# Service difficulty reports: N200PQ

A list on [N200PQ](https://openairdocs.org/aircraft/N200PQ.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 4 · 155 reports

- [SDR REXA2025052900622](https://openairdocs.org/sdr/REXA2025052900622.md): Intercostal · cracked · May 14, 2025 · N200PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK ON INTERCOSTAL BTW FS177 AND FS185 ON FWD EQUIPMENT COMPARTMENT WAS FOUND IN REF. TO NRC 0444. INTERCOSTAL BTW FS177 AND FS185 ON FWD EQUIPMENT COMPARTMENT WAS REPAIRED PER EA CRJ953-19327 REV. IR
- [SDR REXA2025052900621](https://openairdocs.org/sdr/REXA2025052900621.md): Skin · cracked · May 13, 2025 · N200PQ · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > AFTER TO REPAIR SKIN, LEADING EDGE, FIXED, SS201.55 - SS210.69, PER EA CRJ957-19084 REV.IR, CRACK WAS FOUND ON WELDING REPAIR CRACK FOUND ON WELDING REPAIR OF LEADING EDGE, FIXED, SS201.55 - SS210.69 WAS REPAIRED PER EA CRJ957-19084 REV. B
- [SDR REXA2025052900620](https://openairdocs.org/sdr/REXA2025052900620.md): Support · cracked · May 10, 2025 · N200PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK ON FWD SUPPORTS (2EAS) OF INBOARD BRAKE ACCUMULATOR WAS FOUND FWD SUPPORT OF INBOARD BRAKE ACCUMULATOR WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND CRJ900 SRM 51-42-21-001-001-A01
- [SDR REXA2025052900616](https://openairdocs.org/sdr/REXA2025052900616.md): Access Panel · corroded · May 7, 2025 · N200PQ · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > CORROSION / CHAFE DAMAGE AT ALL SETTLEMENT AREA OF HYDRAULIC LOWER ACCESS PANEL 195AB SETTLEMENT (STRAP) AREA OF HYDRAULIC LOWER ACCESS PANEL 195AB WAS REPAIRED PER EA CRJ953-19313 REV IR AND WAS REPLACED PER CRJ900 SRM 51-42-10-001-001-A01
- [SDR REXA2026072801228](https://openairdocs.org/sdr/REXA2026072801228.md): Collector · corroded · May 6, 2025 · N200PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AFTER TO REMOVAL ADG RESTOW PUMP ASSY, WAS FOUND CORROSION ON COLLECTOR TRAY. COLLECTOR TRAY PN: 601R90825-1 WAS REPLACED PER CRJ-900 AMM 24-23-19
- [SDR REXA2025052900615](https://openairdocs.org/sdr/REXA2025052900615.md): Canister · cracked · May 6, 2025 · N200PQ · Cndair CL6002D24 · Wing Main, Frame Structure
  > CRACK IN CANISTER, WELDED NO.3 IN STA WS148 AT LH MAIN FUEL TANK. CRACK IN CANISTER, WELDED NO.3 IN STA WS148 AT LH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577 REV. --
- [SDR REXA2026072801225](https://openairdocs.org/sdr/REXA2026072801225.md): Fitting · corroded · Apr 30, 2025 · N200PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON FITTING (7 EAÏ¿½S) BTW FS280/FS379 AND LBL42/RBL39 AT FLOOR STRUCTURE. FITTING (4 EA) BTW FS280/FS379 AND LBL42/RBL39 AT FLOOR STRUCTURE WAS REPLACED PER CRJ900 SRM 51-42-21-001-001-A01 AND CRJ900 SRM 51-42-10-001-001-A01
- [SDR REXA2025052900614](https://openairdocs.org/sdr/REXA2025052900614.md): Seat Track · corroded · Apr 30, 2025 · N200PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RBL9/LBL9 SEAT TRACK BTW FS661.00+90-FS693.00. AT FLOOR STRUCTURE. DUE TO EXCESSIVE DAMAGE ON RBL9/LBL9 SEAT TRACK BTW FS 661.00 + 16 TO FS 693.00 AT FLOOR STRUCTURE WERE REPLACED PER CRJ900 SRM 53-31-49-101-001-A02 AND CRJ900 AMM 53-00-49 (CONFI
- [SDR REXA2025052900612](https://openairdocs.org/sdr/REXA2025052900612.md): Fitting · corroded · Apr 30, 2025 · N200PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON FITTING (7 EAÏ¿½S) BTW FS280/FS379 AND LBL42/RBL39 AT FLOOR STRUCTURE. FITTING (3 EA'S) BTW FS280/FS379 AND LBL42/RBL39 AT FLOOR STRUCTURE WERE REPLACED PER CRJ900 SRM 51-42-21-001-001-A01 AND CRJ900 SRM 51-42-10-001-001-A01
- [SDR REXA2025052900624](https://openairdocs.org/sdr/REXA2025052900624.md): Access Panel · cracked · Apr 28, 2025 · N200PQ · Cndair CL6002D24 · Wing, Plate/Skin
  > CRACK ON SKIN AND STTIFENER ON ACCESS PANEL 172CR IN REF. TO TASK CARD 900-57-510-700. CRACK ON SKIN AND STTIFENER ON ACCESS PANEL 172CR WAS REPAIRED REO 670-53-82-430 REV: - -
- [SDR REXA2025052900610](https://openairdocs.org/sdr/REXA2025052900610.md): Support · cracked · Apr 23, 2025 · N200PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK ON AFT TRACK SUPPORT FS1047 OF THE AFT BAGGAGE BAY DOOR AFT TRACK SUPPORT (DIAPHRAGM) FS1047 OF THE AFT BAGGAGE BAY DOOR WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 CRJ900 SRM 51-42-21-001-001-A01
- [SDR REXA2025052900609](https://openairdocs.org/sdr/REXA2025052900609.md): Web · cracked · Apr 23, 2025 · N200PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK ON ELECTRICAL BAY WEB FLOOR LH SIDE FS193.00 AT FWD EQUIPMENT COMPARTMENT CRACK ON ELECTRICAL BAY WEB FLOOR LH SIDE FS193.00 AT FWD EQUIPMENT COMPARTMENT WAS REPAIRED PER CRJ900 SRM 53-11-43-201-001-A01
- [SDR REXA2025052900608](https://openairdocs.org/sdr/REXA2025052900608.md): Support · cracked · Apr 23, 2025 · N200PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK ON SUPPORT JB6, FWD CORNER AT FWD EQUIPMENT COMPARTMENT SUPPORT JB6, FWD CORNER AT FWD EQUIPMENT COMPARTMENT WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND CRJ900 SRM 51-42-21-001-001-A01
- [SDR REXA2025052900600](https://openairdocs.org/sdr/REXA2025052900600.md): Web · cracked · Apr 23, 2025 · N200PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK AT UPPER WEB OF ADG COMPARTMENT, BELOW OF SETTLEMENT AREA OF ADG PUMB RH SIDE FS193. UPPER WEB OF ADG COMPARTMENT, BELOW OF SETTLEMENT AREA OF ADG PUMB RH SIDE FS193 WAS REPAIRED PER CRJ-900 SRM 53-11-43-201-001-A01
- [SDR REXA2026072801220](https://openairdocs.org/sdr/REXA2026072801220.md): Fitting · cracked · Apr 22, 2025 · N200PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACKED RECEPTACLE OF POSITION SENSOR AT GALLEY SERVICE DOOR SURROUND STRUCTURE GALLEY SERVICE-DOOR PROXIMITY SENSOR PX36 WAS REMOVED. INSTALLED PER AMM 52-70-06. AND RECEPTACLE OF POSITION SENSOR AT GALLEY SERVICE DOOR SURROUND STRUCTURE WAS REPLACED PER SRM
- [SDR REXA2025052900599](https://openairdocs.org/sdr/REXA2025052900599.md): Angle · corroded · Apr 22, 2025 · N200PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON MID CAP ANGLE LOWER SURROUND STRUCTURE PASSENGER DOOR. MID CAP ANGLE LOWER SURROUND STRUCTURE WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-21-23-101-001-A02 AND WAS REPLACED PER CRJ900 51-41-02-001-001-A01
- [SDR REXA2026072801219](https://openairdocs.org/sdr/REXA2026072801219.md): Skin · worn · Apr 21, 2025 · N200PQ · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > WEAR ON EXTERNAL FUSELAGE SKIN BTW BS 881 TO 913, BTW STGR 27 TO STGR 26LH WEAR ON EXTERNAL FUSELAGE SKIN BTW FS 881.00 TO FS 913.00, BTW STGR 27 TO STGR 26LH WAS REPAIRED PER EA CRJ953-19152 REV. IR
- [SDR REXA2026072801218](https://openairdocs.org/sdr/REXA2026072801218.md): Tie Down · chafed · Apr 21, 2025 · N200PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > WORN TIE DOWN BEAM OF AFT BAGGAGE-BAY CARGO DOOR STRUCTURE (INTERFERENCE WITH AFT BALANCE SPRING CABLE) BEAM OF AFT BAGGAGE-BAY CARGO DOOR STRUCTURE WAS REPAIRED PER EA CRJ953-19196 REV. IR.
- [SDR REXA2025052900607](https://openairdocs.org/sdr/REXA2025052900607.md): Panel · corroded · Apr 21, 2025 · N200PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > CRACKED AFT SIDE PANEL BTW TOP STEP AND MIDDLE STEP AT PASSENGER DOOR INTERNAL STRUCTURE (STEP SETTLEMENT AREA, UPPER & LOWER). AFT SIDE PANEL BTW TOP STEP AND MIDDLE STEP AT PASSENGER DOOR WAS REPAIRED PER CRJ-900 SRM 52-11-04-201-004-A01.
- [SDR REXA2025052900605](https://openairdocs.org/sdr/REXA2025052900605.md): Drag Angle · cracked · Apr 21, 2025 · N200PQ · Cndair CL6002D24 · Vertical Stabilizer Miscellaneous Structure
  > CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00) CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (
- [SDR REXA2026072801211](https://openairdocs.org/sdr/REXA2026072801211.md): Hinge · corroded · Apr 20, 2025 · N200PQ · Cndair CL6002D24 · Fuselage, Door Hinge
  > CORROSION ON DOOR HINGE (2EAS) AT FWD BAGGAGE BAY DOORS SURROUND STRUCTURE. DOOR HINGE FITTING (2 EA) AT FWD BAGGAGE BAY DOORS SURROUND STRUCTURE WERE REPLACED CRJ900 SRM 51-41-02-001-001-A01
- [SDR REXA2025052900602](https://openairdocs.org/sdr/REXA2025052900602.md): Support · corroded · Apr 20, 2025 · N200PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION AT SUPPORT STRUCTURE STRAP BTW FAIRING ACCESS PANEL 193AL & 193AR TO FAIRING ACCESS PANEL 193AB. SUMMARY: CORROSION AT SUPPORT STRUCTURE STRAP BTW FAIRING ACCESS PANEL 193AL & 193AR TO FAIRING ACCESS PANEL 193AB WERE EVALUATED OUT OF LIMITS PER CRJ90
- [SDR REXA2024102200914](https://openairdocs.org/sdr/REXA2024102200914.md): Bracket · none · Oct 17, 2024 · N200PQ · Cndair CL6002D24 · Standard Practices/Structures
  > WHILE INCORPORATING SB 670SH-53-043 REV C, WE ARE UNABLE TO GET PROPER EDGE DISTANCE ON BOTH VOLUMETRIC FUSE BRACKETS SH698-75359-1S AND SH698-75355-1S DUE TO EXISTING AIRCRAFT FASTENER PITCH. COMPLIED WITH MHIRJ EO SH698-75359 SNIEO S11.
- [SDR REXA2024102100902](https://openairdocs.org/sdr/REXA2024102100902.md): Floor Support · mismanufactured · Oct 16, 2024 · N200PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > WHILE INCORPORATING SB 670SH-53-043 REV C, WE HAVE ENCOUNTERED MISMATCHED FACTORY PILOT HOLES @FS 843 LBL 18 COMMON TO THE LBL18 FLOOR BEAM AND PRESSURE BOX EXISTING HOLES. COMPLIED WITH MHIRJ REO 690-53-41-503 REV--10/17/2024.
- [SDR REXA2024102100900](https://openairdocs.org/sdr/REXA2024102100900.md): A/C Pack · unknown · Oct 9, 2024 · N200PQ · Cndair CL6002D24 · Fuselage Main, Attach Fittings
  > WHILE PERFORMING SB 670BA-53-044 REVISION G, DATED JUL05/2022 FOUND LH AND RH STR12A FITTINGS PN CC670-33563-001SB AND CC670-33562-001SB CANNOT BE INSTALLED IAW SERVICE BULLETIN INSTRUCTIONS DUE TO EXISTING FASTENERS LOCATIONS ON THE AIRCRAFT COMPLIED WITH MHI
- [SDR REXA2024103001167](https://openairdocs.org/sdr/REXA2024103001167.md): Seat Track · corroded · Oct 7, 2024 · N200PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > RBL 9 SEAT TRACK FOUND TO BE CORRODED F.S. 693 TO F.S 847. REMOVED AND REPLACED IAW CRJ 900 SRM 53-00-49-201-002-A01, MODSUM IS67053000195, AND CRJ 900 AMM 53-00-49-400-801-A07.
- [SDR REXA2024103001166](https://openairdocs.org/sdr/REXA2024103001166.md): Seat Track · corroded · Oct 7, 2024 · N200PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > LBL 9 SEAT TRACK FOUND TO BE CORRODED F.S. 693 TO F.S 847. REMOVED AND REPLACED IAW CRJ 900 SRM 53-00-49-201-002-A01, MODSUM IS67053000195, AND CRJ 900 AMM 53-00-49-400-801-A07.
- [SDR REXA2024102901094](https://openairdocs.org/sdr/REXA2024102901094.md): Door · cracked · Oct 7, 2024 · N200PQ · Cndair CL6002D24 · Emergency Exits
  > R/H AFT EMERGENCY EXIT DOOR HAS A VISIBLE CRACK BELOW AFT UPPER LUG. REMOVED DAMAGE AND INSTALLED REPAIR PARTS IAW ENDEAVOR EA CRJ928-17503 REV IR 10/12/2024.
- [SDR REXA2024102901093](https://openairdocs.org/sdr/REXA2024102901093.md): Door · cracked · Oct 7, 2024 · N200PQ · Cndair CL6002D24 · Emergency Exits
  > R/H FORWARD EMERGENCY EXIT DOOR HAS A VISIBLE CRACK BELOW THE AFT UPPER LUG. REMOVED DAMAGE AND INSTALLED REPAIR PARTS IAW ENDEAVOR EA CRJ928-17502 REV IR 10/12/2024.
- [SDR REXA2024102901092](https://openairdocs.org/sdr/REXA2024102901092.md): Door · cracked · Oct 7, 2024 · N200PQ · Cndair CL6002D24 · Emergency Exits
  > L/H AFT EMERGENCY EXIT DOOR HAS A VISIBLE CRACK BELOW AFT UPPER LUG. REMOVED DAMAGE AND INSTALLED REPAIR PARTS IAW ENDEAVOR EA CRJ928-17506 REV IR 10/15/2024.
- [SDR REXA2024102901091](https://openairdocs.org/sdr/REXA2024102901091.md): Lug · cracked · Oct 7, 2024 · N200PQ · Cndair CL6002D24 · Emergency Exits
  > L/H FORWARD EMERGENCY EXIT DOOR HAS A VISIBLE CRACK BELOW THE AFT UPPER LUG. REMOVED DAMAGE AND INSTALLED REPAIR PARTS IAW ENDEAVOR EA CRJ928-17473 REV IR 10/15/2024.
- [SDR REXA2024032900315](https://openairdocs.org/sdr/REXA2024032900315.md): Battery Pack · inoperative · Mar 20, 2024 · N200PQ · Cndair CL6002D24 · Emergency Lighting
  > AFT EMERGENCY LIGHTS ON BOTH SIDES INOP. R & R EPSU BATTERY PACK (PS38) IAW JC 33-900-701.
- [SDR REXA2021111600962](https://openairdocs.org/sdr/REXA2021111600962.md): Beam · corroded · Nov 9, 2021 · N200PQ · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > AFT CARGO COMPARTMENT, FLOOR BEAM AT LBL 27 CORRODED IN A COUPLE LOCATIONS FROM APPROX FS 1000.00 TO FS 1031.00. - REPAIRED AFT CARGO FLOORBEAM AT LBL 27 IAW CRJ 900 SRM 53-00-41-201-001-A03 AND INSTALLED MYLAR IAW CRJ 900 SRM 51-27-19-001-001-A01.
- [SDR REXA2021111701006](https://openairdocs.org/sdr/REXA2021111701006.md): Retainer · cracked · Nov 6, 2021 · N200PQ · Cndair CL6002D24 · Cargo/Baggage Doors
  > WHILE CHANGING SEALS ON FWD CENTER CARGO DOOR JOB: 81520046 OP: 25. FOUND SEAL RETAINERS TO BE BENT, CRACKED & BROKEN IN SEVERAL LOCATIONS - REMOVED & REPLACED FWD CARGO DOOR SEAL RETAINER, RECEIVED SERVICEABLE SEAL RETAINERS AND DRILLED AND INSTALLED 2EA SIDE
- [SDR REXA2021111701005](https://openairdocs.org/sdr/REXA2021111701005.md): Retainer · cracked · Nov 6, 2021 · N200PQ · Cndair CL6002D24 · Cargo/Baggage Doors
  > WHILE CHANGING SEALS ON FWD CENTER CARGO DOOR JOB: 81520046 OP: 25. FOUND SEAL RETAINERS TO BE BENT, CRACKED & BROKEN IN SEVERAL LOCATIONS - REMOVED & REPLACED FWD CARGO DOOR SEAL RETAINER, RECEIVED SERVICEABLE SEAL RETAINERS AND DRILLED AND INSTALLED 2EA SIDE
- [SDR REXA2021111701004](https://openairdocs.org/sdr/REXA2021111701004.md): Retainer · cracked · Nov 6, 2021 · N200PQ · Cndair CL6002D24 · Cargo/Baggage Doors
  > WHILE CHANGING SEALS ON FWD CENTER CARGO DOOR JOB: 81520046 OP: 25. FOUND SEAL RETAINERS TO BE BENT, CRACKED & BROKEN IN SEVERAL LOCATIONS - REMOVED & REPLACED FWD CARGO DOOR SEAL RETAINER, RECEIVED SERVICEABLE SEAL RETAINERS AND DRILLED AND INSTALLED 2EA SIDE
- [SDR REXA2021111701003](https://openairdocs.org/sdr/REXA2021111701003.md): Angle · corroded · Nov 6, 2021 · N200PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > PAX DOOR SURROUND STRUCTURE, LOWER MID CAP ANGLE CORRODED BETWEEN FS 310 AND FS 349. - REMOVED AND REPLACE PAX DOOR MID CAP ANGLE AND KICKPLATE ANGLES IAW CRJ900 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01 & 51-40-11-001-001-A01 & ADJUSTED PROX SWITCH IAW
- [SDR REXA2021111701002](https://openairdocs.org/sdr/REXA2021111701002.md): Plate · corroded · Nov 6, 2021 · N200PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR SURROUND STRUCTURE, LOWER MID CAP ANGLE CORRODED BETWEEN FS 310 AND FS 349. - REMOVED AND REPLACE PAX DOOR MID CAP ANGLE AND KICKPLATE ANGLES IAW CRJ900 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01 & 51-40-11-001-001-A01 & ADJUSTED PROX SWITCH IAW
- [SDR REXA2021111701012](https://openairdocs.org/sdr/REXA2021111701012.md): Yoke · nicked · Nov 6, 2021 · N200PQ · Cndair CL6002D24 · Engine Mount Section
  > RIGHT ENGINE FWD YOKE MOUNT HAS SEVERAL NICKS ON THE LOWER END FWD AND AFT EDGES - REPAIRED RIGHT ENGINE FWD YOKE NICKS ON THE LOWER END FWD & AFT EDGES IAW BOMBARDIER REO#670-71-21-057, REV--, DATED 2013-09-13.
- [SDR REXA2021111701001](https://openairdocs.org/sdr/REXA2021111701001.md): Plate · missing · Nov 6, 2021 · N200PQ · Cndair CL6002D24 · Nacelle/Pylon, Main Frame
  > LH PYLON HAS 2 BOND PLATES MISSING ON TOP OF PYLON AND RH PYLON HAS ONE BOND PLATE MISSING. - INSTALLED 3 EA NEW BONDING PLATE ON L/H PYLON TOP SURFACE AND 2 EA NEW BONDING PLATE ON R/H PYLON P/N MM670-37197-007 IAW CRJ 900 SRM 51-42-13-001-001-A01. AND AMM 51
- [SDR REXA2021111600967](https://openairdocs.org/sdr/REXA2021111600967.md): Frame · cracked · Nov 6, 2021 · N200PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FRAME AT FS 333 BETWEEN STGR 1R AND STGR 2R CRACKED. - REPAIRED CRACKED FRAME AT FS 333 BETWEEN STR1R AND STR2R IAW ENDEAVOR EA CRJ 953-12092 REV IR DATED 9/15/21. CUT, REPAIRED, AND LEACK CHECKED POTABLE WATER LINE BTWEEN FS 333 AND FS 349 IAW CRJ 900 AMM 20
- [SDR REXA2021111700998](https://openairdocs.org/sdr/REXA2021111700998.md): Stringer · corroded · Nov 5, 2021 · N200PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STRINGER 24R CORRODED BETWEEN FS 295 TO FS 310. - INSTALLED STR 24R FS 280-333 IAW ENDEAVOR AIR EA# CRJ 953-12340.
- [SDR REXA2021111600950](https://openairdocs.org/sdr/REXA2021111600950.md): Stringer · corroded · Nov 3, 2021 · N200PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STRINGER 19R CORRODED BETWEEN FS 295 AND FS 310 - REMOVED AND REPLACED STR 19R FROM F.S. 295-310 IAW CRJ 900 SRM 51-42-21-001-001-A01 AND EA CRJ953-12283 REV IR DATED 10/15/2021. WVAC EMP STAMP # 711 MTC
- [SDR REXA2021111700991](https://openairdocs.org/sdr/REXA2021111700991.md): Longeron · corroded · Nov 2, 2021 · N200PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > LONGERON AT STR 25R F.S. 333-349 CORRODED - REMOVED & REINSTALLED INTERCOSTAL AT STRGR 25R FOR ACCESS & REMOVED & REPLACED LONGERON IAW CRJ-900 SRM 51-40-11-001-001-A01, 51-42-06-001 001-A01, 51-42-21-001-001-A01 & COMPLIED WITH EA CRJ953-12231 DATED 10/5/2021
- [SDR REXA2021111700997](https://openairdocs.org/sdr/REXA2021111700997.md): Stringer · corroded · Nov 1, 2021 · N200PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STRINGER 23R CORRODED BETWEEN FS 295 TO FS 310. - INSTALLED STR 23R FS 280-333 IAW ENDEAVOR AIR EA# CRJ 953-12284.
- [SDR REXA2021111600965](https://openairdocs.org/sdr/REXA2021111600965.md): Seat Track · corroded · Oct 29, 2021 · N200PQ · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > AFT CARGO BAY SEAT TRACK AT LBL 27 BEGINNING AT APPROX FS 985.00 CORRODED. - REMOVED FABRICATED AND INSTALLED SEAT TRACK @ LBL27 FS 926-988 IAW CRJ 900 SRM 53-51-49-101-001-A02, 53-00-49-201-002-A01 & AMM 53-00-49-000/400-801-A07.
- [SDR REXA2021111600947](https://openairdocs.org/sdr/REXA2021111600947.md): Angle · corroded · Oct 29, 2021 · N200PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > GALLEY SERVICE DOOR SILL ANGLE IS CORRODED BEHIND ATTACH BRACKET FOR SCUFF PLATE. (PROTECTOR PLATE). - REMOVED & REPLACED SERVICE DOOR SILL ANGLE IAW CRJ 900 SRM'S 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-21-001-001-A01. REMOVED & REINSTALLED SERVICE
- [SDR REXA2021111600957](https://openairdocs.org/sdr/REXA2021111600957.md): Intercostal · corroded · Oct 28, 2021 · N200PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT STGR 27R CORRODED BETWEEN FS 349 AND FS 364. - REMOVED, LOCATED, DRILLED & INSTALLED NEW INTERCOSTAL AT STR 27R FS 349-364 AND R/R PROX SENSOR IAW CRJ900 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, 51-40-11-001-001-A01, AND AMM 52-70-08-000/
- [SDR REXA2021111701008](https://openairdocs.org/sdr/REXA2021111701008.md): Angle · corroded · Oct 22, 2021 · N200PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > FRAME ON INNER PAX DOOR STRUCTURE @ FS 327 HAS EVIDENCE OF CORROSION. - REMOVED & REPLACED 327 FRAME & ATTACHING ANGLE ON INNER PAX DOOR IAW CRJ 900 SRM'S 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-21-001-001-A01. WVAC EMP STAMP #774 MTC
- [SDR REXA2021111701007](https://openairdocs.org/sdr/REXA2021111701007.md): Frame · corroded · Oct 22, 2021 · N200PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > FRAME ON INNER PAX DOOR STRUCTURE @ FS 327 HAS EVIDENCE OF CORROSION. - REMOVED & REPLACED 327 FRAME & ATTACHING ANGLE ON INNER PAX DOOR IAW CRJ 900 SRM'S 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-21-001-001-A01. WVAC EMP STAMP #774 MTC

Next page: https://openairdocs.org/aircraft/N200PQ/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 = 'N200PQ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N200PQ/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.