# Service difficulty reports: N773XF

A list on [N773XF](https://openairdocs.org/aircraft/N773XF.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 2 · 95 reports

- [SDR AALA202610160404](https://openairdocs.org/sdr/AALA202610160404.md): Bottle · low pressure · Oct 16, 2026 · N773XF · Airbus A319112 · Passenger/Crew Doors
  > AIRCRAFT WAS NOT GROUNDED: L2 DOOR ASSIST BOTTLE LOW PSI. MAINTENANCE SERVICED L2 DOOR ASSIT BOTTLE IN REFERENCE TO AMM 52-11-14.
- [SDR AALA202607225704](https://openairdocs.org/sdr/AALA202607225704.md): Proximity Sensor · damaged · Jul 19, 2026 · N773XF · Airbus A319112 · Landing Gear Position and Warning
  > AIRCRAFT WAS GROUNDED: ON LANDING GEAR EXTENSION DURING APPROACH, ECAM L/G NOT DOWNLOCKED WITH CRC. FLIGHT CREW RECYCLED GEAR PER ECAM AND THE GEAR EXTENDED SUCCESSFULLY. MAINTENANCE FOUND PROXIMITY SENSOR 34GA OUT OF ADJUSTMENT AND DAMAGED. MAINTENANCE REPLA
- [SDR AALA202607139289](https://openairdocs.org/sdr/AALA202607139289.md): Battery · discharged · Jul 9, 2026 · N773XF · Airbus A319112 · Emergency Lighting
  > AIRCRAFT WAS NOT GROUNDED: MAINTENANCE FOUND THE LEFT MID DOOR EMERGENCY POWER SUPPLY UNIT BATTERY DRAINED. REPLACED BATTERY PER AMM 33-51-38.
- [SDR AALA202607132589](https://openairdocs.org/sdr/AALA202607132589.md): Bottle · low pressure · Jul 9, 2026 · N773XF · Airbus A319112 · Passenger/Crew Doors
  > AIRCRAFT WAS NOT GROUNDED: L4 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00.
- [SDR AALA202606126923](https://openairdocs.org/sdr/AALA202606126923.md): Control Unit · faulted · Jun 8, 2026 · N773XF · Airbus A319112 · Aircraft Fuel Distribution System
  > AIRCRAFT WAS NOT GROUNDED: AN EMERGENCY WAS DECLARED INTO PHL DUE TO THE FLIGHT CREW REPORTING THAT THE RIGHT FUEL OUTER TANK WAS INDICATING GREEN (OPEN. POSITION) BUT FUEL WAS NEVER TRANSFERRED TO THE INNER TANK TILL FINAL AT 20 00 FEET. THE LEFT TRANSFERRED
- [SDR AALA202605045237](https://openairdocs.org/sdr/AALA202605045237.md): Bottle · low pressure · Apr 29, 2026 · N773XF · Airbus A319112 · Passenger/Crew Doors
  > AIRCRAFT IN BASE MAINTENANCE: LH AFT DOOR ACCUMULATOR LOW PRESSURE. MAINTENANCE SERVICED AFT L/H DOOR EMERGENCY ASSIST BOTTLE, IAW AMM 52-10-00.
- [SDR AALA202603274654](https://openairdocs.org/sdr/AALA202603274654.md): Escape Rope · misinstalled · Mar 25, 2026 · N773XF · Airbus A319112 · Emergency Equipment
  > AIRCRAFT WAS NOT GROUNDED: AIRCRAFT LEFT SIDE OVER-WING EMERGENCY EXIT ROPE TANGLED; NEEDS TO BE RE-STOWED CORRECTLY. MAINTENANCE RE-STOWED LH CABIN EMERGENCY ESCAPE ROPE - IAW AMM 25-62-00.
- [SDR AALA202602183501](https://openairdocs.org/sdr/AALA202602183501.md): Fcu · leaking · Feb 16, 2026 · N773XF · Airbus A319112 · APU Engine Fuel and Control
  > AIRCRAFT WAS GROUNDED: AIRCRAFT HAD SUBTLE HINTS OF ODOR SIMILAR TO SOF EVENT BUT NOT BAD ENOUGH OR PERSISTENT ENOUGH TO WARRANT ACTION AIRBORNE. IT WAS NOTICEABLE FOR A SHORT TIME DURING ENGINE START AND TAXI BUT THEN DISSIPATED, AND AGAIN IN A SIMILAR FASHIO
- [SDR AALA202602189663](https://openairdocs.org/sdr/AALA202602189663.md): Fcu · odor · Feb 10, 2026 · N773XF · Airbus A319112 · APU Engine Fuel and Control
  > AIRCRAFT WAS GROUNDED: INBOUND FLIGHT ATTENDANTS REPORTED THAT ON THE DECENT IN THE KEY WEST BELOW 10,000 FT THEY SMELT A VERY STRONG OILY, CAR GARAGE, MUSTY SOCK ODOR SMELL ONE OF THEM FELT FLUSH THE OTHER ONE BEGAN TO GET SYMPTOMS OF A HEADACHE. DURING PRE-
- [SDR AALA202602129663](https://openairdocs.org/sdr/AALA202602129663.md): Apu · odor · Feb 10, 2026 · N773XF · Airbus A319112 · APU Core Engine
  > AIRCRAFT WAS GROUNDED: INBOUND FLIGHT ATTENDANTS REPORTED THAT ON THE DECENT IN THE KEY WEST BELOW 10,000 FT THEY SMELT A VERY STRONG OILY, CAR GARAGE, MUSTY SOCK ODOR SMELL ONE OF THEM FELT FLUSH THE OTHER ONE BEGAN TO GET SYMPTOMS OF A HEADACHE. DURING PRE-
- [SDR AALA202511259933](https://openairdocs.org/sdr/AALA202511259933.md): Girt Bar · out of adjust · Nov 22, 2025 · N773XF · Airbus A319112 · Emergency Equipment
  > AIRCRAFT WAS NOT GROUNDED: DURING SCHED TIME CHANGE OF L4 SLIDE, WITH NEW SLIDE GIRT BAR DOES NOT RE-ENGAGE WITH TELESCOPING PIN ON FWD SIDE OF GIRT BAR FITTING WHEN DOOR IS ARMED AND DOOR HANDLE LIFTED AND ATTEMPTED TO CLOSE. MAINTENANCE REMOVED GIRT BAR PIN
- [SDR AALA202510204988](https://openairdocs.org/sdr/AALA202510204988.md): Battery · no test · Oct 16, 2025 · N773XF · Airbus A319112 · Emergency Equipment
  > AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTS UNABLE TO TEST EMERGENCY FLASHLIGHT LOCATED AT #4 JUMPSEAT. MAINTENANCE REPLACED FLASHLIGHT BATTERY.
- [SDR AALA202505010560](https://openairdocs.org/sdr/AALA202505010560.md): Power Supply · no test · Apr 29, 2025 · N773XF · Airbus A319112 · Emergency Lighting
  > AIRCRAFT WAS NOT GROUNDED: EPSU BATTERY FWD L MSG SHOW ON PTP PANEL DURING PS CHECK STEP 27.E. TEST DO NOT PASS. MAINTENANCE
- [SDR AALA202502242021](https://openairdocs.org/sdr/AALA202502242021.md): Slide · deformed · Feb 22, 2025 · N773XF · Airbus A319112 · Escape Slide
  > AIRCRAFT IN BASE MAINTENANCE: DEFORMED ESCAPE SLIDE LOCT AT PASSENGER CREW DOOR 832. REPLACED ESCAPE SLIDE ESCAPE SLIDE LOCT AT PASSENGER CREW DOOR 832 I.A.W. AMM 25-62-44-000-002-A AND AMM 25-62-44-400-006-A.
- [SDR AALA202502176251](https://openairdocs.org/sdr/AALA202502176251.md): Skin Panel · dented · Feb 12, 2025 · N773XF · Airbus A319112 · Fuselage Main, Plate/Skin
  > AIRCRAFT IN BASE MAINTENANCE: DENT LOC. ON EXTERNAL SKIN AT LEVEL STRG 19RH BTW FR85 AND FR86 ON TAILCONE. DENT MEASURE ARE L=6.013 INCH W=3.453 INCH D=0.007 INCH. MAINTENANCE PERFORMED PERMANENT REPAIR (DOUBLER) CATEGORY (A) ON EXTERNAL SKIN AT LEVEL STRG 19R
- [SDR AALA202502210977](https://openairdocs.org/sdr/AALA202502210977.md): Stringer · bent · Feb 8, 2025 · N773XF · Airbus A319112 · Fuselage Main, Longeron/Stringer
  > AIRCRAFT IN BASE MAINTENANCE: BENT ON STR19 LH LOC INTERNAL SKIN FR85 FR86 AFT FUSELAGE,MEASURE OF BENT ARE L=3.894 INCH W=0.795 INCH. MAINTENANCE REPLACED RIGHT PYLON SPIGOT FITTING IAW SRM 54-51-12-300-001.
- [SDR AALA202502170486](https://openairdocs.org/sdr/AALA202502170486.md): Stringer · cracked · Feb 8, 2025 · N773XF · Airbus A319112 · Fuselage Main, Longeron/Stringer
  > AIRCRAFT IN BASE MAINTENANCE: CRACK ON STR 21 LOC INTERNAL SKIN BTW FR 85 TO FR 86 AFT FUSELAGE L= 0.780 IN. MAINTENANCE REPLACED STR 21 ON INTERNAL SKIN BTW FR 85 TO FR 86 AFT FUSELAGE IAW A319 SRM 51-42-11-801 AND DWG D53585410.
- [SDR AALA202502176900](https://openairdocs.org/sdr/AALA202502176900.md): Bolt · corroded · Feb 1, 2025 · N773XF · Airbus A319112 · Leading Edge Devices
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION SLAT TRACK 9 FWD BOLT ON RH WING L= 0.490 IN W= 0.183 IN D= 0.005 IN. MAINTENANCE REPLACED OLT ATTACHMENT SLAT TRACK 9 FWD POSITION, STA 10204/RIB 19 ON RH WING IAW AMM 27-84-66-400-002-A STEP 4.B.(4).
- [SDR AALA202502114661](https://openairdocs.org/sdr/AALA202502114661.md): Bolt · corroded · Jan 29, 2025 · N773XF · Airbus A319112 · Leading Edge Devices
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION SLAT TRACK 5 LOWER BOLT ON RH WING, CORROSION MEASURES L:0.490IN, W:0.183IN, D:0.005IN. MAINTENANCE
- [SDR AALA202502032683](https://openairdocs.org/sdr/AALA202502032683.md): Attach Bolt · corroded · Jan 29, 2025 · N773XF · Airbus A319112 · Wing Main, Frame Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION SLAT TRACK 5 FWD BOLT ON RH WING, CORROSION MEASURES L:0.493IN, W:0.189IN, D:0.007IN. MAINTENANCE REPLACED SLAT TRACK 5 FWD BOLT ON RH WING IAW AMM 27-84-64-400-002-A,
- [SDR AALA202501306130](https://openairdocs.org/sdr/AALA202501306130.md): Attach Bolt · corroded · Jan 22, 2025 · N773XF · Airbus A319112 · Leading Edge Devices
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION BOLT ATTACHMENT SLAT TRACK 1 MID FWD POSITION RH WING DIMENSION ARE L= 0.495 IN W=0.197 IN D=0.008 IN.MAINTENANCE REPLACED BOLT ATTACHMENT SLAT TRACK 1 MID FWD POSITION RH WING IAW AMM 27-84-63-400-002-A AND JOB CARD 26C
- [SDR AALA202501214102](https://openairdocs.org/sdr/AALA202501214102.md): Hinge Fitting · excess play · Jan 20, 2025 · N773XF · Airbus A319112 · Elevator 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 AALA202502101157](https://openairdocs.org/sdr/AALA202502101157.md): Structure · bent · Jan 18, 2025 · N773XF · Airbus A319112 · Trailing Edge Flaps
  > AIRCRAFT IN BASE MAINTENANCE: BENT OB FLAP TRAILING EDGE AREA ON LH WING L=8.289 INCH W=2.96 INCH. MAINTENANCE PERFORMED PERMANENT REPAIR ON LOWER SURFACE BTW INNER RIB14 TO RIB16 O/B FLAP T/E AREA ON LH WING IAW A319 SRM 57-53-00-300-119.
- [SDR AALA202501180682](https://openairdocs.org/sdr/AALA202501180682.md): Hinge Arm · excess play · Jan 17, 2025 · N773XF · Airbus A319112 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 3 RH ON HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE-ARM END-FITTINGS #3 OF RH ELEVATOR IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
- [SDR AALA202501186329](https://openairdocs.org/sdr/AALA202501186329.md): Hinge Arm · excess play · Jan 17, 2025 · N773XF · Airbus A319112 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 5 RH ON HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE-ARM END-FITTING #5 OF RH ELEVATOR IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
- [SDR AALA202501180276](https://openairdocs.org/sdr/AALA202501180276.md): Hinge Arm · excess play · Jan 17, 2025 · N773XF · Airbus A319112 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 6 RH ON HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE-ARM END-FITTING #6 OF RH ELEVATOR IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
- [SDR AALA202501171117](https://openairdocs.org/sdr/AALA202501171117.md): Hinge Arm · excess play · Jan 16, 2025 · N773XF · Airbus A319112 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM END FITTING 2 RH ON HORIZONTALSTABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE-ARM END-FITTINGS #2 OF RH ELEVATOR IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
- [SDR AALA202501176134](https://openairdocs.org/sdr/AALA202501176134.md): Hinge Arm · excess play · Jan 16, 2025 · N773XF · Airbus A319112 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM END FITTING 1 RH ON HORIZONTALSTABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE-ARM END-FITTINGS #1 OF RH ELEVATOR IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
- [SDR AALA202501112828](https://openairdocs.org/sdr/AALA202501112828.md): Hinge Fitting · excess play · Jan 7, 2025 · N773XF · Airbus A319112 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM END FITTING 5 LH ON HORIZONTALSTABI LIZER. MAINTENANCE REPLACED ELEVATOR HINGE-ARM END-FITTINGS #5 ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A,
- [SDR AALA202502256790](https://openairdocs.org/sdr/AALA202502256790.md): Window Frame · cracked · Jan 2, 2025 · N773XF · Airbus A319112 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON OPEN FASTENER HOLE UPPER JUNTION WINDSHIELD LH SIDE POST,CRACK MEASURE IS L=0.450 INCH. MAINTENANCE ACCOMPLISHED PERMANET REPAIR LOC. LH LATERAL WINDOW FRAME ON WINDSHIELD SIDE POST AT FR4 LOWER ATTACHMENT FOR
- [SDR AALA202502259770](https://openairdocs.org/sdr/AALA202502259770.md): Window Frame · cracked · Jan 2, 2025 · N773XF · Airbus A319112 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: REPLACE RH SIDE WINDSHIELD BY COSTUMER REQUEST. MEASURE CRACK IS L=0.600. MAINTENANCE ACCOMPLISHED PERMANET REPAIR LATERAL WINDOW FRAME ON WINDSHIELD SIDE POST AT FR4 LOWER ATTACHMENT FOR HORIZONTAL STIFFENERS RH SIDE IAW EA #36
- [SDR AALA202502255964](https://openairdocs.org/sdr/AALA202502255964.md): Fitting · corroded · Dec 27, 2024 · N773XF · Airbus A319112 · Nacelle/Pylon, Main Frame
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION SPIGOT FITTING RECEPTACLE ON LH PYLON MEASURES OF CORROSION ARE L= 12.200INCH, W=1.300INCH, D=0.003INCH. MAINTENANCE REPLACED SPIGOT FITTING ON LH PYLON IAW AMM 54-51-41-000-001-A, A319 SRM 54-51-12-300-001 AND AMM 54-5
- [SDR AALA202502258786](https://openairdocs.org/sdr/AALA202502258786.md): Fitting · corroded · Dec 23, 2024 · N773XF · Airbus A319112 · Nacelle/Pylon, Main Frame
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION FITTING BORE OF PYLON SPIGOT RECEPTACLE IN RH PYLON MEASURES OF CORROSION ARE L=12.00INCH, W=1.27INCH, D=0.003INCH. MAINTENANCE REPLACED SPIGOT FITTING ON RH PYLON IAW AMM 54-51-41-000-001-A, A319 SRM 54-51-12-300-001 AN
- [SDR AALA202501283470](https://openairdocs.org/sdr/AALA202501283470.md): Bracket · corroded · Dec 23, 2024 · N773XF · Airbus A319112 · Main Landing Gear
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RH MLG RETRACTION ACTUATOR ATTACHMENT BRACKET UPPER FACE. MEASURES ARE L= 1.000 IN W= 0.500 IN D= 0.0098 IN. MAINTENANCE REWORKED BORE FASTENER HOLE.
- [SDR AALA202502257797](https://openairdocs.org/sdr/AALA202502257797.md): Fitting · cracked · Dec 21, 2024 · N773XF · Airbus A319112 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: REPLACE CONTINUITY FITTING RH SIDE CENTER POST WINDSHIELD COCKPIT IAW EA 360366. MAINTENANCE REPLACE CONTINUITY FITTING RH SIDE CENTER POST WINDSHIELD COCKPIT IAW EA 360366.
- [SDR AALA202502251473](https://openairdocs.org/sdr/AALA202502251473.md): Fitting · cracked · Dec 21, 2024 · N773XF · Airbus A319112 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: REPLACE CONTINUITY FITTING LH SIDE CENTER POST WINDSHIELD COCKPIT IAW EA 360366. MAINTENANCE REPLACED YO CONTINUITY FITTING LH LOC. BTW FR1 TO FR2 AT CENTER WINDSHIELD IAW EA360366.
- [SDR AALA202501111027](https://openairdocs.org/sdr/AALA202501111027.md): Hinge Arm · excess play · Dec 19, 2024 · N773XF · Airbus A319112 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM END FITTING 3 LH ON HORIZONTALSTABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE-ARM END-FITTINGS # 3 ON LH HORIZONTAL STABI LIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.
- [SDR AALA202412217926](https://openairdocs.org/sdr/AALA202412217926.md): Floor Panel · delaminated · Dec 17, 2024 · N773XF · Airbus A319112 · Fuselage Floor Panel
  > AIRCRAFT IN BASE MAINTENANCE: DELAMINATED FLOOR PANEL 251NF IN PASSENGER CABIN. REPLACED FLOOR PANEL PER SRM 53-02-00-300-011.
- [SDR AALA202412188511](https://openairdocs.org/sdr/AALA202412188511.md): Support Bracket · cracked · Dec 17, 2024 · N773XF · Airbus A319112 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK SUPPORT BRACKET LOCATED ON PRESSURE BULKHEAD AFT FACE AT FR 46 LEFT HAND SIDE IN AFT CARGO COMPARTMENT. SUPPORT BRACKET PER SRM 51-42-11-801 AND SRM 51-72-11-801.
- [SDR AALA202502039705](https://openairdocs.org/sdr/AALA202502039705.md): Stringer · corroded · Dec 15, 2024 · N773XF · Airbus A319112 · Fuselage Main, Longeron/Stringer
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION STRINGER 44 BTW FR 63 TO FR 64 IN BULK CARGO COMPARTMENT, CORROSION MEASURES L: 6.269 IN W: 1.490 IN D: 0.004 IN. MAINTENANCE REPLACED STRINGER 44 BTW FR 59 TO FR 64 IN BULK CARGO COMPARTMENT IAW A319 SRM 51-42-11-801, S
- [SDR AALA202502215120](https://openairdocs.org/sdr/AALA202502215120.md): Skin Panel · none · Dec 13, 2024 · N773XF · Airbus A319112 · Standard Practices/Structures
  > AIRCRAFT IN BASE MAINTENANCE: NO REPAIR DOCUMENTATION ON MAJOR REPAIR LIST FOR REPAIR EXTERNAL SKIN LOWER FUSELAGE BETWEEN FR23LH TO FR24LH AND STR24LH TO STR25LH AND SIZE OF REPAIR DOUBLER IS L=9.500IN, W=8.000IN. MAINTENANCE FOUND EXISTING REPAIR IS PCW LOG
- [SDR AALA202501116101](https://openairdocs.org/sdr/AALA202501116101.md): Hinge Arm · excess play · Dec 13, 2024 · N773XF · Airbus A319112 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 1 LH ON HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE-ARM END-FITTINGS # 1 ON LH HORIZONTAL STABI LIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A,REFER TO INDIVIDUAL SINGN
- [SDR AALA202502254316](https://openairdocs.org/sdr/AALA202502254316.md): Skin · cracked · Dec 12, 2024 · N773XF · Airbus A319112 · Fuselage Main, Plate/Skin
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND INTERNAL SURFACE AROUND RIVET ON FR35 AT LEVEL STR30 LH SIDE, CRACK DIRECTION 9 OCLOCK.CRACK MEASURE IS L=0.236 INCH. MAINTENANCE PERFORMED TIME LIMITED REPAIR (INSTALLED BUSHING)ON HOLE W1 LOCATED INTERNAL
- [SDR AALA202412206307](https://openairdocs.org/sdr/AALA202412206307.md): Shear Plate · cracked · Dec 11, 2024 · N773XF · 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 AALA202412200669](https://openairdocs.org/sdr/AALA202412200669.md): Shear Plate · cracked · Dec 11, 2024 · N773XF · Airbus A319112 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACKED AFT CABIN FLOOR SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23L. REPLACED SHEAR PLATE PER SRM 51-42-11.
- [SDR AALA202502251298](https://openairdocs.org/sdr/AALA202502251298.md): Skin · cracked · Dec 7, 2024 · N773XF · Airbus A319112 · Fuselage Main, Plate/Skin
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON AFT LOWER FASTENER HOLE OF FR35 LH AND STR30 CRACK DIRECTION 5 AND 11 OCLOCK. CRACK MEASURE IS L=0.160 INCH. MAINTENANCE PERFORMED TIME LIMITED REPAIR (INSTALLED FILLER) ON HOLE H2 LOC.AT FR35 ON AFT LOW
- [SDR AALA202502215812](https://openairdocs.org/sdr/AALA202502215812.md): Fitting · cracked · Dec 5, 2024 · N773XF · Airbus A319112 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND IN OPEN HOLE LOWER INBOARD POSITION ON FR 16 RH AT LEVEL DOOR STOP 7. CRACK MEASURE: 0.114 INCH. MAINTENANCE REPLACED INTERCOSTAL FITTING LOC. ON FR 16 RH DOOR STOP 7 IAW A319 SRM 51-42-11-801, SRM 51-72-11-
- [SDR AALA202502059681](https://openairdocs.org/sdr/AALA202502059681.md): Fitting · cracked · Dec 5, 2024 · N773XF · Airbus A319112 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACKED INTERCOSTAL FITTING AT FR 16 AND S10L. REPLACED INTERCOSTAL FITTING PER SRM 51-42-11.
- [SDR AALA202502031436](https://openairdocs.org/sdr/AALA202502031436.md): Fitting · cracked · Dec 5, 2024 · N773XF · Airbus A319112 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND IN OPEN HOLE LOWER INBOARD POSITION ON FR16 RH AT LEVEL DOOR STOP FITTING 1, CRACK DIRECTION 3 OCLOCK, CRACK DEPTH: 0.132. MAINTENANCE REPLACED INTERCOSTAL FITTING ON FR16 RH AT LEVEL DOOR STOP 1, IAW A319 S
- [SDR AALA202502257833](https://openairdocs.org/sdr/AALA202502257833.md): Window Frame · cracked · Dec 3, 2024 · N773XF · Airbus A319112 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON INTERNAL AREA WINDSHIELD CENTER POST, LOWER ATTACHMENT AREA, LOWER AND UPPER RADIUS RH SIDE ACCOMPLISH EO 5319Y017 IN COCKPIT (2 EA) (CRACK L:0.751 INCH). MAINTENANCE PERFORMED TIME LIMITED REPAIR (REPLACEMENT

Next page: https://openairdocs.org/aircraft/N773XF/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 = 'N773XF' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N773XF/reports

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