# Service difficulty reports: N625CA

A list on [N625CA](https://openairdocs.org/aircraft/N625CA.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 · 160 reports

- [SDR REXA2026020300028](https://openairdocs.org/sdr/REXA2026020300028.md): Lamp · inoperative · Feb 3, 2026 · N625CA · Cndair CL6002C10 · Emergency Lighting
  > RIGHT AFT EXTERIOR EMERGENCY LIGHT NOT TURNING ON. REPLACED THE LAMP IAW AMM 33-51-15, OPS CHECKED GOOD.
- [SDR REXA2025102000956](https://openairdocs.org/sdr/REXA2025102000956.md): Lamp · inoperative · Oct 18, 2025 · N625CA · Cndair CL6002C10 · Emergency Lighting
  > ROW 15 CEILING EMERGENCY LIGHT INOP. REMOVED & REPLACED ROW 15 CEILING EMERGENCY FLOOD-LIGHT BULB IAW AMM 33-51-09, OPS TEST GOOD.
- [SDR REXA2025022500215](https://openairdocs.org/sdr/REXA2025022500215.md): Channel · cracked · Feb 22, 2025 · N625CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > DURING CONFORMITY NOTED AFT CARGO DOOR, AFT CHANNEL SUPPORT DOOR TRACK CRACKED. (FWD OF THE TWO AFT CHANNELS) REMOVED AND REPLACED AFT CARGO DOOR, AFT CHANNEL SUPPORT (FWD OF THE TWO AFT CHANNELS) IAW CRJ 700 SRM 51-42-06, 51-42-21, 51-77-00. P/N ON/OFF MM67
- [SDR SWIA202410040002](https://openairdocs.org/sdr/SWIA202410040002.md): Warning Message · false activation · Oct 2, 2024 · N625CA · Cndair CL6002C10 · Central Warning
  > L BLEED DUCT WARNING MESSAGE AT FL200. COMPLIED WITH QRH. LANDED NORMALLY. (FLIGHT 4291 - FILED CLOSED)L BLEED DUCT WARNING NO LONGER POPULATED. PLEASE SEE AMLS 1443149, 1443151, AND 1443145 FOR CA.
- [SDR SWIA2024100300002](https://openairdocs.org/sdr/SWIA2024100300002.md): Warning Message · illuminated · Oct 2, 2024 · N625CA · Cndair CL6002C10 · Central Warning
  > L BLEED DUCT WARNING MESSAGE AT FL200. COMPLIED WITH QRH. LANDED NORMALLY. (FLIGHT 4291 - FILED OPEN)
- [SDR SWIA20240920](https://openairdocs.org/sdr/SWIA20240920.md): Skin · damaged · Sep 20, 2024 · N625CA · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > COMPLY WITH REO 670-53-61-2356 " REPAIR TO FUSELAGE SKIN BETWEEN FS1144.00 - FS1162.00 & STR6L - STR9L (FILED CLOSED) COMPLIED WITH REO 670-53-61-2356 REV -- DATED 2024-09-25 " REPAIR TO FUSELAGE SKIN BETWEEN FS1144.00 - FS1162.00 & STR6L - STR9L" AND TA
- [SDR SWIA20241030906](https://openairdocs.org/sdr/SWIA20241030906.md): Stringer · chafed · Sep 6, 2024 · N625CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STGR 7R FOUND TO HAVE CHAFING DAMAGE BEWTEEN FS 1144 AND FS1162 (FILED CLOSED) THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWIA2024090900801](https://openairdocs.org/sdr/SWIA2024090900801.md): Stringer · chafed · Sep 6, 2024 · N625CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STGR 7R FOUND TO HAVE CHAFING DAMAGE BEWTEEN FS 1144 AND FS1162 (FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWIA2024070806](https://openairdocs.org/sdr/SWIA2024070806.md): Windshield · cracked · Jul 6, 2024 · N625CA · Cndair CL6002C10 · Flight Compartment Windows
  > CA€™S WINDSHIELD HAD SMALL FIRE BRIELFY ON OUTSIDE WITH STRONG BURNING SMELL. SMALL CRACK OBSERVED. (FLIGHT 4238 - FILED CLOSED) PLEASE REFERENCE AML 1385365 PLEASE REFERENCE AML 1385367REMOVED AND REPLACED PILOTS MAIN WINDSHIELD IN REFERENCE TO AMM 56-
- [SDR SWIA20240110008](https://openairdocs.org/sdr/SWIA20240110008.md): Unknown · cracked · Jan 8, 2024 · N625CA · Cndair CL6002C10 · Flight Compartment Windows
  > L WINDSHIELD OUTER PLY CRACKED DURING DESCENT. OUTER PLY IS SPIDER WEBBED. INNER PLY APPEARS FINE. (FLIGHT 4252 FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 27657409 WITH THE FOLLOWING CORRECTIVE ACTION: "REMOVED AND REPLACED THE LH WINDSHIELD IN
- [SDR SWIA202401090008](https://openairdocs.org/sdr/SWIA202401090008.md): Unknown · cracked · Jan 8, 2024 · N625CA · Cndair CL6002C10 · Flight Compartment Windows
  > L WINDSHIELD OUTER PLY CRACKED DURING DESCENT. OUTER PLY IS SPIDER WEBBED. INNER PLY APPEARS FINE. (FLIGHT 4252 FILED OPEN)
- [SDR SWIA202310300021](https://openairdocs.org/sdr/SWIA202310300021.md): Window · warning message · Oct 21, 2023 · N625CA · Cndair CL6002C10 · Windshield/Door Rain/Ice Removal
  > D: L WINDOW HEAT MSG ON DESCENT. RAN QRH AND MESSAGE CLEARED.C: MEL 30-41-2CAT A DUE 10/22/23**REPEAT**L WINDOW HEAT MSG ON DESCENT. RAN QRH AND MESSAGE CLEARED. (FILED CLOSED) PLEASE REFERENCE AML 1233110 REMOVED AND REPLACED LEFT SIDE WINDOW IN REF TO
- [SDR SWIA202157096](https://openairdocs.org/sdr/SWIA202157096.md): Fairing · corroded · Mar 7, 2021 · N625CA · Cndair CL6002C10 · Aerodynamic Fairings
  > DURING INSTALLATION OF WING TO BODY PANELS 195DL AND 196DR FOUND CORROSION ON CENTER SPLICE ANGLE ON WING TO BODY STRUCTURE AT FS953.00 (C-CHECK) RO 3/25/2021 REMOVED AND REPLACED SPLICE AT FS953 WING TO BODY STRUCTURE IAW CRJ700 SRM 51-42-06-001-001-A01
- [SDR SWIA202157068](https://openairdocs.org/sdr/SWIA202157068.md): Intercostal · corroded · Feb 19, 2021 · N625CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT STGR 26L BETWEEN FS349.00 AND FS364.00 HAS CORROSION (C-CHECK) RO 3/25/2021 EVAL CORROSION IS WITHIN 2D RADIUS OF FASTENERS MAKING IT OUT OF LIMITS. REMOVED AND INSTALLED NEW INTERCOSTAL ON STRINGER 26L BETWEEN F.S. 349.00 AND F.S. 365.00
- [SDR SWIA202157067](https://openairdocs.org/sdr/SWIA202157067.md): Frame · corroded · Feb 19, 2021 · N625CA · Cndair CL6002C10 · Fuselage Main, Frame
  > CORROSION FOUND ON FRAME AT FS349.00 BETWEEN STGR 25L TO 25R (C-CHECK) RO 3/25/2021 CORROSIONS IS ON MORE THEN ONE ELEMENT OF THE FRAME WHICH MAKES IT OUT OF ALLOWABLE LIMITS IAW CRJ700 SRM 53-21-06-101-006-A01 /. REMOVED AND INSTALLED NEW FRAME AT F.S.
- [SDR SWIA202157071](https://openairdocs.org/sdr/SWIA202157071.md): Drag Angle · cracked · Feb 17, 2021 · N625CA · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR AFT DRAG ANGLE CRACKED (MARKED ON AIRCRAFT) (C-CHECK) RO 3/25/2021 REMOVED AND REPLACED PREVIOUS AFT DRAG ANGLE REPAIR WITH REPLACEMENT SPLICE ANGLE REF. CRJ700 SRM 52-11-04-201-002-A01 TYPE I FIGURE 52-11-04-991-814.
- [SDR SWIA202157066](https://openairdocs.org/sdr/SWIA202157066.md): Doubler · chafed · Feb 14, 2021 · N625CA · Cndair CL6002C10 · Engine Thrust Reverser
  > RH UPPER TRANS COWL LATCH DOUBLER CHAFED FWD OF LATCH (C-CHECK) RO 3/25/2021 REMOVED AND REPLACED RH UPPER TRANS COWL LATCH DOUBLER FWD OF LATCH. REF: REO 670-54-21-1207, REV A, DATE 2015-08-27. / COMPLIED WITH 51-900-1002-SKY
- [SDR SWIA202157095](https://openairdocs.org/sdr/SWIA202157095.md): Stringer · corroded · Feb 12, 2021 · N625CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STR 21R IS CORRODED BETWEEN FS333 AND FS319 (C-CHECK) RO 3/25/2021 REPAIRED CORROSION DAMAGE ON STR21R BETWEEN FS319.00 AND FS333.00 REF. MHIRJ REO 670-53-21-1957 REV €“ DATED 2021-02-18. ALL STEPS 1-5 OF MHIRJ REO 670-53-21-1957 REV €“ DATED 2021-02-18
- [SDR SWIA202157065](https://openairdocs.org/sdr/SWIA202157065.md): Stringer Splice · corroded · Feb 12, 2021 · N625CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STR 26L SPLICE AT FS333 IS CORRODED (C-CHECK) RO 3/25/2021 REMOVED AND REPLACED STRINGER SPLICE AT FS333, STGR 26L. REF. CRJ700 SRM 51-42-06-001-001-A01 AND DWG# SH670-32420 REV. E SHEET 1 AND 3 / COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY (CL600-2C1
- [SDR SWIA202157064](https://openairdocs.org/sdr/SWIA202157064.md): Stringer · corroded · Feb 12, 2021 · N625CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STR 26L IS CORRODED BETWEEN FS333 AND FS349 (C-CHECK) RO 3/25/2021 REMOVED CORROSION FROM STGR 26L BETWEEN FS333 AND FS349. RMAINING THICKNESS IS OUT OF LIMITS. REMOVED AND REPLACED STGR 26L REF CRJ700 SRM 51-42-06-001-001-A01. LEAK CHECK GOOD AT THIS
- [SDR SWIA202157063](https://openairdocs.org/sdr/SWIA202157063.md): Floorbeam · corroded · Feb 12, 2021 · N625CA · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > A-BAY FS280 FLOOR SUPPORT ANGLE IS CORRODED (C-CHECK) RO 3/25/2021 REMOVED AND INSTALLED NEW FLOOR SUPPORT ANGLE P/N#CC670-34256-1 ASSY. IN A-BAY FS280.00 REF. CRJ-700 SRM 51-42-06-001-001-A01, CRJ-700 SRM 51-42-21-001-001-A01 AND DWG # CC670-34010 REV K
- [SDR SWIA202157062](https://openairdocs.org/sdr/SWIA202157062.md): Stringer · corroded · Feb 12, 2021 · N625CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STR 19R IS CORRODED BETWEEN FS319-FS333 (C-CHECK) RO 3/25/2021 CORROSION PRESENT ON MULTIPLE ELEMENTS IN SAME CROSS SECTION, DAMAGE OUT OF LIMITS REF. CRJ-700 SRM, 53-00-00-101-001-A01. INSTALLED NEW STRINGER 19R FROM FS319 TO FS349 REF. CRJ-700 SRM, 51-4
- [SDR SWIA202157061](https://openairdocs.org/sdr/SWIA202157061.md): Stringer · corroded · Feb 12, 2021 · N625CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STR 21R IS CORRODED FORM FS333-FS379 (C-CHECK) RO 3/25/2021 REMOVED AND REPLACED STRINGER 21R FROM FS333 TO FS379. REF. CRJ700 SRM 51-42-06-001-001-A01 AND DWG # SH670-31350 REV. A SHEET 3 / COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY (CL600-2C10) STR
- [SDR SWIA202157060](https://openairdocs.org/sdr/SWIA202157060.md): Skin · chafed · Feb 9, 2021 · N625CA · Cndair CL6002C10 · Nacelle/Pylon, Plate/Skin
  > LH LOWER FAN COWL HAS 2 CHAFES/GOUGES ON AFT SIDE TRAILING EDGE AREA APPROX AT 3 O'CLOCK AND 9 O'CLOCK (MARKED) (C-CHECK) RO 3/25/2021 BLENDED OUT 2 EACH CHAFFES ON LH LOWER FAN COWL AND FOUND ACCEPTABLE TO ENGINEERING REF REO 670-78-30-999 REV -- DATED 2
- [SDR SWIA202157059](https://openairdocs.org/sdr/SWIA202157059.md): Frame · corroded · Feb 9, 2021 · N625CA · Cndair CL6002C10 · Fuselage Main, Frame
  > FS250.00 FRAME IS CORRODED ON BOTH SIDES OF STGR27. (C-CHECK) RO 3/25/2021 CUT AWAY DAMAGED SECTION. FABRICATED AND INSTALLED REPAIR PARTS. COMPLIED WITH ALL STEPS OF REO 670-53-11-1648 REV-- DATED 2021-02-19. PRESSURE CHECK GOOD / SEE CONTINUE CARD FO
- [SDR SWIA202157104](https://openairdocs.org/sdr/SWIA202157104.md): Link · chafed · Feb 2, 2021 · N625CA · Cndair CL6002C10 · Aileron Control System
  > RH AILERON I/B PCU OUTPUT LINK CHAFED. (C-CHECK) RO 3/25/2021 NEW RH AILERON I/B PCU OUTPUT LINK INSTALLED AND OPS TESTED IAW CRJ700 AMM 27-11-00-710-801-A01. SEE CONTINUATION CARD FOR DETAILS.COMPLIED WITH 27-900-1008-SKY.
- [SDR SWIA202157058](https://openairdocs.org/sdr/SWIA202157058.md): Latch · chafed · Feb 2, 2021 · N625CA · Cndair CL6002C10 · Engine Thrust Reverser
  > L/H LOWER TRANSCOWL HAS CHAFE JUST FWD OF FWD LATCH. (C-CHECK) RO 3/25/2021 REPAIRED L/H LOWER TRASCOWL OUTER SKIN JUST FWD OF FWD LATCH. REF REO 670-54-21-1428 REV -- DATED 2021-03-22, REO 670-54-21-1207 REV A DATED 2015-08-27, CRJ-700 SRM 51-23-00-001-0
- [SDR SWIA202157057](https://openairdocs.org/sdr/SWIA202157057.md): Access Door · damaged · Feb 2, 2021 · N625CA · Cndair CL6002C10 · Engine Thrust Reverser
  > L/H UPPER TRANSCOWL ACCESS DOOR LANDING ALIGNMENT HOLE IS ELONGATED. (C-CHECK) RO 3/25/2021 REPLACED L/H UPPER TRANSCOWL COAMING AND DOUBLERS. REF REO 670-54-21-1207 REV A DATED 2015-08-27 REF CRJ 700 SRM 51-42-13-001-001-A01. REPLACED BEARING PADS AND S
- [SDR SWIA202157056](https://openairdocs.org/sdr/SWIA202157056.md): Intercostal · corroded · Jan 31, 2021 · N625CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > * FWD ACFT MOUNT, FWD OF FS280, RH INTERCOSTAL IS CORRODED. (C-CHECK) RO 3/25/2021 PRIOR TO BLENDING INTERCOSTAL, FOUND THAT PART HAS HEAVY CORROSION AND IS MORE THAN 30% OF THE OVERALL LENGTH OF A MEMBER AND THE PART HAS DAMAGE IN MORE THAN ONE ELEMENT
- [SDR SWIA202157055](https://openairdocs.org/sdr/SWIA202157055.md): Intercostal · corroded · Jan 31, 2021 · N625CA · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > * FWD ACFT MOUNT, FWD OF FS280, LH INTERCOSTAL IS CORRODED. (C-CHECK) RO 3/25/2021 PRIOR TO BLENDING INTERCOSTAL FOUND THAT PART HAS HEAVY CORROSION AND IS MORE THAN 30% OF THE OVERALL LENGTH OF A MEMBER AND PART HAS DAMAGE IN MORE THAN ONE ELEMENT AT A
- [SDR SWIA202157094](https://openairdocs.org/sdr/SWIA202157094.md): Seat Track · corroded · Jan 26, 2021 · N625CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR SEAT RAIL AT APPROXIMATELY LBL27 FS985.00-FS1000.00 CORRODED. (C-CHECK) RO 3/25/2021 FOUND FLOOR TRACK AT LBL 27 FS 985 TO FS 1000 100% EXFOILIATED AND INSTALLED NEW TRACK REF CRJ 700 AMM 53-00-49-400-802-A06 USING TW 4978 CAL DUE 30 JUN 21.
- [SDR SWIA202157093](https://openairdocs.org/sdr/SWIA202157093.md): Stop Fitting · corroded · Jan 26, 2021 · N625CA · Cndair CL6002C10 · Passenger/Crew Doors
  > * PAX DOOR LOWER INTERNAL STOP FITTING IS CORRODED. (C-CHECK) RO 3/25/2021 REMOVED CORROSION ON PAX DOOR LOWER STOP FITTING REF. CRJ-700 SRM, 51-21-06-001-001-A01. REPLACED BRACKET (LOWER INTERNAL STOP FITTING) REF. CRJ-700 SRM, 51-42-10-001-001-A01. REST
- [SDR SWIA202157054](https://openairdocs.org/sdr/SWIA202157054.md): Frame · corroded · Jan 26, 2021 · N625CA · Cndair CL6002C10 · Fuselage Main, Frame
  > CORROSION FOUND ON FRAME FS310 BETWEEN STGR 26L AND 26R. (C-CHECK) RO 3/25/2021 REMOVED AND REPLACED FRAME SECTION AT FS310 BETWEEN STGR 23L AND 25R. REF. CRJ700 SRM 53-00-06-201-006-A01, SRM 51-42-21-001-001-A01, SRM 51-42-06-001-001-A01, DWG# SH670-3163
- [SDR SWIA202157053](https://openairdocs.org/sdr/SWIA202157053.md): Stringer · corroded · Jan 26, 2021 · N625CA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON STRINGER 27 BETWEEN FS280 AND FS295. (C-CHECK) RO 3/25/2021 REMOVED AND REPLACED STRINGER 27 BETWEEN FS280 AND FS299. REF. CRJ700 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 AND DWG# SH670-31630 REV. K SHEET 1. / COMPLIED WITH SK
- [SDR SWIA202157052](https://openairdocs.org/sdr/SWIA202157052.md): Hinge · grooved · Jan 25, 2021 · N625CA · Cndair CL6002C10 · Fuselage, Door Hinge
  > * PASSENGER DOOR HINGE HALF ( DOOR SIDE) HAS MULTIPLE HINGE LUGS WITH SHALLOW GROOVES CHAFED INTO BASE OF LUGS FROM CONTACT WITH LUG LANDS OF FUSELAGE SIDE HINGE HALF. (C-CHECK) RO 3/25/2021 COMPLIED WITH REO TYPE I DISPOSITION, REMOVED CHAFFING ON HINGE
- [SDR SWIA202157051](https://openairdocs.org/sdr/SWIA202157051.md): Hinge · gouged · Jan 25, 2021 · N625CA · Cndair CL6002C10 · Fuselage, Door Hinge
  > * PASSENGER DOOR HINGE HALF ( FUSELAGE SIDE) HAS AFT HINGE LUG LAND GOUGED FROM CONTACT WITH ROLL PIN. (C-CHECK) RO 3/25/2021 COMPLIED WITH REO TYPE IV DISPOSITION, REMOVED GOUGE ON HINGE LUG LAND REF. BOMBARDIER REO 670-53-21-582 REV-F DATED: 2017-08-02
- [SDR SWIA202157050](https://openairdocs.org/sdr/SWIA202157050.md): Rivet · missing · Jan 25, 2021 · N625CA · Cndair CL6002C10 · Engine Thrust Reverser
  > * RH ENGINE UPPER TRANSCOWL Z-MEMBER LOOSE AND 1 RIVET HEAD MISSING (C-CHECK) RO 3/25/2021 REMOVED AND INSTALLED Z- MEMBER AT RH ENGINE UPPER TRANSCOWL. REF: REO 670-54-21-1427, REV -- DATE 2021-02-11. TASK CARD 51-900-1002-SKY COMPLETED.
- [SDR SWIA202157049](https://openairdocs.org/sdr/SWIA202157049.md): Skin · chafed · Jan 25, 2021 · N625CA · Cndair CL6002C10 · Nacelle/Pylon, Plate/Skin
  > * LH ENGINE LOWER FAN COWL CHAFED UNDER THRUST REVERSER FLEX LINE (C-CHECK) RO 3/25/2021 REMOVED STIFFENER AND REPLACED WITH NEW STIFFENER REF. CRJ-700 SRM 51-42-06-001-001-A01, AND DWG#CN622-0201 REV. L. / COMPLIED WITH 51-900-1002-SKY
- [SDR SWIA202157048](https://openairdocs.org/sdr/SWIA202157048.md): Slider · chafed · Jan 25, 2021 · N625CA · Cndair CL6002C10 · Engine Thrust Reverser
  > * LH ENGINE UPPER TRANSCOWL, INBD SLIDER CHAFED (C-CHECK) RO 3/25/2021 REMOVED CHAFE. WITHIN LIMITS. COMPLIED WITH REO 670-54-21-1423 REV-- DATED: 2021-02-05. COMPLIED WITH TASK CARD 51-900-1002-SKY.
- [SDR SWIA202157092](https://openairdocs.org/sdr/SWIA202157092.md): Seat Track · corroded · Jan 24, 2021 · N625CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > * FLOOR SEAT RAIL AT APPROXIMATELY LBL9 FS987 - FS1005 CORRODED (C-CHECK) RO 3/25/2021 REMOVED AND REPLACED SEAT RAIL AT APPROX LBL9 FS987-FS1005 REF. CRJ-700 AMM, 53-00-49-000-802-A06 AND CRJ-700 AMM, 53-00-49-400-802-A06
- [SDR SWIA202157091](https://openairdocs.org/sdr/SWIA202157091.md): Seat Track · corroded · Jan 24, 2021 · N625CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > * FLOOR SEAT RAIL AT APPROXIMATELY RBL27 FS977 €“ FS1005 CORRODED (C-CHECK) RO 3/25/2021 REMOVED AND REPLACED FLOOR SEAT RAIL FS977-FS1005 RBL27 REF. CRJ 700 AMM 53-00-49-000-802-A06 AND 53-00-49-400-802-A06.
- [SDR SWIA202157090](https://openairdocs.org/sdr/SWIA202157090.md): Seat Track · corroded · Jan 24, 2021 · N625CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > * FLOOR SEAT RAIL AT APPROXIMATELY RBL9 FS977 €“ FS1005 CORRODED (C-CHECK) RO 3/25/2021 REMOVED AND REPLACED FLOOR SEAT RAIL FS977-FS1005 RBL9 REF. CRJ 700 AMM 53-00-49-000-802-A06 AND 53-00-49-400-802-A06.
- [SDR SWIA202157089](https://openairdocs.org/sdr/SWIA202157089.md): Seat Track · corroded · Jan 24, 2021 · N625CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > * FLOOR SEAT RAIL AT APPROXIMATELY LBL27 FS923 €“ FS977 CORRODED (C-CHECK) RO 3/25/2021 REMOVED AND REPLACED FLOOR SEAT RAIL AT APPROX LBL27 FS923-FS977 REF. CRJ-700 AMM, 53-00-49-000-801-A17 AND CRJ-700 AMM, 53-00-49-400-801-A17
- [SDR SWIA202157088](https://openairdocs.org/sdr/SWIA202157088.md): Seat Track · corroded · Jan 24, 2021 · N625CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > * FLOOR SEAT RAIL AT APPROXIMATELY RBL9 FS839 €“ FS977 CORRODED (C-CHECK) RO 3/25/2021 REMOVED AND REPLACED FLOOR SEAT RAIL AT APPROX RBL9 FS839-FS977 REF. CRJ-700 SRM, 53-00-49-000-801-A03 AND CRJ-700 SRM, 53-00-49-400-801-A03.
- [SDR SWIA202157087](https://openairdocs.org/sdr/SWIA202157087.md): Seat Track · corroded · Jan 24, 2021 · N625CA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > * FLOOR SEAT RAIL AT APPROXIMATELY LBL9 FS839 €“ FS987 CORRODED (C-CHECK) RO 3/25/2021 EVALUATED AND FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED FLOOR SEAT RAIL AT APPROXIMATELY LBL9 FS839 - FS987. REF:CRJ 700, AMM 53-00-49-400-801-A17
- [SDR SWIA202157070](https://openairdocs.org/sdr/SWIA202157070.md): Support · cracked · Jan 24, 2021 · N625CA · Cndair CL6002C10 · Aerodynamic Fairings
  > * AFT WING-TO-BODY FAIRING SUPPORT DIAPHRAGM CRACKED AT APPROXIMATELY FS909 STGR24L (C-CHECK) RO 3/25/2021 COMPLIED WITH WITH ALL STEPS FROM REF 670-53-82-478 REV A DATED 2014-11-12 FOR REPAIR TO DIAPHRAGM AFT WING TO BODY FAIRING SUPPORT APX FS909 STGR
- [SDR SWIA202157047](https://openairdocs.org/sdr/SWIA202157047.md): Floorbeam · corroded · Jan 24, 2021 · N625CA · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > * FLOOR BEAM AT FS985 CORRODED BETWEEN LBL27 €“ LBL36 (C-CHECK) RO 3/25/2021 REPAIRED FLOOR BEAM AT F/S 985.00 BETWEEN LBL 27 AND LBL 36 ALL STEPS COMPLIED WITH IAW REO 670-53-61-1822 REV. -- DATED 2021-03-06 AND COMPLIED WITH 51-900-1002-SKY CARD
- [SDR SWIA202157046](https://openairdocs.org/sdr/SWIA202157046.md): Frame · corroded · Jan 24, 2021 · N625CA · Cndair CL6002C10 · Fuselage Main, Frame
  > * FRAME AT APPROXIMATELY FS863 STGR26L €“ STGR26R CORRODED (C-CHECK) RO 3/25/2021 PERFORMED FRAME REPAIR ON FS863.00 FROM STRINGER 26-26R. REF. CRJ 700 SRM 51-42-06-001-001-A01 AND REO 670-53-51-201, REV -- DATED 2021-02-22. / PRESSURE CHECKS GOOD. / CO
- [SDR SWIA202157045](https://openairdocs.org/sdr/SWIA202157045.md): Bulkhead · corroded · Jan 24, 2021 · N625CA · Cndair CL6002C10 · Fuselage Main, Bulkhead
  > * R/H FS 280.00 BULKHEAD HAS CORROSION AT LOWER INB CORNER ( AT FLIGHT COMPARTMENT OPENING, MARKED) (C-CHECK) RO 3/25/2021 REPAIRED R/H FS 280.00 BULKHEADPOST LOWER END AT RBL11 REF. CRJ 700 SRM 53-11-10-201-006-A01. COMPLIED WITH 51-900-1002-SKY
- [SDR SWIA202157044](https://openairdocs.org/sdr/SWIA202157044.md): Bulkhead · corroded · Jan 24, 2021 · N625CA · Cndair CL6002C10 · Fuselage Main, Bulkhead
  > * L/H FS 280.00 BULKHEAD HAS CORROSION AT LOWER INB CORNER ( AT FLIGHT COMPARTMENT OPENING, MARKED) (C-CHECK) RO 3/25/2021 FOUND LH LOWER POST END TO BE OUT OF LIMITS DURING CORROSION REMOVAL REF. CRJ-700 SRM, 51-21-06-001-001-A01. REPAIRED POST LOWER RE

Next page: https://openairdocs.org/aircraft/N625CA/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 = 'N625CA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N625CA/reports

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