FTW95LA168

NTSB accident investigation · Cessna 172 RG · Tulsa, OK · April 13, 1995

Accident · No injuriesLimited investigationFinal report
Date
April 13, 1995, 16:18 local (21:18 UTC)
Place
Tulsa, OK
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Landing
Aircraft
N6394VCessna 172 RG
Weather
Visual (VMC) · Day
Status
Completed · report October 19, 1995
Report
Approved by Office Director
FAA report
19950413007959A
Case key
19393

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

The pilot's improper emergency procedure preventing emergency gear extension. A factor was the loss of electrical alternator power for undetermined reasons.

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.

In flight collision with terrain/waterLanding - roll
Electrical system,alternator - output lowFactor
Electrical system,circuit breaker - popped/tripped
Reason for occurrence undetermined
Gear extension - not attainedPilot in command
Emergency procedure - improperPilot in commandCause

Analysis

The pilot noticed that the gear up indicator light was not illuminated and that the gear was partially extended. During the second attempt to fully extend the gear, the pilot observed the 'green light' indication in the cockpit; however, the pilot then 'elected to cycle it a couple of more times' and with the gear retracted continued the flight. Subsequently, the pilot noted a reduced electrical power output as the radio lights had faded in intensity and the ammeter indicated a discharge. The pilot reported referring to the operations manual for extension of the landing gear; however, 'despite 60 to 70 strokes, the gear would not lower.' Following the landing, it was determined that the main gear were partially extended and the nose gear was fully extended with structural damage occurring to the fuselage. The alternator circuit breaker was 'popped' for an undetermined reason. Following the accident, the FAA inspector observed the pilot 'pump' the emergency gear handle 'in and out.' The emergency checklist states pump 'perpendicular to handle.'

Factual narrative

On April 13, 1995, at 1618 central daylight time, a Cessna 172 RG, N6394V, was substantially damaged during a gear up landing at Tulsa International Airport, Tulsa, Oklahoma. The commercial pilot was not injured. The flight was being operated as a business aerial photography flight under Title 14 CFR Part 91. Visual meteorological conditions prevailed for the cross country flight and a flight plan was not filed.

The pilot reported that the flight departed at 1330 for the planned aerial photography mission in the areas of McAlester and Kiowa, Oklahoma. Following the photography session where the gear and flaps were extended, the landing gear retraction procedure was initiated by the pilot. During the en route climb through approximately 3,000 feet MSL, the pilot noticed that the gear up indicator light was not illuminated and that the gear was partially extended. The pilot referred to the checklist and during the second attempt the gear extended and the pilot observed the "green light" indication in the cockpit. The pilot then "elected to cycle it a couple of more times" and with the gear retracted continued the en route climb. In the vicinity of Okmulgee, Oklahoma, the pilot noted a reduced electrical power output as the radio lights had faded in intensity and the ammeter indicated a discharge.

The pilot further reported that he referred to the operations manual for a manual extension of the landing gear; however, "despite 60 to 70 strokes, the gear would not lower." While manuevering the airplane in the vicinity of the Tulsa International Airport, the pilot observed a "green light" from the tower and landed the airplane on runway 18R. The main gear were partially extended and the nose gear was fully extended.

The Federal Aviation Administration (FAA) inspector examined the airplane and found the alternator circuit breaker "popped." Structural damaged occurred to the fuselage. During a demonstration by the pilot, the inspector observed the pilot "pump" the emergency gear handle "in and out." The emergency checklist states pump "perpendicular to handle."

Aircraft

Registration
N6394V
Reported as
Cessna 172 RG
Category
Airplane
Serial number
172RG0656
Airframe hours
3,590
Engine
Lycoming IO-360-F1A6, 180 horsepower, reciprocating
Damage
Substantial damage
Flight
Part 91
Operator
Midcontinent Aircraft Services
Registered owner
Lester L. Wagner
Airworthiness certificate
Standard, Normal
Last inspection
Annual · February 8, 1995 · 50 hours before
Departed
TUL
Destination
TUL
Airport
TUL · Tulsa International, runway 18R, 6,101 × 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
Certificate
Commercial
Airplane ratings
Single-engine land
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--no waivers/lim.
Seat
Left
Flight hours
4,252 total · 100 in this make and model · 4,155 as pilot in command · 3 in the last 30 days · 2 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
190° at 8 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
72 °F, dew point 39 °F
Altimeter
30.00 inHg
Observed at
TUL

FAA reports on this event · 1

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