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PROPOSED RULES: Air Tractor, Inc.; correction,
Published: 2005-02-28
Correction
In proposed rule document 052507 beginning on page 6786 in the
issue of Wednesday February 9, 2005, make the following correction: Sec. 39.13 [Corrected]
On page 6788, in Sec. 39.13, in the third column, under the heading
What Airplanes Are Affected by This AD?, paragraph designation ``(b)''
should read paragraph designation
RULES: DG Flugzeugbau GmbH,
Published: 2005-12-28
The FAA adopts a new airworthiness directive (AD) for certain
DG Flugzeugbau GmbH Models DG800B and DG500MB sailplanes. This AD
requires you to modify the connection of the starter ring gear to the
lower drive belt pulley adapter. This AD results from mandatory
continuing airworthiness information (MCAI) issued by the airworthiness
authority for
PROPOSED RULES: McDonnell Douglas,
Published: 2005-12-20
This document revises an earlier proposed airworthiness
directive (AD), applicable to certain McDonnell Douglas Model DC910,
20, 30, 40, and 50 series airplanes; Model DC981 (MD81), 82
(MD82), 83 (MD83), and 87 (MD87) airplanes; and Model MD88
airplanes. That proposed AD would have required repetitive inspections
and functional tests of the static
RULES: Airbus,
Published: 2005-12-14
The FAA is adopting a new airworthiness directive (AD) for
certain Airbus transport category airplanes. This AD requires
repetitive eddy current inspections for cracks of the stiffener
fittings of the fuselage at frame (FR) 12A, and corrective actions if
necessary. This AD also provides a terminating action for the
inspections. This AD results
PROPOSED RULES: Boeing,
Published: 2005-03-23
The FAA proposes to adopt a new airworthiness directive (AD)
for certain Boeing Model 757200 and 300 series airplanes. This
proposed AD would require inspecting for the part number, the serial
number, and the mark ``RETESTED'' on the reaction link of the main
landing gear (MLG), and replacing the reaction link of the MLG with a
retested reaction
PROPOSED RULES: Eurocopter France,
Published: 2005-12-05
This document proposes superseding an existing airworthiness
directive (AD) that currently applies to Eurocopter France (ECF) Model
SA 365N, N1, and AS 365N2 helicopters. That AD currently requires
inspecting the main gearbox (MGB) suspension diagonal crossmember
(diagonal crossmember) for cracks and replacing it with an airworthy
part if any
PROPOSED RULES: Short Brothers,
Published: 2005-04-01
This document revises an earlier proposed airworthiness
directive (AD), applicable to all Short Brothers Model SD360 series
airplanes, that would have required performing an inspection of the
shear attachment fitting for the fintofuselage front spar, and of the
shear cleat for the fin root rib at the aft spar location for
corrosion; reporting
PROPOSED RULES: BAE Systems (Operations) Ltd.,
Published: 2005-04-06
The FAA proposes to adopt a new airworthiness directive (AD)
for all BAE Systems (Operations) Limited (Jetstream) Model 4101
airplanes. This proposed AD would require the overhaul of certain
auxiliary components installed on the main landing gear (MLG) and nose
landing gear (NLG). This proposed AD is prompted by manufacturer
determination that
RULES: Boeing,
Published: 2005-04-11
This amendment supersedes an existing airworthiness directive
(AD), applicable to all Boeing Model 747200F and 200C series
airplanes, that currently requires repetitive detailed inspections or a
onetime openhole high frequency eddy current inspection to detect
cracking of certain areas of the upper deck floor beams, and corrective
actions if
PROPOSED RULES: Bombardier,
Published: 2005-11-10
The FAA proposes to adopt a new airworthiness directive (AD)
for certain Bombardier Model CL6001A11 (CL600), CL6002A12 (CL
601), and CL6002B16 (CL6013A, CL6013R, & CL604) airplanes. This
proposed AD would require modifying the rudder balance spring assembly
by installing a new adjustable balance spring, and rigging the assembly
to suit the rudder
PROPOSED RULES: Pratt & Whitney,
Published: 2005-11-02
The FAA proposes to supersede an existing airworthiness
directive (AD) for Pratt & Whitney (PW) JT9D series turbofan engines.
That AD currently requires revisions to the Airworthiness Limitations
Section (ALS) of the manufacturer's Instructions for Continued
Airworthiness (ICA) to include required enhanced inspection of selected
critical
RULES: Airbus,
Published: 2005-10-26
The FAA is adopting a new airworthiness directive (AD) for
certain Airbus Model A320111, 211, 212, and 231 airplanes. This AD
requires, for certain airplanes, modifying the cables and access holes
to the inner tank fuel pumps; and, for certain other airplanes,
inspecting the fuel pump access holes and modifying the access holes,
if necessary. This
PROPOSED RULES: Eurocopter France,
Published: 2005-10-17
This document proposes adopting a new airworthiness directive
(AD) for Eurocopter France (ECF) Model EC 155B and B1 helicopters. This
proposal would require inspecting an electrical cable bundle for wear.
If wear is present, the AD would require installing an airworthy cable
bundle and modifying the routing of the electrical cable bundles. This
PROPOSED RULES: Boeing,
Published: 2005-10-07
The FAA proposes to adopt a new airworthiness directive (AD)
for all Boeing Model 747 airplanes. This proposed AD would require the
following actions for the drive mechanism of the horizontal stabilizer:
Repetitive detailed inspections for discrepancies and loose ball
bearings; repetitive lubrication of the ballnut and ballscrew;
repetitive
RULES: General Electric,
Published: 2005-05-19
The FAA is adopting a new airworthiness directive (AD) for
General Electric (GE) CF680E1 series turbofan engines that have an
electronic control unit (ECU) with software version E.1.M. or earlier
installed. This AD requires installing improved software for the ECU.
This AD results from an uncommanded engine acceleration event caused by
a failure
PROPOSED RULES: Bombardier; Correction,
Published: 2005-09-30
The FAA is correcting a typographical error in an NPRM that
was published in the Federal Register on September 14, 2005 (70 FR
54316). The error resulted in an incorrect Docket No. The NPRM applies
to certain Bombardier Model DHC8400 series airplanes. The NPRM would
require an inspection of the laminated shims for cracks, damage, or
extrusion
PROPOSED RULES: Eurocopter France,
Published: 2005-09-26
This document proposes to revise an existing airworthiness
directive (AD) for the specified Eurocopter France (ECF) model
helicopters. That AD currently requires certain checks of the magnetic
chip detector plug (chip detector) and the main gearbox (MGB) oilsight
glass, certain inspections of the lubrication pump (pump), and
replacing the MGB and
RULES: Grob-Werke,
Published: 2005-06-07
The FAA adopts a new airworthiness directive (AD) for all
GROBWERKE (GROB) Model G120A airplanes. This AD requires you to
replace the main landing gear front and rear spherical bearings with
improved spherical bearings. This AD results from mandatory continuing
airworthiness information (MCAI) issued by the airworthiness authority
for Germany. We
RULES: Sikorsky,
Published: 2005-06-14
This amendment adopts a new airworthiness directive (AD) for
Sikorsky Aircraft Corporation (Sikorsky) Model S92A helicopters. This
action requires replacing the main gearbox (MGB) lubrication/scavenge
pump vespel spline adapters (vespel spline adapters) before further
flight, and thereafter, replacing them at certain intervals. This
amendment is
RULES: Avions Marcel Dassault-Breguet,
Published: 2005-09-09
The FAA is superseding an existing airworthiness directive
(AD) that applies to all Dassault Model Falcon 10 series airplanes. The
existing AD currently requires revising the airplane flight manual
(AFM) and installing a placard in the flight deck to prohibit flight
into known or forecasted icing conditions. In lieu of the AFM revision
and placard
PROPOSED RULES: Bombardier,
Published: 2005-06-22
The FAA proposes to supersede an existing airworthiness
directive (AD) that applies to certain Bombardier Model CL2151A10
(Water Bomber), CL2156B11 (CL215T Variant), and CL2156B11 (CL415
Variant) series airplanes. The existing AD currently requires
repetitive ultrasonic inspections to detect cracking of the lower caps
of the wing front spar and
RULES: Cessna,
Published: 2005-06-24
This amendment adopts a new airworthiness directive (AD),
applicable to all Cessna Model 650 airplanes, that requires inspecting
to determine the part number of the actuator control unit (ACU) and
replacing the ACU with a new, improved ACU if necessary. This AD also
requires revising the Limitations section of the airplane flight
manual. The
RULES: Boeing,
Published: 2005-06-30
The FAA is adopting a new airworthiness directive (AD) for
Boeing Model 727 airplanes equipped with an auxiliary fuel tank having
a fuel pump installed. This AD requires revising the airplane flight
manual to include limitations on operating the fuel pumps for the
auxiliary fuel tank. This AD is prompted by a design review of the fuel
pump
RULES: Bombardier,
Published: 2005-08-22
The FAA is superseding an existing airworthiness directive
(AD), which applies to all Bombardier Model DHC8100, DHC8200, and
DHC8300 series airplanes. That AD currently requires installation of
a placard on the instrument panel of the cockpit to advise the
flightcrew that positioning of the power levers below the flight idle
stop during flight is
RULES: Hartzell Propeller Inc.,
Published: 2005-07-13
The FAA is adopting a new airworthiness directive (AD) for
Hartzell Propeller, Inc., McCauley Propeller Systems, and Sensenich
Propeller Manufacturing Company, Inc. propellers. This AD requires
maintenance actions amounting to an overhaul of the affected
propellers. This AD results from the investigation of a failed
propeller blade and subsequent