N405CP1990 C A S A C-212-DF
Safety record in brief:No NTSB accidents or incidents since 198211 ADs may apply5 service difficulty reports
Registration
FAA Aircraft Registry · Oct 20, 2026- Registered owner
- Conocophillips Alaska INC
- Owner type
- Corporation
- City, state
- Anchorage, AK
- Certificate issued
- Sep 30, 2021
- Expires
- Sep 30, 2028
- Airworthiness
- Restricted · Patrolling
- Airworthiness date
- Jul 30, 2009
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Airframe & engine
FAA Registry + type dataAirframe
- Manufacturer
- C A S A
- Model
- C-212-DF
- Year
- 1990
- Serial number
- 405
- Aircraft type
- Fixed wing multi engine
- Category
- Land
- Certification
- Type Certificated
- Seats
- 19
- Engines
- 2
- Max takeoff weight
- 12,500 - 19,999 lb
- Mode S code
- A4BF74
Engine
- Make and model
- Honeywell Tpe331-10r
- Type
- Turbo-prop
- Power
- 940 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 2021 – nowConocophillips Alaska INCAnchorage, AK · current
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026NTSB events (0)
No NTSB accidents or incidents found for this airframe since 1982.
ADs published since 1998 that may apply (11)
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2018-22-01 | Turbine Section | Dec 10, 2018 | Engine (TPE331-10R)Only with: Second stage turbine rotor assemblies P/N 3102106-1, -6, -8 or P/N 3101514-1, -10, -12 installed. |
| 2018-13-05 | Turbine Engine Reduction Gear | Jul 26, 2018 | Engine (TPE331-10R)Only with: Hydraulic torque sensor gear assemblies P/Ns 3101726-1, -2, or -3 installed. |
| 2018-02-14 | Turbine Engine Combustion Section | Feb 28, 2018 | Engine (TPE331-10R)Only with: Combustion chamber case assemblies P/Ns 869728-x, 893973-x, 3101668-x, or 3102613-x (any dash number) installed. |
| 2016-21-07 | Honeywell International Inc. Turboprop Engines | Nov 28, 2016 | Engine (TPE331-10R)Only with: Woodward fuel control unit (FCU) assemblies with Honeywell P/Ns listed in Table 1 to paragraph (c) of the AD installed. |
| 2016-18-17 | Honeywell International Inc. Turboprop and Turboshaft Engines | Nov 4, 2016 | Engine (TPE331-10R)Only with: With 2nd stage compressor impeller P/N 893482-1 through -5 inclusive, or P/N 3107056-1 or 3107056-2, installed. |
Show all 11 ADsShow fewer ADs
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2015-18-03 | Honeywell International Inc. Turboprop Engines (Type Certificate Previously Held by… | Nov 13, 2015 | Engine (TPE331-10R)Only with: Engine propeller shaft coupling P/N 3107065-1, 865888-3, 865888-6, or 865888-8 installed. |
| 2014-12-04 | Honeywell International Inc. Turboprop Engines | Jul 22, 2015 | Engine (TPE331-10R)Only with: Woodward fuel control unit (FCU) assemblies with Honeywell P/Ns listed in Table 1 to paragraph (c) (P/N 869199, 893561, 897770, 897375, 897780 dash numbers) installed. |
| 2012-02-06 | Honeywell International Inc. TPE331-10 and TPE331-11 Series Turboprop Engines | Mar 15, 2012 | Engine (TPE331-10R)Serial numbers per Table 2 of Honeywell International Inc. Alert Service Bulletin TPE331-72-A2156, dated December 2, 2008. Only with: First stage turbine disk P/N 3101520-1 or 3107079-1 with S/N listed in the ASB installed. |
| 2009-17-05 | Honeywell International Inc. TPE331-10 and TPE331-11 Series Turboprop Engines | Sep 1, 2009 | Engine (TPE331-10R)Only with: First stage turbine disk P/N 3101520-1 or 3107079-1, S/N 2-03501-2299, 2-03501-2300, 2-03501-2301, 2-03501-2302, or 2-03501-2304 installed. |
| 2002-25-02 | Honeywell International Inc. TPE331-3, -5, -6, -8, -10, and -11 Series Turboprop and… | Jan 21, 2003 | Engine (TPE331-10R) |
| 2002-21-15 | Honeywell International Inc. TPE331 Series Turboprop and TSE331-3U Series Turboshaft… | Nov 26, 2002 | Engine (TPE331-10R)Only with: Engines with second stage turbine stator assemblies P/N 894528-1, -2, -3, -5, -6, -10, or -11 installed. |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (5)
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
- Stabilizers · skin · crackedJan 22, 2026
DURING ROUTINE MAINTENANCE IN ANCHORAGE, AK (ANC), MAINTENANCE NOTED THAT (2EA.) FASTENERS COMMON TO THE HORIZONTAL STABILIZER LOWER SKIN & SPAR CHORD HAVE CRACKED OUT. THE CRACKS MEASURE .204” AND .242” LONG, RESPECTIVELY, AND THEY EMANATE IN THE OUTBOARD DIRECTION FROM THE FASTENER HEADS.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · floorbeam · bentJan 22, 2026
DURING ROUTINE OPERATIONS IN ANCHORAGE, AK (ANC), MAINTENANCE DISCOVERED DAMAGE TO THE ENDS OF LOWER FRAME 13 & 16 INNER FRAME T-CHORD FLANGES AT LBL19 & RBL19, NEAR THE SEAT TRACK SUPPORTS. THE T-CHORD FLANGE CORNERS WERE LOCALLY BENT DOWN WITH GOUGING ON THE TOP SIDE CAUSED BY CONTACT WITH A…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Lights · motor · failedNov 2, 2024
MOTOR INOPERATIVE - RETRACTABLE LANDING/TAXI LAMP ASSY - BURNT ELECTRICAL SMELL IN COCKPIT
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 5 reportsShow fewer reports
- Landing gear · wire harness · chafedSep 25, 2011
MULTIPLE CIRCUIT BREAKERS ON OVERHEAD PANEL POPPED IN FLIGHT. FLIGHT CREW CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. BREAKERS THAT TRIPPED INSTRUMENT LIGHT, ANTI SKID AND TEST, RADIO POWER AND NR 2 INVERTER OUTPUT 26 VAC AND 115 VAC. DETERMINED THE WIRING CHAFED AT ANTI-SKID CONTROL…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Flight controls · servo · jammedNov 22, 2010
RUDDER SERVO FAILED 4.4 HOURS AFTER INSTALL. RUDDER WENT HARD OVER TO THE LT AND JAMMED IN PLACE. ONCE POWER WAS REMOVED THE PILOTS COULD AT LEAST MOVE THE RUDDER EVEN THOUGHT THE CLUTCH WAS STILL ENGAGED. UPON TEARDOWN FOUND CLUTCH HUB SCREWS HAD BACKED OUT CAUSING CLUTCH ENGAGEMENT WITH NO POWER…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026