N651AW

Service difficulty reports · 344

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 = 'N651AW' 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 AALA201604279005Wire Harness · chafedAIRCRAFT IN BASE MX. CHAFING ON FIRE DETECTION ELEC WIRING 2621-0020 FROM CONNECTOR 5WE1 TO CONNECTOR 473VC ON LT PYLON. R & R FIRE DETECTION ELEC WIRING 2621-0020 IAW AMM 26-21-01 & ESPM 20-48-24. PERFORMED OPERATIONAL TEST OF ENG BOTTLE LOW PRESS INDICATIApr 26, 2016 · N651AW · Airbus A320232 · Fire Protection System WiringSDR AALA201604279004Wire Harness · chafedAIRCRAFT IN BASE MX. CHAFING ON FIRE DETECTION ELEC WIRING 2621-0076 FROM CONNECTOR 8WE1 TO CONNECTOR 472VN1 ON LT PYLON. R & R FIRE DETECTION ELEC WIRING 2621-0076 IAW AMM 26-21-02 & ESPM 20-48-21. PERFORMED OPERATIONAL CHECK OF ENG E BOTTLE LOW PRESS INDIApr 26, 2016 · N651AW · Airbus A320232 · Fire Protection System WiringSDR AALA201604259003Wire Harness · chafedAIRCRAFT IN BASE MX. CHAFING ON FIRE DETECTION ELEC WIRING 2621-0001 FROM CONNECTOR 5WE2 TO CONNECTOR 474VC ON RT PYLON. REPLACED ELEC WIRE IAW ESPM 20-48-24 AWM 26-21-03 & PERFORMED OPERATIONAL TEST IS OK IAW AMM 26-12-00-001-A.Apr 24, 2016 · N651AW · Airbus A320232 · Fire Protection System WiringSDR AALA201604149004Slide · brokenAIRCRAFT IN BASE MX. R1 DOOR SLIDE PACK ASSEMBLY BROKEN. REPLACED SLIDE ASSEMBLY IAW TASK CARD 26C84152006.Apr 13, 2016 · N651AW · Airbus A320232 · Escape SlideSDR AALA201604149003Connector · corrodedAIRCRAFT IN BASE MX. R2 DOOR SLIDE PACK ASSEMBLY HAS CORROSION ON ELEC CONNECTOR. REPLACED SLIDE PACK ASSEMBLY IAW TASK CARD 26C8425006.Apr 13, 2016 · N651AW · Airbus A320232 · Equipment/Furnishings WiringSDR AALA201604159001Strut · corrodedAIRCRAFT IN BASE MX. CORRODED LT WING TE FLAP INTERCONNECTING STRUT AT WING STATION 4862. REPLACED INTERCONNECTING STRUT IAW AMM 27-51-44.Apr 8, 2016 · N651AW · Airbus A320232 · Trailing Edge FlapsSDR AALA201604129026Strut · corrodedAIRCRAFT IN BASE MX. RT WING TRAINING EDGE FLAP INTERCONNECTING STRUT HAS CORROSION. REPLACED RT WING TRAINING EDGE FLAP INTERCONNECTING STRUT IAW TASK CARD 26C670577001.Apr 8, 2016 · N651AW · Airbus A320232 · Trailing Edge FlapsSDR AALA201604189001Hinge Fitting · wornAIRCRAFT IN BASE MX. LT ELEVATOR NR 2 HINGE FITTING HAS EXCESSIVE PLAY AT STABILIZER STATION 227 & RIB 6. REPLACED HINGE FITTING IAW AMM 55-16-42.Apr 7, 2016 · N651AW · Airbus A320232 · Elevator StructureSDR AALA201604269013Hinge Fitting · wornAIRCRAFT IN BASE MX. LT ELEVATOR HINGE NR 1 OTBD LUG HAS EXCESSIVE WEAR & BORE DIAMETER EXCEEDS ESTABLISHED LIMITS. REPLACED LT ELEVATOR.Apr 6, 2016 · N651AW · Airbus A320232 · Elevator StructureSDR AALA201604269009Door Frame · crackedAIRCRAFT IN BASE MX. EMER EXIT DOOR 833 AFT FRAME SEGMENT CRACKED AT BEAM 4. REPLACED SEGMENT IAW SRM 51-72-11 & DWG D52279040.Apr 6, 2016 · N651AW · Airbus A320232 · Emergency ExitsSDR AALA201604219005Door Frame · crackedAIRCRAFT IN BASE MX. EMER EXIT DOOR 843 FWD FRAME SEGMENT CRACKED, BETWEEN FRAME 38 & 39 AT BEAM 4. REPLACED FRAME SEGMENT IAW SRM 51-72-11 & DWG D52279040.Apr 6, 2016 · N651AW · Airbus A320232 · Emergency ExitsSDR AALA201604199012Door Frame · crackedAIRCRAFT IN BASE MX. CRACK ON SEGMENT FWD FRAME ON EMER EXIT DOOR 833 AT BEAM 4. REPLACED SEGMENT FWD FRAME ON EMER EXIT DOOR 833 IAW SRM 51-72-11 & DWG D52279040.Apr 6, 2016 · N651AW · Airbus A320232 · Emergency ExitsSDR AALA201604199011Door Frame · crackedAIRCRAFT IN BASE MX. CRACK SEGMENT OF AFT FRAME ON EMER EXIT DOOR 844 & BEAM 4. REPLACED SEGMENT OF AFT FRAME ON EMER EXIT DOOR IAW SRM 51-72-11 & DWG D52279040.Apr 6, 2016 · N651AW · Airbus A320232 · Emergency ExitsSDR AALA201604129016Floor Panel · delaminatedAIRCRAFT IN BASE MX. CABIN FLOOR PANEL 251FF IS DELAMINATED. REPLACED FLOOR PANEL IAW SRM 53-02-00 & IRM 9701 REV G.Apr 6, 2016 · N651AW · Airbus A320232 · Fuselage Floor PanelSDR AALA201604129010Floor Panel · delaminatedAIRCRAFT IN BASE MX. CABIN FLOOR PANEL 241JF IS DELAMINATED. REPLACED FLOOR PANEL IAW 53-02-00 & IRM 9701 REV G.Apr 6, 2016 · N651AW · Airbus A320232 · Fuselage Floor PanelSDR AALA201604209007Stringer · corrodedAIRCRAFT IN BASE MX. CORROSION ON AFT CARGO COMPARTMENT STRINGER, BETWEEN FRAME 64 & 65 AT STRINGER 44. REPAIRED STRINGER IAW SRM 53-00-13.Mar 31, 2016 · N651AW · Airbus A320232 · Fuselage Main, Longeron/StringerSDR AALA201604159003Floor Panel · delaminatedAIRCRAFT IN BASE MX. DELAMINATION ON FLOOR PANEL 251RF IN PAX CABIN, BETWEEN FRAME 58 & 62, AT Y254 & -Y254. REPLACED FLOOR PANEL 251RF IN PAX CABIN REV G.Mar 31, 2016 · N651AW · Airbus A320232 · Fuselage Floor PanelSDR AALA201604019003Door · out of adjustAIRCRAFT IN BASE MX. PAX CREW DOOR 842 DIMENSION A, BETWEEN FINGER & STRIKER LEVER DAMPER MECHANISM IS OUT OF ADJUSTMENT. ADJUSTED PAX CREW DOOR 842 DIMENSION A IAW AMM 52-11-14-820-002-A.Mar 31, 2016 · N651AW · Airbus A320232 · Passenger/Crew DoorsSDR AALA201604019001Door · out of adjustAIRCRAFT IN BASE MX. PAX CREW DOOR 831 DIMENSION A, BETWEEN FINGER & STRIKER LEVER DAMPER MECHANISM IS OUT OF ADJUSTMENT. ADJUSTED PAX CREW DOOR 831 DIMENSION A IAW AMM 52-11-14-820-002-A.Mar 31, 2016 · N651AW · Airbus A320232 · Passenger/Crew DoorsSDR AALA201604269012Hinge Fitting · wornAIRCRAFT IN BASE MX. RUDDER HINGE ARM 4 HAS WEAR ON THE BEARING AT VERTICAL STABILIZER STATION 2632 & RIB 6. REPLACED HINGE ARM FITTING IAW SRM 51-72-11 & AMM 55-36-41-400-001-A.Mar 28, 2016 · N651AW · Airbus A320232 · Rudder StructureSDR AALA201604129023Hinge Fitting · excess playAIRCRAFT IN BASE MX. VERTICAL STABILIZER NR 5 RUDDER HINGE ARM FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM IAW AMM 55-36-41-400-001-A.Mar 28, 2016 · N651AW · Airbus A320232 · Vertical StabilizerSDR AALA201604129021Hinge Fitting · excess playAIRCRAFT IN BASE MX. VERTICAL STABILIZER NR 2 RUDDER HINGE ARM FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM IAW AMM 55-36-41-400-001-A.Mar 28, 2016 · N651AW · Airbus A320232 · Vertical StabilizerSDR AALA201604279012Box Beam · crackedAIRCRAFT IN BASE MX. LT SIDE BOX BEAM FLANGE HAS CRACK INDICATIONS AT FRAME 42, +18.632" & +Y1650. REPAIRED BOX BEAM IAW EO 5315Y066.Mar 27, 2016 · N651AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AALA201604269011Box Beam · crackedAIRCRAFT IN BASE MX. RT SIDE BOX BEAM FLANGE HAS CRACK INDICATIONS AT FRAME 42, 17.518 & -Y1650. REPAIRED BOX BEAM IAW EO 5315Y066.Mar 27, 2016 · N651AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AALA201604269010Box Beam · crackedAIRCRAFT IN BASE MX. LT SIDE BOX BEAM FLANGE HAS CRACK INDICATIONS AT FRAME 42, 17.518" & Y1650. REPAIRED BOX BEAM IAW EO 5315Y066.Mar 27, 2016 · N651AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AALA201604069006Hinge Pin · corrodedAIRCRAFT IN BASE MX. CORROSION ON RT WING AILERON NR 5 HINGE PIN. REPLACED HINGE PIN.Mar 27, 2016 · N651AW · Airbus A320232 · AileronsSDR AALA201604299012Skin · saturatedAIRCRAFT IN BASE MX. RUDDER RT SIDE SKIN HAS INDICATION OF TRAPPED WATER IN 4 AREAS. AREA 1, .25" FROM THE LE & 7.5" FROM THE LOWER EDGE OF THE VERTICAL STABILIZER. AREA 2, 25" FROM THE TE & 8" FROM THE LOWER EDGE OF THE VERTICAL STABILIZER. AREA 3, 33" FRMar 25, 2016 · N651AW · Airbus A320232 · Rudder, Plate/SkinSDR AALA201604229006Angle · corrodedAIRCRAFT IN BASE MX. CORROSION ON ANGLE, STRINGER SECTION, IN THE AFT GALLEY AT FRAME 70 & STRINGER 24 RT. REPLACED ANGLE IAW SRM 51-72-11 & DWG D53474180.Mar 24, 2016 · N651AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AALA201604129025Hinge Fitting · wornAIRCRAFT IN BASE MX. LT MLG DOOR FWD HINGE FITTING BEARING HAS EXCESSIVE PLAY. REPLACED HINGE FITTING IAW CMM 52-81-18.Mar 22, 2016 · N651AW · Airbus A320232 · Landing Gear DoorsSDR AALA201604129017Floor Panel · delaminatedAIRCRAFT IN BASE MX. CABIN FLOOR PANEL 252SF IS DELAMINATED. REPLACED FLOOR PANEL IAW SRM 53-02-00 & IRM 9701 REV G.Mar 21, 2016 · N651AW · Airbus A320232 · Fuselage Floor PanelSDR AALA201605059004Skin Panel · corrodedAIRCRAFT IN BASE MX. CORROSION ON CTR WING BOX UPPER SURFACE SKIN PANEL AT FRAME 42, BETWEEN -765 & -Y1292. REPAIRED IAW EA 259138.Mar 18, 2016 · N651AW · Airbus A320232 · Fuselage Main, Plate/SkinSDR AALA201605059003Skin Panel · crackedAIRCRAFT IN BASE MX. CRACK INDICATIONS ON TWO FASTENER HOLES OF LOWER FUSELAGE OUTER SKIN PANEL AT FRAME 35 & STRINGER 30L. REPAIRED IAW EA 259022.Mar 18, 2016 · N651AW · Airbus A320232 · Fuselage Main, Plate/SkinSDR AALA201604159004Floor Panel · delaminatedAIRCRAFT IN BASE MX. DELAMINATION ON FLOOR PANEL 161 AF IN BULK CARGO COMPARTMENT, BETWEEN FRAME 59 & 64, AT Y765 - Y765. REPLACED FLOOR PANEL 161 AF IAW SRM 53-02-00 PARA 8 H FIG 209 & IRM 9701 REV G.Mar 18, 2016 · N651AW · Airbus A320232 · Fuselage Floor PanelSDR AALA201604129018Floor Panel · delaminatedAIRCRAFT IN BASE MX. AFT CARGO COMPARTMENT FLOOR PANEL 152EF IS DELAMINATED. REPLACED FLOOR PANEL IAW SRM 53-02-00 & IRM 9701 REV G.Mar 18, 2016 · N651AW · Airbus A320232 · Fuselage Floor PanelSDR AALA201604129012Floor Panel · delaminatedAIRCRAFT IN BASE MX. AFT CARGO COMPARTMENT FLOOR PANEL 151BF IS DELAMINATED. REPLACED FLOOR PANEL IAW SRM 53-02-00 & IRM 9701 REV G.Mar 18, 2016 · N651AW · Airbus A320232 · Fuselage Floor PanelSDR AALA201604129011Floor Panel · delaminatedAIRCRAFT IN BASE MX. AFT CARGO COMPARTMENT FLOOR PANEL 152QF IS DELAMINATED. REPLACED FLOOR PANEL IAW SRM 53-02-00 & IRM 9701 REV G.Mar 18, 2016 · N651AW · Airbus A320232 · Fuselage Floor PanelSDR AALA201604129008Floor Panel · delaminatedAIRCRAFT IN BASE MX. FORWARD CARGO COMPARTMENT FLOOR PANEL 131BF IS DELAMINATED. REPLACED FLOOR PANEL IAW SRM 53-02-00 & IRM 9701 REV G.Mar 18, 2016 · N651AW · Airbus A320232 · Fuselage Floor PanelSDR AALA201604129005Floor Panel · delaminatedAIRCRAFT IN BASE MX. FWD CARGO COMPARTMENT FLOOR PANEL 131GF IS DELAMINATED. REPLACED FLOOR PANEL IAW SRM 53-02-00 & IRM 9701 REV G.Mar 18, 2016 · N651AW · Airbus A320232 · Fuselage Floor PanelSDR AALA201604299011Bracket · corrodedAIRCRAFT IN BASE MX. CORROSION ON EMER EXIT DOOR 833, LOWER SECTION BRACKETS, BETWEEN FRAME 38 & 39 AT BEAM 4. REPLACED BRACKETS IAW SRM 51-72-11 & DWG D52279040.Mar 17, 2016 · N651AW · Airbus A320232 · Emergency ExitsSDR AALA201604229005Bracket · corrodedAIRCRAFT IN BASE MX. CORROSION ON EMER EXIT DOOR 843 LOWER FWD BRACKET SECTION T, BETWEEN FRAME 38 & 39 AT BEAM 4.Mar 17, 2016 · N651AW · Airbus A320232 · Emergency ExitsSDR AALA201604159002Floor Panel · delaminatedAIRCRAFT IN BASE MX. DELAMINATION ON FLOOR PANEL 222EF IN FWD GALLEY, BETWEEN FRAME 16 & 20, AT Y254 & -Y765. REPLACED FLOOR PANEL 222EF IAW SRM 53-12-00 SUPPL INFO & IRM 9701 REV G.Mar 17, 2016 · N651AW · Airbus A320232 · Fuselage Floor PanelSDR AALA201604129024Hinge Fitting · wornAIRCRAFT IN BASE MX. VERTICAL STABILIZER NR 7 RUDDER HINGE ARM FITTING BEARING WORN. REPLACED HINGE ARM IAW AMM 55-36-41-400-001-A.Mar 17, 2016 · N651AW · Airbus A320232 · Vertical StabilizerSDR AALA201604129022Hinge Fitting · excess playAIRCRAFT IN BASE MX. VERTICAL STABILIZER NR 3 RUDDER HINGE ARM FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM IAW AMM 55-36-41-400-001-A.Mar 17, 2016 · N651AW · Airbus A320232 · Vertical StabilizerSDR AALA201604129020Hinge Fitting · excess playAIRCRAFT IN BASE MX. VERTICAL STABILIZER NR 1 RUDDER HINGE ARM FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM IAW AMM 55-36-41-400-001-A.Mar 17, 2016 · N651AW · Airbus A320232 · Vertical StabilizerSDR AALA201604129019Floor Panel · delaminatedAIRCRAFT IN BASE MX. AFT GALLEY FLOOR PANEL 261AG IS DELAMINATED. REPLACED FLOOR PANEL IAW SRM 53-02-00 & IRM 9701 REV G.Mar 17, 2016 · N651AW · Airbus A320232 · Fuselage Floor PanelSDR AALA201604129015Floor Panel · delaminatedAIRCRAFT IN BASE MX. FWD GALLEY FLOOR PANEL 231FF IS DELAMINATED. REPLACED FLOOR PANEL IAW SRM 53-12-00 & IRM 9701 REV G.Mar 17, 2016 · N651AW · Airbus A320232 · Fuselage Floor PanelSDR AALA201604129014Floor Panel · delaminatedAIRCRAFT IN BASE MX. FWD GALLEY FLOOR PANEL 231CF IS DELAMINATED. REPLACED FLOOR PANEL IAW SRM 53-12-00 & IRM 9701 REV G.Mar 17, 2016 · N651AW · Airbus A320232 · Fuselage Floor PanelSDR AALA201604129013Floor Panel · delaminatedAIRCRAFT IN BASE MX. FWD CARGO COMPARTMENT FLOOR PANEL 232FF IS DELAMINATED. REPLACED FLOOR PANEL IAW SRM 53-12-00 & IRM 9701 REV G.Mar 17, 2016 · N651AW · Airbus A320232 · Fuselage Floor PanelSDR AALA201604129009Floor Panel · delaminatedAIRCRAFT IN BASE MX. AFT GALLEY FLOOR PANEL 261BG IS DELAMINATED. REPLACED FLOOR PANEL IAW SRM 53-02-00 & IRM 9701 REV G.Mar 17, 2016 · N651AW · Airbus A320232 · Fuselage Floor PanelSDR AALA201604129007Floor Panel · delaminatedAIRCRAFT IN BASE MX. AFT GALLEY FLOOR PANEL 221PF IS DELAMINATED. REPLACED FLOOR PANEL IAW SRM 53-02-00 & IRM 9701 REV G.Mar 17, 2016 · N651AW · Airbus A320232 · Fuselage Floor Panel
Back to N651AW