# Service difficulty reports: N354CA A list on [N354CA](https://openairdocs.org/aircraft/N354CA.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 5 · 203 reports - [SDR REXA2026081201540](https://openairdocs.org/sdr/REXA2026081201540.md): Lamp · inoperative · Aug 4, 2026 · N354CA · Cndair CL6002C10 · Emergency Lighting > AFT SIDE CABIN EMERGENCY LIGHT HAS SEVERAL BULBS INOP OK TO DEFER IAW MEL 33-51-1D CABIN ENCY LIGHT CEILING LEVEL LIGHTED EXIT SIGN AFT SIDE FACING (CAT C) MM02 UPDATED PLACARD INSTALLED NOTIFIED 19724 AT MOC. RELAMPED AFT FACING EMERGENCY LIGHT IN CABIN. RE - [SDR REXA2026081001530](https://openairdocs.org/sdr/REXA2026081001530.md): Lamp · inoperative · Aug 4, 2026 · N354CA · Cndair CL6002C10 · Emergency Lighting > AFT SIDE CABIN EMERGENCY LIGHT HAS SEVERAL BULBS INOP OK TO DEFER PER MEL 33-51-1D CABIN ENCY LIGHT CEILING LEVEL LIGHTED EXIT SIGN AFT SIDE FACING (CAT C) MM02 UPDATED PLACARD INSTALLED NOTIFIED 19724 AT MOC. RELAMPED AFT FACING EMERGENCY LIGHT IN CABIN. RE - [SDR REXA2026052800864](https://openairdocs.org/sdr/REXA2026052800864.md): Lamp · inoperative · May 26, 2026 · N354CA · Cndair CL6002C10 · Emergency Lighting > REAR CEILING EMERGENCY BULB OUT R/R AFT CEILING EMERGENCY FLOOD LIGHT BULB IAW AMM 33-51-09. OLD/NEW PN: 1317 - [SDR REXA2026012600023](https://openairdocs.org/sdr/REXA2026012600023.md): Lamp · inoperative · Jan 24, 2026 · N354CA · Cndair CL6002C10 · Emergency Lighting > CABIN EMERGENCY FLOOD LIGHT OUT AT ROW 9 R/R EMERGENCY FLOOD LIGHT BULB AT ROW 9 IAW CRJ 700 AMM 33-51-09. - [SDR REXA2024111501488](https://openairdocs.org/sdr/REXA2024111501488.md): Pressure Switch · inoperative · Nov 14, 2024 · N354CA · Cndair CL6002C10 · Engine Oil Pressure > AT CRUISE R OIL PRESS WARNING ILLUMINATED ALONG WITH UNCOMMANDED RUDDER MOVEMENTS TO THE LEFT AND RIGHT. OIL PRESSURE ON RIGHT ENGINE SHOWED 64 AND LEFT WAS 69. DISCONNECTED A/P AND RAN QRH FOR R OIL PRESS. AFTER RIGHT ENGINE WAS AT IDLE R OIL PRESS LIGHT CAME - [SDR REXA2022102402292](https://openairdocs.org/sdr/REXA2022102402292.md): Adc · inoperative · Oct 12, 2022 · N354CA · Cndair CL6002C10 · Air Data Computer > #1 ADC FAILURE WITH CORRESPONDING UNRELIABLE AIRSPEED INDICATION AND MULTIPLE EICAS MESSAGES. AIR RETURN TO ATL. R/R #1 ADC IAW CRJ 700 AMM 34-13-01. OPS TEST GOOD, LEAK TEST GOOD. PN OFF/ 822-0472-636, SN OFF/ 24GFK, PN ON /822-0372-436, SN ON/ 10HLG - [SDR REXA2022091502093](https://openairdocs.org/sdr/REXA2022091502093.md): Angle · corroded · Sep 13, 2022 · N354CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure > FRAME (ANGLE) CORRODED AT FS 265.00 BETWEEN STGR 26L AND 27 REMOVED AND REPLACED ANGLE I.A.W. BOMBARDIER CRJ900 SRM 51-42-06-001-001-A01. - [SDR REXA2022091502092](https://openairdocs.org/sdr/REXA2022091502092.md): Frame · cracked · Sep 13, 2022 · N354CA · Cndair CL6002C10 · Emergency Exits > L/H FWD OVERWING EXIT DOOR (S/N SBO532) TOP EDGE MEMBER IS CRACKED. REPAIRED DAMAGE I.A.W. ENDEAVOR EA CRJ952-14342 REV.IR, DATED 08/26/2022 - [SDR REXA2022091502091](https://openairdocs.org/sdr/REXA2022091502091.md): Frame · none · Sep 13, 2022 · N354CA · Cndair CL6002C10 · Emergency Exits > L/H AFT OVERWING EXIT (S/N SBO539) TOP EDGE MEMBER IS CRACKED COMPLIED WITH ENDEAVOR EA CRJ952-14340 REV IR DATED 8/26/22 - [SDR REXA2022091502090](https://openairdocs.org/sdr/REXA2022091502090.md): Battery · inoperative · Sep 8, 2022 · N354CA · Cndair CL6002C10 · Emergency Lighting > RH OVER WING EMERGENCY LIGHT OUT (AFT OF OVERWING EMERGENCY EXIT DOOR) R&R EMERGENCY BATTERY PACK PS37 IAW AMM 33-51-04. OPS CHECKS GOOD. P/N OFF: 2013-1A, S/N OFF: 119615, P/N ON: 2013-1ASMI, S/N ON: 15022 - [SDR REXA2022080201724](https://openairdocs.org/sdr/REXA2022080201724.md): Stringer · corroded · Jul 21, 2022 · N354CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure > FS280-FS319 STR21R CORROSION AROUND FASTENER HOLES. REMOVED AND REPLACED CORRODED STR21R, FROM FS280-FS319 PER CRJ700 SRM 51-42-06. - [SDR REXA2022072601702](https://openairdocs.org/sdr/REXA2022072601702.md): Floorbeam · corroded · Jul 19, 2022 · N354CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure > AFT CARGO FLOOR BEAM CAP AT RBL9.00 FROM FS1041 TO FS1088 HAS SURFACE CORROSION. REMOVED AND REPLACED CORRODED FLOOR BEAM CAP AT RBL9.00 FROM FS976-FS1088 PER CRJ700 SRM 53-00-41. - [SDR REXA2022072101645](https://openairdocs.org/sdr/REXA2022072101645.md): Stringer · corroded · Jul 14, 2022 · N354CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure > FS379 STR24L HAS TWO SPOTS OF CORROSION REMOVED CORROSION @ FS379 STRG24L. FOUND TO BE OUT OF LIMITS DUE TO NO DAMAGE ALLOWED. CUT OUT DAMAGED PORTION OF STRG24L. FABRICATED NEW ANGLE REPAIR AND INSTALLED. RESTORED FINISH ON WORKED SURFACES. PER. CRJ700 SRM 53 - [SDR REXA2022072101642](https://openairdocs.org/sdr/REXA2022072101642.md): Stringer · corroded · Jul 12, 2022 · N354CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure > FS333-FS349, STR26L STRINGER CORRODED. REMOVED AND REPLACED CORRODED STRINGER STR26L,FS333-FS349 IAW CRJ700 SRM 51-42-06. - [SDR REXA2022072101655](https://openairdocs.org/sdr/REXA2022072101655.md): Stringer · corroded · Jul 11, 2022 · N354CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure > STGR 21R FROM FS 394.00 TO FS 477.00 CORRODED REMOVED CORRODED SECTION OF STGR 21R FROM FS 394.00 TO FS 477.00 AND REPLACED WITH NEW SECTION PER CRJ700 SRM 51-42-21-001-001-A01 AND SRM 51-42-06-001-001-A01. - [SDR REXA2022072101654](https://openairdocs.org/sdr/REXA2022072101654.md): Stringer · corroded · Jul 11, 2022 · N354CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure > STGR 21R AT FS 340.00 TO FS 379.00 CORRODED REMOVED CORRODED SECTION OF STRINGER 21R AT FS 340.00 TO FS 379.00 AND REPLACED WITH NEW SECTION OF STRINGER PER CRJ700 SRM 51-42-21 AND SRM 51-42-06 - [SDR REXA2022072101649](https://openairdocs.org/sdr/REXA2022072101649.md): Stringer · corroded · Jul 11, 2022 · N354CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure > CORROSION FOUND ON STGR 19R AT FS 485.00 REMOVED DAMAGED SECTION OF STRINGER 19R FROM FS 479.00 TO FS 491.00 AND REPLACED WITH NEW SECTION OF STRINGER PER CRJ700 SRM 53-00-03 - [SDR REXA2022072101644](https://openairdocs.org/sdr/REXA2022072101644.md): Stringer · corroded · Jul 9, 2022 · N354CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure > CORROSION ON STR19R SECTION FROM FS280 TO FS310. REMOVED AND REPLACED CORRODED STR19R SECTION FROM FS280-FS310 IAW CRJ700 SRM 51-42-06 AND SRM 51-42-21. - [SDR REXA2022072101653](https://openairdocs.org/sdr/REXA2022072101653.md): Seat Track · corroded · Jul 7, 2022 · N354CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure > SEAT TRACK AT FS 379.00 LBL 9.00 CORRODED REMOVED CORRODED SEAT TRACK AT FS 379.00 LBL 9.00 AND REPLACED WITH NEW SEAT TRACK PER CRJ700 AMM 53-00-49 - [SDR REXA2022072101652](https://openairdocs.org/sdr/REXA2022072101652.md): Stringer · corroded · Jul 4, 2022 · N354CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure > STGR 18R AT FS 437.00 TO FS 453.00 CORRODED REMOVED CORRODED SECTION OF STRINGER 18R AT FS 437.00 TO FS 453.00 AND REPLACED WITH NEW SECTION OF STRINGER PER CRJ700 SRM 53-21-03-101-007-A01 - [SDR REXA2022072101651](https://openairdocs.org/sdr/REXA2022072101651.md): Stringer · corroded · Jul 4, 2022 · N354CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure > STGR 19R AT FS 476.00 CORRODED REMOVED CORRODED SECTION OF STGR 19R AT FS 421.00 TO FS 479.00 AND REPLACED WITH STRINGER SECTION PER CRJ700 SRM 53-00-03 - [SDR REXA2022072101650](https://openairdocs.org/sdr/REXA2022072101650.md): Intercostal · corroded · Jul 4, 2022 · N354CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure > INTERCOSTAL AT STGR 27(LH) AFT OF AVIONICS BAY DOOR AT FS 364.00 TO FS 379.00 CORRODED REMOVED CORRODED INTERCOSTAL AT STGR 27(LH) AFT OF AVIONICS BAY DOOR AT FS 364.00 TO FS 379.00 AND REPLACED WITH NEW INTERCOSTAL PER CRJ700 SRM 51-42-06 - [SDR REXA2022072101646](https://openairdocs.org/sdr/REXA2022072101646.md): Floor Support · corroded · Jul 2, 2022 · N354CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure > FLOOR BEAM AT FS 1004.00 TO FS 1088.00 LBL 27.00 CORRODED REMOVED CORRODED FLOOR BEAM AND REPLACED WITH NEW FLOOR BEAM - [SDR REXA2022072101648](https://openairdocs.org/sdr/REXA2022072101648.md): Seat Track · corroded · Jun 24, 2022 · N354CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure > SIDE SEAT RAIL AT FS 711.00 TO FS 761.00 RH SIDE CORRODED REMOVED SIDE SEAT RAIL AT FS 711.00 TO FS 761.00 RH SIDE AND REPLACED WITH NEW SEAT RAIL PER CRJ700 SRM 53-00-49 - [SDR REXA2022072101647](https://openairdocs.org/sdr/REXA2022072101647.md): Seat Track · corroded · Jun 24, 2022 · N354CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure > SIDE SEAT RAIL AT FS 711.00 TO FS 761.00 LH SIDE CORRODED REMOVED SIDE SEAT RAIL AT FS 711.00 TO FS 761.00 LH SIDE AND REPLACED WITH NEW SEAT RAIL PER CRJ700 SRM 53-00-49 - [SDR REXA2022062201305](https://openairdocs.org/sdr/REXA2022062201305.md): Intercostal · corroded · Jun 20, 2022 · N354CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure > INTERCOSTAL CORRODED FS 364.00 STGR 26L REMOVED CORRODED INTERCOSTAL AT FS 364.00 STGR 26L AND REPLACED WITH NEW INTERCOSTAL PER CRJ700 SRM 51-42-06 - [SDR REXA2022062201302](https://openairdocs.org/sdr/REXA2022062201302.md): Intercostal · corroded · Jun 20, 2022 · N354CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure > INTERCOSTAL CORRODED FS 364.00 STGR 26R REMOVED CORRODED INTERCOSTAL AT FS 364.00 STGR 26R AND REPLACED WITH NEW INTERCOSTAL PER CRJ700 SRM 51-42-06 - [SDR REXA2022062201304](https://openairdocs.org/sdr/REXA2022062201304.md): Stringer · corroded · Jun 16, 2022 · N354CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure > STGR 18R AT FS 421.00 TO 437.00 CORRODED REPLACED STGR 18R FROM FS 421.00 TO FS 475.00 PER CRJ700 SRM 51-42-06 - [SDR REXA2022062201303](https://openairdocs.org/sdr/REXA2022062201303.md): Frame · corroded · Jun 10, 2022 · N354CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure > FRAME SECTION AT FS 565.00 STGR 17L TO STGR 18L CORRODED REMOVED CORRODED FRAME SECTION AT FS 565.00 STGR 17L TO STGR 18L AND REPLACED WITH NEW FRAME SECTION PER CRJ700 SRM 51-42-06-001-001-A01 - [SDR REXA2022062201301](https://openairdocs.org/sdr/REXA2022062201301.md): Seat Track · corroded · Jun 8, 2022 · N354CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure > MAIN CABIN SIDE SEAT TRACK AT FS 785.00 TO FS 855.00 CORRODED CA REMOVED CORRODED SIDE SEAT TRACK AT FS 785.00 TO FS 855.00 AND REPLACED WITH SIDE SEAT TRACK PER CRJ700 SRM 53-41-49 AND AMM 53-00-49 - [SDR REXA2022060801126](https://openairdocs.org/sdr/REXA2022060801126.md): Angle · corroded · Jun 6, 2022 · N354CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure > FWD CARGO DOOR CUTOUT AFT UPPER CORNER AT FS 581.00 SIGNS OF CORROSION REMOVED CORROSION ON FWD CARGO DOOR CUTOUT AFT UPPER CORNER PER CRJ700 SRM 51-21-06-001-001-A01 - [SDR REXA2022060801127](https://openairdocs.org/sdr/REXA2022060801127.md): Intercostal · corroded · Jun 3, 2022 · N354CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure > INTERCOSTAL AT STGR 27 FS 364.00 TO 379.00 CORRODED REMOVED CORRODED INTERCOSTAL AT STGR 27 FS 364.00 TO FS 379.00 AND REPLACED WITH NEW INTERCOSTAL PER CRJ700 SRM 51-42-06. - [SDR REXA2022060801125](https://openairdocs.org/sdr/REXA2022060801125.md): Seat Track · corroded · Jun 3, 2022 · N354CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure > MAIN CABIN SIDE SEAT TRACK AT FS 785.00 TO FS 855.00 CORRODED REMOVED AND REPLACED SIDE SEAT TRACK AT FS 785.00 TO 855.00 PER CRJ700 AMM 53-00-49 - [SDR REXA2022060801128](https://openairdocs.org/sdr/REXA2022060801128.md): Bracket · cracked · Apr 18, 2022 · N354CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure > AFT CARGO, AFT LOWER DOOR TRACK SUPPORT HAS CRACK. PNS: MM670-B5552-005 & CC670-58814-1 REMOVED AND REPLACED AFT LOWER DOOR TRACK IAW CRJ700 SRM51-42-06. - [SDR REXA2022072101643](https://openairdocs.org/sdr/REXA2022072101643.md): Bracket · cracked · Mar 23, 2022 · N354CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer > FS 1088.00 STGR 8R SUPPORT BRACKET CRACKED REMOVED CRACKED SUPPORT BRACKET AT FS 1088.00 STGR 8R AND REPLACED WITH NEW SUPPORT BRACKET PER CRJ700 SRM 51-42-06. - [SDR REXA2022081801900](https://openairdocs.org/sdr/REXA2022081801900.md): None · cracked · Mar 9, 2022 · N354CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure > A 1.00 INCH CRACK WAS FOUND IN THE FLOOR BEAM SUPPORT, ADJACENT TO AN EXISTING FASTENER, AT FS 280.00, WL 72.00, LBL 13.50. REPAIRED PER REO 670-53-11-1797. - [SDR N6WA20181115402](https://openairdocs.org/sdr/N6WA20181115402.md): Light · inoperative · Nov 14, 2018 · N354CA · Cndair CL6002C10 · Emergency Lighting > AFT EMERGENCY FLOODLIGHT INOP. R&R AFT EMERGANCY EXIT LIGHT IAW CRJ700 AMM 33-51-15. OPS CHECK GOOD. - [SDR N6WA20181109701](https://openairdocs.org/sdr/N6WA20181109701.md): Seal · detached · Nov 7, 2018 · N354CA · Cndair CL6002C10 · Passenger/Crew Doors > MAIN CABIN DOOR SEAL DETACHED. R&R PAX DOOR SEAL IAW CRJ700 AMM 52-11-07. LEAK CHECK GOOD, NO DEFECTS NOTED AT THIS TIME. - [SDR N6WA201805302901](https://openairdocs.org/sdr/N6WA201805302901.md): Bulb · inoperative · May 29, 2018 · N354CA · Cndair CL6002C10 · Emergency Lighting > CEILING EMERGENCY LIGHT WAS INOPERATIVE AT ROW 6. R & R THE BULB IAW AMM 33-51-09, OPS CHECKED GOOD. - [SDR N6WA20180517601](https://openairdocs.org/sdr/N6WA20180517601.md): Connector · disconnected · May 16, 2018 · N354CA · Cndair CL6002C10 · Light System Wiring > EXIT ROW EMERGENCY LIGHT INOPERATIVE. CONNECTED THE CONNECTOR AND OPS CHECKED GOOD IAW AMM- 33-57-01. - [SDR V0XD20180517006](https://openairdocs.org/sdr/V0XD20180517006.md): Support Angle · cracked · May 11, 2018 · N354CA · Cndair CL6002C10 · Passenger/Crew Doors > PASSENGER DOOR VENT FLAP INTERNAL SUPPORT BRACKET IS CRACKED. REMOVED AND REPLACED ANGLE SUPPORT BRACKET(PN: 601R318072-1) IAW SRM 51-42-06, 51-40-11, AND 51-25-16. - [SDR V0XD20180517005](https://openairdocs.org/sdr/V0XD20180517005.md): Beam · cracked · May 11, 2018 · N354CA · Cndair CL6002C10 · Passenger/Crew Doors > PASSENGER DOOR GAS SPRING BEAM IS CRACKED. CORRECTIVE ACTION: REMOVED AND REPLACED GAS SPRING BEAM(PN: 601R318011-1) IAW SRM 51-42-06, 51-40-11, 51-25-16, AND AMM 52-11-17. - [SDR V0XD20180502007](https://openairdocs.org/sdr/V0XD20180502007.md): Flap · dented · Apr 27, 2018 · N354CA · Cndair CL6002C10 · Trailing Edge Flaps > LT I/B FLAP HAS TWO DENTS. REPAIRED DENTS BY FABRICATING AND INSTALLING REPAIR PARTS IAW REO 670-57-52-412 DATED 20 APR 2018. - [SDR V0XD20180422006](https://openairdocs.org/sdr/V0XD20180422006.md): Floorbeam · cracked · Apr 22, 2018 · N354CA · Cndair CL6002C10 · Fuselage Main, Floor Beam > LEFT SIDE BS 280 FLOORBEAM FOUND CRACKED. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 53-11-41, 51-25-16, 51-21-11, 51-40-11, 51-25-06, 51-42-21, 51-42-13, AMM 20-70-00, AND NDT MANUAL PART 1 51-20-006. - [SDR V0XD20180421005](https://openairdocs.org/sdr/V0XD20180421005.md): Bracket · cracked · Apr 21, 2018 · N354CA · Cndair CL6002C10 · Fuselage Main, Attach Fittings > AFT EQUIPMENT BAY, LT WING ANTI-ICE DUCT MOUNTING BRACKET CRACKED. REMOVED AND REPLACED THE MOUNTING BRACKET IAW SRM 51-42-21. - [SDR V0XD20180420004](https://openairdocs.org/sdr/V0XD20180420004.md): Bracket · cracked · Apr 20, 2018 · N354CA · Cndair CL6002C10 · Leading Edge Devices > LEFT SLAT 1 - 3 SLAT BOX BRACKET CRACKED. CUT AND REMOVED THE DAMAGED AREA, INSTALLED A FABRICATED PART IAW REO 670-57-42-577 REV -, SRM 51-23-00, 51-26-00, AND NDTM PART 01, 51-20-006. - [SDR V0XD20180420003](https://openairdocs.org/sdr/V0XD20180420003.md): Bracket · cracked · Apr 20, 2018 · N354CA · Cndair CL6002C10 · Leading Edge Devices > RIGHT SLAT 1 - 3 SLAT BOX BRACKET CRACKED. CUT AND REMOVED THE DAMAGED AREA, INSTALLED A FABRICATED PART IAW REO 670-57-42-577, REV -, SRM 51-23-00, AND NDTM PART 01 51-20-006. - [SDR V0XD20180420002](https://openairdocs.org/sdr/V0XD20180420002.md): Intercostal · corroded · Apr 20, 2018 · N354CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure > LEFT INBD INTERCOSTAL IN THE FWD AVIONICS BAY BETWEEN BS 349 AND 364, HAD SIGNS OF CORROSION. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-42-06, AND SRM 51-42-21. - [SDR V0XD20180420001](https://openairdocs.org/sdr/V0XD20180420001.md): Intercostal · corroded · Apr 20, 2018 · N354CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure > FWD AVIONICS BAY, LEFT INBD INTERCOSTAL, BS 394 - 409 HAS SIGNS OF CORROSION. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-42-06, AND 51-42-21. - [SDR V0XD20180420005](https://openairdocs.org/sdr/V0XD20180420005.md): Rib · cracked · Apr 19, 2018 · N354CA · Cndair CL6002C10 · Wing, Rib/Bulkhead > LEFT WING PARTIAL RIB AT WS 58.41 IS CRACKED. REMOVED AND REPLACED THE RIB IAW SRM 51-42-06, 51-42-13, 51-42-15, 51-40-11, 51-42-21, AND 51-25-06. Next page: https://openairdocs.org/aircraft/N354CA/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 = 'N354CA' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N354CA/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.