# Service difficulty reports: N434MA, cancelled Nov 19, 2009 A list on [N434MA, cancelled Nov 19, 2009](https://openairdocs.org/deregistered/N434MA-2009-11-19.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR 2006F00054](https://openairdocs.org/sdr/2006F00054.md): Fire Warning · activated · Nov 19, 2006 · N434MA · Frchld SA227CC · Fire Detection > RT ENGINE FIRE WARNING ILLUMINATED, RETURNED TO FIELD. - [SDR MALA965245](https://openairdocs.org/sdr/MALA965245.md): Rib · cracked · Dec 18, 1996 · N434MA · Swrngn SA227AC · Wing, Rib/Bulkhead > DURING AN INSPECTION IN MSP, MAINTENANCE FOUND TWO CRACKS 1INCH 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 A 6.5 INCH, - [SDR MALA965244](https://openairdocs.org/sdr/MALA965244.md): Rib · cracked · Dec 18, 1996 · N434MA · Swrngn SA227AC · Wing, Rib/Bulkhead > DURING AN INSPECTION IN MSP, MAINTENANCE FOUND TWO CRACKS 2 INCH BY 1 INCH IN THE RADIUS OF THE RIGHT WING RIB LOWR ATTACH FLANGE (P/N 27-31023). APPROXIMATE LOCATION IS WS 81 BETWEEN NS 130 AND 141. STOP DRILLED CRACK, FABRICATED AND INSTALLED A 6.5 INCH, - [SDR MALA965239](https://openairdocs.org/sdr/MALA965239.md): Rib · cracked · Dec 18, 1996 · N434MA · Swrngn SA227AC · Wing, Rib/Bulkhead > DURING AN INSPECTION IN MSP, MAINTENANCE FOUND A 5 INCH CRACK IN THE RADIUS OF THE 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 A 8.25 INCH BY 3 INCH BY 1 - [SDR MALA965230](https://openairdocs.org/sdr/MALA965230.md): Skin · chafed · Nov 28, 1996 · N434MA · Swrngn SA227AC · Fuselage Main, Plate/Skin > DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND SKIN CHAFE DAMAGE AT FS 241 AND ON BOTH SIDES OF BL 0.00. CHAF DAMAGE IS APPROX.025 INCH DEEP AND.125 INCH IN DIAMETER. FABRICATED AND INSTALLED EXTERNAL REPAIR DOUBLER (.050 BY 4 BY 5 INCH) IAW FAC S - [SDR MALA965226](https://openairdocs.org/sdr/MALA965226.md): Torque Tube · worn · Nov 28, 1996 · N434MA · Swrngn SA227AC · Rudder Control System > DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE RUDDER TORQUE TUBE WORN BEYOND ALLOWABLE LIMITS OF.003 FROM PHENOLIC SEAL. REPAIRED RUDDER TORQUE TUBE BY REMOVING AND REPLACING WITH A NEW RUDDER TORQUE TUBE, P/N 27-42051-8037, IAW FAIRCHILD MM 27 - [SDR MALA965229](https://openairdocs.org/sdr/MALA965229.md): Rib · cracked · Nov 27, 1996 · N434MA · Swrngn SA227AC · Trailing Edge Flaps > DURING A SCHEDULED INSPECTION IN MSP, MAINTENACNE FOUND A CRACK IN THE LEFT FLAP S/N RPL10-88 OUTBOARD FLAP NOSE RIB. REMOVED AND REPLACED IAW FAC SRM 57-90-60. (M) - [SDR MALA965228](https://openairdocs.org/sdr/MALA965228.md): Angle · cracked · Nov 27, 1996 · N434MA · Swrngn SA227AC · Nacelle/Pylon Structure > DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND A CRACK IN THE RIGHT FORWARD LOWER INBOARD WING TO NACELLE INTRANSIT ANGLE. (M) - [SDR MALA965227](https://openairdocs.org/sdr/MALA965227.md): Intercostal · cracked · Nov 26, 1996 · N434MA · Swrngn SA227AC · Fuselage Miscellaneous Structure > DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND A.25 INCH CRACK IN LT INTERCOSTAL RELIEF RADIUS AT FUSELAGE STATION 377. REPAIRED PER FAC MM 53-90-20 REPAIR NR 20. (M) - [SDR MALA965192](https://openairdocs.org/sdr/MALA965192.md): Rib · cracked · Nov 9, 1996 · N434MA · Swrngn SA227AC · Trailing Edge Flaps > DURING SCHEDULED MAINTENANCE IN MSP, THE LEFT FLAP NOSE RIB HAD A.5 INCH CRACK FROM THE RELIEF RADIUS. COMPLETED REPAIR TO LEFT FLAP BY REPLACING THE INBOARD NOSE RIB P/N 27-36004-007 IAW 51-00-00 PAGE 4 AND 51-40-02. (M) - [SDR MALA965069](https://openairdocs.org/sdr/MALA965069.md): Door Frame · scuffed · Jul 10, 1996 · N434MA · Swrngn SA227AC · Fuselage Miscellaneous Structure > DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE FORWARD CABIN DOOR FUSELAGE FRAME FS 133.87, P/N 27-22126, HAD SCUFF MARKS APPROX.016 INCH DEEP AT LOWER TEFLON GUIDE PAD CONTACT AREA. FABRICATED AND INSTALLED REPAIR PLATE, 'REPLACEABLE WEAR PLAT - [SDR MALA965063](https://openairdocs.org/sdr/MALA965063.md): Mechanism · out of adjust · Jul 6, 1996 · N434MA · Swrngn SA227AC · Cargo/Baggage Doors > FLT 3049 - EN ROUTE FROM LNK, THE CARGO DOOR WARNING LIGHT ILLUMINATED IN FLIGHT. THE AIRCRAFT RETURNED TO LNK. MAINTENANCE ADJUSTED THE CARGO DOOR ROD ENDS ON THE FORWARD BOTTOM BELLCRANK AND THE DOOR HANDLE POSITION SWITCH. ALL CHECKS SATISFACTORY. (M) - [SDR MALA964843](https://openairdocs.org/sdr/MALA964843.md): Seal · out of adjust · Jan 26, 1996 · N434MA · Swrngn SA227AC · Passenger/Crew Doors > FLT NR 3354 - AFTER DEPARTURE FROM DTW, THE CREW NOTED A LOUD SQUEAL FROM THE PASSENGER DOOR. THE CREW ELECTED TO RETURN TO DTW AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL SHIMMED THE PASSENGER DOOR SEAL. ALL SYSTEMS OPERATED SATISFACTOR - [SDR MALA954725](https://openairdocs.org/sdr/MALA954725.md): Frame · cracked · Nov 24, 1995 · N434MA · Swrngn SA227AC · Fuselage Main, Frame > DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED A CRACK IN THE LOWER RIGHT BELT FRAME RELIEF RADIUS AT FS 242.27 AND WL 81.07 BELOW STRINGER NR 11. THE CRACK WAS REPAIRED BY STOP DRILLING IT AND FABRICATING AND INSTALLING A REPAIR DOUBLER IA - [SDR MALA954724](https://openairdocs.org/sdr/MALA954724.md): Door · cracked · Nov 24, 1995 · N434MA · Swrngn SA227AC · Passenger/Crew Doors > DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL FOUND A CRACK IN THE LOWER AFT PASSENGER DOOR CORNER P/N 27-24044 AND WEAR IN THE LOWER AFT PASSENGER DOOR COVER, P/N 27-24150. THE COMPONENTS WERE REMOVED AND REPLACED WITH NEW IAW SRM 51-30-02, -04 - [SDR MALA954723](https://openairdocs.org/sdr/MALA954723.md): Door · cracked · Nov 24, 1995 · N434MA · Swrngn SA227AC · Passenger/Crew Doors > DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL FOUND A CRACK IN THE LOWER FORWARD PASSENGER DOOR CORNER, P/N 27-24044 AND WEAR IN THE LOWER FORWARD PASSENGER DOOR COVER, P/N 27-24150. THE COMPONENTS WERE REMOVED AND REPLACED WITH NEW IN ACCORDANC - [SDR MALA954722](https://openairdocs.org/sdr/MALA954722.md): Stiffener · cracked · Nov 24, 1995 · N434MA · Swrngn SA227AC · Wing Miscellaneous Structure > DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL FOUND A CRACK IN THE CENTER CHANNEL AT BL 0.00 AND FS 254.52. THE CRACK WAS REPAIRED BY REPLACING THE CENTER STIFFENER (P/N 27-31110-031, 032) IAW SRM 157-90-30, REPAIRS NR 1 AND NR 2. (M) - [SDR MALA954705](https://openairdocs.org/sdr/MALA954705.md): Cooling Turbine · seized · Nov 9, 1995 · N434MA · Swrngn SA227AC · Cabin Temperature Control System > FLT NR 3434 - DURING TAXI AFTER LANDING, THE CREW NOTED SMOKE IN THE CABIN AND COCKPIT. THE CREW SHUT DOWN BOTH BLEEDS AND PROCEEDED TO THE GATE. MAINTENANCE PERSONNEL REPLACED THE LEFT COOLING TURBINE. ALL SYSTEMS OPERATED SATISFACTORILY. (M) - [SDR MALA954679](https://openairdocs.org/sdr/MALA954679.md): Altimeter · failed · Oct 27, 1995 · N434MA · Swrngn SA227AC · Altimeter, Barometric/Encoder > FLT NR 3046 - ON CLIMB-OUT FROM DTW, THE CAPTAINS ALTIMETER BECAME INOPERATIVE. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED THE CAPTAINS ALTIMETER AND PURGED THE NR 1 AND NR 2 STATIC SYSTEMS. ALL SYSTEMS OPERATED SATISFACTORILY. (M) - [SDR MALA954677](https://openairdocs.org/sdr/MALA954677.md): Position Sw · failed · Oct 21, 1995 · N434MA · Swrngn SA227AC · Landing Gear Position and Warning > FLT NR 3087 - ON APPROACH IN MSP, THE LEFT GEAR INTRANSIT LIGHT REMAINED ILLUMINATED AFTER THE GEAR INDICATOR SHOWED IT TO BE DOWN AND LOCKED. THE CREW CYCLED THE GEAR AND ALL INDICATIONS WERE NORMAL. MAINTENANCE REPLACED THE LEFT INBOARD POSITION SWITCH, P/ - [SDR MALA954595](https://openairdocs.org/sdr/MALA954595.md): Former · cracked · Aug 20, 1995 · N434MA · Swrngn SA227AC · Nacelle/Pylon Structure > MSP - DURING A SCHEDULED INSPECTION, THE LT INBD FORMER, PN 27-35025-067, AND STR, PN 27-35041-012, WERE FOUND CRACKED AT NACELLE STA 120.00. REPAIRS WERE COMPLETED BY FABRICATING AND INSTALLING REPAIR DOUBLERS IAW FAC LAR NR 95-MALA-225. (X) - [SDR MALA954579](https://openairdocs.org/sdr/MALA954579.md): Switch · failed · Aug 9, 1995 · N434MA · Swrngn SA227AC · Landing Gear Position and Warning > MSP - FLT 3027 - ON APPROACH, LT GEAR INTRANSIT LIGHT WAS VERY DIM WHEN ILLUMINATED DURING GEAR EXTENSION. THE INDICATION LIGHT ILLUMINATED NORMALLY WHEN TESTED. MAINTENANCE REPLACED THE LEFT INBOARD UPPER GEAR POSITION SWITCH. SYSTEM OPERATED SATISFACTORIL - [SDR MALA954469](https://openairdocs.org/sdr/MALA954469.md): Skin · birdstrike · May 19, 1995 · N434MA · Swrngn SA227AC · Wing, Plate/Skin > DURING POSTFLIGHT INSPECTION IN FFM, THE CREW FOUND A DENT IN THE LEFT LEADING EDGE DUE TO A BIRDSTRIKE JUST INBOARD OF WS 131.899. THE AIRCRAFT WAS FERRIED TO MSP FOR REPAIR. MAINTENANCE REPAIRED THE LEADING EDGE BY INSTALLING A FILLER AND REPAIR DOUBLER IA - [SDR MALA954436](https://openairdocs.org/sdr/MALA954436.md): Doubler · worn · Apr 30, 1995 · N434MA · Swrngn SA227AC · Trailing Edge Flaps > DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE LEFT FLAP DOUBLER WORN. REPAIRS WERE COMPLETED BY REPLACING THE ROLLER DOUBLER, P/N 27-31141-001, IAW FAC SRM 51-00-00 PAGE 4. (W) - [SDR MALA954287](https://openairdocs.org/sdr/MALA954287.md): Door Frame · cracked · Feb 5, 1995 · N434MA · Swrngn SA227AC · Fuselage Miscellaneous Structure > DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE FUSELAGE CARGO DOOR FRAME CRACKED AT THE GAS SPRING BOLT MOUNTING HOLE. REPAIRS WERE COMPLETED THROUGH INSTALLATION OF A REPAIR DOUBLER IAW FAC LAR 95-MALA-042 AND FAC 51-00-00 STANDARD PRACTICES. ( - [SDR MALA954270](https://openairdocs.org/sdr/MALA954270.md): Compressor Seal · leaking · Jan 21, 1995 · N434MA · Swrngn SA227AC · Turbine Engine Compressor Section > MSP - FLT 3306 - IN CRUISE FLIGHT, CREW NOTED AN UNPLEASANT SMELL WHILE THE AIRCRAFT WAS PRESSURIZED. THE AIRCRAFT CONTINUED TO MSP WITHOUT INCIDENT. MAINTENANCE REPLACED LT ENGINE COMPRESSOR SEAL. SYSTEM OPERATED SATISFACTORILY. (X) - [SDR MALA954232](https://openairdocs.org/sdr/MALA954232.md): Pitot System · req'd service · Jan 6, 1995 · N434MA · Swrngn SA227AC · Pitot/Static System > FLT NR 3094 - ON CLIMB-OUT FROM DTW, THE CAPTAINS AIRSPEED INDICATOR BEGAN TO DROP. DURING THE CLIMB THE FIRST OFFICERS AIRSPEED INDICATOR ALSO BEGAN TO DROP. THE CREW SELECTED PITOT HEAT ONLY ON BOTH SIDES AND BOTH AIRSPEEDS CAME BACK TO NORMAL. THE AIRCRA ## 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 = 'N434MA' AND deregistration_id = 'N434MA-2009-11-19' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N434MA-2009-11-19/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.