LAX92FA331

NTSB accident investigation · Cessna 152 · Maricopa, AZ · August 3, 1992

Accident · FatalField investigationFinal report
Date
August 3, 1992, 09:06 local (16:06 UTC)
Place
Maricopa, AZ
Injuries
1 fatal
Damage
Destroyed
Phase of flight
Maneuvering
Aircraft
N49016Cessna 152
Weather
Visual (VMC) · Day
Status
Completed · report September 14, 1993
Report
Approved by Office Director
FAA report
19920803028749A
Case key
27446

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 exceeded the design stress limits of the airplane structure by attempting an abrupt maneuver at a speed in excess of the maneuvering speed.

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.

Airframe/component/system failure/malfunctionManeuvering
Maneuver - attemptedPilot in command
Airspeed(va) - exceededPilot in commandCause
Design stress limits of aircraft - exceededPilot in commandCause
Wing,bracing strut - overloadCause
In flight collision with terrain/waterDescent - uncontrolled

Analysis

There were no eye witnesses's to the accident. According to the operator, the pilot rented the airplane to practice ground reference maneuvers in the south practice area. The weather was VMC, and other pilots flying in the vicinity reported no significant weather phenomona. Twelve months prior to the accident at the pilots third class medical certificate renewal he reported 480 total flight hours with no hours in the preceeding six months. According to flight school records he recieved about 2.7 hours after his medical, of dual instruction and a biennial flight review. The pilot then flew solo through July 7, 1992, for about 8.7 hours. According to the metallurgist's factual report, the wings lower strut attatch points failed due to overstress. Cessna aircraft tested a 150K fuselage during certification work on the A152 model and found that the lower lift strut attatch fitting failed at 8.28 g's. engineers calculated that an airspeed of 153.2 mph was required at gross weight to generate the 8.28 g load which caused the strut attatch failure. Maneuvering speed for the aircraft is 103 mph.

Aircraft

Registration
N49016
Reported as
Cessna 152
Category
Airplane
Serial number
15281102
Airframe hours
2,873
Engine
Lycoming O-235-L2C, 110 horsepower, reciprocating
Damage
Destroyed
Flight
Personal · Part 91
Operator
Action Technical Associates
Registered owner
Action Technical Associates
Airworthiness certificate
Standard, Normal
Last inspection
Annual · February 10, 1992 · 87 hours before
Departed
GEU · Glendale, AZ
Destination
GEU

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
40
Certificate
Private
Airplane ratings
Single-engine land
Medical
Class 2, Valid Medical--no waivers/lim.
Seat
Left
Toxicology
Performed
Flight hours
491 total · 2 in the last 90 days · 1 in the last 30 days

Weather

Conditions
Visual (VMC) · Day
Wind
270° at 7 knots
Visibility
20 statute miles
Lowest ceiling
None
Temperature
-0 °F, dew point -0 °F

FAA reports on this event · 1

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