# Service difficulty reports: N769US A list on [N769US](https://openairdocs.org/aircraft/N769US.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 · 252 reports - [SDR AALA202610089691](https://openairdocs.org/sdr/AALA202610089691.md): Manifold · leaking · Oct 4, 2026 · N769US · Airbus A319112 · Landing Gear Brake System > AIRCRAFT WAS GROUNDED: AIRCRAFT SIGNIFICANTLY PULLS TO THE RIGHT DURING TAXI - TAKEOFF AND LANDING - MAINTENANCE FOUND THE RIGHT NORMAL BRAKE SERVO VALVE MANIFOLD LEAKING WHILE APPLYING BRAKES ALLOWING AIR TO ENTER THE SYSTEM WHICH CAUSED TO THE BRAKES TO STIC - [SDR AALA202609027673](https://openairdocs.org/sdr/AALA202609027673.md): Light · inoperative · Aug 31, 2026 · N769US · Airbus A319112 · Emergency Lighting > AIRCRAFT WAS NOT GROUNDED: DURING EMERGENCY LIGHTING TEST FOUND FORWARD AND AFT LAV AUXILIARY EMERGENCY LIGHTS INOP. MAINTENANCE REPLACED FORWARD LAV AND LAV E AUXILIARY EMERGENCY LIGHT IAW AMM 33-24-12. - [SDR AALA202606155165](https://openairdocs.org/sdr/AALA202606155165.md): Life Vest · open · Jun 12, 2026 · N769US · Airbus A319112 · Life Jacket > AIRCRAFT WAS NOT GROUNDED: ONE OF THE AFT FLIGHT ATTENDANT JUMPSEAT LIFE VEST POUCH HAS BEEN OPENED. MAINTENANCE REPLACED LIFE VEST PER AMM 25-60-00. - [SDR AALA202605278279](https://openairdocs.org/sdr/AALA202605278279.md): A/C Pack · contaminated · May 23, 2026 · N769US · Airbus A319112 · Cabin Cooling System > AIRCRAFT WAS GROUNDED: DURING APPROACH, MUSTY SOCK SMELL WAS COMING OUT OF THE VENTS ONTHE FLIGHT DECK AND IN THE CABIN. TURNED OFF CABIN FANS, TURN OFF BOTH PACKS AND OPEN THE AIR AND SMELL WENT AWAY. REF MIC 7354430. MAINTENANCE ACCOMPLISHED J/C 26L00021002, - [SDR AALA202510102661](https://openairdocs.org/sdr/AALA202510102661.md): Power Supply · faulted · Oct 8, 2025 · N769US · Airbus A319112 · Emergency Lighting > AIRCRAFT WAS NOT GROUNDED: FOUND EPSU 12WL FAULT DURING BITE TEST PRIOR TO SLIDE CHANGE. MAINTENANCE REPLACED EPSU 12WL IAW AMM 33-51-38. OPS CHECK NORMAL. - [SDR AALA202505219365](https://openairdocs.org/sdr/AALA202505219365.md): Control Valve · inoperative · May 19, 2025 · N769US · Airbus A319112 · Cabin Temperature Control System > AIRCRAFT WAS GROUNDED: ONE PACK ON MEL. ON CLIMBOUT, THE OTHER PACK FAILED AND A/C WAS UNABLE TO PRESSURIZE OR MAINTAIN TEMPERATURE. RETURNED TO MIA. NO EMERGENCY, NO OVERWEIGHT LANDING. MAINTENANCE REPLACED PACK 1 FLOW CONTROL VALVE IAW AMM 21-51-51. - [SDR AALA202412232835](https://openairdocs.org/sdr/AALA202412232835.md): Support Bracket · cracked · Dec 20, 2024 · N769US · Airbus A319112 · Fuselage Miscellaneous Structure > AIRCRAFT IN BASE MAINTENANCE: CRACKED SUPPORT BRACKET LOCATED FR 47 BETWEEN S41R AND S42R IN AFT CARGO COMPARTMENT. REPLACED SUPPORT BRACKET PER SRM 51-42-11. - [SDR AALA202412210219](https://openairdocs.org/sdr/AALA202412210219.md): Floor Panel · delaminated · Dec 19, 2024 · N769US · Airbus A319112 · Fuselage Floor Panel > AIRCRAFT IN BASE MAINTENANCE: DELAMINATED FLOOR PANEL 261DF AT AFT GALLEY AREA. REPLACED FLOOR PANEL PER JOB CARD 26C26053014. - [SDR AALA202412185669](https://openairdocs.org/sdr/AALA202412185669.md): Plate · cracked · Dec 16, 2024 · N769US · Airbus A319112 · Wing Main, Frame Structure > AIRCRAFT IN BASE MAINTENANCE: CRACK TITANIUM PLATE OUTBOARD FLAP ON RIGHT HAND WING. REPLACED TITANIUM PLATE PER SRM 51-42-11-801. - [SDR AALA202502102043](https://openairdocs.org/sdr/AALA202502102043.md): Hinge Arm · cracked · Dec 10, 2024 · N769US · Airbus A319112 · Vertical Stabilizer > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND IN OPEN FASTENER HOLE (1EA) LOCATED ON HINGE ARM FITTING 1 LOWER AREA. MAINTENANCE REPLACED HINGE ARM #1 ON TRAILING EDGE OF VERTICAL STABILIZER AND FASTENERS IAW EA #360672, A319 SRM 55-36-42-300-003, A319 - [SDR AALA202501275292](https://openairdocs.org/sdr/AALA202501275292.md): Support · corroded · Dec 8, 2024 · N769US · Airbus A319112 · Fuselage Miscellaneous Structure > AIRCRAFT IN BASE MAINTENANCE: CORROSION LOWER SILL BTW FR 66 TO FR 68 STR 23R AT AFT GALLEY AREA, MEASURE CORROSION L: 0.653 IN W:0.603 IN D:0.008 IN. MAINTENANCE REPLACED LOWER SILL BTW FR 66 TO FR 68 STRG 23R AT AFT GALLEY AREA IAW A319 SRM 51-72-911-001, S - [SDR AALA202501115612](https://openairdocs.org/sdr/AALA202501115612.md): Floorbeam · corroded · Dec 8, 2024 · N769US · Airbus A319112 · Fuselage Main, Floor Beam > AIRCRAFT IN BASE MAINTENANCE: CORROSION FLOOR BEAM +Y1292 FR 66 AT AFT GALLEY AREA MEASURES OF CORROSION ARE L=0.426 INCH, W=0.257 INCH, D=0.016 INCH. MAINTENANCE REPLACED FLOOR BEAM +Y1292 LOC BTW FR64 TO FR66 AFT GALLEY AREA IAW A319 SRM 51-72-11-901 AND DW - [SDR AALA202501110464](https://openairdocs.org/sdr/AALA202501110464.md): Floor Support · corroded · Dec 7, 2024 · N769US · Airbus A319112 · Fuselage Miscellaneous Structure > AIRCRAFT IN BASE MAINTENANCE: CORROSION FLOOR BEAM +Y1292 BTW FR 16 TO FR 20 AT FWD GALLEY AREA, MEASURES OF CORROSION ARE L=9.21 INCH, W=1.200 INCH, D=0.037 INCH. MAINTENANCE REPLACED FLOOR BEAM Y1292 BETWEEN FR12 TO FR24 AT FORWARD GALLEY AREA IAW A319 SRM - [SDR AALA202501078636](https://openairdocs.org/sdr/AALA202501078636.md): Floorbeam · corroded · Dec 7, 2024 · N769US · Airbus A319112 · Fuselage Main, Floor Beam > AIRCRAFT IN BASE MAINTENANCE: CORROSION FLOOR BEAM +Y765 AT FR 20 FWD GALLEY AREA L= 0.918 IN W= 0.580 IN D= 0.029 IN. MAINTENANCE REPLACED FLOOR BEAM Y765 LOC BTW FR 12 TO FR 24 IAW A319 SRM 51-42-11-801, SRM 51-72-11-911-001 AND DWG D53110984 AND DWG D531150 - [SDR AALA202502107367](https://openairdocs.org/sdr/AALA202502107367.md): Stringer · corroded · Dec 5, 2024 · N769US · Airbus A319112 · Fuselage Main, Longeron/Stringer > AIRCRAFT IN BASE MAINTENANCE: CORROSION STRINGER 43L LOCATED BETWEEN FR59 AND FR60 IN AFT CARGO COMPARTMENT MEASURE CORROSION IS L=11.230 INCH W=0.840 INCH D=0.015 INCH. MAINTENANCE PERFORMED TIME LIMITED REPAIR ON STRINGER 43L BETWEEN FRAME 59 AND FRAME 60 ON - [SDR AALA202502101519](https://openairdocs.org/sdr/AALA202502101519.md): Stringer · corroded · Dec 5, 2024 · N769US · Airbus A319112 · Fuselage Main, Longeron/Stringer > AIRCRAFT IN BASE MAINTENANCE: CORROSION STRINGER 42L LOCATED BETWEEN FR59 AND FR60 IN AFT CARGO COMPARTMENT. MEASURE CORRORION IS L=11.200 INCH W=0.840 INCH D=0.020 INCH. MAINTENANCE PERFORMED TIME LIMITED REPAIR ON STRINGER 42L AND FRAME 59 AND FRAME 60 ON AF - [SDR AALA202502109532](https://openairdocs.org/sdr/AALA202502109532.md): Shear Tie · corroded · Dec 5, 2024 · N769US · Airbus A319112 · Fuselage Internal Mounting Structure > AIRCRAFT IN BASE MAINTENANCE: CORROSION SHEAR TIE LOCATED FR 65 BETWEEN STR 30R AND STR 31R IN AFT CARGO COMPARTMENT,MEASURE CORROSION IS L=2.300 INCH, W=1.250 INCH AND D=0.010 INCH. MAINTENANCE - [SDR AALA202501306037](https://openairdocs.org/sdr/AALA202501306037.md): Stringer · corroded · Dec 5, 2024 · N769US · Airbus A319112 · Fuselage Main, Longeron/Stringer > AIRCRAFT IN BASE MAINTENANCE: CORROSION STRINGER 31R LOCATED ON FR65 IN AFT CARGO COMPARTMENT MEASURES OF CORROSION ARE, L=8.230INCH, W=0.980INCH, D=0.098INCH. MAINTENANCE REPLACED STRINGER 31 R/H SIDE LOCATED ON FRAME 64 THRU FRAME 67 ON LOWER FUSELAGE IAW A - [SDR AALA202501077026](https://openairdocs.org/sdr/AALA202501077026.md): Bolt · worn · Dec 5, 2024 · N769US · Airbus A319112 · Spoilers > AIRCRAFT IN BASE MAINTENANCE: WEAR ON CENTER HINGE FITTING SPOILER 4 ON BOLT ON RH WING. MAINTENANCE REPLACED BOLT THE SPOILER 4 ON RH WING FOR INSTALACION PROCESS REFER TO JOB CARD 26L00027023. - [SDR AALA202502108460](https://openairdocs.org/sdr/AALA202502108460.md): Hinge Fitting · cracked · Dec 3, 2024 · N769US · Airbus A319112 · Fuselage, Door Hinge > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON ATTACHMENT FITTING ON RH MAIN LANDING GEAR (1EA) CRACK INDICATION FOUND ON RH MLG HINGE FITTING FWD LUG WEB. MEASURE CRACK IS L=0.285 INCH. MAINTENANCE REPLACED MLG DOOR ACTUATOR FWD FITTING FR42 RH SIDE IAW EA - [SDR AALA202502104079](https://openairdocs.org/sdr/AALA202502104079.md): Beam · cracked · Dec 3, 2024 · N769US · Airbus A319112 · Fuselage Main, Structure > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND AT BEAM LAYER POSITION 2 ZONE 1 (VIEW LOOKING AFT), RADIUS BACK SIDE OF THE SPAR VERTICAL STRINGER FR 36, CRACK LENGT H=0.361 INCH APPROX. MAINTENANCE ACCOMPLISHED PERMANENT REPAIR LOCATED BEAM LAYER POSITIO - [SDR AALA202502100040](https://openairdocs.org/sdr/AALA202502100040.md): Beam · cracked · Dec 3, 2024 · N769US · Airbus A319112 · Fuselage Main, Structure > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND AT BEAM LAYER POSITION 4 ZONE 1 (VIEW LOOKING A FT), RADIUS BACK SIDE OF THE SPAR VERTICAL STRINGER FR 36. CRACK LENGT H= 0.352 INCH APPROX. MAINTENANCE ACCOMPLISHED PERMANENT REPAIR LOCATED BEAM LAYER POSIT - [SDR AALA202502101337](https://openairdocs.org/sdr/AALA202502101337.md): Fitting · cracked · Dec 3, 2024 · N769US · Airbus A319112 · Fuselage Main, Attach Fittings > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON LH MLG FWD FITTING FWD LUG WEB. MEASURE CRACK IS L=0.265 INCH. MAINTENANCE REPLACED MLG DOOR ACTUATOR FITTING FR42 LH SIDE IAW EA#361521, DRAWING R53370500, A319 SRM 51-72-11-911-001 AND A319 SRM 51-42-11 - [SDR AALA202502108992](https://openairdocs.org/sdr/AALA202502108992.md): Beam · cracked · Dec 3, 2024 · N769US · Airbus A319112 · Fuselage Main, Structure > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND AT BEAM LAYER POSITION 5 ZONE 1, RADIUS BACK SIDE OF THE SPAR VERTICAL STRINGER FR 36. CRACK LENGT H= 0.367 INCH APPROX. ACCOMPLISHED PERMANENT REPAIR LOCATED BEAM LAYER POSITION 5 ZONE 1 RADIUS BACK SIDE OF - [SDR AALA202502106003](https://openairdocs.org/sdr/AALA202502106003.md): Beam · cracked · Dec 3, 2024 · N769US · Airbus A319112 · Fuselage Main, Structure > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND AT BEAM LAYER POSITION 3 ZONE 1, RADIUS BACK SIDE OF THE SPAR VERTICAL STRINGER FR 36. CRACK LENGT H= 0.351 INCH APPROX. MAINTENANCE ACCOMPLISHED PERMANENT REPAIR LOCATED BEAM LAYER POSITION 3 ZONE 1 RADIUS - [SDR AALA202501072748](https://openairdocs.org/sdr/AALA202501072748.md): Damper · low pressure · Nov 25, 2024 · N769US · Airbus A319112 · Passenger/Crew Doors > AIRCRAFT IN BASE MAINTENANCE: LOW PRESSURE BIN DOOR DAMPER RH AND LH SIDE ALONG PASSENGER CABIN. REPLACED BIN DOOR DAMPER RH AND LH SIDE ALONG PASSENGER CABIN IAW AMM 25-24-41-960-807-A. - [SDR AALA202502115598](https://openairdocs.org/sdr/AALA202502115598.md): Door Frame · cracked · Oct 22, 2024 · N769US · Airbus A319112 · Fuselage Main, Structure > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON DOOR FRAME 16 RH SIDE HOLE 6 IN PASSENGER CABIN (1 EA). REQUIRED EA #360084. MAINTENANCE PERFORMED TIME LIMITED REPAIR ON DOOR FRAME 16 RH IAW EA#360084. - [SDR AALA202502107701](https://openairdocs.org/sdr/AALA202502107701.md): Door Frame · cracked · Oct 22, 2024 · N769US · Airbus A319112 · Fuselage Main, Structure > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON DOOR FRAME 16 RH SIDE HOLE 6 IN PASSENGER CABIN. MAINTENANCE PERFORMED TIME LIMITED REPAIR ON DOOR FRAME 16 RH SIDE IAW EA#360084. - [SDR AALA202408051951](https://openairdocs.org/sdr/AALA202408051951.md): Landing Gear · vibration · Jul 16, 2024 · N769US · Airbus A319112 · Main Landing Gear > AIRCRAFT WAS GROUNDED: UPON LIFT OFF, AIRCRAFT VIBRATES AT A MODERATE LEVEL. MAINLY FROM THE AREA AROUND THE LEFT SIDE/LEFT GEAR. FLT CREW REPORTS VIBRATION IMMEDIATELY CEASES UPON APPLICATION OF LEFT BRAKE. MAINTENANCE REPLACED THE LEFT MAIN LANDING GEAR. - [SDR AALA202407221951](https://openairdocs.org/sdr/AALA202407221951.md): Landing Gear · vibration · Jul 16, 2024 · N769US · Airbus A319112 · Landing Gear System > AIRCRAFT WAS GROUNDED: UPON LIFT OFF, AIRCRAFT VIBRATES AT A MODERATE LEVEL. MAINLY FROM THE AREA AROUND THE LEFT SIDE/LEFT GEAR. FLIGTH CREW REPORTS VIBRATION IMMEDIATELY CEASES UPON APPLICATION OF LEFT BRAKE. **SUPPLEMENTAL REPORT WILL BESUBMITTED** (OPEN) - [SDR AALA202405174170](https://openairdocs.org/sdr/AALA202405174170.md): Pin · worn · May 11, 2024 · N769US · Airbus A319112 · Main Landing Gear > AIRCRAFT WAS GROUNDED: WHILE TROUBLE SHOOTING A REPORT OF EXCESSIVE NOSE WHEEL SHIMMY AFTER TAKEOFF, MAINTENANCE FOUND THE MAIN LANDING GEAR SIDE STAY LOWER CARDAN SUB ASSEMBLIES WERE OUT OF LIMITS ON BOTH THE LEFT AND RIGHT MAIN LANDING GEARS. MAINTENANCE REP - [SDR AALA202405171303](https://openairdocs.org/sdr/AALA202405171303.md): Pin · worn · May 11, 2024 · N769US · Airbus A319112 · Main Landing Gear > AIRCRAFT WAS GROUNDED: WHILE TROUBLE SHOOTING A REPORT OF EXCESSIVE NOSE WHEEL SHIMMY AFTER TAKEOFF, MAINTENANCE FOUND THE MAIN LANDING GEAR SIDE STAY LOWER CARDAN SUB ASSEMBLIES WERE OUT OF LIMITS ON BOTH THE LEFT AND RIGHT MAIN LANDING GEARS. MAINTENANCE REP - [SDR AALA202405074229](https://openairdocs.org/sdr/AALA202405074229.md): Torque Link · worn · May 6, 2024 · N769US · Airbus A319112 · Nose/Tail Landing Gear > AIRCRAFT WAS GROUNDED: FLIGHT CREW REPORTED EXCESSIVE NOSE WHEEL SHIMMY AFTER TAKEOFF. THE WHEEL SHIMMY STOPPED WITH WHEEL RETRACTION. FLIGHT CREW REPORTED ROTATION SPEED WAS 143.MAINTENANCE FOUND THE NOSE LANDING GEAR UPPER TORQUE LINK (AALA202405074229) AND - [SDR AALA202405071013](https://openairdocs.org/sdr/AALA202405071013.md): Pin · worn · May 6, 2024 · N769US · Airbus A319112 · Nose/Tail Landing Gear > AIRCRAFT WAS GROUNDED: FLIGHT CREW REPORTED EXCESSIVE NOSE WHEEL SHIMMY AFTER TAKEOFF. THE WHEEL SHIMMY STOPPED WITH WHEEL RETRACTION. FLIGHT CREW REPORTED ROTATION SPEED WAS 143.MAINTENANCE FOUND THE NOSE LANDING GEAR UPPER TORQUE LINK (AALA202405074229) AND - [SDR AALA202404220130](https://openairdocs.org/sdr/AALA202404220130.md): Torque Link · worn · Apr 20, 2024 · N769US · Airbus A319112 · Nose/Tail Landing Gear > AIRCRAFT WAS GROUNDED: AT TAKEOFF, WHEN WEIGHT OFF NOSE GEAR, SEVERE VIBRATION/SHIMMY ENCOUNTERED. UNABLE TO READ PFD DUE TO SEVERITY. VIBRATION IMMEDIATELY STOPPED UPON SELECTION OF GEAR UP. GROUND OPERATION APPEARED NORMAL, NO VIBRATIONS OR ABNORMALITIES NOT - [SDR AALA202312032090](https://openairdocs.org/sdr/AALA202312032090.md): Inlet Guide Vane · odor · Nov 30, 2023 · N769US · Airbus A319112 · APU Core Engine > AIRCRAFT WAS GROUNDED: FA1 INFORMED ME THAT ALL THE FA'S SMELLED FUEL DURING TAXI BOTH ENGS RUNNING APU BLEED ON 5KTS TAILWIND. LASTED 5-10 MINUTES. MAINTENANCE REPLACED APU INLET GUIDE VANE PER AMM 49-23-51. - [SDR AALA202311271192](https://openairdocs.org/sdr/AALA202311271192.md): Line · out of position · Nov 24, 2023 · N769US · Airbus A319112 · Emergency Equipment > AIRCRAFT WAS GROUNDED: AIRCRAFT RETURNED TO LAX DUE TO THE AFT LEFT DOOR ARMING LEVER KEPT MOVING UP AND THE DOOR WOULD NOT STAY IN THE ARMED POSITION AFTER TAKEOFF. MAINTENANCE FOUND THE SLIDE MOORING LINE WAS WRAPPED AROUND THE GIRTBAR PREVENTING THE DOOR FR - [SDR AALA202301095109](https://openairdocs.org/sdr/AALA202301095109.md): Oven · odor · Jan 6, 2023 · N769US · Airbus A319112 · Buffet/Galleys > AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTED THE FORWARD GALLEY OVEN ON LEFT SIDE PRODUCES STRONG BURNTPLASTIC SMELL WHEN USED. MAINTENANCE REPLACED THE OVEN PER AMM 25-35-19 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK. - [SDR AALA202301043973](https://openairdocs.org/sdr/AALA202301043973.md): Engine · overpressured · Dec 24, 2022 · N769US · Airbus A319112 · Engine Oil Pressure > AIRCRAFT WAS GROUNDED, AN EMERGENCY WAS DECLARED AND ACFT RETURNED TO IND, DUE TO NR 1 ENGINE LOW OIL QUANITY AND LOW OIL PRESSURE INDICATION. FLIGHT CREW MANUALLY SHUT DOWN THE NR 1 ENGINE. ACFT LANDED SAFELY WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND AN - [SDR AALA202212273973](https://openairdocs.org/sdr/AALA202212273973.md): Oil System · leaking · Dec 24, 2022 · N769US · Airbus A319112 · Turbine Engine Oil System > AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO IND DUE TO #1 ENGINE LOW OIL QUANITY AND LOW OIL PRESSURE INDICATION. FLIGHT CREW MANUALLY SHUT DOWN #1 ENGINE. THE AIRCRAFT LANDED SAFELY AT IND WITHOUT FURTHER INCIDENT. MAINTENAN - [SDR AALA202206200060](https://openairdocs.org/sdr/AALA202206200060.md): Battery · inoperative · Jun 17, 2022 · N769US · Airbus A319112 · Emergency Equipment > AIRCRAFT WAS NOT GROUNDED: AFT FLIGHT ATTENDANT EMERGENCY FLASHLIGHT INOPERATIVE. REPLACED EMERGENCY FLASHLIGHT BATTERY AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER CMM 25-60-02. - [SDR AALA202205109948](https://openairdocs.org/sdr/AALA202205109948.md): Filter · odor · May 8, 2022 · N769US · Airbus A319112 · Air Distribution System > AIRCRAFT WAS GROUNDED: DURING DESCENT INTO CLT FLIGHT DECK ODOR DETECTED. MIX OF BURNING RUBBER/ELECTRICAL. ISOLATION ATTEMPTS ALTERNATING PACKS 1 AND 2 OFF THEN ON DID NOT HELP. ODOR IMPROVED AFTER LANDING. MAINTENANCE FOUND THE SOURCE OF THE ODOR WAS THE AVI - [SDR AALA202205181222](https://openairdocs.org/sdr/AALA202205181222.md): Apu · odor · May 6, 2022 · N769US · Airbus A319112 · APU Oil System > AIRCRAFT WAS GROUNDED: FUMES/ODOR REPORTED DURING APPROACH AND LANDING. MAINTENANCE HAS ISOLATED THE SOURCE OF THE ODOR TO THE APU. **SUPPLEMENTAL REPORT FOR AALA202205101222: REPLACED APU AND ACCOMPLISHED A SATISFACTORY LEAK / OPERATIONAL CHECK PER TASK CARD - [SDR AALA202205101222](https://openairdocs.org/sdr/AALA202205101222.md): Apu · odor · May 6, 2022 · N769US · Airbus A300* · APU Oil System > AIRCRAFT WAS GROUNDED: FUMES/ODOR REPORTED DURING APPROACH AND LANDING. MAINTENANCE HAS ISOLATED THE SOURCE OF THE ODOR TO THE APU. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN) - [SDR AALA202203287821](https://openairdocs.org/sdr/AALA202203287821.md): Frame · cracked · Mar 27, 2022 · N769US · Airbus A319112 · Fuselage Main, Frame > AIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME AT FR 68 AND LEFT-HAND DOOR STOP #1 LOWER IN BOARD FASTENER HOLE. REPAIRED FRAME PER SRM 53-41-12-300-011. - [SDR AALA202203228371](https://openairdocs.org/sdr/AALA202203228371.md): Connector · damaged · Mar 17, 2022 · N769US · Airbus A319112 · Emergency Lighting > AIRCRAFT IN BASE MAINTENANCE: CEILING LIGHT CONNECTOR 203WLA ABOVE SEAT 15ABC HAS DAMAGED WIRING. REPLACED CONNECTOR 203WLA AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-00. - [SDR AALA202203184138](https://openairdocs.org/sdr/AALA202203184138.md): Hinge Fitting · corroded · Mar 13, 2022 · N769US · Airbus A319112 · Horizontal Stabilizer Structure > AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER TRAILING EDGE #1 ELEVATOR HINGE BEARING CORRODED. REPLACED HINGE FITTING PER AMM 55-16-42. - [SDR AALA202203189518](https://openairdocs.org/sdr/AALA202203189518.md): Hinge Fitting · corroded · Mar 13, 2022 · N769US · Airbus A319112 · Horizontal Stabilizer Structure > AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER TRAILING EDGE #2 ELEVATOR HINGE BEARING CORRODED. REPLACED HINGE FITTING PER AMM 55-16-42. - [SDR AALA202203185440](https://openairdocs.org/sdr/AALA202203185440.md): Hinge Fitting · corroded · Mar 13, 2022 · N769US · Airbus A319112 · Horizontal Stabilizer Structure > AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER TRAILING EDGE #3 ELEVATOR HINGE BEARING CORRODED. REPLACED HINGE FITTING PER AMM 55-16-42. - [SDR AALA202203187144](https://openairdocs.org/sdr/AALA202203187144.md): Hinge Fitting · corroded · Mar 13, 2022 · N769US · Airbus A319112 · Horizontal Stabilizer Structure > AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER TRAILING EDGE #4 ELEVATOR HINGE BEARING CORRODED. REPLACED HINGE FITTING PER AMM 55-16-42. Next page: https://openairdocs.org/aircraft/N769US/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 = 'N769US' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N769US/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.