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PROPOSED RULES: McDonnell Douglas Model DC 8 11, DC 8 12, DC 8 21, DC 8 31, DC 8 32, DC 8 33, DC 8 41, DC 8 42, and DC 8 43 Airplanes et al.,
Published: 2008-08-12
We propose to adopt a new airworthiness directive (AD) for all
McDonnell Douglas airplanes identified above. This proposed AD would
require repetitive inspections of the lower skin and stringers at
stations Xw = 408 and Xw = 408 and corrective actions if necessary.
This proposed AD results from reports of cracks in the skins and
stringers at the
RULES: Boeing Model 707 Airplanes, and Model 720 and 720B Series Airplanes,
Published: 2008-08-28
We are adopting a new airworthiness directive (AD) for certain
Boeing Model 707 airplanes, and Model 720 and 720B series airplanes.
This AD requires repetitive detailed inspections to detect cracks and
corrosion on any existing repairs and at certain body stations of the
visible surfaces of the wing to body terminal fittings including the
web,
PROPOSED RULES: Bombardier Model CL 600 2B19 (Regional Jet Series 100 & 440) Airplanes,
Published: 2008-09-17
We propose to adopt a new airworthiness directive (AD) for the
products listed above. This proposed AD results from mandatory
continuing airworthiness information (MCAI) originated by an aviation
authority of another country to identify and correct an unsafe
condition on an aviation product. The MCAI describes the unsafe condition as:
PROPOSED RULES: Boeing Model 747-100, et al.,
Published: 2008-10-08
We propose to adopt a new airworthiness directive (AD) for
certain Boeing Model 747100, 747100B, 747100B SUD, 747200B, 747
200C, 747200F, 747300, 747400, 747SR, and 747SP series airplanes.
This proposed AD would require inspecting for skin cracks at the shear
tie end fastener locations of the fuselage frames, and repair if
necessary. This proposed
RULES: General Electric Company (GE) CT58 Series Turboshaft Engines,
Published: 2008-10-27
The FAA is adopting a new airworthiness directive (AD) for
certain GE CT58 series turboshaft engines. This AD requires
recalculating the lives of certain part numbered compressor spools
using a new repetitive heavy lift (RHL) multiplying factor. This AD
results from reports of cracks originating from the inner faces of the
locking screw holes in
RULES: Boeing Model 737-100, -200, -200C, -300, -400, and -500 Series Airplanes,
Published: 2008-11-14
The FAA is revising an existing airworthiness directive (AD)
that applies to certain Boeing Model 737100, 200, 200C, 300, 400,
and 500 series airplanes. That AD currently requires various
repetitive inspections for cracking of the upper frame to side frame
splice of the fuselage, and other specified and corrective actions if
necessary. That AD
RULES: Eurocopter France Model AS355E, F, F1, F2, and N Helicopters,
Published: 2008-11-25
This amendment supersedes an existing airworthiness directive
(AD) for the specified Eurocopter France (Eurocopter) 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: Boeing Model 737-600, -700, -700C, -800, and -900 Series Airplanes,
Published: 2008-04-21
We are adopting a new airworthiness directive (AD) for certain
Boeing Model 737600, 700, 700C, 800, and 900 series airplanes.
This AD requires a onetime inspection to determine the material of the
forward and aft gray water drain masts. For airplanes having composite
gray water drain masts, this AD requires installation of a bonding
jumper between
PROPOSED RULES: General Avia Costruzioni Aeronatiche Models F22B, F22C, and F22R Airplanes,
Published: 2008-04-11
We propose to adopt a new airworthiness directive (AD) for the
products listed above. This proposed AD results from mandatory
continuing airworthiness information (MCAI) originated by an aviation
authority of another country to identify and correct an unsafe
condition on an aviation product. The MCAI describes the unsafe condition as:
ENAC
RULES: MORAVAN a.s. Model Z-143L Airplanes,
Published: 2008-03-26
We are adopting a new airworthiness directive (AD) for the
products listed above. This AD results from mandatory continuing
airworthiness information (MCAI) issued by the aviation authority of
another country to identify and correct an unsafe condition on an
aviation product. The MCAI describes the unsafe condition as:
Installation of Gload
PROPOSED RULES: Dassault Model Mystere Falcon 20 C5, 20 D5, and 20 E5 Airplanes,
Published: 2008-03-13
We propose to adopt a new airworthiness directive (AD) for the
products listed above. This proposed AD results from mandatory
continuing airworthiness information (MCAI) originated by an aviation
authority of another country to identify and correct an unsafe
condition on an aviation product. The MCAI describes the unsafe condition as:
This
RULES: Airbus Model A330-200 Airplanes etc.,
Published: 2008-03-12
The FAA is superseding an existing airworthiness directive
(AD), which applies to all Airbus Model A330200, A330300, A340200,
and A340300 series airplanes. That AD currently requires an
accelerated schedule of repetitive testing of the elevator servo
control loops, and corrective actions if necessary. This new AD retains
the existing requirements,
PROPOSED RULES: Taylorcraft Models A, B, and F Series Airplanes; Correction,
Published: 2008-03-03
This document makes a correction to a current notice of
proposed rulemaking (NPRM), which was published in the Federal Register
on February 20, 2008 (73 FR 9239), and applies to certain Taylorcraft
Models A, B, and F series airplanes. The NPRM proposed to require
inspection of the wing strut attach fittings for corrosion or cracks
and would
PROPOSED RULES: Bombardier Model DHC 8 102, et al. Airplanes,
Published: 2008-02-19
We propose to adopt a new airworthiness directive (AD) for the
products listed above. This proposed AD results from mandatory
continuing airworthiness information (MCAI) originated by an aviation
authority of another country to identify and correct an unsafe
condition on an aviation product. The MCAI describes the unsafe condition as:
RULES: McDonnell Douglas Model DC-8-11 et al.,
Published: 2008-02-05
The FAA is superseding an existing airworthiness directive
(AD), which applies to certain McDonnell Douglas airplanes. The
existing AD currently requires an initial general visual or dye
penetrant inspection, repetitive dye penetrant inspections, and
replacement, as necessary, of the rudder pedal bracket. The existing AD
also currently requires,
RULES: McDonnell Douglas Model 717 200 Airplanes,
Published: 2008-01-24
We are adopting a new airworthiness directive (AD) for certain
McDonnell Douglas Model 717200 airplanes. This AD requires
modification of the conduit for the forward boost pump of the center
fuel tank. This AD results from the finding that a potential chafing
condition exists in the volute assembly of the forward boost pump for
the center fuel
PROPOSED RULES: Boeing Model 727-200 Series Airplanes,
Published: 2008-01-14
The FAA proposes to adopt a new airworthiness directive (AD)
for certain Boeing Model 727200 series airplanes. This proposed AD
would require deactivation of auxiliary fuel tank systems installed in
accordance with Supplemental Type Certificate (STC) SA1350NM. This
proposed AD results from fuel tank system reviews conducted by the
manufacturer
RULES: Bell Helicopter Textron Canada Model 430 Helicopters,
Published: 2008-01-02
This amendment adopts a new airworthiness directive (AD) for
Bell Helicopter Textron Canada (BHTC) Model 430 helicopters that
requires replacing a certain servo actuatortoactuator support
attachment bolt (bolt) with an airworthy bolt. This action also
requires establishing a retirement life for certain bolts and recording
the retirement life on a
PROPOSED RULES: Boeing Model 707 Airplanes, and Model 720 and 720B Series Airplanes,
Published: 2008-05-08
We propose to adopt a new airworthiness directive (AD) for
certain Boeing Model 707 airplanes, and Model 720 and 720B series
airplanes. This proposed AD would require repetitive detailed
inspections to detect cracks and corrosion on any existing repairs and
at certain body stations of the visible surfaces of the wing to body
terminal fittings
RULES: Boeing Model 737 600, 700, 700C, 800, 900, and 900ER Series Airplanes,
Published: 2008-05-29
We are adopting a new airworthiness directive (AD) for all
Boeing Model 737600, 700, 700C, 800, 900, and 900ER series
airplanes. This AD requires repetitive inspections for any cracking of
or damage to the left side and right side flight deck No. 2, No. 4, and
No. 5 windows, as necessary, and corrective actions if necessary. This
AD results from
RULES: Empresa Brasileira de Aeronautica S.A. Model EMB 135BJ and EMB-145XR Airplanes,
Published: 2008-06-11
We are adopting a new airworthiness directive (AD) for the
products listed above. This AD results from mandatory continuing
airworthiness information (MCAI) originated by an aviation authority of
another country to identify and correct an unsafe condition on an
aviation product. The MCAI describes the unsafe condition as:
It has been found that
PROPOSED RULES: BAE Systems (Operations) Limited (Jetstream) Model 4101 Airplanes,
Published: 2008-06-20
The FAA proposes to supersede an existing airworthiness
directive (AD) that applies to all BAE Systems (Operations) Limited
(Jetstream) Model 4101 airplanes. The existing AD currently requires
repetitive tests for free movement of the capsule/bearing of the nose
landing gear (NLG), and related investigative and corrective actions.
This proposed AD
RULES: Boeing Model 767-200, -300, and -400ER Series Airplanes,
Published: 2008-07-02
We are adopting a new airworthiness directive (AD) for certain
Boeing Model 767200, 300, and 400ER series airplanes. This AD
requires an inspection to determine the manufacturer and manufacture
date of the oxygen masks in the passenger service units and the flight
attendant and lavatory oxygen boxes, as applicable. This AD also
requires related
RULES: Cirrus Design Corporation Model SR20 and SR22 Airplanes,
Published: 2008-07-10
We are adopting a new airworthiness directive (AD) for certain
Cirrus Design Corporation (CDC) Models SR20 and SR22 airplanes. This AD
requires you to replace the cabin door rod ends with new parts
including a redesigned nonbinding hinge pin that replaces the existing
pin at the upper door hinge. This AD results from two known occurrences
of
PROPOSED RULES: Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model ERJ 170 Airplanes and Model ERJ 190 Airplanes,
Published: 2008-08-04
We propose to adopt a new airworthiness directive (AD) for the
products listed above. This proposed AD results from mandatory
continuing airworthiness information (MCAI) originated by an aviation
authority of another country to identify and correct an unsafe
condition on an aviation product. The MCAI describes the unsafe condition as:
It has
