# Service difficulty reports: N416XJ, cancelled Nov 18, 2015

A list on [N416XJ, cancelled Nov 18, 2015](https://openairdocs.org/deregistered/N416XJ-2015-11-18.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 · 68 reports

- [SDR MALA090095](https://openairdocs.org/sdr/MALA090095.md): Battery Pack · discharged · Jul 8, 2009 · N416XJ · Saab 340B · Emergency Lighting
  > EMERGENCY LIGHT BATTERY PACK 23LN LOW. REMOVED AND REPLACED 23LN IAW AMM 33-50-10-04-01. OPS CHECK GOOD, IAW JC NR 335003.
- [SDR MALA090094](https://openairdocs.org/sdr/MALA090094.md): Battery Pack · discharged · Jul 8, 2009 · N416XJ · Saab 340B · Emergency Lighting
  > EMERGENCY LIGHT BATTERY PACK 21LN LOW. REMOVED AND REPLACED 21LN IAW AMM 33-50-10-04-01. OPS CHECK GOOD, IAW JC NR 335003, PN ON/OFF 3301-51 SN OFF 1405, SN ON 1455.
- [SDR MALA090080](https://openairdocs.org/sdr/MALA090080.md): Warning System · false activation · Jun 6, 2009 · N416XJ · Saab 340B · Fire Detection
  > ON TAKEOFF RT TAILPIPE HOT LIGHT CAME ON. RAN QRH ALL ENGINE PARAMETERS WERE NORMAL. PERFORMED VISUAL INSPECTION OF RT TAIL PIPE HOT DETECTION CONNECTORS, HARNESS AND DETECTORS. NO DEFECTS NOTED. RAN AIRCRAFT AND PERFORMED OPERATIONAL TEST OF ENG NACELLE F
- [SDR MAL2008F00018](https://openairdocs.org/sdr/MAL2008F00018.md): Motor · malfunctioned · Jul 25, 2008 · N416XJ · Saab 340B · Cabin Cooling System
  > F/A REPORTS STRONG ODOR IN CABIN AGAIN. SMELLS LIKE AN ELECTRICAL SMELL. NOTED STRONG ELECTRICAL SMELL COMING FROM BURNT UP SUPP AIR MOTOR. SYSTEM ON MEL (INOP). RAN ACFT SYSTEMS. NO FURTHER ELECTRICAL SMELL. (S)
- [SDR MALA070182](https://openairdocs.org/sdr/MALA070182.md): Skin · dented · Oct 16, 2007 · N416XJ · Saab 340B · Fuselage Main, Plate/Skin
  > SEVERAL DENTS WERE FOUND IN THE RT FUSELAGE SKIN, IN THE ICE GUARD AREA LOCATED FROM STA 313 AND STA 321, BETWEEN STRINGERS SL1615 AND SL 1622. DOUBLER/TRIPLER INSTALLED IAW EO NR S53494.
- [SDR MALA070016](https://openairdocs.org/sdr/MALA070016.md): Power Supply · inoperative · Jan 22, 2007 · N416XJ · Saab 340B · Emergency Lighting
  > DURING LC2 NOTED EMERGENCY LIGHTS FROM BATTERY PACK 24LN INOP. REMOVED AND REPLACED POWER SUPPLY 24LN PN 3301-51, SN ON 2205, SN OFF 2129.
- [SDR MALA060632](https://openairdocs.org/sdr/MALA060632.md): Battery Pack · no test · Dec 22, 2006 · N416XJ · Saab 340B · Emergency Lighting
  > FAILED CAP CHECK PER BF GOODRICH C.M.M.W.O. 417138. REPLACED BATTERY PACK.
- [SDR MALA060503](https://openairdocs.org/sdr/MALA060503.md): Wire · chafed · Aug 4, 2006 · N416XJ · Saab 340B · Communications System Wiring
  > EMERGENCY CALL LIGHT ON PILOTS OVERHEAD PANEL WAS INOP WHEN EMERGENCY CALL BUTTON WAS PUSHED. LAMP TEST OK. FOUND WIRE RY63-24 CHAFED ALMOST THROUGH. REPLACED WIRE RY63-24 FROM CONNECTOR 91VPP9 TO RESISTOR 10RY.
- [SDR MALA060479](https://openairdocs.org/sdr/MALA060479.md): Engine · making metal · Jul 18, 2006 · N416XJ · Saab 340B · Engine (Turbine/Turboprop)
  > RT CHIP DETECT LIGHT ILLUMINATED INTERMITTENT. AIR RETURNED. CHANGED ENGINE.
- [SDR MALA060332](https://openairdocs.org/sdr/MALA060332.md): Skin · damaged · May 19, 2006 · N416XJ · Saab 340B · Ailerons
  > HAIL CONTACT DAMAGE ON LT AILERON 33 1/4" OB ON LEADING EDGE 2" AFT OF LEADING EDGE AND ALSO AT STA 390.82, 2" FROM AILERON TRAILING EDGE. DAMAGE REPAIRED IAW EOS#51031.
- [SDR MALA060313](https://openairdocs.org/sdr/MALA060313.md): Skin · dented · May 9, 2006 · N416XJ · Saab 340B · Horizontal Stabilizer, Plate/Skin
  > HAIL CONTACT DAMAGE ON LEFT HORIZONTAL STABILIZER CAUSED DENT IN UPPER ALUMINUM SKIN AT HS113,.025 INCH DEEP AND.703 INCH DIAMETER. LOCATED 6.5 INCHES AFT OF FWD EDGE OF SKIN PANEL. DAMAGE REPAIRED WITH BONDED DOUBLER IAW SAAB SRM SECTION 55-10-10 AND MESA
- [SDR MALA060288](https://openairdocs.org/sdr/MALA060288.md): Skin · dented · Apr 28, 2006 · N416XJ · Saab 340B · Horizontal Stabilizer, Plate/Skin
  > HAIL CONTACT DAMAGE ON RIGHT HORIZONTAL STABILIZER CAUSED DENT IN UPPER ALUMINUM SKIN AT HS 38.58,.022 INCH DEEP AND 1.0 INCH DIAMETER. LOCATED 6.5 INCHES FORWARD OF ELEVATOR LEADING EDGE. DAMAGE REPAIRED WITH BONDED DOUBLER IAW SAAB SRM SECTION SRM SECTION
- [SDR MALA060287](https://openairdocs.org/sdr/MALA060287.md): Skin · dented · Apr 28, 2006 · N416XJ · Saab 340B · Horizontal Stabilizer, Plate/Skin
  > HAIL CONTACT DAMAGE ON RIGHT HORIZONTAL STABILIZER CAUSED DENT IN UPPER ALUMINUM SKIN AT HS99.92,.025 INCH DEEP AND 0.640 INCH DIAMETER. LOCATED 11.5 INCHES FROM LEADING EDGE AND 36 INCHES FROM OB ELEVATOR HINGE POINT. DAMAGED REPAIRED WITH BONDED DOUBLER IA
- [SDR MALA060080](https://openairdocs.org/sdr/MALA060080.md): Skin · lightning strike · Feb 16, 2006 · N416XJ · Saab 340B · Fuselage Main, Plate/Skin
  > ON CLIMBOUT FROM DTW A/C STRUCK BY LIGHTNING. THE STRIKE APPEARED TO HIT NEAR CAPTAIN'S SIDE AROUND PITOT TUBE AREA. ALL INSTRUMENTS FINE. AIR RETURNED TO DTW. COMPLETED LIGHTNING STRIKE INSPECTION PER JC 055-303. ALL CHECKS GOOD.
- [SDR MALA050483](https://openairdocs.org/sdr/MALA050483.md): Warning Light · illuminated · Jun 19, 2005 · N416XJ · Saab 340B · Air Intake Anti/De-Ice System
  > CREW RETURNED TO MSP FOLLOWING INDICATION OF DUCT OVER TEMPERATURE INDICATION. NO EMERGENCY DECLARED AND FLIGHT RETURNED TO GATE WITHOUT FURTHER INCIDENT. NO FURTHER INFORMATION AT THIS TIME.
- [SDR MALA050384](https://openairdocs.org/sdr/MALA050384.md): Floor Support · corroded · Apr 26, 2005 · N416XJ · Saab 340B · Fuselage Miscellaneous Structure
  > AIRSTAIR FLOOR RAIL, P/N 7253710-871 IS CORRODED AND WILL BE REPLACED IAW SRM 51-40-21/22.
- [SDR MALA050388](https://openairdocs.org/sdr/MALA050388.md): Skin · dented · Apr 25, 2005 · N416XJ · Saab 340B · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN IS DENTED BETWEEN FS 339 AND FS 363 AND BETWEEN STRINGER'S SL1504 AND SL1506. THE DENTS ARE OUT OF LIMITS AND HAVE BEEN REPAIRED IAW MESABA EO S53009.
- [SDR MALA050386](https://openairdocs.org/sdr/MALA050386.md): Structure · corroded · Apr 25, 2005 · N416XJ · Saab 340B · Fuselage Miscellaneous Structure
  > LEFT WRAP AROUND P/N 7253711-245 IS CORRODED AND HAS BEEN REPLACED IAW SRM 51-40-21.
- [SDR MALA050385](https://openairdocs.org/sdr/MALA050385.md): Structure · corroded · Apr 25, 2005 · N416XJ · Saab 340B · Fuselage Miscellaneous Structure
  > RIGHT WRAP AROUND P/N 7253710243 IS CORRODED AND HAS BEEN REPAIRED IAW SRM 51-40-21.
- [SDR MALA050387](https://openairdocs.org/sdr/MALA050387.md): Seat Track · corroded · Apr 23, 2005 · N416XJ · Saab 340B · Fuselage, Seat/Cargo Attach Fittings
  > GALLEY SEAT TRACK HAD PROFILE P/N'S 7253721-459 AND 7253721-495 ARE CORRODED AND HAVE BEEN REPLACED IAW SRM 51-40-21 AND 51-40-22.
- [SDR MALA050311](https://openairdocs.org/sdr/MALA050311.md): Engine · malfunctioned · Apr 2, 2005 · N416XJ · Saab 340B · Engine (Turbine/Turboprop)
  > LT ENGINE OIL PRESSURE LIGHT ILLUMINATED AND GAUGE WAS READING LOW (ABOUT 25-30 PSI) ON TAKEOFF. CREW FOLLOWED QRH BUT DID NOT SHUT DOWN ENGINE. AIR RETURNED. REMOVED AND REPLACED LT ENGINE.
- [SDR MALA050107](https://openairdocs.org/sdr/MALA050107.md): Warning Light · illuminated · Jan 5, 2005 · N416XJ · Saab 340B · DC Power Distribution System
  > LT MAIN AND ESS BUSS BREAKER POPPED INFLIGHT. AIR RETURN TO DTW. MAINTENANCE RAN BOTH ENGINES, APPLIED HEAVY LOAD ON PDU. NO FAULTS NOTED. REFER TO LOG PG NR 1276924-4 FOR ADDITIONAL INFORMATION.
- [SDR MALA040571](https://openairdocs.org/sdr/MALA040571.md): Control Unit · malfunctioned · Sep 13, 2004 · N416XJ · Saab 340B · Cabin Pressure Control System
  > LOST PRESSURIZATION AT 25,000 FT DESCENDED TO 10,000 FT NOTE CABIN ALTITUDE FOLLOWED TO -1. FOUND C/B G7 POPPED. RESET, SWITCHED TO MANUAL MODE, FOUND IT CONTROLLED PRESSURIZATION SYSTEM. MAINTENANCE REPLACED PRESSURIZATION CONTROL UNIT.
- [SDR MALA040568](https://openairdocs.org/sdr/MALA040568.md): Charger · inoperative · Sep 7, 2004 · N416XJ · Saab 340B · Emergency Equipment
  > CABIN EMERGENCY FLASHLIGHT INOP. MAINTENANCE REPLACED HOLDER.
- [SDR MALA040385](https://openairdocs.org/sdr/MALA040385.md): Generator · failed · May 7, 2004 · N416XJ · Saab 340B · AC Generation System
  > DURING TAXI OUT, LT AC GEN FAILED TO COME ON LINE. PAX REPORTED SMOKE AND FLAMES EXIT A/C OF EXHAUST HOLE. A/C RETURNED TO GATE. MAINTENANCE REPLACED LT AC GEN. ALL CHECKS GOOD DONE IAW SF340MM CHAP 24.
- [SDR MALA040343](https://openairdocs.org/sdr/MALA040343.md): Engine · overtemp · Apr 24, 2004 · N416XJ · Saab 340B · Engine (Turbine/Turboprop)
  > LEFT ENGINE OVER TEMPED INFLIGHT. CLIMBING THROUGH 8000 FT LEFT ENG FAILED APPEARED TO HAVE COMPRESSOR STALL. TORQUE WAS LESS THAN 10 PERCENT ITT WAS 1200-1300C (QRH COMPLETE WITH SHUTDOWN ENG) AIR RETURN TO MSP. REMOVED AND REPLACED ENG IAW JC 7100-301. P
- [SDR MALA020546](https://openairdocs.org/sdr/MALA020546.md): Structure · corroded · Sep 3, 2002 · N416XJ · Saab 340B · Fuselage Miscellaneous Structure
  > DURING 4K-INSPECTION IN CWA, LT FWD SEAT TRACK WRAP AROUND HAS HEAVY CORROSION AT STA 294. MAINTENANCE INSTALLED NEW WRAP AROUND.
- [SDR MALA020539](https://openairdocs.org/sdr/MALA020539.md): Angle · Sep 2, 2002 · N416XJ · Saab 340B · Fuselage Miscellaneous Structure
  > DURING 4K-INSPECTION IN CWA, CARGO FLOOR ANGLE BETWEEN AFT CENTER AISLE SEAT TRACK HAS CORROSION. MAINTENANCE REMOVED AND REPLACED NEW ANGLE IAW SRM CHAP 51. RELEASE DATE 9/4/02. REF 409 # 138436 FOR DETAIL.
- [SDR MALA020547](https://openairdocs.org/sdr/MALA020547.md): Seat Track · corroded · Sep 1, 2002 · N416XJ · Saab 340B · Fuselage Miscellaneous Structure
  > DURING 4K-INSPECTION IN CWA, RH CENTER AISLE SEAT TRACK FWD PORTION AND CLIP HAS CORROSION AT APPROXIMATELY STA 294. MAINTENANCE REMOVED CORROSION IAW SRM 51-70-40. RELEASE DATE 9/4/02. REF 409 # 141859 FOR DETAIL.
- [SDR MALA020545](https://openairdocs.org/sdr/MALA020545.md): Floorboard · corroded · Sep 1, 2002 · N416XJ · Saab 340B · Fuselage Floor Panel
  > DURING 4K-INSPECTION IN CWA, RT O/B FLOORBOARD FLANGE HAS CORROSION AFT OF STA 288. MAINTENANCE REMOVED CORROSION IAW SRM 51-70-40.
- [SDR MALA020544](https://openairdocs.org/sdr/MALA020544.md): Seat Track · corroded · Sep 1, 2002 · N416XJ · Saab 340B · Fuselage, Seat/Cargo Attach Fittings
  > DURING 4K-INSPECTION IN CWA, RT GALLEY I/B SEAT TRACK TOP AND PROFILE HAS CORROSION. MAINTENANCE REMOVED AND REPLACED GALLEY SEAT TRACK IAW SRM 51.
- [SDR MALA020541](https://openairdocs.org/sdr/MALA020541.md): Angle · corroded · Sep 1, 2002 · N416XJ · Saab 340B · Fuselage Miscellaneous Structure
  > DURING 4K-INSPECTION IN CWA, ANGLE AT FRAME STA 225 HAS CORROSION. MAINTENANCE REMOVED CORROSION IAW SRM 51-70-40.
- [SDR MALA020540](https://openairdocs.org/sdr/MALA020540.md): Structure · corroded · Sep 1, 2002 · N416XJ · Saab 340B · Fuselage Miscellaneous Structure
  > DURING 4K-INSPECTION IN CWA, RT SEAT TRACK FWD WRAP AROUND AT STA 294 HAS HEAVY CORROSION. MAINTENANCE INSTALLED NEW WRAP AROUND.
- [SDR MALA020538](https://openairdocs.org/sdr/MALA020538.md): Channel · corroded · Sep 1, 2002 · N416XJ · Saab 340B · Entrance Stairs
  > DURING 4K-INSPECTION IN CWA, AIRSTAIR SLIDE UNIT CHANNEL HAS CORROSION. MAINTENANCE REMOVED CORROSION IAW SRM 51-70-40.
- [SDR MALA020537](https://openairdocs.org/sdr/MALA020537.md): Seat Track · corroded · Sep 1, 2002 · N416XJ · Saab 340B · Fuselage, Seat/Cargo Attach Fittings
  > DURING 4K-INSPECTION IN CWA, LT CENTER AISLE SEAT TRACK FWD PORTION STA 297 HAS CORROSION. MAINTENANCE REMOVED CORROSION IAW SRM 51-70-40.
- [SDR MALA020543](https://openairdocs.org/sdr/MALA020543.md): Frame · corroded · Aug 30, 2002 · N416XJ · Saab 340B · Fuselage Main, Frame
  > DURING 4K-INSPECTION IN CWA, FRAME AND ANGLE TOPS AT STA 258 HAS CORROSION. MAINTENANCE REMOVED CORROSION IAW SRM 51-70-40.
- [SDR MALA020542](https://openairdocs.org/sdr/MALA020542.md): Beam · corroded · Aug 30, 2002 · N416XJ · Saab 340B · Fuselage Miscellaneous Structure
  > DURING 4K-INSPECTION IN CWA, LT BEAM AND ANGLE LBL 10.5 BETWEEN FRAME STA 258 & 236.5 HAS CORROSION. MAINTENANCE REMOVED CORROSION IAW SRM 51-70-40.
- [SDR MALA020352](https://openairdocs.org/sdr/MALA020352.md): Speaker · shorted · Jun 15, 2002 · N416XJ · Saab 340B · Interphone/Passenger Announcement (PA) System
  > ON FLIGHT 3349, F/A NOTED SMOKE FROM ANC SPEAKER, ROW 3 / 4A. FOLLOWED BY AN ELECTRICAL ODOR, F/A SHUT OFF ANC AND ODOR WENT AWAY. MAINTENANCE PERFORMED OPS CHECK OF ANC SYSTEM IAW SF-340 MM 23, NO DEFECTS NOTED.
- [SDR MALA020141](https://openairdocs.org/sdr/MALA020141.md): Module · failed · Jan 29, 2002 · N416XJ · Saab 340B · Air Intake Anti/De-Ice System
  > DURING FLIGHT 3317, RT INTAKE HEAT FAILED, INTAKE HEAT WAS CYCLING ON AND OFF AT ABOUT 14 SECOND INTERVALS. AC DIVERTED TO CWA, BECAUSE OF WEATHER CONDITIONS IN MSP. MAINTENANCE REMOVED AND REPLACED RT DEICE MODULE P/N 44730-501, SN/ON A00421, SN/OFF L248464
- [SDR MALA010284](https://openairdocs.org/sdr/MALA010284.md): Selector Valve · defective · Mar 21, 2001 · N416XJ · Saab 340B · Landing Gear Retraction/Extension System
  > ON FLIGHT 2861, WHILE ON APPROACH IN MSP THE GEAR DISCREPANCY LIGHT ILLUMINATED. AFTER GOING MISS APPROACH AND PERFORMING THE ORH, DISCOVERED THE F7 C/B WAS POPPED. LANDING CONTROL AFTER RESETTING IT WORKED FINE. MAINTENANCE REPLACED LANDING GEAR SELECTOR V
- [SDR MALA010153](https://openairdocs.org/sdr/MALA010153.md): Power Lever · undertorqued · Feb 1, 2001 · N416XJ · Saab 340B · Power Lever
  > LT AND RT ENGINE WILL ONLY MAKE 72 PERCENT TORQUE WITH POWER LEVERS FIREWALLED. AT FL210 WHILE SETTING POWER FOR TREND TRIED TO SET TORQUE TO 74 PERCENT, PL''S MAXED OUT AT 73 - 74 PERCENT AFTER RAM RISE. MAINTENANCE COMPLETED GPA RUNS WITH BOTH ENGINES, FOU
- [SDR MALA000684](https://openairdocs.org/sdr/MALA000684.md): Module · failed · Nov 18, 2000 · N416XJ · Saab 340B · Air Intake Anti/De-Ice System
  > RH ENGINE INTAKE LIGHT ON IN FLIGHT. QRH RESET THEN LIGHT CAME ON AGAIN. AIR TURN BACK TO DTW. MAINTENANCE REPLACED RH DEICE CONTROL MODULEPN 44730-501, SN/ON A00021. PERFORMED 30 MINUTE GROUND RUN.. ALL COMPONENTS VERIFIED TO BE HEATING. ALL CHECKS GOOD AT
- [SDR MALA000624](https://openairdocs.org/sdr/MALA000624.md): Duct · cracked · Sep 26, 2000 · N416XJ · Saab 340B · Nacelle/Pylon Structure
  > FOUND DURING C-CHECK, RT ENGINE INBOARD NACA DUCT CRACKED AT PANEL 463AL. REFER TO CELSIUS TASK CARD 4535, W/O 18843 AND SAAB STATEMENT 340 SDS000144. MAINTENANCE REPAIRED DAMAGE REF SAAB STATEMENT 340SDS000144. PERFORM NDT PER FFVNDT006EC NO CRACKS PAST RO
- [SDR MALA000623](https://openairdocs.org/sdr/MALA000623.md): Skin · dented · Sep 26, 2000 · N416XJ · Saab 340B · Horizontal Stabilizer, Plate/Skin
  > FOUND DURING C-CHECK, RT HORIZONTAL STABILIZER UPPER SURFACE AT HS STA 439.2 HAS SEVERAL DENTS. REFER TO CELSIUS TASK CARD 3510, W/O 18843 AND SAAB STATEMENT 340SDS000144. MAINTENANCE FOUND DENTS OUT OF ALLOWABLE LIMIT REF SAAB SRM 51-10-10 LEXX THAN 4L AND 5
- [SDR MALA000622](https://openairdocs.org/sdr/MALA000622.md): Skin · dented · Sep 23, 2000 · N416XJ · Saab 340B · Fuselage Main, Plate/Skin
  > FOUND DURING C-CHECK, GROUP OF DENTS IN LT FUSELAGE BENEATH ICE SHIELD STA 331, WL 107. REFER TO CELSIUS TASK CARD 2548, W/O 18843, AND SAAB STATEMENT 340SDS000144. MAINTENANCE FOUND DENTS ARE OUT OF LIMITS, REF 51-10-10. DENTS ARE ACCEPTABLE AS IS IAW SAAB
- [SDR MALA000625](https://openairdocs.org/sdr/MALA000625.md): Rib · cracked · Sep 20, 2000 · N416XJ · Saab 340B · Wing, Rib/Bulkhead
  > FOUND DURING C-CHECK, 3 RIBS CRACKED ON LEADING EDGE PANEL 611BR. REFER TO CELSIUS TASK CARD 6506, W/O18843. MAINTENANCE REMOVED CRACKED SECTION OF 3 CRACKED RIBS IAW SRM 57-10-30. NDT PERF FVNDT006EC NO CRACKS NOTED. FABRICATED 3 REPAIR ANGLES AND SHIMS I
- [SDR MALA000620](https://openairdocs.org/sdr/MALA000620.md): Skin · dented · Sep 20, 2000 · N416XJ · Saab 340B · Fuselage Main, Plate/Skin
  > LT FUSELAGE HAS SEVERAL DENTS AT STA 350.0 REFER TO CELSIUS TASK CARD 2531, W/O 18843. MAINTENANCE FOUND DENTS OUT OF ALLOWABLE LIMIT REF SAAB SRM 51-10-10 LEXX THAN 4L. FABRICATED REPAIR DOUBLER/TRIPLER PER PRINCIPLES OF SRM 53-70-10, ALODINED, PRIMED AND T
- [SDR MALA000619](https://openairdocs.org/sdr/MALA000619.md): Skin · dented · Sep 20, 2000 · N416XJ · Saab 340B · Fuselage Main, Plate/Skin
  > FOUND DURING C-CHECK, LT FUSELAGE HAS SEVERAL DENTS AT STA 350.0 REFER TO CELSIUS TASK CARD 2531, W/O 18843. MAINTENANCE FOUND DENTS OUT OF ALLOWABLE LIMIT REF SAAB SRM 51-10-10 LESS THAN 4L. FABRICATED REPAIR DOUBLER / TRIPLER PER PRINCIPLES OF SRM 53-70-10
- [SDR MALA000618](https://openairdocs.org/sdr/MALA000618.md): Skin · dented · Sep 20, 2000 · N416XJ · Saab 340B · Fuselage Main, Plate/Skin
  > FOUND DURING C-CHECK, SEVERAL DENTS IN RT FUSELAGE ABOVE AND BELOW PREVIOUS REPAIR AT STA 339.0. REFER TO CELSIUS TASK CARD 2528, W/O 18843. MAINTENANCE FOUND DENTS OUT OF ALLOWABLE LIMIT REF SAAB SRM 51-10-10 LESS THAN 4L. NDT PERF FVNDT006 EDDY CURRENT, N
- [SDR MALA000617](https://openairdocs.org/sdr/MALA000617.md): Floor Support · corroded · Sep 19, 2000 · N416XJ · Saab 340B · Fuselage Miscellaneous Structure
  > FOUND DURING C-CHECK, CORROSION ON RT FLOORBOARD BL 0 FROM STA 294 TO STA 350. REFER TO CELSIUS TASK CARD 1524, W/O 18843 AND SAAB STATEMENT 340SDS000144. MAINTENANCE REMOVED CORROSION ON RT FLOOR FLANGE FROM STA 294 TO 350 IAW SRM 51-70-40. MATERIAL REMAIN

Next page: https://openairdocs.org/deregistered/N416XJ-2015-11-18/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 = 'N416XJ' AND deregistration_id = 'N416XJ-2015-11-18'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N416XJ-2015-11-18/reports

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