# N441LL: Cessna 441, registration cancelled 2001-01-10

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: January 10, 2001
- Exported to: Canada
- Status when cancelled: Triennial form not returned
- Airframe: [Cessna 441](https://openairdocs.org/model/cessna-441) (registry code 2076020)
- Data sheets: [TCDS A28CE](https://openairdocs.org/tcds/A28CE) (OpenAirDocs)
- Serial number: 441-0139
- Type of aircraft: Fixed wing multi engine
- Certificate issued: June 19, 1997
- Last registry action: October 17, 2000
- Mode S code: A54F59
- Owner when cancelled: [Peninsula Airways Inc](https://openairdocs.org/faa-owner/PENINSULA%20AIRWAYS%20INC)
- Location: [Anchorage, AK](https://openairdocs.org/faa-place/AK/Anchorage)
- Owner type: Corporation
- Owner's area on the map: 61.1637° N, 149.9966° W: Placed by OpenAirDocs at the center of ZIP code 99502, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N441LL
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=441LL
- Page: https://openairdocs.org/deregistered/N441LL-2001-01-10

From the FAA registry file of November 7, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Cessna 441: https://openairdocs.org/model/cessna-441.md

## Service difficulty reports (12)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR PNSA0901](https://openairdocs.org/sdr/PNSA0901), Sep 1, 2000: TRANSDUCER. MALFUNCTIONED. TORQUE INDICATION WENT TO ZERO DURING DESCENT. AFTER UNEVENTFUL LANDING, REPLACED TORQUE TRANSDUCER. OPERATIONAL CHECK OK. (X)
- [SDR PNSA000401](https://openairdocs.org/sdr/PNSA000401), Apr 1, 2000: FAN. FAILED. DURING CLIMB, A SMOKEY SMELL WAS NOTICED IN THE CABIN. BLEED AIR WAS SHUT OFF BUT SMELL CONTINUED. RETURNED FOR LANDING. DISCOVERED WINDINGS FOR CABIN FRESH AIR
- [SDR PNSA000206](https://openairdocs.org/sdr/PNSA000206), Feb 3, 2000: ENGINE. LACK OF LUBE. DURING TAXI OIL PRESSURE INDICATED LOWER THAN NORMAL. RETURNED TO BLOCK. SERVICED OIL, OPS CHECKED OK.
- [SDR PNSA000103](https://openairdocs.org/sdr/PNSA000103), Jan 13, 2000: LINKAGE. OUT OF ADJUST. ON ROLL OUT WHILE RETARDING SPEED LEVER TO THE TAXI POSITION, ENGINE SHUT DOWN. FOUND FUEL SHUT-OFF LINKAGE OUT OF DETENT. RE-INDEXED LINKAGE TO SPEED LEVER, OP
- [SDR PNSA000105](https://openairdocs.org/sdr/PNSA000105), Jan 5, 2000: TIRE. FAILED. WHILE HOLDING AT FAI AT -39F OAT LT MAIN TIRE WENT FLAT. FLIGHT DELAYED WHILE WHEEL ASSY CHANGED.
- [SDR PNSA991102](https://openairdocs.org/sdr/PNSA991102), Nov 27, 1999: COOLER. CRACKED. EN ROUTE FROM BFI TO ANC, RT OIL PRESSURE BEGAN TO FLUCTUATE, DIVERTED TO SIT. ON FINAL, LOST RT OIL PRESSURE COMPLETELY SECURED ENGINE AND LANDED. OIL COOLER W
- [SDR PNSA991101](https://openairdocs.org/sdr/PNSA991101), Nov 21, 1999: CIRCUIT BREAKER. FAILED. WHILE CLIMBING-OUT PILOT NOTICED SMOKE COMING FROM THE RECOGNITION LIGHT SWITCH-BREAKER. SYSTEM WAS TURNED OFF, SMOKE STOPPED. LANDING WAS NORMAL. SWITCH BREAKE
- [SDR PNSA990901](https://openairdocs.org/sdr/PNSA990901), Sep 7, 1999: PUMP. SIEZED. ON RUNWAY, SELECTED SPEEDS HIGH FOR TAKEOFF, RT ENGINE FLAMED OUT. RETURNED TO BLOCK. REPLACED ENGINE DRIVEN FUEL PUMP, OPS CHECKED OK.
- [SDR PNSA980207](https://openairdocs.org/sdr/PNSA980207), Feb 10, 1998: WIRE. LOOSE. ENGINES WOULD NOT CRANK. SECURED WIRE AT SQUAT SWITCH, OPS CHECK OK.
- [SDR PNSA980206](https://openairdocs.org/sdr/PNSA980206), Feb 5, 1998: HSI CARD. FAILED. CAPTAINS HSI CARD DID NOT TURN DURING TAXI. REPLACED HSI, OPS CHECK OK.
- [SDR PNSA971213](https://openairdocs.org/sdr/PNSA971213), Dec 23, 1997: TIRE. FLAT. DURING ROLL OUT, NO BRAKE ACTION FROM RT MAIN, TIRE HAD LOST PRESSURE, WHILE REMOVING AIRCRAFT FROM RUNWAY LT MAIN ALSO WENT FLAT. REPLACED BOTH WHEEL ASSY. NOT
- [SDR 96ZZZX5113](https://openairdocs.org/sdr/96ZZZX5113), Sep 23, 1996: RIB. CRACKED. DURING PHASE INSPECTION, FOUND 1.5 INCH CRACK IN RT WING CANTED RIB TOP CAP. CRACK STARTS AT AFT SIDE OF FORWARD SPAR AND RUNS AFT PARALLEL TO THE BEND RADIUS. 

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