DEN05LA091

NTSB accident investigation · Cessna 340A · Santa Fe, NM · June 17, 2005

Accident · No injuriesLimited investigationFinal report
Date
June 17, 2005, 12:28 local (18:28 UTC)
Place
Santa Fe, NM
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Taxi
Aircraft
N155RPCessna 340A
Weather
Visual (VMC) · Day
Status
Completed · report October 27, 2005
Report
Approved by Office Director
Parties
Albuquerque, New Mexico
FAA report
20050617010769A
Case key
61756

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

On this page

Probable cause

total failure of the main landing gear due to improper installation of the push-pull tubes by maintenance personnel, and their failure to follow proper procedures/directives.

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 collapsedTaxi - from landing
Maintenance,installation - improperOther maintenance personnelCause
Landing gear,main gear - failure,totalCause
Procedures/directives - not followedOther maintenance personnelCause

Analysis

While taxiing from landing following a post-annual inspection flight, the right main landing gear collapsed. Maintenance records indicated both main landing gear push-pull tubes had been removed when the gear was rigged. The service manual requires the drive tubes --- not the push-pull tubes --- be disconnected. The left push-pull appeared to have been installed upside down and had not been properly aligned. Aircraft load was transmitted to the center pivot on the main landing gear bellcrank, causing it to fail. NTSB's Materials Laboratory said there was a "ductile overstress fracture in direct shear," causing instantaneous overload of the bolt.

Factual narrative

On June 17, 2005, at 1228 mountain daylight time, a Cessna 340A, N155RP, piloted by an airline transport pilot, was substantially damaged when the right main landing gear collapsed while taxiing from landing at Santa Fe Municipal Airport (SAF), Santa Fe, New Mexico. Visual meteorological conditions prevailed at the time of the accident. The local personal flight was being conducted under the provisions of 14 CFR Part 91 without a flight plan. The pilot was not injured. The flight originated at Santa Fe, New Mexico, approximately 1155.

The pilot said this was the first flight for the airplane after an annual inspection, and he was "breaking in a new cylinder." The flight, which included an in-flight gear extension and retraction, was uneventful. After landing and while taxiing back to the hangar, the right main landing gear collapsed and the right wing struck the ground.

Postaccident inspection disclosed multiple broken ribs in the right wing. A bolt attached to the lower portion of the bell crank was sheared and the main landing gear trunion was broken. An FAA inspector said that during the annual inspection, maintenance personnel had improperly rigged the main landing gear. According to maintenance records, both main landing gear push-pull tubes were removed when the gear were rigged. The Cessna 340A service manual requires the drive tubes --- not the push-pull tubes --- be disconnected. The left push-pull appeared to be installed upside down. When the center attach point bolt sheared, the load was transmitted to the clevis on the landing gear trunion and it failed. A Cessna Aircraft Company spokesman agreed, saying the failure mode of the bolt suggested improper rigging of the overcenter mechanism. When the push-pull tubes were reinstalled, they were not properly aligned. Aircraft load was transmitted to the center pivot on the main landing gear bellcrank, causing it to fail. The failed bolt was examined by NTSB's Materials Laboratory. Their report confirmed "ductile overstress fracture in direct shear" caused by instantaneous overload of the bolt.

Numerous attempts to obtain a completed NTSB Form 6120.12 from the pilot were unsuccessful.

Aircraft

Registration
N155RP
Reported as
Cessna 340A
Category
Airplane
Serial number
340A1265
Engine
Continental TSIO-520-NB, reciprocating
Damage
Substantial damage
Flight
Flight test · Part 91
Last inspection
Annual · June 1, 2005 · 1 hours before
Departed
SAF · Sante Fe, NM
Destination
SAF · Sante Fe, NM
Airport
KSAF · Sante Fe Municipal, runway 150, 6,307 × 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
57
Injuries
None
Certificates
Commercial, Airline transport
Airplane ratings
Multi-engine land, Single-engine land
Medical
Class 1, With waivers/limitations
Flight hours
9,268 total · 9,166 as pilot in command

Weather

Conditions
Visual (VMC) · Day
Wind
240° at 10 knots, gusting 14
Visibility
10 statute miles
Lowest ceiling
None
Temperature
84 °F, dew point 14 °F
Altimeter
30.04 inHg
Observed at
SAF

FAA reports on this event · 1

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