# Service difficulty reports: N753US

A list on [N753US](https://openairdocs.org/aircraft/N753US.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 · 269 reports

- [SDR AALA202610018807](https://openairdocs.org/sdr/AALA202610018807.md): Bottle · low pressure · Sep 29, 2026 · N753US · Airbus A319112 · Service Doors
  > AIRCRAFT WAS NOT GROUNDED: R2 DOOR DAMPER REQUIRES NITROGEN SERVICING. MAINTENANCE SERVICED THE AFT RIGHT DOOR DAMPER PER JOB CARD 26L80052001.
- [SDR AALA202609030385](https://openairdocs.org/sdr/AALA202609030385.md): Bottle · low pressure · Sep 2, 2026 · N753US · Airbus A319112 · Passenger/Crew Doors
  > AIRCRAFT WAS GROUNDED: FOUND R2 DOOR AT 300 PSI DURING PS CHECK. MAINTENANCE SERVICED R2 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00.
- [SDR AALA202608173316](https://openairdocs.org/sdr/AALA202608173316.md): Battery · no test · Aug 13, 2026 · N753US · Airbus A319112 · Emergency Lighting
  > AIRCRAFT IN BASE MAINTENANCE: FAULT MESSAGE FOR EMERGENCY POWER SUPPLY UNIT 13WL DISPLAYED DURING SYSTEM TEST - MAINTENANCE REPLACED BATTERY FOR EMERGENCY POWER SUPPLY UNIT 13WL PER AMM 33-51-38 AND ACCOMPLISHED A SATISFACTORY OPERTIONAL CHECK WITH NO FAULTS N
- [SDR AALA202608179932](https://openairdocs.org/sdr/AALA202608179932.md): Battery · no test · Aug 13, 2026 · N753US · Airbus A319112 · Emergency Lighting
  > AIRCRAFT IN BASE MAINTENANCE: FAULT MESSAGE FOR EMERGENCY POWER SUPPLY UNIT 12WL DISPLAYED DURING SYSTEM TEST - MAINTENANCE REPLACED BATTERY FOR EMERGENCY POWER SUPPLY UNIT 12WL PER AMM 33-51-38 AND ACCOMPLISHED A SATISFACTORY OPERTIONAL CHECK WITH NO FAULTS N
- [SDR AALA202608176945](https://openairdocs.org/sdr/AALA202608176945.md): Battery · no test · Aug 13, 2026 · N753US · Airbus A319112 · Emergency Lighting
  > AIRCRAFT IN BASE MAINTENANCE: FAULT MESSAGE FOR EMERGENCY POWER SUPPLY UNIT 10WL DISPLAYED DURING SYSTEM TEST - MAINTENANCE REPLACED BATTERY FOR EMERGENCY POWER SUPPLY UNIT 10WL PER AMM 33-51-38 AND ACCOMPLISHED A SATISFACTORY OPERTIONAL CHECK WITH NO FAULTS N
- [SDR AALA202608171032](https://openairdocs.org/sdr/AALA202608171032.md): Bottle · low pressure · Aug 12, 2026 · N753US · Airbus A319112 · Passenger/Crew Doors
  > AIRCRAFT IN BASE MAINTENANCE: L4 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW - SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00
- [SDR AALA202608140260](https://openairdocs.org/sdr/AALA202608140260.md): Bottle · low pressure · Aug 12, 2026 · N753US · Airbus A319112 · Passenger/Crew Doors
  > AIRCRAFT IN BASE MAINTENANCE: L4 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW - SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00
- [SDR AALA202605282237](https://openairdocs.org/sdr/AALA202605282237.md): Bottle · low pressure · May 27, 2026 · N753US · Airbus A319112 · Passenger/Crew Doors
  > AIRCRAFT WAS NOT GROUNDED: R4 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00.
- [SDR AALA202604024487](https://openairdocs.org/sdr/AALA202604024487.md): Check Valve · inoperative · Mar 30, 2026 · N753US · Airbus A319112 · Engine (Turbine/Turboprop)
  > AIRCRAFT WAS GROUNDED: DCA-ALB DIVERTED TO PHL ACCOUNT OF MAINTENANCE, NO.1 ENGINE COMPRESSION STALL INDICATION. AN EMERGENCY WAS DECLARED, AND THE AIRCRAFT WAS NOT OVERWEIGHT FOR LANDING. THE FLIGHT LANDED WITHOUT INCIDENT AND TAXIED TO THE GATE UNDER ITS OWN
- [SDR AALA202603074479](https://openairdocs.org/sdr/AALA202603074479.md): Accumulator · low pressure · Mar 6, 2026 · N753US · Airbus A319112 · Passenger/Crew Doors
  > AIRCRAFT WAS NOT GROUNDED: R2 DOOR CYLINDER ACCUMULATOR REQ SERVICING. MAINTENANCE SERVICED R2 EMER DOOR CYL IAW AMM 52-10-00.
- [SDR AALA202602028653](https://openairdocs.org/sdr/AALA202602028653.md): Elec Connector · corroded · Jan 27, 2026 · N753US · Airbus A319112 · Fuel System Wiring
  > AIRCRAFT WAS NOT GROUNDED: DURING CLIMB THROUGH FL180. FUEL LEFT TANK PUMP 2 LOW PRESSURE MESSAGE DISPLAYED. MAINTENANCE ACCOMPISHED TSM 28-21-00-810-803-A, FOUND BAD CORROSION ON CONNECTOR 27QA, CLEANED CONNECTOR AND PINS ON SWITCH. A SATISFACTORY OPERATIONAL
- [SDR AALA202511247240](https://openairdocs.org/sdr/AALA202511247240.md): Coffeemaker · odor · Nov 21, 2025 · N753US · Airbus A319112 · Buffet/Galleys
  > AIRCRAFT WAS GROUNDED: REF TSI 1694940, NEED TO ACCOMPLISH J/C 26L00021001. MAINTENANCE ACCOMPLISHED J/C 26L00021001, ISOLATED SMELL TO AFT GALLEY COFFEE MAKERS, REMOVED AND REPLACED 2 EACH AFT GALLEY COFFEE MAKER,WITH NO ODERS FOUND, REF TSI 1694940.
- [SDR AALA202511246490](https://openairdocs.org/sdr/AALA202511246490.md): Coffeemaker · odor · Nov 21, 2025 · N753US · Airbus A319112 · Buffet/Galleys
  > AIRCRAFT WAS GROUNDED: FAS REPORT AN INTERMITTENT HOT PLASTIC SMELL IN THE AFT GALLEY ON THE GROUND AND DURING CRUISE THROUGHOUT THE FLIGHT. SMELL IS ONLY NOTICEABLE IN THE AFT GALLEY AND NOWHERE ELSE ON THE AIRCRAFT. MAINTENANCE ACCOMPLISHED TSI BY ACCOMPLISH
- [SDR AALA202510237939](https://openairdocs.org/sdr/AALA202510237939.md): Light · inoperative · Oct 20, 2025 · N753US · Airbus A319112 · Emergency Lighting
  > AIRCRAFT WAS NOT GROUNDED: THE EXIT LIGHT IS NOT WORKING ON AIRCRAFT RIGHT OVER THE WING EXIT. INOP LIGHT LOCATED AC LEFT OVER WING EXIT. MAINTENANCE REPLACED EXIT LIGHT ASSEMBLY, OPS CHECKS GOOD. OK FOR SERVICE.
- [SDR AALA202508086629](https://openairdocs.org/sdr/AALA202508086629.md): Circuit Breaker · closed · Aug 6, 2025 · N753US · Airbus A319112 · Air Conditioning System Wiring
  > AIRCRAFT WAS NOT GROUNDED: ON CLIMB OUT FROM KEUG THE AIRCRAFT WOULD NOT PRESSURIZE CORRECTLY. AIRCRAFT WAS PARTIALLY PRESSURIZED WITH DIFFERENTIAL PRESSURE OF APPROXIMATELY 3 DELTA P. THE CABIN ALTITUDE WAS RISING RAPIDLY. CABIN ALTITUDE MAXED AT 11,400 FEET
- [SDR AALA202503199811](https://openairdocs.org/sdr/AALA202503199811.md): Stop Fitting · out of adjust · Mar 18, 2025 · N753US · Airbus A319112 · Passenger/Crew Doors
  > AIRCRAFT IN BASE MAINTENANCE: DURING POST HEAVY MAINTENANCE VISIT FUNCTIONAL CHECK FLIGHT THE FLIGHT CREW REPORTED THAT THE R1 DOOR UPPER SIDE WAS VIBRATING. MAINTENANCE ADJUSTED THE #7 DOOR STOP ON THE R1 DOOR PER AMM 52-11-11.
- [SDR AALA202503130088](https://openairdocs.org/sdr/AALA202503130088.md): Power Supply · no test · Mar 12, 2025 · N753US · Airbus A319112 · Emergency Lighting
  > AIRCRAFT IN BASE MAINTENANCE: EPSU 10WL FWD GALLEY FAILED TEST. MAINTENANCE REPLACED EPSU 10WL AT FWD GALLEY IAW AMM 33-51-38.
- [SDR AALA202503177308](https://openairdocs.org/sdr/AALA202503177308.md): Fitting · damaged · Mar 11, 2025 · N753US · Airbus A319112 · Emergency Lighting
  > AIRCRAFT IN BASE MAINTENANCE: REPLACE CONTINUITY FITTING LH SIDE FOR REQUIREMENT EA 360716 PART D.
- [SDR AALA202503066495](https://openairdocs.org/sdr/AALA202503066495.md): Attach Bolt · corroded · Feb 24, 2025 · N753US · Airbus A319112 · Leading Edge Devices
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION BOLT ATTACHMENT SLAT TRACK 9 FWD POSITION ON LH WING L= 0.256 IN W= 0.1030 IN D= 0.002 IN. MAINTENANCE REPLACED BOLT ATTACHMENT SLAT TRACK 9 FWD POSITION ON LH WING, THE INSTALLATION PROCEDURE IS DOCUMENTED ON JOB CARD 2
- [SDR AALA202503065611](https://openairdocs.org/sdr/AALA202503065611.md): Bolt · corroded · Feb 10, 2025 · N753US · Airbus A319112 · Leading Edge Devices
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION BOLT ATTACHMENT SLAT TRACK 7 LOWER BOLT ON RH WING. MEASURE L:0.1105 IN,W:0.0525 IN, D:0.011 IN. MAINTENANCE REPLACED BOLT ATTACHMENT SLAT TRACK#7 (LOWER BOLT) ON RH WING AW AMM 27-84-65-400-002-A STEP 4.A(4).
- [SDR AALA202501289421](https://openairdocs.org/sdr/AALA202501289421.md): Hinge Arm · excess play · Jan 27, 2025 · N753US · Airbus A319112 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY BEARING OF THE ELEVATOR HINGE ARM END FITTING 6 ON LH H ORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM END FITTING 6 ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
- [SDR AALA202503139400](https://openairdocs.org/sdr/AALA202503139400.md): Window Frame · cracked · Jan 10, 2025 · N753US · Airbus A319112 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON OPEN FASTENER HOLE JUNCTION WINDSHIELD RH LATERAL POST. CRACK DEPTH: D1-D2=0.302 INCH. MAINTENANCE PERFORMED PERMANENT REPAIR ( REPLACED RH LATERAL WINDOW FRAME) LOCATED BTW FR 4 TO FR 8 AT LEVEL -Y765 IAW EA #
- [SDR AALA202503135568](https://openairdocs.org/sdr/AALA202503135568.md): Door Frame · cracked · Jan 4, 2025 · N753US · Airbus A319112 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON OPEN FASTENER HOLE H1 LOCATED AT FR 16 RH DO OR STOP FITTING N7 MEASURE OF CRACK DEPTH IS L=0.156 INCH. MAINTENANCE REPLACED INTERCOSTAL FITTING #7 LOC. AT LEVEL DOOR STOP #7 BTW FR15 TO FOR FR16 R/H SIDE
- [SDR AALA202501281304](https://openairdocs.org/sdr/AALA202501281304.md): Hinge Arm · excess play · Jan 4, 2025 · N753US · Airbus A319112 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY BEARING OF THE ELEVATOR HINGE ARM END FITTING 6 ON RH H ORIZONTAL STABILIZER. MAINTENANCE 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 AALA202501289633](https://openairdocs.org/sdr/AALA202501289633.md): Hinge Arm · excess play · Jan 4, 2025 · N753US · Airbus A319112 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY BEARING OF THE ELEVATOR HINGE ARM END FITTING 5 ON RH H ORIZONTAL STABILIZER. 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 AALA202501286317](https://openairdocs.org/sdr/AALA202501286317.md): Hinge Arm · excess play · Jan 4, 2025 · N753US · Airbus A319112 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY BEARING OF THE ELEVATOR HINGE ARM END FITTING 4 ON RH H ORIZONTAL STABILIZER. 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 AALA202501289881](https://openairdocs.org/sdr/AALA202501289881.md): Hinge Arm · excess play · Jan 4, 2025 · N753US · Airbus A319112 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY BEARING OF THE ELEVATOR HINGE ARM END FITTING 3 ON RH H ORIZONTAL STABILIZER. 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 AALA202501273681](https://openairdocs.org/sdr/AALA202501273681.md): Hinge Arm · excess play · Jan 4, 2025 · N753US · Airbus A319112 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY BEARING OF THE ELEVATOR HINGE ARM END FITTING 2 ON RH HORIZONTAL STABILIZER. 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 AALA202501272854](https://openairdocs.org/sdr/AALA202501272854.md): Hinge Arm · excess play · Jan 4, 2025 · N753US · Airbus A319112 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY BEARING OF THE ELEVATOR HINGE ARM END FITTING 1ON RH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM END FITTING ON RH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
- [SDR AALA202501228720](https://openairdocs.org/sdr/AALA202501228720.md): Hinge Fitting · excess play · Jan 4, 2025 · N753US · Airbus A319112 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR #1 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.
- [SDR AALA202501229331](https://openairdocs.org/sdr/AALA202501229331.md): Hinge Fitting · excess play · Jan 4, 2025 · N753US · Airbus A319112 · Horizontal Stabilizer Structure
  > AIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR #2 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.
- [SDR AALA202501221148](https://openairdocs.org/sdr/AALA202501221148.md): Hinge Fitting · excess play · Jan 4, 2025 · N753US · Airbus A319112 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR #3 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.
- [SDR AALA202501222559](https://openairdocs.org/sdr/AALA202501222559.md): Hinge Fitting · excess play · Jan 4, 2025 · N753US · Airbus A319112 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR #4 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.
- [SDR AALA202501223726](https://openairdocs.org/sdr/AALA202501223726.md): Hinge Fitting · excess play · Jan 4, 2025 · N753US · Airbus A319112 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR #5 HINGE ARM END FITTING HAS EXCESSIVE PLAY. REPLACED HINGE ARM END FITTING PER AMM 55-16-42.
- [SDR AALA202503171586](https://openairdocs.org/sdr/AALA202503171586.md): Fitting · unserviceable · Jan 3, 2025 · N753US · Airbus A319112 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: REPLACE CONTINUITY FITTING RH SIDE FOR REQUIREMENT EA 360716 PART D. MAINTENANCE REPLACED CONTINUITY FITTING RH SIDE FOR REQUIREMENT IAW EA 360716 PART D LOCATED BTW FR1 AND FR2 AT LEVEL OF Y0 FOR FINAL RESTORATION INSTRUCTIONS R
- [SDR AALA202502102299](https://openairdocs.org/sdr/AALA202502102299.md): Door Sill · corroded · Jan 3, 2025 · N753US · Airbus A319112 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION LOWER SILL LH SIDE BTW FR66 AND FR68 AT AFT GALLET AREA, MEASURES OF CORROSION ARE L=4.144INCH, W=1.995INCH, W=0.028 INCH. MAINTENANCE REPLACED LOWER SILL LH SIDE BTW FR 66 AND FR 68 AT LEVEL STR 23L AT AFT GALLEY AREA I
- [SDR AALA202502066665](https://openairdocs.org/sdr/AALA202502066665.md): Fitting · corroded · Jan 3, 2025 · N753US · Airbus A319112 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT RIGHT PASSENGER / CREW DOOR CUTOUT LOWER SILL CENTER SHAPE FITTING BETWEEN FR 66 AND FR 68 AT S23R. REPLACED CENTER SHAPE FITTING PER SRM 51-42-11.
- [SDR AALA202502040893](https://openairdocs.org/sdr/AALA202502040893.md): Door Sill · corroded · Jan 3, 2025 · N753US · 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 AALA202502031218](https://openairdocs.org/sdr/AALA202502031218.md): Fitting · corroded · Jan 3, 2025 · N753US · Airbus A319112 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION CENTER FITTING AT LEVEL STR 23L BTW FR66 AND FR68 AT AFT GALLEY AREAL=1.916INCH W=0.620INCH D= 0.078INCH. MAINTENANCE REPLACED CENTER FITTING AT LEVEL STR23L BTW FR66 AND FR68 AT AFT GALLEY AREA IAW A319 SRM 51-42-11-801
- [SDR AALA202502039193](https://openairdocs.org/sdr/AALA202502039193.md): Floorbeam · incorrect · Jan 3, 2025 · N753US · Airbus A319112 · Fuselage Main, Floor Beam
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION FLOOR BEAM +Y254 FR 20 FWD GALLEY AREA MEASURES OF CORROSION ARE L=1.206INCH, W=0.682INCH, D=0.030INCH. MAINTENANCE REPLACED FLOOR BEAM Y254 FR 20 FWD GALLEY AREA IAW A319 SRM 51-42-11-801 AND DWG D53110900,DWG D53110984
- [SDR AALA202501306699](https://openairdocs.org/sdr/AALA202501306699.md): Seat Track · corroded · Jan 3, 2025 · N753US · Airbus A319112 · Fuselage, Seat/Cargo Attach Fittings
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION SEAT TRACK -Y1292 FR 20 AT FWD GALLEY AREA L= 0.323 IN W= 0.205 IN D= 0.015 IN. MAINTENANCE
- [SDR AALA202501046268](https://openairdocs.org/sdr/AALA202501046268.md): Hinge Pin · corroded · Jan 2, 2025 · N753US · Airbus A319112 · Ailerons
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AILERON HING PIN 2 R/H WING (L:0.227 INCH,W:0.080INCH,D:0.002 INCH). MAINTENANCE REPLACED AILERON HING PIN 2 R/H WING.
- [SDR AALA202501040784](https://openairdocs.org/sdr/AALA202501040784.md): Hinge Pin · corroded · Jan 2, 2025 · N753US · Airbus A319112 · Leading Edge Devices
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AILERON HING PIN 3 R/H WING (L:0.027 INCH,W:0.022 INCH,D:0.004 INCH).MAINTENANCE REPLACED AILERON HING PIN 3 R/H WING.
- [SDR AALA202501047495](https://openairdocs.org/sdr/AALA202501047495.md): Hinge Pin · corroded · Jan 2, 2025 · N753US · Airbus A319112 · Leading Edge Devices
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AILERON HINGE PIN 4 R/H WING (L:0.418 INCH, W:0.168 INCH, D:0.004 INCH). MAINTENACNE REPLACED HINGE PIN IAW AMM 27-14-41-400-001-A.
- [SDR AALA202501045781](https://openairdocs.org/sdr/AALA202501045781.md): Hinge Pin · corroded · Jan 2, 2025 · N753US · Airbus A319112 · Ailerons
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AILERON HING PIN 5 R/H WING (L:0.386 INCH, W: 0.068 INCH, D:0.002 INCH). MAINTENANCE REPLACED HING PIN 5 IAW AMM 27-14-*41-400-0001-A.
- [SDR AALA202503178586](https://openairdocs.org/sdr/AALA202503178586.md): Floorbeam · cracked · Dec 26, 2024 · N753US · Airbus A319112 · Fuselage Main, Floor Beam
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON FR36 VERTICAL STRINGER 2, ZONE 1 HOLE, CRACK DIRECTION AT 12 O CLOCK LOOKING AFT. D=0.180 IN APPROX. MAINTENANCE PERFORMED INTERIM (BUSHING REPAIR) LOC. ON FR 36 VERTICAL STRINGER 2, ZONE 1 AND FLOOR BEA
- [SDR AALA202503178636](https://openairdocs.org/sdr/AALA202503178636.md): Floorbeam · cracked · Dec 26, 2024 · N753US · Airbus A319112 · Fuselage Main, Floor Beam
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON FR36 HORIZONTAL FLOOR BEAM 5,-Y765,ZONE 1 HOLE CRACK L= 0.180 INCH. MAINTENANCE PERFORMED PERMANENT REPAIR (REPLACED DAMAGE SECTION) LOC AT THE HORIZONTAL FLOOR BEAM 5,-Y765, FRAME 36 IAW EA 360855 P
- [SDR AALA202503173423](https://openairdocs.org/sdr/AALA202503173423.md): Floorbeam · cracked · Dec 26, 2024 · N753US · Airbus A319112 · Fuselage Main, Floor Beam
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON FR36 VERTICAL STRINGER 2, ZONE 2 HOLE, CRACK DIRECTION AT 11 CLOCK LOOKING AFT. D=0.180 IN APPROX. MAINTENANCE PERFORMED INTERIM REPAIR (BUSHING REPAIR) LOC. ON FR 36 VERTICAL STRINGER 2, ZONE 2 AND FLOO
- [SDR AALA202503177920](https://openairdocs.org/sdr/AALA202503177920.md): Floorbeam · cracked · Dec 26, 2024 · N753US · Airbus A319112 · Fuselage Main, Floor Beam
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON FR36 VERTICAL STRINGER 3, ZONE 1 HOLE, CRACK DIRECTION AT 1 CLOCK LOOKING AFT. D=0.180 IN APPROX. MAINTENANCE PERFORMED INTERIM REPAIR (REPAIR BUSHING) LOC. ON FR 36 VERTICAL STRINGER 3, ZONE 1 AND FLOOR
- [SDR AALA202503174060](https://openairdocs.org/sdr/AALA202503174060.md): Beam · cracked · Dec 26, 2024 · N753US · Airbus A319112 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON FR36 VERTICAL STRINGER 3, ZONE 2 HOLE, CRACK DIRECTION AT 11 AND 9 O CLOCK LOOKING AFT. D=0.180 IN APPROX. MAINTENANCE PERFORMED INTERIM REPAIR (REPAIR BUSHING) LOC. ON FR 36 VERTICAL STRINGER 3, ZONE 2

Next page: https://openairdocs.org/aircraft/N753US/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 = 'N753US' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N753US/reports

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