N465AW

Service difficulty reports · 170

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 = 'N465AW' 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 A6WA2013071041057Skin · chafedCHAFED L/E SKIN AT FLA STA 60.005 FOUND TO BE OUT OF LIMITS 040 MATERIAL LOSS ORIG THICK 050" REM MATERIAL 010" MAX ALLOWED 025" IAW REO 601R-57-52-004, REV C. R & R L/E SKIN IAW SRM 51-40-11 & SRM 51-42-13.Jun 26, 2013 · N465AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA2013071041053Structure · corrodedCORROSION FOUND OUT OF LIMITS AT FS 574+10 LBL 9. R & R IAW SRM 53-61-49.Jun 25, 2013 · N465AW · Cndair CL6002B19 · Fuselage Main, StructureSDR A6WA2013071041049Angle · crackedANGLE IS CRACKED. REMOVE UNSERVICEABLE ANGLES REPLACED WITH NEW IAW REO 601R-53-41-059, REV B.Jun 25, 2013 · N465AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA20134M1060Bracket · crackedBRAKE PRESSURE TRANSDUCER BRACKET IN RT WHEEL WELL IS CRACKED. R & R RT BRAKE PRESSURE TRANSDUCER BRACKET, PN 601R75262-157 IAW SRM 51-42-06.Jun 23, 2013 · N465AW · Cndair CL6002B19 · Landing Gear SystemSDR A6WA20121025201Wire Harness · defectiveWHEN GEAR SELECTED TO DOWN NLG DOORS WERE OPENING AND CLOSING RAPIDLY LONGER THAN NORMAL TIME FOR GEAR TO INDICATE DOWN AND LOCKED. INTEROGATED PSEU, FOUND SENSOR S35 FAULT-NGD LK2 REF 237682/2 FOR MEL. REPLACED NLG DOWNLOCK TO PROX SENSOR HARNESS ASSY PER AOct 18, 2012 · N465AW · Cndair CL6002B19 · Landing Gear System WiringSDR A6WA20120926102Wire Harness · faultyANTISKID OUTBOARD CAUTION MESSAGE AT 30KTS. ABORTED TAKEOFF. BTMS MAX READING 3, 3, 3, 3. REMOVED AND REPLACED LEFT OUTBAORD ANTISKID HARNESS.Sep 23, 2012 · N465AW · Cndair CL6002B19 · Landing Gear System WiringSDR A6WA20124C101Warning System · false activationANTISKID CAUTION AT 75KTS, ABORTED TAKEOFF. BTMS MAX READINGS 2, 5, 5,7. HIGH ENERGY STOP INSPECTION NOT REQUIRED PER MXC. WHEN THROTTLES AT IDLE MESSAGE CLEARED AND RECEIVED MOMENTARY CONFIG SPOILERS WARNING. NO WARNING PRESENT NOW.Sep 23, 2012 · N465AW · Cndair CL6002B19 · Brake Anti-Skid SectionSDR A6WA201140740Unknown · odorBURING ODOR NOTED AROUND ROWS 6-7. ALL OVERHEAD LIGHT ARE OFF. NO BURNING ODOR NOTED AROUND ROW 6-7. ACFT OK FOR SERVICE IAW AMM 25-20.Aug 8, 2011 · N465AW · Cndair CL6002B19 · Air Distribution SystemSDR A6WA201140753Sill · corrodedCORROSION ON LT CARGO FLOOR SILL BY CARGO DOOR. REMOVED, FABRICATED, AND INSTALLED NEW LT CARGO FLOOR SILL.Aug 5, 2011 · N465AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201140688Riser · crackedPAX DOOR FWD STEP RISER CRACKED. REPAIRED PAX DOOR, FWD STEP RISER AT 2ND STEP IAW REO 601R-52-11-702, REV E ZONE 2.Aug 3, 2011 · N465AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201140761Bracket · crackedHYD LINE BRACKET IN RT WHEEL WELL CRACKED. R & R HYD LINE BRACKET ON RT WHEEL WELL IAW SRM 51-42-06.Jul 31, 2011 · N465AW · Cndair CL6002B19 · Fuselage, Equipment Attach FittingsSDR A6WA201140685Seat Track · corrodedSEAT TRACKS AT LBL 9 & RBL 9 AT FS 539+112 IN CARGO BAY ARE CORRODED TABLE R & R SEAT TRACKS.Jul 31, 2011 · N465AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201140684Fitting · chafedLT AIRLERON FLUTTER DAMPER SHEAR LINK ATTACH POINT ON AILERON IS CHAFED ON OTBD SIDE. REPAIRED DAMAGE IAW REO 601R-57-61-367 DAMAGE DEPTH .060.Jul 31, 2011 · N465AW · Cndair CL6002B19 · AileronsSDR A6WA201140757Heat Shield · looseAPU EXHAUST AFT HEAT SHIELD HAS LOOSE FASTENERS AND 2 EA PULLED THRU FASTENERS. REPAIRED APU AFT EXHAUST HEAT SHIELD IAW REO 601R-49-81-051.Jul 30, 2011 · N465AW · Cndair CL6002B19 · APU Exhaust SystemSDR A6WA201140755Fitting · crackedBOTH TUB FITTING CRACKED AT 460 AND RBL9. REMOVED UNSERVICEABLE FITTING AND INSTALLED SERVICEABLE FITTING IAW SRM 51-42-21.Jul 29, 2011 · N465AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA201140754Fitting · crackedFS 484, LBL 9 HAS A CRACKED BAT TUB FITTING IN AFT RADIUS. REMOVED UNSERVICEABLE FITTING AND INSTALLED SERVICEABLE FITTING IAW SRM 51-42-21.Jul 29, 2011 · N465AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA2011072940763Skin · chafedRT MLG DOOR CHAFED 2EA PLACES. REPAIRED IAW REO`S 601R-52-82-102 & 601R-52-82-034.Jul 29, 2011 · N465AW · Cndair CL6002B19 · Landing Gear DoorsSDR A6WA201140686Drag Angle · crackedPAX DOOR AFT DRAG ANGLE CRACKED. REMOVED CRACKED AFT DRAG ANGLE SECTION THEN INSTALLED NEW SERVICEABLE SECTION IAW REO 601R-52-11-513, REV A.Jul 29, 2011 · N465AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA2011406687Mount Bracket · crackedPAX DOOR ASSIST MOTOR MOUNTING BRACKET CRACKED. REMOVED CRACKED POWER ASSIST MOTOR SUPPORT ANGLE, THEN INSTALLED NEW SERVICEABLE SUPPORT ANGLE, IAW SRM 51-40-11, 51-42-06.Jul 28, 2011 · N465AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201140622Attach Fitting · crackedFS 484, CLIP CRACKED AT RBL 36. REMOVED UNSERVICEABLE CLIP AND REPLACED WITH SERVICEABLE CLIP IAW REO 601R-53-41-059, REV B.Jul 28, 2011 · N465AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA201140759Skin · chafedLT AILERON UPPER L/E SKIN CHAFED. REPAIR CHAFED AREA IAW REO 601R-57-60-013.Jul 27, 2011 · N465AW · Cndair CL6002B19 · AileronsSDR A6WA201140760Skin · chafedRT AILERON UPPER L/E SKIN CHAFED. REPAIR CHAFED AREA IAW REO 601R-57-60-013.Jul 27, 2011 · N465AW · Cndair CL6002B19 · AileronsSDR A6WA2011072640762Handle · crackedPAX DOOR OUTER HANDLE CRACKED. REMOVED CRACKED OUTER HANDLE AND INSTALLED NEW SERVICEABLE OUTER HANDLE IAW EO E08/007/452, REV A.Jul 26, 2011 · N465AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201140758Intercostal · crackedCRACKED INTERCOSTAL ADJACENT TO STRINGER 14 . REMOVED AND REPLACED IAW REO 601R-53-61-100.Jul 26, 2011 · N465AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201140621Panel · crackedLT ENGINE LOWER NOSE COWL THRUST REVERSER PDU ACCESS DOOR VENT LOUVER CRACKED. R & R VENT IAW SRM 51-42-13.Jul 23, 2011 · N465AW · Cndair CL6002B19 · Nacelle/Pylon, Plate/SkinSDR A6WA201140756Seat Track · corrodedPITTING CORROSION ON NR 2 RT SIDE SEAT TRACK. R & R RT NR 2 SIDE SEAT TRACK.Jul 20, 2011 · N465AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201040336Control Lever · failedAFTER T/O, FLAPS FAILED AT 20 DEGREES. COMPLIED WITH QRH. PERFORMED FLAP RESET PROCEDURE IAW SUPP 98-18D, BOX 12. FLAPS RESET. PLACARDED AND PLACED ON MEL. PERFORMED OPS TEST OF FLAPS SYS IAW AMM 27-51-05. ALL CHECKS GOOD, REMOVED FROM MEL. M/C REF 2018Apr 30, 2010 · N465AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200940436Attach Fitting · crackedCRACK FOUND ON FS 280 RBL 9 INBD AND OTBD CLIP. 2 CLIP REPLACED IAW SRM 51-42-20 AND 51-42-06. (K)Jul 21, 2009 · N465AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200940434Bulkhead · damagedSCRATCH REPAIR ON FS 280 PILOT BULKHEAD RBL 9, WL 94.50 IAW REO 601R53-11-1706. (K)Jul 21, 2009 · N465AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA200940439Angle · crackedCRACK ON PILOT BULKHEAD AFT ANGLE FS 280 LBL 9. REPAIRED IAW REO 601R-53-11-138. (K)Jul 21, 2009 · N465AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200940438Bulkhead · crackedCRACK FOUND ON PILOT BULKHEAD FS 280, RBL 9, LWR FLANGE. PILOT BULKHEAD REPAIR IAW REO 601R-53-11-171, REV D. (K)Jul 21, 2009 · N465AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA200940437Bracket · crackedCRACKS FOUND ON BRACKETS AT FS 280.00, LBL 9 INBD AND OTBD. BRACKET AT FS 280.00, LBL9 REPLACED IAW SRM 51-42-06 AND 51-42-20. (K)Jul 21, 2009 · N465AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200940441Angle · damagedCRACK FOUND ON PILOT BULKHEAD FS 280, LBL 9 LWR FLANGE (CRACK LENGTH .750). REPAIR ON PILOT BULKHEAD AT FS 280, LBL 9 LWR FLANGE CARRIED OUT IAW REO 601R-53-11-171. (K)Jul 20, 2009 · N465AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200940440Threshold · corrodedSERVICE DOOR THRESHOLD PLATE FOUND CORRODED OUT OF LIMIT. SERVICE DOOR THRESHOLD PLATE REPLACED IAW SRM 51-41-02. (K)Jul 17, 2009 · N465AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200940435Support Bracket · crackedRT HYD MANIFOLD SUPPORT BRACKET IN AFT EQUIPMENT COMPT CRACKED (AFT LWR AREA) .20 INCH LONG RT HYD MANIFOLD SUPPORT BRACKET REPLACED IAW REO 601R-53-62-031, REV A. (K)Jul 14, 2009 · N465AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200940442Pressure Blkhd · crackedAFT PRESSURE BULKHEAD CRACKED AT LINTEL FITTING LOCATION. REPAIRED IAW REO 601R-53-61-1230. (K)Jul 14, 2009 · N465AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA200940115Acm · seizedREPORTS NR 1 PACK SMELLS HOT IN AUTO AND MANUAL IN FLIGHT AND ON THE GROUND AND DUCT TEMP UNCONTROLLABLE. FOUND CONNECTOR PLUGS S3HG AND P9HG BROKEN, PLACED NR 1 PACK ON MEL AND PLACARDED. FOUND ACM SEIZED REMOVED AND REPLACED ACM IAW AMM 21-00. OPS CHECKMar 9, 2009 · N465AW · Cndair CL6002B19 · Air Conditioning System WiringSDR A6WA200940061Handle · malfunctionedAFTER GEAR RETRACTION, GEAR STAYED IN DOWN POSITION, ASSOCIATED MESSAGES WERE INBD ANTISKID INOP AND PARK BRAKE SOV CAUTION MESSAGES. AFTER CYCLING GEAR, GEAR RETRACTED AND CYCLED NORMALLY. REMOVED AND REPLACED LANDING GEAR HANDLE IAW AMM 32-31-01. OPS CHECFeb 6, 2009 · N465AW · Cndair CL6002B19 · Landing Gear SelectorSDR A6WA200840580Flap System · malfunctionedFLAPS FAILED AT 20 DEGREES WITH FLAPS FAIL CAUTION AFTER TAKEOFF. LANDED AT FLAPS 20 AFTER COMPLYING WITH QRH. COMPLIED WITH AWAC SUPP 98-018B RESET, FLAPS RESET OK. RESET.Aug 21, 2008 · N465AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200840515Flap System · failedFLAPS FAILED AT 30 DEGREES ON APPROACH, COMPLIED WITH QRH LANDED IN BUF. COMPLIED WITH RESET PROCEDURE IAW AWAC SUPPLEMENT 98-018B STEPS 1.3 AND 1.4 FLAPS SYSTEMS RESET OK. (A)Jun 15, 2008 · N465AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200840337Target · looseLT MLG DID NOT RETREAT AFTER TAKEOFF GEAR DISAGREE MSG C/W QRH RETURN TO LGA AT WS 39800 LBS. FOUND LT UPLOCK TARGET LOOSE AND OUT OF ADJUSTMENT. ADJUSTED TARGET FOR LT MLG UPLOCK. REF AMM 32-32-05. OPS TEST OF LANDING GEAR EXTENTION AND RETRACTION SYSTEM Apr 14, 2008 · N465AW · Cndair CL6002B19 · Landing Gear Position and WarningSDR A6WA200740559Control Unit · faultedINFLIGHT RECEIVED SPOILERON FAULT YELLOW CAUTION MESSAGE AND IB AND OB GROUND SPOILER FAULT STATUS MESSAGES. COMPLIED WITH QRH (FERRY TO PHL). INTERROGATED SECU NR 1 AND SECU NR 2 FAULT LOG FOUND CODE 13 (SECU 1 MODULE A) REMOVED AND REPLACED SECU NR 1 IAW 2Oct 5, 2007 · N465AW · Cndair CL6002B19 · Drag Control SystemSDR A6WA200740459Yoke · looseUNUSUAL NOISE HEARD WHEN FIRST OFFICER YOKE TURNED. MORE NOTICEABLE WHEN TURNED RIGHT. ALSO NOTED THROUGH FLOOR ON CAPTAINS SIDE. RETORQUED FIRST OFFICERS YOKE REF SB CRJ-SL-27-045 REV A AND M 27-11-01. OPERATIONAL CHECK GOOD. (M)Aug 11, 2007 · N465AW · Cndair CL6002B19 · Control Column SectionSDR A6WA200740441Floorbeam · crackedFOUND RIGHT FS 621 FLOOR SUPPORT ANGLE CRACKED. (M) MAINTENANCE REPAIRED IAW REO 601R-53-61-117. (M)Aug 3, 2007 · N465AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200740440Floorbeam · crackedFOUND LEFT FS 621 FLOOR SUPPORT ANGLE CRACKED. (M) MAINTENANCE REPAIRED IAW REO 601R-53-61-117. (M)Aug 3, 2007 · N465AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200740428Skin · corrodedLT WING PLANK LOWER ACCESS HOLE NR 2 510AB HAS MINOR CORROSION IN NON-CRITICAL AREAS APPROX .005 DEEP AND 5 INCHES LONG. (K) MAINTENANCE REPAIRED IAW REO 601R-57-21-030. (M)Jul 28, 2007 · N465AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200740427Skin · corrodedLT WING LOWER PLANK ACCESS HOLE NR 1 540BB HAS MINOR CORROSION IN NON-CRITICAL AREAS APPROX .003 INCH DEEP AND 5 INCH LONG IN (2) PLACES. (K) MAINTENANCE REPAIRED IAW REO 601R-57-21-030. (M)Jul 28, 2007 · N465AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200740426Skin · corrodedRT WING LOWER PLANK ACCESS HOLE NR 1 640BB HAS MINO CORROSION IN NON-CRITICAL AREAS APPPROX .003 DEEP AND 2.5 INCH LONG IN (2) PLACES. (K) MAINTENANCE REPAIRED IAW BSC REO 601R-57-21-030 REV F. (M)Jul 28, 2007 · N465AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200740425Skin · gougedRT WING IB FLAP LOWER SKIN GOUGED/DENTED APPROX 3 INCHES LONG X 3 INCHES WIDE X .205 INCH DEEP, ADJACENT TO RIB AT WS 74.8, APPROX 8 INCHES AFT OF LEADING EDGE OF FLAP. (K) MAINTENANCE REPAIRED FLAP LOWER SKIN IAW BSC EO 601R-57-12572. (M)Jul 28, 2007 · N465AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA200740420Bracket · crackedHYDRAULIC PRESSURE BRACKET IS CRACKED APPROX .1 INCH LONG IN RT MLG WHEEL WELL CEILING. (K) MAINTENANCE REMOVED AND REPLACED HAT CHANNEL P/N 601R75262-157 IAW CRJ 200 SRM 51-42-06. (M)Jul 27, 2007 · N465AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
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