This document proposes the supersedure of three existing airworthiness directives (AD), applicable to certain Boeing Model 767 200, 300, and 300F series airplanes. One AD currently requires modification of the nacelle strut and wing structure for certain Boeing Model 767200, 300, and 300F series airplanes powered by Pratt & Whitney engines. The

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This amendment adopts a new airworthiness directive (AD), applicable to certain Raytheon Model Beech 400A and 400T series airplanes, that requires an inspection to determine the part number of the A194 roll trim printed circuit board (PCB), and replacement of certain PCBs with improved parts. This action is necessary to prevent intermittent

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This amendment adopts a new airworthiness directive (AD), [[Page 10318]]
applicable to certain Airbus Model A319 and A320 series airplanes, that requires an inspection of the clearance space between the fuel quantity indication (FQI) probes located in the center fuel tank and the adjacent structure, an inspection of the position of the support

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This amendment adopts a new airworthiness directive (AD), applicable to all Boeing Model 707 and 720 series airplanes, that requires inspection of the bolt forward of the wing front spar upper chord on the overwing support fittings of the inboard and outboard nacelle struts to verify that BACB30US type bolts are installed. If any other type of

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

The FAA is adopting a new airworthiness directive (AD) for RollsRoyce plc (RR) RB211Trent 500 series turbofan engines. This AD requires revising the Time Limits Manual for RR RB211 Trent 500 series turbofan engines. These revisions include required enhanced inspection of selected critical lifelimited parts at each piecepart exposure. This AD

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This amendment adopts a new airworthiness directive (AD) that is applicable to certain Bombardier Model CL6002C10 (Regional Jet Series 700 & 701) and CL6002D24 (Regional Jet Series 900) series airplanes. This action requires revising the airplane flight manual to advise the flightcrew to monitor the fuel quantity in the center fuel tank throughout

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This amendment adopts a new airworthiness directive (AD), applicable to all CASA Model C212 series airplanes, that requires rework of the nose landing gear (NLG); modification of the hydraulic steering system; a test of the cable tension for the nosewheel steering system when abnormal vibration occurs, and adjustment of the cable tension, if

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This amendment adopts a new airworthiness directive (AD), applicable to certain McDonnell Douglas Model 717200 airplanes, that requires a general visual inspection to detect corrosion of the left and righthand horizontal stabilizer hinge fitting bolts, barrel nuts, and the associated holes in the horizontal stabilizer structure, and to detect

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This document proposes the adoption of a new airworthiness directive (AD) that is applicable to certain Bombardier Model DHC8 301, 311, and 315 airplanes. This proposal would require determining the modification number of the angle of attack (AOA) sensor vanes; testing the movement of the affected vanes to evaluate sticking against both the upper

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This amendment adopts a new airworthiness directive (AD), applicable to all Fokker Model F27 Mark 100, 200, 300, 400, 500, 600, and 700 series airplanes, that requires repetitive inspections of the control panel of the direct current (DC) generator for discrepancies, and replacement of any discrepant part. This action is necessary to prevent loss

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

The FAA is adopting a new airworthiness directive (AD) for Pratt & Whitney (PW) JT9D3A, 7, 7A, 7AH, 7H, 7F, 7J, 20, and 20J turbofan engines. This AD clarifies a life limit for certain part numbers of 6th stage low pressure turbine (LPT) air seals, and requires their removal from service before accumulating 15,000 cyclessincenew (CSN). This AD

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This document makes corrections to Airworthiness Directive (AD) 20030711. That AD applies to RollsRoyce Deutschland Ltd & Co KG (RRD) (formerly RollsRoyce Deutschland GmbH, formerly BMW RollsRoyce GmbH) models BR700710A110 and BR700710A220 turbofan engines. That AD was published in the Federal Register on April 11, 2003 (68 FR 17727).

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This amendment adopts a new airworthiness directive (AD), applicable to certain Fokker Model F.28 Mark 0070 series airplanes, that requires inspection of cables installed on certain contactors in the electrical power center (EPC) for proper installation of wires, and reinstallation of wires if necessary. These actions are necessary to prevent a

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This document revises an earlier proposed airworthiness directive (AD), applicable to certain Dassault Model Fan Jet Falcon series airplanes and Model MystereFalcon 20 series airplanes. That action would have required inspecting and testing for fatigue cracking due to stress corrosion in the vertical posts of the window frames in the flight

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This amendment supersedes an existing airworthiness directive (AD), applicable to all EMBRAER Model EMB135 and 145 series airplanes, that currently requires repetitive inspections of the engine thrust reverser stow/transit switches, and corrective action, if necessary. This amendment continues to require the existing requirements and identifies

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This amendment supersedes an existing airworthiness directive (AD), applicable to certain Bombardier Model DHC8400 airplanes. That AD currently requires revising the Normal and Abnormal sections of the airplane flight manual (AFM) to include procedures that enable the flightcrew to determine if the main landing gear (MLG) is extended before

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This document announces a public meeting of interest to owners and operators of Cessna Aircraft Company (Cessna) Models 401, 401A, 401B, 402, 402A, 402B, 402C, 411, and 411A, and 414A airplanes. The purpose of the meeting is to discuss technical issues and proposed corrective actions related to the potential of wing spar cap failure due to

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This amendment adopts a new airworthiness directive (AD) for Agusta S.p.A. (Agusta) Model A109K2 helicopters. This action requires dyepenetrant inspecting the tail rotor trunnion (trunnion) assembly for a crack at specified intervals, replacing any cracked trunnion with an airworthy trunnion, and reporting any failed trunnion. This amendment is

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

The FAA proposes to adopt a new airworthiness directive (AD) for all Boeing Model 737100, 200, 200C, 300, 400, and 500 series airplanes. This proposed AD would require repetitive inspections for discrepancies of the elevator tab control rod assemblies and/or damage to the surrounding structure, and related corrective action. This proposed AD is

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

The FAA proposes to adopt a new airworthiness directive (AD) for certain Leteck[eacute] Z[aacute]vody Model L 23 SuperBlanik sailplanes. This proposed AD would require you to do a repetitive, non destructive magnetic test (NDMT) inspection on the elevator rocker lever (part number A 730 201 N) for cracks. If cracks are found, this proposed AD would

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

Correction

In rule document 0420015 beginning on page 53794 in the issue of Friday, September 3, 2004, make the following correction:

Sec. 39.13 [Corrected]

On page 53795, in the second column, in Sec. 39.13(c), in the third line ``MD11F'' should read ``MD11, MD11F''.
[FR Doc. C420015 Filed 92004; 8:45 am]
BILLING CODE 150501D

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

The FAA proposes to supersede an existing airworthiness directive (AD) that applies to certain Airbus Model A300 B2 and B4 series airplanes; Model A300 B4600, A300 B4600R, C4605R Variant F, and A300 F4600R (collectively called A300600) series airplanes; and Model A310 series airplanes. The existing AD currently requires replacement of the

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

The FAA is correcting an error in an existing airworthiness directive (AD) that was published in the Federal Register on September 2, 2004 (69 FR 53609). The error resulted in inadvertent reference to inappropriate service information. We are also clarifying reference to a compliance threshold. This AD applies to certain Bombardier Model CL 6002C10

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

The FAA adopts a new airworthiness directive (AD) for all GROBWERKE (GROB) Model G120A airplanes. This AD requires you to repetitively inspect visually the area between the vertical stabilizer main spar and the nearby vertical stabilizer skin for any disbonding/ crack; repair any disbonding/crack found; and calculate weight and balance after any

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration

This amendment adopts a new airworthiness directive (AD), applicable to certain Boeing Model 737600, 700, 700C, 800, and 900 series airplanes, that requires a general visual inspection for sealant at the interface between the diagonal brace fitting and the aft bulkhead and at the four bolts common to the interface. It also requires applying

DEPARTMENT OF TRANSPORTATION : Federal Aviation Administration