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RULES: British Aerospace,
Published: 2000-11-14
This amendment adopts a new airworthiness directive (AD),
applicable to all British Aerospace Model BAC 111 401/AK and 410/AQ
airplanes, that requires replacement of certain landing gear brake
accumulators with improved accumulators. The actions specified by this
AD are intended to prevent loss of hydraulic pressure and possible
structural damage
RULES: Learjet,
Published: 2000-11-01
This amendment adopts a new airworthiness directive (AD),
applicable to certain Learjet Model 45 series airplanes, that requires
repetitive application of grease to the rotating disk assembly of the
nose landing gear squat switch mechanism. Application of grease to the
squat switch assembly is necessary to prevent moisture contamination
and
RULES: British Aerospace,
Published: 2000-10-20
This amendment adopts a new airworthiness directive (AD),
applicable to all British Aerospace BAe Model ATP airplanes. This
action requires repetitive inspections to detect damage of the torque
link apex joint of the leftand righthand main landing gear (MLG); and
replacement of nuts, pins, and bolts with new parts, if necessary. This
action is
RULES: Boeing,
Published: 2000-10-06
This amendment adopts a new airworthiness directive (AD),
applicable to certain Boeing Model 757 series airplanes, 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 analytical loads that were
used during
PROPOSED RULES: Raytheon,
Published: 2000-09-26
This document proposes to adopt a new airworthiness directive
(AD) that would apply to certain Raytheon Aircraft Company (Raytheon)
Beech Models A36, B36TC, and 58 airplanes. The proposed AD would
require you to inspect for missing rivets on the right hand side of the
fuselage and, if necessary, install rivets. Raytheon has identified
several
PROPOSED RULES: Rolls-Royce plc,
Published: 2000-09-14
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to RollsRoyce, plc Tay 65015 and
65154 turbofan engines. This proposal would require initial and
repetitive visual and ultrasonic inspections of fan blades for cracks,
and, if necessary, replacement with serviceable parts. In addition,
this AD requires
PROPOSED RULES: Raytheon,
Published: 2000-09-07
This document proposes to adopt a new airworthiness directive
(AD) that would apply to certain Raytheon Aircraft Company (Raytheon)
Beech Model 58 airplanes. The proposed AD would require you to inspect
the rudder bellcrank interconnect tube for damage; replace or refinish
the interconnect tube, if necessary; and modify the floorboard. Four
PROPOSED RULES: Lockheed,
Published: 2000-08-30
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to all Lockheed Model 188A and 188C
series airplanes. This proposal would require a revision of the
Airplane Flight Manual (AFM) to add procedures for donning the
flightcrew oxygen masks when the cabin altitude warning horn is
activated. This action is
PROPOSED RULES: Boeing,
Published: 2000-05-19
This document proposes the supersedure of an existing
airworthiness directive (AD), applicable to all Boeing Model 777 series
airplanes, that currently requires repetitive testing of the engine
fire shutoff switch (EFSS) to determine if the override mechanism and
the switch handle are operational, and replacement of the EFSS, if
necessary. That AD
RULES: Boeing,
Published: 2000-05-26
This amendment supersedes an existing airworthiness directive
(AD), applicable to certain Boeing Model 747100, 200, 300, 747SR,
and 747SP series airplanes, that currently requires a onetime
inspection to detect cracking of the longeron splice fittings at
stringer 11, on the left and right sides at body station 2598, and
replacement of any cracked
RULES: Boeing,
Published: 2000-06-01
This amendment supersedes an existing airworthiness directive
(AD), applicable to certain Boeing Model 747 and 767 series airplanes,
that currently requires revising the FAAapproved Airplane Flight
Manual (AFM) to prohibit the use of certain fuels; and either replacing
an existing placard with a new placard, or replacing all dribble flow
fuel
RULES: Honeywell International Inc.,
Published: 2000-08-08
This amendment adopts a new airworthiness directive (AD),
applicable to Honeywell International, Inc. (formerly AlliedSignal Inc.
and Garrett Turbine Engine Company) high pressure compressor (HPC)
impellers installed on TFE7312, 3, 4, and 5 series turbofan
engines. This AD requires the removal and inspection of the HPC
impeller and, if necessary,
RULES: CFM International,
Published: 2000-06-13
This amendment supersedes an existing airworthiness directive
(AD), applicable to certain CFM International (CFMI) CFM56 series turbofan engines,
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that requires revisions to the Airworthiness Limitations Section of
applicable Engine Shop Manuals (ESMs). These revisions incorporate
required enhanced inspection of selected critical
PROPOSED RULES: Boeing,
Published: 2000-07-31
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain Boeing Model 777200
series airplanes. This proposal would require replacement of certain
components. This action is necessary to prevent corrosion of the axle
of the main landing gear, which could result in cracking and failure of
the axle, loss
RULES: BFGoodrich,
Published: 2000-07-21
This amendment adopts a new airworthiness directive (AD) that
is applicable to certain BFGoodrich main brake assemblies as installed
on Airbus Model A319 and A320 series airplanes. This action requires
repetitive inspections to determine the length of the wear indicator
pins of the main brake assemblies of the main landing gear (MLG);
followon
PROPOSED RULES: Eurocopter France,
Published: 2000-07-14
This document revises an earlier proposed airworthiness
directive (AD) for Eurocopter France Model AS332C, L, and L1
helicopters. That proposed AD would have required inspecting the
horizontal stabilizer spar tube (spar tube) for corrosion, hardness,
cracks, and scratches, and if necessary, replacing any unairworthy spar
tube and bushing with an
PROPOSED RULES: Cessna Aircraft Co.,
Published: 2000-12-29
This document proposes to adopt a new airworthiness directive
(AD) that would apply to certain Cessna Aircraft Company (Cessna) 150,
172, 175, 180, 182, 185, 206, 210, and 336 series airplanes. The
proposed AD would affect those airplanes equipped with 0513166 series
plastic control wheels. The proposed AD would require you to
repetitively inspect
RULES: Bell,
Published: 2000-12-11
This document publishes in the Federal Register an amendment
adopting superseding Airworthiness Directive (AD) 20002251, which was
sent previously by individual letters to all known U.S. owners and
operators of Model HH1K, TH1F, TH1L, UH1A, UH1B, UH1E, UH1F, UH
1H, UH1L, and UH1P; and Southwest Florida Aviation SW204, SW204HP,
SW205, and SW205A1
RULES: Raytheon,
Published: 2000-12-04
This amendment adopts a new airworthiness directive (AD) that
applies to certain Raytheon Aircraft Corporation (Raytheon) Beech
Models A36, B36TC, and 58 airplanes. This AD requires you to inspect
for misrouted rudder control cables; replace any worn or damaged guard
pins; replace any pulley brackets that are damaged or worn; and replace
any
RULES: Boeing,
Published: 2000-11-21
This amendment adopts a new airworthiness directive (AD),
applicable to certain Boeing Model 777200 series airplanes, that
requires replacement of certain components. The actions specified by
this AD are intended to prevent corrosion of the axle of the main
landing gear, which could result in cracking and failure of one or more
axles, loss of the
RULES: McDonnell Douglas,
Published: 2000-11-08
This amendment supersedes an existing airworthiness directive
(AD), applicable to certain McDonnell Douglas Model DC910, 20, 30,
40, and 50 series airplanes, that currently requires repetitive
radiographic and ultrasonic or eddy current inspections, and
modification of the upper cap of the front spar of the left and right
engine pylons, if
RULES: Short Brothers,
Published: 2000-10-30
This amendment supersedes an existing airworthiness directive
(AD), applicable to all Short Brothers Model SD360 SHERPA series
airplanes, that currently requires a onetime visual inspection to
determine the part number of the power control cable assemblies and
pulleys of the engine controls; and replacement of the power control
cable assemblies
RULES: Aerotechnik s.r.o.,
Published: 2000-10-17
This amendment adopts a new airworthiness directive (AD) that
applies to all Aerotechnik s.r.o. (Aerotechnik) Model L 13 SEH VIVAT
sailplanes. This AD requires you to inspect the tailfuselage hinge for
strength requirements and damage, and also requires you to replace any
hinge with damage or that does not meet strength requirements. This AD
is
RULES: Boeing,
Published: 2000-10-02
This amendment adopts a new airworthiness directive (AD) that
is applicable to certain Boeing Model 767 series airplanes powered by
RollsRoyce RB211 series engines. This action requires modification of
the nacelle strut and wing structure. This action is necessary to
prevent fatigue cracking in primary strut structure and consequent
reduced
PROPOSED RULES: Eurocopter Deutschland GMBH,
Published: 2000-09-20
This document revises an earlier proposed airworthiness
directive (AD) for Eurocopter Deutschland GMBH (ECD) Model BO105CB5
and BO105CBS5 helicopters that would have superseded an existing AD.
The existing AD requires, before further flight, creating a component
log card or equivalent record and determining the calendar age and
number of flights