# Service difficulty reports: N292PQ

A list on [N292PQ](https://openairdocs.org/aircraft/N292PQ.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 2 · 88 reports

- [SDR REXA2025121201037](https://openairdocs.org/sdr/REXA2025121201037.md): Angle · cracked · Oct 31, 2025 · N292PQ · Cndair CL6002D24 · Fuselage, Stabilizer Attach Fittings
  > CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD & AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD & AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATU
- [SDR REXA2025121201036](https://openairdocs.org/sdr/REXA2025121201036.md): Angle · cracked · Oct 31, 2025 · N292PQ · Cndair CL6002D24 · Fuselage, Stabilizer Attach Fittings
  > CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD & AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD & AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DA
- [SDR REXA2025121201034](https://openairdocs.org/sdr/REXA2025121201034.md): Support · cracked · Oct 31, 2025 · N292PQ · Cndair CL6002D24 · Aerodynamic Fairings
  > CRACK ON WING TO FUSELAGE AFT FAIRING SUPPORT STRUCTURE AT FS849, LBL17'' WING TO FUSELAGE AFT FAIRING SUPPORT STRUCTURE AT FS849, LBL17'' WAS REPAIRED PER EA CRJ953-20784 REV IR.
- [SDR REXA2025121201033](https://openairdocs.org/sdr/REXA2025121201033.md): Channel · corroded · Oct 31, 2025 · N292PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION AT LT / RT P-SEAL GANG CHANNELS AND ATTACHED RETAINERS WS10-WS14.T (NUT CHANNEL, 2 EAS, BOTH SIDES LH/RH) LH P-SEAL GANG CHANNELS AND ATTACHED RETAINER WS10-WS14.T (NUT CHANNEL,1EA, SIDE LH) WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND RH P-S
- [SDR REXA2025121201031](https://openairdocs.org/sdr/REXA2025121201031.md): Rib · cracked · Oct 31, 2025 · N292PQ · Cndair CL6002D24 · Wing, Rib/Bulkhead
  > CRACK ON MACHINED RIB LEADING EDGE SS57.16 AT LEFT WING. MACHINED RIB LEADING EDGE SS57.16 AT LEFT WING WAS REPAIRED PER REO 690-57-41-240 REV - -
- [SDR REXA2025121201030](https://openairdocs.org/sdr/REXA2025121201030.md): Support · cracked · Oct 31, 2025 · N292PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK ON RH FWD CORNER TO SUPPORT OF THE JB6 AT FWD EQUIPMENT COMPARTMENT. RH FWD CORNER TO SUPPORT OF THE JB6 AT FWD EQUIPMENT COMPARTMENT WAS REPLACED PER CRJ 900 SRM 51-42-06-001-001-A01
- [SDR REXA2025121201029](https://openairdocs.org/sdr/REXA2025121201029.md): Floorbeam · cracked · Oct 31, 2025 · N292PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > CRACK ON UNION ANGLES OF CROSS BEAM AND LONGITUDINAL BEAM BTW FS 280.00 AND RBL 12 AND LBL 12 AT PASSENGER FLOOR STRUCTURE UNION ANGLES OF CROSS BEAM AND LONGITUDINAL BEAM BTW FS 280.00 AND RBL 12 AND LBL 12 AT PASSENGER FLOOR STRUCTURE WERE REPLACED PER CRJ-9
- [SDR REXA2025121201028](https://openairdocs.org/sdr/REXA2025121201028.md): Stringer · corroded · Oct 31, 2025 · N292PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STGR 20RH BTW FS349.00 TO FS379.00 AT MAIN AVIONICS COMPARTMENT STGR 20RH BTW FS349.00 TO FS379.00 AT MAIN AVIONICS COMPARTMENT WAS REPAIRED PER EA CRJ953-20756 REV. IR
- [SDR REXA2025121201027](https://openairdocs.org/sdr/REXA2025121201027.md): Rib · cracked · Oct 31, 2025 · N292PQ · Cndair CL6002D24 · Wing, Rib/Bulkhead
  > CRACK ON MACHINED RIB LEADING EDGE SS57.16 AT RIGHT WING MACHINED RIB LEADING EDGE SS57.16 AT RIGHT WING WAS REPLACED PER CRJ 900 SRM 51-42-21-001-001-A01 AND SRM 51-42-10-001-001-A01
- [SDR REXA2025121201024](https://openairdocs.org/sdr/REXA2025121201024.md): Bulkhead Web · corroded · Oct 31, 2025 · N292PQ · Cndair CL6002D24 · Fuselage Main, Bulkhead
  > CORROSION ON LOWER WEB OF AFT FACE OF THE BULKHEAD ASSY ON FS 280.00 RH SIDE LOWER WEB OF AFT FACE OF THE BULKHEAD ASSY ON FS 280.00 RH SIDE WAS EVALAUTED PER CRJ900 SRM 53-00-00-101-001-A01 AND IT WAS REPAIRED PER CRJ900 SRM 53-11-10-201-004-A01
- [SDR REXA2025121201022](https://openairdocs.org/sdr/REXA2025121201022.md): Stringer Splice · corroded · Oct 31, 2025 · N292PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > CORROSION ON INTERNAL FUSELAGE STRUCTURE OVER STGR23L SPLICE BTW FS469.00 / FS485.00 AT FWD BAGGAGE COMPARTMENT INTERNAL FUSELAGE STRUCTURE OVER STGR23L SPLICE BTW FS469.00 / FS485.00 AT FWD BAGGAGE COMPARTMENTWAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 A
- [SDR REXA2025121201021](https://openairdocs.org/sdr/REXA2025121201021.md): Floorbeam · corroded · Oct 31, 2025 · N292PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > CORROSION ON LH BEAM OVER FS 280.00 AT PASSENGER FLOOR STRUCTURE LH BEAM OVER FS 280.00 AT PASSENGER FLOOR STRUCTURE WAS REPLACED PER CRJ900 SRM 51-42-21-001-001-A01 AND CRJ900 SRM 51-42-06-001-001-A01
- [SDR REXA2025121201020](https://openairdocs.org/sdr/REXA2025121201020.md): Bulkhead Web · corroded · Oct 31, 2025 · N292PQ · Cndair CL6002D24 · Fuselage Main, Bulkhead
  > CORROSION ON LOWER WEB OF AFT FACE OF THE BULKHEAD ASSY ON FS 280.00 LH SIDE LOWER WEB OF AFT FACE OF THE BULKHEAD ASSY ON FS 280.00 WAS REPAIRED PER CRJ900 SRM 53-11-10-201-004-A01
- [SDR REXA2025121201018](https://openairdocs.org/sdr/REXA2025121201018.md): Floorbeam · corroded · Oct 31, 2025 · N292PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > SECONDARY NRC: AFTER ANGLE FLOOR SUPPORT REMOVAL, CORROSION WAS FOUND ON RH BEAM OVER FS 280.00 AT PASSENGER FLOOR STRUCTURE, IN REF. TO NRC 00259. AFTER ANGLE FLOOR SUPPORT REMOVAL, CORROSION WAS FOUND ON RH BEAM OVER FS 280.00 AT PASSENGER FLOOR STRUCTURE,
- [SDR REXA2025121201004](https://openairdocs.org/sdr/REXA2025121201004.md): Lug · worn · Oct 29, 2025 · N292PQ · Cndair CL6002D24 · Ailerons
  > CORROSION AND WEAR WAS FOUND ON BORE LUG L1, L2, L5 AND L6 AND WEAR WAS FOUND ON EDGE OF LUG L5 AT CENTER FITTING OF LH AILERON L1, L2, L5 AND L6 AT CENTER FITTING OF LH AILERON WERE REPAIRED PER REO 670-57-61-237 REV - -
- [SDR REXA2025121201017](https://openairdocs.org/sdr/REXA2025121201017.md): Frame · corroded · Oct 28, 2025 · N292PQ · Cndair CL6002D24 · Fuselage Main, Frame
  > CORROSION ON FRAME FS 1051.30 AND STRINGERS 23RH-24RH OF FUSELAGE STRUCTURE AT AFT CARGO COMPARMENT. CORROSION ON FRAME FS 1051.30 AND STRINGERS 23RH-24RH OF FUSELAGE STRUCTURE AT AFT CARGO COMPARMENT. WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01, EVALUAT
- [SDR REXA2025121201025](https://openairdocs.org/sdr/REXA2025121201025.md): Doubler · corroded · Oct 27, 2025 · N292PQ · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > CORROSION ON FUSELAGE INTERNAL STRUCTURE ANTENNA DOUBLER BTW FS295.00 / FS310.00 AND STGR 26L / STGR26R AT MAIN AVIONICS COMPARTMENT. CORROSION ON FUSELAGE INTERNAL STRUCTURE ANTENNA DOUBLER BTW FS 295.00 / 310.00 AND STGR26L / STGR 26R AT MAIN AVIONICS COMPA
- [SDR REXA2025121201023](https://openairdocs.org/sdr/REXA2025121201023.md): Seat Track · corroded · Oct 27, 2025 · N292PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION AND SCRATCHES ON FLOOR SEAT RAIL 9RBL (8 E/AS) AND ON FLOOR SEAT RAIL 9LBL (4 E/AS) ALSO ON FLOOR SEAT RAIL 27LBL BTW FS 969 TO FS 985 AT FLOOR STRUCTURE OF PASSENGER CABIN FLOOR SEAT RAIL 9RBL (5 E/AS ON FS 379 TO 485, FS 485 TO 581, FS 708 TO 7
- [SDR REXA2025121201016](https://openairdocs.org/sdr/REXA2025121201016.md): Rib · cracked · Oct 27, 2025 · N292PQ · Cndair CL6002D24 · Wing, Rib/Bulkhead
  > CRACK ON MACHINED RIB OF LEADING EDGE SS27.16 AT RIGHT WING. CRACK ON MACHINED RIB OF LEADING EDGE SS27.16 AT RIGHT WING WAS REPAIRED PER REO 690-57-41-569 REV - -
- [SDR REXA2025121201006](https://openairdocs.org/sdr/REXA2025121201006.md): Seat Track · corroded · Oct 25, 2025 · N292PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > INITIAL INSPECTION: SEVERAL CORROSION POINTS ON RH SIDE SEAT RAIL BTW FS785.15 AND FS847. SEVERAL CORROSION POINTS ON RH SIDE SEAT RAIL BTW FS785.15 AND FS847 WAS EVALUATED DUE TO EXCESSIVE DAMAGE THEREFORE WAS REPLACED PER CRJ-900 SRM 53-41-49-101-001-A02 AN
- [SDR REXA2025121201005](https://openairdocs.org/sdr/REXA2025121201005.md): Seat Track · corroded · Oct 25, 2025 · N292PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > INITIAL INSPECTION: SEVERAL CORROSION POINTS ON LH SIDE SEAT RAILS BTW FS785.15 AND FS847. SEVERAL CORROSION POINTS ON LH SIDE SEAT RAILS BTW FS785.15 AND FS847 WERE FOUND DUE TO EXCESIVE DAMAGE THEREFORE WERE REPLACED PER CRJ-900 SRM 53-41-49-101-001-A02 AND
- [SDR REXA2025121201032](https://openairdocs.org/sdr/REXA2025121201032.md): Striker · corroded · Oct 23, 2025 · N292PQ · Cndair CL6002D24 · Fuselage Main, Structure
  > CORROSION ON LOWER SILL OF GALLEY SERVICE DOOR (LOWER SURROUND STRUCTURE AREA) LOWER SILL OF GALLEY SERVICE DOOR (LOWER SURROUND STRUCTURE AREA) WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01
- [SDR REXA2025121201014](https://openairdocs.org/sdr/REXA2025121201014.md): Channel · corroded · Oct 23, 2025 · N292PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON CHANEL (5 EA) OF SETTLEMENT AREA OF ACCESS PANEL 561AT CORROSION ON CHANEL (4 EAS) OF SETTLEMENT AREA OF ACCESS PANEL 561AT WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 51-21-06-001-001-A01 AND WERE REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND C
- [SDR REXA2025121201013](https://openairdocs.org/sdr/REXA2025121201013.md): Angle · cracked · Oct 23, 2025 · N292PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK ON CLIP THAT ATTACHES STGR 7LH TO FS 1051.30 ON AFT BAGGAGE BAY DOOR SURROUND STRUCTURE. CLIP THAT ATTACHES STGR 7LH TO FS 1051.30 ON AFT BAGGAGE BAY DOOR SURROUND STRUCTURE WAS FABRICATED PER DWG MM670-36471 REV.A. AND WAS REPLACED PER CRJ900 SRM 51-42-
- [SDR REXA2025121201012](https://openairdocs.org/sdr/REXA2025121201012.md): Support Angle · corroded · Oct 23, 2025 · N292PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INITIAL INSPECTION': CORROSION AT FS 280.00 FLOOR ACCESS PANEL SUPPORT ANGLE. CORROSION AT FS 280.00 FLOOR ACCESS PANEL SUPPORT ANGLE WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01, EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-00-00-101-001-A01 AND REPLACED PE
- [SDR REXA2025121201011](https://openairdocs.org/sdr/REXA2025121201011.md): Floorbeam · cracked · Oct 23, 2025 · N292PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > CRACKED CENTER COCKPIT FLOOR BEAM RBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT. CRACKED CENTER COCKPIT FLOOR BEAM RBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT. WAS REPAIRED PER REO 690-53-11-2073
- [SDR REXA2025121201010](https://openairdocs.org/sdr/REXA2025121201010.md): Cleat · cracked · Oct 23, 2025 · N292PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK ON INTERCOSTAL CLEAT AT FS 661.00+90 AND STGR 27 WING-TO-FUSELAJE FAIRING STRUCTURE (PT) FPI WAS PERFORMED ON INTERCOSTAL CLEAT, NO CRACKS WERE FOUND PER CRJ700/900/1000 NDT MANUAL PART 01, 51-20-008-230-A01 (EQUIPMENT: THERMOMETER C/N:1774 EXP:16/JAN/26
- [SDR REXA2025121201015](https://openairdocs.org/sdr/REXA2025121201015.md): Diaphragm · cracked · Oct 20, 2025 · N292PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK ON MAIN LANDING GEAR BINS SUPPORT STRUCTURE RETAINER ANGLE LH (FS 797.00 AND LBL & RBL 34) MAIN LANDING GEAR BINS SUPPORT STRUCTURE RETAINER ANGLE LH (FS 797.00 AND LBL & RBL 34) WERE REPLACED PER CRJ-900 SRM 51-41-02-001-001-A01
- [SDR REXA2025121201009](https://openairdocs.org/sdr/REXA2025121201009.md): Web · cracked · Oct 20, 2025 · N292PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK ON ELECTRICAL BAY FLOOR WEB RIGHT SIDE (BELOW ADG SUPPORT DOUBLER) FS193.00. CRACK ON ELECTRICAL BAY FLOOR WEB RIGHT SIDE (BELOW ADG SUPPORT DOUBLER) FS193.00. WAS REPAIRED PER CRJ900 SRM 53-11-43-201-001-A01
- [SDR REXA2025121201008](https://openairdocs.org/sdr/REXA2025121201008.md): Diaphragm · cracked · Oct 20, 2025 · N292PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK ON MAIN LANDING GEAR BINS SUPPORT STRUCTURE RETAINER ANGLE RH (FS 797.00 AND LBL & RBL 34) MAIN LANDING GEAR BINS SUPPORT STRUCTURE RETAINER ANGLE RH (FS 797.00 AND LBL & RBL 34) WERE REPLACED PER CRJ-900 SRM 51-41-02-001-001-A01
- [SDR REXA2025121201007](https://openairdocs.org/sdr/REXA2025121201007.md): Retainer · corroded · Oct 19, 2025 · N292PQ · Cndair CL6002D24 · Service Doors
  > CORROSION ALONG SEAL RETAINER OF MAIN AVIONICS COMPARTMENT DOOR SEAL RETAINERS (3EAS)OF MAIN AVIONICS COMPARTMENT DOOR WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 51-21-06-001-001-A01 AND WERE REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND SEAL RETAINER (1EA
- [SDR REXA2022020700229](https://openairdocs.org/sdr/REXA2022020700229.md): Angle · cracked · Jan 17, 2023 · N292PQ · Cndair CL6002D24 · Cargo/Baggage Doors
  > AFT CARGO DOOR ANGLE CRACKED BY DOOR TRACK ON AFT SIDE REMOVED AND REPLACED AFT CARGO AFT TRACK DOOR ANGLE IAW CRJ900 SRM 51-42-21-001-001-A01
- [SDR REXA2022031800438](https://openairdocs.org/sdr/REXA2022031800438.md): Doubler · damaged · Mar 11, 2022 · N292PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > 2 BURN MARKS ON EXTERNAL DOUBLER FOR WIFI ANTENNA - COMLIED WITH EA CRJ953-13104. FOR DTWI REFER TO NRWC 812959. THIS IS A MAJOR REPAIR - COMPLIED WITH EA CRJ 953-13104. INITIATE DTWI FOR 12 MONTHS
- [SDR REXA2021062800464](https://openairdocs.org/sdr/REXA2021062800464.md): Battery Pack · inoperative · Jun 24, 2021 · N292PQ · Cndair CL6002D24 · Emergency Lighting
  > EMERGENCY EXIT SIGN ON THE CEILING IN THE MIDDLE OF THE CABIN NOT WORKING. EXIT SIGNS NEAR AFT OVERWING EXITS ALSO NOT WORKING - DEFERRED CABIN EMERGENCY LIGHT IAW MEL 33-51-1A. ENTERED IN MM02. PLACARD PER MEL. MOC NOTIFIED 95784. R & R BATTERY PACK #4 AND C
- [SDR REXA2019032300320](https://openairdocs.org/sdr/REXA2019032300320.md): Striker · worn · Mar 23, 2019 · N292PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INITIAL INSPECTION: WEAR AFT SEAL STRIKER ON CUTOUT AT PASSENGER DOOR (FUS) (SM) SUMMARY OF NRC 00244:SEAL STRIKER WAS REPAIRED PER SRM 53-21-23-201-003-A01.
- [SDR REXA2019032300319](https://openairdocs.org/sdr/REXA2019032300319.md): Striker · worn · Mar 23, 2019 · N292PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INITIAL INSPECTION: WEAR FWD SEAL STRIKER ON CUTOUT AT PASSENGER DOOR (FUS) (SM). SUMMARY OF NRC 00243:DOUBLER WAS REPLACED PER SRM 51-42-06-001-001-A01 AND 53-21-23-201-003-A01.
- [SDR REXA2019032200318](https://openairdocs.org/sdr/REXA2019032200318.md): Stringer · corroded · Mar 22, 2019 · N292PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > INITIAL INSPECTION: CORROSION ON STRINGER 24R BETWEEN FS629 TO FS645. AT FORWARD BAGGAGE BAY. (TCI: 53-20-306) (CCD) SUMMARY: OF NRC 00232: DUE CORROSION LEVEL 2 ON STRINGER 24R BETWEEN FS629 TO FS645. AT FORWARD BAGGAGE BAY WAS REPAIRED PER SRM 53-00-03-20
- [SDR REXA2019032200309](https://openairdocs.org/sdr/REXA2019032200309.md): Angle · corroded · Mar 22, 2019 · N292PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INITIAL INSPECTION: CORROSION ON ANGLE BTW FS=265.00 AND STR 26L / 26R AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT (E/E) (SM) SUMMARY: CORROSION LEVEL-2 IN ANGLE BTW FS=265.00 AND STRINGER 26L/26R WAS MEASURED AND WAS FOUND WITH THE FOLLOWING DIMENSIONS
- [SDR REXA2019032200308](https://openairdocs.org/sdr/REXA2019032200308.md): Support · corroded · Mar 22, 2019 · N292PQ · Cndair CL6002D24 · Fuselage Main, Attach Fittings
  > INITIAL INSPECTION: CORROSION ON JACK FITTING SUPPORT BTW FS=280.00 / FS=265.00 AND STR 26L / 26R. (E/E) (SM). SUMMARY: JACK FITTING SUPPORT BTW FS=280.00 / FS=265.00 AND STR 26L / 26R. (E/E) WAS REPLACED PER SRM 51-42-21-001-001-A01 AND SRM 51-42-06-001-001-A
- [SDR REXA2019032200300](https://openairdocs.org/sdr/REXA2019032200300.md): Stringer · corroded · Mar 22, 2019 · N292PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > INITIAL INSPECTION: CORROSION STR 25R BTW FS=333.00 / FS=280.00 AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT (E/E) (SM). IN REFERENCE NRC 00026 TASK 900-53-140-300 APPENDIX A ]. SUMMARY OF NRC 00093 STR 25R BTW FS=333.00 / FS=280.00 AT INTERNAL STRUCTUR
- [SDR REXA2019032200298](https://openairdocs.org/sdr/REXA2019032200298.md): Stringer · corroded · Mar 22, 2019 · N292PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > INITIAL INSPECTION: CORROSION STR 27 BTW FS=333.00 / FS=295.00 AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT (E/E) (SM). IN REFERENCE NRC 00026 TASK 900-53-140-300 APPENDIX A ]. SUMMARY OF NRC 00091 CORROSION LEVEL 2: STR 27 BTW FS=333.00 / FS=295.00 AT
- [SDR REXA2019032100306](https://openairdocs.org/sdr/REXA2019032100306.md): Stringer Splice · corroded · Mar 21, 2019 · N292PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > INITIAL INSPECTION: CORROSION ON STR SPLICE BTW FS=349.00 / FS=319.00 AND STR 26L / STGR 24R AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT (E/E) (SM). IN REFERENCE NRC 00026 TASK 900-53-140-300 APPENDIX A ]. SUMMARY:STR SPLICE BTW FS=349.00 / FS=319.00 S
- [SDR REXA2019032000304](https://openairdocs.org/sdr/REXA2019032000304.md): Stringer · corroded · Mar 20, 2019 · N292PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > INITIAL INSPECTION: CORROSION STR 27 BTW FS=310.00 / FS=280.00 AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT (E/E) (SM). IN REFERENCE NRC 00026 TASK 900-53-140-300 APPENDIX A ]. SUMMARY: IN NRC: 00098, CORROSION LEVEL 2: DUE TO EXCESSIVE CORROSION STRING
- [SDR REXA2019032000303](https://openairdocs.org/sdr/REXA2019032000303.md): Stringer · corroded · Mar 20, 2019 · N292PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > INITIAL INSPECTION: CORROSION STR 25R BTW FS=333.00 / FS=364.00 AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT (E/E) (SM). IN REFERENCE NRC 00026 TASK 900-53-140-300 APPENDIX A ]. SUMMARY: IN NRC 00096, STRINGER 25R STA. FS=333 TO FS=364 WAS REPLACED PER
- [SDR REXA2019031800315](https://openairdocs.org/sdr/REXA2019031800315.md): Seat Track · corroded · Mar 18, 2019 · N292PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > INITIAL INSPECTION: CORROSION ON FLOOR SEAT RAILS IN SECTIONS FS= 661.00+32 TO FS= 581.00, 9 RBL AT PAX CABIN. (CPAX) SUMMARY: OF NRC 00129: DUE CORROSION LEVEL 2 ON FLOOR SEAT RAILS INSECTIONS FS= 661.00+32 TO FS= 581.00 9 RBL AT PAX CABIN WERE REPLACED PER S
- [SDR REXA2019031800313](https://openairdocs.org/sdr/REXA2019031800313.md): Seat Track · corroded · Mar 18, 2019 · N292PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > INITIAL INSPECTION: CORROSION ON FLOOR SEAT RAILS IN SECTIONS FS= 847.00+16 TO FS= 969.00, 9 RBL AT PAX CABIN. (CPAX) SUMMARY OF NRC:00127 CORRISION LEVEL:2 DUE EXCESSIVE CORROSION ON FLOOR SEAT RAILS IN SECTIONS FS= 847.00+16 TO FS= 969.00, 9 RBL AT PAX CABIN
- [SDR REXA2019031800312](https://openairdocs.org/sdr/REXA2019031800312.md): Seat Track · corroded · Mar 18, 2019 · N292PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > INITIAL INSPECTION: CORROSION ON FLOOR SEAT RAILS IN SECTIONS FS= 847.00+16 TO FS= 969.00, 9 LBL AT PAX CABIN. (CPAX) SUMMARY OF NRC 00126, CORROSION LEVEL-2: SEAT RAILS IN SECTIONS FS= 847.00+16 TO FS= 969.00, 9 LBL WAS REPLACED PER SRM 51-41-02-001-001-A01 A
- [SDR REXA2019031800305](https://openairdocs.org/sdr/REXA2019031800305.md): Stringer · corroded · Mar 18, 2019 · N292PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > INITIAL INSPECTION: CORROSION STR 24R BTW FS=333.00 / FS=485.00 AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT (E/E) (SM). IN REFERENCE NRC 00026 TASK 900-53-140-300 APPENDIX A ] SUMMARY: IN NRC:00099, CORROSION DAMAGE WAS FOUND IN SEVERAL POINTS OF THE
- [SDR REXA2019031700302](https://openairdocs.org/sdr/REXA2019031700302.md): Stringer · corroded · Mar 17, 2019 · N292PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > INITIAL INSPECTION: CORROSION STR 26R BTW FS=333.00 / FS=364.00 AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT (E/E) (SM). IN REFERENCE NRC 00026 TASK 900-53-140-300 APPENDIX A ]. SUMMARY: NRC: 00095, STR 26R BTW FS=333.00 / FS=364.00 AT INTERNAL STRUCTU
- [SDR REXA2019031700301](https://openairdocs.org/sdr/REXA2019031700301.md): Stringer · corroded · Mar 17, 2019 · N292PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > INITIAL INSPECTION: CORROSION STR 24R BTW FS=333.00 / FS=280.00 AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT (E/E) (SM). IN REFERENCE NRC 00026 TASK 900-53-140-300 APPENDIX A ]. SUMMARY OF NRC 00094 CORROSION LEVEL 2:STR 24R BTW FS=333.00 / FS=280.00 AT

Next page: https://openairdocs.org/aircraft/N292PQ/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 = 'N292PQ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N292PQ/reports

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