NTSB CAROL · Event
Event ATL96LA073
Registry · N999TF
FAA Aircraft Registry record.
Make / Model
CIRRUS DESIGN SR22
TCDS
A00009CH · CIRRUS DESIGN CORP
Engine
CONT MOTOR IO-550-N (310 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
20070515
ADS-B equipped
Yes — Mode-S ADF5C1
Registrant of record
SPENCER BRETT
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
the flight crew's inadequate emergency procedure in that they did not manually extend the landing gear, as specified in the airplane flight manual. A factor relating to the accident was: the intermittent operation of the extend solenoid in the nose gear selector valve.
Factual narrative
On April 1, 1996, about 1004 eastern standard time, Canadair CL-600-1A11, N999TF, nose landing gear collapsed on landing at the Raleigh-Durham Airport, Raleigh, North Carolina. The aircraft was being operated by Pal-Waukee Aviation under the provisions of 14 CFR Part 135 and instrument flight rules. Instrument meteorological conditions existed at the time of the accident, and an instrument flight rules flight plan was in effect. The airline transport pilot, his co-pilot, the cabin attendant, and the six passengers were not injured; the aircraft was substantially damaged. The flight departed Milwaukee, Wisconsin at 0830 the same day. The pilot stated that when the landing gear was extended, the landing gear position indicating system presented conflicting information regarding the position of the nose landing gear. The landing gear was then raised, and the indicator lights were all extinguished. The gear was again extended. The main gear indicator lights were illuminated, indicating that the main gear was down, but the nose gear light was extinguished. The light in the gear handle was off, indicating that the system was functioning properly. The pilot did not use the emergency landing gear extension system. The aircraft was landed and the nose gear collapsed. The pilot stated that the clouds and visibility precluded any observation of the landing gear by airport tower personnel. Post accident examination of the nose gear selector valve revealed an intermittently inoperative extend solenoid valve. According to the failure analysis report, the solenoid valve most likely experienced moisture entry. The manufacturer reported that the selector valve was repaired with an upgraded solenoid to preclude recurrence of the failure. During an instrument landing system (ILS) approach the airline transport pilot noticed a discrepancy in the landing gear indicators. He raised the landing gear and lowered it again. The main landing gear indicator lights were illuminated, indicating that the main gear was extended and locked, but the nose gear light was extinguished. The light in the gear handle was off, indicating that the system was functioning properly. The pilot did not use the emergency landing gear extension system. The aircraft was landed, and the nose gear collapsed. Subsequent examination revealed an intermittently operating extend solenoid in the nose gear selector valve. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1996_ATL96LA073.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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