N819AW

Service difficulty reports · 238

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 = 'N819AW' 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 AALA202507251452Light · burnedAIRCRAFT IN BASE MAINTENANCE: BURNED EMERGENCY EXIT LIGHT ON CEILING PANELS INPASSENGER CABIN. MAINTENANC REPLACED EMERGENCY EXIT LIGHT ON CEILING PANEL IN PASSENGER CABIN AND PERFORMED TEST IAW AMM 33-51-16-000-001-A AND AMM 33-51-16-400-001-A.Jul 20, 2025 · N819AW · Airbus A319132 · Emergency LightingSDR AALA202507216168Fitting · wornAIRCRAFT IN BASE MAINTENANCE: ELONGATED HOLE H2 ON ANGLE FITTING LOC ON EXTERNAL SKIN FR35 RH SIDE A ND STRG 30R LOWER FUSELAGE L= 0.068 IN. MAINTENANCE REPLACED ANGLE FITTING LOC ON EXTERNAL SKIN FR35 RH SIDE AND STRG 30R IAW EA 292392B.Jul 16, 2025 · N819AW · Airbus A319132 · Fuselage Internal Mounting StructureSDR AALA202507160102Bottle · no testAIRCRAFT IN BASE MAINTENANCE: PASSENGER / CREW DOOR 832 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER DOES NOT PASS THE DOOR DAMPING FUNCTION OPERATIONAL TEST. REPLACED THE DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-13-14.Jul 15, 2025 · N819AW · Airbus A319132 · Passenger/Crew DoorsSDR AALA202507088171Light · burned outAIRCRAFT IN BASE MAINTENANCE: BURNED EMERGENCY EXIT LIGHT IN PASSENGER CREW DOOR 841 (UPPER) AT FWD GALLEY AREA. MAINTENANCE REPLACED EMERGENCY EXIT LIGHT IN PASSENGER CREW DOOR 841 IAW AMM 33-51-16-000-001-A STEP 4.A AND AMM 33-51-16-400-001-A STEP 4.A THRUJul 7, 2025 · N819AW · Airbus A319132 · Emergency LightingSDR AALA202507088340Light · burned outAIRCRAFT IN BASE MAINTENANCE: BURNED EMERGENCY EXIT LIGHT IN PASSENGER CREW DOOR 831 (UPPER) AT FWD GALLEY AREA. MAINTENANCE REPLACED EMERGENCY EXIT LIGHT IN PASSENGER CREW DOOR 831 IAW AMM 33-51-16-000-001-A STEP 4.A AND AMM 33-51-16-400-001-A STEP 4.A THRUJul 7, 2025 · N819AW · Airbus A319132 · Emergency LightingSDR AALA202507146680Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK EXTERNAL SKIN BTW FR69-FR70 STR23R, L=0.362 INCHES.Jun 23, 2025 · N819AW · Airbus A319132 · Fuselage Main, Plate/SkinSDR AALA202506249394Light · no testAIRCRAFT IN BASE MAINTENANCE: BURNED EMERGENCY EXIT LIGHT IN PASSENGER CREW DOOR 842 AT AFT GALLEY AREA. REPLACED EMERGENCY EXIT LIGHT ASSY IN PASSENGER CREW DOOR 842 AT AFT GALLEY AREA IAW AMM 33-51-16-000-001-A STEP 4.A AND AMM 33-51-16-400-001-A STEP 4.B.Jun 21, 2025 · N819AW · Airbus A319132 · Emergency LightingSDR AALA202506249926Light · no testAIRCRAFT IN BASE MAINTENANCE: BURNED EMERGENCY EXIT LIGHT IN PASSENGER CREW DOOR 832 AT AFT GALLEY AREA. MAINTENANCE REPLACED EMERGENCY EXIT LIGHT ASSY IN PASSENGER CREW DOOR 832 AT AFT GALLEY AREA IAW AMM 33-51-16-000-001-A STEP 4.A AND AMM 33-51-16-400-001-Jun 21, 2025 · N819AW · Airbus A319132 · Emergency LightingSDR AALA202506243514Hinge Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON FITTING HINGE OF MLG DOOR AT LH SIDE KEEL BEAM, FWD LUG IN LOWER WEB POCKET RADIUS. CRACK LENGTH IS 0.085 INCH APPROX. MAINTENANCE PERFORMED PERMANENT REPAIR LH MLG DOOR HINGE FITTING IAW EA 365227 AND DWG R533Jun 19, 2025 · N819AW · Airbus A319132 · Fuselage, Door HingeSDR AALA202506251345Panel · elongatedAIRCRAFT IN BASE MAINTENANCE: ELONGATED HOLES WAS FOUND ON DOOR REINFORCEMENT PANEL (D53480041) ON FRAME 68 RH SIDE AT LEVEL ON STRINGER 9R W=0.210 INCH. MAINTENANCE REPLACED DOOR REINFORCEMENT PANEL AND FASTENERS LOC FRAME 68 RH SIDE AT LEVEL ON STRINGER 9R IJun 12, 2025 · N819AW · Airbus A319132 · Fuselage Main, StructureSDR AALA202506244578Tray · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK ON TRAY LOCATED BTW FR 68 TO FR 69 AND STRG 23R L= 0.077 INCH. MAINTENANCE REPLACED SHEET SHEAR (TRAY) LOCATED BTW FR 68 TO FR 69 AND STRG 23R IAW A319 SRM 51-72-11-911-001 AND DWG D53480019.Jun 10, 2025 · N819AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AALA202506130948Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK ON INTERCOSTAL (HOLE 3) FITTING LOCATED FR 20 RH SIDE AT LEVEL STR 22 AND AT LEVEL DOOR STOP FITTING 1. CRACK DEPTH =0.055 INCH. MAINTENANCE REPLACED INTERCOSTAL FITTING LOCATED FR 20 AT LEVEL STR 22R AND AT LEVEL DOOR STOPMay 21, 2025 · N819AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AALA202505121643Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY FWD BEARING MAIN DOOR AT LH MAIN LANDING GEAR. MAINTENANCE REPLACED AND DRILLED NEW HINGE FITTING ASSY LOCATED AT MAIN DOOR ON LH MAIN LANDING GEAR IAW AIRBUS CMM 52-81-18 AND A319 SRM51-44-11-801.May 10, 2025 · N819AW · Airbus A319132 · Fuselage, Door HingeSDR AALA202505120826Bearing · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY FWD BEARING MAIN DOOR ON RH MAIN LANDING GEAR. MAINTENANCE REPLACED AND DRILLED NEW HINGE FITTING ASSY LOCATED AT MAIN DOOR ON RH MAIN LANDING GEAR IAW AIRBUS CMM 52-81-18 AND A319 SRM 51-44-11-801.May 10, 2025 · N819AW · Airbus A319132 · Fuselage, Landing Gear Attach FittingsSDR AALA202505121654Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY BEARING HINGE ARM 3 ELEVATOR ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM END FITTING 3 ON LH HORIZONTAL STABILIZER IAWAMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A,May 9, 2025 · N819AW · Airbus A319132 · Elevator StructureSDR AALA202507069236Hinge Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON FITTING HINGE OF MLG DOOR AT RH SIDE KEEL BEAM, AFT LUG IN LOWER WEB POCKET RADIUS. CRACK LENGTH IS 0.095 INCH APPROX, IN MAIN WHEEL WELL. MAINTENANCE PERFORMED PERMANENT REPAIR ON RH MLG DOOR HINGE FITTING ( Apr 28, 2025 · N819AW · Airbus A319132 · Fuselage, Door HingeSDR AALA202505272497Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION SPIGOT FITTING LOWER ON RH PYLON MEASURE OF THE DAMAGE ARE: L= 13.50 INCH, W= 1.335 INCH, D= 0.006 INCH. MAINTENANCE REPLACED SPIGOT FITTING LOWER ON RH PYLON BTW SRA 679 TO SRA 829 A319 SRM 54-51-12-300-001.Apr 25, 2025 · N819AW · Airbus A319132 · Nacelle/Pylon, Main FrameSDR AALA202505202458Attach Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION AFT ATTACH FITTING AROUND UPPER HOLE AT FWD PART ON LH PYLON MEASURE OF CORROSION ARE L=1.94 INCH, W=0.16 INCH, D=0.002 INCH. MAINTENANCE REPLACED AFT ATTACH FITTING.Apr 25, 2025 · N819AW · Airbus A319132 · Nacelle/Pylon, Attach FittingsSDR AALA202505085893Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY BEARING HINGE ARM 6 ELEVATOR ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM 6 END FITTING ON LH ELEVATOR HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.Apr 23, 2025 · N819AW · Airbus A319132 · Elevator StructureSDR AALA202505087923Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY BEARING HINGE ARM 5 ELEVATOR ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM 5 END FITTING ON LH ELEVATOR HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.Apr 23, 2025 · N819AW · Airbus A319132 · Elevator StructureSDR AALA202505089530Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY BEARING HINGE ARM 4 ELEVATOR ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM 4 END FITTING ON LH ELEVATOR HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.Apr 23, 2025 · N819AW · Airbus A319132 · Elevator StructureSDR AALA202505082937Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY BEARING HINGE ARM 2 ELEVATOR ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM 2 END FITTING ON LH ELEVATOR HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.Apr 23, 2025 · N819AW · Airbus A319132 · Elevator StructureSDR AALA202505082161Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY BEARING HINGE ARM 1 ELEVATOR ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM 1 END FITTING ON LH ELEVATOR HORIZONTAL STABILIZER (1EA) IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A. REFER TO INDIVApr 23, 2025 · N819AW · Airbus A319132 · Elevator StructureSDR AALA202504294791Attach Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ON BEARING AFT FIXED FAIRING RH FWD SIDE. MSINTENANCE REPLACED FWD ATTACH FITTING AFT FIXED FAIRING RH PYLON. IAW DWGD54530016 ISSUE D, A319 SRM 51-42-11-801, A319 SRM 51-44-11-801,A319 SRM 51-72-11-911-001, A319 SRApr 21, 2025 · N819AW · Airbus A319132 · Nacelle/Pylon Miscellaneous StructureSDR AALA202507251354Beam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FROM ZONE 2 HOLE LOCATED AT CENTER WING BOX FRONT SPAR VERTICAL STRINGER AT FR 36 AND Y 254 L= 0.130IN. MAINTENANCE PERFORMED INTERIM REPAIR INSTRUCTION (REPAIR BUSHING) ZONE 2 HOLE LOCATED AT CENTER WING BOX FRONApr 20, 2025 · N819AW · Airbus A319132 · Fuselage Main, StructureSDR AALA202507214424Floorbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FROM ZONE 1 RADIUS LOCATED AT CENTER WING BOX FRONT S PAR VERTICAL STRINGER AT FRAME 36 AND Y765 LEVEL AT FWD CARGO COMPARTM ENT. CRACK LENGTH IS 0.170 INCH. MAINTENANCE PERFORMED REPAIR LOCATED AT CENTER WING BOXApr 20, 2025 · N819AW · Airbus A319132 · Fuselage Main, Floor BeamSDR AALA202507211260Floorbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FROM ZONE 1 HOLE LOCATED AT CENTER WING BOX FRONT SPAR VERTICAL STINGER AT FRAME 36 AND Y-254 FWD CARGO COMPARTMENT L= 0.141 INCH. MAINTENANCE PERFORMED REPAIR (SPLICE REPAIR) LOCATED AT CENTER WING BOX FRONT SPARApr 20, 2025 · N819AW · Airbus A319132 · Fuselage Main, Floor BeamSDR AALA202505080845Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ON BEARING ELEVATOR RH HINGE ARM END FITTING #2. MAINTENANCE REPLACED HINGE ARM END FITTING #2 ON RH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.Apr 20, 2025 · N819AW · Airbus A319132 · Elevator StructureSDR AALA202505082269Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ON BEARING ELEVATOR RH HINGE ARM END FITTING #6. MAITNENANCE REPLACED HINGE ARM END FITTING #6 ON RH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.Apr 20, 2025 · N819AW · Airbus A319132 · Elevator StructureSDR AALA202505085223Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ON BEARING ELEVATOR RH HINGE ARM END FITTING #5. MAINTENANCE REPLACED HINGE ARM END FITTING #5 ON RH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.Apr 20, 2025 · N819AW · Airbus A319132 · Elevator StructureSDR AALA202505082101Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ON BEARING ELEVATOR RH HINGE ARM END FITTING #4. MAINTENANCE REPLACED HINGE ARM END FITTING #4 ON RH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.Apr 20, 2025 · N819AW · Airbus A319132 · Elevator StructureSDR AALA202505082359Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ON BEARING ELEVATOR RH HINGE ARM END FITTING #3. MAINTENANCE REPLACED HINGE ARM END FITTING #3 ON RH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.Apr 20, 2025 · N819AW · Airbus A319132 · Elevator StructureSDR AALA202505084403Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ON HINGE FITTING #1 ELEVATOR RH. REPLACED HINGE ARM END FITTING #1 ON RH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.Apr 20, 2025 · N819AW · Airbus A319132 · Elevator StructureSDR AALA202505204988Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND IN OPEN FASTENER HOLE H4 ON FRAME 20 RH SIDE , DOOR STOP FITTING 7. CRACK DIRECTION IS: 11 OCLOCK; CRACK DEPTH IS : 0 .158 INCH APPROX. MAINTENANCEApr 19, 2025 · N819AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AALA202505204868Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND IN OPEN FASTENER HOLE H3 ON FR16 LH, DOOR STOP FITTING 7, CRACK DIRECTION IS 3 O CLOCK, CRACK DEPTH IS 0.157 INCH APPROX. MAINTENANCE REPLACED INTERCOSTAL FITTING LOCATED BTW FR15 TO FR16 LH SIDE AT LEVEL BTApr 19, 2025 · N819AW · Airbus A319132 · Fuselage Main, StructureSDR AALA202505150887Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND IN OPEN FASTENER HOLE H3 ON FRAME 16 RH SIDE, DOOR STOP FITTING 1 CRACK DIRECTION IS: 9 OCLOCK; CRACK DEPTH IS: 0.158 INCH. MAINTENANCE REPLACED INTERCOSTAL FITTING BTW FR15 TO FR16 RH SIDE AT LEVEL DOOR STOApr 19, 2025 · N819AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AALA202505151028Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND IN OPEN FASTENER HOLE H1 ON FRAME 16 RH SIDE, DOOR STOP FITTING 7 (CRACK L: 0.168 INCH). MAINTENANCE REPLACED INTERCOSTAL FITTING AND FASTENERS BTW FR15 TO FR 16 RH SIDE AT LEVER DOOR STOP FITTING 7 IAW A319Apr 19, 2025 · N819AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AALA202505131028Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND IN OPEN FASTENER HOLE H1 ON FRAME 16 RH SIDE, DOOR STOP FITTING 7 (CRACK L: 0.168 INCH). MAINTENANCE REPLACED INTERCOSTAL FITTING AND FASTENERS BTW FR15 TO FR 16 RH SIDE AT LEVER DOOR STOP FITTING 7 IAW A319Apr 19, 2025 · N819AW · Airbus A319132 · Fuselage Main, StructureSDR AALA202505209566Stiffener · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK STIFFENER ASSY UPPER POSITION FR1 ON FWD PRESSURE BULKHEAD. L=1.170 INCH. MAINTENANCE REPLACED STIFFENER ASSY LOCATED UPPER POSITION FR1 AND Z-169 ON FORWARD PRESSURE BULKHEAD IAW A319 SRM 51-72-11-911-001, SRM 51-42-11-801 Apr 18, 2025 · N819AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AALA202507210112Shear Plate · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK SHEAR PLATE STR 23 R BTW FR69 TO FR70 AT AFT GALLEY AREA MEASURE CRACK ON SHEAR PLATE IS: L= 0.643 INCH. MAINTENANCE REPLACED SHEAR PLATE ON LOC STR 23R BTW FR69 TO FR70 AT AFT GALLEY AREA IAW A319 SRM 51-42-11-801 AND DWGApr 17, 2025 · N819AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AALA202507180914Shear Plate · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK SHEAR PLATE STR 23L BTW FR69 TO FR70 AT AFT GALLEY AREA. (L: 0.658 IN, W: 0.055 IN). MAINTENANCE REPLACED SHEAR PLATE LOC, STR 23L BTW FR69 TO FR70 AT AFT GALLEY AREA IAW A319 SRM 51-42-11-801 AND SRM 51-72-11-911-001 AND DRApr 17, 2025 · N819AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR AALA202507257127Window Post · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON UPPER RADIUS OF WINDSHIELD CENTER POST LOWER ATTACHMENT AREA INTERNAL SIDE LH. MAINTENANCE PERFORMED TIME LIMITED REPAIR LOC WINDSHIELD CENTER POST LOWER ATTACHMENT AREA INTERNAL FRAME 2 Y0 SIDE LH AND RHApr 16, 2025 · N819AW · Airbus A319132 · Fuselage Main, StructureSDR AALA202507259901Window Post · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON UPPER RADIUS OF WINDSHIELD CENTER POST LOWER ATTACHMENT AREA INTERNAL SIDE LH. CRACK L= 0.160 INCH. MAINTENANCE PERFORMED TIME LIMITED REPAIR LOC WINDSHIELD CENTER POST LOWER ATTACHMENT AREA INTERNAL FRAMApr 16, 2025 · N819AW · Airbus A319132 · Fuselage Main, StructureSDR AALA202507218300Attach Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: REPLACE RH LOWER LATERAL FITTING OF THE ELECTRONICS RACK FIN 80VU PER EA 364061. MAINTENACNE PERFORMED INTERIM REPAIR LOCATED 80VU AREA RH LOWER LATERAL FITTING IAW EA 364061.Apr 16, 2025 · N819AW · Airbus A319132 · Fuselage Main, Attach FittingsSDR AALA202507078655Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON CONTINUITY FITTING ON WINDSHIELD AREA LOWER ATTACHMENT AREA INTERNAL SIDE RH L= 0.200 IN. MAINTENANCE PERFORMED TIME LIMITED REPAIR, REPLACED CONTINUITY FITTING IN WINDSHIELD RH SIDE IAW EA 363987.Apr 16, 2025 · N819AW · Airbus A319132 · Fuselage Main, StructureSDR AALA202507076746Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON CONTINUITY FITTING OF WINDSHIELD AREA LOWER ATTACHMENT AREA INTERNAL SIDE LH L= 0.200 IN. PERFORMED TIME LIMITED REPAIR, REPLACED CONTINUITY FITTING IN WINDSHIELD LH SIDE IAW EA 363987.Apr 16, 2025 · N819AW · Airbus A319132 · Fuselage Main, StructureSDR AALA202506138660Fitting · burredAIRCRAFT IN BASE MAINTENANCE: BURRED MATERIAL ON LH LOWER LATERAL FITTING OF THE ELECTRONICS RACK FIN 80VU, W=0.485 INCH. MAINTENANCE PERFORMED INTERIM REPAIR LOCATED 80VU AREA LH LOWER LATERAL FITTING IAW EA 364061.Apr 16, 2025 · N819AW · Airbus A319132 · Fuselage Main, StructureSDR AALA202505024913Hinge Pin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION AILERON HINGE PIN 5 ON RH WING L= 0.011 IN W= 0.016 IN D= 0.001 IN. MAINTENANCE REPLACED HINGE PIN 5 ON RH WING.Apr 15, 2025 · N819AW · Airbus A319132 · AileronsSDR AALA202505024253Hinge Pin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AILERON HINGE PIN 4 ON RH WING L= 0.009 IN W= 0.017 IN D= 0.003 IN. MAINTENANCE REPLACED HINGE PIN.Apr 15, 2025 · N819AW · Airbus A319132 · AileronsSDR AALA202506135460Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND LATERAL WINDOW FRAME HORIZONTAL UPPER STIFFENER FR4 LH L= 0.125 IN. MAINTENANCE PERFORMED TIME LIMITED REPAIR LOC LATERAL WINDOW FRAME HORIZONTAL UPPER STIFFENER FR 4 LH AND Y511 IAW EA 364298 AND A319 SRM 5Apr 14, 2025 · N819AW · Airbus A319132 · Fuselage Main, Structure
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