# Service difficulty reports: N980AT

A list on [N980AT](https://openairdocs.org/aircraft/N980AT.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 5 · 245 reports

- [SDR DALA2026102305844](https://openairdocs.org/sdr/DALA2026102305844.md): Spar Cap · cracked · Oct 22, 2026 · N980AT · Boeing 717200 · Wing Spar
  > FOUND CRACK AT REAR SPAR LOWER CAP NEAR XRS 164, COMPLIED WITH ER/A 636450-14AD. (1879849) (AIRCRAFT GROUNDED).
- [SDR DALA2026102305840](https://openairdocs.org/sdr/DALA2026102305840.md): Spar Cap · cracked · Oct 22, 2026 · N980AT · Boeing 717200 · Wing Spar
  > FOUND CRACK NEAR XRS-158 AND 170 AT RT WING ERAR SPAR CAP SPLICE, COMPLIED WITH ER/A 636450-14AD. (1879441) (AIRCRAFT GROUNDED).
- [SDR DALA2026102305839](https://openairdocs.org/sdr/DALA2026102305839.md): Spar Angle · cracked · Oct 22, 2026 · N980AT · Boeing 717200 · Wing Spar
  > FOUND CRACK COMMON TO THE RT WING LOWER SPAR CAP, COMMON TO THE RT WING REAR SPAR INSTL AT AFT FLANGE NEAR XRS=164, COMPLIED WITH ER/A 636450-14AD. (1879433) (AIRCRAFT GROUNDED).
- [SDR DALA2026102305838](https://openairdocs.org/sdr/DALA2026102305838.md): Spar Cap · cracked · Oct 22, 2026 · N980AT · Boeing 717200 · Wing Spar
  > FOUND CRACK COMMON TO THE RT WING LOWER SPAR CAP, COMMON TO THE RH WING REAR SPAR INSTL AT AFT FLANGE NEAR XRS=164, CORRECTIVE ACTION: COMPLIED WITH ER/A 636450-14AD. (1879422) (AIRCRAFT GROUNDED).
- [SDR DALA2026101905723](https://openairdocs.org/sdr/DALA2026101905723.md): Skin · damaged · Oct 18, 2026 · N980AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > FOUND A DISCREPANT FASTENER HOLE WAS IDENTIFIED AT THE INTERSECTION OF FRAME Y503 AND LONGERON L1, AT THE FOURTH FASTENER LOCATION AFT OF THE FORWARD EDGE OF STC DOUBLER, CORRECTIVE ACTION: COMPLIED WITH ER/A 637350-14AD. (1871858) (AIRCRAFT GROUNDED).
- [SDR DALA2026100205474](https://openairdocs.org/sdr/DALA2026100205474.md): Doubler · cracked · Oct 1, 2026 · N980AT · Boeing 717200 · Wing, Landing Gear Attach Fittings
  > RT WING UPPER MLG DOUBLER HAS TWO HOLES WITH CRACK INDICATIONS, COMPLIED WITH ER/A 636571-14AD. (1842799) (AIRCRAFT GROUNDED).
- [SDR DALA2026020900914](https://openairdocs.org/sdr/DALA2026020900914.md): Bracket · damaged · Feb 1, 2026 · N980AT · Boeing 717200 · Emergency Equipment
  > GIRT BAR BRACKETS DAMAGED. SECURED THE BRACKET FITTING, OPS CHECKED GOOD. (1430474)
- [SDR DALA2025101707590](https://openairdocs.org/sdr/DALA2025101707590.md): Fuel Cell · leaking · Oct 10, 2025 · N980AT · Boeing 717200 · Fuel Storage
  > FUEL LEAK FOUND DURING INSPECTION OF THE L/H WING AFT LWR SKIN DOUBLER AT XRS=164. CORRECTIVE ACTION: REPAIRED PER ER/A 14-621176. (1243963).
- [SDR DALA2025092306962](https://openairdocs.org/sdr/DALA2025092306962.md): Skin · damaged · Sep 14, 2025 · N980AT · Boeing 717200 · Wing, Plate/Skin
  > EXISTING REPAIR FOUND THAT IMPACTS INSPECTION ACCOMPLISHMENT. REPAIR INVESTIGATION REQUIRED BEFORE FURTHER FLIGHT. RH WING XRS 14- XRS 177. REF. EA 619064-14AD REV. B SECT II. DVI OF AFT SIDE OF SPAR CAP AT STOP DRILL SHOWS NO DISCREPANCY. (1199238)
- [SDR DALA2025090406566](https://openairdocs.org/sdr/DALA2025090406566.md): Sign · detached · Aug 26, 2025 · N980AT · Boeing 717200 · Emergency Lighting
  > EMERGENCY EXIT SIGN ON CEILING ABOVE ROW 1 DETACHING FROM CEILING. RESECURED EXIT SIGN PER B-717 AMM 33-51. (7354500)
- [SDR DALA2025090406560](https://openairdocs.org/sdr/DALA2025090406560.md): Battery Pack · inoperative · Aug 26, 2025 · N980AT · Boeing 717200 · Emergency Lighting
  > EMERGENCY LIGHTS INOPERATIVE ABOVE OVER WINGS EXITS. REMOVED AND REPLACED BATTERY PACK B5-121 REF AMM 33-51 (7280198)
- [SDR DALA2025082206254](https://openairdocs.org/sdr/DALA2025082206254.md): Elec Connector · dirty · Aug 17, 2025 · N980AT · Boeing 717200 · Light System Wiring
  > AFT EMERGENCY LIGHT FLASHING. CLEANED CONNECTOR ON EMERGENCY LIGHT BATTERY PACK B5-260 AND OPS CHECKED IAW AMM 33-51, CHECKED GOOD (7280156).
- [SDR DALA2025081806158](https://openairdocs.org/sdr/DALA2025081806158.md): Battery Pack · no test · Aug 15, 2025 · N980AT · Boeing 717200 · Emergency Lighting
  > EMER LIGHT ABOVE AFT FA JUMPSEAT STAYS ILLUMINATED WHEN IN ARM. T/S REF WDM 33-51. FOUND EMER LIGHT BATTERY PACK B5-260 WATER DAMAGED. R&R'D BATTERY PACK & BATTERY REF B717 AMM 33-51. OPS CHECK GOOD. (7280148)
- [SDR DALA2025070104878](https://openairdocs.org/sdr/DALA2025070104878.md): Sign · detached · Jun 29, 2025 · N980AT · Boeing 717200 · Emergency Lighting
  > SHIP 6546 EMERGENCY EXIT SIGN COVER HANGING LOOSE IN FIRST CLASS CABIN. CORRECTIVE ACTION: RE-SECURED EMERGENCY EXIT SIGN. OK FOR SVC (7552948)
- [SDR DALA2025062604790](https://openairdocs.org/sdr/DALA2025062604790.md): Doubler · leaking · Jun 25, 2025 · N980AT · Boeing 717200 · Wing, Plate/Skin
  > SHIP 9546 FUEL LEAK FOUND DURING INSPECTION OF LH WING AFT LOWER SKIN DOUBLER AT XRS=164. CORRECTIVE ACTION: FUEL LEAK REPAIRED ON ERA 621176-14AD REV C (1044305)
- [SDR DALA2025062604794](https://openairdocs.org/sdr/DALA2025062604794.md): Angle · not reported · Jun 24, 2025 · N980AT · Boeing 717200 · Standard Practices/Structures
  > SHIP 9546 C/W LH WING BULKHEAD CLIP XRS164 PART MANUFACTURE ERA 626984-14 REV ORIG. CORRECTIVE ACTION: COMPLIED WITH LH WING BULKHEAD CLIP XRS164 PART MANUFACTURE ER/A 626894-14 REV A. (1043812)
- [SDR DALA2025062504754](https://openairdocs.org/sdr/DALA2025062504754.md): Spar Cap · damaged · Jun 24, 2025 · N980AT · Boeing 717200 · Wing Spar
  > C/W 621176-14AD REV B LH WING LOWER SPAR CAP LEAK REPAIR. DAMAGED AREA REPAIRED PER ERA 621176-14AD REV B PRI 621176-14AD (1043689).
- [SDR DALA2025062504750](https://openairdocs.org/sdr/DALA2025062504750.md): Repair · no discrepancy · Jun 24, 2025 · N980AT · Boeing 717200 · Standard Practices/Structures
  > EXISTING REPAIR FOUND. CONTACT LIASON ENGINEERING FOR REPAIR PROCEDURES PRIOR TO FURTHER FLIGHT (R/H WING). PER ENGINEERING C/W ERA 619064-14AD REV B SEC II STEP 3. NO ISSUES NOTED.
- [SDR DALA2025060604328](https://openairdocs.org/sdr/DALA2025060604328.md): Repair · damaged · May 25, 2025 · N980AT · Boeing 717200 · Wing Spar
  > SHIP 9546 EXISTING REPAIR FOUND. CONTACT LIASON ENGINEERING FOR REPAIR PROCEDURES PRIOR TO FURTHER FLIGHT. REPAIRED PER ERA 6190064-14AD (0984966)
- [SDR DALA2025043003321](https://openairdocs.org/sdr/DALA2025043003321.md): Repair · not reported · Apr 28, 2025 · N980AT · Boeing 717200 · Standard Practices/Structures
  > -AD- EXISTING REPAIR FOUND, CONTACT LIASON ENGINEERING FOR REPAIR PROCEDURES PRIOR TO FUTHER FLIGHT. FC 5720-01103-01A. OK TO CONT THE WC INSP AS AUTHORIZED BY THE TIME CONT ITEMS STATEMENT FOR SEC II OF ERA 621176-14AD REV A. (LP #7184928)
- [SDR DALA2025043003314](https://openairdocs.org/sdr/DALA2025043003314.md): Repair · not reported · Apr 28, 2025 · N980AT · Boeing 717200 · Wing Structure
  > -AD- EXISTING REPAIR FOUND, OK TO CONT THE WC INSP AS AUTHORIZED BY THE TIME CONT ITEMS STATEMENT FOR SEC I OF ERA 619064-14AD REV B. (LP #7184929)
- [SDR DALA2025041202831](https://openairdocs.org/sdr/DALA2025041202831.md): Fuel Cap · leaking · Apr 11, 2025 · N980AT · Boeing 717200 · Fuel Storage
  > -AD- WORKING PRI 621176-14AD REV "O" B717-200 LH WING REAR SPAR LOWER CAP FUEL LEAK. SUMMARY SEE NRC 004-0001:5720-01103-01A/004 00004: CMOR - COMPLIED WITH ER/A 621176-14 REV A, PRI REV "0", "1", "2", "3", "4", "5", "6", AND "7" REPAIR INSTRUCTIONAL STEPS. EN
- [SDR DALA2025021201090](https://openairdocs.org/sdr/DALA2025021201090.md): None · none · Feb 12, 2025 · N980AT · Boeing 717200 · Standard Practices/Structures
  > IN REFERENCE NRC 00924: LEVEL AND SHORE AIRCRAFT IN ACORDANCE WITH AMM 07-11-00 AS WELL AS PER FIGURE 4 OF BOEING SERVICE SKETCH 3268E PER PRI 621176-14 REV 0 STEP 1 A) AND PERFORM DAILY CHECK UNTIL REMOVED. SUMMARY NRC 00981: SHORINGS WERE INSTALLED AND VERIF
- [SDR DALA2025021201089](https://openairdocs.org/sdr/DALA2025021201089.md): Fitting · damaged · Feb 11, 2025 · N980AT · Boeing 717200 · Wing Main, Frame Structure
  > PERFORM COLDWORK ON INBOARD BRACE FITTING DOUBLER XRS=164 AT LH WING. SUMMARY OF NRC 00924: INBOARD BRACE FITTING DOUBLER XRS=164 AT LH WING WAS REPAIRED PER PRI 621176-14 REV 10 AND ERA 621176-14AD REV ORIGINAL SECTION I: PERMANENT REPAIR. ALSO FAIRING WAS RE
- [SDR DALA2025021001046](https://openairdocs.org/sdr/DALA2025021001046.md): Spar Cap · damaged · Feb 8, 2025 · N980AT · Boeing 717200 · Wing Spar
  > -AD- AWR, AA, AD, IN REF TO AMDS 5720-01103-01B STEP 7: REPAIR IN PROGRESS AT RIGHT WING LOWER REAR SPAR CAP THATS INCLUDES LOWER WING SKIN AND DOUBLER BTW STA XRS 150 AND XRS 177. SUMMARY OF NRC 00918: THIS REPAIR PROVIDED WITH FAA AMOC APPROVAL AND INCLUDES
- [SDR DALA2025020300801](https://openairdocs.org/sdr/DALA2025020300801.md): Spar Cap · cracked · Jan 31, 2025 · N980AT · Boeing 717200 · Wing Spar
  > CRACK ON RH WING LOWER REAR SPAR CAP AROUND SECOND FASTENER FROM FLAP HING FITTING STA XW=154 OUTBOARD TO INBOARD DIRECTION. SUMMARY OF NRC 00347: CRACK ON RH WING LOWER REAR SPAR CAP AROUND SECOND FASTENER FROM FLAP HING FITTING STA XW=154 OUTBOARD TO INBOARD
- [SDR DALA2024100209615](https://openairdocs.org/sdr/DALA2024100209615.md): Unknown · no discrepancy · Sep 26, 2024 · N980AT · Boeing 717200 · Standard Practices/Structures
  > -AD RELATED- AMDS 5720-01103-01A: PERFORM STEP 13. SUMMARY NRC 00919: (ET) HFEC INSPECTION WAS PERFORMED. NO CRACKS WERE FOUND PER B717 CARD 5720-01103-01A, STEP 13 AND B717 DC/MD NDT SPM PART 6, 06-10-01.001. ASSOCIATED AA 5720-01103 ADDED FOR AC 9546. (LP #0
- [SDR DALA2024100209614](https://openairdocs.org/sdr/DALA2024100209614.md): Unknown · no discrepancy · Sep 26, 2024 · N980AT · Boeing 717200 · Standard Practices/Structures
  > -AD RELATED- AMDS 5720-01103-01A: PERFORM STEP 15 AND 16. SUMMARY NRC 00921: SEALANT WAS REMOVED AND APPLIED PER B717 AMM 20-60-01 PER AMDS 5720-01103-01A ALSO (ET) HFEC INSPECTION WAS PERFORMED. NO CRACKS WERE FOUND PER B717 CARD 5720-01103-01A, STEP 16 AND B
- [SDR DALA2024100209613](https://openairdocs.org/sdr/DALA2024100209613.md): Unknown · no discrepancy · Sep 26, 2024 · N980AT · Boeing 717200 · Standard Practices/Structures
  > -AD RELATED- AMDS 5720-01103-01A: PERFORM STEP 14. SUMMARY NRC 00920: (ET) HFEC INSPECTION WAS PERFORMED. NO CRACKS WERE FOUND PER B717 CARD 5720-01103-01A, STEP 14 AND B717 DC/MD NDT SPM PART 6, 06-10-01.001. ASSOCIATED AA 5720-01103 ADDED FOR AC 9546. (LP #0
- [SDR DALA2024091809135](https://openairdocs.org/sdr/DALA2024091809135.md): Fastener · sheared · Sep 16, 2024 · N980AT · Boeing 717200 · Fuselage Main, Frame
  > FASTENER SHEARED OFF ON FRAME REAR SIDE STA Y=1152 AT AFT ACCESORY COMPARTMENT. SUMMARY OF NRC 00441: FRAME REAR SIDE STA Y=1152 AT AFT ACCESSORY COMPARTMENT WAS REPAIRED PER PRI 619773-14 REV 3 AND ERA 619773-14 REV ORIGINAL, SECTION I: PERMANENT REPAIR. ACCO
- [SDR DALA2024091809134](https://openairdocs.org/sdr/DALA2024091809134.md): Fastener · sheared · Sep 16, 2024 · N980AT · Boeing 717200 · Fuselage Main, Frame
  > FASTENER SHEARED OFF ON FRAME REAR SIDE STA Y=1152 AT AFT ACCESORY COMPARTMENT. SUMMARY OF NRC 00441: FRAME REAR SIDE STA Y=1152 AT AFT ACCESSORY COMPARTMENT WAS REPAIRED PER PRI 619773-14 REV 3 AND ERA 619773-14 REV ORIGINAL, SECTION I: PERMANENT REPAIR. ACCO
- [SDR DALA2024091008882](https://openairdocs.org/sdr/DALA2024091008882.md): Lug · corroded · Sep 9, 2024 · N980AT · Boeing 717200 · Wing, Control Surface Attach Fittings
  > CORROSION ON OUTER/INNER LUGS (INNER PART) AND BUSHING OF LH FLAP OUTBOARD HINGE. SUMMARY OF NRC 00657: CORROSION LEVEL 2. LH FLAP OUTBOARD HINGE WAS REPAIRED PER PRI 619369-14 REV 4 & ER/A 619369-14 REV ORIG. REPAIR APPROVAL IS LIMITED TO 24 MONTHS FROM 29AUG
- [SDR DALA2024082408418](https://openairdocs.org/sdr/DALA2024082408418.md): Fuel Cell · corroded · Aug 23, 2024 · N980AT · Boeing 717200 · Fuel Storage
  > AIRCRAFT 9546, 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. CORRECTIVE ACTION: LOWER SKIN OF THE CENTRAL TANK APPROX. STA. Y=748 AND STA XCW=-25 AND Z=-29 WAS REPAIRED PER
- [SDR DALA2024081608210](https://openairdocs.org/sdr/DALA2024081608210.md): Pan · cracked · Aug 15, 2024 · N980AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON INNER PAN WAS FOUND ON BEAM 4 FWD EDGE AT FWD CARGO COMPARTMENT DOOR. SUMMARY OF NRC 00674: INNER PAN ON BEAM 4 FWD EDGE AT FWD CARGO COMPARTMENT DOOR WAS REPAIRED PER ER/A 619393-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 619393-14 REV 3. AS
- [SDR DALA2024081508167](https://openairdocs.org/sdr/DALA2024081508167.md): Pan · cracked · Aug 15, 2024 · N980AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK (3 EA) ON OUTER PAN AT BEAM #3, #4, AND #5 INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT DOOR. SUMMARY OF NRC-00141: OUTER PAN AT BEAM #3, #4, AND #5 INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT DOOR WAS REPAIRED PER ERA 619498-14 REV ORIGINAL. ASSOCIATED E
- [SDR DALA2024081208005](https://openairdocs.org/sdr/DALA2024081208005.md): Housing · cracked · Aug 9, 2024 · N980AT · Boeing 717200 · Passenger/Crew Doors
  > CRACK AT SETTLEMENT AREA OF HANDLE HOUSING WAS FOUND WHILE HOUSING REMOTION DOOR L1. SUMMARY OF NRC 00708: EXTERNAL SKIN ON SETTLEMENT AREA OF HANDLE HOUSING AT PASSENGER DOOR L1 WAS REPAIRED PER ER/A 619355-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI
- [SDR DALA2024080907921](https://openairdocs.org/sdr/DALA2024080907921.md): Cap · corroded · Aug 9, 2024 · N980AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK X=22 STA Y=197-225, -X=44.5 Y=200-237, AND FLOOR SUPPORT AT -X=54.5 Y=210. SUMMARY OF NRC 00719: CORROSION LEVEL 2. SEAT TRACK X=22 STA Y=197-225, AND SEAT TRACK -X=44.5 Y=200-237, WERE REPAIRED PER B717-200 SRM 53-20-52-2R PROCEDURE 5
- [SDR DALA2024080807882](https://openairdocs.org/sdr/DALA2024080807882.md): Frame · cracked · Aug 6, 2024 · N980AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK ON FRAME STA Y=694 LH SIDE AT CANTED KEEL INTERNAL STRUCTURE. SUMMARY OF NRC 00340: LH SIDE FRAME STA Y=694 INBOARD EDGE WAS REPAIRED PER B717-200 SRM 51-70-11-2R PROCEDURE 1 REPAIR 1 AND OUTBOARD EDGE WAS REPAIRED PER ERA 545683-14MA REV ORIGINAL. ASSOC
- [SDR DALA2024080707851](https://openairdocs.org/sdr/DALA2024080707851.md): Frame · cracked · Aug 6, 2024 · N980AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK ON FRAME STA Y=694 LH SIDE AT CANTED KEEL INTERNAL STRUCTURE. SUMMARY OF NRC 00340: LH SIDE FRAME STA Y=694 INBOARD EDGE WAS REPAIRED PER B717-200 SRM 51-70-11-2R PROCEDURE 1 REPAIR 1 AND OUTBOARD EDGE WAS REPAIRED PER ERA 545683-14MA REV ORIGINAL. (LP #
- [SDR DALA2024080607839](https://openairdocs.org/sdr/DALA2024080607839.md): Cusp Web · corroded · Aug 5, 2024 · N980AT · Boeing 717200 · Fuselage Main, Frame
  > CORROSION ON CUSP WEB MEMBRANE STA 565 X=- 59, STA 576 X=-58, STA 579-589 X=-60 AND X=-58 (UPPER AND UNDER), STA 589-617 X=-57 AND X=-59, STA 636 X=-49, STA 647 X=-58 AT PAX CAB. SUMMARY OF NRC 00491: CORROSION LEVEL 2. CUSP WEB MEMBRANE STA 565 X=-59, STA 579
- [SDR DALA2024072907539](https://openairdocs.org/sdr/DALA2024072907539.md): Cusp Web · corroded · Jul 27, 2024 · N980AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON CUSP WEB MEMBRANE STA Y=794 TO Y=813, X=-44 X=-60, AND Y=832/Y=835 AND X=-57. ALSO, CORROSION ON THE REPAIR DOUBLER OF THE CUSP WEB MEMBRANE STA Y= 865 TO Y=870, X=-53 TO X=-60. CABIN PAX. SUMMARY OF NRC 00764: CORROSION LEVEL 2. CUSP WEB MEMBRANE
- [SDR DALA2024072607477](https://openairdocs.org/sdr/DALA2024072607477.md): Frame · cracked · Jul 25, 2024 · N980AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK ON FRAME STA Y=1037 AND STR 17 RH AT C PAX. SUMMARY OF NRC 00360: FRAME STA Y=1037 AND STR 17 RH WAS REPAIRED PER B717 SRM 53-20-07-2R REP 4. (LP #0466007)
- [SDR DALA2024072407442](https://openairdocs.org/sdr/DALA2024072407442.md): Door Frame · corroded · Jul 24, 2024 · N980AT · Boeing 717200 · Fuselage Main, Structure
  > CORROSION ON DOOR JAMB BTW STA Y=387-408 AT FWD CARGO COMPARTMENT DOOR. SUMMARY OF NRC 00079: CORROSION LEVEL 2. DOOR JAMB BTW STA Y=387-408 AT FWD CARGO COMPARTMENT DOOR WAS REPAIRED PER B717-200 SRM 53-20-15-2R PROCEDURE 6 REPAIR 6. (LP #0462776)
- [SDR DALA2024072407441](https://openairdocs.org/sdr/DALA2024072407441.md): Skin · cracked · Jul 23, 2024 · N980AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACK ON EDGE EXTERNAL FUSELAGE SKIN STA Y=991 BTW LONGERON 26-24R AT FUSELAGE. SUMMARY OF NRC 00075: CRACK ON EDGE EXTERNAL FUSELAGE SKIN STA Y=991 BTW LONGERON 26-24R AT FUSELAGE WAS REPAIRED PER B717 SRM 53-20-15-2R PROCEDURE 12. (LP #0461829)
- [SDR DALA2024072307416](https://openairdocs.org/sdr/DALA2024072307416.md): Cusp Web · cracked · Jul 22, 2024 · N980AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON CUSP WEB MEMBRANE STA 403 X=-58 AT PAX CAB. SUMMARY OF NRC 00498: CUSP WEB MEMBRANE STA 403 X=-58 AT PAX CAB WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4, REPAIR 4, FIGURE 212. (LP #0460928)
- [SDR DALA2024072307415](https://openairdocs.org/sdr/DALA2024072307415.md): Longeron · cracked · Jul 22, 2024 · N980AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CRACK ON RH LONGERONS 4 AND 6 STA Y=1022 AT C PAX. SUMMARY OF NRC 00363: CRACK ON RH LONGERONS 4 AND 6 STA Y=1022 AT C PAX WERE REPAIRED PER B 717-200 S.R.M. 53-00-05-2R REPAIR 2. (LP #0460780)
- [SDR DALA2024072207314](https://openairdocs.org/sdr/DALA2024072207314.md): Cusp Web · corroded · Jul 20, 2024 · N980AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON CUSP WEB MEMBRANE BTW STA Y=483 AND X=55 AT CPAX. SUMMARY OF NRC 00488: CORROSION LEVEL 2. CUSP WEB MEMBRANE BTW STA Y=483 AND X=55 AT CPAX WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 FIG 213. (LP #0457527)
- [SDR DALA2024072207313](https://openairdocs.org/sdr/DALA2024072207313.md): Web · corroded · Jul 19, 2024 · N980AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON WEB MEMBRANE STA Y=185-Y=200. SUMMARY OF NRC 00827: CORROSION LEVEL 2. WEB MEMBRANE STA Y=185-Y=200 WAS REPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 2 REP 2. (LP #0456066)
- [SDR DALA2024071707229](https://openairdocs.org/sdr/DALA2024071707229.md): Cusp Web · corroded · Jul 17, 2024 · N980AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION OUT OF LIMITS ON RH CUSP WEB STA 896-904 X=-58 PER B717-200 SRM 53-00-55-1A PROCEDURE 1 ALLOWABLE DAMAGE 1 PAR 4.A. SUMMARY OF NRC S/N 00711: CORROSION LEVEL 2. RH CUSP WEB STA 896 -904 X=-58 WAS REPAIRED PER B717-200 SRM 53-00-55-2R REPAIR 4 FIGURE
- [SDR DALA2024071707228](https://openairdocs.org/sdr/DALA2024071707228.md): Seat Track · corroded · Jul 17, 2024 · N980AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK BTW STA Y=265-301 COORDINATE X=-22. SUMMARY OF NRC 00672: CORROSION LEVEL 2. SEAT TRACK BTW STA Y=265-301 COORDINATE X=-22 WAS REPAIRED PER B717-200 SRM 53-20-52-2R PROCEDURE 5, REPAIR 5, PAR 4, FIG 201. (LP #0451567)

Next page: https://openairdocs.org/aircraft/N980AT/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 = 'N980AT' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N980AT/reports

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