# Service difficulty reports: N247JS, cancelled May 14, 2022

A list on [N247JS, cancelled May 14, 2022](https://openairdocs.org/deregistered/N247JS-2022-05-14.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 · 79 reports

- [SDR VNAA2020012711103](https://openairdocs.org/sdr/VNAA2020012711103.md): Control Lever · failed · Jan 27, 2020 · N247JS · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL IN FLIGHT, RETURNED TO FIELD, DEFERRED THE SYSTEM. MAINTENANCE REMOVED AND REPLACED THE FLAP CONTROL LEVER.
- [SDR VNAA2019120651102](https://openairdocs.org/sdr/VNAA2019120651102.md): Unknown · odor · Dec 5, 2019 · N247JS · Cndair CL6002B19 · Air Distribution System
  > SMELL SMOKE IN CABIN JUST PRIOR TO PUSH BACK. PERFORMED OPS TEST OF THE AIR CONDITIONING SYS IAW CRJ 200 AMM 21-51-00-710-801 NO SMELL OF SMOKE DETECTED AT THIS TIME
- [SDR VNAA2019051099913](https://openairdocs.org/sdr/VNAA2019051099913.md): Bulkhead · cracked · May 10, 2019 · N247JS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 621 REAR PRESSURE BULKHEAD FWD FACE BLO.00 WL127.5-WL113.5 INDICATIONS NOTED APPROX 6" LONG 50% FULL SCREEN HEIGHT, LBL9.5 WL76.50 INDICATION NOTED.6" LONG AND 100% FULL SCREEN HEIGHT FAILING NDT, RBL36 WL74.30 INDICATION NOTED 1.1" LONG AND 100% FULL SCR
- [SDR VNAA2019051099912](https://openairdocs.org/sdr/VNAA2019051099912.md): Seat Track · corroded · May 10, 2019 · N247JS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LBL 9 FLOOR SEAT TRACK FROM FS 399- FS 399 +128 SEGMENT IS CORRODED. C/A: INSTALLED NEW SEAT TRACK IAW REO 601R-53-00-485.
- [SDR VNAA2019051099911](https://openairdocs.org/sdr/VNAA2019051099911.md): Seat Track · corroded · May 10, 2019 · N247JS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RBL 9 FLOOR SEAT TRACK FS 364- FS 399 SEGMENT IS CORRODED. C/A: INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-400-802.
- [SDR VNAA2019051099910](https://openairdocs.org/sdr/VNAA2019051099910.md): Angle · corroded · May 10, 2019 · N247JS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX DOOR LOWER SILL MID ANGLE IS CORRODED BEYOND LIMITS. C/A: REMOVED AND REPLACED MID ANGLE IAW SRM 51-42-06 AND 51-42-21.
- [SDR VNAA2019051099909](https://openairdocs.org/sdr/VNAA2019051099909.md): Bracket · cracked · May 10, 2019 · N247JS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > HYD SYS NR 3 PRESSURE TRANSDUCER BRACKET CRACKED IN LT MLG WHEEL WELL CEILING. C/A: REMOVED AND REPLACED BRACKET IAW SRM 51-42-06.
- [SDR VNAA2019051099908](https://openairdocs.org/sdr/VNAA2019051099908.md): Bracket · cracked · May 10, 2019 · N247JS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > HYD SYS NR 3 TRANSDUCER BRACKET CRACKED IN RT MLG CEILING. C/A: REMOVED AND REPLACED BRACKET IAW SRM 51-42-06.
- [SDR VNAA2019051099907](https://openairdocs.org/sdr/VNAA2019051099907.md): Bracket · cracked · May 10, 2019 · N247JS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > HYD SYS NR 3 PRESSURE TRANSDUCER Z-BRACKET CRACKED IN RT MLG WHEEL WELL CEILING. C/A: REMOVED AND REPLACED Z-BRACKET IAW SRM 51-42-06 AND 51-42-04.
- [SDR VNAA2019051099906](https://openairdocs.org/sdr/VNAA2019051099906.md): Seat Track · corroded · May 10, 2019 · N247JS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LBL 9 FLOOR SEAT TRACK FS 364- FS 399 SEGMENT IS CORRODED. C/A: INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-400-802.
- [SDR VNAA2019051099905](https://openairdocs.org/sdr/VNAA2019051099905.md): Seat Track · corroded · May 10, 2019 · N247JS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RBL 9 FLOOR SEAT TRACK FROM FS399- FS409+128 SEGMENT IS CORRODED. C/A: REMOVED AND REPLACED RBL9 FLOOR SEAT TRACK FS399-FS409+128 SEGMENT IAW SRM 51-40-11, AMM 53-01-11-400-802, AND REO 601R-53-00-485.
- [SDR VNAA2019051099904](https://openairdocs.org/sdr/VNAA2019051099904.md): Floorbeam · corroded · May 10, 2019 · N247JS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > RBL 9 FLOORBEAM, I/B FLOOR SUPPORT FLANGE, IS CORRODED AT FS 591 TO FS 621 AROUND NUT PLATE PULL RIVETS. C/A: INSTALLED NEW SERVICEABLE FLOORBEAM AT RBL 9 BETWEEN FS 574-605 IAW REO #601R-53-61-3780 REV. A DATED 2011-07-15.
- [SDR VNAA2019051099903](https://openairdocs.org/sdr/VNAA2019051099903.md): Floorbeam · corroded · May 10, 2019 · N247JS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > LBL 9 FLOORBEAM, I/B FLOOR SUPPORT FLANGE, IS CORRODED AT FS 595 AROUND NUT PLATE PULL RIVETS. C/A: INSTALLED NEW SERVICEABLE FLOORBEAM AT LBL 9 BETWEEN FS 574-605 IAW REO #601R-53-61-3780 REV. A DATED 2011-07-15.
- [SDR VNAA2019051099902](https://openairdocs.org/sdr/VNAA2019051099902.md): Floorbeam · corroded · May 10, 2019 · N247JS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > RBL9 FLOORBEAM HAS CORROSION AROUND FLOOR NUTPLATE HOLES BETWEEN FS409 AND FS409+128. C/A: REMOVED AND REPLACED RBL9 FLOORBEAM CAP IAW SRM 51-40-11, 51-42-06, 51-42-21 AND REO 601R-53-31-1010 DATED 2019-05-02..
- [SDR VNAA2019051099901](https://openairdocs.org/sdr/VNAA2019051099901.md): Floorbeam · corroded · May 10, 2019 · N247JS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > LBL9 FLOORBEAM HAS CORROSION AROUND FLOOR NUTPLATE HOLES BETWEEN FS409 AND FS409+128. C/A: REMOVED AND REPLACED LBL9 FLOORBEAM CAP IAW SRM 51-40-11, 51-42-06, 51-42-21 AND REO 601R-53-31-1010 DATED 2019-05-02.
- [SDR VNAA2019030811101](https://openairdocs.org/sdr/VNAA2019030811101.md): Light · inoperative · Mar 8, 2019 · N247JS · Cndair CL6002B19 · Emergency Lighting
  > SUPPLEMENTAL INFORMATION:L/H FWD EMERGENCY LIGHT WILL NOT ILLUMINATE. REMOVED AND REPLACED L/H FWD EXTERIOR EMERGENCY LIGHT IAW CRJ200 AMM 33-51-21-000/400-801. OPS CHECK GOOD AT THIS TIME
- [SDR VNAA20181112101](https://openairdocs.org/sdr/VNAA20181112101.md): None · none · Oct 29, 2018 · N247JS · Cndair CL6002B19 · Turbine Engine Combustion Section
  > ON TAKEOFF ABOUT 600 FEET THE CREW OBSERVED A LARGE BIRD GO PAST AND HEARD A "THUMP" AND BEGAN TO RECEIVE ENGINE INDICATIONS THAT THE BIRD MADE IMPACT WITH THE RIGHT HAND ENGINE. THE AIRCRAFT RETURNED TO FIELD AND CURRENTLY UNDER MAINTENANCE INSPECTION. THE AI
- [SDR VNAA2017062911101](https://openairdocs.org/sdr/VNAA2017062911101.md): Bracket · bent · Jun 29, 2017 · N247JS · Cndair CL6002B19 · Main Landing Gear Attach Section
  > AFTER TAKEOFF, THE CREW SELECTED GEAR UP AND THE GEAR DID NOT RETRACT. 6 SECONDS AFTER SELECTING THE HANDLE UP THE MAIN GEAR RETRACTED AND THE NOSE GEAR DID NOT RETRACT. THE AIRCRAFT RETURNED TO THE FIELD AND MAINTENANCE FOUND THE CENTERING PROXIMITY SENSOR B
- [SDR VNAA2017062999902](https://openairdocs.org/sdr/VNAA2017062999902.md): Fitting · cracked · Jun 29, 2017 · N247JS · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR UPPER FWD FITTING CRACKED. INSTALLED NEW SERVICEABLE CARGO DOOR UPPER FORWARD FITTING.
- [SDR VNAA2017062999901](https://openairdocs.org/sdr/VNAA2017062999901.md): Bulkhead · cracked · Jun 28, 2017 · N247JS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > CRACK INDICATIONS AT LBL 36.20, LBL 18.0 AND RBL 18.0 AND WL 74. REPAIRED AREAS AT LBL 36.20 LBL 18.00 AND RBL 18.0 AT WL 74 IAW REO 601R-53-61-6070.
- [SDR VNAA2017062899912](https://openairdocs.org/sdr/VNAA2017062899912.md): Channel · cracked · Jun 28, 2017 · N247JS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > BS 621 DOOR SUPPORTS CHANNEL, LOWER ANGLE CRACKED. REMOVED AND REPLACED THE CHANNEL.
- [SDR VNAA2017062899911](https://openairdocs.org/sdr/VNAA2017062899911.md): Bulkhead Web · cracked · Jun 28, 2017 · N247JS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND REAR PRESSURE BULKHEAD WEB HAS A CRACK INDICATION NOTED AT RBL 27.5, WL 80, APPROXIMATELY 2 INCHES LONG, 50% FSH. REPAIRED THE BULKHEAD WEB IAW REO 601R-53-61-1285, REV E.
- [SDR VNAA2017062899910](https://openairdocs.org/sdr/VNAA2017062899910.md): Bulkhead Web · cracked · Jun 28, 2017 · N247JS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND REAR PRESSURE BULKHEAD WEB HAS A CRACK INDICATION NOTED AT RBL 18, WL 74, APPROXIMATELY 2.5 INCHES LONG, 70% FSH. COMPLIED WITH REO 601R-53-61-6070.
- [SDR VNAA2017062899909](https://openairdocs.org/sdr/VNAA2017062899909.md): Bulkhead Web · cracked · Jun 28, 2017 · N247JS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND REAR PRESSURE BULKHEAD WEB HAS A CRACK INDICATION NOTED AT BL 0, WL 112, APPROXIMATELY 4.0 INCHES LONG, 50% FSH. REPAIRED THE BULKHEAD WEB IAW REO 601R-53-61-1285, REV E.
- [SDR VNAA2017062899908](https://openairdocs.org/sdr/VNAA2017062899908.md): Bulkhead Web · cracked · Jun 28, 2017 · N247JS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND REAR PRESSURE BULKHEAD WEB HAS A CRACK INDICATION NOTED AT LBL 18, WL 74, APPROX 2 INCHES LONG, 90% FSH. REPAIRED THE BULKHEAD WEB IAW REO 601R-53-61-6070, REV -.
- [SDR VNAA2017062899907](https://openairdocs.org/sdr/VNAA2017062899907.md): Bulkhead Web · cracked · Jun 28, 2017 · N247JS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND REAR PRESSURE BULKHEAD WEB HAS A CRACK INDICATION AT LBL 18.00, WL 106, APPROX 2.5 INCHES LONG, 50% FSH. REPAIRED REAR PRESSURE BULKHEAD IAW REO 601R-53-61-1285, REV E.
- [SDR VNAA2017062899906](https://openairdocs.org/sdr/VNAA2017062899906.md): Bulkhead Web · cracked · Jun 28, 2017 · N247JS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND REAR PRESSURE BULKHEAD WEB HAS INDICATION OF A CRACK NOTED AT LBL 36.20, WL 74, APPROX 2.5 INCHES LONG, 90% FSH. REPAIRED THE REAR PRESSURE BULHEAD IAW REO 601R-53-61-6070.
- [SDR VNAA2017062899905](https://openairdocs.org/sdr/VNAA2017062899905.md): Skin · cracked · Jun 28, 2017 · N247JS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > NLG WHEEL CUTOUT HAS VISIBLE SIGNS OF POSSIBLE CRACK IN BOTH AFT CORNERS AT FS 235.00. REPAIRED IAW REO 601R-53-11-010
- [SDR VNAA2017062899904](https://openairdocs.org/sdr/VNAA2017062899904.md): Floor Support · corroded · Jun 28, 2017 · N247JS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON RT SIDE PRESSURE FLOOR SUPPORT IN MULTIPLE LOCATIONS BETWEEN BS 461 AND 529. REPAIRED PER REO 601R-53-41-666
- [SDR VNAA2017062899903](https://openairdocs.org/sdr/VNAA2017062899903.md): Floor Support · corroded · Jun 28, 2017 · N247JS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON LT PRESSURE FLOOR SUPPORT IN MULTIPLE LOCATIONS BETWEEN BS 461 TO 529. REPAIRED IAW REO 601R-53-41-666
- [SDR VNAA2017062899902](https://openairdocs.org/sdr/VNAA2017062899902.md): Frame · cracked · Jun 28, 2017 · N247JS · Cndair CL6002B19 · Fuselage Main, Frame
  > LEFT BS 718 FRAME CRACKED AT STRINGER 11L. REPLACED THE FRAME SECTION.
- [SDR VNAA2017062899901](https://openairdocs.org/sdr/VNAA2017062899901.md): Frame · cracked · Jun 28, 2017 · N247JS · Cndair CL6002B19 · Fuselage Main, Frame
  > RIGHT BS 718 FRAME CRACKED AT STRINGER 11R. REPLACED THE FRAME SECTION.
- [SDR VNAA2017012400033](https://openairdocs.org/sdr/VNAA2017012400033.md): Tire · failed · Jan 24, 2017 · N247JS · Cndair CL6002B19 · Nose/Tail Landing Gear
  > LEFT NOSE TIRE BLEW ON TAKE OFF. REMOVED AND REPLACED BOTH NLG WHEEL AND TIRE ASSEMBLIES.
- [SDR VNAA2016062600028](https://openairdocs.org/sdr/VNAA2016062600028.md): Light · broken · Jun 26, 2016 · N247JS · Cndair CL6002B19 · Emergency Lighting
  > SEGMENT OF EMERGENCY LIGHTING GLOW STICK AND COVER, BROKEN AND MISSING AT SEAT 1D. MAINTENANCE INSPECTED, R & R EMERGENCY FLOOR LIGHT LAMP AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2016053100034](https://openairdocs.org/sdr/VNAA2016053100034.md): Apu · faulty · May 31, 2016 · N247JS · Cndair CL6002B19 · APU Oil System
  > APU LOW OIL PRESSURE CAUTION MESSAGE. THE CREW DIVERTED TO NEAREST FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, PROPERLY SERVICED THE APU AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2016011300010](https://openairdocs.org/sdr/VNAA2016011300010.md): Seal · detached · Jan 13, 2016 · N247JS · Cndair CL6002B19 · Service Doors
  > CREW REPORTED TOP 8" OF SERVICE DOOR SEAL DETACHED IN FLIGHT. MADE A VERY LOUD NOISE. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, REATTACHED SERVICE DOOR SEAL AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.
- [SDR VNAA2015121600010](https://openairdocs.org/sdr/VNAA2015121600010.md): Battery Pack · failed · Dec 16, 2015 · N247JS · Cndair CL6002B19 · Emergency Lighting
  > CREW REPORTED EMERGENCY LIGHT FLOOR STRIP NOT WORKING FROM ROW 9 TO THE AFT OF AIRCRAFT. MAINTENANCE INSPECTED, R & R NR 4 EMERGENCY LIGHT BATTERY PACK AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.
- [SDR VNAA2015083000038](https://openairdocs.org/sdr/VNAA2015083000038.md): Connector · disconnected · Aug 30, 2015 · N247JS · Cndair CL6002B19 · Light System Wiring
  > CREW REPORTED EMERGENCY FLOOR LIGHTS INOPERATIVE FROM ROW 9 AND AFT. MAINTENANCE INSPECTED, FOUND RT AFT EMERGENCY LIGHT CONNECTOR DISCONNECTED, RECONNECTED CONNECTOR AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.
- [SDR VNAA2015081700018](https://openairdocs.org/sdr/VNAA2015081700018.md): Skin · damaged · Aug 17, 2015 · N247JS · Cndair CL6002B19 · Ailerons
  > LIGHTENING STRIKE DAMAGE TO RT AILERON UPPER SKIN AND T/E. REPAIRED THE AILERON IAW REO 601R-57-61-528, REV.
- [SDR VNAA2015081700017](https://openairdocs.org/sdr/VNAA2015081700017.md): Post · cracked · Aug 17, 2015 · N247JS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 409+128, BL 0, VERTICAL POST LT AND RT SIDES HAVE INDICATIONS NOTED IN THE AFT FLANGE RADIUS AT WL 69.250" LONG 60 PERCENT FSH FAILED NDT. R & R VERTICAL POST FS409+128, BLO.O IAW REO 601R-53-41-889, REV A.
- [SDR VNAA2015081700016](https://openairdocs.org/sdr/VNAA2015081700016.md): Cargo Track · corroded · Aug 17, 2015 · N247JS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO TRACK ON RBL 9BETWEEN BS 559+80 AND 559+96 AND CARGO TRACK HAD CORROSION. R & R CARGO TRACK IAW AMM 53-00-49-000-801 AND 53-00-49-400-801.
- [SDR VNAA2015081700014](https://openairdocs.org/sdr/VNAA2015081700014.md): Mount · corroded · Aug 17, 2015 · N247JS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > WARDROBE OTBD MOUNT PAD AT FS 310 HAS CORROSION AROUND BOLT HOLE. R & R 200 DWG 601R38670 AND SRM 51-40-11. INSTALLED NEW PAD IAW SRM 51-42-13 AND 51-21-16.
- [SDR VNAA2015041100014](https://openairdocs.org/sdr/VNAA2015041100014.md): Wire · broken · Apr 11, 2015 · N247JS · Cndair CL6002B19 · Light System Wiring
  > CREW REPORTED MAIN CABIN DOOR EMERGENCY EXIT STRIP WOULD NOT ILLUMINATE. MAINTENANCE INSPECTED, FOUND BROKEN WIRE ON EMERGENCY LIGHT, INSTALLED NEW WIRE SPLICE ON BROKEN WIRE AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.
- [SDR VNAA2014090500001](https://openairdocs.org/sdr/VNAA2014090500001.md): Wire Harness · damaged · Sep 5, 2014 · N247JS · Cndair CL6002B19 · Light System Wiring
  > CREW REPORTED EMERGENCY FLOOR LEVEL LIGHTING AFT OF EMERGENCY EXIT ROW WOULD NOT ILLUMINATE WHEN TESTED. MAINTENANCE TROUBLESHOT, R & R LIGHT WIRE HARNESS AND PERFORMED CHECKS IAW AMM. AIRCRAFT RELEASED FOR SERVICE.
- [SDR VNAA2014060600005](https://openairdocs.org/sdr/VNAA2014060600005.md): Connector · broken · Jun 6, 2014 · N247JS · Cndair CL6002B19 · Light System Wiring
  > CREW REPORTED FLOOR LEVEL EMERGENCY LIGHTS ROW 9, AND AFT INOPERATIVE. MAINTENANCE TROUBLESHOT AND FOUND EMERGENCY LIGHT CONNECTOR PIN BROKEN AT END OF ROW BY LAVATORY. MAINTENANCE R & R SHORT CABLE, PIGTAIL AT LAVATORY ENTRANCE EMERGENCY FLOOR LIGHT AND PERFO
- [SDR VNAA2014040900008](https://openairdocs.org/sdr/VNAA2014040900008.md): Warning Light · false activation · Apr 9, 2014 · N247JS · Cndair CL6002B19 · Landing Gear Steering System
  > CREW REPORTED AMBER STEERING INOPERATIVE MESSAGE ON TAKEOFF. LANDED AT DESTINATION AIRPORT WITHOUT INCIDENT. MAINTENANCE PERFORMED OPS CHECK OF NOSEWHEEL STEERING (NWS) ELECTRONIC CONTROL UNIT (ECU) AND PERFORMED BITE TEST OF STEERING SYS IAW AMM. OPS CHEC
- [SDR VNAA2013121400007](https://openairdocs.org/sdr/VNAA2013121400007.md): Shutoff Valve · failed · Dec 14, 2013 · N247JS · Cndair CL6002B19 · Airfoil Anti/De-ice System
  > CREW REPORTED RED WING OVERHEAT MESSAGE DURING CLIMB. CREW RAN QRH, RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R MODULATING AND SHUTOFF VALVE AND PERFORMED CHECKS IAW AMM. AIRCRAFT RELEASED FOR SERVICE.
- [SDR VNAA2013101700007](https://openairdocs.org/sdr/VNAA2013101700007.md): Pdu · failed · Oct 17, 2013 · N247JS · Cndair CL6002B19 · Engine Thrust Reverser
  > CREW REPORTED LT THRUST REVERSER UNLOCK CAUTION MESSAGE IN DESCENT OUT OF FL200. CREW DECLARED EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. MX TROUBLESHOT, R & R LT THRUST REVERSER PDU AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.
- [SDR VNAA2013091600007](https://openairdocs.org/sdr/VNAA2013091600007.md): Inverter · inoperative · Sep 16, 2013 · N247JS · Cndair CL6002B19 · Emergency Lighting
  > CREW AND MX REPORTED ROWS 6 THROUGH 8 EMERGENCY LIGHT INOPERATIVE AND LOWER RT EMERGENCY LIGHT BY OVERWING EXIT INOPERATIVE. MX TROUBLESHOT, R & R NR 3 EMERGENCY LIGHT INVERTER AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.
- [SDR VNAA2013020500002](https://openairdocs.org/sdr/VNAA2013020500002.md): Fuel Control · leaking · Feb 5, 2013 · N247JS · Cndair CL6002B19 · APU Engine Fuel and Control
  > CREW REPORTED SMOKE TOILET CAUTION MESSAGE ON DESCENT AFTER SWITCH TO APU BLEED. NO SMOKE IN CABIN, BUT FAIRLY STRONG SMELL WHEN BLEEDS WERE SWITCHED. MESSAGE WENT AWAY ON ITS OWN AFTER ONE MINUTE. CREW LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FO

Next page: https://openairdocs.org/deregistered/N247JS-2022-05-14/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 = 'N247JS' AND deregistration_id = 'N247JS-2022-05-14'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N247JS-2022-05-14/reports

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