# Service difficulty reports: N317US, cancelled Aug 14, 2025

A list on [N317US, cancelled Aug 14, 2025](https://openairdocs.org/deregistered/N317US-2025-08-14.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 3 · 143 reports

- [SDR DALA2024121711763](https://openairdocs.org/sdr/DALA2024121711763.md): Actuator · leaking · Dec 15, 2024 · N317US · Airbus A320211 · Rudder Actuator
  > UPON ARRIVAL AT GATE FLIGHT ATTENDANTS IN AFT REPORTED SMELLING WET SOCK ODOR AND FLIGHT ATTENDANTS IN THE FORWARD SMELLED SAME ODOR UPON OPENING DOOR. FLT CREW DID NOT COMPLETELY FILL OUT SMOKE AND FUME QUESTIONNAIRE. RAN PACKS OFF ENG1 BLEED, ENG 2 BLEED, A
- [SDR DALA2024121511715](https://openairdocs.org/sdr/DALA2024121511715.md): Actuator · leaking · Dec 13, 2024 · N317US · Airbus A320211 · Hydraulic System, Main
  > ODOR IN CABIN/ HYD LEAK FROM RUDDER. ISOLATED ODOR TO HYDRAULIC INGESTION IN APU INTAKE FROM LEAKING COILED TUBE FOR RUDDER ACTUATOR. APU TO BE PLACED ON MEL FOR DEC ONTAMINATION. ECS LEVEL B DECONTAMINATION COMPLETE. (LP: 0708319)
- [SDR DALA2024120211306](https://openairdocs.org/sdr/DALA2024120211306.md): Slide · abnormal · Nov 26, 2024 · N317US · Airbus A320211 · Escape Slide
  > SHIP 3217 DISC: CATERING PERSONNEL REMOVED DISARM PIN AND CAUSED SLIDE TO DEPLOY AT GATE. DOOR 2L. AS PER THE EMPLOYEE, PIN WAS PULLED, BUT NEVER MOVED LEVER TO ARM. HE STATED LEVER REMAINED IN DISARM POSITION. HE ONLY OPERATED THE DOOR HANDLE. C/A: 2L DEPLOYE
- [SDR DALA2024062406337](https://openairdocs.org/sdr/DALA2024062406337.md): Bearing · worn · Jun 22, 2024 · N317US · Airbus A320211 · Rudder Structure
  > SHIP 3217 DISC: #7 RUDDER HINGE BEARING WORN, HAS EXCESSIVE PLAY PER AMDS 2720- 7001. C/A: REPLACE #7 RUDDER HINGE FITTING REF A320 SRM 55-36-42-300-001. (LP: 0406974)
- [SDR DALA2024062406336](https://openairdocs.org/sdr/DALA2024062406336.md): Bearing · worn · Jun 22, 2024 · N317US · Airbus A320211 · Rudder Structure
  > SHIP 3217 DISC: #5 RUDDER HINGE BEARING WORN, HAS EXCESSIVE PLAY PER AMDS 2720- 700. C/A: REPLACE #5 RUDDER HINGE FITTING REF A320 SRM 55-36-42-300-001. (LP: 0406970)
- [SDR DALA2024041504409](https://openairdocs.org/sdr/DALA2024041504409.md): Door Frame · cracked · Apr 13, 2024 · N317US · Airbus A320211 · Fuselage Main, Structure
  > SHIP 3217 DISC: FR 66 LH- CRACK INDICATION FOUND ON THE FRAME AT DOOR STOP FITTING #3, HOLE LOCATION #3 DURING HFEC ROTOTEST INSPECTION ON AA 5311-01216. HOLE MEASURES.250". AD RELATED. ACTION REQUIRED PRIOR TO FLIGHT. C/A: SUMMARY SEE NR FOR ADDITIONAL INFOR
- [SDR DALA2024041504403](https://openairdocs.org/sdr/DALA2024041504403.md): Skin · gouged · Apr 13, 2024 · N317US · Airbus A320211 · Fuselage Main, Plate/Skin
  > PCS ANTENNA- EXTERNAL SURFACE OF THE UPPER FUSELAGE HAS GOUGES/ TOOLING DAMAGE IN SEVERAL AREAS WHERE THE ANTENNA IS MOUNTED. REPAIRED FUSELAGE SKIN PER A320 SRM 53-22-11-300-087. REQUIRES SUBSEQUENT INSPECTION.
- [SDR DALA2024010210750](https://openairdocs.org/sdr/DALA2024010210750.md): Unknown · unknown · Dec 27, 2023 · N317US · Airbus A320211 · Oxygen System
  > TWO AFT O2 BOTTLES INSTALLED IMPROPERLY. CAN NOT REMOVE BOTTLES. ADJUSTED AFT TWO O2 BOTTLE BRACKETS AS REQUIRED. O2 BOTTLES CAN NOW BE REMOVED/INSTALLED PROPERLY. (LP: 4595656)
- [SDR DALA2023122610573](https://openairdocs.org/sdr/DALA2023122610573.md): Unknown · unknown · Dec 24, 2023 · N317US · Airbus A320211 · Fuselage Main, Plate/Skin
  > SHIP 3217 DISC: ON WALK AROUND FOUND CREASE & DENTS FR 3, 12" ABOVE LOWER LAP OF SKIN D5311340220600. C/A: TRANSFERRED TO N/R #1 (WIP174073). NON-REOUTINE LOG # 0124665.. (LP 4595639)
- [SDR DALA2023122610572](https://openairdocs.org/sdr/DALA2023122610572.md): Unknown · unknown · Dec 24, 2023 · N317US · Airbus A320211 · Fuselage Main, Plate/Skin
  > SHIP 3217 DISC: TRANSFERRED FROM LP 4595639. ON WALK AROUND FOUND CREASE & DENTS FR3 12" ABOVE LOWER LAP OF SKIN D5311340220600. C/A: REMOVED EXISTING FASTENERS IN THE REPAIR AREA. CUT OUT DAMAGED SKIN AND DEBARR EDGES OF CUTOUT (WIP 174075) PERFORMED HFEC OF
- [SDR DALA2023100208045](https://openairdocs.org/sdr/DALA2023100208045.md): Unknown · unknown · Oct 1, 2023 · N317US · Airbus A320211 · Fuselage Main, Frame
  > SHIP 3217 NEED TO COMPLY WITH KEEL BEEM REPAIR. CORRECTIVE ACTION: COMPLIED WITH ERA 612401-14 SECTION I. (2995568)
- [SDR DALA2023013000765](https://openairdocs.org/sdr/DALA2023013000765.md): Shroud · broken · Jan 25, 2023 · N317US · Airbus A320211 · Emergency Lighting
  > SHIP 3217 EMERGENCY LIGHT AT SEAT 13D BROKEN. CORRECTIVE ACTION: REPLACED LIGHT AND SEAT SHROUD IAW A320 CMM 25-23-51 OPS CK GOOD. (9941872)
- [SDR DALA2022102506931](https://openairdocs.org/sdr/DALA2022102506931.md): Arming Lever · out of adjust · Oct 24, 2022 · N317US · Airbus A320211 · Passenger/Crew Doors
  > SHIP 3217 1L DOOR ARMING LEVER NEEDS EXTRA FORCE TO INDICATE ARMED. CORRECTIVE ACTION: ADJUSTED DOOR PER A320 AMM 52-12. OK FOR SERVICE. (2466042)
- [SDR DALA2022071104829](https://openairdocs.org/sdr/DALA2022071104829.md): None · none · Jul 9, 2022 · N317US · Airbus A320211 · Air Conditioning System
  > SHIP 3217 - ATB - DUE TO STRONG ELECTRICAL BURNING SMELL IN THE COCKPIT. CORRECTIVE ACTION: FOUND CONNECTOR 17RN2 WITH INSULATION DAMAGED AND PINS OUT. REPLACED CONNECTOR. OPS CHECK OK. (2313530)
- [SDR DALA2022071104824](https://openairdocs.org/sdr/DALA2022071104824.md): None · none · Jul 8, 2022 · N317US · Airbus A320211 · Escape Slide
  > SHIP 3217 NEED TO PERFORM PASSENGER CREW DOOR SPECIAL PRECAUTIONS BEFORE AND AFTER WORK AND INSTALL AND REMOVE SAFETY PIN ON HEAD RESERVOIR SLIDERAFT ON DOOR 831,841,832 AND 842 IN PASSENGER CABIN. COMPLIED WITH SPECIAL SAFETY PRECAUTIONS PER A320 AMM 25-62-44
- [SDR DALA2022070804761](https://openairdocs.org/sdr/DALA2022070804761.md): None · none · Jul 7, 2022 · N317US · Airbus A320211 · Trailing Edge Flaps
  > SHIP 3217 CORROSION INTERCONNECTING STRUT OB FLAP ON LH WING. CORRECTIVE ACTION: CLEAN AND REINSTALLED INTERCONNECTING STRUT ON FLAP ON LH WING. OK FOR SERVICE. (2310711)
- [SDR DALA2022070504658](https://openairdocs.org/sdr/DALA2022070504658.md): None · none · Jul 3, 2022 · N317US · Airbus A320211 · Passenger/Crew Doors
  > SHIP 3217 PASS CREW DOOR 842 DAMPER DOES NOT PASS TEST. CORRECTIVE ACTION: REPLACED DAMPER PER A320 AMM 52-13-14. (2304635)
- [SDR DALA2022070504641](https://openairdocs.org/sdr/DALA2022070504641.md): None · none · Jul 3, 2022 · N317US · Airbus A320211 · Fuselage Main, Frame
  > SHIP 3217 NEED TO REPORT SDR FOR REPLACEMENT OF FRAME FOOT 43LH AS PER JOB CARD 53-11-01239-02A STEP 18. CORRECTIVE ACTION: REPLACED PER A320 AMM AND REPORTED SDR. (2304958)
- [SDR DALA2022070504650](https://openairdocs.org/sdr/DALA2022070504650.md): None · none · Jul 1, 2022 · N317US · Airbus A320211 · Passenger/Crew Doors
  > SHIP 3217 PASSENGER CREW DOOR 832 HARD TO OPEN AND CLOSE. CORRECTIVE ACTION: ADJUSTED DOOR PER DELTA WORKCARD AMDS 5210-7089-LA. OK FOR SERVICE. (2302025)
- [SDR DALA2022070604684](https://openairdocs.org/sdr/DALA2022070604684.md): None · none · Jun 30, 2022 · N317US · Airbus A320211 · Emergency Locator Beacon
  > SHIP 3217 EXPIRED DUE DATE OVERHEAD STOWAGE BIN EMERGENCY LOCATOR TRANSMITTER (ELT) IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED ELT PER A320 AMM 25-65-35. OK FOR SERVICE. (2300020)
- [SDR DALA2022031101616](https://openairdocs.org/sdr/DALA2022031101616.md): None · none · Mar 11, 2022 · N317US · Airbus A320211 · Airborne Auxiliary Power Unit (APU) System
  > SHIP 3217 BURNING ODOR WITH APU BLEED AIR REMOVED APU BLEED AND FUMES STOPPED. CORRECTIVE ACTION: T/S PER WORK CARD 0550-2002 FOUND APU LEAKING OIL, APU REPLACEMENT REQUIRED, CONTINUED WORK CARDS 4900-2001 AND 2100- 2005. SMELL REPORTED STILL WITH STAGE 2 CLEA
- [SDR DALA2022010600102](https://openairdocs.org/sdr/DALA2022010600102.md): None · none · Jan 6, 2022 · N317US · Airbus A320211 · Pressure Regulator/Outflow Valve
  > SHIP 3217 - ATB - DUE TO CABIN PRESSURE SAFETY VALVE AND OUTFLOW VALVE SHOWING AMBER AND OPEN ON ECAM. RESET ATTEMPT DID NOT RECOVER THE PRESSURIZATION SYSTEM. CORRECTIVE ACTION: REPLACED PRESSURIZATION PANEL MODE SWITCH, CPC 1 AND SDAC 1. PRESSURIZATION CHECK
- [SDR DALA2021122308010](https://openairdocs.org/sdr/DALA2021122308010.md): Unknown · odor · Dec 23, 2021 · N317US · Airbus A320211 · Air Distribution System
  > SHIP 3217- DIV/FUME - FIRST FLIGHT FROM PRIOR ODOR EVENT, DIVERT TO SLC DUE TO REPORT OF BURNING ODOR IN AFT AND MID CABIN. CORRECTIVE ACTION: OIL CONTAMINATION CONFIRMED IN APU COMPARTMENT FROM PRIOR EVENT. APU IS ON MEL AND WAS NOT USED. GVI WITH BLACK LIGHT
- [SDR DALA2021121607808](https://openairdocs.org/sdr/DALA2021121607808.md): None · none · Dec 14, 2021 · N317US · Airbus A320211 · Emergency Lighting
  > SHIP 3217 10DEF EMERGENCY LIGHT HOUSING DAMAGED. CORRECTIVE ACTION:REPLACED HOUSING IAW A320 CMM 25-23-51. OPS CKS GOOD. (8230250)
- [SDR DALA2021113007376](https://openairdocs.org/sdr/DALA2021113007376.md): None · none · Nov 26, 2021 · N317US · Airbus A320211 · Data Recorders (Flight/Maintenance)
  > SHIP 3217 FOQA DATA DETECTED A LANDING GEAR RETRACTION SPEED EXCEEDANCE. CORRECTIVE ACTION: ACCOMPLISHED A320 AMM TASK 05-51-12-200-001-A. NO TROUBLE FOUND. OK FOR SERVICE. (2031310)
- [SDR DALA2021110306772](https://openairdocs.org/sdr/DALA2021110306772.md): None · none · Nov 2, 2021 · N317US · Airbus A320211 · Passenger Oxygen System
  > SHIP 3217 DURING TEST THE FOLLOWING PSU'S DID NOT OPEN: 1CD, 14 DEF, 20 DEF, 22ABC, 27ABC, 27DEF, 32ABC, LF AFT LAV, R2 DOOR. CORRECTIVE ACTION: REPACKED MASKS PER A320 AMM 35-21-43. OPS TEST GOOD SECOND TIME. (7874965)
- [SDR DALA2021072904269](https://openairdocs.org/sdr/DALA2021072904269.md): Door Frame · cracked · Jul 28, 2021 · N317US · Airbus A320211 · Fuselage Main, Structure
  > SHIP 3217 RT DOOR FRAME 68 FITTING #5 HOLE #1 HAS CRACK INDICATION. CORRECTIVE ACTION: COMPLIED WITH ER/A 592954-14AD REV ORIGINAL. (1891183)
- [SDR DALA2021072904266](https://openairdocs.org/sdr/DALA2021072904266.md): Skin · corroded · Jul 28, 2021 · N317US · Airbus A320211 · Fuselage Main, Plate/Skin
  > SHIP 3217 SKIN CORRODED AND FASTENERS PULLING THROUGH AT FRAME 70 R/H BETWEEN STRG 31 AND 32 R/H, APPROX 13 INCHES AFT OF LAV VENT OUTLET. CORRECTIVE ACTION: COMPLIED WITH ER/A 592914-14 REV ORIGINAL. (1891186)
- [SDR DALA2021120307461](https://openairdocs.org/sdr/DALA2021120307461.md): None · none · Jul 27, 2021 · N317US · Airbus A320211 · Fuselage Main, Plate/Skin
  > SHIP 3217 ERA 592914-14 SECTION I ISSUED FOR REPAIR TO SKIN CORROSION AT FRAME 70 RHS. CORECTIVE ACTION: COMPLIED WITH ERA 592914-14. (1890680)
- [SDR DALA2021072704212](https://openairdocs.org/sdr/DALA2021072704212.md): Stop Fitting · damaged · Jul 26, 2021 · N317US · Airbus A320211 · Fuselage Main, Structure
  > SHIP 3217 FR 68 RH #5 DOORSTOP FITTING HAS 2 HOLES OVERSIZED. CORRECTIVE ACTION: COMPLIED WITH PRI 592973-14AD REV 0 AND ER/A 592973-14AD REV ORIG. (1889161)
- [SDR DALA2021070803790](https://openairdocs.org/sdr/DALA2021070803790.md): Fitting · cracked · Jul 7, 2021 · N317US · Airbus A320211 · Wing Main, Frame Structure
  > SHIP 3217 ER/A 592560-14AD WAS GENERATED FOR THE RH AFT SPAR TO PINTLE FITTING JOINT AT HOLE 51R. (CRACK) CORRECTIVE ACTION: COMPLIED WITH ER/A 592560-14AD. CONTINUE ON MONITOR.
- [SDR DALA2021070703766](https://openairdocs.org/sdr/DALA2021070703766.md): Fitting · not reported · Jul 5, 2021 · N317US · Airbus A320211 · Wing Main, Frame Structure
  > SHIP 3217 ER/A 592560-14AD IS GENERATED FOR THE RH AFT SPAR TO PINTLE FITT ING JOINT AT HOLE 51R. COMPLIED WITH ERA 592560-14AD. (1864976)
- [SDR DALA2021072204139](https://openairdocs.org/sdr/DALA2021072204139.md): Hinge Fitting · corroded · Sep 10, 2020 · N317US · Airbus A320211 · Elevator Structure
  > SHIP 3217 STABILIZERS - RH ELEVATOR - LUG BORE OF HINGE ARM FITTINGS CORROSION. CORRECTIVE ACTION: ACCOMPLISHED ER/A 533420-14 REV B SECTION IV INSPECTION. CONTINUE ON MON. (1612034)
- [SDR DALA2020031001778](https://openairdocs.org/sdr/DALA2020031001778.md): Light · inoperative · Mar 5, 2020 · N317US · Airbus A320211 · Emergency Lighting
  > DURING SVC FOUND EMERGENCY LIGHT MSG. (EXT. LOADS EMER R"), REPLACED 4 BULBS ON RT SIDE & REPLACED RT MID EPCU 12WL OVER WING
- [SDR DALA2019062803921](https://openairdocs.org/sdr/DALA2019062803921.md): Window Frame · cracked · Jun 27, 2019 · N317US · Airbus A320211 · Fuselage Main, Structure
  > CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER ATTACHEMENT AREA INTERNAL SIDE INNER VERTICAL FACE LH FROM UPPER BOLT TO RADIUS (L=0.150) IN COCKPIT (1 EA), PERFORMED REPAIRS INSTRUCTIONS ON FR2 WINDSHIELD CENTER POST LOWER ATTACHMENT INTERNAL SIDE IN
- [SDR DALA2019062703894](https://openairdocs.org/sdr/DALA2019062703894.md): Fork · cracked · Jun 26, 2019 · N317US · Airbus A320211 · Fuselage Main, Structure
  > CRACK INDICATION ON DOOR FRAME FORK FR25 HOLE H1 (CRACK DIRECTION IS 1 0 AND 4 OCLOCK) IN FWD CARGO COMPARTMENT (2 EA), PERFORMED PERMANENT REPAIR ON DOOR FRAME FOR FR25 HOLE H1 AS PER ER/A 577975-14AD REV 4 AND PRI 577975-14 REV 0,1,2 AND 3
- [SDR DALA2019062703893](https://openairdocs.org/sdr/DALA2019062703893.md): Frame · cracked · Jun 26, 2019 · N317US · Airbus A320211 · Fuselage Main, Frame
  > CRACK INDICATION ON FRAME 35 STGR30LH HOLE 6 (CRACK DIRECTION IS 9 OCL OCK) IN FWD CARGO COMPARTMENT, PERFORMED REPAIR INSTRUCTIONS SECTION 1 ON FR35 STR 30LH HOLE 6 IN FWD CARGO COMPARTMENT AS PER ER/A 578013-14AD REVISION ORIGINAL AND PRI 578013-14 REV 0,REV
- [SDR DALA2019062703892](https://openairdocs.org/sdr/DALA2019062703892.md): Frame · cracked · Jun 26, 2019 · N317US · Airbus A320211 · Fuselage Main, Frame
  > CRACK INDICATION ON FRAME 36 UPPER SURFACE OF THE PRESSURE DECK FROM FASTENER 4.200 INCH IB FROM +Y1292 (L=0.200) IN FWD CARGO COMPARTMENT AND OPEN FASTENER HOLE 4.200 INCH IB FROM +Y1523 (CRACK DIRECTION IS 7 OCLOCK) IN FWD CARGO COMPARTMENT, PERMANENT REPAIR
- [SDR DALA2019062823920](https://openairdocs.org/sdr/DALA2019062823920.md): Stringer · corroded · Jun 21, 2019 · N317US · Airbus A320211 · Fuselage Main, Longeron/Stringer
  > CORROSION STRINGER 43L FR 56 TO FR 57 IN AFT CARGO COMPARTMENT (1 EA), PERFORMED PERMANENT REPAIR ON STRINGER 43L FR56 TO FR57 IN AFT CARGO COMPARTMENT AND COUPLING (2EA) AS PER A320 SRM 53-00-13-300 AND DWG D53470345010
- [SDR DALA2019062523848](https://openairdocs.org/sdr/DALA2019062523848.md): Frame · cracked · Jun 21, 2019 · N317US · Airbus A320211 · Fuselage Main, Frame
  > CRACK INDICATION ON FRAME 35 STGR30RH HOLE 5 (CRACK DIRECTION IS 3 AND 9 OCLOCK) IN FWD CARGO COMPARTMENT, PERFORMED TIME LIMITED REPAIR LOC ON FRAME 35RH AT LEVEL OF STR- 30RH ON BULKHEAD LAYER AS PER PRI 578012-14 REV 0,1,2,3 ERA 578012-14AD REV ORIGINAL
- [SDR DALA2019062513846](https://openairdocs.org/sdr/DALA2019062513846.md): Stringer · corroded · Jun 21, 2019 · N317US · Airbus A320211 · Fuselage Main, Longeron/Stringer
  > CORROSION STRINGER 44 BTW FR32 TO FR34 IN FWD CARGO COMPARTMENT, REPLACED STRINGER 44 BETWEEN FR30 TO FR35 IN FWD CARGO COMPARTMENT AS PER A320 SRM 51-72-11 DWG D53231626 AND PRI 578853-14 REV 0 AND ER/A #578853-14
- [SDR DALA2019062003694](https://openairdocs.org/sdr/DALA2019062003694.md): Floorbeam · corroded · Jun 19, 2019 · N317US · Airbus A320211 · Fuselage Main, Floor Beam
  > CORROSION FLOOR STRUCTURE BEAM LOCATED AT FR 66 -Y1292 AT AFT GALLEY AREA, REPLACED FLOOR BEAM -Y1292 AFT GALLEY AREA AS PER A320 SRM 51-72 -11 AND DRAWING D53472000
- [SDR DALA2019062093693](https://openairdocs.org/sdr/DALA2019062093693.md): Strap · corroded · Jun 18, 2019 · N317US · Airbus A320211 · Fuselage Main, Structure
  > CORROSION LOWER CUTOUT ON STRAP IN FWD CARGO COMPARTMENT, REPLACED STRAP ON LOWER FUSELAGE CUT OUT IN FWD CARGO COMPARMENT (1 E/A) AS PER SRM A320 51-72-11 AND DRAWING D53231563
- [SDR DALA2019061763584](https://openairdocs.org/sdr/DALA2019061763584.md): Frame · cracked · Jun 15, 2019 · N317US · Airbus A320211 · Fuselage Main, Frame
  > CRACK INDICATION ON FRAME 36 AT HOLE A, REPAIR IN ACCORDANCE WITH WORK CARD 5311-01171-04A, AA 5311-01171. SB A320- 53-1264. AD-2018-06-04 IN FWD CARGO COMPARTMENT
- [SDR DALA2019061743582](https://openairdocs.org/sdr/DALA2019061743582.md): Floor Support · corroded · Jun 13, 2019 · N317US · Airbus A320211 · Fuselage Miscellaneous Structure
  > CORROSION FLOOR STRUCTURE BEAM LOCATED BTW FR 20 TO FR 21 AND -Y 1292 IN PASSENGER CABIN, REPLACED FLOOR STRUCTURE BEAM LOCATED FROM FR12 TO FR24 AND - Y1292 IN PASSENGER CABIN AS PER A320 SRM 51-72-11 PRI N578653-14 REV O AND ER/A N578653-14 REV ORIGINAL
- [SDR DALA2019060603433](https://openairdocs.org/sdr/DALA2019060603433.md): Floor Support · corroded · Jun 6, 2019 · N317US · Airbus A320211 · Fuselage Floor Panel
  > CORROSION LEVEL 2 FLOOR STRUCTURE BEAM LOCATED BTW FR 20 TO FR 21 AND -Y 765 IN PASSENGER CABIN, REPLACED FLOOR STRUCTURE BEAM LOCATED BTW FR 12 TO FR 24 AND -Y 765 IN PASSENGER CABIN AS PER A320 SRM 51-72-11 AND DWG D53112812
- [SDR DALA2019060653432](https://openairdocs.org/sdr/DALA2019060653432.md): Seat Track · out of limits · Jun 4, 2019 · N317US · Airbus A320211 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AFTER REWORK -Y1292 FOUND OUT LIMITS REPLACED SEAT TRACK -Y1292 BTW FR41 TO FR47 AS PER ER/A 578485-14 REV ORIGINAL AND PRI 578485-14 REV 0.
- [SDR DALA2019060423396](https://openairdocs.org/sdr/DALA2019060423396.md): Floor Support · corroded · Jun 1, 2019 · N317US · Airbus A320211 · Fuselage Miscellaneous Structure
  > CORROSION FLOOR STRUCTURE BEAM LOCATED FR 20 AND -Y250 IN PASSENGER CABIN, REPLACED FLOOR BEAM LOC BTW FR 20 TO FR23 R/H SIDE FWD CABIN AS PER A320 SRM 51-72-11 AND DWG D 53112834
- [SDR DALA2019060423395](https://openairdocs.org/sdr/DALA2019060423395.md): Seat Track · out of limits · Jun 1, 2019 · N317US · Airbus A320211 · Fuselage, Seat/Cargo Attach Fittings
  > EVALUATE STRUCTURE DAMAGE, AFTER REWORK SEAT TRACK Y-1292 BTW FR36 TO FR41, AND FOUND OUT LIMITS, REPLACED SEAT TRACK -Y1292 BTW FR 36 TO FR 41 IN CENTER FUEL TANK (1EA) ASPER A320 SRM 5-72-11 AND DWG D57130147
- [SDR DALA2019060423393](https://openairdocs.org/sdr/DALA2019060423393.md): Floor Support · corroded · Jun 1, 2019 · N317US · Airbus A320211 · Fuselage Miscellaneous Structure
  > CORROSION FLOOR STRUCTURE BEAM LOCATED BTW FR 20 TO FR 21 AND + Y765 IN PASSENGER CABIN, REPLACED FLOOR STRUCTURE BEAM LOC. BTW FR 12 TO FR 24+Y765 PASSENGER CABIN (1 EA) AS PER A320 SRM 51-72-11 AND DRAWING D53112812

Next page: https://openairdocs.org/deregistered/N317US-2025-08-14/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 = 'N317US' AND deregistration_id = 'N317US-2025-08-14'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N317US-2025-08-14/reports

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