# Service difficulty reports: Cessna 441

A list on [Cessna 441](https://openairdocs.org/model/cessna-441.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 11 · 516 reports

- [SDR 2026FA0000788](https://openairdocs.org/sdr/2026FA0000788.md): Engine · failed · Sep 25, 2026 · N440EH · Cessna 441 · Engine (Turbine/Turboprop)
  > DURING CRUISE FLIGHT AT FL290, ONE HOUR AFTER TAKEOFF, RIGHT ENGINE TORQUE QUICKLY FELL TO ZERO AND REMAINED, NO OSCILLATIONS. SIMULTANEOUSLY, RIGHT ENGINE EGT INCREASED TO BEYOND RED LINE AND REMAINED, NO OSCILLATIONS. AIRCRAFT YAWED AND BEGAN TO LOSE ALTITUD
- [SDR 2026FA0000619](https://openairdocs.org/sdr/2026FA0000619.md): Rod End · sheared · Jul 19, 2026 · N274GC · Cessna 441 · Landing Gear Retraction/Extension System
  > AFTER LANDING AND UPON ROLL OUT THE PILOT EXPERIENCED THE NOSE OF THE AIRCRAFT STARTING TO DROP. HE PULLED BACK ON THE YOKE AND THE NOSE CONTINUED TO DROP, AT WHICH TIME THE LEFT AND RIGHT PROPELLERS CONTACTED THE RUNWAY, WHICH CAUSED BOTH ENGINES TO SHUT DO
- [SDR 2026FA0000615](https://openairdocs.org/sdr/2026FA0000615.md): Hydraulic Line · leaking · Jul 9, 2026 · N441SK · Cessna 441 · Hydraulic System, Main
  > ON DESCENT LT AND RT "HYD LOW FLOW" ANNUNCIATORS START FLICKERING THEN WENT FULLY ON. EXTENDED LANDING GEAR BUT ONLY LT MAIN WENT DOWN AND LOCKED. BLEW THE LANDING GEAR BLOWDOWN BOTTLE, HEARD THE BOTTLE BLOW BUT HAD NO FURTHER DOWN AND LOCKED INDICATION. AFTER
- [SDR 2025FA0000003](https://openairdocs.org/sdr/2025FA0000003.md): Governor · faulted · Jan 3, 2025 · N441BW · Cessna 441 · Engine Controls
  > ON TAXI OUT, THE LT FUEL COMPUTER WENT OFF-LINE, THE PILOTS SELECTED BOTH FUEL COMPUTERS OFF AND PROCEEDED TO FLY IN MANUAL IAW THE MANUAL. WHILE APPLYING TAKE OFF POWER SOME SURGING WAS NOTICED ON THE LT ENGINE. ABORTED TAKE OFF. FOUND THE MONOPOLE MALFUCTION
- [SDR 2024FA0000621](https://openairdocs.org/sdr/2024FA0000621.md): Propeller · shutdown · Jul 22, 2024 · Cessna 441 · Propeller Assembly
  > PERFORMED INFLIGHT ENGINE SHUTDOWN BEFORE RELEASE TO SERVICE AS REQUIRED AFTER ENGINE HOT SECTION INSPECTION AND ENGINE INSTALLATION. AT INFLIGHT SHUTDOWN THE ENGINE SPOOLED DOWN AFTER TURNING OFF FUEL AS EXPECTED. HOWEVER, WHEN THE MANUAL FUEL CUTOFF/PROP F
- [SDR 2024F00098](https://openairdocs.org/sdr/2024F00098.md): Antenna · inflt separation · Mar 21, 2024 · N11MM · Cessna 441 · VHF Communications System
  > DURING CRUISE PHASE OF FLIGHT FROM SNP TO ANC PILOT FELT VIBRATION/BUFFETING AND SLOWED HIS AIRSPEED DOWN AND DESCENDED 2000-3000 FEET IN ALTITUDE THINKING MAYBE HE HIT TURBULENCE. ON DESCENT INTO ANC. PILOT TRIED LISTENING TO #2 COM WITH NO RESULTS AND SWITCH
- [SDR 2024F00037](https://openairdocs.org/sdr/2024F00037.md): Gyro · abnormal · Feb 18, 2024 · N92JQ · Cessna 441 · Attitude Gyro and Indicating System
  > AIRCRAFT TOOK OFF AND SHORTLY AFTERWARDS THE CREW NOTICED SMOKE IN THE COCKPIT AND THE EMERGENCY PRESSURIZATION RED LIGHT CAME ON. THE CREW DONNED MASKS AND DEPLOYED THE MASKS FOR THE 2 PAX ONBOARD. PAX PUT MASK ON, THE CREW DECLARED AN EMERGENCY WITH MINNEAPO
- [SDR 6GFA202401220001](https://openairdocs.org/sdr/6GFA202401220001.md): Landing Gear · stuck · Jan 10, 2024 · N441WJ · Cessna 441 · Landing Gear Retraction/Extension System
  > ON APPROACH TO PBI WHEN GEAR WAS SELECTED DOWN, RIGHT GEAR DID NOT INDICATE DOWN. TOWER WAS ADVISED AND REPORTED THEY DID NOT HAVE A VISUAL ON RIGHT GEAR. APPROACH WAS TERMINATED. AFTER A DISCUSSION WITH THE TOWER THE DECISION TO LAND AT FLL WAS MADE DUE TO
- [SDR 2023FA0000357](https://openairdocs.org/sdr/2023FA0000357.md): Bearing Race · galled · Jul 7, 2023 · N441HS · Cessna 441 · Engine (Turbine/Turboprop)
  > TORQUE SENSOR BEARING INNER RACE GALLED [PN: 70100168-1, SN: 19-151725-05170, TSN: 423.1]. RESULTED IN BAD SOAP, 5 SHINY M50 PLATELETS UP TO 0.2MM REPORTED. ENGINE [TPE331-10N-512S, SN: P-77454, TSN: 6,889.1, CSN: 11,904, TSO: 2,424.0, CSO: 1,449].
- [SDR 3SVA202212080001](https://openairdocs.org/sdr/3SVA202212080001.md): Bulkhead · cracked · Dec 8, 2022 · N318AK · Cessna 441 · Fuselage Main, Bulkhead
  > LOWER CABIN BULKHEAD AT FS 235.75 FOUND CRACKED IN LIGHTENING HOLE ON THE RIGHT SIDE AT FLOOR LEVEL. DUE TO COMPLEXITY OF BENDS AND SHAPE OF FORMED METAL, IT WAS NECESSARY TO REMOVE AND REPLACE THE BULKHEAD WITH USED, SERVICEABLE UNIT
- [SDR 3SVA05072022](https://openairdocs.org/sdr/3SVA05072022.md): Bolt · broken · May 7, 2022 · N441SK · Cessna 441 · Landing Gear Retraction/Extension System
  > DURING ROUTINE CLEANING AND GENERAL CARE OF THE AIRCRAFT IN THE HANGAR, A RAMP ATTENDANT NOTICED ONE OF THE CLAMPS SECURING THE TAXI LIGHT HARNESS TO THE AFT DRAG BRACE ASSEMBLY WAS LOOSE. IT IS NORMALLY SECURED TO THE NAS 464 BOLT THAT ATTACHED THE FORWARD A
- [SDR 2021FA0000404](https://openairdocs.org/sdr/2021FA0000404.md): Oil Filter · broken · Dec 14, 2021 · N441X · Cessna 441 · Oil Servicing
  > DURING ROUTINE 100 HOUR ENGINE MAINTENANCE, FOUND OIL FILTER ON RIGHT ENGINE PARTIALLY SEPARATED.
- [SDR 3SVA2021F00069](https://openairdocs.org/sdr/3SVA2021F00069.md): Circuit Breaker · failed · Jul 3, 2021 · N11MM · Cessna 441 · Light System Wiring
  > DURING TAXI-OUT FROM BASE, CAPT. NOTED SMOKE EMITTING FROM LIGHT SWITCH AREA AT THE LOWER LH CONSOLE. THEY TAXIIED BACK HOME BASE UNEVENTFULLY AND HANDED OVER THE AIRCRAFT TO MAINTENANCE. IT WAS IMMEDIATELY APPARENT THAT THE RH STROBE LIGHT CIRCUIT BREAKER S
- [SDR 3SVA20210402001](https://openairdocs.org/sdr/3SVA20210402001.md): Connector · shorted · Apr 2, 2021 · N318AK · Cessna 441 · Engine Indicating System Wiring
  > RT ENGINE TQ, EGT, AND FF OSCILLATIONS. DECLARED EMERGENCY AND RETURNED TO BASE WITHOUT INCIDENT. MX FOUND CHAFFING WIRES AT EGT COMPENSATOR CONNECTOR. REPAIRED WIRING, PERFORMED GROUND RUNS FOR PERFORMANCE WITH NO DEFECTS AND RETURNED AIRCRAFT TO SERVICE.
- [SDR 3SVA20210303001](https://openairdocs.org/sdr/3SVA20210303001.md): Gcu · unknown · Feb 28, 2021 · N128EZ · Cessna 441 · DC Generating System
  > DURING A ROUTINE TRAINING FLIGHT THE LEFT ENGINE WAS SHUTDOWN PER AFM PROCEDURES. THE LEFT BUS CURRENT LIMITER FAILED OPEN AT SOME POINT, RESULTING IN LOSS OF LEFT BUS POWER AND THE INABILITY TO RESTART THE ENGINE DUE TO NO POWER ON THE LEFT BUS. THE CREW DE
- [SDR 3SVA20190607001](https://openairdocs.org/sdr/3SVA20190607001.md): Line · contaminated · Jun 4, 2019 · N441BD · Cessna 441 · Pitot/Static System
  > PILOT SIDE ALTIMETER, VSI, AND AIR SPEED INDICATOR, AND ALTITUDE REPORTING SYSTEM EXPERIENCED UNRELIABLE/INACCURATE INDICATIONS. THE PROBLEM WAS FOUND TO BE MOISTURE (FREEZING) IN THE PILOTS SIDE STATIC SYSTEM LINE LOCATED IN THE BELLY OF THE AIRCRAFT. OF NO
- [SDR 3SVA20190425001](https://openairdocs.org/sdr/3SVA20190425001.md): Push-Pull Rod · corroded · Apr 25, 2019 · Cessna 441 · Elevator Control System
  > DUE TO AGING AIRCRAFT CONCERNS THIS OPERATOR HAS EMBARKED ON A FLEET CAMPAIGN TO REMOVE THE ELEVATOR PUSH PULL TUBES FROM THE C441 AIRCRAFT AND SEND THEM OUT FOR AN XRAY INSPECTION. WE HAVE PERFORMED INSPECTIONS ON FOUR TUBES P/N 5815144-204 (ORIGINAL P/N 581
- [SDR 3SVA20180709001](https://openairdocs.org/sdr/3SVA20180709001.md): Wire · broken · Jul 6, 2018 · N441BD · Cessna 441 · Landing Gear System Wiring
  > DURING APPROACH TO LAND AFTER SELECTING GEAR DOWN AND COMPLETION OF THE CYCLE, THE NOSE GEAR DOWNLOCK GREEN INDICATOR LAMP FAILED TO ILLUMINATE. THE IN TRANSIT LIGHT WAS EXTINGUISHED AND THE NOSE GEAR WAS VISIBLE IN THE DOWN POSITION IN THE VIEWING MIRROR. L
- [SDR 3SVA2017082200001](https://openairdocs.org/sdr/3SVA2017082200001.md): Hsi · spinning · Aug 22, 2017 · N441DK · Cessna 441 · Independent Instruments
  > DURING CLIMB OUT, COPILOTS HSI STARTED SPINNING RAPIDLY. RETURNED TO BASE.
- [SDR 3SVA2017061300001](https://openairdocs.org/sdr/3SVA2017061300001.md): Lamp · burned out · Jun 13, 2017 · N441SK · Cessna 441 · Instrument Panel
  > ON TAXI TO TAKE-OFF, ENGINE IGNITION ON LIGHT BURNED OUT. AIRCRAFT RETURNED TO THE BLOCK, RELAMPED LIGHT AND RELEASED AIRCRAFT.
- [SDR YN8R03172017MC](https://openairdocs.org/sdr/YN8R03172017MC.md): Doubler · cracked · Mar 8, 2017 · Cessna 441 · Fuselage Main, Structure
  > WHILE PERFORMING A PHASE 35 INSPECTION, NOSE GEAR ATTACHMENT & WHEEL WELL STRUCTURE INSPECTION FOUND DOUBLER CRACKED AROUND L/H AFT ATTACH POINT FOR NOSE GEAR DRAG BRACE. MATCH DRILLED AND INSTALLED NEW DOUBLER IAW MM 51-30-01, REV. 16
- [SDR 2017FA0000378](https://openairdocs.org/sdr/2017FA0000378.md): Line · failed · Feb 3, 2017 · N716SM · Cessna 441 · Hydraulic System, Main
  > HYDRAULIC LINE, HIGH PRESSURE, OPERATES LANDING GEAR AND FLAPS. THIS OPERATOR HAS SEEN THIS SAME HARD HYDRAULIC LINE FAIL, HIGH PRESSURE LEAK, ON OTHER C441 ACFT ALONG WITH OTHER HYDRAULIC LINES AFT OF FIRE WALL.
- [SDR 3SVA2017013000001](https://openairdocs.org/sdr/3SVA2017013000001.md): Wire · shorted · Jan 28, 2017 · N441DK · Cessna 441 · Engine Indicating System Wiring
  > RT ENGINE TORQUE INDICATOR WENT TO REDLINE ON TAKEOFF CAUSING THE ENGINE COMPUTER TO REDUCE POWER BECAUSE IT SENSED AN OVER TORQUE SITUATION. THE INDICATION WAS FAULTY AND THERE WAS NOT AN OVER TORQUE ISSUE. INSPECTION OF THE WIRES AT THE TORQUE TRANSDUCER REV
- [SDR YN8R201606220001](https://openairdocs.org/sdr/YN8R201606220001.md): Elt · failed · Jun 22, 2016 · N441EC · Cessna 441 · Emergency Locator Beacon
  > ELT FAILED DURING ANNUAL TEST. BATTERY WAS WITHIN LIFE LIMITS. REPLACED WITH ELT 1000.
- [SDR YN8R20160308002](https://openairdocs.org/sdr/YN8R20160308002.md): Tee Fitting · cracked · Mar 8, 2016 · N441LA · Cessna 441 · Fuselage, Landing Gear Attach Fittings
  > WHILE COMPLYING WITH PHASE 35 OF THE MM AND SID 32-20-01, ON THE RT SIDE OF THE NOSE WHEEL WELL JUST AFT OF THE DRAG BRACE ATTACHMENT, WE FOUND THE RT TEE, PN 5213028-15 TO HAVE A 1" CRACK THROUGH THE UPPER RIVET AND EXTENDING TO THE NEXT RIVET THAT ATTACHES T
- [SDR YN8R20160308001](https://openairdocs.org/sdr/YN8R20160308001.md): Tee Fitting · sheared · Mar 8, 2016 · N441LA · Cessna 441 · Fuselage, Landing Gear Attach Fittings
  > WHILE COMPLYING WITH PHASE 35 OF THE MM INSPECTION PROGRAM AND SID 32-20-01, ON THE LT SIDE OF THE NOSE WHEEL WELL JUST AFT OF THE DRAG BRACE ATTACHMENT, WE FOUND THE LT BRACKET, PN 5213028-200 TO HAVE ALL 3 RIVETS SHEARED THAT ATTACH THE BRACKET TO THE GUSSET
- [SDR IGXR20151124001](https://openairdocs.org/sdr/IGXR20151124001.md): Line · split · Nov 20, 2015 · N441WD · Cessna 441 · Hydraulic System, Main
  > DURING THE CLIMB, THE PILOT NOTICED HYDRAULIC QUANTITY WARNING FLASHING AT FIRST, THEN BECOMING STEADY. HYDRAULIC LEVEL DROPPED TO ZERO. ACFT RETURNED BACK TO THE AIRPORT, GEAR WAS EMERGENCY EXTENDED SAFE LANDING WAS MADE. MAINTENANCE PERSONNEL INVESTIGATED T
- [SDR DSCR20151005001](https://openairdocs.org/sdr/DSCR20151005001.md): Relief Valve · fractured · Sep 24, 2015 · N14FJ · Cessna 441 · Engine Fuel Pump
  > DURING CRUISE PHASE OF FLIGHT, THE RT ENG EXPERIENCED LOSS OF FUEL PRESS. PILOT SHUT THE RT ENG DOWN, CONTACTED ATC & WAS DIVERTED. TECHNICIANS INSPECTED THE ENG & FOUND THE CAP HAD SEPARATED FROM THE HIGH PRESS RELIEF VLV, WHICH RESULTED IN THE LOSS OF FUEL
- [SDR H5GR2015FA0000007](https://openairdocs.org/sdr/H5GR2015FA0000007.md): Skin · cracked · Dec 24, 2014 · N711MB · Cessna 441 · Elevator, Plate/Skin
  > FOUND MULTIPLE CRACKS, ONE TO FOUR INCHES LONG, IN ELEVATOR T/E SKIN, ON BOTTOM SIDE WHERE SKIN JOINS FWD SKIN. UPON REMOVING SKIN WHERE SKIN JOINS FWD SKIN. UPON REMOVING SKIN FOR REPLACEMENT, FOUND REAR/AUX SPAR CRACKED AT OUTBD END WHERE SPAR ATTACHES TO
- [SDR FEHR2015FA0000030](https://openairdocs.org/sdr/FEHR2015FA0000030.md): Bypass Valve · leaking · Dec 1, 2014 · N441G · Cessna 441 · Fuel Control/Turbine Engines
  > WHILE TROUBLESHOOTING THE LT BETA LIGHT SYSTEM, FOUND FUEL LEAKING FROM THE LT ENGINE FUEL CONTROL BYPASS VALVE, DUMPING FUEL ONTO THE HOT SECTION OF THE ENGINE. THE FUEL CONTROL WAS REMOVED AND SENT TO MFG FOR OVERHAUL.
- [SDR YN8R2014111900001](https://openairdocs.org/sdr/YN8R2014111900001.md): Control Cable · broken · Nov 18, 2014 · N441LA · Cessna 441 · Elevator Control System
  > DURING INSPECTION PHASE 51, UP ELEVATOR CABLE, PN 5815103-6 WAS FOUND TO HAVE 3 COMPLETE STRANDS BROKEN. LOCATION OF THE BREAKS IS UNDER THE PULLEY, PN S378-4 AT FS 292.05. THE PULLEY WAS INSPECTED AND IT WAS FOUND TO BE FREE ROLLING. NO OBVIOUS MECHANICAL
- [SDR BGJA20141118001](https://openairdocs.org/sdr/BGJA20141118001.md): Door Frame · cracked · Nov 13, 2014 · N441CT · Cessna 441 · Passenger/Crew Doors
  > WE LOCATED A CRACK OF THE LOWER CABIN DOOR AFT PART OF THE DOOR FRAME NEAR THE DOOR HINGE. LOCATED AT STATION 270. THE CRACK IS ROUGHLY 2 INCHES IN LENGTH ALONG THE CTR LINE OF THE RADIUS OF THE FRAME BEND. THESE CRACKS APPEAR ON THE DOOR FRAMES DUE TO HOW
- [SDR 3SVA2014072100001](https://openairdocs.org/sdr/3SVA2014072100001.md): Filter · clogged · Jul 21, 2014 · N441BD · Cessna 441 · Fuel Control/Turbine Engines
  > DURING TAXI FOR TAKEOFF, LT ENGINE FUEL COMPUTER TRIPPED OFFLINE. THE ENGINE RPMS THEN BEGAN TO DECAY AND THE LT GENERATOR DROPPED OFF LINE. PILOT SHUTDOWN THE ENGINE, PERFORMED A RESTART AND RETURNED TO BASE.
- [SDR CA140818002](https://openairdocs.org/sdr/CA140818002.md): Transducer · erratic · Jun 4, 2014 · Cessna 441 · Engine BMEP/Torque Indicating
  > (CAN) ERRATIC TORQUE INDICATION DURING FLIGHT.
- [SDR 3SVA20131119001](https://openairdocs.org/sdr/3SVA20131119001.md): Connector · shorted · Nov 19, 2013 · N441DK · Cessna 441 · Engine Fuel System Wiring
  > RIGHT ENG WOULD NOT START. START CONTROL CB POPPED, SHORT FOUND IN THE PRIMARY FUEL NOZZLE SOLENOID CONNECTOR. REPLACED SAME, OPERATIONS CHECKED GOOD.
- [SDR 5XWR201307110363](https://openairdocs.org/sdr/5XWR201307110363.md): Structure · misoverhauled · Jul 11, 2013 · N440DA · Cessna 441 · Fuselage Main, Structure
  > PERFORMED A PHASE 2, 3, & D, TASK A361004, BLEED AIR LINE EXHIBITED CORROSION WHERE ITS FLANGE FASTENS TO THE FUSELAGE SKIN BS 187.87 RBL 27, AND WL 62.79. ON DISASSEMBLY, FLANGE TO FUSELAGE JOINT FOUND WITH HEAVY DISSIMILAR METAL CORROSION. INVESTIGATION
- [SDR 2013FA0000325](https://openairdocs.org/sdr/2013FA0000325.md): Engine · failed · Apr 28, 2013 · N6851X · Cessna 441 · Engine (Turbine/Turboprop)
  > RIGHT ENGINE EGT INCREASED. FIRE LIGHT ACTIVATED AND THEN PERFORMED EMERGENCY SHUTDOWN PROCEDURES.
- [SDR CA130425002](https://openairdocs.org/sdr/CA130425002.md): Line · split · Apr 23, 2013 · Cessna 441 · Hydraulic System, Main
  > (CAN) HYDRAULIC LINE HAS SMALL SPLIT, NOT VISIBLE TO NAKED EYE, BUT SHOWS UP WHEN UNDER PRESSURE.
- [SDR YN8R20130404001](https://openairdocs.org/sdr/YN8R20130404001.md): Link · corroded · Apr 4, 2013 · N456GT · Cessna 441 · Main Landing Gear Strut/Axle/Truck
  > DURING PHASE 53 INSPECTION, FOUND BOTH TRAIING LINK PIVOT HOLES CORRODED BEYOND LIMITS. LEVEL 2 CORROSION FOUND. LAST PHASE 53 INSPECTION 3 YEARS AGO
- [SDR YN8R201304040001](https://openairdocs.org/sdr/YN8R201304040001.md): Link · corroded · Apr 4, 2013 · N456GT · Cessna 441 · Main Landing Gear Strut/Axle/Truck
  > DURING PHASE 53 INSPECTION, FOUND BOTH TRAILING LINK PIVOT HOLES CORRODED BEYOND LIMITS. LEVEL 2 CORROSION FOUND. LAST PHASE 53 INSPECTION 3 YEARS AGO.
- [SDR LHO2013F00000](https://openairdocs.org/sdr/LHO2013F00000.md): Bellcrank · deformed · Mar 29, 2013 · N716SM · Cessna 441 · Nose/Tail Landing Gear
  > THE NOSE GEAR TRAPEZE (BELLCRANK) BECAME DEFORMED, PROBABLY FROM THE GEAR DOOR RETRACT RAMP DURING RETRACTION. THE NOSE UNSAFE LIGHT REMAINED ILLUMINATED AND EXTENTION WAS SELECTED. 3 GREENS AND DOWNLOCK WERE ACHIEVED AND AN UNEVENTFUL LANDING FOLLOWED. BOT
- [SDR POSA2013080900001](https://openairdocs.org/sdr/POSA2013080900001.md): Bracket · cracked · Mar 16, 2013 · N771XW · Cessna 441 · Landing Gear Doors
  > CRACK FOUND ON LT NLG DOOR FORWARD RETRACT BRACKET AT RETRACT ROD ATTACHING BOLT LOCATION. CRACK WAS FOUND DURING PRE-FLIGHT INSPECTION.
- [SDR 2013FA0000065](https://openairdocs.org/sdr/2013FA0000065.md): Pump · leaking · Jan 30, 2013 · N599AS · Cessna 441 · Hydraulic Pump (Electric/Engine), Main
  > PILOT NOTICED A "LOW HYDRAULIC FLOW" ANNUNICATOR LAMP WAS ILLUMINATED AND DEVERTED TO GET MX SERVICE. TECHS FOUND RT ENGINE DRIVEN HYD PUMP LEAKING, HYD FLUID AT A LOW RATE. THEY DID NOT KNOW HOW LONG THIS CONDITION EXISTED. R & R THE HYD PUMP AND SYS TESTED
- [SDR YN8R201301152013](https://openairdocs.org/sdr/YN8R201301152013.md): Lug · cracked · Jan 14, 2013 · N441LA · Cessna 441 · Fuselage Main, Attach Fittings
  > CRACK FOUND IN AFT RADIUS OF OTBD ACTUATOR LUG DURING EDDY CURRENT INSPECTION IAW PHASE 24 INSPECTION. PREVIOUSLY INSPECTED BY EDDY CURRENT 27.2 HOURS PRIOR.
- [SDR 2012FA0000771](https://openairdocs.org/sdr/2012FA0000771.md): Line · cracked · Nov 8, 2012 · N441BW · Cessna 441 · Hydraulic System, Main
  > PILOT NOTED HEAVY AMOUNTS OF HYD FLUID AROUND RT GEAR WELL AREA AND T/E OF RT INBD FLAP DURING HIS POST FLIGHT INSP. ACFT TECHS FOUND A HYDRAULIC LINE SPLIT IN A DRY BAY LOCATED JUST AFT OF RT ENG FIREWALL. HYD LINE APPEARED TO BE IN GOOD CONDITION WITH NO S
- [SDR 3SVAN441BD91912](https://openairdocs.org/sdr/3SVAN441BD91912.md): Engine · flamed out · Sep 18, 2012 · N441BD · Cessna 441 · Engine (Turbine/Turboprop)
  > RIGHT ENGINE FLAMED OUT ON CLIMBOUT OF ANC. PLIOT SECURED THE ENGINE AND RETURNED TO BASE.
- [SDR SIMA2012055010](https://openairdocs.org/sdr/SIMA2012055010.md): Light · inoperative · Feb 23, 2012 · N689AE · Cessna 441 · Emergency Lighting
  > DURING MAINTENANCE INSPECTION FOUND THE LT WING NR 2 OVERWING EMERGENCY LIGHT OUT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED LT WING NR 2 OVERWING EMERGENCY LIGHT ASSY IAW EMB AMM 33-50-10, OPERATIONAL CHECK GOOD. THE AIRCRAFT WAS RETURNED
- [SDR 3SVA20111228001](https://openairdocs.org/sdr/3SVA20111228001.md): Door Seal · collapsed · Dec 28, 2011 · N102NA · Cessna 441 · Doors
  > DURING CLIMBOUT AIRCRAFT WOULD NOT PRESSURIZE. RETURNED TO BASE.
- [SDR CA110629005](https://openairdocs.org/sdr/CA110629005.md): Bellcrank · cracked · Jun 24, 2011 · Cessna 441 · Landing Gear Door Retract Section
  > FOUND CRACK IN BELLCRANK DURING CORROSION INSPECTION, REPLACED BELLCRANK WITH NEW.
- [SDR YN8RSVC12620](https://openairdocs.org/sdr/YN8RSVC12620.md): Hinge Fitting · broken · Jun 8, 2011 · N711MB · Cessna 441 · Passenger/Crew Doors
  > UPON VISUAL INSPECTION, DURING POST FLIGHT, AFTER EXITING ACFT FOUND LOWER LT CABIN DOOR HINGE BROKEN. FURTHER INVESTIGATION FOUND RT LOWER DOOR HINGE CRACK FREE (EDDY CURRENT INSPECTION). THESE PARTICULAR HINGES ARE REQUIRED TO BE REPLACED IAW CQB98-09 WITHI

Next page: https://openairdocs.org/model/cessna-441/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE aircraft_model_key = '441'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/cessna-441/reports

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