N19DA
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| dale A Rinehart | Operator | on 1984-08-17 | Operator named in NTSB report |
Accident & incident history
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.
2 reports on file, 2002-02-14 – 2002-06-14.
Part: CIRCUIT BREAKER — TRIPPED (MAIN BUS)
WHILE IN FLIGHT, POWER WAS LOST TO RT SIDE OF INSTUMENT PANEL. PILOT TRIED TO EXTEND LANDING GEAR. GEAR DID NOT EXTEND. EMERGENCY WAS DECLARED AND PILOT RETURNED TO ALTITUDE AND MANUALLY EXTENDED LANDING GEAR. PILOT COMUNICATED WITH ANOTHER PILOT WHO TOLD HIM TO CHECK HIS MAIN BUS CIRCUIT BREAKERS. PILOT FOUND C/B POPPED AND RESENT THEM. POWER RETURNED TO INSTRUMENT PANEL. AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT WAS JACKED. OP CHECK OF GEAR AND ELECTRICALY SYSTEM WAS SATISFACTORY.
Part: TORQUE LINK — BROKEN (MLG)
RT MLG TORQUE KNEE FAILED AT UPPER PIVOT PIN. TORQUE KNEE WAS FOUND WITH SECTION MISSING ON INBOARD HALF AND BROKEN ON OUTBOARD SIDE. CRACKS WENT THROUGH GREASE FITTING HOLES IN BOTH CASES. GREASE FITTINGS WERE BOTH LOST. POSSIBLY CAUSED BY EXCESSIVE SIDE LOAD. TORQUE KNEE WOULD BE STRONGER IF THERE WERE NO GREASE FITTINGS IN IT. PUT GREASE FITTINGS IN PIVOT PIN ENDS.