# Service difficulty reports: N153PQ

A list on [N153PQ](https://openairdocs.org/aircraft/N153PQ.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 · 225 reports

- [SDR REXA2026070701069](https://openairdocs.org/sdr/REXA2026070701069.md): Floorbeam · cracked · Jul 7, 2026 · N153PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > LEFT COCKPIT FLOORBEAM LBL 12 IS CRACKED AT F.S.280 PREVIOUS REPAIR. REPAIRED LT COCKPIT FLOOR BEAM LBL 12 AT BS 280 IAW REO 690-53-11-1159, REV -- DATED 2019-07-29.
- [SDR REXA2026063000998](https://openairdocs.org/sdr/REXA2026063000998.md): Door · cracked · Jun 29, 2026 · N153PQ · Cndair CL6002D24 · Emergency Exits
  > LEFT AFT OVERWING EMERGENCY DOOR HAS SUSPECTED CRACKED AT BASE OF STRIKER. COMPLIED WITH GREO 670-52-21-103 REV-.
- [SDR REXA2026063000996](https://openairdocs.org/sdr/REXA2026063000996.md): Door · cracked · Jun 29, 2026 · N153PQ · Cndair CL6002D24 · Emergency Exits
  > RIGHT AFT OVERWING EMER. DOOR HAS SUSPECTED CRACK AT BASE OF STRIKER. COMPLIED WITH MHIRJ GREO 670-52-21-103 REV-- DATED 2024-11-06
- [SDR REXA2026063000994](https://openairdocs.org/sdr/REXA2026063000994.md): Fitting · damaged · Jun 29, 2026 · N153PQ · Cndair CL6002D24 · Wing, Control Surface Attach Fittings
  > UPON REMOVAL OF THE RT WING SIDE AILERON BUSHINGS, IT WAS FOUND THAT THE LUG LABELED -F- (HINGE NR 3 OTBD) HAS DAMAGE IN THE BORE & CURRENTLY MEASURES (0.8755""). REPAIRED LUG BORE OF THE R/H AILERON HINGE FITTING #3 AT WING TRAILING EDGE W.S.323.058 IAW HNI
- [SDR REXA2026070201000](https://openairdocs.org/sdr/REXA2026070201000.md): Door · cracked · Jun 26, 2026 · N153PQ · Cndair CL6002D24 · Emergency Exits
  > R/H FWD OVERWING EMER. DOOR HAS SUSPECTED CRACK AT BASE OF STRIKER. COMPLIED WITH MHIRJ GREO 670-52-21-103 REV-- DATED 2024-11-06
- [SDR REXA2026062900987](https://openairdocs.org/sdr/REXA2026062900987.md): Drag Angle · cracked · Jun 9, 2026 · N153PQ · Cndair CL6002D24 · Fuselage, Stabilizer Attach Fittings
  > THERE IS A POSSIBLE CRACK IN THE RIGHT-HAND VERTICAL STABILIZER DRAG ANGLE. STRIPPED PAINT FROM FWD DRAG ANGLE IAW CRJ900 SRM 51-26-01-001-001-A01. FOUND FWD DRAG ANGLE TO BE VISUALLY CRACKED 2.35"L, REMOVED FASTENERS FOR ACCESS FOR REPAIR IAW SRM 51-42-06-0
- [SDR REXA2026062600979](https://openairdocs.org/sdr/REXA2026062600979.md): Bushing · damaged · Jun 9, 2026 · N153PQ · Cndair CL6002D24 · Ailerons
  > UPON REMOVAL OF THE LT WING SIDE AILERON BUSHINGS, IT WAS FOUND THAT THE LUG -C- (HINGE NR 2 INBD) WAS PREVIOUSLY O/S & CURRENTLY MEASURES (0.8965"). COMPLIED WITH STEPS NR 1 & 2 OF IAW REO 690-57-51-541, REV -. ENSURED NO PREVIOUS BLENDING ON WING SIDE AIL
- [SDR REXA2026062600977](https://openairdocs.org/sdr/REXA2026062600977.md): Bushing · damaged · Jun 8, 2026 · N153PQ · Cndair CL6002D24 · Ailerons
  > FOUND 4 RT AILERON SIDE BUSHING LUGS -B-, -C-, -F- AND -G- TO BE PREVIOUSLY OVERSIZED. REPAIRED THE RT AILERON BUSHING LUGS BY REAMING TO 3RD OVERSIZE ON LUGS -B- & -G- AND 2ND OVERSIZE ON LUGS -C- & -F- IAW STEPS F.(1)-F.(4) OF GREO 670-57-61-237 REV--. P
- [SDR REXA2026062600976](https://openairdocs.org/sdr/REXA2026062600976.md): Lug · damaged · Jun 8, 2026 · N153PQ · Cndair CL6002D24 · Ailerons
  > FOUND 2 EA LT AILERON SIDE BUSHING LUGS -C- AND -F- TO BE PREVIOUSLY OVERSIZED. REPAIRED 2EA LT AILERON SIDE BUSHING LUGS -C- & -F-, BY REAMING TO 1ST OVERSIZE IAW STEPS F.(1)-F.(4) OF GREO 670-57-61-237 REV--. PERFORMED LPI OF LT AILERON LUG BORES C AND F I
- [SDR REXA2024071700557](https://openairdocs.org/sdr/REXA2024071700557.md): Lamp · inoperative · Jul 17, 2024 · N153PQ · Cndair CL6002D24 · Emergency Lighting
  > EMERGENCY LIGHT EXTERNAL BY PAX DOOR INOP R/R EXTERNAL EMER LIGHT BY PAX DOOR IAW CRJ 900 AMM 33-51-15 OPS CHECK GOOD P/N ON/OFF: 8GH002473-08
- [SDR REXA2022111102526](https://openairdocs.org/sdr/REXA2022111102526.md): Bulb · inoperative · Nov 5, 2022 · N153PQ · Cndair CL6002D24 · Emergency Lighting
  > "RH SERVICE DOOR EXTERNAL EMERGENCY LIGHT DS52 DOES NOT ILLUMINATE WHEN EMERGENCY LIGHTS ARE SWITCHED ON. " "TROUBLESHOT SYSTEM AND DISCOVERED BULB WAS BURNT OUT FOR LIGHT DS52 & INSTALLED NEW SERVICEABLE BULB P/N 8GH002473-08 IAW CRJ 900 SRM 51-41-02-001-00
- [SDR REXA2022110302409](https://openairdocs.org/sdr/REXA2022110302409.md): Drag Angle · cracked · Oct 31, 2022 · N153PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR AFT WEB DRAG ANGLE IS CRACKED. INSTALLED NEW SERVICEABLE DRAG ANGLE IAW CRJ 900 SRM 51-42-06-001-001-A01
- [SDR REXA2022110302407](https://openairdocs.org/sdr/REXA2022110302407.md): Web · corroded · Oct 31, 2022 · N153PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR AFT WEB HAS MULTIPLE SPOTS OF CORROSION. INSTALLED NEW SERVICEABLE AFT WEB ASSY IAW CRJ900 SRM 51-42-06-001-001-A01 AND 51-42-13-001-001-A01
- [SDR REXA2022110302406](https://openairdocs.org/sdr/REXA2022110302406.md): Former · corroded · Oct 27, 2022 · N153PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR AFT FORMER HAS MULTIPLE SPOTS OF CORROSION INSTALLED NEW PAX DOOR AFT FORMER, IAW CRJ900 SRM 51-42-06-001-001-A01, 51-40-11-001-001-A01
- [SDR REXA2022110102362](https://openairdocs.org/sdr/REXA2022110102362.md): Panel · chafed · Oct 21, 2022 · N153PQ · Cndair CL6002D24 · Wing, Control Surfaces
  > FLAP PANEL 684 GB IS CHAFED ON LEADING EDGE. REMOVED AND REPLACED PANEL 684GB
- [SDR REXA2022101302255](https://openairdocs.org/sdr/REXA2022101302255.md): Stringer · corroded · Oct 11, 2022 · N153PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 23R HAS CORROSION AROUND FASTENERS BTWEEN FS280 AND FS295 RECEIVED NEW STRINGER PN#SH670-31211-4U LOCATED AND DRILLED NEW STRINGER IAW CRJ900 SRM 51-40-11-001-001-A01. INSTALLED NEW SERVICEABLE STRINGER 23R BETWEEN FS 280 TO 333 IAW CRJ 900 SRM 51-42-
- [SDR REXA2022101302253](https://openairdocs.org/sdr/REXA2022101302253.md): Angle · corroded · Oct 11, 2022 · N153PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR ANGLE C AT DD7A FOUND TO BE CORRODED LOCATED DRILLED AND INSTALLED NEW SERVICEABLE ANGLE C AT DD7A IAW CRJ900 SRM 51-40-11-001-001-A01 AND 51-42-21-001-001-A01
- [SDR REXA2022101302252](https://openairdocs.org/sdr/REXA2022101302252.md): Intercostal · deformed · Oct 11, 2022 · N153PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR AFT DD7 INTERCOSTAL FOUND TO BE BENT AND BULGED LOCATED DRILLED AND INSTALLED NEW SERVICEABLE PAX DOOR INTERCOSTAL DD7 AT AFT SIDE IAW CRJ900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01 PN: 601R318825-1
- [SDR REXA2022101302250](https://openairdocs.org/sdr/REXA2022101302250.md): Floor Support · corroded · Oct 11, 2022 · N153PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > F.S.319.70 FRAME TO FLOOR SILL FITTING IS CORRODED AT STGR 17R. REMOVED CORROSION ON FS319.70 FRAME TO FLOOR SILL FITTING AT STGR 17R IAW CRJ900 SRM 51-21-06-001-001-A01. FOUND TO BE OUT OF LIMITS IAW CRJ-900 SRM 53-21-23-101-002-A02. REMOVED FITTING AT FS319.
- [SDR REXA2022111002432](https://openairdocs.org/sdr/REXA2022111002432.md): Frame · corroded · Oct 7, 2022 · N153PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > LOWER FRAME SECTOR, FS 364.00, STRGR.26L - 26R CORRODED REMOVED AND REPLACED, LOWER FS 364.00 FRAME SECTOR,IAW CRJ 900 SRM'S,#53-21-23-201-008-A01,#51-40-11-001-001-A01, #51-42-06-001-001-A01, #51-42-21-001-001-A01, AND MHIRJ EO'S, #SH670-32090(SNEIO-01) & #S
- [SDR REXA2022101302254](https://openairdocs.org/sdr/REXA2022101302254.md): Floorbeam · corroded · Oct 7, 2022 · N153PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > FS 280 FLOORBEAM L/H IS CORRODED, REPLACE REQUIRED. REMOVED AND REPLACED IAW CRJ 900SRMS 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-12-001-001-A01, 51-42-21-001-001-A01, AND 51-42-22-001-001-A01
- [SDR REXA2022101302251](https://openairdocs.org/sdr/REXA2022101302251.md): Stringer · corroded · Oct 7, 2022 · N153PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 25L FROM F.S.295 TO F.S.319.70 IS CORRODED. REMOVED AND REPLACED IAW CRJ 900SRMS 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-21-001-001-A01.
- [SDR REXA2022100502207](https://openairdocs.org/sdr/REXA2022100502207.md): None · corroded · Oct 5, 2022 · N153PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > RIGHT SIDE SEAT RAIL BETWEEN FS 785.00 AND 847+16 IS CORRODED REPLACED RH SIDE SEAT RAIL P/N SH670-36260-5 FROM FS 785.00 TO 847+16 IAW CRJ 900 AMM 53-00-49-400-801(A07).
- [SDR REXA2022100602223](https://openairdocs.org/sdr/REXA2022100602223.md): None · corroded · Oct 4, 2022 · N153PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > LEFT SIDE SEAT RAIL BETWEEN FS 744.00 AND 752.00 IS CORRODED INSTALLED NEW SEAT RAIL IAW CRJ 900 AMM 53-00-49-400-801-A07
- [SDR REXA2022100602222](https://openairdocs.org/sdr/REXA2022100602222.md): None · corroded · Oct 4, 2022 · N153PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > R/H SIDE SEAT RAIL IS CORRODED FROM F.S.661+16 TO 677. REMOVED AND REPLACED R/H SIDE SEAT RAIL FROM F.S. 661+16 TO F.S. 677 P/N SH690-36283-1 IAW CRJ-900 AMM 53-00-49-000-801-A07 AND 53-00-49-400-801-A07
- [SDR REXA2022100602221](https://openairdocs.org/sdr/REXA2022100602221.md): None · corroded · Oct 4, 2022 · N153PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > L/H SIDE SEAT RAIL IS CORRODED FROM F.S.661+16 TO 677. INSTALLED NEW SEAT RAIL IAW CRJ 900 AMM 53-00-49-400-801-A07.
- [SDR REXA2022100602220](https://openairdocs.org/sdr/REXA2022100602220.md): Seat Track · corroded · Oct 4, 2022 · N153PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > LBL9 FLOOR SEAT TRACK FROM F.S.661+32 TO F.S.693 IS CORRODED. INSTALLED NEW SEAT TRACK IAW CRJ 900 AMM 53-00-49-400-801-A07.
- [SDR REXA2022100602219](https://openairdocs.org/sdr/REXA2022100602219.md): Seat Track · corroded · Oct 4, 2022 · N153PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > LBL9 FLOOR SEAT TRACK FROM F.S.581 TO F.S.661+32 IS CORRODED INSTALLED NEW SEAT TRACK IAW CRJ 900 AMM 53-00-49-400-801-A07.
- [SDR REXA2022100602218](https://openairdocs.org/sdr/REXA2022100602218.md): Seat Track · corroded · Oct 4, 2022 · N153PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > RBL9 FLOOR SEAT TRACK FROM F.S.661+32 TO F.S.693 IS CORRODED. INSTALLED NEW SEAT TRACK IAW CRJ 900 AMM 53-00-49-400-801-A07.
- [SDR REXA2022100602217](https://openairdocs.org/sdr/REXA2022100602217.md): Seat Track · corroded · Oct 4, 2022 · N153PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > RBL9 FLOOR SEAT TRACK FROM F.S.581 TO F.S.661+32 IS CORRODED. INSTALLED NEW SEAT TRACK PN SH690-33404-1 IAW CRJ 900 AMM 53-00-49-400-801-A07.
- [SDR REXA2022100602216](https://openairdocs.org/sdr/REXA2022100602216.md): Seat Track · corroded · Oct 4, 2022 · N153PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > RBL9 FLOOR SEAT TRACK FROM F.S.485 TO F.S.581 IS CORRODED. INSTALLED NEW SEAT TRACK PN SH690-33407-1 IAW CRJ 900 AMM 53-00-49-400-801-A07.
- [SDR REXA2022100602215](https://openairdocs.org/sdr/REXA2022100602215.md): Seat Track · corroded · Oct 4, 2022 · N153PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > LBL9 FLOOR SEAT TRACK IS CORRODED BETWEEN F.S. 985 TO F.S. 1000. FABRICATED SEAT TRACK RBL 9 FS 849-985 FROM 20276-288-0-0A IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 53-00-49-201002-A01. INSTALLED IAW CRJ 900 AMM 53-00-49-400-801-A07.
- [SDR REXA2022100602212](https://openairdocs.org/sdr/REXA2022100602212.md): Seat Track · corroded · Oct 4, 2022 · N153PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > LBL 9 FLOOR SEAT TRACK IS CORRODED BETWEEN F.S. 693 TO F.S. 830. FABRICATED, LOCATED AND DRILLED AND INSTALLED NEW SEAT TRACK ON LBL 9 BTWN FS 693 TO FS 830 IAW CRJ900 SRM 51-40-11-001-001-A01, 53-00-49-201-002-A01 AND CRJ 900AMM 53-00-49-400-801-A07.
- [SDR REXA2022100502211](https://openairdocs.org/sdr/REXA2022100502211.md): Beam · corroded · Oct 4, 2022 · N153PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FS280 FLOORBEAM R/H IS CORRODED. REMOVED AND REPLACED RH FS 280 FLOORBEAM IAW CRJ 900 SRM 51-42-06-001-001-A01 51-42-21-001-001-A01, 51-42-12-001-001-A01, 51-42-22-001-001-A01
- [SDR REXA2022100502208](https://openairdocs.org/sdr/REXA2022100502208.md): None · corroded · Oct 4, 2022 · N153PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > LEFT SIDE SEAT RAIL BETWEEN FS 785.00 AND 847+16 IS CORRODED, REMOVED SEAT RAIL IAW CRJ 900 AMM 53-00-49-000-801-A07. INSTALLED NEW SEAT RAIL PART NUMBER SH670-36260-5 IAW CRJ 900 AMM 53-00-49-400-801-A07
- [SDR REXA2022100502206](https://openairdocs.org/sdr/REXA2022100502206.md): Angle · corroded · Oct 4, 2022 · N153PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > 280 CROSSBEAM FWD "J" ANGLE IS CORRODED. REMOVED AND REPLACED FWD “J” ANGLE AT FS280 BETWEEN LBL12 TO RBL12 IAW CRJ900 SRM 51-42-06-001-001-A01 AND CRJ900 SRM 51-42-21-001-001-A01
- [SDR REXA2022100502210](https://openairdocs.org/sdr/REXA2022100502210.md): None · corroded · Oct 2, 2022 · N153PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > RIGHT SIDE SEAT RAIL BETWEEN FS 744.00 AND 752.00 IS CORRODED, REMOVED AND REPLACED RH SIDE SEAT RAIL (PN: SH690-36285-1) BETWEEN FS 744 AND FS 752 IAW CRJ-900 AMM 53-00-49-000-801 (A07) AND CRJ-900 AMM 53-00-49-400-801 (A07)
- [SDR REXA2022100502209](https://openairdocs.org/sdr/REXA2022100502209.md): None · corroded · Oct 2, 2022 · N153PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > LEFT SIDE SEAT RAIL BETWEEN FS 913.00 AND 969.00 IS CORRODED, REMOVED AND INSTALLED NEW LH SEAT RAIL PN SH690-37542-1 BETWEEN FS913.00 AND FS969.00 IAW CRJ900 AMM 53-00-49-400-801 (CONFIG A07).
- [SDR REXA2022110302412](https://openairdocs.org/sdr/REXA2022110302412.md): Hinge · damaged · Sep 28, 2022 · N153PQ · Cndair CL6002D24 · Wing Structure
  > FOUND HINGE #2 AILERON WING FITTING NOMINAL OUTBOARD LUG TO BE DAMAGED. REPAIRED LEFT AILERON #2 WING HINGE FITTING IAW MHIRJ REO 690-57-51-276
- [SDR REXA2022100602214](https://openairdocs.org/sdr/REXA2022100602214.md): Seat Track · corroded · Sep 27, 2022 · N153PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > RBL9 FLOOR SEAT TRACK IS CORRODED BETWEEN F.S. 849 TO F.S 985. FABRICATED SEAT TRACK RBL 9 FS 849-985 FROM 20276-288-0-0A IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 53-00-49-201002-A01. INSTALLED IAW CRJ 900 AMM 53-00-49-400-801-A07.
- [SDR REXA2022100602213](https://openairdocs.org/sdr/REXA2022100602213.md): Seat Track · corroded · Sep 27, 2022 · N153PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > LBL9 FLOOR SEAT TRACK IS CORRODED BETWEEN F.S. 830 TO F.S. 849 INSTALLED NEW SEAT TRACK PN BA690-30000-6959 IAW CRJ 900 AMM 53-00-49-400-801-A07
- [SDR REXA2022100502205](https://openairdocs.org/sdr/REXA2022100502205.md): Seat Track · corroded · Sep 27, 2022 · N153PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > RBL9 FLOOR SEAT TRACK IS CORRODED BETWEEN F.S. 830 TO F.S. 849. REMOVED AND REPLACED CORRODED RBL9 SEAT TRACK FROM FS830 TO FS849 WITH NEW SERVICEABLE SEAT TRACK PN BA690-30000-6959 IAW CRJ900 AMM 53-00-49-400-801-A01
- [SDR REXA2022092902153](https://openairdocs.org/sdr/REXA2022092902153.md): Retainer · cracked · Sep 27, 2022 · N153PQ · Cndair CL6002D24 · Cargo/Baggage Doors
  > FWD CARGO DOOR LOWER SEAL RETAINER IS DAMAGED IN MULTIPLE LOCATIONS. FOUND FWD CARGO DOOR LOWER SILL RETAINER TO BE OUT OF LIMITS IAW CRJ 900 SRM 51-42-06-001-001-A01. REMOVED LOWER SEAL RETAINER FROM FWD CARGO DOOR IAW CRJ900 SRM 51-42-06-001-001-A01. INSTALL
- [SDR REXA2022110102361](https://openairdocs.org/sdr/REXA2022110102361.md): Intercostal · corroded · Sep 25, 2022 · N153PQ · Cndair CL6002D24 · Fuselage Main, Structure
  > JACK PAD INTERCOSTAL ON RH SIDE BETWEEN FS 265 TO 280 IS CORRODED ON ATTACH FLANGE. LOCATED AND DRILLED LH AND RH JACK PAD INTERCOSTALS IAW CRJ900 SRM 51-40-11-001-001-A01
- [SDR REXA2022110102357](https://openairdocs.org/sdr/REXA2022110102357.md): Drag Angle · cracked · Sep 25, 2022 · N153PQ · Cndair CL6002D24 · Vertical Stabilizer
  > VERTICAL STAB L/H AFT DRAG ANGLE IS CRACKED INSTALLED NEW AFT DRAG ANGLE ON LH VERTICAL STAB IAW CRJ900 SRM 51-42-21-001-001-A01 AND CRJ900 SRM 51-42-10-001-001-A01.
- [SDR REXA2022110102350](https://openairdocs.org/sdr/REXA2022110102350.md): Stringer · corroded · Sep 25, 2022 · N153PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STGR 26L IS CORRODED BETWEEN F.S. 1000 TO F.S. 1031 INSTALLED NEW SERVICEABLE STRINGER 26L AND CLEATS FROM FS 977 TO FS 1098 IAW CRJ900 SRM 53-00-03-201-001-A02
- [SDR REXA2022110102349](https://openairdocs.org/sdr/REXA2022110102349.md): Stringer · corroded · Sep 25, 2022 · N153PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STRINGER 24L BETWEEN FS 485.00 AND 501.00 IS CORRODED. INSTALLED STRINGER 24L BETWEEN FS 477.40 TO FS 501.00+3 IAW MHIRJ AVIATION REO # 690-53-31-667 REV.P2 DATE 2022-10-06
- [SDR REXA2022111002426](https://openairdocs.org/sdr/REXA2022111002426.md): Frame · corroded · Sep 20, 2022 · N153PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FUSELAGE FRAME F.S.533 IS CORRODED BETWEEN STRINGER 17L AND 18L REPAIRED FRAME F.S.533 IAW CRJ 900 SRM 53-00-06-201-001-A03
- [SDR REXA2022110302411](https://openairdocs.org/sdr/REXA2022110302411.md): Frame · corroded · Sep 20, 2022 · N153PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FS 250 RBL9 AND LBL9 FRAME IS CORRODED INSTALLED NEW FRAME AT F.S. 250 BETWEEN 26L AND 26R IAW MHIRJ REO # 690-53-11-1470
- [SDR REXA2022110302410](https://openairdocs.org/sdr/REXA2022110302410.md): Frame · corroded · Sep 20, 2022 · N153PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FUSELAGE FRAME F.S.549 IS CORRODED BETWEEN STRINGER 17L AND 18L. REPAIRED FRAME SECTOR F.S.549 IAW MHIRJ REO 690-53-31-679

Next page: https://openairdocs.org/aircraft/N153PQ/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 = 'N153PQ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N153PQ/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.