N6908M
Registered owner: GRANT AVIATION INC, AK (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| GRANT AVIATION INC (ENHA) | Certificate holder | — | Matched by certificate designator |
| GRANT AVIATION INC (ENHA) | Operator | on 2022-07-27 | Operator named in NTSB report |
Accident & incident history
Operated by GRANT AVIATION INC (per NTSB report)
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
3 reports on file, 1995-12-01 – 2022-07-27.
Part: CONTROL CABLE — BROKEN (RUDDER) · airframe 40,885 hrs · 40,885 cycles
PILOT REPORTED LOSS OF LEFT RUDDER PEDAL CONTROL. MAINTENANCE INSPECTED AND FOUND BROKEN RUDDER CABLE.
Part: RUDDER BAR — CRACKED (COCKPIT)
THE RUDDER BAR ASSY WAS FOUND TO BE CRACKED ON THE WELD WHERE THE VERTICAL TUBE THAT ATTACHES TO THE LT RUDDER PEDAL MEETS THE HORIZONTAL TUBE.
Part: MOTOR — MALFUNCTION (FLAP ACTUATOR)
WHEN THE PILOT SELECTS FLAPS DOWN FROM 20 DEGREES TO 30 DEGREES ABOVE 90 KNOTS I.A.S., THE FLAP CIRCUIT BREAKER WOULD OPEN. AT AIRSPEEDS BELOW 90 KNOTS WHEN FLAPS WERE AGAIN SELECTED DOWN FROM 20 DEGREES - 30 DEGREES, THE FLAPS WOULD FUNCTION NORMALLY. NO VISUAL DEFECTS WERE FOUND IN THE CIRCUIT WIRING OR COMPONENTS. THE FLAP ACTUATOR MOTOR WAS REPLACED WITH A NEW UNIT AND AIRCRAFT WAS TEST FLOWN SATISFACTORILY.