N650AW

Service difficulty reports · 367

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 = 'N650AW' 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 AALA201606099001Strut · corrodedAIRCRAFT IN BASE MX. CORROSION ON LT WING INBD FLAP INTERCONNECTING STRUT INTERNAL AREA. REPLACED LT WING INBD FLAP INTERCONNECTING STRUT IAW AMM 27-51-44 & TASK CARD 26C57057001.May 24, 2016 · N650AW · Airbus A320232 · Trailing Edge Flap Control SystemSDR AALA201605229002Striker · out of adjustAIRCRAFT IN BASE MX. PAX CREW DOOR 841 DIMENSION B IS OUT OF ADJUSTMENT, BETWEEN FINGER & STRIKER LEVER DAMPER MECHANISM. ADJUSTED DIMENSION B JI ON PAX CREW DOOR 841, BETWEEN FINGER & STRIKER LEVER DAMPER MECHANISM IAW AMM 52-11-14-820-002-A.May 21, 2016 · N650AW · Airbus A320232 · Passenger/Crew DoorsSDR AALA201606109005Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RT WING NR 1 SLAT TRACK 3 FORWARD SLAT BOLTS. REPLACED BOLTS IAW TASK CARD 26C61057005.May 20, 2016 · N650AW · Airbus A320232 · Leading Edge DevicesSDR AALA201606109004Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RT WING NR 1 SLAT TRACK 3 LOWER SLAT BOLTS. REPLACED BOLTS IAW TASK CARD 26C61057005.May 20, 2016 · N650AW · Airbus A320232 · Leading Edge DevicesSDR AALA201606039014Bolt · corrodedCORROSION ON RT WING NR 1 SLAT, NR 4 TRACK FWD BOLT LOCATED BETWEEN WING STATION 2580 - 3059 & BETWEEN RIB 5 & 6. REPLACED BOLT IAW TASK CARD 26C61057005.May 20, 2016 · N650AW · Airbus A320232 · Leading Edge DevicesSDR AALA201605219008Striker · out of adjustAIRCRAFT IN BASE MX. PAX CREW DOOR 831 DIMENSION B IS OUT OF ADJUSTMENT, BETWEEN FINGER & STRIKER LEVER DAMPER MECHANISM. ADJUSTED DIMENSION B JI ON PAX CREW DOOR 831, BETWEEN FINGER & STRIKER LEVER DAMPER MECHANISM IAW AMM 52-11-14-820-002-A.May 20, 2016 · N650AW · Airbus A320232 · Passenger/Crew DoorsSDR AALA201605219007Striker · out of adjustAIRCRAFT IN BASE MX. PAX CREW DOOR 831 DIMENSION A IS OUT OF ADJUSTMENT, BETWEEN FINGER & STRIKER LEVER DAMPER MECHANISM. ADJUSTED DIMENSION A J2 ON PAX CREW DOOR 831, BETWEEN FINGER & STRIKER LEVER DAMPER MECHANISM IAW AMM 52-11-14-820-002-A.May 20, 2016 · N650AW · Airbus A320232 · Passenger/Crew DoorsSDR AALA201605219006Cylinder · low pressureAIRCRAFT IN BASE MX. LOW PRESS DAMPER & EMER OPERATION CYLINDER ON PAX CREW DOOR 841. SERVICED DAMPER & EMER OPERATION CYLINDER IAW AMM 52-10-00-614-001-A.May 20, 2016 · N650AW · Airbus A320232 · Passenger/Crew DoorsSDR AALA201606249022Access Panel · debondedACFT IN BASE MAINTENACE, LT WING FUEL TANK ACCESS PANEL 540CZ HAS DEBONDED ALUMINUM FOIL. REPLACED LT WING FUEL TANK ACCESS PANEL 540CZ IAW AMM 57-27-11-400-007-A.May 18, 2016 · N650AW · Airbus A320232 · Wing, Plate/SkinSDR AALA201606249021Access Panel · debondedAIRCRAFT IN BASE MAINTENANCE, RT WING FUEL TANK ACCESS PANEL 640CZ HAS DEBONDED ALUMINUM FOIL. REPLACED RT WING FUEL TANK ACCESS PANEL 640CZ IAW AMM 57-27-11-400-007-A.May 18, 2016 · N650AW · Airbus A320232 · Wing, Plate/SkinSDR AALA201606249019Access Panel · debondedAIRCRAFT IN BASE MAINTENANCE, LT WING FUEL TANK ACCESS PANEL 540DZ HAS DEBONDED ALUMINUM FOIL. REPLACED ACCESS PANEL 540DZ IAW AMM 57-27-11-400-007-A..May 18, 2016 · N650AW · Airbus A320232 · Wing, Plate/SkinSDR AALA201606249015Pressure Deck · crackedAIRCRAFT IN BASE MAINTENANCE, CRACK INDICATION ON THE SIDE BOX BEAM PRESSURE PLATE AT SECOND HOLE FROM FRAME 43 TO FORWARD BETWEEN Y-1650 AND Z-642.5. REPLACED PRESSURE PLATE IAW SRM 51-72-11 AND 51-42-11.May 15, 2016 · N650AW · Airbus A320232 · Fuselage Main, BulkheadSDR AALA201606249014Box Beam · crackedAIRCRAFT IN BASE MAINTENANCE, LT SIDE BOX BEAM UPPER FLANGE HAS CRACK INDICATION AT FIRST AND SECOND FASTENER HOLE FROM FRAME 43 TO FORWARD BETWEEN +Y1650 AND Z-642.5. REPAIRED BOX BEAM IAW EO 5315Y066.May 15, 2016 · N650AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AALA201606249013Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE, NLG RT AFT DOOR FORWARD HINGE FITTING HAD EXCESSIVE PLAY AND WAS REPLACED IAW CMM 52-82-32 AND AMM 32-22-00-220-002-A.May 15, 2016 · N650AW · Airbus A320232 · Landing Gear DoorsSDR AALA201606249012Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE, NLG RT AFT DOOR AFT HINGE FITTING HAD EXCESSIVE PLAY AND WAS REPLACED IAW CMM 52-82-32 AND AMM 32-22-00-220-002-A.May 15, 2016 · N650AW · Airbus A320232 · Landing Gear DoorsSDR AALA201606249011Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE, NLG LT AFT DOOR AFT HINGE FITTING HAD EXCESSIVE PLAY AND WAS REPLACED IAW CMM 52-82-32 AND AMM 32-22-00-220-002-A.May 15, 2016 · N650AW · Airbus A320232 · Landing Gear DoorsSDR AALA201606249010Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE, NLG LT AFT DOOR FORWARD HINGE FITTING HAD EXCESSIVE PLAY AND WAS REPLACED IAW CMM 52-82-32 AND AMM 32-22-00-220-002-A.May 15, 2016 · N650AW · Airbus A320232 · Landing Gear DoorsSDR AALA201606249007Box Beam · crackedAIRCRAFT IN BASE MAINTENANCE, RT SIDE BOX BEAM UPPER FLANGE 1ST AND 2ND FASTENER HOLE FROM FRAME 43 TO FORWARD BETWEEN Y-1650 AND Z-642.5 HAVE CRCK INDICATION. REPAIRED BOX BEAM IAW EO 5315Y066.May 15, 2016 · N650AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AALA201605259003Hinge Fitting · excess playAIRCRAFT IN BASE MX. LT ELEVATOR NR 6 HINGE, FITTING HAS EXCESSIVE PLAY AT STATION 5894 & RIB 13. REPLACED NR 6 HINGE FITTING IAW AMM 55-16-42.May 13, 2016 · N650AW · Airbus A320232 · Elevator StructureSDR AALA201605239017Hinge Fitting · excess playAIRCRAFT IN BASE MX. LT ELEVATOR NR 4 HINGE FITTING HAS EXCESSIVE PLAY, BETWEEN STATION 2973 & 3416, BETWEEN RIB 8 & 9. REPLACED HINGE FITTING IAW AMM 55-16-42.May 13, 2016 · N650AW · Airbus A320232 · Elevator StructureSDR AALA201605239016Hinge Fitting · excess playAIRCRAFT IN BASE MX. LT ELEVATOR NR 3 HINGE FITTING HAS EXCESSIVE PLAY, BETWEEN STATION 2707 & 2973, BETWEEN RIB 7 & 8. REPLACED HINGE FITTING IAW AMM 55-16-42.May 13, 2016 · N650AW · Airbus A320232 · Elevator StructureSDR AALA201606159012Cover Plate · corrodedCORROSION ON AFT CARGO COMPARTMENT COVER SHEET BETWEEN FRAME 52A AND FRAME 56 BETWEEN STR 39 RT AND STR 41 RIGHT. REPLACED COVER SHEET IAW SRM 51-72-11 AND DWG D53475500.May 11, 2016 · N650AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AALA201606079013Cleat · corrodedAIRCRAFT IN BASE MX. CORROSION ON FWD CARGO COMPARTMENT SHEAR TIE, CLEAT, AT FRAME 32 BETWEEN STRINGER 40 RT & 41 RT. REPLACED FWD CARGO COMPARTMENT SHEAR TIE, CLEAT, IAW SRM 51-72-11 & DWG D53231586.May 10, 2016 · N650AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AALA201606079012Cleat · corrodedAIRCRAFT IN BASE MX. CORROSION ON FWD CARGO COMPARTMENT SHEAR TIE, CLEAT, AT FRAME 32, BETWEEN STRINGER 41 RT & 42 RT. REPLACED FWD CARGO COMPARTMENT SHEAR TIE, CLEAT, IAW SRM 51-72-11 & DWG D53231586.May 10, 2016 · N650AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AALA201606089009Shear Tie · corrodedAIRCRAFT IN BASE MX. CORROSION ON FWD CARGO COMPARTMENT SHEAR TIE AT FRAME 28, BETWEEN STRINGER 42 RT & 43 RT. REPLACED FWD CARGO COMPARTMENT SHEAR TIE IAW SRM 51-72-11 & DWG D53231712.May 9, 2016 · N650AW · Airbus A320232 · Fuselage Internal Mounting StructureSDR AALA201606089008Floor Panel · delaminatedAIRCRAFT IN BASE MX. CABIN FLOOR PANEL 232LF DELAMINATED. REPLACED FLOOR PANEL IAW SRM 53-02-00 & IRM 9701 REV G.May 9, 2016 · N650AW · Airbus A320232 · Fuselage Floor PanelSDR AALA201605239013Shear Tie · corrodedAIRCRAFT IN BASE MX. CORROSION ON SHEAR TIE IN FWD CARGO COMPARTMENT AT FRAME 30, BETWEEN STRINGER 40 RT & 41 RT. REPLACED SHEAR TIE IAW SRM 51-72-11 & DWG D5323647.May 9, 2016 · N650AW · Airbus A320232 · Fuselage Internal Mounting StructureSDR AALA201606249016Skin Panel · crackedAIRCRAFT IN BASE MAINTENANCE, CRACK INDICATION IN SKIN PANEL FASTENER HOLE AT FRAME 35 AND STR 30 LT. REPAIRED SKIN PANEL IAW EA 260369.May 8, 2016 · N650AW · Airbus A320232 · Fuselage Main, Plate/SkinSDR AALA201606249023Skin · delaminatedAIRCRAFT IN BASE MAINTENANCE, LT ELEVATOR UPPER SURFACE SKIN HAS 2 AREAS OF TRAPPED WATER INDICATED BETWEEN STA 181 AND STA 227, RIBS 2-3 AND 2 AREAS OF DELAMINATION BETWEEN STA 466 AND STA 527, RIBS 8-9. REPAIRED ELEVATOR UPPER SURFACE SKIN IAW SRM 55-21-11-May 7, 2016 · N650AW · Airbus A320232 · Elevator, Plate/SkinSDR AALA201606249018Floor Panel · delaminatedAIRCRAFT IN BASE MAINTENANCE, DELAMINATED TOP LAYER FLOOR PANEL 261BG IN AFT GALLEY AREA. REPLACED FLOOR PANEL 261BG IAW IRM 9701, REV G AND SRM 53-02-00.May 7, 2016 · N650AW · Airbus A320232 · Fuselage Floor PanelSDR AALA201606149014Skin · saturatedLEFT ELEVATOR UPPER SURFACE SKIN HAS INDICATION OF TRAPPED WATER, 14" OTBD OF LIGHTNING STRIP NR 3 AND 8" FROM T/E. REPAIRED LT ELEVATOR UPPER SURFACE SKIN IAW SRM 55-21-11-201-1, PARA 5E.May 7, 2016 · N650AW · Airbus A320232 · Elevator, Plate/SkinSDR AALA201606079011Floor Panel · delaminatedAIRCRAFT IN BASE MX. AFT GALLEY FLOOR PANEL 261DF HAS DELAMINATION. REPLACED FLOOR PANEL 261DF IAW SRM 53-02-00-201, IRM 9701 REV G & EA 260481.May 7, 2016 · N650AW · Airbus A320232 · Fuselage Floor PanelSDR AALA201605319013Coupling · damagedAIRCRAFT IN BASE MX. COUPLING AT FRAME 67 + 5" & -Y465, HAS ELONGATED FASTENER HOLE. REPLACED COUPLING IAW SRM A320 51-72-11 & DWG D53472816.May 7, 2016 · N650AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AALA201605319012Coupling · damagedAIRCRAFT IN BASE MX. COUPLING AT FRAME 67 + 5" & -Y465, HAS ELONGATED FASTENER HOLE. REPLACED COUPLING IAW SRM 51-72-11 & DWG D53472816.May 7, 2016 · N650AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AALA201605319011Floorbeam · corrodedAIRCRAFT IN BASE MX. CORROSION ON FLOORBEAM, BETWEEN FRAME 64 & 67 + 5", -Y7465. REPLACED FLOORBEAM IAW SRM 51-72-11 & DWG D53472816.May 7, 2016 · N650AW · Airbus A320232 · Fuselage Main, Floor BeamSDR AALA201605259002Floor Panel · delaminatedAIRCRAFT IN BASE MX. FWD GALLEY FLOOR PANEL 221LF DELAMINATED. REPLACED FLOOR PANEL 221 LF IAW SRM 53-12-00 & IRM 9701.May 7, 2016 · N650AW · Airbus A320232 · Fuselage Floor PanelSDR AALA201605239015Floor Panel · delaminatedAIRCRAFT IN BASE MX. FWD GALLEY FLOOR PANEL 221PF DELAMINATED. REPLACED FLOOR PANEL IAW SRM 53-12-00 7 IRM 9701 REV G.May 7, 2016 · N650AW · Airbus A320232 · Fuselage Floor PanelSDR AALA201605239014Floor Panel · delaminatedAIRCRAFT IN BASE MX. AFT GALLEY FLOOR PANEL 261AG DELAMINATED. REPLACED FLOOR PANEL IAW SRM 53-02-00-201 & IRM 9701 REV G.May 7, 2016 · N650AW · Airbus A320232 · Fuselage Floor PanelSDR AALA201605209004Seat Track · corrodedAIRCRAFT IN BASE MX. CORROSION ON SEAT TRACK, BETWEEN FRAME 64 & 66 AT +Y1292. REPLACED SEAT TRACK IAW SRM 51-72-11 & DWG D53472815.May 7, 2016 · N650AW · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR AALA201606249020Pressure Deck · crackedAIRCRAFT IN BASE MAINTENANCE, SEVERAL CRACKED FASTENER HOLES IN THE PRESSURE DECK PLATE AT FRAME 36 BETWEEN -Y1292 AND -Y1523. REPAIRED PRESSURE DECK PLATE IAW EA 260343.May 6, 2016 · N650AW · Airbus A320232 · Fuselage Main, BulkheadSDR AALA201606249006Pressure Deck · crackedAIRCRAFT IN BASE MAINTENANCE, SEVERAL PRESSURE DECK FASTENER HOLES HAVE CRACK INDICATIONS AT FRAME 36 BETWEEN +Y1292 AND +Y1523. REPAIRED PRESSURE DECK IAW EA 260342.May 6, 2016 · N650AW · Airbus A320232 · Fuselage Main, BulkheadSDR AALA201606249005Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE, EXCESSIVE PLAY ON RUDDER HINGE ARM NR 4 REPLACED HINGE ARM NR 4 IAW AMM 55-36-41-400-001-A, STEP 8, ITEM A, STEP 1 TO STEP 8.May 6, 2016 · N650AW · Airbus A320232 · Rudder StructureSDR AALA201606159013Hinge Fitting · excess playRUDDER NR 5 HINGE ARM FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM FITTING IAW AMM 55-36-41-400-001-A.May 6, 2016 · N650AW · Airbus A320232 · Rudder StructureSDR AALA201606109008Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: RUDDER NR 3 HINGE ARM FITTING HAS EXCESSIVE PLAY. REPLACED RUDDER NR 3 HINGE ARM FITTING IAW AMM 55-36-41-400-001-A.May 6, 2016 · N650AW · Airbus A320232 · Rudder StructureSDR AALA201606109007Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: RUDDER NR 2 HINGE ARM FITTING HAS EXCESSIVE PLAY. REPLACED RUDDER NR 2 HINGE ARM FITTING IAW AMM 55-36-41-400-001-A.May 6, 2016 · N650AW · Airbus A320232 · Rudder StructureSDR AALA201606109006Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENACE: RUDDER NR 1 HINGE ARM FITTING HAS EXCESSIVE PLAY. REPLACED RUDDER NR 1 HINGE ARM FITTING IAW AMM 55-36-41-400-001-A.May 6, 2016 · N650AW · Airbus A320232 · Rudder StructureSDR AALA201605319010Floor Panel · delaminatedAIRCRAFT IN BASE MX. AFT GALLEY FLOOR PANEL 231KF DELAMINATED. REPLACED FLOOR PANEL IAW SRM 53-02-00 & IRM 9701 REV G.May 6, 2016 · N650AW · Airbus A320232 · Fuselage Floor PanelSDR AALA201605209011Floor Panel · delaminatedAIRCRAFT IN BASE MX. AFT CARGO COMPARTMENT FLOOR PANEL 152 EF DELAMINATED. REPLACED FLOOR PANEL IAW SRM 53-02-00-201 & IRM 9701 REV G.May 6, 2016 · N650AW · Airbus A320232 · Fuselage Floor PanelSDR AALA201605209010Floor Panel · delaminatedAIRCRAFT IN BASE MX. AFT CARGO COMPARTMENT FLOOR PANEL 151EF DELAMINATED. REPLACED FLOOR PANEL IAW SRM 53-02-00-201 & IRM 9701 REV G.May 6, 2016 · N650AW · Airbus A320232 · Fuselage Floor PanelSDR AALA201605209009Floor Panel · delaminatedAIRCRAFT IN BASE MX. AFT CARGO COMPARTMENT FLOOR PANEL 151AF DELAMINATED. REPLACED FLOOR PANEL IAW SRM 53-02-00-201 & IRM 9701 REV G.May 6, 2016 · N650AW · Airbus A320232 · Fuselage Floor Panel
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