# Service difficulty reports: N186GJ

A list on [N186GJ](https://openairdocs.org/aircraft/N186GJ.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 · 64 reports

- [SDR REXA2026040800283](https://openairdocs.org/sdr/REXA2026040800283.md): Elec Connector · disconnected · Apr 5, 2026 · N186GJ · Cndair CL6002D24 · Light System Wiring
  > DURING WAKE UP FOUND RH FWD OVERWING DOOR INTERIOR EMERGENCY EXIT LIGHT OUT. FOUND P5311 DISCONNECTED. RE-CONNECTED IAW ESPM 20-26-00 & SWAPPED PS43 & PS35 BATT IAW AMM 33-51-17. OPS CHK GOOD. NO FURTHER DEFECTS NOTED.
- [SDR REXA2025090400848](https://openairdocs.org/sdr/REXA2025090400848.md): Hand Rail · out of adjust · Sep 2, 2025 · N186GJ · Cndair CL6002D24 · Passenger/Crew Doors
  > MAIN CABIN DOOR STICKING CLOSED AND WOULD NOT OPEN UPON ARRIVAL. PERFORMED ADJUSTMENTS TO MAIN CABIN DOOR HAND RAIL IAW 900 AMM 52-11-05. PERFORMED MULTIPLE OPS TESTS IAW 900 AMM 52-11-00 OF MAIN CABIN DOOR, ALL OPS TESTS GOOD. NO FURTHER DEFECTS NOTED.
- [SDR REXA202407010485](https://openairdocs.org/sdr/REXA202407010485.md): Door · inoperative · Jun 25, 2024 · N186GJ · Cndair CL6002D24 · Passenger/Crew Doors
  > MAIN CABIN DOOR WOULD NOT OPEN, PAX DOOR OP, CHK IAW AMM 52-11-00, CAM ROLLERS ON PAX DOOR LUBRICATED, NO DEFECTS NOTED,
- [SDR REXA2022101800896](https://openairdocs.org/sdr/REXA2022101800896.md): Bulb · inoperative · Oct 1, 2023 · N186GJ · Cndair CL6002D24 · Emergency Lighting
  > UPON EMERGENCY LIGHTS OPS TEST FOUND ALL EMERGENCY LIGHTS TO BE INOP ON ENTRANCE STORAGE COMPARTMENT PN: 3071BPEGPL REPLACED EMERGENCY LIGHT BULBS ON ENTRANCE STORAGE COMPARTMENT PN:WL3071BPEGPL IAW CRJ 900 AMM 33-51-05-960-801-A02. O
- [SDR REXA2024012200095](https://openairdocs.org/sdr/REXA2024012200095.md): Bracket · corroded · Sep 26, 2023 · N186GJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > UNDER BLOW OUT PANEL 642AZ HYDRAULICS BRACKET FOR IB BK, LG EX, LG RET CORRODED IN RH MLG WHEEL WELL. INSTALLED NEW SERVICEABLE PANEL 642AZ BRACKET (P/N: CC670-10337-2) IAW CRJ900 AMM 20-21-00-910-801(A01) & AMM 20-22-00-910-801(A01).
- [SDR REXA2024012200092](https://openairdocs.org/sdr/REXA2024012200092.md): Seat Track · corroded · Sep 19, 2023 · N186GJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > RBL 9 SEAT RAIL IS CORRODED BETWEEN FS 661+32 AND FS 693. REMOVED RBL 9 SEAT RAIL BETWEEN FS 661+32 AND FS 693 IAW CRJ900 AMM 53-00-49-000-801-A07 INSTALLED A NEW RBL 9 SEAT RAIL BETWEEN FS 661+32 AND FS 693 IAW CRJ900 AMM 53-00-49-400-801-A07, REO 670-53-00-5
- [SDR REXA2022110100943](https://openairdocs.org/sdr/REXA2022110100943.md): Stringer · corroded · Sep 17, 2023 · N186GJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 25L CORRODED BETWEEN FS333 - FS364. REPAIRED STGR 25L FROM F.S.333 TO F.S.349 IAW ENDEAVOR AIR EA CRJ953-15452 REV IR DATED 9/15/2023.
- [SDR REXA2022110100942](https://openairdocs.org/sdr/REXA2022110100942.md): Seat Track · corroded · Sep 17, 2023 · N186GJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > SIDE SEAT RAIL AT STGR 15R IS CORRODED BETWEEN FS 661+16 AND FS 661+90. REMOVED CORODED R/H SIDE SEAT RAIL FROM F.S.661+16 TO F.S.661+90 AND INSTALLED NEW SERVICABLE SEAT RAIL IAW MHIRJ REO 670-53-00-587 REV C DATED 2023-02-08 AND CRJ 900 AMM 53-00-49-400-801
- [SDR REXA2022110100941](https://openairdocs.org/sdr/REXA2022110100941.md): Seat Track · corroded · Sep 17, 2023 · N186GJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > SIDE SEAT RAIL AT STGR 15L IS CORRODED BETWEEN FS 379 AND FS 485. REMOVED CORODED L/H SIDE SEAT RAIL FROM F.S.379 TO F.S.485 AND INSTALLED NEW SERVICABLE SEAT RAIL IAW MHIRJ REO 670-53-00-587 REV C DATED 2023-02-08 AND CRJ 900 AMM 53-00-49-400-801-A13.
- [SDR REXA2022090700734](https://openairdocs.org/sdr/REXA2022090700734.md): Floorbeam · corroded · Aug 24, 2023 · N186GJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > S 280 CORROSION NOTED AT APPROXIMATELY LBL 15.0 BETWEEN ANGLE (CAP) AND TOP OF CROSSBEAM, AROUND NUTPLATE HOLE FOR CABIN FLOORBOARD LH FS 280 CROSSBEAM IS HEAVILY CORRODED IN MULTIPLE LOCATIONS AND IS CRACKED ON UPPER FLANGE. NO LIMITATIONS PROVIDED IN SRM, R
- [SDR REXA2022083000728](https://openairdocs.org/sdr/REXA2022083000728.md): Angle · cracked · Aug 24, 2023 · N186GJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > RBL 26 (P/N: CC670-34117-6) STIFFENING ANGLE ON RH FS 280 LWR BULKHEAD WEB FOUND TO BE CRACKED. LOCATED AND DRILLED NEW SERVICEABLE STIFFENING ANGLE PN: CC670-34117-6 IAW CRJ 900 SRM 51-40-11-001-001-A01.INSTALLED NEW STIFFENING ANGLE PN: CC670-34117-6 AT RB
- [SDR REXA2022082100681](https://openairdocs.org/sdr/REXA2022082100681.md): Floor Support · corroded · Aug 18, 2023 · N186GJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "LH FLOOR SILL IS CORRODED AT FS 565. REMOVED CORROSION AT FS 565 IAW CRJ900 SRM 53-00-45-201-001-A01 STEPS 6 A-E. PERFORMED UT THICKNESS OF LH FLOOR SILL FS565 REWORKED AREA IAW CRJ 900 NDTM PART 1 51-20-004-270-A01 REV 36 DATED 2/8/22. FOUND LOWEST REMAININ
- [SDR REXA2022082100680](https://openairdocs.org/sdr/REXA2022082100680.md): Skin · corroded · Aug 18, 2023 · N186GJ · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > "FUSELAGE SKIN IS CORRODED UNDER AFT CARGO DOOR PROTECTOR PLATE BETWEEN F.S. 1031 TO F.S. 1051. REMOVED CORROSION IN FUSELAGE SKIN UNDER AFT CARGO DOOR PROTECTOR PLATE, STRG 19L BETWEEN FS. 1031.0 TO FS. 1051.0, IAW CRJ900 SRM 51-21-06-001-001-A01. ORIGINAL TH
- [SDR REXA2022082100679](https://openairdocs.org/sdr/REXA2022082100679.md): Skin · corroded · Aug 18, 2023 · N186GJ · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > "AFT BAGGAGE BAY DOOR SILL CORRODED BETWEEN FS 1000 AND FS1047 AT STRG17L AFT BAGGAGE BAY DOOR SILL CORRODED BETWEEN FS 1000 AND FS1047 AT STRG17L. REMOVED CORROSION ON AFT BAGGAGE BAY DOOR SILL BETWEEN FS1000 AND FS1047 AT STRG17L IAW CRJ900 SRM 53-61-23-201
- [SDR REXA2022081700666](https://openairdocs.org/sdr/REXA2022081700666.md): Skin · corroded · Aug 18, 2023 · N186GJ · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > "LH FLOOR SILL IS CORRODED AT FS 661+16. LH FLOOR SILL IS CORRODED AT FS 661+16. CORROSION REQUIRES REMOVAL REMOVED CORROSION AT FS 661+16 IAW CRJ900 SRM 53-00-45-201-001-A01 STEPS 6A-E UT REQUIRED FOR MRT PERFORMED UT THICKNESS OF LH FLOOR SILL FS661+16 REWO
- [SDR REXA2022091500751](https://openairdocs.org/sdr/REXA2022091500751.md): Stringer · corroded · Aug 17, 2023 · N186GJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 26R CORRODED BETWEEN FS319-FS333. REMOVED UNSERVICEABLE PART. LOCATED AND DRILLED NEW STRINGER 26R PN: SH670-31634-2S FROM FS 280-333 IAW CRJ 900 SRM 51-40-11-001-001-A01. INSTALLED NEW STRINGER 26R FROM FS280-333 IAW CRJ 900 SRM 51-42-06-001-001-A01
- [SDR REXA2022090800741](https://openairdocs.org/sdr/REXA2022090800741.md): Stringer Splice · corroded · Aug 17, 2023 · N186GJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER SPLICE AT 25R FS333 CORRODED. LOCATED AND DRILLED NEW STRINGER SPLICE 25R FS333 P/N: SH670-32429-4S IAW CRJ-900 SRM 51-40-11-001-001-A01.INSTALLED NEW STRINGER SPLICE P/N SH670-32429-4S AT STR 25R FS 333, IAW CRJ-900 SRM 51-42-06-001-001-A01.
- [SDR REXA2022083000727](https://openairdocs.org/sdr/REXA2022083000727.md): Stringer · corroded · Aug 17, 2023 · N186GJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STRINGER 26R CORRODED BETWEEN FS333 - FS364 LOCATED AND DRILLED NEW STGR 26R PN: SH670-31372-4S IAW CRJ 900 SRM 51-40-11-001-001-A01 INSTALLED STGR 26R FROM FS 333-364 IAW CRJ 900 SRM 51-42-06-001-001-A01
- [SDR REXA2022083000726](https://openairdocs.org/sdr/REXA2022083000726.md): Stringer · corroded · Aug 17, 2023 · N186GJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STRINGER 26L CORRODED BETWEEN FS333 - FS349 LOCATED AND DRILLED NEW STRINGER 26L PN: SH670-31372-3S IAW CRJ 900 SRM 51-40-11-001-001-A01 INSTALLED STGR 26L FROM FS333-364 IAW CRJ 900 SRM 51-42-06-001-001-A01
- [SDR REXA2022083000725](https://openairdocs.org/sdr/REXA2022083000725.md): Splice · corroded · Aug 17, 2023 · N186GJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STRINGER 26L SPLICE CORRODED AT FS333 LOCATED AND DRILLED NEW STRINGER SPLICE PN: SH670-32429-3 IAW CRJ 900 SRM 51-40-11-001-001-A01 INSTALLED STGR26L SPLICE AT FS 333 IAW CRJ 900 SRM 51-42-06-001-001-A01
- [SDR REXA2022083000724](https://openairdocs.org/sdr/REXA2022083000724.md): Stringer · corroded · Aug 17, 2023 · N186GJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 26L CORRODED BETWEEN FS319 - FS333 LOCATED AND DRILLED NEW STRINGER P/N: SH670-31634-1S AT STR 26L FROM FS 280 TO FS 333 IAW CRJ-900 SRM 51-40-11-001-001-A01. INSTALLED STGR 26L FROM FS 280-333 IAW CRJ 900 SRM 51-42-06-001-001-A01
- [SDR REXA2022083000723](https://openairdocs.org/sdr/REXA2022083000723.md): Stringer · corroded · Aug 17, 2023 · N186GJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 26R SPLICE CORRODED AT FS333 LOCATED AND DRILLED NEW STINGER SPLICE P/N:SH670-32429-2, STR26R AT FS333 IAW CRJ-900 SRM 51-40-11-001-001-A01. INSTALLED STGR 26R SPLICE AT FS333 IAW CRJ 900 SRM 51-42-06-001-001-A01
- [SDR REXA2022083000722](https://openairdocs.org/sdr/REXA2022083000722.md): Longeron · corroded · Aug 15, 2023 · N186GJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STGR 25R LONGERON IS CORRODED BETWEEN FS 333 AND FS 364 LOCATED AND DRILLED NEW STR 25R LONGERON P/N SH670-32103-4 BETWEEN FS 333 TO FS 364 IAW CRJ-900 SRM 51-40-11-001-001-A01 INSTALLED NEW STR 25R LONGERON P/N: SH670-32103-4 BETWEEN FS333 TO FS364, IAW CR
- [SDR REXA2022090800740](https://openairdocs.org/sdr/REXA2022090800740.md): Angle · cracked · Aug 11, 2023 · N186GJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FS 280 FLOORBEAM TO CROSSBEAM ATTACH BRACKET RBL 9.0 IS CRACKED. LOCATED AND DRILLED SERVICEABLE RBL9 O/B ANGLE P/N: CC670-34269-8 IAW CRJ 900 SRM 51-40-11-001-001-A01. REF. BAR-CODE IDENTIFIER HR00304343 FOR INSTALL OF REMOVED 2EA BRACKET (I/B & O/B SIDE) ON
- [SDR REXA2022090800739](https://openairdocs.org/sdr/REXA2022090800739.md): Angle · cracked · Aug 11, 2023 · N186GJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FS 280 FLOORBEAM TO CROSSBEAM ATTACH BRACKET LBL 9.0 CRACKED ON OUTBOARD SIDE. LOCATED AND DRILLED SERVICEABLE LBL9 O/B ANGLE P/N: CC670-34269-7 IAW CRJ 900 SRM 51-40-11-001-001-A01. REF. BAR-CODE IDENTIFIER HR00304343 FOR INSTALL OF REMOVED 2EA BRACKET (I/B
- [SDR REXA2022090800738](https://openairdocs.org/sdr/REXA2022090800738.md): Handle · cracked · Aug 11, 2023 · N186GJ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR OUTER HANDLE CHAFED AND FLAP HANDLE CRACKED. REPLACED PAX DOOR OUTER HANDLE FLAP IAW CRJ900 SRM TASK 51-42-06-001-001-A01
- [SDR REXA2022090700733](https://openairdocs.org/sdr/REXA2022090700733.md): Floorbeam · corroded · Aug 11, 2023 · N186GJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FS 280 CORROSION NOTED AT APPROXIMATELY RBL 15.0 BETWEEN ANGLE (CAP) AND TOP OF CROSSBEAM, AROUND NUTPLATE HOLE FOR CABIN FLOORBOARD LOCATED AND DRILLED RH FS 280 CROSSBEAM PN: CC670-34094-2 IAW CRJ 900 SRM 51-40-11-001-001-A01. INSTALLED O/B JO-BOLT FASTEN
- [SDR REXA2024021900199](https://openairdocs.org/sdr/REXA2024021900199.md): Seat Track · corroded · Aug 10, 2023 · N186GJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > SIDE SEAT RAIL AT STGR 15L IS CORRODED BETWEEN FS 573 AND FS 661+16. REMOVED SIDE SEAT RAIL AT LEVEL STR15L BETWEEN FS 573 TO FS 661+16. INSTALLED A SERVICEABLE SIDE SEAT RAIL AT STGR 15L BETWEEN FS 573 TO FS 661+16 IAW MHIRJ REO 670-53-00-587 DATED 2023-02-08
- [SDR REXA2022083000720](https://openairdocs.org/sdr/REXA2022083000720.md): Intercostal · corroded · Aug 10, 2023 · N186GJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > MAIN AVIONICS BAY DOOR SURROUND STRUCTURE, INTERCOSTAL BETWEEN FS349 AND FS364 AT STGR 27R CORRODED. LOCATED AND DRILLED NEW INTERCOSTAL P/N SH670-32075-4S, STR27R BETWEEN FS 349 AND FS 364 IAW CRJ-900 SRM 51-40-11-001-001-A01 INSTALLED NEW INTERCOSTAL P/N S
- [SDR REXA2022082900719](https://openairdocs.org/sdr/REXA2022082900719.md): Intercostal · corroded · Aug 10, 2023 · N186GJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > MAIN AVIONICS BAY DOOR SURROUND STRUCTURE, INTERCOSTAL BETWEEN FS349 AND FS364 AT STGR 27L CORRODED. LOCATED AND DRILLED NEW INTERCOSTAL STR 27L BETWEEN FS 349 TO FS 364, P/N SH670-32075-3S, IAW CRJ-900 SRM 51-40-11-001-001-A01 INSTALLED NEW INTERCOSTAL P/N
- [SDR REXA2022082900717](https://openairdocs.org/sdr/REXA2022082900717.md): Frame · corroded · Aug 10, 2023 · N186GJ · Cndair CL6002D24 · Fuselage Main, Frame
  > FRAME AT FS310 CORRODED BETWEEN STGR25R AND STGR25L. REMOVED CORROSION FROM FRAME 310 STGR 25L - STGR 25R IAW CRJ900 SRM 53-00-06-201-005-A01
- [SDR REXA2022082400700](https://openairdocs.org/sdr/REXA2022082400700.md): Floor Support · corroded · Aug 10, 2023 · N186GJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRAWLWAY FLOOR PANEL SUPPORT ANGLE CORRODED AT FS280 BETWEEN STGR26L AND STGR26R INSTALLED NEW CRAWLWAY FLOOR PANEL SUPPORT ANGLE IAW CRJ 900 SRM 51-42-06-001-001-A01 AND CRJ 900 SRM 51-42-21-001-001-A01, P/N CC670-34256-3.
- [SDR REXA2022082200694](https://openairdocs.org/sdr/REXA2022082200694.md): Spacer · corroded · Aug 10, 2023 · N186GJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CROSSBEAM SPACER IS CORRODED AT FS 333, ON THE O/B SIDE OF THE RBL 9 BEAM. REMOVED THE RBL9 O/B CROSSBEAM SPACER AT FS 333 TO FULLY REMOVE ALL CORROSION IAW CRJ-900 51-42-06-001-001-A01. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE SPACER P/N SH670-32167-3 A
- [SDR REXA2024071600521](https://openairdocs.org/sdr/REXA2024071600521.md): Seat Track · corroded · Aug 9, 2023 · N186GJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > SIDE SEAT RAIL AT STGR 15R IS CORRODED BETWEEN FS 744 AND FS 761. REMOVED AND REPLACED SEAT RAIL IAW CRJ900 AMM TASKS 53-00-49-000-801-A13 AND 53-00-49-400-801-A13. FABRICATED PART IAW MHIRJ REO 670-53-00-587 REV C DATED 2023-02-08 REPAIR (B).
- [SDR REXA2024071600520](https://openairdocs.org/sdr/REXA2024071600520.md): Seat Track · corroded · Aug 9, 2023 · N186GJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > SIDE SEAT RAIL AT STGR 15R IS CORRODED BETWEEN FS 680 AND FS 722. REMOVED AND REPLACED SEAT RAIL IAW CRJ900 AMM TASKS 53-00-49-000-801-A13 AND 53-00-49-400-801-A13. FABRICATED PART IAW MHIRJ REO 670-53-00-587 REV C DATED 2023-02-08 REPAIR (B).
- [SDR REXA2022100900839](https://openairdocs.org/sdr/REXA2022100900839.md): Seat Track · corroded · Aug 9, 2023 · N186GJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > LBL 9 SEAT RAIL IS CORRODED BETWEEN FS 661+32 AND FS 693. LBL 9 SEAT RAIL BETWEEN FS 661+32 AND FS 693 IS CORRODED OUT OF LIMITS IAW CRJ900 SRM 53-31-49-101-001-A02. REMOVED, FABBED AND REPLACED SEAT RAIL IAW CRJ900 MHIRJ REO 670-53-00-589 REV-C DATED 2023-02-
- [SDR REXA2022082900718](https://openairdocs.org/sdr/REXA2022082900718.md): Seat Track · corroded · Aug 9, 2023 · N186GJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > LBL 9 SEAT RAIL IS CORRODED BETWEEN FS 581 AND FS 661+32. FABRICATED LBL 9 SEAT RAIL BETWEEN FS 581- FS 661+32 (P/N SH690-33404-1) FROM SEAT TRACK EXTRUSION P/N 20276-288-0-0, PO# W77329 IAW MHIRJ REO 670-53-00-589 REV (-C) DATED 2023-02-08 REPAIR (B). LOCATE
- [SDR REXA2022082900716](https://openairdocs.org/sdr/REXA2022082900716.md): Seat Track · corroded · Aug 9, 2023 · N186GJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > RBL 9 SEAT RAIL IS CORRODED BETWEEN FS 581 AND FS 661+32. INSTALLED RBL 9 SEAT RAIL (P/N SH69033404-1) BETWEEN FS 581 TO 661+32 IAW CRJ900 AMM 53-00-49-400-801-A07.
- [SDR REXA2022090800736](https://openairdocs.org/sdr/REXA2022090800736.md): Floor Panel · cracked · Aug 8, 2023 · N186GJ · Cndair CL6002D24 · Fuselage Main, Structure
  > IN FORWARD EQUIPMENT BAY FLOOR, R/H F.S. 193.00 IS CRACKED. REPAIRED RH ELECTRICAL BAY FLOOR AT FS 193.00 IAW CRJ900 SRM REPAIR 53-11-43-201-001-A01 RHS REPAIR TYPE 2.
- [SDR REXA2022091100742](https://openairdocs.org/sdr/REXA2022091100742.md): Angle · corroded · Aug 6, 2023 · N186GJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > GALLEY SERVICE DOOR SILL ANGLE AND ANGLES FOR LOWER DOOR FITTINGS ARE CORRODED. LOCATED AND DRILLED NEW SILL ANGLE P/N SH670-31996-3S, AT LOWER SERVICE DOOR, IAW CRJ-900 SRM 51-40-11-001-001-A01. INSTALLED GALLEY SERVICE DOOR SILL ANGLE P/N: SH670-31996-3S I
- [SDR REXA2022082800709](https://openairdocs.org/sdr/REXA2022082800709.md): Bracket · cracked · Aug 6, 2023 · N186GJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > IN AFT EQUIPMENT BAY, OUTBOARD OF LH ACM, BRACKET FOR ACM TOP WATER LINE BROKEN. LOCATED, DRILLED AND INSTALL NEW BRACKET ASSY P/N MM670-97111-005 ON STGR 9L BTWN FS 1144.0 & FS 1154.48, IAW CRJ900 SRM 51-40-11-001-001-A01 & 51-42-06-001-001-A01
- [SDR REXA2022082800708](https://openairdocs.org/sdr/REXA2022082800708.md): Bracket · cracked · Aug 6, 2023 · N186GJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > IN AFT EQUIPMENT BAY, OUTBOARD OF LH ACM, BRACKET FOR ACM TOP WATER LINE BROKEN. RECEIVED, LOCATED, DRILLED AND DEBURRED, NEW BRACKET ASSY P/N MM670-97107-001, ON STRG 7L BTWN FS 1162 TO FS 1181, IAW CRJ900 SRM 51-40-11-001-001-A01 INSTALLED NEW BRACKET ASSY P
- [SDR REXA2022092900774](https://openairdocs.org/sdr/REXA2022092900774.md): Bracket · corroded · Aug 5, 2023 · N186GJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > UNDER BLOW OUT PANEL 542AZ HYDRAULICS BRACKET FOR IB BK, LG EX, LG RET CORRODED IN LH MLG WHEEL WELL. UPON FURTHER INVESTIGATION, FOUND LH MLG BLOW OUT PANEL 542AZ BRACKET (P/N: CC670-10337-1) TO BE OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS PROVIDED IN THE SRM
- [SDR REXA2022081600653](https://openairdocs.org/sdr/REXA2022081600653.md): Angle · corroded · Aug 5, 2023 · N186GJ · Cndair CL6002D24 · Wing Miscellaneous Structure
  > RH MLG, UNDER BLOW OUT PANEL 642BZ, BRACKET CORRODED REMOVED UNSERVICEABLE RH MLG BLOW OUT PANEL 642BZ BRACKET (P/N: CC670-10338-2) IAW CRJ-900 SRM 51-42-21-001-001-A01. INSTALLED NEW RH MLG BLOW OUT PANEL 642BZ BRACKET (P/N: CC670-10338-2) IAW CRJ-900 SRM 51-
- [SDR REXA2022082200689](https://openairdocs.org/sdr/REXA2022082200689.md): Bracket · cracked · Aug 4, 2023 · N186GJ · Cndair CL6002D24 · Nose/Tail Landing Gear
  > NOSE HYDRAULICS COMPARTMENT UPPER BRAKE ACCUMULATOR FWD BRACKET (ATTACHED TO INTERCOSTAL) IS CRACKED INSTALLED NEW SERVICEABLE UPPER FWD BRACKET OF NOSE HYDRAULICS COMPARTMENT P/N: CC670-75604-2 IAW CRJ-900 STM 51-42-21-001-001-A01
- [SDR REXA2022091100744](https://openairdocs.org/sdr/REXA2022091100744.md): Access Panel · chafed · Aug 2, 2023 · N186GJ · Cndair CL6002D24 · Wing, Plate/Skin
  > R/H WING ACCESS PANEL 699AB HAS CHAFFING. LOCATED AND DRILLED 1EA NEW SERVICEABLE ACCESS PANEL IAW CRJ-900 SRM 51-40-11-001-001-A01. P/N REMOVED: 601R13440-2 NEW P/N: 601R13440-2
- [SDR N6WA20181227501](https://openairdocs.org/sdr/N6WA20181227501.md): Warning Light · false activation · Dec 25, 2018 · N186GJ · Cndair CL6002D24 · Door Warning System
  > RH AFT EXIT DOOR CAUTION IN FLIGHT. CYCLED THE EMER EXIT DOOR AFT IAW CRJ 900 AMM 52-21-00. MESSAGE CLEARED. ACFT OK FOR SERVICE.
- [SDR N6WA2018121700401](https://openairdocs.org/sdr/N6WA2018121700401.md): Door · warning message · Dec 14, 2018 · N186GJ · Cndair CL6002D24 · Emergency Exits
  > FWD LEFT EMERGENCY EXIT DOOR SHOW CAUTION MSG.AS PER TELCOM DEFERRED FWD LEFT EMERGENCY EXIT DOOR INDICATION OCN 70048929 PER MEL 52-70-03 CAT C
- [SDR N6WA201809100401](https://openairdocs.org/sdr/N6WA201809100401.md): Cover · unsecure · Sep 4, 2018 · N186GJ · Cndair CL6002D24 · Emergency Exits
  > EMERGENCY DOOR HANDLE COVER AT 12A NEEDS TO BE SECURED. RESECURED EMERGENCY DOOR HANDLE COVER AT 12A. OK FOR SERVICE.
- [SDR N6WA2018040601](https://openairdocs.org/sdr/N6WA2018040601.md): Warning Message · illuminated · Apr 6, 2018 · N186GJ · Cndair CL6002D24 · Door Warning System
  > AFT RIGHT WING EMERGENCY EXIT CAUTION.

Next page: https://openairdocs.org/aircraft/N186GJ/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 = 'N186GJ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N186GJ/reports

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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.
