# Service difficulty reports: N966AT

A list on [N966AT](https://openairdocs.org/aircraft/N966AT.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 · 197 reports

- [SDR DALA2026092905408](https://openairdocs.org/sdr/DALA2026092905408.md): Doubler · installed · Sep 26, 2026 · N966AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > FUSELAGE CROWN Y503 - Y522, L-1 - L-3R EXISTING DOUBLER NEAR STC INSTALL AREA. REPAIRED PER ER/A 637037-14. (1833976) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026081904728](https://openairdocs.org/sdr/DALA2026081904728.md): Transmitter · faulted · Aug 13, 2026 · N966AT · Boeing 717200 · Ground Proximity System
  > CORROSION UNDER THE NR 2 RADIO ALTIMETER TRANSMITTER AT STA 569 BETWEEN L-29L AND L-30, CORRECTIVE ACTION: COMPLIED WITH ER/A 631535-14. (1753411) (AIRCRAFT GROUNDED).
- [SDR DALA2026012200497](https://openairdocs.org/sdr/DALA2026012200497.md): Uplock Sensor · faulted · Jan 17, 2026 · N966AT · Boeing 717200 · Landing Gear Position and Warning
  > PERFORMED GO AROUND DUE TO RIGHT MLG UNSAFE INDICATION WHEN GEAR EXTENDED FOR LANDING. INDICATION RETURNED TO NORMAL AIRCRAFT LANDED SAFELY. CORRECTIVE ACTION: FOUND RIGHT MLG UPLOCK SENSOR OUT OF ADJUSTMENT. ADJUSTED SAME. SERVICED RIGHT MLG STRUT PER MCC REQ
- [SDR DALA2026011600381](https://openairdocs.org/sdr/DALA2026011600381.md): Skin · not reported · Jan 11, 2026 · N966AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > AIRCRAFT IS NOT TO BE RELEASE TO SERVICE UNTIL ERA 631535-14 HAS BEEN REVISED TO REFLECT FAA APPROVAL. REPAIRED PER ERA 631535-14. (1397287)
- [SDR DALA2026011600380](https://openairdocs.org/sdr/DALA2026011600380.md): Skin · corroded · Jan 11, 2026 · N966AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CORROSION UNDER NR 2 RECEIVE RADIO ALTIMETER ANTENNA. COMPLIED WITH ERA 631535-14 REV ORIG FUSELAGE SKIN REPAIR. (1397282)
- [SDR DALA2026011600373](https://openairdocs.org/sdr/DALA2026011600373.md): Skin · corroded · Jan 11, 2026 · N966AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > ENGINEERING 12-MONTH DTE LOG PAGE FOR CORROSION UNDER# 2 RADIO ALTIMETER TRANSMITTER AT STA 569 BETWEEN L-29L AND L-30 PER ER/A 631535-14 REV A. REPAIRED PER ERA 631535-14. (1397118)
- [SDR DALA2026010900240](https://openairdocs.org/sdr/DALA2026010900240.md): Seat Track · corroded · Jan 3, 2026 · N966AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND CORROSION ON RT INB SEAT TRACK. REPAIRED SEAT TRACK PER B717 SRM 53-20-52 (1383323)
- [SDR DALA2026010500071](https://openairdocs.org/sdr/DALA2026010500071.md): Seat Track · corroded · Jan 1, 2026 · N966AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND CORROSION ON RH OTBD SEAT TRACK. REPAIRED SEAT TRACK PER B717 SRM 53-20-52. (1380043)
- [SDR DALA2026010509566](https://openairdocs.org/sdr/DALA2026010509566.md): Web · corroded · Dec 29, 2025 · N966AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > AFTER REMOVAL OF INBOARD RT SEAT TRACK, SUB FLOOR SKIN IS CORRODED. REPAIRED SUB FLOOR MEMBRANE IAW SRM 53-00-55 (1375171)
- [SDR DALA2024121611740](https://openairdocs.org/sdr/DALA2024121611740.md): Battery Pack · inoperative · Dec 15, 2024 · N966AT · Boeing 717200 · Emergency Lighting
  > THE EMERGENCY LIGHTS POWERED BY BATTERIES B5-235 AND B5-118 ARE INOPERATIVE. MAINTENANCE REPLACED EMERGENCY BATTERY PACKS B5-235 AND B5-118 PER B717 AMM 33-51. OK FOR SERVICE. (LP #6519628)
- [SDR DALA2024012901232](https://openairdocs.org/sdr/DALA2024012901232.md): Battery Pack · inoperative · Jan 27, 2024 · N966AT · Boeing 717200 · Emergency Lighting
  > FOUND THE FORWARD ENTRANCE EXIT PATHWAY SIGN GOING INTO COCKPIT TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. LIGHT OPERATION NOW CHECKS GOOD IAW B717 AMM 33-51-18. (LP #5448489)
- [SDR DALA2023101608456](https://openairdocs.org/sdr/DALA2023101608456.md): Unknown · unknown · Oct 14, 2023 · N966AT · Boeing 717200 · Emergency Lighting
  > THE EMERGENCY LIGHTS DON'T OPERATE CORRECTLY DURING SERVICE CHECKS. SUMMARY OF NRC 00700: DURING CONTINUITY AND VOLTAGE CHECK TERMINAL 10, 11, AND 12 ON S3-559 WERE FOUND WITH CONTINUITY BETWEEN THEM. TERMINAL 10, 11, AND 12 ON S3-559 WERE INSTALLED CORRECTLY
- [SDR DALA2023101608482](https://openairdocs.org/sdr/DALA2023101608482.md): Unknown · unknown · Oct 13, 2023 · N966AT · Boeing 717200 · Aerodynamic Fairings
  > IMPROPERLY INSTALLED TAIL-CONE KEVLAR LANYARD (CAT). THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY OF NRC 00703: TAIL-CONE KEVLAR LANYARD WAS INSTALLED CORRECTLY PER B717 AMM 53-52-01 400-8
- [SDR DALA2023101408442](https://openairdocs.org/sdr/DALA2023101408442.md): Unknown · unknown · Oct 12, 2023 · N966AT · Boeing 717200 · Horizontal Stabilizer Structure
  > ELONGATED HOLES (2 EA) ON FAIRING PANEL 360AT. SUMMARY OF NRC 00511: ANGLE WAS FABRICATED AND REPLACED PER DWG 5912175 REV BR AND B717-200 SRM 51-41-02-0G AND FAIRING WAS REPAIRED PER ERA 612574-14 REV ORIGINAL, AND PRI 612574-14 REV 1. ASSOCIATED ER/A 14-6125
- [SDR DALA2023100608221](https://openairdocs.org/sdr/DALA2023100608221.md): Unknown · unknown · Oct 4, 2023 · N966AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CORROSION ON LOWER SKIN RBL=35, RBL=45 AND STA 756 AT W/W AREA. SUMMARY OF NRC 00163: CORROSION LEVEL 2. CORROSION ON LOWER SKIN RBL=35, RBL=45 AND STA 756 AT W/W AREA WAS REPAIRED PER PRI 611928-14 REV 3 AND ER/A 611928-14 REV ORIGINAL SECTION I: PERMANENT RE
- [SDR DALA2023100408160](https://openairdocs.org/sdr/DALA2023100408160.md): Unknown · unknown · Oct 4, 2023 · N966AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK ON FRAME STA Y=974 STRG 29R AT AFT CARGO COMPARMENT WAS FOUND. SUMMARY OF NRC 00649: FRAME STA Y=974 STRG 29R AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717 SRM 53-20-07-2R PROCEDURE 3 REPAIR 3 FIG 201 SHEET 1. (LP #0000432)
- [SDR DALA2023100408156](https://openairdocs.org/sdr/DALA2023100408156.md): Unknown · unknown · Oct 4, 2023 · N966AT · Boeing 717200 · Fuselage Main, Structure
  > CORROSION ON SPLICE BTW STA 617 TO 636 FROM L-30 TO L-29L AT FWD COMPARTMENT CARGO. SUMMARY OF NRC 00366: CORROSION LEVEL 2. SPLICE BTW STA 617 TO 636 FROM L-30 TO L-29L AT FWD COMPARTMENT CARGO WAS REPAIRED PER ERA 612306-14 REV ORIGINAL SECTION I: PERMANENT
- [SDR DALA2023100408159](https://openairdocs.org/sdr/DALA2023100408159.md): Unknown · unknown · Oct 3, 2023 · N966AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACK ON BRACKET AND SKIN INSIDE UPPER STA Y=389 AT FWD CARGO DOOR. SUMMARY OF NRC 00099: SKIN INSIDE UPPER STA Y=389 AT FWD CARGO DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R REPAIR 1, AND BRACKET (FITTING) INSIDE UPPER STA Y=389 AT FWD CARGO DOOR WAS REPLA
- [SDR DALA2023100408155](https://openairdocs.org/sdr/DALA2023100408155.md): Unknown · unknown · Oct 3, 2023 · N966AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRG 25L BTW STA Y=1002 TO Y=1022 AT AFT CARGO COMPARTMENT. (CCT) SUMMARY OF NRC 00622: CORROSION LEVEL 2. STRG 25L BTW STA Y=1002 TO Y=1022 AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717 SRM 53-00-05-2R PROCEDURE 2 REPAIR 2. (LP #0000131)
- [SDR DALA2023100408152](https://openairdocs.org/sdr/DALA2023100408152.md): Unknown · unknown · Oct 3, 2023 · N966AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CORROSION ON SPLICE OF LONGERON BTW STA 218 TO STA 237, L-29R BILGE AREA AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00336: CORROSION LEVEL 2. SPLICE OF LONGERON BTW STA 218 TO STA 237, L-29R BILGE AREA AT FWD CARGO COMPARTMENT WAS REPLACED PER B717 SRM 51-41-02-
- [SDR DALA2023100308096](https://openairdocs.org/sdr/DALA2023100308096.md): Unknown · unknown · Oct 2, 2023 · N966AT · Boeing 717200 · Fuselage Main, Structure
  > CORROSION ON FRAME CLIP STA Y=1022 BTW STRG 30/29L AT AFT CARGO COMPARMENT. SUMMARY OF NRC 00230: CORROSION LEVEL 2. FRAME CLIP STA Y=1022 BTW STRG 30/29L AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717 SRM 53-00-06-2R-2 REPAIR 2 & 53-20-06-2R-2 REPAIR 2. (LP #
- [SDR DALA2023100308095](https://openairdocs.org/sdr/DALA2023100308095.md): Unknown · unknown · Oct 2, 2023 · N966AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTAL STA Y=943 OVER STRG 29R AT AFT CARGO COMPARMENT. SUMMARY OF NRC 00203: CORROSION LEVEL 2. INTERCOSTAL STA Y=943 OVER STRG 29R AT AFT CARGO COMPARTMENT WAS REPLACED PER B717 SRM 51-41-02-0G AND 51-41-05-0G. (LP #2996865)
- [SDR DALA2023100308093](https://openairdocs.org/sdr/DALA2023100308093.md): Unknown · unknown · Oct 1, 2023 · N966AT · Boeing 717200 · Fuselage Main, Frame
  > CORROSION ON FRAME CLIP STA Y=905 BTW STRG 30/29L AT AFT CARGO COMPARMENT. SUMMARY OF NRC 00197: CORROSION LEVEL 2. FRAME CLIP STA Y=905 BTW STRG 30/29L AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717 SRM 53-00-06-2R PROCEDURE 2 REPAIR 2. CORROSION ON FRAME WAS
- [SDR DALA2023100308089](https://openairdocs.org/sdr/DALA2023100308089.md): Unknown · unknown · Sep 30, 2023 · N966AT · Boeing 717200 · Fuselage Structure (General)
  > CORROSION ON FRAME CLIP STA Y=832 BTW STRG 28L/27L AT AFT CARGO COMPARMENT. SUMMARY OF NRC 00349: CORROSION LEVEL 2. FRAME CLIP STA Y=832 BTW STRG 28L/27L AT AFT CARGO COMPARMENT WAS REPAIRED PER B717 SRM 53-00-06-2R PROCEDURE 2 REPAIR 2 AND DWG 9912243 REV JS
- [SDR DALA2023100308088](https://openairdocs.org/sdr/DALA2023100308088.md): Unknown · unknown · Sep 30, 2023 · N966AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION EXCESSIVE ON STRAP L-25L STA 1005 TO 1035 AND TERMINAL LONG L-25L STA 1053 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00643: CORROSION LEVEL 2. STRAP L-25L STA 1005 TO 1035 AND TERMINAL LONG L-25L STA 1053 AT AFT CARGO COMPARTMENT WERE REPLACED PER DWG
- [SDR DALA2023100308085](https://openairdocs.org/sdr/DALA2023100308085.md): Unknown · unknown · Sep 29, 2023 · N966AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR FITTING STA 200 TO 218 RBL=11 WAS REMOVED PER B717 SRM 51-10-04-0G PAR 26 C, ORIGINAL THICKNESS IS 0.975IN AND MINIMUM REMAINING THICKNESS IS 0.850IN THEREFORE AREA IS OUT OF LIMITS PER B717 SRM 53-00-00-1A PROCEDURE ALLOWABLE DAMAGE GENERAL
- [SDR DALA2023100308083](https://openairdocs.org/sdr/DALA2023100308083.md): Unknown · unknown · Sep 29, 2023 · N966AT · Boeing 717200 · Fuselage Main, Attach Fittings
  > FITING AT STA 620 TO STA 636 L-30 HAD CORROSION FOUND ON SAME FITTING. CORROSION LEVEL 2. FITTING AT STA 620 TO STA 636 L-30 WAS FABRICATED PER DWG 5971577 REV D. FITTING OF STA 620 TO STA 636 L-30 WAS REPLACED PER DWG 5971577 REV D B717 SRM 51-41-05-0G A
- [SDR DALA2023092908006](https://openairdocs.org/sdr/DALA2023092908006.md): Unknown · unknown · Sep 29, 2023 · N966AT · Boeing 717200 · Fuselage Internal Mounting Structure
  > CORROSION ON FRAME CLIP STA Y=974 BTW STRG 26L/25L AT AFT CARGO COMPARMENT. SUMMARY OF NRC 0345: CORROSION LEVEL 2. FRAME CLIP STA Y=974 BTW STRG 26L/25L AT AFT CARGO COMPARTMENT WAS REPLACED PER DWG 9958215 REV AM. (LP #2992309)
- [SDR DALA2023092908005](https://openairdocs.org/sdr/DALA2023092908005.md): Unknown · unknown · Sep 29, 2023 · N966AT · Boeing 717200 · Fuselage Structure (General)
  > CRACK ON UPPER FITTING AT AFT CABIN COMPARTMENT IN LONGERON 2L AT STA 1116. SUMMARY OF NRC 00224: UPPER FITTING AT AFT CABIN COMPARTMENT IN LONGERON 2L AT STA 1116 WAS REPAIRED PER B717 SRM 53-00-05-2R REPAIR 2 FIG 201 SHEET 2. (LP #2992175)
- [SDR DALA2023092908004](https://openairdocs.org/sdr/DALA2023092908004.md): Unknown · unknown · Sep 28, 2023 · N966AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTAL STA Y=916 OVER STRG 28R AT AFT CARGO COMPARMENT. SUMMARY OF NRC 00328: CORROSION LEVEL 2. INTERCOSTAL ON STA Y=908 TO Y=927 STGR 28 RH WAS REPLACED PER DWG 9957704 REV M, B717 SRM 51-41-02-0G, AND 51-41-05-0G. (LP #2991968)
- [SDR DALA2023092807971](https://openairdocs.org/sdr/DALA2023092807971.md): Unknown · unknown · Sep 27, 2023 · N966AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON WEB BTW STA 940 TO 950 AND L25R TO L26R AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00139: CORROSION LEVEL 2. WEB BTW STA 940 TO 950 AND L25R TO L26R AFT CARGO COMPARTMENT WAS REPAIRED PER B717 SRM 51-70-10-2R PROCEDURE 1, REPAIR 1. (LP #2990111)
- [SDR DALA2023092707953](https://openairdocs.org/sdr/DALA2023092707953.md): Unknown · unknown · Sep 26, 2023 · N966AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACKS ON AFT PAN UPPER SECTION AT L1 DOOR. SUMMARY OF NRC 00603: AFT PAN UPPER SECTION AT L1 DOOR WAS REPAIRED PER B717-200 SRM 52-10-02-2R REPAIR 3. (LP #2988599)
- [SDR DALA2023092707952](https://openairdocs.org/sdr/DALA2023092707952.md): Unknown · unknown · Sep 26, 2023 · N966AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON CABIN FLOOR WEB DOUBLER BTW STA=641 TO 646 X=-58. CORROSION ON WEB DOUBLER BTW STA=476 TO STA=498 RH SIDE AT PAX CABIN. SUMMARY OF NRC 00542: CORROSION LEVEL 1. CORROSION ON CABIN FLOOR WEB DOUBLER (SPLICE ANGLE) BTW STA=641 TO 646 X=-58 WAS REMOV
- [SDR DALA2023092507867](https://openairdocs.org/sdr/DALA2023092507867.md): Unknown · unknown · Sep 24, 2023 · N966AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION OUT OF LIMITS ON CUSP WEB RBL=57 AND STA 266, 331, 926, 935, AND 944. WITH AN ORIGINAL THICKNESS OF 0.020 INCHES AND REMAINING THICKNESS OF 0.007 INCHES, THE AREAS ARE OUT OF LIMITS PER B717-200 SRM 53-00-55-1A PROCEDURE 1, ALLOWABLE DAMAGE 1, PAR 4
- [SDR DALA2023092507860](https://openairdocs.org/sdr/DALA2023092507860.md): Unknown · unknown · Sep 23, 2023 · N966AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON CUSP WEB STA Y=680 X=-50, AT CABIN PAX. SUMMARY OF NRC 00619: CORROSION LEVEL 2. CUSP WEB BTW STA 655 TO STA 684 X=-50 AT CABIN PAX WAS REPAIRED PER B717 SRM 53-00-55-2R-4 PAR 4 AND 5 FIGURE 223. (LP #2983819)
- [SDR DALA2023092507859](https://openairdocs.org/sdr/DALA2023092507859.md): Unknown · unknown · Sep 23, 2023 · N966AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON CABIN FLOOR CUSP WEB UPPER AND LOWER FACE BTW STA=541 TO 560 FROM X=-58 TO X=-54, STA=598 TO 617 FROM X=-58 TO X=-54, STA=620 TO 630 FROM X=-58 TO X=-54, STA=636 TO 655 FROM X=-55 TO X=-46, AND BTW STA=655 TO STA=674 FROM X=-55 TO X=-46 RH SIDE AT
- [SDR DALA2023092507857](https://openairdocs.org/sdr/DALA2023092507857.md): Unknown · unknown · Sep 22, 2023 · N966AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON WEB INSIDE UPPER STA Y=1076 AT AFT BULKHEAD DOOR. SUMMARY OF NRC 00093: WEB INSIDE UPPER STA Y=1076 AT AFT BULKHEAD DOOR WAS FABRICATED AND REPLACED PER DRAWING 9929480-49 REV BW, B717-200 SRM 51-41-02-0G, AND 51-41-05-0G PAR 8. (LP #2982829)
- [SDR DALA2023092507855](https://openairdocs.org/sdr/DALA2023092507855.md): Unknown · unknown · Sep 22, 2023 · N966AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON CUSP WEB STA FROM Y=860 TO Y=870 X=- 58, AT CABIN PAX. SUMMARY OF NRC 00621: CORROSION LEVEL 2. CUSP WEB STA FROM Y=860 TO Y=870 X=- 58 WAS REPAIRED PER B717 SRM 53-00-55-2R REPAIR 4 FIGURE 216. (LP #2982286)
- [SDR DALA2023092207783](https://openairdocs.org/sdr/DALA2023092207783.md): Unknown · unknown · Sep 21, 2023 · N966AT · Boeing 717200 · Passenger/Crew Doors
  > AFTER INNER SKIN REMOVAL, A CRACK WAS FOUND ON BEAM #1 AFT SECTION OF L1 DOOR. SUMMARY OF NRC 00647: BEAM #1 AFT SECTION OF L1 DOOR WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 7 REPAIR 7. (LP #2981121)
- [SDR DALA2023092007728](https://openairdocs.org/sdr/DALA2023092007728.md): Unknown · unknown · Sep 20, 2023 · N966AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON CUSP WEB STA Y=256 X=-58. SUMMARY OF NRC 00618: CORROSION LEVEL 2. CUSP WEB STA 256 X=-58 WAS REPAIRED PER B717 SRM 53-00-55-2R REPAIR 4 FIGURE 220. (LP #2978269)
- [SDR DALA2023092107767](https://openairdocs.org/sdr/DALA2023092107767.md): Unknown · unknown · Sep 19, 2023 · N966AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION OUT OF LIMITS ON CABIN FLOOR CUSP WEB STA=377, STA=390, STA=417, AND STA=636 BTW -X=46 TO -X=59 RH SIDE AT PAX CABIN. ORIGINAL THICKNESS IS 0.020IN REMAINING THICKNESS IS 0.014IN THEREFORE AREAS ARE OUT OF LIMITS PER B717-200 SRM 53-00-55-1A PROCEDUR
- [SDR DALA2023092007724](https://openairdocs.org/sdr/DALA2023092007724.md): Unknown · unknown · Sep 19, 2023 · N966AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION OUT OF LIMITS ON CUSP WEB X=+57 STA 444, 517, 523, 544 TO 557, 608, 646 TO 660, AND 804 AT CPAX. WITH AN ORIGINAL THICKNESS=0.020 INCHES AND REMAINING THICKNESS=0.014 INCHES THEREFORE AREAS ARE OUT LIMITS PER B717-200 SRM 53-00-55-1A PROCEDURE 1, ALL
- [SDR DALA2023091907686](https://openairdocs.org/sdr/DALA2023091907686.md): Unknown · unknown · Sep 19, 2023 · N966AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK ON FRAME STA Y=705 BTW STRG 28R/29R INSIDE CANTED KEEL. SUMMARY OF NRC 00381: FRAME STA Y=705 BTW STRG 28R/29R INSIDE CANTED KEEL WAS REPAIRED PER B717 SRM-51-70-11-2R-1. (LP #2976623)
- [SDR DALA2023091907683](https://openairdocs.org/sdr/DALA2023091907683.md): Unknown · unknown · Sep 18, 2023 · N966AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR STRUCTUTRE (2 EA) BTW STA 148 TO STA 200 AND LBL/RBL=7 AT FWD CPAX. SUMMARY OF NRC 00301: CORROSION LEVEL 2. FLOOR STRUCTUTRE (2 EA) BTW STA 148 TO STA 200 AND LBL/RBL=7 AT FWD CPAX WERE REPLACED PER B717 SRM 51-41-01-0G. (LP #2976176)
- [SDR DALA2023091907682](https://openairdocs.org/sdr/DALA2023091907682.md): Unknown · unknown · Sep 18, 2023 · N966AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK ON FRAME STA Y=706 BTW STRG 27L/28L INSIDE CANTED KEEL. SUMMARY OF NRC 00388: FRAME STA Y=706 BTW STRG 27L/28L INSIDE CANTED KEEL WAS REPAIRED PER B717 SRM-51-70-11-2R-1. (LP #2976018)
- [SDR DALA2023091907681](https://openairdocs.org/sdr/DALA2023091907681.md): Unknown · unknown · Sep 18, 2023 · N966AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION WAS FOUND AT FLOOR SUPPORT ON STA 200.0 LBL 12. SUMMARY OF NRC 00634: CORROSION LEVEL 2. FLOOR SUPPORT ON STA 200.0 LBL 12 WAS REPLACED PER B717 SRM 51-40-08-0G AND WITH NRC 00615. (LP #2976011)
- [SDR DALA2023091907680](https://openairdocs.org/sdr/DALA2023091907680.md): Unknown · unknown · Sep 18, 2023 · N966AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON CUSP WEB STA Y 247, 313, 775, AND X=49 AT PAX CAB. SUMMARY OF NRC 00628: CORROSION LEVEL 2. CUSP WEB STA Y 247, 313, 775, AND X=49 AT PAX CAB WERE REPAIRED PER B717 SRM 53-00-55-2R PROCEDURE 4, FIG 215. (LP #2975964)
- [SDR DALA2023091907679](https://openairdocs.org/sdr/DALA2023091907679.md): Unknown · unknown · Sep 18, 2023 · N966AT · Boeing 717200 · Fuselage Structure (General)
  > CORROSION OUT OF LIMITS ON DIAPHRAGM BTW STA 200 AND LBL=5-10 AT FWD CPAX. WITH AN ORIGINAL THICKNESS OF 0.020 INCHES AND MINIMUM REMAINING THICKNESS OF 0.013, THE AREA IS OUT OF LIMITS PER B717 SRM 53-00-00-1A PROCEDURE ALLOWABLE DAMAGE GENERAL PAR 4 C AND FI
- [SDR DALA2023091807631](https://openairdocs.org/sdr/DALA2023091807631.md): Unknown · unknown · Sep 18, 2023 · N966AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK ON FRAME STA Y=686 BTW STRG 27L/28L INSIDE CANTED KEEL. SUMMARY OF NRC 00389: FRAME STA Y=686 BTW STRG 27L/28L INSIDE CANTED KEEL WAS REPAIRED PER B717 SRM-51-70-11-2R-1. (LP #2975043)
- [SDR DALA2023091807630](https://openairdocs.org/sdr/DALA2023091807630.md): Unknown · unknown · Sep 17, 2023 · N966AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION OUT OF LIMITS WAS FOUND ON THE CUSP WEB STA 696 AND 715 X=-58, AT CABIN PAX. SUMMARY OF NRC 00620: CORROSION LEVEL 2. CUSP WEB STA 696 AND 715 X=-58 WAS REPAIRED PER B717 SRM 53-00-55-2R PROCEDURE 4. (LP #2974760)

Next page: https://openairdocs.org/aircraft/N966AT/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 = 'N966AT' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N966AT/reports

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