N348PQ

Service difficulty reports · 64

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 = 'N348PQ' 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 REXA2026031300237Seal · leakingWHILE AT FL 310 I NOTICED L OIL LOW. BEGAN MONITORING OIL INIDCATIONS. EVENTUALLY RECEIVED A L ENG OIL PRESS WARNING MESSAGE. FOLLOWED CRJ 900 QRH 1-20 AND 1-22 AS DIRECTED. SHUTDOWN LEFT ENGINE IN FLIGHT AS DIRECTED BY QRH. REPLACEED OF LT ENGINE C SUMP INFeb 20, 2026 · N348PQ · Cndair CL6002D24 · Turbine Engine Oil SystemSDR REXA2025082500832Lamp · inoperativeRIGHT SIDE AFT EXTERIOR EMERGENCY LIGHT IS INOP REPLACED LAMP WITH NEW LAMP IAW AMM 33-51-15, OPS CHECK GOOD. P/N OFF/ON 8GH002473-08Aug 21, 2025 · N348PQ · Cndair CL6002D24 · Emergency LightingSDR REXA2026072701189Handle · crackedCRACK ON OUTER HANDLE OF PASSENGER DOOR LATCH MECHANISM OUTER HANDLE OF PASSENGER DOOR LATCH MECHANISM WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01Mar 3, 2025 · N348PQ · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2025031300318Attach Angle · crackedCRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD / AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00) RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD / AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DAMar 3, 2025 · N348PQ · Cndair CL6002D24 · Fuselage, Stabilizer Attach FittingsSDR REXA2025031300316Attach Angle · crackedCRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD / AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). (ET) HFEC INSPECTION WAS PERFORMED. NO CRACKS WERE FOUND ON FWD DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SMar 3, 2025 · N348PQ · Cndair CL6002D24 · Fuselage, Stabilizer Attach FittingsSDR REXA2025031300315Seat Track · corrodedCORROSION ON SEAT TRACK LOCATED BTW FS364.00 TO FS394.00 AND LBL9.00 DUE TO EXCESIVE CORROSION AT SEAT TRACK LOCATED BTW FS364.00 TO FS394.00 AND LBL9.00 FUSELAGE STRUCTURE PASSENGER CABIN WAS REPLACED PER CRJ-900 SRM 53-21-49-101-001-A01 AND CRJ-900 AMM 53Mar 3, 2025 · N348PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2025031300314Floor Support · corrodedCORROSION ON FLOOR SILL LOCATED BTWN FS 280.00/FS 295.00 AND RBL 43 DUE EXCESIVE DAMAGE ON FLOOR SILL LOCATED BTWN FS 280.00/FS 295.00 AND RBL 43 WAS REPAIRED PER CRJ-900 SRM 53-21-43-201-002-A01Mar 3, 2025 · N348PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2025031300313Support Plate · chafed"WEAR ON PLATE SUPPORT OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT LH WING TRAILING EDGE (ROOT WING). PLATE SUPPORT OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT LH WING TRAILING EDGE (ROOT WING) WERE REPLACED PER CRJ900 SRM 51-41-02-001-001-A01 AND SRM 51-42Mar 3, 2025 · N348PQ · Cndair CL6002D24 · Wing Miscellaneous StructureSDR REXA2025031300312Fitting · chafed"WEAR ON FLAP FITTING OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT RH WING TRAILING EDGE (ROOT WING). FLAP FITTING OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT RH WING TRAILING EDGE (ROOT WING) WERE REPLACED PER CRJ900 SRM 51-41-02-001-001-A01 AND SRM 51-42-2Mar 3, 2025 · N348PQ · Cndair CL6002D24 · Trailing Edge FlapsSDR REXA2025031300311Fitting · chafed"WEAR ON FLAP FITTING OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT LH WING TRAILING EDGE (ROOT WING). FLAP FITTING OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT LH WING TRAILING EDGE (ROOT WING) WERE REPLACED PER CRJ900 SRM 51-41-02-001-001-A01 AND SRM 51-42-2Mar 3, 2025 · N348PQ · Cndair CL6002D24 · Trailing Edge FlapsSDR REXA2025031300310Support Plate · chafed"WEAR ON PLATE SUPPORT OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT RH WING TRAILING EDGE (ROOT WING). PLATE SUPPORT OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT RH WING TRAILING EDGE (ROOT WING) WERE REPLACED PER CRJ900 SRM 51-41-02-001-001-A01 AND SRM 51-42Mar 3, 2025 · N348PQ · Cndair CL6002D24 · Wing Miscellaneous StructureSDR REXA2026072701173Hinge · crackedFWD HINGE WAS FOUND CRACKED OF AFT BAGGAGE DOOR STEP PLATE ASSY. FWD HINGE OF AFT BAGGAGE DOOR STEP PLATE ASSY WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01Feb 17, 2025 · N348PQ · Cndair CL6002D24 · Cargo/Baggage DoorsSDR REXA2026072701188Bracket · corrodedCORROSION AT AFT LAVATORY WASTE LEVEL INDICATOR LIGHT SUPPORT OF AFT WASTE TANK (BTW STGR 24RH AND STGR 23RH, FS 927.00). CORROSION AT AFT LAVATORY WASTE LEVEL INDICATOR LIGHT SUPPORT OF AFT WASTE TANK (BTW STGR 24RH AND STGR 23RH, FS 927.00) WAS REMOVED PER CFeb 11, 2025 · N348PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026072701179Hinge · corrodedCORROSION ON BOTH FITTINGS AT ACCESS PANEL 196ER. BOTH FITTINGS AT ACCESS PANEL 196ER WERE REPLACED PER CRJ900 AMM 52-45-01 (CONFIG A01) AND CRJ900 SRM 51-41-02-001-001-A01Feb 11, 2025 · N348PQ · Cndair CL6002D24 · Fuselage, Door HingeSDR REXA2026072701178Hinge · corrodedCORROSION ON BOTH FITTINGS AT ACCESS PANEL 196ER. BOTH FITTINGS AT ACCESS PANEL 196ER WERE REPLACED PER CRJ900 AMM 52-45-01 (CONFIG A01) AND CRJ900 SRM 51-41-02-001-001-A01Feb 11, 2025 · N348PQ · Cndair CL6002D24 · Fuselage, Door HingeSDR REXA2026072701177Hinge · corrodedCORROSION ON BOTH FITTINGS AT ACCESS PANEL 196ER. BOTH FITTINGS AT ACCESS PANEL 196ER WERE REPLACED PER CRJ900 AMM 52-45-01 (CONFIG A01) AND CRJ900 SRM 51-41-02-001-001-A01Feb 11, 2025 · N348PQ · Cndair CL6002D24 · Fuselage, Door HingeSDR REXA2026072701176Access Panel · corrodedCORROSION ON BOTH FITTINGS AT ACCESS PANEL 196ER. BOTH FITTINGS AT ACCESS PANEL 196ER WERE REPLACED PER CRJ900 AMM 52-45-01 (CONFIG A01) AND CRJ900 SRM 51-41-02-001-001-A01Feb 11, 2025 · N348PQ · Cndair CL6002D24 · Service DoorsSDR REXA2025031300308Rib · crackedCRACK ON MACHINED RIB LEADING EDGE SS57.16 AT RIGHT WING. MACHINED RIB LEADING EDGE SS57.16 AT RIGHT WING WAS REPAIRED PER REO 690-57-41-468 REV. --Feb 11, 2025 · N348PQ · Cndair CL6002D24 · Wing, Rib/BulkheadSDR REXA2025031300307Rib · crackedCRACKED WING RIB AT FLS 168.07 AT WING TRAILING EDGE STRUCTURE OF LH WING. CRACKED WING RIB AT FLS 168.07 AT WING TRAILING EDGE STRUCTURE OF LH WING WAS REPAIRED PER REO 690-57-51-408 REV. --Feb 11, 2025 · N348PQ · Cndair CL6002D24 · Wing, Rib/BulkheadSDR REXA2025031300306Rib · crackedCRACKED WING RIB AT FLS 168.07 AT WING TRAILING EDGE STRUCTURE OF RH WING. CRACKED WING RIB AT FLS 168.07 AT WING TRAILING EDGE STRUCTURE OF RH WING WAS REPAIRED PER REO 690-57-51-407 REV. --Feb 11, 2025 · N348PQ · Cndair CL6002D24 · Wing, Rib/BulkheadSDR REXA2025031300305Valve · chafedWEAR ON FLOTATION VALVE ALSO MISSING ITS RUBBER PAD LOCATED AT FS1098.20. FLOTATION VALVE WAS REPLACED PER CRJ-900 AMM 21-32-02-000-801-A01, AMM 21-32-02-400-801-A01 AND RUBBER PAD LOCATED AT FS1098.20 WAS INSTALLED PER CRJ-900 SRM 51-22-00-001-001-A01Feb 11, 2025 · N348PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2025020400118Relay · inoperativeDURING FIRST FLIGHT OF DAY CHECKS, EMERGENCY LIGHTS DID NOT TURN ON. R/R RELAY K198 IAW AMM 33-51-19. OPS CHECK GOOD. A/C OK FOR SVCFeb 2, 2025 · N348PQ · Cndair CL6002D24 · Emergency LightingSDR REXA2022050200309Unknown · inoperativeUNABLE TO OPEN MAIN CABIN DOOR. CLEANED MEETING POINT LATCH ASSY AND VERIFIED GOOD OPERATION OF PASSENGER DOOR IAW CRJ 900 AMM 52-11-00.Apr 23, 2023 · N348PQ · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2022011000101Battery Pack · inoperativeFOUND GALLEY CEILING, PAX DOOR INTERIOR AND EXTERIOR EMERGENCY LIGHTS INOPERATIVE. R & R THE BATTERY PACK AT PS 35 IAW AMM 33-51-17 OPS CHECK GOOD.Jan 3, 2023 · N348PQ · Cndair CL6002D24 · Emergency LightingSDR REXA2021091000728Pivot · corroded"PAX DOOR UPPER AND LOWER HAND RAIL ATTACH POINTS CORRODED. " "BLENDED CORROSION ON UPPER AND LOWER HANDRAIL ATTACH POINTS AND AFTER FURTHER EVALUATION. NO DAMAGE ALLOWED IN AREA PER BOMBARDIER CMM 52-11-00-06. LOCATED AND INSTALLED 4EA NEW POST PIVOSep 1, 2021 · N348PQ · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2021091000704Retainer · corroded"AVI DOOR AFT SEAL RETAINER IS CORRODED. " "REMOVED AND REPLACED SEAL RETAINER IAW CRJ 900 SRM 51-42-06-001- 001-A01. NO DEFECTS NOTED.Aug 31, 2021 · N348PQ · Cndair CL6002D24 · Electrical/Electronic Compartment DoorsSDR REXA2021091000726Lever · cracked"PAX DOOR ICE BREAK VENT LEVER CRACKED. " "REMOVED AND REPLACED ICE BREAK LEVER IAW MHIRJ SNIEO 601R31814 IDENTIFIER 501. OPS CHECK GOOD. ALSO USED SNIEO 601R31703-501 FOR INSTALL. WVAC EMP STAMP Aug 30, 2021 · N348PQ · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2021091000730Lever · damaged"FOUND HANDLE LEVER MOUNT HOLES DAMAGED. " "REMOVED AND REPLACED HANDLE CRJ 900 AMM 52-11-62-400-809-A02 NO DEFECTS NOTED.Aug 29, 2021 · N348PQ · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2021091000713Seat Track · corrodedRIGHT SIDE SEAT TRACK SEGMENT BETWEEN FS 785 TO FS 853.5 IS CORRODED. FABRICATED SEAT TRACKS @ FS 847-847+16 AND 847+16 TO 897 IAW REO 670-53-00-074 & INSTALLED SEAT TRACKS FS 785-897 IAW AMM 53-00-49-400-801-A12.Aug 29, 2021 · N348PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2021091000711Crossbeam · corroded"F.S. 280.00 CROSSBEAM IS CORRODED BETWEEN CROSSBEAM AND J-ANGLE. REMOVED L/H AND R/H CORRODED CROSSBEAM AT FS 280 IAW CRJ SRM 51-40-11-001-001-A01. INSTALLED NEW L/H AND R/H CROSSBEAM AT FS 280 IAW CRJ 900 SRM 51-42-20-001-001-A01 AND 51-42-22-001-001-A01 Aug 29, 2021 · N348PQ · Cndair CL6002D24 · Fuselage Main, StructureSDR REXA2021091000729Stringer · corroded"STRINGER 25R IS CORRODED BETWEEN FS 310 AND FS 319.70. " "REMOVED CORROSION ON STR 25R BETWEEN FS 310 AND 319.70 IAW CRJ900 SRM 51-21-06-001-001-A01. REMOVED 0.042"", ORIGINAL MATERIAL THICKNESS IS 0.063"", REMAINING THICKNESS IS 0.021"". OUT OF LIMIAug 28, 2021 · N348PQ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2021091000722Angle · corroded"PAX DOR UPPER SILL ANGLE IS CORRODED AT F.S. 319.70 BELOW THE FLANGE. " "BLENDED CAP SEAL FOUND OUT OF LIMITS REPLACED IAW SRM 51-42-06-001- 001-A01 AND 51-42-13-001-001-A01, 51-42-11-001-001-A01. FOUND SEALANT TO BE CURED AND PULLED FOD. WVACAug 28, 2021 · N348PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2021091000721Frame · corroded"RIB AT F.S. 295.00 IS CORRODED ON BOTH FWD & AFT SIDES BETWEEN STR STR 25R STR 25L. " "REPAIRED DAMAGED (CORRODED) AREA OF RIB AT FS 295 FWD AND AFT SIDES BETWEEN STR 25R AND STR 25L IAW CRJ 900 SRM 53-00-Aug 28, 2021 · N348PQ · Cndair CL6002D24 · Fuselage Main, FrameSDR REXA2021091000717Intercostal · corroded"INTERCOSTAL FWD OF AVIONICS DOOR BETWEEN FS 364-FS 349 AT STRINGER 27L IS CORRODED. " "REMOVED AND REPLACED INTERCOSTAL AT 27L BETWEEN F.S. 349 AND F.S. 364 IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06-00Aug 28, 2021 · N348PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2021091000712Bulkhead Web · corroded"F.S. 280.00 BULKHEAD IS CORRODED ON AFT SIDE AT RH FLOOR SILL. REMOVED/FABRICATED/INSTALLED RH FS 280 WEB IAW SRM 53-11-10-201-004-A01.Aug 28, 2021 · N348PQ · Cndair CL6002D24 · Fuselage Main, BulkheadSDR REXA2021090900710Floorbeam · corroded"FS 280.00 CROSSBEAM 5 ANGLE IS CORRODED. " "REMOVED AND REPLACED 280 J ANGLE PN CC690-34095-1 IAW SRM 51-42-21-001-001-A01, 51-42-06-001-001-A01. CORRECT PN CC670-34095-1. WVAC EMP STAMP # 703 MTC. Aug 28, 2021 · N348PQ · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR REXA2021090900708Skin · chafedPANEL 684EB HAS EXCESSIVE CHAFFING. LOCATED AND DRILLED NEW SERVICEABLE PANEL 684EB P/N CC670-14177-2 IAW CRJ 900 SRM 51-40-11-001-001-A01 REF M-212 FOR INSTALL. MASTER PANEL BOOK PAGE 110 OF 124.Aug 28, 2021 · N348PQ · Cndair CL6002D24 · Wing, Plate/SkinSDR REXA2021091000725Stringer · corroded" STR 26L BTWN F.S. 310 AND F.S. 319 IS CORRODED THROUGH (100% HOLE) AROUND HYD LINE STAND OFFS. " " REMOVED, LOCATED, DRILLED AND INSTALLED A NEW SERVICEABLE STRINGER @ FS 280 - FS 333 26L IAW CRJ900 SRM 51-40-11-Aug 26, 2021 · N348PQ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2021091000720Skin · corroded"A/C SKIN IS CORRODED IN MAIN AVIONICS BAY BETWEEN F.S. 280.00 & F.S. 295.00 AND BETWEEN STR 25R & STR 26R. " "REPAIRED A/C SKIN IN AVI BAY BETWEEN F.S 280-295 BETWEEN STR 25R & 26R IAW ENDEAVOR AIR, EA# CRJ 953-11928 REV IR DAug 26, 2021 · N348PQ · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR REXA2021091000714Seat Track · corroded"LEFT SIDE SEAT TRACK SEGMENT BETWEEN F.S. 744 TO F.S. 761 IS CORRODED. " "REMOVED, FABRICATED AND INSTALLED NEW L/H SIDE SEAT TRACK BETWEEN FS 744 TO FS 761 IAW CRJ 900 AMM 53-00-49-100-801-A12, SRM 53-41-49-101- 001-A02, AND 51-40-11-001-001-A01, 51-24-3Aug 19, 2021 · N348PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2021091000718Intercostal · corroded"INTERCOSTAL FWD OF AVIONICS DOOR BETWEEN FS 364-FS 349 AT STRINGER 27R IS CORRODED. " "INSTALL INTERCOSTAL AND GUSSET ON 27R BETWEEN FS 349 AND FS 364 IAW CRJ900 SRM 51-40-11-001-001-A01, SRM 51-42-2Aug 19, 2021 · N348PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2021091000716Seat Track · corroded"LEFT SIDE SEAT TRACK SEGMENT BETWEEN F.S. 672 - F.S. 720 IS CORRODED. " "REMOVED & REPLACED LH SEAT TRACK SEGMENT COMMOM TO FS 672-FS 720 IAW CRJ 900 AMM TASK 53-00-49-000-801-A12 AND 53-00-49-400-801-A12. Aug 16, 2021 · N348PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2021091000715Seat Track · corroded"RIGHT SIDE SEAT TRACK SEGMENT BETWEEN F.S. 744 TO F.S. 761 IS CORRODED. " "REMOVED FABRICATED AND INSTALLED SEAT TRACK IAW BOMBARDIER GRFO 670-53-00-074 AND AMM 53-00-49-400-801-A12Aug 11, 2021 · N348PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2021091000727Retainer · corroded"AVIONICS DOOR AFT RH SEAL RETAINER IS CORRODED " "REMOVED AND REPLACED WITH A NEW PART P/N CC670-38675-3$. AVIONICS DOOR SEAL RETAINER AFT R/H IAW CRJ SRM 51-42-06-001-001-A01. WVAC EMP STAMP # 738 MTC "Aug 11, 2021 · N348PQ · Cndair CL6002D24 · Electrical/Electronic Compartment DoorsSDR REXA2021091000724Seat Track · corroded"CABIN SEAT TRACK AT LBL 9.0 IS CORRODED FS 374 TO 440 " "INSTALLED NEW TRACK LBL9 PN SH670-32249-3 IAW CRJ900 AMM 53-00-49-400- 801-A12 WVAC EMP STAMP # 769 MTC "Aug 11, 2021 · N348PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2021091000723Seat Track · corroded"CABIN SEAT TRACK AT RBL9.0 IS CORRODED FS 349 TO 388 TO INCLUDE FWD LAV MOUNTS. " "INSTALLED NEW SEAT TRACK AT RBL 9.0 PN SH670-32159-1 IAW CRJ900 AMM 53-00-49-400-801-A12. STA 349-485 RBL 9 WVAC EMP Aug 11, 2021 · N348PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2021091000719Seat Track · gouged"R/H OUTBD SEAT TRACK GOUGED IN 2 PLACES AT F.S. 549 & 565, RBL9. " "REMOVED SEAT TRACK IAW CRJ900 SRM 53-00-49-000-801-A12 AND INSTALLED NEW P/N SH690-33407-1 IAW CRJ900 SRM 53-00-49-400-801-A12, STA485-581 485-581 RBL9 WVAC EMP STAMP # 769 MTC Aug 11, 2021 · N348PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2021090900706Drag Angle · crackedL/H VERTICAL STABILIZER AFT DRAG ANGLE IS CRACKED. REMOVED LH AFT DRAG ANGLE IAW CRJ 900 SRM 51-42-21-001-001-A01, 51-42-13-001-001-A01 AND 51-42-22-001-001-A01. LOCATED, DRILLED AND INSTALLED LH AFT DRAG ANGLE IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-13-0Aug 10, 2021 · N348PQ · Cndair CL6002D24 · Vertical StabilizerSDR REXA2021090900705Drag Angle · cracked"R/H VERTICAL STABILIZER AFT DRAG ANGLE IS CRACKED. REMOVED R/H AFT DRAG ANGLE IAW CRJ 900 SRM 51-42-21-001-001-A01, 51-42-13-001-001-A01 AND 51-42-22-001-001-A01. LOCATED, DRILLED AND INSTALLED RH AFT DRAG ANGLE IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-1Aug 10, 2021 · N348PQ · Cndair CL6002D24 · Vertical StabilizerSDR REXA2020909100709Plate · chafed"LH LOWER BLOW-OUT DOOR REINFORCING PLATE FOR LATCH CHAFED " "INSTALLED NEW SERVICEABLE REINFORCING PLATE FOR LH LOWER BLOW- OUT DOOR LATCH IAW CRJ-900 SRM 51-42-06-001-001-A01 AND 51-40-11-001- 001-A01. WVAC EMP # 56392 Aug 9, 2021 · N348PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
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