N905J, cancelled Jun 23, 2025

Service difficulty reports · 334

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

Query with SQL
duckdb -csv -c "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 = 'N905J' AND deregistration_id = 'N905J-2025-06-23'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR MASA2023102000013Unknown · unknownAFT CEILING EMERG LIGHT INOP- MEL/SPLICED BROKEN WIRE ON AFT CEILING EMERG LIGHT -Oct 20, 2023 · N905J · Cndair CL6002D24 · Emergency LightingSDR MASA2023102000134Light · burned outAFT CEILING EMERG LIGHT INOP. PLACED ON MELOct 20, 2023 · N905J · Cndair CL6002D24 · Emergency LightingSDR MASA2023100400028Unknown · unknownLH FUEL QTY/TOTAL FUEL QTY DASHES IN FLT- R2 LT #2 AND #6 FUEL PROBESOct 4, 2023 · N905J · Cndair CL6002D24 · Fuel Indicating SystemSDR MASA2023100200026Unknown · unknownFWD EMERGENCY MISSING LIGHT BULB- RELAMPEDOct 2, 2023 · N905J · Cndair CL6002D24 · Emergency LightingSDR MASA2023011200003Bulb · burned outROW 18 CEILING EMER FLOOD LIGHT INOP. MXC DEFERRED WITH CREW.Jan 12, 2023 · N905J · Cndair CL6002D24 · Emergency LightingSDR MASA2022120600268Bulb · inoperativeROW 13 A FLR LVL EXIT SIGN (1) BULB INOP. REPLACED BULBDec 9, 2022 · N905J · Cndair CL6002D24 · Emergency LightingSDR MASA2022082900220None · noneFLAP FAIL CAUTION (EMERGENCY DECLARED). RESET SFECU AND CLEARED INHIBITS, OPS CHECK GOOD.Aug 29, 2022 · N905J · Cndair CL6002D24 · Leading Edge Slat ActuatorSDR MASA2022040900100None · none13A EMERGENCY EXIT SIGN-1 BULB INOP. REPLACED BULB.Apr 9, 2022 · N905J · Cndair CL6002D24 · Emergency LightingSDR MASA2022040900099None · noneSERVICE DOOR EXIT SIGN-2 BULBS INOP. REPLACED BULBS.Apr 9, 2022 · N905J · Cndair CL6002D24 · Emergency LightingSDR MASA2022030300071None · noneGEAR DISAGREE WARN IN FLIGHT -EMER DECLARED. AIRCRAFT CURRENTLY OOS.Mar 3, 2022 · N905J · Cndair CL6002D24 · Landing Gear Retraction/Extension SystemSDR MASA20220208108None · crackedTHE LBL 12.00 FLOOR BEAM (P/N: CC670-33202-15) WAS FOUND WITH A CRACK. PERFORM PERMANENT REPAIR IAW CRJ7/9 STRUCTURAL REPAIR MANUAL (SRM) A) 53-11-43-001-001-A01, FIGURE 53-11-43-991-807, ITEM 108B (REV.38 DATED JUL. 25,2020.) B) 53-11-43-201-003-A01, FIGURE 5Feb 8, 2022 · N905J · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR MASA20220204104None · corrodedSLAT TRACKS 3-1 (P/N CC670-12072-7) AND 3-2 (CC670-12081-9) OF SLAT #3 ON THE LH WING WERE FOUND TO HAVE CORROSION DAMAGE ON THE UPPER AND LOWER FACES. PERFORM PERMANENT REPAIR IAW CRJ7/9 STRUCTURAL REPAIR MANUAL (SRM) 51-12-00 PROCEDURES.Jan 25, 2022 · N905J · Cndair CL6002D24 · Leading Edge DevicesSDR MASA20220204103None · corrodedSLAT TRACKS 2-1 (P/N CC670-12042-7), 2-2 (P/N CC670-12051-11) 2-3 (P/N CC670-12062-7) OF SLAT #2 ON THE LH WING WERE FOUND TO HAVE CORROSION DAMAGE ON THE UPPER AND LOWER FACES. PERFORM PERMANENT REPAIR IAW CRJ7/9 STRUCTURAL REPAIR MANUAL (SRM) 51-12-00 PROCEDJan 25, 2022 · N905J · Cndair CL6002D24 · Leading Edge DevicesSDR MASA20220204102None · corrodedSLAT TRACKS 3-1 (P/N CC670-12072-7) AND 3-2 (CC670-12081-9) OF SLAT #3 ON THE LH WING WERE FOUND TO HAVE CORROSION DAMAGE ON THE UPPER AND LOWER FACES. PERFORM PERMANENT REPAIR IAW CRJ7/9 STRUCTURAL REPAIR MANUAL (SRM) 51-12-00 PROCEDURES.Jan 25, 2022 · N905J · Cndair CL6002D24 · Leading Edge DevicesSDR MASA20220204101None · corrodedSLAT TRACKS 3-1 (P/N CC670-12072-7) AND 3-2 (CC670-12081-9) OF SLAT #3 ON THE LH WING WERE FOUND TO HAVE CORROSION DAMAGE ON THE UPPER AND LOWER FACES. PERFORM PERMANENT REPAIR IAW CRJ7/9 STRUCTURAL REPAIR MANUAL (SRM) 51-12-00 PROCEDURES.Jan 25, 2022 · N905J · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR MASA20220204100None · corrodedSLAT TRACK 1-1 (P/N CC670-12012-15), 1-2 (P/N CC670-12021-11) AND 1-3 (P/N CC670-12032-7) OF SLAT #1 ON THE LH WING WERE FOUND TO HAVE CORROSION DAMAGE ON THE UPPER AND LOWER FACES. PERFORM PERMANENT REPAIR IAW CRJ7/9 STRUCTURAL REPAIR MANUAL (SRM).51-12-00 PRJan 25, 2022 · N905J · Cndair CL6002D24 · Leading Edge DevicesSDR MASA20220204099None · noneSLAT TRACK 1-1 (P/N CC670-12012-15), 1-2 (P/N CC670-12021-11) AND 1-3 (P/N CC670-12032-7) OF SLAT #1 ON THE LH WING WERE FOUND TO HAVE CORROSION DAMAGE ON THE UPPER AND LOWER FACES. PERFORM PERMANENT REPAIR IAW CRJ7/9 STRUCTURAL REPAIR MANUAL (SRM).51-12-00 PRJan 25, 2022 · N905J · Cndair CL6002D24 · Leading Edge DevicesSDR MASA20220204098None · noneSLAT TRACKS 2-1 (P/N CC670-12042-7), 2-2 (P/N CC670-12051-11) 2-3 (P/N CC670-12062-7) OF SLAT #2 ON THE LH WING WERE FOUND TO HAVE CORROSION DAMAGE ON THE UPPER AND LOWER FACES. PERFORM PERMANENT REPAIR IAW CRJ7/9 STRUCTURAL REPAIR MANUAL (SRM) 51-12-00 PROCEDJan 25, 2022 · N905J · Cndair CL6002D24 · Leading Edge DevicesSDR MASA20220204097None · noneSLAT TRACK 1-1 (P/N CC670-12012-15), 1-2 (P/N CC670-12021-11) AND 1-3 (P/N CC670-12032-7) OF SLAT #1 ON THE LH WING WERE FOUND TO HAVE CORROSION DAMAGE ON THE UPPER AND LOWER FACES. PERFORM PERMANENT REPAIR IAW CRJ7/9 STRUCTURAL REPAIR MANUAL (SRM).51-12-00 PRJan 25, 2022 · N905J · Cndair CL6002D24 · Leading Edge DevicesSDR MASA20211223647None · noneTHE MAINTENANCE DISCOVERED CRACK ON THE SKIN PANEL. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 51-14-06, FIG. 51-14-06-991-815, 51-23-00 AND SRM 51-21-16.Dec 23, 2021 · N905J · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR MASA20211223646None · noneTHE PYLON DETACHABLE TRAILING EDGE ASSEMBLY WAS FOUND TO HAVE EROSION DAMAGE AFFECTING THE ALUMINUM MESH. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 51-73-00-201-009-A01, (REV. 38 DATED 7-9-2021).Dec 23, 2021 · N905J · Cndair CL6002D24 · Nacelle/Pylon StructureSDR MASA20211221644Access Panel · noneTHE RH WING L/E SLAT# 2 ACCESS PANEL 63102 WAS FOUND TO HAVE AN ELONGATED FASTENER HOLE. PERFORMED PERMANENT REPAIR IAW CRJ900 IPC 57-42-32, FIG. 5, ITEM 125 (REV. 70DATED JUN. 25. 2021 ).Dec 21, 2021 · N905J · Cndair CL6002D24 · Leading Edge DevicesSDR MASA20211221645None · crackedTHE LH ENGINE LOWER TRANSCOWL INNER SKIN WAS FOUND TO HAVE 11 SMALL CRACKS. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 54-21-05-991-801, ITEMS 2&3 (REV. 38 DATED 7-6-2021). DEFECT LOCATION: LH ENGINE LOWER TRANSCOWL ASSEMBLYDec 21, 2021 · N905J · Cndair CL6002D24 · Engine Thrust ReverserSDR MASA20211221643None · dentedTHE LONGERON SIDE FITTING FUEL VENT AND THE WELDED TUBE ASSEMBLY WERE FOUND TO HAVE DENTS ON THE OUTER SURFACE OF THE TUBES. PERFORMED PERMANENT REPAIR IAW CRJ900 AMM 28-12-00-710-801-A01 (REV 68 DATED 9-21-2021) AND CRJ900 AIPC 28-12-91-05, FIG 5 ITEM 5 (REV Dec 21, 2021 · N905J · Cndair CL6002D24 · Aircraft Fuel SystemSDR MASA20211221642None · noneTHE PASSENGER DOOR FWD SEAL STRIKER WAS FOUND BENT COMMON TO THE OUTBOARD FLANGE OF THE STRIKER. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 53-21-23-001-001-A01, FIG 53-21-23-995-818 ITEM 1388 (REV. 38 DATED JUL. 25, 2020).Dec 21, 2021 · N905J · Cndair CL6002D24 · Fuselage Main, StructureSDR MASA20211221641None · noneTHE LOWER FUSELAGE SKIN PANEL WERE REPORTED WITH TOTAL OF FOUR ZONES WITH MULTIPLE NICK DAMAGES. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 53-31-01-991-806, ITEM 1, A AND B (REV. 37 DATED AUG. 15, 2019. DEFECT LOCATION: FS 501.00 -FS 661.00 AND STGR 19L -STGRDec 21, 2021 · N905J · Cndair CL600* · Fuselage Main, Plate/SkinSDR MASA20211221640Floorbeam · corrodedTHE CROSSBEAM WAS FOUND TO HAVE SEVERE CORROSION DAMAGE ON THE UPPER FLANGE. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 53-21-43-001-A02, FIG. 53-21-43-991-802, ITEM 3.Dec 21, 2021 · N905J · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR MASA20211221639None · noneTHE LH WING L/E SLAT 1 T/E WEDGE WAS FOUND WITH AN EXISTING DAMAGE BLENDOUT.AT THE AFT EDGE, BETWEEN SLAT TRACK 1-2 AND SLAT TRACK 1-3. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 51-00-00, 51-21-16, AND 51-13-02 TABLE 1. DEFECT LOCATION: LH WING LEADING EDGE SLDec 21, 2021 · N905J · Cndair CL600* · Leading Edge DevicesSDR MASA20211221638Panel · noneA MISS DERILLED HOLE WAS FOUND ON THE RH OUTBOARD LEADING EDGE ACESS PANEL #632EB. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 57-42-32-991-801, 29A (REV 38 DATED 9 JUL 2021). PANEL/LE INBD RH PANEL #632EBDec 21, 2021 · N905J · Cndair CL600* · Wing Miscellaneous StructureSDR MASA20211221637None · noneTHE RH WING SLAT #3 WERE FOUND TO HAVE CORROSION DAMAGE ON BOTH THE UPPER AND LOWER SURFACES. PERFORMED PERMANENT REPAIR IAW CRJ900 ILLUSTRATED PARTS CATALOG (IPC) 27-81-41, FIG.10, ITEMS 15,AND 90 (REV. 70 DATED 10 AUG 2021). DEFECT LOCATION: RH WING-SLAT TRADec 21, 2021 · N905J · Cndair CL600* · Leading Edge DevicesSDR MASA20211221636None · noneTHE RH WING SLAT #2 WERE FOUND TO HAVE CORROSION DAMAGE ON BOTH THE UPPER AND LOWER SURFACES. PERFORMED PERMANENT REPAIR IAW CRJ900 ILLUSTRATED PARTS CATALOG (IPC) 27-81-41, FIG. 05, ITEMS 15, 85, AND 105 (REV. 70 DATED 10 AUG 2021). DEFECT LOCATION: RH WING-Dec 20, 2021 · N905J · Cndair CL600* · Leading Edge DevicesSDR MASA20211221635None · noneTHE RH WING SLAT #1 WERE FOUND TO HAVE CORROSION DAMAGE ON BOTH THE UPPER AND LOWER SURFACES. PERFORMED PERMANENT REPAIR IAW CRJ900 ILLUSTRATED PARTS CATALOG (IPC) 27-81-41, FIG. 01, ITEMS 45, 85, AND 105 (REV. 70 DATED 10 AUG 2021). DEFECT LOCATION: RH WING-Dec 20, 2021 · N905J · Cndair CL600* · Leading Edge DevicesSDR MASA20211221634None · noneTHE FUSELAGE SKIN LOWER PANEL WAS FOUND TO HAVE A PREVIOUS BLENDOUT. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 53-61-01-001-003-A02, FIG. 53-61-01-991-806, ITEM 1 AND ITEM F (REV.38 DATED 9 JUL 2021 ). DEFECT LOCATION: FS 1000- FS 10L5 AND STRG 25R AND STRG 26Dec 20, 2021 · N905J · Cndair CL600* · Fuselage Structure (General)SDR MASA20211221633None · noneTHE FUSELAGE LOWER SKIN PANEL WAS FOUND WITH MINOR CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW SRM 53-51-01-001-003-A02 ITEM 1A, D AND E (REV.38 DATED 9 JUL2021). DEFECT LOCATIONS: FS 913.00 -942.00. STGR 20R-STGR 20LDec 20, 2021 · N905J · Cndair CL600* · Fuselage Main, Plate/SkinSDR MASA20211221632None · noneTHE FUSELAGE LH SKIN PANEL WAS FOUND WITH MINOR CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW SRM 53-51-01-001-002-A02 ITEM 1, C, AND D (REV.38 DATED 9 JUL 2021). DEFECT LOCATION: FS 847+16-FS 913 AND STGR 17L-STGR 20LDec 20, 2021 · N905J · Cndair CL600* · Fuselage Main, Plate/SkinSDR MASA20211221631None · noneTHE FUSELAGE RH SKIN PANEL WAS FOUND WITH MINOR CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW SRM 53-51-01-001-004-A02 ITEM 1, A, AND D (REV.38 DATED 9 JUL 2021) - DEFECT LOCATION: FS 875-FS 920 AND STGR 17R - 19RDec 20, 2021 · N905J · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR MASA20211221630None · noneA CRACK WAS DISCOVERED ON THE SKIN PANEL. PERFORMED PERMANENT REPAIR IAW CR7/9 SRM 53-11-01-991-810, ITEM 1A (CRJ7/9 REV. 38 DATED JUL 9TH, 2021).Dec 20, 2021 · N905J · Cndair CL600* · Fuselage Main, Floor BeamSDR MASA20211221629None · noneTHE UPPER CAP OF THE CENTER FUSELAGE FLOOR BEAM WAS FOUND TO HAVE CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 53-61-43-991-801, ITEM 2A (REV. 33 DATED JUN. 25, 2017). DEFECT LOCATION: FS 661+16-FS 661+32, LBL 9Dec 20, 2021 · N905J · Cndair CL600* · Fuselage Main, Floor BeamSDR MASA20211221628None · noneSLAT #3 ON THE LH WING WERE FOUND TO HAVE CORROSION DAMAGE ON THE UPPER AND LOWERFACES. PERFORMED PERMANENT REPAIR IAW CRJ900 ILLUSTRATED PARTS CATALOG (IPC) 27-81-41, FIG.10, ITEM 15, 90 (REV. 70 DATED 10 AUG 2021).Dec 20, 2021 · N905J · Cndair CL600* · Leading Edge DevicesSDR MASA20211221627None · noneSLAT #2 ON THE LH WING WERE FOUND TO HAVE CORROSION DAMAGE ON THE UPPER AND LOWERFACES. PERFORMED PERMANENT REPAIR IAW CRJ900 ILLUSTRATED PARTS CATALOG (IPC) 27-81-41, FIG.1, ITEM 45, 85, AND 105 (REV. 70 DATED 10 AUG 2021).Dec 20, 2021 · N905J · Cndair CL600* · Leading Edge DevicesSDR MASA20211221626None · noneSLAT #1 ON THE LH WING WERE FOUND TO HAVE CORROSION DAMAGE ON THE UPPER AND LOWERFACES. PERFORMED PERMANENT REPAIR IAW CRJ900 ILLUSTRATED PARTS CATALOG (IPC) 27-81-41, FIG.1, ITEM 45, 85, AND 105 (REV. 70 DATED 10 AUG 2021).Dec 20, 2021 · N905J · Cndair CL600* · Leading Edge DevicesSDR MASA20211221625None · noneTHE FORWARD AND AFT SEAL CARRIERS OF THE AFT SERVICE DOOR PLUG WAS FOUND TO HAVE (2) CRACKS. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 52-46-07 FIG. 52-46-07-991-801, ITEM 4 AND 5 (REV. 38 DATED JUL. 9, 2021 ). DEFECT LOCATION: SIDE SEAL CAREER, AFT SERVICE DDec 20, 2021 · N905J · Cndair CL600* · Service DoorsSDR MASA20211221624None · noneTHE PASSENGER DOOR INNER SKIN WAS FOUND WITH A CRACK. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 51-24-36, 51-21-16, 51-23-00. DEFECT LOCATION: FWD PASSENGER DOOR LOWER CORNERDec 20, 2021 · N905J · Cndair CL600* · Passenger/Crew DoorsSDR MASA20211221623None · noneTHE LOWER FUSELAGE SKIN PANEL HAD A PREVIOUS REPAIR INSTALLED PER REO 690-53-21-989 THAT CONFLICTED WITH THE OPERATOR RECOMMENDED SERVICE BULETIN 670BA-53-057 THAT INVOLVES RELOCATING THE DRAIN HOLES FORWARD AND INSTALLING TWO SMALL DOUBLERS FOR THE NEW DRAIN Dec 17, 2021 · N905J · Cndair CL600* · Fuselage Main, Plate/SkinSDR MASA20211221622None · noneTHE LH FUSELAGE SKIN PANEL WAS FOUND WITH DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 51-12-00, SRM 51-40-11-001-001.Dec 17, 2021 · N905J · Cndair CL600* · Fuselage Structure (General)SDR MASA20211221621None · dentedTHE FUSELAGE LOWER SKIN PANEL WAS FOUND TO HAVE THREE PROTRUDING DENTS. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 53-21-01, FIG. 53-21-01-991-802, ITEM 1 (REV. 38 DATED 25 JUL. 2020).Dec 17, 2021 · N905J · Cndair CL6002D24 · Fuselage Floor PanelSDR MASA20211130595None · noneFUSELAGE LOWER SKIN PANEL AT FS394.00 AND STGR20L -STGR21L WAS FOUND TO HAVE A PREVIOUS BLENDOUT, PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-21-01-001-006-A02, FIGURE 53-21-01-991-807, ITEM 1, C, EA 79-2021-264.Nov 30, 2021 · N905J · Cndair CL6002D24 · Fuselage Floor PanelSDR MASA20211130594None · noneLH MAIN LANDING GEAR HYDRAULIC INTERFACE IN THE MLG BAY BETWEEN WS 14.50 AND WS 68.00 WAS FOUND WITH MISSING MATERIAL. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 51-13-02, EA 20-2021-214.Nov 30, 2021 · N905J · Cndair CL6002D24 · Standard Practices/StructuresSDR MASA20211129582None · noneL/H WING LEADING EDGE SLAT NO. 3 TRAILING EDGE WAS FOUND WITH GOUGE DAMAGE. PERFORMED PERMANENT REPAIR JAW CRJ 700/900 SRM 51-13-02, EA 69-2021-201.Nov 24, 2021 · N905J · Cndair CL600* · Standard Practices/StructuresSDR MASA20211129581None · noneL/H WING LEADING EDGE SLAT NO. 2 TRAILING EDGE WAS FOUND WITH GOUGE DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 51-13-02, EA 69-2021-200.Nov 24, 2021 · N905J · Cndair CL600* · Standard Practices/Structures
Back to N905J, cancelled Jun 23, 2025