FTW00LA205

NTSB accident investigation · Piper PA-23-160 · Rio Grande City, TX · July 12, 2000

Accident · No injuriesLimited investigationFinal report
Date
July 12, 2000, 13:30 local (18:30 UTC)
Place
Rio Grande City, TX
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Initial climb
Aircraft
N4322PPiper PA-23-160
Weather
Visual (VMC) · Day
Status
Completed · report July 10, 2001
Report
Approved by Office Director
FAA report
20000712010029A
Case key
49683

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 for undetermined reasons. Contributing factors were the pilot flying the airplane with known deficiencies, and the lack of suitable terrain for the forced landing.

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
2 engines
Reason for occurrence undeterminedCause
Operation with known deficiencies in equipment - performedPilot in commandFactor
Forced landingDescent - emergency
In flight collision with terrain/waterLanding - flare/touchdown
Terrain condition - none suitableFactor
Terrain condition - high vegetation

Analysis

During a cross-country flight, on the day prior to the accident, the airplane experienced a total electrical failure. The pilot made a precautionary landing at an airport, where he had the battery charged. However, the electrical problem was not repaired prior to departing on the day of the accident. After lift-off from the runway, the landing gear was retracted, and the pilot began a left turn. While in the turn, about 300-400 feet agl, the left engine lost power. Subsequently, the right engine lost power. The pilot executed a forced landing to a field with brush and mesquite trees. The airplane had been inspected 6 days before the accident by an FAA inspector, who issued an Aircraft Condition Notice for maintenance defects, which were considered to be an imminent hazard to safety. A special flight permit was required prior to operating the aircraft if corrective action had not been taken. An examination of the airplane revealed that the maintenance defects were not corrected, and a special flight permit had not been obtained. The reason for the loss of engine power could not be determined.

Factual narrative

On July 12, 2000, approximately 1330 central daylight time, a Piper PA-23-160 twin-engine airplane, N4322P, was substantially damaged during a forced landing following a loss of engine power during takeoff climb from the Starr County Airport near Rio Grande City, Texas. The airplane was owned and operated by a private individual. The commercial pilot and his pilot-rated passenger were not injured. Visual meteorological conditions prevailed, and a flight plan was not filed for the 14 Code of Federal Regulations Part 91 positioning flight. The flight was originating at the time of the accident and was destined for the David Wayne Hooks Airport, Spring, Texas.

The flight had departed Corpus Christi, Texas, on the day prior to the accident and was en route to McAllen, Texas, when the airplane experienced a total electrical failure. The pilot made a precautionary landing at the Starr County Airport, where he had the battery charged. However, the electrical problem was not repaired prior to departing on the day of the accident.

According to the pilot, prior to departure, he performed a "through preflight and run-up check." After lift-off from runway 15, the landing gear was retracted, and a left turn was initiated. While in the turn, about 300-400 feet agl, the left engine began "sputtering," and after a "few seconds" the engine lost power. The right engine then began to "sputter." Subsequently, the right engine lost power. The pilot executed a forced landing to a field with brush and mesquite trees. The airplane came to rest one mile north of the Starr County Airport.

An FAA inspector, who responded to the accident site, reported that the fuselage was "partially separated aft of the cabin." Additionally, both wings were structurally damaged. The reason for the loss of engine power could not be determined.

According to the FAA inspector, the airplane had been inspected on July 6, 2000, by another FAA inspector, who issued an Aircraft Condition Notice for maintenance defects, which were considered to be an imminent hazard to safety. A special flight permit was required prior to operating the aircraft if corrective action had not been taken. An examination of the airplane revealed that the maintenance defects were not corrected, and a special flight permit had not been obtained.

Neither the pilot nor the operator responded to requests to provide a completed Pilot/Operator Aircraft Accident Report (NTSB Form 6120.1/2).

Aircraft

Registration
N4322P
Reported as
Piper PA-23-160
Category
Airplane
Serial number
23-1823
Engine
Lycoming O-320-B3B, 160 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Registered owner
Kaur Rajeeep
Airworthiness certificate
Standard, Normal
Departed
67R
Destination
DWH · Spring, TX
Airport
67R · Starr County, runway 15, 3,202 × 50 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
21
Certificate
Commercial
Airplane ratings
Multi-engine land, Single-engine land
Instrument ratings
Airplane
Medical
Class 1, Expired
Seat
Left
Flight hours
286 total

Weather

Conditions
Visual (VMC) · Day
Wind
170° at 15 knots, gusting 19
Visibility
10 statute miles
Lowest ceiling
None
Temperature
99 °F, dew point 68 °F
Altimeter
29.00 inHg
Observed at
MFE, 36 nm away

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 N4322P · 1

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