19970722019489A

Accident · Substantial damage

FAA accident report · Amtr RAF2000GTXSE · Brandon, OR · July 22, 1997

Date
July 22, 1997 · 08:47 local
Place
Brandon, OR
Airport
Brandon State Airport
Phase of flight
To Init Climb(1st Pwr Reduct)
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N6281Y
NTSB investigation
NTSBSEA97LA176
Reported as
Amtr RAF2000GTXSE
Fatal injuries
0
Pilot’s flight hours
18,000 total50 in this make and model50 in the last 90 days

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.

Aircraft was on a local test flight and lost control after takeoff. (.4)the pilot reported that after takeoff the gyroplane pitched nose down and crashed onto the runway. He reported to the gyroplane kit manufacturer that the event occurred at an altitude of 25 to 30 feet, and that just before the occurrence he noted rotor RPM at 260 and airspeed at 40 knots. The aircraft flight manual gives normal operating range of rotor RPM as 275 to 310 RPM, and states that rotor RPM less than 270 must be avoided while flying. The pilot indicated on his accident report that no mechanical malfunction or failure was involved. The pilot held an airline transport pilot certificate with airplane single-engine land and airplane multi-engine land ratings; he did not hold a rotorcraft-gyroplane rating but did possess a gyroplane solo logbook endorsement dated about 6 months before the accident. The pilot reported his total flight time as 18,000 hours, with 50 hours of gyroplane flight time.

As the FAA filed it

AIRCRAFT WAS ON A LOCAL TEST FLIGHT AND LOST CONTROL AFTER TAKEOFF. (.4)THE PILOT REPORTED THAT AFTER TAKEOFF THE GYROPLANE PITCHED NOSE DOWN AND CRASHED ONTO THE RUNWAY. HE REPORTED TO THE GYROPLANE KIT MANUFACTURER THAT THE EVENT OCCURRED AT AN ALTITUDE OF 25 TO 30 FEET, AND THAT JUST BEFORE THE OCCURRENCE HE NOTED ROTOR RPM AT 260 AND AIRSPEED AT 40 KNOTS. THE AIRCRAFT FLIGHT MANUAL GIVES NORMAL OPERATING RANGE OF ROTOR RPM AS 275 TO 310 RPM, AND STATES THAT ROTOR RPM LESS THAN 270 MUST BE AVOIDED WHILE FLYING. THE PILOT INDICATED ON HIS ACCIDENT REPORT THAT NO MECHANICAL MALFUNCTION OR FAILURE WAS INVOLVED. THE PILOT HELD AN AIRLINE TRANSPORT PILOT CERTIFICATE WITH AIRPLANE SINGLE-ENGINE LAND AND AIRPLANE MULTI-ENGINE LAND RATINGS; HE DID NOT HOLD A ROTORCRAFT-GYROPLANE RATING BUT DID POSSESS A GYROPLANE SOLO LOGBOOK ENDORSEMENT DATED ABOUT 6 MONTHS BEFORE THE ACCIDENT. THE PILOT REPORTED HIS TOTAL FLIGHT TIME AS 18,000 HOURS, WITH 50 HOURS OF GYROPLANE FLIGHT TIME.

NTSB investigation

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