1 RULES: General Electric Co.,
This amendment adopts a new airworthiness directive (AD) that is applicable to General Electric Company CF680E1 model turbofan engines. This action requires flex borescope inspections of high pressure turbine (HPT) stage two (S2) nozzle guide vanes (NGV) installed in CF680E1 model turbofan engines. This amendment is prompted by an uncontained
2 RULES: Pilatus Britten-Norman Ltd.,
This amendment adopts a new airworthiness directive (AD) that applies to certain Pilatus BrittenNorman Limited (Pilatus Britten Norman) BN2, BN2A, BN2B, and BN2T series airplanes. This AD requires you to repetitively inspect the inboard brackets of the elevator outboard hinge for loose rivets, structural damage, or cracks and replace any suspect
3 RULES: Boeing,
This amendment adopts a new airworthiness directive (AD), applicable to all Boeing Model 727 series airplanes, that requires repetitive inspections for cracking of the upper chord of the rear spar of the wing, and corrective action, if necessary. This action is necessary to find and fix such cracking, which could result in fuel leaking through the
4 RULES: CFM International, S.A.; correction,
This document makes a correction to Airworthiness Directive (AD) 20020213, applicable to CFM International, S.A. CFM565 series turbofan engines that was published in the Federal Register on February 14, 2002 (67 FR 6850). The Amendment number is incorrect and this document corrects that number. In all other respects, the original
5 PROPOSED RULES: Boeing,
This document proposes the supersedure of an existing airworthiness directive (AD), applicable to certain Boeing Model 737 600, 700, and 800 series airplanes, that currently requires repetitive inspections to detect discrepancies of the quickdisconnect coupling on the fuel hose located at the fan case firewall; corrective action, if necessary; and
6 RULES: Bombardier-Rotax GmbH; correction,
This document makes a correction to Airworthiness Directive (AD) 20021626, applicable to BombardierRotax GmbH type 912 F and 914 F series reciprocating engines. AD 20021626 was published in the Federal Register on August 15, 2002 (67 FR 53296). The effective date in the DATES: section is incorrect. This document corrects that date. In all other
7 PROPOSED RULES: McDonnell Douglas,
This document proposes the supersedure of an existing airworthiness directive (AD), applicable to certain McDonnell Douglas Model MD11 airplanes, that currently requires, among other actions, a onetime inspection to detect discrepancies at certain areas around the entry light connector of the sliding ceiling panel above the forward passenger
8 PROPOSED RULES: Textron Lycoming,
The Federal Aviation Administration (FAA) proposes to supersede an existing airworthiness directive (AD), 981812, applicable to certain Textron Lycoming reciprocating engines with certain Crane/Lear Romec ``AN'' rotary fuel pumps installed. That AD currently requires initial and followup torque check inspections of pump relief valve attaching
9 RULES: Rolls-Royce plc.,
This amendment adopts a new airworthiness directive (AD) that is applicable to RollsRoyce plc. (RR) models RB211535E437, RB211 535E4B37, and RB211535E4B75 turbofan engines, with certain part number (P/N) low pressure (LP) turbine stage 2 discs installed. This action requires establishing new reduced LP turbine stage 2 disc cyclic limits. This
10 PROPOSED RULES: Bell,
This document revises an earlier proposed airworthiness directive (AD) for Bell Helicopter Textron, A Division of Textron Canada (Bell), Model 407 helicopters, that would have required preflight checking and repetitively inspecting for a crack in certain tailbooms that have not been redesigned and replacing the tailboom if a crack is found. That
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