# Service difficulty reports: N930XJ A list on [N930XJ](https://openairdocs.org/aircraft/N930XJ.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 4 · 160 reports - [SDR REXA2026092101839](https://openairdocs.org/sdr/REXA2026092101839.md): Bulb · inoperative · Sep 17, 2026 · N930XJ · Cndair CL6002D24 · Emergency Lighting > AFT RIGHT OVERWING EMERGENCY LIGHT BULB INOPERATIVE. R & R RIGHT OVERWING EMERGENCY LIGHT BULB PER AMM 33-51-15. - [SDR REXA2026091101806](https://openairdocs.org/sdr/REXA2026091101806.md): Rib · cracked · Sep 3, 2026 · N930XJ · Cndair CL6002D24 · Wing, Rib/Bulkhead > CRACK ON MACHINED RIB OF LEADING EDGE SS58.41 AT LH WING. DUE TO EXCESSIVE DAMAGE ON MACHINED RIB OF LEADING EDGE SS58.41 AT LH WING WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01,SRM 51-42-13-001-001-A01 AND SRM 51-10-06-001-001-A - [SDR REXA2026091101805](https://openairdocs.org/sdr/REXA2026091101805.md): Angle · cracked · Aug 9, 2026 · N930XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CRACKS ON UPPER ANGLES (FIRE PROTECTION KIT 2EAS) FWD CORNERS AT FWD/CENTER BOTH BAGGAGE BAY DOORS. UPPER ANGLES (FIRE PROTECTION KIT 2EAS) FWD CORNERS AT FWD/CENTER BOTH BAGGAGE BAY DOORS WERE REPLACED PER CRJ900 SRM 51-41-02-001-001-A01 AND 51-42-13-001-001- - [SDR REXA2026091101804](https://openairdocs.org/sdr/REXA2026091101804.md): Angle · cracked · Aug 9, 2026 · N930XJ · Cndair CL6002D24 · Cargo/Baggage Doors > CRACKS ON UPPER ANGLES (FIRE PROTECTION KIT 2EAS) FWD CORNERS AT FWD/CENTER BOTH BAGGAGE BAY DOORS. UPPER ANGLES (FIRE PROTECTION KIT 2EAS) FWD CORNERS AT FWD/CENTER BOTH BAGGAGE BAY DOORS WERE REPLACED PER CRJ900 SRM 51-41-02-001-001-A01 AND 51-42-13-001-001- - [SDR REXA2026091101822](https://openairdocs.org/sdr/REXA2026091101822.md): Fitting · corroded · Aug 5, 2026 · N930XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CORROSION FLOOR FITTING IN AFT AND FWD ACCESS 306 (1EA) ON GALLEY 3. NEW FLOOR FITTING IN AFT AND FWD ACCESS 306 (1EA) ON GALLEY 3 WAS REPLACED IAW CMM 25-33-18 REV 5. - [SDR REXA2026091101821](https://openairdocs.org/sdr/REXA2026091101821.md): Fitting · corroded · Aug 5, 2026 · N930XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CORROSION FLOOR FITTING IN AFT ACCESS 109 (1EA) ON GALLEY 1. NEW FLOOR FITTING P/N: CDSP2019-7C-620 IN AFT ACCESS 109 (1EA) ON GALLEY 1 WAS REPLACED PER SAFRAN CMM 25-33-67 REV NO10 DATED 20/22 - [SDR REXA2026091101815](https://openairdocs.org/sdr/REXA2026091101815.md): Fitting · corroded · Aug 5, 2026 · N930XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CORROSION FLOOR FITTING IN FWD ACCESS 305 (1EA) ON GALLEY 3. SUMMARY OF NRC 00402: NEW FLOOR FITTING P/N: CDSP2019-7C-700 IN FWD ACCESS 305 (1EA) ON GALLEY 3 WAS REPLACED PER ZODIAC AEROSPACE CMM 25-33-18 REV NO 5 DATED 15/15 - [SDR REXA2026091101814](https://openairdocs.org/sdr/REXA2026091101814.md): Fitting · corroded · Aug 5, 2026 · N930XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CORROSION FLOOR FITTING IN FWD ACCESS 107 (1EA) ON GALLEY 1. SUMMARY OF NRC 00399: NEW FLOOR FITTING P/N: CDSP2019-7C-620 IN FWD ACCESS 107 (1EA) ON GALLEY 1 WAS REPLACED PER SAFRAN CMM 25-33-67 REV NO 10 DATED JUN 20/22 - [SDR REXA2026091601817](https://openairdocs.org/sdr/REXA2026091601817.md): Skin · cracked · Aug 3, 2026 · N930XJ · Cndair CL6002D24 · Passenger/Crew Doors > CRACK ON SETTLEMENT AREA OF PASSENGER DOOR ACCESS PANEL 832DL. SETTLEMENT AREA OF PASSENGER DOOR ACCESS PANEL 832DL WAS REPAIRED PER EA CRJ952-22930 REV B - [SDR REXA2026091601816](https://openairdocs.org/sdr/REXA2026091601816.md): Skin · cracked · Aug 3, 2026 · N930XJ · Cndair CL6002D24 · Passenger/Crew Doors > CRACK ON SETTLEMENT AREA OF PASSENGER DOOR ACCESS PANEL 832AL SETTLEMENT AREA OF PASSENGER DOOR ACCESS PANEL 832AL WAS REPAIRED PER EA CRJ952-22930 REV B - [SDR REXA2026091101812](https://openairdocs.org/sdr/REXA2026091101812.md): Access Panel · corroded · Aug 2, 2026 · N930XJ · Cndair CL6002D24 · Aerodynamic Fairings > CORROSION ON NUTS STRIP OF BODY FAIRING ACCESS PANEL 194AB. 08/02/2026 STRIP OF BODY FAIRING ACCESS PANEL 194AB WAS REPLACED PER CRJ-900 SRM 51-42-13-001-001-A01. - [SDR REXA2026091101811](https://openairdocs.org/sdr/REXA2026091101811.md): Hinge · corroded · Aug 2, 2026 · N930XJ · Cndair CL6002D24 · Fuselage, Door Hinge > CRACK ON HINGE OF FLAP STEP OF AFT BAGAGGE BAY. HINGE OF FLAP STEP OF AFT BAGAGGE BAY WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01. - [SDR REXA2026091101810](https://openairdocs.org/sdr/REXA2026091101810.md): Fitting · cracked · Aug 2, 2026 · N930XJ · Cndair CL6002D24 · Fuselage Main, Structure > CRACK ON LOWER SIDE POST FITTINGS (2 EAS) LH/RH ON INTERNAL STRUCTURE BTW WINDSHIELD AND SIDE WINDOWS. LOWER SIDE POST FITTINGS (2 EAS) LH/RH ON INTERNAL STRUCTURE BTW WINDSHIELD AND SIDE WINDOWS WERE REPLACED PER CRJ-900 SRM 51-42-20-001-001-A01 - [SDR REXA2026091101809](https://openairdocs.org/sdr/REXA2026091101809.md): Seat Track · corroded · Aug 1, 2026 · N930XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings > CORROSION & WEAR ON LH SIDE RAILS (4 EAS) BTW FS 379.00/FS 669.40 AND STGR 15L AT PAX CABIN. LH SIDE RAILS (3 EAS) BTW FS 379.00/FS 669.40 AND STGR 15L AT PAX CABIN WAS CLEANED AND NOT DAMAGE WAS FOUND PER CRJ-900 SRM 51-26-00-001-001-A01, AND ON SECTION OF LH - [SDR REXA2026091101808](https://openairdocs.org/sdr/REXA2026091101808.md): Stringer · corroded · Jul 31, 2026 · N930XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > CORROSION ON STGR22R FROM FS280 TO FS310 AT MAIN AVIONICS COMPARTMENT. SUMMARY: CORROSION ON STGR22R FROM FS280 TO FS310 AT MAIN AVIONICS COMPARTMENT WAS EVALUATED OUT OF LIMITS THEREFORE WAS REPLACED PER CRJ-900 SRM 51-10-06-001-001-A01, CRJ-900 SRM 51-42-06- - [SDR REXA2026091101807](https://openairdocs.org/sdr/REXA2026091101807.md): Seat Track · corroded · Jul 31, 2026 · N930XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings > CORROSION & WEAR ON RH SIDE RAILS (5 EAS) BTW FS 669.40/FS 977.00 AND STGR 15R AT PAX CABIN. CORROSION ON SIDE RAILS (5 EAS) BTW FS 669.40/FS 977.00 AND STGR 15R AT PAX CABIN WERE EVALUATED OUT OF LIMITS THEREFORE WERE REPLACED PER CRJ-900 SRM 53-31-49-101-001 - [SDR REXA2026091101819](https://openairdocs.org/sdr/REXA2026091101819.md): Frame · corroded · Jul 30, 2026 · N930XJ · Cndair CL6002D24 · Fuselage Main, Frame > CORROSION ON FRAME AT FS 333, BTW STGR 25 AND 26R ON MAIN AVIONICS COMPARTMENT CORROSION ON FRAME AT FS 333, BTW STGR 25 AND 26R ON MAIN AVIONICS COMPARTMENT WAS EVALUATED OUT OF LIMITS THEREFORE WAS REPAIRED PER CRJ-900 SRM 53-00-06-201-006-A01 AND CRJ 900 SR - [SDR REXA2026091101820](https://openairdocs.org/sdr/REXA2026091101820.md): Striker · corroded · Jul 28, 2026 · N930XJ · Cndair CL6002D24 · Passenger/Crew Doors > CORROSION ON SEAL STRIKER OF SERVICE DOOR LOWER CUTOUT BTW FS319.70 TO FS349.00 AND STGR-17R. CORROSION ON SEAL STRIKER OF SERVICE DOOR LOWER CUTOUT BTW FS319.70 TO FS349.00 AND STGR-17R. WAS EVALUATED OUT OF LIMITS PER SRM 51-10-06-001-001-A01 AND WAS REPLAC - [SDR REXA2026091101818](https://openairdocs.org/sdr/REXA2026091101818.md): Retainer · corroded · Jul 28, 2026 · N930XJ · Cndair CL6002D24 · Cargo/Baggage Doors > CORROSION ON INNER CHANNEL OF AFTER CARGO DOOR. INNER CHANNEL OF AFTER CARGO DOOR WAS REPLACED PER CRJ 900 SRM 51-42-06-001-001-A01 - [SDR REXA2026091101803](https://openairdocs.org/sdr/REXA2026091101803.md): Support · cracked · Jul 27, 2026 · N930XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CRACKS ON FWD CORNERS AT JB6 PLATE. JB6 PLATE WAS REPLACED PER SRM 51-42-06-001-001-A01 PAR. 6.C. - [SDR REXA2025060500631](https://openairdocs.org/sdr/REXA2025060500631.md): Battery Pack · inoperative · Jun 5, 2025 · N930XJ · Cndair CL6002D24 · Emergency Lighting > EMEGENCY LIGHTS STATUS MESSAGE & EMERGENCY LIGHT COME ON WHEN EMER LTS SWITCH IS IN THE ARMED POSITION. R/R AND PERFORMED OPS TEST OF THE PS43 EMER BATTERY IAW AMM 33-51-17 TEST PASSED A/C OK FOR SVC. - [SDR REXA2025040800402](https://openairdocs.org/sdr/REXA2025040800402.md): Battery Pack · no test · Apr 5, 2025 · N930XJ · Cndair CL6002D24 · Emergency Lighting > DURING LINE CHECK FOUND SEVERAL FWD EMERG ENTRANCE LIGHTS INOP. TROUBLESHOT AND FOUND BATTERY PACK PS35 INOP. REMOVED & REPLACED BATTERY IAW AMM 33-51-17 PERFOMRED OPS TEST IAW AMM 33-51-17. OPS TEST GOOD. - [SDR REXA2024122301605](https://openairdocs.org/sdr/REXA2024122301605.md): Lamp · inoperative · Dec 21, 2024 · N930XJ · Cndair CL6002D24 · Emergency Lighting > DURING COMPLETION OF LINE-900, FOUND PAX DOOR EMERGENCY LIGHT BULB OUT R/R BULB IAW CRJ AMM 33-51-15. PERFORMED OPS TEST OF EXT. EMER. LIGHTS IAW CRJ AMM 33-51-15; OPS TEST GOOD. P/N OFF/ON: 8GH002473-08 NO S/N - [SDR REXA2024050900387](https://openairdocs.org/sdr/REXA2024050900387.md): Lamp · inoperative · May 7, 2024 · N930XJ · Cndair CL6002D24 · Emergency Lighting > EXTERIOR AFT EMERGENCY LIGHT INOP RELAMPED EMERGENCY LEFT AFT OVERWING LIGHT IAW CRJ 900 AMM 33-51-15. OPC GOOD. P/N OFF/ON: 8GH002473-08 - [SDR REXA2024032800313](https://openairdocs.org/sdr/REXA2024032800313.md): Lamp · inoperative · Mar 27, 2024 · N930XJ · Cndair CL6002D24 · Emergency Lighting > RH OVERWING EMERGENCY LIGHT NOT WORKING R/R OVER THE WING EMERGENCY LAMP IAW CRJ 900 AMM 33-51-15 P/N OFF/ON: 8GH005123-06 - [SDR REXA2024041800356](https://openairdocs.org/sdr/REXA2024041800356.md): Stiffener · chafed · Mar 1, 2024 · N930XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > PANEL 172CR BOTTOM AFT STIFFENER CHAFFED. REMOVED AND REPLACED IAW CRJ 900 SRM 51-42-06-001-001-A01. - [SDR REXA2022052300329](https://openairdocs.org/sdr/REXA2022052300329.md): Floor Support · corroded · May 21, 2023 · N930XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > PAX DOOR SILL FLOORBOARD SUPPORT MID CAP ANGLE IS CORRODED. REPLACED PAX DOOR SILL FLOORBOARD SUPPORT MID CAP ANGLE IAW CRJ-900 SRM 51-41-02-001-001AO1 - [SDR REXA2022123002731](https://openairdocs.org/sdr/REXA2022123002731.md): Motor · inoperative · Dec 25, 2022 · N930XJ · Cndair CL6002D24 · Passenger/Crew Doors > PAX DOOR WILL NOT OPEN. REMOVED AND REPLACED PAX DOOR ASSIST MOTOR IAW 52-11-08. AND REPLACED RELAY K138 IAW AMM 20-42-00. - [SDR REXA2020012380048](https://openairdocs.org/sdr/REXA2020012380048.md): Bulb · inoperative · Jan 18, 2020 · N930XJ · Cndair CL6002D24 · Emergency Lighting > EMERGENCY FLOOR LEVEL FLOOD LIGHTS HAVE 1 BULB INOP AT PAX DOOR AND 3 BULBS INOP AT GALLEY SERVICE DOOR REMOVED AND REPLACED EMERGENCY LIGHT BULBS 4 EA PER CRJ-900 AMM 33-51-11. OPS CHECK GOOD - [SDR REXA2019123021840](https://openairdocs.org/sdr/REXA2019123021840.md): Door Frame · nicked · Dec 21, 2019 · N930XJ · Cndair CL6002D24 · Fuselage Main, Structure > FOUND IMPACT DAMAGE ON THE FRAME FOR THE FWD E/E BAY DOOR, RT SIDE. THE FRAME AT BS 310 STRINGERS 24R - 25R WAS REPAIRED IAW EA CRJ953-10116, REV IR. - [SDR REXA2019123021811](https://openairdocs.org/sdr/REXA2019123021811.md): Longeron · corroded · Dec 20, 2019 · N930XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > CORROSION FOUND ON LONGERON 25R AT BS 336 - 349 IN THE MAIN AVIONICS COMPARTMENT. THE LONGERON WAS REPLACED IAW SRM 51-42-06-001-001-A01, AND SRM 51-42-21-001-001-A01. - [SDR REXA2019123071832](https://openairdocs.org/sdr/REXA2019123071832.md): Support Angle · corroded · Dec 17, 2019 · N930XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CORROSION WAS FOUND ON THE LT, CENTER, AND RH SUPPORT ANGLE AT THE AFT WING-TO-FUSELAGE FAIRING, BS 847. THE SUPPORT ANGLE WAS REPLACED IAW SRM 51-42-13-001-001-A01. - [SDR REXA2019123071800](https://openairdocs.org/sdr/REXA2019123071800.md): Support · corroded · Dec 17, 2019 · N930XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CORROSION ON FWD JACK FITTING RT SUPPORT IN THE FWD AVIONICS COMPARTMENT. THE JACK FITTING SUPPORT WAS REPLACED IAW SRM 51-42-06, AND SRM 51-42-20. - [SDR REXA2019123071789](https://openairdocs.org/sdr/REXA2019123071789.md): Hinge Fitting · corroded · Dec 17, 2019 · N930XJ · Cndair CL6002D24 · Fuselage, Door Hinge > CORROSION ON HINGE FITTING AT LAVATORY WASTE SERVICE DOOR NR 196ER AT AFT FAIRING AFT PANEL. THE HINGE FITTING WAS REPLACED IAW SRM 51-41-02-001-001-A01. - [SDR REXA2019123071788](https://openairdocs.org/sdr/REXA2019123071788.md): Stringer · corroded · Dec 17, 2019 · N930XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > CORROSION ON STGR27 AND ANGLE BTW FS250-263 AT FWD AVIONICS COMPARTMENT. (FUS). STGR27 WAS REPAIRED AND ANGLE WAS REPLACED PER CRJ900 SRM 53-00-03-201-001-A02 AND SRM 51-42-20-001-001-A01. - [SDR REXA2019123061841](https://openairdocs.org/sdr/REXA2019123061841.md): Floor Support · corroded · Dec 16, 2019 · N930XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CORROSION WAS ON FOUND ON THE RT FLOOR SUPPORT BETWEEN BS 985 - 1088 IN THE AFT CARGOBAY. THE CORROSION WAS REMOVED IAW SRM 51-21-06 AND FOUND WITHIN LIMITS IAW SRM 53-00-00, BETWEEN BS BS 1031 AND 1051 WAS REPLACED IAW SRM 51-42-06. - [SDR REXA2019123061833](https://openairdocs.org/sdr/REXA2019123061833.md): Skin · damaged · Dec 16, 2019 · N930XJ · Cndair CL6002D24 · Fuselage Main, Plate/Skin > SUNKEN FASTENERS WERE FOUND ON THE FUSELAGE SKIN BETWEEN BS 250 - 265, STRINGER 26L. THESKIN WAS REPAIRED IAW EA CRJ953-09950, REV IR. - [SDR REXA2019123061794](https://openairdocs.org/sdr/REXA2019123061794.md): Floor Support · corroded · Dec 16, 2019 · N930XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CORROSION THE FLOOR SUPPORT BETWEEN BS 977 - 1088, LBL 27 IN THE AFT CARGO COMPARTMENT. THE FLOOR SUPPORT WAS REPAIRED IAW EA CRJ953-09992 REV: IR - [SDR REXA2019123061787](https://openairdocs.org/sdr/REXA2019123061787.md): Skin · damaged · Dec 16, 2019 · N930XJ · Cndair CL6002D24 · Fuselage Main, Plate/Skin > CREASE ON FUSELAGE SKIN BETWEEN BS 310 AND 319, STRINGER 23R. THE FUSELAGE SKIN WAS REPAIRED IAW EA CRJ953-09994 REV. IR. - [SDR REXA2019123051839](https://openairdocs.org/sdr/REXA2019123051839.md): Door · damaged · Dec 15, 2019 · N930XJ · Cndair CL6002D24 · Nacelle/Pylon, Main Frame > WORN AND BENT CUTOUT OF THE COWLING LATCH DOOR FOR THE RT NACELLE. THE COAMING LATCH DOOR WAS REPLACED IAW SRM 51-42-13-001-001-A01, AND SRM 51-42-21-001-001-A01. - [SDR REXA2019123051838](https://openairdocs.org/sdr/REXA2019123051838.md): Latch · worn · Dec 15, 2019 · N930XJ · Cndair CL6002D24 · Nacelle/Pylon, Main Frame > WEAR FOUND ON THE COAMING LATCH DOOR AT THE TRANSCOWL FOR THE RT ENGINE. THE COAMING LATCH DOOR WAS REPLACED IAW SRM 51-42-13-001-001-A01. - [SDR REXA2019123051836](https://openairdocs.org/sdr/REXA2019123051836.md): Retainer · worn · Dec 15, 2019 · N930XJ · Cndair CL6002D24 · Cargo/Baggage Doors > WEAR WAS FOUND ON THE LOWER SEAL RETAINER AFT/FWD CORNER AT CTR/FWD CARGO DOORS. THE DAMAGED SEAL RETAINERS WERE REPLACED IAW SRM 52-35-07-201-001-A01, PAR. 6B, AND AMM 52-35-07-400-802. - [SDR REXA2019123051802](https://openairdocs.org/sdr/REXA2019123051802.md): Floor Support · corroded · Dec 15, 2019 · N930XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > INITIAL INSPECTION: CORROSION ON INTERCOSTAL 2 LBL BTW FS 364-349. AT E/E COMPARTMENT. INTERCOSTAL 2 LBL BTW FS364/349 AT E/E COMPARTMENT WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01. (LEVEL CORROSION 2) - [SDR REXA2019123041837](https://openairdocs.org/sdr/REXA2019123041837.md): Pad · worn · Dec 14, 2019 · N930XJ · Cndair CL6002D24 · Nacelle/Pylon, Main Frame > WEAR WAS FOUND ON THE BEARING PAD LATCH DOOR FOR THE RT ENGINE TRANSCOWL. THE PAD LATCH DOOR FOR THE RT ENGINE TRANSCOWL WAS REPLACED IAW SRM 51-42-06-001-001-A01. - [SDR REXA2019123041790](https://openairdocs.org/sdr/REXA2019123041790.md): Skin · cracked · Dec 14, 2019 · N930XJ · Cndair CL6002D24 · Nacelle/Pylon, Plate/Skin > DAMAGE SEALS AND CRACK ON PYLON ACCESS PANELS SKIN 422CT AND 412CT. DAMAGE SEALS AND CRACKED SKIN ON PYLON ACCESS PANELS 422CT AND 412CT WERE REPLACED IAW SRM 51-42-06-001-001-A01 PAR. 6C, AND SRM 51-42-10-001-001-A01 PAR. 8C. - [SDR REXA201912301842](https://openairdocs.org/sdr/REXA201912301842.md): Stringer · corroded · Dec 13, 2019 · N930XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > CORROSION WAS FOUND ON STRINGER 26L, BETWEEN BS 319 - 327 IN THE MAIN AVIONICS COMPARTMENT. THE STRINGER WAS REPLACED IAW SRM 51-42-06-001-001-A01, AND SRM 51-42-21-001-001-A01. - [SDR REXA201912301835](https://openairdocs.org/sdr/REXA201912301835.md): Retainer · dented · Dec 13, 2019 · N930XJ · Cndair CL6002D24 · Cargo/Baggage Doors > A DENT WAS FOUND ON THE LOWER SEAL RETAINER AT THE FWD CORNER OF THE CENTER CARGO DOOR, AND AFT CORNER OF THE FWD CARGO DOOR. THE LOWER SEAL RETAINERS WERE REPLACED IAW SRM 52-35-07-201-001-A01, AND AMM 52-35-07-400-802. - [SDR REXA2019123011829](https://openairdocs.org/sdr/REXA2019123011829.md): Frame · corroded · Dec 13, 2019 · N930XJ · Cndair CL6002D24 · Fuselage Main, Frame > CORROSION WAS FOUND ON THE FRAME AT BS 349, BETWEEN STRINGERS 26 - 27R IN THE MAIN AVIONIC COMPARTMENT. THE CORROSION WAS REMOVED IAW SRM 51-21-06-001-001-A01, AND THE REWORKED AREAS WERE MEASURED AT ORIGINAL THICKNESS 0.050", MAXIMUM DEPTH REMOVED WAS 0.0 - [SDR REXA2019123011812](https://openairdocs.org/sdr/REXA2019123011812.md): Stringer · corroded · Dec 13, 2019 · N930XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > CORROSION WAS FOUND ON STRINGER 26R, BS 336 - 364 IN THE MAIN AVIONICS COMPARTMENT. THE STRINGER WAS REPLACED IAW SRM 51-42-06-001-001-A01, AND SRM 51-42-21-001-001-A01. - [SDR REXA2019123011808](https://openairdocs.org/sdr/REXA2019123011808.md): Doubler · corroded · Dec 13, 2019 · N930XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CORROSION WAS FOUND ON THE INTERNAL DOUBLER AT BS 295 TO 310, BETWEEN STRINGERS 26L TO 26R IN THE MAIN AVIONICS COMPARTMENT. INTERNAL DOUBLER WAS REPLACED IAW SRM 51-42-06-001-001-A01. Next page: https://openairdocs.org/aircraft/N930XJ/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 = 'N930XJ' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N930XJ/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.