# Service difficulty reports: N749US

A list on [N749US](https://openairdocs.org/aircraft/N749US.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 · 238 reports

- [SDR AALA202610070447](https://openairdocs.org/sdr/AALA202610070447.md): Bottle · low pressure · Oct 4, 2026 · N749US · Airbus A319112 · Passenger/Crew Doors
  > AIRCRAFT WAS NOT GROUNDED: R1 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW - SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00
- [SDR AALA202609220163](https://openairdocs.org/sdr/AALA202609220163.md): Bottle · low pressure · Sep 19, 2026 · N749US · Airbus A319112 · Passenger/Crew Doors
  > AIRCRAFT WAS NOT GROUNDED: RIGHT FORWARD NEEDS SERVICE, PSI AT 900, AMBIENT TEMP 86 F. MAINTENANCE SERVICED FORWARD DOOR DAMPER PER WORK CARD 26L80052001. OK FOR SERVICE.
- [SDR AALA202607177424](https://openairdocs.org/sdr/AALA202607177424.md): Bottle · low pressure · Jul 15, 2026 · N749US · Airbus A319112 · Passenger/Crew Doors
  > AIRCRAFT WAS NOT GROUNDED: R1 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE BELOW LIMITS. MAINTENANCE SERVICED R1 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER TO OPERATIONAL RANGE PER AMM 52-10-00.
- [SDR AALA202605068552](https://openairdocs.org/sdr/AALA202605068552.md): Bottle · low pressure · May 6, 2026 · N749US · Airbus A319112 · Passenger/Crew Doors
  > AIRCRAFT IN BASE MAINTENANCE: WHILE DOING PS CHECK FOUND R1 PASSENGER DOOR DAMPER LOW. APPROXIMATE TEMPERATURE 58F AND PRESSURE 1100. MAINTENANCE SERVICED DOOR DAMPER IAW JOBCARD 26L80052001.
- [SDR AALA202604289203](https://openairdocs.org/sdr/AALA202604289203.md): Fitting · cracked · Apr 22, 2026 · N749US · Airbus A319112 · Fuselage Main, Attach Fittings
  > AIRCRAFT IN BASE MAINTENANCE: FUSELAGE KEEL BEAM LT MLG DOOR FITTING INSPECTION - LOOSE FASTENER. MAINTENANCE REPLACED LH MLG ACTUATOR FITTING IAW EA #374453.
- [SDR AALA202604228310](https://openairdocs.org/sdr/AALA202604228310.md): Bottle · low pressure · Apr 20, 2026 · N749US · Airbus A319112 · Passenger/Crew Doors
  > AIRCRAFT IN BASE MAINTENANCE: R1 DOOR BOTTLE REQUIRES SERVICING. MAINTENANCE SERVICED R1 DOOR DAMPENER IAW AMM 52-10-00.
- [SDR AALA202602069721](https://openairdocs.org/sdr/AALA202602069721.md): Light · inoperative · Feb 5, 2026 · N749US · Airbus A319112 · Emergency Lighting
  > AIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHT AT SEAT 27C DOES NOT TURN ON. REPLACED EMERGENCY LIGHT AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM PER AMM 33-51-00 WITH NO ISSUES NOTED.
- [SDR AALA202511102428](https://openairdocs.org/sdr/AALA202511102428.md): Bottle · low pressure · Nov 10, 2025 · N749US · Airbus A319112 · Passenger/Crew Doors
  > AIRCRAFT WAS NOT GROUNDED: R1 DOOR ASSIST BOTTLE REQUIRES SERVICING. MAINTENANCE SERVICED R1 DOOR DAMPER PER AMM 52-10-00.
- [SDR AALA202508158865](https://openairdocs.org/sdr/AALA202508158865.md): Bottle · low pressure · Aug 14, 2025 · N749US · Airbus A319112 · Service Doors
  > AIRCRAFT WAS NOT GROUNDED: WHILE PREFORMING PS CHECK FOUND R1 DOOR EMERGENCY CYLINDER ACCUMULATOR BELOW LIMITS. MAINTENANCE CHARGED CYLINDER ACCUMLATOR IAW AMM 52-10-00.
- [SDR AALA202507170746](https://openairdocs.org/sdr/AALA202507170746.md): Battery · discharged · Jul 16, 2025 · N749US · Airbus A319112 · Emergency Equipment
  > AIRCRAFT WAS NOT GROUNDED: FWD EMERGENCY BULLHORN INOP. BATTERY DEAD. MAINTENANCE REPLACED FWD BULLHORN AS REQUIRED IAW 25-00.
- [SDR AALA202506020542](https://openairdocs.org/sdr/AALA202506020542.md): Bottle · low pressure · Jun 2, 2025 · N749US · Airbus A319112 · Passenger/Crew Doors
  > AIRCRAFT WAS NOT GROUNDED: R1 DOOR ACCUMULATOR PRESSURE IS 1200PSI AT 70 DEGREES F. MAINTENANCE CHARGED R1 DOOR ACCUMULATOR IAW AMM 52-10-00.
- [SDR AALA202503311172](https://openairdocs.org/sdr/AALA202503311172.md): Switch · inoperative · Mar 28, 2025 · N749US · Airbus A319112 · Emergency Lighting
  > AIRCRAFT WAS NOT GROUNDED: WHEN THE EMERGENCY LIGHT SWITCH IN THE OVERHEAD PANEL IS SELECTED IN THE"OFF" POSITION, ALL EMERGENCY LIGHTS IN THE CABIN TURNAND REMAIN ON. MAINTENANCE REPLACED EMGERGENCY LIGHT SWITCH IAW AMM 31-41-25 OSP CHECK GOOD AT THIS TIME.
- [SDR AALA202503177048](https://openairdocs.org/sdr/AALA202503177048.md): Shade · stuck · Mar 14, 2025 · N749US · Airbus A319112 · Passenger Compartment Equipment
  > AIRCRAFT WAS NOT GROUNDED: WINDOW SHADE AT 14F STUCK MOSTLY CLOSED (EXIT ROW). MAINTENANCE REINSTALLED WINDOW SHADE 14F IAW AMM 25-23-43.
- [SDR AALA202501077392](https://openairdocs.org/sdr/AALA202501077392.md): Damper · no test · Jan 5, 2025 · N749US · Airbus A319112 · Passenger/Crew Doors
  > AIRCRAFT IN BASE MAINTENANCE: DONT PASS TEST DAMPING FUNCTION ON DOOR DAMPER AND EMERGENCY OPERATIONCYLINDER IN PASSENGER CREW DOOR 841. MAINTENANCE REPLACED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER ONPASSENGER CREW DOOR 841 AT FWD GALLEY AREA I.A.W AMM 52
- [SDR AALA202501071451](https://openairdocs.org/sdr/AALA202501071451.md): Floorbeam · cracked · Jan 3, 2025 · N749US · Airbus A319112 · Fuselage Main, Floor Beam
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON FRAME 36 HORIZONTAL FLOOR BEAM AT ATTACHMENT AREA TO VERTICAL STRINGER 5, ZONE 2 AFT FACE VERTICAL RADIUS, CRACK LENGHT IS 0.270 IN. MAINTENANCE PERFORMED PERMANENT REPAIR ON FRAME 36 HORIZONTAL FLOOR BEAM AT A
- [SDR AALA202501075858](https://openairdocs.org/sdr/AALA202501075858.md): Floorbeam · cracked · Jan 3, 2025 · N749US · Airbus A319112 · Fuselage Main, Floor Beam
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON FRAME 36 FRONT SPAR VERTICAL STRINGER 1 OPEN FASTENER HOLE IN ZONE 1, CRACK DIRECTION IS 2 OCLOCK CRACK DEPTH IS 0.119 INCH APPROX IN FWD CARGO COMPARMENT. MAINTENANCE PERFORMED PERMANENT REPAIR ON FRAME 36 FRO
- [SDR AALA202501076299](https://openairdocs.org/sdr/AALA202501076299.md): Floorbeam · cracked · Jan 3, 2025 · N749US · Airbus A319112 · Fuselage Main, Floor Beam
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON FRAME 36 HORIZONTAL FLOOR BEAM AT ATTACHMENT AREA TO VERTICAL STRINGER 3, ZONE 2 AFT FACE VERTICAL RADIUS, CRACK LENGTH IS 0.205 IN. MAINTENANCE PERFORMED PERMANENT REPAIR ON FRAME 36 HORIZONTAL FLOOR BEAM AT A
- [SDR AALA202501078581](https://openairdocs.org/sdr/AALA202501078581.md): Floorbeam · cracked · Jan 3, 2025 · N749US · Airbus A319112 · Fuselage Main, Floor Beam
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON FRAME 36 FRONT SPAR VERTICAL STRINGER 1 OPEN FASTENER HOLE IN ZONE 2, CRACK DIRECTION IS 12 OCLOCK CRACK DEPTH IS 0.110 INCH APPROX IN FWD CARGO COMPARMENT. MAINTENANCE PERFORMED PERMANENT REPAIR ON FRAME 36 FR
- [SDR AALA202501070089](https://openairdocs.org/sdr/AALA202501070089.md): Floorbeam · cracked · Jan 3, 2025 · N749US · Airbus A319112 · Fuselage Main, Floor Beam
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON FRAME 36 FRONT SPAR VERTICAL STRINGER 6 OPEN FASTENER HOLE IN ZONE 1, CRACK DIRECTION IS 12 O CLOCK CRACK LENGHT IS 0.115 IN. MAINTENANCE PERFORMED PERMANENT REPAIR ON FRAME 36 FRONT SPAR VERTICAL STRINGER 6 OP
- [SDR AALA202501071262](https://openairdocs.org/sdr/AALA202501071262.md): Floorbeam · cracked · Jan 3, 2025 · N749US · Airbus A319112 · Fuselage Main, Floor Beam
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON FRAME 36 HORIZONTAL FLOOR BEAM AT ATTACHMENT AREA TO VERTICAL STRINGER 4, ZONE 2 AFT FACE VERTICAL RADIUS. CRACK LENGHT IS 0.280 IN. MAINTENANCE PERFORMED PERMANENT REPAIR ON FRAME 36 HORIZONTAL FLOOR BEAM AT
- [SDR AALA202501076356](https://openairdocs.org/sdr/AALA202501076356.md): Floorbeam · cracked · Jan 3, 2025 · N749US · Airbus A319112 · Fuselage Main, Floor Beam
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON FRAME 36 HORIZONTAL FLOOR BEAM AT ATTCHMENT AREA TO VERTICAL STRINGER 2, ZONE 1 AFT FACE VERTICAL RADIUS CRACK LENGHT IS 0.210 IN. MAINTENANCE PERFORMED PERMANENT REPAIR ON FRAME 36 HORIZONTAL FLOOR BEAM AT ATT
- [SDR AALA202501072096](https://openairdocs.org/sdr/AALA202501072096.md): Stiffener · cracked · Jan 3, 2025 · N749US · Airbus A319112 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON FRAME 36 FRONT SPAR VERTICAL STRINGER 6 OPEN FASTENER HOLE IN ZONE 2, CRACK DIRECTION IS 12 O CLOCK, CRACK LENGHT IS 0.110 IN. MAINTENANCE PERFORMED PERMANENT REPAIR ON FRAME 36 FRONT SPAR VERTICAL STRINGER 6 O
- [SDR AALA202501049917](https://openairdocs.org/sdr/AALA202501049917.md): Shear Plate · cracked · Jan 3, 2025 · N749US · Airbus A319112 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK ON SHEAR PLATE LOCATED BETWEEN FR 69 TO FR 70 AT LEVEL OF STRINGER 23 LH SIDE AFT PAX CABIN. CRACK LENGTH: 1.213 INCHES. MAINTENANCE REPLACED SHEAR PLATE LOCATED BETWEEN FR 69 TO FR 70 AT LEVEL OF STRINGER 23 LH SIDE AFT PAX
- [SDR AALA202501048731](https://openairdocs.org/sdr/AALA202501048731.md): Door · cracked · Jan 3, 2025 · N749US · Airbus A319112 · Passenger/Crew Doors
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION WAS FOUND IN HOLE 7 LOC AT FR16 DOUBLER JUGGLE AREA, LH SIDE, AT LEVEEL DOOR STOP 7. CONFIRM INDICATION USING BOROSCOPE VIEW IAW NTM 51-90-00. CRACK DEPTH: 0.110 INCHES
- [SDR AALA202412234823](https://openairdocs.org/sdr/AALA202412234823.md): Damper · no test · Dec 21, 2024 · N749US · Airbus A319112 · Passenger/Crew Doors
  > AIRCRAFT IN BASE MAINTENANCE: DONT PASS TEST DAMPING FUNCTION ON DOOR DAMPER AND EMERGENCY OPERATIONCYLINDER IN PASSENGER CREW DOOR 831. MAINTENANCE REPLACED DOOR DAMPER ONPASSENGER CREW DOOR 831 AT FWD GALLEY AREAI.A.W AMM 52-11-14-000-001-B AND AMM 52-11-14
- [SDR AALA202412174451](https://openairdocs.org/sdr/AALA202412174451.md): Frame · cracked · Dec 17, 2024 · N749US · Airbus A319112 · Fuselage Main, Frame
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON FORWARD GALLEY AREA FR 16 RIGHT HAND SIDE. REPLACED HALF OF FRAME PER EA 358565.
- [SDR AALA202412170292](https://openairdocs.org/sdr/AALA202412170292.md): Frame · cracked · Dec 17, 2024 · N749US · Airbus A319112 · Fuselage Main, Frame
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON FORWARD GALLEY AREA FR 16 RIGHT HAND SIDE. REPAIRED FRAME PER EA 358565.
- [SDR AALA202412175094](https://openairdocs.org/sdr/AALA202412175094.md): Frame · cracked · Dec 17, 2024 · N749US · Airbus A319112 · Fuselage Main, Frame
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON FORWARD GALLEY AREA FR 16 RIGHT HAND SIDE. REPAIRED FRAME PER EA 358565.
- [SDR AALA202412145243](https://openairdocs.org/sdr/AALA202412145243.md): Window Frame · cracked · Dec 14, 2024 · N749US · Airbus A319112 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION IN FLIGHT DECK FRAME 2 WINDSHIELD CENTER POST LOWER ATTACHMENT INTERNAL AREA LEFT SIDE, FROM UPPER TENSION BOLT IN VERTICAL FLANGE. REPAIRED FRAME PER EA 358602.
- [SDR AALA202412148226](https://openairdocs.org/sdr/AALA202412148226.md): Window Frame · cracked · Dec 13, 2024 · N749US · Airbus A319112 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION IN FLIGHT DECK FRAME 2 WINDSHIELD CENTER POST LOWER ATTACHMENT INTERNAL AREA RIGHT SIDE, FROM UPPER TENSION BOLT IN VERTICAL FLANGE. REPAIRED FRAME PER EA 358602.
- [SDR AALA202412142893](https://openairdocs.org/sdr/AALA202412142893.md): Fitting · cracked · Dec 13, 2024 · N749US · Airbus A319112 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACKED FLIGHT DECK FRONT WINDSHIELD FRAME RIGHT HAND CONTINUITY FITTING AT FR 2. REPLACED CONTINUITY FITTING PER EA 358602
- [SDR AALA202412163890](https://openairdocs.org/sdr/AALA202412163890.md): Bottle · no test · Dec 12, 2024 · N749US · Airbus A319112 · Passenger/Crew Doors
  > AIRCRAFT IN BASE MAINTENANCE: DONT PASS TEST DAMPING FUNCTION ON DOOR DAMPER AND EMERGENCY OPERATIONCYLINDER IN PASSENGER CREW DOOR 841 MAINTENANCE REPLACED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER ONPASSENGER CREW DOOR 841 AT FWD GALLEY AREA I.A.W AMM 52-
- [SDR AALA202412137365](https://openairdocs.org/sdr/AALA202412137365.md): Intercostal · cracked · Dec 12, 2024 · N749US · Airbus A319112 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACKED INTERCOSTAL FITTING AT FR 16 RIGHT AND #7 DOOR STOP FITTING. REPLACED INTERCOSTAL FITTING PER SRM 51-42-11.
- [SDR AAL2024F00008](https://openairdocs.org/sdr/AAL2024F00008.md): Frame · cracked · Nov 5, 2024 · N749US · Airbus A319112 · Fuselage Main, Frame
  > AIRCRAFT IN BASE MAINTENANCE: CRACKED AFT PASSENGER / CREW DOOR CUTOUT AFT UPPER FRAME CORNER FITTING FORWARD FACE AT FR 68 AND S8R. REPLACED FRAME CORNER FITTING PER SRM 51-42-11.
- [SDR AALA202411045383](https://openairdocs.org/sdr/AALA202411045383.md): Bottle · failed insp · Nov 2, 2024 · N749US · Airbus A319112 · Passenger/Crew Doors
  > AIRCRAFT IN BASE MAINTENANCE: DONT PASS OPERATIONAL TEST DAMPING FUNCTION ON PASSENGER CREW DOOR 832. MAINTENANCE REPLACED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER ONPASSENGER CREW DOOR 832 AT AFT GALLEY AREA I.A.W AMM 52-13-14-000-001-B ANDAMM 52-13-14
- [SDR AALA202411016404](https://openairdocs.org/sdr/AALA202411016404.md): Support Frame · excess play · Oct 31, 2024 · N749US · Airbus A319112 · Ailerons
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY AILERON HINGE SUPPORT FRAME 5 ON LH WING. FINAL REPAIR RESOLUTION: FOR OPERATIONAL TEST FOR CORRECT MOVEMENT OF AILERON IAW AMM 27-14-00-710-001-A REFER TO NCN 6833726. MAINTENANCE REPLACED AILERON HINGE SUPPORT FR
- [SDR AALA202411010782](https://openairdocs.org/sdr/AALA202411010782.md): Support Frame · excess play · Oct 31, 2024 · N749US · Airbus A319112 · Ailerons
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY AILERON HINGE SUPPORT FRAME 4 ON LH WING. MAINTENANCE REPLACED AILERON HINGE SUPPORT FRAME #4 ON LH WING I.A.W AMM 57-51-31-000-001-A AND AMM 57-51-31-400-001-A.
- [SDR AALA202410308489](https://openairdocs.org/sdr/AALA202410308489.md): Hinge Bracket · excess play · Oct 29, 2024 · N749US · Airbus A319112 · Ailerons
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY AILERON HINGE SUPPORT FRAME 5 ON RH WING. MAINTENANCE REPLACED AILERON HINGE SUPPORT FRAME #5 ON RH WING I.A.W AMM 57-51-31-000-001-A AND AMM 57-51-31-400-001-A.
- [SDR AALA202410305942](https://openairdocs.org/sdr/AALA202410305942.md): Hinge Bracket · excess play · Oct 29, 2024 · N749US · Airbus A319112 · Ailerons
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY AILERON HINGE SUPPORT FRAME 4 ON RH WING. REPLACED AILERON HINGE SUPPORT FRAME #4 ON RH WING I.A.W AMM 57-51-31-000-001-A AND AMM 57-51-31-400-001-A.
- [SDR AALA202410244882](https://openairdocs.org/sdr/AALA202410244882.md): Hinge Fitting · excess play · Oct 19, 2024 · N749US · Airbus A319112 · Horizontal Stabilizer Structure
  > AIRCRAFT WAS IN BASE MAINTENANCE: EXCESSIVE PLAY ON ELEVATOR HINGE ARM END FITTING NO 4 ON LH HORIZONTAL STABILIZER. REMOVED AND INSTALLED NEW HINGE ARM END-FITTING #4 ON LH ELEVATOR I.A.W AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
- [SDR AALA202410241260](https://openairdocs.org/sdr/AALA202410241260.md): Hinge Fitting · excess play · Oct 19, 2024 · N749US · Airbus A319112 · Horizontal Stabilizer Structure
  > AIRCRAFT WAS IN BASE MAINTENANCE: EXCESSIVE PLAY ON ELEVATOR HINGE ARM END FITTING NO 3 ON LH HORIZONTAL STABILIZER. REMOVED AND INSTALLED NEW HINGE ARM END-FITTING #3 ON LH ELEVATOR I.A.W AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A
- [SDR AALA202410246417](https://openairdocs.org/sdr/AALA202410246417.md): Hinge Fitting · excess play · Oct 19, 2024 · N749US · Airbus A319112 · Horizontal Stabilizer Structure
  > AIRCRAFT WAS IN BASE MAINTENANCE: EXCESSIVE PLAY ON ELEVATOR HINGE ARM END FITTING NO 2 ON LH HORIZONTAL STABILIZER. REMOVED AND INSTALLED NEW HINGE ARM END-FITTING #2 ON LH ELEVATOR I.A.W AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
- [SDR AALA202410241746](https://openairdocs.org/sdr/AALA202410241746.md): Hinge Fitting · excess play · Oct 19, 2024 · N749US · Airbus A319112 · Horizontal Stabilizer Structure
  > AIRCRAFT WAS IN BASE MAINTENANCE: EXCESSIVE PLAY ON ELEVATOR HINGE ARM END FITTING NO 1 ON LH HORIZONTAL STABILIZER. REMOVED AND INSTALLED NEW HINGE ARM END-FITTING #1 ON LH ELEVATOR I.A.W AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
- [SDR AALA202410249997](https://openairdocs.org/sdr/AALA202410249997.md): Hinge Fitting · excess play · Oct 19, 2024 · N749US · Airbus A319112 · Horizontal Stabilizer Structure
  > AIRCRAFT WAS IN BASE MAINTENANCE: EXCESSIVE PLAY ON ELEVATOR HINGE ARM END FITTING NO 6 ON RH HORIZONTAL STABILIZER. REMOVED AND REPLACED HINGE ARM END-FITTING #6 ON RH ELEVATOR I.A.W AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
- [SDR AALA202410244524](https://openairdocs.org/sdr/AALA202410244524.md): Hinge Fitting · excess play · Oct 19, 2024 · N749US · Airbus A319112 · Horizontal Stabilizer Structure
  > AIRCRAFT WAS IN BASE MAINTENANCE: EXCESSIVE PLAY ON ELEVATOR HINGE ARM END FITTING NO 2 ON RH HORIZONTAL STABILIZER. REMOVED AND REPLACE NEW HINGE ARM END-FITTING #2 ON RH ELEVATORI.A.W AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
- [SDR AALA202410240821](https://openairdocs.org/sdr/AALA202410240821.md): Hinge Fitting · excess play · Oct 19, 2024 · N749US · Airbus A319112 · Horizontal Stabilizer Structure
  > AIRCRAFT WAS IN BASE MAINTENANCE: EXCESSIVE PLAY ON ELEVATOR HINGE ARM END FITTING NO 1 ON RH HORIZONTAL STABILIZER. REMOVED AND REPLACED NEW HINGE ARM END-FITTING #1 ON RH ELEVATORI.A.W AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A
- [SDR AALA202410243278](https://openairdocs.org/sdr/AALA202410243278.md): Hinge Fitting · excess play · Oct 19, 2024 · N749US · Airbus A319112 · Horizontal Stabilizer Structure
  > AIRCRAFT WAS IN BASE MAINTENANCE: EXCESSIVE PLAY ON ELEVATOR HINGE ARM END FITTING NO 5 ON RH HORIZONTAL STABILIZER. REMOVED AND REPLACED HINGE ARM END-FITTING #5 ON RH ELEVATOR I.A.W AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A
- [SDR AALA202410243947](https://openairdocs.org/sdr/AALA202410243947.md): Hinge Fitting · excess play · Oct 19, 2024 · N749US · Airbus A319112 · Horizontal Stabilizer Structure
  > AIRCRAFT WAS IN BASE MAINTENANCE: EXCESSIVE PLAY ON ELEVATOR HINGE ARM END FITTING NO 4 ON RH HORIZONTAL STABILIZER. REMOVED AND REPLACED HINGE ARM END-FITTING #4 ON RH ELEVATOR I.A.W AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
- [SDR AALA202410241648](https://openairdocs.org/sdr/AALA202410241648.md): Hinge Fitting · excess play · Oct 19, 2024 · N749US · Airbus A319112 · Elevator Control System
  > AIRCRAFT WAS IN BASE MAINTENANCE: EXCESSIVE PLAY ON ELEVATOR HINGE ARM END FITTING NO 3 ON RH HORIZONTAL STABILIZER. REMOVED AND REPLACED HINGE ARM END-FITTING #3 ON RH ELEVATOR I.A.W AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
- [SDR AALA202410162855](https://openairdocs.org/sdr/AALA202410162855.md): Fitting · corroded · Oct 15, 2024 · N749US · Airbus A319112 · Nacelle/Pylon, Main Frame
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND PYLON SPIGOT FITTING RECEPTACLE BETWEEN PYLONS RIB 4 AND 5. REPLACED SPIGOT FITTING PER SRM 54-51-12.

Next page: https://openairdocs.org/aircraft/N749US/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 = 'N749US' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N749US/reports

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