Years: 200020012002200320042005200620072008200920102011201220132014

Pages: «<45678>»

51  RULES: Airbus,

The FAA is superseding an existing airworthiness directive (AD), which applies to certain Airbus Model A330300, A340200, and 340300 series airplanes. The existing AD requires repetitive inspections to detect cracking of the fuselage skin in the area of the VHF2 antenna, and repair if necessary. The existing AD also provides for optional

52  PROPOSED RULES: Boeing,

The FAA withdraws a notice of proposed rulemaking (NPRM) that proposed a new airworthiness directive (AD) for certain Boeing Model 767300
[[Page 73393]]
and 300F series airplanes. The proposed AD would have required a one time operational test of the pilots' seat locks and the seat tracks to ensure that the seats lock in position and the seat tracks

53  RULES: Airbus,

This amendment supersedes an existing airworthiness directive (AD), applicable to the airplane models listed above. That AD currently requires repetitive inspections to detect discrepancies of the transfer tubes and the collar of the ball nut of the trimmable horizontal stabilizer actuator (THSA), and corrective action if necessary. This amendment

54  RULES: Pratt & Whitney; correction,

Correction

In rule document 0517319 beginning on page 52004 in the issue of Thursday, September 1, 2005 make the following correction:

Sec. 39.13 [Corrected]

On page 52006, in Sec. 39.13(f), in the table, under the heading ``Inspection No.'', in the last entry ``02'' should read ``02''''. [FR Doc. C517319 Filed 112805; 8:45 am]
BILLING CODE

55  PROPOSED RULES: Bombardier,

The FAA proposes to adopt a new airworthiness directive (AD) for certain Bombardier Model DHC8102, 103, 106, 201, 202, 301, 311, and 315 airplanes. This proposed AD would require revising the airworthiness limitations section of the Instructions for Continued Airworthiness by incorporating new and revised structural inspection procedures and new

56  RULES: Cessna; correction,

Correction

In rule document 055915 beginning on page 15223 in the issue of Friday, March 25, 2005, make the following correction:

Sec. 39.13 [Corrected]

On page 15226, in Sec. 39.13(e), in the table, under the heading ``Affected airplanes'', in the fifth entry, in the second line, ``PT6A 114A'' should read ``PT6A114''.
[FR Doc. C55915 Filed

57  PROPOSED RULES: General Electric Co.,

The FAA proposes to adopt a new airworthiness directive (AD) for General Electric Company (GE) CT75A2, 5A3, 7A, 7A1, 9B, 9B1, and 9B2 turboprop engines, with stage 2 turbine aft cooling plate, part number (P/N) 6064T07P01, 6064T07P02, 6064T07P05, or 6068T36P01 installed. This proposed AD would require a onetime eddy current inspection (ECI) of

58  RULES: Boeing,

The FAA is superseding an existing airworthiness directive (AD), which applies to certain Boeing Model 707 airplanes and Model 720 and 720B series airplanes. That AD currently requires a preventive modification of the front spar fitting on the outboard engine nacelle. This new AD removes the requirement to do this preventive modification, and

59  PROPOSED RULES: Boeing,

The FAA proposes to adopt a new airworthiness directive (AD) for all Boeing Model 727 airplanes. This proposed AD would require a onetime inspection of the lower lobe frames of body section 43 to find open holes between stringers 17L and 17R; repetitive high frequency eddy current (HFEC) inspections for cracks of all open holes; and related

60  RULES: CFM International,

The FAA is adopting a new airworthiness directive (AD) for CFM International CFM565, 5B, and 5C series turbofan engines. This AD requires removing certain part number (P/N) air turbine starters from service. This AD results from several reports of uncontained failures of air turbine starters where highenergy particles were not contained within the

Years: 200020012002200320042005200620072008200920102011201220132014

Pages: «<45678>»