturer's manual and an air carrier's approved continuous
airworthiness