# Service difficulty reports: N932AT

A list on [N932AT](https://openairdocs.org/aircraft/N932AT.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 · 265 reports

- [SDR DALA2026081704697](https://openairdocs.org/sdr/DALA2026081704697.md): Spar Cap · damaged · Aug 16, 2026 · N932AT · Boeing 717200 · Wing Spar
  > HOLES 2IB, 6IB, 12 AND 141WERE FOUND DAMAGED AT LT WING, REAR SPAR, LOWER CAP, XRS=164. COMPLIED WITH ER/A 628386-14. (6542957) (AIRCRAFT GROUNDED).
- [SDR DALA2026081204641](https://openairdocs.org/sdr/DALA2026081204641.md): Spar Cap · damaged · Aug 11, 2026 · N932AT · Boeing 717200 · Wing Spar
  > RIGHT WING REAR SPAR LOWER CAP FUEL LEAK. REPAIRED IAW ER/A 628367-14AD (1751283) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026080704570](https://openairdocs.org/sdr/DALA2026080704570.md): Spar Cap · damaged · Aug 6, 2026 · N932AT · Boeing 717200 · Wing Spar
  > DAMAGED FASTENER HOLES ON LH LOWER SPAR CAP BTW XRS=110 TO 200 APROX AND LOWER SKIN PANEL ON LH WING, CORRECTIVE ACTION: COMPLIED WITH ER/A 628386-14AD. (1741965) (AIRCRAFT GROUNDED).
- [SDR DALA2026080404489](https://openairdocs.org/sdr/DALA2026080404489.md): Mount · corroded · Aug 3, 2026 · N932AT · Boeing 717200 · Wing, Control Surface Attach Fittings
  > CORROSION ON FASTENERS HOLES HOLDING (8 EA) ALSO MOUNTING FLANGE (UPPER HOLES) AT RIGHT WING FLAP INNER HINGE. REPAIRED PER BOEING OVERHAL MANUAL 27-50. (1736786) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026080304469](https://openairdocs.org/sdr/DALA2026080304469.md): Fuel Sys · leaking · Jul 31, 2026 · N932AT · Boeing 717200 · Fuel Storage
  > LT WING REAR SPAR LOWER CAP FUEL LEAK. REPAIRED IAW ER/A 00-628386. (1731448) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026080304468](https://openairdocs.org/sdr/DALA2026080304468.md): Fuel Sys · leaking · Jul 31, 2026 · N932AT · Boeing 717200 · Fuel Storage
  > RIGHT WING REAR SPAR LOWER CAP FUEL LEAK. REPAIRED IAW 00-628367. (1731231) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026073004419](https://openairdocs.org/sdr/DALA2026073004419.md): Door Frame · cracked · Jul 30, 2026 · N932AT · Boeing 717200 · Fuselage Main, Structure
  > CRACK ON UPPER DOOR JAMB AT FWD EMERGENCY EXIT DOOR RH SURROUND STRUCTURE. UPPER DOOR JAMB AT FWD EMERGENCY EXIT DOOR RH SURROUND STRUCTURE WAS REPAIRED PER ER/A 635352-14. (1728206) AIRCRAFT GROUNDED.
- [SDR DALA2026072804382](https://openairdocs.org/sdr/DALA2026072804382.md): Lug · gouged · Jul 28, 2026 · N932AT · Boeing 717200 · Wing, Control Surface Attach Fittings
  > GOUGES ON INBD LUG (OUTB FACE) AND WEAR ON OUTBD LUG (INNER FACE) ALSO CORROSION AND SCRATCHES ON BUSHINGS AT LEFT FLAP FWD HINGE FITTING NR 3. REPAIRED PER ERA 628389-14. (1724322) AIRCRAFT GROUNDED.
- [SDR DALA2026072804381](https://openairdocs.org/sdr/DALA2026072804381.md): Lug · worn · Jul 28, 2026 · N932AT · Boeing 717200 · Wing, Control Surface Attach Fittings
  > WORN OUTBD LUG INBD FACE AT RIGHT FLAP FWD HINGE FITTING NO. 3. CORRECTIVE ACTION: REPAIRED PER ERA 628285-14. (1724181) AIRCRAFT GROUNDED.
- [SDR DALA2026072404316](https://openairdocs.org/sdr/DALA2026072404316.md): Control Cable · worn · Jul 24, 2026 · N932AT · Boeing 717200 · Leading Edge Slat Control System
  > WEAR ON CABLE 185B BTW STA XIS 100 AND XIS 120 OF SLAT SYSTEM AT LT WING, REPAIRED SLAT CONTROL CABLE PER B717 AMM 27-81. (1716656) (AIRCRAFT GROUNDED).
- [SDR DALA2026072004259](https://openairdocs.org/sdr/DALA2026072004259.md): Skin · cracked · Jul 17, 2026 · N932AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACKED FUSELAGE SKIN. REPAIRED PER ER/A 605226-14. (1705409) AIRCRAFT GROUNDED.
- [SDR DALA2026071704215](https://openairdocs.org/sdr/DALA2026071704215.md): Skin · corroded · Jul 16, 2026 · N932AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CORROSION ON WING BOX UPPER SKIN AREA BTW STA 716 TO 737 X=-44.5 TO X=-56.0, COMLIED WITH ER/A 634543-14AD. (1702309) (AIRCRAFT GROUNDED).
- [SDR DALA2026071704214](https://openairdocs.org/sdr/DALA2026071704214.md): Doubler · corroded · Jul 16, 2026 · N932AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CORROSION ON DOUBLER STA Y=1053 BTW LONG'S 29RH TO 29LH APROX LWR AREA AT AFT CARGO COMPARTMENT, REPLACED DOUBLER IAW SRM 51-41-05-0G AND SRM 51-41-02-0G. (1702152) (AIRCRAFT GROUNDED).
- [SDR DALA2026071704213](https://openairdocs.org/sdr/DALA2026071704213.md): Doubler · cracked · Jul 15, 2026 · N932AT · Boeing 717200 · Cargo/Baggage Doors
  > CRACK AT PREVIOUS REPAIR DOUBLER ON INTERNAL PAN BTW BEAM 1 AND 2 AT AFT EDGE OF FWD CARGO DOOR (C1), COMPLIED WITH ER/A 634307-14. (1702038) (AIRCRAFT GROUNDED).
- [SDR DALA2026071304127](https://openairdocs.org/sdr/DALA2026071304127.md): Stiffener · cracked · Jul 13, 2026 · N932AT · Boeing 717200 · Cargo/Baggage Doors
  > CRACK ON INNER SKIN BELOW FWD LOWER STIFFENER AT FWD CARGO DOOR. REPAIRED PER PRI 634332-14. (1696617) (AIRCRAFT GROUNDED)
- [SDR DALA2026070603940](https://openairdocs.org/sdr/DALA2026070603940.md): Retainer · cracked · Jul 3, 2026 · N932AT · Boeing 717200 · Horizontal Stabilizer Miscellaneous Structure
  > CRACKED RETAINER BELOW RT ELEVATOR BOOST CYLINDER AT RT HORIZONTAL STAB. RETAINER BELOW RH ELEVATOR BOOST CYLINDER AT RT HORIZONTAL STAB WAS REPLACED IAW AMM 27-33- 01. (1680260)(AIRCRAFT GROUNDED)
- [SDR DALA2026070603938](https://openairdocs.org/sdr/DALA2026070603938.md): Skin · dented · Jul 3, 2026 · N932AT · Boeing 717200 · Rudder, Plate/Skin
  > DENTS ON SKIN PANEL RT SIDE BTW ZRS=75.762 TO ZRS=93.821 RUDDER. REPAIRED IAW SRM 51-70-13-2R. (1680626)(AIRCRAFT GROUNDED)
- [SDR DALA2026070603937](https://openairdocs.org/sdr/DALA2026070603937.md): Skin · dented · Jul 3, 2026 · N932AT · Boeing 717200 · Rudder, Plate/Skin
  > DENTED SKIN PANEL RH SIDE BTW ZRS=75.762 TO ZRS=93.821 RUDDER. MEASURED AND FOUND WITHIN LIMITS IAW SRM 55-40-01-1A. (1680620)(AIRCRAFT GROUNDED)
- [SDR DALA2026070603936](https://openairdocs.org/sdr/DALA2026070603936.md): Skin · dented · Jul 3, 2026 · N932AT · Boeing 717200 · Rudder, Plate/Skin
  > DENTED ON SKIN PANEL RT SIDE AT RUDDER. REPAIRED IAW SRM 51-70-13-2R. (1680621)(AIRCRAFT GROUNDED).
- [SDR DALA2026070303899](https://openairdocs.org/sdr/DALA2026070303899.md): Skin · cracked · Jul 3, 2026 · N932AT · Boeing 717200 · Rudder, Plate/Skin
  > CRACK WAS FOUND ON EXTERNAL SKIN NEXT TO HOLE TO ATTACH SLIN AT RUDDER, REPAIRED EXTERNAL SKIN PER SRM 51 -70-13-2R. (1679238) (AIRCRAFT GROUNDED).
- [SDR DALA2026062903838](https://openairdocs.org/sdr/DALA2026062903838.md): Door Frame · corroded · Jun 27, 2026 · N932AT · Boeing 717200 · Fuselage Main, Structure
  > CORROSION LEVEL 2. DOOR JAMB BTW STA Y=370 TO Y=427. REPLACED DAMAGED COMPONENT IAW SRM 51-41-02-0G AND SRM 51-41-08-0G. (1669491) (AIRCRAFT GROUNDED).
- [SDR DALA2026061903679](https://openairdocs.org/sdr/DALA2026061903679.md): Hinge Fitting · corroded · Jun 19, 2026 · N932AT · Boeing 717200 · Trailing Edge Flaps
  > CORROSION LEVEL 2 IN FASTENERS HOLES HOLDING 8 EAS LT WING FLAP INNER HINGE. LT WING FLAP INNER HINGE WAS REPLACED PER SERVICEABLE INNER HINGE IAW AMM 57-55-25. (LP 1654540 - AIRCRAFT WAS GROUNDED).
- [SDR DALA2026061903678](https://openairdocs.org/sdr/DALA2026061903678.md): Window Frame · cracked · Jun 19, 2026 · N932AT · Boeing 717200 · Fuselage Main, Structure
  > LT AND RT SLIDE WINDOW FRAME UPPER AFT CORNER AT COCKPIT WERE FOUND: CRACKS ON INNER SURFACE AT UPPER/LOWER RETAINERS LT/RT COCKPIT. CRACKS ON INNER SURFACE AT UPPER/LOWER RETAINERS RT SIDE COCKPIT WERE REPAIRED PER SRM 56-10-02-2R. (LP 1654532 - AIRCRAFT WA
- [SDR DALA2026060903436](https://openairdocs.org/sdr/DALA2026060903436.md): Not Reported · corroded · Jun 3, 2026 · N932AT · Boeing 717200 · Fuselage Structure (General)
  > IN REFERENCE TO NRC 706 WIP NR 9, CORROSION OUT OF LIMITS AT RT SIDE. REPAIRED IAW SRM 53-00-55 (1628543) (AIRCRAFT GROUNDED)
- [SDR DALA2026060203340](https://openairdocs.org/sdr/DALA2026060203340.md): Cusp Web · corroded · May 30, 2026 · N932AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION OUT OF LIMITS, IN REFERENCE TO NRC 00700: CORROSION ON LH SIDE FLOOR CUSP WEB. REPAIRED PER B717-200 SRM 53-00-55 (1621710) (AIRCRAFT GROUNDED)
- [SDR DALA2026052903259](https://openairdocs.org/sdr/DALA2026052903259.md): Structure · corroded · May 28, 2026 · N932AT · Boeing 717200 · Horizontal Stabilizer Miscellaneous Structure
  > AFTER BOLT AND BARREL NUT REMOVAL. CORROSION ON INNER HOLE, BOLT, WASHER AND NUT BARREL WERE FOUND. REPAIRED PER ER/A 634191-14AD. (1618112) (AIRCRAFT GROUNDED)
- [SDR DALA2026052903254](https://openairdocs.org/sdr/DALA2026052903254.md): Cusp Web · corroded · May 26, 2026 · N932AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > OUT OF LIMITS CORROSION ON RT SIDE FLOOR CUSP WEB. REPAIRED PER SRM 53-00-55 (1613746) (AIRCRAFT GROUNDED)
- [SDR DALA2026052803224](https://openairdocs.org/sdr/DALA2026052803224.md): Longeron · cracked · May 23, 2026 · N932AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CRACKED LONGERONS 5R, 6R, 7R AND 8R AT BS 1022. REPAIRED PER SRM 53-00-05 (1607816) (AIRCRAFT GROUNDED)
- [SDR DALA2026052803220](https://openairdocs.org/sdr/DALA2026052803220.md): Cusp Web · cracked · May 21, 2026 · N932AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON LH SIDE FLOOR CUSP WEB BTW STA Y= 655 AND STA Y=674 AND STA X=60. CRACK ON LT SIDE FLOOR CUSP WEB BTW STA Y= 655 AND STA Y=674 AND STA X=60 WAS REPAIRED PER B717-200 SRM 53- 00-55 (1606007) (AIRCRAFT GROUNDED)
- [SDR DALA2026051903061](https://openairdocs.org/sdr/DALA2026051903061.md): Not Reported · not reported · May 6, 2026 · N932AT · Boeing 717200 · Standard Practices/Structures
  > DTA ER/A 634191-14 SECTION II MONITOR LOG REQUIRES DTA APPROVAL. C/W ER/A 00-634191. (1592353) (AIRCRAFT GROUNDED)
- [SDR DALA2026051102944](https://openairdocs.org/sdr/DALA2026051102944.md): Beam · cracked · May 6, 2026 · N932AT · Boeing 717200 · Passenger/Crew Doors
  > CRACK ON BEAM 1 FWD UPPER EDGE BEYOND STOP DRILL ON PREVIOUS REPAIR AT PASSENGER ENTRANCE DOOR L1. REPAIRED PER B717-200 S.R.M. 52-10-02 (1579574) (AIRCRAFT GROUNDED)
- [SDR DALA2026051102942](https://openairdocs.org/sdr/DALA2026051102942.md): Wire · broken · May 5, 2026 · N932AT · Boeing 717200 · Equipment/Furnishings Wiring
  > BROKEN WIRES ON LANDYARD ASSEMBLY (2EAS) OF FORWARD SERVICE/PASSENGER DOOR SLIDE. REPAIRED PER AMDS 5211-4002 AND AMDS 5211-4004 (1579444) (AIRCRAFT GROUNDED)
- [SDR DALA2026031301748](https://openairdocs.org/sdr/DALA2026031301748.md): Door Frame · corroded · Mar 12, 2026 · N932AT · Boeing 717200 · Fuselage Main, Structure
  > SHIP 9568 SEVERAL AREAS WITH CORROSION ON DOOR JAMB AT AFT CARGO. CORRECTIVE ACTION: DOOR JAMB AT AFT CARGO WAS REPLACED PER B717-200 SRM 53-20-15-2R PROCEDURE 7 REPAIR 7 (1490650)
- [SDR DALA2025090906667](https://openairdocs.org/sdr/DALA2025090906667.md): None · none · Sep 4, 2025 · N932AT · Boeing 717200 · Standard Practices/Structures
  > DTA ER/A 628389-14 SECTION II MONITOR LOG REQUIRES DTA APPROVAL ON OR BEFORE THE NEXT 24 MONTHS AFTER 04-SEP-25. CORRECTIVE ACTION: REPAIRED ASSOCIATED ER/A 00-628389 (1183511)
- [SDR DALA2025090206465](https://openairdocs.org/sdr/DALA2025090206465.md): None · none · Aug 24, 2025 · N932AT · Boeing 717200 · Standard Practices/Structures
  > DTA ER/A 628285-14 SECTION II MONITOR LOG REQUIRES DTA APPROVAL ON OR BEFORE THE NEXT 24 MONTHS AFTER 24-AUG-25. DISCONTINUE REVENUE SERVICE ON OR BEFORE THE NEXT 24 MONTHS AFTER 24-AUG-25 PENDING A DAMAGE TOLERANCE AND FATIGUE REVIEW. ASSOCIATED ER/A 00-628
- [SDR DALA2025060604331](https://openairdocs.org/sdr/DALA2025060604331.md): Shear Tie · cracked · May 27, 2025 · N932AT · Boeing 717200 · Fuselage Internal Mounting Structure
  > SHIP 9568 INITIAL INSPECTION: CRACKED FRAME CLIP ON STA Y=1144 BTW LONG 1 AND LONG 2L ALSO ON STA Y=1152 BTW LONG 1 AND LONG 2L AT AFT ACC. COMPARTMENT. CORRECTIVE ACTION: REPAIRED PER ER/A 626274-14 REV. (0990391)
- [SDR DALA2025051903829](https://openairdocs.org/sdr/DALA2025051903829.md): Longeron · cracked · May 15, 2025 · N932AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > SHIP 9568 INITIAL INSPECTION: CRACK ON LONG 2 LH STA Y=1133 AT AFT ACC COMPARTMENT. CORRECTIVE ACTION: REPAIRED PER B717-200 SRM 53-00-05-2R REPAIR 2 (0967936)
- [SDR DALA2025051903830](https://openairdocs.org/sdr/DALA2025051903830.md): Tab · delaminated · May 6, 2025 · N932AT · Boeing 717200 · Ailerons
  > SHIP 9568 INITIAL INSPECTION: DELAMINATED CONTROL TAB OF AILERON AT LH WING. CORRECTIVE ACTION: AILERON CONTROL TAB WAS REMOVED (PN: UNK, SN: 5106) AND SERVICEABLE AILERON CONTROL TAB (P/N: 5910047-501 S/N: 5029) WAS INSTALLED AT LH WING PER B717-200 AMM 27-10
- [SDR DALA2025041102822](https://openairdocs.org/sdr/DALA2025041102822.md): Skin · leaking · Apr 9, 2025 · N932AT · Boeing 717200 · Wing, Plate/Skin
  > -AD- FUEL LEAK FOUND DURING INSPECTION OF THE LH WING AFT LOWER SKIN AT XRS=164 AA #FE5720-01103. ALL REPAIRS C/W PER ERA 622371-14AD. RII C/W [DELTA QC 5223]. (LP #0903380)
- [SDR DALA2025041102821](https://openairdocs.org/sdr/DALA2025041102821.md): Access Panel · leaking · Apr 9, 2025 · N932AT · Boeing 717200 · Wing, Plate/Skin
  > -AD- FUEL LEAK FOUND DURING INSPECTION OF THE LH WING AFT LOWER SKIN DOUBLER AT XRS=164. CONTACT LIAISON ENG FOR REPAIR PROCEDURES PRIOR TO FURTHER FLIGHT AA #FE5720-011.03. ALL REPAIRS C/W PER ERA 622371-14AD. RII C/W [DELTA QC5223]. (LP #0903374)
- [SDR DALA2025021101060](https://openairdocs.org/sdr/DALA2025021101060.md): Attach Bracket · cracked · Feb 9, 2025 · N932AT · Boeing 717200 · Wing, Attach Fittings
  > -AD- PRI 622371-14AD, REV 3 HOLE #9 ON OUTBOARD FAIRING ATTACH BRACKET HAS CRACK INDICATION. FLAP FAIRING ATTACH BRACKET REPLACED DURING LEFT WING LOWER SKIN DOUBLER REPAIR ON ER/A 622371-14AD, REV O. JOB COMPLETE. A/C OK FOR SERVICE. (LP #0803598)
- [SDR DALA2025021101059](https://openairdocs.org/sdr/DALA2025021101059.md): Attach Bracket · cracked · Feb 9, 2025 · N932AT · Boeing 717200 · Wing, Attach Fittings
  > -AD- PRI 622371-14AD, REV 3 HOLE #8 ON OUTBOARD FLAP FAIRING ATTACH BRACKET HAS CRACK INDICATION. FLAP FAIRING ATTACH BRACKET REPLACED DURING LEFT WING LOWER SKIN DOUBLER REPAIR ON ER/A 622371-14AD, REV O. A/C OK FOR SERVICE. (LP #0803594)
- [SDR DALA2025021101058](https://openairdocs.org/sdr/DALA2025021101058.md): Attach Bracket · cracked · Feb 9, 2025 · N932AT · Boeing 717200 · Wing, Attach Fittings
  > -AD- PRI 622371-14AD, REV 3 HOLE #5 ON OUTBOARD FLAP FAIRING ATTACH BRACKET HAS CRACK INDICATION. FLAP FAIRING ATTACH BRACKET REPLACED DURING LEFT WING LOWER SKIN DOUBLER REPAIR ON ER/A 622371-14AD, REV O. JOB COMPLETE. A/C OK FOR SERVICE. (LP #0803588)
- [SDR DALA2025021101057](https://openairdocs.org/sdr/DALA2025021101057.md): Attach Bracket · cracked · Feb 9, 2025 · N932AT · Boeing 717200 · Wing, Attach Fittings
  > -AD- PRI 622371-14AD, REV 3 HOLE #1 ON OUTBOARD FLAP FAIRING ATTACH BRACKET HAS CRACK INDICATION. FLAP FAIRING ATTACH BRACKET REPLACED DURING LEFT WING LOWER SKIN DOUBLER REPAIR ON ER/A 622371-14AD, REV O. JOB COMPLETE. A/C OK FOR SERVICE. (LP #0803577)
- [SDR DALA2025021101056](https://openairdocs.org/sdr/DALA2025021101056.md): Attach Fitting · cracked · Feb 9, 2025 · N932AT · Boeing 717200 · Wing, Attach Fittings
  > -AD- PRI 622371-14AD, REV 2 HOLE #6 ON INBOARD FLAP FAIRING ATTACH BRACKET HAS CRACK INDICATION. FLAP FAIRING ATTACH BRACKET REPLACED DURING LEFT WING LOWER SKIN DOUBLER REPAIR ON ER/A 622371-14AD, REV O. JOB COMPLETE. A/C OK FOR SERVICE. (LP #0803565)
- [SDR DALA2025021101055](https://openairdocs.org/sdr/DALA2025021101055.md): Attach Fitting · cracked · Feb 9, 2025 · N932AT · Boeing 717200 · Wing, Attach Fittings
  > -AD- PRI 622371-14AD, REV 2 HOLE #5 ON INBOARD FLAP FAIRING ATTACH BRACKET HAS CRACK INDICATION. FLAP FAIRING ATTACH BRACKET REPLCAED DUEING LEFT WING LOWER SKIN DOUBLER REPAIR ON ER/A 622371-14AD, REV O. JOB COMPLETE. A/C OK FOR SERVICE. (LP #0803562)
- [SDR DALA2025020600921](https://openairdocs.org/sdr/DALA2025020600921.md): Attach Bracket · cracked · Feb 1, 2025 · N932AT · Boeing 717200 · Wing, Attach Fittings
  > -AD- DURING BHEC ON PRI 622371-14AD, REV 2 HOLE #2 ON INBOARD FLAP FAIRING ATTACH BRACKET HAS A CRACK INDICATION. FLAP FAIRING ATTACH BRACKET REPLACED DURING LEFT WING LOWER SKIN DOUBLER REPAIR ON ER/A 622371-14AD, REV O. JOB COMPLETE. A/C OK FOR SERVICE. (LP
- [SDR DALA2025020600920](https://openairdocs.org/sdr/DALA2025020600920.md): Support Fitting · damaged · Feb 1, 2025 · N932AT · Boeing 717200 · Wing, Attach Fittings
  > -AD- ON LEFT WING XRS 164.00 LOWER FLAP HINGE SUPPORT FITTING 2ND NUT FORWARD ON INBOARD SIDE IS LOOSE. FASTENER REPLACED DURING LEFT WING LOWER SKIN REPAIR ON ER/A 622371-14AD, REV O. JOB COMPLETE. A/C OK FOR SERVICE. (LP #0791075)
- [SDR DALA2025020600919](https://openairdocs.org/sdr/DALA2025020600919.md): Attach Bracket · damaged · Feb 1, 2025 · N932AT · Boeing 717200 · Trailing Edge Flaps
  > -AD- DURING BHEC ON PRI 622371-14AD, REV 2 HOLE #4 ON INBOARD FLAP FAIRING ATTACH BRACKET HAS CRACK INDICATION. HOLE #4 OVERSIZED TO 0.363" ON STEP 41 OF PRI 622371-14AD, REV 9. FREEZE PLUG INSTALLED ON PART C, STEP 12 OF PRI 622371-14AD, REV 13. HOLE WILL BE
- [SDR DALA2025020600918](https://openairdocs.org/sdr/DALA2025020600918.md): Attach Bracket · damaged · Feb 1, 2025 · N932AT · Boeing 717200 · Trailing Edge Flaps
  > -AD- DURING BHEC ON PRI 622371-14AD, REV 2 HOLE #3 ON INBOARD FLAP FAIRING ATTACH BRACKET HAS 2 CRACK INDICATIONS. HOLE #3 OVERSIZED TO 0.547" ON STEP 41 OF PRI 622371-14AD, REV 9. FREEZE PLUG INSTALLED IN HOLE #3 ON STEP 12, PART C OF PRI 622371-14AD, REV 13.

Next page: https://openairdocs.org/aircraft/N932AT/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 = 'N932AT' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N932AT/reports

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