# Service difficulty reports: N690CA

A list on [N690CA](https://openairdocs.org/aircraft/N690CA.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 4 · 152 reports

- [SDR REXA2025050900574](https://openairdocs.org/sdr/REXA2025050900574.md): Floor Support · corroded · May 9, 2025 · N690CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT AT PAX DOOR FS310-FS333 HAS CORROSION. REMOVED AND INSTALLED NEW SERVICEABLE PAX DOOR MID CAP ANGLE PN# SH670-31825-9S IAW CRJ 51-41-02-001-001-A01 AND 51-41-04-001-001-A01.
- [SDR REXA2025050900573](https://openairdocs.org/sdr/REXA2025050900573.md): Hinge · damaged · May 8, 2025 · N690CA · Cndair CL6002C10 · Fuselage, Door Hinge
  > PAX DOOR HINGE AFT ROLL PIN HOLE IS ELONGATED COMPLIED WITH MHIRJ REO# 670-52-11-1467 REV. -- DATED 3-13-2025 IN REPAIR OF DAMAGED SPRING PIN HOLE PAX DOOR HINGE
- [SDR REXA2025050800569](https://openairdocs.org/sdr/REXA2025050800569.md): Skin · corroded · May 8, 2025 · N690CA · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > F.S. 533-581 BAGGAGE DOOR SURROUND CORRODED, FWD AND CENTER TOP PLATES CORRODED IN MULTIPLE PLACES. REPAIRED FORWARD BAGGAGE BAY INNER CLOSING SKIN IAW ENDEAVOR AIR EA CRJ753-18690 REV IR DATED 3/17/2025
- [SDR REXA2025050700563](https://openairdocs.org/sdr/REXA2025050700563.md): Hinge · worn · May 5, 2025 · N690CA · Cndair CL6002C10 · Fuselage, Door Hinge
  > AFT MOST OUTER LUGS (10 EA.) ON PAX DOOR HINGE (FUSELAGE SIDE) HAVE INNER DIAMETERS THAT ARE WORN BEYOND THE ALLOWABLE LIMITS OF CRJ 700 SRM 53-21-23-201-010-A01, STEP 1A. REMOVED LOWER STRIKER P/N SH670-31886-1 AND DRAIN TUBE P/N SH670-31904-3 IAW CRJ700 SR
- [SDR REXA2025061300657](https://openairdocs.org/sdr/REXA2025061300657.md): Angle · not reported · May 1, 2025 · N690CA · Cndair CL6002C10 · Standard Practices/Structures
  > FABRICATION REQUIRED OF REINFORCEMENT JOINT ANGLE STA 310 & 349 PN SH670-31947-4. PART REQUIRED FOR MWC BARCODE HN00221783 S/N: 00795. LOCATED AND DRILLED REINFORCEMENT JOINT ANGLE STA 310 & 349 FOR EXAMPLE OF P/N SH670-31947-4 FROM 7075-0 0.040Ï¿½ PO# 5-598
- [SDR REXA2025050600548](https://openairdocs.org/sdr/REXA2025050600548.md): Angle · none · May 1, 2025 · N690CA · Cndair CL6002C10 · Standard Practices/Structures
  > FABRICATION REQUIRED OF REINFORCEMENT JOINT ANGLE STA 310 & 349 PN SH670-31947-4. PART REQUIRED FOR MWC BARCODE HN00221783 S/N: 00795. LOCATED AND DRILLED REINFORCEMENT JOINT ANGLE STA 310 & 349 FOR EXAMPLE OF P/N SH670-31947-4 FROM 7075-0 0.040Ï¿½ PO# 5-598
- [SDR REXA2025050200547](https://openairdocs.org/sdr/REXA2025050200547.md): Frame · corroded · May 1, 2025 · N690CA · Cndair CL6002C10 · Fuselage Main, Frame
  > F.S. 349 STR 26L-25R CORRODED IN MULTIPLE PLACES REMOVED AND REPLACED FRAME PN SH670-31357-5 AT F.S.349
- [SDR REXA2025041400427](https://openairdocs.org/sdr/REXA2025041400427.md): Stringer Splice · corroded · Apr 10, 2025 · N690CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > SPLICE AT FS477 STR21R IS CORRODED. REQUIRE EVALUATION. REMOVED DAMAGED SPLICE AT STR21R AND FS477 IAW CRJ700 SRM 51-42-06-001-001-A01. STRINGER SPLICE AT 21R AND FS477 HAS MORE THAN 50 PERCENT MATERIAL LOSS. NO DAMAGE LIMITS GIVEN FOR SPLICE AT FS477 AND 21
- [SDR REXA2025050200546](https://openairdocs.org/sdr/REXA2025050200546.md): Frame · corroded · Apr 7, 2025 · N690CA · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME SEGMENT AT FS333.00 CORRODED ON ATTACHED FLANGE AND FORWARD SIDE OF WEB BETWEEN STR 24R AND STR 26R. F.S. 333 FRAME SECTION AT STGR 24R - STGR 26R FOUND TO BE CORRODED BEYOND LIMITS IAW CRJ-700 SRM 53-00-06-201-005-A01. REMOVED CORRODED SECTION OF FRAME
- [SDR REXA2025041700444](https://openairdocs.org/sdr/REXA2025041700444.md): Stringer · corroded · Apr 7, 2025 · N690CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRG 23R (P/N SH670-31211-4) FOUND TO BE CORRODED BETWEEN FS295 - FS333. UPON FURTHER INVESTIGATION FOUND STR 23R BETWEEN FS280 - FS333 TO BE OUT OF LIMITS DUE TO EXCESSIVE CORROSION ON MORE THAN ONE ELEMENT OF STR 23R BETWEEN FS280 - FS333 IAW CRJ700 SRM 53-2
- [SDR REXA2025041400426](https://openairdocs.org/sdr/REXA2025041400426.md): Stringer Splice · corroded · Apr 7, 2025 · N690CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > "BTW FS.446 - 453 STGR 21R AND SPLICE IS CORRODED. REQUEST EVALUATION. UPON FURTHER INVESTIGATION CORROSION FOUND ON ST21R BETWEEN FS469 AND FS477 NO DAMAGE IS ALLOWED IN THIS SECTION OF THE STRINGER AS PER CRJ700 SRM 53-21-03-101-006-A01. REQUIRE REPLACEMENT
- [SDR REXA2025041400425](https://openairdocs.org/sdr/REXA2025041400425.md): Stringer · corroded · Apr 7, 2025 · N690CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRG 23R (P/N SH670-31211-4) FOUND TO BE CORRODED BETWEEN FS295 - FS333. UPON FURTHER INVESTIGATION FOUND STR 23R BETWEEN FS280 - FS333 TO BE OUT OF LIMITS DUE TO EXCESSIVE CORROSION ON MORE THAN ONE ELEMENT OF STR 23R BETWEEN FS280 - FS333 IAW CRJ700 SRM 53-2
- [SDR REXA2025041700443](https://openairdocs.org/sdr/REXA2025041700443.md): Stringer Splice · corroded · Apr 5, 2025 · N690CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STGR 23R JOINT PIECE (SPLICE) AT FS333 FOUND TO BE CORRODED INSTALLED NEW SERVICEABLE STGR 23R JOINT PIECE SPLICE (P/N:SH670-32429-4S) AT FS333 IAW CRJ 700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 51-42-21-001-001-A01.
- [SDR REXA2025041700442](https://openairdocs.org/sdr/REXA2025041700442.md): Stringer · corroded · Apr 5, 2025 · N690CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > AT FS 370.00 STGR 20R IS CORRODED. REQUEST EVALUATION. REMOVED AND REPLACED STRINGER 20R (P/N SH670-31405-2) BTW FS 349 TO 477 IAW CRJ700 SRM 51-40-11-001-001-A01.DRILLED NEW STRINGER (P/N SH670-31405-2) BTW FS 364 TO FS 477 IAW CRJ700 SRM 51-40-11-001-001-
- [SDR REXA2025042900524](https://openairdocs.org/sdr/REXA2025042900524.md): Angle · corroded · Mar 31, 2025 · N690CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CLIPS ON FWD AND AFT FORMERS @ FS 320 AND 338 ARE CORRODED AND REQUIRE REPLACEMENT. REMOVED 4 EACH CORRODED CLIPS. LOCATED, DRILLED AND INSTALLED NEW CLIPS, 2 EACH P/N: 600-31902-275 AND 600-31902-276, IAW CRJ 700/900 SRM 51-40-11-001-001-A01, 51-42-06-001-00
- [SDR REXA2025042900522](https://openairdocs.org/sdr/REXA2025042900522.md): Door Sill · corroded · Mar 7, 2025 · N690CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FORWARD CARGO DOOR SURROUND SILL P/N SH670-33764-3 AT STGR 25L IS CORRODED ON SILL TO FUSELAGE SKIN MATING SURFACE AT APPROX. FS526.00. REPAIRED IAW MHIRJ REO 670-53-31-1029 REV -- DATED 2025-04-25.
- [SDR REXA2025041400423](https://openairdocs.org/sdr/REXA2025041400423.md): Skin · corroded · Feb 26, 2025 · N690CA · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > FOUND CORROSION ON INNER SKIN AROUND WHAT APPEARS TO BE A SKIN PLUG RIVET AT APPROXIMATELY F.S. 286 BETWEEN STGR 26R AND STGR 25R. REPAIRED IAW ENDEAVOR AIR EA NO: CRJ753-18599 REV. IR DATED 3/11/2025.
- [SDR REXA2025041100418](https://openairdocs.org/sdr/REXA2025041100418.md): Stringer · corroded · Feb 25, 2025 · N690CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRG 24R (P/N SH670-31212-2) FOUND TO BE CORRODED BETWEEN FS295 - FS333. INSTALLED NEW STGR 24R P/N: SH670-31212-2 IAW CRJ700 SRM 51-42-06-001-001-A01. AND CRJ700 SRM 51-42-21-001-001-A01.
- [SDR REXA2025042500492](https://openairdocs.org/sdr/REXA2025042500492.md): Bracket · corroded · Feb 24, 2025 · N690CA · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR DD1A AFT BRACKET FOUND TO BE CRACKED. REMOVED PAX DOOR DD1A BRACKET. LOCATED, DRILLED AND INSTALLED NEW PART, P/N: 601R318084-2, IAW CRJ 700/900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01 REV. 38 DATED JUL/25/2020.
- [SDR REXA2025042500490](https://openairdocs.org/sdr/REXA2025042500490.md): Former · corroded · Feb 24, 2025 · N690CA · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR AFT FORMER IS CORRODED. REMOVED CORRODED PAX DOOR AFT FORMER. LOCATED, DRILLED AND INSTALLED NEW PART, P/N: 601R318034-5S, IAW CRJ-700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01,51-42-10-001-001-A01 AND 51-42-21-001-001-A01 REV. 38 DATED JUL 25
- [SDR REXA2025042500489](https://openairdocs.org/sdr/REXA2025042500489.md): Intercostal · corroded · Feb 24, 2025 · N690CA · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR AFT UPPER INTERCOSTAL DD1 IS CORRODED/DENTED. REMOVED CORRODED/DENTED PAX DOOR AFT UPPER INTERCOSTAL DD1. LOCATED, DRILLED AND INSTALLED NEW PART, P/N: 601R31902-318, IAW CRJ-700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01 REV. 38 DATED JUL 25
- [SDR REXA2025042400485](https://openairdocs.org/sdr/REXA2025042400485.md): Intercostal · corroded · Feb 24, 2025 · N690CA · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR AFT MID-LWR INTERCOSTAL IS CORRODED/DENTED. REMOVED CORRODED PAX DOOR AFT MID-LWR INTERCOSTAL. LOCATED, DRILLED AND INSTALLED NEW PART, P/N: 601R31902-317, IAW CRJ-700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01 REV. 38 DATED JUL 25/2020.
- [SDR REXA2025042300481](https://openairdocs.org/sdr/REXA2025042300481.md): Intercostal · corroded · Feb 24, 2025 · N690CA · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR AFT MID INTERCOSTAL CORRODED. REMOVED CORRODED PAX DOOR AFT MID INTERCOSTAL. LOCATED, DRILLED AND INSTALLED NEW PART, P/N: 601R31902-317A, IAW CRJ-700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01 REV. 38 DATED JUL 25/2020.
- [SDR REXA2025042300480](https://openairdocs.org/sdr/REXA2025042300480.md): Angle · cracked · Feb 24, 2025 · N690CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > PAX DOOR PRESSURE VENT FLAP ANGLE IS CRACKED. REMOVED CRACKED PAX DOOR PRESSURE VENT FLAP ANGLE. LOCATED, DRILLED AND INSTALLED NEW PART, P/N: 601R319055-1, IAW CRJ-700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01 REV. 38 DATED JUL 25/2020.
- [SDR REXA2025042300478](https://openairdocs.org/sdr/REXA2025042300478.md): Hinge · chafed · Feb 24, 2025 · N690CA · Cndair CL6002C10 · Fuselage, Door Hinge
  > PAX DOOR HINGE AFT FLATS ARE CHAFED. REPAIRED CHAFE DAMAGE TO HINGE LUG LANDS (9) AFT END PAX DOOR HINGE IAW CRJ 700/900 SRM 52-11-01-201-007-A01 D. TYPE IV REV. 38 DATED JUL/25/2020. SEE CRJ 700/900 SRM 52-11-01-210-007-A01 2.A REQUIRES REINSPECT AT INTERVAL
- [SDR REXA2025042200471](https://openairdocs.org/sdr/REXA2025042200471.md): Intercostal · corroded · Feb 24, 2025 · N690CA · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR LWR AFT INTERCOSTAL DD7 IS CORRODED/DENTED. REMOVED CORRODED PAX DOOR LWR AFT INTERCOSTAL DD7. LOCATED, DRILLED AND INSTALLED NEW PART, P/N: 601R318825-1, IAW CRJ-700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01 REV. 38 DATED JUL 25/2020.
- [SDR REXA2025042200470](https://openairdocs.org/sdr/REXA2025042200470.md): Intercostal · corroded · Feb 24, 2025 · N690CA · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR LWR MID INTERCOSTAL DD7A IS CORRODED. REMOVED CORRODED PAX DOOR LWR MID INTERCOSTAL DD7. LOCATED, DRILLED AND INSTALLED NEW PART, P/N: 601R318083-1, IAW CRJ-700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01 REV. 38 DATED JUL 25/2020.
- [SDR REXA2025050600560](https://openairdocs.org/sdr/REXA2025050600560.md): Stringer Splice · corroded · Feb 22, 2025 · N690CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > JOINT PLATE, LOWER EXTERNAL P/N: SH670-33793-4 FS.533, STGR 25L IS HEAVY CORRODED INSTALLED NEW SERVICEABLE JOINT PLATE (PN: SH670-33793-4) IAW CRJ-700 SRM 51-42-22-001-001-A01, AND CRJ-700 SRM 51-42-21-001-001-A01.
- [SDR REXA2025050600559](https://openairdocs.org/sdr/REXA2025050600559.md): Stringer Splice · corroded · Feb 22, 2025 · N690CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > JOINT PLATE, LOWER EXTERNAL P/N: SH670-33793-3 FS.581, STGR 25L IS HEAVY CORRODED. INSTALLED NEW SERVICEABLE JOINT PLATE (PN: SH670-33793-3) IAW CRJ-700 SRM 51-42-22-001-001-A01, AND CRJ-700 SRM 51-42-21-001-001-A01.
- [SDR REXA2025041700440](https://openairdocs.org/sdr/REXA2025041700440.md): Skin · corroded · Feb 19, 2025 · N690CA · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > FOUND CORROSION ON INNER SKIN AROUND WHAT APPEARS TO BE A SKIN PLUG RIVET AT APPROXIMATELY F.S. 286 BETWEEN STGR 26R AND STGR 25R. RECEIVED AND COMPLIED ALL STEPS OF OF ENDEAVOR AIR EA NO: CRJ753-18599 REV. IR DATED 3/11/2025.
- [SDR REXA2025041000417](https://openairdocs.org/sdr/REXA2025041000417.md): Stringer · corroded · Feb 19, 2025 · N690CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRG 22R (P/N SH670-31210-2) FOUND TO BE CORRODED BETWEEN FS280 - FS295. REMOVED STGR 22R P/N:SH670-31210-2 SEGMENT FROM FS 280.00 AND FS 333.00 IAW CRJ700 SRM 51-42-06-001-001-A01. AND CRJ700 SRM 51-42-21-001-001-A01. LOCATED AND DRILLED NEW STGR 22R P/N:SH67
- [SDR REXA2025022500219](https://openairdocs.org/sdr/REXA2025022500219.md): Tie Down · corroded · Feb 18, 2025 · N690CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > FS 530 AT STGR 27L CARGO TIE DOWN PAD IS CORRODED. REMOVED CORRODED CARGO TIE DOWN BRACKET AT FS 530 STGR 27 IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. INSTALLED A SERVICEABLE RH CARGO TIE DOWN BRACKET (SH670-33369-1) AT FS 530 STGR 27 IAW
- [SDR REXA2025052900598](https://openairdocs.org/sdr/REXA2025052900598.md): Intercostal · corroded · Feb 17, 2025 · N690CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > INTERCOSTALS LEFT AND RIGHT OF STR 27 CORRODED F.S. 349-364, MARKED REMOVED CORROSION ON INTERCOSTALS LEFT (P/N SH670-32075-3) AND RIGHT (P/N SH670-32075-4) OF STGR 27 AT FS364. OUT OF LIMITS DUE TO MULTIPLE FACTORS INCLUDING DAMAGE COVERING MORE THAN 30 PERCE
- [SDR REXA2025041700439](https://openairdocs.org/sdr/REXA2025041700439.md): Stringer · corroded · Feb 17, 2025 · N690CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > APPROX F.S.370 STR 21R SEVERELY CORRODED AT FASTENER HOLE (F.S. 364-379), MARKED LOCATED AND DRILLED NEW SERVICEABLE STR 21R PN: SH670-31383-1S AT FS333 TO FS394 IAW CRJ700 SRM 51-40-11-001-001-A01.
- [SDR REXA2025040300392](https://openairdocs.org/sdr/REXA2025040300392.md): Frame · corroded · Feb 17, 2025 · N690CA · Cndair CL6002C10 · Fuselage Main, Frame
  > FS 319 FRAME IS CORRODED BETWEEN STRINGERS 26L-26R. CUT AWAY DAMAGED PORTION OF FRAME AND SPLICED IN REPAIR PARTS IAW CRJ 700 SRM 53-00-06-201-006-A01.
- [SDR REXA2025040300389](https://openairdocs.org/sdr/REXA2025040300389.md): Stringer · corroded · Feb 17, 2025 · N690CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > F.S. 280-310 STR 25R CORRODED. REMOVED AND REPLACED IAW CRJ 700 SRMS 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.
- [SDR REXA2025040300388](https://openairdocs.org/sdr/REXA2025040300388.md): Frame · corroded · Feb 17, 2025 · N690CA · Cndair CL6002C10 · Fuselage Main, Frame
  > F.S. 295 STR 26L-26R CORRODED ON FWD AND AFT SIDE OF FRAME. REPAIRED BY CUTTING AWAY DAMAGED SECTION AND SPLICING IN REPAIR PARTS IAW CRJ700 SRM 53-00-06-201-006-A01.
- [SDR REXA2025040300386](https://openairdocs.org/sdr/REXA2025040300386.md): Stringer · corroded · Feb 17, 2025 · N690CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > F.S. 280-295 STR 26L CORRODED. REMOVED AND REPLACED IAW CRJ 700 SRMS 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.
- [SDR REXA2025040200382](https://openairdocs.org/sdr/REXA2025040200382.md): Seat Track · corroded · Feb 17, 2025 · N690CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RBL9 FLOOR SEAT TRACK IS CORRODED BETWEEN F.S. 1000 TO F.S. 1047. REMOVED RBL9 FLOOR SEAT TRACK BETWEEN F.S. 1000 TO F.S. 1047 INSTALLED RBL9 FLOOR SEAT TRACK BETWEEN F.S. 1000 TO F.S. 1047 IAW CRJ-700 53-00-49-400-802 (CONFIG A06).
- [SDR REXA2025040200381](https://openairdocs.org/sdr/REXA2025040200381.md): Seat Track · corroded · Feb 17, 2025 · N690CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > LBL9 FLOOR SEAT TRACK IS CORRODED BETWEEN F.S. 1000 TO F.S. 1047. REMOVED LBL9 FLOOR SEAT TRACK BETWEEN F.S. 1000 TO F.S. 1047 INSTALLED LBL9 FLOOR SEAT TRACK BETWEEN F.S. 1000 TO F.S. 1047 IAW CRJ-700 53-00-49-400-802 (CONFIG A06).
- [SDR REXA2025032400349](https://openairdocs.org/sdr/REXA2025032400349.md): Stringer · corroded · Feb 17, 2025 · N690CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > STR 26R F.S. 310-364 CORRODED IN MULTIPLE PLACES, MARKED. LOCATED AND DRILLED SERVICEABLE STGR 26R (P/N: SH670-31634-2S) IAW CRJ 700 SRM 51-40-11-001-001-A01. LOCATED AND DRILLED NEW SERVICEABLE STGR 26R AFT (P/N: SH670-31372-4S) IAW CRJ-700 SRM 51-40-11-001-0
- [SDR REXA2025031000296](https://openairdocs.org/sdr/REXA2025031000296.md): Floorbeam · corroded · Feb 15, 2025 · N690CA · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FS280 RH FLOOR SUPPORT HAS CORROSION BETWEEN RBL9 AND FLOOR SILL IN 2EA LOCATIONS. REMOVED DAMAGED FS 280.00 RH CROSSBEAM IAW CRJ700 SRM 51-42-06-001-001-A01. CRJ700 SRM 51-42-21-001-001-A01 AND CRJ700 SRM 51-42-13-001-001-A01. LOCATED AND DRILLED NEW RH FS.28
- [SDR REXA2025041700447](https://openairdocs.org/sdr/REXA2025041700447.md): Intercostal · corroded · Feb 9, 2025 · N690CA · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR LWR FWD INTERCOSTAL DD7 IS CORRODED/DENTED. REMOVED CORRODED/DENTED PAX DOOR LWR FWD INTERCOSTAL DD7. LOCATED, DRILLED AND INSTALLED NEW PART, P/N: 601R318826-1, IAW CRJ-700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01 REV. 38 DATED 25 JUL 20
- [SDR REXA2025041700438](https://openairdocs.org/sdr/REXA2025041700438.md): Angle · corroded · Feb 9, 2025 · N690CA · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR OUTER HANDLE LWR SUPPORT ANGLE IS CORRODED. REMOVED CORRODED PAX DOOR OUTER HANDLE LWR SUPPORT ANGLE. LOCATED, DRILLED AND INSTALLED NEW PART, P/N: 601R317052-1, IAW CRJ-700 SRM 51-40-11-001-001-A01 AND 51-42-21-001-001-A01 REV. 38 DATED JUL 25/20
- [SDR REXA2025041700437](https://openairdocs.org/sdr/REXA2025041700437.md): Intercostal · corroded · Feb 9, 2025 · N690CA · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR LWR MID INTERCOSTAL DD6 IS CORRODED. REMOVED CORRODED PAX DOOR LWR MID INTERCOSTAL DD6. LOCATED, DRILLED AND INSTALLED NEW PART, P/N: 601R318057-1, IAW CRJ-700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01 REV. 38 DATED JUL 25/2020.
- [SDR REXA2025041700436](https://openairdocs.org/sdr/REXA2025041700436.md): Former · corroded · Feb 9, 2025 · N690CA · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR MID FORMER, F.S.329.41, DD5/DD6 IS CORRODED. REMOVED CORRODED PAX DOOR MID FORMER, F.S. 329.41, DD5/DD6. LOCATED, DRILLED AND INSTALLED NEW PART, P/N: 601R318078-3, IAW CRJ-700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01 REV. 38 DATED JUL 25
- [SDR REXA2025041700435](https://openairdocs.org/sdr/REXA2025041700435.md): Former · corroded · Feb 9, 2025 · N690CA · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR MID FORMER, F.S.349.41, DD4/DD5 IS CORRODED. REMOVED CORRODED PAX DOOR MID FORMER, F.S. 349.41, DD4/DD5. LOCATED, DRILLED AND INSTALLED NEW PART, P/N: 601R318078-3, IAW CRJ-700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-42-21-001-00
- [SDR REXA2025041700434](https://openairdocs.org/sdr/REXA2025041700434.md): Intercostal · corroded · Feb 9, 2025 · N690CA · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR MID INTERCOSTAL DD4 IS CORRODED. REMOVED CORRODED PAX DOOR MID INTERCOSTAL DD4. LOCATED, DRILLED AND INSTALLED NEW PART, P/N: 601R318081-15, IAW CRJ-700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 REV. 38 DATED JUL 25
- [SDR REXA2025041700433](https://openairdocs.org/sdr/REXA2025041700433.md): Intercostal · corroded · Feb 9, 2025 · N690CA · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR MID UPPER INTERCOSTAL DD2 IS CORRODED. REMOVED CORRODED PAX DOOR MID UPPER INTERCOSTAL DD2. LOCATED, DRILLED AND INSTALLED NEW PART, P/N: 601R318053-3, IAW CRJ-700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01 REV. 38 DATED 25 JUL 2020.
- [SDR REXA2025041700431](https://openairdocs.org/sdr/REXA2025041700431.md): Intercostal · corroded · Feb 9, 2025 · N690CA · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR FWD MID INTERCOSTAL DD3 IS CORRODED/DENTED. REMOVED CORRODED/DENTED FWD MID INTERCOSTAL DD3. LOCATED, DRILLED AND INSTALLED NEW PART, P/N: 601R318054-1, IAW CRJ-700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01 REV. 38 DATED 25 JUL 2020

Next page: https://openairdocs.org/aircraft/N690CA/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 = 'N690CA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N690CA/reports

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