# Service difficulty reports: N925AT

A list on [N925AT](https://openairdocs.org/aircraft/N925AT.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 4 · 182 reports

- [SDR DALA2025121709200](https://openairdocs.org/sdr/DALA2025121709200.md): Actuator · faulted · Dec 15, 2025 · N925AT · Boeing 717200 · Landing Gear Door Actuator
  > MISC/DE-DECLARED AN EMERGENCY INTO ATL DUE TO LEFT AND RIGHT MAIN GEAR UNSAFE LIGHTS. REPLACED LANDING GEAR DOOR ACTUATOR. OPS TESTED NORMAL.(5447268)
- [SDR DALA2025121009015](https://openairdocs.org/sdr/DALA2025121009015.md): Sensor · out of adjust · Dec 7, 2025 · N925AT · Boeing 717200 · Landing Gear Position and Warning
  > ATB, PERFORMED AN AIR TURN BACK DUE TO LEFT AND RIGHT MAIN GEAR UNSAFE LIGHTS. COMPLIED WITH NO GO MSI LOG, ADJUSTED LEFT DOOR ACTUATOR TO WITHIN LIMITS, ADJUSTED RIGHT GEAR DOOR UP AND LATCHED SENSOR TO WITHIN LIMITS AND REPLACED THE S1-89 LANDING GEAR HAN
- [SDR DALA2025120508918](https://openairdocs.org/sdr/DALA2025120508918.md): Proximity Switch · faulted · Dec 2, 2025 · N925AT · Boeing 717200 · Landing Gear Position and Warning
  > DIVERTED TO CVG DUE TO A GEAR UNSAFE MESSAGE. REPLACED PSEU, ALL TEST PASS. ADJUSTED RIGHT LANDING DOOR LATCH PROX SWITCH. OPS CHECK NORMAL.(5447210)
- [SDR DALA2025111808428](https://openairdocs.org/sdr/DALA2025111808428.md): Spar Cap · cracked · Nov 17, 2025 · N925AT · Boeing 717200 · Wing Spar
  > DISCOVERED A CRACK COMMON TO THE RT WING LOWER REAR SPAR CAP. COMPLIED WITH ERA 620694-14AD (1308670).
- [SDR DALA2025111908462](https://openairdocs.org/sdr/DALA2025111908462.md): Spar Cap · cracked · Nov 16, 2025 · N925AT · Boeing 717200 · Wing Spar
  > WHILE TROUBLESHOOTING A FUEL LEAK, MAINTENANCE DISCOVERED A CRACK COMMON TO THE RH WING LOWER REAR SPAR CAP, COMMON TO THE RH WING REAR SPAR INST AT APPROXIMATELY 5.0" INBD OF XRS 164.000. THE MAIN CRACK MEASURES APPROXIMATELY 0.945" LONG, TERMINATING AT A FAS
- [SDR DALA2025110708136](https://openairdocs.org/sdr/DALA2025110708136.md): Panel · not reported · Nov 2, 2025 · N925AT · Boeing 717200 · Wing Structure
  > L/H UPPER AFT T/E STRUCTURAL PANEL FROM XF 111.250" TO XTE 206.852". REMOVED L/H UPPER AFT T/E STRUCTURAL PANEL FROM XF 111.250" TO XTE 206.852" (1284968)
- [SDR DALA2025102407795](https://openairdocs.org/sdr/DALA2025102407795.md): Access Panel · damaged · Oct 22, 2025 · N925AT · Boeing 717200 · Wing, Plate/Skin
  > FOUND FASTENER HOLE OUT OF ROUND AT TANK PLATE 520HB. REPAIRED REF ERA 629530-14 REV O (1265545)
- [SDR DALA2025063004854](https://openairdocs.org/sdr/DALA2025063004854.md): Stringer Splice · no discrepancy · Jun 25, 2025 · N925AT · Boeing 717200 · Fuselage Structure (General)
  > SHIP 9574 SPLICE STRINGERS 13L AND 14L AT STA 1022 FOR ACCESS REF NR 1585. CORRECTIVE ACTION: COMPLETED AND MATCH FINAL - E/RA 624873-14 (1045986)
- [SDR DALA2025062604795](https://openairdocs.org/sdr/DALA2025062604795.md): Skin · cracked · Jun 25, 2025 · N925AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > SHIP 9574 FUSELAGE SKIN. VISUAL INDICATION OF CRACK. LOCATED ABOVE #1 PYLON AT STA 1022. CORRECTIVE ACTION: REPAIRED PER E/RA 624873-14 REV. ORIG. (1045993)
- [SDR DALA2025052203936](https://openairdocs.org/sdr/DALA2025052203936.md): Skin · cracked · May 15, 2025 · N925AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > SHIP 9574 CRACK INDICATION ABOVE THE L/H PYLON IN THE FUSELAGE SKIN. CORRECTIVE ACTION: DOUBLER REPAIR ON A CRACK DAMAGE ON FUSELAGE SKIN P/N 5936436- 101, STA 1022 ABOVE STRINGER 14L. (0969252)
- [SDR DALA2025050503406](https://openairdocs.org/sdr/DALA2025050503406.md): Frame · damaged · May 2, 2025 · N925AT · Boeing 717200 · Fuselage Main, Frame
  > STA 1053.00 PRESSURE BULKHEAD LOWER Y CHORD DAMAGED BETWEEN LONGERON 26L-LONGERON 28L. SUMMARY SEE NRC 001-0575:5300-2013/024 01395: COMPLIED WITH E/RA 625071-14 REV ORIG. PRI REV 0, 1, 2, 3, 4, 5, 6. REPAIR INSTRUCTIONAL STEPS. ENSURED ALL E/RA 625071-14 RE
- [SDR DALA2025042103075](https://openairdocs.org/sdr/DALA2025042103075.md): Spar · corroded · Apr 19, 2025 · N925AT · Boeing 717200 · Wing Spar
  > LH AUX SPAR WEB 9919401-3 HAS CORROSION ON IB LWR FWD SURFACE. SUMMARY SEE NRC 002-0001:0514-2001/207 01575: REPLACED PER B717 DWG 9919401. (LP #0921231)
- [SDR DALA2025042103074](https://openairdocs.org/sdr/DALA2025042103074.md): Stiffener · corroded · Apr 19, 2025 · N925AT · Boeing 717200 · Wing Miscellaneous Structure
  > LH AUX SPAR WEB STIFFENER 9919401-5 HAS CORROSION ON IB LWR FWD SURFACE. SUMMARY SEE NRC 002-0001:0514-2001/209 01577: REPLACED PER B717 DWG 9919401. (LP #0921228)
- [SDR DALA2026012700608](https://openairdocs.org/sdr/DALA2026012700608.md): Support Angle · corroded · Apr 9, 2025 · N925AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > AFT SIDE OF FRAME WEB & LOWER SUPPORT ANGLE ARE CORRODED, JUST FWD OF PRESSURE DOME FWD FACE, LBL14 -RBL 14. REPLACED DOUBLER SUPPORT ANGLE BETWEEN JACK SUPPORT FITTING AND BS 1053 VERTICAL SUPPORT BULKHEAD WEB AT STRINGER 30, IAW SRM 51-40-02. (0904793)
- [SDR DALA2026012700607](https://openairdocs.org/sdr/DALA2026012700607.md): Seat Track · corroded · Apr 9, 2025 · N925AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT OTBD SEAT TRACK, FWD TIE FITTING AT FWD END OF TRACK, BS 212 CORRODED. REPLACED THE SEAT TRACK END FITTING IAW DWG 5930566. (0903766)
- [SDR DALA2025102407791](https://openairdocs.org/sdr/DALA2025102407791.md): Hinge Fitting · corroded · Apr 9, 2025 · N925AT · Boeing 717200 · Trailing Edge Flaps
  > LT FLAP I/B FWD HINGE FITTING MOUNT PINS ON REAR SPAR CORRODED 4EA. REPAIRED PER ERA 620694-14AD. (0904194)
- [SDR DALA2025040902761](https://openairdocs.org/sdr/DALA2025040902761.md): Web · corroded · Apr 9, 2025 · N925AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > WEB FOUND CORRODED LHS OF Y CHORD AT STA 1053. SUMMARY SEE NRC 001-0575:5300-2013/027 01414: REPAIRED WEB REF B717 SRM 51-70-10-2R REPAIR 1. (LP #0903790)
- [SDR DALA2025040902757](https://openairdocs.org/sdr/DALA2025040902757.md): None · none · Apr 8, 2025 · N925AT · Boeing 717200 · Standard Practices/Structures
  > CUT AND REMOVE LOWER STA 1053.00 ANGLE 9915561-35 AT APPROX LBL 16 FOR MTC ACCESS. SUMMARY SEE NRC 001-0575:5300-2013/018 01367: CUT, REMOVED, AND REINSTALLED ANGLE 9915561-35 REF B717-200 SRM 51-70-11-2R REPAIR 1. TYPICAL FORMED CHANNEL REPAIR AND DAC DWG 991
- [SDR DALA2025040902756](https://openairdocs.org/sdr/DALA2025040902756.md): None · none · Apr 8, 2025 · N925AT · Boeing 717200 · Standard Practices/Structures
  > CUT AND REMOVE LOWER STA 1053.00 ANGLE 9915561-36 AT APPROX RBL 16 FOR MTC ACCESS. SUMMARY SEE NRC 001-0575:5300-2013/019 01368: CUT, REMOVED, AND REINSTALLED ANGLE 9915561-35 REF B717-200 SRM 51-70-11-2R REPAIR 1. TYPICAL FORMED CHANNEL REPAIR AND DAC DWG 991
- [SDR DALA2025040102468](https://openairdocs.org/sdr/DALA2025040102468.md): Frame · corroded · Mar 26, 2025 · N925AT · Boeing 717200 · Fuselage Main, Frame
  > FS 1022, LOWER PRIOR FRAME REPAIR AT STR 29LT-30 IS CORRODED. SUMMARY SEE NRC 001-0545:5331-2001/010 01244: CORROSION LEVEL 2. REPAIRED 3 ROLLED Z-FRAME REPAIR SPLICE PER B717-200 SRM 53-20-07-2R. (LP #0879160)
- [SDR DALA2025031902065](https://openairdocs.org/sdr/DALA2025031902065.md): Frame · corroded · Mar 19, 2025 · N925AT · Boeing 717200 · Fuselage Main, Frame
  > CORROSION FOUND ON FRAME AT F.S. 889 BETWEEN STRINGER 29L. SUMMARY SEE NRC 001-0508:2550-2001/008 01228: CLEANED UP FRAME REF B717-200 SRM 53-00-00-1A ALLOWABLE DAMAGE GENERAL. FOUND TO BE OUT OF LIMITS. REPAIRED REF B717-200 SRM 53-20-07-2R REPAIR 3 ROLLED Z-
- [SDR DALA2025031702026](https://openairdocs.org/sdr/DALA2025031702026.md): Seat Track · corroded · Mar 15, 2025 · N925AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT MID SEAT TRACK CORRODED AT FORWARD END. MARKED. SUMMARY SEE NRC 001-0550:5300-2010/013 00986: REPAIRED PER B717 SRM 53-20-52 REPAIR 5 (CP LEVEL 2) CLOSING REQUIREMENTS RII: INSPECTOR 00316969. CORROSION LEVEL CHANGED FROM 1 TO: 2. (LP #0859488)
- [SDR DALA2025031702024](https://openairdocs.org/sdr/DALA2025031702024.md): Seat Track · corroded · Mar 14, 2025 · N925AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT I/B SEAT TRACK CORRODED AT FORWARD END. MARKED. SUMMARY SEE NRC 001-0550:5300-2010/012 00985: REPAIRED PER B717 SRM 53-20-52-2R PROCEDURE 5 (CPCP LEVEL 1). (LP #0858357)
- [SDR DALA2025031702021](https://openairdocs.org/sdr/DALA2025031702021.md): Fitting · corroded · Mar 14, 2025 · N925AT · Boeing 717200 · Fuselage Main, Structure
  > STR 25R END FITTING CORRODED (MKD). SUMMARY SEE NRC 001-0467:2000-1002/567 01398: CORROSION LEVEL 2. CLEANED UP STRINGER END FITTING REF B717-200 SRM 53-00-00-1A. ALLOWABLE DAMAGE GENERAL. RESTORED FINISH REF B717-200 SRM 51-10-04. (LP #0858004)
- [SDR DALA2025031702020](https://openairdocs.org/sdr/DALA2025031702020.md): Stringer · corroded · Mar 14, 2025 · N925AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > STR 26R END FITTING CORRODED (MKD). SUMMARY SEE NRC 001-0467:2000-1002/566 01397: CORROSION LEVEL 2. CLEANED UP STRINGER END FITTING REF B717-200 SRM 53-00-00-1A. ALLOWABLE DAMAGE GENERAL. RESTORED FINISH REF B717-200 SRM 51-10-04. (LP #0858003)
- [SDR DALA2026012700609](https://openairdocs.org/sdr/DALA2026012700609.md): Longeron · corroded · Mar 13, 2025 · N925AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CORROSION UNDER BATTERY TRAYS, LONGERON. REMOVED AND REPLACED THE LONGERON IAW DWG 5911401. (0855196)
- [SDR DALA2025031201903](https://openairdocs.org/sdr/DALA2025031201903.md): Stringer · corroded · Mar 11, 2025 · N925AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CORRODED STR 30 IN MAIN E&E JUST UNDER BATTERY TRAYS. CLEANED CORROSION ON LONGERON REF: B717-200 SRM 53-00-05-2R REPAIR 3. LONGERON (HAT SECTION) REPAIR. LOCAL BLEND OUT REPAIR. UNABLE TO REPAIR, REPLACED LONGERON REF: DACDWG 5911401. (LP #0853025)
- [SDR DALA2025031101886](https://openairdocs.org/sdr/DALA2025031101886.md): Frame · damaged · Mar 7, 2025 · N925AT · Boeing 717200 · Fuselage Main, Frame
  > STA 1225 CANTED FRAME: TAILCONE ALIGNMENT PIN AND CANTED FRAME DAMAGED AT APPROX 7 O'CLOCK POSITION -MARKED-. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY SEE NRC 001-0586:5300-2004/00
- [SDR DALA2025030601772](https://openairdocs.org/sdr/DALA2025030601772.md): Longeron · corroded · Mar 6, 2025 · N925AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CORROSION ON LONGERON 29R, FWD OF STA. 370. "M" AND PIC ATTACHED. SUMMARY SEE NRC 001-0513:5331-2007/001 00558: CORROSION LEVEL 2. CMOR CLEANED CORROSION ON LONGERON REF B717-200 SRM 53-00-05-2R REPAIR 3. LONGERON (HAT SECTION) REPAIR. LOCAL BLEND OUT REPAIR.
- [SDR DALA2025022101360](https://openairdocs.org/sdr/DALA2025022101360.md): Door · damaged · Feb 19, 2025 · N925AT · Boeing 717200 · Cargo/Baggage Doors
  > C-1 FWD CARGO DOOR HAS EXCESSIVE DAMAGE. REPLACED FWD CARGO DOOR. LOG CREATED FOR PARTS CHANGE DOCUMENTATION. INSTALLED ON ROUTINE CARD 5231-4003. (LP #0818827)
- [SDR DALA2025021201092](https://openairdocs.org/sdr/DALA2025021201092.md): Support · corroded · Feb 11, 2025 · N925AT · Boeing 717200 · Cargo/Baggage Doors
  > AFT CARGO DOOR INNER SUPPORT AT LOWER END IS CORRODED. SUMMARY SEE NRC 001-0467:2000-1002/191 00296: CORROSION LEVEL 1. AFT CARGO DOOR WAS REPLACED ON NRC 293. (LP #0806189)
- [SDR DALA2025020500884](https://openairdocs.org/sdr/DALA2025020500884.md): Spar · cracked · Feb 4, 2025 · N925AT · Boeing 717200 · Wing Spar
  > THE #13 FASTENER HOLE SHOWS A CRACK INDICATION WITH BHEC IN SPAR LAYER. RH WING REAR SPAR LOWER SURFACE. MARKED. SUMMARY SEE NRC 003-0001:0514-2001/024 00024: NR TRANSFERRED TO H-CK PKG#P-384718220250123 - NR# 31. (LP #0795830)
- [SDR DALA2025020500880](https://openairdocs.org/sdr/DALA2025020500880.md): Spar Cap · cracked · Feb 4, 2025 · N925AT · Boeing 717200 · Fuselage Floor Panel
  > A CRACK COMMON TO THE RH WING LOWER REAR SPAR CAP. AS A PRECAUTION AN ER/A HAS BEEN ISSUED REQUIRING MAINTENANCE TO ACCOMPLISH INSPECTIONS OF THE LH WING LOWER REAR SPAR CAP TO ENSURE NO CRACKS ARE FOUND. SUMMARY SEE NRC 003-0001:0514-2001/042 00042: NR TRANSF
- [SDR DALA2025020500879](https://openairdocs.org/sdr/DALA2025020500879.md): Spar · cracked · Feb 4, 2025 · N925AT · Boeing 717200 · Wing Spar
  > THE #12 FASTENER HOLE SHOWS A CRACK INDICATION WITH BHEC IN SPAR LAYER. RH WING REAR SPAR LOWER SURFACE. MARKED. SUMMARY SEE NRC 003-0001:0514-2001/028 00028: NR TRANSFERRED TO H-CK PKG #P-384718220250123 - NR# 35. (LP #0795839)
- [SDR DALA2025020500878](https://openairdocs.org/sdr/DALA2025020500878.md): Spar · cracked · Feb 4, 2025 · N925AT · Boeing 717200 · Wing Spar
  > THE #16 FASTENER HOLE SHOWS MULTIPLE CRACK INDICATIONS WITH BHEC IN SPAR AND SKIN LAYERS. RH WING REAR SPAR LOWER SURFACE. MARKED. SUMMARY SEE NRC 003-0001:0514-2001/027 00027: NR TRANSFERRED TO H-CK PKG#P-384718220250123 - NR# 34. (LP #0795837)
- [SDR DALA2025020500877](https://openairdocs.org/sdr/DALA2025020500877.md): Spar · cracked · Feb 4, 2025 · N925AT · Boeing 717200 · Wing Spar
  > THE #15 FASTENER HOLE SHOWS MULTIPLE CRACK INDICATIONS WITH BHEC IN SPAR AND SKIN LAYERS. RH WING REAR SPAR LOWER SURFACE. MARKED. SUMMARY SEE NRC 003-0001:0514-2001/026 00026: NR TRANSFERRED TO H-CK PKG#P-384718220250123 - NR# 33. (LP #0795835)
- [SDR DALA2025020500876](https://openairdocs.org/sdr/DALA2025020500876.md): Skin · cracked · Feb 4, 2025 · N925AT · Boeing 717200 · Wing, Plate/Skin
  > THE #14 FASTENER HOLE SHOWS MULTIPLE CRACK INDICATIONS WITH BHEC IN SPAR AND SKIN LAYERS. RH WING REAR SPAR LOWER SURFACE. MARKED. SUMMARY SEE NRC 003-0001:0514-2001/025 00025: NR TRANSFERRED TO H-CK PKG#P-384718220250123 - NR# 32. (LP #0795831)
- [SDR DALA2025020500875](https://openairdocs.org/sdr/DALA2025020500875.md): Spar · cracked · Feb 4, 2025 · N925AT · Boeing 717200 · Wing Spar
  > THE #11 FASTENER HOLE SHOWS A CRACK INDICATION WITH BHEC IN SPAR LAYER. RH WING REAR SPAR LOWER SURFACE. MARKED. SUMMARY SEE NRC 003-0001:0514-2001/023 00023: NR TRANSFERRED TO H-CK PKG#P-384718220250123 - NR# 30. (LP #0795829)
- [SDR DALA2025020500874](https://openairdocs.org/sdr/DALA2025020500874.md): Spar · cracked · Feb 4, 2025 · N925AT · Boeing 717200 · Wing Spar
  > THE #10 FASTENER HOLE SHOWS MULTIPLE CRACK INDICATIONS WITH BHEC IN SPAR LAYER. RH WING REAR SPAR LOWER SURFACE. MARKED. SUMMARY SEE NRC 003-0001:0514-2001/022 00022: NR TRANSFERRED TO H-CK PKG#P-384718220250123 - NR# 29. (LP #0795826)
- [SDR DALA2025020500873](https://openairdocs.org/sdr/DALA2025020500873.md): Spar Cap · cracked · Feb 4, 2025 · N925AT · Boeing 717200 · Wing Spar
  > -AD- CRACK COMMON TO THE RH WING LOWER REAR SPAR CAP, COMMON TO THE RH WING REAR SPAR INST AT APPROXIMATELY 5.0" INBD OF XRS 164.000. THE MAIN CRACK MEASURES APPROXIMATELY 0.945" LONG, TERMINATING AT A FASTENER LOCATION. COMPLY WITH RH WING / LOWER REAR SPAR C
- [SDR DALA2024081608214](https://openairdocs.org/sdr/DALA2024081608214.md): Contact · shorted · Aug 16, 2024 · N925AT · Boeing 717200 · Electrical Power System Wiring
  > SHIP 9574 -SMKE- AFTER LIGHT TEST, WE NOTICED THAT THE RIGHT APU BUS LIGHT WAS INOPERATIVE. WE TRIED RESETTING THE LIGHT BUT THE BULB AND SOCKET BRIEFLY EMITS SMOKE. MAINTENANCE FOUND THAT THE KORRY SWITCH BRACKET FOR THE APU LIGHT MADE CONTACT AND BURNT UP TH
- [SDR DALA2023122810695](https://openairdocs.org/sdr/DALA2023122810695.md): Unknown · unknown · Dec 24, 2023 · N925AT · Boeing 717200 · Escape Slide
  > DURING 1L DOOR (LT) SLIDE CHANGE, MAINTENANCE FOUND CONTAINER LANYARD ASSEMBLY CABLE FRAYED. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE INSTALLED A NEW LANYARD, PER AMDS CARD 256
- [SDR DALA2023110709164](https://openairdocs.org/sdr/DALA2023110709164.md): Unknown · unknown · Nov 6, 2023 · N925AT · Boeing 717200 · Emergency Lighting
  > THE EMERGENCY EXIT SIGN AT THE TAILCONE, FELL OFF. MAINTENANCE RESECURED THE LIGHT COVER AS REQUIRED. OK FOR SERVICE. (LP #4279682)
- [SDR DALA2023060704647](https://openairdocs.org/sdr/DALA2023060704647.md): Unknown · unknown · Jun 6, 2023 · N925AT · Boeing 717200 · Emergency Lighting
  > EXIT SIGN AT FRONT OF CABIN IS BROKEN OFF FROM THE CEILING AND IS HANGING BY THE WIRES. MAINTENANCE REPLACED THE FWD CABIN SIGN PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. AIRCRAFT IS OK FOR SERVICE. (LP #9962890)
- [SDR DALA2023032602319](https://openairdocs.org/sdr/DALA2023032602319.md): Unknown · unknown · Mar 25, 2023 · N925AT · Boeing 717200 · Standard Practices/Structures
  > SHIP 9574-ATB-DE/ENVIROMENTAL. PERFORMED AN AIR RETURN DUE TO A BIRD STRIKE TO THE RADOME AND LOSS OF WEATHER RADAR. CORRECTIVE ACTION: MAINTENANCE PERFORMED A BIRD STRIKE INSPECTION, REPLACED THE RADOME AND THE WEATHER RADAR DRIVE UNIT ASSEMBLY. (LP 4043168,4
- [SDR DALA2023031501887](https://openairdocs.org/sdr/DALA2023031501887.md): Unknown · unknown · Mar 14, 2023 · N925AT · Boeing 717200 · Fuel Storage
  > SHIP 9574 -ATB- THE FLIGHT CREW ACCOMPLISHED AN AIR TURN BACK AFTER THE CONTROL TOWER INFORMED THEM OF SOMETHING OBSERVED TRAILING THE AIRCRAFT. THE CREW CONFIRMED A 2000# FUEL IMBALANCE BETWEEN THE LEFT AND THE RIGHT WING TANK QUANTITIES. THE LANDING WAS UNEV
- [SDR DALA2022030201328](https://openairdocs.org/sdr/DALA2022030201328.md): None · none · Mar 1, 2022 · N925AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON UPPER AND LOWER SURFACE AT SEAT TRACK RH RBL=54 BTW STA=715 TO STA=737 AT CPAX REF NRC 202. SUMMARY OF NRC 00292: CORROSION LEVEL 2, SEAT TRACK RH RBL=54 BTW STA=715 TO STA=737 WAS REPAIRED PER B717-200 SRM. 53-20-52 -2R REPAIR 5 FIGURE 201. (LP #
- [SDR DALA2022030201327](https://openairdocs.org/sdr/DALA2022030201327.md): None · none · Mar 1, 2022 · N925AT · Boeing 717200 · Aerodynamic Fairings
  > THE FORWARD RETAINER CLIP, ON THE COVER ASSEMBLY AT THE TAILCONE SLIDE, WAS FOUND BROKEN DURING STEP 13 OF JIC 5352-4002. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY OF NRC 00286: A NEW C
- [SDR DALA2022022401205](https://openairdocs.org/sdr/DALA2022022401205.md): None · none · Feb 23, 2022 · N925AT · Boeing 717200 · Fuselage Floor Panel
  > CORROSION ON JAM BTW STA Y=370 TO Y=425 AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00075: CORROSION LEVEL 2, JAMB BTW STA Y=370 TO Y=425 AT FWD CARGO COMPARTMENT WAS REPAIRED PER B717 SRM 53-20-15 -2R. (LP #2132980)
- [SDR DALA2022022401204](https://openairdocs.org/sdr/DALA2022022401204.md): None · none · Feb 23, 2022 · N925AT · Boeing 717200 · Fuselage Floor Panel
  > CORROSION ON JAMB DOOR LOWER AREA AT AFT CARGO DOOR (C2). SUMMARY OF NRC 00030: CORROSION LEVEL 2, JAMB DOOR LOWER AREA AT AFT CARGO DOOR (C2) WAS REPAIRED PER B717 SRM 53-20-15-2R, REPAIR 7. (LP #2132801)

Next page: https://openairdocs.org/aircraft/N925AT/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 = 'N925AT' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N925AT/reports

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