Grumman American Avn. CORP. AA-5 accident near Fredericksburg, Texas, June 14, 2015
On June 14, 2015 at about 4:27 pm local time, a 1974 Grumman American Avn. CORP. AA-5, registered N6552L, was substantially damaged in an accident during initial climb near Fredericksburg, Texas (Gillespie County Airport). It was a personal flight under general aviation rules (Part 91). 1 person was killed and 1 person was seriously injured. The weather was visual conditions (good weather).
The NTSB's probable cause their words, unchanged
The pilot's failure to maintain adequate airspeed following a partial loss of engine power during initial climb, which resulted in the airplane exceeding its critical angle of attack and experiencing an aerodynamic stall. Also causal was the mechanic's inadequate inspection of the airplane fuel system, which resulted in the partial loss of engine power due to fuel contamination.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- June 14, 2015 · about 4:27 pm local time
- Place
- Fredericksburg, Texas · Gillespie County Airport · map
- Type
- Accident
- Injuries
- 1 person was killed and 1 person was seriously injured.
- Weather
- visual conditions (good weather)
- Aircraft
- Grumman American Avn. CORP. AA-5, built 1974 · all AA-5s on the register
- Registration
- N6552L · no longer on the register · serial AA5-0652
- Damage
- Substantial damage
- Flight
- Personal flight · general aviation rules (Part 91)
The NTSB's narrative final · quoted from the NTSB record
The private pilot reported that his passenger, an aviation mechanic, had completed an annual inspection of the airplane immediately before the flight. The pilot did not identify any anomalies with the airplane during his preflight inspection following the annual inspection nor did he observe any fuel contamination in the samples that he collected from the airplane's four fuel drains. Additionally, he reported that the engine operated normally during a before-takeoff runup. Although the pilot did not recall all portions of the flight, he remembered that the engine lost power shortly after takeoff and had a brief memory of the airplane pointing nose-down toward the ground. The pilot did not recall any corrective actions that he made following the loss of engine power. The pilot reported that, while he was being treated at the hospital, he had apparently told his wife that the engine had lost power shortly after takeoff and that he had lowered the nose to regain airspeed. An onsite examination established that the airplane impacted the ground in a nose-low attitude, and the lack of an appreciable debris path was consistent with an aerodynamic stall. It is likely that the pilot did not maintain adequate airspeed following the loss of engine power, which resulted in the airplane exceeding its critical angle of attack and experiencing an aerodynamic stall at a low altitude. Postaccident examination revealed water and particulate contamination within the fuel distribution system, which likely resulted in a partial loss of engine power during initial climb. Based on the amount of fuel contamination observed after the accident, the mechanic did not adequately inspect the entire fuel system during the annual inspection that he completed immediately before the flight. According to the airplane's maintenance manual, during an annual inspection, the auxiliary electric fuel pump should be disassembled and its filter inspected/cleaned, the fuel tanks and sumps inspected, and the engine carburetor bowl drained. Had the mechanic examined the auxiliary electric fuel pump, he would have noted the extensive water and particulate contamination. The maintenance logbooks did not contain an entry for the annual inspection or any work associated with the inspection.
The complete narrative as the NTSB published it. The NTSB's docket holds the report as a PDF and any photographs, statements and other documents from the investigation.
The factual record from the NTSB's investigation tables, in plain English
What happened, in order
- Aircraft maintenance event during prior to flight
- Fuel contamination during initial climb defining event
- Loss of control in flight during initial climb
- Aerodynamic stall/spin during initial climb
- Collision with terrain or object (not controlled flight into terrain) during uncontrolled descent
The NTSB's findings
- cause Personnel issues › Task performance › Use of equip/info › Aircraft control › Pilot
- cause Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Airspeed › Not attained/maintained
- cause Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Angle of attack › Not attained/maintained
- cause Personnel issues › Task performance › Inspection › Scheduled/routine inspection › Maintenance personnel
- cause Aircraft › Aircraft systems › Fuel system › Fuel distribution › Inadequate inspection
- cause Aircraft › Fluids/misc hardware › Fluids › Fuel › Fluid condition
Pilot
- Certificate: private
- Ratings: single-engine land
- Flight time: 214.1 hours in all; 34.5 in this make and model; 0 in the last 90 days; 0 in the last 30 days
- Last flight review: June 13, 2014
- Medical certificate: Class 3 (with waivers/limitations)
- Seat: left
- Injury: serious injuries
The aircraft
- Airframe total time: 7,032.6 hours
- Last inspection: annual inspection, June 14, 2015; 0 hours since
- Maximum gross weight: 2,200 lb
- Seats: 4
- Landing gear: fixed
- Engine: Lycoming O-320-E2G (piston); 7,033 hours total
The flight
- Departed from: T82 Fredericksburg TX at 4:27 pm
- Destination: T82 Fredericksburg TX
- Flight plan: none
- Runway 14, 5,001 ft by 75 ft
Weather at the time
- Light: daylight
- Wind: from 170° at 7 knots
- Visibility: 10 statute miles
- Sky: broken clouds at 2,100 ft
- Temperature: 79°F (26°C), dew point 70°F (21°C)
- Altimeter: 29.93 inHg
- Observation at 4:15 pm from T82, 1 miles away
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 1 | |||
| Passengers | 1 |
Documents from the investigation the NTSB's docket: the evidence folder behind the report
14 documents, released by the NTSB on May 9, 2017. View them here, or download them; the NTSB redacts some personal details before release, and this site shows the NTSB's own titles rather than its file names.
| # | Document | What it is | |
|---|---|---|---|
| 1 | Memorandum of Conversation (Charles E. Reed) | PDF, 2 pages | View Download |
| 2 | Pilot/operator Aircraft Accident Report, NTSB Form 6120.1 | PDF, 9 pages | View Download |
| 3 | Pilot Logbook (Excerpts) | PDF, 19 pages | View Download |
| 4 | FAA Pilot Registry (Charles E. Reed) | PDF, 1 page | View Download |
| 5 | FAA Aircraft Registry (N6552L) | PDF, 1 page | View Download |
| 6 | Airframe Logbook (Excerpts) | PDF, 3 pages | View Download |
| 7 | Engine Logbook (Excerpts) | PDF, 4 pages | View Download |
| 8 | Grumman AA5 Maintenance Manual - Fuel System (Excerpts) | PDF, 10 pages | View Download |
| 9 | Grumman AA5 Maintenance Manual - Inspection Guidelines (Excerpts) | PDF, 21 pages | View Download |
| 10 | Grumman AA5 Owner's Manual (Excerpts) | PDF, 8 pages | View Download |
| 11 | Weather Reports | PDF, 1 page | View Download |
| 12 | Release of Aircraft Wreckage, NTSB Form 6120.15 | PDF, 1 page | View Download |
| 13 | Statement of Party Representatives to NTSB Investigation | PDF, 1 page | View Download |
| 14 | Photos | PDF, 10 pages | View Download |
The same docket at the NTSB · documents without a copy here are fetched from the NTSB when you open them.
Everything on this page comes from the NTSB's public records. The narrative, probable cause and findings are the NTSB's own words; the coded tables behind the report are written out in plain English, with pilots' ages, home towns and medical details left out. The documents and photographs are the NTSB's docket, shown as the NTSB released them. This site's own text never names anyone involved. A preliminary report can change; the final report usually follows one to two years later, and the page is refreshed when it does.
