Premium research interface

The modern interface for aviation safety intelligence.

Search investigations, review source evidence, monitor watched reports, and trace long-term patterns from one calm, data-first workspace.

63k+
Reports indexed
1940-2026
Coverage
Recent
Last data refresh
Featured Report

Loading…

Loading featured report…

Loading…
Open Report

Safety trends by operating rule

Track fatal and non-fatal accident patterns across Part 91, Part 135, and Part 121 operations.

Loading trend charts…

Browse the aviation graph

Move quickly by aircraft, airport, operator, and time with indexes built for research, not wandering.

Last Data Update

By Decade

By Month

Aircraft Manufacturer

More manufacturers

Airports

More airports

Operators

More operators

About

Aviation safety reports, made easier to study

NTSB Reports is an independent research and search tool for public aviation accident and incident records. It brings NTSB aviation reports, structured fields, docket files, extracted figures, photos, videos, and update history into one searchable interface.

The goal is practical safety education: make it faster to find relevant investigations, compare similar events, review factual records, and understand the evidence behind probable-cause and preliminary reports.

The investigative work and source records belong to the National Transportation Safety Board and the published investigation record. This site is not affiliated with or endorsed by the NTSB.

FAQs

NTSB Report

October 26, 2012 · Grumman American Avn AA-5A · N26380

Fairhope, AL

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
October 26, 2012
Injury Outcomes
No injuries (3 uninjured)
Location
Fairhope, AL
Aircraft
Grumman American Avn AA-5A
Tail Number
N26380
Injuries
None
Aircraft Damage
Substantial
NTSB Number
ERA13LA041

Two airplanes, a Grumman and a Piper, were operating at a non-towered airport. The pilot of the Piper reported that he did not hear any airplane making position reports over the airport’s common traffic advisory frequency and subsequently taxied on a taxiway that was located about 1,000 feet beyond the approach end of the runway and taxied past the hold short line toward the runway. The pilot of the Piper stopped his airplane about 75 feet short of the runway (and beyond the hold short line) when he noticed a Grumman that was on final approach. After touching down, about 500 feet beyond the runway threshold, the Grumman rolled another 300 to 400 feet before it suddenly veered left, and departed the side of the runway. The Grumman struck a taxiway sign before impacting the Piper, resulting in substantial damage to both airplanes. Postaccident examination of the Grumman revealed no discrepancies with the braking system; however, the left main landing gear tire was flat, and its inner tube displayed a small gash. It could not be determined if the damage to the tube occurred before or as a result of side-loading placed on it during the collision.

NTSB Probable Cause

The Grumman pilot’s loss of directional control during landing for undetermined reasons because postaccident examination of the airplane did not reveal any anomalies that would have precluded normal operation. Contributing to the accident was the Piper pilot positioning his airplane beyond the runway hold short line.

Full Narrative

On October 26, 2012, about 1650 central daylight time, a Grumman American Aviation Corp. AA-5A, N26380, and a Piper PA-22, N2633A, were substantially during a ground collision at H. L. Sonny Callahan Airport (CQF), Fairhope, Alabama. The certificated commercial pilot of the Piper, and the certificated private pilot and the passenger aboard the Grumman were not injured. Visual meteorological conditions prevailed, and no flight plan was filed for either of the personal flights, which were both conducted under the provisions of Title 14 Code of Federal Regulations Part 91. According to the pilot of the Grumman, he arrived at the airport around 1500 to begin the preflight inspection of the airplane, which included a visual inspection of the tires. About 1620, the pilot and the passenger departed for a local flight, and at the conclusion of the flight, returned to CQF from the east. About 3 to 4 miles from the airport, the pilot advised via radio that he would cross overhead of the airport and enter on the left downwind leg of the traffic pattern for landing on runway 1. After entering the traffic pattern, the pilot observed the Piper on taxiway A2, and announced that he was turning onto the base, then final legs of the traffic pattern. The pilot of the Grumman stated that he did not hear transmissions from any other airplanes while in the traffic pattern, and noted that the Piper had remained stationary on the taxiway. The pilot of the Grumman stated that his airplane touched down about 500 feet down the runway, and rolled another 300 to 400 feet before it suddenly veered left. The pilot responded by applying the right toe brake, which momentarily corrected the airplane’s track, but the airplane continued off the left side of the runway toward the Piper. The Grumman subsequently departed the runway south of taxiway A2, continued to turn left, and its left wing contacted the propeller of the Piper. The Grumman then pivoted to the left, and the propeller of the Grumman contacted the wing of the Piper. Upon exiting the airplane, the pilot of the Grumman noted that his airplane’s left tire appeared to be “flat.” According to the pilot of the Piper, following an uneventful preflight inspection and run up of the engine, he approached the runway from taxiway A2. After hearing no other traffic on the airport common traffic advisory frequency, the pilot of the Piper turned his airplane to gain an unobstructed view of the final approach path, and observed the Grumman as it was on final approach to the runway. He then stopped his airplane about 75 feet short of the runway edge in order to wait for the Grumman to land. The pilot watched as the Grumman landed, veered off the left side of the runway, struck a taxiway marker, and impacted the Piper. A Federal Aviation Administration inspector examined both airplanes following the accident and determined that each of them sustained substantial damage during the collision. The inspector further examined the brake system of the Grumman, and found that they appeared to operate normally, with neither brake displaying evidence of binding, uneven wear, or scoring. The flat left tire was removed from the wheel, and a small 1/4-inch gash was noted on the tire tube. No visible marks, debris, or puncture was noted anywhere on the tire. The area of the tire that covered the gash in the tube did appear to display some wrinkling. It could not be determined whether this damage occurred prior to or during the ground collision. The single asphalt runway at CQF was 6,604 feet long by 100 feet wide and was configured in a 1/19 orientation. A parallel taxiway spanning the full length of the runway was present on the west side of the runway. Taxiway A1 was located at the southernmost end of the runway, at the runway 1 approach threshold. Taxiway A2 intersected the runway about 1,000 feet beyond the runway threshold. The airport was not served by a local air traffic control tower. The weather conditions reported at CQF, at 1655, included winds from 320 degrees magnetic at 5 knots, clear skies, 10 statute miles visibility, temperature 28 degrees Celsius (C), dewpoint 18 degrees C, and an altimeter setting of 29.89 inches of mercury.

Flight

Event TypeAccident
Event Time16:50 CDT
Nearest AirportH L Sonny Callahan Airport (0nm)
Runway01
Runway Length6604 ft
Runway Width100 ft
Flight Plan FiledNone
Flight Plan ActivatedNo
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftGrumman American Avn AA-5A
Tail NumberN26380
Aircraft CategoryAir
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · O-320 · Reciprocating · 160 | Lycoming · O-290-D2 · Reciprocating · 135
Seats4

People & Injuries

Injury SummaryNo injuries (3 uninjured)
Fatal0
Serious0
Minor0
Uninjured3
Total3
Crew 1Age 61 · Third Class · None
Crew 2Age 54 · Second Class · None

Conditions

ConditionsVMC
LightDaylight
Wind320° @ 5 kt
Visibility10 sm
CeilingNone
Temperature / Dew Point64 F
Altimeter29.88 inHg
Observation Time21:55
Weather SourceWFAC

Appendix: Source Data