SEA00LA025

NTSB accident investigation · Dassault DA-20 · Boise, ID · November 27, 1999

Accident · No injuriesLimited investigationFinal report
Date
November 27, 1999, 01:34 local (08:34 UTC)
Place
Boise, ID
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Approach
Aircraft
N216SADassault DA-20
Weather
Visual (VMC) · Night/dark
Status
Completed · report May 17, 2001
Report
Approved by Office Director
FAA report
19991127041999A
Case key
48525

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

Failure of the forward gear door lock pin. An inoperative landing gear door and inadequate maintenance inspection of the aircraft were factors.

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/malfunctionApproach - vfr pattern - final approach
Door,landing gear - inoperativeFactor
Miscellaneous,dowel/pin - failure,totalCause
Maintenance,inspection - inadequateOther maintenance personnelFactor
Dragged wing,rotor,pod,float or tail/skidLanding - roll

Analysis

After extending the gear for landing, the down-and-locked indication (green light) for the left main gear was not illuminated. The crew performed the emergency checklist procedures for abnormal gear extension with no success. The aircraft subsequently landed with the left main landing gear retracted. Inspection of the landing gear revealed that the pin (part number MY20248-001), which is part of the forward gear door lock, was corroded and cracked at the point of rotation, preventing proper movement of the gear door uplock.

Factual narrative

On November 27, 1999, about 0134 mountain standard time, a Dassault Falcon DA-20 twin turbo fan jet, N216SA, registered to RBS Aviation Group, Incorporated, and operated by Smith Air, Incorporated, as a 14CFR135 non-scheduled domestic cargo flight, was substantially damaged while landing at Boise Air Terminal, Boise, Idaho. Visual meteorological conditions prevailed and an instrument flight plan was filed. The captain, an airline transport pilot, and commercially-rated first officer were uninjured. The flight originated from Eppley Field, Omaha, Nebraska, approximately two hours and 45 minutes prior to the accident.

In a written statement prepared by both the captain and first officer, the pilots reported that while on final approach to runway 10L, the captain instructed the first officer to lower the landing gear. After the gear handle was placed in the down position, the pilots noted that the down-and-locked indication (green light) for the left main gear was not illuminated. The pilots completed the abnormal gear extension procedures (A through C) as outlined by the checklist, (see attached Landing Gear checklist) but were unable to extend the left main gear.

After confirming that the left main gear was not extended, the pilot was cleared to land on runway 10L. During the landing roll-out, the aircraft skidded off the runway, and came to rest on the north side of the runway. The aircraft received substantial damage to the left aileron and leading edge devices.

After the accident, a maintenance crew lifted the left wing and then opened the emergency gear panel and pulled the left hand cable for the left-hand main gear uplock. The door lock released, and the left main gear door opened and the gear extended. The maintenance crew then pushed the gear into the down locks.

Further inspection of the landing gear revealed that the pin, (part number MY20248-001) which is part of the forward gear door lock, (part number VTS4424) was corroded (rusted) and cracked at the point of rotation (see attached Illustrated Parts Catalog and Figures).

The mechanic performing the inspection reported that a more detailed inspection of the landing gear door locks might have prevented this accident.

Aircraft

Registration
N216SA
Reported as
Dassault DA-20
Category
Airplane
Serial number
16
Airframe hours
28,855
Engine
GE CF-700, 4,500 lbs thrust, turbo fan
Damage
Substantial damage
Flight
Part 135
Operator
Smith Air, Inc.
Registered owner
Rbs Aviation Group
Airworthiness certificate
Standard, Normal
Last inspection
AAIP · October 27, 1999 · 142 hours before
Departed
OMA · Omaha, NE
Destination
BOI
Flight plan
IFR
Airport
BOI · Boise Air Terminal, runway 10L, 10,000 × 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
48
Certificates
Flight instructor, Airline transport, Commercial
Airplane ratings
Multi-engine land, Single-engine land
Instrument ratings
Airplane
Medical
Class 1, Valid Medical--w/ waivers/lim
Seat
Left
Flight hours
19,519 total · 341 in this make and model · 17,143 as pilot in command · 208 in the last 90 days · 106 in the last 30 days

Weather

Conditions
Visual (VMC) · Night/dark
Wind
140° at 9 knots
Visibility
10 statute miles
Lowest ceiling
7,000 ft broken
Temperature
43 °F, dew point 36 °F
Altimeter
29.00 inHg
Observed at
BOI

FAA reports on this event · 1

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