20000725008019A

Accident · No damage

FAA accident report · Hughes 269C · Sherman, TX · July 25, 2000

Date
July 25, 2000 · 11:00 local
Place
Sherman, TX
Airport
Sherman Municipal Airport
Operating rules
General operating rules (Part 91)
Damage
No damage
Aircraft
N298SH
NTSB investigation
NTSBFTW00LA216
Reported as
Hughes 269C
Fatal injuries
0

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.

(-23) On approach to landing at approx 20' AGL acft engine surged and yawed right. Pilot reduced throttle and collective and applied aft cyclic. Just prior to ground contact pilot applied collective for landing. Acft impacted ground approx 5' from edge of runway. With ground impact acft pitched level made contact with runway on right front skid. Pilot appeared to have aft cyclic still applied. Right front crossmember failed at engine cage cluster, acft impacted runway at that point, blade to runway contact occurred, blades flexed tailboom contact occurred with one blade severing tail rotor. Tailboom failure occurred near main attaching points. Acft came to rest on left side. No fire. Further investigation by NTSB has revealed possible material failure.

As the FAA filed it

(-23) ON APPROACH TO LANDING AT APPROX 20' AGL ACFT ENGINE SURGED AND YAWED RIGHT. PILOT REDUCED THROTTLE AND COLLECTIVE AND APPLIED AFT CYCLIC. JUST PRIOR TO GROUND CONTACT PILOT APPLIED COLLECTIVE FOR LANDING. ACFT IMPACTED GROUND APPROX 5' FROM EDGE OF RUNWAY. WITH GROUND IMPACT ACFT PITCHED LEVEL MADE CONTACT WITH RUNWAY ON RIGHT FRONT SKID. PILOT APPEARED TO HAVE AFT CYCLIC STILL APPLIED. RIGHT FRONT CROSSMEMBER FAILED AT ENGINE CAGE CLUSTER, ACFT IMPACTED RUNWAY AT THAT POINT, BLADE TO RUNWAY CONTACT OCCURRED, BLADES FLEXED TAILBOOM CONTACT OCCURRED WITH ONE BLADE SEVERING TAIL ROTOR. TAILBOOM FAILURE OCCURRED NEAR MAIN ATTACHING POINTS. ACFT CAME TO REST ON LEFT SIDE. NO FIRE. FURTHER INVESTIGATION BY NTSB HAS REVEALED POSSIBLE MATERIAL FAILURE.

NTSB investigation

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