# Service difficulty reports: N819AW

A list on [N819AW](https://openairdocs.org/aircraft/N819AW.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 5 · 238 reports

- [SDR AALA202507251452](https://openairdocs.org/sdr/AALA202507251452.md): Light · burned · Jul 20, 2025 · N819AW · Airbus A319132 · Emergency Lighting
  > AIRCRAFT 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.
- [SDR AALA202507216168](https://openairdocs.org/sdr/AALA202507216168.md): Fitting · worn · Jul 16, 2025 · N819AW · Airbus A319132 · Fuselage Internal Mounting Structure
  > AIRCRAFT 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.
- [SDR AALA202507160102](https://openairdocs.org/sdr/AALA202507160102.md): Bottle · no test · Jul 15, 2025 · N819AW · Airbus A319132 · Passenger/Crew Doors
  > AIRCRAFT 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.
- [SDR AALA202507088171](https://openairdocs.org/sdr/AALA202507088171.md): Light · burned out · Jul 7, 2025 · N819AW · Airbus A319132 · Emergency Lighting
  > AIRCRAFT 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 THRU
- [SDR AALA202507088340](https://openairdocs.org/sdr/AALA202507088340.md): Light · burned out · Jul 7, 2025 · N819AW · Airbus A319132 · Emergency Lighting
  > AIRCRAFT 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 THRU
- [SDR AALA202507146680](https://openairdocs.org/sdr/AALA202507146680.md): Skin · cracked · Jun 23, 2025 · N819AW · Airbus A319132 · Fuselage Main, Plate/Skin
  > AIRCRAFT IN BASE MAINTENANCE: CRACK EXTERNAL SKIN BTW FR69-FR70 STR23R, L=0.362 INCHES.
- [SDR AALA202506249394](https://openairdocs.org/sdr/AALA202506249394.md): Light · no test · Jun 21, 2025 · N819AW · Airbus A319132 · Emergency Lighting
  > AIRCRAFT 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.
- [SDR AALA202506249926](https://openairdocs.org/sdr/AALA202506249926.md): Light · no test · Jun 21, 2025 · N819AW · Airbus A319132 · Emergency Lighting
  > AIRCRAFT 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-
- [SDR AALA202506243514](https://openairdocs.org/sdr/AALA202506243514.md): Hinge Fitting · cracked · Jun 19, 2025 · N819AW · Airbus A319132 · Fuselage, Door Hinge
  > AIRCRAFT 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 R533
- [SDR AALA202506251345](https://openairdocs.org/sdr/AALA202506251345.md): Panel · elongated · Jun 12, 2025 · N819AW · Airbus A319132 · Fuselage Main, Structure
  > AIRCRAFT 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 I
- [SDR AALA202506244578](https://openairdocs.org/sdr/AALA202506244578.md): Tray · cracked · Jun 10, 2025 · N819AW · Airbus A319132 · Fuselage Miscellaneous Structure
  > AIRCRAFT 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.
- [SDR AALA202506130948](https://openairdocs.org/sdr/AALA202506130948.md): Fitting · cracked · May 21, 2025 · N819AW · Airbus A319132 · Fuselage Miscellaneous Structure
  > AIRCRAFT 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 STOP
- [SDR AALA202505121643](https://openairdocs.org/sdr/AALA202505121643.md): Hinge Fitting · excess play · May 10, 2025 · N819AW · Airbus A319132 · Fuselage, Door Hinge
  > AIRCRAFT 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.
- [SDR AALA202505120826](https://openairdocs.org/sdr/AALA202505120826.md): Bearing · excess play · May 10, 2025 · N819AW · Airbus A319132 · Fuselage, Landing Gear Attach Fittings
  > AIRCRAFT 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.
- [SDR AALA202505121654](https://openairdocs.org/sdr/AALA202505121654.md): Hinge Fitting · excess play · May 9, 2025 · N819AW · Airbus A319132 · Elevator Structure
  > AIRCRAFT 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,
- [SDR AALA202507069236](https://openairdocs.org/sdr/AALA202507069236.md): Hinge Fitting · cracked · Apr 28, 2025 · N819AW · Airbus A319132 · Fuselage, Door Hinge
  > AIRCRAFT 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 (
- [SDR AALA202505272497](https://openairdocs.org/sdr/AALA202505272497.md): Fitting · corroded · Apr 25, 2025 · N819AW · Airbus A319132 · Nacelle/Pylon, Main Frame
  > AIRCRAFT 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.
- [SDR AALA202505202458](https://openairdocs.org/sdr/AALA202505202458.md): Attach Fitting · corroded · Apr 25, 2025 · N819AW · Airbus A319132 · Nacelle/Pylon, Attach Fittings
  > AIRCRAFT 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.
- [SDR AALA202505085893](https://openairdocs.org/sdr/AALA202505085893.md): Hinge Fitting · excess play · Apr 23, 2025 · N819AW · Airbus A319132 · Elevator Structure
  > AIRCRAFT 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.
- [SDR AALA202505087923](https://openairdocs.org/sdr/AALA202505087923.md): Hinge Fitting · excess play · Apr 23, 2025 · N819AW · Airbus A319132 · Elevator Structure
  > AIRCRAFT 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.
- [SDR AALA202505089530](https://openairdocs.org/sdr/AALA202505089530.md): Hinge Fitting · excess play · Apr 23, 2025 · N819AW · Airbus A319132 · Elevator Structure
  > AIRCRAFT 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.
- [SDR AALA202505082937](https://openairdocs.org/sdr/AALA202505082937.md): Hinge Fitting · excess play · Apr 23, 2025 · N819AW · Airbus A319132 · Elevator Structure
  > AIRCRAFT 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.
- [SDR AALA202505082161](https://openairdocs.org/sdr/AALA202505082161.md): Hinge Fitting · excess play · Apr 23, 2025 · N819AW · Airbus A319132 · Elevator Structure
  > AIRCRAFT 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 INDIV
- [SDR AALA202504294791](https://openairdocs.org/sdr/AALA202504294791.md): Attach Fitting · excess play · Apr 21, 2025 · N819AW · Airbus A319132 · Nacelle/Pylon Miscellaneous Structure
  > AIRCRAFT 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 SR
- [SDR AALA202507251354](https://openairdocs.org/sdr/AALA202507251354.md): Beam · cracked · Apr 20, 2025 · N819AW · Airbus A319132 · Fuselage Main, Structure
  > AIRCRAFT 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 FRON
- [SDR AALA202507214424](https://openairdocs.org/sdr/AALA202507214424.md): Floorbeam · cracked · Apr 20, 2025 · N819AW · Airbus A319132 · Fuselage Main, Floor Beam
  > AIRCRAFT 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 BOX
- [SDR AALA202507211260](https://openairdocs.org/sdr/AALA202507211260.md): Floorbeam · cracked · Apr 20, 2025 · N819AW · Airbus A319132 · Fuselage Main, Floor Beam
  > AIRCRAFT 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 SPAR
- [SDR AALA202505080845](https://openairdocs.org/sdr/AALA202505080845.md): Hinge Fitting · excess play · Apr 20, 2025 · N819AW · Airbus A319132 · Elevator Structure
  > AIRCRAFT 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.
- [SDR AALA202505082269](https://openairdocs.org/sdr/AALA202505082269.md): Hinge Fitting · excess play · Apr 20, 2025 · N819AW · Airbus A319132 · Elevator Structure
  > AIRCRAFT 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.
- [SDR AALA202505085223](https://openairdocs.org/sdr/AALA202505085223.md): Hinge Fitting · excess play · Apr 20, 2025 · N819AW · Airbus A319132 · Elevator Structure
  > AIRCRAFT 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.
- [SDR AALA202505082101](https://openairdocs.org/sdr/AALA202505082101.md): Hinge Fitting · excess play · Apr 20, 2025 · N819AW · Airbus A319132 · Elevator Structure
  > AIRCRAFT 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.
- [SDR AALA202505082359](https://openairdocs.org/sdr/AALA202505082359.md): Hinge Fitting · excess play · Apr 20, 2025 · N819AW · Airbus A319132 · Elevator Structure
  > AIRCRAFT 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.
- [SDR AALA202505084403](https://openairdocs.org/sdr/AALA202505084403.md): Hinge Fitting · excess play · Apr 20, 2025 · N819AW · Airbus A319132 · Elevator Structure
  > AIRCRAFT 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.
- [SDR AALA202505204988](https://openairdocs.org/sdr/AALA202505204988.md): Fitting · cracked · Apr 19, 2025 · N819AW · Airbus A319132 · Fuselage Miscellaneous Structure
  > AIRCRAFT 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. MAINTENANCE
- [SDR AALA202505204868](https://openairdocs.org/sdr/AALA202505204868.md): Fitting · cracked · Apr 19, 2025 · N819AW · Airbus A319132 · Fuselage Main, Structure
  > AIRCRAFT 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 BT
- [SDR AALA202505150887](https://openairdocs.org/sdr/AALA202505150887.md): Fitting · cracked · Apr 19, 2025 · N819AW · Airbus A319132 · Fuselage Miscellaneous Structure
  > AIRCRAFT 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 STO
- [SDR AALA202505151028](https://openairdocs.org/sdr/AALA202505151028.md): Fitting · cracked · Apr 19, 2025 · N819AW · Airbus A319132 · Fuselage Miscellaneous Structure
  > AIRCRAFT 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 A319
- [SDR AALA202505131028](https://openairdocs.org/sdr/AALA202505131028.md): Fitting · cracked · Apr 19, 2025 · N819AW · Airbus A319132 · Fuselage Main, Structure
  > AIRCRAFT 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 A319
- [SDR AALA202505209566](https://openairdocs.org/sdr/AALA202505209566.md): Stiffener · cracked · Apr 18, 2025 · N819AW · Airbus A319132 · Fuselage Miscellaneous Structure
  > AIRCRAFT 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
- [SDR AALA202507210112](https://openairdocs.org/sdr/AALA202507210112.md): Shear Plate · cracked · Apr 17, 2025 · N819AW · Airbus A319132 · Fuselage Miscellaneous Structure
  > AIRCRAFT 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 DWG
- [SDR AALA202507180914](https://openairdocs.org/sdr/AALA202507180914.md): Shear Plate · cracked · Apr 17, 2025 · N819AW · Airbus A319132 · Fuselage Miscellaneous Structure
  > AIRCRAFT 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 DR
- [SDR AALA202507257127](https://openairdocs.org/sdr/AALA202507257127.md): Window Post · cracked · Apr 16, 2025 · N819AW · Airbus A319132 · Fuselage Main, Structure
  > AIRCRAFT 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 RH
- [SDR AALA202507259901](https://openairdocs.org/sdr/AALA202507259901.md): Window Post · cracked · Apr 16, 2025 · N819AW · Airbus A319132 · Fuselage Main, Structure
  > AIRCRAFT 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 FRAM
- [SDR AALA202507218300](https://openairdocs.org/sdr/AALA202507218300.md): Attach Fitting · excess play · Apr 16, 2025 · N819AW · Airbus A319132 · Fuselage Main, Attach Fittings
  > AIRCRAFT 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.
- [SDR AALA202507078655](https://openairdocs.org/sdr/AALA202507078655.md): Fitting · cracked · Apr 16, 2025 · N819AW · Airbus A319132 · Fuselage Main, Structure
  > AIRCRAFT 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.
- [SDR AALA202507076746](https://openairdocs.org/sdr/AALA202507076746.md): Fitting · cracked · Apr 16, 2025 · N819AW · Airbus A319132 · Fuselage Main, Structure
  > AIRCRAFT 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.
- [SDR AALA202506138660](https://openairdocs.org/sdr/AALA202506138660.md): Fitting · burred · Apr 16, 2025 · N819AW · Airbus A319132 · Fuselage Main, Structure
  > AIRCRAFT 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.
- [SDR AALA202505024913](https://openairdocs.org/sdr/AALA202505024913.md): Hinge Pin · corroded · Apr 15, 2025 · N819AW · Airbus A319132 · Ailerons
  > AIRCRAFT 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.
- [SDR AALA202505024253](https://openairdocs.org/sdr/AALA202505024253.md): Hinge Pin · corroded · Apr 15, 2025 · N819AW · Airbus A319132 · Ailerons
  > AIRCRAFT 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.
- [SDR AALA202506135460](https://openairdocs.org/sdr/AALA202506135460.md): Window Frame · cracked · Apr 14, 2025 · N819AW · Airbus A319132 · Fuselage Main, Structure
  > AIRCRAFT 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 5

Next page: https://openairdocs.org/aircraft/N819AW/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/aircraft/N819AW/reports

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