# Service difficulty reports: N187GJ

A list on [N187GJ](https://openairdocs.org/aircraft/N187GJ.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR REXA2025082600837](https://openairdocs.org/sdr/REXA2025082600837.md): Fitting · out of limits · Aug 25, 2025 · N187GJ · Cndair CL6002D24 · Wing, Control Surface Attach Fittings
  > "ON THE RH AILERON, FOUND BOTH CENTER UPPER LUG BORE DIAMETERS TO BE OUT OF LIMITS. IB LUG IS.986"" AND OB LUG IS.985"", NOMINAL LIMIT IS.975 +-.0005 REPAIRED OVERSIZED BORES AND PITTING CORROSION TO THE AILERON ACTUATOR CENTER HINGE FITTING LUGS AT AIL ST
- [SDR REXA2025082600836](https://openairdocs.org/sdr/REXA2025082600836.md): Lug · corroded · Aug 25, 2025 · N187GJ · Cndair CL6002D24 · Wing, Control Surface Attach Fittings
  > THE L/H AILERON PCU LUG L2 HAS CORROSION INSIDE THE BORE FOR THE BUSHING COMPLIED WITH REPAIR TO RTM AILERON CENTRE HINGE FITTING LUGS IAW BOMBARDIER REO 670-57-61-237 REV-- DATED 2017-07-25.
- [SDR REXA2025081900821](https://openairdocs.org/sdr/REXA2025081900821.md): Floorbeam · corroded · Aug 18, 2025 · N187GJ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > LEFT F.S.280 CROSSBEAM APPEARS TO BE CORRODED ON AFT EDGE UNDER CAP ANGLE, LBL11. REMOVED LH FS280 BULKHEAD CROSSBEAM BETWEEN BL 0 TO RBL37, IAW CRJ-900 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 AND CRJ900 SRM 51-42-13-001-001-A01. INSTALLED NEW SER
- [SDR REXA2025081900820](https://openairdocs.org/sdr/REXA2025081900820.md): Lug · cracked · Aug 18, 2025 · N187GJ · Cndair CL6002D24 · Emergency Exits
  > RIGHT AFT OVERWING EMERGENCY EXIT DOOR S/N SB0739 HAS POSSIBLE CRACK AROUND TOP ALIGNMENT LUG. REPAIRED CRACK TO OVERWING EMERGENCY EXIT DOOR S/N SB0739 TOP SECTION (AROUND BASE OF DOOR PROXIMITY SENSOR STRIKER) IAW MHIRJ REO 670-52-21-103 REV -- DATED 2024-1
- [SDR REXA2025081800808](https://openairdocs.org/sdr/REXA2025081800808.md): Floorbeam · corroded · Aug 18, 2025 · N187GJ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > R/H F.S.280 CROSSBEAM APPEARS TO BE CORRODED ON AFT EDGE UNDER CAP ANGLE, RBL 11. REMOVED RH FS280 BULKHEAD CROSSBEAM BETWEEN BL 0 TO RBL37, IAW CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01. INSTALLED NEW SERVICEABLE RH FS280 BULKHEAD CROSSBE
- [SDR REXA2025082200827](https://openairdocs.org/sdr/REXA2025082200827.md): Angle · corroded · Jul 29, 2025 · N187GJ · Cndair CL6002D24 · Emergency Exits
  > AFT BELLY FAIRNG SUPPORT STRUCTURE F.S.881 IS CORRODED AT STGR 27. REMOVED CORROSION FROM AFT BELLY FAIRNG SUPPORT STRUCTURE BS 881 AT S27 IAW SRM 51-21-06-001-001-A01 PER SRM 53-82-55-101-001-A02 ANGLE IS OUT OF LIMITS ON MULTIPLE ELEMENTS & REQUIRES ENGINEER
- [SDR REXA2024062400473](https://openairdocs.org/sdr/REXA2024062400473.md): Door Frame · cracked · Apr 17, 2024 · N187GJ · Cndair CL6002D24 · Fuselage Main, Structure
  > R/H FWD EMERGENCY DOOR HAS A VISIBLE CRACK BELOW UPPER AFT LUG. REPAIRED IAW ENDEAVOR EA CRJ952-16408 REV IR DATED 4/27/2024.
- [SDR REXA2024062400472](https://openairdocs.org/sdr/REXA2024062400472.md): Door Frame · cracked · Apr 17, 2024 · N187GJ · Cndair CL6002D24 · Fuselage Main, Structure
  > L/H AFT EMERGENCY DOOR HAS A VISIBLE CRACK BELOW UPPER AFT LUG. REPAIRED IAW ENDEAVOR EA CRJ952-16409 REV IR DATED 4/29/2024.
- [SDR REXA2022060100335](https://openairdocs.org/sdr/REXA2022060100335.md): Light · inoperative · May 30, 2023 · N187GJ · Cndair CL6002D24 · Emergency Lighting
  > EXTERIOR OVERWING EMERGENCY EXIT LIGHT ON LEFT SIDE INOP R/R DS101 OVERWING EMERGENCY EXIT LIGHT IAW CRJ-900 AMM 33-51-15. GROUND WIRE WAS FOUND PULLED OUT OF PIN, RE-CRIMPED GROUND PIN IAW CRJ-900 ESPM 20-16-05. OPS CHECK GOOD. EMERGENCY LIGHT PN ON/OFF: 2L
- [SDR REXA2022030600248](https://openairdocs.org/sdr/REXA2022030600248.md): Lamp · inoperative · Feb 25, 2023 · N187GJ · Cndair CL6002D24 · Emergency Lighting
  > LEFT OVERWING FAIRING EMERGENCY LIGHT WAS BURNT OUT. R/R BULB IAW AMM 33-51-15. OPC GOOD. P/N OFF/ON: 8GH005123-06
- [SDR REXA2022011400010](https://openairdocs.org/sdr/REXA2022011400010.md): Floorbeam · corroded · Jan 6, 2022 · N187GJ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > 280 FLOOR BEAM IS CORRODED BETWEEN LBL9-BL0. MEASURING 3.5" X 1.25" X.062" DEEP. THIS IS BEYOND SRM LIMITS. - REMOVE AND REPLACE FLOOR BEAM. THIS WAS FOUND WHILE COMPLETING TASK CARD 900-53-130-300.
- [SDR REXA2022011400009](https://openairdocs.org/sdr/REXA2022011400009.md): Bracket · cracked · Nov 27, 2021 · N187GJ · Cndair CL6002D24 · Main Landing Gear
  > MAIN LANDING GEAR SIDE STAY FITTING L/H LOWER BRACKET CRACK J/C:900-57-510-500 - REMOVED AND REPLACED PN CC670-39025-1 ON LH MAIN LANDING GEAR IAW CRJ 900 SRM 51-42-06 AND 53-83-85
- [SDR REXA2022011400007](https://openairdocs.org/sdr/REXA2022011400007.md): Skin · gouged · Nov 22, 2021 · N187GJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AFT LOWER SKIN HAS 2EA GAUGES BTW F.S 927.00 & F.S 913.00 STRG 27 - REPAIRED AFT LOWER SKIN BTW F.S 913.00 & F.S 927.00, STRG 27, IAW BOMBARDIER REO#670-53-00-290
- [SDR REXA2022011400008](https://openairdocs.org/sdr/REXA2022011400008.md): Angle · corroded · Nov 18, 2021 · N187GJ · Cndair CL6002D24 · Cargo/Baggage Doors
  > GALLEY SERVICE DOOR SILL STRUCTURE IS CORRODED ON TWO PLACES DOT#-CA-009 J/C:900-53-230-500 - EVALUATED AREA REMOVED CORROSION IAW CRJ900 SRM 51-21-06 REPAIRED AREA IAW BOMBARDIER EA# CRJ953-12534
- [SDR REXA2022011400006](https://openairdocs.org/sdr/REXA2022011400006.md): Handle · cracked · Nov 17, 2021 · N187GJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > PAX DOOR-DOOR HANDLE- "PUSH IN" FLAP HAS A CRACK IN THE CORNER OF IT JC:900-52-830-300 EMP#:290BA - RMOVED AND REPLACED PAX DOOR-DOOR HANDLE- "PUSH IN" FLAP I.A.W. CRJ900 SRM 51-42-06
- [SDR V0XD20190325001](https://openairdocs.org/sdr/V0XD20190325001.md): Protector · cracked · Mar 23, 2019 · N187GJ · Cndair CL6002D24 · Cargo/Baggage Doors
  > CENTER BAG BAY DOOR FWD COUNTER BALANCE ARM UPPER HARNESS PROTECTOR CRACKED. CORRECTIVE ACTION: REMOVED AND REPLACED CENTER BAG BAY DOOR HARNESS PROTECTOR (P/N:LE670-39725-1) IAW AMM 20-21-00.
- [SDR V0XD20180305](https://openairdocs.org/sdr/V0XD20180305.md): Longeron · corroded · Mar 5, 2018 · N187GJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > LONGERON BETWEEN BS 333 AND 364 IS CORRODED. REMOVED AND REPLACED THE LONGERON IAW SRM 51-42-02, 51-42-06, 51-5-42-21, 51-40-11, AND 51-42-13.
- [SDR V0XD20180305005](https://openairdocs.org/sdr/V0XD20180305005.md): Stringer · corroded · Mar 5, 2018 · N187GJ · Cndair CL6002D24 · Fuselage Main, Structure
  > STRINGER 26R BETWEEN BS 333 AND 349 IS CORRODED. REMOVED AND REPLACED THE STRINGER IAW SRM 51-42-02, 51-42-03, 51-42-21, 51-40-11, AND 51-42-13.
- [SDR V0XD20180305004](https://openairdocs.org/sdr/V0XD20180305004.md): Stringer · corroded · Mar 5, 2018 · N187GJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 25R BETWEEN BS 295 AND 310 WAS CORRODED. REMOVED AND REPLACED THE STRINGER IAW SRM 51-42-02, 51-42-06, 51-42-21, 51-40-11, AND 51-42-13.
- [SDR V0XD20180305003](https://openairdocs.org/sdr/V0XD20180305003.md): Floorbeam · cracked · Mar 4, 2018 · N187GJ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > BS 280 FLOORBEAM ANGLE CRACKED. REMOVED AND REPLACED THE FLOORBEAM ANGLE IAW SRM 51-42-20, 51-21-0051-25-06, 51-40-11, 51-42-43, 51-42-06, AND 51-21-11.
- [SDR V0XD20180304002](https://openairdocs.org/sdr/V0XD20180304002.md): Door Sill · corroded · Mar 4, 2018 · N187GJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > RIGHT HAND FLOOR SILL AT FS 280.00 IS CORRODED. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS IAW REO 670-53-21-139 REV B DATED 2017-04-03.
- [SDR V0XD20180301002](https://openairdocs.org/sdr/V0XD20180301002.md): Intercostal · cracked · Mar 1, 2018 · N187GJ · Cndair CL6002D24 · Passenger/Crew Doors
  > INTERCOSTAL ON PAX DOOR INTERNAL STRUCTURE FOUND CRACKED. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-42-06, 51-40-11, AND 51-42-21.
- [SDR V0XD20180301001](https://openairdocs.org/sdr/V0XD20180301001.md): Web · cracked · Mar 1, 2018 · N187GJ · Cndair CL6002D24 · Passenger/Crew Doors
  > PASSENGER DOOR AFT STAIR WEB IS CRACKED IN TWO SPOTS. CUT OUT DAMAGE AND FABRICATED A DOUBLER AND FILLER AND INSTALLED IAW SRM 51-42-06, AND 52-11-04.
- [SDR V0XD2018031500001](https://openairdocs.org/sdr/V0XD2018031500001.md): Skin · cracked · Feb 22, 2018 · N187GJ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR AFT PULL-IN-CAM DOUBLER INSIDE PANEL 832AR AND INNER SKIN AT FWD PULL-IN-CAM DOUBLER INSIDE PANEL 832AL HAVE CRACKS. REPLACED PAX DOOR AFT PULL-IN-CAM DOUBLER AND FWD PULL-IN-CAM DOUBLER SKIN IAW SRM 51-42-22, 51-40-11, 51-42-06, 51-42-21, 51-42-13, 5
- [SDR N6WA2017011501](https://openairdocs.org/sdr/N6WA2017011501.md): Battery Pack · discharged · Jan 15, 2017 · N187GJ · Cndair CL6002D24 · Emergency Lighting
  > EMERGENCY LIGHTS WILL NOT STAY ILLUMINATED. CHARGED FOR SIX HOURS OPS NORMAL IAW AMM 33-51-17.
- [SDR N6WA2016122602](https://openairdocs.org/sdr/N6WA2016122602.md): Controller · malfunctioned · Dec 26, 2016 · N187GJ · Cndair CL6002D24 · Windshield/Door Rain/Ice Removal
  > RIGHT WINDOW HEAT CAUTION MESSAGE IN FLIGHT. EMERGENCY DELARED. REMOVED AND REPLACED RIGHT WINDOW TEMP CONTROLER IAW AMM 30-41-06
- [SDR N6WA2016122601](https://openairdocs.org/sdr/N6WA2016122601.md): Light · unknown · Dec 26, 2016 · N187GJ · Cndair CL6002D24 · Emergency Lighting
  > EXIT LIGHT ON MAIN CABIN DOOR INOPERATIVE. PERFORMED OPS CHECK OF EMERGENCY LIGHTS IAW AMM 33-51-00. OPS CHECKED GOOD.
- [SDR N6WA2016022504](https://openairdocs.org/sdr/N6WA2016022504.md): Indication Sys · faulty · Feb 25, 2016 · N187GJ · Cndair CL6002D24 · Door Warning System
  > PASSENGER DOOR LATCH MSG. DEFERRED PAX DOOR LATCH INDICATING SYS IAW MEL 52-70-01 CAT A.
- [SDR N6WA2016022102](https://openairdocs.org/sdr/N6WA2016022102.md): Warning System · activated · Feb 21, 2016 · N187GJ · Cndair CL6002D24 · Door Warning System
  > PASSENGER DOOR LATCH CAUTION. DEFERRED PAX DOOR INDICATION SYS IAW MEL 52-70-01 CAT A.
- [SDR N6WA2016010901](https://openairdocs.org/sdr/N6WA2016010901.md): Target · obstructed · Jan 9, 2016 · N187GJ · Cndair CL6002D24 · Door Warning System
  > PASSENGER DOOR LATCH CAUTION INTERMITTENT SEVERAL TIMES IN FLIGHT. INSPECTED PAX DOOR LATCH PROX SWITCH PX107, FOUND UNCURED SEALANT OBSTRUCTING TARGET PLATE. REMOVED SEALANT AS REQUIRED, PERFORMED OPERATIONS CHECK OF DOOR WARNING SYS. OPERATIONS CHECKED GO
- [SDR N6WA2015120901](https://openairdocs.org/sdr/N6WA2015120901.md): Warning System · false activation · Dec 9, 2015 · N187GJ · Cndair CL6002D24 · Door Warning System
  > PASSENGER DOOR OUTER HANDLE, CAUTION MSG ALONG WITH PROX SYS 2 FAULT STATUS MSG IN FLIGHT. PERFORMED SHAKEDOWN & SECURITY CHECK OF PAX DOOR WARNING & INSPECTION OF WIRING OF PAX DOOR IAW AMM 52-11-00. PERFORMED OPERATIONS CHECK OF PAX DOOR IAW 52-11-00. NO

## 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 = 'N187GJ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N187GJ/reports

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