- Registered owner
- Everts Air Fuel
- Location
- Fairbanks, AK
- Owner type
- Corporation
- Serial number
- 44612
- Year built
- 1953
- Type
- Fixed wing multi engine
- Engine
- Reciprocating
- Airworthiness
- Standard, transport
- Airworthiness date
- June 23, 1989
- Certificate issued
- April 26, 2012
- Expires
- April 30, 2028
- Mode S code
- A25B6C
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Pratt & Whitney R-2800 model are included below.
On this page
Airworthiness directives that may apply · 0
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
No ADs matched this aircraft’s modelsADs on appliances, propellers and installed equipment aren’t matched by model; check those separately.
Information bulletins that may apply
Advisory, not mandatory.
No bulletins matched this aircraft’s models
NTSB investigations
No NTSB investigations matched to N251CEMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Douglas C-118A aircraft
FAA incident reports
No FAA accident or incident reports matched to N251CEMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Douglas C-118A aircraft
Service difficulty reports · 7
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR FXGA201606231615Skin · wornLOOSE 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 LSDR FXGA201606231607Stringer · crackedCRACKED 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 SSDR FXGA201606160001Stringer · crackedCRACKED 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 9115SDR FXGA201507141528Web · crackedTO REPAIR CRACKED WEB AT FS 600 BULKHEAD. PERFORM REPAIR IAW A & B OVERHAUL MANUAL FIGURE 12-6.SDR FXGA201501261503Skin · crackedTHE 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.SDR FXGAN251CE1145Skin · corrodedFOUND CORROSION ON LT LEADING EDGE AT WING STATION 176.5 TO 184.0 WHICH REQUIRED A MAJOR REPAIR.SDR FXGA20110323001Line · crackedHYD 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.
STCs that may be installed
No STCs matched this aircraft’s modelsSTCs are matched through the model’s type certificate data sheet, and this registry model isn’t matched to one.