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RULES: Boeing,
Published: 2001-04-23
This amendment supersedes two existing airworthiness
directives (AD), applicable to all Boeing Model 707 and 720 series
airplanes, that currently require inspections of the upper chords of
the wing front and rear spars, repair, if necessary, and application of
corrosion inhibitor to the inspected areas. This amendment requires
repetitive
PROPOSED RULES: McDonnell Douglas,
Published: 2001-04-19
This document proposes the supersedure of an existing
airworthiness directive (AD), applicable to certain McDonnell Douglas
Model MD11 series airplanes, that currently requires a revision of the
Airplane Flight Manual to alert the flightcrew that both flight
management computers (FMC) must be installed and operational. This
action would require an
RULES: Fokker,
Published: 2001-08-06
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 inspection to detect the
presence of filler plates of the engine support fittings, and
corrective action, if necessary. The actions specified by this AD are
intended to detect and
RULES: Boeing,
Published: 2001-07-31
This amendment supersedes an existing airworthiness directive
(AD), applicable to all Boeing Model 767 series airplanes, that
currently requires revising the Airplane Flight Manual (AFM) to include
procedures that will ensure that the center tank fuel pumps are not
operated with less than 1,000 pounds of fuel in the center tank. This
amendment
RULES: Boeing,
Published: 2001-08-27
This amendment adopts a new airworthiness directive (AD);
applicable to certain Boeing Model 737100, 200, and 200C series
airplanes; that requires repetitive inspections of certain floor beams
and transverse beams, and corrective actions, if necessary. For certain
airplanes, this AD also provides optional terminating action for the
repetitive
RULES: Boeing,
Published: 2001-07-24
This amendment adopts a new airworthiness directive (AD),
applicable to certain Boeing Model 737100 and 200 series airplanes,
that requires repetitive inspections to find fatigue cracking in the
main deck floor beams located at certain body stations, and repair, if
necessary. This AD also provides for optional terminating action for
the repetitive
PROPOSED RULES: Pilatus Aircraft Ltd.,
Published: 2001-01-02
This document proposes to supersede Airworthiness Directive
(AD) 980822, which currently requires inspecting the elevator and
rudder attachment brackets for cracks and corrosion, and replacing any
cracked or corrosiondamaged parts on certain Pilatus Aircraft Ltd.
(Pilatus) Model PC7 airplanes. AD 980822 resulted from mandatory
continuing
PROPOSED RULES: Airbus,
Published: 2001-01-10
This document proposes to revise an existing airworthiness
directive (AD), applicable to all Airbus Model A300600 series
airplanes, that currently requires repetitive ultrasonic inspections to
detect cracks on the forward fittings in the radius of frame 40
adjacent to the tension bolts in the center section of the wings, and
various followon
PROPOSED RULES: Fokker,
Published: 2001-01-16
This document proposes the supersedure of an existing
airworthiness directive (AD), applicable to all Fokker Model F.28 Mark
0070 and Mark 0100 series airplanes, that currently requires revising
the Airplane Flight Manual (AFM) to provide the flightcrew with
instructions not to arm the liftdumper system prior to commanding the
landing gear to
RULES: Fairchild,
Published: 2001-10-12
This amendment adopts a new airworthiness directive (AD) that
applies to certain Fairchild Aircraft SA226 and SA227 series airplanes.
This AD requires you to replace the brake shuttle valves with parts of
improved design and install a shield over the hydraulic lines. This AD
also requires replacing the rubber fuel hose with a metal device for
PROPOSED RULES: McDonnell Douglas,
Published: 2001-10-05
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 an inspection to
detect discrepancies of the wire bundles in the avionics compartment in
the vicinity of the pedestal extension area of the First Officer's
seat; and
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 proposed AD would require replacing
certain flight warning computers (FWCs) with improved FWCs. This
proposed AD is prompted by mandatory continuing airworthiness
information issued by a
PROPOSED RULES: Dornier,
Published: 2001-08-21
This document proposes to adopt a new airworthiness directive
(AD) that would apply to certain Dornier Luftfahrt GmbH (Dornier) Models 228100, 228101, 228200, 228201, 228202, and 228212
airplanes. The proposed AD would require you to repetitively inspect
the horizontal stabilizer skin and ribs for damage and cracks and
repair any damaged skin or
PROPOSED RULES: British Aerospace,
Published: 2001-07-18
This document proposes to supersede Airworthiness Directive
(AD) 981303, which currently requires repetitive inspections of the
main landing gear (MLG) hinge fittings, support angles, and attachment
bolts on British Aerospace H.P. 137 Mk1, Jetstream series 200, and
Jetstream Model 3101 airplanes. This AD also requires eventual
installation of
RULES: Bombardier,
Published: 2001-07-06
This amendment adopts a new airworthiness directive (AD),
applicable to certain Bombardier Model DHC8102, 103, and 301 series
airplanes, that requires repair of the flight deck angle. The actions
specified by this AD are intended to prevent the flight deck angle from
interfering with the clevis of the roll control disconnect cable, which
could
RULES: Airbus,
Published: 2001-06-27
This amendment adopts a new airworthiness directive (AD) that
is applicable to all Airbus Model A330 and A340 series airplanes. This
action requires revising the Airplane Flight Manual to advise the
flight crew of appropriate procedures to follow in the event of lost or
erroneous airspeed indications. This action is necessary to prevent
PROPOSED RULES: General Electric Co.,
Published: 2001-06-12
The Federal Aviation Administration (FAA) proposes to
supersede an existing airworthiness directive (AD), applicable to
certain General Electric Company (GE) GE90 series turbofan engines.
That AD currently requires inspecting and purging the P3B and Ps3 lines
and associated fittings and ports of moisture. This proposal would
allow the installation
RULES: Sikorsky,
Published: 2001-12-20
This amendment adopts a new airworthiness directive (AD) for
Sikorsky Aircraft Corporation (Sikorsky) Model S76B and S76C
helicopters. This action requires modifying the electrical power
distribution system to change the source of the 28 volts supplied to
Nos. 1 and 2 attitude and heading reference (AHRS) WARN circuits. This
amendment is prompted
RULES: Bell,
Published: 2001-12-11
This amendment revises an existing airworthiness directive
(AD) for Bell Helicopter Textron, Inc. (BHTI) Model 206A, 206B, 206A1,
206B1, 206L, and 206L1 helicopters that currently establishes a
retirement life for the main rotor trunnion (trunnion) based on hours
timeinservice (TIS). This amendment retains those requirements but
revises the AD to
PROPOSED RULES: Boeing,
Published: 2001-11-28
This document proposes the supersedure of an existing
airworthiness directive (AD), applicable to certain Boeing Model 777
series airplanes, that currently requires repetitive inspections to
detect cracking of the coveskin on the outboard leading edge slats, and
corrective actions, if necessary. The existing AD also provides for an
optional
RULES: Bell,
Published: 2001-02-13
This amendment adopts a new airworthiness directive (AD) for
Bell Helicopter Textron, Inc. (BHTI) Model 214B and 214B1 helicopters.
This action requires, within 10 hours timeinservice (TIS),
determining the hours TIS for certain main rotor outboard strap fitting
assemblies and creating appropriate records. This action also requires,
if any main
PROPOSED RULES: Boeing,
Published: 2001-02-15
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain Boeing Model 727, 737,
757200, 757200CB, and 757300 series airplanes. This proposal would
require modification of the latch assembly of the escape slides. For
certain airplanes, this proposal would also require installation of a
cover assembly
RULES: Bombardier,
Published: 2001-02-22
This amendment supersedes an existing airworthiness directive
(AD), applicable to certain Bombardier Model CL6002B19 series
airplanes, that currently requires, among other actions, certain
revisions to the Airplane Flight Manual; and removal of all elevator
flutter dampers. That AD also requires installation of new elevator
flutter dampers, and
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 767300 series
airplanes modified by supplemental type certificate (STC) SA5765NM or
SA5978NM. This proposal would require removal of the inflight
entertainment (IFE) system installed by those STC's. This action is
necessary to prevent the
RULES: General Electric Co.,
Published: 2001-05-18
This amendment adopts a new airworthiness directive (AD), that
is applicable to General Electric Co. (GE) CF680C2 turbofan engines
with certain stage 1 high pressure turbine (HPT) rotor disks installed.
This amendment requires initial and repetitive inspections of certain
HPT rotor disks for cracks in the bottom of the dovetail slot. This