# Service difficulty reports: N978AT

A list on [N978AT](https://openairdocs.org/aircraft/N978AT.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 · 226 reports

- [SDR DALA2026101305623](https://openairdocs.org/sdr/DALA2026101305623.md): Web · cracked · Oct 10, 2026 · N978AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACKS ON RT WEBS (2EAS) BTW STA Y= 645 TO 715 AT C PAX. REPAIRED PER B717-200 SRM 53-00-55-2R. (1858343) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026101305622](https://openairdocs.org/sdr/DALA2026101305622.md): Frame · cracked · Oct 10, 2026 · N978AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK ON OVERWING FRAME STA Y= 674 RH SIDE. OVERWING FRAME STA Y= 674 RH SIDE WAS REPLACED PER CARD 5310-01436-03B. (1857798) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026101305625](https://openairdocs.org/sdr/DALA2026101305625.md): Skin · cracked · Oct 9, 2026 · N978AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > DENT AND CRACK FUSELAGE SKIN STA Y=370-389, L-29R & L-30. REPAIRED PER ER/A 610692-14. (1857452) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026100905574](https://openairdocs.org/sdr/DALA2026100905574.md): Web · cracked · Oct 8, 2026 · N978AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > FOUND CRACK AT RT WEB ON BS 655-715, R & R WEB IAW SRM 53-00-55-2R-4. (1855606) (AICRAFT GROUNDED).
- [SDR DALA2026100605530](https://openairdocs.org/sdr/DALA2026100605530.md): Skin · dented · Oct 5, 2026 · N978AT · Boeing 717200 · Trailing Edge Flaps
  > SEVERAL DENTS ON LOWER SKIN OF RT AFT MOVABLE VANE WAS FOUND AT RT WING. AREA AT RT AFT MOVABLE VANE RT WING WAS REPAIRED IAW ER/A 637238-14. (1850252) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026100605529](https://openairdocs.org/sdr/DALA2026100605529.md): Vane · dented · Oct 4, 2026 · N978AT · Boeing 717200 · Wing, Plate/Skin
  > DENT ON LOWER SURFACE OF RT FWD MOVABLE VANE WAS FOUND AT RT WING. WD MOVABLE VANE AT RT WING WAS REPAIRED IAW SRM 57-53-01-2R, PROCEDURE 1, REPAIR 1. AND SRM 51-70-02-0G. (1848375) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026100205472](https://openairdocs.org/sdr/DALA2026100205472.md): Slat Track · cracked · Oct 1, 2026 · N978AT · Boeing 717200 · Leading Edge Devices
  > CRACK PLATE OF SLAT TRACK 5 NEAR XOS 530 AT LT WING, COMPLIED WITH ER/A 540095-14MA. (1843372) (AIRCRAFT GROUNDED).
- [SDR DALA2026100105449](https://openairdocs.org/sdr/DALA2026100105449.md): Repair · dented · Oct 1, 2026 · N978AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > DENTS ON PREVIOUS FLUSH REPAIR BTW BS 218-256 BTW LONG 17LT TO 18 LT, R & R FLUSH REPAIR PER SRM 53-00-01-2R. (1841666) (AIRCRAFT GROUNDED).
- [SDR DALA2026100105451](https://openairdocs.org/sdr/DALA2026100105451.md): Roller · worn · Sep 30, 2026 · N978AT · Boeing 717200 · Leading Edge Devices
  > WEAR ON SIDE ROLLER STA XOS 136 UPPER INB/ OUTB AND LOWER OUTB (SLAT TRACK 2) ALSO SIDE ROLLER UPPER INBOARD AND LOWER OUTBOARD STA XOS 240 (SLAT TRACK 5) LH WING, CORRECTIVE ACTION: R/R UPPER AND LOWER ROLLERS PER B717 AMM 27-80-02. (1841097) (AIRCRAFT GROUND
- [SDR DALA2026091805218](https://openairdocs.org/sdr/DALA2026091805218.md): Circuit Breaker · faulted · Sep 17, 2026 · N978AT · Boeing 717200 · Communications System Wiring
  > COMM 1 EXTREMELY GIVING INTERFERENCE WHEN IN FLIGHT, RESET C/B REF AMM 23-12. (9488892) (AIRCRAFT GROUNDED).
- [SDR DALA2026080604550](https://openairdocs.org/sdr/DALA2026080604550.md): Unknown · odor · Aug 5, 2026 · N978AT · Boeing 717200 · Air Distribution System
  > ELECTRICAL RUBBER ODOR COMING FROM AFT FA JUMP SEAT AREA, T/S PER FIM 21-22-00-810-815. FOUND NO RUBBER ODOR, COULD NOT REPLICATE ISSUE. ACFT OK FOR SERVICE. (9093748) (AIRCRAFT GROUNDED).
- [SDR DALA2026072104278](https://openairdocs.org/sdr/DALA2026072104278.md): Doubler · damaged · Jul 19, 2026 · N978AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > DAMAGE TO AFT CARGO DOOR JAMB DOUBLER. REPAIRED PER B717 SRM 53-20-15-2R. (1707868) AIRCRAFT GROUNDED.
- [SDR DALA2026072104277](https://openairdocs.org/sdr/DALA2026072104277.md): Skin · damaged · Jul 19, 2026 · N978AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > DAMAGE TO FUSELAGE SKIN. REPAIRED PER B717 SRM 53-20-15-2R. (1708438) AIRCRAFT GROUNDED.
- [SDR DALA2026060203344](https://openairdocs.org/sdr/DALA2026060203344.md): Battery Pack · no test · May 27, 2026 · N978AT · Boeing 717200 · Emergency Lighting
  > SHIP 9543 DURING SVC CHECK, FOUND AFT EXIT DOOR EMERGENCY LIGHT NOT ILLUMINATING. CORRECTIVE ACTION: R/R'D AFT EMERGENCY LIGHT BATTERY PACK PER B717 AMM 33-51. (8660314) (AIRCRAFT GROUNDED)
- [SDR DALA2025122309344](https://openairdocs.org/sdr/DALA2025122309344.md): Pump · faulted · Dec 20, 2025 · N978AT · Boeing 717200 · Hydraulic Pump (Electric/Engine), Main
  > THE CREW REPORTED LT HYDRAULIC QTY LOW MESSAGE, FOLLOWED QRH AND LANDED WITH SYSTEM PRESSURE AND QUANTITY. MAINTENANCE REPLACED THE LEFT ENGINE DRIVEN HYDRAULIC PUMP AND THE LEFT RESERVOIR.(7954928)
- [SDR DALA2025030401651](https://openairdocs.org/sdr/DALA2025030401651.md): Control Module · faulted · Feb 28, 2025 · N978AT · Boeing 717200 · Trailing Edge Flap Control System
  > SHIP 9543 -FCNT/DE- THE FLIGHT CREW DECLARED AN EMERGENCY WITH ATC DUE TO THE TRAILING EDGE FLAPS BEIN INOPERATIVE ON APPROACH. A NORMAL LANDING WAS ACCOMPLISHED AND NO ISSUES WITH BREAKING DURING ROLLOUT. CORRECTIVE ACTION: MAINTENANCE REPLACED THE FLAP/SLAT
- [SDR DALA2024122712032](https://openairdocs.org/sdr/DALA2024122712032.md): Pan · corroded · Dec 24, 2024 · N978AT · Boeing 717200 · Fuselage Main, Structure
  > CORROSION ON E/E DOOR JAMB PAN STA Y=160 BTW LONG 29LH TO 29RH. SUMMARY OF NRC 00644: CORROSION LEVEL 2. CORROSION ON E/E DOOR JAMB PAN STA Y=160 BTW LONG 29LH TO 29RH WAS REPAIRED PER ER/A 623018-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 623018-14 R
- [SDR DALA2024122311963](https://openairdocs.org/sdr/DALA2024122311963.md): Support · cracked · Dec 21, 2024 · N978AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON LH TRACK SUPPORT STA Y=918-915, STA Y=879-876, AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00252: LH TRACK SUPPORT STA Y=876 TO 1022 AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-20-52-2R- PROCEDURE 4 REPAIR 4. (LP #0721119)
- [SDR DALA2024122311960](https://openairdocs.org/sdr/DALA2024122311960.md): Structure · corroded · Dec 19, 2024 · N978AT · Boeing 717200 · Horizontal Stabilizer Structure
  > CORROSION ON BARREL NUTS HOLES XH=-7 RH [7, 8, 11, 12, 16, 18, 21, 26, 28] AND XH=7 LH [10, 18, 26, 27, 29] AT HORIZONTAL STABILIZER CENTER BOX. SUMMARY OF NRC 00407: CORROSION LEVEL 2. BARREL NUTS HOLES XH=-7 RH [7, 8, 11, 12, 16, 18, 21, 26, 28] AND XH=7 LH
- [SDR DALA2024122311959](https://openairdocs.org/sdr/DALA2024122311959.md): Structure · corroded · Dec 19, 2024 · N978AT · Boeing 717200 · Horizontal Stabilizer Structure
  > CORROSION ON BARREL NUTS HOLES XH=-7 RH [7, 8, 11, 12, 16, 18, 21, 26, 28] AND XH=7 LH [10, 18, 26, 27, 29] AT HORIZONTAL STABILIZER CENTER BOX. SUMMARY OF NRC 00407: CORROSION LEVEL 2. CORRODED BARREL NUTS HOLES XH=-7 RH [7, 8, 11, 12, 16, 18, 21, 26, 28] AND
- [SDR DALA2024122311958](https://openairdocs.org/sdr/DALA2024122311958.md): Structure · worn · Dec 19, 2024 · N978AT · Boeing 717200 · Horizontal Stabilizer Structure
  > FOUND WEAR ON BARREL NUT HOLE #30 AT LH HORIZONTAL STABILIZER CENTER. SUMMARY OF NRC 00754: BARREL NUT HOLE #30 AT LH HORIZONTAL STABILIZER CENTER WAS REPAIRED PER ER/A 622465-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. REPAIR APPROVAL IS LIMITED TO 24 MONTHS
- [SDR DALA2024121911827](https://openairdocs.org/sdr/DALA2024121911827.md): Bearing · worn · Dec 19, 2024 · N978AT · Boeing 717200 · Trailing Edge Flaps
  > WORN BEARING OF FLAP AND ELONGATED HOLES ON OUTB HINGE OF LH FLAP WERE FOUND. SUMMARY OF NRC 00684: OUTB HINGE OF LH FLAP WAS REPAIRED PER ER/A 622136-14 REV ORIG, SECTION I: PERMANENT REPAIR. "DTE" TIME CONTROLLED ITEM WITH LOG PAGE #0701683. ASSOCIATED ER/A
- [SDR DALA2024121811801](https://openairdocs.org/sdr/DALA2024121811801.md): Skin · cracked · Dec 18, 2024 · N978AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACKS ON EXTERNAL SKIN STA Y 1153, BTW LONGERON 3L/4L AND BTW LONGERON 2R/3R AT AFT FUSELAGE. SUMMARY OF NRC 00050: EXTERNAL SKIN STA Y 1153, BTW LONGERON 3L/4L AND BTW LONGERON 2R/3R AT AFT FUSELAGE WAS REPAIRED PER ER/A 621926-14 REV ORIG SECTION I PERMANEN
- [SDR DALA2024121711768](https://openairdocs.org/sdr/DALA2024121711768.md): Skin · damaged · Dec 17, 2024 · N978AT · Boeing 717200 · Vertical Stabilizer, Plate/Skin
  > -AD- WEAR AND ELONGATED COUNTERSINK OF FASTENERS ON REMOVABLE VERTICAL STABILIZER LEADING EDGE. SUMMARY OF NRC 00053: COUNTERSINK OF FASTENERS ON REMOVABLE VERTICAL STABILIZER LEADING EDGE WERE REPAIRED PER ERA 621994-14AD REV ORIGINAL. ASSOCIATED ER/A 14-6219
- [SDR DALA2024121611734](https://openairdocs.org/sdr/DALA2024121611734.md): Skin · cracked · Dec 12, 2024 · N978AT · Boeing 717200 · Vertical Stabilizer, Plate/Skin
  > ELONGATED HOLES AND CRACKS ON COUNTERSINK OF PANEL 370CR. SUMMARY OF NRC 00658: PANEL 370CR WAS REPAIRED PER ERA 622046-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 622046-14 REV 1. ASSOCIATED ER/A 14-622046.
- [SDR DALA2024121311704](https://openairdocs.org/sdr/DALA2024121311704.md): Retainer · cracked · Dec 12, 2024 · N978AT · Boeing 717200 · Fuselage Main, Structure
  > CRACK INNER RETAINER OF COCKPIT WINDOW FRAME, UNDER BRACKET, UPPER AFT RH SIDE ON FLIGHT COMPARTMENT. SUMMARY OF NRC 00663: CRACK ON INNER RETAINER OF COCKPIT WINDOW FRAME, UNDER BRACKET, UPPER AFT RH SIDE ON FLIGHT COMPARTMENT WAS REPAIRED B717-200 SRM 56-10-
- [SDR DALA2024121311702](https://openairdocs.org/sdr/DALA2024121311702.md): Frame · worn · Dec 12, 2024 · N978AT · Boeing 717200 · Fuselage Main, Frame
  > WEAR AT FRAME OF STA Y=598 LH SIDE WAS FOUND OUT OF LIMITS. SUMMARY OF NRC 00716: FRAME OF STA Y=598 LH SIDE WAS REPAIRED PER ER/A 622297-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PER PRI 622297-14 REV 4. ASSOCIATED ER/A 14-622297 ADDED FOR AC 9543. (LP
- [SDR DALA2024121211664](https://openairdocs.org/sdr/DALA2024121211664.md): Skin · cracked · Dec 11, 2024 · N978AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACK AND WEAR AT SKIN CUTOUT STA Y 994 AT LONGERON 25R AT AFT CARGO COMPARMENT. SUMMARY OF NRC 00774: CRACK AND WEAR AT SKIN CUTOUT STA Y 994 AT LONGERON 25R AT AFT CARGO COMPARMENT WAS REPAIRED PER B717-200 SRM 53-20-15-2R, PROCEDURE 12, REPAIR 12, FIG 201.
- [SDR DALA2024120911536](https://openairdocs.org/sdr/DALA2024120911536.md): Angle · corroded · Dec 6, 2024 · N978AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON CUSP ANGLE OF FWD SERVICE DOOR JAMB AT FOUR POINTS; THE FIRST ONE, FORWARD OF STA Y=167; THE SECOND ONE, UNDER THE PAN AFT OF STA Y=167; THE THIRD ONE, ALSO UNDER THE PAN FORWARD OF STA Y=200; AND THE FOURTH ONE, AFT OF STA Y=200. SUMMARY OF NRC 0
- [SDR DALA2024120911534](https://openairdocs.org/sdr/DALA2024120911534.md): Pan · corroded · Dec 5, 2024 · N978AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON SEVERAL POINTS OF FORWARD CARGO DOOR JAMB PAN LOWER SECTION AT FORWARD CARGO COMPARTMENT. SUMMARY OF NRC 00224: CORROSION LEVEL 2. FORWARD CARGO DOOR JAMB PAN LOWER SECTION AT FORWARD CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-20-15-2R, RE
- [SDR DALA2024120911530](https://openairdocs.org/sdr/DALA2024120911530.md): Floor Support · corroded · Dec 5, 2024 · N978AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORTS (8 EA) X=-53.5, BTW STA Y=160 TO Y=200; STA X=44.5, BTW STA Y=160 TO Y=196; STA X=56, BTW STA Y=160 TO Y=196; STA Y=180.5, BTW STA X=13 TO X=38.25; STA Y=196, BTW STA X=15.5 TO X=44.5; STA Y=200, BTW STA X=-7 TO X=-44.5; STA Y=200,
- [SDR DALA2024120911529](https://openairdocs.org/sdr/DALA2024120911529.md): Web · cracked · Dec 3, 2024 · N978AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK WAS FOUND ON WEB IN STA Y=247 AND X-44.5 APPROX IN AREA OF X-44.5 (MEDIUM) AT STA Y=200 TO STA Y=266 RH SIDE. SUMMARY OF NRC 00671: CRACK ON WEB IN STA Y=247 AND X-44.5 APPROX WAS REPAIRED PER B717-200 SRM 53-00-55-2R REPAIR 4 FIG 215. (LP #0691502)
- [SDR DALA2024120911528](https://openairdocs.org/sdr/DALA2024120911528.md): Seat Track · corroded · Dec 3, 2024 · N978AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LH SEAT TRACK X=22 BTW STA Y=200-214 AT PASSENGER CABIN. SUMMARY OF NRC 00660: CORROSION LEVEL 2. LH SEAT TRACK X=22 BTW STA Y=200-214 AT PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 53-20-52-2R PROCEDURE 5 REPAIR 5. (LP #0691470)
- [SDR DALA2024120911527](https://openairdocs.org/sdr/DALA2024120911527.md): Fuel Tank · corroded · Dec 3, 2024 · N978AT · Boeing 717200 · Fuel Storage
  > -AD- CORROSION ON CENTER TANK UPPER SURFACE, AFT BULKHEAD STA Y=747 X=39 TO X=44 AT CENTER WING (LH WHELL WELL AREA). SUMMARY OF NRC 00678: CORROSION LEVEL 2. CORROSION ON CENTER TANK UPPER SURFACE, AFT BULKHEAD STA Y=747 X=39 TO X=44 AT CENTER WING (LH WHELL
- [SDR DALA2024120911526](https://openairdocs.org/sdr/DALA2024120911526.md): Cusp Web · corroded · Dec 3, 2024 · N978AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON CUSP WEB STA X=-44.5 TO X=-56 AND STA Y=313 AT CPAX. SUMMARY OF NRC 00738: CORROSION LEVEL 2. CUSP WEB STA X=-44.5 TO X=-56 AND STA Y=313 AT CPAX WAS REPAIRED PER B717-200 SRM 51-70-10-2R, PROCEDURE 2, REPAIR 2. (LP #0691024)
- [SDR DALA2024120311395](https://openairdocs.org/sdr/DALA2024120311395.md): Cusp Web · corroded · Dec 3, 2024 · N978AT · Boeing 717200 · Fuselage Main, Frame
  > CORROSION WAS FOUND ON LH CUSP ANGLE BTW STA Y=200-207 AT PASSENGER CABIN. SUMMARY OF NRC 00630: CORROSION LEVEL 2. LH CUSP ANGLE BTW STA Y=200-207 WAS REPAIRED PER B717 SRM 53-00-55-2R REPAIR 3. (LP #0690306)
- [SDR DALA2024120311394](https://openairdocs.org/sdr/DALA2024120311394.md): Cusp Web · cracked · Dec 3, 2024 · N978AT · Boeing 717200 · Fuselage Main, Frame
  > CRACKED IN FIVE PLACES OF THE CUSP WEB MEMBRANE AT STA Y=266, STA X=-44.5; STA Y=589, STA X=-44.5; STA Y= 663, STA X=-44.5; STA Y=716, STA X=-44.5; AND STA Y=1012, STA X=-56. SUMMARY OF NRC 00472: (ET) (HFEC) INSPECTION WAS ACCOMPLISHED ONLY ON STA Y=663, STA
- [SDR DALA2024120311393](https://openairdocs.org/sdr/DALA2024120311393.md): Cusp Web · corroded · Dec 2, 2024 · N978AT · Boeing 717200 · Fuselage Main, Frame
  > CORROSION ON CUSP WEB BTW X=-56 TO X=-60 AND BTW STA Y=794-813 AT CPAX. SUMMARY OF NRC 00739: CORROSION LEVEL 2. CUSP WEB BTW X=-56 TO X=-60 AND BTW STA Y=794-813 AT CPAX WERE REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR PARAGRAPH 5 B (14) FIG 216.
- [SDR DALA2024121311700](https://openairdocs.org/sdr/DALA2024121311700.md): Cusp Web · cracked · Nov 30, 2024 · N978AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CUSP WEB LOCATED BETWEEN Y=218 TO Y=237, BETWEEN X=-56 TO X=-44 WAS FOUND CRACKED. SUMMARY OF NRC 00647: DUE TO CRACKS, NEW CUSP WEB LOCATED AT BETWEEN Y=218 TO Y=237, BETWEEN X=-56 TO X=-44 WAS FABRICATED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4 FIG
- [SDR DALA2024120211374](https://openairdocs.org/sdr/DALA2024120211374.md): Seat Track · corroded · Nov 30, 2024 · N978AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LH SEAT TRACK X=44 BTW STA Y=200-214 AT PASSENGER CABIN. SUMMARY OF NRC 00661: CORROSION LEVEL 2. LH SEAT TRACK X=44 STA Y=200 TO Y=304 AT PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 53-20-52-2R PROCEDURE 5 REPAIR 5. (LP #0685816)
- [SDR DALA2024120211373](https://openairdocs.org/sdr/DALA2024120211373.md): Door Frame · corroded · Nov 30, 2024 · N978AT · Boeing 717200 · Fuselage Main, Frame
  > CORROSION ON ANGLE AND WEB ON LOWER DOOR JAMB STA Y=200 AT PAX CABIN (L1). SUMMARY OF NRC 00386: CORROSION LEVEL 2. ANGLE AND WEB ON LOWER DOOR JAMB STA Y=200 AT PAX CABIN WERE REPLACED PER B717-200 SRM 51-41-01-0G, 51-41-02-0G, 51-41-05-0G, AND 51-41-08-0G. (
- [SDR DALA2024112711258](https://openairdocs.org/sdr/DALA2024112711258.md): Seat Track · corroded · Nov 26, 2024 · N978AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RH SEAT TRACK X=22 BTW STA Y=200-256 IN PASSENGER CABIN. SUMMARY OF NRC 00662: CORROSION LEVEL 2. SEAT TRACK RH X=22 STA Y=200 TO Y=266 WAS REPAIRED PER B717-200 SRM 53-20-52-2R REPAIR 5, 51-41-01-0G, AND 51-41-05-0G PAR 8. (LP #0679793)
- [SDR DALA2024112611227](https://openairdocs.org/sdr/DALA2024112611227.md): Cusp Web · cracked · Nov 25, 2024 · N978AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > FOUND RACKS ON CUSP WEB BTW STA Y=239-258 X=44 AT PASSENGER CABIN (CPAX). SUMMARY OF NRC 00737: CRACKS ON CUSP WEB BTW STA Y=239-258 X=44 AT PASSENGER CABIN WERE REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4. (LP #0678225)
- [SDR DALA2024112611226](https://openairdocs.org/sdr/DALA2024112611226.md): Longeron · cracked · Nov 25, 2024 · N978AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CRACKS ON LONGERONS 6R, 3L, AND 6L STA Y 1020 AT C. PAX. SUMMARY OF NRC 0486: CRACKS ON LONGERONS 6R, 3L, AND 6L STA Y 1020 AT C. PAX WERE REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURE 2 REPAIR 2. (LP #0678029)
- [SDR DALA2024112511165](https://openairdocs.org/sdr/DALA2024112511165.md): Skin · dented · Nov 23, 2024 · N978AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > DENTS AND NICKS WERE FOUND ON THE EXTERNAL SKIN FLUSH REPAIR STA Y 237 AND BTW LONGERON 17L/18L. ALSO WRONG INSTALLED FASTENERS ON INTERNAL DOUBLERS BTW STA Y218/256 AND BTW LONGERONS 16/18 AT FUSELAGE. SUMMARY OF NRC 00343: PREVIOUS REPAIR ON STA Y 237 AND BT
- [SDR DALA2024112511162](https://openairdocs.org/sdr/DALA2024112511162.md): Skin · dented · Nov 21, 2024 · N978AT · Boeing 717200 · Trailing Edge Flaps
  > SEVERAL DENTS ON SKIN OF AFT MOVABLE FLAP VANE GUIDE AT RH WING. SUMMARY OF NRC 00196: AFT RH FLAP VANE WAS REPLACED PER AMDS 2750-4008. (LP #0670862)
- [SDR DALA2024112211133](https://openairdocs.org/sdr/DALA2024112211133.md): Frame · dented · Nov 21, 2024 · N978AT · Boeing 717200 · Fuselage Main, Frame
  > DENT ON FRAME STA Y=408 AND LONG 27LH AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 634: DENT ON FRAME STA Y=408 AND LONG 27LH AT FWD CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 2, REPAIR 2, FIG. 201. (LP #0670995)
- [SDR DALA2024112111102](https://openairdocs.org/sdr/DALA2024112111102.md): Hinge Fitting · cracked · Nov 20, 2024 · N978AT · Boeing 717200 · Trailing Edge Flaps
  > CRACKED OUTBOARD LOWER BORE OF FLAP HINGE FITTING #3 AT RH WING. RH OUTBOARD WING FLAP HINGE FITTING WAS REMOVED PER B717-200 AMM 57-55-25 000-803 STEP A TO STEP E (2). RH OUTBOARD WING FLAP HINGE FITTING WAS REPLACED & INSTALLED PER B717-200 AMM 57-55-25 400-
- [SDR DALA2024111911028](https://openairdocs.org/sdr/DALA2024111911028.md): Cusp Web · cracked · Nov 18, 2024 · N978AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK AT LH CUSP MEMBRANE AT STA 800 X=55 ON CPAX. SUMMARY OF NRC 00406: CRACK AT LH CUSP MEMBRANE AT STA 800 X=55 ON CPAX WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4. (LP #0666517)
- [SDR DALA2024111911026](https://openairdocs.org/sdr/DALA2024111911026.md): Cusp Web · cracked · Nov 15, 2024 · N978AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACKS ON CUSP MEMBRANE AT STA 655 X=45 AND STA 674 X=46 IN CPAX. SUMMARY OF NRC 00405: CRACKS ON CUSP MEMBRANE AT STA 655 X=45 AND STA 674 X=46 IN CPAX WERE REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4. PERFORM GVI EVERY C-CHECK PER B717 SRM 53-00-55-2R

Next page: https://openairdocs.org/aircraft/N978AT/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 = 'N978AT' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N978AT/reports

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