N296PQ

Service difficulty reports · 115

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 = 'N296PQ' 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 REXA2026101601894Seal Depressor · bentWEAR AND BENT FWD SEAL DEPRESSOR OF PASSENGER DOOR ON STGR7L AND STGR14L AT PAX CABIN. SEAL DEPRESSOR OF PASSENGER DOOR ON STGR7L AND STGR14L AT PAX CABIN WERE REPLACED PER SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.Aug 20, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Main, StructureSDR REXA2026101601893Support · crackedCRACK ON SUPPORTS FAIRING 194AB (2EAS) BTWN BS 797 AND LBL-RBL 40 APPROX AT WHEEL WELL AREA SUPPORTS FAIRING 194AB (2EA) BTWN BS 797 AND LBL-RBL=40 APPROX AT WHEEL WELL AREA WERE REPLACED IAW SRM 51-41-02-001-001-A01.Aug 20, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026101601892Diaphragm · crackedCRACK ON SUPPORTS FAIRING 194AB (2EA) BTW BS 797, LBL - RBL 40 APPROX AT WHEEL WELL AREA SUPPORTS FAIRING 194AB (2EA) BTW BS 797 & LBL-RBL 40 APPROX AT WHEEL WELL AREA WERE REPLACED IAW SRM 51-41-02-001-001-A01.Aug 20, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026101601891Strap · corrodedCORROSION ON SETTLEMENT SUPPORTS STRAPS (2 EA LT & RT) AREA OF FAIRINGS ON STRAP FS847.00 + 32.00. SETTLEMENT SUPPORTS STRAPS (2 EA LT & RT) AREA OF FAIRINGS ON STRAP FS847.00 + 32.00. WERE REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND SRM 51-42-13-001-001-Aug 20, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026102201996Stringer · corrodedCORROSION ON STGR 21 RH BTW FS421.00 AND FS437.00 AT CENTER FUSELAGE STGR 21 RH AT CENTER FUSELAGE REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01Aug 18, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2026101601931Support · crackedCRACKED ON SUPPORT, JB 6 MODULE IN THE FWD EQUIPMENT COMPARTMENT. THE SUPPORT WAS REPLACED IAW SRM 51-42-06-001-001-A01.Aug 18, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026101601898Retainer · corrodedCORROSION ON SEAL RETAINER AT MAIN AVIONICS COMPARTMENT DOOR. SEAL RETAINER AT MAIN AVIONICS COMPARTMENT DOOR WERE REMPLACED IAW SRM 51-42-06-001-001-A01.Aug 18, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026101601897Retainer · corrodedCORROSION ON SEAL RETAINER AT MAIN AVIONICS COMPARTMENT DOOR. SEAL RETAINER AT MAIN AVIONICS COMPARTMENT DOOR WERE REPLACED IAW SRM 51-42-06-001-001-A01.Aug 18, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026101601890Support · crackedCRACKED FLOOR WEB RIGHT SIDE AT ELECTRICAL BAY (BELOW ADG SUPPORT DOUBLER) FS 193. FLOOR WEB RIGHT SIDE AT ELECTRICAL BAY (BELOW ADG SUPPORT DOUBLER) FS193.00. WAS REPAIRED IAW SRM 53-11-43-201-001-A01.Aug 18, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026101601889Roller Guide · chafedWEAR AND BEND ON LOWER AFT DOOR TRACK ANGLE AT AFT BAGGAGE BAY DOOR AREA LOWER AFT DOOR TRACK ANGLE AT AFT BAGGAGE BAY DOOR AREA WAS BLEND OUT PER SRM 51-12-00-001 -001-A01 AND CONFORM PER SRM 51-24-21-001-001-A01 AND WAS EVALUATED OUT LIMITS PER CRJ900 53-61Aug 18, 2026 · N296PQ · Cndair CL6002D24 · Cargo/Baggage DoorsSDR REXA2024102801017Light · inoperativeEXTERIOR EMERGENCY LIGHT NEAR THE SERVICE DOOR IS BURNT OUT. R/R EMERGENCY LIGHT IAW CMM 33-52-07. OPS CHECK GOOD. P/N ON/OFF: 2LA004305-76.Oct 19, 2024 · N296PQ · Cndair CL6002D24 · Emergency LightingSDR REXA2022063000428Panel · crackedPERM REPAIR PAX DOOR UPPER AFT SIDE PNL REPAIRED IAW BOMBARDIER REO 670-52-11-848 REV -A DATED 2017-01-05.Jun 29, 2023 · N296PQ · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2022062700401Channel · chafedRH LOWER TRANS COWLING DOOR COAMING OUTER EDGE CHAFFED. REPAIRED R/H LOWER TRANS COWL DOOR COAMING IAW REO 670-54-21-1207 REV A DATED 2015-08-27.Jun 26, 2023 · N296PQ · Cndair CL6002D24 · Engine Thrust ReverserSDR REXA2022062700398Angle · corrodedPAX DOOR UPPER MID SILL ANGLE IS CORRODED. REMOVED PAX DOOR UPPER MID SILL ANGLE IAW CRJ 900 SRM 51-41-02-001-001-A01. INSTALLED NEW SERVICEABLE PAX DOOR MID SILL ANGLE CAP P/N SH670-31825-9 IAW CRJ-900 SRM 51-41-02-001-001-A01.Jun 26, 2023 · N296PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2022063000425Fitting · chafedRH FLAP STUB FAIRING (172DR) HAS A FLAP FITTING (PN 601R10371-2) CHAFFED THRU. REQUIRES REPLACEMENT. UPON FURTHER INVESTIGATION, FOUND BOTH R/H FLAP STUB FAIRING FLAP FITTING AND ATTACHING PLATE TO BE EXCESSIVELY CHAFED. REMOVED R/H FLAP STUB FAIRING FLAP FITTJun 25, 2023 · N296PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2022062600393Coaming · chafedL/H ENGINE LOWER TRANS COWLING FWD EDGE IS CHAFED. CHAFE IS APPROX 2 INCHES LONG 0.375 WIDE AND 0.030 DEEP. REMOVED L/H LOWER TRANS COWL ACCESS DOOR COAMING, LATCHES AND ANGLE IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, 51-42-02-001-001-A01 IJun 25, 2023 · N296PQ · Cndair CL6002D24 · Engine Thrust ReverserSDR REXA2022071700504Web · corrodedL/H FS 280 LOWER WEB IS CORRODED AT LBL !2 BEHIND CORROSION CAP AND CROSSBEAM REPAIRED IAW CRJ-900 SRM 53-11-10-201-004-A01.Jun 22, 2023 · N296PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2022071700503Floorbeam · corrodedFS280 CROSSBEAM IS CORRODED FROM BL0 TO RBL12 INSTALLED NEW SERVICEABLE R/H F.S. 280 CROSSBEAM P/N CC670-34094JP-2S IAW CRJ-900 SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01 AND 51-42-22-001-001-A01.Jun 22, 2023 · N296PQ · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR REXA2022071700502Web · corrodedR/H FS 280 LOWER WEB IS CORRODED BETWEEN RBL 36.00 TO RBL 45.00 REPAIRED IAW CRJ-900 SRM 53-11-10-201-004-A01.Jun 22, 2023 · N296PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2022071700501Angle · corroded" F.S. 280 FWD J ANGLE IS CORRODED. INSTALLED NEW SERVICEABLE F.S. 280 ""J"" ANGLE P/N CC670-34095-1 IAW CRJ-900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. "Jun 22, 2023 · N296PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2022061600361Retainer · chafedCENTER CARGO DOOR LOWER OUTER SEAL RETAINER CHAFFED AND BENT (AS MARKED) REMOVED DAMAGED SEAL RETAINER FROM CENTER CARGO DOOR AND INSTALLED NEW P/N LE670-39644-1 IAW CRJ-900 SRM 51-42-06-001-001-A01Jun 6, 2023 · N296PQ · Cndair CL6002D24 · Cargo/Baggage DoorsSDR REXA2022110102346Bulb · inoperativeRH OVER WING EMERGENCY LIGHT BURNT OUT AND GLASS COVER BROKEN R/R'D BULB AND GLASS COVER IAW CRJ 900 AMM 33-51-15 OPC NOMAL BULB P/N OFF/ON 8GH005123-06 COVER P/N OFF/ON 9EL408042-00Oct 27, 2022 · N296PQ · Cndair CL6002D24 · Emergency LightingSDR REXA2020012850104Skin · worn"INITIAL INSPECTION: WEAR ON EXTERNAL SKIN AROUND OF OUTER HANDLE AT GALLEY SERVICE DOOR (PTAS). ""DIAPHARAMG (INTERCOSTAL) (3 EA) AND INNER SKIN (WEB) WERE REMOVED/INSTALLED PER CRJ-900 SRM 51-42-06-001-001-A01 PAJan 25, 2020 · N296PQ · Cndair CL6002D24 · Galley DoorsSDR REXA2020012840105Seal · worn"INITIAL INSPECTION: WEAR ON PRESSURE SEAL RETAINERS IN ALL AROUND ATFORWARD BAGGAGE BAY DOOR. (CCD) "SUMMARY: PRESSURE SEAL RETAINERS IN ALL AROUND AT FORWARD BAGGAGE BAY DOOR WERE REPLACED PER. CRJ-900 SRM 51-42-06-001Jan 24, 2020 · N296PQ · Cndair CL6002D24 · Cargo/Baggage DoorsSDR REXA2020012820132Flap Track · corroded"INITIAL INSPECTION: PREVIOUS TOOL MARK ON SKIN (INNER FACE) IN STA. FSL 36.00 FLS TO FSL 42.00 (AD)(BORESCOPE) ""PREVIOUS TOOL MARK ON SKIN (INNER FACE) IN STA. FSL 36.00 FLS TO FSL 42.00 WAS BLENDED OUT PER CRJ900 SRM 51-12-00-Jan 22, 2020 · N296PQ · Cndair CL6002D24 · Trailing Edge FlapsSDR REXA2020012810125Channel · corroded"INITIAL INSPECTION: CRACKED AFT FAIRING PANEL C CHANNEL AT PANNEL NBR196DR (FUS)(TC: 100-19) "AFT FAIRING PANEL C CHANNEL AT PANNEL NBR 196DR WAS REPLACED PER CRJ-900 SRM 51-42-10-001-A01 PAR 9. Jan 21, 2020 · N296PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA202001280111Stringer · corroded"[ IN REFERENCE NRC 00211 ]: INITIAL INSPECTION: CORROSION ON STRINGER26RH IN STA. FS= 337 TO FS= 364 AT MAIN AVIONICS COMPARTMENT. (E/E) [TASK 900-53-140-300 APPENDIX A ] TCI: 100-09, 100-09E4, 100-09E5 "SUMMARY: STRINGER 26RH IN STA. FS= 337 TO FS= 364Jan 20, 2020 · N296PQ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA202001280110Stringer · corroded"[ IN REFERENCE NRC 00211 ]: INITIAL INSPECTION: CORROSION ON STRINGER25RH IN STA. FS= 337 TO FS= 364 AT MAIN AVIONICS COMPARTMENT. (E/E) [TASK 900-53-140-300 APPENDIX A ] TCI: 100-09, 100-09E4, 100-09E5 "CORROSION LEVEL 2, STRINGER 25RH IN STA. FS= 337 Jan 20, 2020 · N296PQ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA202001280109Stringer Splice · corroded"[ IN REFERENCE NRC 00211 ]: INITIAL INSPECTION: CORROSION ON STRINGERSPLICE 26RH AT MAIN AVIONICS COMPARTMENT. (E/E) [ TASK 900-53-140-300APPENDIX A ] TCI: 100-09, 100-09E4, 100-09E5 "SUMMARY: STRINGER SPLICE 26RH AT MAIN AVIONICS COJan 20, 2020 · N296PQ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA202001280108Stringer Splice · corroded"[ IN REFERENCE NRC 00211 ]: INITIAL INSPECTION: CORROSION ON STRINGER SPLICE 24RH AT MAIN AVIONICS COMPARTMENT. (E/E) [ TASK 900-53-140-300 APPENDIX A ] TCI: 100-09, 100-09E4, 100-09E5 ""SUMMARY: SPLICE 24RH STA 333 WAS REPLACED PERJan 20, 2020 · N296PQ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA202001280106Floorbeam · corroded"INITIAL INSPECTION: CORROSION ON FLOOR PANEL SUPPORT ANGLE OF ACCESS PANEL 221ALF IN STA. FS= 280 BETWEEN 11 LBL/RBL AT COCKPIT. (CPIL) TCI 53-10-219 "SUMMARY: ANGLE, FLOOR PANEL SUPPORT WAS REPLACJan 20, 2020 · N296PQ · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR REXA2020012890107Stringer · corroded"[ IN REFERENCE NRC 00211 ]: INITIAL INSPECTION: CORROSION ON STRINGER26RH IN STA. FS= 280 TO FS= 327 AT MAIN AVIONICS COMPARTMENT. (E/E) [TASK 900-53-140-300 APPENDIX A ] TCI: 100-09, 100-09E4, 100-09E5 ""SUMMARY: STRINGER 26RH IN STA. FS= 280 TO FS= 32Jan 19, 2020 · N296PQ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2020012880124Stringer · corroded"[ IN REFERENCE NRC 00211 ]: INITIAL INSPECTION: CORROSION ON STRINGER25RH IN STA. FS= 280 TO FS= 327 AT MAIN AVIONICS COMPARTMENT. (E/E) [TASK 900-53-140-300 APPENDIX A ] TCI: 100-09, 100-09E4, 100-09E5 ""CORROSION LEVEL 2, STRINGER 25RH STA 280 TO 327Jan 18, 2020 · N296PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2020012870133Stringer Splice · corroded"LATE FINDING: CORROSION ON STRINGER AND SPLICE 21RH IN STA. FS= 333 TO FS= 349 AT MAIN AVIONICS COMPARTMENT. (E/E) (W1) TCI: 53-20-305 ""CORROSION LEVEL 2. STRINGER AND SPLICE 21RH IN STA. FS= 333 TO FS= 349 AT MAIN AVIONICS COMPARTMENT WERE REPLACED PJan 17, 2020 · N296PQ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2020012870122Electrical Box · cracked"INITIAL INSPECTION: CRACK IN BOX AT A/C EXTERNAL POWER RECEPTACLE SURROUND STRUCTURE. (FUS) ""BOX AT A/C EXTERNAL POWER RECEPTACLE SURROUND STRUCTURE WAS REPLACED PER CRJ/900 SRM 51-42-06-001-001-A01, CRJ900 SJan 17, 2020 · N296PQ · Cndair CL6002D24 · Fuselage Main, StructureSDR REXA2020012860129Angle · corroded"AWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON MID CAP ANGLE IN STA. FS= 310 TO FS= 349 AND 41LBL AT MAIN ENTRANCE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) ""CORROSION LEVEL 2. MID CAP ANGLE IN STA. FS=Jan 16, 2020 · N296PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2020012830131Seat Track · corroded"INITIAL INSPECTION: CORROSION ON SIDE SEAT RAILS IN SECTIONS [ FS= 667 TO FS= 720, STGR 15LH/RH ] AND [ FS= 744 TO FS= 761, STGR 15LH/RH ] AT PAX CABIN. (CPAX) (TCI: 53-20-318) ""CORROSION LEVEL 2. SEAT RAILS IN SECTIONS [Jan 13, 2020 · N296PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2020012830130Seat Track · corroded"INITIAL INSPECTION: CORROSION ON FLOOR SEAT RAILS IN SECTIONS [ FS= 677 TO FS= 847+16, 9LBL/RBL ] AND [ FS= 847+16 TO 977, 9LBL/RBL ] AT PAX CABIN. (CPAX) (TCI: 53-20-233) " "CORROSION LEVEL 2. FLOOR SEAT RAILS IN SECTJan 13, 2020 · N296PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2020012830128Seat Track · corroded"AWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON FLOOR SEAT RAIL IN SECTIONS [ FS= 374 TO FS= 485, 9LBL ] AND [ FS= 349 TO FS= 485, 9RBL ] AT PAX CABIN FWD WET AREA. (W1) (CPAX) ""CORROSION LEVEL 2. SEAT RAIL IN SECTIONS [ FSJan 13, 2020 · N296PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2020012830126Floor Support · cracked"AWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CRACK ON LONGITUDUNAL FLOOR BEAM 12LBL IN STA. FS= 279 AT COCKPIT. (CPIL) "LONGITUDUNAL FLOOR BEAM 12LBL IN STA. FS= 279 AT COCKPIT WAS REPAIREDPER CRJ-900 SRM 53-11-43-201-003-A01 Jan 13, 2020 · N296PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2020012830123Bracket · corroded"INITIAL INSPECTION: CORROSION ON LIGHT CLIP SUPPORT ASSY IN STA. FS= 897 BETWEEN STGR 23RH TO 24RH AT AFT LAVATORY SERVICE PANELS. (FUS) (TCI: 100-19) ""LIGHT CLIP SUPPORT ASSY IN STA. FS= 897 BETWEJan 13, 2020 · N296PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2020012800127Door Sill · corroded"AWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON SILLS IN STA. FS= 349 TO FS= 409 BETWEEN 41RBL TO 46RBL AT PAX CABIN FWD WET AREA. (W1) (CPAX) "CORROSION LEVEL 2. SILLS IN STA. FS= 349 TO FSJan 10, 2020 · N296PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2020012810121Striker · corroded"AWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON LOWER STRIKER IN STA. FS= 319 TO FS= 349 AND 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) " "CORROSION LEVEL 2. LOWER STRIKER IN STA. FSJan 10, 2020 · N296PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2020012810119Web · corroded"AWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON PROTECTION PLATE SUPPORT IN STA. FS= 346 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) ""SUMMARY. CORROSION LEVEL 2. PROTECTION PLATE Jan 10, 2020 · N296PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2020012890117Web · corroded"AWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON PROTECTION PLATE SUPPORT IN STA. FS= 329 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) ""SUMMARY. CORROSION LEVEL 2. PROTECTION PLATE Jan 9, 2020 · N296PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2020012890116Support · corroded"AWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON PROTECTION PLATE SUPPORT IN STA. FS= 322 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) "SUMMARY. CORROSION LEVEL 2. PROTECTION PLATE SJan 9, 2020 · N296PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2020012890115Support Angle · corroded"AWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON PROTECTION PLATE SUPPORTS ANGLE IN STA. FS= 346 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) "SUMMARY. CORROSION LEVEL 2. PROTECTION PLATE SJan 9, 2020 · N296PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2020012890114Support Angle · corroded"AWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON PROTECTION PLATE SUPPORTS ANGLE IN STA. FS= 339 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) "SUMMARY. CORROSION LEVEL 2. PROTECTION PLATE SJan 9, 2020 · N296PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2020012890113Support Angle · corroded"AWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON PROTECTION PLATE SUPPORTS ANGLE IN STA. FS= 329 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) ""SUMMARY. CORROSION LEVEL 2. PROTECTION PLATE Jan 9, 2020 · N296PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2020012890112Floorbeam · corroded"AWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON PROTECTION PLATE SUPPORTS ANGLE IN STA. FS= 322 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) "SUMMARY. CORROSION LEVEL 2. PROTECTION PLATE SJan 9, 2020 · N296PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
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