# Service difficulty reports: N923AT

A list on [N923AT](https://openairdocs.org/aircraft/N923AT.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 · 102 reports

- [SDR DALA2026060903482](https://openairdocs.org/sdr/DALA2026060903482.md): Longeron · cracked · Jun 8, 2026 · N923AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CRACK LONGERONS NBR 2 RT/LT SIDES AT STA Y=1133 AT 12HRS POSITION AT AFT ACCESORY COMPARTMENT. CRACK LONGERONS NR 2 RT/LT SIDES AT STA Y=1133 AT 12HRS POSITION AT AFT ACCESORY COMPARTMENT WERE REPAIRED PER SRM 53-00-05-2R PROCEDURE 2, REPAIR 2 AND LOG PAGE N
- [SDR DALA2026060903481](https://openairdocs.org/sdr/DALA2026060903481.md): Skin · cracked · Jun 8, 2026 · N923AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > AIRCRAFT 9559, CRACK ON EXTERNAL SKIN STA Y= 1133 BTW PROJECTION LONG 2 RH TO LONG 3 RH AT AFT FUSELAGE SECTION. CORRECTIVE ACTION: CRACK ON EXTERNAL SKIN STA Y= 1133 BTW PROJECTION LONG 2 RH TO LONG 3 RH AT AFT FUSELAGE SECTION WAS REPAIRED PER PRI 634850-14
- [SDR DALA2026060903437](https://openairdocs.org/sdr/DALA2026060903437.md): Control Cable · low tension · Jun 4, 2026 · N923AT · Boeing 717200 · Leading Edge Slat Control System
  > IN REF TO AMDS 2780-2003: LOW TENSION ON EXTEND CONTROL CABLE OF SLAT 1 AT RIGHT WING. FINAL ADJUSTMENT OF THE EXTEND CONTROL CABLE (195A-B) AT SLAT 1 AT RIGHT WING WAS PERFORMED PER B717- 200 AMM 27-80-00 AND ADJUSTMENT OK (1630078) (AIRCRAFT GROUNDED)
- [SDR DALA2026020900915](https://openairdocs.org/sdr/DALA2026020900915.md): Battery Pack · inoperative · Feb 5, 2026 · N923AT · Boeing 717200 · Emergency Lighting
  > DURING SERVICE CHECK, FOUND EMERGENCY LIGHTS INOPERATIVE. R1 GALLEY OVERHEAD. REMOVED & REPLACED THE B5-259 BATTERY IAW AMM 33-51. (8406307)
- [SDR DALA2025121709201](https://openairdocs.org/sdr/DALA2025121709201.md): Skin · cracked · Dec 16, 2025 · N923AT · Boeing 717200 · Trailing Edge Flaps
  > LEFT FLAP TRAILING EDGE CRACK AND DELAMINATION. REPAIRED PER ER/A 631162-14. (8401817)
- [SDR DALA2025111808422](https://openairdocs.org/sdr/DALA2025111808422.md): None · none · Nov 13, 2025 · N923AT · Boeing 717200 · Standard Practices/Structures
  > DTA ER/A 618121-14 REV A SECTION I MONITOR LOG REQUIRES DTA STATE 3 APPROVAL ON OR BEFORE 82,000 TOTAL CYCLES. C/W ER/A 00-618121 (1304050).
- [SDR DALA2025071605343](https://openairdocs.org/sdr/DALA2025071605343.md): Longeron · damaged · Jul 15, 2025 · N923AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > AIRCRAFT 9559, LONGERON BETWEEN ST 256 & 275 DAMAGED. REMOVED DAMAGE SECTION OF LONGERON IAW B717 SRM 53-00-05-2R PRO 2. FABRICATED LONGERON AND HATS P717 SRM 53-00-05-2R PROCEDURE 2. PERFORMED BHEC OF REMOVED FASTENERS IAW B717 NDT SPM PART 6, 06-10-01.003
- [SDR DALA2024122712035](https://openairdocs.org/sdr/DALA2024122712035.md): Battery Pack · inoperative · Dec 25, 2024 · N923AT · Boeing 717200 · Emergency Lighting
  > THE FOUR LOWER OVERWING EXIT LIGHTS, LEFT AND RIGHT, ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND BATTERY R5-119 PER B717 AMM 33-51-03. SYSTEM NOW OPERATIONALLY CHECKS GOOD. THE AIRCRAFT IS OK FOR SERVICE. (LP #6976208)
- [SDR DALA2024061306057](https://openairdocs.org/sdr/DALA2024061306057.md): Beam · cracked · Jun 7, 2024 · N923AT · Boeing 717200 · Fuselage Main, Bulkhead
  > CRACKS ON INTERNAL BEAM #1 AT AFT CABIN BULKHEAD DOOR (CPAX). SUMMARY OF NRC 00356: INTERNAL BEAM #1 (UPPER WEB) AT AFT CABIN BULKHEAD DOOR (CPAX) WAS FABRICATED AND REPLACED PER DWG 9915565 REV BD, B717-200 SRM 51-41-01-0G, 51-41-02-0G, AND 51-41-05-0G. (LP #
- [SDR DALA2024053105689](https://openairdocs.org/sdr/DALA2024053105689.md): Fuel Tank · corroded · May 30, 2024 · N923AT · Boeing 717200 · Fuel Storage
  > -AD- CORROSION ON THE LOWER SKIN OF THE CENTRAL TANK APPROX STA Y=748 AND STA XCW=-25 AND Z=-29 IN THE FRONT WALL ON RH MLG WHEEL WELL. SUMMARY OF NRC 00777: LOWER SKIN OF THE CENTRAL TANK APPROX STA Y=748 AND STA XCW=-25 AND Z=-29 IN THE FRONT WALL ON RH MLG
- [SDR DALA2024051605255](https://openairdocs.org/sdr/DALA2024051605255.md): Attach Fitting · corroded · May 14, 2024 · N923AT · Boeing 717200 · Fuselage, Landing Gear Attach Fittings
  > RUSTED ON LUG AT ATTACH FIXED STRUT, ALSO ON FITTING TO RH LANDING GEAR. SUMMARY OF NRC 00731: RUSTED ON FITTING TO RH LANDING GEAR WAS REMOVED PER BOEING OM 57-40-1 REPAIR PAR 2 G (6) (B), (UT) THICKNESS MEASUREMENT WAS ACCOMPLISHED ON FITTING TO RH LANDING G
- [SDR DALA2024051405170](https://openairdocs.org/sdr/DALA2024051405170.md): Jackscrew · nicked · May 10, 2024 · N923AT · Boeing 717200 · Stabilizer Actuator
  > -AD- A NICK WAS FOUND ON THREAD OF THE ACME SCREW AT THE HORIZONTAL STAB. SUMMARY OF NRC 00485: HORIZONTAL STABILIZER ACTUATOR JACKSCREW ASSY WAS REPLACED FOR SERVICEABLE ACTUATOR JACKSCREW. WAS INSTALLED PER B717 AMM 27-41-04 AND TESTED OK. ALSO, TRIM GEARBOX
- [SDR DALA2024050204889](https://openairdocs.org/sdr/DALA2024050204889.md): Not Reported · scratched · May 1, 2024 · N923AT · Boeing 717200 · Horizontal Stabilizer Miscellaneous Structure
  > -AD- SCRATCHES WERE FOUND AT FWD/LH BARREL NUT HOLE HORIZONTAL STABILIZER. SUMMARY OF NRC 00666: FWD/LH BARREL NUT HOLE HORIZONTAL STABILIZER (HOLE #19) WAS REPAIRED PER PRI 617393-14 REV 1 AND ER/A 617393AD REV ORIG SECTION I: PERMANENT REPAIR. REPAIR APPROVA
- [SDR DALA2024042604728](https://openairdocs.org/sdr/DALA2024042604728.md): Pan · cracked · Apr 26, 2024 · N923AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACKS WERE FOUND ON PAN, BTW BEAMS 3/4 AND AFT SIDE AT AFT CARGO DOOR (C2). SUMMARY OF NRC 00348: AFT INNER PAN ON BEAM #3 AND BEAM #4 AT AFT CARGO COMPARTMENT DOOR WAS REPAIRED PER ER/A 617066-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 617066-14 REV
- [SDR DALA2024050104837](https://openairdocs.org/sdr/DALA2024050104837.md): None · none · Apr 25, 2024 · N923AT · Boeing 717200 · Standard Practices/Structures
  > -AD- AMOC ER/A 617393-14AD MONITOR LOG REQUIRES DTA WITH NEW AMOC ON OR BEFORE THE NEXT 24 MONTHS AFTER 25-APR-2024. CONTACT LIAISON ENGINEERING, DEPT 555 FOR RESULTS. NOTE TO MONITOR RECORDS / PLANNING. DISCONTINUE REVENUE SERVICE ON OR BEFORE THE NEXT 24 M
- [SDR DALA2024050104836](https://openairdocs.org/sdr/DALA2024050104836.md): None · none · Apr 25, 2024 · N923AT · Boeing 717200 · Standard Practices/Structures
  > -AD- DTA ER/A 616393-14AD MONITOR LOG REQUIRES DTA APPROVAL ON OR BEFORE THE NEXT 24 MONTHS AFTER 25-APR-2024. CONTACT LIAISON ENGINEERING, DEPT 555 FOR RESULTS. NOTE TO MONITOR RECORDS / PLANNING. DISCONTINUE REVENUE SERVICE ON OR BEFORE THE NEXT 24 MONTHS
- [SDR DALA2024042404673](https://openairdocs.org/sdr/DALA2024042404673.md): Skin · cracked · Apr 23, 2024 · N923AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACK ON FUSELAGE SKIN BTW STA 1078 AND LONGERON 14R. SUMMARY OF NRC 00041: FUSELAGE SKIN BTW STA 1078 AND LONGERON 14R WAS REPAIRED PER ERA 617080-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ACCOMPLISH REPETITIVE INSPECTIONS WITHIN EVERY 24 MONTHS AFTER ACCO
- [SDR DALA2024041904566](https://openairdocs.org/sdr/DALA2024041904566.md): Diaphragm · cracked · Apr 18, 2024 · N923AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON DIAPHRAGM BTW STA Y=171 TO STA Y=172 AND -X56 APPROX AT CABIN PAX (W1). SUMMARY OF NRC 00689: DIAPHRAGM BTW STA Y=171 TO STA Y=172 AND -X56 APPROX AT CABIN PAX WAS REPAIRED PER B717-200 SRM 51-70-10- 2R REPAIR 2 FIG 201. (LP #0300282)
- [SDR DALA2024041804533](https://openairdocs.org/sdr/DALA2024041804533.md): Cusp Web · corroded · Apr 17, 2024 · N923AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON CUSP WEB BTW STA Y=396 AND Y=401, BTW STA Y=416 AND Y=420, BTW STA Y=429 AND Y=434, AND BTW STA Y=459 AND Y=462 X-56 (IN REFERENCE TO NRC 00542). SUMMARY OF NRC 00661: CORROSION LEVEL 2. CUSP WEB BTW STA Y=396 AND Y=401, BTW STA Y=416 AND Y=420, B
- [SDR DALA2024041804529](https://openairdocs.org/sdr/DALA2024041804529.md): Beam · cracked · Apr 16, 2024 · N923AT · Boeing 717200 · Cargo/Baggage Doors
  > CRACKS ON FWD PANE BEAM 1 OF LOWER CORNER AT FWD CARGO DOOR. SUMMARY OF NRC 00245: FWD PANE BEAM 1 OF LOWER CORNER AT FWD CARGO DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1. (LP #0296713)
- [SDR DALA2024041804528](https://openairdocs.org/sdr/DALA2024041804528.md): Beam · cracked · Apr 16, 2024 · N923AT · Boeing 717200 · Cargo/Baggage Doors
  > CRACKS 2 EA ON FWD PANE BEAM 5 AT FWD CARGO DOOR. SUMMARY OF NRC 00243: FWD PANE BEAM 5 AT FWD CARGO DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1. (LP #0296705)
- [SDR DALA2024041504428](https://openairdocs.org/sdr/DALA2024041504428.md): Beam · cracked · Apr 13, 2024 · N923AT · Boeing 717200 · Fuselage Main, Structure
  > CRACKS ON FWD PANE BEAM 3 AT FWD CARGO DOOR. SUMMARY OF NRC 00244: FWD PANE BEAM 3 AT FWD CARGO DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1. (LP #0292323)
- [SDR DALA2024041204363](https://openairdocs.org/sdr/DALA2024041204363.md): Beam · cracked · Apr 12, 2024 · N923AT · Boeing 717200 · Fuselage Main, Structure
  > CRACK ON BEAM #1 STA 161 AND STA 197 AT PASSENGER ENTRANCE DOOR (L1). SUMMARY OF NRC 00216: DAMAGED SECTIONS (STA 161 AND STA 197) OF BEAM #1 AT PASSENGER ENTRANCE DOOR WERE REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 7, REPAIR 7, FIG 201 AND FIG 202. (LP
- [SDR DALA2024041204359](https://openairdocs.org/sdr/DALA2024041204359.md): Web · cracked · Apr 11, 2024 · N923AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON OUT WEB AREA STA 674 PROYECTION L 14L AT LH FWD EMERGENCY DOOR. SUMMARY OF NRC 00252: OUTER WEB AREA STA 674 PROYECTION L 14L AT LH FWD EMERGENCY DOOR WAS REPAIRED PER B717-200 SRM 52-20-02-2R REPAIR 1. (LP #0288528)
- [SDR DALA2024041204358](https://openairdocs.org/sdr/DALA2024041204358.md): Beam · cracked · Apr 11, 2024 · N923AT · Boeing 717200 · Fuselage Main, Structure
  > CRACK ON AFT PANE BEAM 5 AT FWD CARGO DOOR. SUMMARY OF NRC 00242: AFT PANE BEAM 5 AT FWD CARGO DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1. (LP #0287685)
- [SDR DALA2023091407542](https://openairdocs.org/sdr/DALA2023091407542.md): Unknown · unknown · Sep 13, 2023 · N923AT · Boeing 717200 · Fuselage Internal Mounting Structure
  > AFT CARGO SLANT PANEL DAMAGED LT SIDE FWD OF CARGO DOOR. REMOVED SLANT FLOOR PANEL PER B717 AMM 25-58. FABRICATED AND INSTALLED PANEL PER ER/A 612079-14 REV 0 SECTION I PERMANENT REPAIR. OK FOR SVC. (LP #4095470)
- [SDR DALA2023070305306](https://openairdocs.org/sdr/DALA2023070305306.md): Unknown · unknown · Jul 2, 2023 · N923AT · Boeing 717200 · Emergency Lighting
  > SEVERAL EMERGENCY LIGHTS IN THE CABIN COMPARTMENT ARE INOPERATIVE OR DIE IN LESS THAN 30 SECONDS AT TAXI. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK REF B717 AMM 33-51. BATTERY PACK LOCATIONS REPLACED ARE B5-116, -227, -120, -230, AND -231. OPERATIO
- [SDR DALA2022100406444](https://openairdocs.org/sdr/DALA2022100406444.md): None · none · Oct 2, 2022 · N923AT · Boeing 717200 · Hydraulic System, Main
  > SHIP 9559 - DE/HYD - THE CREW DECLARED AN EMERGENCY ON DESCENT FOR LANDING DUE TO THE RIGHT HYDRAULIC SYSTEM FLUID LOSS. THE ALTERNATE LANDING GEAR EXTENSION PROCEDURES WERE COMPLIED WITH AS PER THE QRH. THE LANDING WAS UNEVENTFUL EXCEPT FOR THE MAIN LANDING G
- [SDR DALA2022030901526](https://openairdocs.org/sdr/DALA2022030901526.md): None · none · Mar 4, 2022 · N923AT · Boeing 717200 · Emergency Lighting
  > DURING THE EMERGENCY LIGHT CHECK ON A SERVICE CHECK, MAINTENANCE FOUND THE LEFT AND RIGHT OVER WING EVACUATION LIGHTS TO BE INOPERATIVE. SUMMARY SEE NRC 053-0001:0514-2001/006 00431: MAINTENANCE REPLACED THE OVER WING EMERGENCY EVACUATION BATTERY POWER SUPPLY
- [SDR DALA2022030201330](https://openairdocs.org/sdr/DALA2022030201330.md): None · none · Mar 2, 2022 · N923AT · Boeing 717200 · Escape Slide
  > THE TAILCONE RELEASE LANYARD IS WORN. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY SEE NRC 001-0138:5352-4002/001 00429: REPLACED LANYARD REF B717 AMM 53-52-01 AND RIG TO BE ACCOMPLISHED O
- [SDR DALA2022030201326](https://openairdocs.org/sdr/DALA2022030201326.md): None · none · Mar 1, 2022 · N923AT · Boeing 717200 · Fuselage Floor Panel
  > SUPPLEMENTAL INFORMATION: 001-0210:5300-1001/001 00403 INSTALLED FWD CARGO, LOWER DOOR PAN PER B717 SRM 53-20-15-2R PROCEDURE 6. CORROSION LEVEL CLASSIFIED AS LVL 1. CLOSING REQUIREMENTS RII: INSPECTOR 00899097. FORWARD CARGO COMPARTMENT, LOWER DOOR JAM HAS MU
- [SDR DALA2022021701036](https://openairdocs.org/sdr/DALA2022021701036.md): None · none · Feb 16, 2022 · N923AT · Boeing 717200 · Landing Gear Selector
  > SHIP 9559 - THE CREW DIVERTED THE AIRCRAFT TO LAX DUE TO ALL THREE GEAR NOT RETRACTING WHEN SELECTED. CORRECTIVE ACTION: MAINTENANCE FOUND THAT THE GEAR HANDLE WAS DIFFICULT TO OPERATE. THE GEAR WAS CLEANED AND FUNCTIONALLY CHECKED ON JACKS SEVERAL TIMES WITHO
- [SDR DALA2019062003670](https://openairdocs.org/sdr/DALA2019062003670.md): Lens · missing · Jun 20, 2019 · N923AT · Boeing 717200 · Emergency Lighting
  > THE AFT DOOR EMERGENCY LIGHT LESN MISSING. MAINTENANCE REPLACED THE LENS IAW B717 AMM 33-51.
- [SDR 2019F00197](https://openairdocs.org/sdr/2019F00197.md): Spoiler · delaminated · Apr 30, 2019 · N923AT · Boeing 717200 · Spoilers
  > RT WING SPOILER DELAMINATED.
- [SDR DALA2024010500204](https://openairdocs.org/sdr/DALA2024010500204.md): Unknown · unknown · Apr 26, 2019 · N923AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN DAMAGE AFT OF R1 DOOR. CUTOUT DAMAGED SECTION OF SKIN APPROX. 3" X 7.4" PER B717 SRM 53-03-01-2R-1 REPAIR 1. CUTOUT CONTAINMENT ACCOMPLISHED PER NDTSPM 06-10-01.001 QC2018. FABRICATED & ROLLED NEW DOUBLER. COUNTERSUNK, DEBURRED, TREATED, & PRIMED
- [SDR DALA2019042202555](https://openairdocs.org/sdr/DALA2019042202555.md): Battery Pack · inoperative · Apr 21, 2019 · N923AT · Boeing 717200 · Emergency Lighting
  > THE EMERGENCY LIGHTS AT STA 389 ARE INOPERATIVE. MAINTENANCE INSTALLED A SERVICEABLE BATTERY PACK PER B717 AMM 33-51-03. (LP #5456807)
- [SDR DALA2018091005512](https://openairdocs.org/sdr/DALA2018091005512.md): Battery Pack · discharged · Sep 7, 2018 · N923AT · Boeing 717200 · Emergency Lighting
  > LOWER OVERWING EXIT SIGNS ARE INOPERATIVE DURING EEPLS TEST. MAINTENANCE REPLACED THE BATTERY PACK B5-119. CHECK IS OK REF AMM 33-51.
- [SDR DALA2018082205204](https://openairdocs.org/sdr/DALA2018082205204.md): Battery Pack · inoperative · Aug 21, 2018 · N923AT · Boeing 717200 · Emergency Lighting
  > DURING A SERVICE CHECK, MAINTENANCE THE FOUND L1 AND R1 DOOR EMERGENCY EXIT LIGHTS TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY EXIT LIGHT BATTERY IAW AMM 33-55. OPS CHECKED GOOD.
- [SDR DALA2018073104780](https://openairdocs.org/sdr/DALA2018073104780.md): Battery Pack · discharged · Jul 27, 2018 · N923AT · Boeing 717200 · Emergency Lighting
  > MULTIPLE CABIN EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED BATTERY PACKS B5-121 AND B5-235 REF AMM 33-51. OPERATIONAL CHECK IS GOOD.
- [SDR DALA2017082306343](https://openairdocs.org/sdr/DALA2017082306343.md): Battery Pack · inoperative · Aug 23, 2017 · N923AT · Boeing 717200 · Emergency Lighting
  > THE EMERGENCY EXIT LIGHTS AT THE FORWARD DROP CEILING, EXIT IDENTIFIER IN FIRST CLASS CABIN AND THE SERVICE DOOR OVERHEAD LIGHT ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY B5-529 IAW AMM 33-51. ALL CHECKED GOOD.
- [SDR DALA2017071305389](https://openairdocs.org/sdr/DALA2017071305389.md): Lens · missing · Jul 12, 2017 · N923AT · Boeing 717200 · Emergency Lighting
  > EMERGENCY LIGHT LENS MISSING. INSTALLED THE LIGHT LENS.
- [SDR DALA2017042603395](https://openairdocs.org/sdr/DALA2017042603395.md): Lamp · inoperative · Apr 26, 2017 · N923AT · Boeing 717200 · Emergency Lighting
  > FOUND LT EMERGENCY LIGHT INOP. REPLACED THE LAMPS IAW AMM 33-51. OPS CHECKED GOOD. ACFT IS GOOD FOR SERVICE.
- [SDR DALA2017021501229](https://openairdocs.org/sdr/DALA2017021501229.md): Skin · cracked · Feb 14, 2017 · N923AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > SKIN CRACKED BS 1133 OTDB OF LONGERON2L. REPAIRED THE SKIN IAW ER/A 553669-14AD REV 0.
- [SDR DALA2017021501266](https://openairdocs.org/sdr/DALA2017021501266.md): Skin · corroded · Feb 13, 2017 · N923AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > FORWARD CARGO HAS CORROSION ON SKIN INBOARD OF LONGERON 28L BETWEEN STA 636 AND STA 655. REMOVED CORRODED INTERNAL DOUBLER AND INSTALLED NEW INTERNAL DOUBLER BETWEEN STATIONS 636 AND 655 IAW SRM 51-41-02 AND 51-41-05 AND DWG 5940882.
- [SDR DALA2017021501267](https://openairdocs.org/sdr/DALA2017021501267.md): Door · corroded · Feb 9, 2017 · N923AT · Boeing 717200 · Entrance Stairs
  > L1 PASSENGER DOOR AIRSTAIR DOOR HAS CORROSION IN FORWARD AND AFT LOWER CORNERS AND AROUND AND INCLUDING NUT CLIPS AND GOUGES IN LOWER FLANGE. INSTALLED NEW AIRSTAIR DOOR IAW AMM 52-63-01 420-801, AND SRM 51-40-02, 51-40-04.
- [SDR DALA2017020801035](https://openairdocs.org/sdr/DALA2017020801035.md): Seat Track · corroded · Feb 7, 2017 · N923AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK RBL 44.5 IS CORRODED AND GOUGED IN SEVERAL AREAS FROM BS 900 - 986. BLENDED AND FOUND TO BE OUT OF LIMITS IAW SRM 51-30-07 FIG 18, 53-00-00-1A. LOCATED AND DRILLED REPLACEMENT SEAT TRACK IAW SRM 51-40-08, INSTALLED IAW SRM 53-20-52-2R-5, 51-41-01, 5
- [SDR DALA2017020801034](https://openairdocs.org/sdr/DALA2017020801034.md): Frame · cracked · Feb 7, 2017 · N923AT · Boeing 717200 · Fuselage Main, Frame
  > BS 1022 BULKHEAD REAR FRAME ANGLE IS CRACKED STRINGER 7L, VERIFIED WITH HFEC. REPAIRED IAW SRM 51-70-11 REPAIR 1.
- [SDR DALA2017020901078](https://openairdocs.org/sdr/DALA2017020901078.md): Cusp Web · cracked · Feb 3, 2017 · N923AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > UPPER CABIN CUSP WEB FOUND CRACKED AT STA 832 LBL 58. UPPER CABIN CUSP WEB CRACK REPAIRED IAW SRM 53-00-55-R2-4. REMOVED AND INSTALLED SEAT TRACK TO ACCESS, IAW SRM 51-40-04-06. ALODINED AND PRIMED AREA, IAW SRM 51-10-04 PG 10. 17-21. CUSP REPAIR PERFORMED AT
- [SDR DALA2017020601004](https://openairdocs.org/sdr/DALA2017020601004.md): Seat Track · corroded · Feb 3, 2017 · N923AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT CENTER SEAT TRACK STA 556-656 RBL 44.5 HAS CORROSION AND NEED PAINT TOUCHED UP. REPAIRED SEAT TRACK SECTION RBL 44.5 BETWEEN STA 581-644 BLENDED OUT OF LIMITS IN SEVERAL AREA'S.048 MAT LOSS FROM.100 ORG IAW B717 SRM 53-20-52 FIG 101 & REPAIR 5/7001.
- [SDR DALA2017020601003](https://openairdocs.org/sdr/DALA2017020601003.md): Seat Track · corroded · Feb 3, 2017 · N923AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT CENTER SEAT TRACK HAS AREAS OF CORROSION, GOUGING, AND AREAS OF MISSING PRIMER AND TOPCOAT FROM STA 556 TO STA 656. REPAIRED SEAT TRACK SECTION 44.5 BETWEEN STA 533-646 BLENDED TRACK OUT OF LIMITS MAT LOSS WAS.050 FROM.100 ORIGINAL TAG 2736 IAW SRM 53-2

Next page: https://openairdocs.org/aircraft/N923AT/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 = 'N923AT' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N923AT/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.