# Service difficulty reports: N744P A list on [N744P](https://openairdocs.org/aircraft/N744P.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 · 221 reports - [SDR AALA202607275053](https://openairdocs.org/sdr/AALA202607275053.md): Proximity Sensor · out of rig · Jul 23, 2026 · N744P · Airbus A319112 · Door Warning System > AIRCRAFT WAS GROUNDED: 2R DOOR INDICATES DISARMED IN FLIGHT WITH ARMING LEVER IN THE ARMED POSITION. INDICATED ARMED ON THE GROUND AND IN CLIMB. MAINTENANCE FOUND THE R2 DOOR ARM HANDLE DETECTOR PROXIMITY SWITCH 7WN2 OUT OF RIG AND ADJUSTED IT PER AMM 52-71-00 - [SDR AALA202607209324](https://openairdocs.org/sdr/AALA202607209324.md): Slide · faulted · Jul 15, 2026 · N744P · Airbus A319112 · Escape Slide > AIRCRAFT WAS GROUNDED: 2R DOOR DISARMED INFLIGHT, FLIGHT CREW REPORTED THE R2 DOOR INDICATED ARMED ON THE GROUND AND THROUGH 10000FT. FLIGHT ATTENDED RECEIVED FLASHING SLIDE ARMED ON FAP AND DOOR PAGE SHOWED UNARMED AT THROUGH FL230. DOOR REARMED ON DESCENT A - [SDR AALA202607164846](https://openairdocs.org/sdr/AALA202607164846.md): Proximity Switch · intermittent · Jul 14, 2026 · N744P · Airbus A319112 · Door Warning System > AIRCRAFT WAS NOT GROUNDED: RIGHT AFT DOOR SLIDE INTERMITTENTLY BECOMES UMARMED AND ARMED. MAINTENANCE REPLACED AFT RIGHT CABIN ARMED PROXIMITY S/W FIN #: 7WN2 IAW AMM 52-73-11. - [SDR AALA202607166621](https://openairdocs.org/sdr/AALA202607166621.md): Indicator · intermittent · Jul 13, 2026 · N744P · Airbus A319112 · Door Warning System > AIRCRAFT WAS GROUNDED: RIGHT AFT DOOR SLIDE INTERMITTENTLY BECOMES UMARMED AND ARMED. MAINTENANCE REPLACED THE SLIDE ARMED INDICATOR LIGHT PER AMM 52-73-21 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK. - [SDR AALA202607142477](https://openairdocs.org/sdr/AALA202607142477.md): Proximity Sensor · intermittent · Jul 11, 2026 · N744P · Airbus A319112 · Door Warning System > AIRCRAFT WAS GROUNDED: BACK RIGHT SLIDE ARM INDICATOR INTERMITTENT DURING FLIGHT. MAINTENANCE REPLACED THE DETECTOR PROXIMITY SWITCH 15WV2 PER AMM 52-71-11 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK WITH NO ISUSES NOTED. - [SDR AALA202606293839](https://openairdocs.org/sdr/AALA202606293839.md): Bottle · low pressure · Jun 25, 2026 · N744P · Airbus A319112 · Passenger/Crew Doors > AIRCRAFT WAS NOT GROUNDED: AFT LEFT PASSENGER / CREW DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER 26L80052001. - [SDR AALA202606293815](https://openairdocs.org/sdr/AALA202606293815.md): Bottle · low pressure · Jun 25, 2026 · N744P · Airbus A319112 · Passenger/Crew Doors > AIRCRAFT WAS NOT GROUNDED: FORWARD RIGHT PASSENGER / CREW DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER 26L80052001. - [SDR AALA202606294236](https://openairdocs.org/sdr/AALA202606294236.md): Bottle · low pressure · Jun 25, 2026 · N744P · Airbus A319112 · Passenger/Crew Doors > AIRCRAFT WAS NOT GROUNDED: FORWARD LEFT PASSENGER / CREW DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER 26L80052001. - [SDR AALA202602119700](https://openairdocs.org/sdr/AALA202602119700.md): Fcu · inoperative · Feb 10, 2026 · N744P · Airbus A319112 · Autopilot System > AIRCRAFT WAS GROUNDED: FO BARO REF SET KNOB REVERTS TO STANDARD REGARDLESS OF PUSH/PULL UNABLE TO SET BARO ON FO SIDE. DECESION MADE TO RETURN TO DFW, NO EMERGENCY AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED FCU IAW AMM 22-81-12. - [SDR AALA202602029624](https://openairdocs.org/sdr/AALA202602029624.md): Handle · loose · Jan 30, 2026 · N744P · Airbus A319112 · Flight Compartment Windows > AIRCRAFT WAS NOT GROUNDED: FLIGHT DECK LEFT HAND SLIDING WINDOW HANDLE LOOSE. MAINTENANCE SECURED HANDLE AND ACCOMPLISHED A SATISFACTORY OPS CHECKED IAW AMM 56-12-11. - [SDR AALA202601083058](https://openairdocs.org/sdr/AALA202601083058.md): Bottle · low pressure · Jan 7, 2026 · N744P · Airbus A319112 · Passenger/Crew Doors > AIRCRAFT WAS NOT GROUNDED: L1 DOOR EMERGENCY ACCUMULATOR LOW PRESSURE. MAINTENANCE SERVICED L1 DOOR EMERGENCY ACCUMULATOR IAW AMM 52-10-00. - [SDR AALA202601081959](https://openairdocs.org/sdr/AALA202601081959.md): Bottle · low pressure · Jan 7, 2026 · N744P · Airbus A319112 · Passenger/Crew Doors > AIRCRAFT WAS NOT GROUNDED: R1 DOOR EMERGENCY ACCUMULATOR LOW. MAINTENANCE SERVICED R1 DOOR EMERGENCY ACCUMULATOR IAW AMM 52-10-00. - [SDR AALA202508146641](https://openairdocs.org/sdr/AALA202508146641.md): Strut · out of rig · Aug 13, 2025 · N744P · Airbus A319112 · Trailing Edge Flap Control System > AIRCRAFT WAS GROUNDED: F/CTL FLAPS LOCKED ALIGNMENT FAULT. DECESION MADE TO DIVERT TO IAD FOR LANGER RUMWAY, AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT IAW 27-51-00-810-818-A AND FOUND LH INTERCONNECTING STRUT OUT OF RIG, REMOVED AND REPLACED L - [SDR AALA202507080099](https://openairdocs.org/sdr/AALA202507080099.md): Light · inoperative · Jul 7, 2025 · N744P · Airbus A319112 · Emergency Lighting > AIRCRAFT IN BASE MAINTENANCE: FOUND ROW 23 OVERHEAD EMERGENCY LIGHTING ASSEMBLIES INOP DURING OPERATIONAL TEST OF EMERGENCY LIGHTS AS REQUIRED IN PERIODIC SERVICE CHECK W/C 26L00005005. MAINTENANCE REPLACED OVHD EMERGENCY LIGHTS AT ROW23, REF AMM 33-51-11. - [SDR AALA202507088902](https://openairdocs.org/sdr/AALA202507088902.md): Light · inoperative · Jul 7, 2025 · N744P · Airbus A319112 · Emergency Lighting > AIRCRAFT IN BASE MAINTENANCE: FOUND ROW 9 OVERHEAD EMERGENCY LIGHTING ASSEMBLIES INOP DURING OPERATIONAL TEST OF EMERGENCY LIGHTS AS REQUIRED IN PERIODIC SERVICE CHECK W/C 26L00005005. MAINTENANCE REPLACED OVHD EMERGENCY LIGHTS AT ROWS 9 REF AMM 33-51-11. - [SDR AALA202507080832](https://openairdocs.org/sdr/AALA202507080832.md): Power Supply · fault message · Jul 7, 2025 · N744P · Airbus A319112 · Emergency Lighting > AIRCRAFT WAS GROUNDED: RECEIVED "EPSU UNIT EMER R" MESSAGE DURING OPERATIONAL TEST OF EMERGENCY LIGHTS AS REQUIRED IN PERIODIC SERVICE CHECK W/C 26L00005005. MAINTENANCE REPLACED EPSU UNIT EMER ATA 33-51-38. - [SDR AALA202508015828](https://openairdocs.org/sdr/AALA202508015828.md): Floor Support · corroded · Feb 8, 2025 · N744P · Airbus A319112 · Fuselage Miscellaneous Structure > AIRCRAFT IN BASE MAINTENANCE: CORROSION FLOOR BEAM -Y1292 FR 20 FWD GALLEY AREA L= 2.550 W= 1.479 IN D= 0.068 IN. MAINTENANCE REPLACED FLOOR BEAM -Y1292 LOC BTW FR 12 TO FR 24 AT FWD GALLEY AREA IAW A319 SRM 51-42-11-801 AND DWG D53110984, DWG D53112812 AND DW - [SDR AALA202411181358](https://openairdocs.org/sdr/AALA202411181358.md): Warning Message · illuminated · Nov 9, 2024 · N744P · Airbus A319112 · Nose/Tail Landing Gear > AIRCRAFT WAS GROUNDED: AFTER ROTATION, WE GOT LANDING STRUT FAULT. THE GEAR APPEARED TO RETRACT NORMALLY AND DURING CLIMB OUT AFTER CONNECTING THE AUTO PILOT, THE AUTO PILOT DISENGAGED, AND THEN WE GOT A MASTER WARNING THAT THE AUTO THRUST HAD DISENGAGED AS WE - [SDR AALA202411111358](https://openairdocs.org/sdr/AALA202411111358.md): Warning Message · illuminated · Nov 9, 2024 · N744P · Airbus A319112 · Nose/Tail Landing Gear Strut/Axle > AIRCRAFT WAS GROUNDED: AFTER ROTATION, WE GOT LANDING STRUT FAULT. THE GEAR APPEARED TO RETRACT NORMALLY AND DURING CLIMB OUT AFTER CONNECTING THE AUTO PILOT, THE AUTO PILOT DISENGAGED, AND THEN WE GOT A MASTER WARNING THAT THE AUTO THRUST HAD DISENGAGED AS WE - [SDR AALA202410109874](https://openairdocs.org/sdr/AALA202410109874.md): Proximity Sensor · faulted · Oct 9, 2024 · N744P · Airbus A319112 · Trailing Edge Flap Control System > AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO BFL DUE TO THE FLIGHT CREW REPORTING A FLAPS LOCKED ECAM MESSAGE ON APPROACH. THE AIRCRAFT LANDED SAFELY AT BFL AND TAXIED TO THE GATE UNDER ITS OWN POWER. MAINTENANCE FOUND LEFT FLA - [SDR AALA202410108529](https://openairdocs.org/sdr/AALA202410108529.md): Proximity Sensor · faulted · Oct 9, 2024 · N744P · Airbus A319112 · Trailing Edge Flap Control System > AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO BFL DUE TO THE FLIGHT CREW REPORTING A FLAPS LOCKED ECAM MESSAGE ON APPROACH. THE AIRCRAFT LANDED SAFELY AT BFL AND TAXIED TO THE GATE UNDER ITS OWN POWER. MAINTENANCE FOUND LEFT FLA - [SDR AALA202410117817](https://openairdocs.org/sdr/AALA202410117817.md): Brake · faulted · Oct 7, 2024 · N744P · Airbus A319112 · Trailing Edge Flaps > AIRCRAFT WAS NOT GROUNDED: AN EMERGENCY WAS DECLARED INBOUND TO DFW DUE TO THE FLIGHT CREW REPORTING THAT A FLIGHT CONTROL FLAPS LOCKED - ALIGNMENT FAULT ECAM MESSAGE DISPLAYED ON FINAL APPROACH WHEN SELECTING FLAPS 2. FLIGHT CREW ACCOMPLISHED THE ECAM PROCEDU - [SDR AALA202409127614](https://openairdocs.org/sdr/AALA202409127614.md): Handle · inoperative · Sep 11, 2024 · N744P · Airbus A319112 · Passenger/Crew Doors > AIRCRAFT WAS IN BASE MAINTENANCE: R1 DOOR HANDLE DOES NOT LOCK IN UP POSITION WHEN OPENED. PERFORMED ADJUSTMENT OF HOOK INNER CONTROL HANDLE IN PASSENGER CREW DOOR 841 (R1) PER AMM 52-11-21-400-001-A. - [SDR AALA202409122153](https://openairdocs.org/sdr/AALA202409122153.md): Handle · out of adjust · Sep 11, 2024 · N744P · Airbus A319112 · Flight Compartment Windows > AIRCRAFT WAS IN BASE MAINTENANCE: CAPTAIN SLIDING WINDOW WONT OPEN IF ANY AFT PRESSURE IS APPLIED TO HANDLE. PERFORMED ADJUSTMENT ON SLIDING WINDOW CAPTAIN HANDLE PER AMM 56-12-11-400-001-A STEP 4F. - [SDR AALA202409126028](https://openairdocs.org/sdr/AALA202409126028.md): Sliding Window · inoperative · Sep 10, 2024 · N744P · Airbus A319112 · Flight Compartment Windows > AIRCRAFT WAS IN BASE MAINTENANCE: CHECK WINDOW SLIDING LH ADJUSTMENT DOES NOT SECURE THE HANDLE CLIP ATCOCKPIT IN COCKPIT. REPLACED SLIDING WINDOW CAPT SIDE IN COCKPIT IAW AMM 56-12-11-000-001-A ANDAMM 56-12-11-400-001-A REFER TO INDIVIDUAL SIGN OFF ENTRIES FO - [SDR AALA202409045883](https://openairdocs.org/sdr/AALA202409045883.md): Reservoir · warning message · Sep 3, 2024 · N744P · Airbus A319112 · Escape Slide > AIRCRAFT IN BASE MAINTENANCE: FAULT MESSAGE FOR THE RIGHT HAND OFFWING ESCAPE SLIDE INFLATION RESERVOIR DISPLAYED WHILE ACCOMPLISHING A BITE TEST OF THE SYSTEM. MAINTENANCE REPLACED THE ESCAPE SLIDE INFLATION RESERVOIR AND ACCOMPLISHED A SATISFACTORY BITE TEST - [SDR AALA202408146377](https://openairdocs.org/sdr/AALA202408146377.md): Floorbeam · cracked · Aug 12, 2024 · N744P · Airbus A319112 · Fuselage Main, Floor Beam > AIRCRAFT IN BASE MAINTENANCE: CABIN FLOOR BEAM HAS 1 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 354373. - [SDR AALA202408273578](https://openairdocs.org/sdr/AALA202408273578.md): Power Supply · inoperative · Aug 11, 2024 · N744P · Airbus A319112 · Emergency Lighting > AIRCRAFT WAS IN BASE MAINTENANCE: INOP EPSU-EMERGENCY POWER SUPPLY UNIT 11WL IN PASSENGER CABIN. REPLACED EPSU-EMERGENCY POWER SUPPLY UNIT 11WL IN PASSENGER CABIN I.A.W AMM33-51-38-000-001-A AND AMM 33-51-38-400-001-APERFORMED OPERATIONAL CHECK OF THE EPSU THR - [SDR AALA202408275448](https://openairdocs.org/sdr/AALA202408275448.md): Power Supply · inoperative · Aug 11, 2024 · N744P · Airbus A319112 · Emergency Lighting > AIRCRAFT WAS IN BASE MAINTENANCE: INOP EPSU-EMERGENCY POWER SUPPLY UNIT 12WL IN PASSENGER CABIN. REPLACED EPSU-EMERGENCY POWER SUPPLY UNIT 12WL IN PASSENGER CABIN I.A.W AMM33-51-38-000-001-A AND AMM 33-51-38-400-001-APERFORMED OPERATIONAL CHECK OF THE EPSU THR - [SDR AALA202408209847](https://openairdocs.org/sdr/AALA202408209847.md): Splice · none · Aug 10, 2024 · N744P · Airbus A319112 · Standard Practices/Structures > AIRCRAFT IN BASE MAINTENANCE: AS PART OF THE MAJOR REPAIR BEING ACCOMPLISHED ON THE FORWARD RIGHT HAND DOOR CUTOUT SURROUND PANEL AND FRAME AT FR 16 RIGHT PER EA 353946, THE LOWER FRAME SPLICE AT FR 16 AND S28R NEEDS TO BE REPLACED AS OUTLINED IN THE INSTRUCTI - [SDR AALA202408208003](https://openairdocs.org/sdr/AALA202408208003.md): Doubler · not reported · Aug 10, 2024 · N744P · Airbus A319112 · Standard Practices/Structures > AIRCRAFT IN BASE MAINTENANCE: AS PART OF THE MAJOR REPAIR BEING ACCOMPLISHED ON THE FORWARD RIGHT HAND DOOR CUTOUT SURROUND PANEL AND FRAME AT FR 16 RIGHT PER EA 353946, THE UPPER CORNER DOUBLER AT FR 16 AND S12R NEEDS TO BE REPLACED AS OUTLINED IN THE INSTRUC - [SDR AALA202407104770](https://openairdocs.org/sdr/AALA202407104770.md): Window Frame · none · Jul 5, 2024 · N744P · Airbus A319112 · Standard Practices/Structures > AIRCRAFT IN BASE MAINTENANCE: DUE TO THE MAJOR REPAIR BEING ACCOMPLISHED TO THE FLIGHT DECK CENTER WINDSHIELD LEFT HAND FRAME CENTER POST LOWER NODE ATTACHMENT, INTERNAL AREA LEFT HAND VERTICAL FLANGE THE RIGHT-HAND FRAME AT FR 2 AND Y0. NEEDS TO BE MODIFIED B - [SDR AALA202407109141](https://openairdocs.org/sdr/AALA202407109141.md): Fitting · corroded · Jun 30, 2024 · N744P · Airbus A319112 · Nacelle/Pylon, Main Frame > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND PYLON SPIGOT RECEPTACLE FITTING BETWEEN PYLON RIBS 4 AND 5. REPLACED SPIGOT FITTING PER SRM 51-51-12. - [SDR AALA202407058276](https://openairdocs.org/sdr/AALA202407058276.md): Fitting · corroded · Jun 30, 2024 · N744P · Airbus A319112 · Nacelle/Pylon, Main Frame > AIRCRAFT IN BASE MAITENANCE: CORROSION ON LEFT HAND PYLON SPIGOT RECEPTACLE BETWEEN PYLON RIBS 4 AND 5. REPLACED SPIGOT FITTING PER SRM 54-51-12. - [SDR AALA202406269398](https://openairdocs.org/sdr/AALA202406269398.md): Hinge Fitting · excess play · Jun 25, 2024 · N744P · Airbus A319112 · Elevator Structure > AIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER, ELEVATOR HINGE ARM #1 BEARING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42. - [SDR AALA202406262212](https://openairdocs.org/sdr/AALA202406262212.md): Hinge Fitting · excess play · Jun 25, 2024 · N744P · Airbus A319112 · Elevator Structure > AIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER, ELEVATOR HINGE ARM #2 BEARING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42. - [SDR AALA202406264664](https://openairdocs.org/sdr/AALA202406264664.md): Hinge Fitting · excess play · Jun 25, 2024 · N744P · Airbus A319112 · Elevator Structure > AIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER, ELEVATOR HINGE ARM #3 BEARING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42. - [SDR AALA202406267533](https://openairdocs.org/sdr/AALA202406267533.md): Hinge Fitting · excess play · Jun 25, 2024 · N744P · Airbus A319112 · Elevator Structure > AIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER, ELEVATOR HINGE ARM #4 BEARING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42. - [SDR AALA202406268236](https://openairdocs.org/sdr/AALA202406268236.md): Hinge Fitting · excess play · Jun 25, 2024 · N744P · Airbus A319112 · Elevator Structure > AIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER, ELEVATOR HINGE ARM #5 BEARING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42. - [SDR AALA202406267915](https://openairdocs.org/sdr/AALA202406267915.md): Hinge Fitting · excess play · Jun 25, 2024 · N744P · Airbus A319112 · Elevator Structure > AIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER, ELEVATOR HINGE ARM #6 BEARING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42. - [SDR AALA202407103480](https://openairdocs.org/sdr/AALA202407103480.md): Fitting · none · May 13, 2024 · N744P · Airbus A319112 · Standard Practices/Structures > AIRCRAFT IN BASE MAINTENANCE: DUE TO THE MAJOR REPAIR BEING ACCOMPLISHED ON THE FLIGHT DECK CENTER WINDSHIELD FRAMING THE RIGHT HAND CONTINUITY FITTING BETWEEN FR 1 AND FR 3 AT Y0 MUST BE REPLACED PER INSTRUCTIONS OUTLINED IN EA 354062. REPLACED RIGHT HAND CON - [SDR AALA202407110176](https://openairdocs.org/sdr/AALA202407110176.md): Seat Track · corroded · May 9, 2024 · N744P · Airbus A319112 · Fuselage, Seat/Cargo Attach Fittings > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD GALLEY AREA SEAT TRACK AT FR 20 AND -Y765. REPLACED SEAT TRACK PER SRM 51-42-11. - [SDR AALA202407053431](https://openairdocs.org/sdr/AALA202407053431.md): Floor Support · corroded · May 9, 2024 · N744P · Airbus A319112 · Fuselage Miscellaneous Structure > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD GALLEY AREA FLOOR BEAM LOCATED BETWEEN FR 12 AND FR24 AT Y765. REPLACED SEAT TRACK IAW SRM 51-42-11-801. - [SDR AALA202406275160](https://openairdocs.org/sdr/AALA202406275160.md): Seat Track · corroded · May 9, 2024 · N744P · Airbus A319112 · Fuselage, Seat/Cargo Attach Fittings > AIRCRAFT IN BASE MAINTENANCE: CORROSION FORWARD CABIN FLOOR BEAM-SEAT TRACK AT FR 20 AND -Y1292. REPLACED BEAM-SEAT TRACK PER SRM 51-42-11. - [SDR AALA202406251522](https://openairdocs.org/sdr/AALA202406251522.md): Fitting · corroded · May 9, 2024 · N744P · Airbus A319112 · Fuselage Miscellaneous Structure > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT RIGHT PASSENGER / CREW DOOR CUTOUT LOWER AFT CORNER SHAPE FITTING AT FR 68 AND S23R. REPLACED AFT CORNER SHAPE FITTING PER SRM 51-72-11. - [SDR AALA202407108529](https://openairdocs.org/sdr/AALA202407108529.md): Fitting · none · May 8, 2024 · N744P · Airbus A319112 · Standard Practices/Structures > AIRCRAFT IN BASE MAINTENANCE: DUE TO THE MAJOR REPAIR BEING ACCOMPLISHED ON THE FLIGHT DECK CENTER WINDSHIELD FRAMING THE LEFT HAND CONTINUITY FITTING BETWEEN FR 1 AND FR 3 AT Y0 MUST BE REPLACED PER INSTRUCTIONS OUTLINED IN EA 354062. REPLACED LEFT HAND CONTI - [SDR AALA202406263961](https://openairdocs.org/sdr/AALA202406263961.md): Door Sill · corroded · May 8, 2024 · N744P · Airbus A319112 · Fuselage Miscellaneous Structure > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT RIGHT PASSENGER / CREW DOOR CUTOUT LOWER SILL BETWEEN FR 66 AND FR 68 AT S23R. REPLACED LOWER SILL PER SRM 51-42-11. - [SDR AALA202405240560](https://openairdocs.org/sdr/AALA202405240560.md): Stringer Splice · corroded · May 8, 2024 · N744P · Airbus A319112 · Fuselage Main, Longeron/Stringer > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON SPLICE INBOARD UPPER POSITION LOCATED AT -Y1292, STR 23R AND FR 66 IN AFT GALLEY AREA. REPLACED SPLICE PER SRM 51-42-11-801. - [SDR AALA202405235924](https://openairdocs.org/sdr/AALA202405235924.md): Splice · corroded · May 8, 2024 · N744P · Airbus A319112 · Fuselage Miscellaneous Structure > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON INBOARD UPPER SPLICE AT FR 68 AND -Y1162. REPLACED SPLICE PER SRM 51-42-11. - [SDR AALA202408138284](https://openairdocs.org/sdr/AALA202408138284.md): Shear Plate · cracked · May 7, 2024 · N744P · Airbus A319112 · Fuselage Miscellaneous Structure > AIRCRAFT IN BASE MAINTENANCE: CRACK ON SHEAR PLATE LOCATED BETWEEN FR 69 AND FR 70 AT LEVEL STR 23R IN AFT GALLEY AREA. REPLACED SHEAR PLATE PER SRM 51-72-11-911-001. Next page: https://openairdocs.org/aircraft/N744P/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 = 'N744P' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N744P/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.