N445AW

Service difficulty reports · 154

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 = 'N445AW' 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 A6WA201240692Floor Support · corrodedFLOOR SUPPORT CORRODED FOUND AROUND SCREW HOLES ON TOP OF CAP ON LBL 27 BETWEEN FS 574 & FS 621. R & R WITH SERVICEABLE FLOOR SUPPORT CAP IAW REO 601R-53-61-3778.Jun 26, 2012 · N445AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201240699Retainer · crackedPANEL 422BT, AFT DIVIDER PANEL RETAINER CRACKED. REMOVED UNSERVICEABLE AFT DIVIDER ON PANEL 422BT AND REPLACED WITH SERVICEABLE DIVIDER 601R37003-180 IAW SRM 51-42-06.Jun 24, 2012 · N445AW · Cndair CL6002B19 · Nacelle/Pylon, Main FrameSDR A6WA201240698Trunnion · damagedLEFT LOWER AFT, LOWER FLANGE OF MLG TRUNNION FITTING HAS ONE OVERSIZE HOLE. REPAIRED HOLE ON LT LOWER MLG TRUNNION FLANG IAW REO 601R-57-21-1699, REV.Jun 24, 2012 · N445AW · Cndair CL6002B19 · Wing, Landing Gear Attach FittingsSDR A6WA201240700Panel · damagedPANEL NR422 DB DIVIDER PANEL KNIFE EDGED. REMOVED UNSERVICEABLE DIVIDERS AND REPLACED WITH SERVICEABLE IAW SRM 51-42-06.Jun 24, 2012 · N445AW · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous StructureSDR A6WA201240703Skin · gougedPAX DOOR CUT OUT FWD SEAL STRIKER AT FS 310.00 IS GOUGED. C/W REO 601R-53-22-033, REV C BY TRIMMING OUT DAMAGE & INSTALLING STRAP DOUBLER.Jun 23, 2012 · N445AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA201240694Handle · crackedCARGO DOOR OUTER HANDLE CRACKED. R & R CARGO DOOR OUTER HANDLE IAW SRM 51-42-21.Jun 22, 2012 · N445AW · Cndair CL6002B19 · Cargo/Baggage DoorsSDR A6WA201240701Stiffener · crackedLEFT JET PIPE FWD STIFFENER AT 3 O`CLOCK POSITION IS CRACKED BEYOND STOP DRILL. REPAIRED LT JET PIPE FWD STIFFENER AT 3 O`CLOCK POSITION IAW CMM 78-11-00, SRS 042.Jun 22, 2012 · N445AW · Cndair CL6002B19 · Engine Collector/Tailpipe/NozzleSDR A6WA201240702Support Bracket · crackedHYS SYSTEM NR 1 ACMP CASE DRAIN FILTER SUPPORT BRACKET CRACKD AND WARPED. R & R BRACKET IAW SRM 51-42-06.May 28, 2012 · N445AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA201240004Adc · malfunctionedIN CRUISE, AT 25,000 FT AND 300 KNTS, ADC 2 FAILED. R & R ADC NR2 IAW AMM 34-13-01, OPS CK AND LEAK CK GOOD AT THIS TIME.Dec 31, 2011 · N445AW · Cndair CL6002B19 · Air Data ComputerSDR A6WA201140981Sensor · malfunctionedAFTER LANDING GEAR UP- RECEIVED ANTI SKID INBD CAUTION MESSAGE, FOLLOWED BY PARKING BRAKE SOV MESSAGE FOLLOWED BY A GEAR DISAGREE WARNING MESSAGE, LT MAIN GEAR INDICATED DOWN AND LOCKED WHILE THE NOSE AND RT MAIN INDICATED UP AND LOCKED. QRH PERFORMED QRH, RENov 17, 2011 · N445AW · Cndair CL6002B19 · Landing Gear Position and WarningSDR A6WA201040938Duct · disconnectedRT 10TH STAGE DUCT WARNING MESSAGE. CLEARED WHEN TURNING OFF RT PACK. INSP AND FOUND DISCONNECTED DUCT BETWEEN PRECOOLER AND HEAT EXCHANGER ON RT PACK. REPLACED SEAT AND CLAMP IAW AMM 21-51-07. OPS CK GOOD.Dec 12, 2010 · N445AW · Cndair CL6002B19 · Pneumatic Distribution SystemSDR A6WA201040755Handle · bindingF/A UNABLE TO OPEN SERVICE DOOR FROM INSIDE OR OUTSIDE. INSPECTED AND CLEANED SERVICE DOOR HANDLE. DOOR OPERATES NORMALLY FROM INSIDE OR OUT.Oct 4, 2010 · N445AW · Cndair CL6002B19 · Service DoorsSDR A6WA201040746Angle · crackedPAX DOOR DRAG ANGLE AFT SECTION CRACKED. REMOVED CRACKED AFT DRAG ANGLE SECTION AND INSTALLED NEW SECTION OF DRAG ANGLE IAW REO 601R-52-11-513, REV A.Aug 13, 2010 · N445AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201040745Handle · crackedPAX DOOR OUTER HANDLE CRACKED. R & R WITH NEW SERVICEABLE OUTER HANDLE IAW AMM 52-11-03.Aug 11, 2010 · N445AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201040736Bulkhead · damagedRT FS280 BULKHEAD HAS A CREASE ON AFT SIDE MEASURING 20" IN LENGTH, CREASE STARTS @ 45" ABOVE FLOOR LEVEL ON INBD SIDE AND PROTRUDES DOWN AND OTBD. REPAIRED RT FS 280 BULKHEAD WEB IAW REO 601R-53-11-1954.Aug 11, 2010 · N445AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA201040584Frame · crackedFOUND RBL 9 CRACKED INBD SIDE FROM LOWEST RIVET TO EDGE OF POST REPAIR BY INCORPORATION OF REO 601R-53-41-260, REV D, 601R-53-41-609, REV B & REO 601R-53-41-1116, REV A TO LT AND RT SIDES, LBL 27 TO RBL.Aug 11, 2010 · N445AW · Cndair CL6002B19 · Fuselage Main, FrameSDR A6WA201040735Bulkhead · chafedRT FS 280 BULKHEAD HAS 2 EA AREAS OF CHAFING ON INBD AFT SIDE. 1 MEASURES 2" LENGTH & 2ND MEASURES 1.5" IN LENGTH AT IS 21" FROM FLOOR. REPAIRED FS280 BULKHEAD @ RBL 11.00 BETWEEN STR 13A & STR 14A IAW REO 601R-53-11-1727.Aug 10, 2010 · N445AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA201040744Angle · crackedRT INBD FLAP HINGE OTBD FAIRING ANGLE ON INBD HINGE CRACKED REF 16 SRM 57-21-55. R & R WITH DUPLICATED PART IAW SRM.Aug 9, 2010 · N445AW · Cndair CL6002B19 · Wing Miscellaneous StructureSDR A6WA201040740Panel · chafedCHAFE ON EDGE AT PANEL 412DB DIVIDERS. R & R PANLE 412DB DIVIDERS.Aug 9, 2010 · N445AW · Cndair CL6002B19 · Nacelle/Pylon, Plate/SkinSDR A6WA201040743Bracket · crackedRT INBD FLAP INBD HINGE MIDDLE INBD FLAP FAIRING BRACKET/ANGLE CRACKED. R & R WITH DUPLICATED PART IAW SRM.Aug 9, 2010 · N445AW · Cndair CL6002B19 · Nacelle/Pylon, Attach FittingsSDR A6WA201040742Channel · chafedLT PYLON PANEL 412BT DIVIDER CHANNELS ARE CHAFED. R & R DIVIDER CHANELS ON PANEL 412BT.Aug 8, 2010 · N445AW · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous StructureSDR A6WA201040741Channel · chafedPANEL 422DB DIVIDERS CHAFED. R & R DIVIDERS ON PANEL 422DB.Aug 8, 2010 · N445AW · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous StructureSDR A6WA201040586Skin · chafedRUDDER L/E SKIN IS CHAFED. REPAIRED DAMAGE ON RUDDER L/E SKINS IAW SRM 55-40-00.Aug 7, 2010 · N445AW · Cndair CL6002B19 · Rudder, Plate/SkinSDR A6WA201040585Fitting · crackedFITTING AT RBL 9 AND FS 641.00 CRACKED FITTING CHANGED IAW SRM 51-42-21.Aug 6, 2010 · N445AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA201040587Angle · crackedRT OBLIQUE ANGLE CRACKED. R & R RT OBLIQUE ANGLE IAW SRM 51-42-06, SRM 51-42-21 AND REV 601R-53-61-422.Aug 6, 2010 · N445AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201040739Attach Fitting · corrodedLT INBD 484.00 CLIP IS CRACKED. R & R ANGLE IAW SRM 51-42-21 AND 51-23-00.Aug 5, 2010 · N445AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA201040738Floorbeam · crackedCLIP AT RBL9 AND FS 280 IS CRACKED. LOCATED ON OTBD SIDE OF RBL9.0. R & R CLIP AT FS280 OTBD SIDE OF RBL9.0 IAW SRM 51-42-21.Aug 4, 2010 · N445AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA201040737Floorbeam · crackedFLOOR ANGLE AT FS 280 IS CRCKED JUST OTBD OF LBL 9.0. REPAIRED FS280 AFT FLOOR SUPPORT ANGLE IAW REO 601R-53-11-138.Aug 4, 2010 · N445AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA201040734Pressure Blkhd · crackedCRACK ON BULKHEAD AT FS202 AT PARKING BRAKE FEED THROUGH REPAIRED CRACKED FS202, BULKHEAD AT BL 23.71 IAW REO 601R-53-11-563.Aug 1, 2010 · N445AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA201040613Rib · crackedLT BATT RIB CRACKED AT WS 53.60, REO 601R-57-51-046 CARRIED OUT.Jul 12, 2010 · N445AW · Cndair CL6002B19 · Wing, Rib/BulkheadSDR A6WA200840578Crossbeam · crackedFS 280.00, LBL 9.0, WL 70.00 CROSS BEAM CRACKED IN THE LOWER RADIUS. FS 280, LBL9, WL 70.00. CROSSBEAM CUTOUT IAW REO 601R-53-11-171, REV D. (K)Aug 8, 2008 · N445AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200840577Crossbeam · crackedFS 280.00, RBL 9.00, WL 70.00, CROSS BEAM IS CRACKED IN THE LOWER RADIUS. CROSSBEAM AT FS 280.00, RBL 9.0, WL 70.00. REPAIRED IAW REO 601R-43-11-171, REV D. (K)Aug 8, 2008 · N445AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200840576Attach Fitting · crackedFS 280, RBL 9.00, WL 71.00 IB CLIP CRACKED. FS 280, RBL 9, WL 71.00 IB CLIP REPLACED IAW CRJ 200, SRM 51-42-06 AND 51-42-20. (K)Aug 8, 2008 · N445AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200840575Support · crackedFS 280.00 LBL 9.0, WL 71.00 IB SUPPORT CLIP IS CRACKED. IB SUPPORT CLIP AT FS 280.00, LBL 9.00, WL 71.00. REPLACED IAW REO 601R-53-11-171, REV D. (K)Aug 8, 2008 · N445AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200840573Support Bracket · crackedRT WHEEL WELL HYDRAULIC SUPPORT BRACKET AT FS 523.60 IS CRACKED. RT WHEEL WELL HYDRAULIC SUPPORT BRACKET AT FS 523.60 IS REPLACED IAW CRJ 200, SRM 51-42-06. (K)Aug 8, 2008 · N445AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200840572Channel · crackedRT ENGINE UPPER CORE COWL AFT U CHANNEL IB SIDE CRACKED. RT ENGINE UPPER CORE COWL AFT U CHANNEL IB SIDE REPAIRED IAW SHORTS CMM 20-12-00. (K)Aug 8, 2008 · N445AW · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous StructureSDR A6WA200840571Support Bracket · crackedLT WHEEL WELL HYDRAULIC SUPPORT BRACKET AT FS 531.75, BTW LBL 18-27 IS CRACKED LENGTH OF CRACK IS 0.350". LT WHEEL WELL HYDRAULIC SUPPORT BRACKET AT FS 531.75 BTW LBL 18-27, IS REPLACED IAW CRJ 200 SRM 51-42-06. (K)Aug 8, 2008 · N445AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200840569Sill · crackedCRACK FOUND ON LOWER SILL OF CARGO DOOR FS 589, LBL 45. ON LOWER SILL OF CARGO DOOR FS 589 LBL45, CRACK IS REPAIRED IAW REO 601R-53-61-433. (K)Aug 6, 2008 · N445AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200840568Sill · crackedCRACK FOUND ON CARGO BAY FLOOR SILL FS 574, LBL 45. ON CARGO BAY FLOOR SILL FS 574, LBL45 CRACK IS REPAIRED IAW REO 601R53-61-1741. (K)Aug 6, 2008 · N445AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200840566Drag Angle · crackedCRACK FOUND IN THE AFT DRAG ANGLE OF THE PAX DOOR STAIR ASSY LENGTH OF CRACK 1.50". DRAG ANGLE OF THE PAX DOOR STAIR ASSY, AFT SIDE, REPAIRED IAW CRJ 200 REO 601R 52-11-513. (K)Aug 6, 2008 · N445AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200840570Intercostal · crackedINTERCOSTAL CLIP FS 484 LBL 27 CRACKED. NEW INTERCOSTAL CLIP INSTALLED FS 484, LBL 27 IAW CRJ 200 SRM 51-42-21. (K)Aug 5, 2008 · N445AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200840565Intercostal · crackedINTERCOSTAL AT FS 484, RBL 36 CRACKED. INTERCOSTAL AT FS 484, RBL 36 REPAIRED IAW CRJ 200, REO 601R-53-41-059 REV A. (K)Aug 5, 2008 · N445AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200840567Support Bracket · crackedRT WHEEL HYDRAULIC SUPPORT BRACKET AT FS 529.98, BTW RBL 18-27 IS CRACKED. CRACK LENGTH IS .250 INCH. NEW RT WHEEL WELL HYDRAULIC SUPPORT BRACKET INSTALLED AT FS 529.98 BTW RBL 18-27 IAW CRJ 200 SRM 51-42-06. (K)Jul 30, 2008 · N445AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200840544Wire Harness · damagedENG NR 1 SHUTDOWN IN FLIGHT, NO ASSOCIATED EICAS MESSAGES ILLUMINATED BEFORE SHUTDOWN. THRUST LEVERS WERE ABOVE IDLE AT APPROXIMATELY 80%. RAN QRH, TRIED TO RELIGHT. ENG RELIT FOR 15-20 SECONDS THEN GOT LOW OIL PRESSURE RED WARNING. DID PRECAUTIONARY SHUTDJul 15, 2008 · N445AW · Cndair CL6002B19 · Turbine Engine System WiringSDR A6WA200740591Coalescer Bag · odorODOR AND HAZE DETECTED IN CABIN, SMOKE TOILET CASS MESSAGE NO VISIBLE SIGN OF SMOKE IN LAV. TURNED OFF RIGHT PACK AND CASS MESSAGE WENT AWAY AS DID HAZE AND ODOR. TROUBLESHOT PER FIM, 79-20-0. REMOVED AND REPLACED COALESCER SOCKS ON LT AND RT SIDE. OPS CHEOct 17, 2007 · N445AW · Cndair CL6002B19 · Humidity Control SystemSDR A6WA200740367Fire Bottle · unknownMAINTENANCE REPORTED RT ENGINE BOTTLE NR 2 PUS-TO DISCHARGE GREEN PUSHBUTTON WOULD NOT ILLUMINATE WHEN TESTED. REMOVED AND REPLACED RT ENGINE FIRE BOTTLE FIRE BOTTLE. OPS CHECK GOOD. (K)Jul 8, 2007 · N445AW · Cndair CL6002B19 · Extinguishing SystemSDR A6WA200640387Recorder · malfunctionedWOW OUTPUT CAUTION IN FLIGHT, AS WELL AS WOW OUTPUT CAUTION PROX SYSTEM FAULT, WOW OUTPUT FAIL. REMOVED AND REPLACED CVR IAW AMM 23-71-01, OPS CHECK GOOD AT THIS TIME PERFORMED TEST OF PSEU IAW AMM. OPS CHECK GOOD. CRV FIXED THE PSEU AND WOW PROBLEM. (K)Nov 16, 2006 · N445AW · Cndair CL6002B19 · Data Recorders (Flight/Maintenance)SDR A6WA200640332Floor Support · crackedFOUND LEFT FS 621 FLOOR SUPPORT ANGLE IS CRACKED. MAINTENANCE CUT AWAY DAMAGED SECTION OF ANGLE. FABRICATED STRAP FROM 7024-73 .090. LOCATED AND DRILLED ANGLE. REPAIR ANGLE AND STRAP IAW BSC REO 601R-53-61-117 STEPS 1/2. COMPLETED REPAIR IAW REO 601R-53-6Aug 21, 2006 · N445AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200640331Floor Support · crackedFOUND RIGHT FS 621 FLOOR SUPPORT ANGLE IS CRACKED. COMPLETED REPAIR IAW BSC REO 601R-53-61-117 STEPS 2-7 BY FINISHING CUTLINES, INSTALLING REPAIR ANGLES AND FASTENERS WET. UP TO LEAK CHECK. LEAK CHECK GOOD IAW CRJ AMM TASK 21-32-00-863-801. (M)Aug 21, 2006 · N445AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200640330Intercostal · crackedFOUND INTERCOSTAL ATTACH FLANGE IS CRACKED .3 INCH AT FS 484, LBL 36, WL 73. CUT AWAY DAMAGED FLANGE FABRICATED REPAIR ANGLE USING 56144-14 PREFORMED ANGLE 2024-T42-063 WET INSTALLED ANGLE AIW REO 601R-53-41-059. (M)Aug 21, 2006 · N445AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
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