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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

December 30, 1997 · Cessna 172RG · N5404V

Van Nuys, CA

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
December 30, 1997
Injury Outcomes
No injuries (2 uninjured)
Location
Van Nuys, CA
Aircraft
Cessna 172RG
Tail Number
N5404V
Operator
Carus Air
Injuries
None
Aircraft Damage
Substantial
NTSB Number
LAX98LA065

The flight instructor stated that the student pilot had extended the landing gear on the downwind leg of the traffic pattern, but then retracted it after being told to go around by the control tower. On the second downwind leg, the student again placed the gear switch in the down position; however, neither the student nor the instructor visually verified that the gear was down and locked. During the final flare for landing, the instructor noted that the gear was not down and that the 5 amp gear warning circuit breaker had opened. He then closed the circuit breaker and noted the gear starting to extend, but it had achieved only an intermediate position at the time of touchdown. The airplane subsequently settled on to the runway and incurred damage to the underside, the right wing, and the right horizontal stabilizer. A review of the Cessna 172RG Service Manual, Drawing No. 2471000, 'Wiring Diagram-Landing Gear System' indicated that subject circuit breaker, in addition to providing power to the gear indicator lights and warning horn, also powers the main gear downlock switches and the stall warning horn.

NTSB Probable Cause

The student and flight instructor's failure to verify that the landing gear was in the down position, and the design of the electrical system in which a single-point aircraft system malfunction (one open circuit breaker) disabled both the landing gear warning system and the main gear downlock switches.

Full Narrative

On December 30, 1997, at 1400 hours Pacific standard time, a Cessna 172RG, N5404V, was substantially damaged during landing with the gear partially extended at the Van Nuys, California, airport. There were no injuries to the flight instructor or student pilot. The flight departed Van Nuys on a local instructional flight and no flight plan was filed. Visual meteorological conditions prevailed for the personal flight. The flight instructor stated in his report of accident that the student pilot had extended the landing gear on the downwind leg of the traffic pattern, but then retracted it after being told to go around by the control tower. On the second downwind leg, the student again placed the gear switch in the down position; however, neither the student pilot nor the instructor visually verified that the gear was down and locked. During the final flare for landing, the instructor noted that the gear was not down and that the 5 amp gear warning circuit breaker had opened. He then closed the circuit breaker and noted the gear starting to extend but it had achieved only an intermediate position at the time of touchdown. The airplane subsequently settled on to the runway and incurred damage to the underside, the right wing, and the right horizontal stabilizer. A review of the Cessna 172RG Service Manual, Drawing No. 2471000, "Wiring Diagram-Landing Gear System" indicated that subject circuit breaker, in addition to providing power to the gear indicator lights and warning horn, also powers the main gear downlock switches and the stall warning horn. This was verified by a telephone conversation with the Cessna Aircraft Engineering Department.

Flight

Event TypeAccident
Event Time14:00 PST
Nearest AirportVANNUYS (0nm)
Runway34
Runway Length8000 ft
Runway Width150 ft
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftCessna 172RG
Tail NumberN5404V
Aircraft CategoryAir
DamageSubstantial
OperatorCarus Air
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · O-360-F1A6 · Reciprocating · 180
Seats4

People & Injuries

Injury SummaryNo injuries (2 uninjured)
Fatal0
Serious0
Minor0
Uninjured2
Total2
Crew 1Age 36 · First Class

Conditions

ConditionsVMC
LightDaylight
Wind350° @ 5 kt
Visibility25 sm
CeilingNone
Temperature / Dew Point37 C
Altimeter29.00 inHg
Observation Time21:30
Weather SourceWFAC

Appendix: Source Data