CHI89FA183

NTSB accident investigation · McDonnell Douglas MD-80 · Chicago, IL · September 12, 1989

Accident · Minor injuriesField investigationFinal report
Date
September 12, 1989, 17:46 local (22:46 UTC)
Place
Chicago, IL
Injuries
2 minor, 108 uninjured
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N244AAMcDonnell Douglas MD-80
Weather
Visual (VMC) · Night/dark
Status
Completed · report September 11, 1992
Report
Approved by Office Director
FAA report
19890912036139A
Case key
14275

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

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Probable cause

A loss of hydraulic system pressure due to the operator's failure to replace a system component that had a known history of failures, and the pilot's improper use powerplant controls resulting in a degradation of rudder effectiveness. A contributing factor was the failure of the power transfer unit shutoff valve.

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.

Airframe/component/system failure/malfunctionDescent - normal
Hydraulic system,shutoff valve - failure,totalFactor
Material defectManufacturerFactor
Hydraulic system - no pressureCause
Maintenance,replacement - not performedCompany maintenance personnelCause
Loss of control - on ground/waterLanding - roll
Powerplant controls - improper use ofPilot in commandCause
Directional control - not maintainedPilot in commandCause
Ground loop/swerve - inadvertentPilot in command
On ground/water collision with objectLanding - roll
Object - other
Nose gear collapsedLanding - roll

Analysis

During descent a complete hydraulic system failure occurred. During the landing rollout the airplane ran off the side of the runway & collided with a manhole cover collapsing the nose gear. The power transfer unit shutoff valve, p/n 240695, failed; one of the dual valve body halves separated at the mounting plate. The valve had a known history of failures, and a kit version of a 'fix' to the valve had been available by the manufacturer. The flight manual cautions that for landing with no hydraulic power, increasing amounts of reverse thrust significantly reduces rudder effectiveness, and in the event of directional control problems to reduce reverse thrust as required and select forward idle if necessary to maintain or regain control. Dfdr readout show the application of thrust greater than idle reverse during the the landing rollout.

Aircraft

Registration
N244AA
Reported as
McDonnell Douglas MD-80
Category
Airplane
Serial number
49256
Airframe hours
16,332
Engine
P&W JT8D-217A & C, turbo fan
Damage
Substantial damage
Flight
Part 121
Operator
American Airlines
Registered owner
Connecticut National Bank
Airworthiness certificate
Standard, Transport
Last inspection
Continuous airworthiness · September 11, 1989 · 6 hours before
Departed
ROC · Rochester, NY
Flight plan
IFR
Airport
ORD · Chicago O'Hare Intl, runway 9R, 10,141 × 150 ft, asphalt

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
39
Certificate
Airline transport
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Airplane
Medical
Class 1, Valid Medical--no waivers/lim.
Seat
Left
Flight hours
4,600 total · 876 in this make and model · 160 in the last 90 days

Weather

Conditions
Visual (VMC) · Night/dark
Wind
10° at 6 knots
Visibility
15 statute miles
Lowest ceiling
11,000 ft broken
Temperature
63 °F, dew point 46 °F
Altimeter
30.00 inHg
Observed at
ORD

FAA reports on this event · 1

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

Other investigations on N244AA · 1

Matched to the same aircraft by N-number and date.