# Service difficulty reports: N678CA

A list on [N678CA](https://openairdocs.org/aircraft/N678CA.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 · 214 reports

- [SDR REXA2026052800865](https://openairdocs.org/sdr/REXA2026052800865.md): Contact · inoperative · May 27, 2026 · N678CA · Cndair CL6002D24 · Light System Wiring
  > AFT EMER CEILING LIGHT INOPERATIVE. REPINNED P361 IAW CRJ 900 ESPM 20-26-03. P# OFF/ON 350690-7. OPS CHECKS GOOD IAW AMM 33-51-00.
- [SDR REXA2026052700691](https://openairdocs.org/sdr/REXA2026052700691.md): Stand Off · cracked · Feb 15, 2026 · N678CA · Cndair CL6002D24 · Engine Thrust Reverser
  > PARTS RACK: CRACKED INNER SUPPORT ANGLE (STANDOFF 1 EA) ON LH LOWER TRANSCOWL. INNER SUPPORT ANGLE (STANDOFF 1 EA) ON LH LOWER TRANSCOWL WAS REPAIRED AND REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01, CRJ-900 SRM 51-42-28-001-001-A01, EA CRJ954-21413 REV A, C
- [SDR REXA2026052700703](https://openairdocs.org/sdr/REXA2026052700703.md): Hinge · corroded · Jan 29, 2026 · N678CA · Cndair CL6002D24 · Ailerons
  > CORROSION AT INNER LUG BORES OF RH AILERON, CENTER HINGE FITTING AILS R1,R2,R5 AND R6 WAS FOUND LUGS BORES R1, R5 AND R6 RH AILERON WERE CLEANED PER CRJ 900 SRM 51-26-00-001-001-A01 CLEANING AND NOT FOUND CORROSION & R2 WERE REPAIRED PER REO 670-57-61-107 REV
- [SDR REXA2026052700706](https://openairdocs.org/sdr/REXA2026052700706.md): Packer · corroded · Jan 17, 2026 · N678CA · Cndair CL6002D24 · Fuselage Main, Structure
  > AFTER FWD WASTE LAVATORY SERVICE PANEL DOOR REMOVAL, CORROSION ON PACKERS (2EAS) WERE FOUND PACKERS (2EAS) WERE REPLACED ON FWD WASTE LAVATORY SERVICE PANEL DOOR PER CRJ900 SRM 51-10-06-001-001-A01 AND INSTALLED WITH NRC 00030.
- [SDR REXA2026052700705](https://openairdocs.org/sdr/REXA2026052700705.md): Hinge · corroded · Jan 17, 2026 · N678CA · Cndair CL6002D24 · Fuselage, Door Hinge
  > SECONDARY NRC FROM RC 900-32-710-902Ï¿½: AFTER HARDWARE REMOVAL, CORROSION ON LH/RH FITTING, NLG W/W AREA WAS FOUND LH/RH FITTING, NLG W/W WERE REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01
- [SDR REXA2026052700702](https://openairdocs.org/sdr/REXA2026052700702.md): Diaphragm · cracked · Jan 12, 2026 · N678CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AFTER CLEANING, CRACK IN LH FAIRING SUPPORT DIAPHRAGM IN STA. FS= 797 TO FS= 807 AND 35LBL AT LH MLG WHEEL WELL WAS FOUND. FAIRING SUPPORT DIAPHRAGM LH IN STA. FS= 797 TO FS= 807 AND 35LBL AT LH MLG WHEEL WELL WAS REPLACED PER CRJ/900 SRM 51-41-02-001-001-A01
- [SDR REXA2026052700709](https://openairdocs.org/sdr/REXA2026052700709.md): Hinge · cracked · Jan 11, 2026 · N678CA · Cndair CL6002D24 · Fuselage Main, Structure
  > INITIAL INSPECTION: CRACK ON HINGE OF THE BUTTER DOOR ACCESS PANEL 591LB AT LH WING. CRACK ON HINGE OF THE BUTTER DOOR ACCESS PANEL 591LB AT LH WING WAS REPAIRED PER EA NO: CRJ957-21363 REV. IR
- [SDR REXA2026052700707](https://openairdocs.org/sdr/REXA2026052700707.md): Frame · cracked · Jan 11, 2026 · N678CA · Cndair CL6002D24 · Fuselage Main, Frame
  > CRACK ON FUSELAGE FRAME FS 533.00 BTW STGR 0/ STGR 1R CRACK ON FUSELAGE FRAME FS 533.00 BTW STGR 0/ STGR 1R WAS REPAIRED PER EA CRJ953-19684 REV IR
- [SDR REXA2026052700701](https://openairdocs.org/sdr/REXA2026052700701.md): Hinge · corroded · Jan 11, 2026 · N678CA · Cndair CL6002D24 · Fuselage, Door Hinge
  > SECONDARY NRC FROM NRC 00129: AFTER REMOVAL OF FLAP STEP PLATE, CORROSION ON FLAP STEP PLATE HINGES (ALL) WAS FOUND. FLAP STEP PLATE HINGES (FWD,MID, AFT) WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND EA CRJ953-21415 REV, IR.
- [SDR REXA2026052700700](https://openairdocs.org/sdr/REXA2026052700700.md): Hinge · corroded · Jan 11, 2026 · N678CA · Cndair CL6002D24 · Fuselage, Door Hinge
  > SECONDARY NRC FROM NRC 00129: AFTER REMOVAL OF FLAP STEP PLATE, CORROSION ON FLAP STEP PLATE HINGES (ALL) WAS FOUND. FLAP STEP PLATE HINGES (FWD,MID, AFT) WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND EA CRJ953-21415 REV, IR.
- [SDR REXA2026052700699](https://openairdocs.org/sdr/REXA2026052700699.md): Hinge · corroded · Jan 11, 2026 · N678CA · Cndair CL6002D24 · Fuselage, Door Hinge
  > SECONDARY NRC FROM NRC 00129: AFTER REMOVAL OF FLAP STEP PLATE, CORROSION ON FLAP STEP PLATE HINGES (ALL) WAS FOUND. FLAP STEP PLATE HINGES (FWD,MID, AFT) WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND EA CRJ953-21415 REV, IR.
- [SDR REXA2026052700696](https://openairdocs.org/sdr/REXA2026052700696.md): Seat Track · corroded · Jan 11, 2026 · N678CA · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > INITIAL INSPECTION: CORROSION ON SEAT TRACK LOCATED BTW FS349.00 TO FS379.00 AND RBL9.00. SEAT TRACK LOCATED BTW FS349.00 TO FS379.00 AND RBL9.00 WAS REPLACED PER CRJ-900 AMM 53-00-49-000-801-A07. AND AMM 53-00-49-400-801-A07.
- [SDR REXA2026052700692](https://openairdocs.org/sdr/REXA2026052700692.md): Angle · cracked · Jan 11, 2026 · N678CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > OUT OF SCOPE: CRACKED INTERNAL ANGLE OF EXTERNAL POWER RECEPTACLE. INTERNAL ANGLE OF EXTERNAL POWER RECEPTACLE. WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND SRM 51-42-13-001-001-A01.
- [SDR REXA2026052700690](https://openairdocs.org/sdr/REXA2026052700690.md): Skin · chafed · Jan 11, 2026 · N678CA · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > WEAR ON FUSELAGE SKIN BTW STA FS=910 TO FS=930 AND BTW STGR 24 LH AND 24 RH. WEAR ON FUSELAGE SKIN BTW STA FS=910 TO FS=930 AND BTW STGR 24 LH AND 24 RH WERE BLEND OUT AND EVALUATED WITHIN LIMITS BTW FS913 TO FS930, STRG 24L/24R PER CRJ900 SRM 51-12-00-001-0
- [SDR REXA2026052700698](https://openairdocs.org/sdr/REXA2026052700698.md): Floor Support · cracked · Jan 10, 2026 · N678CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACKED FLOOR SUPPORT BTW FS=295.00 TO 319.70 AND RBL 27 AT PASSENGER FLOOR STRUCTURE FLOOR SUPPORT BTW FS=295.00 TO 319.70 AND RBL 27 AT PASSENGER FLOOR STRUCTURE WAS REPLACED PER CRJ900 SRM 51-42-13-001-001-A01 & SRM 51-42-06-001-001-A01
- [SDR REXA2026052700695](https://openairdocs.org/sdr/REXA2026052700695.md): Fitting · corroded · Jan 10, 2026 · N678CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION FLOOR FITTING ON ACCESS 107 (1EA) AISLE SIDE AND ACCESS 109 (1EA) ON GALLEY 1. SUMMARY OF NRC 00251: FLOOR FITTING (1EA) AND DOUBLER FLOOR FITTING (1EA) AISLE SIDE ON ACCESS 107 AND FLOOR FITTING (1EA) ON ACCESS 109 AT GALLEY 1 WERE REPLACED PER SAFR
- [SDR REXA2026052700693](https://openairdocs.org/sdr/REXA2026052700693.md): Fitting · corroded · Jan 10, 2026 · N678CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION FLOOR FITTING ON ACCESS 107 (1EA) AISLE SIDE AND ACCESS 109 (1EA) ON GALLEY 1. SUMMARY OF NRC 00251: FLOOR FITTING (1EA) AND DOUBLER FLOOR FITTING (1EA) AISLE SIDE ON ACCESS 107 AND FLOOR FITTING (1EA) ON ACCESS 109 AT GALLEY 1 WERE REPLACED PER SAFR
- [SDR REXA2026052700679](https://openairdocs.org/sdr/REXA2026052700679.md): Door · cracked · Jan 10, 2026 · N678CA · Cndair CL6002D24 · Emergency Exits
  > CRACKED TOP EDGE STRUCTURE OF LEFT FORWARD OVERWING EMERGENCY EXIT DOOR. TOP EDGE STRUCTURE OF LEFT FORWARD OVERWING EMERGENCY EXIT DOOR WAS REPAIRED PER REO 670-52-21-103 REV. --
- [SDR REXA2026052700689](https://openairdocs.org/sdr/REXA2026052700689.md): Door Sill · cracked · Jan 8, 2026 · N678CA · Cndair CL6002D24 · Fuselage Main, Structure
  > INITIAL INSPECTION: CRACK ON AFT RH DOOR LANDING FS 188.0 (LATCH CUT OUT OF ACCESS DOOR 212AR) AT FWD EQUIPMENT COMPARTMENT. DOOR LANDING (LATCH CUT OUT OF ACCESS DOOR 212AR) AT FWD EQUIPMENT COMPARTMENT WAS REPLACED PER EA CRJ953-21314 REV. IR AND CRJ-900 SR
- [SDR REXA2026052700681](https://openairdocs.org/sdr/REXA2026052700681.md): Landing · cracked · Jan 8, 2026 · N678CA · Cndair CL6002D24 · Passenger/Crew Doors
  > CRACK ON SETTLEMENT AREA OF ACCESS PANEL 832DR AT PASSENGER DOOR. SETTLEMENT AREA OF ACCESS PANEL 832DR AT PASSENGER DOOR WAS REPAIRED PER EA NO. CRJ952-21312 REV. A.
- [SDR REXA2026052700708](https://openairdocs.org/sdr/REXA2026052700708.md): Skin · corroded · Jan 6, 2026 · N678CA · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > CORROSION ON INTERNAL SKIN FROM STA FS 364 TO 394 BTW STGR 25L-25R AT E/E COMPARTMENT DOOR CUTOUT INTERNAL SKIN FROM STA FS 364 TO 394 BTW STGR 25L-25R AT E/E COMPARTMENT DOOR CUTOUT WAS REPAIRED PER REO 690-53-21-032 REV. --
- [SDR REXA2022121402705](https://openairdocs.org/sdr/REXA2022121402705.md): Bracket · cracked · Dec 14, 2022 · N678CA · Cndair CL6002D24 · Fuselage Main, Attach Fittings
  > WHILE REMOVING ASSEMBLY MADE BRACKET, FOUND BRACKETS CRACKED ON TOP OF BS 220 LT & RT. REMOVED AND REPLACED THE BRACKETS IAW SRM 51-42-06-001-001-A01.
- [SDR REXA2022071401594](https://openairdocs.org/sdr/REXA2022071401594.md): Sign · inoperative · Jul 6, 2022 · N678CA · Cndair CL6002D24 · Emergency Lighting
  > FWD OVER WING BOTTOM DOOR EXIT LIGHT INOP. R/R IDENTIFIER EXIT ASSEMBLY @ EXIT SING DS177 IAW AMM 33-51-05. OPS TEST GOOD. P/N ON/OFF: BR9279-013
- [SDR REXA2022071401595](https://openairdocs.org/sdr/REXA2022071401595.md): Light · inoperative · Jun 29, 2022 · N678CA · Cndair CL6002D24 · Emergency Lighting
  > RH OVERWING EMERGENCY LIGHTS ARE INOP.
- [SDR REXA2022062401338](https://openairdocs.org/sdr/REXA2022062401338.md): Intercostal · corroded · Jun 22, 2022 · N678CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT STRINGER 20R IS CORRODED BETWEEN F.S.333 TO F.S.349 REMOVED AND REPLACED INTERCOSTAL IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.
- [SDR REXA2022062401337](https://openairdocs.org/sdr/REXA2022062401337.md): Angle · cracked · Jun 22, 2022 · N678CA · Cndair CL6002D24 · Vertical Stabilizer
  > R/H FWD VERT DRAG ANGLE IS CRACKED. REPAIRED R/H FWD DRAG ANGLE IAW CRJ 900 SRM 55-31-00-201-001-A01
- [SDR REXA2022070101449](https://openairdocs.org/sdr/REXA2022070101449.md): Stringer · corroded · Jun 21, 2022 · N678CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STRINGER 25L BETWEEN FS 485.00 AND FS 517.00 IS CORRODED REPAIRED STRINGER IAW ENDEAVOR EA CRJ953-13740 REV A DATED 6/24/2022.
- [SDR REXA2022062401339](https://openairdocs.org/sdr/REXA2022062401339.md): Doubler · corroded · Jun 21, 2022 · N678CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > ANTENNA DOUBLER CORRODED AT STGR 27 BETWEEN FS 485.00 AND FS 501.00 REMOVED AND REPLACED DOUBLER (NUT PLATE SUB ASSEMBLY) I.A.W. CRJ 900 SRM'S #51-40-11-001-001-A01 AND51-42-06-0001-001-A01
- [SDR REXA2022062701351](https://openairdocs.org/sdr/REXA2022062701351.md): Fitting · corroded · Jun 19, 2022 · N678CA · Cndair CL6002D24 · Passenger/Crew Doors
  > FOUND CORROSION ON PAX DOOR FWD CLOSING FITTING AFTER REMOVING UPPER DOOR SILL ANGLE. REMOVED & REPLACED FITTING IAW CRJ 900 SRM 51-40-11-001-001-A01 & 51-42-06-001-001-A01.
- [SDR REXA2022062201320](https://openairdocs.org/sdr/REXA2022062201320.md): Stringer · corroded · Jun 19, 2022 · N678CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STRINGER 24R CORRODED BETWEEN FS581.00 AND FS597.00 REPAIRED IAW ENDEAVOR EA CRJ953-13716 REV IR DATED; 5/27/2022
- [SDR REXA2022062201315](https://openairdocs.org/sdr/REXA2022062201315.md): Former · corroded · Jun 19, 2022 · N678CA · Cndair CL6002D24 · Passenger/Crew Doors
  > FORMER ON PASSENGER DOOR AT FS329.41 BETWEEN DD5 AND DD6 IS CORRODED. REPLACED FORMER IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.
- [SDR REXA2022062201309](https://openairdocs.org/sdr/REXA2022062201309.md): Frame · cracked · Jun 19, 2022 · N678CA · Cndair CL6002D24 · Emergency Exits
  > LEFT FORWARD EMERGENCY EXIT DOOR TOP EDGE MEMBER HAS POSSIBLE CRACK AT DOOR SWITCH STOP. REPAIRED TOP EDGE MEMBER ON L/H FWD EMERGENCY EXIT DOOR IAW ENDEAVOR AIR EA CRJ952-13633 REV IR DATED 5-17-2022.
- [SDR REXA2022062701364](https://openairdocs.org/sdr/REXA2022062701364.md): Stringer · corroded · Jun 17, 2022 · N678CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STGR 22R IS CORRODED BETWEEN FS 319.00 - FS 333.00. REMOVED, FABRICATED & REPLACED STRINGER IAW ENDEAVOR AIR EA CRJ953-13763.
- [SDR REXA2022062201321](https://openairdocs.org/sdr/REXA2022062201321.md): Intercostal · corroded · Jun 15, 2022 · N678CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INTERCOSTAL CORRODED BETWEEN FS 865 AND FS 881 @ STGR 21R. REPAIRED INTERCOSTAL IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 & ENDEAVOR AIR EA CRJ953-13700.
- [SDR REXA2022062201306](https://openairdocs.org/sdr/REXA2022062201306.md): Angle · cracked · Jun 15, 2022 · N678CA · Cndair CL6002D24 · Vertical Stabilizer
  > R/H AFT VERT DRAG ANGLE IS CRACKED. REMOVED & REPLACED R/H AFT DRAG ANGLE IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-13-001-001-A01, 51-42-22-001-001-A01, 51-42-21-001-001-A01 & 51-25-01-001-001-A01.
- [SDR REXA2022070101447](https://openairdocs.org/sdr/REXA2022070101447.md): Drag Angle · cracked · Jun 13, 2022 · N678CA · Cndair CL6002D24 · Horizontal Stabilizer Structure
  > LH AFT VERTICAL DRAG ANGLE CRACKED. REPLACED LH AFT DRAG ANGLE IAW CRJ 900 SRM 51-42-13-001-001-A01, 51-42-21-001-001-A01, AND 51-42-22-001-001-A01.
- [SDR REXA2022070101446](https://openairdocs.org/sdr/REXA2022070101446.md): Stringer · corroded · Jun 13, 2022 · N678CA · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STGR 24R BETWEEN FS 295 TO FS310 FOUND 2 LOCATIONS AROUND FASTENERS CORRODED. REPAIRED STRINGER IAW ENDEAVOR EA CRJ953-13804 REV IR DATED 6/24/2022.
- [SDR REXA2022070101445](https://openairdocs.org/sdr/REXA2022070101445.md): Stringer · corroded · Jun 13, 2022 · N678CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STGR 24R BETWEEN FS 333 TO FS409 FOUND 4 LOCATIONS AROUND FASTENERS CORRODED. REPAIRED STRINGER IAW ENDEAVOR EA CRJ953-13887 REV IR DATED 6/27/2022.
- [SDR REXA2022062701357](https://openairdocs.org/sdr/REXA2022062701357.md): Seat Track · corroded · Jun 13, 2022 · N678CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > PASSENGER SEAT TRACK AT LBL 9 FS 977 - FS 1000 IS CORRODED. REMOVED, FABRICATED & REPLACED SEAT TRACK IAW CRJ 900 SRM 51-40-11-001-001-A01, 53-00-49-201-002-A01 & AMM 53-00-49-000/400-801-A07.
- [SDR REXA2022062301332](https://openairdocs.org/sdr/REXA2022062301332.md): None · corroded · Jun 13, 2022 · N678CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > LH SIDE SEAT RAIL F.S. 673.- 720 HAS MULTIPLE SPOTS OF CORROSION REMOVED, FABRICATED AND REPLACED SIDE SEAT RAIL IAW CRJ SRM 53-00-49-201-002-A01 & AMM 53-00-49-000/400-801-A07
- [SDR REXA2022062201323](https://openairdocs.org/sdr/REXA2022062201323.md): Frame · corroded · Jun 13, 2022 · N678CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FRAME CORRODED @ FS 942 BETWEEN STGR 27 AND STGR 25R. SPLICE REPAIRED FRAME USING FRAME SECTOR PART NUMBER SH690-37073-5 IN LIEU OF P/N SH690-37095-3 IAW ENDEAVOR AIR EA CRJ953-13822.
- [SDR REXA2022062701365](https://openairdocs.org/sdr/REXA2022062701365.md): Stringer · corroded · Jun 12, 2022 · N678CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STGR 21R IS CORRODED BETWEEN FS 333.00-349.00. REMOVED & REPLACED STRINGER IAW CRJ 900 SRM 51-40-11-001-001-A01 & 51-42-06-001-001-A01.
- [SDR REXA2022062701363](https://openairdocs.org/sdr/REXA2022062701363.md): Stringer · corroded · Jun 12, 2022 · N678CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STRINGER/SH670-31636-1/CORRODED/STRINGER/SH670-31636-1 STRINGER/SH670-31636-1/CORRODED
- [SDR REXA2022062701361](https://openairdocs.org/sdr/REXA2022062701361.md): Splice · corroded · Jun 12, 2022 · N678CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STGR SPLICE (JOINT PIECE) 21R IS CORRODED AT FS 333.00. REMOVED & REPLACED SPLICE IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 & 51-42-21-001-001-A01.
- [SDR REXA2022062701360](https://openairdocs.org/sdr/REXA2022062701360.md): Hinge · worn · Jun 12, 2022 · N678CA · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR HINGE, FUSELAGE SIDE FAILS INSPECTION. AFT 12 LUGS FAIL. REMOVED & REPLACED PAX DOOR FUSELAGE SIDE HINGE IAW CRJ 900 SRM 51-42-21-001-001-A01 & 53-21-23-201-007-A01.
- [SDR REXA2022062701347](https://openairdocs.org/sdr/REXA2022062701347.md): Frame · corroded · Jun 12, 2022 · N678CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > F.S.847+16 FRAME IS CORRODED FROM STGR 26L TO 26R. SPLICE REPAIRED FRAME IAW CRJ 900 SRM 53-00-06-201-001-A03.
- [SDR REXA2022062301331](https://openairdocs.org/sdr/REXA2022062301331.md): Striker · corroded · Jun 12, 2022 · N678CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > LOWER SERVICE DOOR SURROUND HAS MULTIPLE SPOTS OF CORROSION. REMOVED & REPLACED SEAL STRIKER FITTING IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-21-001-001-A01 & 51-42-06-001-001-A01.
- [SDR REXA2022062201324](https://openairdocs.org/sdr/REXA2022062201324.md): Beam · corroded · Jun 12, 2022 · N678CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FRAME STA 1031, LBL9, FLOOR BEAM CORRODED TO FS 1051. SPLICE REPAIRED BEAM IAW CRJ 900 SRM 53-00-41-201-001-A03.
- [SDR REXA2022062201322](https://openairdocs.org/sdr/REXA2022062201322.md): Frame · corroded · Jun 12, 2022 · N678CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FRAME CORRODED @ FS 927 BETWEEN STGR 27 AND STGR 25R. SPLICE REPAIRED FRAME IAW CRJ 900 SRM 53-00-06-201-001-A03
- [SDR REXA2022062701366](https://openairdocs.org/sdr/REXA2022062701366.md): Stringer · corroded · Jun 11, 2022 · N678CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STGR 20R IS CORRODED BETWEEN FS 319.00 - FS349.00 INSTALLED NEW STGR 20R I.A.W. CRJ 900 SRM 51-40-11-001-001-A01, 51-42-21-001-001-A01, & #51-42-06-001-001-A01.

Next page: https://openairdocs.org/aircraft/N678CA/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 = 'N678CA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N678CA/reports

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