# Service difficulty reports: N751UW A list on [N751UW](https://openairdocs.org/aircraft/N751UW.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 · 250 reports - [SDR AALA202606169249](https://openairdocs.org/sdr/AALA202606169249.md): Buffer · out of adjust · Jun 14, 2026 · N751UW · Airbus A319112 · Passenger/Crew Doors > AIRCRAFT WAS GROUNDED: L1 DOOR GUST LOCK INOPERATIVE. ADJUSTED L1 DOOR BUFFER PER AMM 52-11-00-820-001-A STEP 4N AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK WITH NO ISSUES NOTED. - [SDR AALA202604302696](https://openairdocs.org/sdr/AALA202604302696.md): Apu · odor · Apr 25, 2026 · N751UW · Airbus A319112 · APU Core Engine > AIRCRAFT WAS GROUNDED: FA REPORTS ROW 14 THRU 19 HAS A FOUL ODOR. MAINTENANCE REPLACED APU - [SDR AALA202604139869](https://openairdocs.org/sdr/AALA202604139869.md): Control Valve · odor · Apr 9, 2026 · N751UW · Airbus A319112 · Cabin Cooling System > AIRCRAFT WAS GROUNDED: DIRTY SOCK FUMES PERSISTED THROUGHOUT ENTIRE FLIGHT. THE WORST FUMES WERE BELOW 10,000 FEET. MAINTENANCE REPLACED L/H CONDENSER IAW AMM 21-52-32, L/H REHEATER IAW AMM 21-52-31, L/H OZONE FILTER IAW AMM 21-51-41 AND L/H FLOW CONTROL VALVE - [SDR AALA202604137797](https://openairdocs.org/sdr/AALA202604137797.md): Reheater · odor · Apr 9, 2026 · N751UW · Airbus A319112 · Cabin Cooling System > AIRCRAFT WAS GROUNDED: DIRTY SOCK FUMES PERSISTED THROUGHOUT ENTIRE FLIGHT. THE WORST FUMES WERE BELOW 10,000 FEET. MAINTENANCE REPLACED L/H CONDENSER IAW AMM 21-52-32, L/H REHEATER IAW AMM 21-52-31, L/H OZONE FILTER IAW AMM 21-51-41 AND L/H FLOW CONTROL VALVE - [SDR AALA202604136393](https://openairdocs.org/sdr/AALA202604136393.md): Control Valve · odor · Apr 9, 2026 · N751UW · Airbus A319112 · Cabin Cooling System > AIRCRAFT WAS GROUNDED: DIRTY SOCK FUMES PERSISTED THROUGHOUT ENTIRE FLIGHT. THE WORST FUMES WERE BELOW 10,000 FEET. MAINTENANCE REPLACED R/H CONDENSER IAW AMM 21-52-32, R/H REHEATER IAW AMM 21-52-31, R/H OZONE FILTER IAW AMM 21-51-41 AND R/H FLOW CONTROL VALVE - [SDR AALA202604137654](https://openairdocs.org/sdr/AALA202604137654.md): Reheater · odor · Apr 9, 2026 · N751UW · Airbus A319112 · Cabin Cooling System > AIRCRAFT WAS GROUNDED: DIRTY SOCK FUMES PERSISTED THROUGHOUT ENTIRE FLIGHT. THE WORST FUMES WERE BELOW 10,000 FEET. MAINTENANCE REMOVED AND REPLACED R/H CONDENSER IAW AMM 21-52-32, R/H REHEATER IAW AMM 21-52-31, R/H OZONE FILTER IAW AMM 21-51-41 AND R/H FLOW C - [SDR AALA202604137669](https://openairdocs.org/sdr/AALA202604137669.md): Condenser · odor · Apr 9, 2026 · N751UW · Airbus A319112 · Cabin Cooling System > AIRCRAFT WAS GROUNDED: DIRTY SOCK FUMES PERSISTED THROUGHOUT ENTIRE FLIGHT. THE WORST FUMES WERE BELOW 10,000 FEET. MAINTENANCE REPLACED R/H CONDENSER IAW AMM 21-52-32, R/H REHEATER IAW AMM 21-52-31, R/H OZONE FILTER IAW AMM 21-51-41 AND R/H FLOW CONTROL VALVE - [SDR AALA202604139038](https://openairdocs.org/sdr/AALA202604139038.md): Condenser · odor · Apr 9, 2026 · N751UW · Airbus A319112 · Cabin Cooling System > AIRCRAFT WAS GROUNDED: DIRTY SOCK FUMES PERSISTED THROUGHOUT ENTIRE FLIGHT. THE WORST FUMES WERE BELOW 10,000 FEET. MAINTENANCE REPLACED L/H CONDENSER IAW AMM 21-52-32, L/H REHEATER IAW AMM 21-52-31, L/H OZONE FILTER IAW AMM 21-51-41 AND L/H FLOW CONTROL VALVE - [SDR AALA202603275442](https://openairdocs.org/sdr/AALA202603275442.md): Plug · leaking · Mar 25, 2026 · N751UW · Airbus A319112 · APU Oil System > AIRCRAFT WAS GROUNDED: REF MIC 7196981 SOF EVENT. MAINTENANCE FOUND EVIDENCE OF DRY HYDRAULIC FLUID IN AND AROUND THE APUPLENUM AND BULK HEAD SEAL AND THE COOLING FAN. FOUND APU GEN DRAIN PLUG LEAKING. REMOVED AND REPLACED APU GEN DRAIN PLUG O-RING IAW AMM 24- - [SDR AALA202602093307](https://openairdocs.org/sdr/AALA202602093307.md): Skin Panel · cracked · Feb 6, 2026 · N751UW · Airbus A319112 · Fuselage Main, Plate/Skin > AIRCRAFT IN BASE MAINTENANCE: CRACK IN FUSELAGE SKIN PANEL BETWEEN FR 13 AND FR 14, BETWEEN WL Z+780 AND WL Z+950. REPAIRED SKIN PANEL PER EA372180 AND SRM 51-70-20. - [SDR AALA202512142117](https://openairdocs.org/sdr/AALA202512142117.md): Gasket · torn · Dec 11, 2025 · N751UW · Airbus A319112 · Passenger/Crew Doors > AIRCRAFT WAS NOT GROUNDED: LEFT EMERGENCY EXIT HANDLE ASSY GASKET TORN. MAINTENANCE REPLACED HATCH LOCKING MECHANISM FOR A TORN GASKET IAW AMM 52-21-11-400. - [SDR AALA202508040410](https://openairdocs.org/sdr/AALA202508040410.md): Apu · contaminated · Jul 23, 2025 · N751UW · Airbus A319112 · APU Oil System > AIRCRAFT WAS GROUNDED: APU DETERMINED TO BE SOURCE OF ODOR. PLACED ON MEL. MAINTENANCE DECONTAMINATED APU PER JC 26L00021014. - [SDR AALA202507230410](https://openairdocs.org/sdr/AALA202507230410.md): Apu · odor · Jul 23, 2025 · N751UW · Airbus A319112 · Airborne Auxiliary Power Unit (APU) System > AIRCRAFT WAS GROUNDED, APU DETERMINED TO BE SOURCE OF ODOR. PLACED ON MEL. (OPEN) - [SDR AALA202505283150](https://openairdocs.org/sdr/AALA202505283150.md): Shade · stuck · Apr 18, 2025 · N751UW · Airbus A319112 · Passenger Compartment Equipment > AIRCRAFT WAS NOT GROUNDED: WINDOW SHADE AT EXIT ROW14F WON'T OPEN. **SUPPLEMENTAL REPORT FOR SDR AALA202504213150.** (CLOSED)** MAINTENANCE INSTALLED EMERGENCY EXIT WINDOW SHADE AT 14 F PER AMM 25-23-47. - [SDR AALA202504213150](https://openairdocs.org/sdr/AALA202504213150.md): Shade · stuck · Apr 18, 2025 · N751UW · Airbus A319112 · Passenger Compartment Equipment > AIRCRAFT WAS NOT GROUNDED: WINDOW SHADE AT EXIT ROW14F WON'T OPEN. (OPEN) - [SDR AALA202504174792](https://openairdocs.org/sdr/AALA202504174792.md): Wire · loose · Apr 16, 2025 · N751UW · Airbus A319112 · Equipment/Furnishings Wiring > AIRCRAFT WAS GROUNDED: REAR FLIGHT ATTENDANTS AND PASSENGERS SMELLED A STRONG ELECTRIC/BATTERY BURNING SMELL IN THE REAR OF THE AIRCRAFT DURING DESCENT. SMELL DISAPPEARED PRIOR TO LANDING. MAINTENANCE FOUND ROW 22F POWER PORTS WIRING LOOSE RESCUE WIREING AND L - [SDR AALA202411271500](https://openairdocs.org/sdr/AALA202411271500.md): Angle · bent · Nov 26, 2024 · N751UW · Airbus A319112 · Fixed Inner Doors > AIRCRAFT WAS NOT GROUNDED: FORWARD LAVATORY DOOR EXTREMELY DIFFICULT TO OPEN AND CLOSED. SEEMS TO BE GETTING JAMMED AT THE BOTTOM OF THE DOOR AND FLOOR. MAINTENANCE FOUND FORWARD LAV DOOR STOP ANGLE BENT STRAIGHTENED ANGLE AS NEEDED OPS CK GOOD. - [SDR AALA202410217404](https://openairdocs.org/sdr/AALA202410217404.md): Hook · inoperative · Oct 17, 2024 · N751UW · Airbus A319112 · Service Doors > AIRCRAFT WAS IN BASE MAINTENANCE: DOOR R2 DOOR HANDLE DOES NOT LATCH UP WHEN DOOR IS OPEN. REPLACED HOOK OF LOCKING MECHANISM DOOR R2 IAW AMM 52-13-21-400-001-A. - [SDR AALA202410217903](https://openairdocs.org/sdr/AALA202410217903.md): Switch · no test · Oct 17, 2024 · N751UW · Airbus A319112 · Emergency Equipment > AIRCRAFT WAS IN BASE MAINTENANCE: EVAC COMMAND SWITCH DOES NOT WORK PROPERLY. MAINTENANCE REPLACED EVAC COMMAND SWITCH IAW ESPM 20-45-11 PAGEBLOCK 0101 CONFIG 02 AND PERFORMED OPERATIONAL TEST IAW AMM 23-73-00-710-004-A - [SDR AALA202410191382](https://openairdocs.org/sdr/AALA202410191382.md): Floorbeam · cracked · Oct 17, 2024 · N751UW · Airbus A319112 · Fuselage Main, Floor Beam > AIRCRAFT IN BASE MAINTENANCE: CABIN FLOOR BEAM BACK SIDE RADIUS CRACKED IN ZONE 2 AT THE CENTER WING BOX FRONT SPAR COMMON TO VERTICAL STRINGER 2 AT FR 36 AND +Y765. REPAIRED FLOOR BEAM PER EA 357344. - [SDR AALA202410197726](https://openairdocs.org/sdr/AALA202410197726.md): Floorbeam · cracked · Oct 17, 2024 · N751UW · Airbus A319112 · Fuselage Main, Floor Beam > AIRCRAFT IN BASE MAINTENANCE: CABIN FLOOR BEAM BACK SIDE RADIUS CRACKED IN ZONE 2 AT THE CENTER WING BOX FRONT SPAR COMMON TO VERTICAL STRINGER 4 AT FR 36 AND -Y254. REPAIRED FLOOR BEAM PER EA 357344. - [SDR AALA202410198162](https://openairdocs.org/sdr/AALA202410198162.md): Floorbeam · cracked · Oct 17, 2024 · N751UW · Airbus A319112 · Fuselage Main, Floor Beam > AIRCRAFT IN BASE MAINTENANCE: CABIN FLOOR BEAM HAS CRACKED ZONE 2 FASTENER HOLE AT THE CENTER WING BOX FRONT SPAR COMMON TO VERTICAL STRINGER 5 AT FR 36 AND -Y765. REPAIRED FLOOR BEAM PER EA 357344. - [SDR AALA202410193864](https://openairdocs.org/sdr/AALA202410193864.md): Floorbeam · cracked · Oct 17, 2024 · N751UW · Airbus A319112 · Fuselage Main, Floor Beam > AIRCRAFT IN BASE MAINTENANCE: CABIN FLOOR BEAM HAS CRACKED ZONE 2 FASTENER HOLE AT THE CENTER WING BOX FRONT SPAR COMMON TO VERTICAL STRINGER 3 AT FR 36 AND +Y254. REPAIRED FLOOR BEAM PER EA 357344. - [SDR AALA202410199911](https://openairdocs.org/sdr/AALA202410199911.md): Floorbeam · cracked · Oct 17, 2024 · N751UW · Airbus A319112 · Fuselage Main, Floor Beam > AIRCRAFT IN BASE MAINTENANCE: CABIN FLOOR BEAM HAS CRACKED ZONE 1 FASTENER HOLE AT THE CENTER WING BOX FRONT SPAR COMMON TO VERTICAL STRINGER 5 AT FR 36 AND -Y765. REPAIRED FLOOR BEAM PER EA 357344. - [SDR AALA202410197524](https://openairdocs.org/sdr/AALA202410197524.md): Floorbeam · cracked · Oct 17, 2024 · N751UW · Airbus A319112 · Fuselage Main, Floor Beam > AIRCRAFT IN BASE MAINTENANCE: CABIN FLOOR BEAM HAS CRACKED ZONE 1 FASTENER HOLE AT THE CENTER WING BOX FRONT SPAR COMMON TO VERTICAL STRINGER 3 AT FR 36 AND +Y254. REPAIRED FLOOR BEAM PER EA 357344. - [SDR AALA202410196761](https://openairdocs.org/sdr/AALA202410196761.md): Skin Panel · corroded · Oct 17, 2024 · N751UW · Airbus A319112 · Wing, Plate/Skin > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING TRALING EDGE TOP SKIN PANEL #2 LOWER SURFACE AT RIB 11 PLUS 3.900 INCHES. REPAIRED SKIN PANEL; PER EA 357532. - [SDR AALA202410190667](https://openairdocs.org/sdr/AALA202410190667.md): Skin Panel · corroded · Oct 17, 2024 · N751UW · Airbus A319112 · Wing, Plate/Skin > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING TRALING EDGE TOP SKIN PANEL #2 LOWER SURFACE AT RIB 17 PLUS 18.856 INCHES. REPAIRED SKIN PANEL; PER EA 357532. - [SDR AALA202410172515](https://openairdocs.org/sdr/AALA202410172515.md): Frame · cracked · Oct 16, 2024 · N751UW · Airbus A319112 · Fuselage Main, Frame > AIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME FORWARD FACE TO PRESSURE BULKHEAD ATTACHMENT AROUND FASTENER LOCATED 1.5 IN BELOW S30L AND FR 35. REPAIRED FRAME PER EA 357424. - [SDR AALA202410169020](https://openairdocs.org/sdr/AALA202410169020.md): Frame · cracked · Oct 15, 2024 · N751UW · Airbus A319112 · Fuselage Main, Frame > AIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME FASTENER HOLE AT FR 16 RIGHT AND DOOR STOP #7. REPLACED FRAME PER EA 357214. - [SDR AALA202410166578](https://openairdocs.org/sdr/AALA202410166578.md): Reservoir · low pressure · Oct 15, 2024 · N751UW · Airbus A319112 · Escape Slide > AIRCRAFT IN BASE MAINTENANCE: PASSENGER / CREW DOOR ESCAPE SLIDE INFLATION RESERVOIR PRESSURE LOW. REPLACED SLIDE ASSEMBLY PER TASK CARD 26C83252008. - [SDR AALA202410110862](https://openairdocs.org/sdr/AALA202410110862.md): Shear Plate · cracked · Oct 10, 2024 · N751UW · Airbus A319112 · Fuselage Miscellaneous Structure > AIRCRAFT IN BASE MAINTENANCE: CRACKED AFT CABIN FLOOR SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23R. REPLACED SHEAR PLATE PER SRM 51-42-11. - [SDR AALA202410113321](https://openairdocs.org/sdr/AALA202410113321.md): Frame · cracked · Oct 9, 2024 · N751UW · Airbus A319112 · Fuselage Main, Frame > AIRCRAFT IN BASE MAINTENANCE: CRACK ON FRAME 68 LOCATED AT LEVEL STRINGER 8R IN AFT GALLEY AREA. ACCOMPLISHED TIME LIMITED REPAIR LOCATED ON FRAME 68 AT LEVEL STRINGER 8R AT AFT GALLEY AREA PER EA 357325. - [SDR AALA202410086076](https://openairdocs.org/sdr/AALA202410086076.md): Handle · cracked · Oct 7, 2024 · N751UW · Airbus A319112 · Flight Compartment Windows > AIRCRAFT WAS IN BASE MAINTENANCE: PERFORM HFEC INSPECTION AT HANDLE SLIDING WINDOW CAPTAIN SIDE INCOCKPIT. PERFORMED HFEC INSPECTION AT HANDLE SLIDING WINDOW CAPTAIN SIDE IN COCKPITIAW CRACK INDICATION FOUND. REMOVED AND REPLACED HANDLE ON SLIDING WINDOW CAPTA - [SDR AALA202410081858](https://openairdocs.org/sdr/AALA202410081858.md): Handle · cracked · Oct 7, 2024 · N751UW · Airbus A319112 · Flight Compartment Windows > AIRCRAFT WAS IN BASE MAINTENANCE: PERFORM HFEC INSPECTION AT HANDLE SLIDING WINDOW F/O SIDE IN COCKPIT. PERFORMED HFEC INSPECTION AT HANDLE SLIDING WINDOW F/O SIDE IN COCKPIT IAW NTM 51-10-08 CRACK INDICATION FOUND. REMOVED AND REPLACED HANDLE ON SLIDING WINDO - [SDR AALA202410043099](https://openairdocs.org/sdr/AALA202410043099.md): Window Frame · cracked · Oct 3, 2024 · N751UW · Airbus A319112 · Fuselage Main, Structure > AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK CENTER WINDSHIELD FRAMING CRACKED AT THE LEFT HAND CENTER POST FRAME UPPER CORNER RADIUS AT FR 2. REPAIRED WINDHIELD FRAME PER EA 356971. - [SDR AALA202410042429](https://openairdocs.org/sdr/AALA202410042429.md): Window Frame · cracked · Oct 3, 2024 · N751UW · Airbus A319112 · Fuselage Main, Structure > AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK CENTER WINDSHIELD FRAMING CRACKED AT THE RIGHT HAND CENTER POST FRAME UPPER CORNER RADIUS AT FR 2. REPAIRED WINDHIELD FRAME PER EA 356971. - [SDR AALA202410043177](https://openairdocs.org/sdr/AALA202410043177.md): Pressure Panel · cracked · Oct 3, 2024 · N751UW · Airbus A319112 · Fuselage Main, Structure > AIRCRAFT IN BASE MAINTENANCE: CRACKED CENTER FUSELAGE PRESSURE DECK MEMEBRANE OPEN HOLES AT FR 36 AND +Y1292. REPAIRED PRESSURE DECK MEMBRANE PER EA 357069. - [SDR AALA202410038712](https://openairdocs.org/sdr/AALA202410038712.md): None · none · Oct 2, 2024 · N751UW · 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 AT FR 2 AND Y0 MUST BE REPLACED PER INSTRUCTIONS OUTLINED IN EA 356971. REPLACED LEFT HAND CONTINUITY FITTING - [SDR AALA202410037759](https://openairdocs.org/sdr/AALA202410037759.md): None · none · Oct 2, 2024 · N751UW · 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 AT FR 2 AND Y0 MUST BE REPLACED PER INSTRUCTIONS OUTLINED IN EA 356971. REPLACED RIGHT HAND CONTINUITY FITTI - [SDR AALA202410032123](https://openairdocs.org/sdr/AALA202410032123.md): Shear Plate · cracked · Oct 2, 2024 · N751UW · Airbus A319112 · Fuselage Miscellaneous Structure > AIRCRAFT IN BASE MAINTENANCE: CRACK ON AFT GALLEY SHEAR PLATE LOCATED BETWEEN FR 69 AND FR 70 AT STR 23L. REPLACED SHEAR PLATE PER SRM 51-42-11-801 - [SDR AALA202409276319](https://openairdocs.org/sdr/AALA202409276319.md): Frame · cracked · Sep 26, 2024 · N751UW · Airbus A319112 · Fuselage Main, Frame > AIRCRAFT IN BASE MAINTENANCE: AFT RIGHT PASSENGER / CREW DOOR CUT OUT UPPER AFT CORNER FRAME FITTING CRACKED AT FR68 AND S8R. REPLACED UPPER AFT CORNER FRAME FITTING PER SRM 51-72-11. - [SDR AALA202409035347](https://openairdocs.org/sdr/AALA202409035347.md): Floor Support · corroded · Aug 30, 2024 · N751UW · Airbus A319112 · Fuselage Miscellaneous Structure > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN SUPPORT BEAM BETWEEN FR 64 AND FR 66 AT +Y1292. REPLACED FLOOR SUPPORT PER SRM 51-42-11. - [SDR AALA202408287997](https://openairdocs.org/sdr/AALA202408287997.md): Hinge Fitting · excess play · Aug 24, 2024 · N751UW · Airbus A319112 · Horizontal Stabilizer Structure > AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR #4 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42. - [SDR AALA202408274183](https://openairdocs.org/sdr/AALA202408274183.md): Bolt · corroded · Aug 24, 2024 · N751UW · Airbus A319112 · Leading Edge Devices > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON BOLT ATTACHMENT LOCATED AT SLAT TRACK 12 (LOWER MID BOLT) ON LEFT-HAND WING. REPLACED BOLT PER AMM 27-84-62-400-001-A. - [SDR AALA202408272604](https://openairdocs.org/sdr/AALA202408272604.md): Bolt · corroded · Aug 24, 2024 · N751UW · Airbus A319112 · Leading Edge Devices > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON BOLT ATTACHMENT LOCATED AT SLAT TRACK 12 (LOWER FORWARD BOLT) ON LEFT-HAND WING. REPLACED BOLT PER AMM 27-84-62-400-001-A. - [SDR AALA202408278305](https://openairdocs.org/sdr/AALA202408278305.md): Fitting · corroded · Aug 24, 2024 · N751UW · Airbus A319112 · Nacelle/Pylon, Main Frame > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON SPIGOT FITTING RECEPTACLE ON RIGHT-HAND PYLON. REPLACED SPIGOT FITTING PER SRM 54-51-12-300-001. - [SDR AALA202408277155](https://openairdocs.org/sdr/AALA202408277155.md): Fitting · corroded · Aug 24, 2024 · N751UW · Airbus A319112 · Nacelle/Pylon, Main Frame > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON SPIGOT FITTING RECEPTACLE ON LEFT-HAND PYLON. REPLACED SPIGOT FITTING PER SRM 54-51-12-300-001. - [SDR AALA202408281014](https://openairdocs.org/sdr/AALA202408281014.md): Hinge Arm · excess play · Aug 23, 2024 · N751UW · Airbus A319112 · Horizontal Stabilizer Structure > AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR #1 HINGE ARM HAS EXCESSIVE PLAY. REPLACED HINGE ARM PER AMM 55-16-42. - [SDR AALA202408281072](https://openairdocs.org/sdr/AALA202408281072.md): Hinge Arm · excess play · Aug 23, 2024 · N751UW · Airbus A319112 · Horizontal Stabilizer Structure > AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR #3 HINGE ARM HAS EXCESSIVE PLAY. REPLACED HINGE ARM PER AMM 55-16-42. - [SDR AALA202408286253](https://openairdocs.org/sdr/AALA202408286253.md): Hinge Arm · excess play · Aug 23, 2024 · N751UW · Airbus A319112 · Horizontal Stabilizer Structure > AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR #2 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM PER AMM 55-16-42. Next page: https://openairdocs.org/aircraft/N751UW/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 = 'N751UW' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N751UW/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.