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RULES: Airbus,
Published: 2001-08-06
This amendment adopts a new airworthiness directive (AD) that
is applicable to certain Airbus Model A330301, 321, 322, 341, and
342 series airplanes, and certain Model A340 series airplanes. This
action requires repetitive inspections to detect cracking of the aft
cargo compartment door, and corrective action if necessary. This action
also
PROPOSED RULES: Airbus,
Published: 2001-08-31
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain Airbus Model A319, A320,
and A321 series airplanes. This proposal would require 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
PROPOSED RULES: Bombardier,
Published: 2001-08-29
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
repetitive inspections of the rudder pedal adjustment fittings for
cracks and replacement of cracked fittings with new fittings. The
proposal would also provide
PROPOSED RULES: Boeing,
Published: 2001-08-23
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to all Boeing Model 767200, 300,
and 300F series airplanes. This proposal would require examination of
maintenance records to determine if Titanine JC5A corrosion inhibiting
compound (``C.I.C'') was ever used; inspection for cracks or corrosion
and
RULES: Rolls-Royce, plc,
Published: 2001-11-13
This amendment adopts a new airworthiness directive (AD), that
is applicable to RollsRoyce, plc models Tay 65015 and 65154 turbofan
engines. This amendment requires initial and repetitive visual and
ultrasonic inspections of fan blades for cracks, and, if necessary,
replacement with serviceable parts. In addition, this AD requires
recording
PROPOSED RULES: DG Flugzeugbau GmbH,
Published: 2001-01-09
This document proposes to adopt a new airworthiness directive
(AD) that would apply to certain DG Flugzeugbau GmbH (DG Flugzeugbau)
Model DG800B Sailplanes. The proposed AD would require you to install
an additional filter for the primer valve; inspect and align the
exhaust system; modify the placement of the fuel lines if the fuel
filter is
PROPOSED RULES: Boeing,
Published: 2001-10-26
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain Boeing Model 767200,
300, and 300F series airplanes. This proposal would require a onetime
inspection for discrepancies of certain wire bundles in the forward
cargo compartment, and corrective actions, if necessary. This action is
necessary to
RULES: Boeing,
Published: 2001-10-16
This amendment adopts a new airworthiness directive (AD),
applicable to certain Boeing Model 757 series airplanes, that requires
revising the Airworthiness Limitations Section of the maintenance
manual (757 Airworthiness Limitations Instructions (ALI)). The revision
will incorporate into the ALI certain inspections and compliance times
to detect
PROPOSED RULES: Pilatus Aircraft Ltd.,
Published: 2001-10-10
This document proposes to adopt a new airworthiness directive
(AD) that would apply to certain Pilatus Aircraft Ltd. (Pilatus) Model
PC7 airplanes. This proposed AD would require you to inspect the
landinggear emergencyextension cable for damage and replace if
necessary; verify the correct installation of the bowdencable conduit
clamp and correct
RULES: Eurocopter France,
Published: 2001-10-03
This amendment revises an existing airworthiness directive
(AD) for Eurocopter France (ECF) Model SA365N1, AS365N2, and SA366G1
helicopters. That AD currently requires inspecting each tail rotor
blade for bonding separation, measuring the clearance between the tip
of each tail rotor blade and the circumference of the air duct, and
replacing the
RULES: Aerospatiale,
Published: 2001-08-22
This amendment adopts a new airworthiness directive (AD),
applicable to all Aerospatiale Model ATR42200, 300, 320, and 500
series airplanes; and all Model ATR72 series airplanes. The AD requires
revising the Airplane Flight Manual to modify procedures for
calculating takeoff performance when Type II or IV deicing or anti
icing fluids have been
PROPOSED RULES: Boeing,
Published: 2001-07-23
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain Boeing Model 747 series
airplanes. This proposal would require a onetime inspection for
chafing between the hose for the passenger oxygen system (hereinafter
called the ``oxygen hose'') and adjacent electrical wire bundles at
certain passenger
RULES: Cessna,
Published: 2001-07-11
This amendment adopts a new airworthiness directive (AD) that
is applicable to certain Cessna Model 560XL airplanes. This action
requires inspection of certain electrical wiring of the landing light
switch, associated components, and the aft Jbox fairing light relay
wire for chafing, discoloration, or damage; rerouting of certain
wiring; and
RULES: Eurocopter France,
Published: 2001-06-27
This amendment adopts a new airworthiness directive (AD) for
Eurocopter France Model EC 155B helicopters. This AD requires, before
each takeoff with a cabin sliding door in the open position, visually
checking each sliding door to ensure that each door roller is inside
its rail. If a roller is outside its rail, before further flight, each
roller
RULES: General Electric Co.,
Published: 2001-06-15
This amendment adopts a new airworthiness directive (AD) that is
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applicable to certain General Electric Company (GE) CT58 series and
former military T58 series turboshaft engines. This action requires the
removal from service of certain fuel flow divider assemblies, and
replacement with serviceable parts. This amendment is prompted
RULES: McDonnell Douglas,
Published: 2001-12-26
This amendment adopts a new airworthiness directive (AD),
applicable to certain McDonnell Douglas Model DC8 series airplanes
that have been converted from a passengerto a cargocarrying
(``freighter'') configuration. This amendment requires, among other
actions, modification of the main deck cargo door structure and
fuselage structure; modification
RULES: McDonnell Douglas,
Published: 2001-12-12
This amendment adopts a new airworthiness directive (AD),
applicable to certain McDonnell Douglas Model DC1010, 15, 30, 30F
(KC10A and KDC10 military), and 40 series airplanes; and Model MD
1010F series airplanes, that requires an inspection to verify that the
wire connections at circuit breakers are properly connected, and
correction of any
RULES: Empresa Brasileira de Aeronautica S.A. (EMBRAER),
Published: 2001-02-02
This document publishes in the Federal Register an amendment
adopting airworthiness directive (AD) 20010251 that was sent
previously to all known U.S. owners and operators of EMBRAER Model EMB
145 and EMB135 series airplanes by individual notices. This AD
requires revising the FAAapproved airplane flight manual and
installing placards to alert the
PROPOSED RULES: Pratt & Whitney,
Published: 2001-11-23
The Federal Aviation Administration (FAA) proposes to adopt a
new airworthiness directive (AD) that is applicable to Pratt & Whitney
(PW) PW4090, PW40903, PW4074D, PW4077D, PW4090D, and PW4098 turbofan
engines with 15th stage high pressure compressor (HPC) disks having
certain part numbers (P/N's). This proposal would require initial and
PROPOSED RULES: Bombardier,
Published: 2001-02-14
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
removing certain foam filters from the cabin ducting installation
located below the dado panels on the left and righthand sides of the
airplane. This action is
RULES: Boeing,
Published: 2001-02-21
This amendment adopts a new airworthiness directive (AD);
applicable to all Boeing Model 747100, 200, 300, 400, and 747SR
series airplanes; that requires a onetime inspection to determine
whether H11 steel bolts are installed as attach and support bolts at
the trailing edge flap transmissions, and replacement of any H11 steel
bolt with an Inconel
PROPOSED RULES: General Electric Co.,
Published: 2001-02-27
The FAA proposes to adopt a new airworthiness directive (AD)
that applies to GE CF341 and 3 series turbofan engines with No. 5
bearing rotating air seal part number (P/N) 4019T60G01 installed. This
proposal would require initial and repetitive checks of the magnetic
chip detector indicators, which are located in the lubrication system
for the
RULES: Bell; correction,
Published: 2001-03-06
Correction
In rule document 0028235 beginning on page 66617 in the issue of
Tuesday, November 7, 2000, the docket number is corrected to read as set forth above.
[FR Doc. C028235 Filed 3501; 8:45 am]
BILLING CODE 150501D
RULES: General Electric Co.,
Published: 2001-05-16
This amendment adopts a new airworthiness directive (AD) that
is applicable to General Electric Company (GE) CF341A, 3A, 3A1,
3A2, 3B, and 3B1 turbofan engines. This action requires a onetime
inspection, and if necessary replacement of certain fan disks for
electrical arcout indications, and assigns a reduction in the life
limit of certain fan
RULES: Boeing,
Published: 2001-05-09
This amendment adopts a new airworthiness directive (AD) that
is applicable to certain Boeing Model 767200, 300, and 300F series
airplanes. This action requires inspections for fatigue cracking of the
horizontal stabilizer pivot bulkhead, and repetitive inspections or
other followon actions. This action also provides a permanent repair,
which is