# Service difficulty reports: N185GJ

A list on [N185GJ](https://openairdocs.org/aircraft/N185GJ.md).

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

- [SDR REXA2026081001536](https://openairdocs.org/sdr/REXA2026081001536.md): Lamp · inoperative · Aug 7, 2026 · N185GJ · Cndair CL6002D24 · Emergency Lighting
  > LH AFT EMERGENCY LIGHT DS93 INOPERATIVE. R & R LT EMERGENCY LIGHT DS93 LAMP IAW AMM 33-51-15, OPS TESTED GOOD.
- [SDR REXA2024111801490](https://openairdocs.org/sdr/REXA2024111801490.md): Floorbeam · cracked · Sep 13, 2024 · N185GJ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > RH FS 280 CROSSBEAM FOUND TO BE CRACKED ON OB END UNDER RH FLOOR SILL. REMOVED CROSSBEAM P/N CC670-34094-2 AT FS280 RH SIDE IAW CRJ900 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 AND 51-42-13-001-001-A01. LOCATED AND DRILLED NEW RH CROSSBEAM P/N CC670-34094
- [SDR REXA2024093000738](https://openairdocs.org/sdr/REXA2024093000738.md): Attach Angle · cracked · Sep 11, 2024 · N185GJ · Cndair CL6002D24 · Fuselage Main, Attach Fittings
  > IB & OB ATTACH ANGLES @ FS 280 & RBL 9 REQUIRE REPLACEMENT. LOCATED AND DRILLED NEW IB & OB ATTACH ANGLES @ FS 280 & RBL 9, IAW CRJ-900 51-40-11-001-001-A01.INSTALLED NEW SERVICEABLE ATTACH ANGLES, IB (PN CC670-34269-7) & OB (PN CC670-34269-8) AT FS 280 & RBL
- [SDR REXA2024091100709](https://openairdocs.org/sdr/REXA2024091100709.md): Stringer Splice · corroded · Aug 30, 2024 · N185GJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > UPON REMOVAL OF STR 25R SPLICE @ FS 333 IT WAS IDENTIFIED THAT THE SPLICE, PN SH670-32429-4, IS HEAVILY CORRODED AT SEVERAL LOCATIONS AND REQUIRES REPLACEMENT LOCATED AND DRILLED NEW SERVICEABLE STRINGER JOINT 25R @ FS 333, PN SH670-32429-4, IAW CRJ 900 SRM 51
- [SDR REXA2024111401483](https://openairdocs.org/sdr/REXA2024111401483.md): Stringer · corroded · Aug 29, 2024 · N185GJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STR 24R BETWEEN FS 280 TO FS 333 HAS CORROSION. UPON EVAL STR 24R HAS CORROSION THAT EXCEEDS THE ALLOWABLE LIMITS OF 10 PERCENT MATERIAL LOSS DUE TO EXCESSIVE CORROSION NEAR MULTIPLE FASTENER LOCATIONS IAW CRJ 900 SRM 53-21-03-101-003-A04 REMOVE AND REPLACE RE
- [SDR REXA2024091000701](https://openairdocs.org/sdr/REXA2024091000701.md): Web · corroded · Aug 29, 2024 · N185GJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "RH FS 280 LOWER WEB IS CORRODED AT RBL 11 UNDER CAP ANGLE. REMOVED CAP ANGLE AT FS280 RH SIDE IAW CRJ900 SRM 51-42-06-001-001-A01 AND 51-42-13-001-001-A01. REMOVED CORROSION ON LOWER WEB AT RBL 11 ORIGINAL MATERIAL 0.040"", MRT 0.029"" MATERIAL REMOVED 0.011"
- [SDR REXA2024091000699](https://openairdocs.org/sdr/REXA2024091000699.md): Stringer Splice · corroded · Aug 29, 2024 · N185GJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER SPLICE FROM STR 23R AND FS 333 IS CORRODED. STRINGER 23R SPLICE AT F.S. 333 IS IDENTIFIED AS P/N SH670-32429-4 AND IS CORRODED ACROSS ENTIRE LENGTH. NO ALLOWABLE DAMAGE LIMITS PROVIDED IN CR- J-900 SRM. PART REQUIRES REPLACE. REMOVED STRINGER SPLICE F
- [SDR REXA2024091000698](https://openairdocs.org/sdr/REXA2024091000698.md): Stringer · corroded · Aug 29, 2024 · N185GJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STR 25R BETWEEN FS 280 TO FS 333 HAS CORROSION. REMOVED STR 25R @ FR 333 IAW CRJ 900 SRM 51-42-06-001-001-A01 REMOVED 1 WIRE STANDOFF @ FS 319 - FS 333, AND 1 WIRE STANDOFF @ FS 295 - FS 310 ON STR 25R IAW CRJ 900 SRM 51-42-06-001-001-A01 REMOVED 2 STANDOFFS A
- [SDR REXA2024091000697](https://openairdocs.org/sdr/REXA2024091000697.md): Stringer · corroded · Aug 29, 2024 · N185GJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STR 22R BETWEEN FS 280 TO FS 333 HAS CORROSION. UPON EVAL STR 22R FROM FS 280 TO FS 333 HAS CORROSION THAT EXCEEDS THE ALLOWABLE LIMITS OF 10 PERCENT MATERIAL LOSS DUE TO EXCESSIVE CORROSION NEAR MULTIPLE FASTENER LOCATIONS IAW CRJ 900 SRM 53-21-03-101-002-A04
- [SDR REXA2024090600685](https://openairdocs.org/sdr/REXA2024090600685.md): Stringer Splice · corroded · Aug 29, 2024 · N185GJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER SPLICE FROM STGR 22R AND FS 333 IS CORRODED. REMOVED STRINGER SPLICE FROM STGR 22R F.S. 333 IAW CRJ 900 SRM 51-42-06-001-001-A01 & CRJ 900 SRM 51-42-21-001-001-A01. INSTALLED NEW SERVICEABLE STGR 22R STRINGER SPLICE P/N: SH670-32429-4 IAW CRJ900 SRM 5
- [SDR REXA2024090600684](https://openairdocs.org/sdr/REXA2024090600684.md): Stringer · corroded · Aug 29, 2024 · N185GJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STR 23R BETWEEN FS 280 TO FS 333 HAS CORROSION. REMOVED STR 23R FROM FS 280 - FS 333 IAW CRJ 900 SRM 51-42-06-001-001-A01 & CRJ 900 SRM 51-42-21-001-001-A01. INSTALLED NEW SERVICEABLE STGR 23R P/N: SH670-31211-4U IAW CRJ900 SRM 51-42-06-001-001-A01. AND CRJ900
- [SDR REXA2024092300717](https://openairdocs.org/sdr/REXA2024092300717.md): Angle · cracked · Aug 26, 2024 · N185GJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "ANGLE AT FS 280 LBL 9.0 INBOARD CRACKED P/N CC670-34269-6 FABRICATED 1EA ANGLE PN CC670-34010-S0201 AS REQUIRED USING 7475-T7351 PO# W93332 IAW STEPS 1-2 OF MHIRJ SNIEO CC670-34010 IDENTIFIER S21.APPLIED PROTECTIVE FINISH AND IDENTIFY NEW FABRICATED ANGLE WIT
- [SDR REXA2024091000696](https://openairdocs.org/sdr/REXA2024091000696.md): Stringer · corroded · Aug 23, 2024 · N185GJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STR27 BETWEEN F.S. 280-295 CORRODED. UPON FURTHER INVESTIGATION STR 27 FROM FS 280 - FS 295 FOUND TO BE OUT OF LIMITS PER CRJ 900 SRM 53-21-03-101-002-A04 REMOVED CLEAT ON F.S. 295, STGR 27 FOR ACCESS AND EVAL. IAW CRJ900 SRM 51-42-06-001-001-A01. REMOVED STR
- [SDR REXA2024100900865](https://openairdocs.org/sdr/REXA2024100900865.md): Floor Support · corroded · Aug 21, 2024 · N185GJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > RBL 9 FLOOR BEAM BETWEEN FS 1000 AND FS 1069 IS CORRODED REPAIRED IAW CRJ900 SRM SRM 53-00-41-201-001-A03.
- [SDR REXA2024091000695](https://openairdocs.org/sdr/REXA2024091000695.md): Seat Track · corroded · Aug 21, 2024 · N185GJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > RBL 9 SEAT TRACK FROM FS 669 - FS 847 IS CORRODED. REMOVED RBL 9 SEAT TRACK FROM FS 669 - FS 847 IAW CRJ900 AMM 53-00-49-100-801 (CONFIG A13) FABRICATED NEW RBL 9 SEAT TRACK P/N KBA690-41125-26 USING EXTRUSION TRACK PN 20276-288-0-0A PO: W77329 IAW REO-670-53-
- [SDR REXA2024091000694](https://openairdocs.org/sdr/REXA2024091000694.md): Seat Track · corroded · Aug 21, 2024 · N185GJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK STA 744-752 STR 15R CORREDED AND REQUIRES REPLACEMENT REMOVE SEAT TRACK IAW REO # 670-53-00-587 AND MOD SUM # IIS670530000195 PRIMED AND PAINTED INSTALLED SEAT TRACK STA 744-752 STR 15R IAW CRJ900 AMM 53-00-49-400-801 (CONFIG A13)
- [SDR REXA2024111401482](https://openairdocs.org/sdr/REXA2024111401482.md): Stringer · corroded · Aug 19, 2024 · N185GJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STR 20R BETWEEN 295-319 IN RIVET ROW CORRODED REMOVED CORROSION ON STGR 20R IAW CRJ900 SRM 51-21-06-001-001-A01. FOUND TO BE OUT OF LIMITS ALLOWED DAMAGE IAW CRJ900 SRM 53-21-03-101-002-A04. REQUIRES REPLACE. REMOVED STGR 20R SEGMENT FROM FS 280.00 TO FS 319.
- [SDR REXA2024111101459](https://openairdocs.org/sdr/REXA2024111101459.md): Channel · corroded · Aug 19, 2024 · N185GJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "ANTENA DOUBLER F.S. 295-310 STR 27 CORRODED. UPON FURTHER INVESTIGATION, FOUND CORROSION ON ANTENNA DOUBLER AT F.S. 295-310 STR 27, ORIGINAL MATERIAL THICKNESS OF 0.050"", AFTER CORROSION REMOVAL OF 0.050"", 100% MATERIAL LOSS, DOUBLER FOUND TO BE OUT OF LIMI
- [SDR REXA2024091000692](https://openairdocs.org/sdr/REXA2024091000692.md): Stringer · corroded · Aug 19, 2024 · N185GJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "STGR 23R BETWEEN FS 364 AND FS 379 HAS CORROSION. REMOVED CAP ANGLE AT FS280 RH SIDE IAW CRJ900 SRM 51-42-06-001-001-A01 AND 51-42-13-001-001-A01. REMOVED CORROSION ON LOWER WEB AT RBL 11 ORIGINAL MATERIAL 0.040"", MRT 0.029"" MATERIAL REMOVED 0.011"" MATERIA
- [SDR REXA2024091000691](https://openairdocs.org/sdr/REXA2024091000691.md): Stringer · corroded · Aug 19, 2024 · N185GJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STR 26R CORRODED FROM F.S. 280-333 REMOVED CORROSION ON STGR 26R (P/N:SH670-31634-2) BETWEEN F.S 280.00 TO F.S. 333.00 IAW CRJ900 SRM 51-21-06-001-001-A01. FOUND TO BE OUT OF LIMITS ALLOWED IAW CRJ90 SRM 53-21-03-101-002-A04. REQUIRES REPLACE. REMOVED STGR 26
- [SDR REXA2024091000690](https://openairdocs.org/sdr/REXA2024091000690.md): Door Sill · corroded · Aug 19, 2024 · N185GJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > PAX DOOR SURROUND STRUCTURE INTERCOSTAL AT STR. 21L BETWEEN FS.319.00 AND FS.333.00 IS CORRODED. PAX DOOR SURROUND STRUCTURE INTERCOSTAL AT STR. 21L BETWEEN FS.319.00 AND FS.333.00 IS CORRODED. INTERCOSTAL AT STR. 21L BETWEEN FS.319.00 AND FS.333.00 IS CORRODE
- [SDR REXA2024090400680](https://openairdocs.org/sdr/REXA2024090400680.md): Angle · corroded · Aug 19, 2024 · N185GJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FS.280 J ANGLE IS CORRODED. EVALUATED FS 280 J ANGLE ORIGINAL MATERIAL IS.063 REMAINING IS.048 LOSS OF.015 FOUND TO BE OUT OF LIMITS IAW CRJ 900 SRM 53-21-43-101-001-A03. REMOVED AND REPLACED J ANGLE P/N: CC670-34095-1 AT FS 280IAW CRJ 900 SRM 51-42-06-00
- [SDR REXA2024111401481](https://openairdocs.org/sdr/REXA2024111401481.md): Angle · corroded · Aug 18, 2024 · N185GJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > THE TWO CENTER INTERCOSTALS AT THE FRONT END OF THE MAIN AVIONICS DOOR SURROUND STRUCTURE ARE CORRODED. 2 EA. INTERCOSTALS AT F.S. 349 - F.S. 364 STGR 27L & 27R CORRODED AND FOUND TO BE OUT OF LIMITS IAW CRJ-900 SRM 53-21-23-101-003-A02. REMOVED AND INSTALLED
- [SDR REXA2024101400872](https://openairdocs.org/sdr/REXA2024101400872.md): Cargo Track · corroded · Aug 18, 2024 · N185GJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > "THE BEAM AT LBL9 HAS AREAS OF CORROSION BETWEEN FS 1015 AND FS 1069. THE BEAM AT LBL9 BETWEEN FS 1015 AND FS 1069 REMOVED CORROSION IAW CRJ 900 SRM 51-21-06-001-001-A01 REQUIRES NDT. PERFORMED UT THICKNESS OF FLOOR BEAM LBL9 FS1015-FS1069 REWORKED AREAS IAW
- [SDR REXA2024100700850](https://openairdocs.org/sdr/REXA2024100700850.md): Floor Support · corroded · Aug 18, 2024 · N185GJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "AREAS OF CORROSION FOUND ON FLOOR BEAM AT LBL 27 BETWEEN FS 1005 AND FS 1047. INSTALLED LBL 27 FLOOR BEAM SEGMENT FROM FS985 TO FS1051 IAW CRJ900 SRM 53-00-41-201-001-A03. STEPS 5B(8-11). DAMAGE SECTION OF THE FLOOR BEAM WAS CUT AT LBL27 FS1056 IAW CRJ900 SRM
- [SDR REXA2024101400873](https://openairdocs.org/sdr/REXA2024101400873.md): Angle · corroded · Aug 10, 2024 · N185GJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > GALLEY SERVICE DOOR LOWER SILL ANGLE IS CORRODED BETWEEN F.S.319 TO F.S.349 REMOVED AND REPLACED SERVICE DOOR LOWER SILL ANGLE PN SH670-31996-3 IAW CRJ 900 SRM 51-41-02-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.
- [SDR REXA2024082200662](https://openairdocs.org/sdr/REXA2024082200662.md): Angle · corroded · Aug 10, 2024 · N185GJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > GALLEY SERVICE DOOR LOWER SILL ANGLE IS CORRODED BETWEEN F.S.319 TO F.S.349 REMOVED AND REPLACED SERVICE DOOR LOWER SILL ANGLE PN SH670-31996-3 IAW CRJ 900 SRM 51-41-02-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.
- [SDR V0XD0201802200002](https://openairdocs.org/sdr/V0XD0201802200002.md): Fitting · cracked · Feb 17, 2018 · N185GJ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR LINTEL CRACKED. ACCOMPLISHED REO 670-53-493 REV D DATED 2015-07-10 BY PERFORMING PERMANENT REPAIR SB 670-53-040 PART B REV C DATED SEP 20 2012.
- [SDR V0XD20180216003](https://openairdocs.org/sdr/V0XD20180216003.md): Floorbeam · cracked · Feb 16, 2018 · N185GJ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > LEFT BS 280 FLOORBEAM HAS A CRACK. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-42-13, AND SRM 51-42-06.
- [SDR V0XD20180216002](https://openairdocs.org/sdr/V0XD20180216002.md): Floorbeam · corroded · Feb 16, 2018 · N185GJ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > RT FWD FLOORBEAM ANGLE HAS SIGNS OF CORROSION AT BS 280. REPAIRED FLOORBEAM ANGLEL IAW REO 670-53-21-139, REV B.
- [SDR V0XD20180216001](https://openairdocs.org/sdr/V0XD20180216001.md): Floorbeam · corroded · Feb 16, 2018 · N185GJ · Cndair CL6002D24 · Fuselage Structure (General)
  > RIGHT BS 280 FLOORBEAM HAS SIGNS OF CORROSION. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-42-21, 51-42-06, AND 51-42-13,
- [SDR V0XD20180211001](https://openairdocs.org/sdr/V0XD20180211001.md): Stiffener · cracked · Feb 11, 2018 · N185GJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > RT FS 280 BULKHEAD WEB SUPPORT STIFFENER ANGLE AT RT BL 26.00 IS CRACKED. REMOVED AND REPLACED CRACKED WEB STIFFENER ANGLE IAW SRM 51-40-11, 51-42-06, 51-42-21.
- [SDR V0XD20170213DP01](https://openairdocs.org/sdr/V0XD20170213DP01.md): Stringer Splice · corroded · Feb 6, 2018 · N185GJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER SPLICE 26R CORRODED OUT OF LIMITS IAW SRM 53-21-03, BETWEEN BS 319.70 AND 349. REMOVED AND REPLACED THE STRINGER SPLICE IAW SRM 51-42-06.
- [SDR N6WA2017030801](https://openairdocs.org/sdr/N6WA2017030801.md): Assist System · inoperative · Mar 8, 2017 · N185GJ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR ASSIST INOPERATIVE.
- [SDR V0XD20170305012](https://openairdocs.org/sdr/V0XD20170305012.md): Stringer · cracked · Feb 23, 2017 · N185GJ · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > PASSENGER DOOR LINTEL STR 3 AT FS 280.00 IS CRACKED. REMOVED CRACKED ANGLE, FABRICATED AND INSTALLED REPAIR PARTS IAW REO 670-53-21-493 REV D, AND SRM 20-30-00 AND 20-20-00. NDT PERFORMED. THIS REPAIR IS A TEMPORARY REPAIR GOOD FOR 6000 FLIGHT HRS IAW REO 67
- [SDR N6WA2016062001](https://openairdocs.org/sdr/N6WA2016062001.md): Lens · misinstalled · Jun 20, 2016 · N185GJ · Cndair CL6002D24 · Emergency Lighting
  > PAX DOOR EMERGENCY LIGHT LENS UPSIDE DOWN. REPOSTIONED MAIN DOOR EMERGENCY LIGHT IAW AMM 33-51-15.
- [SDR N6WA2016021301](https://openairdocs.org/sdr/N6WA2016021301.md): Warning System · activated · Feb 13, 2016 · N185GJ · Cndair CL6002D24 · Door Warning System
  > PASSENGER DOOR OUTER HANDLE MSG. DEFERRED PAX DOOR OUTER HANDLE MSG IAW MEL 52-70-01 CAT A.
- [SDR N6WA2016010802](https://openairdocs.org/sdr/N6WA2016010802.md): Cover · unsecure · Jan 8, 2016 · N185GJ · Cndair CL6002D24 · Emergency Exits
  > LEFT SIDE EMER EXIT HANDLE COVER FALLING DOWN. SECURED EMER EXIT HANDLE COVER WITH VELCRO IAW AMM 51-22-61.
- [SDR N6WA2015111501](https://openairdocs.org/sdr/N6WA2015111501.md): Tire · separated · Nov 15, 2015 · N185GJ · Cndair CL6002D24 · Tire
  > HIGH SPEED ABORTED TAKEOFF AT 100 KTS FOR BLOWN TIRE, NOSE. TIRE NOT BLOWN, FOUND TREAD SEPARATION. R & R LT & RT NOSE WHEEL ASSEMBLIES.

## 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 = 'N185GJ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N185GJ/reports

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