N251CE
Registered owner: EVERTS AIR FUEL, AK (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
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.
7 reports on file, 2011-03-23 – 2016-06-23.
Part: STRINGER — CRACKED (RT WING)
CRACKED WING STR 21R AT WING STA 203R, TO REPAIR WING STRINGER 21R CRACKED AT WING STA 203R. REMOVE EXISTING SKIN DOUBLER INSTALLED IAW T/O 1C-118A-3-1, FIGURE 2-61, REPAIR CRACKED STR IAW EAC EO 9915 AND EXTENDED EXTERNAL REPAIR DOUBLER TO INCLUDE EXISTING SKIN DOUBLER. MFG EXTERNAL REPAIR DOUBLER FROM 2024-T3, 0.080".
Part: SKIN — WORN (RT WING)
LOOSE RIVETS AT FORWARD SPAR UPPER CAP BETWEEN ENGINE NR 3 AND NR 4. REPAIR OF WORN WING SKIN COUNTERSINKS CAUSED BY LOOSE RIVETS BETWEEN WING STA 201 AND 280. PERFORM SKIN CUTOUT AT FRONT SPAR AFT TANG BETWEEN WING STA 201R AND 280R. PERFORM NEW FASTENER LAY-OUT AND MFG DOUBLER FROM 2024-T3 0.071" IAW DWG 1615-01.
Part: STRINGER — CRACKED (RT WING) · airframe 46,770 hrs
CRACKED WING STR 18R AT WING STA 242R. TO REPAIR WING STR 18R CRACKED AT WING STA 242R, CUT CRACKED STR CAP AT WING STA 223.5 AND 255.25. STOP DRILL CRACKS IN STR 18L BETWEEN WING STA 239 AND STA 244. MANUFACTURE AND INSTALL STR REPAIR PARTS IAW EAC EO 9115. MANUFACTURE AND INSTALL CAP REPAIR PARTS IAW EAC EO 9915.
Part: WEB — CRACKED (FUSELAGE)
TO REPAIR CRACKED WEB AT FS 600 BULKHEAD. PERFORM REPAIR IAW A & B OVERHAUL MANUAL FIGURE 12-6.
Part: SKIN — CRACKED (WING)
THE SKIN IS CRACKED AT THE END OF AN EXISTING STRINGER REPAIR DOUBLER, SEE DWG 1503-01. REMOVE EXISTING REPAIR DOUBLER & STRAPS. CUT OUT SKIN IAW DWG 1503-02. MANUFACTURE NEW REPAIR PARTS IAW DWG 1503-03 & EO 9915.
Part: SKIN — CORRODED (LT WING) · airframe 45,365 hrs
FOUND CORROSION ON LT LEADING EDGE AT WING STATION 176.5 TO 184.0 WHICH REQUIRED A MAJOR REPAIR.
Part: LINE — CRACKED (HYD SYSTEM) · airframe 45,062 hrs
HYD FAILURE, ZERO PRESSURE, ZERO QUANTITY. UPON LANDING, CREW REPORTED HAVING USE OF THE BRAKES USING THE AUXILLARY PUMP. FOUND FLAP VALVE BYPASS LINE CRACKED AT FLARE. REPAIRED IAW 01-40NLA-2, PAGE 3-15, PARA 3-30. LEAK AND OPS CHECK GOOD.