# Service difficulty reports: N979AT

A list on [N979AT](https://openairdocs.org/aircraft/N979AT.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 · 219 reports

- [SDR DALA2026090204948](https://openairdocs.org/sdr/DALA2026090204948.md): Spar Cap · corroded · Sep 1, 2026 · N979AT · Boeing 717200 · Horizontal Stabilizer, Spar/Rib
  > FOUND CORROSION IN BARREL NUT HOLE AFFECTING THE FRONT SPAR UPPER CAP BARREL NUT HOLE NR 27 OF THE RT HORIZONTAL STAB, COMPLIED WITH ER/A 622779-14. (1789394) (AIRCRAFT GROUNDED).
- [SDR DALA2026082704864](https://openairdocs.org/sdr/DALA2026082704864.md): Lamp · inoperative · Aug 27, 2026 · N979AT · Boeing 717200 · Emergency Lighting
  > OVERHEAD EMERGENCY LIGHT INOP AT 27AB SEAT, RE-LAMP EMERGENCY LIGHT AT SEAT 27AB IAW AMM 33-51. (9222934) (AIRCRAFT GROUNDED).
- [SDR DALA2026060203343](https://openairdocs.org/sdr/DALA2026060203343.md): Lanyard · out of position · May 31, 2026 · N979AT · Boeing 717200 · Emergency Equipment
  > R1 DOOR GIRT BAR IRREGULARITY. FOUND LANYARD OUT OF PLACE. RE-POSITIONED LANYARD. OK FOR SVC. (8236554) (AIRCRAFT GROUNDED)
- [SDR DALA2026020900916](https://openairdocs.org/sdr/DALA2026020900916.md): Light · damaged · Feb 1, 2026 · N979AT · Boeing 717200 · Emergency Lighting
  > FLOOR EMERGENCY PHOTO LUMINESCENT STRIP DAMAGED AT ROW 21 ABC EXIT ROW. REPLACED IAW AMM 33-52. OPS CHECKED FINE. OK FOR SERVICE. (7421382)
- [SDR DALA2025101707597](https://openairdocs.org/sdr/DALA2025101707597.md): None · none · Oct 16, 2025 · N979AT · Boeing 717200 · Standard Practices/Structures
  > SHIP 9544 REPETITIVE INSPECTIONS WITHIN FORTY-SIX HUNDRED (4,600) FLIGHT CYCLES UPON ER/A 617313-14. CORRECTIVE ACTION: C/W REPAIRED PER ERA 617313 (1255743).
- [SDR DALA2025101707596](https://openairdocs.org/sdr/DALA2025101707596.md): Not Reported · not reported · Oct 16, 2025 · N979AT · Boeing 717200 · Vertical Stabilizer
  > SHIP 9544 ACCOMPLISH ER/A 617313-14 REV A. CORRECTIVE ACTION: REPARIED PER ER/A 14-617313. (1255302)
- [SDR DALA2025022501470](https://openairdocs.org/sdr/DALA2025022501470.md): Fuel Cell · leaking · Feb 22, 2025 · N979AT · Boeing 717200 · Fuel Storage
  > -AD- FUEL LEAK FOUND DURING INSPECTION OF THE RH WING AFT LOWER SKIN BTW STA XRS 154 TO STA XRS 164, AFT EDGE BTW LOWER PRODUCTION DOUBLER AND LOWER WING SKIN. CONTACT LIAISON ENGINEERING FOR REPAIR PROCEDURES PRIOR TO THE FURTHER FLIGHT. SUMMARY OF NRC 00061:
- [SDR DALA2025032602224](https://openairdocs.org/sdr/DALA2025032602224.md): Not Reported · not reported · Feb 20, 2025 · N979AT · Boeing 717200 · Standard Practices/Structures
  > -AD- DAMAGE TOLERANCE EVALUATION, ER/A 622334-14 SECT II WITH AMOC TO AD 2024-21-01. DTA MONITOR INSPECTION REQUIRES DTA / AMOC APPROVAL BEFORE THE 1ST OF 30 DAYS OR 177 CYCLES. CONTACT MSP LIAISON ENGINEERING. DISCONTINUE REVENUE SERVICE ON OR BEFORE 30 DAYS
- [SDR DALA2025021801194](https://openairdocs.org/sdr/DALA2025021801194.md): Cable · out of position · Feb 13, 2025 · N979AT · Boeing 717200 · Aerodynamic Fairings
  > TAILCONE DEPLOYMENT SYSTEM CABLE OUT POSITION OF PULLEY STA 1225 IN 2 O'CLOCK POSITION AT AFT ACCESSORY 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 00952: CABLE RO
- [SDR DALA2025100807321](https://openairdocs.org/sdr/DALA2025100807321.md): Hinge Fitting · corroded · Feb 5, 2025 · N979AT · Boeing 717200 · Trailing Edge Flaps
  > IN REFERENCE TO NRC 00309: AFTER REMOVAL SEALANT WAS FOUND CORROSION ON CENTER FLAP HINGE AT LH WING. CENTER WING FLAP HINGE FITTING WAS REMOVED PER B717 AMM 57-55-25-000-802 AND CENTER WING FLAP HINGE (0797513)
- [SDR DALA2025020300803](https://openairdocs.org/sdr/DALA2025020300803.md): Retainer · cracked · Feb 1, 2025 · N979AT · Boeing 717200 · Fuselage Main, Structure
  > CRACK AROUND DRAIN OF RH SLIDING WINDOW RETAINER AT COCKPIT. SUMMARY OF NRC 00468: CRACK AROUND DRAIN OF RH SLIDING WINDOW RETAINER AT COCKPIT WAS REPAIRED PER PRI 622332-14 REV 1 AND ER/A 622332-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-
- [SDR DALA2025013000725](https://openairdocs.org/sdr/DALA2025013000725.md): Drain · cracked · Jan 29, 2025 · N979AT · Boeing 717200 · Fuselage Main, Structure
  > CRACK AROUND DRAIN OF LH SLIDING WINDOW RETAINER AT COCKPIT. SUMMARY OF NRC 00027: CRACK AROUND DRAIN OF LH SLIDING WINDOW RETAINER AT COCKPIT WAS REPAIRED PER PRI 622331-14 REV 1 AND ER/A 622331-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-
- [SDR DALA2025012000466](https://openairdocs.org/sdr/DALA2025012000466.md): Frame · cracked · Jan 18, 2025 · N979AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK ON FRAME DOUBLER STA Y=1178 CANT BTW LONGERON 2-3LH AT AFT ACCESSORY COMPARTMENT. SUMMARY OF NRC 264: FRAME DOUBLER STA Y=1178 CANT BTW LONGERON 2-3LH AT AFT ACCESSORY COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-30-08-2R PROCEDURE 7 REPAIR 7. (LP #07673
- [SDR DALA2025011600360](https://openairdocs.org/sdr/DALA2025011600360.md): Frame · corroded · Jan 15, 2025 · N979AT · Boeing 717200 · Fuselage Main, Frame
  > CORROSION ON FRAME BTW STA Y=851 BTW L29L TO L29R, AND STA Y=870 BTW L29L TO L29R AT AFT CARGO COMPARMENT. SUMMARY OF NRC 00839: CORROSION LEVEL 2. CORROSION ON FRAME BTW STA Y=851 BTW L29L TO L29R, AND STA Y=870 BTW L29L TO L29R AT AFT CARGO COMPARMENT WERE R
- [SDR DALA2025011400313](https://openairdocs.org/sdr/DALA2025011400313.md): Pan · worn · Jan 13, 2025 · N979AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > WEAR ON INNER PAN FWD LOWER CORNER OF FWD CARGO DOOR. SUMMARY OF NRC 00083: INNER AND OUTER PAN FWD EDGE LOWER CORNER OF FWD CARGO DOOR WAS REPAIRED PER PRI 622673-14 REV 4 AND ERA 622673-14, SECTION I, PERMANENT REPAIR, REV ORIGINAL. ASSOCIATED ER/A 14-622673
- [SDR DALA2025011300270](https://openairdocs.org/sdr/DALA2025011300270.md): Skin · damaged · Jan 9, 2025 · N979AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > -AD- ELONGATED HOLES (3 EA) ON CENTER WINGBOX UPPER SKIN STA Y=750 BTW X=44 AND X=50, ALSO ON SAME ANGLE BTW X=44 AND X=50 (4 EA) AT WINGBOX AREA. (CPAX). SUMMARY OF NRC 00750: ELONGATED HOLES (3 EA) ON CENTER WINGBOX UPPER SKIN STA Y=750 BTW X=44 AND X=50 AT
- [SDR DALA2025011300268](https://openairdocs.org/sdr/DALA2025011300268.md): Skin · damaged · Jan 9, 2025 · N979AT · Boeing 717200 · Horizontal Stabilizer, Plate/Skin
  > CORROSION AND TOOL MARKS WERE FOUND ON INNER HOLE #27 AND WEAR ON UPPER SKIN AROUND FROM #27 AT RH HORIZONTAL STAB. SUMMARY OF NRC 00735: CORROSION LEVEL 2. CORROSION IN HOLE #27 AT RH HORIZONTAL STAB WAS REPAIRED PER PRI 622779-14 REV 2 & ER/A 622779-14 REV O
- [SDR DALA2025011300267](https://openairdocs.org/sdr/DALA2025011300267.md): Structure · damaged · Jan 9, 2025 · N979AT · Boeing 717200 · Horizontal Stabilizer Structure
  > CORROSION AND SCRATCHES ON INNER BOLT HOLE AND HOLE OF BARREL NUT (HOLE #26) AT HORIZONTAL STAB. SUMMARY OF NRC 00742: LEVEL CORROSION 2. CORROSION IN INNER BOLT HOLE AND HOLE OF BARREL NUT (HOLE #26) AT HORIZONTAL STAB WAS REPAIRED PER PRI 622843-14 REV 1 & E
- [SDR DALA2025011300265](https://openairdocs.org/sdr/DALA2025011300265.md): Bulkhead · corroded · Jan 9, 2025 · N979AT · Boeing 717200 · Fuselage Main, Bulkhead
  > -AD- CORROSION ON FWD BULKHEAD OF LH WHEEL WELL BTW STA Y737 AND X=18 TO X=30 (UNDER SLANT PANELS). SUMMARY OF NRC 00140: CORROSION LEVEL 2. CORROSION ON FWD BULKHEAD OF LH WHEELL WELL BTW STA Y737 AND X=18 TO X=30 (UNDER SLANT PANELS) WAS REPAIRED PER PRI 622
- [SDR DALA2025011300264](https://openairdocs.org/sdr/DALA2025011300264.md): Structure · damaged · Jan 9, 2025 · N979AT · Boeing 717200 · Rudder Structure
  > SCRATCHES AND MISSING MATERIAL WERE FOUND ON INTERIOR DIAMETER OF ATTACHMENT AREA AT RUDDER. SUMMARY OF NRC 00729: INTERIOR DIAMETER OF ATTACHMENT AREA AT RUDDER WAS REPAIRED PER PRI 622781-14 REV 2 & ER/A 622781-14 REV ORIGINAL. ASSOCIATED ER/A 14-622781 ADDE
- [SDR DALA2025010700129](https://openairdocs.org/sdr/DALA2025010700129.md): Frame · cracked · Jan 6, 2025 · N979AT · Boeing 717200 · Fuselage Main, Frame
  > -AD- CRACK OF 1.00 IN ON UPPER RADIUS OF THE FRAME TAB OF THE OVERWING FRAME AT STA Y=696.000 RH (REF CARD 5310-01436-01D). SUMMARY OF NRC 0470: OVERWING FRAME AT STA Y=696.000 RH WAS REPLACED PER B717-200 SRM 51-41-05-0G, 51-41-02-0G, 51-41-01-0G, AND CARD 53
- [SDR DALA2025010500067](https://openairdocs.org/sdr/DALA2025010500067.md): Cargo Track · corroded · Jan 4, 2025 · N979AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ALONG CARGO TRACK RH AT AFT CARGO COMPARTMENT. SUMMARY: CORROSION LEVEL 2. CORROSION ALONG TRACK RH BTW STA Y=813 TO STA Y=954, AT AFT CARGO COMPARTMENT WAS REMOVED PER B717-200 SRM 51-10-04-0G. (UT) THICKNESS MEASUREMENT WAS ACOMPLISHED WITH ORIGINA
- [SDR DALA2025010300045](https://openairdocs.org/sdr/DALA2025010300045.md): Door Frame · corroded · Jan 2, 2025 · N979AT · Boeing 717200 · Fuselage Main, Structure
  > CORROSION ON DOOR JAMB PAN. ALSO ON PREVIOUS REPAIR DOUBLER AT AFT CARGO COMPARMENT BTW STA Y=954 TO STA Y=994 APROX C2. SUMMARY OF NRC 00133: CORROSION LEVEL 2. DOOR JAMB PAN AT AFT CARGO COMPARTMENT BTW STA Y=954 TO STA Y=994 APPROX C2 WAS REPLACED PER B717-
- [SDR DALA2024123012068](https://openairdocs.org/sdr/DALA2024123012068.md): Skin · cracked · Dec 29, 2024 · N979AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACK ON AFT UPPER CORNER SKIN OF RH SLIDING WINDOW FRAME AT COCKPIT. SUMMARY OF NRC 00707: AFT UPPER CORNER SKIN OF RH SLIDING WINDOW FRAME AT COCKPIT WAS REPAIRED PER B717-200 SRM 56-10-02-2R REPAIR 1 AND FIXED UPPER FLIGHT COMPARTMENT WINDOW RH WAS INSTALLE
- [SDR DALA2024122411973](https://openairdocs.org/sdr/DALA2024122411973.md): Cargo Track · corroded · Dec 24, 2024 · N979AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON TRACK OF AFT CARGO COMPARTMENT STA Y=994 (DOOR JAMB AREA). SUMMARY OF NRC 00722: CORROSION LEVEL 2. TRACK OF AFT CARGO COMPARTMENT STA Y=994 (DOOR JAMB AREA) WAS REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-01-0G. (LP #0725967)
- [SDR DALA2024122712029](https://openairdocs.org/sdr/DALA2024122712029.md): Pin · out of position · Dec 23, 2024 · N979AT · Boeing 717200 · Escape Slide
  > THE INFLATION CABLE PIN WAS OUT OF PLACE. ALSO MISSING THE VALVE LOCK PIN ON THE FWD PASSENGER ENTRANCE DOOR SLIDE (L1). 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 00065: SLID
- [SDR DALA2024122311966](https://openairdocs.org/sdr/DALA2024122311966.md): Cusp Web · cracked · Dec 21, 2024 · N979AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON CUSP WEB BTW STA Y=636-655 X=- 44 TO X=-60 AT PASSENGER CABIN (CPAX). SUMMARY OF NRC 826: CUSP WEB BTW STA Y=636-655 X=-44 TO X=-60 AT PASSENGER CABIN WAS REPAIRED PER B717 SRM 53-00-55-2R-4. (LP #0721136)
- [SDR DALA2024121911826](https://openairdocs.org/sdr/DALA2024121911826.md): Stop Fitting · cracked · Dec 18, 2024 · N979AT · Boeing 717200 · Cargo/Baggage Doors
  > DOOR STOP FITTING #4 WAS FOUND CRACK ON INNER PAN FWD SIDE OF AFT CARGO DOOR. SUMMARY OF NRC 00716: INNER PAN ON FWD SIDE STOP #4 AT AFT CARGO COMPARTMENT DOOR WAS REPAIRED PER ER/A 622684-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 622684-14 REV 1. AS
- [SDR DALA2024121711767](https://openairdocs.org/sdr/DALA2024121711767.md): Cusp Web · corroded · Dec 16, 2024 · N979AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON LH CUSP WEB BTW STA Y=908 TO STA Y=927. SUMMARY OF NRC 00725: CORROSION LEVEL 2. CORROSION ON LH CUSP WEB BTW STA Y=908 TO STA Y=927 WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4, REPAIR 4, PAR 6 FIG 208. (LP #0713769)
- [SDR DALA2024121611737](https://openairdocs.org/sdr/DALA2024121611737.md): Frame · cracked · Dec 14, 2024 · N979AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK ON FRAME STA Y=1037 BTW L-17L AND L-18L AT PASSENGER COMPARTMENT (CPAX). SUMMARY OF NRC 00579: FRAME STA Y=1037 BTW L-17L AND L-18L AT PASSENGER COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-20-07-0G PROCEDURE 4 REPAIR 4. (LP #0709303)
- [SDR DALA2024121311701](https://openairdocs.org/sdr/DALA2024121311701.md): Longeron · cracked · Dec 12, 2024 · N979AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CRACKED LONGERONS L-3R, L-4R, L-5R, AND L-8R ON STA Y=1022 AT PASSENGER COMPARTMENT. (CPAX). SUMMARY OF NRC 00580: LONGERONS L-3R, L-4R, L-5R, AND L-8R ON STA Y=1022 AT PASSENGER COMPARTMENT WERE REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURE 2 REPAIR 2. (LP
- [SDR DALA2024121111615](https://openairdocs.org/sdr/DALA2024121111615.md): Cusp Web · cracked · Dec 10, 2024 · N979AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON CUSP WEB STA Y=815 X=44 AT PASSENGER CABIN (CPAX). SUMMARY OF NRC 00606: CUSP WEB STA Y=815 X=44 AT PASSENGER CABIN (CPAX) WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4 FIG 221. (LP #0703712)
- [SDR DALA2024121111614](https://openairdocs.org/sdr/DALA2024121111614.md): Beam · cracked · Dec 10, 2024 · N979AT · Boeing 717200 · Passenger/Crew Doors
  > CRACK ON INTERNAL STRUCTURE LL BEAM #1 STA 195 AT PASSENGER DOOR. SUMMARY OF NRC 00293: BEAM #1 ON INTERNAL STRUCTURE STA 195 AT PASSENGER DOOR (L1) WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 7 REPAIR 7. (LP #0703468)
- [SDR DALA2024121111613](https://openairdocs.org/sdr/DALA2024121111613.md): Longeron · cracked · Dec 10, 2024 · N979AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CRACKED LONGERONS L-4L AND L-5L ON STA Y=1022 AT PASSENGER COMPARTMENT. (CPAX) SUMMARY OF NRC 00581: LONGERONS L-4L AND L-5L ON STA Y=1022 AT PASSENGER COMPARTMENT WERE REPAIRED PER B717-200 SRM 53-00-05-2R REPAIR 2. (LP #0703457)
- [SDR DALA2024121111612](https://openairdocs.org/sdr/DALA2024121111612.md): Frame Angle · cracked · Dec 10, 2024 · N979AT · Boeing 717200 · Nacelle/Pylon, Main Frame
  > CRACK ON FRAME CLIP (ENGINE PYLON SUPPORT BULKHEAD) IN STA Y=1022 AT L7 LH. SUMMARY OF NRC 00536: FRAME CLIP (ENGINE PYLON SUPPORT BULKHEAD) IN STA Y=1022 AT L7 LH WAS REPAIRED PER ERA 622468-14 REV ORIGINAL. (LP #0703045)
- [SDR DALA2024120911539](https://openairdocs.org/sdr/DALA2024120911539.md): Cusp Web · damaged · Dec 8, 2024 · N979AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > TOOL MARK ON CUSP WEB AND SPLICE BTW STA Y=794, X44 TO X54 AT CABIN PASENGER. SUMMARY OF NRC 00547: CUSP WEB ON STA 796 X44 TO X54 WAS REPAIRED PER B717 SRM 53-00-55-2R. (LP #0700055)
- [SDR DALA2024120911538](https://openairdocs.org/sdr/DALA2024120911538.md): Doubler · cracked · Dec 6, 2024 · N979AT · Boeing 717200 · Cargo/Baggage Doors
  > CRACK ON EXTERNAL DOUBLER OF CUTOUT CLOSE/OPEN HANDLE AT FWD CARGO DOOR (C1). SUMMARY OF NRC 00088: EXTERNAL DOUBLER OF CUTOUT CLOSE/OPEN HANDLE AT FWD CARGO DOOR (C1) WAS FABRICATED AND REPLACED PER B717-200 SRM 52-30-01-2R PROCEDURE 1 REPAIR 1 PAR. 4B (9), (
- [SDR DALA2024120911537](https://openairdocs.org/sdr/DALA2024120911537.md): Longeron · cracked · Dec 6, 2024 · N979AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CRACK ON LONGERON 17 LH, LONGERON 8 LH, AND LONGERON 13 LH BTW STA Y=1020 AND STA Y=1023 LH SIDE. SUMMARY OF NRC 537: LONGERON 17 LH AND LONGERON 8 LH BTW STA Y=1020 AND STA Y=1023 LH WERE REPAIRED PER B717-200 SRM 53-00-05-2R REPAIR 2. AND LONGERON 13 LH HAD
- [SDR DALA2024120911535](https://openairdocs.org/sdr/DALA2024120911535.md): Seat Track · corroded · Dec 5, 2024 · N979AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK X=56 AND STA 996 IN PAX CABIN. SUMMARY OF NRC 723: CORROSION LEVEL 2. SEAT TRACK X=56 AND STA 996 IN PAX CABIN WAS REPAIRED PER B717 SRM 53-20-52-2R PROCEDURE 1 REPAIR 1 FIGURE 201. PERFORM DECAL INSPECTION CONDITION EVERY C-CHECK PER T
- [SDR DALA2024120211372](https://openairdocs.org/sdr/DALA2024120211372.md): Doubler · corroded · Nov 29, 2024 · N979AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CORROSION ON DOUBLER BELOW TEE FITTING STA 1053 LONGERON 30 AT AFT BULKHEAD. SUMMARY OF NRC 00563: CORROSION LEVEL 2. DOUBLER BELOW TEE FITTING STA 1053 LONGERON 30 AT AFT BULKHEAD WAS REPLACED PER B717 SRM 53-20-08-0I PROCEDURE 2 AND 51-41-05-0G. (LP #0684614
- [SDR DALA2024111911025](https://openairdocs.org/sdr/DALA2024111911025.md): Vane · dented · Nov 15, 2024 · N979AT · Boeing 717200 · Trailing Edge Flaps
  > -AD- DENTS ON RH WING FWD MOVABLE VANE INBD SURFACE. SUMMARY OF NRC 00326: DENTS (3 LOCATIONS) ON LOWER SKIN OF FWD MOVABLE VANE RH WING WERE EVALUATED AND FOUND OUT LIMITS. RH WING FWD MOVABLE VANE WAS REPAIRED PER B717-200 SRM 57-53-01-2R PROCEDURE 1 REPAIR
- [SDR DALA2024041804532](https://openairdocs.org/sdr/DALA2024041804532.md): Skin · cracked · Apr 16, 2024 · N979AT · Boeing 717200 · Vertical Stabilizer, Plate/Skin
  > -AD- FOUND 4 EA HOLES ON LT VERT BELOW EXISTING DOUBLER AT SPLICE SHOWING CRACK INDICATIONS. C/W ER/A 617313-14AD REV ORIG SECTION I PERMANENT REPAIR. ALL RII C/W (QC1430) REF TO LOG PAGE 0297160 AND BUFF NRC 001. ASSOCIATED ER/A 14-6173133
- [SDR DALA2024041804530](https://openairdocs.org/sdr/DALA2024041804530.md): Skin · cracked · Apr 16, 2024 · N979AT · Boeing 717200 · Vertical Stabilizer, Plate/Skin
  > -AD- VERTICAL STAB LEFT SIDE 4 EA HOLES HAVE CRACK INDICATIONS, IN SKIN LAYER ONLY, JUST BELOW ZFS 52.267. BHEC INSP CONFIRMS CRACKS IN 4 EA HOLES IN SKIN LAYER ONLY REF AA 5530-01048 AND AD 2018-10-08 -MARKED-. COMPLIED WITH PRI 617313-14AD REV 0. C/W PRI 617
- [SDR DALA2024011900811](https://openairdocs.org/sdr/DALA2024011900811.md): Lens · missing · Jan 18, 2024 · N979AT · Boeing 717200 · Emergency Lighting
  > CABIN EMERGENCY LIGHT LENS MISSING AT 2B. MAINTENANCE FOUND STAND-BY OVERHEAD EMERGENCY LIGHT COVER MISSING AT ROW 2. INSTALLED THE LIGHT COVER AS REQUIRED REF B717 AMM 33-51. AIRCRAFT IS OK FOR SERVICE. (LP #0160810)
- [SDR DALA2023102308703](https://openairdocs.org/sdr/DALA2023102308703.md): Unknown · unknown · Oct 20, 2023 · N979AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > ELONGATED AND CRACKED HOLES ON FUSELAGE SKIN AT STA Y=1178 PROJECTION OF SPAR 14L IN REF NRC 00086. SUMMARY OF NRC 00123: DAMAGE IN HOLES ON FUSELAGE SKIN AT STA Y=1178 PROJECTION OF SPAR 14L WAS REPAIRED PER B717-200 SRM 53-03- 01-2R REPAIR I. PAR. 6 J. FIG.
- [SDR DALA2023102008643](https://openairdocs.org/sdr/DALA2023102008643.md): Unknown · unknown · Oct 19, 2023 · N979AT · Boeing 717200 · Trailing Edge Flaps
  > SEVERAL DENTS ON UPPER SKIN ON AFT MOVABLE FLAP VANE AT LH WING. SUMMARY OF NRC 00053: UPPER SKIN ON AFT MOVABLE FLAP VANE AT LH WING WAS REPAIRED PER ER/A 612869-14 REV ORIGINAL. ASSOCIATED ER/A 14-612869 ADDED FOR AC 9544. (LP #0025737)
- [SDR DALA2023102008640](https://openairdocs.org/sdr/DALA2023102008640.md): Unknown · unknown · Oct 19, 2023 · N979AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON PAN AT AFT CARGO DOOR 994 BTW BEAM 1 TO 2. SUMMARY OF NRC-0087: INNER AND OUTBOARD PAN AT AFT CARGO DOOR 994 BTW BEAM 1 TO 2 WERE REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 8, REPAIR 8, PAR 4. (LP #0024588)
- [SDR DALA2023092507854](https://openairdocs.org/sdr/DALA2023092507854.md): Unknown · unknown · Sep 21, 2023 · N979AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > FOUND INTERCOSTAL CRACKED BETWEEN STA 946.5 AND 954. FABBED NEW INTERCOSTAL PER DWG 9915578 AND SRM 53-20-51-0I PROC 7. INSTALLED INTERCOSTAL PER B717 SRM 51-41. (LP #2980699)
- [SDR DALA2023022701432](https://openairdocs.org/sdr/DALA2023022701432.md): Panel · damaged · Feb 22, 2023 · N979AT · Boeing 717200 · Fuselage Internal Mounting Structure
  > PANEL DAMAGED AND BENT. REPAIRED AND FABRICATED PANEL.
- [SDR DALA2022080205278](https://openairdocs.org/sdr/DALA2022080205278.md): Battery · inoperative · Jul 27, 2022 · N979AT · Boeing 717200 · Emergency Lighting
  > THE OVER WING EMERGENCY EXIT LIGHTS ARE NOT ILLUMINATING. MAINTENANCE REPLACED THE FWD OVER WING EMERGENCY EXIT LIGHT BATTERY ASSEMBLY PER B717 AMM 33- 11. OPERATIONAL CHECK WAS GOOD. OK FOR SERVICE. (LP #8967630)

Next page: https://openairdocs.org/aircraft/N979AT/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 = 'N979AT' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N979AT/reports

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