# Service difficulty reports: N538CA

A list on [N538CA](https://openairdocs.org/aircraft/N538CA.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 · 219 reports

- [SDR REXA2026060800947](https://openairdocs.org/sdr/REXA2026060800947.md): Thrust Reverser · cracked · Jun 6, 2026 · N538CA · Cndair CL6002D24 · Engine Thrust Reverser
  > LEFT ENGINE TRANSCOWL FOUND NYLON BIFURCATION PANEL CRACKED. LEFT ENGINE TRANSCOWL FOUND NYLON BIFURCATION PANEL WAS REPAIRED PER EA NO: CRJ954-22351 REV. IR
- [SDR REXA2026060800949](https://openairdocs.org/sdr/REXA2026060800949.md): Angle · cracked · May 25, 2026 · N538CA · Cndair CL6002D24 · Vertical Stabilizer Miscellaneous Structure
  > CRACK ON RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD & AFT DRAG ANGLE BTW 61.56% STRG DATUM TO 67.5% REAR SPAR DATUM CRACK ON RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD & AFT DRAG ANGLE BTW 61.56% STRG DATUM TO 67.5% REAR SPAR DATUM WAS REPAIRED P
- [SDR REXA2026060800961](https://openairdocs.org/sdr/REXA2026060800961.md): Fitting · corroded · May 14, 2026 · N538CA · Cndair CL6002D24 · Fuselage, Equipment Attach Fittings
  > CORROSION FLOOR FITTING IN FWD ACCESS 305 (1EA) ON GALLEY 3. SUMMARY OF NRC 00190: NEW FLOOR FITTING P/N: CDSP2019-7C-700 IN FWD ACCESS 305 (1EA) ON GALLEY 3. WAS REPLACED PER SAFRAN CMM 25-33-13 REV NO 12 DATED OCT 27/25
- [SDR REXA2026060800960](https://openairdocs.org/sdr/REXA2026060800960.md): Fitting · corroded · May 14, 2026 · N538CA · Cndair CL6002D24 · Fuselage, Equipment Attach Fittings
  > CORROSION FLOOR FITTING IN FWD ACCESS 107 (1EA) ON GALLEY 1. SUMMARY OF NRC 00188: NEW FLOOR FITTING P/N: CDSP2019-7C-620 IN FWD ACCESS 107 (1EA) ON GALLEY 1. WAS REPLACED PER SAFRAN CMM 25-33-67 REV NO 10 DATED JUN 20/22
- [SDR REXA2026060800959](https://openairdocs.org/sdr/REXA2026060800959.md): Fitting · corroded · May 14, 2026 · N538CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION FLOOR FITTING IN FWD AND AFT ACCESS 306 (2EAS) ON GALLEY 3. SUMMARY OF NRC 00191: NEW FLOOR FITTING P/N: CDSP2019-7C-650 IN FWD AND AFT ACCESS 306 (2EAS) ON GALLEY 3. WERE INSTALLED PER CMM 25-33-13 REV NO 12. DATED OCT 27/25
- [SDR REXA2026060800954](https://openairdocs.org/sdr/REXA2026060800954.md): Fitting · corroded · May 14, 2026 · N538CA · Cndair CL6002D24 · Fuselage, Equipment Attach Fittings
  > CORROSION FLOOR FITTING IN THE FWD LAV FRONT SIDE LH(1EA). SUMMARY OF NRC 00192:FLOOR FITTING IN THE FWD LAV FRONT SIDE LH(1EA) WAS FABRICATED PER EA NO. CRJ953-22315 ISSUE DATE: 5/24/2026 REV. A AND INSTALL PER SAFRAN CMM 25-40-76 REV. NO.17
- [SDR REXA2026060800953](https://openairdocs.org/sdr/REXA2026060800953.md): Fitting · corroded · May 14, 2026 · N538CA · Cndair CL6002D24 · Fuselage, Equipment Attach Fittings
  > CORROSION FLOOR FITTING IN AFT AND FWD ACCESS 205 (2EAS) ON GALLEY 2. SUMMARY OF NRC 00189: FLOOR FITTING IN FWD ACCESS 205 (1EA) ON GALLEY 2. WAS REPLACED PER SAFRAN CMM 25-32-84 REV. 9 JUN 06/24 AND FLOOR FITTING IN AFT ACCESS 205 (1EA) ON GALLEY 2 WAS FABRI
- [SDR REXA2026060900955](https://openairdocs.org/sdr/REXA2026060900955.md): Tube · corroded · May 9, 2026 · N538CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON TUBE BTW FS 310.00 AND FS333.00 AT PASSENGER DOOR SURROUND STRUCTURE CORROSION ON TUBE BTW FS 310.00 AND FS333.00 AT PASSENGER DOOR SURROUND STRUCTURE WAS REMOVED AND EVALUATED OUT LIMITS PER CRJ-900 SRM 53-00-00-101-001, SRM 51-21-00-001-001-A0
- [SDR REXA2026060800957](https://openairdocs.org/sdr/REXA2026060800957.md): Fitting · corroded · May 9, 2026 · N538CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON CLOSING FITTING ON FS342 (PASSENGER DOOR LOWER SILL AREA) AT PAX CABIN FLOOR STRUCTURE DUE TO EXCESSIVE DAMAGE ON FITTING, CLOSING ON FS342 (PASSENGER DOOR LOWER SILL AREA) AT PAX CABIN FLOOR STRUCTURE WAS REPLACED PER SRM 51-42-06-001-001-A01
- [SDR REXA2026060800952](https://openairdocs.org/sdr/REXA2026060800952.md): Seat Track · corroded · May 9, 2026 · N538CA · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK ON RBL9 FROM FS349 TO FS409 AT PAX CABIN FLOOR STRUCTURE DUE TO EXCESSIVE DAMAGE ON SEAT TRACK ON RBL9 FROM FS349 TO FS409 AT PAX CABIN FLOOR STRUCTURE WAS REPLACED PER CRJ900 SRM 51-10-06-001-001-A01 AND AMM 53-00-49
- [SDR REXA2026060800950](https://openairdocs.org/sdr/REXA2026060800950.md): Angle · cracked · May 9, 2026 · N538CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACKED SUPPORT ANGLE OF SHEAR BOX BTW FS 280 AND RBL 12.0 MAIN AVIONICS COMPARTMENT. SUPPORT ANGLE OF SHEAR BOX BTW FS 280 AND RBL 12.0 MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ900 SRM 51-42-21-001-001-A01
- [SDR REXA2026060800948](https://openairdocs.org/sdr/REXA2026060800948.md): Angle · cracked · May 9, 2026 · N538CA · Cndair CL6002D24 · Vertical Stabilizer Miscellaneous Structure
  > CRACK ON LH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD & AFT DRAG ANGLE BTW 61.56% STRG DATUM TO 67.5% REAR SPAR DATUM CRACK ON LH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD & AFT DRAG ANGLE BTW 61.56% STRG DATUM TO 67.5% REAR SPAR DATUM WERE REPAIRED
- [SDR REXA2026060800940](https://openairdocs.org/sdr/REXA2026060800940.md): Angle · corroded · May 9, 2026 · N538CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON MID CAP ANGLE FROM FS310 TO FS349 (PASSENGER DOOR LOWER SILL AREA) AT PAX CABIN FLOOR STRUCTURE MID CAP ANGLE FROM FS310 TO FS349 (PASSENGER DOOR LOWER SILL AREA) AT PAX CABIN FLOOR STRUCTURE WAS REPLACED PER CRJ-900 SRM 51-41-02-001-001-A01
- [SDR REXA2026060800939](https://openairdocs.org/sdr/REXA2026060800939.md): Door Frame · cracked · May 9, 2026 · N538CA · Cndair CL6002D24 · Emergency Exits
  > CRACK ON UPPER FRAME AT AFT RH/LH & FWD RH/LH OVERWING EMERGENCY EXIT DOORS CRACK ON UPPER FRAME AT AFT RH/LH & FWD RH/LH OVERWING EMERGENCY EXIT DOORS WERE REPAIRED PER REO 670-52-21-103 REV. - -
- [SDR REXA2026060800956](https://openairdocs.org/sdr/REXA2026060800956.md): Bracket · cracked · May 8, 2026 · N538CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACKS ON SUPPORT BASE MAIN BATTERY DIRECT BUS (JB6) AT FWD EQUIPMENT COMPARTMENT. SUPPORT BASE MAIN BATTERY DIRECT BUS (JB6) AT FWD EQUIPMENT COMPARTMENT WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01
- [SDR REXA2026050400448](https://openairdocs.org/sdr/REXA2026050400448.md): Lamp · inoperative · Apr 29, 2026 · N538CA · Cndair CL6002D24 · Emergency Lighting
  > EMER LIGHT CEILING ROW 17 INOP. REMOVED AND REPLACED LAMP AT EMER LIGHT CEILING ROW 17, OPS TEST GOOD PER AMM 33-51-09.
- [SDR REXA2026050400444](https://openairdocs.org/sdr/REXA2026050400444.md): Bulb · inoperative · Apr 29, 2026 · N538CA · Cndair CL6002D24 · Emergency Lighting
  > TWO LAMPS IN ENTRANCE EMERGENCY FLOOD LAMP INOPERATIVE. R & R TWO ENTRANCE EMERGENCY FLOODLIGHT BULBS P/N OL3071BPE/GPL REF AMM 33-51-05. OPS CHECKED GOOD.
- [SDR REXA2022101800899](https://openairdocs.org/sdr/REXA2022101800899.md): Starter · leaking · Oct 17, 2023 · N538CA · Cndair CL6002D24 · Engine Starter
  > IN CLIMB, L ENG OIL PRESS WARNING FOLLOWED BY L ENG IN-FLIGHT SHUTDOWN PER QRH AND EMERGENCY CHECKLIST. REMOVED L/H STARTER FOR INSPECTION, FOUND PACKING ITEM 15 MISINSTALLED. REPLACED L/H STARTER IAW CRJ 900 AMM 80-11-01. REPLACED OIL FILTER AND INSPECTED IA
- [SDR REXA2022113002611](https://openairdocs.org/sdr/REXA2022113002611.md): Frame · corroded · Nov 26, 2022 · N538CA · Cndair CL6002D24 · Fuselage Main, Frame
  > FRAME, BS 581 FOUND CORRODED, BETWEEN STRINGERS 25L & 25R. REPAIRED THE STRINGER IAW REO 690-53-31-707 REV.
- [SDR REXA2022112302598](https://openairdocs.org/sdr/REXA2022112302598.md): Frame · corroded · Nov 22, 2022 · N538CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FS 501 FRAME CORRODED ON LOWER FLANGE BETWEEN STGR 27 AND STGR 26L. COMPLIED WITH IAW REO 690-53-31–690 REV— DATED 2022-10-28.
- [SDR REXA2022112202597](https://openairdocs.org/sdr/REXA2022112202597.md): Frame · corroded · Nov 22, 2022 · N538CA · Cndair CL6002D24 · Fuselage Main, Frame
  > FOUND AREA OF CORROSION ON FRAME AT FS 533.00 BETWEEN STGR 26L AND 27 " COMPLIED WITH REO 690-53-31-704 REV -- DATE 2022-11-17 "
- [SDR REXA2022112102564](https://openairdocs.org/sdr/REXA2022112102564.md): Stringer · corroded · Nov 16, 2022 · N538CA · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRG23L IS CORRODED BETWEEN FS1031 AND FS1047. REPLACED STRINGER P/N MM670-35151-035 I.A.W. CRJ-900 SRM 53-00-03-201-001-A01.
- [SDR REXA2022113002646](https://openairdocs.org/sdr/REXA2022113002646.md): Stringer · corroded · Nov 15, 2022 · N538CA · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 23R HAS PITTING BETWEEN FS549-581. COMPLIED WITH REO 690-53-31-715 REV-.
- [SDR REXA2022113002645](https://openairdocs.org/sdr/REXA2022113002645.md): Structure · corroded · Nov 8, 2022 · N538CA · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR CLIP ON MID DD6 FOUND TO BE CORRODED. REMOVED THE DOOR CLIP IAW SRM 51-40-11-001-001-A01. LOCATED, AND DRILLED A NEW DOOR CLIP, AND INSTALLED IAW SRM 51-42-06-001-001-A01.
- [SDR REXA2022113002628](https://openairdocs.org/sdr/REXA2022113002628.md): Skin · corroded · Nov 8, 2022 · N538CA · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR INNER SKIN FOUND TO BE CORRODED. REMOVED AND REPLACE PAX DOOR INNER SKIN IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01.
- [SDR REXA2022113002625](https://openairdocs.org/sdr/REXA2022113002625.md): Intercostal · corroded · Nov 8, 2022 · N538CA · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL DD3 AT FWD SIDE FOUND TO BE CORRODED. REMOVED THE INTERCOSTAL IAW SRM 51-42-06-001-001-A01. INSTALLED A NEW INTERCOSTAL IAW SRM 51-42-06-001-001-A01 AND 51-40-11-001-001-A01.
- [SDR REXA2022112302601](https://openairdocs.org/sdr/REXA2022112302601.md): Web · corroded · Nov 8, 2022 · N538CA · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR FWD STAIR WEB IS CORRODED FOUND FWD STAIR WEB TO BE OUT OF ALLOWABLE LIMITS IAW CRJ 900 SRM 52-11-04-101-001-A01. REMOVED AND INSTALLED SUPPORT ANGLES, DRAG ANGLE AND COUNTERBALANCE SUPPORT MOUNT STRUCTURE IAW CRJ 900 SRM 51-42-06-001-001-A01. LOCATE
- [SDR REXA2022112302600](https://openairdocs.org/sdr/REXA2022112302600.md): Drag Angle · damaged · Nov 8, 2022 · N538CA · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR AFT DRAG ANGLE HAS ELONGATED HOLES. FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW CRJ 900 SRM 52-11-04-101-001-A01. LOCATED AND DRILLED NEW SERVICEABLE DRAG ANGLE PN 601R31772-5S IAW CRJ 900 SRM 51-40-11-001-001-A01 REFERENCE JOB 81515751 OP 659 FOR
- [SDR REXA2022120602673](https://openairdocs.org/sdr/REXA2022120602673.md): Floorbeam · corroded · Nov 3, 2022 · N538CA · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > AFT CARGO FLOORBEAM CORRODED AT FS1051.30, LBL 39.50. REPAIRED IAW REO 690-53-61-1146 REV -.
- [SDR REXA2022111502541](https://openairdocs.org/sdr/REXA2022111502541.md): Gusset · corroded · Oct 31, 2022 · N538CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FWD INTERCOSTAL GUSSET AT STGR 20R @ FS 349.00 HAS CORROSION. REPLACED FWD INTERCOSTAL GUSSET IAW SRM 51-23-00-001-001-A01 AND SRM 51-42-21-001-001-A01. "
- [SDR REXA2022111502540](https://openairdocs.org/sdr/REXA2022111502540.md): Stringer · corroded · Oct 31, 2022 · N538CA · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STGR 21R BETWEEN F.S.295 - F.S.310 IS CORRODED. REPLACED THE STRINGER IAW SRM 51-42-06-001-001-A01, AND 51-42-21-001-001-A01. "
- [SDR REXA2022111502539](https://openairdocs.org/sdr/REXA2022111502539.md): Stringer · corroded · Oct 31, 2022 · N538CA · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STGR 22R BETWEEN F.S.280 - F.S.295 IS CORRODED. REPLACED THE STRINGER IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. "
- [SDR REXA2022113002627](https://openairdocs.org/sdr/REXA2022113002627.md): Structure · corroded · Oct 28, 2022 · N538CA · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR CLIP AT FWD FRAME STATION 323 AND THE HINGE FOUND TO BE CORRODED. REMOVED THE CLIP IAW SRM 51-42-06-001-001-A01. LOCATED, DRILLED, AND INSTALLED A NEW DOOR CLIP IAW SRM 51-42-06-001-001-A01 AND 51-40-11-001-001-A01.
- [SDR REXA2022113002626](https://openairdocs.org/sdr/REXA2022113002626.md): Cleat · corroded · Oct 28, 2022 · N538CA · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR CLEAT ON FWD INTERCOSTAL DD4 AND FRAME STATION 313.56 FOUND TO BE CORRODED. REMOVED THE DOOR CLEAT IAW SRM 51-42-06-001-001-A01. LOCATED, DRILLED, AND INSTALLED A NEW DOOR CLEAT IAW SRM 51-42-06-001-001-A01 AND 51-40-11-001-001-A01.
- [SDR REXA2022113002624](https://openairdocs.org/sdr/REXA2022113002624.md): Intercostal · corroded · Oct 26, 2022 · N538CA · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL DD2, FOUND TO BE CORRODED. LOCATED, DRILLED, AND INSTALLED A NEW INTERCOSTAL IAW SRM 51-40-11-001-001-A01, AND 51-42-06-001-001-A01.
- [SDR REXA2022113002623](https://openairdocs.org/sdr/REXA2022113002623.md): Intercostal · corroded · Oct 26, 2022 · N538CA · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL DD2, FOUND TO BE CORRODED. LOCATED, & DRILLED A NEW INTERCOSTAL IAW SRM 51-40-11-001-001-A01, INSTALLED THE NEW INTERCOSTAL IAW SRM 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.
- [SDR REXA2022113002622](https://openairdocs.org/sdr/REXA2022113002622.md): Intercostal · corroded · Oct 26, 2022 · N538CA · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL DD5 AFT, FOUND TO BE CORRODED. LOCATED, & DRILLED A NEW INTERCOSTAL IAW SRM 51-40-11-001-001-A01. INSTALLED THE NEW INTERCOSTAL IAW SRM 51-42-06-001-001-A01.
- [SDR REXA2022113002621](https://openairdocs.org/sdr/REXA2022113002621.md): Intercostal · corroded · Oct 26, 2022 · N538CA · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL DD4 FOUND TO BE CORRODED. LOCATED, AND DRILLED A NEW INTERCOSTAL IAW SRM 51-40-11-001-001-A01, INSTALLED THE NEW INTERCOSTAL IAW SRM 51-42-06-001-001-A01.
- [SDR REXA2022113002620](https://openairdocs.org/sdr/REXA2022113002620.md): Intercostal · corroded · Oct 26, 2022 · N538CA · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL DD7A FOUND TO BE CORRODED. LOCATED, DRILLED, AND INSTALLED A NEW INTERCOSTAL IAW SRM 51-40-11-001-001-A01, AND 51-42-06-001-001-A01.
- [SDR REXA2022113002619](https://openairdocs.org/sdr/REXA2022113002619.md): Angle · corroded · Oct 26, 2022 · N538CA · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR ANGLE C AT INTERCOSTAL DD7A FOUND TO BE CORRODED. REMOVED, LOCATED, DRILLED, AND INSTALLED A NEW ANGLE C IAW SRM 51-40-11-001-001-A01, AND 51-42-21-001-001-A01.
- [SDR REXA2022113002606](https://openairdocs.org/sdr/REXA2022113002606.md): Stringer · corroded · Oct 26, 2022 · N538CA · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON STRINGER 26L, BS 295 - 310. COMPLIED REO 690-53-21-1555, REV-.
- [SDR REXA2022112302599](https://openairdocs.org/sdr/REXA2022112302599.md): Intercostal · corroded · Oct 26, 2022 · N538CA · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL DD1 AT AFT SIDE FOUND TO BE CORRODED. EVALUATED AND FOUND TO BE OUT OF LIMITS IAW CRJ900 SRM 52-11-00-001-001-A01. REMOVED DD1 AT AFT SIDE IAW CRJ900 SRM 51-42-06-001-001-A01. LOCATED DRILLED AND INSTALLED NEW SERVICEABLE INTERCOSTAL P/N:
- [SDR REXA2022111502556](https://openairdocs.org/sdr/REXA2022111502556.md): Intercostal · corroded · Oct 26, 2022 · N538CA · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL DD6 MID FOUND TO BE CORRODED. LOCATED AND DRILLED PAX DOOR INTERCOSTAL DD6 P/N 601R318057-1 IAW CRJ900 51-40-11-001-001-A01, INSTALLED INTERCOSTAL DD6 IAW CRJ900 51-42-06-001-001-A01 AND 51-42-21-001-001-A01
- [SDR REXA2022111502551](https://openairdocs.org/sdr/REXA2022111502551.md): Seat Track · corroded · Oct 26, 2022 · N538CA · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > LBL 9 FLOOR SEAT TRACK FS 693-835 HAS SEVERAL AREAS OF CORROSION. INSTALLED PASSENGER FLOOR SEAT TRACK LBL 9 FS 693 TO 835 IAW CRJ-900 AMM 53-00-49-400-801-A07
- [SDR REXA2022111502550](https://openairdocs.org/sdr/REXA2022111502550.md): Angle · corroded · Oct 26, 2022 · N538CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > SERVICE DOOR LOWER SILL ANGLE (P/N SH670-31986-1) IS CORRODED. REMOVED AND REPLACED LOWER SILL ANGLE IAW CRJ-900 SRM 51-42-06-001-001-A01,51-42-21-001-001-A01 AND 51-42-36-001-001-A01.
- [SDR REXA2022111102516](https://openairdocs.org/sdr/REXA2022111102516.md): Intercostal · corroded · Oct 26, 2022 · N538CA · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL DD7A CLIP FOUND TO BE CORRODED. REPLACED PAX DOOR INTERCOSTAL DD7A CLIP IAW CRJ900 SRM 51-42-06-001-001-A01 AND 51-40-11-001-001- A01.
- [SDR REXA2022111102512](https://openairdocs.org/sdr/REXA2022111102512.md): Seat Track · corroded · Oct 26, 2022 · N538CA · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT LBL9 FROM FS 661+16 AND 693.00 IS CORRODED. REPLACED SEAT TRACK LOCATED AT LBL 9 BETWEEN FS 661+16 TO FS 693.00 IAW CRJ 900 AMM 53-00-49-000-801-A07 AND 53-00-49-400-801-A07.
- [SDR REXA2022111102510](https://openairdocs.org/sdr/REXA2022111102510.md): Seat Track · corroded · Oct 26, 2022 · N538CA · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT RBL9 FROM FS 581.00 AND 661+16 IS CORRODED. INSTALLED SEAT TRACK SH690-33404-1 AT RBL9 FS 581.00 AND 661+16 IAW CRJ 900 AMM 53-00-49-400-801-A07
- [SDR REXA2022111102509](https://openairdocs.org/sdr/REXA2022111102509.md): Seat Track · corroded · Oct 26, 2022 · N538CA · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT LBL9 FROM FS 581.00 AND 661+16 IS CORRODED. INSTALLED SH690-33404-1 SEAT TRACK IAW CRJ 900 AMM 53-00-49-400-801-A07.
- [SDR REXA2022111102508](https://openairdocs.org/sdr/REXA2022111102508.md): Seat Track · corroded · Oct 26, 2022 · N538CA · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT RBL9 FROM FS 485.00 AND 581.00 IS CORRODED. INSTALLED NEW SEAT TRACK PN SH690-33407-1 IAW CRJ 900 AMM 53-00-49-400-801-A07.

Next page: https://openairdocs.org/aircraft/N538CA/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 = 'N538CA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N538CA/reports

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