# Service difficulty reports: N540GJ A list on [N540GJ](https://openairdocs.org/aircraft/N540GJ.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR N6WA2026040803](https://openairdocs.org/sdr/N6WA2026040803.md): Lamp · inoperative · Apr 7, 2026 · N540GJ · Cndair CL6002C11 · Emergency Lighting > AFT CEILING EMERGENCY FLOODLIGHT INOPERATIVE. LAMPED THE AFT FLOODLIGHT IAW CRJ AMM 33-51-09. OPS CHECK GOOD. - [SDR N6WA2026012901](https://openairdocs.org/sdr/N6WA2026012901.md): Filter · odor · Jan 28, 2026 · N540GJ · Cndair CL6002C11 · Air Distribution System > ACIDIC SMOKE ODOR IN CABIN AFTER DEICE-RTG. R & R RT & LT RECIRCULATION FAN FILTERS IAW AMM 21-22-21. OPS CHECKED GOOD. NO SMOKE DETECTED. - [SDR N6WA2025111202](https://openairdocs.org/sdr/N6WA2025111202.md): Door · no discrepancy · Nov 10, 2025 · N540GJ · Cndair CL6002C11 · Emergency Exits > LH OVERWING EMERG. EXIT DOOR HARD TO OPEN. OPS CHECKED LH EMERG. EXIT DOOR IAW CRJ AMM 52-21-00. OPS CHECK GOOD. NO DEFECTS NOTED. - [SDR N6WA2025111201](https://openairdocs.org/sdr/N6WA2025111201.md): Door · obstructed · Nov 10, 2025 · N540GJ · Cndair CL6002C11 · Emergency Exits > OVERHEAD BIN AT LT EMERG. EXIT OBSTRUCTING DOOR OPERATION. ADJUSTED OVERHEAD BIN IAW CRJ AMM 25-23-00. OPS CHECK GOOD. - [SDR N6WA2025041903](https://openairdocs.org/sdr/N6WA2025041903.md): Frame · corroded · Apr 18, 2025 · N540GJ · Cndair CL6002C11 · Fuselage Main, Frame > CORROSION ON ATTACHED FLANGE AND WEB AT FS295 BETWEEN STGR26L AND STGR25R. REMOVED AND REPLACED FRAME AND ATTACHED FLANGE IAW AWATS EO-25-CRJ5-53-066 AND GOJET EO-C550-53MR-065-O. - [SDR N6WA2025041902](https://openairdocs.org/sdr/N6WA2025041902.md): Frame · corroded · Apr 18, 2025 · N540GJ · Cndair CL6002C11 · Fuselage Main, Frame > CORROSION ON ATTACHED FLANGE AND WEB AT FS310.00 BETWEEN STGR26L AND STGR25R. REMOVED AND REPLACED FRAME AND ATTACHED FLANGE IAW AWATS EO-25-CRJ5-53-065 AND GOJET EO-C550-53MR-066-O - [SDR N6WA2025041901](https://openairdocs.org/sdr/N6WA2025041901.md): Fire Bottle · failed insp · Apr 16, 2025 · N540GJ · Cndair CL6002C11 · Extinguishing System > LAV TRASH CAN FIRE BOTTLE WEIGHT CHECK BAD. REMOVED AND REPLACED LAV FIRE BOTTLE IAW CRJ AMM 26-26-01. - [SDR N6WA2025041601](https://openairdocs.org/sdr/N6WA2025041601.md): Angle · corroded · Apr 16, 2025 · N540GJ · Cndair CL6002C11 · Fuselage Miscellaneous Structure > CORROSION ON FWD SUPPORT OF AVI BAY MID FLOORBOARD AT FS280 AND STRINGER 27 IS OUT OF LIMITS. REMOVED AND REPLACED THE FWD SUPPORT OF THE AVI BAY MID FLOORBOARD AT FS280 AND STRINGER 27 IAW CRJ SRM 51-42-06 - [SDR N6WA2025041505](https://openairdocs.org/sdr/N6WA2025041505.md): Frame · corroded · Apr 15, 2025 · N540GJ · Cndair CL6002C11 · Fuselage Main, Frame > CORROSION ON FRAME AT FS319 BETWEEN STRINGER 25L AND STRINGER 25R IS OUT OF LIMITS. REPAIRED FRAME AT FS319 BETWEEN STRINGER 25L AND STRINGER 25R IAW GOJET EO C550-53MR-049. - [SDR N6WA2025041504](https://openairdocs.org/sdr/N6WA2025041504.md): Frame · corroded · Apr 15, 2025 · N540GJ · Cndair CL6002C11 · Fuselage Main, Frame > CORROSION ON FS349 BETWEEN STRINGER 25R AND STRINGER 25L. REPAIRED FS349 BETWEEN STRINGER 25R AND STRINGER 25L IAW GOJET EO C550-53MR-049. - [SDR N6WA2025041503](https://openairdocs.org/sdr/N6WA2025041503.md): Stringer · corroded · Apr 15, 2025 · N540GJ · Cndair CL6002C11 · Fuselage Main, Longeron/Stringer > CORROSION ON STRINGER BETWEEN FS349 - FS364 AND STRINGER 20L IS OUT OF LIMITS. REPAIRED STRINGER BETWEEN FS349 - FS364 AND STRINGER 20L IAW GOJET EO C550-53MR-064 AND STS EA 129-2025-063IR. - [SDR N6WA2025041502](https://openairdocs.org/sdr/N6WA2025041502.md): Doubler · gouged · Apr 15, 2025 · N540GJ · Cndair CL6002C11 · Fuselage Main, Plate/Skin > DAMAGE ON THE FUSELAGE AFT BELLY SKIN DOUBLER AT FS985 AND STRINGER 27. REPAIRED THE FUSELAGE AFT BELLY SKIN DOUBLER AT FS985 AND STRINGER 27 IAW GOJET EO C550-53MR-063. - [SDR N6WA20250415001](https://openairdocs.org/sdr/N6WA20250415001.md): Doubler · gouged · Apr 15, 2025 · N540GJ · Cndair CL6002C11 · Fuselage Main, Plate/Skin > DAMAGE ON THE FUSELAGE AFT BELLY SKIN DOUBLER AT FS985 AND STRINGER 27. REPAIRED THE FUSELAGE AFT BELLY SKIN DOUBLER AT FS985 AND STRINGER 27 IAW GOJET EO C550-53MR-063. - [SDR N6WA2025041501](https://openairdocs.org/sdr/N6WA2025041501.md): Skin · dented · Apr 15, 2025 · N540GJ · Cndair CL6002C11 · Wing, Plate/Skin > RH WING HAS A DENT AT SLAT TRACK 1-3. REPAIRED RH WING AT SLAT TRACK 1-3 IAW GOJET EO-C550-57MR-009 AND STS EA 79-2025-066. - [SDR N6WA2025040812](https://openairdocs.org/sdr/N6WA2025040812.md): Seat Track · corroded · Apr 8, 2025 · N540GJ · Cndair CL6002C11 · Fuselage, Seat/Cargo Attach Fittings > RH SIDE SEAT RAIL AT FS797.00 - FS830.00 IS CORRODED OUT OF LIMITS. REMOVED AND REPLACED RH SIDE SEAT RAIL AT FS797.00 - FS830.00 IAW CRJ AMM 53-00-49. - [SDR N6WA2025040811](https://openairdocs.org/sdr/N6WA2025040811.md): Floor Support · corroded · Apr 8, 2025 · N540GJ · Cndair CL6002C11 · Fuselage Miscellaneous Structure > CORROSION ON RH SILL AT FS280.00 - FS319.00 IS OUT OF LIMITS. REMOVED AND REPLACED THE RH SILL AT FS280.00 - FS319.00 IAW CRJ SRM 51-42-06. - [SDR N6WA2025040810](https://openairdocs.org/sdr/N6WA2025040810.md): Seat Track · corroded · Apr 8, 2025 · N540GJ · Cndair CL6002C11 · Fuselage, Seat/Cargo Attach Fittings > RHIB #4 SEAT TRACK IS CORRODED OUT OF LIMITS AT FS682 - FS837. REMOVED AND REPLACED THE RHIB #4 SEAT TRACK AT FS682 - FS837. - [SDR N6WA2025040809](https://openairdocs.org/sdr/N6WA2025040809.md): Seat Track · corroded · Apr 8, 2025 · N540GJ · Cndair CL6002C11 · Fuselage, Seat/Cargo Attach Fittings > RHIB #3 SEAT TRACK IS CORRODED AND OUT OF LIMITS AT FS581.00 - FS682.00. REMOVED AND REPLACED RHIB #3 SEAT TRACK IAW CRJ AMM 53-00-49. - [SDR N6WA2025040808](https://openairdocs.org/sdr/N6WA2025040808.md): Seat Track · corroded · Apr 8, 2025 · N540GJ · Cndair CL6002C11 · Fuselage, Seat/Cargo Attach Fittings > RHIB #2 SEAT TRACK IS CORRODED OUT OF LIMITS AT FS485.00 - 581.00. REMOVED AND REPLACED RHIB #2 SEAT TRACK IAW CRJ AMM 53-00-49. - [SDR N6WA2025040807](https://openairdocs.org/sdr/N6WA2025040807.md): Seat Track · corroded · Apr 8, 2025 · N540GJ · Cndair CL6002C11 · Fuselage, Seat/Cargo Attach Fittings > RHIB #1 SEAT TRACK IS CORRODED IS OUT OF LIMITS AT FS350 TO FS485. REMOVED AND REPLACED RHIB #1 SEAT TRACK IAW CRJ AMM 53-00-49. - [SDR N6WA2025040806](https://openairdocs.org/sdr/N6WA2025040806.md): Seat Track · corroded · Apr 8, 2025 · N540GJ · Cndair CL6002C11 · Fuselage, Seat/Cargo Attach Fittings > LHIB #4 SEAT TRACK IS CORRODED OUT OF LIMITS AT FS682 - FS837. REMOVED AND REPLACED THE LHIB #4 SEAT TRACK IAW CRJ AMM 53-00-49. - [SDR N6WA2025040805](https://openairdocs.org/sdr/N6WA2025040805.md): Seat Track · corroded · Apr 8, 2025 · N540GJ · Cndair CL6002C11 · Fuselage, Seat/Cargo Attach Fittings > LHIB #1 SEAT TRACK IS CORRODED OUT OF LIMITS AT FS475 - FS485. REPAIRED LHIB #1 SEAT TRACK IAW MHIRJ REO670-53-00-589. - [SDR N6WA2025040804](https://openairdocs.org/sdr/N6WA2025040804.md): Intercostal · corroded · Apr 8, 2025 · N540GJ · Cndair CL6002C11 · Fuselage Miscellaneous Structure > CORROSION ON INTERCOSTAL AT STRINGER 26L BETWEEN FS349 - FS364 IS OUT OF LIMITS. REMOVED AND REPLACED INTERCOSTAL AT STRINGER 26L BETWEEN FS349 - FS364 IAW CRJ SRM 51-42-06. - [SDR N6WA2025040803](https://openairdocs.org/sdr/N6WA2025040803.md): Intercostal · corroded · Apr 8, 2025 · N540GJ · Cndair CL6002C11 · Fuselage Miscellaneous Structure > CORROSION ON INTERCOSTAL AT STRINGER 26R BETWEEN FS349 - FS364 IS OUT OF LIMITS. REMOVED AND REPLACED INTERCOSTAL AT STRINGER 26R AND FS349 - FS364 IAW CRJ SRM 51-42-06. - [SDR N6WA2025040802](https://openairdocs.org/sdr/N6WA2025040802.md): Support · corroded · Apr 8, 2025 · N540GJ · Cndair CL6002C11 · Fuselage Miscellaneous Structure > CORROSION ON BACK UP SILL AT FS333 - FS349 AT STRINGER 21L IS OUT LIMITS. REMOVED AND REPLACED BACK UP SILL AT FS333 - FS349 AND STRINGER 21L IAW CRJ SRM 51-42-06. - [SDR N6WA2025040801](https://openairdocs.org/sdr/N6WA2025040801.md): Support · corroded · Apr 8, 2025 · N540GJ · Cndair CL6002C11 · Fuselage Miscellaneous Structure > CORROSION ON BACK UP SILL AT FS310 - FS333 AND STRINGER 21L IS OUT OF LIMITS. REMOVED AND REPLACED BACK UP SILL AT FS310 - FS333 AND STINGER 21L IAW CRJ SRM 51-42-06. - [SDR N6WA2024020501](https://openairdocs.org/sdr/N6WA2024020501.md): Battery Pack · inoperative · Feb 4, 2024 · N540GJ · Cndair CL6002C11 · Emergency Lighting > EMERGENCY LIGHTS ON WITH SWITCH IN ARM. REMOVED AND REPLACED ALL 4 EMERGENCY BATTERIES, OPS CHECK GOOD CRJ 550 AMM 33-51-17. - [SDR N6WA2023061901](https://openairdocs.org/sdr/N6WA2023061901.md): Loop · grounded · Jun 17, 2023 · N540GJ · Cndair CL600* · Detection System > L CAI DUCT WARNING IN FLIGHT. (RAN QRH MSG PERSISTED, SHUT ENGINE DOWN). FOUND COWL ANTI-ICE VALVE BLEED DUCT LOOPS TOUCHING AND MAKING CONTACT WITH THE CLAMPS. REPOSITIONED LOOPS IAW CRJ 550 AMM 36-21-01. PERFORMED LOOP TEST IN AILC IAW CRJ AMM 30-12-12. NO F - [SDR N6WA2023052502](https://openairdocs.org/sdr/N6WA2023052502.md): Bulb · inoperative · May 24, 2023 · N540GJ · Cndair CL600* · Emergency Lighting > CEILING EMERGENCY LIGHT ABOVE ROW 7 IS BURNT OUT. DEFERRED CEILING EMERGENCY LIGHT ABOVE ROW 7 IAW MEL 33-51-01B-2A CAT C OCN 70081895 AUTH BY MXC. - [SDR N6WA2023030601](https://openairdocs.org/sdr/N6WA2023030601.md): A/C Pack · inoperative · Mar 4, 2023 · N540GJ · Cndair CL600* · Cabin Cooling System > LEFT PACK TEMP FOLLOWED BY LEFT PACK CAUTION LIGHT. DEFERRED LEFT PACK TEMP FOLLOWED BY LEFT PACK CAUTION LIGHT IAW MEL 21-51-01B CATEGORY C ON OCN 70081227. CORRECTY PRIOR TO 3-15-23. AUTHORIZED BY MXC ADAM BUELOW 80794 - [SDR N6WA2023022704](https://openairdocs.org/sdr/N6WA2023022704.md): Bulb · inoperative · Feb 26, 2023 · N540GJ · Cndair CL600* · Emergency Lighting > EMERGENCY CABIN OVERHEAD LIGHT ROW 7 AND 9 INOP. R&R CEILING EMERGENCY FLOOD LIGHT BULBS IN ROWS 7 &9. OPS CHECK GOOD AT THIS TIME. ALL WORK DONE IAW CRJ 550 AMM 33-51-09. - [SDR N6WA20220606](https://openairdocs.org/sdr/N6WA20220606.md): Battery · inoperative · Jun 5, 2022 · N540GJ · Cndair CL600* · Emergency Lighting > EMERGENCY LIGHTS SWITCH FOUND IN THE ON POSITION ON THE F/A PANEL.CHARGED EMERGENCIES BATTERIES AND PERFORMED OPS CHECK IAW CRJ550 AMM 33-51-00. OPS CHECK GOOD. OK FOR SERVICE. - [SDR N6WA2022020402](https://openairdocs.org/sdr/N6WA2022020402.md): None · none · Feb 2, 2022 · N540GJ · Cndair CL600* · Aircraft Fuel Distribution System > FUEL IMBALANCE IN FLIGHT - RETURN FROM FLIGHT. PERFORMED FUEL SYS. OPERATIONAL CHECKS IAW CRJ 550 AMM # 28-41-22/ 28-13-00. OPS. CHECK GOOD ALL INDICATIONS NORMAL. - [SDR N6WA2021052901](https://openairdocs.org/sdr/N6WA2021052901.md): Stringer · worn · May 29, 2021 · N540GJ · Cndair CL600* · Fuselage Main, Longeron/Stringer > STRINGER 7R @ FS1144 TO FS1162 DAMAGED. R&R STRINGER 7R @ FS1144 TO FS1162 IAW STR 7R IAW DRAWING MM670-38025 REV AA - [SDR N6WA2021020301](https://openairdocs.org/sdr/N6WA2021020301.md): Acm · seized · Feb 3, 2021 · N540GJ · Cndair CL6002C10 · Cabin Cooling System > LEFT AND RIGHT PACK FAULT STATUS. FOUND LEFT PACK ACM SEIZED, REMOVED AND REPLACED ACM IAW CRJ 550 AMM 21-51-08. SEE LOG PG 498927 ITEM 2 FOR OPS CHECK. LH AND RH PACKS OPS CHECK GOOD IAW CRJ 550 AMM 21-51-00 P/NON/OFF GG670-95009-7 S/N ON 02193 S/N OFF 02184 - [SDR N6WA2020110604](https://openairdocs.org/sdr/N6WA2020110604.md): Fitting · corroded · Nov 6, 2020 · N540GJ · Cndair CL600* · Passenger/Crew Doors > PAX DOOR FWD FRAME AT LOWER TENSION FITTING EVIDENCE OF CORROSION. INSTALLED REPAIR,IAW EA 72-2020-205. - [SDR N6WA2020110603](https://openairdocs.org/sdr/N6WA2020110603.md): Door Sill · corroded · Nov 6, 2020 · N540GJ · Cndair CL600* · Fuselage Miscellaneous Structure > SERVICE DOOR SILL MOUNTING ANGLE HAS CORROSION UNDER LOWER SILL ANGLES. REMOVED AND REPLACED SERVICE DOOR SILL MOUNTING ANGLE, IAW CRJ700 SRM 51-40-06. - [SDR N6WA2020110602](https://openairdocs.org/sdr/N6WA2020110602.md): Skin · corroded · Nov 6, 2020 · N540GJ · Cndair CL600* · Fuselage Main, Plate/Skin > CORROSION ON INNER SKIN STRG 27-26 RT, FS 319.7-327.00. REPAIRED CORROSION ON INNER SKIN, IAW REO 670-53-21-1844. - [SDR N6WA2020110601](https://openairdocs.org/sdr/N6WA2020110601.md): Transcowl · cracked · Nov 6, 2020 · N540GJ · Cndair CL600* · Engine Thrust Reverser > RT LOWER T/R EXTRUSION CRACKED ON INBOARD SIDE. REMOVED AND REPLACED RT LOWER TRANS COWL, IAW CRJ 700 AMM 78-33-01. PERFORMED OPERATIONS CHECK, NO DEFECTS FOUND. - [SDR N6WA2020102202](https://openairdocs.org/sdr/N6WA2020102202.md): Slat Track · cracked · Oct 22, 2020 · N540GJ · Cndair CL600* · Leading Edge Devices > LT SLAT TRACK 2-3 CANISTER AFT ATTACH FLANGE CRACKED. FABRICATED PARTS AND COMPLEATED REPAIRS, IAW REO 670-57-42-577. - [SDR N6WA2020102201](https://openairdocs.org/sdr/N6WA2020102201.md): Skin · dented · Oct 22, 2020 · N540GJ · Cndair CL600* · Leading Edge Devices > RT NR 1 SLAT DENTED AT SS 177.875 REPAIR COMPLETE, IAW STS EA 80-2020-021. - [SDR N6WA2020102101](https://openairdocs.org/sdr/N6WA2020102101.md): Support · cracked · Oct 21, 2020 · N540GJ · Cndair CL600* · Fuselage Miscellaneous Structure > AFT WING TO FUSE FAIRING SUPPORT ATTACHMENT PIECE IS CRACKED ON THE LT SIDE JUST AFT OF FS 909.00. REMOVED DAMAGED AREA, IAW EA20-2020-095. REPAIRED IAW EA20-2020-095 AND CRJ 700 SRM 51-42-00. - [SDR N6WA2020101907](https://openairdocs.org/sdr/N6WA2020101907.md): Intercostal · corroded · Oct 19, 2020 · N540GJ · Cndair CL600* · Fuselage Miscellaneous Structure > CORROSION AT REAR AVIONICS DOOR SURROUND INTERCOSTAL 27R. INSPECTED CORROSION DAMAGE, IAW CRJ 700 SRM 51-21-06. REMOVED.001 METAL, PAINTED REAR AVIONICS DOOR SURROUND INTERCOSTAL 27R, IAW CRJ 700 SRM 51-25-01. - [SDR N6WA2020101906](https://openairdocs.org/sdr/N6WA2020101906.md): Intercostal · corroded · Oct 19, 2020 · N540GJ · Cndair CL600* · Fuselage Miscellaneous Structure > CORROSION AT REAR AVIONICS DOOR SURROUND INTERCOSTAL 27R. INSPECTED CORROSION DAMAGE, IAW CRJ 700 SRM 51-21-06. REMOVED.001 METAL, PAINTED REAR AVIONICS DOOR SURROUND INTERCOSTAL 27R, IAW CRJ 700 SRM 51-25-01. - [SDR N6WA2020101905](https://openairdocs.org/sdr/N6WA2020101905.md): Intercostal · corroded · Oct 19, 2020 · N540GJ · Cndair CL600* · Fuselage Miscellaneous Structure > CORROSION AT FWD AVIONICS DOOR SURROUND INTERCOSTAL 27L. INSPECTED CORROSION DAMAGE, IAW CRJ 700 SRM 51-21-06. REMOVED.001 METAL, PAINTED FWD AVIONICS DOOR SURROUND INTERCOSTAL 27L, IAW CRJ 700 SRM 51-25-01. - [SDR N6WA2020101904](https://openairdocs.org/sdr/N6WA2020101904.md): Intercostal · corroded · Oct 19, 2020 · N540GJ · Cndair CL600* · Fuselage Miscellaneous Structure > CORROSION AT FWD AVIONICS DOOR SURROUND INTERCOSTAL 27R. INSPECTED CORROSION DAMAGE, IAW CRJ 700 SRM 51-21-06. REMOVED.001 METAL, PAINTED FWD AVIONICS DOOR SURROUND INTERCOSTAL 27R, IAW CRJ 700 SRM 51-25-01. - [SDR N6WA2020101903](https://openairdocs.org/sdr/N6WA2020101903.md): Bulkhead Web · corroded · Oct 19, 2020 · N540GJ · Cndair CL600* · Fuselage Main, Bulkhead > RT FS 280 BULKHEAD WEB CORRODED ABOVE FLOORBEAM. R & R RT FS 280 BULKHEAD LOWER WEB, IAW CRJ SRM 51-42-06. - [SDR N6WA2020101902](https://openairdocs.org/sdr/N6WA2020101902.md): Bulkhead Web · corroded · Oct 19, 2020 · N540GJ · Cndair CL6002C10 · Fuselage Main, Bulkhead > LT FS 280 BULKHEAD WEB CORRODED ABOVE FLOORBEAM. R & R LT FS 280 BULKHEAD LOWER WEB, IAW CRJ SRM 51-42-06. - [SDR N6WA2020100801](https://openairdocs.org/sdr/N6WA2020100801.md): Support · corroded · Oct 8, 2020 · N540GJ · Cndair CL600* · Fuselage Miscellaneous Structure > AFT WING TO FAIRING SUPPORT BOTTOM CENTER SPLICE ANGLE AT FS 939 HAS SURFACE CORROSION. REMOVED AND REPLACED SPLICE ANGLE ON AFT WING TO FAIRING SUPPORT, IAW CRJ700 SRM 51-42-06. ## 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 = 'N540GJ' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N540GJ/reports --- 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.