# Service difficulty reports: N531EG

A list on [N531EG](https://openairdocs.org/aircraft/N531EG.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 · 89 reports

- [SDR VNAA2026030913501](https://openairdocs.org/sdr/VNAA2026030913501.md): Unknown · odor · Mar 7, 2026 · N531EG · Cndair CL6002C10 · Air Distribution System
  > STRONG FUMES AFTER APU START AFT LANDING THROUGHOUT THE WHOLE CABIN. / TROUBLESHOT SMELL PER CRJ7 FIM 22-21-00-810-806. NO SMELL OBSERVED. COULDN€™T REPLICATE FAULT AT THIS TIME.
- [SDR VNAA2026022813001](https://openairdocs.org/sdr/VNAA2026022813001.md): Pcb · failed · Feb 24, 2026 · N531EG · Cndair CL6002C10 · Engine Indicating System
  > L VIB FAULT, R VIB FAULT, STATUS MESSAGE AT FL230. REMOVED AND REPLACED JB2, PCB2 IAW CRJ 700 AMM 24-01-05-000/400-801-A01. OPS CHECK GOOD AT THIS TIME.
- [SDR VNAA20251025001](https://openairdocs.org/sdr/VNAA20251025001.md): Hinge · gouged · Oct 25, 2025 · N531EG · Cndair CL6002C10 · Fuselage, Door Hinge
  > PAX DOOR HINGE HAS SEVERAL LUGS GOUGED ON BOTH HINGES. REMOVED AND REPLACED PAX DOOR FUSELAGE SIDE HINGE IAW CRJ 700 SRMS 53-21-23-201-007-A01 AND 51-42-21-001-001-A01.
- [SDR VNA202310091005](https://openairdocs.org/sdr/VNA202310091005.md): Fitting · damaged · Oct 9, 2023 · N531EG · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > PERFORM PERMANENT REPAIR TO NOSE FUSELAGE JACKING PAD HELICOIL INSERT.
- [SDR VNA202310092004](https://openairdocs.org/sdr/VNA202310092004.md): Web · corroded · Oct 9, 2023 · N531EG · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR FWD SIDE INTERCOSTAL DD7 BRACKET FOUND TO BE CRACKED IN THE RADIUS.
- [SDR VNA202310092003](https://openairdocs.org/sdr/VNA202310092003.md): Floorbeam · corroded · Oct 9, 2023 · N531EG · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FOUND CORROSION ON RH FS 280 FLOOR BEAM PN# CC670-34094-2.
- [SDR VNA20231009001](https://openairdocs.org/sdr/VNA20231009001.md): Web · cracked · Oct 9, 2023 · N531EG · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR STAIR FWD WEB HAS MULTIPLE CRACKS AT STEP CORNER LOCATIONS, CORROSION AT STAIR FASTENER ATTACH POINTS AND PREVIOUS REPAIRS THAT INTERFERE WITH INTEGRATION OF MODSUM IS67052110210. REQUIRES REPLACEMENT.
- [SDR VNA2023F00005](https://openairdocs.org/sdr/VNA2023F00005.md): Fitting · damaged · Oct 9, 2023 · N531EG · Cndair CL6002C10 · Fuselage Main, Structure
  > PERFORM PERMANENT REPAIR TO NOSE FUSELAGE JACKING PAD HELICOIL INSERT.
- [SDR VNA2023F00004](https://openairdocs.org/sdr/VNA2023F00004.md): Web · corroded · Oct 9, 2023 · N531EG · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR FWD SIDE INTERCOSTAL DD7 BRACKET FOUND TO BE CRACKED IN THE RADIUS.
- [SDR VNA2023F00003](https://openairdocs.org/sdr/VNA2023F00003.md): Floorbeam · corroded · Oct 9, 2023 · N531EG · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FOUND CORROSION ON RH FS 280 FLOOR BEAM PN# CC670-34094-2.
- [SDR VNA2023F00002](https://openairdocs.org/sdr/VNA2023F00002.md): Floorbeam · corroded · Oct 9, 2023 · N531EG · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FOUND CORROSION ON FS 280 L/H FLOOR BEAM ON FWD PN# CC670-34094-1.
- [SDR VNAA202310090004](https://openairdocs.org/sdr/VNAA202310090004.md): Skin · dented · Oct 9, 2023 · N531EG · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > THE FWD LH FUSELAGE SKIN IS DENTED BELOW THE ADG FS 177-185, STR 23.
- [SDR VNA2023F00001](https://openairdocs.org/sdr/VNA2023F00001.md): Web · cracked · Oct 9, 2023 · N531EG · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR STAIR FWD WEB HAS MULTIPLE CRACKS AT STEP CORNER LOCATIONS, CORROSION AT STAIR FASTENER ATTACH POINTS AND PREVIOUS REPAIRS THAT INTERFERE WITH INTEGRATION OF MODSUM IS67052110210. REQUIRES REPLACEMENT.
- [SDR VNAA202310090002](https://openairdocs.org/sdr/VNAA202310090002.md): Former · corroded · Oct 9, 2023 · N531EG · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR FWD FORMER CORRODED.
- [SDR VNAA202310090001](https://openairdocs.org/sdr/VNAA202310090001.md): Stringer · corroded · Oct 9, 2023 · N531EG · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 24L IS CORRODED BETWEEN FS 953.00 AND 969.00.
- [SDR VNAA202303131111](https://openairdocs.org/sdr/VNAA202303131111.md): Windshield · burned · Mar 9, 2023 · N531EG · Cndair CL6002C10 · Flight Compartment Windows
  > CA WINDSHIELD CRACKED AND CAUGHT FIRE ALONG UPPER EDGE CRACKED ABOUT 18 INCHES. REMOVED AND REPLACED LH WINDSHIELD IAW CRJ7 AMM 56-11-01-000/400-801-A01-PSA.
- [SDR VNAA202301181111](https://openairdocs.org/sdr/VNAA202301181111.md): Handle · out of position · Jan 16, 2023 · N531EG · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR INNER HANDLE MOVED OUT OF LOCKED POSITION MULTIPLE TIMES DURING FLIGHT. PERFORMED GVI OF INTERNAL PAX DOOR IAW CRJ 700 AMM 52-11-00-210-803. PERFORMED FUNCTIONAL TEST MULTIPLE TIMES IAW AMM 52-11-00-720-802. NO DEFECTS NOTED AT THIS TIME AND OPS
- [SDR VNAA2022090399914](https://openairdocs.org/sdr/VNAA2022090399914.md): Fitting · corroded · Sep 3, 2022 · N531EG · Bombdr CL6002D15 · Standard Practices/Structures
  > L/H JACK FITTING WEB IS CORRODED/CRACKED. REMOVED AND REPLACED NOSE JACK FITTING AND LH + RH INTERCOSTALS IAW CRJ-700 SRM 51--42-06-001-001-A01 AND 51-42-21-001-001-A01
- [SDR VNAA2022090399913](https://openairdocs.org/sdr/VNAA2022090399913.md): Angle · corroded · Sep 3, 2022 · N531EG · Bombdr CL6002D15 · Doors
  > PAX DOOR SILL ANGLE HAS AREAS OF CORROSION ON THE UNDERSIDE.: INSTALLED NEW SERVICEABLE PAX DOOR SILL ANGLE AND ATTACHMENT PARTS IAW CRJ700 SRM 51--42-06-001-001-A01 AND CRJ700 SRM 51-42-06--001-001-A01
- [SDR VNAA2022090399912](https://openairdocs.org/sdr/VNAA2022090399912.md): Skin · damaged · Sep 3, 2022 · N531EG · Bombdr CL6002D15 · Standard Practices/Structures
  > LEFT HAND SIDE EXTERNAL FUSELAGE AT APPROX FS360.00 JUST FWD OF THE EXTERNAL EMERGENCY LIGHT AND AFT OF PAX DOOR HAS LIGHT SCRATCHES VISIBLE. L/H SIDE EXTERNAL FUSELAGE AT APPROX. F.S360.00 JUST FWD OF THE EXTERNAL EMERGENCY LIGHT AND AFT OF PAX DOOR LIGHT S
- [SDR VNAA2022090399911](https://openairdocs.org/sdr/VNAA2022090399911.md): Frame · corroded · Sep 3, 2022 · N531EG · Bombdr CL6002D15 · Standard Practices/Structures
  > FRAME CORRODED AT FS 969.00 BETWEEN STGR 25L AND 26R. REPAIRED CORROSION FRAME 969.00 STGR 25L - 26R IAW EA 22-C7-53-0968 REV IR DATED 08/09/2022. DTE TO BE ACCOMPLISHED WITHIN 12 MONTHS OF THE RETURN TO SERVICE DATE FOR THE SECTION III REPAIR IN ACCORDANCE W
- [SDR VNAA202209039999](https://openairdocs.org/sdr/VNAA202209039999.md): Intercostal · corroded · Sep 3, 2022 · N531EG · Bombdr CL6002D15 · Standard Practices/Structures
  > AVI BAY DOOR INTERCOSTAL IS CORRODED BETWEEN STGR 27 TO 26R. INSTALLED NEW INTERCOSTAL AT STGR 27 - 26R FWD ON AVI BAY DOOR IAW CRJ700 SRM 51--42-06-001-001-A01
- [SDR VNAA202209039998](https://openairdocs.org/sdr/VNAA202209039998.md): Intercostal · corroded · Sep 3, 2022 · N531EG · Bombdr CL6002D15 · Standard Practices/Structures
  > L/H AVI DOOR INTERCOSTAL BETWEEN STGR 27 TO STGR 26L IS CORRODED. REMOVED AND INSTALLED NEW INTERCOSTAL AT LH AVI DOOR BETWEEN STGR 27 AND STGR 26L IAW CRJ700 SRM 51-42–06-001-001-A01 AND SRM 51-42-21-001-001-A01
- [SDR VNAA202209039997](https://openairdocs.org/sdr/VNAA202209039997.md): Frame · corroded · Sep 3, 2022 · N531EG · Bombdr CL6002D15 · Standard Practices/Structures
  > FRAME AT F.S 319 IS CORRODED BETWEEN STR 23R TO STR 25L. FRAME @ F.S. 319 WAS REPAIRED AS REQUIRED IAW CRJ 700 SRM 53-00-06-201-- 006-A01.
- [SDR VNAA202209039996](https://openairdocs.org/sdr/VNAA202209039996.md): Frame · corroded · Sep 3, 2022 · N531EG · Bombdr CL6002D15 · Standard Practices/Structures
  > FRAME AT F.S 295.00 FOUND IS CORRODED. REPAIRED FS295 AS REQUIRED IAW CRJ700 SRM 53-00-06-201-006-A01. NO FURTHER DEFECT NOTED
- [SDR VNAA202209039995](https://openairdocs.org/sdr/VNAA202209039995.md): Frame · corroded · Sep 3, 2022 · N531EG · Bombdr CL6002D15 · Standard Practices/Structures
  > "F.S 349 FRAME IS CORRODED BETWEEN STGR 25R TO 25L. FS 349 FRAME BETWEEN STR23L TOSTR22R WAS REMOVED AND REPLACED IAW CRJ 700 SRM 51-42-06-001-001-A01 & CRJ 700 SRM 51-42-21-001-001-A01.
- [SDR VNAA202209039994](https://openairdocs.org/sdr/VNAA202209039994.md): Seat Track · corroded · Sep 3, 2022 · N531EG · Bombdr CL6002D15 · Standard Practices/Structures
  > LH SIDE SEAT RAIL STRUCTURE TRIM RETAINER AT FS 797.00 IS CORRODED. REPLACED SIDE SEAT TRACK AND NEW TRIM RETAINER IAW CRJ700 AMM 53-00-49-400-801-A03
- [SDR VNAA202209039993](https://openairdocs.org/sdr/VNAA202209039993.md): None · cracked · Sep 3, 2022 · N531EG · Bombdr CL6002D15 · Standard Practices/Structures
  > WHILE PERFORMING LOWER WING PLANK SB 670BA-57-020C NDT FOUND 5EA HOLES TO HAVE INDICATIONS
- [SDR VNAA202209039992](https://openairdocs.org/sdr/VNAA202209039992.md): Angle · cracked · Sep 3, 2022 · N531EG · Bombdr CL6002D15 · Standard Practices/Structures
  > FOUND LIGHTENING DIVERTER SUPPORT CHANNEL BETWEEN FRAME STATION 333 AND 349 TO BE CRACKED. INSTALLED NEW CLIPS AND ANGLE IAW CRJ 700 SRM 51-42-13-001-001-A01.
- [SDR VNAA202209039991](https://openairdocs.org/sdr/VNAA202209039991.md): Intercostal · corroded · Sep 3, 2022 · N531EG · Bombdr CL6002D15 · Electrical/Electronic Compartment Doors
  > SERVICE DOOR INTERCOSTAL IS CORRODED BETWEEN F.S. 333 TO F.S. 349 AT STGR 20R. REPLACED CORRODED SERVICE DOOR INTERCOSTAL BETWEEN FS 333 TO FS 349 AT STGR 20R IAW CRJ 700 SRM 51-42-06-001-001-A01, 51-42-21--001-001-A01.
- [SDR VNAA202206271112](https://openairdocs.org/sdr/VNAA202206271112.md): Fuel Sys · warning message · Jun 24, 2022 · N531EG · Cndair CL6002C10 · Fuel Quantity Indicator
  > JUST AFTER T/O RAPID FUEL IMBALANCE WITH RH TANK WHILE LH TANK STAYED LEVEL PROBLEM FIXED ITSELF DURING DECENT / PERFORMED OPS TEST OF GRAVITY XFLOW SOV IAW CRJ 700 AMM 28-13-16-710-803-A01, OPS CHECK GOOD. PERFORMED OPS TEST OF FUEL QTY GAUGING COMPUTER IAW A
- [SDR VNAA202206101111](https://openairdocs.org/sdr/VNAA202206101111.md): Adhesive · odor · Jun 8, 2022 · N531EG · Cndair CL6002C10 · Cabin Equipment/Furnishings
  > BURNING SMELL COMING FROM FWD CLOSET / T/S BURNING SMELL CHECKED CLOSET LT,GALLEY HEATER/FAN, PACKS,AVIONICS FANS,RECIRC FANS,APU AND WIFI IAW CRJ FIM 21-22-00-810-806-A01 FOUND NO DEFECTS FOR LISTED ITEMS SMELL STILL PRESENT SEE NEXT ITEM FOR FURTHER MX. CONT
- [SDR VNAA202111301111](https://openairdocs.org/sdr/VNAA202111301111.md): Transmitter · unserviceable · Nov 30, 2021 · N531EG · Cndair CL6002C10 · Engine Oil Indicating System
  > IN FLIGHT AT APPROX 8000FT, WE NOTICED RH OIL PRESS INDICATION OF ZERO, RAN QRC/QRH FOR NON MSG LOW OIL PRESSURE. OIL PRESSURE REMAINED AT ZERO, OIL TEMP INCREASING QRH DROVE US TO TO SHUT DOWN RH ENGINE; DID NOT RECEIVED THE RH ENG OIL PRESSURE WARNING MSG, O
- [SDR 2021F00355](https://openairdocs.org/sdr/2021F00355.md): Transmitter · unserviceable · Nov 26, 2021 · N531EG · Cndair CL6002C10 · Engine Integrated Instrument System
  > IN FLIGHT AT APPROX 8000FT, WE NOTICED RH OIL PRESS INDICATION OF ZERO, RAN QRC/QRH FOR NON MSG LOW OIL PRESSURE. OIL PRESSURE REMAINED AT ZERO, OIL TEMP INCREASING QRH DROVE US TO TO SHUT DOWN RH ENGINE; DID NOT RECEIVED THE RH ENG OIL PRESSURE WARNING MSG, O
- [SDR VNAA202110131111](https://openairdocs.org/sdr/VNAA202110131111.md): Keelbeam · corroded · Oct 10, 2021 · N531EG · Cndair CL6002C10 · Fuselage Main, Keel
  > DURING SCHEDULED MAINTENANCE AT THE GREENVILLE-SPARTANBURG INTERNATIONAL AIRPORT (GSP) FACILITIES IN GREER, SC, THE MAINTENANCE TEAM FOUND MULTIPLE AREAS OF CORROSION DAMAGE AS FOLLOWS: / CORROSION DAMAGE FOUND IN THREE (3) AREAS (Ï¿½AÏ¿½, Ï¿½BÏ¿½, AND Ï¿½CÏ¿½
- [SDR VNAA201911121102](https://openairdocs.org/sdr/VNAA201911121102.md): Connector · disconnected · Nov 10, 2019 · N531EG · Cndair CL6002C10 · Light System Wiring
  > MAINTENANCE FOUND FWD EMERGENCY EXIT SIGN AT THE PASSENGER WIND SCREEN INOP. RECONNECTED PLUG AND THE SIGN OPS CHECKED GOOD.
- [SDR SIMA2019102304005](https://openairdocs.org/sdr/SIMA2019102304005.md): Floorbeam · corroded · Oct 4, 2019 · N531EG · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > RH FLOOR CROSS BEAM AT FS280.00 HAS NUMEROUS AREAS OF CORROSION ON UPPER SURFACE WHERE IT IS LAYERED BETWEEN DRIP TRAY AND THE UPPER L ANGLE OF BULKHEAD WALL.-C/A-REMOVED AND REPLACED RH CROSSBEAM 280.00 IAW SRM 51-42-06 AND 51-42-10.
- [SDR SIMA201910154004](https://openairdocs.org/sdr/SIMA201910154004.md): Floorbeam · cracked · Oct 4, 2019 · N531EG · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > LH CENTER COCKPIT FLOOR BEAM BL 12.00 IS CRACKED, LOCATED JUST FWD OF FLOOR BEAM AT FS 280.00. COMPLETED INSTALLATION OF LH CENTER COCKPIT FLOOR BEAM AT BL12.00 / IAW SRM 53-11-43.
- [SDR SIMA201910140002](https://openairdocs.org/sdr/SIMA201910140002.md): Angle · cracked · Oct 4, 2019 · N531EG · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > RH CENTER COCKPIT FLOORBEAM BL 12.00 IS CRACKED, LOCATED JUST FWD OF FLOOR BEAM AT FS 280.00 -C/A-COMPLETED REPAIR AT RH CENTER COCKPIT FLOOR BEAM BL 12.00 LOCATED JUST FWD OF FLOOR BEAM FS280.00 IAW SRM 53-11-43.
- [SDR SIMA201910140003](https://openairdocs.org/sdr/SIMA201910140003.md): Floorbeam · corroded · Oct 4, 2019 · N531EG · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > LH FLOOR CROSS BEAM AT FS280.00 HAS NUMEROUS AREAS OF CORROSION ON UPPER SURFACE WHERE IT IS LAYERED BETWEEN DRIP TRAY AND THE UPPER L ANGLE OF BULKHEAD WALL.-C/A-COMPLETED REPAIR OF THE LH FLOOR CROSSBEAM AT FS280.00 IAW SRM 51-42-06, 51-42-10 AND 53-11-41.
- [SDR SIMA201908198002](https://openairdocs.org/sdr/SIMA201908198002.md): Unknown · odor · Aug 18, 2019 · N531EG · Cndair CL6002C10 · Air Distribution System
  > SMELL OF FUMES ON FLT DECK DURING FLIGHT, SMELLED LIKE POPCORN, FA 1 & FA 2 SMELLED STRONG SMELL BY THE EMERGENCY EXIT. SMELL LASTED 20 MIN THEN SUBSIDED BOTH PACKS ON & RECIR FAN, TURN FAN OFF SMELLED POPCORN BURNING REMAINED. UPON MTX ARRIVAL FOUND POPCORN
- [SDR SIMA201906173006](https://openairdocs.org/sdr/SIMA201906173006.md): Flashlight · inoperative · Jun 13, 2019 · N531EG · Cndair CL6002C10 · Emergency Equipment
  > FA FLASHLIGHT INOP-C/A-REPLACED FLASHLIGHT AS REQ OPC GOOD IAW CRJ-700 AMM 25-61-00
- [SDR SIMA20190511002](https://openairdocs.org/sdr/SIMA20190511002.md): Flashlight · inoperative · May 11, 2019 · N531EG · Cndair CL6002C10 · Emergency Lighting
  > SUPPLEMENTAL AFT FA FLASHLIGHT INOP. C/A-FLIGHT CREW PLACARDED AFT FA FLASHLIGHT MEL 2514 AUTH #050031 MOC #680993. REMOVED AND REPLACED AFT FA FLASHLIGHT AND CRADLE IAW AMM 25-61-02. OPC GOOD. MEL ITEM RESTORED.
- [SDR SIMA2019040329008](https://openairdocs.org/sdr/SIMA2019040329008.md): Module · failed · Mar 29, 2019 · N531EG · Cndair CL6002C10 · Landing Gear Steering System
  > SEE ITEM 2 THIS LOG PAGE, STEERING INOP MSG FOR THE SECOND TIME WHILE TAXIING TO THE RUNWAY.-C/A-REMOVED AND REPLACED STEERING MANIFOLD OPC LK CK GOOD AMM 32-51-50
- [SDR SIMA2018121211003](https://openairdocs.org/sdr/SIMA2018121211003.md): Compressor · contaminated · Dec 11, 2018 · N531EG · Cndair CL6002C10 · Turbine Engine Compressor Section
  > DURING CLIMB THROUGH APPROXIMATELY 9,000FT VMC AIRCRAFT CLEAN CONFIG NO ICING. M.W. FOR AFT LAV SMOKE ILLUMINATED. PAX AND CREW NOTICED ODOR. ALERT EXTINGUISHED AFTER APPROXIMATELY 1 MINUTE OR SO. ODOR LIKENED TO BURNING EXHAUST. LDG WT UNDER 64,000 #'S.-C/A-N
- [SDR SIMA201810098004](https://openairdocs.org/sdr/SIMA201810098004.md): Warning System · activated · Oct 8, 2018 · N531EG · Cndair CL6002C10 · Drag Control System
  > OB FLT SPLR & OB SPOILERONS CAUTION MESSAGE WHEN APPROACHING MCI EMERGENVY DECLARED. -C/A-INTERROGATED MDC R OB MFSPCU JAM MDC MESSAGE B1-007920 PERFORMED SPOST1 RESET PERFORMED OPS CK IAW ETN-CR-27-093 OPS CHEK GOOD FIRST OCCURANCE THIS AC.
- [SDR SIMA20180716002](https://openairdocs.org/sdr/SIMA20180716002.md): Insert · defective · Jul 16, 2018 · N531EG · Cndair CL6002C10 · Pneumatic Indicating System
  > L BLEED DUCT WARNING MESSAGE ON EICAS WHILE CLIMBING THROUGH 1500 FEET. R ENG BLEED ALSO CLOSED. NO BLEED SOURCE AVAILABLE-C/A-INTERROGATED MDC, FOUND CORRELATED CODE B1-349536. T/S PER FIM 36-21-01. LRU TEST INDICATES MT137 - 100%. REMOVED AND REPLACED CERAMI
- [SDR SIMA201804040004](https://openairdocs.org/sdr/SIMA201804040004.md): Bulb · failed · Mar 22, 2018 · N531EG · Cndair CL6002C10 · Water/Waste System Wiring
  > SMOKE COMING FROM WIRES IN THE LAVATORY SERVICE PANEL. ELECTRICAL SMOKE ODOR. WASTE SYSTEM CIRCUIT BREAKER TRIPPED. FOUND FLUID LEVEL LIGHT BULB BURNED OUT WHICH WAS THE CAUSE OF THE SMOKE IN THE AREA. RESET THE CIRCUIT BREAKER CB2-M9. REMOVED AND REPLACE
- [SDR SIMA20180302003](https://openairdocs.org/sdr/SIMA20180302003.md): Slat System · malfunctioned · Mar 2, 2018 · N531EG · Cndair CL6002C10 · Leading Edge Slat Control System
  > SLATS FAIL CAUTION ON APPROACH. INTERROGATED MDC, FOUND SLAT ACTUATOR SYSTEM, MECHANICAL BINDING MESSAGE B1-007772. PERFORMED ETN-CR-27-084. FOUND THE RTWING NR 2 AND 3 ACTUATORS TRIPPED. PERFORMED OPS TEST OF SLAT SYSTEM IAW AMM 27-50-00. OPS CHECK FAILE
- [SDR SIMA20170418004](https://openairdocs.org/sdr/SIMA20170418004.md): Web · cracked · Apr 18, 2017 · N531EG · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > LEFT FORWARD EQUIPMENT BAY FLOOR WEB HAS A 1/8" CRACK. COMPLETED A REPAIR TO LT FWD EQUIPMENT COMPARTMENT FLOOR IAW ETN-CR-53-099.

Next page: https://openairdocs.org/aircraft/N531EG/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 = 'N531EG' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N531EG/reports

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