ATL03LA054

NTSB accident investigation · Piper PA-28R · Enterprise, AL · March 16, 2003

Accident · No injuriesLimited investigationFinal report
Date
March 16, 2003, 17:15 local (23:15 UTC)
Place
Enterprise, AL
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Maneuvering
Aircraft
N7635JPiper PA-28R
Weather
Visual (VMC) · Day
Status
Completed · report June 28, 2006
Report
Approved by Office Director
Parties
FSDO 09 Birmingham Alabama
FAA report
20030316003639A
Case key
56669

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 loss of engine power due to oil starvation resulting from a crack in the propeller governor external oil line. A factor was the soft terrain.

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 power(total) - mech failure/malfManeuvering
Fluid,oil - exhaustionCause
Propeller system/accessories,governorCause
Lubricating system,oil line - crackedCause
Forced landingDescent - emergency
In flight collision with terrain/waterEmergency landing
Terrain condition - softFactor

Analysis

According to the student pilot, while simulating an emergency descent, there was a surge in engine rpm and a significant drop in engine oil pressure. The CFI checked the engine oil pressure and within seconds the engine seized, and by this time the windshield was covered with oil. The certified flight instructor (CFI) diverted to an open wheat field three miles southwest of Enterprise Municipal Airport. During the emergency landing, the airplane touched down but became difficult to control after rollout and the airplane spun 120 degrees to the right, colliding with the terrain. Examination of the aircraft found that the propeller assembly was bent, all three landing gear had collapsed and both wings were damaged in the vicinity of the collapsed landing gear. There was also damage to the fuselage just aft of the baggage compartment. Examination of the engine revealed that there was a crack in the propeller governor external oil line located at the first 90-degree bend radius aft the forward B-nut. A review of the aircraft maintenance log disclosed that the oil line was installed about 30 hours before the accident.

Factual narrative

On March 16, 2003, at 1715 central standard time, a Piper PA-28R, N7635J, registered to and operated by Double Bridges Aviation LLC, collided with the ground during an emergency landing three miles southwest of Enterprise Municipal Airport, Enterprise Alabama. The instructional flight was operated under the provision of Title 14 Part 91. Visual weather conditions prevailed at the time of the accident. No flight plan was filed. The airplane sustained substantial damage. The certified flight instructor and student pilot were not injured. The flight departed Enterprise Municipal Airport, Enterprise Alabama on March 16, 2003, at 1545.

According to the student pilot, while simulating an emergency descent, there was a surge in engine rpm and a significant drop in engine oil pressure. The CFI checked the engine oil pressure and within seconds the engine seized, and by this time the windshield was covered with oil. The CFI diverted to an open wheat field three miles southwest of Enterprise Municipal Airport. During the emergency landing, the airplane touched down but became difficult to control after rollout and the airplane spun 120 degress to the right, colliding with the terrain.

Examination of aircraft found that the propeller assembly was bent, all three landing gear had collapsed and both wings were damaged in the vicinity of the collapsed landing gear. There was also damage to the fuselage just aft of the baggage compartment. Examination of the engine revealed that there was a crack in the propeller governor external oil line located at the first 90-degree bend radius aft the forward B-nut. A review of the aircraft maintenance log disclosed that the oil line was installed about 30 hours before the accident.

Aircraft

Registration
N7635J
Reported as
Piper PA-28R
Category
Airplane
Serial number
28R-31032
Airframe hours
8,000
Engine
Lycoming IO-360-BIE, 180 horsepower, reciprocating
Damage
Substantial damage
Flight
Instructional · Part 91
Registered owner
Double Bridges Aviation, LLC.
Airworthiness certificate
Standard, Normal
Last inspection
Annual · January 30, 2003 · 22 hours before
Departed
KEDM · Enterprise, AL

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 · 2

As NTSB recorded them. NTSB leaves out names.

Role
Flight instructor
Age
61
Injuries
None
Certificates
Commercial, Flight instructor
Airplane ratings
Single-engine sea, Single-engine land, Multi-engine land
Instrument ratings
Helicopter, Airplane
Medical
Class 2, With waivers/limitations
Last flight review
July 1, 2002
Seat
Right
Flight hours
4,270 total · 120 in this make and model · 3,994 as pilot in command · 30 in the last 90 days · 17 in the last 30 days
Role
Student pilot
Age
31
Injuries
None
Certificates
Military, Commercial, Private
Airplane ratings
Single-engine land
Instrument ratings
Helicopter, Airplane
Medical
Class 2, Without waivers/limitations
Last flight review
December 6, 2002
Seat
Left
Flight hours
450 total · 7 in this make and model · 250 as pilot in command · 10 in the last 90 days · 7 in the last 30 days

Weather

Conditions
Visual (VMC) · Day
Wind
120° at 6 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
66 °F, dew point 59 °F
Altimeter
29.78 inHg
Observed at
DHN

FAA reports on this event · 1

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