The U.S. aircraft register, updated daily
FAA orders · airworthiness directive · historical

98-24-51: AFM - Autoland System

FAA order 98-24-51 is an airworthiness directive in force since December 7, 1998. The FAA's subject line: AFM - Autoland System. It names Mcdonnell Douglas MD-11: about 104 aircraft on the U.S. register today, though an order usually covers particular versions or serial numbers rather than every one. System: flight controls.

What it applies to as the FAA lists it

Kind of product
Aircraft
Makes
McDonnell Douglas Corporation
Models
MD-11 Series (all)
On this site
Mcdonnell Douglas MD-11 104 registered

Dates and paperwork

In force since
December 7, 1998
Published
December 2, 1998
Docket
98-NM-334-AD
Replaced by
2002-23-18
Status
Historical
The FAA's document
Read the order on the FAA's site

The FAA's summary their words, unchanged

This document publishes in the Federal Register an amendment adopting airworthiness directive (AD) T98-24-51 that was sent previously to all known U.S. owners and operators of certain McDonnell Douglas Model MD-11 series airplanes by individual telegrams. This AD requires a revision to the Airplane Flight Manual to prohibit autopilot coupled autoland operations in certain conditions; or, for certain airplanes, replacement of certain Collins LRA-900 radio altimeters with Collins LRA-700 radio altimeters. This action is prompted by a report that a fault in certain Collins LRA-900 radio altimeters could result in an incorrect and unbounded output of radio altitude to other airplane systems. The actions specified by this AD are intended to prevent an undetected anomalous radio altitude signal that is passed along to the flare control law of the flight control computer, which could cause the airplane to flare too high or too low during landing, and consequently result in a hardlanding.

The order itself the regulatory text, as published

Show the full text (2,618 characters)
98-24-51 MCDONNELL DOUGLAS: Amendment 39-10929. Docket 98-NM-334-AD. \n\n\tApplicability: Model MD-11 series airplanes, equipped with certain Collins LRA-900 radio altimeters, having part number 822-0334-002, 822-0334-020, or 822-0334-220; certificated in any category. \n\n\tCompliance: Required as indicated, unless accomplished previously. \n\n\tTo detect and correct an undetected anomalous radio altitude signal that is passed along to the flare control law of the flight control computer, which could cause the airplane to flare too high or too low during landing, and consequently result in a hard landing, accomplish the following: \n\n\t(a)\tWithin 24 hours after the effective date of this AD, accomplish either paragraph (a)(1) or (a)(2) of this AD: \n\n\t\t(1)\tRevise the Limitations Section of the FAA-approved Airplane Flight Manual to include the following statement: \n\n"Autopilot coupled autoland operations below 100 feet above ground level (AGL) are prohibited."\n\n\t\t(2)\tFor airplanes on which the LRA-700 radio altimeter installation has been approved in accordance with Type Certificate or Supplemental Type Certificate procedures: Replace both Collins LRA-900 radio altimeters having part number 822-0334-002, 822-0334-020, or 822-0334-220, with Collins LRA-700 radio altimeters having part number 622-4542-221. \n\n\t(b)\tAs of the effective date of this AD, no person shall install on any airplane a Collins LRA-900 radio altimeter, having part number 822-0334-002, 822-0334-020, or 822-0334-220. \n\n\t(c)\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, Los Angeles Aircraft Certification Office (ACO), FAA, Transport Airplane Directorate. Operators shall submit their requests through an appropriate FAA Principal Maintenance Inspector, who may add comments and then send it to the Manager, Los Angeles ACO. \n\n\tNOTE: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Los Angeles ACO. \n\n\t(d)\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(e)\tThis amendment becomes effective on December 7, 1998, to all persons except those persons to whom it was made immediately effective by telegraphic AD T98-24-51, issued on November 19, 1998, which contained the requirements of this amendment.

Related safety bulletins advice on the same designs, not orders

2018-12-17NM-18-33 · Engine Fuel and Control
2014-11-24NM-15-03 · Flight Controls
2008-12-11NM-09-03 · Engine Fuel and Control - Implementing Fuel Tank System Airworthiness Limitations
2007-04-24NM-07-31 · Rigid hydraulic case drain lines
2006-07-27NM-06-57 · Reports of damage to airplanes and to property on the ground caused by blue or clear ice falling from airplanes.

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/98-24-51.json · aircraft systems.