LAX92IA390

NTSB incident investigation · McDonnell Douglas MD-11 · Yuma, AZ · September 17, 1992

Incident · No injuriesIncident investigationFinal report
Date
September 16, 1992, 22:20 local (Sep 17, 1992, 05:20 UTC)
Place
Yuma, AZ
Injuries
8 uninjured
Damage
Minor damage
Phase of flight
Landing
Aircraft
N90187McDonnell Douglas MD-11
Weather
Visual (VMC) · Night/bright
Status
Completed · report September 14, 1993
Report
Approved by Office Director
FAA report
19920916042139I
Case key
27461

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the incident.

On this page

Probable cause

An unstable interaction between the center body main landing gear and the brake system.

Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

Other gear collapsedLanding - roll
Landing gear,anti-skid brake system - erraticCause
Acft/equip,inadequate designManufacturer
Landing gear,main gear strut scissors - failure,total
Landing gear,main gear - collapsed

Analysis

Mcdonnell Douglas instrumented a flight test MD11 to explore two previous in service incidents of center main body landing gear drag link failures. The test protocol was designed to replicate the known circumstances of the two in service failures. During the landing on the test flight, a failure of the drag link was induced, which allowed the center main body gear to fold aft damaging the wheel well and adjacent skin panels. Examination of the instrumentation data revealed that the drag link failure was the result of a dynamic instability of the center body gear due to an unfavorable interaction between the center body landing gear and the brake control system (including the anti skid and auto brake sub systems). As a corrective action, the manufacturer developed a modification to the anti skid control unit.

Aircraft

Registration
N90187
Reported as
McDonnell Douglas MD-11
Category
Airplane
Serial number
48437
Engine
P&W PW4460, 60,000 lbs thrust, turbo fan
Damage
Minor damage
Flight
Part 91
Operator
Mcdonnel Douglass Corp
Registered owner
Mcdonnel Douglass Corp
Airworthiness certificate
Standard, Transport
Last inspection
Continuous airworthiness · January 2, 2000
Flight plan
IFR
Airport
YUM · Yuma Intl, runway 21, 13,299 × 200 ft, concrete

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
47
Certificate
Airline transport
Airplane ratings
Multi-engine land, Single-engine land
Instrument ratings
Airplane
Medical
Class 1, Valid Medical--w/ waivers/lim
Seat
Left
Flight hours
15,000 total

Weather

Conditions
Visual (VMC) · Night/bright
Visibility
50 statute miles
Lowest ceiling
None
Temperature
90 °F, dew point -0 °F

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.