N294PQ

Service difficulty reports · 74

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 = 'N294PQ' 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 REXA2026070201001Stringer · chafedMAINTENANCE FOUND CHAFE DAMAGE ON STR 7L BETWEEN FS 1144.00 AND 1162.00 CAUSED BY LOOSE AND DAMAGED HEAT EXCHANGER DIFFUSER AND WATER SPRAYER LINE. REPAIRED CHAFE DAMAGE TO STR 7L IAW GREO 670-53-61-292 REV EJun 30, 2026 · N294PQ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2025122401056Switch · out of positionBURNING WIRE ODOR COMING FROM FO SIDE PFD OR MFD MAINLY IN FLIGHT. PERFORMED OPS TEST OF THE DISPLAY COOLING SYSTEM IAW AMM 21-24-00. OPS CHECK GOOD SWITCH WAS FOUND IN STBY.Dec 21, 2025 · N294PQ · Cndair CL6002D24 · Indicating/Recording SystemSDR REXA2026052800831Bracket · corrodedCORROSION ON BRACKETS, MACHINED (6EAS) OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT. CORROSION ON BRACKETS, MACHINED (6EAS) OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT WAS EVALUATED OUT PER CRJ-900 SRM 51-21-06-001-001-A01 AND REPLACED PER CRJ 900 SRM 51-Nov 2, 2025 · N294PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026052800827Stiffener · crackedCRACK ON UPPPER STIFFENER ATTACHED TO POWER-ASSIST MOTOR BTW DATUM 4 AND DATUM 5 (AFT SIDE PANEL) OF PASSENGER DOOR INTERNAL STRUCTURE CRACK ON UPPPER STIFFENER ATTACHED TO POWER-ASSIST MOTOR BTW DATUM 4 AND DATUM 5 (AFT SIDE PANEL) OF PASSENGER DOOR INTERNALNov 2, 2025 · N294PQ · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2026052800838Floorbeam · crackedAFTER CUT DOOR POST RBL12 AT FS 280.00 LOWER SECTION OF THE BULKHEAD POST, CRACK ON FLOORBEAM WAS FOUND. FLOORBEAM WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01Oct 14, 2025 · N294PQ · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR REXA2026052800818Lug · corrodedCORROSION WAS FOUND ON LUGS BORES R1, R2, R3, R4, R5 AND R6 AT RH AILERON CENTER FITTING. BORE LUGS R3 AND R4 OF AILERON CENTER FITTING WAS CLEANED PER CRJ 900 SRM 51-26-00-001-001-A01 AND NOT DAMAGE FOUND & CENTER FITTING LUG BORES R1, R2, R5 AND R6 AILERON Oct 8, 2025 · N294PQ · Cndair CL6002D24 · AileronsSDR REXA2026052800816Floor Support · corrodedCORROSIN ON FLOOR SUPPORT LOCATED BTW FS1010.00AND LBL38. CORROSION ON FLOOR SUPPORT LOCATED BTW FS1010.00AND LBL38 WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 AND EVALUATED OUT OFF LIMITS PER CRJ-900 SRM 53-00-00-101-001-A01 AND SUPPORT WAS REPLACED PER Oct 8, 2025 · N294PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026052800837Seat Track · corrodedCORROSION ON FLOOR SEAT RAILS IN SECTIONS [ BTW FS= 474 TO FS= 394, FS=437 AND BTW FS=597 TO 613 LBL 9.00 ] AT PAX CABIN. CORROSION ON FLOOR SEAT RAILS IN SECTIONS [ BTW FS= 474 TO FS= 394, FS=437 AND BTW FS=597 TO 613 LBL 9.00 ] AT PAX CABIN WAS EVALUATED OUOct 7, 2025 · N294PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2026052800836Bearing · excess playFREE PLAY ON SELF-ALIGN SELF-LUB BEARING PLAIN ON HINGE FITTING NR 2 AND NR 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION. FITTING BEARINGS ON HINGE NO. 2 AND NO. 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION WERE REPLACED AND FREE PLAY WAS CORRECTEDOct 7, 2025 · N294PQ · Cndair CL6002D24 · Vertical Stabilizer Miscellaneous StructureSDR REXA2026052800817Seat Track · corrodedCORROSION ON SIDE SEAT RAILS IN SECTIONS [ FS= 744, BTW FS=785 TO FS=793, FS=847+16 AND BTW FS=897 TO FS=913 STGR 15LH ] AND [ BTW FS= 744 TO FS=764, FS=785, BTW FS=846 TO FS=847+16 AND BTW FS=897 TO FS=927 STGR 15RH ] AT PAX CABIN. CORROSION ON SIDE TRACK IN Oct 7, 2025 · N294PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2026052800835Seat Track · corrodedCORROSION ON SEAT RAIL 9RBL FS693 TO FS 847+16 (1E/A) FS847+16 TO FS977 (1E/A) AND SEAT RAIL 9LBL FS693 TO FS 847+16 (1E/A) FS847+16 TO FS977 (1E/A). CORROSION ON SEAT RAIL 9RBL FS693 TO FS 847+16 (1E/A) FS847+16 TO FS977 (1E/A) AND SEAT RAIL 9LBL FS693 TO FS Oct 6, 2025 · N294PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2026052800834Strap · corrodedCORROSION ON INTERNAL STRAP, SETTLEMENT AREA OF FAIRING ACCESS PANEL 194AB & 193AB CORROSION ON INTERNAL STRAP, SETTLEMENT AREA OF FAIRING ACCESS PANEL 194AB & 193AB WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 AND EVALUATED OUT LIMITS PER CRJ900 SRM 51-1Oct 6, 2025 · N294PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026052800821Bonding Plate · corrodedCORROSION ON UPPER/LOWER BONDING PLATES AT AFT SKIN, LH/RH PYLONS. CORROSION ON UPPER/LOWER BONDING PLATES AT AFT SKIN, LH/RH PYLONS WAS EVALUATED WITH EXCESSIVE DAMAGE PER CRJ-900 SRM 53-00-00-101-001-A01 AND UPPER/LOWER BONDING PLATES AT AFT SKIN WERE REPLACOct 6, 2025 · N294PQ · Cndair CL6002D24 · Nacelle/Pylon, Plate/SkinSDR REXA2026052800832Stringer Splice · corrodedCORROSION ON STGR 21RH BTW FS394.00 TO FS 409.00 AT MAIN AVIONICS COMPARTMENT STGR 21RH BTW FS394.00 TO FS 409.00 AT MAIN AVIONICS COMPARTMENT WAS REPAIRED AND SFECU 2, COVER, RACK AND GS (GS484, GS454, GS464) WERE REMOVED/INSTALLED OPS CHECK GOOD PER EA CRJ95Oct 5, 2025 · N294PQ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2026052800820Retainer · crackedWEAR ON LOWER SEAL RETAINER OF CENTER BAGGAGE-BAY DOOR; CRACKS ON LOWER SEAL RETAINER OF FWD BAGGAGE-BAY DOOR; AND BENTS ON LOWER PLATE OF CENTER AND FWD BAGGAGE-BAY DOOR. LOWER SEAL RETAINER OF CENTER BAGGAGE-BAY DOOR AND LOWER PLATE OF CENTER AND FWD BAGGAGEOct 5, 2025 · N294PQ · Cndair CL6002D24 · Cargo/Baggage DoorsSDR REXA2026052800815Intercostal · corroded"CORROSION ON INTERCOSTAL (3E/A) BTW FS 364 TO FS 369 STGR 26L TO STGR 25R CORROSION ON INTERCOSTAL (3E/A) BTW FS 364 TO FS 369 STGR 26L TO STGR 25R WAS REMOVED PER CRJ 900 SRM 51-21-06-001-001-A01 AND EVALUATED INTERCOSTALS (2EA'S) BTW FS 364 TO FS 369 STOct 5, 2025 · N294PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026052800814Bolt · stuckA STUCK BOLT WAS DETECTED IN THE AILERON LUG T/E ALSO DAMAGE TO BOTH LUG 2 AND 3. A STUCK BOLT WAS REMOVED PER CRJ 900 SRM 51-40-11-001-001-A01 AND DAMAGE TO BOTH LUG 2 AND 3 WERE REPAIRED PER REO 690-57-51-482 REV. -AOct 3, 2025 · N294PQ · Cndair CL6002D24 · AileronsSDR REXA2026052800839Web · crackedCRACK ON ELECTRICAL BAY FLOOR WEB RIGHT SIDE (BELOW ADG SUPPORT DOUBLER) FS193.00 REPAIR ON ELECTRICAL BAY FLOOR WEB RIGHT SIDE (BELOW ADG SUPPORT DOUBLER) FS193.00 WAS PERFORMED PER CRJ900 SRM 53-11-43-201-001-A01Oct 2, 2025 · N294PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026052800828Floor Support · crackedCRACK ON FLOOR SUPPORT RBL 12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENT FLOOR STRUCTURE BELOW WL79.50). CRACK ON FLOOR SUPPORT RBL 12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENTOct 2, 2025 · N294PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026052800813Support · crackedCRACK ON JB6 SUPPORT AT FWD EQUIPMENT COMPARTMENT. JB6 SUPPORT AT FWD EQUIPMENT COMPARTMENT/JUNCTION BOX 6 (JB-6) WERE REMOVED AND INSTALLED PER CRJ 900 SRM 51-42-06-001-001-A01, AMM 24-04-15-000-801-A01 AND AMM 24-04-15-400-801-A01. JB6 SUPPORT (P/N: CC670-5Oct 2, 2025 · N294PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026052800826Support Plate · corroded"CORROSION ON HYDRAULIC SUPPORT PLATES(2E/A) ALSO CORROSION ON SEVERAL WASHERS AT 40 RBL/LBL IN THE WHEEL WELL AREA. CORROSION ON HYDRAULIC SUPPORT PLATES(2E/A AT 40 RBL/LBL IN THE WHEEL WELL AREA WAS REMOVED AND EVALUATED IN LH SUPPORT ORIGINAL THICKNESS IS: Oct 1, 2025 · N294PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026052800825Structure · crackedCRACK AT OVERWING EMERGENCY EXIT DOOR RH AFT TOP SECTION (AROUND BASE OF DOOR PROXIMITY SENSOR STRIKER). EMERGENCY EXIT DOOR RH AFT TOP SECTION (AROUND BASE OF DOOR PROXIMITY SENSOR STRIKER) WAS REPAIRED PER REO 670-52-21-103 REV. --Sep 30, 2025 · N294PQ · Cndair CL6002D24 · Emergency ExitsSDR REXA2026052800824Structure · crackedCRACK AT OVERWING EMERGENCY EXIT DOOR RH FWD TOP SECTION (AROUND BASE OF DOOR PROXIMITY SENSOR STRIKER). EMERGENCY EXIT DOOR RH FWD TOP SECTION (AROUND BASE OF DOOR PROXIMITY SENSOR STRIKER) WAS REPAIRED REO 670-52-21-103 REV. --Sep 30, 2025 · N294PQ · Cndair CL6002D24 · Emergency ExitsSDR REXA2026052800812Drag Angle · crackedCRACK ON RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 61.56% STRG DATUM TO 67.5% REAR SPAR DATUM REPAIR ON CRACK ON RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 61.56% STRG DATUM TO 67.5% REAR SPAR DATUM WAS PERFORMED PESep 30, 2025 · N294PQ · Cndair CL6002D24 · Fuselage, Stabilizer Attach FittingsSDR REXA2026052800811Striker · crackedCRACK AT OVERWING EMERGENCY EXIT DOOR LH FWD TOP SECTION (AROUND BASE OF DOOR PROXIMITY SENSOR STRIKER). EMERGENCY EXIT DOOR LH FWD TOP SECTION (AROUND BASE OF DOOR PROXIMITY SENSOR STRIKER) WAS REPAIRED PER REO 670-52-21-103 REV -.Sep 30, 2025 · N294PQ · Cndair CL6002D24 · Emergency ExitsSDR REXA2026052800810Door · crackedCRACK AT OVERWING EMERGENCY EXIT DOOR LH AFT TOP SECTION (AROUND BASE OF DOOR PROXIMITY SENSOR STRIKER). EMERGENCY EXIT DOOR LH AFT TOP SECTION (AROUND BASE OF DOOR PROXIMITY SENSOR STRIKER) WAS REPAIRED PER REO 670-52-21-103 REV. --Sep 30, 2025 · N294PQ · Cndair CL6002D24 · Emergency ExitsSDR REXA2026052800822Support Angle · crackedCRACKED SUPPORT ANGLE OF WING RH SIDE, SUPPORT ANGLE OF ACCESS PANEL 642AZ. SUPPORT ANGLE OF WING RH SIDE, SUPPORT ANGLE OF ACCESS PANEL 642AZ WAS REPLACED PER CRJ 900 SRM 51-42-21-001-001-A01Sep 26, 2025 · N294PQ · Cndair CL6002D24 · Wing Miscellaneous StructureSDR REXA2025013100108Unknown · odorDURING FLIGHT AFTER SETTING TO POWER ODD ODOR BEGAN COMING OUT OF AIR VENT. NO VISIBLE SMOKE AND SCENT OF THE SMELL WAS THROUGHOUT AIRPLANE. SCENT DISSAPATED AFTER A FEW MINUTES. CREW REPORTED PLASTIC ODOR IN AIRCRAFT, C/W FIM 21-22-00 AND TS# 002736-R1, NOJan 28, 2025 · N294PQ · Cndair CL6002D24 · Air Distribution SystemSDR REXA2022120602680Web · crackedPAX DOOR AFT WEB IS CRACKED AT (2) STEP LOCATIONS. REPAIRED IAW REO 690-52-11-798 REV-.Dec 2, 2022 · N294PQ · Cndair CL6002D24 · Fuselage Main, StructureSDR REXA2022120602679Channel · crackedAFT CARGO DOOR OPENING UPPER SUPPORT C CHANNEL IS CRACKED. REPLACED IAW CRJ 900 SRMS 51-42-06-001-001-A01, 51-41-02-001-001-A01, 51-42-13-001-001-A01, AND 51-25-21-001-001-A01.Dec 2, 2022 · N294PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2022120602678Striker · corrodedSERVICE DOOR LOWER SEAL STRIKER CORRODED AT ALL SCREW HOLES. REPLACED IAW CRJ 900 SRMS 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.Dec 2, 2022 · N294PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2022120602677Bulkhead Web · corrodedFS 280.00 LH AFT LOWER WEB IS CORRODED. REPLACED IAW CRJ 900 SRM 53-11-10-201-004-A01.Dec 1, 2022 · N294PQ · Cndair CL6002D24 · Fuselage Main, BulkheadSDR REXA2022120202668Web · corrodedFS 280.00 RH AFT LOWER WEB IS CORRODED. REPLACED IAW CRJ 900 SRM 53-11-10-201-004-A01.Dec 1, 2022 · N294PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2022120602676Panel · chafedPANEL 584LB IS CHAFED. REQUIRES EVAL. BLENDED CHAFE IAW SRM 51-12-00-001-001-A01. FOUND TO BE OUT OF ALLOWABLE LIMITS IAW SRM 57-52-01-101-001-A01. REPAIRED PANEL 584LB IAW EO CL-600-2D24-57-LO7275.Nov 21, 2022 · N294PQ · Cndair CL6002D24 · Wing, Control SurfacesSDR REXA2022120102651Seat Track · corrodedTHE FWD FLOOR SEAT TRACK AT RBL 9 IS HEAVILY CORRODED AT APPROX. FS 349-364 AND REQUIRES REPLACEMENT. NSTALLED NEW SERVICEABLE SEAT TRACK (PN:SH670-32159-1) IAW CRJ 900 AMM 53-00-49-400-801-A12Nov 18, 2022 · N294PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2022120102629Floor Support · corrodedRH FLOOR SUPPORT CORRODED AT BS 280. REPLACED THE FLOOR SUPPORT BETWEEN BS 280 - 319 IAW SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01 & 51-42-21-001-001-A01.Nov 16, 2022 · N294PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2022120102632Floorbeam · corrodedFS 280.00 RH CROSS BEAM IS CORRODED. REPLACED RH FS 280 CROSS BEAM PN CC670-34094-2 IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01Nov 14, 2022 · N294PQ · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR REXA2022120102631Angle · corrodedFS 280.00 CROSSBEAM J-ANGLE IS CORRODED. REPLACED FS280 CROSSBEAM J ANGLE IAW SRM 51-42-06-001-001-A01 51-42-21-001-001-A01Nov 14, 2022 · N294PQ · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR REXA2022120102630Drag Angle · crackedVERTICAL STABILIZER, L/H AFT DRAG ANGLE IS CRACKED. REPLACED AFT L/H VERT DRAG ANGLE IAW CRJ-900-SRM-51-42-13-001-001-A01, 51-42-22-001-001-A01 AND 51-42-21-001-001-A01.Nov 13, 2022 · N294PQ · Cndair CL6002D24 · Vertical StabilizerSDR REXA2019060730812Overhead Bin · out of rigFOUND LH FWD EMER DOOR DOES NOT OPEN. RERIGGED OVER HEAD BIN ABOVE LH FWD EMER DOOR IAW 25-23-01 OPS CHECK GOODJun 3, 2019 · N294PQ · Cndair CL6002D24 · Passenger Compartment EquipmentSDR REXA2019041250460Light · missingEMER LIGHT STRIP MISSING 9 A/B. REPLACED EMER LIGHT IAW AMM 33-51-01.Apr 5, 2019 · N294PQ · Cndair CL6002D24 · Emergency LightingSDR REXA2019031300280Angle · corrodedAWR: CORROSION ON ANGLE MOUNTING AND PROTECTOR WED FLOOR AT SERVICE DOOR SILL FS 319 TO FS 349, STR 17R. (TCI: 53-20-315) (CPAX) SUMMARY OF CARD 00127: ANGLE MOUNTING AND PROTECTOR WED FLOOR AT SERVICE DOOR SILL FS 319 TO FS 349, STR 17R WERE REPLACED PER SRM Mar 13, 2019 · N294PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2019031200272Door Sill · corrodedINITIAL INSPECTION: CORROSION ON RH FLOOR SILLS FS 280 TO FS 310. (TCI: 53-20-315) (CPAX) DUE TO SEVERAL CORROSION ON RH FLOOR SILL FS 280 TO FS 310 SILL WAS REPLACED PER SRM 53-00-45-201-001-A01 PAR.6.B, SRM 51-42-10-001-001-A01, SRM 51-42-06-001-001-A01 AND Mar 12, 2019 · N294PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2019031100286Seat Track · corrodedINITIAL INSPECTION. CORROSION AND SCRATCHES ON SIDE SEAT RAIL (RT/LT) FROM 672 TO 722, 743 TO 763, 785 TO 847, 847 TO 907, 907 TO 986 AT PAX CABIN. (SM)(CPAX)(TCI 53-20-318). (CORROSION LEVEL 2) SEAT RAILS (RT/LT) FROM 672 TO 722, 743 TO 763, 785 TO 847, 847 TMar 11, 2019 · N294PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2019031100285Seat Track · corrodedINITIAL INSPECTION. CORROSION AND SCRATCHES ON SIDE SEAT RAIL (LT/RT) FROM 379 TO 483, 483 TO 573, 573 TO 661+14, 661+14 TO 672 AT PAX CABIN. (SM)(CPAX)(TCI 53-20-301). (CORROSION LEVEL 2) SEAT RAIL (LT/RT) FROM 379 TO 483, 483 TO 573, 573 TO 661+14, 661+14 TOMar 11, 2019 · N294PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2019031100284Seat Track · corrodedINITIAL INSPECTION. CORROSION AND SCRATCHES ON FLOOR SEAT RAIL (LBL9, RBL9) FROM 485 TO 581, 581 TO 661+32, 661+32 TO 683 AT PAX CABIN. (SM)(CPAX)(TCI 53-20-318). (CORROSION LEVEL 2) FLOOR SEAT RAIL (LBL9, RBL9) FROM 485 TO 581, 581 TO 661+32, 661+32 TO 683 AMar 11, 2019 · N294PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2019031100283Seat Track · corrodedINITIAL INSPECTION. CORROSION AND SCRATCHES ON FLOOR SEAT RAIL FROM 364 TO 485 (LBL27, LBL9, RBL9) AT PAX CABIN. (CORROSION LEVEL 2) SEAT RAIL FROM 364 TO 485 (LBL27, LBL9, RBL9) WAS REPLACED PER AMM 53-00-49-400-801 (CONF. A12)Mar 11, 2019 · N294PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2019031100278Stringer · corrodedINITIAL INSPECTION: CORROSION ON STRINGER 25R AND 26R FROM FS= 280 TO FS= 330 AT MAIN AVIONICS COMPARTMENT. (E/E) (TCI:53-20-304). STRINGER 25R AND 26R FROM FS= 280 TO FS= 330 WERE REPLACED PER SRM 51-42-06-001-001-A01 AND SRM 51-42-20-001-001-A01 AND EA NO: Mar 11, 2019 · N294PQ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2019031100275Frame · corrodedINITIAL INSPECTION: CORROSION ON FRAME IN STA. FS= 295 BETWEEN STRG 26L TO 25R AT MAIN AVIONIC COMPARTMENT. (E/E)(TCI:53-20-304. FRAME IN STA. FS= 295 WAS REPAIR PER EA NO. : CRJ953-08476 REV IRMar 11, 2019 · N294PQ · Cndair CL6002D24 · Fuselage Main, FrameSDR REXA2019031100274Doubler · corrodedINITIAL INSPECTION: CORROSION ON INTERNAL DOUBLER IN STA. FS= 295 TO FS= 310 BETWEEN STRG 26L TO 26R AT MAIN AVIONICS COMPARTMENT. (E/E)(TCI:53-20-304. COMPLETE: INTERNAL DOUBLER IN STA. FS= 295 TO FS= 310 BETWEEN STRG 26L TO 26R WAS REPAIR PER EA NO. : CRJ95Mar 11, 2019 · N294PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
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