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RULES: Eurocopter France,
Published: 2000-11-14
This amendment supersedes an existing airworthiness directive
(AD) that applies to Eurocopter France Model SA330F, G, and J
helicopters and requires inspecting the tail rotor blade (blade) skin
for cracks and replacing, as necessary, the blade. This amendment
requires skin bonding and eddy current inspections of the blade skin
for cracks and would
PROPOSED RULES: Bombardier,
Published: 2000-10-31
This document proposes the supersedure of 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 (AFM); and
removal of all elevator flutter dampers. That AD also requires
installation of new elevator
RULES: Lockheed,
Published: 2000-10-20
This amendment adopts a new airworthiness directive (AD),
applicable to all Lockheed Model L1011385 series airplanes, that
requires repetitive inspections to detect corrosion or fatigue cracking
of certain structural elements of the airplane; corrective action, if
necessary; and incorporation of certain structural modifications. This
amendment is
RULES: Empresa Brasileira de Aeronautica S.A.,
Published: 2000-10-06
This amendment adopts a new airworthiness directive (AD), [[Page 59709]]
applicable to certain EMBRAER Model EMB120 series airplanes, that
requires revising the Airplane Flight Manual (AFM), and either
installing hydraulic tube assemblies incorporating a check valve, or
visually inspecting the check valve if already installed and corrective
action,
RULES: Boeing,
Published: 2000-09-22
This amendment supersedes an existing airworthiness directive
(AD), applicable to all Boeing Model 777 series airplanes. The existing
AD requires repetitive detailed visual inspections to detect cracking
of the coveskin on the outboard leading edge slats; a slat adjustment
check; and corrective actions, if necessary. This amendment reduces the
PROPOSED RULES: British Aerospace,
Published: 2000-09-19
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to all British Aerospace Model BAC 1
11 401/AK and 410/AQ airplanes. This proposal would require replacement
of certain landing gear brake accumulators with improved accumulators.
This action is necessary to prevent loss of hydraulic pressure and
possible
RULES: Boeing,
Published: 2000-05-01
This amendment adopts a new airworthiness directive (AD),
applicable to all Boeing Model 747 series airplanes, that requires
repetitive inspections to detect cracking of the forward and aft inner
chords and the splice fitting of the forward inner chord of the station
2598 bulkhead, and repair, if necessary. This amendment is prompted by
reports of
PROPOSED RULES: Schweizer Aircraft Corp.,
Published: 2000-05-09
This document proposes the supersedure of an existing
airworthiness directive (AD) applicable to Schweizer Aircraft
Corporation (Schweizer) Model 269A, 269A1, 269B, 269C, 269C1, and
269D helicopters. That AD currently requires inspecting the tail rotor
swashplate shaft (shaft) nut for looseness and, if loose, inspecting
the shaft for proper size;
PROPOSED RULES: Short Brothers & Harland Ltd.; withdrawn,
Published: 2000-08-30
This document withdraws a notice of proposed rulemaking (NPRM)
that would have applied to all Short Brothers & Harland Ltd. (Shorts)
Models SC7 Series 2 and SC7 Series 3 airplanes. The proposed AD would
have required you to revise the Airplane Flight Manual (AFM) to include
requirements for activation of the airframe pneumatic deicing boots.
The
RULES: Bell,
Published: 2000-05-22
This amendment adopts a new airworthiness directive (AD) for
BHTC Model 222, 222B, 222U, and 230 helicopters that requires
inspecting each flapping bearing to yoke attachment bolt (bolt) and
replacing each bolt that shows thread damage, shank wear, or corrosion
pitting with an airworthy bolt. This amendment is prompted by the
discovery of a
Part V: Department of Transportation, Federal Aviation Administration,
Published: 2000-05-26
This amendment adopts a new airworthiness directive (AD),
applicable to certain McDonnell Douglas Model DC980 and MD9030
series airplanes, and Model MD88 airplanes, that requires a
determination be made of whether, and at what locations, metallized
polyethyleneteraphthalate (MPET) insulation blankets are installed, and
replacement of MPET
RULES: Air Tractor Inc.,
Published: 2000-06-02
This amendment adopts a new airworthiness directive (AD) that
applies to certain Air Tractor Incorporated (Air Tractor) Models AT
301, AT401, and AT501 airplanes that are equipped with a \3/16\inch
thick aluminum fin front spar fitting and an all metal rudder. This AD
requires that you repetitively inspect the vertical fin front spar
attachment
RULES: McCauley Propeller,
Published: 2000-08-08
This amendment adopts a new airworthiness directive (AD) that
is applicable to McCauley Propeller Systems 4HFR34C653/L106FA0 model
propellers that are installed on Jetstream Series 3200 airplanes. This
action is also applicable to 4HFR34C653/L106FA0 model propellers that
are installed on Ayres S2RG5 and S2RG10 airplanes if the propeller
was
PROPOSED RULES: Airbus,
Published: 2000-06-13
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain Airbus Model A300 and
A300600 series airplanes. This proposal would require repetitive
inspections to detect chafing and the existence of repairs of the
harness of the highlevel sensor of the fuel surge tanks, and to detect
chafe marks on the
PROPOSED RULES: Raytheon,
Published: 2000-06-16
This document proposes the supersedure of an existing
airworthiness directive (AD), applicable to all Raytheon Model DH.125
1A, 3A, and 400A series airplanes, that currently requires a onetime
inspection to detect scoring of the upper fuselage skin around the
periphery of the cockpit canopy blister interface, and repair, if
necessary. This action
PROPOSED RULES: New Piper Aircraft, Inc.,
Published: 2000-07-21
This document proposes to revise an earlier proposed
airworthiness directive (AD) that would apply to The New Piper
Aircraft, Inc. (Piper) PA31 series airplanes. The earlier NPRM would
have superseded AD 802605, which requires you to repetitively inspect
the main landing gear (MLG) inboard door hinges and attachment angles
for cracks on the
RULES: Boeing,
Published: 2000-07-13
This amendment supersedes an existing airworthiness directive
(AD), applicable to certain Boeing Model 747 series airplanes, that
currently requires a onetime inspection to determine the part number
of the fuel shutoff spar valve for the outboard engines. That AD also
requires replacement of certain valves with new valves, or modification
of the
RULES: Airbus,
Published: 2000-12-28
This document publishes in the Federal Register an amendment
adopting airworthiness directive (AD) 20002553, which was sent
previously to all known U.S. owners and operators of Airbus Model A330
series airplanes by individual notices. This AD requires either
repetitive detailed visual inspections or repetitive borescopic
inspections to detect
RULES: S.N. Centrair,
Published: 2000-12-11
This amendment adopts a new airworthiness directive (AD) that
applies to certain S.N. CENTRAIR 101 series gliders. This AD requires
you to inspect the airbrake control system for cracks; and if cracks
are detected, replace the airbrake control system. This AD is the
result of mandatory continuing airworthiness information (MCAI) issued
by the
PROPOSED RULES: Eurocopter France,
Published: 2000-12-01
This NPRM proposes the supersedure of an existing
airworthiness directive (AD) for Eurocopter France (ECF) Model SA.315B,
SA.316B, SA.316C, SE.3160, and SA.319B helicopters. That AD requires
initial and recurring inspections of the main rotor blade (blade) spar
for cracks. This action would require initial and recurring dye
penetrant or eddy
RULES: McDonnell Douglas,
Published: 2000-11-20
This amendment adopts a new airworthiness directive (AD) that
is applicable to all McDonnell Douglas Model DC10, Model MD10, and
Model MD11 series airplanes. This action requires revising the
Airplane Flight Manual (AFM) to ensure that the flight crew is advised
of appropriate procedures for disabling certain fuel pump electrical
circuits
RULES: Bell,
Published: 2000-11-07
This amendment revises an existing airworthiness directive
(AD) that applies to Model HH1K, TH1F, TH1L, UH1A, UH1B, UH1E,
UH1F, UH1H, UH1L, and UH1P; and Southwest Florida Aviation SW204,
SW204HP, SW205, and SW205A1 helicopters, manufactured by Bell
Helicopter Textron Inc. (BHTI) for the Armed Forces of the United
States, and requires removing and
RULES: Pilatus Aircraft Ltd.,
Published: 2000-10-27
This amendment adopts a new airworthiness directive (AD) that
applies to certain Pilatus Aircraft Ltd. (Pilatus) Models PC12 and PC
12/45 airplanes. This AD requires you to perform a onetime inspection
for abrasion damage, distortion, and proper clearance of the torque
oilpressure tubes and py pressure pipe, and if necessary, adjust and
replace
PROPOSED RULES: Dornier,
Published: 2000-10-17
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to all Dornier Model 328100 series
airplanes. This proposal would require revising the Airworthiness
Limitations Section of the Instructions for Continued Airworthiness to
incorporate life limits for certain items and inspections to detect
fatigue cracking
RULES: Turbomeca,
Published: 2000-10-02
This amendment adopts a new airworthiness directive (AD) that
is applicable to certain Turbomeca Arriel 1 series turboshaft engines.
This action requires the installation of a chip detector with
electronic warning on the rear bearing oil return system. This
amendment is prompted by reports of gas generator rear bearing
failures. The actions