# Service difficulty reports: N669CA

A list on [N669CA](https://openairdocs.org/aircraft/N669CA.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 · 187 reports

- [SDR REXA2026020300029](https://openairdocs.org/sdr/REXA2026020300029.md): Pushrod · inoperative · Jan 30, 2026 · N669CA · Cndair CL6002C10 · Passenger/Crew Doors
  > MAIN PASSENGER DOOR UNABLE TO OPEN. FOUND PUSH ROD AT MID PIVOT OUT OF ADJUSTMENT. ADJUSTED PUSH ROD TO PAWL CONTROL ROD IAW AMM 52-11-02.
- [SDR REXA2025032800362](https://openairdocs.org/sdr/REXA2025032800362.md): Frame · corroded · Mar 27, 2025 · N669CA · Cndair CL6002C10 · Fuselage Main, Frame
  > FS 549 IS CORRODED BETWEEN STGR 26L AND STGR 27 IN THE FWD BAGGAGE BAY REMOVED AND REPLACED FRAME SECTION BETWEEN STGR 26L AND STGR 27 IAW ENDEAVOR EA CRJ753-18457 REV--IR DATE 02/19/2025.
- [SDR REXA2025032000336](https://openairdocs.org/sdr/REXA2025032000336.md): Seat Track · corroded · Mar 19, 2025 · N669CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > "THERE IS EVIDENCE OF CORROSION IN MULTIPLE AREAS OF THE FLOOR BEAM FROM FS 1000 TO FS 1051 RBL 27 FABRICATED, LOCATED, DRILLED AND INSTALLED NEW FLOOR BEAM SECTION FROM RBL 27 FS977 TO FS 1088.20. ITEM 12 (6EA) MADE FROM 7075-T6 0.100"" PO# W83825, ITEM 25 (
- [SDR REXA2025031700329](https://openairdocs.org/sdr/REXA2025031700329.md): Seat Track · corroded · Mar 14, 2025 · N669CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RBL 9.0 FLOOR TRACK CORRODED BETWEEN FS 977 AND FS 1005. FABRICATED AND INSTALLED REPLACEMENT RBL 9.0 FLOOR TRACK P/N: BA670-45073-3 OUT OF BULK STOCK P/N: 20276-288-0-0A, PO# W77329 IAW MHIRJ REO 670-53-00-589 REV-C. DATE: 2023-02-08
- [SDR REXA2025031700328](https://openairdocs.org/sdr/REXA2025031700328.md): Stringer Clip · corroded · Mar 14, 2025 · N669CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > F.S. 310 FRAME TO STGR 22L CLIP IS CORRODED. REMOVED AND REPLACED STRINGER CLEAT P/N: SH670-35625-2 AT FS310 & STR 22L IAW CRJ700 SRM 51-42-06-001-001-A01
- [SDR REXA2025031700327](https://openairdocs.org/sdr/REXA2025031700327.md): Intercostal · corroded · Mar 14, 2025 · N669CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > PAX DOOR INTERCOSTAL BETWEEN F.S. 319 TO F.S. 333 IS CORRODED. DISPLACED WIRE BUNDLE AT F.S. 310 BETWEEN 19L AND 18L FOR ACCESS TO CORRODED AREA IAW CRJ-700 SRM 51-41-02-001-001-A01. DISPLACED 10EA GROUND WIRES (#1,GS443, GS1839,GS1841,#2,GS329,GS319,GS317,#3
- [SDR REXA2025031100299](https://openairdocs.org/sdr/REXA2025031100299.md): Stringer · corroded · Mar 3, 2025 · N669CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STGR 24L IS CORRODED BETWEEN F.S. 333 TO F.S. 349. REPAIRED DAMAGED SECTION OF STGR 24L FROM PRODUCTION SPLICE AT F.S. 333 TO REPAIR SPLICE AT F.S. 379-394 IAW CRJ-700 SRM 53-00-03-201-001-A01 FIG. 53-00-03-991-804 SOLUTION II - S6294 TYPE Z7.
- [SDR REXA2025022100212](https://openairdocs.org/sdr/REXA2025022100212.md): Intercostal · corroded · Feb 20, 2025 · N669CA · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR FWD DD5 INTERCOSTAL FOUND TO BE CORRODED. REQUIRES REPLACEMENT. PN: 601R318091-3 REPAIRED INTERCOSTAL IAW ENDEAVOR AIR EA CRJ752-18154 REV IR DATED 1/27/2025 REFERENCE ATTACHMENTS FOR COMPLETED EA
- [SDR REXA2025032100340](https://openairdocs.org/sdr/REXA2025032100340.md): Stringer · corroded · Feb 19, 2025 · N669CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > UPON REMOVAL OF STGR 19L CLEAT @ FS 295 FOUND STGR 19L TO BE CORRODED. REPLACED STRINGER SECTION PER EA#: CRJ753-18568, ISSUE DATE: 3/3/2025, EA REV IR
- [SDR REXA2025022100211](https://openairdocs.org/sdr/REXA2025022100211.md): Frame · corroded · Feb 15, 2025 · N669CA · Cndair CL6002C10 · Fuselage Main, Frame
  > FS 565 IS CORRODED BETWEEN STR 17L AND 18L. REOAIRED PER ENDEAVOR AIR EA# CRJ753-18348.
- [SDR REXA2025031400319](https://openairdocs.org/sdr/REXA2025031400319.md): Frame · corroded · Feb 13, 2025 · N669CA · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME SEGMENT AT FS319.70 IS CORRODED BETWEEN STR 20L AND STR 21L. LOCATED AND DRILLED NEW SERVICEABLE FRAME SEGMENT PN: SH670-31891-3S IAW CRJ700 SRM 51-40-11-001-001-A01.INSTALLED NEW SERVICEABLE FRAME SEGMENT PN: SH670-31891-3S IAW CRJ700 SRM 51-42-06-001-0
- [SDR REXA2025021200189](https://openairdocs.org/sdr/REXA2025021200189.md): Seat Track · corroded · Feb 11, 2025 · N669CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > R/H SIDE SEAT TRACK IS CORRODED BETWEEN F.S. 724 TO F.S. 761. REMOVED UNSERVICEABLE R/H SIDE SEAT TRACK BETWEEN F.S.713 TO F.S.761 IAW CRJ 700 AMM 53-00-49-000-801-A03.PAINTED NEW SERVICEABLE R/H SIDE SEAT TRACK (P/N:SH670-37509-1) IAW BOMBARDIER MODSUM IS670
- [SDR REXA2025020500132](https://openairdocs.org/sdr/REXA2025020500132.md): Seat Track · corroded · Feb 4, 2025 · N669CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > MULTIPLE AREAS OF CORROSION ON THE FLOOR SEAT TRACK FROM FS 847 TO FS 989 AT RBL9 REMOVED CORRODED SEAT TRACK AND INSTALLED NEW SERVICEABLE FLOOR SEAT TRACK FROM FS 847 TO FS 989 AT RBL9 (P/N: SH670-37411-3) IAW CRJ 700 AMM 53-00-49-400-801-A17.
- [SDR REXA2025020500124](https://openairdocs.org/sdr/REXA2025020500124.md): Bracket · chafed · Feb 4, 2025 · N669CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > R/H WHEEL WELL FWD WHEEL BIN ATTACHMENT BRACKET AFT FACE IS CHAFED. REMOVED AND EPLACED WHEEL BIN BRACKET CC670-39221-4: LOCATED 13 HOLES FOR HI-LITES IAW CRJ700 SRM 51-40-11-001-001-A01 INSTALLED 13 HI-LITES IAW CRJ700 SRM 51-42-21-001-001-A01 LOCATED 8 HOLES
- [SDR REXA2025032400353](https://openairdocs.org/sdr/REXA2025032400353.md): Floorbeam · corroded · Feb 3, 2025 · N669CA · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > TOP OF R/H F.S. 280 BEAM IS CORRODED BETWEEN RBL 9 TO RBL18. REPLACED FLOOR BEAM PER REO'S 670-53-11-579 AND 670-53-21-2563.
- [SDR REXA2025022500218](https://openairdocs.org/sdr/REXA2025022500218.md): Floorbeam · corroded · Feb 3, 2025 · N669CA · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > TOP OF L/H F.S. 280 BEAM IS BENT AND CORROSION BETWEEN LBL 9 TO LBL 27. COMPLIED WITH BOMBARDIER GREO 670-53-11-579, REV. B, DATED 2013/05/01
- [SDR REXA2025022100210](https://openairdocs.org/sdr/REXA2025022100210.md): Angle · corroded · Feb 3, 2025 · N669CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > RBL 11 FIGHT COMPARTMENT ENTRY WAY BEAM IS CORRODED AT THE BOTTOM. COMPLETED REPAIR AT RBL 11 IAW CRJ-700 SRM 53-11-10-201-006-A01
- [SDR REXA2025021000156](https://openairdocs.org/sdr/REXA2025021000156.md): Floorbeam · corroded · Feb 3, 2025 · N669CA · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > TOP OF L/H F.S. 280 BEAM IS BENT AND CORROSION BETWEEN LBL 9 TO LBL 27. INSTALLED NEW L/H FS 280 BEAM IAW CRJ-700 SRM
- [SDR REXA2025022500217](https://openairdocs.org/sdr/REXA2025022500217.md): Post · corroded · Jan 30, 2025 · N669CA · Cndair CL6002C10 · Fuselage Main, Structure
  > RBL9 COCKPIT DOOR POST IS CORRODED AT FLOOR LEVEL. REPAIRED RBL9 COCKPIT DOOR POST IAW CRJ700 SRM 53-11-10-201-006-A01 IAW CRJ700 SRM 53-11-10-201-006-A01 REPAIR OPTION A.
- [SDR REXA2025031000295](https://openairdocs.org/sdr/REXA2025031000295.md): Floorbeam · corroded · Jan 25, 2025 · N669CA · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > THERE IS EVIDENCE OF CORROSION IN MULTIPLE AREAS OF THE FLOOR CROSS BEAM AT FS 1031 BETWEEN RBL9 AND RBL27. REPAIRED PER REO 670-53-61-2471.
- [SDR REXA2025031000294](https://openairdocs.org/sdr/REXA2025031000294.md): Stringer · corroded · Jan 24, 2025 · N669CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STGR19R HAS CORROSION BETWEEN FS501 AND FS517. REPAIRED STR 19R AT APPROX. FS604 AND REPLACE DAMAGED SECTION FROM FS604 SPLICE REPAIR TO FS477 PRODUCTION SPLICE PER CRJ 700 SRM 53-00-03-201-001-A01.
- [SDR REXA2025030300248](https://openairdocs.org/sdr/REXA2025030300248.md): Seat Track · corroded · Jan 24, 2025 · N669CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RBL 9.0 FLOOR TRACK CORRODED BETWEEN FS 1005 AND FS 1041. REMOVED FLOOR TRACK PN: BA670-35546-001 IAW CRJ700 AMM 53-00-49-000-802. INSTALLED NEW FLOOR TRACK P/N BA670-35546-001 IAW CRJ 700 AMM 53-00-49-400-802-A06 AND PAINTED NEW SERVICEABLE FLOOR SEAT TRACK I
- [SDR REXA2025022600229](https://openairdocs.org/sdr/REXA2025022600229.md): Frame · corroded · Jan 24, 2025 · N669CA · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME AT FS549 HAS CORROSION BETWEEN STGR 17L AND 18L. COMPLIED WITH EA NO: CRJ753-18456 REV IR DATED 02/19/2025.
- [SDR REXA2025033100365](https://openairdocs.org/sdr/REXA2025033100365.md): Stringer · corroded · Jan 23, 2025 · N669CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > "FS333-349 STGR 24R HAS CORROSION. REMOVED CORROSION AT STR 24R BETWEEN FS 333 TO FS364 IAW CRJ-700 SRM 51-21-06-001-001-A01. EVALUATED AND FOUND TO BE OUT OF LIMITS DUE TO HAVING A 100% LOSS MATERIAL ON STRINGER AT STR 24R BETWEEN FS333 TO FS364, AND NO DAMAG
- [SDR REXA2025031000293](https://openairdocs.org/sdr/REXA2025031000293.md): Stringer · corroded · Jan 23, 2025 · N669CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > FS364-379 STGR 19R HAS CORROSION. EVALUATED AND FOUND TO BE OUT OF LIMITS DUE TO HAS A 100% OF LOSS MATERIAL, IAW CRJ-700 SRM 53-21-03-101-007-A01. REMOVED AND REPLACED STGR 19R PN SH670-31103-4S. LOCATED AND DRILLED NEW SERVICEABLE STGR 19R BETWEEN FS 349 - F
- [SDR REXA2025031000292](https://openairdocs.org/sdr/REXA2025031000292.md): Support · corroded · Jan 23, 2025 · N669CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > STGR 21L IS CORRODED AT FS333-349. UPON FURTHER INVESTIGATION FOUND THE DAMAGE IS ON THE BACKUP SILL, NO ON THE STRINGER, AND THE BACKUP SILL IS OUT OF LIMIT DUE TO HAS CORROSION ON TWO ELEMENT, IAW CRJ-700 SRM 53-21-23-101-001-A01. LOCATED AND DRILLED STR 21L
- [SDR REXA2025030400255](https://openairdocs.org/sdr/REXA2025030400255.md): Intercostal · corroded · Jan 23, 2025 · N669CA · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR MID INTERCOSTAL DD3 FOUND TO BE CORRODED. REMOVED MID INTERCOSTAL DD3 IAW CRJ700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. INSTALLED MID INTERCOSTAL DD3 IAW CRJ700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
- [SDR REXA2025030400254](https://openairdocs.org/sdr/REXA2025030400254.md): Intercostal · corroded · Jan 23, 2025 · N669CA · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR DD6 MID INTERCOSTAL IS CORRODED. PAX DOOR MID INTERCOSTAL DD6 REMOVED AND INSTALLED NEW DD6 MID INTERCOSTAL IAW CRJ700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 PN: 601R318057-1.
- [SDR REXA2025030300247](https://openairdocs.org/sdr/REXA2025030300247.md): Stringer Splice · corroded · Jan 23, 2025 · N669CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STGR21R CORRODED BETWEEN FS379 AND FS394. REMOVED STGR 21R JOINT PIECE P/N: SH670-32301-5 IAW CRJ 700 SRM 51-42-06-001-001-A01.INSTALLED RIVETS INTO NEW SERVICEABLE STR 21R JOINT PIECE PN:SH670-32301-5 IAW CRJ700 SRM 51-42-06-001-001-A01.
- [SDR REXA2025030300246](https://openairdocs.org/sdr/REXA2025030300246.md): Frame · corroded · Jan 23, 2025 · N669CA · Cndair CL6002C10 · Fuselage Main, Frame
  > FS379 BETWEEN 20R AND 21R HAS CORROSION. REMOVED DAMAGED FRAME AT FS379 BETWEEN STR20R TO STR24R IAW CRJ-700 SRM 51-42-06-001-001-A01. INSTALLED SKIN RIVETS INTO NEW SERVICEABLE FRAME PN: SH670-32118-3S AND INSTALLED 15EA RIVETS INTO FRAME/REINFORCEMENT ANGLE
- [SDR REXA2025022600228](https://openairdocs.org/sdr/REXA2025022600228.md): Floorbeam · corroded · Jan 23, 2025 · N669CA · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > RBL 9 FLOOR BEAM IS CORRODED AT F.S. 549. REMOVED UNSERVICEABLE FLOOR BEAM RBL9 FROM FS.540 TO FS.571.45 IAW CRJ700 SRM 53-00-41-201-001-A01 INSTALLED NEW SECTION OF BEAM FROM FS540 TO FS571.45 FROM P/N B0549003BF IAW CRJ700 SRM 53-00-41-201-001-A01 INSTALLED
- [SDR REXA2025040100375](https://openairdocs.org/sdr/REXA2025040100375.md): Floorbeam · corroded · Jan 22, 2025 · N669CA · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > TOP OF R/H F.S. 280 BEAM IS CORRODED BETWEEN RBL 9 TO RBL18. REPAIRED IAW REO NO: 670-53-11--2099, REV. --, DATE: 2025-02-12 AND GREO 670--53-11-579, REV. B, DATED 2013/05/01.
- [SDR REXA2025033100364](https://openairdocs.org/sdr/REXA2025033100364.md): Frame · corroded · Jan 22, 2025 · N669CA · Cndair CL6002C10 · Fuselage Main, Frame
  > FS 565 IS CORRODED BETWEEN STGR 26L AND STGR 27 IN THE FWD BAGGAGE BAY REMOVED 6 EACH RIVETS FROM FS565 BETWEEN STR 26L AND STR27 TO FACILITATE EVALUATION IAW CRJ700 SRM 51-42-06-001-001-A01. RIVETS REPLACED IAW ENEDAVOR AIR EA CRJ753-18450 REV IR (PRELIMINAR
- [SDR REXA2025032100339](https://openairdocs.org/sdr/REXA2025032100339.md): Stringer · corroded · Jan 22, 2025 · N669CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON STGR 27 FROM FS 517 TO FS 597 IN THE FWD BAGGAGE BAY INSTALLED NEW STRINGER 27 AND REPAIR SPLICE IAW CRJ700 SRM 53-00-03-201-001-A01
- [SDR REXA2025031700325](https://openairdocs.org/sdr/REXA2025031700325.md): Floorbeam · corroded · Jan 22, 2025 · N669CA · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FLOOR CROSS BEAM IS CORRODED AROUND SCREW HOLE BETWEEN LBL9 TO RBL9 AT F.S. 333. REPAIRED FLOOR CROSSBEAM LBL 9 - RBL 9 FS 333 IAW REO 670-53-21-2571 REV -- DATED 2025-03-12
- [SDR REXA2025030400253](https://openairdocs.org/sdr/REXA2025030400253.md): Stringer · corroded · Jan 22, 2025 · N669CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STGR 21L IS CORRODED AT F.S. 379 UPON FURTHER INVESTIGATION FOUND ADDITIONAL DAMAGE ON THE JOINT ANGLE AT FS364 STR 21L, (FS 379 STR 21L) AFT AND JOINT ANGLE. REMOVED AND REPLACED 3EA RIVETS TO GAIN ACCESS TO CORROSION IAW CRJ700 SRM 51-42-06-001-001-A01. EVAL
- [SDR REXA2025030300244](https://openairdocs.org/sdr/REXA2025030300244.md): Seat Track · corroded · Jan 22, 2025 · N669CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RBL9 FLOOR SEAT TRACK IS CORRODED BETWEEN F.S. 349 TO F.S. 485. REMOVED CORRODED SEAT TRACK IAW CRJ700 AMM 53-00-49-000-801. REINSTALLED NEW SEAT TRACK P/N: SH670-32159-1 IAW CRJ 700 AMM 53-00-49-400-801-A03
- [SDR REXA2025022600227](https://openairdocs.org/sdr/REXA2025022600227.md): Stringer · corroded · Jan 22, 2025 · N669CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STGR 26R IS CORRODED BETWEEN F.S. 310 TO F.S. 333. INSTALLED NEW SERVICEABLE STGR 26R (P/N: SH670-31634-2S) BETWEEN FS 280 - FS 333 IAW CRJ 700 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01.
- [SDR REXA2025031000291](https://openairdocs.org/sdr/REXA2025031000291.md): Stringer · corroded · Jan 20, 2025 · N669CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > FS364-379 STGR 20R HAS CORROSION. EVALUATED STRINGER AT STR 20R BETWEEN FS364 TO FS379 AND FOUND TO BE OUT OF LIMITS DUE TO HAS A 100% OF LOSS MATERIAL, AND NO DAMAGE ALLOWED ON THIS AREA IAW CRJ-700 SRM 53-21-03-101-006-A01, FIG. 53-21-03-991-864 (SHEET 1). R
- [SDR REXA2025031000290](https://openairdocs.org/sdr/REXA2025031000290.md): Stringer · corroded · Jan 20, 2025 · N669CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > STGR 23L IS CORRODED BETWEEN F.S. 349 TO F.S. 364. REMOVED CORROSION FROM STR 23L BETWEEN FS 349 TO FS 364 IAW CRJ700 SRM 51-21-06-001-001-A01. STR 23L BETWEEN FS 349 TO FS 364 FOUND TO BE CRACKED. LOCATED AND DRILLED NEW SECTION STRINGER P/N: SH690-31358-1S A
- [SDR REXA2025031000289](https://openairdocs.org/sdr/REXA2025031000289.md): Stringer · corroded · Jan 20, 2025 · N669CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > "STGR 22L IS CORRODED BETWEEN F.S. TO F.S. 364. EVALUATED AND FOUND TO BE OUT OF LIMITS DUE TO HAS A 100% OF LOSS MATERIAL, IAW CRJ-700 SRM 53-21-03-101-006-A01. CUT AWAY DAMAGE AND MADE CUT EDGES SMOOTH IAW CRJ700 SRM 53-00-03-201-001-A01 STEPS 5A(1) AND 5A(2
- [SDR REXA2025030700285](https://openairdocs.org/sdr/REXA2025030700285.md): Floor Support · corroded · Jan 20, 2025 · N669CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > "THERE IS EVIDENCE OF CORROSION ON THE L/H FLOOR BEAM BETWEEN FS 1000 AND FS 1051 AT LBL27. REMOVED CORROSION FROM PREVIOUS REPAIR FLOOR BEAM AT LBL27 SEGMENT BETWEEN FS 1009.00 AND FS 1037.00. LOST MORE THAN 50% MATERIAL CLOSE TO THE FWD CUT LINE. FLOOR BEAM
- [SDR REXA2025030300243](https://openairdocs.org/sdr/REXA2025030300243.md): Seat Track · corroded · Jan 20, 2025 · N669CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > L/H SIDE SEAT TRACK IS CORRODED BETWEEN F.S. 485 TO F.S. 565. REMOVED LH SIDE SEAT TRACK P/N:SH670-32234-951 BETWEEN FS 485.00 AND FS 565.00 IAW CRJ700 AMM 53-00-49-000-801-A03. FABRICATED L/H SIDE SEAT TRACK OUT OF P/N 20276-288-0-0A TO MAKE P/N:SH670-32234
- [SDR REXA2025022500216](https://openairdocs.org/sdr/REXA2025022500216.md): Floor Support · corroded · Jan 20, 2025 · N669CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > THERE IS EVIDENCE OF CORROSION ON THE FLOOR BEAM BETWEEN FS 1015 AND FS 1051 AT LBL9 REPAIRED LBL 9 FLOOR BEAM BETWEEN FS 977 TO 1069.75+12 IAW CRJ700 SRM 53-00-41-201-001-A01. SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
- [SDR REXA2025030300242](https://openairdocs.org/sdr/REXA2025030300242.md): Floor Support · corroded · Jan 16, 2025 · N669CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > UNDERFLOOR BOARD SUPPORT AT FS280 HAS CORROSION ON AFT SIDE AROUND FASTENER HOLE. REMOVED UNSERVICEABLE SUPPORT ANGLE P/N: CC670-34256-3 IAW CRJ 700 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01. INSTALLED NEW SERVICEABLE SUPPORT ANGLE P/N CC670-34256-3 AT
- [SDR REXA2025020700153](https://openairdocs.org/sdr/REXA2025020700153.md): Intercostal · cracked · Jan 16, 2025 · N669CA · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR AFT DD1 INTERCOSTAL FOUND TO BE CRACKED. REQUIRES REPLACEMENT. PN: 601R31902-318. REMOVED UNSERVICABLE AND INSTALLED A NEW SERVICEABLE PAX DOOR DD1 INTERCOSTAL P/N 601R31902-318 IAW CRJ 700 SRM 51-42-06-001-001-A01.
- [SDR REXA2025020700152](https://openairdocs.org/sdr/REXA2025020700152.md): Former · corroded · Jan 16, 2025 · N669CA · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR AFT FORMER FOUND TO BE CORRODED. REQUIRES REPLACEMENT. PN: 601R318034-5S REMOVED UNSERVICEABLE PAX DOOR AFT FORMER. INSTALLED A SERVICEABLE PAX DOOR AFT FORMER P/N 601R318034-5IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
- [SDR REXA2025020700151](https://openairdocs.org/sdr/REXA2025020700151.md): Intercostal · corroded · Jan 16, 2025 · N669CA · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR AFT DD5 INTERCOSTAL FOUND TO BE CORRODED. REQUIRES REPLACEMENT. PN: 601R31902-317A. REMOVED UNSERVICABLE PAX DOOR INTERCOSTAL AND INSTALLED A SERVICEABLE PAX DOOR INTERCOSTAL P/N 601R31902-317A IAW CRJ 700 SRM 51-42-06-001-001-A01.
- [SDR REXA2025020700150](https://openairdocs.org/sdr/REXA2025020700150.md): Intercostal · corroded · Jan 16, 2025 · N669CA · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR AFT DD2 INTERCOSTAL FOUND TO BE CORRODED REQUIRES REPLACEMENT. PN: 601R318052-1. REMOVED UNSERVICEABLE PAX DOOR AFT INTERCOSTAL DD2 AND INSTALLED A SERVICEABLE PAX DOOR AFT INTERCOSTAL DD2 P/N 601R318052-1 IAW CRJ 700 SRM 51-42-06-001-001-A01.
- [SDR REXA2025012100065](https://openairdocs.org/sdr/REXA2025012100065.md): Former · corroded · Jan 16, 2025 · N669CA · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR F.S. 320.163 BETWEEN DD7A FWD AND DD7 FWD FOUND TO BE CORRODED. REQUIRES REPLACEMENT. PN:601R318038-3. (INSIDE OF PAX DOOR) REMOVED CORRODED FRAME 320.163. PAX DOOR FS 320.163 HAS BEEN LOCATED AND DRILLED IAW CRJ700 SRM 51-40-11-001-001-A01. INSTALLED

Next page: https://openairdocs.org/aircraft/N669CA/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 = 'N669CA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N669CA/reports

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