OpenAirDocs.org

19750731023039A

Accident · Substantial damage
Open the Markdown

FAA accident report · Ayres S-2R · Augusta, AR · July 31, 1975

FAA Aviation Safety Information Portal

© OpenStreetMap
Date
July 31, 1975
Place
Augusta, AR
Airport
Private
Phase of flight
Forced/Precautionary Landing
Damage
Substantial damage
Aircraft
N4913X
NTSB investigation
NTSBFTW76DPG12
Reported as
Ayres S2R
Fatal injuries
0
Pilot’s flight hours
6,000 total530 in this make and model480 in the last 90 days
N4913XRegistration cancelled Aug 30, 2017 · Rockwell International S-2RS/N 2104R · Built 1974Airframe modelRockwell International S-2REngine modelPratt & Whitney R1340 seriesReciprocating

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

Bolt came loose at carb. Eng went to idle.

As the FAA filed it

BOLT CAME LOOSE AT CARB. ENG WENT TO IDLE.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.

NTSB FTW76DPG12Accident · No injuriesClosedAugusta, ARJul 31, 1975 · Substantial damage

Other reports on N4913X · 2

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

Accident 20170801010239AManeuver · Brawley, CAPilot reported while flying on the north side of the field he noticed a loss of power. He leveled the wings flying north west some power was received then another power loss which forced him to land in nutmeg 4 field with substantial damgage to the aircraft.Aug 1, 2017 · Substantial damageAccident 19840616027299ALow Level Operations · Pocahontas, ARPropeller blade separated in flight caused by fatigue crack. High stress area at crack during STC certification.Jun 16, 1984 · Substantial damage