CHI93IA035

NTSB incident investigation · McDonnell Douglas DC-8-71 · Chicago, IL · November 13, 1992

Incident · No injuriesIncident investigationFinal report
Date
November 13, 1992, 06:50 local (12:50 UTC)
Place
Chicago, IL
Injuries
3 uninjured
Damage
Minor damage
Phase of flight
Enroute
Aircraft
N870SJMcDonnell Douglas DC-8-71
Weather
Visual (VMC) · Not reported
Status
Completed · report September 14, 1993
Report
Approved by Office Director
FAA report
19921113055949I
Case key
15590

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 improper repair of the retract pin boss area by the overhaul facility.

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.

Gear not retractedClimb - to cruise
Landing gear,main gear - movement restricted
Airframe/component/system failure/malfunctionClimb - to cruise
Landing gear,normal retraction/extension assembly - failure,totalFactor
Maintenance,major repair - improperOther maintenance personnelCause
Landing gear,normal retraction/extension assembly - fatigueFactor

Analysis

The crew of the mcdonnell-douglas DC-8 cargo airplane retracted the landing gear during its climb to cruise altitude. The crew advised air traffic control that the landing gear had not retracted properly. During an attempt to ensure the landing gear was in the down and locked position the crew heard a loud bang. Coincidental with the aircrew's actions, a person residing in a single family home reported that a metal object had penetrated her home's roof and imbedded itself in the floor. The airplane returned to land without further incident. An on-scene investigation revealed the right main landing gear retract pin had separated from the landing gear leg. Portions of the gear leg retract pin boss area had separated and were found wedged along side the gear assembly. Subsequent metallurgical investigation revealed the pin boss area had metal fracture features consistent with overload, one of which was consistent with a preexisting fracture area. The pin boss area had previously been over-bored and chrome plated prior to a return to service. The airplane manufacturer stated the pin boss bore should not be chrome plated.

Aircraft

Registration
N870SJ
Reported as
McDonnell Douglas DC-8-71
Category
Airplane
Serial number
46039
Airframe hours
27
Engine
GE CFM56-2C1, turbo fan
Damage
Minor damage
Flight
Part 121
Operator
Southern Air Transport
Registered owner
Aero USA
Airworthiness certificate
Standard, Transport
Last inspection
Continuous airworthiness · May 21, 1992 · 1,554 hours before
Flight plan
IFR

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
54
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
7,850 total · 338 in this make and model

Weather

Conditions
Visual (VMC) · Not reported
Wind
330° at 10 knots
Visibility
5 statute miles
Lowest ceiling
15,000 ft overcast
Temperature
36 °F
Observed at
ORD, 10 nm away

FAA reports on this event · 1

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