# N403XJ: Saab-Scania SAAB 340B, registration cancelled 2019-06-07

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: June 7, 2019
- Exported to: Australia
- Status when cancelled: Valid registration
- Airframe: [Saab-Scania SAAB 340B](https://openairdocs.org/model/saab-scania-saab-340b) (registry code 7860101)
- Engine: [GE CT7-SER series](https://openairdocs.org/engine/ge-ct7-ser-series) (registry code 30031)
- Data sheets: [TCDS A52EU](https://openairdocs.org/tcds/A52EU) (OpenAirDocs)
- Serial number: 340B-403
- Year built: 0
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: October 30, 1996
- Certificate issued: May 21, 2010
- Last registry action: December 22, 2016
- Mode S code: A4B9DC
- Owner when cancelled: [US Bank Na Trustee](https://openairdocs.org/faa-owner/US%20BANK%20NA%20TRUSTEE)
- Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington)
- Owner type: Corporation
- Owner's area on the map: 39.7236° N, 75.5412° W: Placed by OpenAirDocs at the center of ZIP code 19801, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N403XJ
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=403XJ
- Page: https://openairdocs.org/deregistered/N403XJ-2019-06-07

From the FAA registry file of October 29, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Saab-Scania SAAB 340B: https://openairdocs.org/model/saab-scania-saab-340b.md

## Service difficulty reports (72, newest 50)

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

- [SDR PNSA2015070201](https://openairdocs.org/sdr/PNSA2015070201), Jul 2, 2015: POWER SUPPLY. NO TEST. 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 
- [SDR PNSA2014121802](https://openairdocs.org/sdr/PNSA2014121802), Dec 18, 2014: WIRE. DAMAGED. 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), Nov 25, 2014: WARNING SYSTEM. FALSE ACTIVATION. CARGO SMOKE LIGHT ON CWP ILLUMINATED INFLIGHT THEN CARGO, LAVATORY & AVIONICS LIGHTS ILLUMINATED ON SHUTDOWN. PERFORMED CONTINUITY CHECKS ON SYSTEM'S WIRING, NO
- [SDR PNSA2014082003](https://openairdocs.org/sdr/PNSA2014082003), Aug 20, 2014: LIGHT. INOPERATIVE. FLIGHT ATTENDANT PANEL EMERGENCY LIGHTING ARM LIGHT INOPERATIVE. RE-LAMPED THE ARM LIGHT. OPERATIONS CHECKED GOOD.
- [SDR PNSA2014062102](https://openairdocs.org/sdr/PNSA2014062102), Jun 21, 2014: CONNECTOR. LOOSE. 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), May 14, 2014: LIGHT. INOPERATIVE. FLIGHT ATTENDANT PANEL EMERGENCY LIGHTS ARM DOES NOT ILLUMINATE WHEN ARMED.
- [SDR PNSA2014031102](https://openairdocs.org/sdr/PNSA2014031102), Mar 11, 2014: RELAY. FAILED. RIGHT INTAKE LIGHT REMAINS ON. R & R RIGHT INTAKE HEAT AC POWER RELAY.
- [SDR PNSA2014020401](https://openairdocs.org/sdr/PNSA2014020401), Feb 4, 2014: TRANSCEIVER. FAILED. NR 2 COM BLACKED OUT, STUCK ON ONE FREQUENCY INSTALLED SERVICABLE NR 2 COM.
- [SDR PNSA2013081707](https://openairdocs.org/sdr/PNSA2013081707), Aug 17, 2013: LAMP. INOPERATIVE. FOUND ARM LIGHT BURNED OUT DURING EMERGENCY LIGHTING TEST. REPLACED LAMP, OPS CHECKED GOOD.
- [SDR PNSA2013060501](https://openairdocs.org/sdr/PNSA2013060501), Jun 5, 2013: LIGHT. INOPERATIVE. 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), Mar 27, 2013: POWER SUPPLY. FAILED. 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 
- [SDR MALA090020](https://openairdocs.org/sdr/MALA090020), Feb 8, 2009: SKIN. DENTED. DENT LOCATED IN LT FLAP ASSY 38.5 INCHES OUTBOARD FROM INBOARD EDGE ON PANEL 541AT, REPAIRED.
- [SDR MALA090019](https://openairdocs.org/sdr/MALA090019), Feb 8, 2009: SKIN. DENTED. 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), Jul 23, 2008: SKIN PANEL. DENTED. 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), Jul 23, 2008: SKIN. DAMAGED. 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), Jul 23, 2008: SEAT TRACK. CORRODED. 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), Jul 23, 2008: STRUCTURE. DAMAGED. FLAP FAIRING AFT BULKHEAD UPPER FLANGE TO REAR SPAR FASTENERS. REPLACED IAW EOS57051. (S)
- [SDR MAL2008F00013](https://openairdocs.org/sdr/MAL2008F00013), Jul 23, 2008: FRAME. DAMAGED. UPPER FLANGE ON BOTTOM FUSELAGE FRAME STA 294, RBL 18.38. REPAIRED IAW EONRS53108. (S)
- [SDR MAL2008F00012](https://openairdocs.org/sdr/MAL2008F00012), Jul 23, 2008: SKIN. DENTED. DENT NOTED ON FWD LT CORNER OUTER SKIN OF CREW ESCAPE HATCH. REPAIRED IAW EONRS52028. (S)
- [SDR MALA080052](https://openairdocs.org/sdr/MALA080052), Mar 31, 2008: SEAL. LOOSE. 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), Sep 26, 2006: COMPUTER. MALFUNCTIONED. 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 
- [SDR MALA060520](https://openairdocs.org/sdr/MALA060520), Aug 16, 2006: ODOR. DETECTED. 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 
- [SDR MALA060323](https://openairdocs.org/sdr/MALA060323), May 14, 2006: SKIN. DAMAGED. 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), May 10, 2006: SEAT TRACK. CORRODED. 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 MESA
- [SDR MALA060316](https://openairdocs.org/sdr/MALA060316), May 10, 2006: SKIN. DENTED. 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 I
- [SDR MALA060308](https://openairdocs.org/sdr/MALA060308), May 8, 2006: SEAT TRACK. CORRODED. 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), May 8, 2006: SEAT TRACK. CORRODED. 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 
- [SDR MALA050636](https://openairdocs.org/sdr/MALA050636), Aug 7, 2005: FRAME. CORRODED. IRREGULAR ROUTING DUE TO AIRFRAME CORROSSION NOTED DURING ROUTINE MAINTENANCE. NO FURTHER INFORMATION AT THIS TIME.
- [SDR MALA050402](https://openairdocs.org/sdr/MALA050402), Apr 29, 2005: SENSOR. DIRTY. 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), Apr 29, 2005: SENSOR. DIRTY. IN MEM, THE CREW ABORTED THE TAKEOFF DUE TO HIGH TAIL PIPE TEMPERATURE INDICATION. CLEANED SENSOR.
- [SDR MALA050390](https://openairdocs.org/sdr/MALA050390), Apr 27, 2005: SWITCH. BROKEN. 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. OP
- [SDR MALA050130](https://openairdocs.org/sdr/MALA050130), Jan 10, 2005: CONNECTOR. LOOSE. 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 INSPEC
- [SDR MALA040590](https://openairdocs.org/sdr/MALA040590), Sep 9, 2004: BATTERY. DISCHARGED. 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 PA
- [SDR MALA040372](https://openairdocs.org/sdr/MALA040372), Apr 29, 2004: INDICATOR. INOPERATIVE. 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
- [SDR MALA030573](https://openairdocs.org/sdr/MALA030573), Dec 14, 2003: MOUNT. CORRODED. 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 ME
- [SDR MALA030574](https://openairdocs.org/sdr/MALA030574), Dec 12, 2003: SEAT TRACK. CORRODED. 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 - F
- [SDR MALA030442](https://openairdocs.org/sdr/MALA030442), Sep 30, 2003: POWER LEVER. OUT OF RIG. 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 APPROXI
- [SDR MALA020689](https://openairdocs.org/sdr/MALA020689), Dec 22, 2002: BATTERY. DEAD EMERGENCY FLASHLIGHT BATTERIES. MAINTENANCE REPLACED BATTERY PN P4-01-0021. OPS CHECKS GOOD.
- [SDR MALA010604](https://openairdocs.org/sdr/MALA010604), Aug 1, 2001: COMPUTER. FAILED. 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 2
- [SDR MALA010595](https://openairdocs.org/sdr/MALA010595), Jul 20, 2001: ACTUATOR. FAULTY. DURING FLIGHT 3052 MAIN AILERON TRIM RUNAWAY. LEFT WING HAD STRONG DOWNLOAD FORCES. TRIM INDICATOR INDICATED FULL-UP ON INDICATOR, UNABLE TO NEUTRALIZE FORCES W
- [SDR MALA010565](https://openairdocs.org/sdr/MALA010565), Jun 30, 2001: CONTROL CABLE. CHAFED. 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 M
- [SDR MALA010564](https://openairdocs.org/sdr/MALA010564), Jun 25, 2001: CONTROL CABLE. CHAFED. 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), Jun 25, 2001: CONTROL CABLE. CHAFED. 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
- [SDR MALA010562](https://openairdocs.org/sdr/MALA010562), Jun 25, 2001: CONTROL CABLE. CHAFED. 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 IA
- [SDR MALA010561](https://openairdocs.org/sdr/MALA010561), Jun 25, 2001: CONTROL CABLE. CHAFED. 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, IA
- [SDR MALA010560](https://openairdocs.org/sdr/MALA010560), Jun 24, 2001: CONTROL CABLE. CHAFED. 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), Jun 24, 2001: CONTROL CABLE. CHAFED. 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), Jun 24, 2001: CONTROL CABLE. CHAFED. 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 RIG
- [SDR MALA010557](https://openairdocs.org/sdr/MALA010557), Jun 24, 2001: CONTROL CABLE. CHAFED. 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 RIGGI
- [SDR MALA010556](https://openairdocs.org/sdr/MALA010556), Jun 24, 2001: ANGLE. CORRODED. 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

All 72: https://openairdocs.org/deregistered/N403XJ-2019-06-07/reports.md

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB MIA02LA134](https://openairdocs.org/ntsb/MIA02LA134), Jul 16, 2002: Saab-Scania SF340B (N403XJ), Tupelo, MS, no damage. Probable cause: The failure of the ground agent to follow procedures and directives and to maintain a visual lookout due to a diversion of attention caused by paperwork being sucked toward the rotating propeller,…

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Accident 20020716016819A](https://openairdocs.org/incident/20020716016819A), Jul 16, 2002: Saab 340B (N403XJ), Tupelo, MS. (-23) Ground handler lost grip on paperwork and was chasing the documents when her right hand made contact with the left prop, severing the right thumb, index…

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