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PROPOSED RULES: Eurocopter France,
Published: 2001-11-28
This document proposes adopting a new airworthiness directive
(AD) for Eurocopter France (ECF) Model AS350B, AS350B1, AS350B2,
AS350B3, AS350BA, AS350C, AS350D, AS350D1, AS355E, AS355F, AS355F1,
AS355F2, and AS355N helicopters. This proposal would require replacing
the tail rotor hub pitch change plate ``SNR'' bearing (bearing). This
proposal is
PROPOSED RULES: Hartzell Propeller, Inc.,
Published: 2001-11-20
The Federal Aviation Administration (FAA) proposes to
supersede an existing airworthiness directive (AD) that is applicable
to Hartzell models ( )HC( )( )Y( )( )( )( ) compact series, constant
speed or feathering propellers with Hartzell manufactured ``Y'' shank
blades. That AD currently requires initial and repetitive blade
inspections; rework of
PROPOSED RULES: Boeing,
Published: 2001-02-15
This document proposes the supersedure of an existing
airworthiness directive (AD), applicable to certain Boeing Model 747
series airplanes, that currently requires repetitive inspections and
torque checks of the hanger fittings and strut forward bulkhead of the
forward engine mount and adjacent support structure, and corrective
actions, if
RULES: Empresa Brasileira de Aeronautica, S.A. (EMBRAER),
Published: 2001-02-22
This amendment adopts a new airworthiness directive (AD),
applicable to certain EMBRAER Model EMB145 series airplanes, that
requires inspection of the bolts on the hinge fittings that attach the
spring tab and the servo tab to the rear spar of the elevators for
evidence of loosening; inspection of the region of the hinge fittings
on the spring tab
Part III: Department of Transportation, Federal Aviation Administration,
Published: 2001-03-02
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to all Boeing Model 767200 series
airplanes modified by supplemental type certificate SA5134NM. This
proposal would require modification of the inflight entertainment
(IFE) system. This action is necessary to prevent the inability of the
flight crew to
RULES: DG Flugzeugbau GmbH,
Published: 2001-03-12
This amendment adopts a new airworthiness directive (AD) that
applies to certain DG Flugzeugbau GmbH (DG Flugzeugbau) Model DG500MB
sailplanes equipped with a SOLO 2625 02 engine. This AD requires you to
install additional access holes in the propeller mount and modify the
engine. This AD also requires you to do a ground test run and replace
the
RULES: Eagle Aircraft Pty. Ltd.,
Published: 2001-05-10
This amendment adopts a new airworthiness directive (AD) that
applies to certain Eagle Aircraft Pty. Ltd. (Eagle) Model 150B
airplanes. This AD requires you to inspect the rudder cables for
fraying, broken strands, etc. (referred to as damage), and replace any
damaged cables. This AD also requires you to replace the rudder cable
pulleys with
PROPOSED RULES: Airbus,
Published: 2001-05-04
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to all Airbus Model A300 B21C, B2
203, B2K3C, B42C, B4103, and B4203 series airplanes. This proposal
would require a onetime inspection of the space between the fuel
quantity indication (FQI) probes and any adjacent structures for
minimum clearance, and
PROPOSED RULES: Bombardier,
Published: 2001-03-29
This document proposes the supersedure of an existing
airworthiness directive (AD), applicable to certain Bombardier Model
CL6002B19 series airplanes, that currently requires repetitive
ultrasonic inspection to detect damage of the actuator lugs of the
flight spoiler center hinge; and corrective action, if necessary. This
proposal would mandate
RULES: McDonnell Douglas,
Published: 2001-04-26
This amendment adopts a new airworthiness directive (AD),
applicable to certain McDonnell Douglas Model DC8 series airplanes,
that requires an inspection of the antifogging or heating wiring to
detect chafing or damage, as applicable; inspection of the insulation
blankets to detect damage; and repair, if necessary. This amendment
also requires
RULES: Cessna,
Published: 2001-04-10
This document makes a correction to Airworthiness Directive
(AD) 20010617, which was published in the Federal Register on March
30, 2001 (66 FR 17345), and concerns certain Cessna Aircraft Company
(Cessna) Models 172R and 172S airplanes. The FAA incorrectly referenced
the AD number as ``AD 20010614'' instead of ``AD 20010617.'' This
AD requires a
PROPOSED RULES: Bell,
Published: 2001-09-13
This document proposes to revise an existing airworthiness
directive (AD) for Bell Helicopter Textron, Inc. (BHTI) Model 206A,
206B, 206A1, 206B1, 206L, and 206L1 helicopters that currently
establishes a retirement life for the main rotor trunnion (trunnion)
based on hours timeinservice (TIS). This action would retain those
requirements but would
PROPOSED RULES: McDonnell Douglas,
Published: 2001-08-03
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain McDonnell Douglas Model
DC981, 82, 83, and 87 series airplanes, and Model MD88 airplanes.
This proposal would require replacement of the dust seals of the
passenger service unit (PSU) panels of the overhead stowage compartment
with new dust
RULES: Agusta S.p.A.,
Published: 2001-08-29
This amendment supersedes an existing airworthiness directive
(AD) for Agusta S.p.A. (Agusta) Model A109E helicopters that currently
requires visually checking and inspecting each tail rotor blade (blade)
for a crack at specified intervals. That AD also requires replacing any
cracked blade with an airworthy blade. This amendment contains the same
PROPOSED RULES: SOCATA-Groupe AEROSPATIALE,
Published: 2001-08-24
This document proposes to adopt a new airworthiness directive
(AD) that would apply to all SOCATAGroupe Aerospatiale (SOCATA)
Models TB 9, TB 10, TB 20, TB 21, and TB 200 airplanes that do not have
factory Modification 165, any edition, incorporated on the front seats.
The proposed AD would require you to modify the front seats. The
proposed AD is
RULES: Airbus,
Published: 2001-08-23
This amendment adopts a new airworthiness directive (AD) that
is applicable to all Airbus Model A330 and A340 series airplanes. This
action requires a onetime inspection to detect cracking of the bogie
beams of the main landing gear (MLG), and followon actions, if
necessary. This action is necessary to detect and correct cracking of
the MLG bogie
RULES: Overland Aviation Services,
Published: 2001-11-02
This amendment adopts a new airworthiness directive (AD) that
applies to certain Overland Aviation Services (OAS) fire extinguishing
system bottle cartridges that were distributed during a certain time
period and are installed on aircraft. This AD requires you to remove
from service any of these fire extinguishing system bottle cartridges.
This AD
RULES: Dassault,
Published: 2001-10-29
This amendment adopts a new airworthiness directive (AD),
applicable to all Dassault Model MystereFalcon 50, MystereFalcon 900,
and Falcon 900EX series airplanes, that requires revising the Emergency
Procedures and Abnormal Procedures sections of the airplane flight
manual to advise the flightcrew to immediately don oxygen masks in the
event of
RULES: Eurocopter Deutschland GmbH,
Published: 2001-01-22
This amendment supersedes an existing airworthiness directive
(AD) that applies to Eurocopter Deutschland GMBH (ECD) Model MBBBK 117
helicopters. That AD currently requires, before further flight,
creating a component log card or equivalent record and determining the
calendar age and number of flights on each tensiontorsion (TT) strap.
This
RULES: CFM International,
Published: 2001-01-30
This amendment adopts a new airworthiness directive (AD) that
is applicable to CFMI model CFM567B turbofan engines. This action
requires a onetime onwing torque inspection, and torque if needed, of
all the PS3 pressure line fittings to insure proper torque. This
amendment is prompted by service events which resulted in two inflight
shutdowns
PROPOSED RULES: McDonnell Douglas,
Published: 2001-10-05
This document proposes the supersedure of an existing
airworthiness directive (AD), applicable to certain McDonnell Douglas
Model MD11 series airplanes, that currently requires a onetime
detailed visual inspection of the wire bundle installation behind the
first observer's station to detect damaged or chafed wires; and
corrective action, if
PROPOSED RULES: McDonnell Douglas,
Published: 2001-09-20
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain McDonnell Douglas Model DC1010, 10F, 15, 30, 30F (KC10A and KDC10), 40, and 40F
series airplanes; Model MD1010F and 30F series airplanes; and Model
MD11 and 11F series airplanes. This proposal would require repetitive
tests for electrical
RULES: Boeing,
Published: 2001-08-17
This amendment adopts a new airworthiness directive (AD),
applicable to all Boeing Model 767200 series airplanes modified by
supplemental type certificate SA5134NM, that requires modification of
the inflight entertainment (IFE) system. This action is necessary to
prevent the inability of the flight crew to remove power from the IFE
system when
RULES: Boeing,
Published: 2001-07-12
This amendment adopts a new airworthiness directive (AD),
applicable to all Boeing Model 747400 series airplanes modified by
Supplemental Type Certificate (STC) SA8843SW, that requires modifying
the passenger entertainment system (PES) installed by that STC and
revising the Airplane Flight Manual. This action is necessary to ensure
that the flight
PROPOSED RULES: McDonnell Douglas,
Published: 2001-06-29
This document proposes the supersedure of an existing
airworthiness directive (AD), applicable to certain McDonnell Douglas
Model DC9818283, and87 series airplanes, Model MD88 airplanes,
and Model MD9030 series airplanes, that currently requires a revision
to the applicable Airplane Flight Manual (AFM) to provide the
flightcrew with the