DEN88MA203

NTSB accident investigation · Mcdonnell Douglas DC-10-10 · Denver, CO · September 12, 1988

Accident · Minor injuriesMajor investigationFinal report
Date
September 12, 1988, 13:50 local (19:50 UTC)
Place
Denver, CO
Injuries
1 minor, 206 uninjured
Damage
Substantial damage
Phase of flight
Landing
Aircraft
N1830UMcdonnell Douglas DC-10-10
Weather
Visual (VMC) · Day
Status
Completed · report July 12, 1991
Report
Approved by Office Director
FAA report
19880912041389A
Case key
17547

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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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/malfunctionLanding - roll
Thrust reverser,cockpit control - bentCause
Thrust reverser,cockpit control - binding(mechanical)Cause
Thrust reverser - inoperativeCause
Loss of control - on ground/waterLanding - roll
Monitoring - inadequateFlight engineerCause
Reversers - improper use ofPilot in commandCause
Directional control - not maintainedPilot in commandCause
Nose gear collapsedLanding - roll
Terrain condition - rough/uneven
Landing gear,nose gear - overload

Analysis

As the capt was deploying reversers drg lndg, #2 & #3 reversers unlocked & deployed (green lgt cond), but #1 reverser was binding & only moved to the unlocked psn (amber lgt cond). Capt was not warned of this cond, though 2nd officer should have monitored lgts. Capt said he rchd to check #1 lever. At abt that time, acft yawed rgt. Despite imt action bythe capt, drctnl ctl of acft was lost due to yawing caused by inop thrust reverser. Acft contd off rwy, crossed 2 twys &nose gear collapsed. After stopping, evacuation was ordered. Evacuation slides deployed nmly, but with the acft on its nose, use of slides at doors 4L & 4R was discontinued due to excessive vertical angle of slides. Inv revealed that aftertchdwn, #1 eng accelerated with fwd thrust as #2 & #3 engs provided reverse thrust. At abt the same time, the acft's nose lifted off the rwy to a 4 deg attitude & the acft went off the rwy. An exam of the throttle quadrant revealed the S1-847 sw was curled/twisted & 2 support shafts (holding the sws) were bent causing intmt opn of the #1 reverser.

Aircraft

Registration
N1830U
Reported as
Mcdonnell Douglas DC-10-10
Category
Airplane
Serial number
46629
Airframe hours
37,265
Engine
GE CF6-6D, 39,300 lbs thrust, turbo fan
Damage
Substantial damage
Flight
Part 121
Registered owner
United Airlines
Airworthiness certificate
Standard, Transport
Last inspection
Continuous airworthiness · June 19, 1988 · 1,130 hours before
Departed
ORD · Chicago, IL
Destination
DEN
Flight plan
IFR
Airport
DEN · Stapleton Intl, runway 26L, 10,004 × 150 ft, concrete

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
56
Certificates
Commercial, 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
22,500 total · 233 in the last 90 days · 79 in the last 30 days · 3 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
360° at 7 knots
Visibility
5 statute miles
Lowest ceiling
1,400 ft overcast
Temperature
45 °F, dew point 43 °F
Altimeter
30.00 inHg
Observed at
DEN

FAA reports on this event · 1

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