# Service difficulty reports: N740UW A list on [N740UW](https://openairdocs.org/aircraft/N740UW.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 6 · 258 reports - [SDR AALA202607312899](https://openairdocs.org/sdr/AALA202607312899.md): Diaphragm · leaking · Jul 29, 2026 · N740UW · Airbus A319112 · Passenger/Crew Doors > AIRCRAFT WAS NOT GROUNDED: R1 DOOR DAMPENER REQUIRES SERVICING ALONG WITH NEW DIAPHRAGM. MAINTENANCE REPLACED R1 DOOR DAMPENER DIAPHRAGM AND SERVICED PER AMM 52-10-00. - [SDR AALA202607145965](https://openairdocs.org/sdr/AALA202607145965.md): Power Supply · no test · Jul 11, 2026 · N740UW · Airbus A319112 · Emergency Lighting > AIRCRAFT IN BASE MAINTENANCE: AFT LEFT EMERGENCY POWER SUPPLY UNIT FAULTING DURING SYSTEM TEST. REPLACED EMERGENCY POWER SUPPLY UNIT PER AMM 33-51-38 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK. - [SDR AALA202512292282](https://openairdocs.org/sdr/AALA202512292282.md): Battery · no test · Dec 27, 2025 · N740UW · Airbus A319112 · Emergency Lighting > AIRCRAFT WAS NOT GROUNDED: DURING PS CHECK FOUND THAT EPSU LEFT MID CABIN BATTERY FAILED. MAINTENANCE REPLACED THE BATTERY OF THE EMERGENCY POWER SUPPLY UNIT LEFT MID CABIN IAW AMM 33-51-38. - [SDR AALA202510287446](https://openairdocs.org/sdr/AALA202510287446.md): Power Supply · faulted · Oct 24, 2025 · N740UW · Airbus A319112 · Emergency Lighting > AIRCRAFT IN BASE MAINTENANCE: ON FAP PANEL ESPU EXT LOAD AFT L AND ESPU INT LOAD AFT L FAULT FOUND. MAINTENANCE REPLACED EPSU. - [SDR AALA202510288378](https://openairdocs.org/sdr/AALA202510288378.md): Power Supply · faulted · Oct 24, 2025 · N740UW · Airbus A319112 · Emergency Lighting > AIRCRAFT IN BASE MAINTENANCE: ON FAP PANEL ESPU EXT LOAD AFT L AND ESPU INT LOAD AFT L FAULT FOUND. MAINTENANCE REPLACED EPSU. - [SDR AALA202510283355](https://openairdocs.org/sdr/AALA202510283355.md): Slide Raft · faulty · Oct 24, 2025 · N740UW · Airbus A319112 · Escape Slide > AIRCRAFT IN BASE MAINTENANCE: ON FAP PANEL ESPU EXT LOAD AFT L AND ESPU INT LOAD AFT L FAULT FOUND. MAINTENANCE REPLACED L2 SLIDE IAW JOBCARD 26L00025011. - [SDR AALA202510284581](https://openairdocs.org/sdr/AALA202510284581.md): Slide Raft · faulty · Oct 24, 2025 · N740UW · Airbus A319112 · Escape Slide > AIRCRAFT IN BASE MAINTENANCE: ON FAP PANEL ESPU EXT LOAD AFT L AND ESPU INT LOAD AFT L FAULT FOUND. MAINTENANCE REPLACED R2 SLIDE IAW JOB CARD 26L00025011. - [SDR AALA202510245086](https://openairdocs.org/sdr/AALA202510245086.md): Skin · cracked · Oct 17, 2025 · N740UW · Airbus A319112 · Fuselage Main, Plate/Skin > AIRCRAFT IN BASE MAINTENANCE: FATIGUE CRACK 0.25" LONG FORWARD FROM FASTENER HOLE BETWEEN FR13 AND FR141.25" FORWARD OF FR14 HALFWAY BETWEEN Z780 & Z950, MAINTENANCE REPAIRED SKIN WITH A DOUBLER IAW EA 369009 AND SRM 53-11-11-300-041. - [SDR AALA202510212886](https://openairdocs.org/sdr/AALA202510212886.md): Skin Panel · cracked · Oct 16, 2025 · N740UW · Airbus A319112 · Fuselage Main, Plate/Skin > AIRCRAFT IN BASE MAINTENANCE: FATIGUE CRACK 0.5" LONG AFT FROM FASTNER HOLE BETWEEN FR 13 & FR 14., HALFWAY BETWEEN Z+780 AND Z+950. MAINTENANCE CUT OUT DAMAGE AND INSTALLED DOUBLER REPAIR IAW EA 369008, SRM 53-11-11. - [SDR AALA202409255832](https://openairdocs.org/sdr/AALA202409255832.md): Flashlight · inoperative · Sep 24, 2024 · N740UW · Airbus A319112 · Emergency Equipment > AIRCRAFT WAS NOT GROUNDED: FORWARD FLIGHT ATTENDANT'S FLASHLIGHT UNDER THE JUMPSEAT IS NOT WORKING. REPLACED FLASHLIGHT PER AMM 25-65-00. - [SDR AALA202408084006](https://openairdocs.org/sdr/AALA202408084006.md): Contactor · faulty · Aug 7, 2024 · N740UW · Airbus A319112 · Starter-Generator > AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO TPA DUE TO THE FLIGHT CREW REPORTING THAT IN FLIGHT ELECTRICAL GENERATOR 1 FAULT ECAM ANNUNCIATED MULTIPLE TIMES. THE FLIGHT CREW ACCOMPLISHED ECAM AND GENERATOR 1 RESET. AFTER THE 3 - [SDR AALA202407103582](https://openairdocs.org/sdr/AALA202407103582.md): Hook · worn · Jul 9, 2024 · N740UW · Airbus A319112 · Passenger/Crew Doors > AIRCRAFT WAS IN BASE MAINTENANCE: WEAR ON PASSENGER CREW DOOR 832 HOOK AT AFT GALLEY AREA (1 EA). REPLACED HOOK AT PASSENGER CREW DOOR 832 ON AFT GALLEY AREA (1 EA) IAW AMM 52-13-21-400-001-A REFER TO INDIVIDUAL SIGNS OFF ENTRIES FOR WORK STEP PERFORMED, AT - [SDR AALA202407108487](https://openairdocs.org/sdr/AALA202407108487.md): Frame · cracked · Jul 8, 2024 · N740UW · Airbus A319112 · Fuselage Main, Frame > AIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME FASTENER HOLE "A" ON DOUBLE JOGGLE AREA AT FR 16 LEFT AND DOOR STOP FITTING #7. REPLACED FRAME PER EA 354355. - [SDR AALA202406263936](https://openairdocs.org/sdr/AALA202406263936.md): Window Frame · cracked · Jun 26, 2024 · N740UW · Airbus A319112 · Fuselage Main, Structure > AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK WINDSHIELD FRAME CENTER POST LOWER ATTACHMENT AREA RIGHT HAND SIDE LOWER RADIUS CRACKED AT FR 2 AND Y0. REPAIRED WINDSHIELD FRAME PER EA 353883. - [SDR AALA202406262189](https://openairdocs.org/sdr/AALA202406262189.md): Window Frame · cracked · Jun 26, 2024 · N740UW · Airbus A319112 · Fuselage Main, Structure > AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK WINDSHIELD FRAME CENTER POST LOWER ATTACHMENT AREA LEFT HAND SIDE UPPER RADIUS CRACKED AT FR 2 AND Y0. REPAIRED WINDSHIELD FRAME PER EA 353883. - [SDR AALA202407101511](https://openairdocs.org/sdr/AALA202407101511.md): Frame · worn · Jun 3, 2024 · N740UW · Airbus A319112 · Fuselage Main, Frame > AIRCRAFT IN BASE MAINTENANCE: FRAME HAS ELONGATED / WORN FASTENER HOLE AT FR 16 LEFT BETWEEN Z1590 AND Z1330. REPLACED FRAME PER EA 354355. - [SDR AALA202407100471](https://openairdocs.org/sdr/AALA202407100471.md): Fitting · worn · Jun 3, 2024 · N740UW · Airbus A319112 · Fuselage Miscellaneous Structure > AIRCRAFT IN BASE MAINTENANCE: INTERCOSTAL FITTING HAS ELONGATED / WORN FASTENER HOLE AT FR 16 LEFT BETWEEN Z1590 AND Z1330. REPLACED INTERCOSTAL FITTING PER EA 354355. - [SDR AALA202407108931](https://openairdocs.org/sdr/AALA202407108931.md): Fitting · worn · Jun 3, 2024 · N740UW · Airbus A319112 · Fuselage Main, Frame > AIRCRAFT IN BASE MAINTENANCE: FRAME CORNER HAS ELONGATED / WORN FASTENER HOLE AT FR 16 LEFT BETWEEN Z1590 AND Z1330. REPAIRED FRAME CORNER PER EA 354355. - [SDR AALA202405283622](https://openairdocs.org/sdr/AALA202405283622.md): Bottle · low pressure · May 24, 2024 · N740UW · Airbus A319112 · Emergency Equipment > AIRCRAFT WAS IN BASE MAINTENANCE: LOW PRESSURE DAMPER ON PASSENGER CREW DOOR 842 IN AFT GALLEY AREA. REPLACED DOOR DAMPER ON PASSENGER CREW DOOR 842 AT AFT GALLEY AREA PER AMM 52-13-14-000-001-B. - [SDR AALA202405244301](https://openairdocs.org/sdr/AALA202405244301.md): Slide Raft · deformed · May 22, 2024 · N740UW · Airbus A319112 · Escape Slide > AIRCRAFT WAS IN BASE MAINTENANCE: DEFORMATION SLIDE RAFT PACK ASSEMBLY AT DOOR 831. REPLACED SLIDE RAFT PACK ASSEMBLY AT DOOR 831. - [SDR AALA202405226502](https://openairdocs.org/sdr/AALA202405226502.md): Window · scratched · May 19, 2024 · N740UW · Airbus A319112 · Door Windows > AIRCRAFT IN BASE MAINTENANCE: AFT PASSENGER / CREW DOOR 832 OUTER WINDOW PANE SCRATCHED. REPLACED WINDOW PANEL PER AMM 56-31-13. - [SDR AALA202406048511](https://openairdocs.org/sdr/AALA202406048511.md): Fitting · corroded · May 13, 2024 · N740UW · Airbus A319112 · Nacelle/Pylon Structure > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND PYLON SPIGOT FITTING RECEPTACLE BETWEEN PYLON RIBS 4 AND 5. REPLACED SPIGOT FITTING PER SRM 54-51-12-300-001. - [SDR AALA202405305151](https://openairdocs.org/sdr/AALA202405305151.md): Fitting · corroded · May 13, 2024 · N740UW · Airbus A319112 · Nacelle/Pylon, Main Frame > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT HAND PYLO SPIGOT FITTING RECEPTACLE BETWEEN WS 679 AND WS 706, BETWEEN RIB 4 AND RIB 5. REPLACED SPIGOT FITTING PER SRM 54-51-12-300-001. - [SDR AALA202406273283](https://openairdocs.org/sdr/AALA202406273283.md): Fitting · none · May 9, 2024 · N740UW · Airbus A319112 · Standard Practices/Structures > AIRCRAFT IN BASE MAINTENANCE: DUE TO THE MAJOR REPAIR BEING ACCOMPLISHED TO THE FLIGHT DECK CENTER WINDSHIELD FRAMING PER EA 353883, THE RIGHT HAND CONTINUITY FITTING BETWEEN FR 1 AND FR 2 AT Y0 NEEDS TO BE REPLACED. MAINTENANCE REPLACED THE RIGHT HAND CONTINU - [SDR AALA202406276625](https://openairdocs.org/sdr/AALA202406276625.md): Fitting · none · May 9, 2024 · N740UW · Airbus A319112 · Standard Practices/Structures > AIRCRAFT IN BASE MAINTENANCE: DUE TO THE MAJOR REPAIR BEING ACCOMPLISHED TO THE FLIGHT DECK CENTER WINDSHIELD FRAMING PER EA 353883, THE LEFT HAND CONTINUITY FITTING BETWEEN FR 1 AND FR 2 AT Y0 NEEDS TO BE REPLACED. MAINTENANCE REPLACED THE LEFT HAND CONTINUIT - [SDR AALA202406282207](https://openairdocs.org/sdr/AALA202406282207.md): Floorbeam · cracked · May 5, 2024 · N740UW · Airbus A319112 · Fuselage Main, Floor Beam > AIRCRAFT IN BASE MAINTENANCE: CABIN FLOOR BEAM HAS 2 CRACKED FASTENER HOLES AT THE CENTER WING BOX FRONT SPAR COMMON TO VERTICAL STRINGER 2 AT FR 36 AND +Y765. REPAIRED FLOOR BEAM PER EA 354472. - [SDR AALA202406264450](https://openairdocs.org/sdr/AALA202406264450.md): Floorbeam · cracked · May 5, 2024 · N740UW · Airbus A319112 · Fuselage Main, Floor Beam > AIRCRAFT IN BASE MAINTENANCE: CABIN FLOOR BEAM HAS 2 CRACKED FASTENER HOLES AT THE CENTER WING BOX FRONT SPAR COMMON TO VERTICAL STRINGER 4 AT FR 36 AND -Y254. REPAIRED FLOOR BEAM PER EA 354472. - [SDR AALA202406262682](https://openairdocs.org/sdr/AALA202406262682.md): Floorbeam · cracked · May 5, 2024 · N740UW · Airbus A319112 · Fuselage Main, Floor Beam > AIRCRAFT IN BASE MAINTENANCE: CABIN FLOOR BEAM HAS 2 CRACKED FASTENER HOLES AT THE CENTER WING BOX FRONT SPAR COMMON TO VERTICAL STRINGER 3 AT FR 36 AND +Y254. REPAIRED FLOOR BEAM PER EA 354472. - [SDR AALA202406268618](https://openairdocs.org/sdr/AALA202406268618.md): Floorbeam · cracked · May 5, 2024 · N740UW · Airbus A319112 · Fuselage Main, Floor Beam > AIRCRAFT IN BASE MAINTENANCE: CABIN FLOOR BEAM HAS CRACKED FASTENER HOLE AT THE CENTER WING BOX FRONT SPAR COMMON TO VERTICAL STRINGER 5 AT FR 36 AND -Y765. REPAIRED FLOOR BEAM PER EA 354472. - [SDR AALA202405295635](https://openairdocs.org/sdr/AALA202405295635.md): Support · corroded · May 3, 2024 · N740UW · Airbus A319112 · Fuselage Miscellaneous Structure > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LOWER SILL LOCATED AT FR 68 AT LEVEL STR 23R IN AFT GALLEY AREA. PERFORMED PERMANENT REPAIR ON LOWER SILL PER SRM 53-41-14-300-001. - [SDR AALA202405295558](https://openairdocs.org/sdr/AALA202405295558.md): Support · corroded · May 3, 2024 · N740UW · Airbus A319112 · Fuselage Main, Structure > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LOWER SILL LOCATED AT FR 68 AND AT LEVEL STR 23 IN AFT GALLEY AREA. PERFORMED PERMANENT REPAIR ON LOWER SILL PER SRM 53-41-14-300-001. - [SDR AALA202406217947](https://openairdocs.org/sdr/AALA202406217947.md): Fork · worn · May 1, 2024 · N740UW · Airbus A319112 · Fuselage Main, Structure > AIRCRAFT IN BASE MAINTENANCE: AFT AVIONIC COMPARTMENT RACK 80VU LEFT HAND LATERAL FORK END FITTING WORN BETWEEN FR 23 AND FR 24 AT+Y1263 AND S32L. REPLACED LEFT HAND LATERAL FORK END FITTING PER EA 354085. - [SDR AALA202406212593](https://openairdocs.org/sdr/AALA202406212593.md): Fork · worn · May 1, 2024 · N740UW · Airbus A319112 · Fuselage Main, Structure > AIRCRAFT IN BASE MAINTENANCE: AFT AVIONIC COMPARTMENT RACK 80VU RIGHT HAND LATERAL FORK END FITTING WORN BETWEEN FR 23 AND FR 24 AT+Y1263 AND S32L. REPLACED RIGHT HAND LATERAL FORK END FITTING PER EA 354085. - [SDR AALA202407033674](https://openairdocs.org/sdr/AALA202407033674.md): Shear Plate · cracked · Apr 30, 2024 · N740UW · Airbus A319112 · Fuselage Miscellaneous Structure > AIRCRAFT IN BASE MAINTENANCE: CRACKED AFT GALLEY FLOOR SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23R. REPLACED SHEAR PLATE PER SRM 51-42-11. - [SDR AALA202406247301](https://openairdocs.org/sdr/AALA202406247301.md): Shear Plate · cracked · Apr 30, 2024 · N740UW · Airbus A319112 · Fuselage Miscellaneous Structure > AIRCRAFT IN BASE MAINTENANCE: CRACKED AFT GALLEY AREA SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23L. REPLACED SHEAR PLATE PER SRM 51-72-11. - [SDR AALA202407104912](https://openairdocs.org/sdr/AALA202407104912.md): Frame · cracked · Apr 29, 2024 · N740UW · Airbus A319112 · Fuselage Main, Frame > AIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME LOWER AFT HOLE AT FR 35 AND S30L. REPAIRED FRAME PER EA 354064. - [SDR AALA202406071711](https://openairdocs.org/sdr/AALA202406071711.md): Web · corroded · Apr 29, 2024 · N740UW · Airbus A319112 · Fuselage Miscellaneous Structure > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON WEB FRAME LOCATED BETWEEN FR 20 AND FR 24 AND AT STR 23R IN FORWARD GALLEY AREA. REPLACED WEB PER SRM 51-42-11-801. - [SDR AALA202406036729](https://openairdocs.org/sdr/AALA202406036729.md): Seat Track · corroded · Apr 29, 2024 · N740UW · Airbus A319112 · Fuselage, Seat/Cargo Attach Fittings > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CABIN FLOOR BEAM-SEAT TRACK AT FR 16 AND +Y765. REPLACED BEAM-SEAT TRACK PER SRM 51-42-11. - [SDR AALA202406038900](https://openairdocs.org/sdr/AALA202406038900.md): Seat Track · corroded · Apr 29, 2024 · N740UW · Airbus A319112 · Fuselage, Seat/Cargo Attach Fittings > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CABIN FLOOR BEAM-SEAT TRACK AT FR 16 AND +Y1292. REPLACED BEAM-SEAT TRACK PER SRM 51-42-11. - [SDR AALA202407102060](https://openairdocs.org/sdr/AALA202407102060.md): Skin Panel · worn · Apr 24, 2024 · N740UW · Airbus A319112 · Leading Edge Devices > AIRCRAFT IN BASE MAINTENANCE: RIGHT WING LEADING EDGE #1 SLAT UPPER SURFACE BOTTOM SKIN WORN AT SLAT TRACK #2. REPAIRED SLAT SKIN PER EA 355439 - [SDR AALA202406212826](https://openairdocs.org/sdr/AALA202406212826.md): Skin Panel · corroded · Apr 23, 2024 · N740UW · Airbus A319112 · Wing, Plate/Skin > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING SKIN TRAILING EDGE UPPER SKIN PANEL, UPPER SURFACE BETWEEN RIBS 8 AND 9. REPAIRED SKIN PANEL PER EA 354632. - [SDR AALA202404220381](https://openairdocs.org/sdr/AALA202404220381.md): Hinge Fitting · excess play · Apr 20, 2024 · N740UW · Airbus A319112 · Fuselage, Door Hinge > AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND MAIN LANDING GEAR DOOR FORWARD HINGE FITTING HAS EXCESSIVE PLAY. REPLACED HINGE FITTING PER CMM 52-81-18. - [SDR AALA202404114417](https://openairdocs.org/sdr/AALA202404114417.md): Bulb · inoperative · Apr 10, 2024 · N740UW · Airbus A319112 · Emergency Lighting > AIRCRAFT WAS NOT GROUNDED: THREE BULBS OUT ON OVERHEAD EXIT SIGN AT MID CABIN. RELAMPED 3 BULBS EMERGENCY EXIT SIGN MID CABIN AS REQUIRED. - [SDR AALA202404117417](https://openairdocs.org/sdr/AALA202404117417.md): Switch · faulty · Apr 10, 2024 · N740UW · Airbus A319112 · Emergency Lighting > AIRCRAFT WAS GROUNDED: EMERGENCY EXIT LIGHTS ON WHEN SWITCH IN ARM POSITION PERFORMED TSM 33-51-00-810-881-A FOUND SWITCH 4WL BAD. REPLACED SWITCH PER AMM 33-51-00. - [SDR AALA202311131188](https://openairdocs.org/sdr/AALA202311131188.md): Bushing · damaged · Nov 9, 2023 · N740UW · Airbus A319112 · Passenger/Crew Doors > AIRCRAFT WAS GROUNDED: CATERING FOUND 2L DOOR HARD TO OPEN AND CLOSE. MAINTENANCE FOUND LOWER SUPPORT ARM BUSHING AND HARDWARE DAMAGED REF SRM 51-70-10 FOR REPAIR. - [SDR AALA202305307927](https://openairdocs.org/sdr/AALA202305307927.md): Battery · inoperative · May 27, 2023 · N740UW · Airbus A319112 · Emergency Equipment > AIRCRAFT WAS NOT GROUNDED: FORWARD GALLEY FLIGHT ATTENDANT FLASHLIGHT DOES NOT FLASH. REPLACED FLASHLIGHT BATTERY AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK. - [SDR AALA202305187687](https://openairdocs.org/sdr/AALA202305187687.md): Door · sticking · May 8, 2023 · N740UW · Airbus A319112 · Fixed Inner Doors > AIRCRAFT WAS NOT GROUNDED: FORWARD LAVATORY DOOR DIFFICULT TO OPEN/CLOSE. **SUPPLEMENTAL REPORT FOR AALA202305127687: MAINTENANCE PERFORMED A FUNCTIONAL CHECK OF THE FORWARD LAVATORY DOOR AND COULD NOT DUPLICATE THE DISCREPANCY. NO FURTHER DISCREPANCIES WERE F - [SDR AALA202305127687](https://openairdocs.org/sdr/AALA202305127687.md): Unknown · unknown · May 8, 2023 · N740UW · Airbus A319112 · Fixed Inner Doors > AIRCRAFT WAS NOT GROUNDED: FORWARD LAVATORY DOOR DIFFICULT TO OPEN/CLOSE. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN) - [SDR AALA202302231457](https://openairdocs.org/sdr/AALA202302231457.md): Door Latch · unsecure · Feb 21, 2023 · N740UW · Airbus A319112 · Fixed Inner Doors > AIRCRAFT WAS NOT GROUNDED: FORWARD LAVATORY DOOR DIFFICULT TO OPEN /CLOSE. MAINTENANCE SECURED THE FORWARD LAVATORY DOOR LATCH PER AMM 25-45-00 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK. - [SDR AALA202302249649](https://openairdocs.org/sdr/AALA202302249649.md): Apu · leaking · Feb 18, 2023 · N740UW · Airbus A319112 · Airborne Auxiliary Power Unit (APU) System > AIRCRAFT WAS GROUNDED: DURING DESCENT AROUND 6000 THE FLIGHT CREW NOTICED A DIRTY SOCK SMELL THAT REMAINED UNTIL AFTER LANDING. MAINTENANCE ISOLATED THE SOURCE OF THE ODOR TO THE APU DUE TO FINDING EVIDENCE OF OIL LEAKS. **SUPPLEMENTAL REPORT FOR AALA202302229 Next page: https://openairdocs.org/aircraft/N740UW/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 = 'N740UW' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N740UW/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.