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Part III: Department of Transportation, Federal Aviation Administration,
Published: 2001-03-02
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to all Boeing Model 747400 series
airplanes modified by supplemental type certificate SA8843SW. This
proposal would require modifying the passenger entertainment system
(PES) installed by that STC and revising the Airplane Flight Manual.
This action is
RULES: Boeing,
Published: 2001-05-24
This amendment adopts a new airworthiness directive (AD) that
is applicable to certain Boeing Model 737, 747, 757, 767, and 777
series airplanes. This action requires repetitive inspections of any
chemical oxygen generators and/or passenger, attendant, or lavatory
service unit assemblies of the passenger oxygen system that have been
replaced, to
PROPOSED RULES: McDonnell Douglas,
Published: 2001-05-15
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain McDonnell Douglas Model
717 series airplanes. This proposal would require repetitive
inspections of the rod ends of the spoiler holddown actuators for
breakage along the intersection of the thread runout and the outer
spherical surface of the
PROPOSED RULES: Fokker,
Published: 2001-05-04
This document revises an earlier proposed airworthiness
directive (AD), applicable to certain Fokker Model F.28 Mark 1000,
2000, 3000, and 4000 series airplanes. The proposed AD would have
required an eddy current inspection to detect cracks in the upper
girder of the two main landing gear (MLG) brackets; and repair of a
cracked bracket followed
PROPOSED RULES: Airbus,
Published: 2001-03-29
This document proposes the supersedure of an existing
airworthiness directive (AD), applicable to certain Airbus Model A320
series airplanes, that currently requires modification of the autopilot
mode engagement/disengagement lever of the rudder artificial feel unit.
This action would require a different modification of the lever. It
would also
RULES: Boeing,
Published: 2001-04-02
This amendment adopts a new airworthiness directive (AD),
applicable to certain Boeing Model 767 series airplanes powered by
General Electric engines, that requires modification of the nacelle
strut and wing structure. This amendment is prompted by reports
indicating that the actual operational loads applied to the nacelle are
higher than the
RULES: Boeing,
Published: 2001-04-23
This amendment supersedes an existing airworthiness directive
(AD), applicable to certain Boeing Model 737200 and 300 series
airplanes, that currently requires a onetime inspection to detect
cracks of the lower frames and reinforcing angles of the main deck
cargo door where the door latch fittings attach between certain
fuselage stations and water
RULES: McDonnell Douglas,
Published: 2001-04-10
This amendment adopts a new airworthiness directive (AD) that
is applicable to all McDonnell Douglas Model MD11 series airplanes
equipped with Pratt & Whitney Model PW4400 series engines. This action
requires revising the Airplane Flight Manual (AFM) to advise the flight
crew of applicable operational limits. This action is necessary to
ensure
RULES: Fokker,
Published: 2001-09-06
This amendment adopts a new airworthiness directive (AD),
applicable to all Fokker Model F.28 Mark 1000, 2000, 3000, and 4000
series airplanes, that requires a onetime eddy current inspection for
cracks of the fuselage butt joint which is forward of the emergency
exits on the left and righthand sides of the airplane at the level of
stringers
RULES: Pratt & Whitney,
Published: 2001-07-31
This amendment adopts a new airworthiness directive (AD), that
is applicable to Pratt & Whitney (PW) JT8D series turbofan engines.
This amendment requires removing certain 2nd stage compressor disks,
specified by part number (P/N) and serial number (SN), from service.
This amendment is prompted by a report from PW of a number of JT8D
engine 2nd
RULES: Boeing,
Published: 2001-08-27
This amendment adopts a new airworthiness directive (AD),
applicable to certain Boeing Model 707 and 720 series airplanes, that
requires replacement of wiring for the fuel boost pumps and override pumps with new
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wiring, installation of Teflon sleeving on the wiring, and associated
actions. This amendment also requires repetitive
RULES: Boeing,
Published: 2001-07-24
This amendment adopts a new airworthiness directive (AD),
applicable to certain Boeing Model 727, 737, 757200, 757200CB, and
757300 series airplanes. This AD requires modification of the latch
assembly of the escape slides. For certain airplanes, this AD also
requires installation of a cover assembly on the trigger housing of the
inflation
PROPOSED RULES: SOCATA-Groupe AEROSPATIALE,
Published: 2001-01-02
This document proposes to adopt a new airworthiness directive
(AD) that would apply to certain SOCATAGroupe AEROSPATIALE (Socata)
Model TBM 700 airplanes. The proposed AD would require you to apply
Loctite on attaching bolt threads of inboard, central, and outboard
carriages; increase tightening torques; and replace central carriage
attaching
RULES: Boeing,
Published: 2001-10-30
This amendment supersedes an existing airworthiness directive
(AD), applicable to all Boeing Model 747 series airplanes, that
currently requires, for certain airplanes, revising the Airplane Flight
Manual, and, for all airplanes, performing repetitive inspections for
wear or damage of the inlet check valves and inlet adapters of the
PROPOSED RULES: Saab,
Published: 2001-01-16
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain Saab Model SAAB 2000
series airplanes. This proposal would require a modification involving
nondestructive test inspections of the 34 fastener holes in each rear
wing spar, corrective action, if necessary, and cold working of the
holes to
RULES: Pratt & Whitney,
Published: 2001-10-12
This amendment adopts a new airworthiness directive (AD), that
is applicable to certain models of Pratt & Whitney PW4000 series
turbofan engines. This amendment requires operators to perform initial
and repetitive inspections for cracking of high pressure compressor
(HPC) front drum rotors based on cycle usage. This amendment also
requires the
PROPOSED RULES: McDonnell Douglas,
Published: 2001-10-05
This document proposes the supersedure of an existing
airworthiness directive (AD), applicable to certain McDonnell Douglas
Model MD11 and MD11F series airplanes, that currently requires
replacement of the existing terminal strips and supports above the main
cabin area; and installation of spacers between terminal strips and
mounting brackets in
PROPOSED RULES: Airbus,
Published: 2001-09-25
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 replacement of
the lowpressure solenoid valve for the crew oxygen supply with a
modified valve. This action is necessary to prevent faulty operation of
the
RULES: Airbus,
Published: 2001-08-20
This amendment supersedes an existing airworthiness directive
(AD), which is applicable to all Model A320 series airplanes, that
currently requires repetitive measurements of the deflection of the
elevator trailing edge; inspections of the elevator servo controls and
their attachments; and replacement of worn or damaged parts, if
necessary. This
RULES: Gulfstream,
Published: 2001-07-17
This amendment adopts a new airworthiness directive (AD),
applicable to certain Gulfstream Model GV series airplanes, that
requires repetitively replacing the existing nose wheel steering
actuator with a new or reworked actuator having the same part number.
The actions specified by this AD are intended to prevent loss of nose
wheel steering
RULES: Bombardier,
Published: 2001-07-06
This amendment supersedes an existing airworthiness directive
(AD), applicable to certain Bombardier Model DHC8200 and 300 series
airplanes, that currently requires repetitive inspections to detect
chafing or arcing damage to the cable/wire and fuel tube assemblies on
the righthand side of each engine, and replacement with new
components, if
RULES: Bell,
Published: 2001-06-27
This amendment adopts a new airworthiness directive (AD) for
Bell Helicopter Textron Canada (BHTC) Model 407 helicopters that
requires replacing certain cockpit warning horns. This amendment is
prompted by reports that pilots have had difficulty in distinguishing
between the FADEC Fail horn, the Engine Out horn, and the Low Rotor RPM
horn. The
PROPOSED RULES: Honeywell International, Inc.,
Published: 2001-06-12
The Federal Aviation Administration (FAA) proposes to adopt a
new airworthiness directive (AD) that is applicable to Honeywell
International, Inc., (formerly AlliedSignal, Inc., and Textron
Lycoming) T5313B series, T5317 series, and former military T53 series,
turboshaft engines having certain serial number centrifugal compressor
impellers,
PROPOSED RULES: Cessna; withdrawn,
Published: 2001-12-20
This document withdraws a notice of proposed rulemaking (NPRM)
that would have applied to certain Cessna Aircraft Company (Cessna)
150, 172, 175, 180, 182, 185, 206, 210, and 336 series airplanes. The
proposed AD would have affected those airplanes equipped with 0513166
series plastic control wheels. The proposed AD would have required you
to
RULES: Cirrus Design Corp.,
Published: 2001-12-11
This amendment adopts a new airworthiness directive (AD) that
applies to certain Cirrus Design Corporation (CDC) Models SR20 and SR22
airplanes. This AD requires you to inspect one time for understrength
rivets on the elevator torque tube and rudder hinge and replace any
understrength rivets. This AD is the result of CDC notifying FAA that