# Service difficulty reports: N430MA

A list on [N430MA](https://openairdocs.org/aircraft/N430MA.md).

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

- [SDR DUFA20180529001](https://openairdocs.org/sdr/DUFA20180529001.md): Gear · stripped · May 16, 2018 · N430MA · Swrngn SA227AC · Engine Fuel Pump
  > WHILE IN CRUISE DURING A PART 91 REPOSITION FLIGHT, THE NR 2 ENGINE FLAMED OUT AND SHUT DOWN. MAINTENANCE CREW WAS DISPATCHED TO THE LOCATION AND THE ENGINE GEARBOX OPENED UP FOR INVESTIGATION. FOUND ACCESSORY GEAR ASSEMBLY HAD FAILED LOSING CONTINUITY TO FUEL
- [SDR 2006F00039](https://openairdocs.org/sdr/2006F00039.md): Indication Sys · malfunctioned · Sep 13, 2006 · N430MA · Swrngn SA227AC · Landing Gear Position and Warning
  > LEFT LANDING GEAR INDICATION SHOWED GEAR NOT DOWN. CLEANED ANNUNCIATOR CONTACTS. OPS CHECK OK.
- [SDR 2006F00038](https://openairdocs.org/sdr/2006F00038.md): Contactor · dirty · Sep 13, 2006 · N430MA · Swrngn SA227AC · Landing Gear Position and Warning
  > LEFT MAIN DOWN LIGHT FAILED TO ILLUMINATE. FLYOVER SHOWED GEAR DOWN. ANNUNCIATOR CONTACTS WERE CLEANED. GEAR WAS CYCLED AND DISCREPANCY WAS CLEARED.
- [SDR 2005FA0000041](https://openairdocs.org/sdr/2005FA0000041.md): Acm · seized · Dec 31, 2004 · N430MA · Swrngn SA227AC · Cabin Cooling System
  > ON TOUCHDOWN, THE CREW NOTICED AN ACRID SMELL IN THE COCKPIT. THE CREW LANDED AND TAXIED IN WITH NO FURTHER INCIDENT. TROUBLESHOOTING FOUND THE SOURCE TO THE RT ACM. INITALLY DEFERRED ACM IAW MEL, LATER CHANGED THE ACM, MEL WAS CLEARED. (NM05200403534) (K
- [SDR 2005FA0000064](https://openairdocs.org/sdr/2005FA0000064.md): Scavenge Pump · failed · Dec 6, 2004 · N430MA · Swrngn SA227* · Turbine Engine Oil System
  > MRR-M04-23, NR 2 ENGINE OIL PRESSURE LIGHT CAME ON AS FLIGHT LEVELED OUT IN CRUISE, OIL PRESSURE GAUGE WAS CHECKED AND FOUND PRESSURE DROPPING. CREW DID A PRECAUTIONARY INFLIGHT SHUTDOWN, AND RETURNED TO STATION. LOSS OF OIL PRESSURE DUE TO LOSS OF OIL FRM R
- [SDR 2005FA0000043](https://openairdocs.org/sdr/2005FA0000043.md): Warning System · malfunctioned · Mar 4, 2004 · N430MA · Swrngn SA227AC · Door Warning System
  > CARGO DOOR WARNING LIGHT CAME ON IN FLIGHT DURING THE START OF THE DESCENT TO THE NEXT STATION. ATC WAS NOTIFIED. THE LIGHTS STAYED ON FOR APPROXIMATELY 10 MINUTES. DOOR CLOSING PROCEDURES, DOOR HARD TO CLOSE, DOOR CLICK CLACK RIGGING/LUBRICATION, OR SWITCH
- [SDR 2003F00624](https://openairdocs.org/sdr/2003F00624.md): Line · leaking · Aug 9, 2003 · N430MA · Swrngn SA227AC · Engine Oil Distribution (Airframe Furnished)
  > DURING CRUISE THE RT ENGINE OIL PRESS WARN LIGHT CAME ON, THIS VERIFIED WITH THE OIL PRESSURE GAUGE. CREW FOLLOWED CHECKLIST PROCEDURES AND SHUTDOWN THE ENGINE. OIL TEMPERATURE STAYED IN THE NORMAL RANGE THROUGH THE SHUTDOWN. CREW DIVERTED TO CLOSEST STATIO
- [SDR 2003F00632](https://openairdocs.org/sdr/2003F00632.md): Pump · malfunctioned · Jul 16, 2003 · N430MA · Swrngn SA227AC · Engine Oil System (Airframe Furnished)
  > RT ENGINE OIL PRESSURE LIGHT DIDN'T GO OUT AFTER 50 PERCENT RPM DURING START. OIL PRESSURE WAS ALSO LOW. MAINTENANCE FOUND OIL LEVEL LOW AND OIL IN THE TAIL PIPE. REPLACED REAR OIL SCAVENGE PUMP. OPS CHECK AND FLIGHT CHECK. (M)
- [SDR 2003F00626](https://openairdocs.org/sdr/2003F00626.md): Water Injection · failed · Jul 2, 2003 · N430MA · Swrngn SA227AC · Water Injection System
  > CAWI DID NOT FIRE ON TAKEOFF ROLL. LIGHTS OPERATE NORMALLY BUT NO RISE IN PERCENT TORQUE. DEFERRED CAWI SYSTEM. NO DEFECTS NOTED WHEN AIRCRAFT CAME IN FOR REPAIR. (M)
- [SDR 2003F00241](https://openairdocs.org/sdr/2003F00241.md): Indicator · failed · Feb 5, 2003 · N430MA · Swrngn SA227AC · Air Collision Avoidance System
  > FLT 2579 - BIL - NR 1 VSI FAILED DURING DESCENT. CREW LANDED WITH NO FURTHER INCIDENT AFTER DECLARING EMERGENCY. TCAS/VSI INDICATOR WAS BAD. REPLACED VSI/TCAS INDICATOR, SYSTEM TEST GOOD. (M)
- [SDR BSAA030231](https://openairdocs.org/sdr/BSAA030231.md): Indicator · failed · Feb 5, 2003 · N430MA · Swrngn SA227AC · Air Collision Avoidance System
  > NR 1 VSI FAILED DURING DESCENT. CREW LANDED WITH NO FURTHER INCIDENT AFTER DECLARING EMERGENCY. REPLACED VSI/TCAS INDICATOR, SYSTEM TEST GOOD.
- [SDR MALA965240](https://openairdocs.org/sdr/MALA965240.md): Rib · cracked · Dec 18, 1996 · N430MA · Swrngn SA227AC · Wing, Rib/Bulkhead
  > DURING AN INSPECTION IN MSP, MAINTENANCE FOUND TWO CRACKS 1 INCH BY 1 INCH IN THE RADIUS OF THE LT WING RIB LOWER ATTACH FLANGE (P/N 27-31023). APPROXIMATE LOCATION IS WS 81 AND BETWEEN NS 130 AND 141. STOP DRILLED CRACK, FABRICATED AND INSTALLED AN APPROPRI
- [SDR MALA965241](https://openairdocs.org/sdr/MALA965241.md): Rib · cracked · Dec 17, 1996 · N430MA · Swrngn SA227AC · Wing, Rib/Bulkhead
  > DURING AN INSPECTION IN MSP, FOUND TWO CRACKS IN THE RADIUS OF THE RT WING RIB LOWER ATTACH FLANGE (P/N 27-31023). APPROXIMATE LOCATION IS WS 81 AND BETWEEN NS 130 AND 141. STOP DRILLED CRACK, FABRICATED AND INSTALLED AN APPROPRIATE SIZED 3 INCH BY 1 INCH BY
- [SDR MALA965215](https://openairdocs.org/sdr/MALA965215.md): Rib · cracked · Nov 21, 1996 · N430MA · Swrngn SA227AC · Trailing Edge Flaps
  > DURING A BLOCK INSPECTION IN MSP, MAINTENANCE FOUND A CRACK APPROX.75 INCH LONG IN RIGHT INBOARD FLAP NOSE RIB. REMOVED AND REPLACED FLAP NOSE RIB P/N 27-36015-002 IAW FAIRCHILD STRUCTURAL REPAIR MANUAL 52-00-00 PAGE 4 AND 51-40-02. (M)
- [SDR MALA965214](https://openairdocs.org/sdr/MALA965214.md): Rib · cracked · Nov 21, 1996 · N430MA · Swrngn SA227AC · Trailing Edge Flaps
  > DURING A BLOCK INSPECTION IN MSP, MAINTENANCE FOUND TWO CRACKS IN LEFT FLAP SN C-134 OUTBOARD FLAP NOSE RIB. REMOVED AND REPLACED FLAP NOSE RIB P/N 27-36015-001 IAW FAIRCHILD STRUCTURAL REPAIR MANUAL 57-90-60 PAGES 43-46. (M)
- [SDR MALA965213](https://openairdocs.org/sdr/MALA965213.md): Angle · cracked · Nov 20, 1996 · N430MA · Swrngn SA227AC · Nacelle/Pylon Structure
  > DURING A BLOCK INSPECTION IN MSP, MAINTENANCE FOUND THE LEFT INBOARD UPPER NACELLE TO WING TRANSIT ANGLE CRACKED AT THE FORWARD EDGE. REPAIR WAS COMPLETED BY INSTALLING A REPAIR DOUBLER IAW ARP 54-20-9101 REV B AND FAIRCHILD SRM 51-30-02, 51-40 AND 51-30-03.
- [SDR MALA965212](https://openairdocs.org/sdr/MALA965212.md): Angle · cracked · Nov 20, 1996 · N430MA · Swrngn SA227AC · Nacelle/Pylon Structure
  > DURING A BLOCK INSPECTION IN MSP, MAINTENANCE FUOND LEFT INBOARD LOWER NACELLE TO WING TRANSIT ANGLE CRACKED AT FORWARD EDGE. COMPLETED REPAIR BY REMOVING EXISTING REPAIR, FABRICATING AND WET INSTALLING NEW DOUBLER IAW ARP 54-20-9101 REV B DATED MAY 12, 1993,
- [SDR MALA965211](https://openairdocs.org/sdr/MALA965211.md): Angle · cracked · Nov 20, 1996 · N430MA · Swrngn SA227AC · Nacelle/Pylon Structure
  > DURING A BLOCK INSPECTION IN MSP, MAINTENANCE FOUD THE RIGHT INBOARD LOWER NACELLE TO WING TRANSIT ANGLE CRACKED AT THE FORWARD EDGE. REPAIR WAS COMPLETED BY INSTALLING A REPAIR DOUBLER IAW ARP 54-20-9101 REV B AND FAIRCHILD SRM 51-30-02, 51-40 AND 51-30-03.
- [SDR MALA964977](https://openairdocs.org/sdr/MALA964977.md): Engine · failed · Apr 30, 1996 · N430MA · Swrngn SA227AC · Engine (Turbine/Turboprop)
  > TOL/DTW - FLT 3328 - IN CRUISE FLIGHT, THE LEFT ENGINE CHIP DETECTOR LIGHT ILLUMINATED. THE CREW PERFORMED QUICK REFERENCE PROCEDURES. (X)
- [SDR MALA964970](https://openairdocs.org/sdr/MALA964970.md): Switch · out of adjust · Apr 19, 1996 · N430MA · Swrngn SA227AC · Landing Gear Retraction/Extension System
  > FLIGHT 3234 - ON CLIMB-OUT FROM BJI, THE NOSE GEAR CONTINUED TO CYCLE IN THE WHEEL WELL AFTER THE GEAR WAS RETRACTED. MAINTENANCE ADJUSTED THE UPLIMIT SWITCH. ALL SYSTEMS OPERATED SATISFACTORILY. (M)
- [SDR MALA954774](https://openairdocs.org/sdr/MALA954774.md): Shear Bolt · sheared · Dec 26, 1995 · N430MA · Swrngn SA227AC · Landing Gear Door Retract Section
  > FLT NR 3250 - DURING LANDING AT GFK, THE RIGHT GEAR DOOR POSITION LIGHT ILLUMINATED. THE AIRCRAFT CONTINUED THE LANDING WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED THE RIGHT GEAR DOOR ROLLER SHEAR BOLT. ALL SYSTEMS OPERATED SATISFACTORILY. (M)
- [SDR MALA954689](https://openairdocs.org/sdr/MALA954689.md): Skin Patch · damaged · Oct 29, 1995 · N430MA · Swrngn SA227AC · Landing Gear Doors
  > DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE RIGHT OUTBOARD GEAR DOOR FLUSH PATCH DOOR SKIN REPAIR DAMAGED. REPAIRS WERE COMPLETED BY REPLACING THE FILLER IAW FAC SRM 52-90-30. (M)
- [SDR MALA954688](https://openairdocs.org/sdr/MALA954688.md): Seat Track · cracked · Oct 29, 1995 · N430MA · Swrngn SA227AC · Fuselage, Seat/Cargo Attach Fittings
  > DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE PILOTS SEAT TRACK ATTACH POINTS AT FS 107 TO BE CRACKED. REPAIRS WERE COMPLETED BY FABRICATING AND INSTALLING A REPAIR FLAGNE IAW ARP 53-10-8913. (M)
- [SDR MALA954687](https://openairdocs.org/sdr/MALA954687.md): Seat Track · cracked · Oct 29, 1995 · N430MA · Swrngn SA227AC · Fuselage, Seat/Cargo Attach Fittings
  > DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND A CRACK AT THE NUT PLATES FOR THE PILOTS OUTBOARD SEAT TRACK ATTACHMENT JUST AFT OF FS 107. REPAIRS WERE COMPLETED BY INSTALLING A REPAIR DOUBLER IAW ARP 53-10-9322. (M)
- [SDR MALA954686](https://openairdocs.org/sdr/MALA954686.md): Torque Tube · corrosion · Oct 29, 1995 · N430MA · Swrngn SA227AC · Elevator Structure
  > DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE RIGHT ELEVATOR TORQUE TUBE WELDMENT TO HAVE SIGNS OF CORROSION. REPAIRS WERE COMPLETED BY REPLACING THE RIGHT ELEVATOR ASSEMBLY. (M)
- [SDR MALA954685](https://openairdocs.org/sdr/MALA954685.md): Door Corner · cracked · Oct 29, 1995 · N430MA · Swrngn SA227AC · Passenger/Crew Doors
  > DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE UPPER PASSENGER DOOR CORNER CRACKED. REPAIRS WERE COMPLETED BY REPLACING THE CORNER, P/N 27-24044-010, IAW FAC SRM 51-00-00 PAGE 4. (M)
- [SDR MALA954684](https://openairdocs.org/sdr/MALA954684.md): Door Corner · cracked · Oct 29, 1995 · N430MA · Swrngn SA227AC · Passenger/Crew Doors
  > DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE AFT UPPER PASSENGER DOOR CORNER CRACKED. REPAIRS WERE COMPLETED BY REPLACING THE CORNER, P/N 27-24044-009, IAW FAC SRM 51-00-00 PAGE 4. (M)
- [SDR MALA954683](https://openairdocs.org/sdr/MALA954683.md): Stairs · cracked · Oct 29, 1995 · N430MA · Swrngn SA227AC · Passenger/Crew Doors
  > DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE PASSENGER DOOR STAIR ASSEMBLY CRACKED. REPAIRS WERE COMPLETED BY REPLACING THE STAIR ASSEMBLY, P/N 27-24150-297. (M)
- [SDR MALA954682](https://openairdocs.org/sdr/MALA954682.md): Skin · cracked · Oct 29, 1995 · N430MA · Swrngn SA227AC · Passenger/Crew Doors
  > DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE PASSENGER DOOR AFT LOWER SKIN CRACKED NEAR THE HINGE. REPAIRS WERE COMPLETED BY REPLACING THE SKIN SEGMENT IAW FAC SRM 51-90-10, PAGES 12-14. (M)
- [SDR MALA954615](https://openairdocs.org/sdr/MALA954615.md): Door Frame · cracked · Aug 31, 1995 · N430MA · Swrngn SA227AC · Fuselage Miscellaneous Structure
  > MSP - DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND THE CARGO DOOR FUSELAGE FRAME AT FS 438 CRACKED AT THE GAS STRUT MOUNT POST HOLE. REPAIRS WERE COMPLETED BY INSTALLING A REPAIR ANGLE, PLATE AND FILLER IAW FAC ARP 53-20-9503. (X)
- [SDR MALA954614](https://openairdocs.org/sdr/MALA954614.md): Frame · cracked · Aug 31, 1995 · N430MA · Swrngn SA227AC · Fuselage Miscellaneous Structure
  > MSP - DURING A SCHEDULED INSPECTION, FOUND THE CARGO DOOR FUSELAGE FRAME AT FS 491 CRACKED AT THE GAS STRUT MOUNT POST HOLE. REPAIRS WERE COMPLETED BY FABRICATING AND INSTALLING A REPAIR ANGLE, PLATE, AND FILLER IAW ARP 53-20-9503. (X)
- [SDR MALA954585](https://openairdocs.org/sdr/MALA954585.md): Doubler · worn · Aug 16, 1995 · N430MA · Swrngn SA227AC · Trailing Edge Flaps
  > DURING SCHEDULED MAINTENANCE IN MSP, THE RIGHT FLAP ROLLER DOUBLER WAS WORN. REPAIRS WERE COMPLETED BY REPLACING THE DOUBLER IAW FAC 57-10-9207 AND ARP 57-20-9024. (M)
- [SDR MALA954541](https://openairdocs.org/sdr/MALA954541.md): Switch · failed · Jul 15, 1995 · N430MA · Swrngn SA227AC · Landing Gear Position and Warning
  > FLT 3027 - ON APPROACH TO MSP, THE CREW DIDN'T RECEIVE A DOWN AND LOCKED INDICATION FROM THE NOSE GEAR POSITION AFTER GEAR EXTENSION. THE CREW CYCLED THE GEAR TWICE BEFORE A DOWN AND LOCKED INDICATION WAS RECEIVED. THE AIRCRAFT CONTINUED TO MSP AND LANDED WI
- [SDR MALA954533](https://openairdocs.org/sdr/MALA954533.md): Position Ind · malfunctioned · Jul 10, 1995 · N430MA · Swrngn SA227AC · Landing Gear Position and Warning
  > FLT 3253 - ON APPROACH TO MSP, THE NOSE GEAR GREEN LIGHT FAILED TO ILLUMINATE UPON GEAR EXTENSION. THE CREW CYCLED THE GEAR UNTIL THE LIGHT ILLUMINATED. MAINTENANCE WAS UNABLE TO DUPLICATE THE DISCREPANCY. THE GEAR POSITION INDICATOR WAS REPLACED AS A PRECA
- [SDR MALA954496](https://openairdocs.org/sdr/MALA954496.md): Eel Bulbs · failed · Jun 7, 1995 · N430MA · Swrngn SA227AC · Emergency Lighting
  > MSP - DURING WALKAROUND, THE FORWARD EMERGENCY EXIT ESCAPE FLOOR PATH LIGHTS HAD TWO BULBS INOPERATIVE. MAINTENANCE REPLACED THE LT AFT BATTERY PACK. SYSTEM OPERATED SATISFACTORILY. (W)
- [SDR MALA954497](https://openairdocs.org/sdr/MALA954497.md): Feed Back Pot · failed · Jun 6, 1995 · N430MA · Swrngn SA227AC · Landing Gear Steering System
  > DTW - FLT 3186 - DURING LANDING AT DTW, AIRCRAFT PROCEEDED LEFT UNCOMMANDED WHEN NOSE WHEEL STEERING WAS ENGAGED. MAINTENANCE REPLACED THE NOSE WHEEL STEERING FEEDBACK POT MOUNT ASSEMBLY. THE SYSTEM OPERATED SATISFACTORILY. (X)

## 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 n_number = 'N430MA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N430MA/reports

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