# Service difficulty reports: N981AT

A list on [N981AT](https://openairdocs.org/aircraft/N981AT.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 · 199 reports

- [SDR DALA2026101905721](https://openairdocs.org/sdr/DALA2026101905721.md): Skin · dented · Oct 18, 2026 · N981AT · Boeing 717200 · Rudder, Plate/Skin
  > FOUND DENT AT VERTICAL STABILIZER RUDDER TAP SKIN, BETWEEN ZRT=5.70 - 30.30, CORRECTIVE ACTION: COMPLIED WITH ER/A 637462-14. (1872819) (AICRAFT GROUNDED).
- [SDR DALA2026101605698](https://openairdocs.org/sdr/DALA2026101605698.md): Sealant · missing · Oct 15, 2026 · N981AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > FOUND CRACKS ON SCUFF PLATE FWD/INBD EDGE AND CENTER SECTION OF AFT CARGO COMPARTMENT ALSO MISSING SEALANT ON SCUFF PLATE FWD CARGO COMPARTMENT, COMPLIED WITH ER/A 542149-14TR. (1867743) (AIRCRAFT GROUNDED).
- [SDR DALA2026101605697](https://openairdocs.org/sdr/DALA2026101605697.md): Door Frame · damaged · Oct 15, 2026 · N981AT · Boeing 717200 · Fuselage Main, Structure
  > FOUND BENTS AND CRACKS ON AFT EDGE OF AFT CARGO DOOR CUTOUT AT Y=984 APPROX. BTW L-24R AND L-26R, REPAIRED AFT EDGE OF AFT CARGO DOOR CUTOUT PER SRM 53-20-15-2R. (1867765) (AIRCRAFT GROUNDED).
- [SDR DALA2026101505659](https://openairdocs.org/sdr/DALA2026101505659.md): Longeron · cracked · Oct 14, 2026 · N981AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > FOUND A CRACK AT LONGERON 2L BS 1133 AT AFT ACCESORY COMPARTMENT, R/R LONGERON PER B717-200 SRM 53-00-05-2R. (1866121) (AIRCRAFT GROUNDED).
- [SDR DALA2026101405653](https://openairdocs.org/sdr/DALA2026101405653.md): Structure · cracked · Oct 14, 2026 · N981AT · Boeing 717200 · Leading Edge Devices
  > CRACK FOUND ON FIXED LEADING EDGE XFS:537 & TORN SEAL, SLAT NR 5 AT RT WING. COMPLIED WITH ER/A 545680-14TR. (1864537) (AIRCRAFT GROUNDED).
- [SDR DALA2026101405652](https://openairdocs.org/sdr/DALA2026101405652.md): Retainer · chafed · Oct 14, 2026 · N981AT · Boeing 717200 · Leading Edge Devices
  > FOUND WEAR DAMAGE ON FIXED LEADING EDGE, XW= 536, CHAFING ON THE OTBD SEAL RETAINER ON SLAT NR 5 AT LT WING. COMPLIED WITH ER/A 545680-14TR. (1864542) (AIRCRAFT GROUNDED).
- [SDR DALA2026091805211](https://openairdocs.org/sdr/DALA2026091805211.md): Skin · damaged · Sep 18, 2026 · N981AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > FOUND EXISTING LIGHTNING STRIKE (PLUG) TEMPORARY REPAIR BETWEEN Y522 AND Y541, 2.750 OTBD STC DOUBLER, COMPLIED WITH ER/A 636812-14. (1818758) (AIRCRAFT GROUNDED).
- [SDR DALA2026091805210](https://openairdocs.org/sdr/DALA2026091805210.md): Repair · interference · Sep 18, 2026 · N981AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > FOUND EXISTING CIRCULAR REINFORCEMENT REPAIR, INTERFERING WITH STC DOUBLER AT Y560 AND STRG L-2R, COMPLIED WITH ER/A 636811-14AD. (1818755) (AIRCRAFT GROUNDED).
- [SDR DALA2026091805209](https://openairdocs.org/sdr/DALA2026091805209.md): Doubler · demodification · Sep 18, 2026 · N981AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > FOUND EXISTING (DEMOD) ANTENNA, INCLUDING AN INTERNAL DOUBLER, INTERFERING WITH STC DOUBLER BETWEEN Y503 TO Y522 AND STRG L-1 TO STRG L-3R, COMPLIED WITH ER/A 636936-14AD. (1818736) (AIRCRAFT GROUNDED).
- [SDR DALA2026091805217](https://openairdocs.org/sdr/DALA2026091805217.md): Plug · temp repair · Sep 17, 2026 · N981AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > FOUND EXISTING LIGHTNING STRIKE (PLUG) TEMPORARY REPAIR BETWEEN Y522 AND Y541, 2.750 OTBD STC DOUBLER, COMPLIED WITH ER/A 636812-14. (1818080) (AIRCRAFT GROUNDED).
- [SDR DALA2026091805216](https://openairdocs.org/sdr/DALA2026091805216.md): Doubler · interference · Sep 17, 2026 · N981AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > FOUND EXISTING CIRCULAR REINFORCEMENT REPAIR, INTERFERING WITH STC DOUBLER (P/N 8485-5310-404-3) AT Y560 AND STRG L-2R, COMPLIED WITH ER/A 636811-14AD. (1817946) (AIRCRAFT GROUNDED).
- [SDR DALA2026091805215](https://openairdocs.org/sdr/DALA2026091805215.md): Doubler · interference · Sep 17, 2026 · N981AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > FOUND EXISTING CIRCULAR REINFORCEMENT REPAIR, INTERFERING WITH STC DOUBLER Y560 AND STRG L-2R, COMPLIED WITH ER/A 636811-14. (1817938) (AIRCRAFT GROUNDED).
- [SDR DALA2026091805214](https://openairdocs.org/sdr/DALA2026091805214.md): Antenna · demodification · Sep 17, 2026 · N981AT · Boeing 717200 · Fuselage Main, Structure
  > FOUND EXISTING (DEMOD) ANTENNA, INCLUDING AN INTERNAL DOUBLER, INTERFERING WITH STC DOUBLER (P/N 8485-5310-404-1) BETWEEN Y503 TO Y522 AND STRG L-1 TO STRG L-3R, COMPLIED WITH ER/A 636936-14. (1817872) (AIRCRAFT GROUNDED).
- [SDR DALA2026072204286](https://openairdocs.org/sdr/DALA2026072204286.md): Slide · unsecure · Jul 22, 2026 · N981AT · Boeing 717200 · Escape Slide
  > L1 DOOR SLIDE CAME LOOSE DURING DOOR OPENING, SECURED 1L DOOR SLIDE IAW AMM 25-61. (8543436) (AIRCRAFT GROUNDED).
- [SDR DALA2026062303739](https://openairdocs.org/sdr/DALA2026062303739.md): Lamp · inoperative · Jun 23, 2026 · N981AT · Boeing 717200 · Emergency Lighting
  > FLIGHT DECK O/H EMERGENCY LIGHT INOP. RELAMPED IAW AMM 33-51-11. (LP 7959221 - AIRCRAFT WAS GROUNDED)
- [SDR DALA2025100807327](https://openairdocs.org/sdr/DALA2025100807327.md): Sealant · not reported · Oct 2, 2025 · N981AT · Boeing 717200 · Wing Structure
  > WORKING ERA 629612-14AD REV ORIG STEPS 18-20 NEED TO BE ACCOMPLISHED. C/W STEP 18 OF ERA 629612-14AD REV ORIG, RESTORED SEALANT REMOVED FOR INSPECTIONS PER B717 51-24-00 & DWG'S. C/W STEP 19 OF ERA 629612-14AD (1239562)
- [SDR DALA2025100807326](https://openairdocs.org/sdr/DALA2025100807326.md): Skin · leaking · Oct 2, 2025 · N981AT · Boeing 717200 · Wing, Plate/Skin
  > WORKING PRI 629612-14, RH WING LOWER SKIN XRS 164 FUEL SEEP. C/W SECTION I LEAK EVALUATION OF ERA 629612-14AD (1231435)
- [SDR DALA2025092907061](https://openairdocs.org/sdr/DALA2025092907061.md): Cover · missing · Sep 26, 2025 · N981AT · Boeing 717200 · Leading Edge Devices
  > LEFT WING HAS ONE LOWER SLAT TRACK COVER MISSING. FWD TO CDL 57-47-03. PLAC. INSTALLED. (7709014)
- [SDR DALA2025010900177](https://openairdocs.org/sdr/DALA2025010900177.md): Pin · out of position · Jan 8, 2025 · N981AT · Boeing 717200 · Aerodynamic Fairings
  > TAIL CONE EXIT RELEASE CAM PIN IS NOT 34.5 TO 38.5 DEGREES FROM THE CENTERLINE OF THE BASE AT AFT ACCESORIES COMPARTMENT. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY OF NRC 00899: REL
- [SDR DALA2025010800158](https://openairdocs.org/sdr/DALA2025010800158.md): Rod End · damaged · Jan 7, 2025 · N981AT · Boeing 717200 · Drag Control System
  > DAMAGED DURING ADJUSTMENT OF RH INBD SPOILER PANEL. THE HOLDDOWN ACTUATOR ROD-END INADVERTENTLY EXTENDED CAUSING A PUNCTURE ON RH INBD GUIDE VANE. SUMMARY OF NRC 00886: THE RH INBD GUIDE VANE WAS REPAIRED PER B717 SRM 51-70-02-0G PROCEDURE GENERAL AND IN REFER
- [SDR DALA2025010700130](https://openairdocs.org/sdr/DALA2025010700130.md): Angle · cracked · Jan 7, 2025 · N981AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > UPPER ANGLE COMMON TO FUSELAGE SKIN AND RH PYLON UPPER SKIN LOCATED AT Y=1178 CANTED WAS REMOVED. LOWER ANGLE COMMON TO REMOVED ANGLE WAS FOUND CRACKED. SUMMARY OF NRC 00820: LOWER ANGLE COMMON TO FUSELAGE SKIN AND RH PYLON UPPER SKIN LOCATED AT Y=1178 CANTED
- [SDR DALA2024122712033](https://openairdocs.org/sdr/DALA2024122712033.md): Angle · corroded · Dec 24, 2024 · N981AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON CUSP ANGLE FROM STA Y=157 TO STA Y=200 BTW -X=61.5 TO -X=66 INNER STRUCTURE OF SERVICE DOOR JAMB AT CPAX. SUMMARY OF NRC 00506: CORROSION LEVEL 2. CORROSION ON CUSP ANGLE FROM STA Y=157 TO STA Y=200 BTW -X=61.5 TO -X=66 INNER STRUCTURE OF SERVICE
- [SDR DALA2024121911829](https://openairdocs.org/sdr/DALA2024121911829.md): Frame · corroded · Dec 19, 2024 · N981AT · Boeing 717200 · Fuselage Main, Frame
  > CORROSION ON FRAME STA Y=908 FROM LONG 26LH TO LONG 29RH AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00609: CORROSION LEVEL 2. CORROSION ON FRAME STA Y=908 FROM LONG 26LH TO LONG 29RH AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 3
- [SDR DALA2024121711766](https://openairdocs.org/sdr/DALA2024121711766.md): Retainer · cracked · Dec 16, 2024 · N981AT · Boeing 717200 · Fuselage Main, Structure
  > CRACK INNER RETAINER OF COCKPIT WINDOW FRAME, UNDER BRACKET, UPPER AFT LH SIDE ON FLIGHT COMPARTMENT. SUMMARY OF NRC 00782: CRACK INNER RETAINER OF COCKPIT WINDOW FRAME, UNDER BRACKET, UPPER AFT LH SIDE ON FLIGHT COMPARTMENT WAS REPAIRED PER ER/A 622289-14 REV
- [SDR DALA2024121611736](https://openairdocs.org/sdr/DALA2024121611736.md): Pan · gouged · Dec 13, 2024 · N981AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > GOUGE ON INNER PAN AFT EDGE, 2 INCHES BELLOW BEAM #1 AFT EDGE, ON AFT CARGO DOOR (C2). SUMMARY OF NRC 00321: INNER PAN ON AFT LOWER CORNER CLOSE TO BEAM #1 AT AFT CARGO DOOR (C2) WAS REPAIRED PER ER/A 621854-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI
- [SDR DALA2024121611735](https://openairdocs.org/sdr/DALA2024121611735.md): Longeron · corroded · Dec 13, 2024 · N981AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CORROSION ON LONGERON 29L UPPER/LOWER SURFACE BTW STA Y=900-946 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00630: CORROSION LEVEL 2. LONGERON 29L BTW STA Y= 898 TO 964 AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-02-0G, 51-41-05-0G, AND PER B717-
- [SDR DALA2024121311703](https://openairdocs.org/sdr/DALA2024121311703.md): Skin · dented · Dec 12, 2024 · N981AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > DAMAGE T: ELONGATE HOLES, PROTRUDING DENTS, AND GOUGES ON FUSELAGE SKIN STA Y 1037 BTW LONG 7R-13R. SUMMARY OF NRC 00627: ELONGATED HOLES, PROTRUDING DENTS, AND GOUGES ON FUSELAGE SKIN STA Y 1037 BTW LONG 7R-13R WERE REPAIRED PER PRI 622118-14 REV 3 AND ER/A 6
- [SDR DALA2024121211665](https://openairdocs.org/sdr/DALA2024121211665.md): Floor Support · corroded · Dec 12, 2024 · N981AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION OUT OF LIMITS ON FLOOR SUPPORTS ON STA Y=157-200 AND X=45 (1 EA) PER B717-200 SRM 53-00-00-1A PROCEDURE, ALLOWABLE DAMAGE GENERAL, PAR 4.C, FIG 103. SUMMARY OF NRC 00821: CORROSION LEVEL 2. FLOOR SUPPORT ON STA Y=157-200 AND X=45 WAS REPLACED PER B71
- [SDR DALA2024121611738](https://openairdocs.org/sdr/DALA2024121611738.md): Hinge Fitting · corroded · Dec 11, 2024 · N981AT · Boeing 717200 · Trailing Edge Flaps
  > CORROSION ON ALL INNER CAVITY LUGS (9 EA) OF THE INBOARD WING FLAP HINGE FITTING AT LH WING, AND WEAR ON FAIRING SUPPORTS OF THE INBOARD WING FLAP HINGE FITTING AT LH WING. ALSO WEAR ON INNER CAVITY (4 EA) SUPPORT AT LH WING. CORROSION ON ACTUATOR SUPPORT LUGS
- [SDR DALA2024121111616](https://openairdocs.org/sdr/DALA2024121111616.md): Lug · worn · Dec 11, 2024 · N981AT · Boeing 717200 · Wing, Control Surface Attach Fittings
  > WEAR ON HOLES AND INTERNAL FACE LUGS OF LH HINGE #3 OF LH WING. SUMMARY OF NRC 00803: HOLES AND INTERNAL FACE LUGS OF LH HINGE #3 OF LH WING WERE REPAIRED PER PRI 622848-14 REV 0 & ER/A 622848-14 REV ORIG. ASSOCIATED ER/A 14-622848 ADDED FOR AC 9548. (LP #0703
- [SDR DALA2024120211371](https://openairdocs.org/sdr/DALA2024120211371.md): Cusp Web · cracked · Nov 28, 2024 · N981AT · Boeing 717200 · Fuselage Floor Panel
  > CRACKS ON LH CUSP WEB (3 EA) STA Y=657 & X=56 AND STA Y=716 & X=44.5 AND Y=888 & X=56 AT PASSENGER CABIN. SUMMARY OF NRC 00426: FABRICATED WEB STA Y-655 TO Y-715 PER B717-200 SRM 53-20-51-01 PROCEDURE 2. REPAIRED CUSP WEB STA 888 & X 56 PER B717-200 SRM 53-00-
- [SDR DALA2024120211370](https://openairdocs.org/sdr/DALA2024120211370.md): Rib · elongated · Nov 27, 2024 · N981AT · Boeing 717200 · Elevator, Spar/Rib
  > ELONGATED HOLE ON RIB ON COUNTERWEIGHT-TO-L.E. CONNECTION FITTING AT RIGHT ELEVATOR STA XH 217. SUMMARY OF NRC 00410: RIB ON COUNTERWEIGHT-TO-L.E. CONNECTION FITTING AT RIGHT ELEVATOR STA XH 217 WAS REPAIRED PER B717 SRM 55-00-00-2R REPAIR 2 PAR 4. THIS REPAIR
- [SDR DALA2025011500350](https://openairdocs.org/sdr/DALA2025011500350.md): Skin · damaged · Nov 26, 2024 · N981AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKE ON THE FUSELAGE AT THE RH WINDOW PANEL, STA 484 TO 503. ACCOMPLISH ER/A 622755-14 SECTION II INSPECTION WITHIN EVERY 24 MONTHS UNTIL ACCOMPLISHMENT OF SECTION III PERMANENT REPAIR NO LATER THAN 48,400 TOTAL CYCLES. ASSOCIATED ER/A 00-622755 AD
- [SDR DALA2024112711259](https://openairdocs.org/sdr/DALA2024112711259.md): Skin · mechanic error · Nov 26, 2024 · N981AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > EXTERNAL SURFACE OF FUSELAGE SKIN COMMON TO VHF ANTENA MATING SURFACE WAS FOUND MISDRILLED, LOCATED Y=917 L-30/L-29L IN REF NRC 12. SUMMARY OF NRC 00169: FUSELAGE SKIN COMMON TO ANTENA MATING SURFACE WAS FOUND MISDRILLED, LOCATED Y=917 L-30/L-29L WAS REPAIRED
- [SDR DALA2024112511164](https://openairdocs.org/sdr/DALA2024112511164.md): Door Frame · corroded · Nov 23, 2024 · N981AT · Boeing 717200 · Fuselage Main, Structure
  > CORROSION ON DOOR JAMB FWD/AFT AT REPAIR SPLICES AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00806: CORROSION LEVEL 2. AFT CARGO DOOR JAMB FWD/AFT REPAIR SPLICES WERE REPLACED PER B717-200 SRM 53-20-15-2R PROCEDURE 7 REPAIR 7. (LP #0674286)
- [SDR DALA2024112511163](https://openairdocs.org/sdr/DALA2024112511163.md): Cusp Web · cracked · Nov 23, 2024 · N981AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACKS ON LH CUSP WEB (2 EA) STA Y=595 & X=56 AND STA Y=907 & X=56 BELOW SEAT TRACK SPLICE IN PASSENGER CABIN. SUMMARY OF NRC 00425: CUSP WEBS BTW STA Y 579-598 AND X=54 TO X=60 AND BTW STA Y 889-908 AND X=54 TO X=60 WERE REPLACED PER B717 SRM 53-00-55-2R REPA
- [SDR DALA2024112011084](https://openairdocs.org/sdr/DALA2024112011084.md): Seat Track · mechanic error · Nov 20, 2024 · N981AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > MISDRILLED SEAT TRACK (SETTLEMT AREA) BTW STA Y=908-927 AND X=54 LH AT PASSENGER CABIN. SUMMARY OF NRC 00751: SEAT TRACK (SETTLEMT AREA) BTW STA Y=908-927 AND X=54 LH AT PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 53-20-52-2R REPAIR 5. PERFORM DECAL CONDITIO
- [SDR DALA2024112011083](https://openairdocs.org/sdr/DALA2024112011083.md): Tripler · corroded · Nov 19, 2024 · N981AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CORROSION ON PREVIOUS REPAIR TRIPLER ON FUSELAGE UNDER FILLET FAIRINGS AREA STA Y=843-860 LONG 28L-28R. SUMMARY OF NRC 00467: CORROSION LEVEL 2. PREVIOUS REPAIR TRIPLER WAS REPLACED PER B717 SRM 53-20-70-2R REP 1. PERFORM EXTERNAL VISUAL INSPECTION EVERY 8,000
- [SDR DALA2024111911027](https://openairdocs.org/sdr/DALA2024111911027.md): Longeron Splice · corroded · Nov 18, 2024 · N981AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CORROSION ON UPPER AND LOWER SURFACE OF LONGERON AND LONGERON SPLICE (RH 29) FROM STA Y=218 TO Y=237. SUMMARY OF NRC 00344: CORROSION LEVEL 2. LONGERON L29 R/H STA Y=157 TO Y=237 AND LONGERON SPLICE (RH 29) FROM STA Y=218 TO Y=237 WERE REPLACED PER B717-200 SR
- [SDR DALA2024111510968](https://openairdocs.org/sdr/DALA2024111510968.md): Skin · cracked · Nov 15, 2024 · N981AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACKED FUSELAGE SKIN STA Y 1022 BTW LOG 7R-8R CLOSE TO THE LAP SKIN JOINT. SUMMARY OF NRC 00054: FUSELAGE SKIN STA Y 1022 BTW LOG 7R-8R CLOSE TO THE LAP SKIN JOINT WAS REPAIRED PER ER/A 621690-14 REV ORIGINAL SECTION I PERMANENT REPAIR AND PRI 621690-14 REV 1
- [SDR DALA2024111510966](https://openairdocs.org/sdr/DALA2024111510966.md): Cusp Web · corroded · Nov 14, 2024 · N981AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON RH CUSP WEB UPPER/LOWER SURFACES ON STA Y=492, Y=501-503 AT PASSENGER CABIN. SUMMARY OF NRC 730: CORROSION LEVEL 2. RH CUSP WEB UPPER/LOWER SURFACES ON STA Y=492, Y=501-503 AT PASSENGER CABIN WERE REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4
- [SDR DALA2024111410948](https://openairdocs.org/sdr/DALA2024111410948.md): Diaphragm · cracked · Nov 13, 2024 · N981AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON DIAPHRAGM BTW STA Y=200/218 AND X-54/X-22 AT CABIN PAX. SUMMARY OF NRC 00632: CORROSION LEVEL 2. DIAPHRAGM BTW STA Y=200 /218 AND X-54/X-22 WAS REPLACED PER DRAWING 9936535 REV CS. (LP #0658856)
- [SDR DALA2024111410947](https://openairdocs.org/sdr/DALA2024111410947.md): Intercostal · cracked · Nov 13, 2024 · N981AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL BTW STA Y=1002 AND STA Y=1022, X=0 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00310: INTERCOSTAL BTW STA Y=1002 AND STA Y=1022, X=0 WAS REPAIRED PER B717 SRM 51-70-11-2R REP. 1. (LP #0658130)
- [SDR DALA2024111210887](https://openairdocs.org/sdr/DALA2024111210887.md): Seat Track · misinstalled · Nov 11, 2024 · N981AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > WRONG INSTALLED FASTENERS ON SEAT TRACK AND CUSP WEB STA Y=914-919 & X =56 AT PASSENGER CABIN. SUMMARY OF NRC 00427: CUSP WEB STA Y=914-919 & X =56 AT PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R REPAIR 4. (LP #0655354)
- [SDR DALA2024111110806](https://openairdocs.org/sdr/DALA2024111110806.md): Channel · corroded · Nov 11, 2024 · N981AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION AT CHANNEL BETWEEN STA 827 AND 832 L22R EXTERNAL FUSELAGE. SUMMARY OF NRC 407: CORROSION LEVEL 2. CHANNEL BTW STA Y=827 AND Y=832 L22R EXTERNAL FUSELAGE WAS FABRICATED PER DWG 5924872 REV BT AND REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G.
- [SDR DALA2024111110801](https://openairdocs.org/sdr/DALA2024111110801.md): Skin · cracked · Nov 9, 2024 · N981AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACKED FUSELAGE SKIN STA Y 1087 LONG 14R LOCATED CLOSE TO THE LAP SKIN JOINT AND PREVIOUS REPAIR DOUBLER. SUMMARY OF NRC 00052: FUSELAGE SKIN STA Y 1087 LONG 14R LOCATED CLOSE TO THE LAP SKIN JOINT AND PREVIOUS REPAIR DOUBLER WAS REPAIRED PER ER/A 621691-14 R
- [SDR DALA2024111110797](https://openairdocs.org/sdr/DALA2024111110797.md): Longeron · cracked · Nov 8, 2024 · N981AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CRACK ON LONGERON #8RH STA Y1022 AT PAX CABIN. SUMMARY OF NRC 00501: LONGERON #8RH STA Y1022 AT PAX CABIN WAS REPAIRED PER B-717-200 SRM 53-00-05-2R-2. (LP #0650326)
- [SDR DALA2024110810726](https://openairdocs.org/sdr/DALA2024110810726.md): Vane · dented · Nov 7, 2024 · N981AT · Boeing 717200 · Trailing Edge Flaps
  > DENTS (2 EA) ON UPPER SURFACE AFT MOVABLE VANE APPROX BTW STA XRS=69 AND XRS=91 AT RH WING. SUMMARY OF NRC 00143: UPPER SURFACE AFT MOVABLE VANE APPROX BTW STA XRS=69 AND XRS=76 OF RH WING WAS REPAIRED PER B717-200 SRM 57-53-01-2R PROCEDURE 1 REPAIR 1. (LP #06
- [SDR DALA2024110710703](https://openairdocs.org/sdr/DALA2024110710703.md): Longeron · cracked · Nov 7, 2024 · N981AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CRACK ON LONGERON 6LH STA Y=1022 AT PAX CABIN. SUMMARY OF NRC 00499: LONGERON 6LH STA Y=1022 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURE 2, REPAIR 2. (LP #0647976)
- [SDR DALA2024110710702](https://openairdocs.org/sdr/DALA2024110710702.md): Floor Support · corroded · Nov 5, 2024 · N981AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORTS (2 EA) X=-55/X=55 FROM STA Y=1022 TO STA Y=1053 AT PASSENGER CABIN. SUMMARY OF NRC 00475: CORROSION LEVEL 2. FLOOR SUPPORTS (2 EA) X=-55/X=55 FROM STA Y=1022 TO STA Y=1053 WERE REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G.

Next page: https://openairdocs.org/aircraft/N981AT/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 = 'N981AT' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N981AT/reports

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