# Service difficulty reports: N927XJ A list on [N927XJ](https://openairdocs.org/aircraft/N927XJ.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 · 193 reports - [SDR REXA2026070701015](https://openairdocs.org/sdr/REXA2026070701015.md): Hinge · corroded · Jun 3, 2026 · N927XJ · Cndair CL6002D24 · Fuselage, Door Hinge > CORROSION ON HINGES AND HINGES FITTINGS (4 EAS) ON ACCESS DOOR 196ER. DUE TO EXCESSIVE CORROSION ON HINGES AND HINGES FITTINGS (4 EAS) ON ACCESS DOOR 196ER WERE REPLACED IAW SRM 51-10-06-001-001-A01 AND SRM 51-41-02-001-001-A01. - [SDR REXA2026070301014](https://openairdocs.org/sdr/REXA2026070301014.md): Hinge · corroded · Jun 3, 2026 · N927XJ · Cndair CL6002D24 · Fuselage, Door Hinge > CORROSION ON HINGES AND HINGES FITTINGS (4 EAS) ON ACCESS DOOR 196ER. DUE TO EXCESSIVE CORROSION ON HINGES AND HINGES FITTINGS (4 EAS) ON ACCESS DOOR 196ER WERE REPLACED PER CRJ 900 SRM 51-10-06-001-001-A01 AND SRM 51-41-02-001-001-A01 - [SDR REXA2026070301013](https://openairdocs.org/sdr/REXA2026070301013.md): Hinge · corroded · Jun 3, 2026 · N927XJ · Cndair CL6002D24 · Fuselage, Door Hinge > CORROSION ON HINGES AND HINGES FITTINGS (4 EAS) ON ACCESS DOOR 196ER. DUE TO EXCESSIVE CORROSION ON HINGES AND HINGES FITTINGS (4 EAS) ON ACCESS DOOR 196ER WERE REPLACED PER CRJ 900 SRM 51-10-06-001-001-A01 AND SRM 51-41-02-001-001-A01 - [SDR REXA2026070301012](https://openairdocs.org/sdr/REXA2026070301012.md): Hinge · corroded · Jun 3, 2026 · N927XJ · Cndair CL6002D24 · Fuselage, Door Hinge > CORROSION ON HINGES AND HINGES FITTINGS (4 EAS) ON ACCESS DOOR 196ER. DUE TO EXCESSIVE CORROSION ON HINGES AND HINGES FITTINGS (4 EAS) ON ACCESS DOOR 196ER WERE REPLACED PER CRJ 900 SRM 51-10-06-001-001-A01 AND SRM 51-41-02-001-001-A01 - [SDR REXA2026070301004](https://openairdocs.org/sdr/REXA2026070301004.md): Acoustic Panel · cracked · Jun 3, 2026 · N927XJ · Cndair CL6002D24 · Engine Thrust Reverser > CRACK ON ACOUSTIC PANEL AFTER REMOVAL OF ZEE STIFFENER AT LH UPPER TRANSCOWL ACOUSTIC PANEL AT LT UPPER TRANSCOWL WAS REPAIRED PER EA NO CRJ954-22246 REV IR. - [SDR REXA2026070301066](https://openairdocs.org/sdr/REXA2026070301066.md): Stringer · corroded · May 19, 2026 · N927XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > CORROSION ON STRG 26R BTW FS 333.00 TO 364.00 AT FUSELAGE INTERNAL STRUCTURE. DUE TO EXCESSIVE CORROSION ON STGR 26 STRG 26R BTW FS 333.00 TO 364.00 AT FUSELAGE INTERNAL STRUCTURE WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 AND - [SDR REXA2026070301065](https://openairdocs.org/sdr/REXA2026070301065.md): Skin · corroded · May 19, 2026 · N927XJ · Cndair CL6002D24 · Fuselage Main, Plate/Skin > CORROSION ON SUPPORTS FRAME ALSO EXTERNAL FUSELAGE SKIN SETTLEMENT AREA OF FAIRINGS 195AB, 195BB, 195AL, 195DL, 196DR AND 196AR AT LOWER FUSELAGE STRUCTURE BTW FS847.00 TO FS942.00 AND LBL 45.00 TO RBL 45.00. CORROSION ON SUPPORTS FRAME ALSO EXTERNAL FUSELAGE - [SDR REXA2026070301064](https://openairdocs.org/sdr/REXA2026070301064.md): Plate · corroded · May 19, 2026 · N927XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CORROSION ON BRACKET MACHINED (4E/A) AND PLATE (2E/A) AT FWD CARGO COMPARTMENT. BRACKET MACHINED FS517 BTW STGR 22LH TO STGR 23LH AND PATE BTW FS 645 TO FS 661 WERE CLEANED PER CRJ900 SRM 51-26-00-001-001-A01 AND PAINT WAS REMOVED PER CRJ-900 SRM 51-26-01-001- - [SDR REXA2026070301063](https://openairdocs.org/sdr/REXA2026070301063.md): Bracket · corroded · May 19, 2026 · N927XJ · Cndair CL6002D24 · Fuselage Main, Attach Fittings > CORROSION ON BRACKET MACHINED (4E/A) AND PLATE (2E/A) AT FWD CARGO COMPARTMENT. BRACKET MACHINED FS517 BTW STGR 22LH TO STGR 23LH AND PATE BTW FS 645 TO FS 661 WERE CLEANED PER CRJ900 SRM 51-26-00-001-001-A01 AND PAINT WAS REMOVED PER CRJ-900 SRM 51-26-01-001- - [SDR REXA2026070301061](https://openairdocs.org/sdr/REXA2026070301061.md): Bracket · corroded · May 19, 2026 · N927XJ · Cndair CL6002D24 · Fuselage Main, Attach Fittings > CORROSION ON BRACKET MACHINED (4E/A) AND PLATE (2E/A) AT FWD CARGO COMPARTMENT. BRACKET MACHINED FS517 BTW STGR 22LH TO STGR 23LH AND PATE BTW FS 645 TO FS 661 WERE CLEANED PER CRJ900 SRM 51-26-00-001-001-A01 AND PAINT WAS REMOVED PER CRJ-900 SRM 51-26-01-001- - [SDR REXA2026070301042](https://openairdocs.org/sdr/REXA2026070301042.md): Seat Track · corroded · May 19, 2026 · N927XJ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings > CORROSION ON SEAT TRACK BTW FS375.00 TO FS485.00 LBL9.00 AND FS349.00 TO FS485.00 RBL9.00 ALSO CORROSION ON SIDE SEAT RAIL BTW FS785.15 TO FS847.00+16 AND STGR 15LH/15RH AT PASSENGER CABIN SEAT RAIL BTW FS375.00 TO FS485.00 LBL9.00 AND FS349.00 TO FS485.00 RB - [SDR REXA2026070301034](https://openairdocs.org/sdr/REXA2026070301034.md): Door Frame · cracked · May 19, 2026 · N927XJ · Cndair CL6002D24 · Fuselage Main, Structure > CRACK ON UPPER AFT SHIELD OF CORNER FRAME AT FWD BAGGAGE DOOR. UPPER AFT SHIELD OF CORNER FRAME AT FWD BAGGAGE DOOR WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-41-02-001-001-A01 - [SDR REXA2026070301056](https://openairdocs.org/sdr/REXA2026070301056.md): Hinge Fitting · corroded · May 9, 2026 · N927XJ · Cndair CL6002D24 · Fuselage, Door Hinge > AFTER BUSHINGS REMOVAL, CORROSION WAS FOUND ON LH/RH NLG AFT DOOR HINGE FITTING (2 EAS) AND CORROSION ON RH/LH AIRFRAME HINGE FITTING (2 EAS) AT NLG. LH/RH NLG AFT DOOR HINGE FITTING (2 EAS) AND RH/LH AIRFRAME HINGE FITTING (2 EAS) AT NLG WERE REPLACED PER CRJ - [SDR REXA2026070301055](https://openairdocs.org/sdr/REXA2026070301055.md): Hinge Fitting · corroded · May 9, 2026 · N927XJ · Cndair CL6002D24 · Fuselage, Door Hinge > AFTER BUSHINGS REMOVAL, CORROSION WAS FOUND ON LH/RH NLG AFT DOOR HINGE FITTING (2 EAS) AND CORROSION ON RH/LH AIRFRAME HINGE FITTING (2 EAS) AT NLG. LH/RH NLG AFT DOOR HINGE FITTING (2 EAS) AND RH/LH AIRFRAME HINGE FITTING (2 EAS) AT NLG WERE REPLACED PER CRJ - [SDR REXA2026070301054](https://openairdocs.org/sdr/REXA2026070301054.md): Hinge Fitting · corroded · May 9, 2026 · N927XJ · Cndair CL6002D24 · Fuselage, Door Hinge > AFTER BUSHINGS REMOVAL, CORROSION WAS FOUND ON LH/RH NLG AFT DOOR HINGE FITTING (2 EAS) AND CORROSION ON RT & LT AIRFRAME HINGE FITTING (2 EAS) AT NLG. LH/RH NLG AFT DOOR HINGE FITTING (2 EAS) AND RH/LH AIRFRAME HINGE FITTING (2 EAS) AT NLG WERE REPLACED PER C - [SDR REXA2026070301058](https://openairdocs.org/sdr/REXA2026070301058.md): Fitting · corroded · May 7, 2026 · N927XJ · Cndair CL6002D24 · Ailerons > CORROSION AND WEAR WAS FOUND ON LUG BORE ON AIL STA.336.4015 (LUG L1) AND 337.657 (LUG L2) AT LH AILERON. LUG BORE L 1=(STA=336.4015), L2=(STA=337.657), L5=(STA=342.911) & L6=(STA=344.1665) ON CENTTER FITTING AT LH AILERON WERE REPAIRED PER REO 670-57-61-237 - [SDR REXA2026070301053](https://openairdocs.org/sdr/REXA2026070301053.md): Door Frame · corroded · May 6, 2026 · N927XJ · Cndair CL6002D24 · Fuselage Main, Structure > CORROSION WAS FOUND ON MID CAP AT PASSENEGER DOOR SURROUND STRUCTURE. NEW MID CAP AT PASSENEGER DOOR SURROUND STRUCTURE WAS DRILLED, COUNTERSINK AND TREAT HOLES PER CRJ 900 SRM 51-40-11-001-001-A01, CRJ 900 SRM 51-40-11-001-001-A01, CRJ 900 SRM 51-21-11-001-0 - [SDR REXA2026070301033](https://openairdocs.org/sdr/REXA2026070301033.md): Stringer · corroded · May 6, 2026 · N927XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > CORROSION ON STRINGERS (2E/A) ON STGR26L FROM FS1069 TO FS1088 AND ON STGR21L FROM FS1015 TO FS1031 AT AFT BAGGAGE COMPARTMENT. CORROSION ON STRINGER (1E/A) ON STGR26L FROM FS1069 TO FS1088 WAS REPAIRED PER CRJ953-22227 REV. IR AND STGR21L FROM FS1015 TO FS103 - [SDR REXA2026070701003](https://openairdocs.org/sdr/REXA2026070701003.md): Support Web · cracked · May 5, 2026 · N927XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CRACKED EDGE OF ADSHC SUPPORT WEB (LH SIDE) AT COCKPIT ADSHC SUPPORT WEB (LH SIDE) AT COCKPIT WAS REPAIRED PER SRM 51-71-28-001-001-A01 AND SRM 51-42-06-001-001-A01. - [SDR REXA2026070301059](https://openairdocs.org/sdr/REXA2026070301059.md): Fitting · corroded · May 5, 2026 · N927XJ · Cndair CL6002D24 · Fuselage, Equipment Attach Fittings > CORROSION FLOOR FITTING IN AFT AND FWD ACCESS 107 (2EAS) ON GALLEY 1. FLOOR FITTING IN AFT AND FWD ACCESS 107 (2EAS) ON GALLEY 1 WERE REPLACED PER SAFRAN CMM 25-33-67 REV NO.10 - [SDR REXA2026070301057](https://openairdocs.org/sdr/REXA2026070301057.md): Lug · corroded · May 5, 2026 · N927XJ · Cndair CL6002D24 · Ailerons > CORROSION AND WEAR WAS FOUND ON LUG BORE ON AIL STA 336.4015 (LUG R1), 337.657 (LUG R2), 342.123 (LUG R4), 342.911 (LUG R5), 344.1665 (LUG R6) AND CORROSION ON LUG FACE ON AIL STA 337.657 (LUG R2) AT RH AILERON LUG BORE STA 336.4015 (LUG R1), STA 337.657 (LUG - [SDR REXA2026070301052](https://openairdocs.org/sdr/REXA2026070301052.md): Stringer · corroded · May 5, 2026 · N927XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > CORROSION ON STRINGERS (1E/A) ON STGR23L FROM FS985 TO FS1051 AT AFT BAGGAGE COMPARTMENT. STRINGERS (1E/A) ON STGR23L FROM FS985 TO FS1051 AT AFT BAGGAGE COMPARTMENT WAS EVALUATED DUE TO EXCESIVE CORROSION PER CRJ-900 SRM 53-61-03-101-003-A02, THEREFORE WAS RE - [SDR REXA2026070301051](https://openairdocs.org/sdr/REXA2026070301051.md): Floorbeam · corroded · May 5, 2026 · N927XJ · Cndair CL6002D24 · Fuselage Main, Floor Beam > CORROSION ON FLOOR CROSSBEAM FS1051 BTW RBL27 AND RBL47 AT AFT BAGGAGE COMPARTMENT FLOOR CROSSBEAM FS1051 BTW RBL27 AND RBL47 AT AFT BAGGAGE COMPARTMENT WAS REPAIRED PER EA NO. CRJ953-22332 REV IR - [SDR REXA2026070301050](https://openairdocs.org/sdr/REXA2026070301050.md): Skin · corroded · May 5, 2026 · N927XJ · Cndair CL6002D24 · Fuselage Main, Plate/Skin > CORROSION ON SKIN AND STGR 21R BTW FS 349.00 TO 364.00 AND BTW STGR 20R TO 21R AT FUSELAGE INTERNAL STRUCTURE. CORROSION ON SKIN WAS REPAIRED PER EA CRJ953-22252 REV. IR AND STGR 21R BTW FS 349.00 TO 364.00 AND BTW STGR 20R TO 21R WAS CLEANED AND NOT FOUND CO - [SDR REXA2026070301049](https://openairdocs.org/sdr/REXA2026070301049.md): Frame · corroded · May 5, 2026 · N927XJ · Cndair CL6002D24 · Fuselage Main, Frame > CORROSION ON FRAME FS 1000 BTW STGR 25R TO STGR 26R FRAME FS 1000 BTW STGR 25R TO STGR 26R WAS EVALUATED AND ALLOWABLE DAMAGE IS NOT PERMITED PER CRJ-900 SRM 53-61-06-101-003-A02, THEREFORE WAS REPAIRED PER CRJ-900 SRM 53-00-06-201-001-A03 - [SDR REXA2026070301048](https://openairdocs.org/sdr/REXA2026070301048.md): Angle · cracked · May 5, 2026 · N927XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CRACKED FLOOR SUPPORT ANGLES BTW FS 259.20 TO FS 280.00 AND LBL 12 AND RBL 12 AT PASSENGER CABIN FLOOR STRUCTURE. FLOOR SUPPORT ANGLES BTW FS 259.20 TO FS 280.00 AND LBL 12 AND RBL 12 AT PASSENGER CABIN FLOOR STRUCTURE WERE REPLACED PER CRJ 900 SRM 51-42-06-0 - [SDR REXA2026070301047](https://openairdocs.org/sdr/REXA2026070301047.md): Angle · cracked · May 5, 2026 · N927XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CRACKED FLOOR SUPPORT ANGLES BTW FS 259.20 TO FS 280.00 AND LBL 12 AND RBL 12 AT PASSENGER CABIN FLOOR STRUCTURE. FLOOR SUPPORT ANGLES BTW FS 259.20 TO FS 280.00 AND LBL 12 AND RBL 12 AT PASSENGER CABIN FLOOR STRUCTURE WERE REPLACED PER CRJ 900 SRM 51-42-06-0 - [SDR REXA2026070301032](https://openairdocs.org/sdr/REXA2026070301032.md): Support · corroded · May 5, 2026 · N927XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CORROSION ON SUPPORTS (7EAS) OF WHEEL BIN 173BZ AND 174BZ AT FS797.00 TO FS830.40 AND LBL 45.00 TO RBL 45.00 MLG WHEEL WELL AREA. CORROSION ON SUPPORTS (6EAS) OF WHEEL BIN 173BZ AND 174BZ AT FS797.00 TO FS830.40 AND LBL 45.00 TO RBL 45.00 MLG WHEEL WELL AREA W - [SDR REXA2026070301023](https://openairdocs.org/sdr/REXA2026070301023.md): Fitting · corroded · May 5, 2026 · N927XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CORROSION FLOOR FITTING IN AFT AND FWD ACCESS 107 (2EAS) ON GALLEY 1. FLOOR FITTING IN AFT AND FWD ACCESS 107 (2EAS) ON GALLEY 1 WERE REPLACED PER SAFRAN CMM 25-33-67 REV NO.10 - [SDR REXA2026070301022](https://openairdocs.org/sdr/REXA2026070301022.md): Fitting · corroded · May 5, 2026 · N927XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CORROSION FLOOR FITTING FWD ACCESS 306 (1EA) AND AFT ACCESS 305 (1EA) ON GALLEY 3 FLOOR FITTING FWD ACCESS 306 (1EA) AND AFT ACCESS 305 (1EA) ON GALLEY 3 WERE REPLACED PER ZODIAC AEROSPACE CMM 25-33-18 REV NO.5 - [SDR REXA2026070301020](https://openairdocs.org/sdr/REXA2026070301020.md): Fitting · corroded · May 5, 2026 · N927XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CORROSION FLOOR FITTING FWD ACCESS 306 (1EA) AND AFT ACCESS 305 (1EA) ON GALLEY 3 FLOOR FITTING FWD ACCESS 306 (1EA) AND AFT ACCESS 305 (1EA) ON GALLEY 3 WERE REPLACED PER ZODIAC AEROSPACE CMM 25-33-18 REV NO.5 - [SDR REXA2026070301016](https://openairdocs.org/sdr/REXA2026070301016.md): Stringer · corroded · May 5, 2026 · N927XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > CORROSION ON STGR 20R BTW FS 295 TO FS 310. STGR 20R BTW FS 295 TO FS 310 WAS EVALUATED OUT OFF LIMITS PER CRJ-900 SRM 53-21-03-101-002-A04 AND STGR 20R BTW FS 280 TO FS 319 WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01 - [SDR REXA2026070301011](https://openairdocs.org/sdr/REXA2026070301011.md): Frame · corroded · May 5, 2026 · N927XJ · Cndair CL6002D24 · Fuselage Main, Frame > CORROSION ON FRAME BTW FS=969/ STGR 25L TO 26L,FS=847+16/STGR 27 AND FS=847+32/STGR 26L TO 26R AT FUSELAGE INTERNAL STRUCTURE DUE TO EXCESSIVE CORROSION ON FRAME FS=847+32/STGR 26L TO 26R WAS REPLACED IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01 - [SDR REXA2026070301002](https://openairdocs.org/sdr/REXA2026070301002.md): Frame · corroded · May 5, 2026 · N927XJ · Cndair CL6002D24 · Fuselage Main, Frame > CORROSION ON FRAME BTW FS 319.00 AND STGR 26R TO 26L AT FUSELAGE INTERNAL STRUCTURE. CORROSION ON FRAME BTW FS 319.00 AND STGR 26R TO 26L AT FUSELAGE INTERNAL STRUCTURE WAS REMOVED CRJ900 SRM 51-21-06-001-001-A01 AND EVALUATED OUT LIMITS PER CRJ-900 SRM 53-21 - [SDR REXA2026070301046](https://openairdocs.org/sdr/REXA2026070301046.md): Beam · worn · May 4, 2026 · N927XJ · Cndair CL6002D24 · Fuselage Main, Structure > WEAR ON BEAM FS 1000 AND FS 1047 AT SURROUND STRUCTURE OF THE AFT CARGO DOOR CUTOUT BEAM FS 1000 AND FS 1047 AT SURROUND STRUCTURE OF THE AFT CARGO DOOR CUTOUT WAS EVALUATED OUT LIMITS DUE TO EXCESSIVE WEAR PER CRJ 900 SRM 51-10-06-001-001-A01, THEREFORE WAS R - [SDR REXA2026070301045](https://openairdocs.org/sdr/REXA2026070301045.md): Skin · corroded · May 4, 2026 · N927XJ · Cndair CL6002D24 · Fuselage Main, Plate/Skin > CORROSION ON SEATTLEMENT AREA OF AFTER CARGO PROTECTOR PLATE. SEATTLEMENT AREA OF AFTER CARGO PROTECTOR PLATE WAS REPAIRED PER EA CRJ953-22285 REV IR - [SDR REXA2026070301044](https://openairdocs.org/sdr/REXA2026070301044.md): Stringer · corroded · May 4, 2026 · N927XJ · Cndair CL6002D24 · Fuselage Main, Frame > CORROSION ON STGR 21R FS 418 TO FS 421. STGR 21R FS 418 TO FS 421 WAS EVALUATE DUE TO EXCESSIVE CORROSION PER CRJ-900 SRM 53-21-03-101-006-A04, THEREFORE WAS REPLACED PER CRJ 900 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, SRM 51-42-10-001-001-A01 - [SDR REXA2026070301021](https://openairdocs.org/sdr/REXA2026070301021.md): Angle · corroded · May 4, 2026 · N927XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CORROSION ON ANGLES (3EAS) INSIDE OF ACCESS DOOR 192AR. AREA WAS CLEANED ON ANGLE (1EA) INSIDE ACCESS DOOR 192AR IAW SRM 51-26-00-001-001-A01 AND GVI WAS PERFOMED PER SRM 51-11-00-001-001-A01 AND ONLY PRIMER WAS FOUND DAMAGE. ANGLE BRACKETS (2EAS) INSIDE ACCES - [SDR REXA2026070301010](https://openairdocs.org/sdr/REXA2026070301010.md): Support · corroded · May 4, 2026 · N927XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CORROSION ON LT LOWER SILL BTW FS1000 TO 1051 AT AFT CARGO COMPARTMENT DOOR. DUE TO EXCESSIVE CORROSION ON LOWER SILL WAS REPLACED PER SRM 51-10-06-001-001-A01, SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 AND SRM 51-42-13-001-001-A01. - [SDR REXA2026070301007](https://openairdocs.org/sdr/REXA2026070301007.md): Channel · corroded · May 4, 2026 · N927XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CORROSION ON P-SEALS GANG CHANNELS AT INBOARD WING DRY BAY LT & RT SIDE APPROX WS10 & FS763/783 P-SEALS GANG CHANNELS AT INBOARD WING DRY BAY LT & RT SIDE APPROX WS10 & FS763/783 WERE REPLACED IAW SRM 51-41-02-001-001-A01. - [SDR REXA2026070301006](https://openairdocs.org/sdr/REXA2026070301006.md): Stringer · corroded · May 4, 2026 · N927XJ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > CORROSION ON STGR 19R BTW FS 394.00 TO 409.00 AND BTW FS 437.00 TO 453.00 AT FUSELAGE INTERNAL STRUCTURE. CORROSION ON STGR 19 BTW FS 437.00 TO 453.00 FS 437.00 TO 453.00 HAS NOT ALLOWABLE DAMAGE SECTION PER CRJ-900 SRM 53-00-03-201-001-A02, STRINGER WAS REPAI - [SDR REXA2026070301043](https://openairdocs.org/sdr/REXA2026070301043.md): Frame · corroded · May 3, 2026 · N927XJ · Cndair CL6002D24 · Fuselage Main, Frame > CORROSION ON FRAMES (5E/A) FS 469 BTW STGR 26L TO STGR 25L,FS 661+74 BTW STGR 26R TO STGR 27, FS 661+62 BTW STGR 26R TO STGR 26L, FS 661+32 STGR 26R TO STGR 27 AND FS 661+41 STGR 26R TO STGR 27 AT FWD CARGO COMPARTMENT. CORROSION ON FRAMES FS 661+74 BTW STGR - [SDR REXA2026070301041](https://openairdocs.org/sdr/REXA2026070301041.md): Frame · damaged · May 3, 2026 · N927XJ · Cndair CL6002D24 · Fuselage Main, Frame > SECONDARY NRC FROM NRC 006 DURING THE REMOVAL OF AFT RAIL DOUBLER (CHANNEL): TWO ELONGATE HOLES WERE FOUNDED ON FRAME STA 1047 BTW STRINGER 17LH AND 16LH ELONGATE HOLES ON FRAME STA 1047 BTW STRINGER 17LH AND 16LH WERE REPAIRED PER REO 690-53-61-1774 REV. - - - [SDR REXA2026070301008](https://openairdocs.org/sdr/REXA2026070301008.md): Angle · corroded · May 2, 2026 · N927XJ · Cndair CL6002D24 · Passenger/Crew Doors > CORROSION ON LOWER SILL AT PASSENGER DOOR SURROUND STRUCTURE DUE TO EXCESSIVE CORROSION ON LOWER SILL AT PASSENGER DOOR SURROUND STRUCTURE (KICKPLATE) WAS REPLACED PER CRJ-900 SRM 51-10-06-001-001-A01 AND SRM 51-42-06-001-001-A01 - [SDR REXA2026070301005](https://openairdocs.org/sdr/REXA2026070301005.md): Rib · cracked · May 2, 2026 · N927XJ · Cndair CL6002D24 · Wing, Rib/Bulkhead > CRACK ON PARTIAL RIB AT LEFT INBOARD FIXED LEADING EDGE SS27.75 PARTIAL RIB AT LEFT INBD FIXED LEADING EDGE SS27.75 WAS REPLACED IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 AND SRM 51-42-10-001-001-A01. - [SDR REXA2026070301060](https://openairdocs.org/sdr/REXA2026070301060.md): Floorbeam · corroded · May 1, 2026 · N927XJ · Cndair CL6002D24 · Fuselage Main, Floor Beam > SECONDARY NRC FROM NRC 00088': AFTER REMOVAL SUPPORT ANGLE, CORROSION ON FS 280 CROSS BEAM LH SIDE WAS FOUND. DUE TO EXCESSIVE CORROSION ON FS 280 CROSS BEAM LH SIDE WAS REPLACED PER CRJ/900 SRM 51-10-06-001-001-A01, SRM 51-42-06-001-001-A01, SRM 51-42-10-001- - [SDR REXA2026070301019](https://openairdocs.org/sdr/REXA2026070301019.md): Floorbeam · damaged · May 1, 2026 · N927XJ · Cndair CL6002D24 · Fuselage Main, Floor Beam > SEVERAL ELONGATE HOLES WERE FOUND ON CROSSBEAM AND ANGLE ATTACHED TO CROSSBEAM. ELONGATE HOLES ON LH SIDE WERE ATTENDED WITH THE REPLACE OF CROSSBEAM UNDER NRC 00097 AND ELONGATE HOLES RH SIDE WERE REPAIRED PER REO 690-53-11-2188 REV. A. - [SDR REXA2026070301018](https://openairdocs.org/sdr/REXA2026070301018.md): Rib · cracked · May 1, 2026 · N927XJ · Cndair CL6002D24 · Wing, Rib/Bulkhead > CRACK ON LEADING EDGE RIB SS57.16 AT RH WING. CRACKED ON LEADING EDGE RIB SS57.16 AT RH WING WAS REPAIRED PER REO 690-57-41-604 REV. -- - [SDR REXA2026070301017](https://openairdocs.org/sdr/REXA2026070301017.md): Floorbeam · corroded · May 1, 2026 · N927XJ · Cndair CL6002D24 · Fuselage Main, Floor Beam > CORROSION ON ANGLE FLOOR SUPPORT AT FS 280.00 AND BRW LBL 9.00 TO RBL 9.00 CORROSION ON ANGLE FLOOR SUPPORT AT FS 280.00 AND BRW LBL 9.00 TO RBL 9.00 WAS EVALUATED OUT OF LIMITS CRJ/900 SRM 51-10-06-001-001-A01 AND ANGLE WAS REPLACED PER CRJ 900 SRM 51-42-06-0 - [SDR REXA2026070301039](https://openairdocs.org/sdr/REXA2026070301039.md): Intercostal · corroded · Apr 30, 2026 · N927XJ · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CORROSION ON INTERCOSTALS (3 EAS) BTW FS 349 TO FS 364 NEAR STGR 27 ALSO STGR 26R AT MAIN AVIONICS COMPARTMENT INTERCOSTALS BTW 7LH AND 27RH, BTW FS 349 TO FS 364 NEAR STGR 27R WERE REPAIRED PER EA CRJ953-22320 REV IR AND EA NO: CRJ953-22321 REV IR AND INTERC Next page: https://openairdocs.org/aircraft/N927XJ/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 = 'N927XJ' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N927XJ/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.