BFO93LA020

NTSB accident investigation · Dornier DO-228-202 · Manchester, NH · January 10, 1993

Accident · No injuriesLimited investigationFinal report
Date
January 10, 1993, 13:25 local (18:25 UTC)
Place
Manchester, NH
Injuries
5 uninjured
Damage
Substantial damage
Phase of flight
Initial climb
Aircraft
N245RPDornier DO-228-202
Weather
Visual (VMC) · Day
Status
Completed · report October 13, 1993
Report
Approved by Office Director
FAA report
19930110000269A
Case key
11893

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

Incorrect installation of the seals in the nose gear assembly, which prevented the nose gear from locking in the down position.

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/malfunctionTakeoff - initial climb
Landing gear,gear warning system - inoperative
Landing gear,gear locking mechanism - not engagedCause
Installation - improperOther maintenance personnelCause
Gear not extendedLanding - roll
Landing gear,nose gear assembly - jammed

Analysis

During the initial climb after takeoff, the pilot reported that when the gear was retracted, there was an unsafe gear warning. After several unsuccessful attempts to correct the condition, including recycling the gear four times, the flight diverted. Although the pilot had down and lock indication for the three gear during the recycling, after the fourth cycle, there was no gear indication, despite attempts to extend it using the emergency gear extension system. The pilot did a low pass over the airport where air traffic control personnel confirmed the nose gear was not extended. The pilot subsequently landed nose gear up. Examination of the nose gear assembly revealed the nose gear shock strut was collapsed about three quarters of an inch from full extension, which prevented the strut from engaging the uplock during retraction, and prevent the deactivation of the unsafe warning during extension. It was also determined that the partially extended strut could improperly contact the uplock, restricting the movement of the strut. Further disassembly confirmed the incorrect installation of the two internal seals, which would prevent the strut from extending fully.

Aircraft

Registration
N245RP
Reported as
Dornier DO-228-202
Category
Airplane
Serial number
8125
Airframe hours
8,202
Engine
Garrett TPE331 5252D, 715 horsepower, turbo prop
Damage
Substantial damage
Flight
Part 135
Operator
Precision Airlines
Registered owner
Deutsche Credit Corporation
Airworthiness certificate
Standard, Normal
Last inspection
Continuous airworthiness · January 8, 1993 · 7 hours before
Departed
BOS · Boston, MA
Destination
MHT · NH
Flight plan
IFR
Airport
MHT · Manchester, runway 35, 7,001 × 250 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
30
Certificate
Airline transport
Airplane ratings
Multi-engine land, Single-engine land
Instrument ratings
Airplane
Medical
Class 1, Valid Medical--no waivers/lim.
Seat
Left
Flight hours
3,700 total · 2,650 in this make and model

Weather

Conditions
Visual (VMC) · Day
Wind
30° at 3 knots
Visibility
25 statute miles
Lowest ceiling
10,000 ft broken
Temperature
18 °F, dew point 1 °F
Altimeter
30.00 inHg
Observed at
MHT, 1 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.