N925XJ

Service difficulty reports · 192

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 = 'N925XJ' AND registry_match = 'registration'
  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 REXA2026082501640Bulb · burned outFLOOR LEVEL EMERGENCY FLOOD LIGHTS AT PAX & SERVICE DOOR HAVE BURNED OUT BULBS R & R BULBS OPC GOOD IAW AMM 33-51-00.Aug 23, 2026 · N925XJ · Cndair CL6002D24 · Emergency LightingSDR REXA2026073001348Lug · damagedFABRICATE OVERSIZE BUSHINGS FOR LUGS R1, R2, R5 & R6. LUG R1 WAS REWORKED AND BUSHINGS OVERSIZE FOR LUGS R2, R5 & R6 WERE FABRICATED PER REO 670-57-61-237 REV.--Jul 28, 2026 · N925XJ · Cndair CL6002D24 · Wing, Control Surface Attach FittingsSDR REXA2026073001347Lug · corrodedCORROSION AND WEAR WAS FOUND ON LUG BORE ON AIL STA 336.4015 (LUG L1), 337.657 (LUG L2), 342.911 (LUG L5), 344.1665 (LUG L6) AT LH AILERON. CORROSION AND WEAR ON LUG BORE ON AIL STA 336.4015 (LUG L1), 337.657 (LUG L2), 342.911 (LUG L5), 344.1665 (LUG L6) AT LHJul 18, 2026 · N925XJ · Cndair CL6002D24 · Wing, Control Surface Attach FittingsSDR REXA2026073001334Web · corrodedCORROSION ON WEB FLOOR PROTECTOR (4EAS) AT SERVICE DOOR SURROUND STRUCTURE CORROSION ON WEB FLOOR PROTECTOR (4EAS) AT SERVICE DOOR SURROUND STRUCTURE WAS REMOVED AND EVALUATED OUT OF LIMITS PER CRJ900 SRM 51-21-06-001-001-A01 AND CRJ-900 SRM 53-00-00-101-001-Jun 18, 2026 · N925XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026073001333Bracket · corrodedCORROSION ON WEB FLOOR PROTECTOR (4EAS) AT SERVICE DOOR SURROUND STRUCTURE CORROSION ON WEB FLOOR PROTECTOR (4EAS) AT SERVICE DOOR SURROUND STRUCTURE WAS REMOVED AND EVALUATED OUT OF LIMITS PER CRJ900 SRM 51-21-06-001-001-A01 AND CRJ-900 SRM 53-00-00-101-001-Jun 18, 2026 · N925XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026073001332Protector · corrodedCORROSION ON WEB FLOOR PROTECTOR (4EAS) AT SERVICE DOOR SURROUND STRUCTURE CORROSION ON WEB FLOOR PROTECTOR (4EAS) AT SERVICE DOOR SURROUND STRUCTURE WAS REMOVED AND EVALUATED OUT OF LIMITS PER CRJ900 SRM 51-21-06-001-001-A01 AND CRJ-900 SRM 53-00-00-101-001-Jun 18, 2026 · N925XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026073001331Bracket · corrodedCORROSION ON WEB FLOOR PROTECTOR (4EAS) AT SERVICE DOOR SURROUND STRUCTURE CORROSION ON WEB FLOOR PROTECTOR (4EAS) AT SERVICE DOOR SURROUND STRUCTURE WAS REMOVED AND EVALUATED OUT OF LIMITS PER CRJ900 SRM 51-21-06-001-001-A01 AND CRJ-900 SRM 53-00-00-101-001-Jun 18, 2026 · N925XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026073001335Seal · wornLT WING TRAILING EDGE P-SEAL WORN BELOW MFS LOWER TRAILIND EDGE. LT WING TRAILING EDGE P-SEAL ON MFS LOWER TRAILIND EDGE WAS REPLACED PER CRJ-900 AMM 57-50-07 (CONFIG A01)Jun 17, 2026 · N925XJ · Cndair CL6002D24 · Wing Main, Frame StructureSDR REXA2026073001351Fitting · corrodedCORROSION FLOOR FITTING IN AFT ACCESS 108 (1EA) ON GALLEY 1. SUMMARY OF NRC 00306: NEW FLOOR FITTING P/N: CDSP2019-7C-760 IN AFT ACCESS 108 (1EA) ON GALLEY 1. WAS REPLACED PER SAFRAN CMM 25-33-67 REV. NO 10 DATED JUN 20/22Jun 14, 2026 · N925XJ · Cndair CL6002D24 · Fuselage, Equipment Attach FittingsSDR REXA2026073001350Fitting · corrodedCORROSION FLOOR FITTING IN FWD ACCESS 306 (1EA) ON GALLEY 3. SUMMARY OF NRC 00304: NEW FLOOR FITTING P/N: CDSP2019-7C-650 IN FWD ACCESS 306 (1EA) ON GALLEY 3. WAS REPLACED PER ZODIAC AEROSPACE CMM 25-33-18 REV NO 5 DATED MAY 15/15Jun 14, 2026 · N925XJ · Cndair CL6002D24 · Fuselage, Equipment Attach FittingsSDR REXA2026073001349Fitting · corrodedCORROSION FLOOR FITTING IN FWD ACCESS 107 (1EA) ON GALLEY 1. SUMMARY OF NRC 00303: 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 20/22Jun 14, 2026 · N925XJ · Cndair CL6002D24 · Fuselage, Equipment Attach FittingsSDR REXA2026073001346Hinge · corrodedCORROSION ON STEP DOOR HINGE FWD, CENTER, AFT AT AFT BAGGAGE BAY DOOR AREA STEP DOOR HINGE CENTER, AFT AT AFT BAGGAGE BAY DOOR AREA WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01, AND STEP DOOR HINGE FWD AT AFT BAGGAGE BAY DOOR AREA WAS FABRICATED PER EA Jun 14, 2026 · N925XJ · Cndair CL6002D24 · Fuselage, Door HingeSDR REXA2026073001345Hinge · corrodedCORROSION ON STEP DOOR HINGE FWD, CENTER, AFT AT AFT BAGGAGE BAY DOOR AREA STEP DOOR HINGE CENTER, AFT AT AFT BAGGAGE BAY DOOR AREA WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01, AND STEP DOOR HINGE FWD AT AFT BAGGAGE BAY DOOR AREA WAS FABRICATED PER EA Jun 14, 2026 · N925XJ · Cndair CL6002D24 · Fuselage, Door HingeSDR REXA2026073001344Hinge · corrodedCORROSION ON STEP DOOR HINGE FWD, CENTER, AFT AT AFT BAGGAGE BAY DOOR AREA STEP DOOR HINGE CENTER, AFT AT AFT BAGGAGE BAY DOOR AREA WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01, AND STEP DOOR HINGE FWD AT AFT BAGGAGE BAY DOOR AREA WAS FABRICATED PER EA Jun 14, 2026 · N925XJ · Cndair CL6002D24 · Fuselage, Door HingeSDR REXA2026073001330Seat Track · corrodedCORROSION ON STGR 24R AND FS333.00/FS349.00. CORROSION ON STGR 24R AND FS333.00/FS349.00. WAS EVALUATED OUT LIMITS THEREFORE WAS REPAIRED PER CRJ-900 SRM 53-21-03-101-002-A04 AND SRM 53-00-03-201-001-A0Jun 13, 2026 · N925XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2026073001329Floorbeam · crackedCRACK ON FLOOR BEAM ANGLE RBL 12 AT FS 280.00 WAS FOUND. NEW FLOOR BEAM ANGLE RBL 12 AT FS 280.00 WAS VERIFIED PER CRJ900 SRM 53-11-43-001-001-A01 ///REPLACE WAS PERFORMED UNDER NRC 0057Jun 13, 2026 · N925XJ · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR REXA2026073001328Stub Frame · corrodedCORROSION ON STUB FRAME AT FS 533.00 AND FS 549.00 APROX STGR 18 LH AT SURROUND STRUCTURE OF FWD BAGGAGE BAY DOOR STUB FRAME AT FS 533.00 AND FS 549.00 APROX STGR 18 LH AT SURROUND STRUCTURE OF FWD BAGGAGE BAY DOOR WERE EVALUATED OUT LIMITS PER CRJ 900 SRM 51-Jun 13, 2026 · N925XJ · Cndair CL6002D24 · Fuselage Main, StructureSDR REXA2026073001327Stub Frame · corrodedCORROSION ON STUB FRAME AT FS 533.00 AND FS 549.00 APROX STGR 18 LH AT SURROUND STRUCTURE OF FWD BAGGAGE BAY DOOR STUB FRAME AT FS 533.00 AND FS 549.00 APROX STGR 18 LH AT SURROUND STRUCTURE OF FWD BAGGAGE BAY DOOR WERE EVALUATED OUT LIMITS PER CRJ 900 SRM 51-Jun 13, 2026 · N925XJ · Cndair CL6002D24 · Fuselage Main, StructureSDR REXA2026073001326Floor Support · corrodedCORROSION ON FLOOR SILL AT FLOOOR STRUCTURE PASSENGER CABIN BTW FS 280.00 TO 319.70 FLOOR SILL AT FLOOOR STRUCTURE PASSENGER CABIN BTW FS 280.00 TO 319.70 WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01, SRM 51-42-10-001-001-A01 AND CRJ900 SRM 51-42-13-001-00Jun 13, 2026 · N925XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026073001325Fitting · corrodedCORROSION ON FITTING APROX ON RBL12 FITTING ON RBL12 FS:290 APROX WAS REMPLACED PER. CRJ900 SRM 51-42-21-001-001-A01 6. C.Jun 13, 2026 · N925XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026073001322Skin Splice · corrodedCORROSION ON INTERNAL SKIN SPLICE AT FS 280.00 TO FS 282.00 FROM STGR 24RH TO 26LH CORROSION ON INTERNAL SKIN SPLICE AT FS 280.00 TO FS 282.00 FROM STGR 24RH TO 26LH WAS REMOVED PER CRJ-900 SRM SRM 51-21-06-001-001-A01 EVALUATED BTW FS 280.00 TO FS 282.00 FROMJun 12, 2026 · N925XJ · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR REXA2026073001339Collector · corrodedCORROSION ON COLLECTOR TRAY CORROSION OF THE COLLECTOR TRAY WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 AND WAS EVALUATED PER CRJ-900 SRM 53 -00-00-101-001-A01 AND WAS DETERMINING WITH EXCESSIVE DAMAGE. NEW COLLECTOR TRAY WAS VERIFIED PER CRJ900 AIPC 24-2Jun 11, 2026 · N925XJ · Cndair CL6002D24 · Cabin Equipment/FurnishingsSDR REXA2026073001343Strap · corrodedCORROSION ON STRAP AT FAIRING 193AB. STRAP(2EAS) AT FAIRING 193AB WERE REPLACED PER SRM 51-42-10-001-001-A01 AND SRM 51-42-06-001-001-A01Jun 9, 2026 · N925XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026073001342Strap · corrodedCORROSION ON STRAP AT FAIRING 193AB. STRAP(2EAS) AT FAIRING 193AB WERE REPLACED PER CRJ-900 SRM 51-42-10-001-001-A01 AND SRM 51-42-06-001-001-A01Jun 9, 2026 · N925XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026073001341Bracket · corrodedCORROSION ON INTERNAL ANGLES IN REFUEL/DEFUEL PANEL AT INTERNAL AREA OF FAIRING 192AR. CORROSION ANGLE (1 EA) IN REFUEL/DEFUEL PANEL AT INTERNAL AREA OF FAIRING 192AR WERE REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 AND WAS FOUND WITHIN OF LIMITS PER CRJ-900Jun 9, 2026 · N925XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026073001324Stringer · corrodedCORROSION ON STGR 21 RH BTWN FS 364.00 TO FS 379.00 CORROSION ON STGR 21 RH BTWN FS 364.00 TO FS 379.00 WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 EVALUATED OUT LIMITS PER CRJ-900 SRM 53-21-03-101-006-A04 THEREFORES WAS REPLACED PER CRJ 900 SRM 51-42-21-Jun 9, 2026 · N925XJ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2026073001323Angle · corrodedCORROSION ON MOUNITNG ANGLE OF SERVICE DOOR BTW FS 319 TO 349 AT CPAX MOUNITNG ANGLE OF SERVICE DOOR BTW FS 319 TO 349 AT CPAX WAS EVALUATED OUT OF LIMITS DUE TO EXCESIVE CORROSION PER CRJ-900 SRM 53-00-00-101-001-A01, THEREFORE WAS REPLACED PER CRJ-900 SRM 51Jun 9, 2026 · N925XJ · Cndair CL6002D24 · Service DoorsSDR REXA2026073001340Access Panel · corrodedCORROSION ON ACCESS PANEL 542AZ, 542BZ, 642AZ AND 642BZ. CORROSION WERE REMOVED ON ACCESS PANEL 542BZ AND 642BZ PER CRJ-900 SRM 51-21-06-001-001-A01 AND WERE FOUND WITHIN LIMITS PER CRJ-900 SRM 53-00-01-101-001-A01. ACCESS PANELS 542AZ AND 642AZ WERE REPLACED Jun 8, 2026 · N925XJ · Cndair CL6002D24 · Fuselage Main, StructureSDR REXA2026073001321Seat Track · corrodedCORROSION ON SIDE SEAT RAILS BTW STA FS379 TO FS699 STGR15LH AND STGR15RH SIDE SEAT RAILS BTW STA FS379 TO FS699 STGR15LH AND STGR15RH WERE EVALUATED OUT LIMITS PER CRJ/900 SRM 53-21-49-101-001-A01, SRM 53-31-49-101-001-A02 THEREFORE WERE REPLACED PER CRJ 900 Jun 6, 2026 · N925XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2026073001319Strap · crackedCRACK ON STRAP AT GROUND SPOILERS (2EAS INB/OUT) AT LH WING AND (1EA INB) AT RH WING SPS 21.80 PROTECTOR PLATE AT SERVICE DOOR SURROUND STRUCTURE WAS EVALUATED DUE EXCCESSIVE CORROSION AND WILL BE REPLACED PER CRJ900 SRM 51-10-06-001-001-A01, THEREFORE NEW PROJun 6, 2026 · N925XJ · Cndair CL6002D24 · SpoilersSDR REXA2026073001318Strap · crackedCRACK ON STRAP AT GROUND SPOILERS (2EAS INB/OUT) AT LH WING AND (1EA INB) AT RH WING SPS 21.80 PROTECTOR PLATE AT SERVICE DOOR SURROUND STRUCTURE WAS EVALUATED DUE EXCCESSIVE CORROSION AND WILL BE REPLACED PER CRJ900 SRM 51-10-06-001-001-A01, THEREFORE NEW PROJun 6, 2026 · N925XJ · Cndair CL6002D24 · SpoilersSDR REXA2026073001317Stringer · corrodedCORROSION ON STGR 27 BTW FS1162.00 AND FS 1181.00 AT REAR FUSELAGE INERNAL STRUCURE. NEW STRINGER STGR 27 BTW FS1162.00 AND FS 1181.00 AT REAR FUSELAGE INERNAL STRUCURE WAS FABRICATED PER CRJ-900 DGW: MM670-38134 REV. F AND REPLACED PER CRJ-900 SRM 51-42-06-00Jun 6, 2026 · N925XJ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2026073001316Support Angle · crackedCRACK ON LH WING BRACKET SUPPORT ANGLE SS 15.50, LOWER INNER AREA. CRACK ON LH WING BRACKET SUPPORT ANGLE SS 15.50, LOWER INNER AREA WAS REPAIRED PER EA NO: CRJ957-22519 EA REV IRJun 6, 2026 · N925XJ · Cndair CL6002D24 · Wing Miscellaneous StructureSDR REXA2026073001315Track · wornWEAR LOWER AFT RAIL OF AFT BAGGAGE DOOR LOWER AFT RAIL OF AFT BAGGAGE DOOR WAS REPAIRED PER EA:CRJ953-22520 REV IRJun 6, 2026 · N925XJ · Cndair CL6002D24 · Cargo/Baggage DoorsSDR REXA2026073001314Roller · wornWEAR AFT ROLLER GUIDE UPPER AT AFT BAGGAGE BAY DOOR AFT ROLLER GUIDE UPPER AT AFT BAGGAGE BAY DOOR WAS EVALUATED OUT LIMITS PER CRJ 900 SRM 53-00-00-101-001-A01 THEREFORE WAS REPLACED PER CRJ 900 SRM 51-42-06-001-001-A01Jun 6, 2026 · N925XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2025031000298Battery Pack · inoperativeL AND R AFT EXTERIOR EMERGENCY LIGHTS INOP R/R AFT(PS38) EMERGENCY LIGHT BATTERY ASSY AND CHARGER ASSY IAW CRJ900 AMM 33-51-17 OPC GOODMar 9, 2025 · N925XJ · Cndair CL6002D24 · Emergency LightingSDR REXA2025031000297Battery Pack · inoperativeFOUND EMERGENCY LIGHTING IN CABIN REAR AND EXTERNAL REAR NOT WORKING R/R EPSU BATTERY PACK PS38 IAW JOB CARD 33-900-701. OPS CHECK GOOD, NO FURTHER DEFECTS NOTED P/N ON/OFF 2013-1ASMI S/N ON 19356 S/N OFF 19241Mar 6, 2025 · N925XJ · Cndair CL6002D24 · Emergency LightingSDR REXA2024062400483Windshield · inoperativeDURING TAKEOFF AT ABOUT 1000 FEET, CAPTAIN'S WINDSHIELD ON LOWER LEFT SIDE STARTED SMOKING. TURNED OFF WINDSHIELD HEAT AND RETURNED TO CVG. ALSO SMELLED SMOKE FOR THE REMAINDER OF THE FLIGHT. REMOVED AND REPLACED LH CAPTAINS WINDSHIELD IAW 700/900 JC 900-56-9Jun 19, 2024 · N925XJ · Cndair CL6002D24 · Flight Compartment WindowsSDR REXA2022042100295Beam · crackedRBL 18 POST AT INBOARD FLANGE CRACKED. REMOVED AND REPLACED IAW CRJ 900 SRMS 51-40-11-001-001-A01, AND 51-42-06-001-001-A01.Apr 4, 2023 · N925XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2022031600261Web · crackedFWD EQUIPMENT COMPARTMENT, L/H FLOOR IS CRACKED AT F.S.193. REPAIRED L/H FLOOR IN THE FWD EQUIPMENT COMPARTMENT AT F.S. 193.Mar 15, 2023 · N925XJ · Cndair CL6002D24 · Fuselage Main, StructureSDR REXA2021080300527Bulb · inoperativeRIGHT SIDE AFT MOST EMER LIGHT EXTERIOR IS INOP. REMOVED AND REPLACED RH AFT MOST OVERWING EMER. EXIT LIGHT BULB IAW AMM 33-51-15. OP/C GOOD.Jul 29, 2021 · N925XJ · Cndair CL6002D24 · Emergency LightingSDR REXA2021042000246Battery Pack · dischargedEPSU BATTERY PACK DEAD (PS38). REMOVED AND REPLACED EPSU BATTERY PACK (PS38). OPERATIONAL TEST OF THE EPSU CHECK GOOD IAW AMM 33-51-17 PN OFF 2013-1A SN OFF 101377 PN ON 2013-1ASMI SN ON 12016Apr 16, 2021 · N925XJ · Cndair CL6002D24 · Emergency LightingSDR REXA2020122100839Strap · damagedLT LOWER BUTT STRAP COMMON TO LOWER WING PLANK HAS 1 EA 2ND OVERSIZE 3/8 HOLE LOCATED IN COLD WORK AREA OF TRUNNION. REPAIRED AREA, IAW REO 690-57-21-380 REV-- DATED 12/15/20.Dec 16, 2020 · N925XJ · Cndair CL6002D24 · Wing Miscellaneous StructureSDR REXA201910141426Stop Fitting · corrodedCORROSION ON LOWER STOP FITTING AT PASSENGER DOOR. BRACKET ASSY WAS REPLACED FOR NEW ONE (P/N: 601R38921-9) PER CRJ-900 SRM 51-42-06-001-001-A01. PAR 6C.Oct 10, 2019 · N925XJ · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2019101491474Shield · perforatedWEAR ON PRODUCTION DOUBLER OF PANEL BLOW OFF DOOR AT FORWARD CORE COWL ASSEMBLY UPPER RIGHT SIDE.(INNER FACE) ENGINE NR 2. A NEW BLOW OFF DOOR FIRESHIELD WAS INSTALLED PER SRM 51-22-00-001-001-A01, PAR.5, SRM 51-42-06-001-001-A01, SRM 51-42-10-001-001-A01, AOct 9, 2019 · N925XJ · Cndair CL6002D24 · Engine (Turbine/Turboprop)SDR REXA2019101491461Insert · missingMISSING INSERT ON FLOOR PANEL 282JRF AT AFT CARGO COMPARTMENT. THE FLOOR PANEL WAS REPLACED FOR NEW ONE IAW AMM 53-00-47.Oct 9, 2019 · N925XJ · Cndair CL6002D24 · Fuselage Floor PanelSDR REXA2019101491423Intercostal · corrodedCORROSION ON INTERCOSTAL DD6 BTW FORMER FS320.163 TO 338.963 AT PASSENGER DOOR. INTERCOSTAL DD6 BTW FORMER FS320.163 TO 338.963 AT PASSENGER DOOR WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 PAR. 6. C. AND SRM 51-42-21-001-001-A01 PAR. 6. COct 9, 2019 · N925XJ · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2019101491420Retainer · dentedSEVERAL DENTS ON LOWER RETAINER SEAL ALSO LOWER EDGE AT FWD AND MID CARGO COMPARTMENT DOOR. LOWER RETAINER SEAL FWD AND MID WERE REPLACED PER CRJ/900 AMM 52-35-07-400-802-A02, TOOL USED; TORQUEMETER P/N:QDRIVER4 S/N:0515405073 D/D:06/MAR/20.Oct 9, 2019 · N925XJ · Cndair CL6002D24 · Cargo/Baggage DoorsSDR REXA2019101481465Angle · corrodedCORROSION ON SUPPORT MOUNTING ANGLE BTW BS 319 TO 349 AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX). SUPPORT MOUNTING ANGLE BTW FS= 319 TO 349 AT GALLEY SERVICE DOOR LOWER WAS REPLACED PER SRM 51-42-06-001-001-A01.Oct 8, 2019 · N925XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2019101401458Floor Support · corrodedCORROSION ON FLOOR BEAM 9LBL BTW STA. FS= 1015 AND FS= 1047 AT AFT BAGGAGE BAY. FLOOR BEAM 9LBL BTW FS:1015 AND FS:1047 AT AFT BAGGAGE BAY WAS REPAIRED PER CRJ-900 SRM. 53-00-41-201-001-A03 AND CRJ-900 SRM 51-21-06-001-001-A01. CORROSION LEVEL 2.Oct 7, 2019 · N925XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
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