# Service difficulty reports: N920AT

A list on [N920AT](https://openairdocs.org/aircraft/N920AT.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 · 144 reports

- [SDR DALA2026101205599](https://openairdocs.org/sdr/DALA2026101205599.md): Skin · mechanic error · Oct 9, 2026 · N920AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > DRILL START INDENTATIONS AT CABIN CEILING BS 927, BTWN STRINGER 3R & 4R. REPAIRED PER ER/A 637414-14. (1856706) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026100905576](https://openairdocs.org/sdr/DALA2026100905576.md): Frame · damaged · Oct 9, 2026 · N920AT · Boeing 717200 · Fuselage Main, Frame
  > FOUND TOOLING DAMAGE ON FUSELAGE FRAME Y908, STR 2R-3R, COMPLIED WITH ER/A 637401-14. (1855981) (AICRAFT GROUNDED).
- [SDR DALA2026100905575](https://openairdocs.org/sdr/DALA2026100905575.md): Frame · damaged · Oct 9, 2026 · N920AT · Boeing 717200 · Fuselage Main, Frame
  > FOUND TOOLING DAMAGE ON FUSELAGE FRAME Y927 BETWEEN STRG L3R TO L4R, ADDITIONAL ENGINEERING AUTHORIZATION ER/A REVISION IS REQUIRED. (1855903) (AICRAFT GROUNDED).
- [SDR DALA2026082404797](https://openairdocs.org/sdr/DALA2026082404797.md): Pcdu · faulted · Aug 23, 2026 · N920AT · Boeing 717200 · Electrical Power System
  > MISC/DE- DECLARED AN EMERGENCY DUE TO RIGHT DC BUSS OFF MESSAGE WITH NUMEROUS FAULTS. REPLACED RT PCDU IAW AMM 24-21. OPS CHECK NORMAL. (9197048) (AIRCRAFT GROUNDED).
- [SDR DALA2026020200758](https://openairdocs.org/sdr/DALA2026020200758.md): Radio · odor · Jan 28, 2026 · N920AT · Boeing 717200 · Communications System
  > OOD SMELL IN FWD LAV AND EMERG EQUIP DOOR TO RIGHT OF LAV. ODOR LIKE A HOT ELECTRIC MOTOR OR ARMATURE. VERY FAINT ODOR BUT SEVERAL CREW MEMBERS SMELLED IT. FWD LAV AREA. REPLACED PRIMARY RADIO RACK FAN IAW AMM 21-21-01. FAN OPS NORM. ODOR HAS DISSAPATED. (838
- [SDR DALA2025122909459](https://openairdocs.org/sdr/DALA2025122909459.md): Release Mech · out of adjust · Dec 21, 2025 · N920AT · Boeing 717200 · Aerodynamic Fairings
  > FOUND TAIL CONE RELEASE MECHANISM CAM CLOCKED WRONG. TAILCONE RELEASE MECHANISM CAM REF B717 AMM 53-52-03 (1362721)
- [SDR DALA2025122909452](https://openairdocs.org/sdr/DALA2025122909452.md): None · none · Dec 19, 2025 · N920AT · Boeing 717200 · Standard Practices/Structures
  > ERA 631006-14.: DAMAGE TOLERANCE EVALUATION IS REQUIRED IN ACCORDANCE WITH PROCEDURES ESTABLISHED IN FAA ADVISORY CIRCULAR 120-93. ASSOCIATED ER/A 00-631006 (1359454)
- [SDR DALA2025121509136](https://openairdocs.org/sdr/DALA2025121509136.md): Skin · damaged · Dec 11, 2025 · N920AT · Boeing 717200 · Wing, Plate/Skin
  > FUEL LEAK FOUND DURING INSPECTION OF THE RH WING AFT LOWER SKIN STA 164. REPAIRED PER ERA 629782-14AD (1346873)
- [SDR DALA2025121509134](https://openairdocs.org/sdr/DALA2025121509134.md): Spar · damaged · Dec 10, 2025 · N920AT · Boeing 717200 · Wing Spar
  > ER/A 629782-14. REPAIR AT RH REAR SPAR AT XRS 164. C/W WITH ER/A 629782-14. (1345202)
- [SDR DALA2025121509133](https://openairdocs.org/sdr/DALA2025121509133.md): Spar · damaged · Dec 10, 2025 · N920AT · Boeing 717200 · Wing Spar
  > ER/A 629782-14AD REV ORIGINAL. REPAIR TO RH WING REAR SPAR AT XRS 164. REPAIRED PER ER/A 14-629782. (1345195)
- [SDR DALA2025121009018](https://openairdocs.org/sdr/DALA2025121009018.md): Doubler · corroded · Dec 4, 2025 · N920AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > AFT CARGO CORROSION - INTERNAL DOUBLER STR 23R STA 1022 CORRODED. REPAIRED COMPLIED WITH ER/A 630153-14 REV. ORIG. (1335432)
- [SDR DALA2025120808964](https://openairdocs.org/sdr/DALA2025120808964.md): Scuff Plate · cracked · Nov 29, 2025 · N920AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > AFT CARGO SCUFF PLATE CRACKED. REPLACED JAMB PAN ON NR 408 IAW LOG 1325090. (1327367)
- [SDR DALA2025120808963](https://openairdocs.org/sdr/DALA2025120808963.md): Pan · corroded · Nov 27, 2025 · N920AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > AFT CARGO: C-2 DOOR THRESHOLD PAN CORRODED. REPLACED REPAIR AFT CARGO DOOR LOWER JAMB PAN IAW SRM 53-20-15-2R, PROCEDURE 7, REPAIR 7. AFT CARGO DOOR LOWER JAMB PAN CORROSION SPLICE REPAIR. (1325090)
- [SDR DALA2025120108776](https://openairdocs.org/sdr/DALA2025120108776.md): None · none · Nov 27, 2025 · N920AT · Boeing 717200 · Standard Practices/Structures
  > REPETITIVE INSP PER SECT II. OF ERA 630153-14 REV ORIGINAL. C/W ER/A630153-14 REV ORIGINAL. (1324948)
- [SDR DALA2025111908464](https://openairdocs.org/sdr/DALA2025111908464.md): Stringer Fitting · corroded · Nov 18, 2025 · N920AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > AFT CARGO P/R: STRINGER END FITTING MARKED FS1053 28R IS CORRODED. REPLACED AFT END FITTING LONGERON 28R PER B717 DWG 5910228 (1310506)
- [SDR DALA2025111908463](https://openairdocs.org/sdr/DALA2025111908463.md): Longeron Splice · corroded · Nov 18, 2025 · N920AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > AFT CARGO BAY BS 1002 L25R END SPLICE CORRODED. REPLACED LONGERON 25R AND FWD END FITTING REF: DACDWG 5919707-521 (1310504)
- [SDR DALA2025111808440](https://openairdocs.org/sdr/DALA2025111808440.md): Threshold · corroded · Nov 12, 2025 · N920AT · Boeing 717200 · Fuselage Main, Structure
  > C1 DOOR THRESHOLD: LIGHT SURFACE CORROSION IN DOOR SILL AREA. REPLACED REPAIRED FORWARD CARGO DOOR LOWER JAMB PAN REF: B717-200 SRM 53-20-15-2R (1300666).
- [SDR DALA2025090906665](https://openairdocs.org/sdr/DALA2025090906665.md): Access Panel · mechanic error · Sep 2, 2025 · N920AT · Boeing 717200 · Wing, Plate/Skin
  > LEFT WING OUTER, LOWER SURFACE, ACCESS COVER SETTLEMENT AREA, XRS=383-414, MISDRILLED HOLE. ACCOMPLISH ER/A 611899-14 (1178468)
- [SDR DALA2025040802705](https://openairdocs.org/sdr/DALA2025040802705.md): Lens · missing · Apr 7, 2025 · N920AT · Boeing 717200 · Emergency Lighting
  > THE OVERHEAD EMERGENCY LIGHT LENS AT 24L IS MISSING. MAINTENANCE REPLACED LENS IAW B717 AMM 33-51-08. (LP #6963274)
- [SDR DALA2025021801198](https://openairdocs.org/sdr/DALA2025021801198.md): Autopilot Sys · failed · Feb 16, 2025 · N920AT · Boeing 717200 · Autopilot System
  > SHIP 9578 -DIV/DE- THE CREW DECLARED AN EMERGENCY WITH ATC AND DIVERTED THE AIRCRAFT TO JAX (VFR) DUE TO LOSS OF AUTOPILOT AND LATERAL ROLL MODE GUIDANCE ON APPROACH FOR LANDING AT ATL (IMC). CORRECTIVE ACTION: MAINTENANCE REPLACED THE GLARE SHIELD CONTROL PAN
- [SDR DALA2023110709163](https://openairdocs.org/sdr/DALA2023110709163.md): Unknown · unknown · Nov 7, 2023 · N920AT · Boeing 717200 · Emergency Lighting
  > ON WALK AROUND DURING THE SERVICE CHECK, MAINTENANCE FOUND THAT THE AFT RIGHT HAND EXTERIOR EMERGENCY LIGHT STAYS ON AT ALL TIMES. MAINTENANCE REPLACED RELAY R2-273 PER B717 SWPM CHAPTER 20-25 AND REPLACED THE OVERWING EMERGENCY LIGHT BATTERY PACK AND CHARGER
- [SDR DALA2023101808565](https://openairdocs.org/sdr/DALA2023101808565.md): Unknown · unknown · Oct 17, 2023 · N920AT · Boeing 717200 · Trailing Edge Flaps
  > DENTS ON INB SURFACE AFT MOVABLE FLAP VANE AT LH WING. SUMMARY OF NRC 00098: INBOARD SURFACE OF AFT MOVABLE FLAP VANE (LH WING) WAS REPAIRED PER ER/A 612278-14 REV. ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-612278 ADDED FOR AC 9578. (LP #0021458
- [SDR DALA2023101408447](https://openairdocs.org/sdr/DALA2023101408447.md): Unknown · unknown · Oct 14, 2023 · N920AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTAL BTW STA 1022-1037 AND LONGERON 30, AFT CARGO COMPARTMENT. SUMMARY OF NRC 00708: CORROSION LEVEL 2. INTERCOSTAL BTW STA 1022-1037 AND LONGERON 30, AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP #001
- [SDR DALA2023101408439](https://openairdocs.org/sdr/DALA2023101408439.md): Unknown · unknown · Oct 11, 2023 · N920AT · Boeing 717200 · Wing, Plate/Skin
  > IN REF AMDS: 2040-0009: OPEN LEFT WING, FUEL TANK ZONE 520, DURING REMOVED ACCESS PLATE NBR 520 MB; CUT OUT SKIN OF FUEL ACCESS PLATE 520MB WAS DRILLED AT LH WING. SUMMARY OF NRC 00104: CUT OUT SKIN OF FUEL ACCESS PLATE 520MB WAS REPAIRED PER SECTION I: TIME L
- [SDR DALA2023101408436](https://openairdocs.org/sdr/DALA2023101408436.md): Unknown · unknown · Oct 11, 2023 · N920AT · Boeing 717200 · Fuselage Main, Structure
  > CORROSION ON PAN OF PASSENGER DOOR JAMB (EXTERNAL/INTERNAL SURFACE) BTW STA Y=200 AND PROJECT LONG 18L AT PAX CABIN. SUMMARY OF NRC 00236: CORROSION LEVEL 2. PAN OF PASSENGER DOOR JAMB (EXTERNAL/INTERNAL SURFACE) BTW STA Y=200 AND PROJECT LONG 18L AT PAX CABIN
- [SDR DALA2023101408435](https://openairdocs.org/sdr/DALA2023101408435.md): Unknown · unknown · Oct 11, 2023 · N920AT · Boeing 717200 · Fuselage Main, Bulkhead
  > CORROSION ON CHORD ANGLE AT AFT FUSELAGE PRESSURE BULKHEAD LOWER AREA STA Y=1053 BTW LONG 27LH-27RH AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00230: CORROSION LEVEL 2. CHORD ANGLE AT AFT FUSELAGE PRESSURE BULKHEAD LOWER AREA STA Y=1053 BTW LONG 28LH-28RH A
- [SDR DALA2023101008308](https://openairdocs.org/sdr/DALA2023101008308.md): Unknown · unknown · Oct 9, 2023 · N920AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CORROSION ON L30 BTW STA 908 TO STA 950 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00578: CORROSION LEVEL 2. LONGERON SECTION OF L30 BTW STA 908 TO STA 950 AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G PAR 8. (LP #0009610)
- [SDR DALA2023101008305](https://openairdocs.org/sdr/DALA2023101008305.md): Unknown · unknown · Oct 8, 2023 · N920AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ALONG OF TIE TRACK STA 954 TO 1022 LONGERON 28LH AT AFT CARGO IN REF NRC 213. SUMMARY OF NRC 00625: CORROSION LEVEL 2. TIE TRACK STA 954 TO 1022 LONGERON 28LH AT AFT CARGO WAS REPLACED PER DWG 5936663 REV Y AND PER B717-200 SRM 51-41-01-0G. (LP #0007
- [SDR DALA2023101008306](https://openairdocs.org/sdr/DALA2023101008306.md): Unknown · unknown · Oct 7, 2023 · N920AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON INTERCOSTAL STA 1223 CANT 12 O'CLOCK POSITION AT AFT ACCESORY COMPARMENT. SUMMARY OF NRC 00251: RUDDER STOP SPRING RH (1 EA) WAS REMOVED AND INSTALLED PER B717-200 AMM 27-26-03 AND ANGLE BRACKET AND INTERCOSTAL WERE REPLACED PER B717 SRM 51-41-02-0G.
- [SDR DALA2023100608224](https://openairdocs.org/sdr/DALA2023100608224.md): Unknown · unknown · Oct 5, 2023 · N920AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK X 56 ON STA: Y=332 TO Y=333 ORIGINAL T. SUMMARY OF NRC 00428: CORROSION LEVEL 2. SEAT TRACK X=56R BTW STA Y=218 AND STA Y=334 WAS REPLACED PER DWG 5930547 AND PER B-717 SRM 51-41-01-0G. (LP #0003244)
- [SDR DALA2023100608223](https://openairdocs.org/sdr/DALA2023100608223.md): Unknown · unknown · Oct 5, 2023 · N920AT · Boeing 717200 · Fuselage Main, Structure
  > CRACK ON BEAM 6 UNDER THE MECHANISM DOOR AT PASSENGER DOOR (L1). SUMMARY OF NRC 00296: BEAM 6 UNDER THE MECHANISM DOOR AT PASSENGER DOOR WAS REPAIRED PER B717-200 SRM 51-70-11-2R PROCEDURE 1 REPAIR 1. (LP #0002773)
- [SDR DALA2023100608220](https://openairdocs.org/sdr/DALA2023100608220.md): Unknown · unknown · Oct 4, 2023 · N920AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CORROSION ON FWD REPAIR DOUBLER SPLICE ON AFT CARGO DOOR JAMB. CORROSION LEVEL 2. REPAIR DOUBLER SPLICES (2 EA) WERE REPLACED PER SRM 53-20-15-2R PROCEDURE 7 REPAIR 7. (LP #0001412)
- [SDR DALA2023100408157](https://openairdocs.org/sdr/DALA2023100408157.md): Unknown · unknown · Oct 3, 2023 · N920AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK ON FRAME STA Y=1037 BTW LONGERON L15 - L17 AT PAX CABIN. SUMMARY OF NRC 00441: FRAME STA Y=1037 BTW LONGERON L15 - L17 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 4. (LP #2999578)
- [SDR DALA2023100308099](https://openairdocs.org/sdr/DALA2023100308099.md): Unknown · unknown · Oct 3, 2023 · N920AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CORROSION ON LONGERON END 24RH AND STA 1011 AT AFT CARGO. SUMMARY OF NRC 00650: CORROSION LEVEL 2. LONGERON END 24RH AND STA 1011 AT AFT CARGO WAS REPLACED PER B717-200 SRM 51-41-05-0G. (LP #2998688)
- [SDR DALA2023100308097](https://openairdocs.org/sdr/DALA2023100308097.md): Unknown · unknown · Oct 2, 2023 · N920AT · Boeing 717200 · Passenger/Crew Doors
  > CRACK ANGLE INSIDE DOOR MECHANISM BTW BEAM 4 AND 5 AT PASSENGER DOOR (L1). SUMMARY OF NRC 00156: ANGLE (INTERCOSTAL) INSIDE DOOR MECHANISM BTW BEAM 4 AND 5 AT PASSENGER DOOR (L1) WAS FABRICATED AND REPLACED PER B717-200 SRM 51-40-02-0G AND DWG 9955763 REV K. (
- [SDR DALA2023100308094](https://openairdocs.org/sdr/DALA2023100308094.md): Unknown · unknown · Oct 1, 2023 · N920AT · Boeing 717200 · Passenger/Crew Doors
  > CRACKS (2 EA) ON FWD AND AFT PANS UPPER CORNER AT PASSENGER DOOR (L1). SUMMARY OF NRC 00151: FWD PAN UPPER CORNER AT PASSENGER DOOR (L1) WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 3 REPAIR 3. NO CRACKS WERE FOUND AT AFT PAN PER B717 DC-MD/BOEING NDTSP
- [SDR DALA2023100308091](https://openairdocs.org/sdr/DALA2023100308091.md): Unknown · unknown · Oct 1, 2023 · N920AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CORROSION ON LONGERON END (1 EA) STA Y:1053 LONGERON 27RH AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00652: CORROSION LEVEL 2. LONGERON END AT STA Y:1053 LONGERON 27RH WAS REPLACED PER B717-200 SRM 51-41-05-0G. (LP #2996387)
- [SDR DALA2023100308087](https://openairdocs.org/sdr/DALA2023100308087.md): Unknown · unknown · Sep 30, 2023 · N920AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK ON FRAME STA Y=1037 BTW LONGERON R15 - R17 AT PAX CABIN. SUMMARY OF NRC 00442: FRAME STA Y=1037 BTW LONGERON R15 - R17 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 4, REPAIR 4. (LP #2994735)
- [SDR DALA2023092908002](https://openairdocs.org/sdr/DALA2023092908002.md): Unknown · unknown · Sep 28, 2023 · N920AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CORROSION ON INNER DOUBLER AT AFT FUSELAGE PRESSURE BULKHEAD LOWER AREA STA Y=1053 BTW LONG 29LH-29RH AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00231: CORROSION LEVEL 2. INNER DOUBLER AT AFT FUSELAGE PRESSURE BULKHEAD LOWER AREA STA Y=1053 BTW LONG 29LH-29
- [SDR DALA2023092908001](https://openairdocs.org/sdr/DALA2023092908001.md): Unknown · unknown · Sep 28, 2023 · N920AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > BROKEN INTERCOSTAL OF FLOOR CPAX STA 1022 AND BL=0 AT AFT CARGO. SUMMARY OF NRC 00214: INTERCOSTAL OF FLOOR CPAX STA 1022 AND BL= 0 AT AFT CARGO WAS REPAIRED B717-200 SRM 51-70-11-2R-1 REPAIR 1. (LP #2991792)
- [SDR DALA2023092807974](https://openairdocs.org/sdr/DALA2023092807974.md): Unknown · unknown · Sep 27, 2023 · N920AT · Boeing 717200 · Fuselage Main, Structure
  > CRACK ON BEAM 1 BELOW FWD UPPER CORNER AT PASSENGER DOOR (L1). SUMMARY OF NRC 00152: BEAM NBR 1 BELOW FWD UPPER CORNER AT PASSENGER DOOR (L1) WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 7 REPAIR 7. (LP #2990273)
- [SDR DALA2023092707956](https://openairdocs.org/sdr/DALA2023092707956.md): Unknown · unknown · Sep 26, 2023 · N920AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON CUSP WEB FROM Y=160 TO Y=200 -X8 TO -X37 AT PAX CABIN IN REF NRC 00538. SUMMARY OF NRC 00614: CORROSION LEVEL 2. CUSP WEB FROM Y=160 TO Y=200 -X8 TO -X37 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 1 PAR 4 FIG 201 SHEET 1. (LP
- [SDR DALA2023092707950](https://openairdocs.org/sdr/DALA2023092707950.md): Unknown · unknown · Sep 26, 2023 · N920AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORT Y=180 FROM X=-10 TO X=-43, FROM Y=162 TO Y=198 X=-45 AT W-1 AREA CPAX IN REF NRC 00541. SUMMARY OF NRC 00610: CORROSION LEVEL 2. FLOOR SUPPORTS Y=180 FROM X=-10 TO X=-43 AND FLOOR SUPPORT FROM Y=162 TO Y=198 X=-45 AT W-1 AREA CPAX WE
- [SDR DALA2023092507865](https://openairdocs.org/sdr/DALA2023092507865.md): Unknown · unknown · Sep 24, 2023 · N920AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORT FROM Y=148 TO Y=200 X=8 W-1 AREA AT CPAX. SUMMARY OF NRC 00324: CORROSION LEVEL 2. FLOOR SUPPORT FROM Y=148 TO Y=200 X=8 W-1 AREA AT CPAX WAS REPLACED PER B717-200 SRM 51-41-01-0G. (LP #2984541)
- [SDR DALA2023092507864](https://openairdocs.org/sdr/DALA2023092507864.md): Unknown · unknown · Sep 24, 2023 · N920AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK ON FRAME STA Y=275 BTW STRG 15L/14L AT CPAX. SUMMARY OF NRC 00286: FRAME STA Y=275 BTW STRG 15L/14L AT CPAX WAS REPAIRED PER B-717-200 SRM 53-20-07-2R REPAIR 1. (LP #2984454)
- [SDR DALA2023092107770](https://openairdocs.org/sdr/DALA2023092107770.md): Unknown · unknown · Sep 20, 2023 · N920AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORTS (3 EA) VERTICAL AND HORIZONTAL BTW STA 200 TO STA 160 BTW LBL15, LBL45, AND LBL55 AT CPAX. SUMMARY OF NRC 00437: CORROSION LEVEL 2. FLOOR SUPPORTS (3 EA) VERTICAL AND HORIZONTAL BTW STA 200 TO STA 160 BTW LBL15, LBL45, AND LBL55 AT
- [SDR DALA2023092107768](https://openairdocs.org/sdr/DALA2023092107768.md): Unknown · unknown · Sep 20, 2023 · N920AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON WEB ON STA Y=579 AND X=-44 AT PAX CABIN. SUMMARY OF NRC 00389: WEB ON STA Y=579 AND X=-44 AT PAX CABIN WAS REPAIRED PER B 717-200 SRM 53-00-55-2R REPAIR 4. (LP #2979222)
- [SDR DALA2023091907684](https://openairdocs.org/sdr/DALA2023091907684.md): Unknown · unknown · Sep 18, 2023 · N920AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON WEB STA Y 190, LBL44 AT CPAX. SUMMARY OF NRC 00436: WEB STA Y 190, LBL44 WAS REPAIRED PER B 717-200 SRM 51-70-10-2R REP 1 FIG 201. (LP #2976349)
- [SDR DALA2023091807628](https://openairdocs.org/sdr/DALA2023091807628.md): Unknown · unknown · Sep 17, 2023 · N920AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > REWORKED CORRODED AREA RH CUSP WEB BTW STA Y=465 AND STA=484. ORIGINAL THICKNESS OF 0.020 IN AND MINIMUM REMAINING THICKNESS OF 0.014 IN. REWORKED AREA IS OUT LIMITS. SUMMARY OF NRC 00569: CORROSION LEVEL 2. RH CUSP WEB BTW STA Y=465 AND STA=484 WAS REPAIRED P
- [SDR DALA2023091807624](https://openairdocs.org/sdr/DALA2023091807624.md): Unknown · unknown · Sep 15, 2023 · N920AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON SHIELD X=56R AND X=44.5R BTW STA Y=1022 TO Y=1053 AND WEB X=56R STA Y=1042 AT PAX CABIN. SUMMARY OF NRC 00233: CORROSION LEVEL 2. SUPPORT X=56R AND X=44.5R BTW STA Y=1022 TO Y=1053 WAS FABRICATED PER DWG 9981474 REV L AND REPLACED PER B717-200 SRM

Next page: https://openairdocs.org/aircraft/N920AT/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 = 'N920AT' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N920AT/reports

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