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Aviation safety reports, made easier to study

NTSB Reports is an independent research and search tool for public aviation accident and incident records. It brings NTSB aviation reports, structured fields, docket files, extracted figures, photos, videos, and update history into one searchable interface.

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NTSB Report

August 11, 2005 · Agusta Spa SF 260D · N402FD

Redding, CA

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
August 11, 2005
Injury Outcomes
No injuries (1 uninjured)
Location
Redding, CA
Aircraft
Agusta Spa SF 260D
Tail Number
N402FD
Injuries
None
Aircraft Damage
Substantial
NTSB Number
LAX05LA266

The airplane's canopy separated from the cockpit during the landing descent, and substantially damaged the empennage. The pilot indicated that he had not experienced any malfunction with the canopy's operation when he initiated the flight, and that the latch was in the closed position when the separation occurred. A subsequent search for the separated canopy was unsuccessful. An examination of the airplane revealed that the leading edge of the left horizontal stabilizer was crushed inward over approximately a 1-foot-long span. Also, the leading edge of the vertical stabilizer was similarly crushed in an aft direction. This was the first flight following the company's removal and reinstallation of a serviceable canopy. The company mechanics suggested that they may not have verified that the canopy's locking pins were positively engaged in the support lugs on the airframe during reinstallation of the canopy.

NTSB Probable Cause

the company maintenance personnel's failure to follow a prescribed canopy installation procedures.

Full Narrative

On August 11, 2005, about 1259 Pacific daylight time, an Agusta SPA, SF.260D, N402FD, experienced the separation of its canopy during descent for landing at the Redding Municipal Airport, Redding, California. The airplane was substantially damaged, and the commercial pilot was not injured. The airplane was owned and operated by Air Combat USA, Inc., Fullerton, California. Visual meteorological conditions prevailed at the time of the work-related flight, and no flight plan had been filed. The flight was performed under the provisions of 14 CFR Part 91, and it originated from Fullerton about 1000. The pilot reported to the National Transportation Safety Board investigator that between 8 and 10 miles from Redding the entire canopy separated from the airplane. Also, the helmet he was wearing came off his head, and baggage exited the airplane. The pilot was unable to contact the Redding control tower, so he changed to the emergency transponder code. Thereafter, he received a green light signal from the control tower, and he landed without further mishap. The pilot indicated that he had not experienced any malfunction with the canopy's operation when he initiated the flight. He stated that when the canopy separated its latch was in the closed position. Company personnel reported to the Safety Board investigator that their search for the separated canopy was unsuccessful. An examination of the airplane revealed that the leading edge of the left horizontal stabilizer was crushed inward over approximately a 1-foot-long span. Also, the leading edge of the vertical stabilizer was similarly crushed in an aft direction. According to company personnel, this was the first flight following the company's removal and reinstallation of a serviceable canopy. A company mechanic opined that this procedure to reinstall a canopy involved checking that the canopy's locking pins were positively engaged in the support lugs on the airframe. The mechanic indicated to the Safety Board investigator that this verification procedure had evidently not been complied with by the mechanics who had installed the canopy.

Flight

Event TypeAccident
Event Time12:59 PDT
Nearest AirportREDDING (10nm)
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftAgusta Spa SF 260D
Tail NumberN402FD
Aircraft CategoryAir
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · O-540-E4AS · Reciprocating · 260
Seats2

People & Injuries

Injury SummaryNo injuries (1 uninjured)
Fatal0
Serious0
Minor0
Uninjured1
Total1
Crew 1Age 37 · Second Class · None

Conditions

ConditionsVMC
LightDaylight
Wind330° @ 8 kt
Visibility10 sm
CeilingNone
Temperature / Dew Point10 C / 37 C
Altimeter29.88 inHg
Observation Time19:59
Weather SourceWFAC

Appendix: Source Data