- Registered owner
- Conocophillips Alaska Inc
- Location
- Anchorage, AK
- Owner type
- Corporation
- Serial number
- 405
- Year built
- 1990
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Airworthiness
- Restricted, patrolling
- Airworthiness date
- July 30, 2009
- Certificate issued
- September 30, 2021
- Expires
- September 30, 2028
- Mode S code
- A4BF74
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 59
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 | 2 |
| 1986 | 1 |
| 1987 | 7 |
| 1988 | 2 |
| 1989 | 7 |
| 1991 | 1 |
| 1992 | 1 |
| 1993 | 2 |
| 1995 | 2 |
| 1996 | 2 |
| 1997 | 3 |
| 1998 | 6 |
| 1999 | 2 |
| 2003 | 1 |
| 2004 | 2 |
| 2005 | 1 |
| 2006 | 2 |
| 2007 | 1 |
| 2008 | 1 |
| 2009 | 2 |
| 2011 | 1 |
| 2012 | 1 |
| 2014 | 1 |
| 2015 | 3 |
| 2016 | 2 |
| 2017 | 2 |
| 2018 | 5 |
| 2020 | 1 |
| 2021 | 1 |
| 2022 | 1 |
Airframe · C A S A C-212-DF
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 N405CPMatched 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 C A S A C-212-DF aircraft
FAA incident reports
No FAA accident or incident reports matched to N405CPMatched 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 C A S A C-212-DF aircraft
Service difficulty reports · 5
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 8TNC202601220054Floorbeam · bentDURING 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 THESDR 8TNC202601220001Skin · crackedDURING 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 DIRSDR 2024F00264Motor · failedMOTOR INOPERATIVE - RETRACTABLE LANDING/TAXI LAMP ASSY - BURNT ELECTRICAL SMELL IN COCKPITSDR SROM2011011Wire Harness · chafedMULTIPLE 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 TSDR SROM2010016Servo · jammedRUDDER 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 OU
STCs that may be installed · 41
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · C A S A C-212-DF
STC ST01305WI-DModification of a Collins ALT-50A or ALT-55B Radio Altimeter system installation to a Collins ALT-1000 or ALT-4000 Radio Altimeter system installation in accordance with Collins Drawing Index as listed on AML No. ST01305WI-D, Revision -, or later FAA approved revision.STC ST04105NYInstallation of Flight Data Recorder, Flight Data Acquisition Unit, Traffic Advisory Altering System and Navigation SuiteSTC ST04109NYUpdate of COMBI