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Part II: Department of Transportation, Federal Aviation Administration,
Published: 2000-07-27
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 of
the one phase remote control circuit breaker (RCCB) in the main
avionics compartment and center accessory compartment to determine its
part number and
RULES: Empresa Brasileira de Aeronautica S.A.,
Published: 2000-06-27
This amendment adopts a new airworthiness directive (AD) that
is applicable to certain EMBRAER Model EMB135 and EMB145 series
airplanes. This action requires revising the Airplane Flight Manual,
and eventual disconnection of the precooler differential pressure
switches. This action is necessary to prevent incorrect operation of
the precooler
PROPOSED RULES: Raytheon,
Published: 2000-07-05
This document provides additional time for the public to
comment on a proposal to supersede Airworthiness Directive (AD) 9912
02, which currently requires flight and operating limitations on
Raytheon Aircraft Corporation (Raytheon) Beech Models 45 (YT34), A45
(T34A, B45), and D45 (T34B) airplanes. AD 991202 resulted from a
report of an inflight
RULES: New Piper Aircraft, Inc.,
Published: 2000-12-18
This amendment supersedes Airworthiness Directive (AD) 80-26-
05, which currently requires you to repetitively inspect the main
landing gear (MLG) inboard door hinges and attachment angles for cracks
on certain The New Piper Aircraft, Inc. (Piper) PA31 series airplanes.
AD 802605 also requires you to replace any cracked MLG inboard door
hinge or
RULES: Bombardier,
Published: 2000-12-04
This amendment adopts a new airworthiness directive (AD) that
is applicable to certain Bombardier Model CL6001A11 (CL600), CL600 2A12 (CL601), and CL6002B16 (CL6013A, CL6013R, and CL604)
series airplanes. This action requires installation of protection
shields in the wheel bay of the main landing gear (MLG). This action is
necessary to prevent
RULES: McDonnell Douglas,
Published: 2000-11-27
This amendment supersedes an existing airworthiness directive
(AD), applicable to certain McDonnell Douglas Model DC910, 20, 30,
40, and 50 series airplanes and C9 (military) airplanes, that
currently requires a onetime visual inspection to determine if the
doorstops and corners of the doorjamb of the forward passenger door
have been modified,
RULES: Bombardier,
Published: 2000-11-14
This amendment adopts a new airworthiness directive (AD) that
is applicable to certain Bombardier Model CL6002B16 (CL604) series
airplanes. This action requires, among other actions, a general visual
inspection to detect gaps between the vane bracket(s) and the adjacent
skin; corrective actions, if necessary; and replacement of the six flap
vane
RULES: International Aero Engines AG,
Published: 2000-11-01
This amendment adopts a new airworthiness directive (AD) that
is applicable to certain International Aero Engines AG (IAE) V2500A5
and D5 series turbofan engines, identified by serial number. This
amendment requires the removal of engines assembled with an improper
High Pressure Turbine (HPT) module configuration from service prior to
accumulating
RULES: Boeing,
Published: 2000-10-20
This amendment adopts a new airworthiness directive (AD),
applicable to certain Boeing Model 747 series airplanes, that requires
a detailed visual inspection to detect evidence of wear or contact
between the precooler support fitting and link assembly; and rework and
reidentification of the fitting. This amendment is prompted by a report
of
PROPOSED RULES: Boeing,
Published: 2000-10-10
This document proposes the supersedure of an existing
airworthiness directive (AD), applicable to certain Boeing Model 757
200 series airplanes, that currently requires inspections to detect
cracking on the free edge of the tang, if necessary, and of the
fastener holes in the lower spar chord; and various followon actions.
That AD also provides for
PROPOSED RULES: Honeywell International Inc.,
Published: 2000-09-26
This document proposes the supersedure of an existing
airworthiness directive (AD), applicable to certain Honeywell
International Inc. (formerly AlliedSignal Inc. and Textron Lycoming
Inc.) LTS101 series turboshaft and LTP101 series turboprop engines. The
existing airworthiness directive (AD) superseded priority letter AD 94
1901 and currently
RULES: Eurocopter Deutschland,
Published: 2000-04-28
This amendment adopts a new airworthiness directive (AD) that
applies to Eurocopter Deutschland GMBH (ECD) Model MBBBK 117 A1, A3,
A4, B1, B2, and C1 helicopters. This AD requires modifying the
engine and transmission cowling doors (cowling doors). This amendment
is prompted by an emergency landing of an ECD Model MBBBK 117
helicopter after the
RULES: Airbus,
Published: 2000-09-08
This amendment adopts a new airworthiness directive (AD),
applicable to certain Airbus Model A300, A300600, and A310 series
airplanes, that requires replacement of the transformer rectifier units
(TRU) in the avionics compartment with new, improved TRU's. This
amendment is prompted by issuance of mandatory continuing airworthiness
information by a
PROPOSED RULES: McDonnell Douglas,
Published: 2000-09-01
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain McDonnell Douglas Model
DC8 series airplanes. This proposal would require replacing the toilet
flushing circuit breakers of the lavatory with new circuit breakers,
and marking applicable nameplates. This action is necessary to prevent
RULES: McDonnell Douglas,
Published: 2000-05-17
This amendment adopts a new airworthiness directive (AD),
applicable to all McDonnell Douglas Model DC10 series airplanes, that
requires a onetime detailed visual inspection to determine if wire
segments of the wire bundle routed through the feed through on the aft
side of the flight engineer's station are damaged or chafed, and
corrective
PROPOSED RULES: Raytheon,
Published: 2000-08-24
This document proposes to adopt a new airworthiness directive
(AD) that would apply to certain Raytheon Aircraft Corporation
(Raytheon) Beech Models A36, B36TC, and 58 airplanes. The proposed AD
would require you to inspect for misrouted rudder control cables;
replace any worn or damaged guard pins; replace any pulley brackets
that are damaged or
RULES: Boeing,
Published: 2000-05-26
This amendment adopts a new airworthiness directive (AD) that
is applicable to certain Boeing Model 737 series airplanes. This action
requires a onetime general visual inspection of the seat locks and
seat tracks of the flightcrew seats to ensure that the seats lock in
position and to verify that lock nuts and bolts of adequate length are
PROPOSED RULES: Raytheon,
Published: 2000-08-14
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain Model BAe.125, Hawker 800
(U125A), and Hawker 800XP series airplanes. This proposal would
require removal of existing clamps, bedding tapes, and rubber
connecting sleeves at the ends of the turbine air discharge duct and
the water separator, and
RULES: Eurocopter France,
Published: 2000-06-07
This amendment supersedes an existing airworthiness directive
(AD) that applies to Eurocopter France Model SA365N1, AS365N2, and
SA366G1 helicopters and that currently requires initial and repetitive
inspections of the tail rotor blade Kevlar tiebar (Kevlar tiebar) for
cracks or delaminations. This amendment requires the same actions
required by
RULES: British Aerospace,
Published: 2000-06-13
This amendment adopts a new airworthiness directive (AD),
applicable to certain British Aerospace BAe Model ATP airplanes, that
requires repetitive inspections to detect discrepancies of the downlock
support assembly and attachment of the nose landing gear (NLG), and of
the bulkhead and adjacent structure in the NLG bay; and corrective
action, if
RULES: McDonnell Douglas,
Published: 2000-07-31
This amendment adopts a new airworthiness directive (AD),
applicable to certain McDonnell Douglas Model DC10 series airplanes,
that requires a onetime detailed visual inspection of the galley power
feeder cables and fuselage structure at a certain station to detect
chafing or arcing damage to the cables and structure or to detect
arcing damage to
RULES: Mitsubishi,
Published: 2000-07-24
This amendment clarifies information contained in
Airworthiness Directive (AD) 20000915, which currently requires you
to incorporate modifications to the airplane operating systems on all
Mitsubishi Heavy Industries, Ltd. (Mitsubishi) MU2B series airplanes.
The Federal Aviation Administration (FAA) inadvertently omitted service
information from
PROPOSED RULES: Boeing,
Published: 2000-06-28
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain Boeing Model 747400
series airplanes. This proposal would require repetitive inspections to
detect fatigue cracking of the longeron splice fittings at stringer 11
on the left and right sides at body station 2598, and various followon
actions.
PROPOSED RULES: Boeing,
Published: 2000-12-29
This document proposes the adoption of a new airworthiness
directive (AD) that would apply to certain Boeing Model 737300, 737
400, 737500, 737600, 737700, 737800, 757200, 757200PF, 757200CB,
and 757300 series airplanes. This proposal would require a test of the
two electrical circuits that close the fuel shutoff valve on the wing
spar, and repair,
PROPOSED RULES: Rolls-Royce Corp.,
Published: 2000-12-12
This document proposes to adopt a new airworthiness directive
(AD), applicable to RollsRoyce Corporation, (formerly Allison Engine
Company), AE 2100 and AE 3007 series engines. This proposed AD would
require a onetime acid etch inspection of the 2nd stage high pressure
turbine (HPT) wheel for cracks. If the wheel is cracked, this proposed
AD would