# Service difficulty reports: N110XJ, cancelled Jul 19, 2010

A list on [N110XJ, cancelled Jul 19, 2010](https://openairdocs.org/deregistered/N110XJ-2010-07-19.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 · 73 reports

- [SDR PNSA123](https://openairdocs.org/sdr/PNSA123.md): Switch · inoperative · Aug 2, 2009 · N110XJ · Saab 340B · Emergency Lighting
  > EMERGENCY LIGHTING SYSTEM "ARM" STATUS LIGHT ON FLIGHT ATTENDANT PANEL INOP. CAUSED BY AN INOPERATIVE EMERGENCY LIGHT SWITCH ON COCKPIT OVERHEAD PANEL.
- [SDR MAL2008F00052](https://openairdocs.org/sdr/MAL2008F00052.md): Wire · loose · Oct 1, 2008 · N110XJ · Saab SF340A · Light System Wiring
  > DURING INSPECTION EMERGENCY FLOOD LIGHT FOUND INOPERATIVE. FOUND DEFECTIVE SOLDER JOINT ON LAMP ASSY.
- [SDR PNSA070601](https://openairdocs.org/sdr/PNSA070601.md): Indicator · faulty · Jun 8, 2007 · N110XJ · Saab SF340A · Engine BMEP/Torque Indicating
  > RIGHT ENGINE ERRATIC TORQUE INDICATIONS ABORTED TAKEOFF. REMOVED AND REPLACED TORQUE INDICATOR.
- [SDR MALA050684](https://openairdocs.org/sdr/MALA050684.md): Power Supply · inoperative · Sep 1, 2005 · N110XJ · Saab SF340A · Emergency Lighting
  > CABIN EMERGENCY LIGHTS ASSOCIATED WITH POWER SUPPLIES 23LN & 21LN INOP. REPLACED SUPPLIES WITH SERVICEABLE UNITS. OPS CHECK GOOD.
- [SDR MALA050632](https://openairdocs.org/sdr/MALA050632.md): Frame · chafed · Aug 2, 2005 · N110XJ · Saab SF340A · Fuselage Main, Frame
  > DURING 4Y/2Y INSPECTION IN BNA, FRAME 686.888 RT SIDE OF FUSELAGE HAS BEEN CHAFED BY CARGO DOOR CABLE. DAMAGE HAS BEEN REPAIRED IAW MESABA EO#53308. REFER EAMS WORK ORDER #212691 TASK 2505.
- [SDR MALA050389](https://openairdocs.org/sdr/MALA050389.md): Battery Pack · inoperative · Apr 27, 2005 · N110XJ · Saab SF340A · Emergency Lighting
  > DURING LC1, NOTED LT AND RT AFT EXT EMERGENCY LIGHTS INOP. NOTED SEVERAL OTHER INT LIGHTS INOP ALSO. REMOVED AND REPLACED EMERGENCY SUPPLY AND BATTERY PACK 24LN. OPS CHECK GOOD. DOCUMENTED AND MM 409 237757.
- [SDR MALA050306](https://openairdocs.org/sdr/MALA050306.md): Skin · dented · Mar 28, 2005 · N110XJ · Saab SF340A · Horizontal Stabilizer, Plate/Skin
  > DURING 30/12 CYC CHECK IN BNA FOUND RIGHT LOWER HORIZONTAL STAB SKIN IS DENTED AND HAS BEEN REPAIRED IAW MESABA EO S55053. DAMAGE IS 2.1 INCHES AFT OF FRONT SPAR AND 13.3 INCHES FROM I/B EOP.
- [SDR MALA050175](https://openairdocs.org/sdr/MALA050175.md): Battery Pack · failed · Jan 27, 2005 · N110XJ · Saab SF340A · Emergency Lighting
  > BATTERY PACK 61-0478-9, S/N 1875. FAILED SCHEDULED CAPACITY CHECK. REPLACED BATTERY ASSEMBLY P/N 55-2198-1, UNIT PASSES, RTS 1/31/05.
- [SDR MALA050194](https://openairdocs.org/sdr/MALA050194.md): Wire · burned · Jan 22, 2005 · N110XJ · Saab SF340A · Light System Wiring
  > EMERGENCY POWER SUPPLY P/N 60-1321-1 S/N 16238 INSPECTION HAS BURNED WIRE INSIDE. REPAIRED GROUND WIRE. UNIT PASSES CMM CHECKS, RTS 1/25/05.
- [SDR MALA040909](https://openairdocs.org/sdr/MALA040909.md): Ice Shield · dented · Dec 20, 2004 · N110XJ · Saab SF340A · Fuselage Main, Plate/Skin
  > DENTS DISCOVERED ON RT ICE SHIELD. MAINTENANCE CARRIED OUT REPAIR IAW MESABA EO NR S53276. REFER TO LOG PAGE 1335862 FOR ADDITIONAL INFORMATION.
- [SDR MALA040489](https://openairdocs.org/sdr/MALA040489.md): Circuit Breaker · failed · Jul 14, 2004 · N110XJ · Saab SF340A · Pitot/Static Anti-Ice System
  > DURING FLIGHT L ALPHA LIGHT CAME ON, RAN QRH LIGHT STAYED ON. AIR RETURN TO DTW. MAINTENANCE REMOVED AND REPLACED CIRCUIT BREAKER 13 XA, ALL CHECKS GOOD IAW SF-340MM CH 24.
- [SDR MALA040418](https://openairdocs.org/sdr/MALA040418.md): Relay · failed · May 24, 2004 · N110XJ · Saab SF340A · AC Power Distribution System
  > AFTER DEPARTURE FROM MSP, CREW REPORTED RT AVIONICS FAILURE. AIR RETURN TO MSP. MAINTENANCE REPLACED RELAY 4PP RT AVIONICS BUSS. CHECKS GOOD IAW CHAP 24.
- [SDR MALA030530](https://openairdocs.org/sdr/MALA030530.md): Engine · malfunctioned · Dec 3, 2003 · N110XJ · Saab SF340A · Engine (Turbine/Turboprop)
  > DURING FLIGHT 3009, LT ENGINE SHOWING GRADUAL LOSS IN ITT MARGIN. LT ENGINE PLACED ON DERIVITIVE POWER FOR CONTINUED SERVICE. CTOT AND ANTI SKID SYSTEMS MUST BE OPERATIVE. MAINTENANCE PROCEDURES COMPLIED WITH FOR DERIVATIVE POWER PROGRAM. CHAP 2, SECTION 2
- [SDR MALA030521](https://openairdocs.org/sdr/MALA030521.md): Control Module · failed · Dec 2, 2003 · N110XJ · Saab SF340A · Air Intake Anti/De-Ice System
  > DURING FLIGHT 3183, LEFT INTAKE CAUTION LIGHT ILLUMINATES, MOVING POWER LEVER WILL EXTINGUISH LIGHT FOR APPROXIMATELY 2 MINUTES THEN COMES ON AGAIN. AIR RETURN TO MSP. MAINTENANCE REMOVED AND REPLACED DEICE CONTROL MODULE (LT) P/N44730-501, S/N OFF A0072, S/
- [SDR MALA030397](https://openairdocs.org/sdr/MALA030397.md): Computer · malfunctioned · Aug 29, 2003 · N110XJ · Saab SF340A · Propeller Indication System
  > AUTOCOURSEN LIGHT ILLUMINATED ON TAKEOFF ROLL. ABORTED TAKEOFF. REPLACED AUTOCOURSEN COMPUTER. P/N ON AND OFF 8542M2, SN/ON 504, S/N OFF 215
- [SDR MALA030156](https://openairdocs.org/sdr/MALA030156.md): Gcu · failed · Feb 14, 2003 · N110XJ · Saab SF340A · AC Generation System
  > DURING FLIGHT 3294, ON MISSED APPROACH RT AC GEN CAUTION LIGHT ILLUMINATED, RH AC GEN WAS UNABLE TO RESET AND WAS TURNED OFF PER QRH. AIRCRAFT IN ICING CONDITIONS FOR APPROXIMATELY 10 MINUTES WITH RH AC GEN OFFLINE. MAINTENANCE REPLACED GEN, DID NOT FIX, INST
- [SDR MALA020535](https://openairdocs.org/sdr/MALA020535.md): Hinge · lack of lube · Sep 4, 2002 · N110XJ · Saab SF340A · Ailerons
  > DURING FLIGHT 3321, WITH AUTO-PILOT OFF, A/C HARD TO TURN TO THE LEFT. MAINTENANCE PERFORMED REQUIRED AILERON CHECKS, ALL CHECKS GOOD. LUBRICATED AILERON HINGE POINTS, FREEDOM FORCE CHECK OF PILOTS AND F/O'S CONTROL COLUMN IS GOOD.
- [SDR MALA020400](https://openairdocs.org/sdr/MALA020400.md): Transmitter · malfunctioned · Jul 10, 2002 · N110XJ · Saab SF340A · Engine Oil Pressure
  > DURING CRUISE ON FLIGHT 3001, LT ENGINE MASTER WARNING LIGHT FLICKERED TWICE AT CRUISE. CREW NOTED LT PROP OIL PRESSURE DROPPED FROM NORMAL RANGE TO ZERO CAUSING MASTER WARNING LIGHT TO "FLICK" ON/OFF. ENGINE /PROP RAN FINE. LANDED WITHOUT INCIDENT. MAINTE
- [SDR MALA020401](https://openairdocs.org/sdr/MALA020401.md): Connector · failed · Jul 10, 2002 · N110XJ · Saab SF340A · Engine Oil Pressure
  > DURING FLIGHT 3084 LT PROP OIL PSI DROPPED TO ZERO AFTER START. A/C RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED PGB OIL PRESSURE TRANSMITTER CONNECTOR PLUG 15HE. ALL CHECKS GOOD IAW SF-340, MM CHAP. 79.
- [SDR MALA020372](https://openairdocs.org/sdr/MALA020372.md): Connector · arced · Jun 29, 2002 · N110XJ · Saab SF340A · Electrical Power System Wiring
  > FLIGHT ATTENDANT REPORTED SPARKS BEHIND FA PANEL. MX FOUND CONNECTOR PLUG ARCING TO SWITCHES. WRAPPED CONNECTOR PLUG WITH COMPRESSION TAPE. ALL CHECKS GOOD.
- [SDR MALA010792](https://openairdocs.org/sdr/MALA010792.md): Valve · failed · Dec 12, 2001 · N110XJ · Saab SF340A · Engine Anti-Icing System
  > DURING FLIGHT 2868 LT AIR VALVE LIGHT ILLUMINATED. AIR RETURN TO DTW. WEATHER CONDITIONS WARRANT THE RETURN. MAINTENANCE REMOVED AND REPLACED THE LT GARRET VALVE, (SWAPPED LEFT TO RIGHT AND PROBLEM FOLLOWED) IAW SAAB MM CH 75. OPS AND SECURITY CHECK GOOD.
- [SDR MALA010740](https://openairdocs.org/sdr/MALA010740.md): Seat Track · corroded · Sep 26, 2001 · N110XJ · Saab SF340A · Fuselage, Seat/Cargo Attach Fittings
  > DURING 4K-CHECK IN CWA, LT CENTER AISLE SEAT TRACK LBL 18.3 FWD PORTION OF FLOOR BOARD FLANGE HAS CORROSION, STARTING AT APPROXIMATELY STA 297. MAINTENANCE INSTALLED NEW SECTION OF SEAT TRACK ON LT CENTER AISLE IAW EO S53060 DATED 11-07-2000.
- [SDR MALA010739](https://openairdocs.org/sdr/MALA010739.md): Control Cable · broken · Sep 25, 2001 · N110XJ · Saab SF340A · Elevator Control System
  > DURING 4K-CHECK IN CWA, LT INBOARD AFT ELEVATOR CABLE HAS A BROKEN WIRE. MAINTENANCE REPLACED LT INBOARD AFT ELEVATOR CABLE P/N 7227215-946 IAW SF340 AMM 27-31-15-4.
- [SDR MALA010738](https://openairdocs.org/sdr/MALA010738.md): Control Cable · corroded · Sep 25, 2001 · N110XJ · Saab SF340A · Elevator Control System
  > DURING 4K-CHECK IN CWA, LT OUTBOARD AFT ELEVATOR CABLE CORRODED. MAINTENANCE REPLACED LT OUTBOARD AFT ELEVATOR CABLE P/N 7227215-841 IAW SF340 AMM 27-31-15-4.
- [SDR MALA010737](https://openairdocs.org/sdr/MALA010737.md): Control Cable · chafed · Sep 23, 2001 · N110XJ · Saab SF340A · Elevator Control System
  > DURING 4K-CHECK IN CWA, LT OUTBOARD FWD FUSELAGE ELEVATOR CABLE CHAFED. MAINTENANCE REMOVED AND REPLACED LT OUTBOARD FWD ELEVATOR CABLE P/N 7227105-712, IAW SF3 AMM 27-31-15.
- [SDR MALA010736](https://openairdocs.org/sdr/MALA010736.md): Control Cable · chafed · Sep 23, 2001 · N110XJ · Saab SF340A · Aileron Control System
  > DURING 4K-CHECK IN CWAM LT INBOARD AILERON FWD FUSELAGE CABLE IS CHAFED. MAINTENANCE INSTALLED NEW LT I/B FWD AILERON FUSELAGE CABLE P/N 7227105-623 IAW SAAB AMM 27-11-25.
- [SDR MALA010735](https://openairdocs.org/sdr/MALA010735.md): Control Cable · chafed · Sep 23, 2001 · N110XJ · Saab SF340A · Elevator Control System
  > DURING 4K-CHECK IN CWA, LT I/B ELEVATOR FWD FUSELAGE CABLE IS CHAFFED. MAINTENANCE REMOVED AND REPLACED LT I/B FWD FUSELAGE ELEVATOR CABLE PN7227705-644 IAW SF3 AMM 27-31-15.
- [SDR MALA010734](https://openairdocs.org/sdr/MALA010734.md): Control Cable · chafed · Sep 22, 2001 · N110XJ · Saab SF340A · Rudder Control System
  > DURING 4K-CHECK IN CWA, FOUND LT I/B FWD FUSELAGE RUDDER CIRCUIT 1 CABLE CHAFFED. MAINTENANCE REMOVED AND REPLACED LT I/B FWD FUSELAGE RUDDER PN 7227105-571 CIRCUIT 1 CABLE IAW SF3 AMM 27-21-25.
- [SDR MALA010733](https://openairdocs.org/sdr/MALA010733.md): Control Cable · chafed · Sep 21, 2001 · N110XJ · Saab SF340A · Rudder Control System
  > DURING 4K-CHECK IN CWA, RT O/B RUDDER SYSTEM CABLE OF DUAL CIRCUIT IS CHAFFED. MAINTENANCE INSTALLED SERVICEABLE RT O/B DUAL CIRCUIT CABLE PN 7227105-562 IAW SF340 AMM 27-21-25.
- [SDR MALA010732](https://openairdocs.org/sdr/MALA010732.md): Control Cable · chafed · Sep 21, 2001 · N110XJ · Saab SF340A · Rudder Control System
  > DURING 4K-CHECK IN CWA, FWD RT FUSELAGE RUDDER CIRCUIT AFT SINGLE CABLE IS CHAFFED. MAINTENANCE INSTALLED SERVICEABLE RT SINGLE AFT RUDDER CABLE PN 7227105-582 IAW SF340 AMM 27-21-25.
- [SDR MALA010731](https://openairdocs.org/sdr/MALA010731.md): Control Cable · chafed · Sep 21, 2001 · N110XJ · Saab SF340A · Aileron Control System
  > DURING 4K-CHECK IN CWA, LT O/B AILERON FWD WING CABLE IS CHAFFED. MAINTENANCE REMOVED AND REPLACED FWD LT O/B WING CABLE PN 7227151-522 IAW SAAB 340 AMM 27-11-25.
- [SDR MALA010730](https://openairdocs.org/sdr/MALA010730.md): Control Cable · chafed · Sep 19, 2001 · N110XJ · Saab SF340A · Aileron Control System
  > DURING 4K-CHECK IN CWA, RT O/B FWD AILERON WING CABLE IS CHAFED. MAINTENANCE REPLACED RT O/B FWD AILERON CABLE ASSEMBLY PN 7227151-522 IAW SAAB AMM 27-11-00-2.
- [SDR MALA010655](https://openairdocs.org/sdr/MALA010655.md): Probe · defective · Aug 21, 2001 · N110XJ · Saab SF340A · Engine Oil Temperature
  > DURING FLIGHT NR 3354, LT PROP OIL TEMP FLUCTUATES. AIR RETURN TO DTW. MAINTENANCE REPLACED LT ENGINE OIL TEMP PROBE IAW GE MM CHAP 79. REPLACED LT ENGINE OIL TEMP/PRESS INDICATOR IAW SAAB AMM CH 77. PERFORMED GROUND RUNS. ALL INDICATIONS NORMAL OIL QUANT
- [SDR MALA010647](https://openairdocs.org/sdr/MALA010647.md): Computer · failed · Aug 14, 2001 · N110XJ · Saab SF340A · Integrated Flight System
  > DURING FLIGHT 3372 AFTER TAKEOFF, YD OR AUTO-PILOT WOULD NOT STAY ENGAGED. F/O'S ADI SHOWED 8 DEGREE BANK TO LEFT IN STRAIGHT AND LEVEL. AIR RETURN TO MSP. MAINTENANCE REPLACED NR 2 AHRS COMPUTER P/N 622-6190-113, S/N OFF 9285, S/N ON 248. NR 2 AHRS, OPS C
- [SDR MALA010603](https://openairdocs.org/sdr/MALA010603.md): Battery · defective · Aug 1, 2001 · N110XJ · Saab SF340A · Battery/Charger System
  > DURING FLIGHT 2831, CREW REPORTED NO BATTERY START LIGHT WAS ON. AIR TURNBACK TO MSP. MAINTENANCE REMOVED AND REPLACED LT & RT BATTERY LT P/N 4078-7 SN/ON GO2561, RT P/N 4078-7 SN/ON EO2584 IAW TASK CARD 243401. OPS CHECK GOOD.
- [SDR MALA000748](https://openairdocs.org/sdr/MALA000748.md): Computer · failed · Dec 12, 2000 · N110XJ · Saab SF340A · Integrated Flight System
  > AFTER TAKEOFF FO'S EFIS WENT TO SKELETON MODE ON BOTH TUBES, ATT, PITCH, ROLL AND HDG FLAGS APPEARED, QRH COMPLETED -XSIDE DATA SELECTED. AIRCRAFT RETURNED TO MSP. MAINTENANCE COULD NOT DUPLICATE ON GROUND. REPLACED NR 2 AHRS AS PRECAUTIONARY MEASURE. SYST
- [SDR MALA000747](https://openairdocs.org/sdr/MALA000747.md): Computer · failed · Dec 9, 2000 · N110XJ · Saab SF340A · Attitude and Direction Data System
  > RED THEN YELLOW HEADING FLAG IN FLIGHT. AC RETURNED TO MSP. MAINTENANCE REPLACED NR 2 AHRS COMPUTER. OPS CHECKS GOOD IAW SF340 MM CHAP 34.
- [SDR MALA000672](https://openairdocs.org/sdr/MALA000672.md): Connector · contaminated · Nov 16, 2000 · N110XJ · Saab SF340A · Air Intake Anti/De-Ice System
  > RT INTAKE HEAT LIGHT ILLUMINATED AFTER TAKEOFF. AIRCRAFT RETURNED TO DTW DUE TO WEATHER. MAINTENANCE CLEANED OIL AT UPPER DUCT CANNON PLUG, GROUND RAN 30 MINUTES. ALL CHECKS GOOD. SEE 409 135155 FOR FURTHER DETAILS.
- [SDR MALA000447](https://openairdocs.org/sdr/MALA000447.md): Transmitter · failed · Jul 24, 2000 · N110XJ · Saab SF340A · Engine Oil Indicating System
  > LT PROP OIL PRESSURE FLUCUATES. AIR RETURN TO DTW. MAINTENANCE REPLACED LG PGD OIL TRANSMITTER. OPS CHECK GOOD.
- [SDR MALA976648](https://openairdocs.org/sdr/MALA976648.md): Skin · chafed · Dec 1, 1999 · N110XJ · Saab SF340A · Nacelle/Pylon, Plate/Skin
  > DURING HEAVY CHECK INSPECTION FOUND RIGHT INBOARD NACELLE SKIN CHAFED. MAINTENANCE PERFORMED PERMENANT REPAIR IAW EO NR S54022.
- [SDR MALA976647](https://openairdocs.org/sdr/MALA976647.md): Skin · chafed · Dec 1, 1999 · N110XJ · Saab SF340A · Nacelle/Pylon, Plate/Skin
  > DURING HEAVY CHECK INSPECTION FOUND CHAFED SKIN ON LEFT INBOARD NACELLE SKIN. MAINTENANCE PERFORMED PERMANENT REPAIR IAW EO NR S54021.
- [SDR MALA976646](https://openairdocs.org/sdr/MALA976646.md): Seat Track · corroded · Nov 20, 1999 · N110XJ · Saab SF340A · Fuselage, Seat/Cargo Attach Fittings
  > DURING HEAVY CHECK INSPECTION, FOUND CENTER FORWARD SEAT TRACK CORRODED FROM STA 297 TO 357. MAINTENANCE REPAIRED BY COMPLETING SEAT TRACK SPLICE REPAIR PER IAW EO NR S53060.
- [SDR MALA976593](https://openairdocs.org/sdr/MALA976593.md): Power Supply · inop · Oct 5, 1999 · N110XJ · Saab SF340A · Emergency Lighting
  > EMERGENCY LIGHTS ON WHEN SWITCHED IN ARMED POSITION. MAINTENANCE REPLACED POWER SUPPLY 20LN. OPS CHECKS GOOD.
- [SDR MALA976577](https://openairdocs.org/sdr/MALA976577.md): Transducer · failed · Sep 21, 1999 · N110XJ · Saab SF340A · Engine Oil Pressure
  > AFTER TAKEOFF, LEFT PROP OIL INCREASED TO 150 PSI. CREW BEGAN QRH PROCEDURES AND LEFT RPM BEGAN TO FLUCTUATE AND LEFT PROP PSI BEGAN TO INCREASE. CREW ACCOMPLISHED ENGINE SHUTDOWN AS PER QRH AND LANDED IN CWA. MAINTENANCE FOUND GAUGE STUCK AT 160 PSI, REMOV
- [SDR MALA976575](https://openairdocs.org/sdr/MALA976575.md): Gauge · failed · Sep 16, 1999 · N110XJ · Saab SF340A · Engine Oil Pressure
  > WHILE EN ROUTE AT 16,000 FT, NOTICED THE LEFT PROP OIL PRESSURE INDICATING 160 PSI, COMPLETED QRH. MONITORED PROP OIL PRESSURE WAS FLUCTUATING UP TO 190 PSI. DIVERTED TO MKG. MAINTENANCE INSPECTED LT PGB OIL SYSTEM, RAN A/C AT HIGH POWER SETTING TO DUPLICAT
- [SDR MALA976494](https://openairdocs.org/sdr/MALA976494.md): Weu · failed · May 30, 1999 · N110XJ · Saab SF340A · Smoke Detection
  > CARGO SMOKE ANNUN ILLUMINATED SIX MINUTES AFTER TAKEOFF AROUND 6000 FEET. ILLUMINATED INTERMITTENTLY FOUR TIMES THEN REMAINED OFF FOR THE REMAINING TRIP BACK TO DTW. MAINTENANCE REPLACED WEU. ALL WORK DONE IAW SAAB 340 MM. ALL CHECKS GOOD.
- [SDR MALA976493](https://openairdocs.org/sdr/MALA976493.md): Smoke Detector · contaminated · May 29, 1999 · N110XJ · Saab SF340A · Smoke Detection
  > CARGO SMOKE ANNUN ILLUMINATED, DURING GROUND OPERATIONS. RETURNED TO GATE. MAINTENANCE REPLACED CARGO SMOKE DETECTOR, SUSPECTED ANTS IN DETECTOR CAUSING FAULT. OPS CHECK GOOD.
- [SDR MALA976446](https://openairdocs.org/sdr/MALA976446.md): Valve · failed · May 7, 1999 · N110XJ · Saab SF340A · Engine Start Valves/Controls
  > RIGHT INTAKE LIGHT ILLUMINATED IN FLIGHT. AIRCRAFT RETURNED TO MSP. MAINTENANCE CANNOT DUPLICATE PROBLEM. FOLLOWING FLIGHT REPLACED START AIR VALVE IAW CT7 MM 75-00-00 PG 403-404 A/B, OPS CHECK GOOD.
- [SDR MALA976414](https://openairdocs.org/sdr/MALA976414.md): Swivel · leaking · Mar 30, 1999 · N110XJ · Saab SF340A · Hydraulic System, Main
  > AFTER TAKEOFF FROM FORT DODGE, GEAR WAS SELECTED UP FOLLOWED BY A HYDRAULIC CAUTION LIGHT, HYDRAULIC QUANTITY WAS NEAR RED LINE AND MAIN ACCUMULATOR WAS AT ZERO. CREW FOLLOWED QRH, UPON ARRIVAL AND SHUTDOWN IN MCW, NOTED HYDRAULIC FLUID PUDDLING UNDER RIGHT M
- [SDR MALA976410](https://openairdocs.org/sdr/MALA976410.md): Bulb · failed · Mar 29, 1999 · N110XJ · Saab SF340A · Emergency Lighting
  > DURING INSPECTION 4C, EMERGENCY LIGHT INOP. REPLACED LAMP, OPS CHECK GOOD.

Next page: https://openairdocs.org/deregistered/N110XJ-2010-07-19/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 = 'N110XJ' AND deregistration_id = 'N110XJ-2010-07-19'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N110XJ-2010-07-19/reports

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