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96-04-11 R1: Fuel Flow Governors

FAA order 96-04-11 R1 is an airworthiness directive in force since November 30, 2011. The FAA's subject line: Fuel Flow Governors. It names Boeing 757: about 440 aircraft on the U.S. register today, though an order usually covers particular versions or serial numbers rather than every one. System: engine.

What it applies to as the FAA lists it

Kind of product
Aircraft
Makes
The Boeing Company
Models
757-200 Series, 757-200CB Series, 757-200PF Series
On this site
Boeing 757 440 registered

Dates and paperwork

In force since
November 30, 2011
Published
February 23, 1996
Docket
98-NM-294-AD
Status
Current
The FAA's document
Read the order on the FAA's site

The FAA's summary their words, unchanged

This amendment revises an existing airworthiness directive (AD), applicable to certain Boeing Model 757-200 series airplanes, that currently requires a revision to the Airplane Flight Manual to ensure that the flightcrew activates the engine cowl thermal anti-ice (CTAI) system for both engines at the top of descent to avoid engine rundown (loss of engine power). This amendment clarifies the relationship between two existing AD's. The actions specified in this AD are intended to ensure that the flightcrew activates the engine cowl thermal anti-ice system for both engines prior to descent; activation of the engine CTAI system in the middle of descent could result in a compressor stall and subsequent engine rundown of multiple engines.

The order itself the regulatory text, as published

Show the full text (2,681 characters)
96-04-11R1 BOEING: Amendment 39-10887. Docket 96-NM-30-AD. Revises AD 96-04-11, amendment 39-9523.\n\n\tApplicability: Model 757-200 series airplanes, equipped with Rolls Royce Model RB211- 535E4/E4B engines; certificated in any category. \n\n\tCompliance: Required as indicated, unless accomplished previously. \n\n\tTo reduce the risk of engine rundown during idle descents, accomplish the following: \n\t(a)\tWithin 30 days after the effective date of this AD, revise the Limitations Section of the FAA-approved Airplane Flight Manual (AFM) to include the following statement. \n \nThis may be accomplished by inserting a copy of this AD in the AFM. \n\n\n"Limitations Section 1 \n\nIn order to reduce the risk of engine rundown during idle descents, activate the engine cowl thermal anti-ice system for both engines prior to idle descents above flight level (FL) 200. Below FL 200, use normal engine cowl thermal anti-ice system procedures (as defined in the AFM). \n\nNOTE: The Master Minimum Equipment List (MMEL) for Model 757 series airplanes currently specifies that an airplane may be dispatched with an engine anti-ice valve locked in the closed position. The requirement of this section to activate the engine cowl thermal anti-ice system prior to descent will prevent the dispatch of airplanes with an engine anti-ice valve locked in the closed or open position. Where differences exist between the current specification of the MMEL and the requirements of this AFM limitation, the AFM limitation prevails." \n\n\tNOTE 1: AD 97-02-12, amendment 39-9897, requires installation of improved fuel flow governors (FFG) on both engines of Boeing Model 757-200 series airplanes. Accomplishment of this installation constitutes terminating action for the requirement of this AD.\n\n\t(b)\tAn alternative method of compliance or adjustment of the compliance time that provides an acceptable level of safety may be used if approved by the Manager, Seattle Aircraft Certification Office (ACO),FAA, Transport Airplane Directorate. Operators shall submit their requests through an appropriate FAA Principal Operations Inspector, who may add comments and then send it to the Manager, Seattle ACO. \n\n\tNOTE 2: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Seattle ACO. \n\n\t(c)\tSpecial flight permits may be issued in accordance with sections 21.197 and 21.199 of the Federal Aviation Regulations (14 CFR 21.197 and 21.199) to operate the airplane to a location where the requirements of this AD can be accomplished. \n\n\t(d)\tThis amendment becomes effective on November 30, 1998.

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Source: FAA Dynamic Regulatory System, airworthiness directives. The FAA's document is the authority; the register counts are this site's, from the FAA register of November 6, 2026. Connections as data: /graph/directive/96-04-11 R1.json · aircraft systems.