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PROPOSED RULES: Eurocopter France,
Published: 2000-07-20
This document proposes the supersedure of an existing
airworthiness directive (AD) that applies to Eurocopter France Model
AS350B, BA, B1, B2, C, D, and D1, and AS355E, F, F1, and F2
helicopters. That AD currently requires inspections of the main rotor
head components, the main gearbox (MGB) suspension bars, and the ground
resonance prevention
PROPOSED RULES: McDonnell Douglas,
Published: 2000-07-13
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
opening the circuit breaker of the pneumatic sense line heater tape,
installing an inoperative ring, and coiling and stowing the electrical
wire to the circuit
RULES: Airbus,
Published: 2000-12-21
This amendment adopts a new airworthiness directive (AD),
applicable to all Airbus Model A300 B2 and B4 series airplanes, and
Model A300600 series airplanes, that requires verifying the correct
location of the labels of the hydraulic pipes supplying the strut
unlocking actuator of the lefthand main landing gear (MLG), and of the
pipes of the left
PROPOSED RULES: Fairchild,
Published: 2000-12-05
This document proposes to revise an earlier proposed
airworthiness directive (AD) that would apply to certain Fairchild
Aircraft SA226 and SA227 series airplanes. The earlier NPRM would have
required you to replace the brake shuttle valves with parts of improved
design and install a shield over the hydraulic lines. The earlier NPRM
resulted from a
RULES: Bombardier,
Published: 2000-11-28
This amendment supersedes an existing airworthiness directive
(AD), applicable to certain Bombardier Model DHC8102, 103, and 301
series airplanes, that currently requires a onetime inspection for
wear and breakage of wire segments of the individual lighting units of
the ceiling and sidewall lights, and replacement of any damaged wiring.
The
RULES: Bell,
Published: 2000-11-15
This document publishes in the Federal Register an amendment
adopting Airworthiness Directive (AD) 20001852 which was sent
previously to all known U.S. owners and operators of Bell Helicopter
Textron, Inc. (BHTI)manufactured Model OH13E, OH13H, and OH13S
helicopters by individual letters. This AD requires a liquid penetrant
or eddy current
PROPOSED RULES: British Aerospace,
Published: 2000-11-02
This document proposes to adopt a new airworthiness directive
(AD) that would apply to all British Aerospace HP137 Mk1, Jetstream
series 200, and Jetstream Models 3101 and 3201 airplanes that are
equipped with certain main landing gear (MLG) radius rods. The proposed
AD would require inspection of the MLG radius rods for cracks with
replacement of
RULES: Pratt & Whitney,
Published: 2000-10-24
This amendment supersedes an existing airworthiness directive
(AD), applicable to certain Pratt & Whitney JT8D series turbofan engines, that
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currently requires revisions to the Time Limits Section (TLS) of the
JT8D Turbofan Engine Manual to include required enhanced inspection of
selected critical lifelimited parts at each piecepart
PROPOSED RULES: General Electric Co.,
Published: 2000-10-12
This document proposes to revise an existing airworthiness
directive (AD), applicable to certain GE turbofan engines. That AD
currently requires initial and repetitive inspections of high pressure
compressor (HPC) rear shafts and installation of a certain rear shaft
flange bolt configuration. This action would add additional HPC rear
shaft part
PROPOSED RULES: Bombardier,
Published: 2000-09-27
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain Bombardier Model DHC8
100, 200, and 300 series airplanes. This proposal would require
inspecting the endcaps of the main landing gear selector valve for
leaks of hydraulic oil and, if leaks are detected, replacing the
leaking endcaps or the
PROPOSED RULES: Bombardier,
Published: 2000-04-28
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to all Bombardier Model DHC7100,
and DHC8100, 200, and 300 series airplanes. This proposal would
require a onetime inspection of maintenance records to determine the
method used during the most recent weight and balance check of the
airplane and, if
RULES: Allison Engine Co.,
Published: 2000-05-05
This amendment adopts a new airworthiness directive (AD) that
is applicable to certain Allison Engine Company AE 3007 series turbofan
engines. This AD would require removal of certain cone shafts from
service before exceeding new cyclic life limits and replacement with
serviceable parts. This amendment is prompted by additional testing and
low
PROPOSED RULES: Siam Hiller Holdings, Inc.,
Published: 2000-08-31
This document proposes the adoption of a new airworthiness
directive (AD) for Siam Hiller Holdings, Inc. (Hiller), formerly
Rogerson Hiller Corporation, Model UH12, UH12A, UH12B, UH12C, UH
12D, UH12E, UH12El, UH12L, and UH12L4 helicopters. The AD would
require replacing all undrilledshank bolts at pivoting joints in the
control system linkage with
RULES: Eurocopter Deutschland GMBH,
Published: 2000-08-28
This amendment supersedes an existing airworthiness directive (AD) that applies to Eurocopter Deutschland
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GMBH (ECD) Model BO105A, BO105C, BO105 C2, BO105 CB2, BO105 CB
4, BO105S, BO105 CS2, BO105 CBS2, BO105 CBS4, and BO105LS A1
helicopters. That AD requires creating a component log card or
equivalent record and determining the
RULES: British Aerospace and Jetstream,
Published: 2000-08-21
This amendment adopts a new airworthiness directive (AD) that
applies to all British Aerospace HP137 Mk1, Jetstream series 200, and
Jetstream Models 3101 and 3201 airplanes. This AD requires you to
inspect the nose wheel steering system to assure that the free play
between the steering handle or knob and the nose wheels is within
acceptable
RULES: Dassault,
Published: 2000-06-01
This amendment adopts a new airworthiness directive (AD) that
is applicable to all Dassault Model Falcon 2000, MystereFalcon 900,
Falcon 900EX, Fan Jet Falcon, MystereFalcon 50, MystereFalcon 20, and
MystereFalcon 200 series airplanes. This action requires revising the
Airplane Flight Manual to include speed limitations in the event of
failure
PROPOSED RULES: LET Aeronautical Works,
Published: 2000-08-09
This document proposes to adopt a new airworthiness directive
(AD) that would apply to all LET Aeronautical Works (LET) Model L13
``Blanik'' sailplanes. The proposed AD would require you to inspect the
tailfuselage hinge for strength requirements and damage, and would
require you to replace any hinge with damage or that does not meet
strength
RULES: Airbus,
Published: 2000-06-13
This amendment adopts a new airworthiness directive (AD) that
is applicable to certain Airbus Model A319, A320, and A321 series
airplanes. This action requires a onetime ultrasonic inspection to
detect disbonding of the skin attachments at the stringers and spars of
the vertical stabilizer, and repair, if necessary. This action is
necessary to
RULES: Saab,
Published: 2000-06-15
This amendment adopts a new airworthiness directive (AD),
applicable to certain Saab Model SAAB SF340A and SAAB 340B series
airplanes, that requires a onetime inspection to detect corrosion and
scratches on the bearing housing surfaces of the support assembly on
the main landing gear (MLG), and corrective actions, if necessary. This
amendment is
PROPOSED RULES: Empresa Brasileira de Aeronautica S.A.,
Published: 2000-07-26
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain EMBRAER Model EMB120
series airplanes. This proposal would require a onetime inspection to
detect wear of the hydraulic pump hoses, and corrective action, if
necessary. This proposal would also require relocation of the clip that
secures the
PROPOSED RULES: Boeing,
Published: 2000-06-27
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain Boeing Model 737100,
200, 300, 400, and 500 series airplanes. This proposal would require
inspection of wire bundles in two junction boxes in the main wheel well
to detect chafing or damage, and followon actions. This action is
necessary to
RULES: McDonnell Douglas,
Published: 2000-07-07
This document corrects and clarifies information in an
existing airworthiness directive (AD) that applies to certain McDonnell
Douglas Model DC8 series airplanes. That AD currently requires a
revision to the Airplane Flight Manual Supplement to ensure that the
main deck cargo door is closed, latched, and locked; repetitive
inspections of the wire
RULES: Bell,
Published: 2000-12-13
This amendment adopts a new airworthiness directive (AD) for
Bell Helicopter Textron Inc. (BHTI) Model 205A1, 205B, 212, 412, and
412CF helicopters. This action requires inspecting the locking washer
on each main rotor actuator (actuator) for twisting or damage to the
tab and replacing any locking washer that has a twisted or damaged tab.
RULES: McDonnell Douglas,
Published: 2000-12-04
This amendment adopts a new airworthiness directive (AD),
applicable to certain McDonnell Douglas Model MD11 series airplanes,
that requires relocating the B728 bus located in the upper main
circuit breaker in the rear cockpit observer's station from the lower
to the upper terminals of the circuit breakers in Row P. This action is
necessary to
RULES: Turbomeca; correction,
Published: 2000-11-27
This document makes a correction to Airworthiness Directive
(AD) 20002001 applicable to Turbomeca Arriel 1 series turboshaft
engines that was published in the Federal Register on October 2, 2000
(65 FR 58640). The listing of helicopters on which the affected engines
might be installed in the table in the Applicability section is
incorrect. This