# Service difficulty reports: N298PQ

A list on [N298PQ](https://openairdocs.org/aircraft/N298PQ.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 · 70 reports

- [SDR REXA2024021900201](https://openairdocs.org/sdr/REXA2024021900201.md): Hinge · corroded · Dec 26, 2023 · N298PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR TOP FOLDING STEP HINGE IS CORRODED. REMOVED CORRODED HINGE, LOCATED AND DRILLED NEW HINGE IAW CRJ 900 SRM 51-40-11-001-001-A01. INSTALLED NEW HINGE AS NEEDED IAW CRJ 900 AMM 52-11-04-400-801 STEP (4) (A) (3 & 4). HINGE PN# CC670-31981-3.
- [SDR REXA2024102901141](https://openairdocs.org/sdr/REXA2024102901141.md): Handle · cracked · Dec 18, 2023 · N298PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR INNER HAND LEVER (P/N 600-31887-15) CRACKED. EVAL. PAX DOOR INNER HAND LEVER (P/N 600-31887-15) FOUND TO BE CRACK ORDER REPLACEMENT HANDLE IAW CRJ900 IPC 52-11-02 FIG 5 ITEM 242REMOVED INNER HANDLE ASSEMBLY IAW CRJ-900 AMM 52-11-02-000-809 (CONFIG. A
- [SDR REXA2024021900200](https://openairdocs.org/sdr/REXA2024021900200.md): Bracket · cracked · Dec 18, 2023 · N298PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR AFT GAS SPRING BRACKET CRACKED. REMOVED PAX DOOR AFT GAS SPRING BRACKET P/N 601R318011-1 IAW CRJ-900 SRM 51-42-06-001-001-A01. INSTALLED AFT GAS SPRING BRACKET WITH P/N 601R318011-1 AT PAX DOOR IAW CRJ900 SRM 51-42-06-001-001-A01.
- [SDR REXA2022122601060](https://openairdocs.org/sdr/REXA2022122601060.md): Stringer · corroded · Dec 10, 2023 · N298PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > FOUND CORROSION ON STGR 20R BETWEEN F.S 379-394 REMOVED DAMAGED STR 20R BETWEEN FS 349 TO FS 477 IAW CRJ-900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 LOCATED AND DRILLED NEW STR 20R BETWEEN FS 349 TO FS 477 IAW CRJ900 SRM 51-40-11-001-001-A01 INSTALLE
- [SDR REXA2022122601058](https://openairdocs.org/sdr/REXA2022122601058.md): Angle · corroded · Dec 6, 2023 · N298PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "PASSENGER DOOR SURROUND STRUCTURE, MID CAP ANGLE IS CORRODED. REMOVED PASSENGER DOOR SURROUND STRUCTURE, MID CAP ANGLE P/N SH670-31825-9 IAW CRJ900 SRM 51-41-02-001-001-A01.AND LOCATED, DRILLED, AND INSTALLED PASSENGER DOOR MID CAP ANGLE P/N SH670-31825-9 IA
- [SDR REXA2024031300270](https://openairdocs.org/sdr/REXA2024031300270.md): Floor Support · cracked · Dec 5, 2023 · N298PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "FWD EQUIPMENT COMPARTMENT RH FLOOR CRACKED AT FS 169. PERFORMED REPAIR TYPE 2, ON R/H SIDE OF FWD EQUIPMENT COMPARTMENT IAW CRJ-900 SRM 52-11-43-201-001-A01, STEP 4.A(2)(G -K), DOUBLER PO# 5-5403, 0.040Ï¿½, CLEAT PO# W89584, 0.032Ï¿½. INSTALLED DOUBLER PO# 5
- [SDR REXA2022122601057](https://openairdocs.org/sdr/REXA2022122601057.md): Floor Panel · cracked · Dec 4, 2023 · N298PQ · Cndair CL6002D24 · Fuselage Floor Panel
  > FWD EQUIPMENT COMPARTMENT LH FLOOR CRACKED AT FS 193.00. REPAIRED IAW CRJ900 SRM 53-11-43-201-001-A01.
- [SDR REXA2024102901140](https://openairdocs.org/sdr/REXA2024102901140.md): Drag Angle · cracked · Dec 3, 2023 · N298PQ · Cndair CL6002D24 · Vertical Stabilizer Miscellaneous Structure
  > LH AFT DRAG ANGLE ON VERTICAL STABILIZER IS CRACKED.: REMOVED LH AFT DRAG ANGLE FROM VERTICAL STABILIZER IAW CRJ900 SRM 51-42-21-001-001-A01, 51-42-13-001-001-A01, & 51-42-22-001-001-A01. AND FIT, DRILLED AND TRANSFERED HOLES INTO NEW ANGLE IAW CRJ900 SRM 51-
- [SDR REXA2022122601053](https://openairdocs.org/sdr/REXA2022122601053.md): Angle · cracked · Dec 3, 2023 · N298PQ · Cndair CL6002D24 · Vertical Stabilizer
  > LH FWD DRAG ANGLE ON VERTICAL STABILIZER IS CRACKED. PERFORMED PERMANENT REPAIR OF LH FWD DRAG ANGLE ON VERTICAL STAB IAW CRJ900 SRM TASK 55-31-00-201-001-A01.
- [SDR REXA2020030400292](https://openairdocs.org/sdr/REXA2020030400292.md): Frame · corroded · Mar 2, 2020 · N298PQ · Cndair CL6002D24 · Fuselage Main, Frame
  > "INITIAL INSPECTION: CORROSION ON FRAME FS=310 BTW STGR 25LH / 25RH AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT (SM) (E/E) (TCI:53-20-304). " "SUMMARY: ON NRC. 00266 CORROSION LEVEL 2. F
- [SDR REXA2020030400288](https://openairdocs.org/sdr/REXA2020030400288.md): Access Panel · worn · Mar 2, 2020 · N298PQ · Cndair CL6002D24 · Wing, Plate/Skin
  > "PART RACKS:WEAR ON ACCESS PANEL 521AT, 622DB, 622CB, 584JB,584EB, 584LB, 684GB, 684JB,684EB,584AB AND 584GB. (SM) ""SUMMARY: OF NRC. 00246. WEAR ON ACCCESS PANELS 521AT, 622DB, 622CB, 584JB, 584LB, 684GB, 684JB,584AB AND 584GB WERE
- [SDR REXA2020030400271](https://openairdocs.org/sdr/REXA2020030400271.md): Frame · corroded · Mar 2, 2020 · N298PQ · Cndair CL6002D24 · Fuselage Main, Frame
  > "INITIAL INSPECTION: CORROSION ON FRAME FS=295 BTW STGR 25LH / 25RH AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT (SM) (E/E) (TCI:53-20-304). ""SUMMARY: ON NRC. 00264 CORROSION LEVEL 2. FRA
- [SDR REXA2020030400303](https://openairdocs.org/sdr/REXA2020030400303.md): Floor Panel · delaminated · Mar 1, 2020 · N298PQ · Cndair CL6002D24 · Fuselage Floor Panel
  > "INITIAL INSPECTION: DAMAGE FLOOR PANELS 282FRF, 281CLF, 281GLF AND 281DLF AT AFTER CARGO COMPARTMENT. " "SUMMARY: FLOOR PANEL 281CLF P/N: BA670-31684-7 WAS VERIFIED AND REPLACED PER CRJ 900 IPC 53-00-47 ITEM 55A, FLOOR
- [SDR REXA2020030400302](https://openairdocs.org/sdr/REXA2020030400302.md): Floor Panel · delaminated · Mar 1, 2020 · N298PQ · Cndair CL6002D24 · Fuselage Floor Panel
  > "INITIAL INSPECTION: DELAMINATED FLOOR PANEL 281BLF AT AFTER CARGO COMPARTMENT. " "SUMMARY: FLOOR PANEL 281BLF AT AFT BAGGAGE BAY ARE OUT OF LIMITS WITH DIMENSION 152IN^2 PER CRJ 900 CMM ATA 53 CO
- [SDR REXA2020030400298](https://openairdocs.org/sdr/REXA2020030400298.md): Intercostal · corroded · Mar 1, 2020 · N298PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "INITIAL INSPECTION: CORROSION ON INTERCOSTAL BTW STGR 20RH AND FS=349 / FS=319 AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT (SM) (E/E) (TCI:53-20-305). ""SUMMARY: INTERCOSTAL BTW STGR 20RH AND FS=349
- [SDR REXA2020030400296](https://openairdocs.org/sdr/REXA2020030400296.md): Intercostal · corroded · Feb 29, 2020 · N298PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "INITIAL INSPECTION: CORROSION ON INTERCOSTAL (2EAS) BTW FS=349 / FS=364 AND STGR 26LH / 26RH AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT (SM) (E/E) (TCI:53-20-305). " "SUMMARY: ON NRC. 00275 CORROSION LEVEL 2. I
- [SDR REXA2020030400304](https://openairdocs.org/sdr/REXA2020030400304.md): Rub Strip · torn · Feb 28, 2020 · N298PQ · Cndair CL6002D24 · Vertical Stabilizer, Plate/Skin
  > "PART RACKS: TORN AND LOOSE TEFLON STRIP AT VERTICAL STABILIZER ACCESS PANEL NBR, 326DL, AND 326DR ( SM) " "SUMMARY: NEW STRIPS, RUBBER, UPPER VISOR ACCESS PANEL 326DL AND 326DRWERE INSTALLED PER CRJ/900 SRM 51-42-06-001-
- [SDR REXA2020030400305](https://openairdocs.org/sdr/REXA2020030400305.md): Grill · cracked · Feb 27, 2020 · N298PQ · Cndair CL6002D24 · Cargo Compartments
  > "PART RACKS: CRACKED CHIMNEY GRILLS (3 E/A) AT FWD CARGO COMPARTMENT. " "SUMMARY: OF NRC:00421; CHIMNEY GRILLS (2 E/A´S) WERE VERIFIED AND REPLACED PER CRJ-900 IPC 53-32-31-01 ITEM: 270 P/N: A843021-501 AND ITEM: 300 P/N: A843021-505, AND CRACKED CHIMNEY GRI
- [SDR REXA2020030400301](https://openairdocs.org/sdr/REXA2020030400301.md): Floor Panel · delaminated · Feb 27, 2020 · N298PQ · Cndair CL6002D24 · Fuselage Floor Panel
  > "INITIAL INSPECTION: DELAMINATED FLOOR PANEL 252DRF AT PAX CABIN. " "SUMMARY: FLOOR PANEL 252DRF AT AFT BAGGAGE BAY ARE OUT OF LIMITS WITH DIMENSION 149IN^2 PER CRJ 900 CMM ATA 53 COMCMM-030 REV. T PAR. 8.0 THEREFORE WAS REPLACED PER CRJ900 AMM 53-00-47-400-
- [SDR REXA2020030400289](https://openairdocs.org/sdr/REXA2020030400289.md): Stringer · corroded · Feb 26, 2020 · N298PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > "INITIAL INSPECTION: CORROSION ON STGR 26RH BTW FS=280 / FS=333 AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT (SM) (E/E) (TCI:53-20-304) ""SUMMARY OF NRC:00262 CORROSION LEVEL:2 ON STGR 26RH BTW FS=280 / FS=333, STRG 26 RH BTW FS=280 / FS=333 WAS REPLACE
- [SDR REXA2020030400293](https://openairdocs.org/sdr/REXA2020030400293.md): Frame · corroded · Feb 24, 2020 · N298PQ · Cndair CL6002D24 · Fuselage Main, Frame
  > "INITIAL INSPECTION: CORROSION ON FRAME FS=319 BTW STGR 25LH / 24RH AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT (SM) (E/E) (TCI:53-20-304). " "SUMMARY OF NRC 00267 CORROSION LEVEL 2:FRAM
- [SDR REXA2020030400269](https://openairdocs.org/sdr/REXA2020030400269.md): Cover · dented · Feb 24, 2020 · N298PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > "INITIAL INSPECTION: DENT ON FWD/AFT LOWER CORNERS AT PASSENGER DOOR (PTAS). " "FWD/AFT LOWER CORNERS AT PASSENGER DOOR WERE REPLACED PER CRJ-900 SRM51-42-10-001-001-A01
- [SDR REXA2020030400295](https://openairdocs.org/sdr/REXA2020030400295.md): Frame · corroded · Feb 23, 2020 · N298PQ · Cndair CL6002D24 · Fuselage Main, Frame
  > "INITIAL INSPECTION: CORROSION ON FRAME FS=349 BTW STGR 26LH / 26RH AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT (SM) (E/E) (TCI:53-20-305). " "SUMMARY: FRAME FS=349 BTW STGR 26LH / 26RH
- [SDR REXA2020030400286](https://openairdocs.org/sdr/REXA2020030400286.md): Angle · corroded · Feb 22, 2020 · N298PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "INITIAL INSPECTION: CORROSION ON ANGLE MOUNTING LOWER SURROUND STRUCTURE AT GALLEY SERVICE DOOR. " "SUMMARY: OF NRC:00213 CORROSION LEVEL 2. ON ANGLE MOUNTING LOWER SURROUND STRUCTURE AT GALLEY SERVICE DOOR. ANGLE
- [SDR REXA2020030400291](https://openairdocs.org/sdr/REXA2020030400291.md): Doubler · corroded · Feb 21, 2020 · N298PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "INITIAL INSPECTION: CORROSION ON DOUBLER BTW FS=295 / FS=310 AND STGR 26LH / 26RH AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT (SM) (E/E) (TCI:53-20-304). " "SUMMARY ON NRC 00265: CORROSION LEVEL 2. DO
- [SDR REXA2020030400275](https://openairdocs.org/sdr/REXA2020030400275.md): Striker · nicked · Feb 21, 2020 · N298PQ · Cndair CL6002D24 · Fuselage Main, Structure
  > "INITIAL INSPECTION: NICK ON EDGE TO FS169.00 STRUCTURE NEAR TO WL79.50 AT LH FWD EQUIPMENT (FUS) " "SUMMARY: ON NRC. 00155 SEAL STRIKER WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01.
- [SDR REXA2020030400294](https://openairdocs.org/sdr/REXA2020030400294.md): Stringer · corroded · Feb 20, 2020 · N298PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > "INITIAL INSPECTION: CORROSION ON STGR 27 BTW FS=333 / FS=364 AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT (SM) (E/E) (TCI:53-20-305) " "SUMMARY OF NRC 00273: DUE CORROSION LEVEL 2 ON STGR 27 BTW FS=333 / FS=364 AT INTERNAL STRUCTURE OF MAIN AVIONICS
- [SDR REXA2020030400290](https://openairdocs.org/sdr/REXA2020030400290.md): Stringer · corroded · Feb 20, 2020 · N298PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > "INITIAL INSPECTION: CORROSION ON STGR 27 BTW FS=280 / FS=333 AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT (SM) (E/E) (TCI:53-20-304). " "SUMMARY OF NRC 00263: DUE CORROSION LEVEL 2 ON STGR 27 BTW FS=280 / FS=333 AT INTERNAL STRUCTURE OF MAIN AVIONICS
- [SDR REXA2020030400287](https://openairdocs.org/sdr/REXA2020030400287.md): Angle · corroded · Feb 20, 2020 · N298PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "INITIAL INSPECTION: CORROSION ON ANGLES (4 E/A) OF SUPPORTS PROTECTORPLATE LOWER SURROUND STRUCTURE AT GALLEY SERVICE DOOR. ""SUMMARY: ON NRC. 00214 ANGLES (4 E/A) OF SUPPORTS PROTECTOR PLATE LOWER SURROUND STRUCTURE AT GALLEY SERVICE DOOR WER
- [SDR REXA2020030400285](https://openairdocs.org/sdr/REXA2020030400285.md): Striker · corroded · Feb 20, 2020 · N298PQ · Cndair CL6002D24 · Fuselage Main, Structure
  > "INITIAL INSPECTION: CORROSION ON STRIKER SEAL ON LOWER SURROUND STRUCTURE AT GALLEY SERVICE DOOR. " "SUMMARY: ON NRC. 00212 STRIKER SEAL ON LOWER SURROUND STRUCTURE AT GALLEY SERVICE DOOR WAS REPLACED PER CRJ-900 S
- [SDR REXA2020030400272](https://openairdocs.org/sdr/REXA2020030400272.md): Structure · cracked · Feb 20, 2020 · N298PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "INITIAL INSPECTION: CRACK IN BOX AT A/C EXTERNAL POWER RECEPTACLE SURROUND STRUCTURE. (FUS) (SM) " "SUMMARY: ON NRC. 00010 BOX AT A/C EXTERNAL POWER RECEPTACLE WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 A
- [SDR REXA2020030400270](https://openairdocs.org/sdr/REXA2020030400270.md): Striker · corroded · Feb 20, 2020 · N298PQ · Cndair CL6002D24 · Fuselage Main, Structure
  > "INITIAL INSPECTION: CORROSION ON STRIKER SEAL ON LOWER SURROUND STRUCTURE AT GALLEY SERVICE DOOR. " "SUMMARY: ON NRC. 00212 STRIKER SEAL ON LOWER SURROUND STRUCTURE AT GALLEY SERVICE DOOR WAS REPLACED PER CRJ-900 S
- [SDR REXA2020030400300](https://openairdocs.org/sdr/REXA2020030400300.md): Floorbeam · corroded · Feb 19, 2020 · N298PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > "AWR: HIDDEN DAMAGE; AFTER REMOVAL THE FLOOR PANEL SUPPORT ANGLE CORROSION WAS FOUND ON CROSSBEAM FS280 BTW BL0/RBL12 IN REF NRC: 00198 (SM) ""SUMMARY OF NRC 00306: DUE CORROSION LEVEL 2 ON CROSSBEAM FS280 BTW BL0/RBL12 IT WAS REPLACED PER CRJ/900 SRM 51-42-
- [SDR REXA2020030400299](https://openairdocs.org/sdr/REXA2020030400299.md): Floorbeam · corroded · Feb 19, 2020 · N298PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > "AWR: HIDDEN DAMAGE; AFTER REMOVAL THE FLOOR PANEL SUPPORT ANGLE CORROSION WAS FOUND ON CROSSBEAM FS280 BTW BL0/LBL12 IN REF NRC: 00198 (SM) " "SUMMARY OF NRC 00304: DUE CORROSION LEVEL 2 ON CROSSBEAM FS280 BTW BL0/LBL12 IT WAS REPLACED PER CRJ/900 SRM 51-4
- [SDR REXA2020030400297](https://openairdocs.org/sdr/REXA2020030400297.md): Stringer · corroded · Feb 18, 2020 · N298PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > "INITIAL INSPECTION: CORROSION ON STGR 21RH BTW FS=333 / FS=379 AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT (SM) (E/E) (TCI:53-20-305) ""SUMMARY OF NRC:00280 CORROSION LEVEL:2 ON STGR 21RH BTW FS=333 / FS=379 AT INTERNAL STRUCTURE OF MAIN AVIONICS COMP
- [SDR REXA2020030400279](https://openairdocs.org/sdr/REXA2020030400279.md): Seat Track · corroded · Feb 17, 2020 · N298PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > "INITIAL INSPECTION: CORROSION ON SIDE SEAT RAILS BTW FS=379.00 / FS=699.40 AND STGR 15LH (CPAX) (SM) (TCI:53-20-217). " "SUMMARY: ON NRC. 00201 CORROSION LEVEL 2. SIDE SEAT RAILS BTW FS=379.00 / FS=699.40 AND STGR 15LH WERE REPLACED P
- [SDR REXA2020030400282](https://openairdocs.org/sdr/REXA2020030400282.md): Seat Track · corroded · Feb 15, 2020 · N298PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > "INITIAL INSPECTION: CORROSION ON FLOOR SEAT RAILS BTW FS=477.40 / FS=669.40 AND LBL 9. (CPAX) (SM) (TCI:53-20-245). ""FLOOR SEAT RAILS BTW FS=477.40 / FS=669.40 AND LBL 9 WERE REPLACED PER CRJ-900 AMM 53-00-49 (CONFIG A12).
- [SDR REXA2020030600273](https://openairdocs.org/sdr/REXA2020030600273.md): Lens · eroded · Feb 14, 2020 · N298PQ · Cndair CL6002D24 · Exterior Lighting
  > "INITIAL INSPECTION: EROSION ON NAVIGATION LIGHT LENS AT LH WING ( AI) " "SUMMARY OF NRC S/N 00059: NAVIGATION LIGHT LENS AT LH WING WAS REPLACED PER CRJ-900 A.M.M 57-32-39. TOOL USED TORQU
- [SDR REXA2020030400278](https://openairdocs.org/sdr/REXA2020030400278.md): Seat Track · corroded · Feb 14, 2020 · N298PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > "INITIAL INSPECTION: CORROSION ON SIDE SEAT RAILS BTW FS=699.40 / FS=977.00 AND STGR 15RH (CPAX) (SM) (TCI:53-20-233). " "SUMMARY: ON NRC. 00200, CORROSION LEVEL 2. SIDE SEAT RAILS BTW FS=699.40 / FS=977.00 AND STGR 15RH, WERE REPLACED
- [SDR REXA2020030400277](https://openairdocs.org/sdr/REXA2020030400277.md): Seat Track · corroded · Feb 14, 2020 · N298PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > "INITIAL INSPECTION: CORROSION ON SIDE SEAT RAILS BTW FS=699.40 / FS=977.00 AND STGR 15LH (CPAX) (SM) (TCI:53-20-233). " "SUMMARY OF NRC 00199, CORROSION LEVEL 2: NEW SIDE SEAT RAILS BTW FS=699.40 / FS=977.00 AND STGR 15LH, WERE REPLAC
- [SDR REXA2020030400274](https://openairdocs.org/sdr/REXA2020030400274.md): Striker · worn · Feb 14, 2020 · N298PQ · Cndair CL6002D24 · Fuselage Main, Structure
  > "INITIAL INSPECTION: WEAR ON FWD/CENTER SEAL STRIKER AT MIDDLE BAGGAGEBAY DOOR CUT OUT (CCD) " "SUMMARY: ON NRC. 00130, STRIKER AT MIDDLE BAGGAGE BAY DOOR WAS REPLACED PER CRJ/900 SRM 51-41-02-001-001-A01 PAR 6.
- [SDR REXA2020030400276](https://openairdocs.org/sdr/REXA2020030400276.md): Support · cracked · Feb 13, 2020 · N298PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "INITIAL INSPECTION: CRACK ON EGDE TO THE SUPPORT OF THE JUNCTION BOX 6 AT RH FWD EQUIPMENT (FUS) " "SUMMARY: ON NRC. 00156 SUPPORT OF THE JUNCTION BOX 6 AT RH FWD EQUIPMENT WAS REPLACED PER CRJ-900 SRM 51-42-06-00
- [SDR REXA2020030400283](https://openairdocs.org/sdr/REXA2020030400283.md): Seat Track · corroded · Feb 12, 2020 · N298PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > "INITIAL INSPECTION: CORROSION ON FLOOR SEAT RAILS BTW FS=477.40 / FS=669.40 AND RBL 9. (CPAX) (SM) (TCI:53-20-245). ""SUMMARY: ON NRC 00206 CORROSION LEVEL 2. FLOOR SEAT RAILS BTW FS=477.40 / FS=669.40 AND RBL 9 WERE REPLACED PER CRJ
- [SDR REXA2020030400284](https://openairdocs.org/sdr/REXA2020030400284.md): Seat Track · corroded · Feb 11, 2020 · N298PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > "INITIAL INSPECTION: CORROSION ON FLOOR SEAT RAIL BTW FS=485 / FS=533 AND LBL 27. (CPAX) (SM) (TCI:53-20-245). " "SUMMARY OF NRC 00207 CORROSION LEVEL2:FLOOR SEAT RAIL BTW FS=485 / FS=533 AND LBL 27.WAS REPACED PER CRJ-900 AMM
- [SDR REXA2020030400281](https://openairdocs.org/sdr/REXA2020030400281.md): Seat Track · corroded · Feb 11, 2020 · N298PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > "INITIAL INSPECTION: CORROSION ON FLOOR SEAT RAILS BTW FS=349.00 / FS=477.40 AND RBL 9. (CPAX) (SM) (TCI:53-20-243). ""SUMMARY OF NRC 00204 CORROSION LEVEL 2:SEAT RAILS BTW FS=349.00 / FS=477.40 AND RBL 9.WERE REPLACED PER CRJ 900 AMM
- [SDR REXA2020030400280](https://openairdocs.org/sdr/REXA2020030400280.md): Seat Track · corroded · Feb 11, 2020 · N298PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > "INITIAL INSPECTION: CORROSION ON FLOOR SEAT RAILS BTW FS=349.00 / FS=477.40 AND LBL 9. (CPAX) (SM) (TCI:53-20-243). " "SUMMARY OF NRC 00203 CORROSION LEVEL 2:FLOOR SEAT RAILS BTW FS=349.00 / FS=477.40 AND LBL 9.WERE REPLACED PER CRJ
- [SDR REXA2020030400268](https://openairdocs.org/sdr/REXA2020030400268.md): Plate · bent · Feb 4, 2020 · N298PQ · Cndair CL6002D24 · Cargo/Baggage Doors
  > "INITIAL INSPECTION: BENT AND WEAR ON LOWER PLATES AT FWD/CENTER BAGGAGE BAY DOOR (CCD) " "SUMMARY: ON NRC. 00129 LOWER PLATES AT FWD/CENTER BAGGAGE BAY DOOR WERE REPLACED PER CRJ-900 AMM 52-35-07-400-802
- [SDR REXA2020030400267](https://openairdocs.org/sdr/REXA2020030400267.md): Retainer · bent · Feb 4, 2020 · N298PQ · Cndair CL6002D24 · Cargo/Baggage Doors
  > "INITIAL INSPECTION: WEAR ON LOWER PRESSURE SEAL RETAINERS FWD/AFT CORNER AT FWD/CENTRAL BAGGAGE BAY DOOR (CCD) ""LOWER (PRESSURE SEAL) RETAINERS AT FWD AND CENTRAL BAGGAGE BAY DOOR WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-
- [SDR REXA2017120101215](https://openairdocs.org/sdr/REXA2017120101215.md): Oxygen Mask · broken · Dec 1, 2017 · N298PQ · Cndair CL6002D24 · Passenger Oxygen System
  > FLIGHT ATTENDANT O2 MASK BROKEN. GAVE MASK TO FA AS REQUIRED.
- [SDR REXA2017100801075](https://openairdocs.org/sdr/REXA2017100801075.md): Acm · failed · Oct 8, 2017 · N298PQ · Cndair CL6002D24 · Cabin Cooling System
  > FA REPORTED A BURNING ODOR IN THE CABIN. RT PACK AUTOFAIL MESSAGE. SMOKE/HAZE THROUGHOUT CABIN. SHUTDOWN THE RT PACK AND APU. FOUND THE RT PACK FAILED. REMOVED AND REPLACED THE RT ACM IAW 21-51-08. OPS CHECKED GOOD.

Next page: https://openairdocs.org/aircraft/N298PQ/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 = 'N298PQ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N298PQ/reports

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