N146PQ

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 = 'N146PQ' 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 REXA2026080401459Access Panel · corrodedCORROSION ON MLG WHEEL WELL ACCESS PANELS NO. 542AZ, 542BZ, 642AZ AND 642BZ CORROSION ON MLG WHEEL WELL ACCESS PANELS NO. 542BZ, 642AZ AND 642BZ WAS REMOVED PER SRM 51-21-06-001-001-A01 AND WERE FOUND WITHIN LIMITS PER SRM 53-00-00-101-001-A01. NEW MLG WHEEL WMay 21, 2026 · N146PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026080401436Channel · chafedOUT OF SCOPE: WEAR ON BEAM OF AFT BAGGAGE-BAY CARGO DOOR STRUCTURE (INTERFERENCE WITH AFT/FWD BALANCE SPRING CABLE) BEAM OF AFT BAGGAGE-BAY CARGO DOOR STRUCTURE (INTERFERENCE WITH AFT/FWD BALANCE SPRING CABLE) WAS BLENDED OUT PER CRJ900 SRM 51-12-00-001-001-A0May 21, 2026 · N146PQ · Cndair CL6002D24 · Cargo/Baggage DoorsSDR REXA2026080401476Plate · worn"INITIAL INSPECTION': WEAR ON FLAP FITTING AND PLATE SUPPORT OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT RH/LH WING TRAILING EDGE. FLAP FITTING AND PLATE SUPPORT OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT RH/LH WING TRAILING EDGE WERE REPLACED PER CRJ900 SRM May 20, 2026 · N146PQ · Cndair CL6002D24 · Trailing Edge FlapsSDR REXA2026080401475Plate · worn"INITIAL INSPECTION': WEAR ON FLAP FITTING AND PLATE SUPPORT OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT RH/LH WING TRAILING EDGE. FLAP FITTING AND PLATE SUPPORT OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT RH/LH WING TRAILING EDGE WERE REPLACED PER CRJ900 SRM May 20, 2026 · N146PQ · Cndair CL6002D24 · Trailing Edge FlapsSDR REXA2026080401474Fitting · worn"INITIAL INSPECTION': WEAR ON FLAP FITTING AND PLATE SUPPORT OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT RH/LH WING TRAILING EDGE. FLAP FITTING AND PLATE SUPPORT OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT RH/LH WING TRAILING EDGE WERE REPLACED PER CRJ900 SRM May 20, 2026 · N146PQ · Cndair CL6002D24 · Trailing Edge FlapsSDR REXA2026080401473Fitting · worn"INITIAL INSPECTION': WEAR ON FLAP FITTING AND PLATE SUPPORT OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT RH/LH WING TRAILING EDGE. FLAP FITTING AND PLATE SUPPORT OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT RH/LH WING TRAILING EDGE WERE REPLACED PER CRJ900 SRM May 20, 2026 · N146PQ · Cndair CL6002D24 · Trailing Edge FlapsSDR REXA2026080401428Skin · chafedWEAR PREVIOUS REPAIR OF OUTER SKIN UPPER EDGE AT AFT BAGGAGE DOOR OUTER SKIN UPPER EDGE AT AFT BAGGAGE DOOR PER EA CRJ952-15060 REV.IRMay 20, 2026 · N146PQ · Cndair CL6002D24 · Cargo/Baggage DoorsSDR REXA2026080401422Door Sill · crackedCRACK ON AFT RT DOOR LANDING AT FS 188.00 (LATCH CUT OUT OF ACCESS DOOR 212AR). AFT RH DOOR LANDING AT FS 188.00 (LATCH CUT OUT OF ACCESS DOOR 212AR) WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01, CRJ-900 SRM 51-42-21-001-001-A01 AND CRJ-900 SRM 51-42-10-0May 20, 2026 · N146PQ · Cndair CL6002D24 · Fuselage Main, StructureSDR REXA2022061500355Light · inoperativeOVERWING EMERGENCY LIGHT UNDER AFT EMER. EXIT DOOR IS NOT WORKING - DS 102 POSITION. R/R OVERWING EMERGENCY LIGHT UNDER AFT EMER. EXIT DOOR IAW AMM 33-51-1 5 OPS CHECK GOOD PN ON/OFF - 2LA006954-00Jun 4, 2023 · N146PQ · Cndair CL6002D24 · Emergency LightingSDR REXA2022041800294Floorbeam · corrodedL/H F.S. 280.00 CROSSBEAM IS CORRODED BETWEEN LBL 12.00 AND B.L. 0.00. REMOVED AND REPLACED BEAM I.A.W. BOMBARDIER CRJ 900 SRM 51-40-11-001-001-A01, 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.Apr 18, 2023 · N146PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2022041800291Angle · corroded"J"" ANGLE @ FS280 IS CORRODED INSTALLED FS 280 J ANGLE PN CC670-34095-3S IAW CRJ900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01."Apr 17, 2023 · N146PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2022041300288Floorbeam · corrodedR/H FS 280 CROSSBEAM IS CORRODED BETWEEN RBL 12 ABD BL 0. REMOVED RH FS 280 CROSSBEAM 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 LOCATED AND DRILLED NEW SERVICEABLE R/H FS 280 CROSSBEAM P/N CC670Apr 12, 2023 · N146PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2022040500277Angle · crackedSTIFFENING ANGLE ON FS280 BULKHEAD AT LBL 26 IS CRACKED. REMOVED, LOCATED, DRILLED, AND INSTALLED NEW SERVICEABLE STIFFENING ANGLE PN: CC670-34117-5 AT LBL 26 FS 280 IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.Apr 2, 2023 · N146PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2019102361555Strap · corroded"AWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON "CORROSION LEVEL 2, ON FRAME STRAP IN FS= 319 BETWEEN STGR 17RH TO 18RH AND 41RBL AT PAX CABIN FWD WET. THE FRAME STRAP WAS REPLACED PER CRJ-900 SRM 51-42-20-001-001-A01 Oct 16, 2019 · N146PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2019102341558Seal · torn"PART RACK: TORN SEAL AT FORWARD FACE OF THE AFT CORE-COWL RH/LH ENGINE. (MOT1)(MOT2) " "SEAL AT FORWARD FACE OF THE AFT CORE-COWL RH/LH ENGINE. (MOT1)(MOT2) WERE REPAIRED PER CRJ-900 SRM 54-13-00-201-0Oct 14, 2019 · N146PQ · Cndair CL6002D24 · Nacelle/Pylon, Main FrameSDR REXA2019102341537Frame · corroded"[ IN REFERENCE NRC 00131 & 00134 ]: INITIAL INSPECTION: CORROSION ON FRAME FS= 333 BETWEEN STRG 25LH TO 25RH AT MAIN AVIONICS COMPARTMENT. (E/E) [ TASK 900-53-140-300 APPENDIX A ] TCI: 100-09, 100-09E4, 100-09E5 Oct 14, 2019 · N146PQ · Cndair CL6002D24 · Fuselage Main, FrameSDR REXA201910231559Bracket · cracked"PARTS RACK: CRACK IN INNER BRACKET AT RH AFT CORE COWL. (MOT2) " "SUMMARY INNER BRACKET AT RH AFT CORE COWL. WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 "Oct 13, 2019 · N146PQ · Cndair CL6002D24 · Nacelle/Pylon, Main FrameSDR REXA2019102331546Support Plate · 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 PLATEOct 13, 2019 · N146PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2019102331545Support Plate · corroded"AWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON PROTECTION PLATE SUPPORT IN STA. FS= 339 BETWEEN 41RBL TO 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) " "SUMMARY: CORROSION LEVEL 2. PROTECTION PLATOct 13, 2019 · N146PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2019102301557Bolt · missing"INITIAL INSPECTION: MISSING FITTING ATTACHED TO FWD RIGHT RAIL AND MISSING BOLTS OF HIS FITTING AT FWD BAGGAGE BAY. (CCD) " "NEW FITTING FWD RIGHT IN RAILAT FWD BAGGAGE BAY WILL BE INSTALLED UNDER CARD 900-53-900-125 STEP 29. Oct 12, 2019 · N146PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2019102301556Helicoil · missing"INITIAL INSPECTION: MISSING HELICOIL INSERT IN FITTING ATTACHED TO AFT RIGHT RAIL AND MISSING BOLT OF HIS FITTING AT FWD BAGGAGE BAY. (CCD) " "NEW FITTING AFT RIGHT RAIL AT FWD BAGGAGE BAY WILL BE INSTALLED UNDER CARD 900-53-900-125 STEP 29. Oct 12, 2019 · N146PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2019102301554Scuff Plate · worn"INITIAL INSPECTION: WAVINESS SCUFF PLATES AT FWD BAGGAGE BAY CUT-OUT.(CCD) "SCUFF PLATES AT FWD BAGGAGE BAY CUT-OUT WERE REMOVED, PER EXCESSIVE DAMAGE WILL BE REPLACED AND NEW SCUFF PLATES AT FWD BAGGAGE BAY CUTOUT WILL BE INSTALLED UNDER CARD 900-53-900-125Oct 12, 2019 · N146PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2019102301553Counterbalance · worn"INITIAL INSPECTION : WEAR ON COUNTER BALANCE ARM BOTH SIDE AT FWD CARGO DOOR (SM) ""WEAR WAS BLEND OUT ON COUNTER BALANCE ARMS, BOTH SIDE OF THE FWD CARGO DOOR PER CRJ-900 SRM 52-35-09-201-001-A01 , Oct 12, 2019 · N146PQ · Cndair CL6002D24 · Cargo/Baggage DoorsSDR REXA2019102301552Fairing · worn"INITIAL INSPECTION: WEAR ON LOWER FAIRING AFT RH PYLON (MOT 2). " "SUMMARY: LOWER FAIRING AFT RH PYLON WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 "Oct 10, 2019 · N146PQ · Cndair CL6002D24 · Nacelle/Pylon Miscellaneous StructureSDR REXA2019102391550Angle · corroded"AWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON MID CAP ANGLE [ JUMPER/PROX-SENSOR/CONNECTOR-WIRING ANGLE ] IN STA. FS= 310 TO FS= 349 AND 41LBL AT MAIN ENTRANCE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) Oct 9, 2019 · N146PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2019102391549Angle · corroded"AWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON KICKPLATE ANGLE IN STA. FS= 310 TO FS= 349 AND 41LBL AT MAIN ENTRANCE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) " "CORROSION LEVEL 2. KICKPLATE ANGLE IN STA. Oct 9, 2019 · N146PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2019102391538Striker · worn"INITIAL INSPECTION: WEAR ON FWD/AFT SEAL STRIKER AT FWD BAGGAGE BAY DOOR CUT-OUT. (CCD) " "WEAR ON AFT SEAL STRIKER AT FWD BAGGAGE BAY DOOR CUT-OUT WAS BLENDED OUT PER CRJ/900 SRM 51-12-00-001-001-A01. AROct 9, 2019 · N146PQ · Cndair CL6002D24 · Cargo/Baggage DoorsSDR REXA2019102391526Step · corroded"AWR: OUT OF LIMITS: [ DURING EVALUATION/MEASURE OF LH FWD/AFT SILL STEP PLATE RELATED WITH NRC 00324 ]: CORROSION ON SILL STEP PLATE AT LH FWD/AFT EMERGENCY EXIT SURROUNDING STRUCTURE. (CPAX)TCI: 53-20-258 " "CORROSION LEVEL 2. SILL STEP PLATE AT LH FWOct 9, 2019 · N146PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2019102381548Striker · 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. FS=Oct 8, 2019 · N146PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2019102381542Support 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) " "CORROSION LEVEL 1. ON SUPPORT ANGLE IN STAOct 8, 2019 · N146PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2019102381536Frame · corroded"[ IN REFERENCE NRC 00131 & 00134 ]: INITIAL INSPECTION: CORROSION ON FRAME FS= 319 BETWEEN STRG 25LH TO 25RH AT MAIN AVIONICS COMPARTMENT. (E/E) [ TASK 900-53-140-300 APPENDIX A ] TCI: 100-09, 100-09E4, 100-09E5 Oct 8, 2019 · N146PQ · Cndair CL6002D24 · Fuselage Main, FrameSDR REXA2019102381535Stringer · corroded"[ IN REFERENCE NRC 00131 & 00134 ]: INITIAL INSPECTION: CORROSION ON STRINGER 26LH 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 Oct 8, 2019 · N146PQ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2019102381534Stringer · corroded"[ IN REFERENCE NRC 00131 & 00134 ]: INITIAL INSPECTION: CORROSION ON STRINGER 26LH IN STA. FS= 295 TO FS= 319 AT MAIN AVIONICS COMPARTMENT. (E/E) [ TASK 900-53-140-300 APPENDIX A ] TCI: 100-09, 100-09E4, 100-09E5 Oct 8, 2019 · N146PQ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2019102381533Stringer · corroded"[ IN REFERENCE NRC 00131 & 00134 ]: INITIAL INSPECTION: CORROSION ON STRINGER 25LH IN STA. FS= 295 TO FS= 327 AT MAIN AVIONICS COMPARTMENT. (E/E) [ TASK 900-53-140-300 APPENDIX A ] TCI: 100-09, 100-09E4, 100-09E5 Oct 8, 2019 · N146PQ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2019102381532Stringer · corroded"[ IN REFERENCE NRC 00131 & 00134 ]: INITIAL INSPECTION: CORROSION ON STRINGER 27 IN STA. FS= 310 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 27 IN STA. FS= 31Oct 8, 2019 · N146PQ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2019101381531Stringer · corroded"[ IN REFERENCE NRC 00131 & 00134 ]: INITIAL INSPECTION: CORROSION ON STRINGER 24RH IN STA. FS= 295 TO FS= 310 AT MAIN AVIONICS COMPARTMENT. (E/E) [ TASK 900-53-140-300 APPENDIX A ] TCI: 100-09, 100-09E4, 100-09E5 Oct 8, 2019 · N146PQ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2019102381530Stringer · corroded"[ IN REFERENCE NRC 00131 & 00134 ]: INITIAL INSPECTION: CORROSION ON STRINGER 26RH 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 Oct 8, 2019 · N146PQ · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2019102381529Support Angle · corroded"[ IN REFERENCE NRC 00131 & 00134 ]: INITIAL INSPECTION: CORROSION ON FLOOR SUPPORT IN STA. FS= 280 BETWEEN STRG 26LH TO 26RH AT MAIN AVIONICS COMPARTMENT. (E/E) [ TASK 900-53-140-300 APPENDIX A ] TCI: 100-09, 100-09E4, 100-09E5 Oct 8, 2019 · N146PQ · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR REXA2019102381525Support · damaged"AWR; PER MTC REQUEST: [ DURING REMOTION OF MLG WHEEL BINS RELATED WITH TASK 900-27-900-112 STEP 5 ]: ELONGATED HOLE IN RH FAIRING SUPPORT IN STA. FS= 797 TO FS= 807 AND 35RBL AT RH MLG WHEEL WELL. (FYT) " "SUMMARY: FAIRING SUPPORT IN STA. FS= 797 TOct 8, 2019 · N146PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2019102371544Support Angle · 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) " "CORROSION LEVEL 2, ROTECTION PLATE SUPPORT Oct 7, 2019 · N146PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2019102371543Support Angle · 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) " "CORROSION LEVEL 2,PROTECTION PLATE SUPPORT Oct 7, 2019 · N146PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2019102371541Support 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) " "CORROSION LEVEL 1. CORROSION ON PROTECTION Oct 7, 2019 · N146PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2019102371540Support 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) " "CORROSION LEVEL 2. PROTECTION PLATE SUPPORTOct 7, 2019 · N146PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2019102371528Channel · corroded"INITIAL INSPECTION: CORROSION ON ANGLE IMPACT CHANNEL AT FWD LAVATORY SERVICE PANEL. (FUS) (TCI: 100-16) " "SUMMARY: ANGLE IMPACT CHANNEL AT FWD LAVATORY SERVICE PANEL WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01. PAOct 7, 2019 · N146PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2019102371524Support · cracked"AWR; PER MTC REQUEST: [ DURING REMOTION OF MLG WHEEL BINS RELATED WITH TASK 900-27-900-112 STEP 5 ]: CRACK IN LH FAIRING SUPPORT DIAPHRAGM IN STA. FS= 797 TO FS= 807 AND 35LBL AT LH MLG WHEEL WELL. (FYT) " "FAIRING SUPPORT DIAPHRAGM LH IN STA. FS= 79Oct 7, 2019 · N146PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2019102351539Support Plate · 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) " "AWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECOct 5, 2019 · N146PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2019102341551Cover · cracked"AWR; HIDDEN CRACK:[DURING REMOTION OF FASTENERS, RELATED WITH NRC 0465 ] CRACK IN AFT UPPER CORNER AT MAIN PASSENGER DOOR. (L1) (PTAS) " "SUMMARY: AFTER CORNER WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 PAR. 6. (C). AND SRM 51-42-13-001-001-A01Oct 4, 2019 · N146PQ · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2019102331547Angle · corroded"AWR; [ TASK R53520 STEP 7 ]; INITIAL INSPECTION: CORROSION ON SUPORT MOUNTING ANGLE IN STA. FS= 319 TO FS= 349 AND 41RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX) " "SUMMARY: SUPORT MOUNTING ANGLE ON RBL 44 BTOct 3, 2019 · N146PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2019102391527Skin · crackedINITIAL INSPECTION: CRACK IN RECEPTACLE PLATE AT FUSELAGE. (FUS) "SUMMARY: RECEPTACLE PLATE AT FUSELAGE WAS REPLACE PER CRJ/900 SRM 51-42-20-001-001-A01 PAR.6A "Sep 30, 2019 · N146PQ · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR REXA2019070101054Pin · out of positionON ARRIVAL TO BNA MAIN CABIN DOOR WOULD NOT OPEN. IT FEELS JAMMED CLOSED. FOUND PAX STAIRS STOR PIN LANYARD JAMMED IN DOOR. INSPECTED DOOR AND STOWED PINS. FOUND NO APPARANT DAMAGE. OPS CHK GOOD IAW AMM 52-11-00. OK FOR SVC.Jul 1, 2019 · N146PQ · Cndair CL6002D24 · Passenger/Crew Doors
Back to N146PQ