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RULES: Eurocopter France,
Published: 2001-08-02
This amendment adopts a new airworthiness directive (AD) for
Eurocopter France (ECF) Model AS365N3 helicopters that requires
modifying the Full Authority Digital Engine Control (FADEC) software
within 90 days after the effective date of this AD. This amendment is
prompted by a design problem in the FADEC ``power loss printed circuit
board''
RULES: Airbus,
Published: 2001-08-29
This amendment adopts a new airworthiness directive (AD) that
is applicable to certain Airbus Model A300 B2 and B4 series airplanes,
and certain Model A300 B4600, B4600R, and F4600R (collectively
called A300600) series airplanes. This action requires a onetime
inspection to detect cracks in gear rib 5 (left and right) of the main
landing gear
RULES: Aerospatiale,
Published: 2001-07-25
This amendment adopts a new airworthiness directive (AD),
applicable to certain Aerospatiale Model ATR42200, 300, 320, and
500 series airplanes; and Model ATR72 series airplanes; that requires
replacement of the existing uplock boxes of the main and nose landing
gears with modified uplock boxes. The actions specified by this AD are
intended to
PROPOSED RULES: McDonnell Douglas,
Published: 2001-07-23
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain McDonnell Douglas Model
DC1010, 15, 30, 30F (KC10A and KDC10 military), and 40 series
airplanes; and Model MD1010F series airplanes. This proposal would
require an inspection to verify that the wire connections at circuit
breakers are properly
RULES: Boeing,
Published: 2001-11-01
This amendment supersedes an existing airworthiness directive
(AD), applicable to all Boeing Model 737600, 700, and 800 series
airplanes, that currently requires an inspection of the power
distribution panels (PDP) to verify proper installation of the power
feeder terminals and associated hardware, and corrective actions, if
necessary. The
RULES: SOCATA-Groupe AEROSPATIALE,
Published: 2001-01-11
This amendment adopts a new airworthiness directive (AD) that
applies to certain SOCATAGroupe AEROSPATIALE (Socata) Model TBM 700
airplanes. This AD requires you to inspect for a low point in the fuel
tank air vent valve hose; and reroute the hose as necessary. This AD is
the result of mandatory continuing airworthiness information (MCAI)
issued
RULES: MD Helicopters, Inc.,
Published: 2001-01-22
This document publishes in the Federal Register an amendment
adopting Emergency Airworthiness Directive (AD) 20002552 which was
sent previously to all known U.S. owners and operators of MD
Helicopters, Inc. (MDHI) Model 369A, H, HE, HM, HS, D, E, FF, and 500N
helicopters. This amendment supersedes an existing emergency AD that
requires, before
RULES: Short Brothers,
Published: 2001-01-30
This amendment adopts a new airworthiness directive (AD),
applicable to all Short Brothers Model SD360 SHERPA, SD3SHERPA, SD3
30, and SD360 series airplanes, that requires replacement of the
existing pneumatic deicing boot pressure indicator switch with a newly
designed switch. This amendment is prompted by an occurrence on a
similar airplane model
PROPOSED RULES: McDonnell Douglas,
Published: 2001-10-05
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain McDonnell Douglas Model
MD11 series airplanes. This proposal would require installation of
protective sleeving on the right emergency alternating current wire
assembly of the overhead switch panel. This action is necessary to
ensure that
PROPOSED RULES: Enstrom Helicopter Corp.,
Published: 2001-09-18
This document proposes the adoption of a new airworthiness
directive (AD) for Enstrom Helicopter Corporation (EHC) Model TH28 and
480 helicopters. The AD would require establishing a life limit for
certain upper and lower main rotor hub plates of 5000 hours timein
service (TIS), creating a component history card or equivalent record,
and replacing
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 SA4998NM, that requires modification of
the inflight entertainment (IFE) system to connect it to a different
power source. This action is necessary to prevent the inability of the
flight crew to
RULES: McDonnell Douglas,
Published: 2001-07-12
This amendment adopts a new airworthiness directive (AD),
applicable to certain McDonnell Douglas Model DC10 series airplanes,
Model MD10 series airplanes, and Model MD11 series airplanes, that
requires repetitive inspections of the number 1 and 2 electric motors
of the auxiliary hydraulic pump for electrical resistance, continuity,
mechanical
PROPOSED RULES: Saab,
Published: 2001-06-29
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain Saab Model SAAB SF340A
series airplanes. This proposal would require replacement of the air
recirculation fans in the flight compartment and the passenger
compartment. These fans may be replaced with upgraded fans with new
brushes having
RULES: McDonnell Douglas,
Published: 2001-06-20
This amendment adopts a new airworthiness directive (AD),
applicable to certain McDonnell Douglas Model MD9030 series
airplanes, that requires revising the wiring of the selective calling
(SELCAL) system. The actions specified by this AD are intended to
prevent inadvertent very high frequency transmissions and subsequent
loss of radio
RULES: Hamilton Sundstrand,
Published: 2001-12-28
This amendment adopts a new airworthiness directive (AD) that
is applicable to certain Hamilton Sundstrand model 247F propellers.
This action requires a onetime rework of certain model 247F propellers
by removing all four propeller blades from service, replacing those
blades with serviceable propeller blades, and marking the propeller
with a new
RULES: Boeing,
Published: 2001-12-12
This amendment adopts a new airworthiness directive (AD),
applicable to certain Boeing Model 747 series airplanes, that requires
performing a onetime inspection for chafing of certain electrical wire
bundles behind the flight engineer's panel in the cockpit; repairing
any chafed wire bundles, if necessary; and installing Teflon sleeving
over the
RULES: Eurocopter France,
Published: 2001-12-03
This amendment supersedes an existing airworthiness directive
(AD) that applies to Eurocopter France (ECF) Model EC120B helicopters
and currently requires adjusting the clearance of the cabin sliding
door if necessary. This amendment requires adding an end stop to the
front rail and modifying the rear stop of the middle rail to increase
its
RULES: Dassault,
Published: 2001-11-26
This amendment adopts a new airworthiness directive (AD) that
is applicable to certain Dassault Model MystereFalcon 50 series
airplanes. This action requires revising the Airplane Flight Manual to
prohibit flight operation under reduced vertical separation minimum
(RVSM). This action is necessary to prevent near misses or collision
with other
RULES: SOCATA-Groupe Aerospatiale,
Published: 2001-11-19
This amendment adopts a new airworthiness directive (AD) that
applies 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. This AD
requires you to modify the front seats that have solid metal seat pans.
This AD is
PROPOSED RULES: McDonnell Douglas,
Published: 2001-02-20
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain McDonnell Douglas Model
MD11 series airplanes. This proposal would require replacement of the
insulation blankets of the forward and center cargo compartments in the
area of the cargo control units (CCU) with new insulation blankets.
This action
PROPOSED RULES: Boeing,
Published: 2001-06-05
This document proposes the supersedure of an existing
airworthiness directive (AD), applicable to all Boeing Model 747 series
airplanes, that currently requires a onetime inspection of the
fuselage skin adjacent to the drag splice fitting to detect cracking,
and followon actions, if necessary. This action would mandate new
repetitive inspections
PROPOSED RULES: Pratt & Whitney,
Published: 2001-02-27
This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to Pratt & Whitney (PW) JT9D7R4
series turbofan engines. This proposal would require initial and
repetitive fluorescent penetrant inspection (FPI) of the high pressure
turbine (HPT) 1st stage disk aft lugs, and if the aft lug(s) are
cracked, replacement of
RULES: Boeing,
Published: 2001-03-06
This amendment adopts a new airworthiness directive (AD) that
is applicable to certain Boeing Model 747 series airplanes. This action
requires repetitive detailed visual inspections to find discrepancies
of the installation of the midspar fuse pins of the inboard and
outboard struts, and followon actions, if necessary. This action also
provides
RULES: BMW Rolls-Royce GmbH,
Published: 2001-03-14
This amendment adopts a new airworthiness directive (AD) that
is applicable to BMW RollsRoyce (RR) GmbH models BR700710A110
turbofan engines with fan disk part numbers (P/N's) BRR18803, BRR19248,
or BRR20791 installed, and BR700710A220 turbofan engines with fan
disks P/N's BRR19248 or BRR20791 installed. This action requires
initial and repetitive
PROPOSED RULES: McDonnell Douglas,
Published: 2001-03-21
This document proposes the supersedure of an existing
airworthiness directive (AD), applicable to certain McDonnell Douglas
Model DC1010, 15, 30, and 30F (KC10A military) series airplanes,
and Model MD1010F and 30F series airplanes, that currently requires
repetitive inspections to determine the condition of the lockwires on
the forward engine