- Registered owner
- Ryan Air Inc
- Location
- Anchorage, AK
- Owner type
- Corporation
- Serial number
- 265
- Year built
- 1982
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, transport
- Airworthiness date
- March 6, 2020
- Certificate issued
- December 16, 2020
- Expires
- December 31, 2027
- Mode S code
- A088D4
Construcciones Aeronauticas C-212-CCTCDS A43EUAirframe · Construcciones Aeronauticas C-212-CCTCDS E4WEEngine · Honeywell TPE331-10R
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 64
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1983 | 1 |
|---|---|
| 1984 | 3 |
| 1986 | 1 |
| 1987 | 7 |
| 1988 | 2 |
| 1989 | 7 |
| 1991 | 1 |
| 1992 | 1 |
| 1993 | 2 |
| 1995 | 2 |
| 1996 | 3 |
| 1997 | 3 |
| 1998 | 6 |
| 1999 | 2 |
| 2003 | 1 |
| 2004 | 2 |
| 2005 | 1 |
| 2006 | 4 |
| 2007 | 1 |
| 2008 | 1 |
| 2009 | 3 |
| 2011 | 1 |
| 2012 | 1 |
| 2014 | 1 |
| 2015 | 3 |
| 2016 | 2 |
| 2017 | 2 |
| 2018 | 5 |
| 2020 | 1 |
| 2021 | 1 |
| 2022 | 1 |
Airframe · Construcciones Aeronauticas C-212-CC
AD 2022-17-06FuselageAD 2020-03-18Flight ControlsAD 2018-19-02Flight controlsInformation bulletins that may apply · 2
Advisory, not mandatory.
Engine · Honeywell TPE331-10R
SAIB NE-16-19Turbine Engine Compressor Section Stator Nozzle DistressSAIB NE-16-18Power Lever Loss of Power ControlNTSB investigations
No NTSB investigations matched to N1331CMatched 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 Construcciones Aeronauticas C-212-CC aircraft
FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Service difficulty reports · 13
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR UATA2650916265301Skin · damagedFS 27 LOWER BEAM & LOWER SKINS DAMAGED. REMOVED F27 LOWER BEAM. PREVIOUSLY REPAIRED RT LOWER SKIN SECTION, LT & RT FS27 TO C CHANNEL BRACKETS/CVR BOX MOUNTING STRUCTURE. CUT MIDDLE/LH LOWER SKINS JUST AHEAD OF F28 FLANGE REMOVING FWD ~13" OF BOTH SKINS. FAB'D SDR UATA2650406267901Oil Cooler · failedLEFT ENGINE OIL TEMPERATURE INCREASED TO REDLINE, PERFORMED PRECAUTIONARY SHUTDOWN. REMOVED AND REPLACED #1 OIL COOLER REF CASA MM 79-20-00 LEAK CHECK GOOD.SDR UATA2650214255303Web · crushedRH SEAT RAIL LONGITUDINAL WEB CRUSHED AT F17. REPAIRED IAW C212 SRM B26. SEE 337 DATED 02/10/2025 FOR FURTHER DETAIL. REMOVED DAMAGED SECTION OF WEB ~4.5 X 9". FABRICATED REPLACEMENT WEB SECTION TO SAME DIMENSIONS AS REMOVED FROM 2024T3 0.025", AND SPLICE PLATSDR UATA2650214255302Web · crushedLH SEAT RAIL LONGITUDINAL WEB CRUSHED AT F17. REPAIRED IAW C212 SRM B26. SEE 337 DATED 02/10/2025 FOR FURTHER DETAIL. REMOVED DAMAGED SECTION OF WEB ~ 5.5" X 9.5". FABRICATED REPLACEMENT WEB SECTION TO SAME DIMENSIONS AS REMOVED FROM 2024T3 0.025", AND SPLICESDR UATA2650214255301Frame · puncturedFOUND A SMALL PUNCTURE IN THE AFT SIDE OF THE RH WEB OF FRAME 11, 2 INCHES ABOVE FLOOR LEVEL. REPAIRED PER CASA ENGINEERING DOC 252EA-00020 REV A. SEE 337 DATED 02/10/2025 FOR FURTHER DETAIL. REMOVED DAMAGED MATERIAL. DAMAGED AREA INSPECTED BY HFEC, NO INDICASDR UATA202402023312Skin · crackedWHILE INSPECTING THE AIRFRAME PER AD2022-17-06, AOT C212-53-0001 AND SB212-53-0055, A CRACK OF 0.070" WAS FOUND ON THE FUSELAGE SKIN IN THE AREA OUTLINED TO BE INSPECTED BY THE AOT. THE OEM HAS BEEN CONTACTED, HE SITUATION REPORTED, AND A REPAIR SCHEME REQUESTSDR UATA202203243311Skin · gougedA FORKLIFT LOADING THE AIRCRAFT SLIPPED ON ICE, AND HIT THE AFT UPPER CARGO DOOR AS WELL AS THE AIRCRAFT STRUCTURE DIRECTLY AFT OF THE DOOR, CAUSING GOUGING, AS WELL AS BUCKLING OF THE ASSOCIATED FRAMES. DAMAGE WAS REPAIRED IAW THE SRM, AND A FAA FORM 337 WAS SDR UATA202104133317Governor · inoperativeON T/O ROLL OUT OF OOK AT V1 SPEED, #1 ENGINE BETA LIGHT CAME ON. PILOTS ELECTED TO TAKE OFF. TORQUE DROPPED 40%, AND PROPELLER SPEED INCREASED ON THE SAME ENGINE. #1 ENGINE FEATHERED DUE TO DRAG AND OVERSPEED OF THE PROP. ENGINE WAS DOWN TO 20%TQ, AND NP PEAKSDR 2021F00004Floorbeam · corrodedINTERGRANULAR CORROSION FOUND ON UPPER FLOOR BEAM "T" CAP ANGLE AT FRAME 1F. THE SECTION OF EXTRUDED T-ANGLE WAS CUT, REMOVED AND REPLACED WITH A PIECE OF 2024T3511 OF SIMILAR SIZE AND LENGTH. IT WAS ETCHED, ALODINED AND PAINTED AS REQUIRED, AND INSTALLED USSDR UATA202101073315Firewall · crackedNR 1 AND 2 ENGINE AFT SIDE OF FIREWALL LOWER DOUBLERS FOUND CRACKED NEAR OUTER EDGE OF BOTH LEFT AND RIGHT LOWER MOUNT FITTINGS. REPAIRED BOTH LT AND RT CRACKED DOUBLERS ON BOTH ENGINE FIREWALLS BY INSERTION OF NEW DOUBLER SECTIONS OF SIMILAR THICKNESS AND SISDR UATA202101073312Attach Fitting · corrodedINTERGRANULAR CORROSION WAS FOUND ON THE RT FWD HORIZONTAL STABILIZER LOWER FWD ATTACH FITTING AROUND THE BUSHING HOLE. THE AFFECTED ATTACH FITTING WAS REMOVED AND REPLACED WITH A NEW FITTING OF THE SAME P/N, UTILIZING THE SAME TYPE ATTACHING FASTENERS. WORKSDR UATA202101073314Skin · crackedAIRFRAME SKIN CRACKED TO THE EDGE ON LT SIDE OF CENTER WING CUTOUT AT FR 5. REMOVED DAMAGE, FABRICATED A FLUSH PATCH AND DOUBLER, IAW CASA SRM APPX II FIG B9.SDR UATA202101073313Skin · crackedAIRFRAME SKIN CRACKED TO THE EDGE ON RT FWD SIDE OF CENTER WING CUTOUT AT FR 5. REMOVED DAMAGE, FABRICATED A FLUSH PATCH AND DOUBLER, IAW CASA SRM APPX II FIG B9.
STCs that may be installed · 67
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.