# Service difficulty reports: Convair 440

A list on [Convair 440](https://openairdocs.org/model/convair-440.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 5 · 206 reports

- [SDR VGCA20210606002](https://openairdocs.org/sdr/VGCA20210606002.md): Skin · gouged · Jun 6, 2021 · N171FL · Cvac 440 · Wing, Plate/Skin
  > GOUGE/DENT IN RIGHT WING LOWER SURFACE SKIN BEWTEEN WS 3 AND WS 4. PERFORMED REPAIR PER ENGINEERING REPAIR DRAWING.
- [SDR VGCA20210606001](https://openairdocs.org/sdr/VGCA20210606001.md): Spar · corroded · Jun 6, 2021 · N171FL · Cvac 440 · Wing Spar
  > RH WING REAR SPAR UPPER RAIL CORRODED NEAR WS 2 AND WS 3. PERFORMED BLENDOUT IN THIS LOCATION PER ENGINEERING REPAIR
- [SDR VGCA20201125001](https://openairdocs.org/sdr/VGCA20201125001.md): Fire Loop · shorted · Nov 25, 2020 · N181FL · Cvac 440 · Smoke Detection
  > ZONE 3 (WHEEL WELL) FIRE WARNING ON NR 2 ILLUMINATED AFTER TAKE OFF. SHUT DOWN NR 2 ENGINE, DISCHARGED PRIMARY FIRE BOTTLES AND RETURNED TO KMIA.
- [SDR VGCA20191108001](https://openairdocs.org/sdr/VGCA20191108001.md): Hinge · cracked · Nov 8, 2019 · N181FL · Cvac 440 · Fuselage, Door Hinge
  > WHILE PERFORMING TASK CARD SSD 52-3-3 "2 YEAR REPEAT" INSPECTION DISCOVERED HINGE NODE WAS CRACKED. LOCATION OF NODE DAMAGE GROUP F NODE L. REPAIRED IAW DRAWING R387-052-001-001.
- [SDR CA190604026](https://openairdocs.org/sdr/CA190604026.md): Clamp · damaged · Jun 2, 2019 · Cvac 440 · Engine Collector/Tailpipe/Nozzle
  > (CAN) #1 ENGINE ZONE 1 FIRE INDICATION SHORTLY AFTER TAKEOFF. FIRE INDICATION CEASED FOLLOWING REDUCTION IN POWER. LOAD ABORTED AND #1 ENGINE EMERGENCY HANDLE ACTIVATED. #1 ENGINE TAILPIPE CLAMP P/N 4215AF18.92 FOUND BROKEN, CAUSING TAILPIPE SEPARATION. #1 ENG
- [SDR CA190527025](https://openairdocs.org/sdr/CA190527025.md): Starter · malfunctioned · May 23, 2019 · Cvac 440 · Engine Starter
  > (CAN) #1 STARTER OVERSPEED LIGHT ILLUMINATED IN FLIGHT, TRIGGERING MASTER CAUTION LIGHT. #1 STARTER OVERSPEED LIGHT REMAINED ILLUMINATED ON THE GROUND WITH #1 ENGINE STOPPED. #1 STARTER FAILED TO ENGAGE ON SUBSEQUENT START ATTEMPT. #1 STARTER REPLACED, STARTER
- [SDR CA190508004](https://openairdocs.org/sdr/CA190508004.md): Bushing · loose · Mar 5, 2019 · Cvac 440 · Landing Gear Retraction/Extension System
  > (CAN) RH MLG WOULD NOT LATCH UP AFTER TAKE-OFF, BUSHING FOUND LOOSE ON EMERGENCY UPLATCH CYLINDER, PREVENTING UPLATCH FROM FULLY RETRACTING. CYLINDER REPLACED, FUNCTION NORMAL. (TC# 20190508004)
- [SDR VGCA20160404001](https://openairdocs.org/sdr/VGCA20160404001.md): Release Cable · broken · Apr 4, 2016 · N181FL · Cvac 440 · Landing Gear Retraction/Extension System
  > LEFT MAIN GEAR FAILED TO EXTEND NORMALLY. EMER RELEASE WORKED NORMAL.
- [SDR CA150619008](https://openairdocs.org/sdr/CA150619008.md): Flange · cracked · Jun 17, 2015 · Cvac 440 · Landing Gear Brake System
  > (CAN) MAIN GEAR SENT TO SHOP FOR REPAIR. CRACKS ON BOTH LT & RT IB BRAKE FLANGES VISUALLY INDICATED. CRACKS (2) CONFIRMED USING MAGNETIC PARTICLE INSPECT METHOD.
- [SDR CA150610007](https://openairdocs.org/sdr/CA150610007.md): Yoke · sheared · Jun 9, 2015 · Cvac 440 · Cargo/Baggage Doors
  > (CAN) C1 DOOR AFT YOKE SHEARED DURING FLIGHT AT FL220, RAPID DECOMPRESSION & EMER DESCENT. NO INJURIES.
- [SDR CA140910006](https://openairdocs.org/sdr/CA140910006.md): Bearing · unserviceable · Aug 22, 2014 · Cvac 440 · Turbine Section
  > (CAN) NUMBER 2 ENGINE RGB OIL PRESSURE INDICATION STARTED TO FLUCUATE, FOLLOWED SHORTLY BY, OIL PRESSURE LOW, WARNING LIGHT ILLUMINATING. SHORTLY THERE AFTER THE NR 2 OIL QUANTITY GAUGE WENT TO ZERO. NR 2 ENGINE WAS SHUTDOWN AND DIVERSION MADE TO NEAREST AIR
- [SDR CA140714018](https://openairdocs.org/sdr/CA140714018.md): Adapter · leaking · Jul 13, 2014 · Cvac 440 · Phase Adapter
  > (CAN) THE AIRCRAFT RETURNED TO BASE AFTER COMPLETING THEIR MISSION AND THE PILOT REPORTED A SMOKY ODOR IN THE COCKPIT. IT WAS NOT AN ELECTRIC BURNING ODOR. THE ODOR WAS TRACKED DOWN TO BE COMING FROM THE HR 2 AC PHASE ADAPTOR. THERE WAS A YELLOW FLUID COMING
- [SDR VGCA20140430001](https://openairdocs.org/sdr/VGCA20140430001.md): Angle · cracked · Apr 30, 2014 · N171FL · Cvac 440 · Fuselage Miscellaneous Structure
  > RIGHT HAND BEAM UPPER CORD ANGLE CRACKED IN RADIUS.
- [SDR CA130827003](https://openairdocs.org/sdr/CA130827003.md): Oil System · leaking · Aug 16, 2013 · Cvac 440 · Turbine Engine Oil System
  > (CAN) NR 2 ENGINE EMITTING OIL FROM BEARING AREA.
- [SDR 2013FA0000487](https://openairdocs.org/sdr/2013FA0000487.md): Engine · rough · Aug 2, 2013 · N24DR · Cvac 440 · Engine (Reciprocating)
  > IN FLIGHT PRECAUTIONARY ENGINE SHUTDOWN. ENGINE ROUGHNESS, CAUSE TO BE DETERMINED 8/2/2013.
- [SDR CA130425001](https://openairdocs.org/sdr/CA130425001.md): Fitting · broken · Apr 24, 2013 · Cvac 440 · Landing Gear Actuator
  > (CAN) MECHANIC FOUND BROKEN LT MLG ACTUATOR FITTING ON WALKAROUND, SERVICE CHECK.
- [SDR CA121224001](https://openairdocs.org/sdr/CA121224001.md): Gearbox · failed · Dec 21, 2012 · Cvac 440 · Turbine Engine Reduction Gear
  > (CAN) AT APPROXIMATELY 60 MILES EAST OF AIRPORT, ACFT OPERATING AS NRL950 ON A IFR FLIGHT, REPORTED LOSS OF AN ENGINE AND DECLARED AN EMERGENCY. ARFF RESPONDED AND ACFT LANDED WITHOUT INCIDENT AT 1949Z. SUSPECTED ENGINE GEAR BOX FAILURE, SHOP REPORT TO FOLL
- [SDR CA120822010](https://openairdocs.org/sdr/CA120822010.md): Clamp · broken · Aug 19, 2012 · Cvac 440 · Engine Collector/Tailpipe/Nozzle
  > (CAN) ON CLIMBOUT, THE CREW HAD A ZONE 1 FIRE INDICATION, THEY THROTTLED BACK AND INDICATION LIGHT WENT OUT. THEY E-HANDLED THE ENGINE, JETTISONED THE LOAD AND RETURNED TO THE AIRPORT. A BROKEN EXHAUST CLAMP WAS FOUND AT THE FWD END OF THE AFT LONG PORTION
- [SDR CA120813031](https://openairdocs.org/sdr/CA120813031.md): Fcu · malfunctioned · Aug 5, 2012 · Cvac 440 · Fuel Control/Turbine Engines
  > (CAN) WITH ENGINES RUNNING ON GRID IN HIGH PILOT DOWN SHIFTED TO LOW. NR 1 ENGINE EXPERIENCED A LEAN FUEL BLOW OUT. THIS OCCURED TWICE. FCU REPLACED FUNCTION CHECKED. PROBLEM GONE.
- [SDR CA120706006](https://openairdocs.org/sdr/CA120706006.md): Solenoid · shorted · Jul 4, 2012 · Cvac 440 · Propeller Controlling System
  > (CAN) RIGHT PROPELLER SOLENOID CIRCUIT BREAKER TRIPPED. RESET BREAKER RT PROPELLER SOLENOID SHORT INTERNALLY WAS REPLACED ABOUT 30 FLIGHT HRS AGO.
- [SDR CA120517001](https://openairdocs.org/sdr/CA120517001.md): Valve · faulted · Apr 24, 2012 · Cvac 440 · Propeller Controlling System
  > (CAN) THE AIRCRAFT TAKEOFF, LT PROPELLER ENCOUNTERED AN UNDERSPEED SITUATION. THE ACFT RETURNED TO DEPARTURE. THE AME TROUBLESHOT THE PROBLEM, WE FOUND THE PITCH LOCK VALVE AT FAULT. THE PITCH LOCK VALVE, PN 6506196 WAS REPLACED AND THE ACFT RETURNED TO SERV
- [SDR CA110915002](https://openairdocs.org/sdr/CA110915002.md): Bearing · faulty · Sep 7, 2011 · Cvac 440 · Turbine Engine Compressor Section
  > (CAN) ON A RUNNING TEST RUN ENGINE NR 1 LOST HP AND TIT STARTED TO RAPIDLY CLIMB, PILOT E-HANDLE, LANDED WITH NR 1 ENGINE FEATHERED. ON GROUND INSPECTION, THE COMPRESSOR BLADES WERE RUBBING AGAINST THE CASE. SUSPECT FAULTY BEARING.
- [SDR CA110624002](https://openairdocs.org/sdr/CA110624002.md): Line · leaking · Jun 19, 2011 · Cvac 440 · Hydraulic System, Main
  > LEAKING HYD FLUID AT BULKHEAD FITTING. TUBE WAS EITHER CRACKED OR THE FLARE WAS BAD.
- [SDR 2011FA0000277](https://openairdocs.org/sdr/2011FA0000277.md): Downlock Switch · defective · Mar 7, 2011 · N24DR · Cvac 440 · Landing Gear Position and Warning
  > UPON LANDING GEAR DEPLOYMENT ON LANDING AT AIRPORT, NO GEAR SAFE LIGHT OBSERVED FOR NLG. INSP REVEALED DEFECTIVE MICRO SWITCH ON NLG DOWN LOCK. THIS SYS IS FUNCTION TESTED ON PERIODIC INSP.
- [SDR VGCA201100002](https://openairdocs.org/sdr/VGCA201100002.md): Angle · cracked · Feb 24, 2011 · N361FL · Cvac 440 · Fuselage Miscellaneous Structure
  > DURING PHASE INSPECTION FOUND CRACKED ANGLE IN NOSE LANDING GEAR WELL.
- [SDR RDS121112SDR](https://openairdocs.org/sdr/RDS121112SDR.md): Pitot Tube · failed · Feb 23, 2011 · N587CA · Cvac 440 · Pitot/Static System
  > NR 2 PITOT SWITCH TRIPPED IN-FLIGHT, PULLED CIRCUIT BREAKER AS PRECAUTION, SMELLED "ELECTRICAL" ODOR PRIOR TO PITOT TRIPPING. NR 2 PITOT SYS CHECK. ALL ELECTRICAL CONNECTIONS AND BREAKER, NO "ELECTRICAL" ODOR. ALL IAW MM 34-11-1, PAGE 200-(3).
- [SDR CA110215001](https://openairdocs.org/sdr/CA110215001.md): Gearbox · failed · Feb 11, 2011 · Cvac 440 · Turbine Engine Reduction Gear
  > DURING APPROACH, ALL PRE DESCENT CHECKS COMPLETED, AT FL230 NR 2 GEARBOX PRESSURE FALL RAPIDLY AND ANNUNCIATOR LOW PRESSURE LIGHT CAME ON, EXPERIENCE DROP IN HP AND HIGHER THAN NORMAL TIT. A PRECAUTIONARY SHUTDOWN CHECKLIST COMPLETED, PROPELLER FEATHERED ATC
- [SDR MV1R336K11024](https://openairdocs.org/sdr/MV1R336K11024.md): Circuit Breaker · failed · Jan 24, 2011 · N39 · Cvac 440 · Hydraulic Power System Wiring
  > ON START UP, THE FLIGHT CREW APPLIED AC POWER TO ACFT AND TURNED AC HYD PUMP SWITCH ON. A SMALL FLASH, THEN SMOKE EMITTED AT THE CIRCUIT BREAKER. THE FORWARD FACE DISINTEGRATED INTO FRAGMENTS.
- [SDR CA101129006](https://openairdocs.org/sdr/CA101129006.md): Arm · damaged · Nov 25, 2010 · Cvac 440 · Landing Gear Retraction/Extension System
  > DURING CLIMB-OUT FROM AIRPORT, THE PILOT REPORTED THAT THE GEAR UNLOCK LIGHT WAS ON AND SUSPECTED THE NLG AT FAULT. THEY COULD SEE DAYLIGHT THROUGH OUT THE VIEWING WINDOW WITH THE RED DOWNLOCK MARKS. AFTER A FEW GEAR UP AND DOWN SELECTIONS WITH NO SUCCESS, T
- [SDR RDS121107](https://openairdocs.org/sdr/RDS121107.md): Relay · failed · Aug 3, 2010 · N587CA · Cvac 440 · Fire Detection
  > NR1 ENGINE FIRE LIGHT CAME ON INTERMITTENTLY DURING TURBULENCE AND ROUGH PAVEMENT. R & R FIRE DETECTOR BOX PN 33958-3, SN OFF 3654, ON 829 TEST OK. TEST IAW CH 20-1-PAGE 1-20.1-2-3 CV 440 MM. "NOTE" TAPPING ON FIRE DETECTOR PANEL COVER SIMULATED THE LIGHT C
- [SDR CA100804022](https://openairdocs.org/sdr/CA100804022.md): Brake Assy · unserviceable · Jul 31, 2010 · Cvac 440 · Brake
  > NR 2 BRAKE ASSY MISSING BRAKE PADS, FOUND WHEN COMPLETING POST FLIGHT BRAKE ASSY. DISC AND WHEEL ASSY REPLACED SERVICEABLE.
- [SDR CA100608007](https://openairdocs.org/sdr/CA100608007.md): Warning Light · illuminated · May 31, 2010 · Cvac 440 · Landing Gear Position and Warning
  > (CAN) AIRCRAFT WAS ON A BOMB RUN AND AFTER DROPPING ITS RETARDANT LOAD, THE PILOT NOTICED THE GEAR UNLOCK LIGHT WAS ON. PILOTS SELECT HYD SELECTOR FROM BYPASS TO PRESS MODE, LIGHT EXTINGUISHED. UPON ARRIVAL PILOT TRIED TO DUPLICATE THE PROBLEM AND SELECT HYD
- [SDR CA100521007](https://openairdocs.org/sdr/CA100521007.md): Bolt · broken · May 18, 2010 · Cvac 440 · Engine Collector/Tailpipe/Nozzle
  > T-BOLT ON THE EXHAUST CLAMP BROKE ALLOWING THE CLAMP TO COME FREE, THE ALLOWING THE EXHAUST DUCT TO SEPARATE, LEADING TO THE ENGINE TO BE SHUTDOWN.
- [SDR RDS121092](https://openairdocs.org/sdr/RDS121092.md): Pcu · failed · Jan 27, 2010 · N587CA · Cvac 440 · Propeller Controlling System
  > ON 6/18/09, WHILE TAXIING FOR TAKEOFF, OBSERVED SMOKE COMING FROM THE RT ENGINE, THE ENGINE WAS SHUTDOWN AND SECURED. THE PROPELLER MOVED OUT OF "FINE" PITCH POSITION CAUSING THE ENGINE TO OVERHEAT. THE CAUSE OF PROPELLER MOVEMENT WAS THE INTERNAL FAILURE OF
- [SDR CA090928002](https://openairdocs.org/sdr/CA090928002.md): Gear · damaged · Sep 21, 2009 · Cvac 440 · Turbine Engine Reduction Gear
  > (CAN) ON SEPT 21, 2009 DURING CRUISE ALTITUDE OF 22,000 FT AT APPROX 13:45 ZULU. PILOT IN COMMAND (PIC) NOTICED RAPID DECREASE IN OIL PRESSURE FOLLOWED BY A DECREASE IN RPM AND HIGH PRESSURE ON NR 2 (RT) ENG. WITH THIS INDICATION THEY PROCEEDED TO PRECAUTION
- [SDR CA091130001](https://openairdocs.org/sdr/CA091130001.md): Regulator · malfunctioned · Aug 20, 2009 · Cvac 440 · Propeller Controlling System
  > (CAN) DURING CRUISE AT FL200 RT PROPELLER OVERSPEED WITHOUT DECOUPLING, ENGINE SHUTDOWN, PROPELLER FEATHERED AND LANDED AT CLEVELAND USA. PROPELLER REGULATOR REPLACED DUE INTERNAL FAILURE AND AIRCRAFT RETURNED TO SERVICE REF. AIRCRAFT LOG BOX PAGE 10872 DEFE
- [SDR CA090807009](https://openairdocs.org/sdr/CA090807009.md): Engine · disconnected · Aug 2, 2009 · Cvac 440 · Engine (Turbine/Turboprop)
  > BANG FOLLOWED BY METALIC GRINDING NOISE AS REPORTED BY PILOT. GEAR BOX OIL PRESS FUNCTUATION NOTICED (NR 1 ENG) AND ZERO HORSEPOWER REGARDLESS OF POWER LEVER POSITION, ENGINE STILL RUNNING. ENGINE FOUND TO BE DECOUPLED UPON GROUND INSP.
- [SDR CA090713004](https://openairdocs.org/sdr/CA090713004.md): Engine · overtemp · Jul 9, 2009 · Cvac 440 · Engine (Turbine/Turboprop)
  > (CAN) AS ACFT APPROACHED FIRE TO DROP LOAD, ENG NR 1 SURGE WAS NOTICED, FOLLOWED BY OVER TEMP CONDITION, POWER LEVER WAS RETARDED. AS ACFT PASSED THROUGH SMOKE ENGINE OPS RETURNED TO NORMAL. ENG PRECAUTIONARY SHUTDOWN WAS DONE DUE TO OVER TEMP.
- [SDR JRA2009F00001](https://openairdocs.org/sdr/JRA2009F00001.md): Engine · overtemp · Jun 18, 2009 · N587CA · Cvac 440 · Engine (Turbine/Turboprop)
  > WHILE TAXIING FOR TAKEOFF, OBSERVED SMOKE COMING FROM THE RT ENGINE, ENGINE WAS SHUTDOWN AND SECURED. THE PROPELLER MOVED OUT OF "FINE" PITCH POSITION CAUSING THE ENGINE TO OVERHEAT, CAUSE OF PROPELLER MOVEMENT AT THIS TIME UNKNOWN. THE ENGINE NEEDS TO BE RE
- [SDR CA090623002](https://openairdocs.org/sdr/CA090623002.md): Lever · sticking · Jun 17, 2009 · Cvac 440 · Landing Gear Selector
  > (CAN) ON FLIGHT, DURING APPROACH AT FLIGHT LEVEL 2000 NO GREEN LIGHTS (3) ON GEAR DOWN ACTION AND NO GEAR UNSAFE INDICATION. 3 GEARS WERE DOWN AND 3 GREEN LIGHTS NOT ILLUMINATED, CHECK SUPPLEMENT COMPLETED AND GEARS (3) CONFIRMED DOWN VISUALLY, NO FLAPS AND N
- [SDR CA090506013](https://openairdocs.org/sdr/CA090506013.md): Pin · sheared · May 4, 2009 · Cvac 440 · Rudder Control System
  > (CAN) DURING ROUTINE INSP IT WAS NOTED THAT THE RUDDER GUST LOCK WAS INOPERATIVE. THE GUST LOCK PIN WAS FOUND SHEARED.
- [SDR JRA2009F00000](https://openairdocs.org/sdr/JRA2009F00000.md): Filter · dirty · Mar 7, 2009 · N587CA · Cvac 440 · Engine Fuel Distribution
  > RT FUEL FILTER BLOCKED LIGHT CAME ON DURING TAKEOFF. TAKEOFF WAS WITH WATER METH (ON) AND WAS ABORTED, THE WARNING LIGHT WENT OUT ON POWER REDUCTION. MX PERFORMED AN INSP OF THE NR 2 FUEL FILTER, REMOVED AND REPLACED FUEL FILTER ENGINE NR 2, RUN UP CHECKED S
- [SDR CA090224002](https://openairdocs.org/sdr/CA090224002.md): Tube · leaking · Feb 12, 2009 · Cvac 440 · Turbine Engine Oil System
  > ON FEBRUARY 12, 2009 NR 1 ENGINE WAS SHUT DOWN 30 MINUTE BEFORE LANDING DUE TO OIL PRESSURE INDICATION OSCILLATING AND LOW OIL PRESSURE LIGHT ON. 20 LITERS OF OIL ADDED, FOUND OIL SUPPLY TUBE FOR THE TURBINE BEARING WAS LEAKING BADLY, REF. ROLLS-ROYCE PICK 72
- [SDR I5H2008F00002](https://openairdocs.org/sdr/I5H2008F00002.md): Spar · corroded · Aug 2, 2008 · N587X · Cvac 440 · Horizontal Stabilizer, Spar/Rib
  > REMOVED INTERGRANULAR CORROSION FROM THE RT HORIZONTAL STABILIZER SN 384RH UPPER REAR SPAR (3) FT OB OF THE UPPER AFT RT HORIZONTAL STABILIZER ATTACH FITTING. REPAIR ACCOMPLISHED IAW DWG NR R361-055-001-001, REV A DATED JULY 15, 2008. (K)
- [SDR CA080630004](https://openairdocs.org/sdr/CA080630004.md): Switch · shorted · Jun 27, 2008 · Cvac 440 · Engine Cranking
  > (CAN) NR 1 ENG STARTED TO ROTATE WHEN START ARM SWITCH SELECTED TO START POSITION, WHILE NR 1 START BUTTON NOT ENGAGED AND ATTEMPTING TO START NR2 ENG. NR 1 ENGINE START SWITCH FOUND SHORTING INTERMITTENTLY INTERNALLY WHEN START BUTTON IS ROCKED SIDE TO SIDE.
- [SDR I5HA0858002](https://openairdocs.org/sdr/I5HA0858002.md): Skin · corroded · Apr 10, 2008 · N582P · Cvac 440 · Wing, Plate/Skin
  > DURING A ROUTINE MAINT INSP THE UPPER RT OB WING SKIN TE WAS FOUND CORRODED WITH CRACKS COMING AROUND SEVERAL RIVETS. THE RT UPPER OB WING SKIN WAS REMOVED, ALL THE CORROSION WAS REMOVED, THE WING STRUCTURE INSPECTED, AND THE SKIN WAS REPLACED IAW THE SRM.
- [SDR VGCA20080212](https://openairdocs.org/sdr/VGCA20080212.md): Fire Detector · malfunctioned · Feb 12, 2008 · N361FL · Cvac 440 · Fire Detection
  > RT ZONE 1 FIRE ALARM CAME ON JUST BEFORE LEVELING AT 12000', CREW FOLLOWED EMERGENCY PROCEDURES TO SHUTDOWN AND SECURE ENGINE.
- [SDR CA080214009](https://openairdocs.org/sdr/CA080214009.md): Downlock Switch · defective · Jan 14, 2008 · Cvac 440 · Landing Gear Position and Warning
  > (CAN) ON APPROACH, ON A FERRY FLIGHT AND WHEN GEARS SELECTED DOWN, THE LT GEAR DID NOT INDICATE DOWN AND LOCKED, LANDING WAS ABORTED. AFTER COMPLETING THE INDICATION, MALFUNCTION CHECKLIST, FOUND IN FACT THAT THE LT GEAR WAS DOWN AND LOCKED. FOR PRECAUTIONAR
- [SDR CA080215009](https://openairdocs.org/sdr/CA080215009.md): Connector · damaged · Jan 11, 2008 · Cvac 440 · Electrical Power System Wiring
  > (CAN) ON CLIMBOUT, AT 5500FT, THE ADI, HSI AND VSI WENT UNSERVICEABLE AT THE SAME TIME, COMPLETE LOSS OF ELECTRICAL POWER, RT SIDE. AT THE SAME TIME, THE NR 2 ENGINE FIRE WARNING (ILLUMINATED) CAME ON ALL 3 ZONES. CREW COMPLETED ENGINE FIRE DRILL. ATC ADVISED
- [SDR CA080214006](https://openairdocs.org/sdr/CA080214006.md): Shaft · damaged · Dec 19, 2007 · Cvac 440 · Turbine Section
  > (CAN) IN CRUISE AT 22,000 FEET, THE CREW OBSERVED A DROP IN RPM FOLLOWED BY A FIRE WARNING IN ENGINE NR1. THE FLIGHT CREW PULLED THE (E) HANDLE AND DISCHARGED THE (2) FIRE EXTINGUISHER BOTTLES. THE FLIGHT CREW THEN PROCEEDED, AFTER DECLARING AN EMERGENCY. THE

Next page: https://openairdocs.org/model/convair-440/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 = '440'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/convair-440/reports

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