N528AP
Registered owner: ARROW PLANE LC, UT (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| Keystone Aviation, LLC (B8MA) | Certificate holder | — | Matched by certificate designator |
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
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.
6 reports on file, 2009-11-04 – 2019-06-04.
Part: CONTROL UNIT — FAILED (WINDSHIELD HEAT) · airframe 5,760 hrs · 2,058 cycles
RIGHT WINDSHILED STOPPED HEATING AFTER 45 TO 60 MIN WITH NO CASS MESSAGE OF FAILURE
Part: SOCKET — BURNED (LIGHT) · airframe 4,351 hrs · 1,392 cycles
WHILE PERFORMING AN AIRCRAFT SERVICE CHECK, FOUND EXTERIOR LOGO LIGHTS INOPERATIVE. PERFORMED TROUBLESHOOTING AND FOUND THAT THE P3 AND J3 PLUG AND CONNECTOR HAD SHORTED AT PIN DD AND MELTED THE PIN AND FEMALE PIN RECEPTACLE. CONNECTOR AND PLUG ARE LOCATED IN LT ELECTRONIC EQUIPMENT RACK, LEER, REF DES 327VB49. P3 AND J3 CONNECTOR AND PLUG ASSY WERE R & R. OPS CHECK OF LOGO LIGHTS WERE SATISFACTORY.
Part: BRAKE ASSY — CRACKED (ZONE 700) · airframe 4,233 hrs · 1,341 cycles
WHILE PERFORMING THE NR 1 AND NR 2 WHEEL AND TIRE CHANGE. UPON REMOVING THE WHEEL ASSEMBLIES FROM THE ACFT FOUND NR 1 AND NR 2 BRAKE ASSEMBLY CARBON ROTOR ASSEMBLIES TO BE CRACKED AND BROKEN OFF FROM THE KEY WAY GUIDES IN SEVERAL PLACES. R & R NR 1 AND NR 2 BRAKE ASSEMBLIES.
Part: ELBOW — CRACKED (FUEL LINE) · airframe 3,597 hrs · 1,162 cycles
WHILE PERFORMING A SERVICE CHECK ON THE ACFT, NOTICED HYDRAULIC FLUID LEAKING FROM THE LT MLG WHEEL WELL. ON FURTHER INVESTIGATION, FOUND AUXILARY SYS SUCTION LINE LEAKING. REMOVED LINE ASSY AND FOUND 90 DEGREE ELBOW CRACKED. R & R SUCTION LINE AND 90 DEGREE FITTING WITH NEW PARTS. LEAK CHECKED SATISFACTORY.
Part: CABLE — DAMAGED (FUEL S/O VALVE)
(K5SR) WHILE PERFORMING A 500 HR/12 MONTH INSP ON THE LT ENGINE, DISCOVERED THE EMERGENCY FUEL SHUTOFF CABLE HAD UN-TWISTED AT THE CABLE END GOING FROM THE FUEL SHUTOFF VALVE. R & R WITH NEW CABLE ASSY. OPD CKD SATISFACTORY.
Part: CONNECTOR — UNSECURE (RUDDER SWICH)
WHILE PERFORMING CMP 27301 RUDDER SYS HARD-OVER PREVENTION SYS OPS TEST. FOUND THAT SYS FAILED CHECK. TROUBLESHOOTING THE SYS FOUND CONNECTOR PLUG NR 155A26P3 PIN NR 3 GOING TO RUDDER HARD OVER SWITCHES WAS NOT LOCKED INTO PLUG ASSY. RESECURED PIN NR 3 INTO CONNECTOR PLUG 155A26P3 AND PERFORMED RUDDER HARD-OVER PREVENTION CHECK. WITH SATISFACTORY RESULTS. (K)