FTW02LA096

NTSB accident investigation · Mooney M20A · Norman, OK · March 16, 2002

Accident · Minor injuriesLimited investigationFinal report
Date
March 16, 2002, 09:16 local (15:16 UTC)
Place
Norman, OK
Injuries
1 minor
Damage
Substantial damage
Phase of flight
Initial climb
Aircraft
N8390EMooney M20A
Weather
Visual (VMC) · Day
Status
Completed · report September 30, 2003
Report
Approved by Office Director
Parties
Lycoming, FAA FSDO
FAA report
20020316004859A
Case key
54356

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

On this page

Probable cause

Maintenance personnel's improper clamp installation on the mixture control cable, which resulted in a loss of engine power.

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.

Loss of engine powerTakeoff - initial climb
Mixture control,cable - loose part/bolt/nut/clamp/etcCause
Maintenance,installation - improperOther maintenance personnelCause
Forced landingDescent - emergency
In flight collision with terrain/waterEmergency landing
Terrain condition - ground
In flight collision with objectEmergency landing
Object - aircraft parked/standing

Analysis

During takeoff initial climb, approximately 800-900 feet agl, the engine lost power. With no options to land straight ahead, the pilot elected to make a right 180-degree turn back to the runway. The airplane's right wing struck the ground followed by the fuselage. The airplane slid upright into two parked airplanes that were tied down on the ramp. Examination of the aircraft revealed an improper clamp installed on the mixture cable that would not allow the mixture cable to extend to the full rich position.

Factual narrative

On March 16, 2002, 0916 central standard time, a Mooney M20A single-engine airplane, N8390E, was substantially damaged when it impacted the ground during a forced landing following a loss of engine power during takeoff/initial climb from the University of Oklahoma Westheimer Airport near Norman, Oklahoma. The airplane was owned and operated by the pilot. The private pilot, sole occupant of the airplane, sustained minor injuries. Visual meteorological conditions prevailed, and a flight plan was not filed for the 14 Code of Federal Regulations Part 91 personal flight. The cross-country flight was destined for Nashua, New Hampshire, with Newton, Kansas as the first fuel stop. The flight was originating at the time of the accident.

The 346-hour pilot reported to the FAA inspector, that during initial climb out from runway 3, while climbing through approximately 800-900 feet agl, the engine lost power without warning. With no options to land straight ahead, the pilot elected to make a right 180-degree turn to attempt to return to the airport. The pilot stated that the landing gear was fully extended and the flaps were up. The airplane's right wing struck the ground followed by the fuselage. The airplane slid upright into two parked airplanes that were tied down on the ramp.

Examination of the airplane, by the FAA inspector, revealed that the airplanes right wing was separated from the fuselage.

An examination of the aircraft at Air Salvage of Dallas near Lancaster, Texas, conducted by the NTSB investigator-in-charge and a Textron Lycoming representative revealed that an improper clamp was found installed on the mixture control cable that would not allow the mixture cable to fully extend to the full rich position. Examination of the engine revealed the #1 fuel injector nozzle was loose, and the #2 fuel injector line was loose at the nozzle. All fuel injectors were found to be clean.

After multiple attempts, the NTSB was unable to obtain a completed Pilot/Operator Aircraft Accident Report (NTSB Form 6120.1/2).

Aircraft

Registration
N8390E
Reported as
Mooney M20A
Category
Airplane
Serial number
1568
Airframe hours
3,015.6
Engine
Lycoming IO-360-A1A, 200 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Registered owner
Jeffrey A. Evans
Airworthiness certificate
Standard, Normal
Last inspection
Annual · March 1, 2002 · 6.28 hours before
Departed
OUN · Norman, OK
Destination
EWK · Newton, KS
Airport
OUN · University Of Oklahoma Westhei, runway 3, 4,747 × 100 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
39
Injuries
Minor
Certificate
Private
Airplane ratings
Single-engine land
Medical
Class 3, Valid Medical--no waivers/lim.
Seat
Left
Flight hours
346 total

Weather

Conditions
Visual (VMC) · Day
Wind
60° at 13 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
41 °F, dew point 27 °F
Altimeter
30.17 inHg
Observed at
OUN

Docket · 4

The files NTSB released with the investigation on July 7, 2003, on NTSB’s docket system: statements, records, photos and specialists’ reports. 1.3 MB in all.

FAA reports on this event · 1

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

Other investigations on N8390E · 4

Matched to the same aircraft by N-number and date.