# Service difficulty reports: N187PQ

A list on [N187PQ](https://openairdocs.org/aircraft/N187PQ.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 3 · 144 reports

- [SDR SWIA2025122400002](https://openairdocs.org/sdr/SWIA2025122400002.md): Steering Sys · faulted · Dec 22, 2025 · N187PQ · Cndair CL6002D24 · Landing Gear Steering System
  > STEERING INOP CAUTION MESSAGE AFTER TAKEOFF. COMPLIED WITH QRH, REQUIRED TOW TO GATE. (FLIGHT 3699 - FILED CLOSED)FOUND RH NLG PROXIMITY SENSOR HARNESS WIRING TO BE INOP. SEE EAML 1779428 FOR REPLACEMENT OF HARNESS. OPS CHECKED NOSE WHEEL STEERING, CHECKED OK
- [SDR SWIA20251223022](https://openairdocs.org/sdr/SWIA20251223022.md): Warning Message · illuminated · Dec 22, 2025 · N187PQ · Cndair CL6002D24 · Landing Gear Steering System
  > STEERING INOP CAUTION MESSAGE AFTER TAKEOFF. COMPLIED WITH QRH, REQUIRED TOW TO GATE. (FLIGHT 3699) OPEN.
- [SDR SWI2025F01849](https://openairdocs.org/sdr/SWI2025F01849.md): Steering Sys · warning message · Dec 21, 2025 · N187PQ · Cndair CL6002D24 · Landing Gear Steering System
  > STEERING INOP CAUTION MESSAGE ON AFTER ROTATION ON TAKE-OFF. QRH COMPLETE. LANDED AND HAD TO BE TOWED TO THE GATE. (FLIGHT 4625 - FILED CLOSED)FOUND B1 CODE 007467 AND CYCLED A/C POWER AND TROUBLESHOT PER CRJ 900 FIM 32-52-01 PREFORMED OPS TEST OF NOSE WHEEL
- [SDR SWIA2025081800718](https://openairdocs.org/sdr/SWIA2025081800718.md): Rib · cracked · Jul 18, 2025 · N187PQ · Cndair CL6002D24 · Wing, Rib/Bulkhead
  > RH WING BAT RIB AT WS14.50 CRACKED ALL THE WAY THROUGH TO THE LIGHTNING/PASS-THROUGH HOLE. CRACK LOCATED APPROXIMATELY 7 INCHES AFT OF THE REAR SPAR. THIS DISCREPANCY IS CONSIDER A MAJOR REPAIR. (FILED CLOSED)REPLACEMENT OF RH BAT RIB AT WS14.50 WAS COMPLETED
- [SDR SWI2025F01005](https://openairdocs.org/sdr/SWI2025F01005.md): Rib · cracked · Jul 18, 2025 · N187PQ · Cndair CL6002D24 · Wing, Rib/Bulkhead
  > RH WING BAT RIB AT WS14.50 CRACKED ALL THE WAY THROUGH TO THE LIGHTNING/PASS-THROUGH HOLE. CRACK LOCATED APPROXIMATELY 7 INCHES AFT OF THE REAR SPAR. THIS DISCREPANCY IS CONSIDER A MAJOR REPAIR. (FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWIA2024090900006](https://openairdocs.org/sdr/SWIA2024090900006.md): Insert · damaged · Sep 6, 2024 · N187PQ · Cndair CL6002D24 · Overheat Detection
  > L BLEED DUCT WARNING MSG CLIMBING THROUGH 14,500. COMPLIED WITH QRH. DIVERTED TO CDC. (FLIGHT 4320 - FILED CLOSED) TROUBLESHOT IN REFERENCE TO FIM 36-21-01. INTEROGATED MDC AND FOUND LH BLEED TO HAVE A LEAK/SHORT EVENT ON LOOP B AND A LEAK EVENT FOR LOOP
- [SDR SWI202408260780](https://openairdocs.org/sdr/SWI202408260780.md): Frame · damaged · Jul 28, 2024 · N187PQ · Cndair CL6002D24 · Fuselage Main, Frame
  > PERFORM FRAME SPLICE REPAIR TO FRAME FS985.00 TO FOM. STRINGER 23L REPAIR FOR JOB HN00166318 (MX TRANS #28602248) (C-CHECK RO 8/24/2024) FABRICATED REPAIR PARTS AND INSTALLED ON FS985, STGR 19L TO STGR26L REF. CRJ-900 SRM, 51-42-06-001-001-A01, CRJ-900
- [SDR SWI2024082600779](https://openairdocs.org/sdr/SWI2024082600779.md): Bracket · corroded · Jul 22, 2024 · N187PQ · Cndair CL6002D24 · Fuselage Main, Attach Fittings
  > BRACKET ASSY SH670-96034 BETWEEN FS280 - FS 295 AT STR 22R IS 100% CORRODED REPLACE WITH NEW (C-CHECK RO 8/24/2024) REMOVED AND INSTALLED NEW FABRICATED BRACKET ASSY BETWEEN FS280 - FS295 AT STR 22R REF CRJ-900 SRM 51-42-06-001-001-A01 AND DWG SH670-96
- [SDR SWI2024082600799](https://openairdocs.org/sdr/SWI2024082600799.md): Frame · damaged · Jul 19, 2024 · N187PQ · Cndair CL6002D24 · Fuselage Main, Frame
  > CUT, REMOVE AND REINSTALL MAIN AVIONICS BAY FS333.00 FRAME FROM STR 20R TO STR 25R TO FOM STRINGER REPLACEMENTS ON RH SIDE. (C-CHECK RO 8/24/2024) REMOVED AND INSTALLED NEW FRAME FS333 FROM STR 20R - STR25R AND FRAME SPLICE (-2) AND REINFORCEMENT ANGLE
- [SDR SWI202408260798](https://openairdocs.org/sdr/SWI202408260798.md): Stringer · corroded · Jul 19, 2024 · N187PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > MAIN AVIONICS BAY STR 21R CORRODED BETWEEN FS295.00 AND FS333.00 (C-CHECK RO 8/24/2024) REMOVED AND REPLACED STGR 21R FROM FS280-FS333 REF CRJ-900 SRM 51-42-21-001-001-A01, CRJ-900 SRM 51-42-21-001-001-A01 AND DWG SH670-31630 REV K. COMPLIED WITH SKYWES
- [SDR SWIA202408260019](https://openairdocs.org/sdr/SWIA202408260019.md): Stringer · corroded · Jul 19, 2024 · N187PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > MAIN AVIONICS BAY STR 24R CORRODED BETWEEN FS333.00 AND FS364.00. (C-CHECK RO 8/24/2024) REMOVED AND SPLICED IN NEW SECTION OF STGR AT 24R FROM FS333 TO FS671 REF CRJ900 SRM 53-00-03-201-001-A02 FIG 53-00-03-995-806 (SHT 7 OF 23). COMPLIED WITH SKYWEST
- [SDR SWI202408260797](https://openairdocs.org/sdr/SWI202408260797.md): Stringer · corroded · Jul 18, 2024 · N187PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > MAIN AVIONICS BAY STR 23R CORRODED BETWEEN FS280.00 AND FS333.00 (C-CHECK RO 8/24/2024) INSTALLED NEW STRINGER STR 23R FROM FS280 - FS333 REF CRJ-700 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01 AND DWG SH670-31630 REV K COMPLIED WITH SKYCARD
- [SDR SWI202408260796](https://openairdocs.org/sdr/SWI202408260796.md): Stringer Splice · corroded · Jul 18, 2024 · N187PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > MAIN AVIONICS BAY STR 21R SPLICE AT FS333.00 CORRODED (C-CHECK RO 8/24/2024) REMOVED AND INSTALLED NEW STR 21R SPLICE AT FS333 REF CRJ-900 SRM 51-42-06-001-001-A01 AND DWG SH670-32420 REV E. COMPLIED WITH SKYWEST TASK CARD: 51-900-1002-SKY. LEAK CHECK G
- [SDR SWI202408260795](https://openairdocs.org/sdr/SWI202408260795.md): Stringer · corroded · Jul 18, 2024 · N187PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > MAIN AVIONICS BAY STR 21R CORRODED BETWEEN FS333.00 AND FS349.00 (C-CHECK RO 8/24/2024) REMOVED AND INSTALLED NEW STR 21R FROM FS333 - FS379 REF CRJ-900 SRM 51-42-06-001-001-A01 AND DWG SH690-31350 REV M. COMPLIED WITH SKYWEST TASK CARD: 51-900-1002-SKY
- [SDR SWI202408260794](https://openairdocs.org/sdr/SWI202408260794.md): Stringer · corroded · Jul 18, 2024 · N187PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > MAIN AVIONICS BAY STR 23R SPLICE AT FS333.00 CORRODED (C-CHECK RO 8/24/2024) REMOVED AND INSTALLED NEW STR 23R SPLICE AT FS333 REF CRJ-900 SRM 51-42-06-001-001-A01 AND DWG SH670-32420 REV E. COMPLIED WITH SKYWEST TASK CARD: 51-900-1002-SKY. LEAK CHECK
- [SDR SWI2024F08260793](https://openairdocs.org/sdr/SWI2024F08260793.md): Stringer · corroded · Jul 18, 2024 · N187PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > MAIN AVIONICS BAY STR 23R CORRODED BETWEEN FS333.00 AND FS349.00 (C-CHECK RO 8/24/2024) REMOVED AND INSTALLED NEW STR 23R FROM FS333 - FS379 REF CRJ-900 SRM 51-42-06-001-001-A01 AND DWG SH690-31350 REV M. COMPLIED WITH SKYWEST TASK CARD: 51-900-1002-SKY
- [SDR SWIA202408260718](https://openairdocs.org/sdr/SWIA202408260718.md): Stringer Splice · corroded · Jul 18, 2024 · N187PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > MAIN AVIONICS BAY STR 24R SPLICE AT FS333.00 CORRODED (C-CHECK RO 8/24/2024) REMOVED AND INSTALLED NEW STR 24R SPLICE AT FS333 REF CRJ-900 SRM 51-42-06-001-001-A01 AND DWG SH670-32420 REV E. COMPLIED WITH SKYWEST TASK CARD: 51-900-1002-SKY. LEAK CHECK G
- [SDR SWI202408260792](https://openairdocs.org/sdr/SWI202408260792.md): Stringer · corroded · Jul 17, 2024 · N187PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > *AFTER REMOVAL OF AVIONOICS EQUIPMENT FOR REPAIR ACCESS FOUND STGR 22R HAS CORROSION BETWEEN FS310 AND FS319.70. (C-CHECK RO 8/24/2024) INSTALLED NEW STRINGER STR 22R FROM FS280 - FS333 REF CRJ-700 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01 A
- [SDR SWI202408260791](https://openairdocs.org/sdr/SWI202408260791.md): Stringer · corroded · Jul 17, 2024 · N187PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > *AFTER REMOVAL OF AVIONOICS EQUIPMENT FOR REPAIR ACCESS FOUND STGR 22R HAS CORROSION AT FS349. (C-CHECK RO 8/24/2024) REMOVED AND INSTALLED NEW STR 22R BETWEEN FS333.00 AND FS349.00 REF CRJ-900 SRM 51-42-06-001-001-A01 AND DWG SH690-31350 REV M. COMPLIE
- [SDR SWI202408260790](https://openairdocs.org/sdr/SWI202408260790.md): Stringer Splice · corroded · Jul 17, 2024 · N187PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > *AFTER REMOVAL OF AVIONOICS EQUIPMENT FOR REPAIR ACCESS FOUND STGR 22R SPLICE UNDER FRAME AT FS333 HAS CORROSION. (C-CHECK RO 8/24/2024) REMOVED AND REPLACED STGR 22R SPLICE AT FS333 REF. CRJ-900 SRM, 51-42-06-001-001- A01 AND DWG SH670-32420 REV E. COM
- [SDR SWIA202408260717](https://openairdocs.org/sdr/SWIA202408260717.md): Attach Angle · corroded · Jul 17, 2024 · N187PQ · Cndair CL6002D24 · Fuselage Main, Attach Fittings
  > *AFTER REMOVAL OF AVIONOICS EQUIPMENT FOR REPAIR ACCESS FOUND CLIP ATTACHING STGR 22R TO FRAME AT FS319 HAS CORROSION. (C-CHECK RO 8/24/2024) REMOVED AND INSTALLED STRINGER CLEAT AT STR 22R FS319 REF CRJ-900 SRM 51-42-06-001-001-A01 AND DWG SH670-35624
- [SDR SWIA202408260714](https://openairdocs.org/sdr/SWIA202408260714.md): Seat Track · damaged · Jul 14, 2024 · N187PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > DAMAGED HOLES FOUND BEHIND LH SIDE SEAT RAIL (847.00+48-FS865) AT LOCATION FS 847.00+62 AND FS 881.00 (C-CHECK RO 8/24/2024) COMPLIED WITH ALL STEPS OF REO 690-53-51-428 REV -- DATED: 2024-07-29, REPAIR FOR DAMAGED HOLES IN SIDE SEAT TRACK SUPPORT STRUC
- [SDR SWIA202408260712](https://openairdocs.org/sdr/SWIA202408260712.md): Angle · corroded · Jul 12, 2024 · N187PQ · Cndair CL6002D24 · Emergency Exits
  > SERVICE DOOR LOWER MOUNTING ANGLE, BETWEEN FS 349.0 TO FS 319.0 IS CORRODED. PART# SH670-31996-3. (C-CHECK RO 8/24/2024) SERVICE DOOR LOWER MOUNTING ANGLE, BETWEEN FS 349.0 TO FS 319.0 CORROSION IS OUT OF LIMITS. REMOVED AND INSTALLED REPLACEMENT ANGLE
- [SDR SWIA202408260710](https://openairdocs.org/sdr/SWIA202408260710.md): Fairing · chafed · Jul 10, 2024 · N187PQ · Cndair CL6002D24 · Nacelle/Pylon, Main Frame
  > DURING AUDIT OF 1C TASK CARD 54-440-301 (INTERNAL ZONAL INSPECTION OF THE LEFT NACELLE (EWIS)), FOUND LOWER HINGE LINE FAIRING RUBBING ON BOTTOM SIDE OF FWD. ENGINE MOUNT. (C-CHECK RO 8/24/2024) REWORKED LEFT FWD ENGINE MOUNT LOWER SIDE REF REO 670-71-
- [SDR SWIA202408260707](https://openairdocs.org/sdr/SWIA202408260707.md): Panel · damaged · Jul 7, 2024 · N187PQ · Cndair CL6002D24 · Wing, Plate/Skin
  > FOUND ELONGATED HOLES ON PANEL 511AZ AND ASSOCIATED STRUCTURE (MARKED) CAMP 28489966 (C-CHECK RO 8/24/2024) PERFORMED REPAIR FOR ELONGATED FASTENER HOLES TO LH COLLECTOR TANK PANEL AND ACCESS PANEL 511AZ IAW ALL STEPS OF REO 690-57-11-127 REV--, DATED 2
- [SDR SWIA202408260703](https://openairdocs.org/sdr/SWIA202408260703.md): Floor Support · cracked · Jul 3, 2024 · N187PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > ANGLE FLOOR SUPPORT ON LBL 12.00 BETWEEN FS 250 - FS 280.00 HAS CRACK (C-CHECK RO 8/24/2024) REMOVED AND INSTALLED NEW LH ANGLE FLOOR SUPPORT P/N CC670-33199-3 ON LBL 12.00 FS 250.00 - FS 280.00 REF CRJ900 SRM 51-42-06-001-001-A01 AND DWG CC670-33052
- [SDR SWIA202408260701](https://openairdocs.org/sdr/SWIA202408260701.md): Floorbeam · cracked · Jul 1, 2024 · N187PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > CRACK FOUND ON R/H FLOOR SUPPORT ANGLE COMMON TO CENTER FLOORBEAM AT FS 280.0 RBL 12.0 (C-CHECK RO 8/24/2024) REMOVED AND REPLACED FLOOR SUPPORT ANGLE AT RBL 12.0 FS 280.0 REF CRJ900 SRM 51-42-06-001-001-A01 AND DWG CC670-33052 REV-G. COMPLIED WITH SKYW
- [SDR SWIA202408260027](https://openairdocs.org/sdr/SWIA202408260027.md): Floor Support · corroded · Jun 27, 2024 · N187PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR BEAM LBL 27.0 BETWEEN FS1000.00 AND FS1031.00, TOP EXTERNAL SURFACE. AREAS MARKED (C-CHECK RO 8/24/2024) REMOVED AND REPLACED FLOOR BEAM SECTION AT LBL27 REF CRJ900 SRM 53-00-41-201-001-A03 AND DWG MM690-35041 REV AB. COMPLIED WITH AL
- [SDR SWIA202408260025](https://openairdocs.org/sdr/SWIA202408260025.md): Bulkhead · corroded · Jun 25, 2024 · N187PQ · Cndair CL6002D24 · Fuselage Main, Bulkhead
  > CORROSION FOUND ON R/H LOWER BULKHEAD WEB AT FS 280.0 (C-CHECK RO 8/24/2024) REMOVED AND INSTALLED NEW AT FS 280.0 R/H LOWER BULKHEAD WEB REF CRJ 900 SRM 53-11-10-201-004-A01. COMPLIED WITH 51-900-1002-SKY.PART EXFOLIATED. 100% MATERIAL LOSS. OUT OF
- [SDR SWIA202408260020](https://openairdocs.org/sdr/SWIA202408260020.md): Coaming · chafed · Jun 20, 2024 · N187PQ · Cndair CL6002D24 · Nacelle/Pylon, Main Frame
  > L/H LWR TRANSCOWL INNER COAMING IS CHAFED @ FWD LATCH (C-CHECK RO 8/24/2024) REPAIRED L/H LWR TRANSCOWL INNER COAMING PER REO 690-54-21-504 REV -- DATED 2024-07-25. COMPLIED WITH STEPS 1-26. SEE CONTINUE CARD FOR INDIVIDUAL SIGN OFFS. COMPLIED WITH TASK
- [SDR SWI202408260789](https://openairdocs.org/sdr/SWI202408260789.md): Floorbeam · cracked · Jun 19, 2024 · N187PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > CRACK FOUND IN LOWER RADIUS OF R/H CENTER COCKPIT FLOORBEAM AT FS 280.0 STR RBL 12.0 (C-CHECK RO 8/24/2024) REMOVED AND INSTALLED NEW RH CENTER FLOOR BEAM SECTION REF CRJ 900 SRM 53-11-43-201-003-A01 REPAIR 4. COMPLIED WITH SKYWEST TASK CARD: 51-900-100
- [SDR SWIA202408260017](https://openairdocs.org/sdr/SWIA202408260017.md): Doubler · corroded · Jun 17, 2024 · N187PQ · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > THE WIFI AFT ATG ANTENNA DOUBLER HAS CORROSION ON THE EXTERIOR SURFACE AND FRETTING CORROSION ON MATING SURFACE FOR ANTENNA. (MARKED) (C-CHECK RO 8/24/2024) REMOVED AND INSTALLED NEW EXTERNAL DOUBLER AT WIFI AFT ATG ANTENNA BETWEEN FS1000-FS1050 STGR 25
- [SDR SWI202408260788](https://openairdocs.org/sdr/SWI202408260788.md): Fitting · gouged · Jun 16, 2024 · N187PQ · Cndair CL6002D24 · Fuselage Main, Attach Fittings
  > THE RH MLG SIDE STAY FITTING IS GOUGED ON THE INBD SIDE. (MARKED) (C-CHECK RO 8/24/2024) REPAIRED THE RH MLG SIDE STAY FITTING ON THE INBD SIDE BY COMPLYING WITH REO 690-57-11-128 REV -- DATED 2024-07-14, COMPLIED WITH 51-900-1002-SKY
- [SDR SWI202408260787](https://openairdocs.org/sdr/SWI202408260787.md): Attach Angle · corroded · Jun 16, 2024 · N187PQ · Cndair CL6002D24 · Fuselage, Landing Gear Attach Fittings
  > THE LH MLG WHEEL WELL TIRE BURST PANEL ATTACH ANGLE ON THE FWD SIDE OF WHEEL WELL IS CORRODED. (MARKED) (C-CHECK RO 8/24/2024) TIRE BURST ANGLE P/N CC670-10338-1 ON L/H WING REAR SPAR HAS EXFOLIATED CORROSION ON MULTIPLE ELEMENTS ACROSS ENTIRE LENGTH OF
- [SDR SWI202408260786](https://openairdocs.org/sdr/SWI202408260786.md): Attach Angle · corroded · Jun 16, 2024 · N187PQ · Cndair CL6002D24 · Fuselage, Landing Gear Attach Fittings
  > THE RH MLG WHEEL WELL TIRE BURST PANEL ATTACH ANGLE ON THE FWD SIDE OF WHEEL WELL IS CORRODED. (MARKED) (C-CHECK RO 8/24/2024) TIRE BURST ANGLE P/N CC670-10338-2 ON R/H WING REAR SPAR HAS EXFOLIATED CORROSION ON MULTIPLE ELEMENTS ACROSS ENTIRE LENGTH OF
- [SDR SWI202408260785](https://openairdocs.org/sdr/SWI202408260785.md): Crossbeam · corroded · Jun 16, 2024 · N187PQ · Cndair CL6002D24 · Fuselage Main, Structure
  > CORROSION FOUND ON R/H CROSSBEAM FS 280.0 BETWEEN RBL 9.0 - LBL 9.0 (C-CHECK RO 8/24/2024) REMOVED AND INSTALLED NEW R/H CROSSBEAM AT REWORK AREA REF BOMBARDIER DWG CC670-34010 REV K / CRJ 900 SRM 51-42-06-001-001-A01 / CRJ 900 SRM 51-42-21-001-001-A01
- [SDR SWI202408260784](https://openairdocs.org/sdr/SWI202408260784.md): Crossbeam · corroded · Jun 16, 2024 · N187PQ · Cndair CL6002D24 · Fuselage Main, Structure
  > CORROSION FOUND ON L/H CROSSBEAM FS 280.0 BETWEEN RBL 9.0 - LBL 9.0 (C-CHECK RO 8/24/2024) REMOVED AND INSTALLED NEW LH CROSSBEAM AT FS 280.00 REF CRJ900 SRM 51-42-06-001-001-A01, SRM 51-42-22-001-001-A01, SRM 51-42-13-001-001-A01 AND DWG CC670-34010 RE
- [SDR SWI202408260783](https://openairdocs.org/sdr/SWI202408260783.md): Hinge · gouged · Jun 16, 2024 · N187PQ · Cndair CL6002D24 · Fuselage, Door Hinge
  > PAX DOOR PIANO HINGE, FUSELAGE SIDE, LUG #18 IS GOUGED (MARKED) (C-CHECK RO 8/24/2024) REMOVED DAMAGE AT PAX DOOR PIANO HINGE, FUSELAGE SIDE, LUG #18 REF CRJ900 SRM 51-12-00-001-001-A01. WITHIN LIMITS IAW CRJ900 SRM 53-21-23-201-010-A01 TYPE I STEP 2.
- [SDR SWI202408260782](https://openairdocs.org/sdr/SWI202408260782.md): Hinge · gouged · Jun 16, 2024 · N187PQ · Cndair CL6002D24 · Fuselage, Door Hinge
  > PAX DOOR PIANO HINGE, FUSELAGE SIDE, LAST LANDING #27 IS GOUGED FROM THE MIGRATED SPRING PIN (MARKED) (C-CHECK RO 8/24/2024) REMOVED DAMAGE ON PAX DOOR PIANO HINGE FUSELAGE SIDE AT LUG LAND AND LUG LOCATION IAW CRJ 900 SRM 53-21-23-201-010-A01 TYPE I STEP
- [SDR SWIA2024082600016](https://openairdocs.org/sdr/SWIA2024082600016.md): Hinge · gouged · Jun 16, 2024 · N187PQ · Cndair CL6002D24 · Fuselage, Door Hinge
  > PAX DOOR PIANO HINGE, DOOR SIDE, HAS NUMEROUS LUGS GOUGED (MARKED) (C-CHECK RO 8/24/2024) REMOVED DAMAGE ON PAX DOOR PIANO HINGE DOOR SIDE AT LUG LAND AND LUG LOCATION IAW CRJ 900 SRM 52-11-01-201-007-A01 TYPE I STEP 1 AND TYPE IV STEP 1. FOUND REWORKE
- [SDR SWIA2024082600014](https://openairdocs.org/sdr/SWIA2024082600014.md): Fairing · chafed · Jun 14, 2024 · N187PQ · Cndair CL6002D24 · Nacelle/Pylon, Main Frame
  > DURING AUDIT OF 1C TASK CARD 54-440-301 (INTERNAL ZONAL INSPECTION OF THE RIGHT NACELLE (EWIS)), FOUND LOWER HINGE LINE FAIRING RUBBING ON BOTTOM SIDE OF FWD. ENGINE MOUNT. (C-CHECK RO 8/24/2024) REPAIRED BOTTOM SIDE OF FWD. ENGINE MOUNT BY COMPLYING WI
- [SDR SWI202408260776](https://openairdocs.org/sdr/SWI202408260776.md): Vane · chafed · Jun 12, 2024 · N187PQ · Cndair CL6002D24 · Trailing Edge Flaps
  > LH INBOARD FLAP VANE LEADING EDGE CENTER VANE CAP CHAFFED (C-CHECK RO 8/24/2024) REMOVED REPAIR ITEM REF CRJ900 SRM 51-42-13-001-001-A01.INSTALLED NEW REPLACEMENT LH INBD FLAP VANE CAP, PN:CC670-14022-1, REF INSTALLATION DWG# CC670-14010, REV -E. AND CR
- [SDR SWIA2024082600612](https://openairdocs.org/sdr/SWIA2024082600612.md): Frame · cracked · Jun 12, 2024 · N187PQ · Cndair CL6002D24 · Fuselage Main, Frame
  > FRAME CRACKED FS333.00 BETWEEN STGR1R & 2R. (MARKED) (C-CHECK RO 8/24/2024) PERFORMED REPAIR AT FS333.00 BETWEEN STGR 1R AND 2R REF. REO 690-53-21-1792 REV.-- ISSUED 2024-07-04 COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY (CL600-2D24) STRUCTURAL MAJO
- [SDR SWI202408260775](https://openairdocs.org/sdr/SWI202408260775.md): Bracket · bent · Jun 11, 2024 · N187PQ · Cndair CL6002D24 · Nacelle/Pylon Miscellaneous Structure
  > L/H UPPER TRANSCOWL INBD "A" BRACKET STANDOFF IS BENT AND NOT SEATING PROPERLY (C-CHECK RO 8/24/2024) INSTALLED 1 EA. NEW INBD. STANDOFF P/N CN 624-2082-201 ON L/H UPPER TRANS COWL, REF. REO 670-54-21-971, REV. B. 2023-11-28. COMPLIED WITH STEPS 1-3, A
- [SDR SWI202408260774](https://openairdocs.org/sdr/SWI202408260774.md): Bracket · cracked · Jun 11, 2024 · N187PQ · Cndair CL6002D24 · Nacelle/Pylon Miscellaneous Structure
  > L/H UPPER TRANSCOWL OTBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 8/24/2024) INSTALLED 1 EA. NEW OTBD. STANDOFF P/N CN 624-2082-201 ON L/H UPPER TRANS COWL, REF. REO 670-54-21-971, REV. B, 2023-11-28. COMPLIED WITH STEPS 1-3, AND COMPLIED WITH 51-90
- [SDR SWI202408260773](https://openairdocs.org/sdr/SWI202408260773.md): Stiffener · loose · Jun 11, 2024 · N187PQ · Cndair CL6002D24 · Engine Thrust Reverser
  > R/H LWR TRANSCOWL Z STIFFENER RIVETS ARE PULLED/LOOSE (C-CHECK RO 8/24/2024) REPAIRED R/H LWR TRANSCOWL PER REO 690-54-21-501 REV -- DATED 2024-07-04. STEPS 1-14. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.
- [SDR SWI202408260772](https://openairdocs.org/sdr/SWI202408260772.md): Intercostal · corroded · Jun 11, 2024 · N187PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INTERCOSTAL LOWER FLANGE IS CORRODED BETWEEN FS394.00 -409.00 & STGR27 - 26L. (MARKED) (C-CHECK RO 8/24/2024) REMOVED AND REPLACED INTERCOSTAL, STGR 27 P/N: SH670-32075-4 WITH NEW ASSEMBLY REF DWG SH670-32050 REV J AND CRJ900 SRM 51-42-06-001-001-A01
- [SDR SWI202408260771](https://openairdocs.org/sdr/SWI202408260771.md): Skin · cracked · Jun 11, 2024 · N187PQ · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > RH TRU DOOR FUSELAGE SKIN CUT OUT, THE AFT LOWER CORNER POSSIBLY CRACKED IN THE RADIUS (MARKED) (C-CHECK RO 8/24/2024) REMOVED AND REPLACED THE CRACKED RH ADG SKIN ON THE RHS NOSE UNDER TRU BAY WITH NEW REPLACEMENT SKIN (P/N CC670-33109-3) USING ALL NEW
- [SDR SWI202408260770](https://openairdocs.org/sdr/SWI202408260770.md): Skin · cracked · Jun 11, 2024 · N187PQ · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > LH TRU DOOR FUSELAGE SKIN CUT OUT, THE AFT LOWER CORNER POSSIBLY CRACKED IN THE RADIUS (MARKED) (C-CHECK RO 8/24/2024) REMOVED AND REPLACED THE CRACKED HYDRAULIC BAY SKIN ON THE LHS NOSE UNDER TRU BAY WITH NEW REPLACEMENT SKIN (P/N CC670-33106-5S) USIN
- [SDR SWI202408260769](https://openairdocs.org/sdr/SWI202408260769.md): Latch · cracked · Jun 11, 2024 · N187PQ · Cndair CL6002D24 · Electrical/Electronic Compartment Doors
  > LH TRU DOOR AFT LATCH CUT OUT ON THE FUSELAGE, POSSIBLY CRACKED IN THE RADIUS (MARKED) (C-CHECK RO 8/24/2024) REMOVED AND REPLACED CRACKED TRU BAY LANDING WITH NEW REPLACEMENT LANDING (P/N CC670-33151-3), USING ALL NEW FASTENERS, REF CRJ900 SRM 51-42-0

Next page: https://openairdocs.org/aircraft/N187PQ/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 = 'N187PQ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N187PQ/reports

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