# Service difficulty reports: N391CA

A list on [N391CA](https://openairdocs.org/aircraft/N391CA.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 6 · 270 reports

- [SDR REXA2026051500587](https://openairdocs.org/sdr/REXA2026051500587.md): Lamp · inoperative · May 14, 2026 · N391CA · Cndair CL6002C10 · Emergency Lighting
  > LAMPS INOP IN RIGHT EXIT ROW FLOOD LIGHT. R+R 5 LAMPS FROM RIGHT EXIT ROW FLOOD LIGHT REF AIPC 33-51-05 P/N: 6100928.
- [SDR REXA2022060701057](https://openairdocs.org/sdr/REXA2022060701057.md): Contact · damaged · Jun 1, 2022 · N391CA · Cndair CL6002C10 · Emergency Lighting
  > PASSENGER COMPARTMENT CEILING PANEL (243CLC) HAS A BROKEN WIRE FOR EMERGENCY LIGHTS NSTALLED NEW CONTACT ON P357 WIRE BUNDLE IAW CRJ 700 ESPM 20-16-11. OPS TEST GOOD.
- [SDR REXA2022061001154](https://openairdocs.org/sdr/REXA2022061001154.md): Frame · corroded · May 26, 2022 · N391CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > F.S. 863.00 FRAME IS CORRODED BETWEEN STGR 26L AND 26R. REPAIRED F.S. 863.00 FRAME IAW ENDEAVOR EA CRJ753-13478 REV IR DATED 4/29/22.
- [SDR REXA2022061001152](https://openairdocs.org/sdr/REXA2022061001152.md): Bulkhead · corroded · May 26, 2022 · N391CA · Cndair CL6002C10 · Fuselage Main, Structure
  > AFT SIDE OF NLG BULKHEAD IS CORRODED AT F.S. 235.00 BETWEEN STGR 26L AND 26R. REPAIRED BULKHEAD FRAME AT F.S. 235.00 IAW MHIRJ REO 670-53-11-1800 REV -- DATED 5/23/22.
- [SDR REXA2022061001141](https://openairdocs.org/sdr/REXA2022061001141.md): Seat Track · corroded · May 24, 2022 · N391CA · Cndair CL6002C10 · Fuselage Main, Structure
  > R/H SIDE SEAT TRACK BETWEEN F.S. 784.00 TO F.S. 861.00 IS CORRODED. REMOVED AND REPLACED SEAT TRACK I.A.W. BOMBARDIER CRJ700 AMM 53-00-49-000/400-801-A03.
- [SDR REXA2022060901121](https://openairdocs.org/sdr/REXA2022060901121.md): Frame · corroded · May 23, 2022 · N391CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FRAME 364.00 IS CORRODED BETWEEN STRINGER 26R AND STRINGER 27. REPAIRED FRAME I.A.W. BOMBARDIER REO 670-53-21-687 REV.A, DATED 2016-06-06.
- [SDR REXA2022060901102](https://openairdocs.org/sdr/REXA2022060901102.md): Seat Track · corroded · May 23, 2022 · N391CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > LBL 9.00 SEAT TRACK IS CORRODED BETWEEN F.S. 1000.00 TO F.S. 1051.30. REMOVED AND REPLACED CORRODED L/H SEAT TRACK I.A.W. BOMBARDIER CRJ700 AMM 53-00-49-000/400-801-A03.
- [SDR REXA2022060901123](https://openairdocs.org/sdr/REXA2022060901123.md): Beam · corroded · May 20, 2022 · N391CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FLOOR BEAM AT LBL 9.0 FS 1000-1033 HAS CORROSION ON UPPER SURFACE. BLENDED UPPER SURFACE OF FLOOR BEAM. FOUND TO BE OUT OF LIMITS IAW CRJ 700 SRM 53-61-43-101-001-A01. REMOVED AND REPLACED FLOOR BEAM SEGMENT FROM FS 977.00 TO FS 1037.00 IAW CRJ 700 SRM 53-00-
- [SDR REXA2022061001159](https://openairdocs.org/sdr/REXA2022061001159.md): None · corroded · May 19, 2022 · N391CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > LBL 27 FLOOR BEAM IS CORRODED BETWEEN F.S. 1015.00 AND 1096.00. BLENDED AND REPAIRED FLOOR BEAM IAW CRJ 700 SRM 53-00-41-201-001-A01 AND ENDEAVOR EA# CRJ753-13566 REV IR DATED 5/8/22.
- [SDR REXA2022061001169](https://openairdocs.org/sdr/REXA2022061001169.md): Stringer · corroded · May 14, 2022 · N391CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > STRINGER 24R IS CORRODED BETWEEN F.S. 333.00 AND 364.00. REPAIRED STRINGER 24R IAW CRJ 700 SRM 53-00-03-201-001-A01.
- [SDR REXA2022061001165](https://openairdocs.org/sdr/REXA2022061001165.md): Angle · cracked · May 14, 2022 · N391CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > 221ALF R/H FLOOR SUPPORT ANGLE CRACKED. REMOVED & REPLACED IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-13-001-001-A01, AND 51-42-21-001-001-A01.
- [SDR REXA2022061001160](https://openairdocs.org/sdr/REXA2022061001160.md): None · corroded · May 14, 2022 · N391CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > STRINGER CLIP CORRODED AT STRINGER 21R AND FS 379.00. REMOVED & REPLACED IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.
- [SDR REXA2022061001158](https://openairdocs.org/sdr/REXA2022061001158.md): Seat Track · corroded · May 14, 2022 · N391CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > RBL 9 SEAT TRACK IS CORRODED BETWEEN FS985 -FS1000. REMOVED RBL 9 SEAT TRACK. FABRIACTED SEAT TRACK AND INSTALLED A SERVICEABLE SEAT TRACK AT RBL 9 BETWEEN F.S. 985 TO F.S. 1000 IAW CRJ 700 SRM 53-00-49-201-002-A01 AND CRJ 700 AMM 53-00-49-400-801-A17.
- [SDR REXA2022061001151](https://openairdocs.org/sdr/REXA2022061001151.md): Intercostal · corroded · May 14, 2022 · N391CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT STRINGER 27R IS CORRODED BETWEEN F.S. 349.00 AND 364.00. REMOVED & REPLACED IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.
- [SDR REXA2022061001155](https://openairdocs.org/sdr/REXA2022061001155.md): Stringer · corroded · May 13, 2022 · N391CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > STGR20R IS CORRODED BETWEEN FS310 AND FS319 REPLACED STGR20R BETWEEN FS280 AND FS319 IAW CRJ-700 SRM 51-40-11-001-001-A01, AND 51-42-06-001-001-A01.
- [SDR REXA2022061001172](https://openairdocs.org/sdr/REXA2022061001172.md): Cleat · corroded · May 12, 2022 · N391CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > UPON GAINING ACCESS TO REMOVED FS295 FRAME FOUND GROUNDING POINT BRACKET AT FS333 STGR21R FOUND TO BE CORRODED. REPLACED GROUNDING POINT CLEAT PN: SH670-32605-2 AT FS333 STGR21R IAW CRJ-700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A
- [SDR REXA2022061001168](https://openairdocs.org/sdr/REXA2022061001168.md): Stringer · corroded · May 12, 2022 · N391CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON STGR23R BETWEEN FS364 AND FS379. REPLACED STGR 23R PN: SH670-31380-1 BETWEEN FS333 AND FS379 IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.
- [SDR REXA2022061001167](https://openairdocs.org/sdr/REXA2022061001167.md): Bracket · corroded · May 12, 2022 · N391CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > AVIONICS BRACKET ON STGR21R BETWEEN FS349 AND FS364 IS CORRODED. REPLACED BRACKET ON STGR21R BETWEEN FS349 AND FS364 IAW CRJ-700 SRM 53-42-13-001-001-A01.
- [SDR REXA2022061001166](https://openairdocs.org/sdr/REXA2022061001166.md): Splice · corroded · May 12, 2022 · N391CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON STGR JOINT SPLICE AT FS333 AND STGR21R. REPLACED STGR JOINT SLPICE AT FS333 STGR21R IAW CRJ-700 SRM 51-40-11-001-001-A01, AND 51-42-06-001-001-A01.
- [SDR REXA2022061001164](https://openairdocs.org/sdr/REXA2022061001164.md): Stringer · corroded · May 12, 2022 · N391CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION FOUND AT STGR 21R BETWEEN FS333 TO FS349. REPLACED STRG 21R BETWEEN FS333 AND FS379 IAW CRJ-700 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, AND 51-40-11-001-001-A01.
- [SDR REXA2022061001163](https://openairdocs.org/sdr/REXA2022061001163.md): Cleat · corroded · May 12, 2022 · N391CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION FOUND AT STGR CLEAT LOCATED AT FS349 AND STGR21R. REPLACED STRG 21R CLEAT AT FS349 IAW CRJ-700 SRM 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.
- [SDR REXA2022061001162](https://openairdocs.org/sdr/REXA2022061001162.md): Gusset · worn · May 12, 2022 · N391CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > UPON REMOVING FS319 AND FS333 CLEAT FOUND GUSSET AT FS319 TO HAVE ELONGATED HOLES. REPLACED GUSSET AT FS319 AND STGR20R IAW CRJ-700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.
- [SDR REXA2022061001161](https://openairdocs.org/sdr/REXA2022061001161.md): Cleat · corroded · May 12, 2022 · N391CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > UPON GAINING ACCESS TO REMOVED FS295 FRAME FOUND GROUNDING POINT BRACKET AT FS319 STGR21R FOUND TO BE CORRODED. REPLACED GROUNDING POINT CLEAT PN: SH670-32695-7 AT FS319 STGR21R IAW CRJ-700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A
- [SDR REXA2022061001171](https://openairdocs.org/sdr/REXA2022061001171.md): None · corroded · May 11, 2022 · N391CA · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR AFT HANDRAIL CLIP IS CORRODED. REPLACED PAX DOOR HANDRAIL CLIP LOCATED AT STGR 18L FS342 IAW CRJ-700 SRM 51-40-11-001-001-A01, 51-41-02-001-001-A01, 51-42-06-001-001-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01 AND 51-42-15-001-001-A01
- [SDR REXA2022061001153](https://openairdocs.org/sdr/REXA2022061001153.md): None · corroded · May 11, 2022 · N391CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > PAX DOOR LOWER SILL PLATE CORRODED. REPLACED PAX DOOR LOWER SILL PLATE IAW CRJ-700 SRM 51-40-11-001-001-A01, 51-41-02-001-001-A01, 51-42-06-001-001-A01, AND 51-42-15-001-001-A01
- [SDR REXA2022061001150](https://openairdocs.org/sdr/REXA2022061001150.md): Angle · corroded · May 11, 2022 · N391CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > PAX DOOR LOWER SILL MID CAP ANGLE CORRODED. REPLACED PAX DOOR LOWER SILL MID CAP ANGLE IAW CRJ-700 SRM 51-40-11-001-001-A01, 51-41-02-001-001-A01, 51-42-06-001-001-A01, AND 51-42-15-001-001-A01
- [SDR REXA2022061001149](https://openairdocs.org/sdr/REXA2022061001149.md): None · corroded · May 11, 2022 · N391CA · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR FWD HANDRAIL CLIP IS CORRODED. REPLACED PAX DOOR HANDRAIL CLIP LOCATED AT STGR 18L FS314 IAW CRJ-700 SRM 51-40-11-001-001-A01, 51-41-02-001-001-A01, 51-42-06-001-001-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01 AND 51-42-15-001-001-A01
- [SDR REXA2022061001147](https://openairdocs.org/sdr/REXA2022061001147.md): Stringer · corroded · May 10, 2022 · N391CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION FOUND AT STRINGER 21R BETWEEN F.S. 319.00 AND F.S. 333.00. REMOVED AND REPLACED STRINGER SEGMENT I.A.W. BOMBARDIER CRJ700 SRM 53-21-03-101-002-A01.
- [SDR REXA2022060701065](https://openairdocs.org/sdr/REXA2022060701065.md): Cleat · corroded · May 10, 2022 · N391CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CLEAT AT STRINGER 20R IS CORRODED BETWEEN F.S. 310.00 AND F.S. 319.00. REMOVED AND REPLACED CLEAT I.A.W. BOMBARDIER CRJ700 SRM 51-40-11-001-001-A1 AND 51-42-06-001-001-A01.
- [SDR REXA2022061001129](https://openairdocs.org/sdr/REXA2022061001129.md): Web · corroded · May 9, 2022 · N391CA · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR AFT WEB CORRODED ON UPPER AND LOWER SIDES. REMOVED AND REPLACED PAX DOOR AFT WEB I.A.W. BOMBARDIER CRJ700 SRM 51-42-06-001-001-A01 AND 51-42-13-001-001-A01.
- [SDR REXA2022060901124](https://openairdocs.org/sdr/REXA2022060901124.md): Web · corroded · May 9, 2022 · N391CA · Cndair CL6002C10 · Passenger/Crew Doors
  > FWD PAX DOOR WEB PANEL CORRODED ON UPPER SIDE AND LOWER SIDE. REMOVED & REPLACED PANEL IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-42-13-001-001-A01 & 51-42-06-001-001-A01.
- [SDR REXA2022060801080](https://openairdocs.org/sdr/REXA2022060801080.md): Intercostal · corroded · May 9, 2022 · N391CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > L/H AND R/H JACK FITTING SUPPORT INTERCOSTALS BETWEEN F.S. 265.00 AND F.S. 280.00 ARE CORRODED. REMOVED AND REPLACED L/H AND R/H JACK FITTING SUPPORT INTERCOSTALS I.A.W. ENDEAVOR AIRLINES EA# CRJ753-13413 REV.IR, DATED 04/19/2022.
- [SDR REXA2022060701060](https://openairdocs.org/sdr/REXA2022060701060.md): Doubler · corroded · May 9, 2022 · N391CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > DOUBLER AT STRINGER 26L BETWEEN F.S. 533.00 AND F.S. 581.00 IS CORRODED AND GOUGED. REPAIRED DAMAGE I.A.W. ENDEAVOR AIRLINES EA# CRJ753-13466 REV.IR, DATED 05/07/2022.
- [SDR REXA2022061001145](https://openairdocs.org/sdr/REXA2022061001145.md): Stiffener · corroded · May 7, 2022 · N391CA · Cndair CL6002C10 · Passenger/Crew Doors
  > 5 STIFFENERS ON TOP PANEL FOR PASSENGER DOOR FOUND TO BE CORRODED. REMOVED AND REPLACED STIFFENERS IAW CRJ 700 SRM 51-42-06-001-001-A01.
- [SDR REXA2022061001142](https://openairdocs.org/sdr/REXA2022061001142.md): Angle · corroded · May 7, 2022 · N391CA · Cndair CL6002C10 · Passenger/Crew Doors
  > PASSENGER DOOR BOTTOM ANGLE FOUND TO BE CORRODED. REMOVED AND REPLACED PASSENGER DOOR BOTTOM ANGLE IAW CRJ 700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.
- [SDR REXA2022060701067](https://openairdocs.org/sdr/REXA2022060701067.md): Frame · corroded · May 7, 2022 · N391CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FRAME CORRODED AT F.S. 250, BETWEEN STGR 26L AND 26R. SPLICE REPAIRED FRAME SECTOR IAW ENDEAVOR AIR EA CRJ753-13396.
- [SDR REXA2022060701055](https://openairdocs.org/sdr/REXA2022060701055.md): None · cracked · May 7, 2022 · N391CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CRACK ABOVE RH AFT TRU BAY DOOR LATCH ON DOOR LANDING REMOVED &REPLACED LANDING IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 & 51-42-13-001-001-A01.
- [SDR REXA2022061001146](https://openairdocs.org/sdr/REXA2022061001146.md): Intercostal · corroded · May 6, 2022 · N391CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > INTERCOSTAL JUST LEFT OF STRINGER 27 BETWEEN F.S.349 AND F.S.364 IS CORRODED. REMOVED AND REPLACED INTERCOSTAL LEFT OF STRINGER 27 BETWEEN F.S. 349 TO FS 364 IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.
- [SDR REXA2022060901091](https://openairdocs.org/sdr/REXA2022060901091.md): Skin · corroded · May 6, 2022 · N391CA · Cndair CL6002C10 · Passenger/Crew Doors
  > PASSENGER DOOR INNER SKIN IS CORRODED AT F.S.338.0 BETWEEN DOOR DATUM A1 AND 1 REMOVED AND REPLACED PASSENGER DOOR INNER SKIN IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-13-001-001-A01. AND 51-42-21-001-001-A01
- [SDR REXA2022061001157](https://openairdocs.org/sdr/REXA2022061001157.md): Fitting · corroded · May 5, 2022 · N391CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > INSIDE CABIN AT F.S.310 LH SILL, PASSENGER DOOR FORWARD FRAME FLOOR LEVEL, TEAR STRAP IS CORRODED. REMOVED AND REPLACED FLOOR BEAM FITTING IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 51-42-20-001-001-A01.
- [SDR REXA2022061001156](https://openairdocs.org/sdr/REXA2022061001156.md): None · chafed · May 5, 2022 · N391CA · Cndair CL6002C10 · Engine Thrust Reverser
  > RIGHT HAND UPPER TRANS COWL LATCH DOOR AND DOOR CUT OUT IS CHAFED. REMOVED AND REPLACED LATCH DOOR CUT OUT IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-13-001-001-A01 AND BOMBARDIER REO 670-54-21-1207.
- [SDR REXA2022061001148](https://openairdocs.org/sdr/REXA2022061001148.md): Doubler · corroded · May 3, 2022 · N391CA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > ANTENNA DOUBLER CORRODED BETWEEN FS 1031.00 AND FS 1047.00 RIGHT OF STGR 27. REMOVED & REPLACED DOUBLER IAW CRJ 700 SRM 51-40-11-001-001-A01 & 51-42-06-001-001-A01.
- [SDR REXA2022061001132](https://openairdocs.org/sdr/REXA2022061001132.md): Hinge Fitting · none · May 3, 2022 · N391CA · Cndair CL6002C10 · Wing Structure
  > RH AILERON LUG MARKED "C" CAME IN WITH O/S BORE. REPAIRED AILERON CENTER HINGE FITTING LUG IAW BOMBARDIER REO 670-57-61-107.
- [SDR REXA2022061001131](https://openairdocs.org/sdr/REXA2022061001131.md): Hinge Fitting · corroded · May 3, 2022 · N391CA · Cndair CL6002C10 · Wing Structure
  > CENTER HINGE PCU LUGS "C" AND "F" ON LH AILERON HAVE CORROSION ON INNER BORES BOTH HAVE BEEN PREVIOUSLY OVERSIZED. REPAIRED AILERON CENTER HINGE FITTING LUG IAW BOMBARDIER REO 670-57-61-107.
- [SDR REXA2022061001130](https://openairdocs.org/sdr/REXA2022061001130.md): Hinge Fitting · corroded · May 3, 2022 · N391CA · Cndair CL6002C10 · Wing Structure
  > O/B PCU LUG "F" ON RH AILERON HAS CORROSION ON INNER BORE AND FOUND TO BE PREVIOUSLY OVERSIZED. REPAIRED AILERON CENTER HINGE FITTING LUG IAW BOMBARDIER REO 670-57-61-107.
- [SDR REXA2022061001144](https://openairdocs.org/sdr/REXA2022061001144.md): Stiffener · corroded · May 2, 2022 · N391CA · Cndair CL6002C10 · Passenger/Crew Doors
  > UPON REMOVAL FOUND 2EA. SIDE PANEL STIFFENERS TO BE DAMAGED, REQUIRES REPLACEMENT. REMOVED AND REPLACED PASSENGER DOOR AFT WEB STIFFENERS IAW CRJ 700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.
- [SDR REXA2022061001143](https://openairdocs.org/sdr/REXA2022061001143.md): Angle · corroded · May 2, 2022 · N391CA · Cndair CL6002C10 · Passenger/Crew Doors
  > UPON REMOVAL FOUND DRAG ANGLE TO BE CORRODED, REQUIRES REPLACEMENT. REMOVED AND REPLACED DRAG ANGLE IAW CRJ 700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.
- [SDR REXA2022061001140](https://openairdocs.org/sdr/REXA2022061001140.md): Angle · corroded · May 2, 2022 · N391CA · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR FWD FORMER SUPPORT ANGLE FOUND TO BE CORRODED (P/N: 601R318731-3). REMOVED AND REPLACED ANGLE IAW CRJ 700 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01
- [SDR REXA2022061001136](https://openairdocs.org/sdr/REXA2022061001136.md): Frame · corroded · May 2, 2022 · N391CA · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR FRAME CORRODED BETWEEN DD4 AND DD5. APPROX. F.S. 313.56. REMOVED AND REPLACED FRAME I.A.W. BOMBARDIER CRJ700 SRM 51-42-06-001-001-A01.
- [SDR REXA2022060901122](https://openairdocs.org/sdr/REXA2022060901122.md): Hinge · worn · May 2, 2022 · N391CA · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR HINGE (FUSELAGE SIDE) LANDINGS/BORES WORN BEYOND LIMITS, ROLL PIN DAMAGE ON AFT END. REPLACED PAX DOOR HINGE (FUSELAGE SIDE) IAW CRJ 700 SRM 53-21-23-201-007-A01.

Next page: https://openairdocs.org/aircraft/N391CA/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 = 'N391CA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N391CA/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.