# Service difficulty reports: N549CA

A list on [N549CA](https://openairdocs.org/aircraft/N549CA.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 3 · 129 reports

- [SDR REXA2026090801779](https://openairdocs.org/sdr/REXA2026090801779.md): Fitting · damaged · Sep 6, 2026 · N549CA · Cndair CL6002D24 · Wing, Control Surface Attach Fittings
  > FOUND R/H AILERON SIDE BEARING LUGS LABELED H AND I TO BE OVERSIZED. REPAIRED R/H AILERON LUG LABELED H AND I IAW MHIRJ REO 690-57-61-549 REV -- DATED 2026-08-21.
- [SDR REXA2026091401769](https://openairdocs.org/sdr/REXA2026091401769.md): Bearing · failed · Aug 24, 2026 · N549CA · Cndair CL6002D24 · Aileron Control System
  > RUDDER PCU SYSTEMS NR 1 & 2 FAILED BOTH PCU AND BEARING BACKLASH. SYSTEM NR 1 PCU MEASURED 0.330IN WITH A MAX OF 0.250IN & A BEARING BACKLASH OF 0.180IN WITH A MAX OF 0.120IN. SYS NR 2 PCU MEASURED 0.273IN WITH A MAX OF 0.250IN & A BEARING BACKLASH OF 0.135IN
- [SDR REXA2026091001795](https://openairdocs.org/sdr/REXA2026091001795.md): Door · cracked · Aug 24, 2026 · N549CA · Cndair CL6002D24 · Emergency Exits
  > "RH AFT EMERGENCY EXIT UPPER FORMER CRACKED AT AFT LUG. PERFORMED LPI OF RH AFT EMERGENCY EXIT FORMER AT AFT LUG IAW MHIRJ REO 670-52-21-103 REV -- DATED 2024-11-06 STEP 1 FOUND FORMER HAS INDICATION NOTED.750 INCHES LONG FAILED NDT AREA MARKED ON FORMER. COM
- [SDR REXA2026083101766](https://openairdocs.org/sdr/REXA2026083101766.md): Web · corroded · Aug 24, 2026 · N549CA · Cndair CL6002D24 · Fuselage Main, Bulkhead
  > "RH FS 280 WEB IS CORRODED AT RBL 11. REMOVED CORROSION FROM R/H F.S. 280 WEB IAW CRJ 900 SRM 51-21-06-001-001-A01. FOUND TO BE OUT OF LIMITS IAW CRJ 900 SRM 53-11-10-201-003-A01. ORIG..040"", REMOVED.010"" REMAINING.030"", ALLOWABLE.005"". REQUIRES REPLAC
- [SDR REXA2026083101765](https://openairdocs.org/sdr/REXA2026083101765.md): Web · corroded · Aug 24, 2026 · N549CA · Cndair CL6002D24 · Fuselage Main, Bulkhead
  > "LH FS 280 WEB IS CORRODED AT LBL 11. REMOVED CORROSION FROM L/H F.S. 280 WEB IAW CRJ 900 SRM 51-21-06-001-001-A01. FOUND TO BE OUT OF LIMITS IAW CRJ 900 SRM 53-11-10-201-003-A01. ORIG..040"", REMOVED.007"" REMAINING.033"", ALLOWABLE.005"" REQUIRES REPLACE
- [SDR REXA2026082501638](https://openairdocs.org/sdr/REXA2026082501638.md): Angle · cracked · Aug 24, 2026 · N549CA · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FLOOR STRUCTURE ANGLE P/N CC670-34099-1 AT FS280.00, LBL12.0 IS CRACKED. LOCATED AND DRILLED SERVICEABLE LBL 12 AT FS 280 ATTACH ANGLE P/N CC670-34099-1SB IAW CRJ900 SRM 51-40-11-001-001-A01. INSTALLED NEW SERVICEABLE ATTACH ANGLE AT FS 280 LBL 12 P/N CC670-34
- [SDR REXA2026090401774](https://openairdocs.org/sdr/REXA2026090401774.md): Bushing · abnormal · Aug 20, 2026 · N549CA · Cndair CL6002D24 · Wing, Control Surface Attach Fittings
  > RIGHT AILERON CENTER HINGE FITTING BUSHING LUG MARKED C FOUND TO BE O/S UPON BUSHING REMOVAL. REPAIRED RT AILERON SIDE LUG LABELED C IAW STEP F.(1) - F.(4) OF GREO 670-57-61-237 REV --. LPI PERFORMED ON REAMED BORE IAW STEP F.(5) OF GREO 670-57-61-237 REV --.
- [SDR REXA2026092101831](https://openairdocs.org/sdr/REXA2026092101831.md): Floorbeam · corroded · Aug 9, 2026 · N549CA · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > RT BS 280 BEAM HAS CORROSION UNDER UPPER SPLICE STRIP. BLENDED CORROSION ON RT BEAM UNDER UPPER SPLICE STRIP IAW SRM 51-21-06-001-001-A01 & FOUND TO HAVE 100% MATERIAL LOSS. BEAM REQUIRES REPLACEMENT. LOCATED & DRILLED NEW SERVICEABLE RT CROSSBEAM IAW SRM 5
- [SDR REXA2026092101830](https://openairdocs.org/sdr/REXA2026092101830.md): Floorbeam · corroded · Aug 9, 2026 · N549CA · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > LT FS280 BEAM HAS CORROSION ON FWD SIDE UNDER J-ANGLE. BLENDED CORROSION ON LH FS280 BEAM UNDER J-ANGLE & UNDER UPPER SPLICE STRIP IAW SRM 51-21-06-001-001-A01 & FOUND TO HAVE 100% MATERIAL LOSS. LT 280 BEAM REQUIRES REPLACEMEMNT. INSTALLED UPPER SPLICE STRIP
- [SDR REXA2026091401827](https://openairdocs.org/sdr/REXA2026091401827.md): Drag Angle · cracked · Aug 8, 2026 · N549CA · Cndair CL6002D24 · Fuselage, Stabilizer Attach Fittings
  > RH VERTICAL STAB FWD DRAG ANGLE IS CRACKED REPAIRED R/H VERTICAL STAB FWD DRAG ANGLE BY COMPLYING WITH ALL PERMANENT REPAIR STEPS PROVIDED IN CRJ-900 SRM 55-31-00-201-001-A01.
- [SDR REXA2026091401826](https://openairdocs.org/sdr/REXA2026091401826.md): Drag Angle · cracked · Aug 8, 2026 · N549CA · Cndair CL6002D24 · Fuselage, Stabilizer Attach Fittings
  > LH VERTICAL STAB AFT DRAG ANGLE IS CRACKED REMOVED CRACKED DRAG ANGLE AND LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE L/H VERT. STAB AFT DRAG ANGLE P/N AV670-21186-003 IAW CRJ-900 SRM 51-40-11-001-001-A01, AND 51-42-13/21/22-001-001-A01.
- [SDR REXA2026091401825](https://openairdocs.org/sdr/REXA2026091401825.md): Drag Angle · cracked · Aug 8, 2026 · N549CA · Cndair CL6002D24 · Fuselage, Stabilizer Attach Fittings
  > LH VERTICAL STAB FWD DRAG ANGLE IS CRACKED REPAIRED L/H VERTICAL STAB FWD DRAG ANGLE BY COMPLYING WITH ALL PERMANENT REPAIR STEPS PROVIDED IN CRJ-900 SRM 55-31-00-201-001-A01.
- [SDR REXA2026090401773](https://openairdocs.org/sdr/REXA2026090401773.md): Floorbeam · corroded · Aug 8, 2026 · N549CA · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > J-ANGLE AT BS 280 IS CORRODED AROUND FASTENER HOLES. EVAL CORROSION ON FS280 J-ANGLE. UPON FURTHER INVESTIGATION FOUND DAMAGE TO BE 100% MATERIAL LOSS AT CAMLOCK RECEPTACLE. J-ANGLE REQUIRES REPLACEMENT. LOCATED AND DRILLED NEW SERVICEABLE J-ANGLE FROM FS 280
- [SDR REXA2026091101799](https://openairdocs.org/sdr/REXA2026091101799.md): Door · cracked · Aug 4, 2026 · N549CA · Cndair CL6002D24 · Emergency Exits
  > LH AFT EMERGENCY EXIT DOOR UPPER FORMER CRACKED AT AFT LUG. PERFORMED LPI OF LH AFT EMERGENCY EXIT FORMER AT AFT LUG IAW REO 670-52-21-103 REV -, STEP 1 FOUND FORMER HAS INDICATION NOTED 1.2 INCHES LONG FAILED NDT AREA MARKED ON FORMER. COMPLETED STEPS 2, 3 A
- [SDR REXA2026091001794](https://openairdocs.org/sdr/REXA2026091001794.md): Door · cracked · Aug 4, 2026 · N549CA · Cndair CL6002D24 · Emergency Exits
  > "LH FWD EMERGENCY EXIT DOOR UPPER FORMER CRACKED AT AFT LUG. PERFORMED LPI OF LH FWD EMERGENCY EXIT FORMER AT AFT LUG IAW MHIRJ REO 670-52-21-103 REV -- DATED 2024-11-06 STEP 1 FOUND FORMER HAS INDICATION NOTED 1.2 INCHES LONG FAILED NDT AREA MARKED ON FORMER.
- [SDR REXA2026042200297](https://openairdocs.org/sdr/REXA2026042200297.md): Handle · stuck · Apr 9, 2026 · N549CA · Cndair CL6002D24 · Passenger/Crew Doors
  > PASSENGER DOOR INNER HANDLE GETTING STUCK MOVING UP TRYING TO OPEN DOOR. COULD NOT OPEN DOOR FROM INSIDE OR FROM THE OUTSIDE. RAMPERS TRIED. HANDLE WAS STUCK BETWEEN BEING FULLY DOWN AND FULLY UP. FELT LIKE LIKE ANY MORE PRESSURE WOULD BREAK OFF HANDLE, IN EI
- [SDR SWIA2025111700014](https://openairdocs.org/sdr/SWIA2025111700014.md): Windshield · cracked · Nov 14, 2025 · N549CA · Cndair CL6002D24 · Flight Compartment Windows
  > FRONT LEFT WINDSHIELD CRACKED AND STARTED SMOKING. (FLIGHT 3922) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 31192916 WITH THE FOLLOWING CORRECTIVE ACTION: REMOVED AND REPLACED FRONT LEFT WINDSHIELD IN REF TO AMM 56-11-01.
- [SDR SWIA2025010301](https://openairdocs.org/sdr/SWIA2025010301.md): Bracket · out of adjust · Jan 1, 2025 · N549CA · Cndair CL6002D24 · Main Landing Gear
  > GEAR DISAGREE WARNING MESSAGE AFTER TAKEOFF. THE GEAR INDICATION SHOWED THE LEFT MAIN GEAR WAS NOT UP. RAN THE QRH AND THE MESSAGE CLEARED AND ALL THREE GEAR SHOWED DOWN AND GREEN. MLG FAULT AND MDC STATUS MESSAGES REMAIN ON AT THE GATE (FLIGHT 4066 - FILED
- [SDR SWIA202501020001](https://openairdocs.org/sdr/SWIA202501020001.md): Landing Gear · warning message · Jan 1, 2025 · N549CA · Cndair CL6002D24 · Landing Gear Retraction/Extension System
  > GEAR DISAGREE WARNING MESSAGE AFTER TAKEOFF. THE GEAR INDICATION SHOWED THE LEFT MAIN GEAR WAS NOT UP. RAN THE QRH AND THE MESSAGE CLEARED AND ALL THREE GEAR SHOWED DOWN AND GREEN. MLG FAULT AND MDC STATUS MESSAGES REMAIN ON AT THE GATE (FLIGHT 4066 - FILED
- [SDR SWIA20230326](https://openairdocs.org/sdr/SWIA20230326.md): Unknown · smoke · Mar 26, 2023 · N549CA · Cndair CL6002D24 · Air Conditioning System
  > FA REPORTS ON TAKEOFF AIRCRAFT HAS A SMOKE SMELL, FOLLOWED BY VERY LIGHT GREY SMOKE SETTLING AT FLOOR LEVEL IN FIRST CLASS, FOLLOWED BY A SOLVENT SMELL THAT REMAINED FOR THE DURATION OF THE 20 MINUTE FLIGHT. (FLIGHT 4504 - FILED OPEN) PLEASE REFERENCE AM
- [SDR SWIA2023030013](https://openairdocs.org/sdr/SWIA2023030013.md): Unknown · smoke · Mar 13, 2023 · N549CA · Cndair CL6002D24 · Buffet/Galleys
  > AFTER DEPARTURE F/A'S NOTIFIED CREW OF THIN GRAY SMOKE THROUGHOUT THE CABIN AND AN ODOR MORE PRONOUNCED IN THE FRONT OF THE CABIN. (FLIGHT 3583 FILED CLOSED)PRIOR TO TROUBLESHOOTING, COULD NOT IDENTIFY THE SOURCE AND TYPE OF SMELL. TROUBLESHOT PER FIM 21-22-00
- [SDR SWIA202265530](https://openairdocs.org/sdr/SWIA202265530.md): None · corroded · Mar 14, 2022 · N549CA · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > RH LATCH-PIN INTERCOSTAL BETWEEN FS349.00 AND FS364.00 HAS CORROSION AROUND SEVERAL FASTENER HOLES (C-CHECK RO 4/25/2022) REMOVED AND INSTALLED RH LATCH-PIN INTERCOSTAL FROM FS349.00 TO FS364.00 REF DWG SH670-32050 REV. J, CRJ 900 SRM 51-42-06-001-001-A
- [SDR SWIA202265529](https://openairdocs.org/sdr/SWIA202265529.md): None · corroded · Mar 14, 2022 · N549CA · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > LH LATCH-PIN INTERCOSTAL BETWEEN FS349.00 AND FS364.00 HAS CORROSION AROUND SEVERAL FASTENER HOLES (C-CHECK RO 4/25/2022) REMOVED AND INSTALLED LH LATCH-PIN INTERCOSTAL FROM FS349.00 TO FS364.00 REF DWG SH670-32050 REV. J, CRJ 900 SRM 51-42-06-001-001-A
- [SDR SWIA202265528](https://openairdocs.org/sdr/SWIA202265528.md): None · elongated · Mar 9, 2022 · N549CA · Cndair CL6002D24 · Fuselage Main, Keel
  > STRINGER SPLICE AT FS333, STGR 22L HAS ELONGATED HOLES. (C-CHECK RO 4/25/2022) REMOVED AND INSTALLED NEW STRINGER SPLICE AT FS333, STGR 22L. REF CRJ900 SRM 51-42-06-001-001-A01, CRJ900 SRM 51-42-21-001-001-A01 AND DWG: SH670-32420 REV E. COMPLIED WITH T
- [SDR SWIA202265527](https://openairdocs.org/sdr/SWIA202265527.md): None · elongated · Mar 9, 2022 · N549CA · Cndair CL6002D24 · Fuselage Main, Keel
  > STRINGER CLEAT AT FS295, STGR 23L HAS ELONGATED HOLES. (C-CHECK RO 4/25/2022) REMOVED AND REPLACED STRINGER CLEAT AT FS295, STGR 23L. REF. CRJ900 SRM 51-42-06-001-001-A01 AND DWG # SH670-31630 REV. K. / COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY (
- [SDR SWIA202265526](https://openairdocs.org/sdr/SWIA202265526.md): None · cracked · Mar 8, 2022 · N549CA · Cndair CL6002D24 · Wing, Fuselage Attach Fittings
  > RH SLAT TRACK 1-3 CANNISTER SUPPORT FITTING INSIDE WING FUEL PANEL 651AB POSSIBLE CRACK (MARKED) (C-CHECK RO 4/25/2022) REMOVED BRACKET (CC670-12942-2) INSIDE WING FUEL PANEL 651AB REF REO 670-57-42--577, REV --, DATED 2016-12-02 AND INSTALLED ALL REPAI
- [SDR SWIA202265525](https://openairdocs.org/sdr/SWIA202265525.md): None · corroded · Mar 3, 2022 · N549CA · Cndair CL6002D24 · Fuselage Structure (General)
  > MAIN AVIONICS BAY STR 22L CORRODED BETWEEN FS319.70 AND FS333.00 (C-CHECK RO 4/25/2022) REMOVED AND INSTALLED NEW STGR 22L BETWEEN FS280.00 TO FS333.00 REF. CRJ900 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 AND DWG # SH670-31630 REV. K. COMPLIED
- [SDR SWIA202265524](https://openairdocs.org/sdr/SWIA202265524.md): None · corroded · Mar 3, 2022 · N549CA · Cndair CL6002D24 · Fuselage Structure (General)
  > MAIN AVIONICS BAY STR 23L CORRODED BETWEEN FS319.70 AND FS333.00 (C-CHECK RO 4/25/2022) REMOVED AND INSTALLED NEW STGR 23L BETWEEN FS280.00 TO FS333.00 REF. CRJ900 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 AND DWG # SH670-31630 REV. K. COMPLIED
- [SDR SWIA202265523](https://openairdocs.org/sdr/SWIA202265523.md): None · corroded · Mar 3, 2022 · N549CA · Cndair CL6002D24 · Fuselage Structure (General)
  > MAIN AVIONICS BAY STR 24L CORRODED BETWEEN FS319.70 AND FS333.00 (C-CHECK RO 4/25/2022) REMOVED AND INSTALLED NEW STR 24L BETWEEN FS280.00 TO FS333.00 IAW CRJ900 SRM 51-42-06-001-001-A01, CRJ900 SRM 51-42-21-001-001-A01 AND DWG:SH670-31630 REV K. COMPLI
- [SDR SWIA202265522](https://openairdocs.org/sdr/SWIA202265522.md): None · corroded · Mar 3, 2022 · N549CA · Cndair CL6002D24 · Fuselage Structure (General)
  > MAIN AVIONICS BAY STR 25L CORRODED BETWEEN FS295.00 AND FS319.70 (C-CHECK RO 4/25/2022) REMOVED AND INSTALLED NEW STR 25L BETWEEN FS280.00 TO FS333.00 REF CRJ900 SRM 51-42-06-001-001-A01, CRJ900 SRM 51-42-21-001-001-A01 AND DWG: SH670-31630 REV K. COMPL
- [SDR SWIA202265521](https://openairdocs.org/sdr/SWIA202265521.md): None · corroded · Mar 3, 2022 · N549CA · Cndair CL6002D24 · Fuselage Structure (General)
  > MAIN AVIONICS BAY STR 23R SPLICE AT FS333.00 CORRODED (C-CHECK RO 4/25/2022) REMOVED AND INSTALLED NEW STR 23R SPLICE AT FS333.00 REF CRJ900 SRM 51-42-06-001-001-A01 AND DWG:SH670-32420 REV E. COMPLIED WITH TASK CARD 51-900-1002-SKY. LEAK CHECK GOOD. SE
- [SDR SWIA202265520](https://openairdocs.org/sdr/SWIA202265520.md): None · damaged · Mar 1, 2022 · N549CA · Cndair CL6002D24 · Fuselage Floor Panel
  > UPON REMOVAL OF PREVIOUSLY REPAIRED LOCATION ON COCKPIT FLOOR BEAM LOCATED AT FS274 RBL 12.0 FOUND DAMAGE ON COCKPIT FLOOR SKIN. (C-CHECK RO 4/25/2022) REPAIRED COCKPIT FLOORBEAM LOCATED AT FS274 RBL 12.0 REF REO 690-53-11-1407 REV.-- DATED 2022-03-11 A
- [SDR SWIA202265519](https://openairdocs.org/sdr/SWIA202265519.md): None · gouged · Feb 28, 2022 · N549CA · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > INTERCOSTAL IS GOUGED BELOW FWD BAGGAGE BAY TIE DOWN FITTING AT FS517.00/STGR 26L-27 (C-CHECK RO 4/25/2022) REMOVED AND REPLACED INTERCOSTAL FS 517 STGR 26L-27 REF. DWG SH690-33600 REV. AG, CRJ 900 SRM 51-42-21-001-001-A01, CRJ 900 SRM 51-42-06-001-001-
- [SDR SWIA202265518](https://openairdocs.org/sdr/SWIA202265518.md): None · corroded · Feb 27, 2022 · N549CA · Cndair CL6002D24 · Cabin Equipment/Furnishings
  > FWD CARGO TIE DOWN FITTING @ FS629.00, STGR 26L-27 (PN SH670-33389-1) REQUIRES REPLACEMENT DUE TO CORROSION. (C-CHECK RO 4/25/2022) REMOVED AND INSTALLED NEW TIE DOWN FITTING P/N SH670-33389-1 AT FS629. REF: DWG SH690-33600, REV: AG, CRJ900 SRM 51-42-21
- [SDR SWIA202265517](https://openairdocs.org/sdr/SWIA202265517.md): None · corroded · Feb 27, 2022 · N549CA · Cndair CL6002D24 · Cabin Equipment/Furnishings
  > FWD CARGO TIE DOWN FITTING @ FS517.00, STGR 26L-27 (PN SH670-33389-1) REQUIRES REPLACEMENT DUE TO CORROSION. (C-CHECK RO 4/25/2022) REMOVED AND REPLACED CARGO TIE DOWN FITTING FS 517 STGR 26L-27 REF. DWG SH690-33600 REV. AG, CRJ 900 SRM 51-42-21-001-001
- [SDR SWIA202265516](https://openairdocs.org/sdr/SWIA202265516.md): None · corroded · Feb 24, 2022 · N549CA · Cndair CL6002D24 · Fuselage Structure (General)
  > MAIN AVIONICS BAY STR 23L CORRODED BETWEEN FS349.00 AND FS364.00 (C-CHECK RO 4/25/2022) REMOVED AND INSTALLED STR 23L FROM FS333.00 TO FS357.00 AND STR 23L SPLICE REPAIR AT FS357.00 REF DWG SH690-31350 REV-M, CRJ900 SRM 51-42-06-001-001-A01 AND CRJ900 S
- [SDR SWIA202265515](https://openairdocs.org/sdr/SWIA202265515.md): None · corroded · Feb 24, 2022 · N549CA · Cndair CL6002D24 · Fuselage Structure (General)
  > MAIN AVIONICS BAY STR 22R CLEAT AT FS319.70 CORRODED (C-CHECK RO 4/25/2022) REMOVED AND INSTALLED NEW STR 22R CLEAT AT FS319.70 REF CRJ900 SRM 51-42-06-001-001-A01 AND DWG SH670-31950 REV-Y. COMPLIED WITH TASK CARD 51-900-1002-SKY. SEE CONTINUE CARD FOR
- [SDR SWIA202265514](https://openairdocs.org/sdr/SWIA202265514.md): None · corroded · Feb 24, 2022 · N549CA · Cndair CL6002D24 · Fuselage Structure (General)
  > MAIN AVIONICS BAY STR 21R SPLICE AT FS333.00 CORRODED (C-CHECK RO 4/25/2022) REMOVED AND INSTALLED NEW STGR 21R SPLICE AT FS333.00 REF CRJ900 SRM 51-42-06-001-001-A01, CRJ900 SRM 51-42-21-001-001-A01 AND DWG: SH690-30006 REV-C. COMPLIED WITH TASK CARD 5
- [SDR SWIA202265513](https://openairdocs.org/sdr/SWIA202265513.md): None · corroded · Feb 24, 2022 · N549CA · Cndair CL6002D24 · Fuselage Structure (General)
  > MAIN AVIONICS BAY STR 22R SPLICE AT FS333.00 CORRODED (C-CHECK RO 4/25/2022) REMOVED AND INSTALLED NEW STR 22R SPLICE AT FS333.00 REF CRJ900 SRM 51-42-06-001-001-A01 AND DWG: SH690-30006 REV-C. COMPLIED WITH TASK CARD 51-900-1002-SKY. LEAK CHECK GOOD. S
- [SDR SWIA202265512](https://openairdocs.org/sdr/SWIA202265512.md): None · corroded · Feb 24, 2022 · N549CA · Cndair CL6002D24 · Fuselage Structure (General)
  > MAIN AVIONICS BAY STR 21R CORRODED BETWEEN FS295.00 AND FS310.00 (C-CHECK RO 4/25/2022) REPLACED MAIN AVIONICS BAY STR 21R BETWEEN FS280.00 TO FS333.00 REF CRJ900 SRM 51-42-06-001-001-A01, CRJ900 SRM 51-42-21-001-001-A01, ALL STEPS 1-4 OF REO 690-53-21-
- [SDR SWIA202265511](https://openairdocs.org/sdr/SWIA202265511.md): None · corroded · Feb 24, 2022 · N549CA · Cndair CL6002D24 · Fuselage Structure (General)
  > MAIN AVIONICS BAY STR 22R CORRODED BETWEEN FS319.70 AND FS333.00 (C-CHECK RO 4/25/2022) REMOVED AND INSTALLED NEW STRINGER 22RH FROM FS280.00 TO FS333.00 REF CRJ900 SRM 51-42-06-001-001-A01, CRJ900 SRM 51-42-21-001-001-A01, AND DWG SH670-31630 REV K. CO
- [SDR SWIA202265510](https://openairdocs.org/sdr/SWIA202265510.md): None · corroded · Feb 24, 2022 · N549CA · Cndair CL6002D24 · Fuselage Structure (General)
  > MAIN AVIONICS BAY STR 23R CORRODED BETWEEN FS295.00 AND FS310.00 (C-CHECK RO 4/25/2022) REMOVED AND INSTALLED NEW STR 23R BETWEEN FS280.00 TO FS333.00 REF CRJ900 SRM 51-42-06-001-001-A01, CRJ900 SRM 51-42-21-001-001-A01 AND DWG: SH670-31630 REV-K. COMPL
- [SDR SWIA202265509](https://openairdocs.org/sdr/SWIA202265509.md): None · corroded · Feb 24, 2022 · N549CA · Cndair CL6002D24 · Fuselage Structure (General)
  > MAIN AVIONICS BAY STR 24R CORRODED BETWEEN FS295.00 AND FS310.00 (C-CHECK RO 4/25/2022) REMOVED AND INSTALLED NEW STR 24R BETWEEN FS280.00 TO FS333.00 REF CRJ900 SRM 51-42-06-001-001-A01, CRJ900 SRM 51-42-21-001-001-A01 AND DWG: SH670-31630 REV-K. ALL S
- [SDR SWIA202265508](https://openairdocs.org/sdr/SWIA202265508.md): None · cracked · Feb 24, 2022 · N549CA · Cndair CL6002D24 · Fuselage Main, Frame
  > UPON REMOVAL OF DAMAGED RH BEAM AT FS 280 AND APPROX. RBL 26.00 ANGLE P/N CC670-34117-6 IS CRACKED. (C-CHECK RO 4/25/2022) REMOVED AND REPLACED ANGLE AT FS 280 LOWER WEB, RBL 26. REF: CRJ-900 SRM 51-42-06-001-001-A01 AND DWG. CC670-34010 REV K. SEE CON
- [SDR SWIA202265507](https://openairdocs.org/sdr/SWIA202265507.md): None · corroded · Feb 21, 2022 · N549CA · Cndair CL6002D24 · Fuselage Main, Frame
  > FOUND CORROSION ON FRAME STUB P/N: SH670-33260-3 AT FWD BAGGAGE BAY FS501.00. (C-CHECK RO 4/25/2022) REMOVED FRAME P/N: SH670-33260-3 FROM STRG 25L TO STRG 26L, FS 501.00 REF. CRJ900 SRM 51-42-06-001-001-A01 AND CRJ900 SRM 51-42-21-001-001-A01 AND INS
- [SDR SWIA202265506](https://openairdocs.org/sdr/SWIA202265506.md): None · corroded · Feb 21, 2022 · N549CA · Cndair CL6002D24 · Fuselage Main, Frame
  > IN MAIN CABIN, AT FS549, UNDERR STR17L, BELOW L/H SILL, FRAME HAS AREAS OF CORROSION. (MARKED) (C-CHECK RO 4/25/2022) REPAIRED FRAME AT FS549 STGR 18L-16L REF REO 690-53-31-628 REV.-- DATED 2022-03-01, CRJ900 SRM 51-42-21-001-001-A01 AND CRJ900 SRM 51-
- [SDR SWIA202265505](https://openairdocs.org/sdr/SWIA202265505.md): None · corroded · Feb 21, 2022 · N549CA · Cndair CL6002D24 · Fuselage Main, Frame
  > IN MAIN CABIN, AT FS533, UNDER STR17L, BELOW L/H SILL, FRAME HAS AREAS OF CORROSION. (MARKED) (C-CHECK RO 4/25/2022) REPLACED FRAME SECTOR, FRAME SPLICE ANGLE, STRINGER CLEAT REF REO 690-53-31-628 REV.-- DATED 2022-03-01 AND DWG SH690-33100 REV. N, CRJ
- [SDR SWIA202265504](https://openairdocs.org/sdr/SWIA202265504.md): None · corroded · Feb 20, 2022 · N549CA · Cndair CL6002D24 · Fuselage Internal Mounting Structure
  > * FLOOR BEAM LBL 18 BETWEEN FS 1015.00- FS 1051.00 HAS AREAS OF CORROSION (C-CHECK RO 4/25/2022) REPAIRED FLOOR BEAM LBL 18 BETWEEN FS1005.5 TO FS1037.5 REF CRJ900 SRM 53-00-41-201-001-A03. COMPLIED WITH 51-900-1002-SKY.
- [SDR SWIA202265503](https://openairdocs.org/sdr/SWIA202265503.md): None · corroded · Feb 20, 2022 · N549CA · Cndair CL6002D24 · Fuselage Internal Mounting Structure
  > * FLOOR BEAM LBL 9 BETWEEN FS 1015.00- FS 1051.00 HAS AREAS OF CORROSION (C-CHECK RO 4/25/2022) REMOVED CORROSION ON LBL9 FLOOR BEAM UPPER SURFACE FS1005-FS1025.5 AND FS1037.5-FS1057 REF. CRJ900 SRM 51-21-06-001-001-A01. REQUESTED ENGINEERING, RECEIVED
- [SDR SWIA202265502](https://openairdocs.org/sdr/SWIA202265502.md): None · out of tolerance · Feb 19, 2022 · N549CA · Cndair CL6002D24 · Fuselage Main, Frame
  > REPLACE FS280 RH BEAM DUE TO FOUND OUT OF LIMITS ON CAMP#24366017. (C-CHECK RO 4/25/2022) REPLACED RH FS280 BEAM REF CRJ900 SRM 51-42-06-001-001-A01, CRJ900 SRM 51-42-10-001-001-A01, CRJ900 SRM 53-11-10-201-004-A01 AND DWG CC670-34010 REV. K. COMPLIED W

Next page: https://openairdocs.org/aircraft/N549CA/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 = 'N549CA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N549CA/reports

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