LAX07FA272

NTSB accident investigation · Grumman American AA-5 · Joshua Tree, CA · September 12, 2007

Accident · FatalField investigationFinal report
Date
September 11, 2007, 22:28 local (Sep 12, 2007, 05:28 UTC)
Place
Joshua Tree, CA
Injuries
1 fatal
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N119GGrumman American AA-5
Weather
Visual (VMC) · Night
Status
Completed · report December 28, 2008
Report
Approved by Office Director
Parties
Lycoming, Federal Aviation Administration
FAA report
20070911018869A
Case key
66668

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 failure to maintain terrain clearance during descent. Contributing to the accident were dark night conditions and mountainous 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.

In flight collision with terrain/waterDescent - normal
Light condition - dark nightFactor
Altimeter - not setPilot in command
Clearance - not maintainedPilot in commandCause
Terrain condition - mountainous/hillyFactor
Airport facilities,runway edge lights - inoperative

Analysis

The pilot had informed his girlfriend that on the accident flight he was going to stay out longer than normal for night currency. Following the VFR night cross-country flight, the pilot initiated a descent for his destination airport. While descending, the airplane, in a wings-level attitude, struck hilly terrain 57 feet below the top of a 2,973 foot ridgeline. The accident flight was between two airports, which was a frequent flight for the pilot. Extracted GPS data confirmed a normal descent profile to the pilot's home airport. Due to a local power outage, which also impacted the airport, the pilot was descending without the benefit of the ground illumination. The pilot also had not reset his altimeter to the destination airports current altimeter setting, which resulted in the altimeter indicating a higher than actual altitude.

Factual narrative

History of flight

On September 11, 2007, at 2228 Pacific daylight time, a Grumman AA-5, N119G, collided with elevated terrain near Joshua Tree, California. The pilot was operating the airplane under the provisions of 14 Code of Federal Regulations Part 91. The private pilot, the sole occupant was killed; the airplane sustained substantial damage. The cross-country personal flight departed Big Bear Airport (L35), Big Bear, California, at 2100, with a planned destination of Roy Williams Airport (L80), Joshua Tree. Visual meteorological conditions prevailed; no flight plan had been filed.

According to the pilot's girlfriend, the pilot made the flight from L35 to L80 on a regular basis, and it usually took about 30 minutes. She also stated that on this occasion the pilot indicated he would extend the flight in order to build his night currency.

A Garmin 296 handheld GPS receiver was recovered from the main wreckage and inspected by the National Transportation Safety Board investigator-in-charge (IIC). The GPS coordinates data for the accident flight was extracted. The data indicated that the airplane departed from L35 on a northerly heading. After flying approximately 10 miles, the airplane turned right on a southeast heading for an additional 50 miles. For the remaining 50 minutes of flight, the airplane circled L80, making multiple meandering passes over the city of Twentynine Palms in the region east of Copper Mountain. Shortly thereafter, at an altitude of 4,380 feet, and 12 miles east of L80, the airplane made a turn to the west and began a gradual descent heading towards the airport. The last recorded GPS position was at an altitude of 3,020 feet, 3.4 miles east of L80.

According to local law enforcement, on the night of the accident a power outage was reported between 2100 and 0300, affecting about 800 area residents. The Joshua Tree airport manager confirmed that the airport was without power during this time.

Personnel information

A review of Federal Aviation Administration (FAA) airman records revealed that the 72-year-old pilot held a private pilot certificate with ratings for airplane single-engine land.

The pilot held a third-class medical certificate issued on May 24, 2007. It had the limitations that the pilot must wear corrective lenses for distant vision and must possess glasses for near vision.

No personal flight records were located for the pilot. The IIC obtained the aeronautical experience listed in this report from a review of the FAA airmen medical records on file in the Airman and Medical Records Center located in Oklahoma City, Oklahoma. The pilot reported on his medical application that he had a total time of 1,000 hours.

Aircraft information

The airplane was a Grumman AA-5, serial number AA5-0324. A review of the airplane's logbooks revealed that the airplane had a total airframe time of 3,913.2 hours at the last annual inspection dated July 12, 2007. The tachometer read 3,913.2 at the last inspection. The tachometer read 3,919.5 at the accident scene.

The engine was a Lycoming O-320-E2G, serial number L-22493-27A. No engine logbooks were recovered for the accident airplane.

Meteorological information

The closest weather reporting station was in Twentynine Palms EAF Airport (NXP), 9 miles north of the accident site. An aviation routine weather report (METAR) was issued at 2255, and reported an altimeter setting of 29.99 inHg (inches of Mercury). A METAR for L35 that was issued at 2110 reported the altimeter setting of 31.31 inHg.

The Safety Board investigator at the accident location observed the airplane altimeter setting as 30.10 inHg.

Airport information

The Airport/Facility Directory, Southwest U. S., indicated that Roy Williams Airport (L80) runway 24 was 2,493 feet long and 50 feet wide. The runway surface was asphalt. The runway edge lights were a non-standard low density lighting system.

Wreckage and impact information

Investigators examined the wreckage at the accident scene. The first identified point of contact (FIPC) was a ground scar. The debris path was along a magnetic heading of 240 degrees.

The wreckage was located on a 45-degree, southeast facing, lose shale-covered slope, 3.4 miles east of L80; The top of the ridgeline was measured at 2,973 feet. The fuselage, wings, and empennage were intact, and came to rest on a heading of approximately 240 degrees. The engine and propeller had separated from the fuselage and came to rest 10 feet upslope from the main wreckage.

The left fuel tank had breached along the entire leading edge and contained no fuel. The right fuel tank was intact, and recovery personnel removed five gallons of aviation grade fuel.

Medical and pathological information

The San Bernardino County Coroner completed an autopsy on September 14, 2007. The FAA Civil Aerospace Medical Institute (CAMI), Oklahoma City, performed toxicological testing of specimens of the pilot.

The report contained the following positive findings for tested drugs: 2 (mg/dL,mg/hg) N-Propanol detected in blood; 3 (mg/dL,mg/hg) N-Propanol detected in Urine.

The report contained the following positive findings for volatiles: 84 (mg/dL,mg/hg) Ethanol detected in blood; 42 (mg/dL,mg/hg) Ethanol detected in Urine; and 15 (mg/dL,mg/hg) Ethanol detected in blood. The report from the San Bernardino County Coroner indicated that the ethanol found in this case may potentially be from post-mortem ethanol formation and not from the ingestion of ethanol.

Tests and research

Investigators examined the wreckage at Aircraft Recovery Service, Littlerock, California, on September 17, 2007.

The airframe and engine were examined with no mechanical anomalies identified.

Additional information

According to the Aeronautical Information Manual (AIM), 7-2-3, the following is reported under the heading of "Altimeter Errors:"

b. Once in flight, it is very important to obtain frequently current altimeter settings en route. If you do not reset your altimeter when flying from an area of high pressure into an area of low pressure, your aircraft will be closer to the surface than your altimeter indicates. An inch error in the altimeter setting equals 1,000 feet of altitude. To quote an old saying: "GOING FROM A HIGH TO A LOW, LOOK OUT BELOW."

Aircraft

Registration
N119G
Reported as
Grumman American AA-5
Category
Airplane
Serial number
AA5-0324
Airframe hours
3,919.5
Engine
Lycoming O-320-E2G, 160 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Airworthiness certificate
Standard, Normal; Standard, Utility
Last inspection
Annual · July 12, 2007 · 6 hours before
Departed
L35 · Big Bear City, CA
Destination
L80 · Joshua Tree, CA
Airport
L80 · Roy Williams Airport

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
72
Injuries
Fatal
Certificate
Private
Airplane ratings
Single-engine land
Medical
Class 3, With waivers/limitations
Last flight review
April 6, 2005
Seat
Left
Toxicology
Performed
Flight hours
1,000 total

Weather

Conditions
Visual (VMC) · Night
Wind
250° at 3 knots
Visibility
7 statute miles
Lowest ceiling
None
Temperature
86 °F, dew point 25 °F
Altimeter
29.98 inHg
Observed at
NXP, 10 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.