# Service difficulty reports: Cessna 404

A list on [Cessna 404](https://openairdocs.org/model/cessna-404.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 53 reports

- [SDR 2024FA0000433](https://openairdocs.org/sdr/2024FA0000433.md): Engine · power loss · May 26, 2024 · N475R · Cessna 404 · Engine (Turbine/Turboprop)
  > ON DEPARTURE FROM KBFL, THE LEFT ENGINE LOST POWER SHORTLY AFTER TAKEOFF, THE ENGINE RETAINED PARTIAL POWER AND THE PROPELLER WAS NOT FEATHERED. THE PILOT IMMEDIATELY RETURNED TO KBFL. INSPECTION OF THE ENGINE REVEALED A LARGE HOLE THROUGH THE TOP OF BOTH HALV
- [SDR 2023FA0000115](https://openairdocs.org/sdr/2023FA0000115.md): Landing Gear · inoperative · Jan 27, 2023 · N97AQ · Cessna 404 · Landing Gear System
  > PILOT REPORTED RIGHT LANDING GEAR WOLD NOT EXTEND, WHEN SELECTED. THE EMERGENCY BLOW DOWN BOTTLE WAS ACTIVATED AND ALL GEARS CAME DOWN AND LOCKED.
- [SDR HTKA202001080000](https://openairdocs.org/sdr/HTKA202001080000.md): Engine · failed · Nov 14, 2019 · N502RA · Cessna 404 · Engine (Reciprocating)
  > ENGINE FAILED IN FLIGHT. NUMBER 1 CONNECTING ROD AND (CRANK END) PROTRUDING THROUGH TOP OF ENGINE CASE. RIGHT MAGNETO BROKEN OFF ITS MOUNT. THE ENGINE HAS BEEN IN SERVICE SINCE 05/2017. IT IS A FACTORY REBUILT ENGINE. THIS IS THE SECOND ENGINE IN OUR FLEE
- [SDR 2020FA0000006](https://openairdocs.org/sdr/2020FA0000006.md): Engine · malfunctioned · Oct 28, 2019 · N37127 · Cessna 404 · Engine (Reciprocating)
  > ENGINE DEVELOPED LOW OIL PRESSURE IN FLIGHT APPROX 20 PSI. REMOVED AND CLEANED OIL PRESSURE RELIEF PLUNGER. FOUND CARBON BITS IN OIL FROM CAVITY. ABOUT 20 HOURS LATER THE LOW OIL PRESSURE RETURNED. REMOVED OIL PRESSURE RELIEF PLUNGER. MORE CARBON BITS F
- [SDR HTKA2020010800001](https://openairdocs.org/sdr/HTKA2020010800001.md): Engine · failed · Aug 16, 2019 · N5409G · Cessna 404 · Engine (Reciprocating)
  > ENGINE FAILED IN FLIGHT. NR 5 AND NR 6 CONNECTING ROD (CRANK END) PROTRUDING THROUGH TOP OF ENGINE CASE. HOLES IN BOTH SIDES OF CASE BELOW NR 5 AND NR 6 CYLINDERS ABOVE OIL PAN FLANGE. THE ENGINE HAS BEEN IN SERVICE SINCE 07/2016. IT IS A FACTORY REBUILT E
- [SDR DUFA20190619001](https://openairdocs.org/sdr/DUFA20190619001.md): Case · cracked · Jun 15, 2019 · N103RC · Cessna 404 · Engine (Reciprocating)
  > WHILE ON A ONE MILE FINAL APPROACH, THE RIGHT HAND ENGINE DEVELOPED A SEVERE VIBRATION AND BEGAN TO LOSE POWER. THE AUXILIARY FUEL PUMP WAS SELECTED TO HIGH BUT THE LOSS OF POWER DID NOT IMPROVE. THE ENGINE WAS SHUTDOWN AND THE PROPELLER FEATHERED. THE APPROAC
- [SDR DUFA20170330001](https://openairdocs.org/sdr/DUFA20170330001.md): Line · failed · Mar 28, 2017 · N80BS · Cessna 404 · Hydraulic System, Main
  > DEPARTED, SELECTED GEAR UP AND SHORTLY AFTER BEGAN TO GET A PETROLEUM ODOR IN THE CABIN. IMMEDIATELY AFTER THAT THE LEFT HYD FLOW ANNUNCIATOR LIGHT ILLUMINATED, FOLLOWED BY THE RIGHT. ACTIVATED THE EMERGENCY LANDING GEAR EXTENSION BLOW DOWN SYSTEM AND MADE
- [SDR DUFA20140506002](https://openairdocs.org/sdr/DUFA20140506002.md): Hose · deteriorated · May 6, 2014 · N103RC · Cessna 404 · Engine Oil Distribution (Airframe Furnished)
  > WHILE IN CRUISE FLIGHT, THE PILOT NOTICED THE LT ENG OIL PRESS DROPPING. ONCE THE OIL PRESS DROPPED BELOW THE GREEN ARC, SHUT DOWN THE LT ENG & CONTACTED CTR. DIVERTED TO ALTERNATE AIRPORT, MADE AN UNEVENTFUL LANDING. THE OIL WAS BEING DUMPED OVERBOARD THRO
- [SDR BGJA2014042300002](https://openairdocs.org/sdr/BGJA2014042300002.md): Alternator · failed · Apr 3, 2014 · N550MA · Cessna 404 · DC Generator-Alternator
  > THE ACFT HAD TOTAL ELECTRICAL FAILURE DURING FLIGHT, DUE TO BOTH CHARGING SYSTEMS FAILING TOGETHER. RT ALTERNATOR FAILED DURING CRUISE, SHORTLY AFTER LT ALTERNATOR FAILED DUE TO A FAILED DRIVE CLUTCH. THE RT ALTERNATOR APPEARED TO HAVE AN INTERNAL SHORT THAT
- [SDR BGJA201404230001](https://openairdocs.org/sdr/BGJA201404230001.md): Clutch · failed · Apr 3, 2014 · N550M · Cessna 404 · Alternator-Generator Drive
  > DURING FLIGHT, THE LT ENGINE ALTERNATOR STOPPED PRODUCING POWER DUE TO THE DRIVE CLUTCH SLIPPING. AFTER LANDING, REMOVED ALTERNATOR AND CHECKED THE DRIVE CLUTCH. COULD TURN THE CLUTCH BY HAND WITH SOME FORCE. REPLACED THE CLUTCH, REGULATOR AND ALTERNATOR.
- [SDR KY7A20131204001](https://openairdocs.org/sdr/KY7A20131204001.md): Gasket · failed · Dec 4, 2013 · N404MG · Cessna 404 · Reciprocating Engine Oil System
  > PRIOR TO DEPARTURE FROM DEN, THE PILOT REPORTED THAT THE LT PNEUMATIC PUMP WAS INOPERATIVE. MX REPLACED THE PNEUMATIC PUMP & THE ACFT DEPARTED, CRUISING AT FL200. THE PILOT NOTED A DECREASE IN POWER & DECREASING OIL PRESS. THE PILOT SHUT DOWN & SECURED THE
- [SDR KY7A20120727002](https://openairdocs.org/sdr/KY7A20120727002.md): Oil System · low pressure · Jul 26, 2012 · N404MG · Cessna 404 · Reciprocating Engine Oil System
  > PILOT REPORTED THAT WHEN CONFIGURING THE ACFT FOR CRUISE FLIGHT THE LT ENGINE MANIFOLD PRESSURE DECREASED. PILOT NOTED THAT THE OIL PRESSURE WAS DECLINING AND SHUTDOWN THE ENGINE AS A PRECAUTIONARY MEASURE. OPEN
- [SDR KY7A12052501](https://openairdocs.org/sdr/KY7A12052501.md): Hinge · cracked · May 25, 2012 · N37127 · Cessna 404 · Landing Gear Doors
  > NLG FAILED TO EXTEND DURING NORMAL OPERATIONS DURING TRAINING FLIGHT. FLIGHT CREW PERFORMED EMERGENCY LANDING GEAR EXTENSION PROCEDURES; NOSE GEAR EXTENDED AND LOCKED. FLIGHT CREW PERFORMED NORMAL LANDING WITH NO FURTHER DIFFICULTY. MX PERSONNEL INSPECTED A
- [SDR CA120227001](https://openairdocs.org/sdr/CA120227001.md): Indication Sys · split · Feb 12, 2012 · Cessna 404 · Engine BMEP/Torque Indicating
  > (CAN) DURING SCHEDULED PRE-FLIGHT AUTO-FEATHER CHECKS, THE PILOTS REPORTED A TORQUE SPLIT OF 300 LB FT, NR 2 LAGGING. AFTER RETURNING TO THE RAMP, RETARDING & ADVANCING THE POWER LEVERS CLEARED THE DEFECT, BUT UPON SELECTING FEATHER THE NR 2 ENGINE FLAMED OUT
- [SDR 2010FA0000387](https://openairdocs.org/sdr/2010FA0000387.md): Bracket · broken · Apr 1, 2010 · N88719 · Cessna 404 · Elevator Miscellaneous Structure
  > (H12R) PREFLIGHT CONTROL CHECKED GOOD, THE ELEVATOR WAS HITTING THE CONTROL STOPS, ON TAKEOFF THE ACFT HAD PARTIAL ELEVATOR CONTROL, ON LANDING THE ACFT HAD PARTIAL ELEVATOR CONTROL, BEFORE FURTHER FLIGHTS THE CONTROLS WERE CHECKED, THE ELEVATOR BELLCRANK BRAC
- [SDR KY7A14756](https://openairdocs.org/sdr/KY7A14756.md): Control Cable · worn · Jul 6, 2009 · N404MG · Cessna 404 · Aileron Control System
  > ALL FOUR AILERON PRIMARY CONTROL CABLES FOUND WORN, SEVERING SEVERAL STRANDS AT WING STATION 50.021 WHERE IS PASSES IN FRONT OF THE OUTBOARD FLAP BELLCRANK. ONE CABLE HAD 3 OF THE 7 STRANDS SEVERED. CABLES WERE COVERED WITH GREASE AND GRIME MAKING IT DIFFICULT
- [SDR KY7A14634A](https://openairdocs.org/sdr/KY7A14634A.md): Line · fractured · Jun 5, 2009 · N37127 · Cessna 404 · Hydraulic System, Main
  > HYDRAULIC PRESSURE LINE FAILURE IN RIGHT WING LEADING EDGE BETWEEN FLOW VALVE AND FILTER HOUSING OCCURRED IN 90° BEND.
- [SDR KY7A14634](https://openairdocs.org/sdr/KY7A14634.md): Line · failed · Jun 5, 2009 · N37127 · Cessna 404 · Hydraulic System, Main
  > HYDRAULIC LINE FAILURE CAUSED TOTAL LOSS OF FLUID PREVENTING NORMAL GEAR EXTENSION. EMERGENCY BLOWDOWN FAILED DUE TO FAILURE OF PNEUMATIC LINE FAILURE AT BLOWDOWN BOTTLE.
- [SDR 2009FA0000483](https://openairdocs.org/sdr/2009FA0000483.md): Line · cracked · May 27, 2009 · N442EH · Cessna 404 · Hydraulic System, Main
  > HYDRAULIC FLUID DEPLETION HAVE OCCURRED. (TWO WERE FLAP FAILURE TO EXTEND AND ONE THE LANDING GEAR HAD TO BE EXTENDED USING THE EMERGENCY EXTENSION SYS. THESE FAILURES WERE CAUSED BY A CRACK AND LEAK FORMING IN A.3750 ALUM ALLOY HYDRAULIC LINE AT A BEND RAD
- [SDR GNB2009F00000](https://openairdocs.org/sdr/GNB2009F00000.md): Sleeve · cracked · May 26, 2009 · N5388J · Cessna 404 · Reciprocating Engine Cylinder Section
  > AFTER TAKEOFF, PILOT FELT ENGINE RUNNING ROUGH. ACFT RETURNED TO FIELD. MX DISCOVERED NR 2 CYLINDER UPPER DECK NOZZLE TUBE CRACKED. POSSIBLE WEAK WELD OF OUTSIDE TUBE. RECOMMENDED CLOSER ATTENTION TO LEANING ON LINES WHEN WASHING ON ENGINE AND INSPECTING A
- [SDR M7JA2009030200001](https://openairdocs.org/sdr/M7JA2009030200001.md): Engine · malfunctioned · Sep 13, 2008 · N404EN · Cessna 404 · Engine (Turbine/Turboprop)
  > IN CRUISE FLIGHT THE CAPTAIN NOTICE A DROP IN THE RT ENGINE OIL PRESSURE WITH INCREASE IN OIL TEMP. THERE WAS NOT VIBRATION OR VISIBLE OIL LEAKS ON THE MENTION ENGINE. THE PILOT FOLLOWED THE PROPER CHECKLIST EXECUTING A PRECAUTIONARY ENGINE SHUTDOWN. THE FL
- [SDR DUFA20070002](https://openairdocs.org/sdr/DUFA20070002.md): Stud · sheared · Apr 10, 2007 · N80BS · Cessna 404 · Reciprocating Engine Cylinder Section
  > WHILE ON APPROACH TO AIRPORT, THE PILOT NOTICED MANIFOLD PRESSURE DROPPING AS WELL AS OIL PRESSURE FROM THE RIGHT ENGINE. HE ALSO BEGAN TO FEEL A VIBRATION FROM THE SAME ENGINE. HE ELECTED TO SHUT THE ENGINE DOWN AND MADE AN UNEVENTFUL LANDING. UPON INSPECTION
- [SDR DUFA041007001](https://openairdocs.org/sdr/DUFA041007001.md): Stud · sheared · Apr 10, 2007 · N80BS · Cessna 404 · Reciprocating Engine Cylinder Section
  > WHILE ON APPROACH TO AIRPORT, THE PILOT NOTICED MANIFOLD PRESSURE DROPPING AS WELL AS OIL PRESSURE FROM THE RT ENGINE. HE ALSO BEGAN TO FEEL A VIBRATION FROM THE SAME ENGINE. HE ELECTED TO SHUT THE ENGINE DOWN AND MADE AN UNEVENTFUL LANDING. UPON INSPECTION, T
- [SDR 2007FA0000226](https://openairdocs.org/sdr/2007FA0000226.md): Engine · failed · Feb 20, 2007 · N442EH · Cessna 404 · Engine (Reciprocating)
  > THIS ENGINE FAILED TO THE TERMINOLOGY OF CATASTROPHIC AT THE NR 1 AND NR 2 CYLINDER CONNECTING ROD LOCATIONS DURING A MAINTENANCE TEST FLIGHT WITHIN TEN MINUTES INTO THAT FLIGHT WITH A MECHANIC ON BOARD MONITORING THE ENGINE INSTRUMENTS. THE OIL PRESSURE SUDD
- [SDR BAC001](https://openairdocs.org/sdr/BAC001.md): Line · disconnected · Aug 2, 2006 · N80BS · Cessna 404 · Engine Fuel Distribution
  > PILOT REPORTED THAT WHILE IN CRUISE FLIGHT THE LEFT ENGINE FUEL FLOW SUDDENLY DROPPED OFF AND THE ENGINE BEGAN TO RUN ROUGH AND LOSE POWER. THE BOOST PUMP WAS SELECTED TO HIGH AND THE MIXTURE INCREASED TO FULL RICH WHICH HAD LITTLE EFFECT. THE PILOT CONTACTE
- [SDR BAC005](https://openairdocs.org/sdr/BAC005.md): Tube · disconnected · Aug 2, 2006 · N80BS · Cessna 404 · Fuel Pressure Indicator
  > PILOT REPORTED THAT WHILE IN CRUISE FLIGHT THE LT ENGINE FUEL FLOW SUDDENLY DROPPED OFF AND THE ENGINE BEGAN TO RUN ROUGH AND LOSE POWER. THE BOOST PUMP WAS SELECTED TO HIGH AND MIXTURE INCREASED TO FULL RICH WHICH HAD LITTLE EFFECT. THE PILOT CONTACTED DISPAT
- [SDR BGJ2006F00000](https://openairdocs.org/sdr/BGJ2006F00000.md): Cylinder · cracked · Jan 6, 2006 · N155TT · Cessna 404 · Reciprocating Engine Cylinder Section
  > THE AIRCRAFT WAS IN CRUISE POWER CONFIGURATION. NR 5 CYLINDER BARREL ON RT ENGINE CRACKED AND SEPARATED APPROXIMATELY 3 INCHES FROM MOUNTING BASE IN THE BARREL AREA. DAMAGE WAS DONE TO THE PISTON AND CONNECTING ROD AT THE TIME OF SEPARATION. CAUSE IS UNKNOW
- [SDR AU510002176](https://openairdocs.org/sdr/AU510002176.md): Connector · faulty · Dec 12, 2005 · Cessna 404 · Landing Gear System Wiring
  > (AUS) RT MAIN LANDING GEAR DOWN MICROSWITCH WIRE CONNECTOR FAULTY. SUSPECT CONNECTOR WAS NOT AN APPROVED ITEM. (OTHER CAUSE: MAINTENANCE CONTROL ISSUE) (CASA NR 510002176)
- [SDR AU510001970](https://openairdocs.org/sdr/AU510001970.md): Hub · corroded · Dec 12, 2005 · Cessna 404 · Propeller Hub Section
  > PROPELLER HUB CORRODED BEYOND LIMITS IN BLADE SOCKET AREA.
- [SDR AU510001816](https://openairdocs.org/sdr/AU510001816.md): Stud · broken · Dec 12, 2005 · Cessna 404 · Reciprocating Engine Power Section
  > RT ENGINE NR 5 CYLINDER HOLD-DOWN STUDS (2OFF) BROKEN OFF FLUSH WITH THE CYLINDER BASE.
- [SDR AU510001799](https://openairdocs.org/sdr/AU510001799.md): Switch · unserviceable · Dec 12, 2005 · Cessna 404 · Landing Gear Position and Warning
  > (AUS) RT MAIN LANDING GEAR UPLOCK MICROSWITCH FAILED. SWITCH HAD ONLY 54.5 HOURS OPERATION SINCE REPLACEMENT. (CASA NR 510001799)
- [SDR AU510001730](https://openairdocs.org/sdr/AU510001730.md): Bearing · collapsed · Dec 12, 2005 · Cessna 404 · DC Generator-Alternator
  > RT ENG DRIVEN ALT FAILED. ALT DRIVE COUPLING SHEARED AND ALT FRONT BEARING COLLAPSED. RED ELASTOMER MAT`L FROM ALT DRIVE COUPLING AND MINOR METALLIC PARTICLES VISIBLE INTERNALLY THRU ALT ATTACHMENT PORT. ALT DISASSEMBLED AND INSPECTED. FRONT BEARING SERIOU
- [SDR AU510001695](https://openairdocs.org/sdr/AU510001695.md): Bearing · damaged · Dec 12, 2005 · Cessna 404 · Reciprocating Engine Power Section
  > ENGINE METAL CONTAMINATION. BULK STRIP FOUND THAT THE TWO REARMOST MAIN BEARINGS WERE DAMAGED. INSPECTION OF THE CRANKSHAFT IN THE VICINITY OF THE TWO REARMOST JOURNALS FOUND CRACKS RUNNING LONGITUDINALLY ACROSS JOURNALS TO THE CRANK.
- [SDR AU510001619](https://openairdocs.org/sdr/AU510001619.md): Heater · faulty · Dec 12, 2005 · Cessna 404 · Heating System
  > (AUS) CABIN HEATER FAULTY. SMOKE IN CABIN. INVESTIGATION FOUND THE FORWARD VENT BLOWER INOPERATIVE DUE MOTOR BRUSH HANGUP. INSPECTION OF THE HEATER FOUND DISCOLORATION ON THE HEATER OUTER SHROUD. INTERNAL INSPECTION FOUND THE PAINT ON THE INSIDE OF THE HEATER
- [SDR AU510001530](https://openairdocs.org/sdr/AU510001530.md): Uplock Switch · failed · Dec 12, 2005 · Cessna 404 · Landing Gear Position and Warning
  > LT MAIN LANDING GEAR UPLOCK MICROSWITCH FAULTY.
- [SDR AU510001489](https://openairdocs.org/sdr/AU510001489.md): Bearing · failed · Dec 12, 2005 · Cessna 404 · Reciprocating Engine Power Section
  > (AUS) ENGINE METAL CONTAMINATION. WORKSHOP STRIP AND INVESTIGATION FOUND NR 2 AND NR 3 MAIN BEARINGS FAILED. BEARING SHELLS BROKE UP CAUSING DAMAGE TO CRANKCASE AND SEVERE DAMAGE TO CRANKSHAFT WITH CRACKING ON JOURNALS. (CASA NR 510001489)
- [SDR AU510001447](https://openairdocs.org/sdr/AU510001447.md): Bolt · broken · Dec 12, 2005 · Cessna 404 · Reciprocating Engine Power Section
  > (AUS) ENGINE INTERNAL DAMAGE. SUSPECT CAUSED BY FAILURE OF NR 5 CONNECTING ROD BOLT OR CONNECTING ROD. INVESTIGATION CONTINUING.
- [SDR AU510001529](https://openairdocs.org/sdr/AU510001529.md): Uplock Switch · damaged · Sep 6, 2005 · Cessna 404 · Landing Gear Position and Warning
  > LT MAIN LANDING GEAR MICROSWITCH DAMAGED INTERNALLY.
- [SDR AU510002082](https://openairdocs.org/sdr/AU510002082.md): Circuit Card · failed · Aug 11, 2005 · Cessna 404 · Global Positioning System
  > GPS DATA CARD FAILED.
- [SDR 2005FA0000621](https://openairdocs.org/sdr/2005FA0000621.md): Control Cable · damaged · Apr 11, 2005 · N5388J · Cessna 404 · Elevator Control System
  > DURING INSPECTION, FOUND CABLE TO BE BLENDED AT FAIRLEAD APPROX 6 INCHES FROM AFT END OF CABLE. PROBABLE CAUSE FROM NEW STYLE (STAINLESS STEEL) CABLE. NEW STYLE LASTED ONLY FRACTION OF TIME AS OLD STYLE. (SW01200504154) (K)
- [SDR AU510001856](https://openairdocs.org/sdr/AU510001856.md): Switch · failed · Mar 6, 2005 · Cessna 404 · Engine Cranking
  > LT ENGINE STARTER SWITCH FAILED. SWITCH REMAINED ENGAGED.
- [SDR GNB2005F00003](https://openairdocs.org/sdr/GNB2005F00003.md): Line · corroded · Jan 11, 2005 · N54ZP · Cessna 404 · Hydraulic System, Main
  > FAILED HYDRAULIC PRESSURE CHECK. LINE LAYING ON DUCTING FOR HEATING CAUSING CORROSION TO FORM. (SW01200502894) (K)
- [SDR 2004F00429](https://openairdocs.org/sdr/2004F00429.md): Sensor · burned out · Nov 29, 2004 · N80BS · Cessna 404 · DC Generator-Alternator
  > WHILE IN CRUISE FLIGHT, THE PILOT NOTICED SPARKS COMING FROM THE LEFT ENGINE FORWARD COWL AREA. AS A PRECAUTION, THE ENGINE WAS SHUTDOWN AND SECURED. THE AIRCRAFT THEN MADE AN UNEVENTFUL LANDING. UPON INVESTIGATION, IT WAS DISCOVERED THAT THE ALTERNATOR OUT
- [SDR 2004FA0000839](https://openairdocs.org/sdr/2004FA0000839.md): Spar Cap · corroded · Oct 14, 2004 · N677MF · Cessna 404 · Wing Spar
  > DURING OUR INITIAL INSPECTION OF THIS AIRCRAFT, DISCOVERED SEVERE INTERGRANULAR CORROSION ON UPPER AND LOWER REAR SPAR CAPS. THE AREA OF CORROSION IS LOCATED INSIDE THE MAIN GEAR WELL ON BOTH LEFT AND RT WINGS. NOTE: THIS AIRCRAFT IS OPERATED IN A SALT AIR
- [SDR 2004FA0000838](https://openairdocs.org/sdr/2004FA0000838.md): Spar Cap · corroded · Oct 14, 2004 · N677MF · Cessna 404 · Wing Spar
  > DURING OUR INITIAL INSPECTION OF THIS AIRCRAFT, DISCOVERED SEVERE INTERGARNULAR CORROSION ON UPPER AND LOWER REAR SPAR CAPS. THE AREA OF CORROSION IS LOCATED INSIDE THE MAIN GEAR WELL ON BOTH LEFT AND RIGHT WINGS. NOTE: AIRCRAFT IS OPERATED IN A SALT AIR EN
- [SDR EAT2003F00000](https://openairdocs.org/sdr/EAT2003F00000.md): Spar · damaged · Feb 1, 2003 · N167SA · Cessna 404 · Nacelle/Pylon, Main Frame
  > DURING A REPAIR FOR A EXHAUST BRACKET AND LOWER SKIN REPAIRS ON THE LEFT ENGINE NACELLE HEAT DAMAGE WAS FOUND ON THE LFET FORWARD SPAR BETWEEN WING STA CWS88-10555555. THIS DAMAGE IS MOST LIKELY DUE TO A CRACKED EXHAUST OUTLET OFF THE TURBO DIRECTING HOT EXHA
- [SDR J7H2002F00000](https://openairdocs.org/sdr/J7H2002F00000.md): Crankcase · cracked · Sep 1, 2002 · Cessna 404 · Reciprocating Engine Power Section
  > THREE FACTORY NEW ENGINE CRANK CASE CRACKED JUST OVER ONE THOUSAND HOURS OF OPERATIONS, DURING NORMAL OPERATIONS. THE LAST ENGINE CRANK CASE CRACKED AT 1034 AND PRIOR 1038 AND 1032 HOURS, WHICH APPEARS TO BE A TREND.
- [SDR GNB2002F00001](https://openairdocs.org/sdr/GNB2002F00001.md): Control Cable · damaged · May 30, 2002 · N165SA · Cessna 404 · Rudder Control System
  > DURING FUSELAGE INSPECTION FORWARD LEFT RUDDER CABLE BLENDED WERE THE CABLE WEST THRU A RIB WHICH HAD A FANALIC BLOCK ON RIB FOR ANTI-CHAFE PROTECTION.
- [SDR 2001FA0000062](https://openairdocs.org/sdr/2001FA0000062.md): Control Cable · inoperative · Jun 11, 2001 · N165SA · Cessna 404 · Aileron Control System
  > LEFT HAND AFT AILERON CABLE. PN 5815103-26CR ( BLENDED)
- [SDR 2001FA0000061](https://openairdocs.org/sdr/2001FA0000061.md): Link · bent · Jun 11, 2001 · N165SA · Cessna 404 · Main Landing Gear
  > LINK ASSEMBLY DRAG. PN 0842122-19

Next page: https://openairdocs.org/model/cessna-404/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 = '404'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/cessna-404/reports

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