N447AW

Service difficulty reports · 175

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 = 'N447AW' 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 A6WA201441853Door Sill · corrodedPAX DOOR LOWER SILL IS CORRODED AT INBD & OTBD SIDES BETWEEN FS 310 & 349.Aug 9, 2014 · N447AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201441854Seat Track · corrodedFLOOR SEAT RAIL AT LBL 9 IS CORRODED AT FWD END FROM FS 364 TO FS 379.Aug 9, 2014 · N447AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201441852Cleat · corrodedPAX DOOR FWD & AFT CLEATS AT LOWER SILL ARE CORRODED.Aug 9, 2014 · N447AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201441465Light · inoperativeROW 13AC CEILING LIGHT INOPERATIVE. CAN SMELL ELEC BURNING ON GND AT GATE.Apr 29, 2014 · N447AW · Cndair CL6002B19 · Passenger Compartment LightingSDR A6WA201301214004Flap · failedON DEPARTURE, DURING FLAP RETRACTION, FLAPS FAILED AT 11 DEGREES. COMPLIED WITH QRH. LANDED AT DCA. BTMS 7, 4, 3, 3. C/B RESET DID NOT WORK. ATTEMPTED FLAP RESET PER AWAC SUP 98-018E. FLAP FAIL MESSAGE DID NOT EXTINGUISH. REF 235830/4 AND 235831/1 AND /Jan 19, 2013 · N447AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA201301084001Sensor · malfunctionedJUST AFTER TAKEOFF WHILE MOVING FLAP LEVER 20 DEG TO 8 DEG RECEIVED FLAP FAIL CAUTION MSG. COMPLIED WITH QRH. COMPLIED WITH RESET PER AWAC SUP 98-018E. RESET FAILED. REMOVED AND REPLACED SENSORS L3 AND L4 REF AMM 27-51-15. OPS CHECK GOOD. RE-ACTIVATED SDJan 8, 2013 · N447AW · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR A6WA201211204J054Control Unit · malfunctionedFLAPS FAIL AT 41 DEGREES, MISSED APPROACH. COMPLIED WITH QRH, LANDED UNEVENTFUL AT LGA, EMERGENCY DECLARED. PERFORMED FLAP RESET PROCEDURES IAW AWAC SUPP 98-18E BOX 12 FLAPS RESET. REMOVED AND REPLACED FECU. PERFORMED FUNCTIONAL AND OPS CHECK, ALL CHECKED GDec 10, 2012 · N447AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA201240761Tube · dentedRT FLAP CENTER & INBD VANE ACTUATOR TUBES HAVE INDENTATIONS FROM THE ROLLERS. REPAIRED IAW REO 601R-57-52-1544, REV A.Aug 4, 2012 · N447AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201240804Skin · gougedLT LOWER CORE COWL INNER SKIN GOUGED 3 SPOTS, 10 GOUGED LOCATIONS ON LT LOWER CORE COWL INNER SKIN 4 FOUND TO BE WITHIN ALLOWABLE DAMAGE LIMITS AND TO 6 AREAS. REPAIRED IAW REO 601R-71-12-4122.Aug 1, 2012 · N447AW · Cndair CL6002B19 · Nacelle/Pylon, Plate/SkinSDR A6WA201240740Skin · dentedLT LOWER CORE COWL INNER SKIN DENTED IN MULTIPLE SPOTS. 10 DENTS LOCATIONS ON LT LOWER CORE COWL. INNER SKIN WITH FOUR REQUIRED AND 6 FOUND TO BE WITHIN ALLOWABLE DAMAGE REO.Aug 1, 2012 · N447AW · Cndair CL6002B19 · Nacelle/Pylon, Plate/SkinSDR A6WA201240742Skin · gougedGOUGED ON FUSELAGE AT FS 559 FROM CONTACT WITH RT STUB FAIRING COMPLIED WITH REO 601R-53-41-610.Jul 31, 2012 · N447AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA201240748Beam · damagedLT INBD FLAP VANE ACTUATORS SLIDING BEAMS HAVE DAMAGE ON UPPER AND LOWER SURFACES FROM ROLLERS. REPAIRED BY BLENDING IAW REO 601R-57-52-1942.Jul 30, 2012 · N447AW · Cndair CL6002B19 · Wing Main, Frame StructureSDR A6WA201240747Skin · gougedPANEL 445AB HAS NUMEROUS SMALL DENTS AND GOUGES ON INNER SKIN. REPAIR IAW REO 601R-71-12-4124.Jul 30, 2012 · N447AW · Cndair CL6002B19 · Nacelle/Pylon, Plate/SkinSDR A6WA201240746Fitting · crackedFITTING CRACKED OUT APPROX FS 461, RBL 9. REMOVED CRACKED FITTING AT FS 461, RBL 9. INSTALLED NEW SERVICEABLE FITTING PN 600-31068-19.Jul 30, 2012 · N447AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA201240744Floor Support · corrodedCORROSION AT FLOOR SUPPORT STRUCTURE FS 621 & LBL14 NUTPLATE HOLE. REMOVED CORROSION, MEASURED & FOUND IT TO BE WITHIN ALLOWABLE LIMITS, DEPTH .012" WITH .05" LENGTH 0.7" IAW REO 601R-53-61-4600.Jul 29, 2012 · N447AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201240745Floor Support · corrodedCORROSION ON FLOOR SUPPORT STRUCTURE FS 621 & LBL 31 AT NUTPLATE HOLE BLENDED CORROSION ON FLOOR STRUCTURE. FOUND TO BE WITHIN LIMITS IAW REO 601R-53-61-4600.Jul 29, 2012 · N447AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201240737Mount Bracket · crackedSYS 3 BROKEN ACCUMULATOR FWD MOUNTING BRACKET CRACKED. REMOVED UNSERVICEABLE BRACKET AND REPLACED WITH SERVICEABLE BRACKET, PN 601R75250-25, IAW AWC SRM 51-42-06, 51-40-11 AND 51-42-21.Jul 28, 2012 · N447AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA201240749Bulkhead · damagedDOUBLE DRILLED HOLE ON FS 559 BULKHEAD AT RBL 18. DURING INCORPORATION OF GREO 601R-53-41-1116, REV B. CW REO 601R-53-41-1594 BY CUTTING OUT DAMAGED REINFORCING ANGLE STEPPING UP HOLES, AND INSTALLING FREEZE PLUGS AND A FILLER.Jul 27, 2012 · N447AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA201240739Angle · crackedANGLE CRACKED AT APPROX FS 484, RBL 27. REMOVED CRACKED ANGLE AT FS 484, RBL 27, DUPLICATED ANGLE AND INSTALLED ANGLE IAW REO 601R-53-41-059, REV B.Jul 26, 2012 · N447AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201240803Door · chafedLT MLG DOOR L/E CHAFED. LT MLG DOOR L/E PREVIOUS. R & R IAW REO 601R-52-82-016.Jul 25, 2012 · N447AW · Cndair CL6002B19 · Landing Gear DoorsSDR A6WA201240743Floor Support · corrodedCARGO FLOOR SUPPORT LBL 27 HAS CORRODED NUTPLATE HOLES BETWEEN FS 574 AND FS 605. REMOVED UNSERVICEABLE, LBL 27 FLOOR SUPPORT AND INSTALLED SERVICEABLE FLOOR SUPPORT IAW 51-40-11, 51-42-06, 51-24-36. REMOVED UNSERVICEABLE WEB AND INSTALLED SERVICEABLE WEB IAJul 25, 2012 · N447AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201240738Skin · chafedINNER SKIN CHAFED ON BUTTE DOOR 694PB. R & R SKIN IAW SRM 51-42-06, 51-40-11, 51-25-16.Jul 25, 2012 · N447AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA201240741Mount Bracket · crackedPAX DOOR POWER ASSIST MOTOR MOUNT BRACKET CRACKED. R & R PAX DOOR POWER ASSIST MOTOR MOUNT BRACKET IAW SRM 51-42-06 & 51-42-13.Jul 24, 2012 · N447AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA201240762Door · chafedLT MLG DOOR IS CHAFED ON THE INSIDE T/E. REPAIRED LT MLG DOOR CHAFE ON THE INSIDE T/E IAW REO 601R-52-82-351, REV A.May 6, 2012 · N447AW · Cndair CL6002B19 · Landing Gear DoorsSDR A6WA201141047Unknown · odorDETECTED A STRONG ELECTRICAL ODOR AFTER LANDING AND DURING TAXI, ODOR CONTINUED TO GATE WITH ENGINE SHUTDOWN, PERFORMED INSPECTION OF ACFT LOWER AVIONICS BAY, PAX COMPARTMENT BALLASTS, GALLEY HEATERS, & COFFEEMAKER. NO FAULTS INDICATED. NO ODOR NOTED AT THNov 22, 2011 · N447AW · Cndair CL6002B19 · Air Distribution SystemSDR A6WA201140606Landing Gear · unknownGEAR DISAGREE WARNING MESSAGE AFTER T/O. WHEN GEAR SELECTING UP. C/W QRH NOSE GEAR DASHED AMBER MSG CLEARED 20 SECONDS AFTER GEAR UP SELECTED DOWN AGAIN GOT GEAR DISAGREE WITH NLG SHOWING DASHED. INSPECTED ALL 3 GEAR BAY/LEGS NO DISCREPANCIES NOTED.Jul 11, 2011 · N447AW · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR A6WA201040687Sill · gougedSERVICE DOOR SILL HAS GOUGE BEYOND REPAIRABLE LIMITS NEEDS TO BE REPLACED. SERVICE DOOR SILL R & R IAW SRM 51-41-02.Sep 8, 2010 · N447AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201040685Seat Track · corrodedAFT RT SIDE OF SEAT TRACK IN CARGO BAY CORRODED AROUND SCREW HOLES. R & R SEAT TRACK AT RBL 9.Sep 7, 2010 · N447AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201040730Angle · crackedRT OBLIQUE ANGLE IN THE AFT SIDE OF AFT PRESSURE BULKHEAD IS CRACKED. R & R UNSERVICEABLE RT OBLIQUE ANGLE AND REPLACED WITH NEW ANGLE IAW SRM.Sep 2, 2010 · N447AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201040674Seat Track · corrodedCARGO SEAT TRACK SIDE IS CORRODED. R & R SEAT TRACK.Aug 29, 2010 · N447AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201040662Handle · gougedCARGO DOOR OUTER HANDLE CUT OUT IS GOUGED IN 3 PLACES. REPAIRED CARGO DOOR OUTER HANDLE CUT OUT IAW REO 601R-52-31-133 REV, ORIGINAL DATED 8/29/10.Aug 29, 2010 · N447AW · Cndair CL6002B19 · Cargo/Baggage DoorsSDR A6WA201040667Sill · corrodedCARGO BAY DOOR CUT OUT FLOOR SILL HAS CORROSION. R & R CARGO BAY DOOR CUT OUT FLOOR SILL IAW REO 601R-53-61-1574.Aug 29, 2010 · N447AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201040732Attach Angle · crackedFWD CARGO DOOR LOWER TRACK CHANNEL CRACKED. R & R CARGO DOOR FWD TRACK LOWER ATTACH ANGLE IAW SRM 51-40-11, 51-42-21, 51-42-06, AND 51-25-21.Aug 27, 2010 · N447AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201040686Angle · crackedLT OBLIQUE ANGLE CRACKED. R & R.Aug 27, 2010 · N447AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201040666Spar · chafedRT PYLON FWD ENGINE MOUNT SUPPORT SPAR HAS CHAFE DAMAGE FROM 14TH STAGE DUCT BLEND IAW REO 601R-54-51-091.Aug 27, 2010 · N447AW · Cndair CL6002B19 · Nacelle/Pylon, Main FrameSDR A6WA201040731Bulkhead · chafedAFT SIDE OF THE 280 BULKHEAD IS CHAFED NEXT TO MISC JACK. REPAIRED FS 280 BULKHEAD WEB BETWEEN RBL 11.00 & RBL 18.00, BETWEEN STR 134 & STR 14A IAW REO 601R-53-11-1727, REV C.Aug 26, 2010 · N447AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA201040733Structure · chafedLIGHT CHAFING ON MLG L/E DOOR. REPAIRED IAW REO 601R-52-82-016 & REO 601R-52-82-102.Aug 26, 2010 · N447AW · Cndair CL6002B19 · Landing Gear DoorsSDR A6WA201040665Door · chafedRT MLG DOOR L/E IS CHAFED IN 2 PLACES. REPAIRED DOOR (RT MLG) IAW REO 601R-52-82-102 AND REO 601R-52-82-033, REV A.Aug 26, 2010 · N447AW · Cndair CL6002B19 · Landing Gear DoorsSDR A6WA201040663Rib · crackedBATT RIB CRACKED IN LT MLG WHEEL WELL. REPAIRED LT BATT RIB IAW REO 601R-57-51-046 REV B REPAIR NR 2.Aug 26, 2010 · N447AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA201040664Rib · crackedBATT RIB IN RT W/W IS CRACKED. REAPIRED RT BATT RIB IAW REO 601R-57-51-046 REV B, REPAIR NR 2.Aug 26, 2010 · N447AW · Cndair CL6002B19 · Wing, Rib/BulkheadSDR A6WA200940071Wire · looseAPU AUTO SHUTDOWN AND TOWER REPORTS SMOKE FROM AIRCRAFT. REMOVED AND REPLACED APU FUEL SOLENOID CONNECTOR PLUG AND BACKSHELL (P5) IAW ESPM 20-17-10. APU OPS CHECK GOOD, REMOVED FROM MEL. (K)Feb 16, 2009 · N447AW · Cndair CL6002B19 · APU System WiringSDR A6WA200940102Door Seal · damagedRT OVER-WING EMERGENCY EXIT SEAL DAMAGED AT BOTTOM CORNER. SEAL REPAIRED IAW REO 601R-52-21-019. (K)Feb 10, 2009 · N447AW · Cndair CL6002B19 · Emergency ExitsSDR A6WA200940054Attach Bracket · crackedHYD LINES BRACKET CRACKED IN RT W/W, RBL 18 TO RBL 27, FS 523.6. CRACKED HYD LINE BRACKET FABRICATED AND REPLACED IAW REO 601R-53-42-007, REV A. (K)Feb 5, 2009 · N447AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200940053Attach Bracket · crackedHYD LINES BRACKET IN RT W/W RBL 18 TO RBL 27, FS 527.73, 2 CRACKS. HYD LINES BRACKET MFG AND REPLACED IAW REO 601R-53-42-007, REV A. (K)Feb 5, 2009 · N447AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200940096Floorbeam · crackedCRACK FOUND ON BRACKET FS 280, LBL 9 INBD AND OTBD NEW BRACKET INSTALL AT FS 280, RBL 9 INBD AND OTBD IAW SRM 51-42-21. (K)Feb 3, 2009 · N447AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200940097Bracket · crackedCRACK FOUND ON BRACKET FS 280, RBL 9 INBD NEW BRACKET INSTALL AT FS 280, RBL 9 INBD IAW SRM 51-42-21. (K)Feb 3, 2009 · N447AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200940064Pressure Blkhd · crackedCRACK FOUND ON PRESSURE BULKHEAD FS 202.75 AT BL 36.71 AROUND PARKING BRAKE CABLE. CRACK ON PRESSURE BULKHEAD FS 202.75 AT LBL 36.71 REPAIRED IAW REO 601R-53-11-563. (K)Feb 3, 2009 · N447AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA200940060Sill · crackedCARGO DOOR FLOOR SILL UPPER SURFACE CRACKED UNDER ANGLE AT FS 575.00. CARGO DOOR FLOOR SILL UPPER SURFACE REPAIRED DOOR. UNDER ANGLE AT FS 575 IAW REO 601R-53-61-1741. (K)Feb 3, 2009 · N447AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200940056Angle · crackedCRACK FOUND ON PILOT BULKHEAD AFT ANGLE FS 280, LBL 9 REPAIR TO BULKHEAD AFT ANGLE FS 280, LBL 9 CARRIED OUT IAW REO 601R-53-11-138. (K)Feb 3, 2009 · N447AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200940055Bulkhead · crackedCRACK FOUND ON PILOT BULKHEAD FS 280, RBL 9. REPAIR TO PILOT BULKHEAD CARRIED OUT IAW REO 601R-53-11-171, REV D. (K)Feb 3, 2009 · N447AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
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