# Service difficulty reports: N161PQ

A list on [N161PQ](https://openairdocs.org/aircraft/N161PQ.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 · 227 reports

- [SDR SWIA20241222](https://openairdocs.org/sdr/SWIA20241222.md): Window · arced · Dec 22, 2024 · N161PQ · Cndair CL6002D24 · Flight Compartment Windows
  > LEFT WINDOW IS ARCING AT THE BOTTOM CENTER REMOVED AND REPLACED LH SIDE WINDOW PER AMM 56-12-01. LEAK TEST GOOD. NO FURTHER DEFECTS NOTED. OK FOR SERVICE. PLEASE REFERENCE AML 1498038 FOR FWD DISCREPANCY. COMPLIED WITH TASK CARD 56-220-1000-SKY.
- [SDR SWIA2024120201322](https://openairdocs.org/sdr/SWIA2024120201322.md): Button · sparks · Dec 1, 2024 · N161PQ · Cndair CL6002D24 · Windshield/Door Rain/Ice Removal
  > BUTTON LEFT WINDOW HEATER (CPT SIDE FRONT WINDOW) SPARKED AND THEN SMOKE FOLLOWED. I TURNED OFF BOTH IMMEDIATELY FOR THE REMAINDER OF THE FLIGHT. (FLIGHT 4048 - FILED CLOSED) COMPLIED WITH RIL 11891 REV. A. DEFERRED LH WINDOW HEAT PER MEL 30-41-1A. PULLE
- [SDR SWIA20241202011](https://openairdocs.org/sdr/SWIA20241202011.md): Button · sparks · Dec 1, 2024 · N161PQ · Cndair CL6002D24 · Windshield/Door Rain/Ice Removal
  > BUTTON LEFT WINDOW HEATER (CPT SIDE FRONT WINDOW) SPARKED AND THEN SMOKE FOLLOWED. I TURNED OFF BOTH IMMEDIATELY FOR THE REMAINDER OF THE FLIGHT. (FLIGHT 4048 - FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWIA2024112500019](https://openairdocs.org/sdr/SWIA2024112500019.md): Anti-Ice System · smoke · Nov 19, 2024 · N161PQ · Cndair CL6002D24 · Windshield/Door Rain/Ice Removal
  > LEFT WINDSHIELD HEAT BLOCK SMOKING ON CLIMB OUT.C: DEFERRED THE L WINDSHIELD ANTI-ICE SYSTEM PEER MEL 30-41-1A. MX ACTIONS COMPLIED WITH; PLACARD INSTALLED. DEFERRED THE L WINDSHIELD ANTI-ICE SYSTEM PEER MEL 30-41-1A. MX ACTIONS COMPLIED WITH; PLACARD INSTALL
- [SDR SWI2024F01280](https://openairdocs.org/sdr/SWI2024F01280.md): Heater · smoke · Nov 19, 2024 · N161PQ · Cndair CL6002D24 · Windshield/Door Rain/Ice Removal
  > D: L WINDSHIELD HEAT BLOCK SMOKING ON CLIMB OUT.C: DEFERRED THE L WINDSHIELD ANTI-ICE SYSTEM PEER MEL 30-41-1A. MX ACTIONS COMPLIED WITH; PLACARD INSTALLED.CAT: CDUE DATE: 29 NOV 2024***ODI EVENT/DO NOT CLEAR WITHOUT MOD APPROVAL*** (FLIGHT 4060 - FILED OPE
- [SDR SWIA2024111200922](https://openairdocs.org/sdr/SWIA2024111200922.md): Angle · cracked · Sep 22, 2024 · N161PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK FOUND IN RADIUS OF LOWER SPLICE ANGLE P/N CC670-34098-1 AT FS280, BL0. (CAMP. # 28883246) (C-CHECK RO 11/11/2024) REMOVED AND REPLACED LOWER SPLICE ANGLE P/N CC670-34098-1 AT FS280, BL0. REF. CRJ900 SRM 51-42-06-001-001-A01 AND DWG# CC670-34010 RE
- [SDR SWIA20240918](https://openairdocs.org/sdr/SWIA20240918.md): Floor Support · cracked · Sep 18, 2024 · N161PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > RH FLOOR SUPPORT ANGLE AT RBL 12.00 BETWEEN FS 260.00 - FS 280.00 HAS CRACK (28862750) (C-CHECK RO 11/11/2024) REMOVED AND INSTALLED NEW FLOOR SUPPORT ANGLE ON RBL 12 BETWEEN FS262-FS280 PER REF CRJ 900 SRM 51-42-06-001-001-A01 AND CRJ 900 SRM 51-42-21-
- [SDR SWI2024F01237](https://openairdocs.org/sdr/SWI2024F01237.md): Floorbeam · damaged · Sep 18, 2024 · N161PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > DAMAGED L/H OUTBOARD FLOOR SUPPORT ANGLE AT LBL12 ATTACHED TO FS280 CROSSBEAM (C-CHECK RO 11/11/2024) REMOVED AND REPLACED ANGLE P/N CC670-34099-1SB AT LBL12, FS280. REF. CRJ900 SRM 51-42-21-001-001-A01 AND DWG # KBA670-30026 REV. J.COMPLIED WITH SKYWES
- [SDR SWI2024F01240](https://openairdocs.org/sdr/SWI2024F01240.md): Floorbeam · corroded · Sep 15, 2024 · N161PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > EVIDENCE OF CORROSION ON RH FS280 CROSS BEAM AT FWD TOP ANGLE (C-CHECK RO 11/11/2024) REMOVED AND REPLACED RH CROSSBEAM AT FS280.00 WITH NEW REF. CRJ 900 SRM 51-42-06-001-001-A01, CRJ 900 SRM 51-42-13-001-001-A01, CRJ 900 SRM 51-42-22-001-001-A01 AND DW
- [SDR SWI2024F01239](https://openairdocs.org/sdr/SWI2024F01239.md): Floorbeam · corroded · Sep 15, 2024 · N161PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > EVIDENCE OF CORROSION ON LH FS280 CROSS BEAM AT FWD TOP ANGLE (C-CHECK RO 11/11/2024) REMOVED AND REPLACED LH CROSSBEAM AT FS280.00 WITH NEW REF. CRJ 900 SRM 51-42-06-001-001-A01, CRJ 900 SRM 51-42-13-001-001-A01, CRJ 900 SRM 51-42-22-001-001-A01 AND DW
- [SDR SWI2024F01238](https://openairdocs.org/sdr/SWI2024F01238.md): Floorbeam · corroded · Sep 15, 2024 · N161PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > EVIDENCE OF CORROSION ON FWD FLOOR SUPPORT ANGLE AT FS280 BETWEEN RBL9-LBL12 (C-CHECK RO 11/11/2024) REMOVED AND REPLACED FWD FLOOR SUPPORT ANGLE P/N CC670-34095-1SB AT FS280 BETWEEN RBL9 TO LBL9. REF. CRJ900 SRM 51-42-06-001-001-A01 AND DWG# CC670-3305
- [SDR SWIA202411120915](https://openairdocs.org/sdr/SWIA202411120915.md): Bracket · corroded · Sep 15, 2024 · N161PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > LEFT MLG WHEEL WELL BRACKET FOR Z PANEL HAS CORROSION AS MARKED (C-CHECK RO 11/11/2024) REMOVED AND INSTALLED NEW ANGLE P/N CC670-10338-1 ON LH MLG WELL SUPPORT STRUCTURE TIRE BURST FOR Z PANEL REF CRJ900 SRM 51-42-21-001-001-A01 AND DWG CC670-10320 REV
- [SDR SWI2024F01228](https://openairdocs.org/sdr/SWI2024F01228.md): Floorbeam · cracked · Sep 13, 2024 · N161PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > R/H FLOOR BEAM AT RBL12 ATTACHING FLANGE IS CRACKED AT 280 CROSSBEAM (MARKED) (C-CHECK RO 11/11/2024) REMOVED AND REPLACED PREVIOUS REPAIR R/H FLOOR BEAM SECTION AT RBL 12, FWD OF FS280. REF. CRJ900 SRM 53-11-43-201-003-A01 REPAIR TYPE IV. COMPLIED WIT
- [SDR SWI2024F01227](https://openairdocs.org/sdr/SWI2024F01227.md): Drag Angle · cracked · Sep 13, 2024 · N161PQ · Cndair CL6002D24 · Vertical Stabilizer Miscellaneous Structure
  > VERTICAL STAB RH AFT DRAG ANGLE HAS A CRACK (MARKED) (C-CHECK RO 11/11/2024) FABRICATED AND INSTALLED -6 AFT ANGLE DOUBLER AND -8 AFT ANGLE FILLER FROM 2024-T3.090" PO# 5-24830 REF. CRJ 900 SRM 55-31-00-201-001-A01. SEE CONTINUE CARD FOR WORK PERFORMED
- [SDR SWIA202411120913](https://openairdocs.org/sdr/SWIA202411120913.md): Floorbeam · cracked · Sep 13, 2024 · N161PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > L/H FLOOR BEAM AT LBL12 ATTACHING FLANGE IS CRACKED AT 280 CROSSBEAM (MARKED) (C-CHECK RO 11/11/2024) REMOVED AND REPLACED PREVIOUS REPAIR LBL12 FLOOR BEAM SECTION -33. REF. CRJ900 SRM 53-11-43-201-003-A01 FIGURE 53-11-43-995-819 REPAIR TYPE 4.COMPLIED
- [SDR SWI2024F01233](https://openairdocs.org/sdr/SWI2024F01233.md): Drag Angle · cracked · Sep 11, 2024 · N161PQ · Cndair CL6002D24 · Vertical Stabilizer Miscellaneous Structure
  > VERTICAL STAB RH FWD DRAG ANGLE HAS A SUSPECTED CRACK (MARKED). (C-CHECK RO 11/11/2024) CUT AWAY DAMAGE ON RH FWD. DRAG ANGLE AND PERFORMED A DOUBLER REPAIR TO RH FWD. DRAG ANGLE IAW CRJ900 SRM 55-31-00-201-001-A01. COMPLIED WITH SKYWEST TASK CARD: 51-
- [SDR SWI2024F01232](https://openairdocs.org/sdr/SWI2024F01232.md): Floorbeam · corroded · Sep 11, 2024 · N161PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > AVIONICS BAY FWD FLOOR BOARD SUPPORT ANGLE AT FS.280.00 HAS SPOTS OF CORROSION (MARKED). (C-CHECK RO 11/11/2024) REMOVED AND INSTALLED NEW ANGLE P/N: CC670-34256-3 AT AVIONICS BAY FS280.00 REF. CRJ900 SRM 51-42-21-001-001-A01, CRJ900 SRM 51-42-06-001-0
- [SDR SWI2024F01231](https://openairdocs.org/sdr/SWI2024F01231.md): Nut Plate · sheared · Sep 11, 2024 · N161PQ · Cndair CL6002D24 · Engine Thrust Reverser
  > R/H UPPER TRANSCOWL HAS 2 EA NUTPLATES SHEARED @ LOCKOUT (C-CHECK RO 11/11/2024) REPAIRED LOCKOUT HOLES ON R/H UPPER TRANSCOWL AND INSTALLED NEW HARDWARE REF. REO 690-54-21-518 REV. --, 2024-10-21. COMPLIED WITH SKYWEST TASK CARD: 51-900-1002-SKY.
- [SDR SWI2024F01230](https://openairdocs.org/sdr/SWI2024F01230.md): Spar · damaged · Sep 11, 2024 · N161PQ · Cndair CL6002D24 · Wing Spar
  > INSIDE FUEL PANEL 541BB, REAR WING SPAR HAS TOOLING DAMAGE AROUND NUMEROUS FASTENERS WHERE SEALANT HAS BEEN REMOVED (MARKED) (C-CHECK RO 11/11/2024) REPAIRED REAR WING SPAR AT WS27.96 ON LEFT WING REF REO 690-57-21-490 REV -- DATED 2024-09-27. COMPLIED
- [SDR SWI2024F01229](https://openairdocs.org/sdr/SWI2024F01229.md): Stand Off · cracked · Sep 11, 2024 · N161PQ · Cndair CL6002D24 · Engine Thrust Reverser
  > L/H UPPER TRANSCOWL INBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 11/11/2024) INSTALLED NEW L/H UPPER TRANSCOWL I/B "A" BRACKET REF REO# 670-54-21-971, REV B, DATED 11/28/23. COMPLIED FULLY W/SKYCARD 51-900-1002-SKY.
- [SDR SWI2024F01236](https://openairdocs.org/sdr/SWI2024F01236.md): Stiffener · sheared · Sep 11, 2024 · N161PQ · Cndair CL6002D24 · Nacelle/Pylon Miscellaneous Structure
  > L/H LWR TRANSCOWL Z STIFFENER HAS SHEARED RIVETS (C-CHECK RO 11/11/2024) REPAIRED L/H LOWER TRANSCOWL INNER SKIN COMMON TO ZED STIFFENER P/N CN624-2038-204, REF. REO 690-54-21-517, REV. --, 2024-10-02. COMPLIED WITH MAJOR REPAIR M-337 AND SKY CARD 51-9
- [SDR SWI2024F01235](https://openairdocs.org/sdr/SWI2024F01235.md): Stand Off · cracked · Sep 11, 2024 · N161PQ · Cndair CL6002D24 · Nacelle/Pylon Miscellaneous Structure
  > L/H LWR TRANSCOWL INBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 11/11/2024) REMOVED AND REPLACE I/B STAND-OFF ANGLE P/N CN624-2082-201 ON L/H LOWER TRANSCOWL, REF. REO 670-54-21-971, REV. B, 2023-11-28. COMPLIED WITH MAJOR REPAIR M-337 AND SKY CARD
- [SDR SWI2024F01234](https://openairdocs.org/sdr/SWI2024F01234.md): Stand Off · cracked · Sep 11, 2024 · N161PQ · Cndair CL6002D24 · Nacelle/Pylon Miscellaneous Structure
  > R/H UPPER TRANSCOWL INBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 11/11/2024) REMOVED AND REPLACED INBD STANDOFF P/N CN624-2082-201 ON R/H UPPER TRANSCOWL REF. REO 670-54-21-971 REV. B, 2023-11-28 AND CRJ 900 SRM 51-42-28-001-001-A01. COMPLIED WITH
- [SDR SWIA2024111200911](https://openairdocs.org/sdr/SWIA2024111200911.md): Support Bracket · cracked · Sep 11, 2024 · N161PQ · Cndair CL6002D24 · Wing Miscellaneous Structure
  > INSIDE FUEL PANEL 651AB, RH SLAT TRACK 1-3 CANNISTER, THE SUPPORT BRACKET POSSIBLY CRACKED (MARKED) (C-CHECK RO 11/11/2024) PERFORMED REPAIR TO SLAT CANISTER NO 3, AT RH SLAT TRACK 1-3 REF REO 670-57-42-577 REV -- DATED: 2016-12-02. COMPLIED WITH SKYWE
- [SDR SWI2024F0111229](https://openairdocs.org/sdr/SWI2024F0111229.md): Stand Off · cracked · Sep 11, 2024 · N161PQ · Cndair CL6002D24 · Nacelle/Pylon Miscellaneous Structure
  > L/H UPPER TRANSCOWL INBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 11/11/2024) INSTALLED NEW L/H UPPER TRANSCOWL I/B "A" BRACKET REF REO# 670-54-21-971, REV B, DATED 11/28/23. COMPLIED FULLY W/SKYCARD 51-900-1002-SKY.
- [SDR SWI2024F01204](https://openairdocs.org/sdr/SWI2024F01204.md): Hinge · gouged · Sep 10, 2024 · N161PQ · Cndair CL6002D24 · Fuselage, Door Hinge
  > PAX DOOR HINGE, FUSELAGE SIDE, LUG LANDING #27 HAS BEEN GOUGED BY THE SPRING PIN (MARKED) (C-CHECK RO 11/11/2024) REMOVED THE GOUGE IN THE PAX DOOR HINGE, THE FUSELAGE SIDE, THE LUG LANDING #27. REF. CRJ900 SRM 53-21-23-201-010-A01. THE PAX DOOR HINGE,
- [SDR SWI2024F01203](https://openairdocs.org/sdr/SWI2024F01203.md): Hinge · scratched · Sep 10, 2024 · N161PQ · Cndair CL6002D24 · Fuselage, Door Hinge
  > PAX DOOR HINGE (DOOR SIDE) HAS SEVERAL LUGS WITH SCRATCHES (MARKED) (C-CHECK RO 11/11/2024) REMOVED THE SCRATCHES ON THE PAX DOOR HINGE, DOOR SIDE REF. CRJ900 SRM 52-11-01-201-007-A01.THE PAX DOOR HINGE, DOOR SIDE, OUTER LUGS ARE IN LIMITS REF. CRJ900
- [SDR SWIA20240910](https://openairdocs.org/sdr/SWIA20240910.md): Door Sill · corroded · Sep 10, 2024 · N161PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AFT BAGGAGE-BAY LOWER SILL HAS AREAS OF CORROSION. HN00186463 (C-CHECK RO 11/11/2024) REMOVED AND REPLACED AFT BAGGAGE BAY DOOR LOWER SILL. REF. CRJ900 SRM 51-42-06-001-001-A01, SRM 51-42-13-001-001-A01, SRM 51-42-21-001-001-A01 AND DWG# MM670-35085 REV
- [SDR SWI2024F01226](https://openairdocs.org/sdr/SWI2024F01226.md): Vane · damaged · Sep 5, 2024 · N161PQ · Cndair CL6002D24 · Trailing Edge Flaps
  > RIGHT INBOARD FLAP VANE INBOARD ACTUATOR BEAM HAS A MARK PERPENDICULAR TO THE BEAM ON ITS LOWER SURFACE BETWEEN THE FLAP AND VANE. (MARKED IN RED) (C-CHECK RO 11/11/2024) REPAIRED RH INBD FLAP VANE INBD ACTUATOR BEAM REF REO 670-57-52-257 REV -A DATED:
- [SDR SWI2024F01225](https://openairdocs.org/sdr/SWI2024F01225.md): Vane · damaged · Sep 5, 2024 · N161PQ · Cndair CL6002D24 · Trailing Edge Flaps
  > LEFT INBOARD FLAP VANE INBOARD ACTUATOR BEAM HAS 3 MARKS THAT ARE PERPENDICULAR TO THE BEAM ON ITS LOWER SURFACE BETWEEN THE FLAP AND VANE. (MARKED IN RED) (C-CHECK RO 11/11/2024) REPAIRED LH INBD FLAP VANE INBD ACTUATOR BEAM IAW REO 670-57-52-257 REV
- [SDR SWIA2024111200903](https://openairdocs.org/sdr/SWIA2024111200903.md): Structure · cracked · Sep 3, 2024 · N161PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK ON THE TRU BAY FLOOR LEFT SIDE FS193.25 AT CUT OUT FOR FRAME. (MARKED IN RED) (C-CHECK RO 11/11/2024) REPAIRED TRU BAY FLOOR LEFT SIDE FS193.25 REF CRJ-900 SRM 53-11-43-201-001-A01.COMPLIED WITH 51-900-1002-SKY
- [SDR SWIA2024111200902](https://openairdocs.org/sdr/SWIA2024111200902.md): Skin · dented · Sep 2, 2024 · N161PQ · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > FS1015 - 1031 STRG 4RH 2EA EXTERIOR FUSELAGE SKIN DENTS ON TOP OF A FASTENER (MARKED) (C-CHECK RO 11/11/2024) REPAIRED FS1015 - 1031 STRG 4RH 2EA EXTERIOR FUSELAGE SKIN DENTS ON TOP REF CRJ 900 SRM 53-00-01-201-001-A03, FOR REPAIR TYPE 9- NOTED ON FIGU
- [SDR SWIA2024111200831](https://openairdocs.org/sdr/SWIA2024111200831.md): Beam · gouged · Aug 31, 2024 · N161PQ · Cndair CL6002D24 · Fuselage Main, Structure
  > AFT BAGGAGE BAY STRUCTURE UPPER/OUTBOARD BEAM HAS GOUGES AT FS 1000.00 AND FS 1047.00. (C-CHECK RO 11/11/2024) REMOVED BAD AND INSTALLED REPLACEMENT OUTBOARD BEAM FOR AFT BAGGAGE BAY STRUCTURE AT FS 1000.00 TO FS 1047.00 REF CRJ900 SRM 51-42-21-001-001-
- [SDR SWIA2024111200827](https://openairdocs.org/sdr/SWIA2024111200827.md): Skin · dented · Aug 27, 2024 · N161PQ · Cndair CL6002D24 · Spoilers
  > ADM #7770. LH IB GROUND SPOILER AFT IB SECTOR, IB CENTER SECTOR, OB FWD SECTOR. FURTHEST OB DENT IS LOCATED 9.25" FROM OB EDGE, AND 4" FROM FWD EDGE WITH DIMENSION OF L=1" W=1" AND DEPTH OF.019". THE MORE CENTRALIZED OF THE THREE DENTS IS 17.5" FROM IB EDGE A
- [SDR SWIA202404190007](https://openairdocs.org/sdr/SWIA202404190007.md): Stringer · damaged · Apr 7, 2024 · N161PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > DAMAGE 8 - STGR26R HAS PROCESS INDUCED DAMAGE NEAR FS437. (FILED CLOSED)PERMANENTLY REPAIRED FUSELAGE STGR26R BETWEEN FS421 AND FS453 IN REFERENCE TO REO 690-53-21-1746 REV -- DATED 2024-04-015. M-337 AND RII CARD 51-900-1002-SKY ATTACHED. DTA DUE WITHIN 12 M
- [SDR SWIA20240419329](https://openairdocs.org/sdr/SWIA20240419329.md): Skin · gouged · Mar 29, 2024 · N161PQ · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > DAMAGE 4 & 5) GOUGE MEASUREMENTS 9.5 INCHES LONG AND 0.5 INCH WIDE. DEPTH IS FROM 0.005 INCH TO 0.059 INCH DEEP. LOCATED 0.5 INCH AFT OF FS 421 BETWEEN STGR24R AND STGR 27.DAMAGE 5) GOUGE 13.5 INCHES LONG AND 0.5 INCH WIDE DEPTH NOT MEASURED, DUE TO ALL BEING
- [SDR SWI2023F00568](https://openairdocs.org/sdr/SWI2023F00568.md): Unknown · leaking · Dec 12, 2023 · N161PQ · Cndair CL6002D24 · Flight Compartment Windows
  > FO SIDE WINDSHIELD FAILED LEAK CHECK AFTER INSTALLATION (FILED CLOSED)REMOVED AND REPLACED RT WINDSHIELD IAW AMM 56-11-01. OPS CHECK AND LEAK CHECK GOOD. COMPLIED WITH TASK CARD 56-220-1000-SKY.
- [SDR SWI2023F00566](https://openairdocs.org/sdr/SWI2023F00566.md): Unknown · smoke · Dec 11, 2023 · N161PQ · Cndair CL6002D24 · Flight Compartment Windows
  > FO SIDE WINDSHIELD HEAD WOOD BLOCK HAD SMOKE COMING FROM IT AND IS BURNT ON THE SIDE. (FLIGHT 4604 FILED CLOSED)
- [SDR SWIA202312120011](https://openairdocs.org/sdr/SWIA202312120011.md): Unknown · smoke · Dec 11, 2023 · N161PQ · Cndair CL6002D24 · Flight Compartment Windows
  > FO SIDE WINDSHIELD HEAD WOOD BLOCK HAD SMOKE COMING FROM IT AND IS BURNT ON THE SIDE. (FLIGHT 4604 FILED OPEN)
- [SDR SWIA202306080001](https://openairdocs.org/sdr/SWIA202306080001.md): Unknown · odor · Jun 7, 2023 · N161PQ · Cndair CL6002D24 · Humidity Control System
  > OVERHEATING PLASTIC ODOR DURING FLIGHT LEFT SIDE OF FLIGHT DECK. (FLT 3801 FILED CLOSED) TROUBLESHOT FDE PER FIM 21-21-00. COMPLIED WITH OPERATIONAL TEST OF THE AIR-CONDITIONING DISTRIBUTION SYSTEM PER AMM 21-51-00 PROCEDURE 4. COULD NOT DUPLICATE THE ODOR. V
- [SDR SWIA202304240018](https://openairdocs.org/sdr/SWIA202304240018.md): Unknown · fumes · Apr 18, 2023 · N161PQ · Cndair CL6002D24 · Humidity Control System
  > DURING TAKEOFF AND THROUGHOUT CLIMB TO CRUISE ALTITUDE, AIRCRAFT EMITTED A PUNGENT FUMY ODOR RESEMBLING OIL AND/OR EXHAUST INTO THE FLIGHT DECK. ODOR DISSIPATED IN CRUISE BUT RETURNED DURING FINAL APPROACH FROM 3,000 FT TO LANDING. APU WAS OFF IN BOTH OCCURREN
- [SDR SWIA202301167116](https://openairdocs.org/sdr/SWIA202301167116.md): A/C Pack · smoke · Jan 13, 2023 · N161PQ · Cndair CL6002D24 · Cabin Cooling System
  > TROUBLESHOOT PACK 1 AUTO FAIL. STATES COCK PIT SMELLS LIKE OIL BADLY AND SMOKEY MIST IN THE AIR FOR ABOUT 20 SECONDS THROUGHOUT THE COCKPIT AND CABIN. (FILED CLOSED)TROUBLESHOT PACK 1 AUTO FAIL, PILOT STATED COCKPIT SMELLS LIKE OIL AND SMOKEY MIST IN THE AIR.
- [SDR SWIA2022122767025](https://openairdocs.org/sdr/SWIA2022122767025.md): Pulley · damaged · Dec 17, 2022 · N161PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR ASSIST MOTOR CABLE PULLEY ATTATCHMENT POINT HAS SHEET METAL DAMAGE AND IS PULLED AWAY FROM DOOR STRUCTURE (FILED CLOSED) REPAIRED PAX DOOR CABLE PULLY ATTACHMENT POINT IN REFERENCE WITH REO 690-52-11-804 AND COMPLIED WITH M337. OPS CHECKS OF PAX D
- [SDR SWIA202155870](https://openairdocs.org/sdr/SWIA202155870.md): Spar · cracked · Jan 23, 2021 · N161PQ · Cndair CL6002D24 · Wing Spar
  > COMPLY WITH BOMBARDIER SERVICE BULLETIN 670BA-57-016 REV D DATED 09/12/2014 FOR THE LH AND RH REAR SPAR LINK ASSY REPLACEMENTS (BOTH ARE CRACKED AT CLEVIS BEARINGS) (C-CHECK) RO 2/1/2021 COMPLIED WITH BOMBARDIER SERVICE BULLETIN 670BA-57-016 REV D DATED 09
- [SDR SWIA202155868](https://openairdocs.org/sdr/SWIA202155868.md): Stringer Splice · corroded · Jan 2, 2021 · N161PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > MAIN AVIONICS BAY STR 23R SPLICE AT FS333.00 CORRODED (C-CHECK) RO 2/1/2021 MAIN AVIONICS BAY STR 23R SPLICE AT FS333.00 AS FOUND TO BE EXFOLIATED WITH 100% MATERIAL LOSS. REF: CRJ 900 SRM 53-00-00-101-001-A01. CORRODED SPLICE WAS REMOVED AND NEW SPLICE WA
- [SDR SWIA202155867](https://openairdocs.org/sdr/SWIA202155867.md): Stringer · corroded · Jan 2, 2021 · N161PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > MAIN AVIONICS BAY STR 27 CORRODED BETWEEN FS310.00 AND FS319.70 (C-CHECK) RO 2/1/2021 INSTALLED NEW STRINGER 27 IN MAIN AVIONICS BAY BETWEEN FS306.00 AND FS319.70 REF DWG SH670-31630 REV. K, CRJ 900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01. C
- [SDR SWIA202055864](https://openairdocs.org/sdr/SWIA202055864.md): Stringer · corroded · Dec 30, 2020 · N161PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 23R AT FS319.70-FS333.00 HAS CORROSION. (C-CHECK) RO 2/1/2021 REMOVED AND REPLACED STGR 23R FROM FS280 TO FS333. REF.REO 690-53-21-1301 REV.-- DATED 01/11/2021 AND DWG# SH670-31630 REV. K SHEET 1, AND CRJ 900 SRM 51-42-06-001-001-A01.SEE CONTINUA
- [SDR SWIA202055863](https://openairdocs.org/sdr/SWIA202055863.md): Shear Tie · corroded · Dec 29, 2020 · N161PQ · Cndair CL6002D24 · Fuselage Internal Mounting Structure
  > CORROSION FOUND ON CLEAT AFT OF FRAME AT FS310.00, STGR 20R. (C-CHECK) RO 2/1/2021 REMOVED AND REPLACED STR 20R CLEAT AT FS310.00 REF. DRWG SH670-31950 REV. Y AND CRJ 900 SRM 51-42-06-001-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY
- [SDR SWIA202055862](https://openairdocs.org/sdr/SWIA202055862.md): Cleat · corroded · Dec 28, 2020 · N161PQ · Cndair CL6002D24 · Fuselage Main, Attach Fittings
  > CLEAT LOCATED ON STGR22R AT FS 319.7 IS CORRODED (C-CHECK) RO 2/1/2021.REMOVED AND REPLACED CLEAT AT FS319.7, STGR 22R REF. CRJ900 SRM 51-42-06-001-001-A01 AND DWG# SH670-31950 SHEET 3 REV. Y / COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY (CL600-2D24)
- [SDR SWIA202055924](https://openairdocs.org/sdr/SWIA202055924.md): Bracket · corroded · Dec 26, 2020 · N161PQ · Cndair CL6002D24 · Fuselage Main, Attach Fittings
  > BRACKET ASSY ON STR20R BETWEEN FS280.00 AND FS295.00 HEAVILY CORRODED (C-CHECK) RO 2/1/2021 REMOVED AND REPLACED BRACKET ASSY. AT STGR 20R BETWEEN FS280 AND FS295 REF. CRJ900 SRM 51-42-06-001-001-A01

Next page: https://openairdocs.org/aircraft/N161PQ/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 = 'N161PQ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N161PQ/reports

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