# Service difficulty reports: N768US

A list on [N768US](https://openairdocs.org/aircraft/N768US.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 · 226 reports

- [SDR AALA202610053610](https://openairdocs.org/sdr/AALA202610053610.md): Deu · fault message · Sep 30, 2026 · N768US · Airbus A319112 · Emergency Exits
  > AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTS EMERGENCY EXIT DOOR RIGHT AND EMERGENCY EXIT DOOR LEFT INDICATE TO CHECK SLIDE PRESSURE AND SLIDE PRESSURE LOW ON CIDS PANEL - MAINTENANCE REPLACED DEU B 300RH4 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHE
- [SDR AALA202607018500](https://openairdocs.org/sdr/AALA202607018500.md): Megaphone · no test · Jun 30, 2026 · N768US · Airbus A319112 · Emergency Equipment
  > AIRCRAFT WAS NOT GROUNDED: FORWARD MEGAPHONE INOPERATIVE. REPLACED MEGAPHONE PER JOB CARD 26C00025003.
- [SDR AALA202605252810](https://openairdocs.org/sdr/AALA202605252810.md): Oil Cooler · leaking · May 20, 2026 · N768US · Airbus A319112 · APU Oil System
  > AIRCRAFT WAS GROUNDED: DIRTY SOCK ODOR IN COCKPIT ON DESCENT WITH POWERS AT IDLE. DISSIPATES WHEN THRUST COMES BACK IN. FA'S DID NOT SMELL ANY ODOR INTHE CABIN. MAIBNTENANCE REPLACED OIL COOLING FAN PER JC 26L000021002 AND AMM 49-52-51.
- [SDR AALA202602034464](https://openairdocs.org/sdr/AALA202602034464.md): Bulb · inoperative · Feb 1, 2026 · N768US · Airbus A319112 · Emergency Lighting
  > AIRCRAFT WAS NOT GROUNDED: EMERGENCY EXIT RIGHT SIDEWALL LIGHT INOPERATIVE AT 14 RIGHT. REPLACED BULB PER AMM 33-20-004.
- [SDR AALA202510317479](https://openairdocs.org/sdr/AALA202510317479.md): Warning Light · false activation · Oct 28, 2025 · N768US · Airbus A319112 · Extinguishing System
  > AIRCRAFT WAS NOT GROUNDED: FLIGHT CREW REPORTED THAT THE APU DISCHARGE SWITCH LIGHT WAS ON IN FLIGHT. NO RELATED ECAM MESSAGES WERE NOTED. MAINTENANCE PERFORMED OPERATIONAL TEST OF THE APU FIRE EXTINGUISHING LOOP/SQUIB PER AMM 26-22-00 AND NO ISSUES WERE NOTED
- [SDR AALA202510270990](https://openairdocs.org/sdr/AALA202510270990.md): Battery Pack · inoperative · Oct 23, 2025 · N768US · Airbus A319112 · Emergency Lighting
  > AIRCRAFT IN BASE MAINTENANCE: INOP BATTERY EMERGENCY POWER SUPPLY UNIT 10WL AT FWD GALLEY AREA. MAINTENANCE REPLACED BATTERIES OF THE EMERGENCY POWER SUPPLY UNIT (EPSU) 10WL IAW A320 FAM AMM 33-51-38-000-002-A AND A320 FAM AMM 33-51-38-400-002-A.
- [SDR AALA202510270081](https://openairdocs.org/sdr/AALA202510270081.md): Power Supply · inoperative · Oct 23, 2025 · N768US · Airbus A319112 · Emergency Lighting
  > AIRCRAFT IN BASE MAINTENANCE: INOP BATTERY EMERGENCY POWER SUPPORT UNIT 13WL IN AFT GALLEY AREA. MAINTENANCE REPLACED BATTERIES OF THE EMERGENCY POWER SUPPLY UNIT (EPSU) 13WL IAW A320 FAM AMM 33-51-38-000-002-A AND A320 FAM AMM 33-51-38-400-002-A.
- [SDR AALA202510244542](https://openairdocs.org/sdr/AALA202510244542.md): Power Supply · inoperative · Oct 23, 2025 · N768US · Airbus A319112 · Emergency Lighting
  > AIRCRAFT IN BASE MAINTENANCE: INOP BATTERY EMERGENCY POWER SUPPORT UNIT 12WL IN PAX CABIN. MAINTENANCE REPLACED BATTERIES OF THE EMERGENCY POWER SUPPLY UNIT (EPSU) 12WL IAW A320 FAM AMM 33-51-38-000-002-A AND A320 FAM AMM 33-51-38-400-002-A.
- [SDR AALA202510244234](https://openairdocs.org/sdr/AALA202510244234.md): Power Supply · inoperative · Oct 23, 2025 · N768US · Airbus A319112 · Emergency Lighting
  > AIRCRAFT IN BASE MAINTENANCE: INOP BATTERY EMERGENCY POWER SUPPLY UNIT 11WL IN PAX CABIN. MAINTENANCE REPLACED BATTERIES OF THE EMERGENCY POWER SUPPLY UNIT (EPSU) 11WL IAW A320 FAM AMM 33-51-38-000-002-A AND A320 FAM AMM 33-51-38-400-002-A.
- [SDR AALA202509295546](https://openairdocs.org/sdr/AALA202509295546.md): Frame · cracked · Aug 9, 2025 · N768US · Airbus A319112 · Fuselage Main, Frame
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FRAME 68 AROUND ANCHOR NUT AT LEVEL OF STRG 23 LH AT AFT GALLEY AREA MEASURES CORROSION ARE L=0.104 INCHES, W=0.312 INCHES, D=0.001 INCHES. MAINTENANCE PERFORMED TIME LIMITED REPAIR ON FR 68 AROUND ANCHOR NUT AT LEVEL
- [SDR AALA202508268185](https://openairdocs.org/sdr/AALA202508268185.md): Fitting · corroded · Aug 9, 2025 · N768US · Airbus A319112 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON CORNER FITTING LOCATED AT FR68 AT LEVEL STRG 23LH SIDE AFT CABIN MEASURE OF CORROSION ARE L: 0.905 INCH, W: 0.735 INCH, D: 0.050 INCH. MAINTENANCE REPLACED CORNER FITTING LOCATED AT FR68 AT LEVEL STRG 23LH SIDE AFT CA
- [SDR AALA202508264045](https://openairdocs.org/sdr/AALA202508264045.md): Splice · corroded · Aug 9, 2025 · N768US · Airbus A319112 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON SPLICE UPPER OUTBOARD POSITION LOCATED AT FR66 AT LEVEL STRG 23LH SIDE AFT GALLEY AREA MEASURE OF DAMAGE ARE L: 0.744 INCHES; W: 0.596 INCHES, D: 0.050 INCHES. MAINTENANCE REPLACED SPLICE COUPLING AT FR66 AT LEVEL ST
- [SDR AALA202508126563](https://openairdocs.org/sdr/AALA202508126563.md): Sleeve · damaged · Aug 9, 2025 · N768US · Airbus A319112 · Nacelle/Pylon, Attach Fittings
  > AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND PYLON LEFT HAND SIDE FORWARD UPPER ATTACH FITTING SLEEVE (PIN) HAS DAMAGED THREADS. REPLACED SLEEVE (PIN) PER TASK CARD 26C42554028.
- [SDR AALA202509022440](https://openairdocs.org/sdr/AALA202509022440.md): Spigot · corroded · Aug 7, 2025 · N768US · Airbus A319112 · Nacelle/Pylon, Main Frame
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION SPIGOT FITTING RECEPTACLE ON LH PYLON, MEASURES ARE L= 6.310 IN; W= 0.780 IN; D= 0.003 IN. MAINTENANCE REPLACED SPIGOT FITTING RECEPTACLE ON LH PYLON IAW A319 SRM 54-51-12-300-001.
- [SDR AALA202508082110](https://openairdocs.org/sdr/AALA202508082110.md): Hinge Fitting · excess play · Aug 7, 2025 · N768US · Airbus A319112 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM END FITTING N2 ON RH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM END FITTING #2 ON RH ELEVATOR IAW AMM 55-16-42-400-001-A.
- [SDR AALA202508083551](https://openairdocs.org/sdr/AALA202508083551.md): Hinge Fitting · excess play · Aug 7, 2025 · N768US · Airbus A319112 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM END FITTING N5 ON RH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM END FITTING #5 ON RH ELEVATOR IAW AMM 55-16-42-400-001-A.
- [SDR AALA202508084830](https://openairdocs.org/sdr/AALA202508084830.md): Hinge Fitting · excess play · Aug 7, 2025 · N768US · Airbus A319112 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM END FITTING N3 ON RH HORIZONTAL STABILIZER. MAINTENACE REPLACED HINGE ARM END FITTING #3 ON RH ELEVATOR IAW AMM 55-16-42-400-001-A.
- [SDR AALA202508083734](https://openairdocs.org/sdr/AALA202508083734.md): Hinge Fitting · excess play · Aug 7, 2025 · N768US · Airbus A319112 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM END FITTING N4 ON RH HORIZONTAL STABILIZER. REPLACED HINGE ARM END FITTING #4 ON RH ELEVATOR IAW AMM 55-16-42-400-001-A.
- [SDR AALA202508079672](https://openairdocs.org/sdr/AALA202508079672.md): Hinge Fitting · excess play · Aug 5, 2025 · N768US · Airbus A319112 · Elevator Tab, Attach Fittings
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM END FITTING #4 ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM END FITTING # 4 ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-400-001-A.
- [SDR AALA202508077999](https://openairdocs.org/sdr/AALA202508077999.md): Hinge Fitting · excess play · Aug 5, 2025 · N768US · Airbus A319112 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM END FITTING #5 ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM END FITTING #5 ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-400-001-A.
- [SDR AALA202508076169](https://openairdocs.org/sdr/AALA202508076169.md): Hinge Fitting · excess play · Aug 5, 2025 · N768US · Airbus A319112 · Horizontal Stabilizer, Attach Fittings
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM END FITTING #2 ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM END FITTING # 2 ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-400-001-A.
- [SDR AALA202508077253](https://openairdocs.org/sdr/AALA202508077253.md): Hinge Fitting · excess play · Aug 5, 2025 · N768US · Airbus A319112 · Horizontal Stabilizer, Attach Fittings
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM END FITTING #1 ON LH HORIZONTAL STABILIZER. MSINTENANCE REPLACED ELEVATOR HINGE ARM END FITTING # 1 ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-400-001-A.
- [SDR AALA202508076933](https://openairdocs.org/sdr/AALA202508076933.md): Hinge Fitting · excess play · Aug 5, 2025 · N768US · Airbus A319112 · Elevator Tab, Attach Fittings
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM END FITTING #3 ON LH HORIZONTAL STABILIZER. MSINTENANCE REPLACED ELEVATOR HINGE ARM END FITTING # 3 ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-400-001-A.
- [SDR AALA202508072492](https://openairdocs.org/sdr/AALA202508072492.md): Hinge Fitting · excess play · Aug 5, 2025 · N768US · Airbus A319112 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM END FITTING #6 ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM END FITTING #6 ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-400-001-A.
- [SDR AALA202509023798](https://openairdocs.org/sdr/AALA202509023798.md): Spigot · corroded · Aug 3, 2025 · N768US · Airbus A319112 · Nacelle/Pylon, Main Frame
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION SPIGOT FITTING RECEPTACLE ON RH PYLON, MEASURES ARE L= 4.092 IN; W= 0.652 IN; D= 0.004 IN. MAINTENANCE REPLACED SPIGOT FITTING RECEPTACLE ON RH PYLON IAW A319 SRM 54-51-12-300-001.
- [SDR AALA202508111601](https://openairdocs.org/sdr/AALA202508111601.md): Hinge Fitting · excess play · Aug 1, 2025 · N768US · Airbus A319112 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM END FITTING # 1 ON RH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM END FITTING #1 ON RH ELEVATOR IAW AMM 55-16-42-400-001-A.
- [SDR AALA202508262719](https://openairdocs.org/sdr/AALA202508262719.md): Fitting · corroded · Jul 31, 2025 · N768US · Airbus A319112 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION CENTER FITTING AT STR23L AND BTW FR66 TO FR68 AFT GALLEY AREA MEASURE CORROSION ARE L=1.756 INCH W=0.601 INCH D=0.043 INCH. MAINTENANCE REPLACED CENTER FITTING ON LOWER SILL LOC. BTW FR66 TO FR68 STR 23LH AFT GALLEY AREA
- [SDR AALA202508094228](https://openairdocs.org/sdr/AALA202508094228.md): Web · corroded · Jul 30, 2025 · N768US · Airbus A319112 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON WEB LOC BTW FR69 TO FR70 AT STGR 23RH IN AFT GALLEY AREA MEASURE OF DAMAGE ARE L= 1.167 INCH, W= 0.506 INCH, D= 0.010 INCH. MAINTENANCE REPLACED WEB LOC BTW FR69 TO FR70 AT STGR 23RH IN AFT GALLEY AREA IAW A319 SRM 51
- [SDR AALA202510067340](https://openairdocs.org/sdr/AALA202510067340.md): Intercostal · cracked · Jul 27, 2025 · N768US · Airbus A319112 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON OPEN HOLE H1 FR16RH DOOR STOP 7. CRACK DIRECTION 6 AND 8 OCLOCK. CRACK DEPTH 0.100 INCH. MAINTENANCE REPLACED INTERCOSTAL FITTING #7 LOC. BTW FR15 RH AND FR16 RH IAW A319 SRM 51-72-11-911-001 AND DWG #53
- [SDR AALA202509050518](https://openairdocs.org/sdr/AALA202509050518.md): Stiffener · cracked · Jul 27, 2025 · N768US · Airbus A319112 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: AIRCRAFT IN BASE MAINTENANCE: CRACK FWD PRESSURE BULKHEAD ON STIFFENER Z-1329 FRAME 1 IN FWD AVIONIC COMPARTMENT, MEASURE CRACK IS L=0.587 INCH. MAINTENANCE REPLACED STIFFENER Z-1329 FWD PRESSURE BULKHEAD FRAME 1 IN FWD AVIONIC CO
- [SDR AALA202510218930](https://openairdocs.org/sdr/AALA202510218930.md): Floor Support · cracked · Jul 26, 2025 · N768US · Airbus A319112 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON FASTENER HOLE LOCATED AT PRESSURE DECK MENBRANE TO CENTER WING BOX AREA, ON FR36, Y1523 LH SIDE, LOWER FUSELAGE. (CRACK L: 0.098 INCH). MAINTENANCE PERFORMED TIME LIMITED REPAIR ON (HOLE L100) PRESSURE DE
- [SDR AALA202509025325](https://openairdocs.org/sdr/AALA202509025325.md): Rib · corroded · Jul 26, 2025 · N768US · Airbus A319112 · Elevator Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ELEVATOR ON END RIB ON LH HORIZONTAL STABILIZER MEASURE OF DAMAGE ARE: L=0.608 IN, W= 0.591 IN, D=0.04IN. MAINTENANCE REPLACED RIB 10 IN ELEVATOR ON LH HORIZONTAL STABILIZER IAW A319 SRM 55-21-12-300-002 AND SRM A319 51
- [SDR AALA202510214178](https://openairdocs.org/sdr/AALA202510214178.md): Dummy Rail · corroded · Jul 25, 2025 · N768US · Airbus A319112 · Fuselage, Seat/Cargo Attach Fittings
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION RAIL DUMMY Y503.2 LOCATED BTW FR12 AND FR16 FWD GALLEY AREA. MEASURES OF CORROSION ARE: L=1.073 IN, W=0.849 IN, D=0.070 IN. MAINTENANCE REPLACED RAIL DUMMY Y503.2 LOCATED BTW FR12 AND FR16 FWD GALLEY AREA. IAW A319 SRM 5
- [SDR AALA202510148181](https://openairdocs.org/sdr/AALA202510148181.md): Shear Plate · cracked · Jul 25, 2025 · N768US · Airbus A319112 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: BROKEN SHEAR PLATE AFT GALLEY FR69-FR70 RIGHT SIDE PASSENGER CABIN. MEASURE IS L= 1.069 INCH. MAINTENANCE REPLACED SHEAR PLATE LOC, BTW FR69 AND FR70 AT STGR 23R IN AFT GALLEY AREA IAW A319 SRM 51-42-11-801, A319 SRM 51-72-11-911
- [SDR AALA202510068859](https://openairdocs.org/sdr/AALA202510068859.md): Shear Plate · cracked · Jul 25, 2025 · N768US · Airbus A319112 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: BROKEN PLATE AFT GALLEY FR69-FR70 LEFT SIDE PASSENGER CABIN MEASURES OF CRACKED ARE IS: L=0.831 INCH. MAINTENANCE REPLACED SHEAR PLATE LOCATED BETWEEN FR 69 TO FR 70 AT LEVEL OF STR 23 LH SIDE AFT GALLEY AREA IAW A319 SRM 51-72-11
- [SDR AALA202509156290](https://openairdocs.org/sdr/AALA202509156290.md): Support · corroded · Jul 25, 2025 · N768US · Airbus A319112 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION LOWER SILL LOCATED FR 68 AND STR 23L AFT GALLEY AREA L=2.222 INCH W=1.865 INCH D=0.003 INCH. MAINTENANCE REPLACED LOWER SILL LH SIDE BTW FR66 TO FR68 AND STR 23L AFT GALLEY AREA IAW A319 SRM 51-42-11-801, A319 SRM 51-72-
- [SDR AALA202508267651](https://openairdocs.org/sdr/AALA202508267651.md): Floorbeam · corroded · Jul 25, 2025 · N768US · Airbus A319112 · Fuselage Main, Floor Beam
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION FLOOR BEAM Y1292 LOCATED FR16 FWD GALLEY AREA MEASURE CORROSION ARE L=2.595 INCH W=1.940 INCH D=0.058 INCH. MAINTENANCE REPLACED FLOOR BEAM Y1292 LOC FR 16 FWD GALLEY AREA IAW A319 SRM 51-72-11-911-001,DWG D53918122 AND
- [SDR AALA202508093505](https://openairdocs.org/sdr/AALA202508093505.md): Support · corroded · Jul 25, 2025 · N768US · Airbus A319112 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION LOWER SILL LOCATED BTW FR 66 TO FR 68 AND STR 23R AFT GALLEY AREA MEASURE CORROSION ARE L=0.375 INCH W=0.220 INCH D=0.050 INCH. MAINTENANCE PERFORMED PERMANENT REPAIR ON LOWER SILL LOC BTW FR66 TO FR68 AND STGR 23R AFT G
- [SDR AALA202509294348](https://openairdocs.org/sdr/AALA202509294348.md): Floorbeam · cracked · Jul 23, 2025 · N768US · Airbus A319112 · Fuselage Main, Floor Beam
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON RADIUS OF HORIZONTAL FLOOR BEAM 3 BACKSIDE OF THE SPAR VERTICAL STRINGER AT FR 36 CRACK L=0.410 INCH
- [SDR AALA202509295988](https://openairdocs.org/sdr/AALA202509295988.md): Floorbeam · cracked · Jul 23, 2025 · N768US · Airbus A319112 · Fuselage Main, Floor Beam
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON RADIUS OF HORIZONTAL FLOOR BEAM 2 BACKSIDE O F THE SPAR VERTICAL STRINGER AT FR 36. CRACK L= 0.235 INCH. MAINTENANCE PERFORMED PERMANENT REPAIR ON HORIZONTAL BEAM Y765 (NUMBER 2) LOC CENTER BOX FR36 FRONT
- [SDR AALA202509299460](https://openairdocs.org/sdr/AALA202509299460.md): Floorbeam · cracked · Jul 23, 2025 · N768US · Airbus A319112 · Fuselage Main, Floor Beam
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON RADIUS OF HORIZONTAL FLOORBEAM 5 BACKSIDE OF THE SPAR VERTICAL STRINGER AT FR 36 CRACK L=0.280 INCH. MAINTENANCE PERFORMED PERMANENT REPAIR ON HORIZONTAL BEAM -Y765 (BEAM 5) LOC CENTER BOX FR36 FRONT SPAR
- [SDR AALA202509295457](https://openairdocs.org/sdr/AALA202509295457.md): Floorbeam · cracked · Jul 23, 2025 · N768US · Airbus A319112 · Fuselage Main, Floor Beam
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON RADIUS OF HORIZONTAL FLOOR BEAM 4 BACKSIDE OF THE SPAR VERTICAL STRINGER AT FR 36. CRACK L= 0.470 INCH. MAINTENANCE PERFORMED PERMANENT REPAIR ON HORIZONTAL BEAM -Y254 (NUMBER 4) LOC CENTER WING BOX FR36
- [SDR AALA202509058698](https://openairdocs.org/sdr/AALA202509058698.md): Fork · worn · Jul 23, 2025 · N768US · Airbus A319112 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: FOUND RACK 80VU LATERAL FITTING IN CONTACT WITH STRUCTUR RH SIDE IN AFT AVIONIC COMPARTMENT. DAMAGED AREA: 0.080 IN. MAINTENANCE PERFORMED INTERIM REPAIR AT LOWER LATERAL SUPPORT RH OF 80VU RACK LOC BTW FR23 TO FR24 AT LEVEL STR 3
- [SDR AALA202509050259](https://openairdocs.org/sdr/AALA202509050259.md): Fork · worn · Jul 23, 2025 · N768US · Airbus A319112 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: FOUND RACK 80VU FITTING IN CONTACT WITH STRUCTURE LH SIDE IN AFT AVIONIC COMPARTMENT. DAMAGED AREA L: 0.063 IN. MAINTENANCE PERFORMED INTERIM REPAIR AT LOWER LATERAL SUPPORT LH OF 80VU RACK LOC BTW FR23 TO FR24 AT LEVEL STR 32LH I
- [SDR AALA202510158861](https://openairdocs.org/sdr/AALA202510158861.md): Skin Panel · worn · Jul 21, 2025 · N768US · Airbus A319112 · Wing, Plate/Skin
  > AIRCRAFT IN BASE MAINTENANCE: WEAR ON SLAT 1 TRAILING EDGE AT LEVEL SLAT 2 TRACK 2 LOWER SURFACE RIGHT HAND WING MEASURE L= 3.628 IN, W= 0.347. MAINTENANCE PERFORMED PERMANENT REPAIR ON SLAT 1 TRAILING EDGE AT LEVEL SLAT TRACK 2 LOWER SURFACE RH WING IAW EA 36
- [SDR AALA202510213980](https://openairdocs.org/sdr/AALA202510213980.md): Door Frame · cracked · Jul 9, 2025 · N768US · Airbus A319112 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON FRAME 16 RH FROM THE THIRD FASTENER HOLE 6 FROM UPPER TO LOWER) OF AFT ROW AND 7 DOORSTOP FITTING LEVEL AT FWD GALLEY AREA L= 0.098IN. MAINTENANCE PERFORMED TIME LIMITED REPAIR (PARTIAL FRAME REPLACEMENT) ON FR
- [SDR AALA202505152078](https://openairdocs.org/sdr/AALA202505152078.md): Oxygen Mask · inoperative · May 11, 2025 · N768US · Airbus A319112 · Passenger Oxygen System
  > AIRCRAFT WAS GROUNDED: ROW 15 ABC O2 MASKS DID NOT DROP DURING EMERGENCY DECENT. MAINTENANCE FOUND MASKS NOT STOWED CORRECTLY, INSTALLED MASKS IAW AMM 35-21-43,
- [SDR AALA202505132078](https://openairdocs.org/sdr/AALA202505132078.md): Oxygen Mask · inoperative · May 11, 2025 · N768US · Airbus A319112 · Passenger Oxygen System
  > AIRCRAFT WAS GROUNDED: ROW 15 ABC O2 MASKS DID NOT DROP DURING EMERGENCY DECENT. MAINTENANCE FOUND MASKS NOT STOWED CORRECTLY, INSTALLED MASKS IAW AMM 35-21-43,
- [SDR AALA202503036839](https://openairdocs.org/sdr/AALA202503036839.md): Hinge Fitting · gouged · Mar 2, 2025 · N768US · Airbus A319112 · Fuselage, Door Hinge
  > AIRCRAFT IN BASE MAINTENANCE: RH MLG DOOR KEELBEAM FWD HINGE FITTING GUAGED FROM MLG DOOR HING PLATE. MAINTENANCE REPLACED FWD HINGE FITTING IAW EA 362560.
- [SDR AALA202502176687](https://openairdocs.org/sdr/AALA202502176687.md): Girt Bar · out of position · Feb 15, 2025 · N768US · Airbus A319112 · Emergency Equipment
  > AIRCRAFT WAS NOT GROUNDED: 1L DOOR DIFFICULT TO MOVE ARMING LATCH. FOUND GIRT BAR SLIGHTLY SLID OUT OF PLACEMENT ON SLIDE. ADJUSTED GIRT BAR IAW AMM 25-62-44. OPS CHECK GOOD FOR ARMED/DISARMED HANDLE.

Next page: https://openairdocs.org/aircraft/N768US/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 = 'N768US' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N768US/reports

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