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RULES: McDonnell Douglas,
Published: 2002-04-23
This amendment adopts a new airworthiness directive (AD) that
is applicable to one McDonnell Douglas Model DC931 airplane. This
action requires an inspection to determine if a certain alternating
current (AC) crosstie relay is installed; replacement of a certain AC
crosstie relay with a new AC crosstie relay; and repetitive cleaning,
inspection,
RULES: Gulfstream Aerospace,
Published: 2002-12-27
This amendment adopts a new airworthiness directive (AD),
applicable to all Gulfstream Aerospace LP Model Astra SPX and 1125
Westwind Astra series airplanes, that requires revising the Airplane
Flight Manual to advise the flightcrew to don oxygen masks as a first
and immediate step following a cabin altitude alert. This action is
necessary to
RULES: Aerostar,
Published: 2002-12-04
This amendment adopts a new airworthiness directive (AD) that
applies to certain Aerostar Aircraft Corporation (Aerostar) Models PA
60601 (Aerostar 601), PA60601P (Aerostar 601P), PA60602P (Aerostar
602P), and PA60700P (Aerostar 700P). This AD requires you to replace
RotoMaster and Rajay scavenge pumps with improved design Aerostar
scavenge pumps.
PROPOSED RULES: Fokker,
Published: 2002-11-21
This document proposes the adoption of a new airworthiness directive (AD) that is applicable to all
[[Page 70190]]
Fokker Model F.28 Mark 1000, 2000, 3000, and 4000 series airplanes.
This proposal would require repetitive inspections for discrepancies of
the internal fuselage skin panels located in the stub wing areas; and
corrective action if
PROPOSED RULES: de Havilland,
Published: 2002-11-08
This document proposes to adopt a new airworthiness directive
(AD) that would apply to certain Robert E. Rust (R.E. Rust) Models
DeHavilland DH.C1 Chipmunk 21, 22, and 22A airplanes. This proposed AD
would require you to check the airplane logbook to determine whether
certain modifications have been incorporated on the airplane and
incorporate the
RULES: Pilatus Aircraft Ltd.,
Published: 2002-10-21
This amendment adopts a new airworthiness directive (AD) that
applies to certain Pilatus Aircraft Ltd. (Pilatus) Model PC6
airplanes. This AD requires you to inspect the aileron assembly for
correct configuration and modify as necessary. This AD is the result of
mandatory continuing airworthiness information (MCAI) issued by the
airworthiness
RULES: Boeing,
Published: 2002-09-30
This amendment supersedes an existing airworthiness directive
(AD), applicable to all Boeing Model 737600, 700, 700C, 800, and
900 series airplanes; Model 747 series airplanes; and Model 757 series
airplanes, that currently requires revision of the FAAapproved
airplane flight manual (AFM) to advise the flight crew of certain
operating restrictions
PROPOSED RULES: Airbus,
Published: 2002-09-13
This document proposes the supersedure of an existing
airworthiness directive (AD), applicable to certain Airbus Model A330
and A340 series airplanes, that currently requires a onetime
inspection of the rail release pins and parachute pins of the escape
slide/raft pack assembly for correct installation, and corrective
actions, if necessary. This
Part II: See Coast Guard; See Federal Aviation Administration; See Federal Highway Administration; See Federal Transit Administration; See Maritime Administration; See Internal Revenue Service; Department of Transportation, Federal Aviation Administration,
Published: 2002-08-15
This amendment adopts a new airworthiness directive (AD),
applicable to certain Boeing Model 727 series airplanes that have been
converted from a passenger to a cargocarrying (``freighter'')
configuration, that requires require, among other actions, installation
of a failsafe hinge, redesigned main deck cargo door warning and power
control
RULES: Standard provisions added and CFR part revised; Correction,
Published: 2002-08-01
This document contains a correction to the final rule,
published in the Federal Register on July 22, 2002 (67 FR 47998). That
final rule incorporates several standard provisions previously included
in most airworthiness directives into the Code of Federal Regulations.
FAA will no longer include these provisions in individual airworthiness
PROPOSED RULES: Eurocopter France,
Published: 2002-07-19
This document proposes adopting a new airworthiness directive
(AD) for Eurocopter France (ECF) Model AS332C, AS332L, AS332L1, SA330F,
SA330G, and SA330J helicopters. This proposal would require inspecting
the tail rotor pitch change rod (change rod) bearing and replacing the
bearing if the bearing does not meet the specified tolerance. Also,
this
PROPOSED RULES: Pratt & Whitney,
Published: 2002-07-03
The Federal Aviation Administration (FAA) proposes to adopt a
new airworthiness directive (AD) that is applicable to Pratt & Whitney
Canada (PWC) models PW118, PW118A, PW118B, PW119B, PW119C, PW120,
PW120A, PW121, PW121A, PW123, PW123B, PW123C, PW123D, PW123E, PW123AF,
PW124B, PW125B, PW126, PW126A, PW127, PW127B, PW127E, PW127F, PW127G,
PW127H,
RULES: Boeing,
Published: 2002-06-18
This amendment adopts a new airworthiness directive (AD),
applicable to certain Boeing Model 757200, 200CB, and 200PF; and
767200, 300, and 300F series airplanes; that requires modification
of the right main landing gear and autospeedbrake control system to
provide an air/ground signal to the system. This action is necessary to
prevent uncommanded
RULES: Eurocopter Deutschland,
Published: 2002-05-30
This amendment adopts a new airworthiness directive (AD) for
Eurocopter Deutschland (Eurocopter) Model EC135 helicopters with
Turbomeca Arrius 2B1 engines installed. This action requires modifying
the engine electrical control unit (FADEC) software and the collective
linear transducer (LVDT). This amendment is prompted by a parameter
discrepancy
PROPOSED RULES: Boeing,
Published: 2002-05-15
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain Boeing Model 757200
series airplanes with stowage bins installed forward of door 2 at
Station 680. This proposal would require a onetime inspection to
determine if a certain intercostal is installed for support of the
overhead stowage bin(s) at
RULES: Boeing,
Published: 2002-04-26
This document publishes in the Federal Register an amendment
adopting airworthiness directive (AD) 20020852, that was sent
previously to all known U.S. owners and operators of all Boeing Model
737600, 700, and 700C series airplanes by individual notices. This
AD requires revising the Airplane Flight Manual (AFM) to prohibit
operating the airplane
RULES: McDonnell Douglas,
Published: 2002-01-04
This amendment adopts a new airworthiness directive (AD),
applicable to certain McDonnell Douglas Model DC981, 82, 83, and
87 series airplanes, and Model MD88 airplanes, that requires a
detailed visual inspection of certain wires to detect chafing and
preload; repair, if necessary; and modification of certain wire
assemblies. This action is
RULES: Airbus,
Published: 2002-01-30
This amendment adopts a new airworthiness directive (AD),
applicable to certain Airbus Model A319, A320, and A321 series
airplanes, that requires replacement of the trigger spring of the slide
bar on each of the passenger doors with a new, stronger trigger spring.
This action is necessary to prevent corrosion of the trigger spring on
the slide bar
RULES: Eurocopter France,
Published: 2002-02-11
This document publishes in the Federal Register an amendment
adopting Airworthiness Directive (AD) 20012655, which was sent
previously to all known U.S. owners and operators of Eurocopter France
(ECF) Model AS350B, AS350B1, AS350B2, AS350BA, AS350B3, AS350C, AS350D,
AS350D1, AS355E, AS355F, AS355F1, AS355F2, and AS355N helicopters by
individual
RULES: Dornier,
Published: 2002-02-20
This amendment adopts a new airworthiness directive (AD),
applicable to certain Dornier Model 328100 and 300 series airplanes,
that requires testing of the left and righthand potentiometer levers
of the aileron flight control system, and followon or corrective
action, as applicable. This amendment is necessary to prevent
detachment of an aileron
RULES: Sikorsky,
Published: 2002-03-18
This amendment supersedes an existing airworthiness directive
(AD) for Sikorsky Aircraft Corporation Model S76A helicopters that
currently requires a service life limit on certain landing gear parts
based on hours timeinservice (TIS). This amendment adds another
method of calculating the life limit for certain landing gear parts
based on cycles
RULES: McDonnell Douglas,
Published: 2002-04-02
This amendment adopts a new airworthiness directive (AD)
applicable to certain McDonnell Douglas Model DC1010, 10F, 15, 30,
30F (KC10A and KDC10), 40, and 40F series airplanes; and Model MD
1010F and MD1030F series airplanes. This action requires an
inspection of the parallel power feeder cables of the number 2
generator for chafing or structure
RULES: Fairchild,
Published: 2002-04-17
This amendment adopts a new airworthiness directive (AD) that
applies to certain Fairchild Aircraft, Inc. (Fairchild) SA226 and SA227
series airplanes equipped with SkidmoreWilheim Manufacturing Co.
(SkidmoreWilheim) (formerly Hydromotive) Model V1151000 brake master
cylinders. This AD requires you to replace these brake master cylinders
with new
PROPOSED RULES: Boeing,
Published: 2002-08-30
This document proposes the adoption of a new airworthiness [[Page 55740]]
directive (AD) that is applicable to certain Boeing Model 747 series
airplanes powered by GE CF680C2 series engines. This proposal would
require repetitive inspections and torque checks to find discrepancies
of the fasteners that attach the diagonal brace fittings of the lower
PROPOSED RULES: Pilatus Aircraft Ltd.,
Published: 2002-12-18
This document proposes to adopt a new airworthiness directive
(AD) that would apply to all Pilatus Aircraft Ltd. (Pilatus) Models PC
12 and PC12/45 airplanes. This proposed AD would require you to
repetitively replace the nose landing gear (NLG) drag link righthand
part every 4,000 landings until an improved design NLG drag link right
hand part is