# Service difficulty reports: N971AT

A list on [N971AT](https://openairdocs.org/aircraft/N971AT.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 · 229 reports

- [SDR DALA2026092405329](https://openairdocs.org/sdr/DALA2026092405329.md): Bracket · loose · Sep 24, 2026 · N971AT · Boeing 717200 · Emergency Equipment
  > R1 GIRT BAR DISARM BRACKET LOOSE, REMOVED & REINSTALLED SLIDE IAW W/C 2561-9005 AND R & R EVACUATION SLIDE COMPARTMENT DOOR IAW AMM 52-42. (9504750) (AIRCRAFT GROUNDED).
- [SDR DALA2026012700605](https://openairdocs.org/sdr/DALA2026012700605.md): Hinge Fitting · corroded · Dec 7, 2025 · N971AT · Boeing 717200 · Trailing Edge Flaps
  > CORROSION ON HARWARE AND AROUND OF BORE IN OTBD HINGE. LT WING FLAP. THE OTBD FLAP HINGE WAS REPLACED IAW AMM 57-55-25. (1340373)
- [SDR DALA2025121009009](https://openairdocs.org/sdr/DALA2025121009009.md): Skin · cracked · Dec 5, 2025 · N971AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACKS ON FUSELAGE SKIN ON BS 1037 & 1022, L12R & L14R AT RH FUSELAGE. DAMAGED AREA REPAIRED PER ER/A 630558-14 REV.ORIG. (1337089)
- [SDR DALA2025120808960](https://openairdocs.org/sdr/DALA2025120808960.md): Skin · cracked · Dec 1, 2025 · N971AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACK ON FUSELAGE SKIN BS 1037, BTW L-14L AND L-13L. FUSELAGE SKIN BS 1037 BTW L-14L AND L-13L WAS REPAIRED IAW PRI 630562-14 REV 5 AND ER/ A 630562-14 REV. (1330895)
- [SDR DALA2025112408546](https://openairdocs.org/sdr/DALA2025112408546.md): Skin · cracked · Nov 24, 2025 · N971AT · Boeing 717200 · Nacelle/Pylon, Plate/Skin
  > AIRCRAFT 9533, CRACK ON PANEL UPPER SKIN AREA STA Y= 1142 OF LH AND RH PYLON. CORRECTIVE ACTION: PANEL UPPER SKIN AREA STA Y= 1142 OF LH AND RH PYLON WERE REPAIRED PER B717-200 SRM 54-00-00-2R REPAIR 1. (LP 1318816)
- [SDR DALA2025061604511](https://openairdocs.org/sdr/DALA2025061604511.md): Wire · broken · Jun 16, 2025 · N971AT · Boeing 717200 · Light System Wiring
  > AIRCRAFT 9533, EMER EXIT SIGN FWD OF PAX DOOR LOWER INOP. CORRECTIVE ACTION: FOUND BROKEN WIRE AT CONNECTOR OF EMER EXIT LIGHT. REPAIRED CONNECTOR IAW 717 SWPM 20-31. (LP 7475133)
- [SDR DALA2025062504755](https://openairdocs.org/sdr/DALA2025062504755.md): Drain Valve · leaking · May 25, 2025 · N971AT · Boeing 717200 · Fuel Storage
  > AFT BAG BIN HAS FUEL SMELL. FOUND FUEL DRAIN FROM FUEL SHROUD DRAIN VALVE BEHIND RT WHEEL WELL. CLEANING BELOW FLOOR. CHECK GOOD (6811338)
- [SDR DALA2025020500883](https://openairdocs.org/sdr/DALA2025020500883.md): Lamp · failed · Feb 5, 2025 · N971AT · Boeing 717200 · Emergency Lighting
  > THE LEFT AND RIGHT EXTERIOR EMERGENCY LIGHTS DIM WITH THE SWITCH OFF. THE SYSTEM WAS DEFERRED PER MEL 33-51-02A AND PLACARDS WERE INSTALLED. MAINTENANCE VERIFIED 2232 LAMPS WERE INSTALLED PER B-717 IPC 33-50-30-01 ITEM #130J. (NOTE: LEFT LAMP IS BAD, NASI BWI)
- [SDR DALA2023120409902](https://openairdocs.org/sdr/DALA2023120409902.md): Unknown · unknown · Dec 2, 2023 · N971AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON PAN FWD/AFT INTERNAL UPPER EDGE AT LH FWD PASSENGER DOOR (L1). SUMMARY OF NRC 00095: PAN FWD/AFT INTERNAL UPPER EDGE AT LH FWD PASSENGER DOOR (L1) WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 3. IN THE PROCESS, DOOR REMOVAL/INSTALL WAS NEEDED A
- [SDR DALA2023112909803](https://openairdocs.org/sdr/DALA2023112909803.md): Unknown · unknown · Nov 29, 2023 · N971AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CORROSION ON LONGERON TERMINAL 25R STA Y=946 AFT CARGO COMPARTMENT (C1). SUMMARY OF NRC 00730: CORROSION LEVEL 2. LONGERON TERMINAL 25R STA Y=946 AFT CARGO COMPARTMENT WAS REPLACED PER B717-SRM 51-41-05-0G. (LP #0086710)
- [SDR DALA2023112909800](https://openairdocs.org/sdr/DALA2023112909800.md): Unknown · unknown · Nov 28, 2023 · N971AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON WING BOX UPPER SURFACE STA Y=684 X=-59. SUMMARY OF NRC 00398: CORROSION LEVEL 2. WING BOX UPPER SKIN SURFACE STA Y=684 X=-59 WAS REPAIRED PER ER/A 612910-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-612910 ADDED FOR AC 9533. (LP
- [SDR DALA2023112809757](https://openairdocs.org/sdr/DALA2023112809757.md): Unknown · unknown · Nov 27, 2023 · N971AT · Boeing 717200 · Cargo/Baggage Doors
  > CRACK ON PAN (2 EA) AFT UPPER SIDE BEAM 5, STA Y 425 APROX FWD UPPER SIDE STA Y 389 APROX (HINGE DOOR) AT FWD CARGO DOOR. SUMMARY OF NRC 00137: PAN AFT UPPER SIDE BEAM 5, STA Y 425 APROX FWD UPPER SIDE STA Y 389 APROX (HINGE DOOR) AT FWD CARGO DOOR WAS REPAIRE
- [SDR DALA2023112809754](https://openairdocs.org/sdr/DALA2023112809754.md): Unknown · unknown · Nov 27, 2023 · N971AT · Boeing 717200 · Horizontal Stabilizer, Plate/Skin
  > CORROSION ON HOLE UPPER SURFACE NBR 28 AT RH HORIZONTAL STABILIZER CENTER BOX PLATE. SUMMARY OF NRC 00492: CORROSION LEVEL 2. HOLE UPPER SURFACE NBR 28 AT RH HORIZONTAL STABILIZER CENTER BOX PLATE WAS REPAIRED PER PRI 612928-14 REV 6 AND ER/A 612928-14 REV ORI
- [SDR DALA2023112709721](https://openairdocs.org/sdr/DALA2023112709721.md): Unknown · unknown · Nov 23, 2023 · N971AT · Boeing 717200 · Fuselage Main, Structure
  > CRACK ON INNER SKIN WAS FOUND ON UPPER AFT CORNER AT RH SLIDING WINDOW CUTOUT. SUMMARY OF NRC 00706: CRACK ON UPPER AFT CORNER AT RH SLIDING WINDOW CUTOUT INNER SKIN WAS REPAIRED PER ER/A 613654-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-6
- [SDR DALA2023112009517](https://openairdocs.org/sdr/DALA2023112009517.md): Unknown · unknown · Nov 16, 2023 · N971AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION (SEVERAL PLACES) ON TIE TRACK UPPER AND LOWER FACE BTW LONGERONS 27 TO 28 LH/RH BTW STA 817 TO STA=946 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00357: CORROSION LEVEL 2. TIE TRACK UPPER AND LOWER FACE BTW LONGERONS 27 TO 28 LH/RH BTW STA 817 TO STA=9
- [SDR DALA2023111609442](https://openairdocs.org/sdr/DALA2023111609442.md): Unknown · unknown · Nov 16, 2023 · N971AT · Boeing 717200 · Fuselage Main, Structure
  > CORROSION ON LOWER DOOR JAMB FROM STA 954 TO STA 994 AT AFT CARGO (C2). SUMMARY OF NRC 00160: CORROSION LEVEL 2. LOWER DOOR JAMB FROM STA 954 TO STA 994 AT AFT CARGO (C2) WAS REPAIR PER B717 SRM 53-20-15-2R-7. (LP #0067279)
- [SDR DALA2023111609440](https://openairdocs.org/sdr/DALA2023111609440.md): Unknown · unknown · Nov 16, 2023 · N971AT · Boeing 717200 · Fuselage Main, Frame
  > CORROSION ON FRAME STA 889.0 BTW LONG 28RH TO 28LH AT AFT CARGO COMPARTMENT IN REF TO NRC 00254. SUMMARY OF NRC S/N 00654: CORROSION LEVEL 2. FRAME AT STA 889.0 BTW LONG 28RH TO 28LH AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717 SRM 53-20-07-2R REP. 3, 51-41-
- [SDR DALA2023111609438](https://openairdocs.org/sdr/DALA2023111609438.md): Unknown · unknown · Nov 15, 2023 · N971AT · Boeing 717200 · Wing, Plate/Skin
  > CORROSION ON UPPER SKIN STA XOS 395 AT RH WING. SUMMARY OF NRC 00080: CORROSION LEVEL 2. UPPER SKIN STA XOS 395 AT RH WING WAS REPAIRED PER ER/A 612778-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 612778-14 REV 2. ASSOCIATED ER/A 14-612778 ADDED FOR AC
- [SDR DALA2023111409354](https://openairdocs.org/sdr/DALA2023111409354.md): Unknown · unknown · Nov 14, 2023 · N971AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACK ON INNER SKIN WAS FOUND ON UPPER AFT CORNER AT LH SLIDING WINDOW CUTOUT. SUMMARY OF NRC 00707: CRACK ON INNER SKIN ON UPPER AFT CORNER AT LH SLIDING WINDOW CUTOUT WAS REPAIRED PER B-717 SRM 56-10-02-2R PROCEDURE 1, REPAIR 1. (LP #0063939)
- [SDR DALA2023111309306](https://openairdocs.org/sdr/DALA2023111309306.md): Unknown · unknown · Nov 13, 2023 · N971AT · Boeing 717200 · Fuselage Main, Structure
  > CORROSION ON LOWER DOOR JAMB FROM STA 370 STA 427 AT FWD CARGO (C1). SUMMARY OF NRC 00222: CORROSION LEVEL 2. LOWER DOOR JAMB FROM STA 370 STA 427 AT FWD CARGO (C1) WAS REPAIRED PER B717 SRM 53-20-15-2R REPAIR 6. (LP #0062282)
- [SDR DALA2023111309305](https://openairdocs.org/sdr/DALA2023111309305.md): Unknown · unknown · Nov 11, 2023 · N971AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CORROSION ON UNION SKIN BTW STA=908 TO STA=948 LONGERON 26 LH AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00702: CORROSION LEVEL 2. UNION SKIN (FINGER DOUBLER) BTW STA=908 TO STA=948 LONGERON 26 LH AT AFT CARGO COMPARTMENT WAS FABRICATED AND INSTALLED PER B-717 S
- [SDR DALA2023111309300](https://openairdocs.org/sdr/DALA2023111309300.md): Unknown · unknown · Nov 10, 2023 · N971AT · Boeing 717200 · Fuel Storage
  > EXFOLIATION UPPER SKIN OF CENTRAL TANK ON REAR SPAR AREA STA Y=748 AND STA XCW 1 TO 3, XCW 24 TO 26, ALSO XCW 42 TO 52 APROX AT LH MLG WHELLWELL. SUMMARY OF NRC 00195: CORROSION LEVEL 2. UPPER SKIN OF CENTRAL TANK ON REAR SPAR AREA STA Y=748 AND STA XCW 1 TO 3
- [SDR DALA2023111309299](https://openairdocs.org/sdr/DALA2023111309299.md): Unknown · unknown · Nov 10, 2023 · N971AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CORROSION ON FUSELAGE SKIN EXTERNAL SURFACE (SETTLEMENT AREA OF FUSELAGE FILLET FARING 150RL) BTW STA 851-870 LONG 28L IN REF TO NRC 00671. SUMMARY OF NRC 00705: CORROSION LEVEL 2. FUSELAGE SKIN EXTERNAL SURFACE (SETTLEMENT AREA OF FUSELAGE FILLET FARING 150RL
- [SDR DALA2023111309297](https://openairdocs.org/sdr/DALA2023111309297.md): Unknown · unknown · Nov 9, 2023 · N971AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION SKIN WEB STA=201 BTW LONG 18LH TO 17LH ALSO CORROSION ON HORIZONTAL STRAP BTW STA Y=201-208 AT PAX CABIN. SUMMARY OF NRC 00674: CORROSION LEVEL 2. SKIN WEB STA=201 BTW LONG 18LH TO 17LH WAS REPAIRED PER ERA 613271-14 REV ORIGINAL SECTION I. PERMANENT
- [SDR DALA2023110609115](https://openairdocs.org/sdr/DALA2023110609115.md): Unknown · unknown · Nov 4, 2023 · N971AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK X=-44 BTW STA 218 TO STA 237 AT PAX CABIN. SUMMARY OF NRC 00553: CORROSION LEVEL 2. SEAT TRACK AT X=-44 BTW Y=200 TO 341 WAS DRILLED, ADJUSTED, AND REPLACED PER B717 SRM 51 -41-01-0G, PAR 6, 51-41-02-0G, 51-41-05-0G PAR 8, AND 51-40-08-
- [SDR DALA2023110108978](https://openairdocs.org/sdr/DALA2023110108978.md): Unknown · unknown · Nov 1, 2023 · N971AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > WEAR AND CORROSION WAS FOUND ON FLOOR SUPPORT STA Y=674 AND X=56 AT PAX CABIN. SUMMARY OF NRC 00678: CORROSION LEVEL2. FLOOR SUPPORT STA Y=674 AND X=56 AT PAX CABIN WAS REPLACED PER B717-200 SRM 51-41-02-0G. (LP #0044262)
- [SDR DALA2023110108977](https://openairdocs.org/sdr/DALA2023110108977.md): Unknown · unknown · Oct 31, 2023 · N971AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK ON FRAME STA Y=1037 LONGERON 17 LH AT CPAX (W2). SUMMARY OF NRC 00407: FRAME STA 1037 LONGERON 17 LH AT CPAX WAS REPAIRED PER B-717-200 SRM 53-20-07-2R REPAIR 4. (LP #0043842)
- [SDR DALA2023110108975](https://openairdocs.org/sdr/DALA2023110108975.md): Unknown · unknown · Oct 31, 2023 · N971AT · Boeing 717200 · Fuselage Main, Frame
  > HFEC INSPECTION WAS PERFORMED ON UPPER RADIUS OF THE FRAME TAB STA Y=715 AND 01 CRACK WAS FOUND OF 0.097IN. PER CARD 5310-01436-04B. STEP 13. SUMMARY OF NRC 00194: FRAME STA 715 LH WAS REPAIRED PER AMDS CARD 5310-01436-02A. STEPS 4,7,10,14,15,16, AND 17. ASSOC
- [SDR DALA2023103108930](https://openairdocs.org/sdr/DALA2023103108930.md): Unknown · unknown · Oct 30, 2023 · N971AT · Boeing 717200 · Trailing Edge Flaps
  > DENT ON PREVIOUS REPAIR AT LH AFT MOVABLE FLAP VANE. SUMMARY OF NRC 00539: LH AFT MOVABLE FLAP VANE WAS REPAIRED PER B717-200 SRM 57-53-01-2R-1, 51-70-02-2R-3, AND 51-70-02-0G REPAIR GENERAL. (LP #0041842)
- [SDR DALA2023103108929](https://openairdocs.org/sdr/DALA2023103108929.md): Unknown · unknown · Oct 30, 2023 · N971AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK WAS FOUND ON WEB BTW STA Y=715 TO 756 X=44 TO X=60. SUMMARY OF NRC 00601: WEB BTW STA Y=715 TO 756 X=44 TO X=60 WAS REPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 2 REPAIR 2. (LP #0041807)
- [SDR DALA2023103008883](https://openairdocs.org/sdr/DALA2023103008883.md): Unknown · unknown · Oct 30, 2023 · N971AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON CUSP WEB BTW STA Y=589 AND X=-46 AT PAX CABIN. SUMMARY OF NRC 00393: CUSP WEB BTW STA Y=589 AND X=-46 AT PAX CABIN WAS MANUFACTURED AND REPAIRED PER DGW 9910151-116 PER B717 -200 SRM 53-00-55-2R-4 REPAIR 4 FIG 226. (LP #0041174)
- [SDR DALA2023103008881](https://openairdocs.org/sdr/DALA2023103008881.md): Unknown · unknown · Oct 29, 2023 · N971AT · Boeing 717200 · Fuselage Main, Bulkhead
  > WEAR AND DENT ON RH LOWER ANGLE NEAR TO LOWER HINGE AT AFT CABIN PRESSURE BULKHEAD EMERGENCY EXIT DOOR. SUMMARY OF NRC 00110: RH LOWER ANGLE NEAR TO LOWER HINGE AT AFT CABIN PRESSURE BULKHEAD EMERGENCY EXIT DOOR WAS REPAIRED PER B717-200 SRM 52-10-02-2R-16 AND
- [SDR DALA2024022002331](https://openairdocs.org/sdr/DALA2024022002331.md): Hinge · corroded · Oct 28, 2023 · N971AT · Boeing 717200 · Trailing Edge Flaps
  > CORROSION WAS FOUND AT HINGE HOLES AT LH WING. SUMMARY NRC 00598: FLAP HINGE WAS REPLACED PER B717-200 AMM 57-55-25 AND EFECTIVITY WAS VERIFIED PER B717-200 IPC 57-51-32-01. (LP #0039472)
- [SDR DALA2023103008880](https://openairdocs.org/sdr/DALA2023103008880.md): Unknown · unknown · Oct 28, 2023 · N971AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON LH FLOOR SUPPORTS BTW STA 160 TO STA 196 BTW X=43, STA 196 TO STA 200 BTW X=53. SUMMARY OF NRC 00683: CORROSION LEVEL 2. FLOOR SUPPORT STA 160 TO STA 196 BTW X=43 WAS ADJUSTED AND DRILLED PER B717-200 51-40-08-0G AND FLOOR SUPPORT STA 196 TO STA 2
- [SDR DALA2023103008879](https://openairdocs.org/sdr/DALA2023103008879.md): Unknown · unknown · Oct 28, 2023 · N971AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK ON FRAME STA Y=1037 LONGERON 17 RH AT CPAX (W2). SUMMARY OF NRC 00408: FRAME STA Y=1037 LONGERON 17 RH AT CPAX (W2) WAS REPAIRED PER B717-200 SRM-53-20-07-2R-4. (LP #0039065)
- [SDR DALA2023103008878](https://openairdocs.org/sdr/DALA2023103008878.md): Unknown · unknown · Oct 28, 2023 · N971AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON SUPPORT BTW STA Y=1056-1022 X=-54 AT CPAX. SUMMARY OF NRC 00672: CORROSION LEVEL 2. SUPPORT BTW STA Y=1056-1022 X=-54 WAS FABRICATED AND REPLACED PER DRAWING 9981474 REV H, B717-200 SRM 51-41-02-0G AND 51-41-05-0G PAR 8. (LP #0038822)
- [SDR DALA2023102708864](https://openairdocs.org/sdr/DALA2023102708864.md): Unknown · unknown · Oct 26, 2023 · N971AT · Boeing 717200 · Cargo/Baggage Doors
  > WEAR ON PAN STA 954 AND 990 BETWEEN BEAM 1 AND BEAM 2 OF DOOR STRUCTURE AT AFT CARGO COMPARTMENT DOOR C2. SUMMARY OF NRC 00134: INNER PAN ON STA 954 AND 990 BETWEEN BEAM 1 AND BEAM 2 OF DOOR STRUCTURE AT AFT CARGO COMPARTMENT DOOR C2 WAS REPAIRED PER B717-200
- [SDR DALA2023102608796](https://openairdocs.org/sdr/DALA2023102608796.md): Unknown · unknown · Oct 25, 2023 · N971AT · Boeing 717200 · Fuselage Main, Structure
  > CRACK ON INNER PAN (2 EA) BEAM 5 UPPER FWD SIDE, BEAM 3 AFT SIDE AT FWD CARGO DOOR COMPARTMENT. SUMMARY OF NRC 00146: INNER PAN (2 EA) ON BEAM 5 UPPER FWD SIDE AND ON BEAM 3 AFT SIDE AT FWD CARGO DOOR COMPARTMENT WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCE
- [SDR DALA2023102508760](https://openairdocs.org/sdr/DALA2023102508760.md): Unknown · unknown · Oct 25, 2023 · N971AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON WEB, BOTH SIDES, BTW STA 178 TO STA 218, BTW X=-44 AND -52 RH SIDE AT CPAX. SUMMARY OF NRC 00366: CORROSION LEVEL 2. CUSP WEB BTW STA 178 TO STA 218, BTW X=-44 AND -52 RH SIDE WAS REPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 1 REPAIR 1 FIG 201.
- [SDR DALA2023102308702](https://openairdocs.org/sdr/DALA2023102308702.md): Unknown · unknown · Oct 19, 2023 · N971AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK ON CUSP WEB STA 636 AND X=50 AT CPAX. SUMMARY OF NRC 00396: CUSP WEB WAS REPAIRED PER B717 SRM 51-70-10 2R PROCEDURE 2 PAR 4. (LP #0025277)
- [SDR DALA2023102008642](https://openairdocs.org/sdr/DALA2023102008642.md): Unknown · unknown · Oct 19, 2023 · N971AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON CUSP WEB STA Y=341 WAS FOUND AFTER SEAT TRACK STA Y=-44 REMOVAL. SUMMARY OF NRC 00606: CUSP WEB STA Y=-44 STA Y=341 WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 FIGURE 221. (LP #0025272)
- [SDR DALA2023102008638](https://openairdocs.org/sdr/DALA2023102008638.md): Unknown · unknown · Oct 18, 2023 · N971AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON CUSP WEB (BELOW) BTW STA Y=252 AND X=-46 AT CABIN PAX. SUMMARY OF NRC 00390: CUSP WEB STA Y=252 AND X=-46 WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4-REPAIR 4 FIG 221. (LP #0023628)
- [SDR DALA2023071805820](https://openairdocs.org/sdr/DALA2023071805820.md): Unknown · unknown · Jul 18, 2023 · N971AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKE DAMAGE LOCATED ON STATION 1166, LH SIDE OF FUSELAGE. (LABELED #7) COMPLIED WITH ER/A 610530-14 REV ORIG. ALL PRI REVISION INSTRUCTIONS ARE COMPLIED WITH AND MATCH FINALE ER/A 610530-14 REV ORIG SECTION I PERMANENT REPAIR INSTRUCTIONS. FUSELAGE
- [SDR DALA2023071705782](https://openairdocs.org/sdr/DALA2023071705782.md): Unknown · unknown · Jul 17, 2023 · N971AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKE DAMAGE LOCATED BETWEEN STATION 487 AND STRINGER 28L. (LABELED #1) REPAIRED SKIN DAMAGE LOCATED BETWEEN STATION 487 AND STRINGER 28L PER B717 SRM 53-03-01-2R PROCEDURE 1. CLASS II REPAIR ZONE 1. EXTERNAL LFEC OR EXTERNAL ULTRASONIC INITIAL INSP
- [SDR DALA2022061604217](https://openairdocs.org/sdr/DALA2022061604217.md): Power Supply · inoperative · Jun 14, 2022 · N971AT · Boeing 717200 · Emergency Lighting
  > THE LEFT AFT OVERWING EXIT ILLUMINATOR IS INOPERATIVE. MAINTENANCE REPLACED THE LEFT OVERWING EXIT POWER SUPPLY. OPERATIONAL CHECK WAS GOOD REF B717 AMM 33-51-06. (LP #8628970)
- [SDR DALA2022061604218](https://openairdocs.org/sdr/DALA2022061604218.md): Anti-Skid Sys · warning message · Jun 13, 2022 · N971AT · Boeing 717200 · Brake Anti-Skid Section
  > SHIP 9533 - DUE TO THE "ANTI-SKID FAIL" MESSAGE CYCLING ON & OFF AT LEAST THREE TIMES ON APPROACH, A GO-AROUND WAS EXECUTED. THE MESSAGE HAPPENED AGAIN ON THE SECOND APPROACH, SO THE FLIGHT CREW DECLARED AN EMERGENCY AND LANDED UNEVENTFULLY. THIS IS A REPEAT O
- [SDR DALA2022061604219](https://openairdocs.org/sdr/DALA2022061604219.md): Anti-Skid Sys · warning message · Jun 12, 2022 · N971AT · Boeing 717200 · Brake Anti-Skid Section
  > SHIP 9533 - WHILE ON APPROACH, THE CREW NOTICED THE "ANTI-SKID FAIL" MESSAGE WAS CYCLING ON & OFF. A GO-AROUND WAS EXECUTED, BUT MESSAGE PERSISTED SO AN EMERGENCY WAS DECLARED BY ATC. THE LANDING WAS UNEVENTFUL. CORRECTIVE ACTION: CONTRACT MAINTENANCE PERFORME
- [SDR DALA2022051903435](https://openairdocs.org/sdr/DALA2022051903435.md): None · none · May 17, 2022 · N971AT · Boeing 717200 · Brake Anti-Skid Section
  > SHIP 9533 - THE CREW DECLARED AN EMERGENCY FOR AN ANTI-SKID FAIL MESSAGE ON FINAL APPROACH. THE QRH WAS COMPLIED WITH, AND ON THE NEXT APPROACH, THE FAILURE MESSAGE DID NOT RETURN. CORRECTIVE ACTION: MAINTENANCE REPLACED THE LEFT LANDING GEAR INTERLOCK RELAY (
- [SDR DALA2021121607776](https://openairdocs.org/sdr/DALA2021121607776.md): None · none · Dec 14, 2021 · N971AT · Boeing 717200 · Landing Gear Position and Warning
  > SHIP 9533 - THE FLIGHT CREW DECLARED AN EMERGENCY DUE TO THE "RT GEAR UNSAFE" INDICATION ILLUMINATING SHORTLY AFTER TAKEOFF. ON APPROACH, THE GEAR WAS SELECTED DOWN AND THREE GREEN "DOWN & LOCKED" INDICATIONS ILLUMINATED. CORRECTIVE ACTION: THE AIRCRAFT WAS FE
- [SDR DALA2021111206965](https://openairdocs.org/sdr/DALA2021111206965.md): None · none · Nov 11, 2021 · N971AT · Boeing 717200 · Emergency Lighting
  > THE OVERHEAD CABIN CEILING EMERGENCY LIGHTS ARE OUT AT ROWS 1-4 AND 10-13CDE. MAINTENANCE REPLACED THE BATTERY PACK AT 10CDE PER B717 AMM 33-51. THE EMERGENCY LIGHTS OPERATIONAL CHECK IS GOOD. (LP #5362028)

Next page: https://openairdocs.org/aircraft/N971AT/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 = 'N971AT' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N971AT/reports

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