N9820F
Registered owner: AVION CAPITAL CORP, 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 |
| Peninsula Airways Inc. | Operator | on 2004-05-16 | Operator named in NTSB report |
Accident & incident history
Operated by Peninsula Airways, 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.
13 reports on file, 2000-02-24 – 2019-04-23.
Part: FLAP TRACK — WORN (RT WING) · airframe 19,889 hrs · 40,251 cycles
FLAP TRACKS WORN
Part: FLAP TRACK — WORN (LT WING) · airframe 19,889 hrs · 40,251 cycles
FLAP TRACKS WORN
Part: STRUCTURE — DENTED (ELEVATOR) · airframe 19,889 hrs · 40,251 cycles
DENTED ELEVATOR
Part: TORQUE TUBE — CORRODED (RUDDER) · airframe 19,889 hrs · 40,251 cycles
RUDDER TORQUE TUBE REQUIRES REPLACEMENT
Part: SKIN — CHAFED (COWL) · airframe 19,889 hrs · 40,251 cycles
CHAFE DAMAGE ON LOWER COWLING
Part: DOOR FRAME — CORRODED (CARGO DOORWAY) · airframe 19,889 hrs · 40,251 cycles
LOWER CARGO DOOR THRESHOLD AIRFRAME SKIN CORRODED
Part: SUPPORT BRACKET — CHAFED (LT WING TE FLAP) · airframe 19,889 hrs · 40,251 cycles
FLAP LEADING EDGE CHAFING AND SUPPORT BRACKET WEAR
Earlier reports · 2000–2017 · 6 reports
2017
Part: BOLT — SHEARED · airframe 18,443 hrs · 37,864 cycles
TWO AN5-40A BOLTS SHEARED UPON LANDING. TORQUES WASH VERIFIED TO BE CORRECT AND WHEN WHEEL WAS BUILT UP TORQUE SEAL WAS USED. THREADED PORTION OF THE BOLT SHEARED CLEAN THIS IS THE SECOND AIRCRAFT IN THE FLEET TO HAVE THIS ISSUE. WHEEL WAS REMOVED AND A NEW WHEEL INSTALLED. WE LOCATED THE BAG FROM WHICH THE BOLTS APPEARED TO COME FROM IN THE PARTS ROOM AND REMOVED ALL BOLTS WITHIN THIS LOT NUMBER. ALL MECHANICS AND PILOTS ARE INSPECTING THE WHEEL BOLTS UPON EACH LANDING. LOT NUMBER 84295/3214
2011
Part: ANNUNCIATOR — SMOKE (COCKPIT) · airframe 12,022 hrs · 24,844 cycles
SMOKE COMING FROM TOP OF PANEL IMMEDIATELY BELOW GLARE SHIELD.
2006
Part: ALTERNATOR — FAILED (ENGINE) · airframe 8,116 hrs · 14,917 cycles
DURING CRUISE FROM DLG TO TOG, STANDBY ALTERNATOR WARNING LIGHT ILLUMINATED. PILOT RETURNED TO DLG WHERE MAINTENANCE REPLACED STANDBY ALTERNATOR AND RETURNED AIRCRAFT TO SERVICE.
2005
Part: CALIPER — SHEARED (RT BRAKE) · airframe 7,258 hrs · 13,083 cycles
ON LANDING AT KCQ RIGHT BRAKE FAILED. MX FOUND TOP ANCHOR PIN OF RT BRAKE CALIBER SHEARED. BRAKE CAUSED DAMAGE TO WHEEL ASSY AND BRAKE TORQUE PLATE. REPLACED BRAKE TORQUE PLATE, ANCHOR PINS, WHEEL ASSY AND BRAKE PADS. AIRCRAFT RETURNED TO SERVICE.
2004
Part: HUB — DAMAGED (PROPELLER) · airframe 6,296 hrs
SLUGGISH RESPONSE TO TAKEOFF POWER AND RPM/TORQUE DROPPED OFF AT FLIGHT IDLE POWER SETTINGS. AIRCRAFT MADE NORMAL LANDING WITH POWER LEVER FURTHER FORWARD THAN NORMAL. MAINTENANCE FOUND PROPELLER BLADE ANGLE IN HUB 2 DEGREES OFF AND BETA RING BENT. AT TEARDOWN BLADE HUB BOLTS WERE FOUND TO BE TIGHT AND BETA RING WAS REPLACED.
2000
Part: INVERTER — FAILED (ELECTRICAL)
WHILE ON A DATA GATHERING NIGHT FLIGHT. THE EQUIPMENT POWERED BY THE INVERTER LOST POWER. WHILE REACHING FOR THE POWER DISCONNECT SWITCH, A FLASH WAS NOTICED IN THE AREA IN WHICH THE INVERTER WAS INSTALLED. POWER TO THE INVERTER WAS CUT OFF AND THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. (X)