# Accident 19990508019969A: Gulstm AA5B, Claremore, OK, May 8, 1999 - Type: FAA accident report (Accident/Incident Data System), as reported - Date: May 8, 1999 - Place: Claremore, OK - Airport: Claremore Municipal Airport - Damage: Substantial damage - Phase of flight: Fcd/Prec Ldg From Cruise - Operating rules: General operating rules (Part 91) - Location: 36.3094° N, 95.6097° W: From the FAA, an estimate near the named town, within about 3 miles - Nearby events: https://openairdocs.org/map.md?lat=36.3094&lon=-95.6097&mi=10 - Aircraft: N4546J, registered now (https://openairdocs.org/aircraft/N4546J) (OpenAirDocs) - Registry model: Grumman American Avn. AA-5B (registry code 3960105, https://openairdocs.org/model/grumman-american-avn-aa-5b) (OpenAirDocs) - Registry engine: Lycoming O&VO-360 series (registry code 41514, https://openairdocs.org/engine/lycoming-o-vo-360-series) (OpenAirDocs) - Reported make and model: GULSTM AA5B - People aboard: 1 - Fatal injuries: 0 - NTSB investigation: [NTSB FTW99FA132](https://openairdocs.org/ntsb/FTW99FA132) (OpenAirDocs) - FAA source: FAA Aviation Safety Information Portal (https://asip.faa.gov/) - Page: https://openairdocs.org/incident/19990508019969A ## Narrative As the FAA filed it, in capitals; the FAA replaces private details with ^PRIVACY DATA OMITTED^. ON MAY 8, 1999, AT 0830 CENTRAL DAYLIGHT TIME, A GRUMMAN AMERICAN AA-5B AIRPLANE, N4546J, WAS SUBSTANTIALLY DAMAGED DURING A FORCED LANDING FOLLOWING THE SEPARATION OF THE PROPELLER ASSEMBLY FROM THE ENGINE WHILE IN CRUISE FLIGHT NEAR CLAREMORE, OKLAHOMA. THE COMMERCIAL RATED PILOT, SOLE OCCUPANT AND OWNER/OPERATOR OF THE AIRPLANE, WAS NOT INJURED. VISUAL METEOROLOGICAL CONDITIONS PREVAILED, AND A FLIGHT PLAN WAS NOT FILED FOR THE 14 CODE OF FEDERAL REGULATIONS (CFR) PART 91 PERSONAL FLIGHT. THE FLIGHT ORIGINATED FROM THE PILOT'S PRIVATE GRASS STRIP NEAR KETCHUM, OKLAHOMA, AT 0615, AND WAS DESTINED FOR THE OKLHOMA CITY DOWNTOWN AIRPORT. DURING AN INTERVIEW CONDUCTED BY THE INVESTIGATOR-IN-CHARGE, THE PILOT STATED THAT HE WAS IN LEVEL CRUISE FLIGHT AT 2,500 FEET MSL, WHEN HE NOTICED A VIBRATION IN THE AIRCRAFT. ACCORDING TO THE PILOT, THE VIBRATION BECAME MORE VIOLENT AND SUBSEQUENTLY, THE PROPELLER DEPARTED THE AIRCRAFT'S ENGINE. THE PILOT INITIATED AN EMERGENCY LANDING TO A FIELD; HOWEVER, NOTICING THAT HIS GLIDE RATIO HAD IMPROVED WITHOUT THE PROPELLER, HE ELECTED TO LAND AT THE CLAREMORE MUNICIPAL AIRPORT. THE PILOT STATED THAT DURING THE APPROACH, THE AIRPLANE STARTED TO PORPOISE, SO HE ELECTED TO TOUCH DOWN IN THE GRASS SECTION BETWEEN RUNWAY 34 AND THE TAXIWAY TO ABSORB SOME OF THE LANDING ENERGY. DURING THE LANDING ROLL, THE NOSE LANDING GEAR COLLAPSED AND SEPARATED FROM THE AIRCRAFT. THE AIRPLANE SLID ACROSS THE RUNEAY AND CAME TO REST BETWEEN TWO RUNWAY LIGHTS. THE PROPELLER ASSEMBLY (PROPELLER WITH APPROXIMATELY 5 INCHES OF ONE BLADE TIP MISSING, SPACER, AND FORWARD BULKHEAD ASSEMBLY) WERE LOCATED THREE MILES WEST OF THE AIRPORT. THE BLADE TIP WAS FOUND IN THE ENGINE COWLING AND THE STARTER FLYWHEEL WAS LOCATED IN THE GRASS SECTION BETWEEN THE RUNWAY AND TAXIWAY. THE PROPELLER FLANGE WAS FOUND INTACT WITH THE ENGINE CRANKSHAFT. THE AIRPLANE'S FIREWALL WAS BUCKLED, THE LANDING GEAR-TO-FUSELAGE ATTACHMENT POINTS WERE STRUCTURALLY DAMAGED, AND THE WING ROOTS SHOWED EVIDENCE OF STRUCTURAL DAMAGE. (-23)THE FLIGHT ORIGINATED FROM THE PILOT'S PRIVATE GRASS STRIP NEAR KETCHUM, OKLAHOMA, AT 0815, AND WAS DESTINED FOR THE OKLAHOMA CITY DOWNTOWN AIRPARK. THE PILOT STATED THAT HE WAS IN LEVEL CRUISE FLIGHT WHEN HE NOTICED A VIBRATION IN THE AIRCRAFT. THE VIBRATION BECAME MORE VIOLENT AND THEN THE PROPELLER LEFT THE AIRCRAFT. THE PILOT GLIDED TO AN EMERGENCY LANDING AT THE CLAREMORE MUNICIPAL AIRPORT. ON LANDING ROLLOUT ON THE GRASS BESIDE THERUNWAY THE NOSE GEAR BUCKLED AND SEPARATED FROM THE AIRCRAFT. ## The NTSB's investigation of this event (1) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB FTW99FA132](https://openairdocs.org/ntsb/FTW99FA132), May 8, 1999: Grumman American AA-5B (N4546J), Claremore, OK, substantial damage. Probable cause: The fatigue fracture of the propeller bolts resulting from the improper installation of the propeller assembly. ## Other reports on N4546J (1) Matched to the same aircraft by N-number and date. - [Accident 19950806022319A](https://openairdocs.org/incident/19950806022319A), Aug 6, 1995: Gulstm AA5B (N4546J), Owasso, OK, Substantial damage. Aborted takeoff due poor performance. Overran runway. Struck fence. Short grass runway. Near gross. Hot day. From the FAA Accident/Incident Data System. Reports are matched to registry aircraft 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. For accidents, the NTSB's own investigation is the fuller record. --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.