# Service difficulty reports: N403XJ, cancelled Jun 7, 2019

A list on [N403XJ, cancelled Jun 7, 2019](https://openairdocs.org/deregistered/N403XJ-2019-06-07.md).

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

Page 1 of 2 · 72 reports

- [SDR PNSA2015070201](https://openairdocs.org/sdr/PNSA2015070201.md): Power Supply · no test · Jul 2, 2015 · N403XJ · Saab 340B · Emergency Lighting
  > EMERGENCY LIGHTING POWER SUPPLIES POSITION 23LN FAILED ITS 6-MONTH CAPACITY TEST. POWER SUPPLY 23LN HAS BEEN REPLACED AND NOW PASSES BOTH FUNCTION AND CAPACITY CHECKS.
- [SDR PNSA2014121802](https://openairdocs.org/sdr/PNSA2014121802.md): Wire · damaged · Dec 18, 2014 · N403XJ · Saab 340B · Light System Wiring
  > LEFT GALLEY EXIT LOCATOR LIGHT INOPERATIVE DURING SCHEDULED INSPECTION. TROUBLESHOT SYS. PINNED WIRES AT CONNECTOR. OPS CHECKED GOOD.
- [SDR PNSA2014112502](https://openairdocs.org/sdr/PNSA2014112502.md): Warning System · false activation · Nov 25, 2014 · N403XJ · Saab 340B · Smoke Detection
  > CARGO SMOKE LIGHT ON CWP ILLUMINATED INFLIGHT THEN CARGO, LAVATORY & AVIONICS LIGHTS ILLUMINATED ON SHUTDOWN. PERFORMED CONTINUITY CHECKS ON SYSTEM'S WIRING, NO DEFECTS NOTED. R & R AVIONICS & LAVATORY SMOKE DETECTORS FOR TROUBLESHOOTING OPERATIONS CHECK OK.
- [SDR PNSA2014082003](https://openairdocs.org/sdr/PNSA2014082003.md): Light · inoperative · Aug 20, 2014 · N403XJ · Saab 340B · Emergency Lighting
  > FLIGHT ATTENDANT PANEL EMERGENCY LIGHTING ARM LIGHT INOPERATIVE. RE-LAMPED THE ARM LIGHT. OPERATIONS CHECKED GOOD.
- [SDR PNSA2014062102](https://openairdocs.org/sdr/PNSA2014062102.md): Connector · loose · Jun 21, 2014 · N403XJ · Saab 340B · Landing Gear System Wiring
  > NO LT MAIN GEAR GREEN LIGHT ON GEAR EXTENSION DECLARED EMERGENCY. FOUND LT DOWN LOCK CONNECTOR 5/6 GA LOOSE.
- [SDR PNSA2014051401](https://openairdocs.org/sdr/PNSA2014051401.md): Light · inoperative · May 14, 2014 · N403XJ · Saab 340B · Emergency Lighting
  > FLIGHT ATTENDANT PANEL EMERGENCY LIGHTS ARM DOES NOT ILLUMINATE WHEN ARMED.
- [SDR PNSA2014031102](https://openairdocs.org/sdr/PNSA2014031102.md): Relay · failed · Mar 11, 2014 · N403XJ · Saab 340B · Air Intake Anti/De-Ice System
  > RIGHT INTAKE LIGHT REMAINS ON. R & R RIGHT INTAKE HEAT AC POWER RELAY.
- [SDR PNSA2014020401](https://openairdocs.org/sdr/PNSA2014020401.md): Transceiver · failed · Feb 4, 2014 · N403XJ · Saab 340B · HF Communications System
  > NR 2 COM BLACKED OUT, STUCK ON ONE FREQUENCY INSTALLED SERVICABLE NR 2 COM.
- [SDR PNSA2013081707](https://openairdocs.org/sdr/PNSA2013081707.md): Lamp · inoperative · Aug 17, 2013 · N403XJ · Saab 340B · Emergency Lighting
  > FOUND ARM LIGHT BURNED OUT DURING EMERGENCY LIGHTING TEST. REPLACED LAMP, OPS CHECKED GOOD.
- [SDR PNSA2013060501](https://openairdocs.org/sdr/PNSA2013060501.md): Light · inoperative · Jun 5, 2013 · N403XJ · Saab 340B · Emergency Lighting
  > F/A PANEL EMERGENCY ARMED LAMP OUT THAT WAS DISCOVERED DURING LINE MAINTENANCE. RELAMPED EMERGENCY LIGHT ARMED LIGHT ON F/A PANEL.
- [SDR PNSA2013041802](https://openairdocs.org/sdr/PNSA2013041802.md): Power Supply · failed · Mar 27, 2013 · N403XJ · Saab 340B · Emergency Lighting
  > DURING SCHEDULED MAINTENANCE CHECK. CHECK OF EMERGENCY LIGHTING POWER SUPPLY; ONE POWER SUPPLY OF THE 4 ON THE AIRCRAFT FAILED THE CAPACITANCE CHECK PORTION OF THE TEST. IT WAS REMOVED FROM THE AIRCRAFT AND REPLACED WITH A SERVICEABLE ASSEMBLY.
- [SDR MALA090020](https://openairdocs.org/sdr/MALA090020.md): Skin · dented · Feb 8, 2009 · N403XJ · Saab 340B · Trailing Edge Flaps
  > DENT LOCATED IN LT FLAP ASSY 38.5 INCHES OUTBOARD FROM INBOARD EDGE ON PANEL 541AT, REPAIRED.
- [SDR MALA090019](https://openairdocs.org/sdr/MALA090019.md): Skin · dented · Feb 8, 2009 · N403XJ · Saab 340B · Trailing Edge Flaps
  > DENT LOCATED IN RT FLAP ASSY TOP SKIN 19.5 INCH FROM INBOARD EDGE, 3 INCHES FROM, AFT EDGE. REPAIRED
- [SDR MAL2008F00017](https://openairdocs.org/sdr/MAL2008F00017.md): Skin Panel · dented · Jul 23, 2008 · N403XJ · Saab 340B · Trailing Edge Flaps
  > THREE DENTS WERE FOUND ON RT FLAP UPPER SKIN PANEL 641AT FROM WS 94.5 TO WS 99. DENTS WERE REPAIRED IAW EOS57201. (S)
- [SDR MAL2008F00016](https://openairdocs.org/sdr/MAL2008F00016.md): Skin · damaged · Jul 23, 2008 · N403XJ · Saab 340B · Trailing Edge Flaps
  > DURING INSTALLATION OF RT FLAP DAMAGE OCCURRED TO THE LEADING EDGE AT WS 174.3. DAMAGE WAS REPAIRED IAW EO57204 AND EO57060. (S)
- [SDR MAL2008F00015](https://openairdocs.org/sdr/MAL2008F00015.md): Seat Track · corroded · Jul 23, 2008 · N403XJ · Saab 340B · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION NOTED ON I/B FWD SIDE OF CENTER SEAT TRACK BL 0 STA 297-STA 303.25. REPAIRED IAW EOS53342. (S)
- [SDR MAL2008F00014](https://openairdocs.org/sdr/MAL2008F00014.md): Structure · damaged · Jul 23, 2008 · N403XJ · Saab 340B · Trailing Edge Flaps
  > FLAP FAIRING AFT BULKHEAD UPPER FLANGE TO REAR SPAR FASTENERS. REPLACED IAW EOS57051. (S)
- [SDR MAL2008F00013](https://openairdocs.org/sdr/MAL2008F00013.md): Frame · damaged · Jul 23, 2008 · N403XJ · Saab 340B · Fuselage Main, Frame
  > UPPER FLANGE ON BOTTOM FUSELAGE FRAME STA 294, RBL 18.38. REPAIRED IAW EONRS53108. (S)
- [SDR MAL2008F00012](https://openairdocs.org/sdr/MAL2008F00012.md): Skin · dented · Jul 23, 2008 · N403XJ · Saab 340B · Emergency Exits
  > DENT NOTED ON FWD LT CORNER OUTER SKIN OF CREW ESCAPE HATCH. REPAIRED IAW EONRS52028. (S)
- [SDR MALA080052](https://openairdocs.org/sdr/MALA080052.md): Seal · loose · Mar 31, 2008 · N403XJ · Saab 340B · Overheat Detection
  > R TAILPIPE HOT INDICATION ON TAKEOFF CLIMB-OUT. RESEALED DETECTOR IAW SAAB MM 26-00-00, ALL CKS GOOD.
- [SDR MALA060565](https://openairdocs.org/sdr/MALA060565.md): Computer · malfunctioned · Sep 26, 2006 · N403XJ · Saab 340B · Attitude and Direction Data System
  > ON TAKEOFF AFTER GEAR CAME UP, THE VERBAL BANK ANGLE SOUNDED CONTINUOUSLY. QRH, PROBLEM REMAINS. ALSO THE YELLOW HDG FLAG ON EHSI CAME ON BOTH CAPTAIN AND FO'S DISPLAY. RESET IAW QRH, PROBLEM REMAINS. REMOVED AND REPLACED NR 1 AHRS COMPUTER. P/N ON/OFF 622-61
- [SDR MALA060520](https://openairdocs.org/sdr/MALA060520.md): Odor · detected · Aug 16, 2006 · N403XJ · Saab 340B · Air Distribution System
  > CREW REPORTED THAT AFTER THE START OF THE RIGHT ENGINE THE PAX AND FA COMPLAINED OF A BURNING SMELL IN THE CABIN. NO SMOKE WAS REPORTED. RAN ENGINE WITH LP, HP ON, ALL LIGHTS ON. NO BURNING SMELL NOTED. A/C GOOD FOR RETURN TO SERVICE.
- [SDR MALA060323](https://openairdocs.org/sdr/MALA060323.md): Skin · damaged · May 14, 2006 · N403XJ · Saab 340B · Ailerons
  > DURING 4K CHECK IN BNA FOUND RT AILERON LEAKING EDGE 651DB HAS MINOR COMPOSITE DAMAGE AND HAS BEEN REPAIRED IAW MESABA EO S51031.
- [SDR MALA060317](https://openairdocs.org/sdr/MALA060317.md): Seat Track · corroded · May 10, 2006 · N403XJ · Saab 340B · Fuselage, Seat/Cargo Attach Fittings
  > DURING 4K CHECK IN BNA FOUND SEAT TRACK AT BL 0 AT FS 297, PREVIOUS REPAIR IS CORRODED OUT OF LIMITS. THE PREVIOUS REPAIR HAS BEEN REMOVED AND REPLACED IAW MESABA EO S53342.
- [SDR MALA060316](https://openairdocs.org/sdr/MALA060316.md): Skin · dented · May 10, 2006 · N403XJ · Saab 340B · Fuselage Main, Plate/Skin
  > DURING 4K CHECK IN BNA FOUND RT FUSELAGE IS DENTED BETWEEN FS 319 AND 390 AND BETWEEN SL1616 AND SL1620. TWO EXTERNAL DOUBLERS HAVE BEEN INSTALLED IN THE AREA IAW MESABA EO S53005.
- [SDR MALA060308](https://openairdocs.org/sdr/MALA060308.md): Seat Track · corroded · May 8, 2006 · N403XJ · Saab 340B · Fuselage, Seat/Cargo Attach Fittings
  > DURING 4K CHECK IN BNA FOUND SEAT TRACK AT BL 0 BETWEEN FS 300 AND 339 IS CORRODED OUT OF LIMITS. THE DAMAGED TRACK HAS BEEN REPAIRED IAW MESABA EO S53342.
- [SDR MALA060307](https://openairdocs.org/sdr/MALA060307.md): Seat Track · corroded · May 8, 2006 · N403XJ · Saab 340B · Fuselage, Seat/Cargo Attach Fittings
  > DURING 4K CHECK IN BNA FOUND SEAT TRACK AT LBL 18.3, BETWEEN FS 300 AND 319 IS CORRODED OUT OF LIMITS. THE DAMAGED SEAT TRACK HAS BEEN REMOVED AND REPLACED IAW MESABA EO S53060.
- [SDR MALA050636](https://openairdocs.org/sdr/MALA050636.md): Frame · corroded · Aug 7, 2005 · N403XJ · Saab 340B · Fuselage Main, Frame
  > IRREGULAR ROUTING DUE TO AIRFRAME CORROSSION NOTED DURING ROUTINE MAINTENANCE. NO FURTHER INFORMATION AT THIS TIME.
- [SDR MALA050402](https://openairdocs.org/sdr/MALA050402.md): Sensor · dirty · Apr 29, 2005 · N403XJ · Saab 340B · Overheat Detection
  > ON TAKEOFF ROLL, THE RIGHT TAIL PIPE HOT LIGHT ILLUMINATED. CREW ABORTED TAKEOFF AT 70 KNTS WITH MINIMUM BRAKING. CLEANED SENSOR.
- [SDR MALA050403](https://openairdocs.org/sdr/MALA050403.md): Sensor · dirty · Apr 29, 2005 · N403XJ · Saab 340B · Overheat Detection
  > IN MEM, THE CREW ABORTED THE TAKEOFF DUE TO HIGH TAIL PIPE TEMPERATURE INDICATION. CLEANED SENSOR.
- [SDR MALA050390](https://openairdocs.org/sdr/MALA050390.md): Switch · broken · Apr 27, 2005 · N403XJ · Saab 340B · Engine Indicating System
  > AIR TURNBACK- CTOT SWITCH BROKE OFF AFTER TAKEOFF. REMOVED AND REPLACED CTOT PANEL P/N BOTH 7239060-503, S/N ON 872621, S/N OFF 0339 NEEDS OPS CHECK LB 9850. OPS CHECKED CTOT SYSTEM IAW AMM CH 71-00-00-5.
- [SDR MALA050130](https://openairdocs.org/sdr/MALA050130.md): Connector · loose · Jan 10, 2005 · N403XJ · Saab 340B · Power Indicating System
  > LEFT PROP NP INDICATION WENT TO ZERO WHEN PROPS WENT TO MAX ON FINAL. AFTER LANDING IT WENT BACK TO NORMAL. MAINTENANCE COULD NOT DUPLICATE PROBLEM. UPON INSPECTION OFF LEFT ENGINE YELLOW HARNESS FOUND CONNECTOR TO DECU EXTREMELY LOOSE AND CONNECTOR TO NP S
- [SDR MALA040590](https://openairdocs.org/sdr/MALA040590.md): Battery · discharged · Sep 9, 2004 · N403XJ · Saab 340B · Emergency Lighting
  > DURING SCHEDULED CAPACITY CHECK, BATTERY POWER SUPPLY P/N 3301-51, S/N 1317 FAILED CAPACITY CHECK. MAINTENANCE REPLACED BATTERY ASSEMBLY P/N 3301-31 AND UNIT PASSES CMM TESTS. A/C RETURNED TO SERVICE 9/15/04.
- [SDR MALA040372](https://openairdocs.org/sdr/MALA040372.md): Indicator · inoperative · Apr 29, 2004 · N403XJ · Saab 340B · Propeller Indication System
  > AFTER TAKEOFF LEFT PROP RPM INDICATOR INDICATED ZERO CYCLED C/B J-8, INDICATOR STILL INDICATED ZERO. WHILE RETURNING TO DTW INDICATOR WORKED INTERMITTENTLY. AIR RETURN TO DTW. MAINTENANCE REMOVED AND REPLACED GAUGE P/N 10223N01R00, S/N OFF 117, S/N ON BG05.
- [SDR MALA030573](https://openairdocs.org/sdr/MALA030573.md): Mount · corroded · Dec 14, 2003 · N403XJ · Saab 340B · Fuselage, Seat/Cargo Attach Fittings
  > DURING 4K INSPECTION IN LCQ, FWD LAV AFT I/B MOUNT HAS EVIDENCE OF CORROSION. MAINTENANCE REMOVED CORRODED LAV MOUNT, FABRICATED NEW MOUNT AND INSTALLED, IAW MESABA EO S25063, REV 0 DATED 19 DEC 2003. A/C RELEASE DATE 12/24/03.
- [SDR MALA030574](https://openairdocs.org/sdr/MALA030574.md): Seat Track · corroded · Dec 12, 2003 · N403XJ · Saab 340B · Fuselage, Seat/Cargo Attach Fittings
  > DURING 4K INSPECTION IN LCQ, FS 620 TO FS 686, LT BL 18.3 SEAT TRACK HAS CORROSION. MAINTENANCE REMOVED AND REPLACED CORRODED SEAT TRACK SECTION FROM FS 620 - FS 686 IAW MESABA EO A53060 DATED 3 NOV 2003. A/C RELEASE DATE 12/24/03.
- [SDR MALA030442](https://openairdocs.org/sdr/MALA030442.md): Power Lever · out of rig · Sep 30, 2003 · N403XJ · Saab 340B · Power Lever
  > DURING CLIMBOUT ON FLIGHT 2987, LT ENGINE WAS FIREWALLED FROM 17000 TO CRUISE ALTITUDE 22000. RAN APPROX 5 - 6 PERCENT LESS THAN CHARTED TORQUE. ITT WAS APPROXIMATELY 830-840. AIR RETURN TO MSP AS PER MXC, AND DISPATCH UNABLE TO MAKE CHARTED TORQUE POWER LE
- [SDR MALA020689](https://openairdocs.org/sdr/MALA020689.md): Battery · Dec 22, 2002 · N403XJ · Saab 340B · Emergency Equipment
  > DEAD EMERGENCY FLASHLIGHT BATTERIES. MAINTENANCE REPLACED BATTERY PN P4-01-0021. OPS CHECKS GOOD.
- [SDR MALA010604](https://openairdocs.org/sdr/MALA010604.md): Computer · failed · Aug 1, 2001 · N403XJ · Saab 340B · Integrated Flight System
  > DURING FLIGHT NR 2820, RT AHARS COMPUTER FAILED. AIR RETURN TO MSP. MAINTENANCE REMOVED AND REPLACED NR 2 AHRS COMPUTER P/N 622-6190-113, S/N ON 2247, S/N OFF 2788, SYSTEM OPS CHECK GOOD IAW SF340 MM CHAPTER 34.
- [SDR MALA010595](https://openairdocs.org/sdr/MALA010595.md): Actuator · faulty · Jul 20, 2001 · N403XJ · Saab 340B · Aileron Control System
  > DURING FLIGHT 3052 MAIN AILERON TRIM RUNAWAY. LEFT WING HAD STRONG DOWNLOAD FORCES. TRIM INDICATOR INDICATED FULL-UP ON INDICATOR, UNABLE TO NEUTRALIZE FORCES WITH MAIN TRIM STANDBY TRIM WORKED. AIR RETURN TO RHI. MAINTENANCE FOUND LT AILERON TRIM ACTUATOR
- [SDR MALA010565](https://openairdocs.org/sdr/MALA010565.md): Control Cable · chafed · Jun 30, 2001 · N403XJ · Saab 340B · Rudder Control System
  > FOUND DURING 4K-CHECK IN CWA, LT FUSELAGE AFT CIRCUIT I SINGLE RUDDER CABLE CHAFED. MAINTENANCE REMOVED CABLE AND INSTALLED NEW CABLE P/N 7227105-582 IAW SAAB MM 27-21.
- [SDR MALA010564](https://openairdocs.org/sdr/MALA010564.md): Control Cable · chafed · Jun 25, 2001 · N403XJ · Saab 340B · Rudder Control System
  > FOUND DURING 4K-CHECK IN CWA, RHOB FUSELAGE DUAL CIRCUIT I RUDDER CABLE CHAFED. MAINTENANCE REPLACED CABLE P/N 7227105-562 IAW SF340 27-21-25-4.
- [SDR MALA010563](https://openairdocs.org/sdr/MALA010563.md): Control Cable · chafed · Jun 25, 2001 · N403XJ · Saab 340B · Rudder Control System
  > FOUND DURING 4K-CHECK IN CWA, RHIB FUSELAGE DUAL CIRCUIT I RUDDER CABLE CHAFED. MAINTENANCE REPLACED RHIB FUSELAGE DUAL CIRCUIT RUDDER CABLE P/N 7227105-571 IAW SF340 27-21-25-4.
- [SDR MALA010562](https://openairdocs.org/sdr/MALA010562.md): Control Cable · chafed · Jun 25, 2001 · N403XJ · Saab 340B · Rudder Control System
  > FOUND DURING 4K-CHECK IN CWA, LHIB FUSELAGE DUAL CIRCUIT I RUDDER CABLES CHAFED. MAINTENANCE REPLACED LHIB FUSELAGE DUAL CIRCUIT RUDDER CABLE P/N 7227105-571 IAW SF340 27-21-25-4.
- [SDR MALA010561](https://openairdocs.org/sdr/MALA010561.md): Control Cable · chafed · Jun 25, 2001 · N403XJ · Saab 340B · Rudder Control System
  > FOUND DURING 4K-CHECK IN CWA, LHOB FUSELAGE DUAL CIRCUIT I RUDDER CABLE CHAFED. MAINTENANCE REPLACED LHOB FUSELAGE DUAL CIRCUIT RUDDER CABLE P/N 7227105-562, IAW SF340 27-21-25-4.
- [SDR MALA010560](https://openairdocs.org/sdr/MALA010560.md): Control Cable · chafed · Jun 24, 2001 · N403XJ · Saab 340B · Elevator Control System
  > FOUND DURING 4K-CHECK IN CWA, RHIB FUSELAGE ELEVATOR CABLE CHAFED. MAINTENANCE REMOVED AND REPLACED I/B CABLE P/N 7227705-644 IAW SF340A MM 27-31-15.
- [SDR MALA010559](https://openairdocs.org/sdr/MALA010559.md): Control Cable · chafed · Jun 24, 2001 · N403XJ · Saab 340B · Elevator Control System
  > FOUND DURING 4K-CHECK IN CWA, RHOB FWD FUSELAGE ELEVATOR CABLE CHAFED. MAINTENANCE REMOVED AND REPLACED RHOB CABLE P/N 7227105-712 IAW SF340A MM 27-31-15.
- [SDR MALA010558](https://openairdocs.org/sdr/MALA010558.md): Control Cable · chafed · Jun 24, 2001 · N403XJ · Saab 340B · Elevator Control System
  > FOUND DURING 4K-CHECK IN CWA, LHIB FWD FUSELAGE ELEVATOR CABLE CHAFED. MAINTENANCE REPLACED LHIB ELEVATOR CABLE P/N 7227705-644 IAW SF 340A MM 27-31-15, FOR RIGGING SEE 409 024307.
- [SDR MALA010557](https://openairdocs.org/sdr/MALA010557.md): Control Cable · chafed · Jun 24, 2001 · N403XJ · Saab 340B · Elevator Control System
  > FOUND DURING 4K-CHECK IN CWA, LHOB FWD FUSELAGE ELEVATOR CABLE CHAFED. MAINTENANCE REPLACED LHOB ELEVATOR CABLE P/N 7227105-712 IAW SF340 AMM 27-31-15 FOR RIGGING SEE 409 024307.
- [SDR MALA010556](https://openairdocs.org/sdr/MALA010556.md): Angle · corroded · Jun 24, 2001 · N403XJ · Saab 340B · Fuselage Miscellaneous Structure
  > Found during 4K-Check in CWA, Angle between Frame 237 and 258 is corroded. Maintenance installed new Angle at Frame 237 and 258. IAW Saab SRM 51 PN 7253721-447

Next page: https://openairdocs.org/deregistered/N403XJ-2019-06-07/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 n_number = 'N403XJ' AND deregistration_id = 'N403XJ-2019-06-07'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N403XJ-2019-06-07/reports

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