N118US

Service difficulty reports · 266

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 = 'N118US' 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 AALA2018100219019Fitting · crackedCRACKED INTERCOSTAL FITTING AT FRAME 16, NR 7 DOOR STOP FITTING. REPLACED THE INTERCOSTAL FITTING IAW SRM 51-72-11, AND 51-42-11.Sep 25, 2018 · N118US · Airbus A320214 · Fuselage Miscellaneous StructureSDR AALA2018092109004Attach Fitting · corrodedCORROSION FOUND ON THE RIGHT WING OTBD FLAP TRACK SPHERICAL BEARING ATTACH FITTING. REPLACED THE FLAP IAW TC 26L00027009.Sep 19, 2018 · N118US · Airbus A320214 · Trailing Edge FlapsSDR AALA2018092199013Strut · corrodedCORROSION FOUND ON THE LEFT WING INTERCONNECTING STRUT. REPLACED LEFT WING INTERCONNECTING STRUT.Sep 18, 2018 · N118US · Airbus A320214 · Trailing Edge FlapsSDR AALA2018092199012Strut · corrodedCORROSION FOUND ON THE RIGHT WING INTERCONNECTING STRUT. REPLACED RIGHT WING INTERCONNECTING STRUT.Sep 18, 2018 · N118US · Airbus A320214 · Trailing Edge FlapsSDR AALA201809209045Fitting · wornPASSENGER DOOR FITTING OF THE SLIDE RAFT WAS WORN. REPLACED FITTING IAW CMM 52-13-15-000-827-B03 STEP 2.A (7), AND CMM 52-13-15-400-802-B04, STEP 3.A (7)(A) THRU (C).Sep 18, 2018 · N118US · Airbus A320214 · Escape SlideSDR AALA201809139017Fitting · wornWEAR FOUND ON THE PASSENGER DOOR FITTING FOR THE SLIDE RAFT. REPLACED THE SLIDE RAFT FITTING IAW CMM 52-11-15-400-801-A 01, SUBTASK 52-11-15-400-002-A01, STEP A (7).Sep 12, 2018 · N118US · Airbus A320214 · Escape SlideSDR AALA201809139016Fitting · wornWEAR FOUND ON THE PASSENGER DOOR FITTING FOR THE SLIDE RAFT. REPLACED THE SLIDE FITTING IAW CMM 52-11-15-400-801-A 01, SUBTASK 52-11-15-400-002-A01, STEP A (7).Sep 12, 2018 · N118US · Airbus A320214 · Escape SlideSDR AALA201809139005Cylinder · malfunctionedDURING AN OPERATIONAL TEST OF THE PASSENGER CREW DOOR DAMPING FUNCTION, FOUND A HARD IMPACT BETWEEN FUSELAGE AND BUFFER OF THE DOOR AT AFT GALLEY AREA. REPLACED THE DAMPER CYLINDER IAW AMM 52-13-14-400-001-B.Sep 12, 2018 · N118US · Airbus A320214 · Emergency EquipmentSDR AALA2018091439029Door · out of adjustAIRCRAFT IN BASE MAINTENANCE: OUT OF ADJUSTMENT PASSENGER CREW DOOR 832, RIGGING POINT DOOR HIGH LOCKING MECHANISM (LOWERING SHAFT) AT AFT GALLEY AREA. ADJUSTED RIGGING POINT PER AMM 52-13-21-400-001-A STEP 4.C(17)(A)(B)(F) THRU (K) AND (P).Sep 11, 2018 · N118US · Airbus A320214 · Passenger/Crew DoorsSDR AALA201809179042Bolt · corrodedCORROSION FOUND ON THE RIGHT WING NR 11 SLAT TRACK UPPER BOLT. REPLACED THE BOLT IAW AMM 27-84-67Sep 7, 2018 · N118US · Airbus A320214 · Leading Edge DevicesSDR AALA201810089043Fitting · crackedAIRCRAFT IN BASE MAINTENANCE. FRONT WINDSHIELD FRAME CONTINUITY FITTING AT FR 2 AND Y88R. REPLACED FRONT WINDSHIELD FRAME CONTINUITY FITTING PER EA 284102.Sep 6, 2018 · N118US · Airbus A320214 · Fuselage Miscellaneous StructureSDR AALA201810089042Fitting · crackedAIRCRAFT IN BASE MAINTENANCE. FRONT WINDSHIELD FRAME CONTINUITY FITTING AT FR 2 AND Y88L. REPLACED FRONT WINDSHIELD FRAME CONTINUITY FITTING PER EA 284102.Sep 6, 2018 · N118US · Airbus A320214 · Fuselage Miscellaneous StructureSDR AALA201809079013Seal · chafedCHAFED PRESSURE SEAL ON THE PASSENGER DOOR LOWER AREA. REPLACED THE PRESSURE SEAL IAWAMM 52-11-18-400-001-A.Sep 4, 2018 · N118US · Airbus A320214 · Passenger/Crew DoorsSDR AALA201809059005Mechanism · out of adjustAIRCRAFT WAS IN BASE MAINTENANCE. PASSENGER DOOR RIGGING POINT, DOOR HIGH LOCKING MECHANISM LOWERING SHAFT WAS OUT OF ADJUSTMENT. ADJUSTED THE RIGGING POINT HIGH LOCKING MECHANISM LOWERING SHAFT IAW AMM 52-13-21-400-001-A STEP 4.Sep 2, 2018 · N118US · Airbus A320214 · Passenger/Crew DoorsSDR AALA201809259005Floor Panel · delaminatedFLOOR PANEL 212EF DELAMINATED IN THE COCKPIT. REPLACED THE FLOOR PANEL IAW SRM 53-12-00-300-006, FIGURE 20106.Sep 1, 2018 · N118US · Airbus A320214 · Fuselage Floor PanelSDR AALA201809189005Fitting · corrodedCORROSION ON LOWER SILL AFT CORNER FITTING AT FR 20 AND S23L. REPLACED AFT CORNER FITTING PER SRM 51-72-11 AND 51-42-11.Sep 1, 2018 · N118US · Airbus A320214 · Fuselage Miscellaneous StructureSDR AALA201809189004Fitting · corrodedCORROSION FOUND ON THE LOWER SILL CENTER FITTING BETWEEN FRAMES 16 AND 20, STRINGER 23L. REPLACED THE FITTING IAW SRM 51-72-11, AND 51-42-11.Sep 1, 2018 · N118US · Airbus A320214 · Fuselage Miscellaneous StructureSDR AALA201809289007Fitting · corrodedCORROSION FOUND ON THE SILL FITTING FWD LT, UNDERNEATH THE FWD AND AFT GIRT BAR ATTACH FITTINGS. BETWEEN FRAMES 16 TO 20, STRINGER 23L. REPLACED SILL FITTING IAW SRM 51-72-11, SRM 51-42-11, AND DWG D5311033.Aug 31, 2018 · N118US · Airbus A320214 · Fuselage Main, Attach FittingsSDR AALA201810049014Hinge Fitting · crackedRIGHT MAIN LANDING GEAR DOOR FORWARD ATTACHMENT HINGE FITTING ON THE KEEL BEAM AT FRAME 42. REPLACED THE HINGE FITTING IAW EA 285074.Aug 29, 2018 · N118US · Airbus A320214 · Fuselage, Door HingeSDR AALA2018092109008Bolt · corrodedCORROSION ON RIGHT WING NR 3 FLAP TRACK PIVOT BOLT. REPLACED THE BOLT IAW AMM 27-54-62-400-001-A.Aug 29, 2018 · N118US · Airbus A320214 · Trailing Edge FlapsSDR AALA2018092109007Bolt · corrodedCORROSION ON THE RIGHT WING NR 2 FLAP TRACK PIVOT BOLT. REPLACED THE BOLT IAW AMM 27-54-62-400-001-A.Aug 29, 2018 · N118US · Airbus A320214 · Trailing Edge FlapsSDR AALA2018091429005Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION FOUND ON THE RT WING TRAILING EDGE FLAP TRACK NR 4 PIVOT BOLT. REPLACED THE PIVOT BOLT IAW AMM 27-54-62-400-001.Aug 29, 2018 · N118US · Airbus A320214 · Trailing Edge FlapsSDR AALA2018100919007Support · corrodedCORROSION FOUND ON SUPPORT, FRAME 66 TO 68, STRINGER 23R. REPLACED THE SUPPORT IAW SRM 51-72-11, 51-42-11, AND DRAWING D53480505.Aug 26, 2018 · N118US · Airbus A320214 · Fuselage Miscellaneous StructureSDR AALA201810089036Shear Plate · crackedAIRCRAFT IN BASE MAINTENANCE. CRACKED SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23L. REPLACED SHEAR PLATE PER SRM 51-72-11 AND 51-42-11.Aug 26, 2018 · N118US · Airbus A320214 · Fuselage Miscellaneous StructureSDR AALA2018100819006Tray · crackedCRACKED TRAY BETWEEN FRAMES 68 TO 69, STRINGER 23L. REPLACED THE TRAY IAW SRM 51-72-11, 51-42-11, AND DRAWING D53480019.Aug 26, 2018 · N118US · Airbus A320214 · Fuselage Miscellaneous StructureSDR AALA2018100819005Fitting · crackedCRACKED INTERCOSTAL FITTING AT FRAME 20, RIGHT SIDE AT THE NR 7 DOOR STOP FITTING. REPLACED THE INTERCOSTAL FITTING IAW SRM 51-72-11 AND 51-42-11.Aug 25, 2018 · N118US · Airbus A320214 · Fuselage Miscellaneous StructureSDR AALA2018100219018Fitting · crackedCRACKED INTERCOSTAL FITTING AT FRAME 16, NR 7 DOOR STOP FITTING. REPLACED THE INTERCOSTAL FITTING IAW SRM 51-72-11.Aug 25, 2018 · N118US · Airbus A320214 · Fuselage Miscellaneous StructureSDR AALA2018100219017Fitting · crackedCRACKED INTERCOSTAL FITTING AT FRAME 16, NR 7 DOOR STOP FITTING. REPLACED THE INTERCOSTAL FITTING IAW SRM 51-72-11.Aug 25, 2018 · N118US · Airbus A320214 · Fuselage Miscellaneous StructureSDR AALA2018100219016Fitting · crackedCRACKED INTERCOSTAL FITTING AT FRAME 16, NR 7 DOOR STOP FITTING. REPLACED INTERCOSTAL FITTING IAW SRM 51-72-11 AND 51-42-11.Aug 25, 2018 · N118US · Airbus A320214 · Fuselage Miscellaneous StructureSDR AALA201809289002Hinge Fitting · excess playEXCESSIVE PLAY ON THE AFT DOOR HINGE FITTING, NOSE LANDING GEAR DOOR. REPLACED THE AFT DOOR HINGE FITTING IAW CMM 52-82-32, AND SRM A320 51-72-11.Aug 25, 2018 · N118US · Airbus A320214 · Landing Gear DoorsSDR AALA201809289001Hinge Fitting · excess playEXCESSIVE PLAY FOUND ON THE FORWARD AFT DOOR HINGE FITTING ON THE NOSE LANDING GEAR DOOR. REPLACED THE HINGE FITTING IAW CMM 52-82-32, AND SRM 51-72-11.Aug 25, 2018 · N118US · Airbus A320214 · Landing Gear DoorsSDR AALA201809249005Hinge Fitting · excess playTHE AFT HINGE FITTING ON THE NOSE LANDING GEAR, RT DOOR WAS FOUND TO BE LOOSE AND HAVE EXCESSIVE PLAY. REPLACED THE HINGE FITTING IAW SRM 51-72-11, AND CMM 52-82-32.Aug 25, 2018 · N118US · Airbus A320214 · Landing Gear DoorsSDR AALA201809249004Hinge Fitting · excess playTHE FORWARD HINGE FITTING ON THE NOSE LANDING GEAR FORWARD RT DOOR WAS FOUND TO BE LOOSE AND HAVE EXCESSIVE PLAY. REPLACED THE HINGE FITTING IAW SRM 51-72-11, AND CMM 52-82-32-400-805.Aug 25, 2018 · N118US · Airbus A320214 · Landing Gear DoorsSDR AALA2018092179060Floor Panel · delaminatedDELAMINATION ON FLOOR PANEL 231LF. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-011.Aug 25, 2018 · N118US · Airbus A320214 · Fuselage Floor PanelSDR AALA201809189007Floor Panel · corrodedCORROSION FOUND ON FLOOR PANEL 222FF IN THE FORWARD GALLEY. REPLACED THE FLOOR PANEL IAW AMM 53-00-00.Aug 25, 2018 · N118US · Airbus A320214 · Fuselage Floor PanelSDR AALA2018091879040Floor Panel · delaminatedDELAMINATION FOUND ON FLOOR PANEL 231KF. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-011, AND IRM 9701, REV H.Aug 25, 2018 · N118US · Airbus A320214 · Fuselage Floor PanelSDR AALA2018091879039Floor Panel · delaminatedDELAMINATION FOUND ON FLOOR PANEL 261BG. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-011, AND IRM 9701, REV H.Aug 25, 2018 · N118US · Airbus A320214 · Fuselage Floor PanelSDR AALA2018091879038Floor Panel · delaminatedDELAMINATION FOUND ON FLOOR PANEL 251WF. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-011, AND IRM 9701, REV H.Aug 25, 2018 · N118US · Airbus A320214 · Fuselage Floor PanelSDR AALA2018091439003Floor Panel · delaminatedCABIN FLOOR PANEL 252GF DELAMINATED. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-011, AND IRM 9701, REV H.Aug 25, 2018 · N118US · Airbus A320214 · Fuselage Floor PanelSDR AALA201809149017Floor Panel · delaminatedDELAMINATION FOUND ON FLOOR PANEL 231FF IN THE FORWARD GALLEY. REPLACED THE FLOOR PANEL IAW SRM 53-12-00-300-006, FIGURE 20106, AND IRM 9701, REVISION H.Aug 25, 2018 · N118US · Airbus A320214 · Fuselage Floor PanelSDR AALA201809149016Floor Panel · delaminatedDELAMINATION FOUND ON FLOOR PANEL 231BF IN THE FORWARD GALLEY. REPLACED THE FLOOR PANEL IAW SRM 53-12-00-300-006, FIGURE 20106, AND IRM 9701, REVISION H.Aug 25, 2018 · N118US · Airbus A320214 · Fuselage Floor PanelSDR AALA201809129004Floor Panel · delaminatedDELAMINATION FOUND ON FLOOR PANEL 261DF, FRAMES 66 TO 68, BETWEEN -Y765 TO Y765, IN THE AFT GALLEY. REPLACED THE FLOOR PANEL IAW AMM 53-00-00-400-801-A, AND SRM 51-72-11.Aug 25, 2018 · N118US · Airbus A320214 · Fuselage Floor PanelSDR AALA2018090769002Floor Panel · delaminatedDELAMINATION ON FLOOR PANEL 261AG, FRAMES 64 TO 66, Y512.5 TO -Y464.5. REPLACED THE FLOOR PANEL IAW AMM 53-00-00-400-801-A, AND SRM 51-72-11.Aug 25, 2018 · N118US · Airbus A320214 · Fuselage Floor PanelSDR AALA201809069003Floor Panel · delaminatedDELAMINATION FOUND ON FLOOR PANEL 262BG IN THE AFT GALLEY AREA. REPLACED THE FLOOR PANEL IAW AMM 53-00-00-400-801-A, AND SRM 51-72-11.Aug 25, 2018 · N118US · Airbus A320214 · Fuselage Floor PanelSDR AALA201810089046Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE. FRONT WINDSHIELD FRAME CRACKED BETWEEN FR 1 AND FR 4 AND +Y675 AND -Y675. REPAIRED FRONT WINDSHIELD FRAME PER EA 284085.Aug 23, 2018 · N118US · Airbus A320214 · Fuselage Main, StructureSDR AALA201810089037Skin · crackedAIRCRAFT IN BASE MAINTENANCE. FUSELAGE SKIN CRACKED AT FR 35 AND S30L. REPAIRED SKIN PER EA 284027.Aug 23, 2018 · N118US · Airbus A320214 · Fuselage Main, Plate/SkinSDR AALA201810089045Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE. CRACKED LATERAL WINDOW FRAME BETWEEN FR 4 AND FR 8. REPAIRED LATERAL WINDOW FRAME PER EA 284313.Aug 22, 2018 · N118US · Airbus A320214 · Fuselage Main, StructureSDR AALA201810089041Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE. CRACKED LATERAL WINDOW FRAME BETWEEN FR 4 AND FR 8. REPAIRED LATERAL WINDOW FRAME PER EA 284314.Aug 22, 2018 · N118US · Airbus A320214 · Fuselage Main, StructureSDR AALA2018091879044Floor Panel · delaminatedDELAMINATION FOUND ON FLOOR PANEL 131AF. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-011, AND IRM 9701, REV H.Aug 21, 2018 · N118US · Airbus A320214 · Fuselage Floor PanelSDR AALA2018091879037Floor Panel · delaminatedDELAMINATION FOUND ON FLOOR PANEL 151AF. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-011, AND IRM 9701, REV H.Aug 21, 2018 · N118US · Airbus A320214 · Fuselage Floor Panel
Back to N118US