# Service difficulty reports: N970AT

A list on [N970AT](https://openairdocs.org/aircraft/N970AT.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 · 201 reports

- [SDR DALA2026102105788](https://openairdocs.org/sdr/DALA2026102105788.md): Skin · dented · Oct 20, 2026 · N970AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > FOUND DENTS AT LOWER FUSELAGE SKIN BETWEEN STA Y=495 & Y=507/L-28L & L-29, COMPLIED WITH ER/A 625374-14. (1876653) (AIRCRAFT GROUNDED).
- [SDR DALA2026101405655](https://openairdocs.org/sdr/DALA2026101405655.md): Scuff Plate · damaged · Oct 14, 2026 · N970AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > FOUND AFT CARGO BAY SCUFF PLATE DAMAGED. COMPLIED WITH ER/A 637522-14. (8981866) (AIRCRAFT GROUNDED).
- [SDR DALA2026100605531](https://openairdocs.org/sdr/DALA2026100605531.md): Window · delaminated · Oct 2, 2026 · N970AT · Boeing 717200 · Door Windows
  > WINDOW AT 19E SHOWS SIGNS OF DELAMINATION. R & R FWD RT O/W EMERGENCY EXIT DOOR ASSY IAW AMM 52-21-01. OPS & LEAK CHKD GOOD. (8981818) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026091105081](https://openairdocs.org/sdr/DALA2026091105081.md): Windshield · cracked · Sep 10, 2026 · N970AT · Boeing 717200 · Flight Compartment Windows
  > CA WINDSHIELD CRACKED DURING FLIGHT ARCING NEAR TOP, R & R LT SIDE FLIGHT COMPARTMENT WINDSHIELD IAW AMM 56-11. (9184422) (AIRCRAFT GROUNDED).
- [SDR DALA2026090304978](https://openairdocs.org/sdr/DALA2026090304978.md): Oxygen Mask · unwanted deploy · Sep 2, 2026 · N970AT · Boeing 717200 · Passenger Oxygen System
  > O2 MASK DROPPED OVER SEATS 15CDE, RESTOWED O2 MASKS IAW AMM 35-23. (8816982) (AIRCRAFT GROUNDED).
- [SDR DALA2026071704218](https://openairdocs.org/sdr/DALA2026071704218.md): Light · inoperative · Jul 15, 2026 · N970AT · Boeing 717200 · Emergency Lighting
  > FOUND OVERHEAD L1 EMERGENCY LIGHT INOPERATIVE, REMOVED & REPLACED LIGHT ASSEMBLY L2-789. IAW AMM 33-51. (8820878) (AIRCRAFT GROUNDED).
- [SDR DALA2026070103878](https://openairdocs.org/sdr/DALA2026070103878.md): Lamp · inoperative · Jun 27, 2026 · N970AT · Boeing 717200 · Emergency Lighting
  > R1 DOOR ENTRY LIGHTS INOP, RELAMPED IAW AMM 33-23-09. (8543381) (AIRCRAFT GROUNDED).
- [SDR DALA2025090906668](https://openairdocs.org/sdr/DALA2025090906668.md): Brace · damaged · Sep 2, 2025 · N970AT · Boeing 717200 · Wing Main, Frame Structure
  > PER DAL ENGINEERING REQUEST: PERFORM INSPECTIONS ON REAR SPAR AT RT WING. LOWER FLAP BRACE DOUBLER AT STA XRS 164 ON LOWER SURFACE AND REAR SPAR OF RH WING WERE REPAIRED PER PRI 626006-14 (1177079)
- [SDR DALA2025090406559](https://openairdocs.org/sdr/DALA2025090406559.md): Doubler · cracked · Aug 26, 2025 · N970AT · Boeing 717200 · Wing, Plate/Skin
  > CRACK ON DOUBLER BTW STA: XRS164 AND 150.450 AT LT WING. LOWER SURFACE OF LT WING WAS REPAIRED PER ER/A 626343-14AD (1165171)
- [SDR DALA2025090406561](https://openairdocs.org/sdr/DALA2025090406561.md): Repair · cracked · Aug 22, 2025 · N970AT · Boeing 717200 · Wing, Plate/Skin
  > LEFT WING, LOWER SURFACE, LOWER FLAP BRACE DOUBLER AT XRS 164 HAS A CRACK IN TIME LIMITED REPAIR. REPAIRED LOWER WING SKIN AND SPAR PER ERA 626343-14AD (1158212).
- [SDR DALA2025040802703](https://openairdocs.org/sdr/DALA2025040802703.md): Skin · dented · Apr 7, 2025 · N970AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > DENTS ON SKIN BTW STA Y=493 AND STA Y=510 BTW LONG 28L AND LONG 29R AT CTR LOWER FUSELAGE. SUMMARY OF NRC 00025: DENTS ON SKIN BTW STA Y=493 AND STA Y=510 BTW LONG 28L AND LONG 29R WERE REPAIRED PER ER/A 625374-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSO
- [SDR DALA2024050104840](https://openairdocs.org/sdr/DALA2024050104840.md): Battery Pack · no test · May 1, 2024 · N970AT · Boeing 717200 · Emergency Lighting
  > ON SERVICE CHECK THE EMERGENCY EXIT SIGN ABOVE THE L1 DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND POWER SUPPLY B5-235 PER B717 AMM 33-51. LIGHT OPERATION NOW CHECKS GOOD. THE AIRCRAFT IS OK FOR SERVICE. (LP #5307990)
- [SDR DALA2024060405770](https://openairdocs.org/sdr/DALA2024060405770.md): Window · missing · Apr 20, 2024 · N970AT · Boeing 717200 · Passenger Compartment Windows
  > 17A OUTER GLASS WINDOW MISSING ON POST FLIGHT INSPECTION. REPLACED OUTER PANE AT SEAT 17A PER B717 AMM 56-20. NO LEAKS A/C OK FOR SVC. (LP #5307957)
- [SDR DALA2023051203749](https://openairdocs.org/sdr/DALA2023051203749.md): Unknown · unknown · May 12, 2023 · N970AT · Boeing 717200 · Fuselage Floor Panel
  > CRACK ON PAN (FASTENER HOLE AREA) ABOVE SEAL RETEINER AT AFT CARGO DOOR. SUMMARY OF NRC-00071: PAN ON 3 AREAS AT AFT CARGO COMPARTMENT DOOR WAS REPAIRED PER ERA 608442-14, REV ORIGINAL, SECTION I AND PRI 608442-4, REV 1. (LP #2763196)
- [SDR DALA2023051203743](https://openairdocs.org/sdr/DALA2023051203743.md): Unknown · unknown · May 10, 2023 · N970AT · Boeing 717200 · Emergency Lighting
  > DURING TEST OF EMERGENCY LIGHTS, THE OVERWING LIGHTS STAY ON WITH THE SWITCH AT THE FORWARD ATTENDANT PANEL, IN THE OFF POSITION. SUMMARY OF NRC 00565: THE OVERWING EMERGENCY EVACUATION BATTERY POWER SUPPLY WAS REPLACED PER B717-200 AMM 33-51-06. TEST OK. (LP
- [SDR DALA2023051103711](https://openairdocs.org/sdr/DALA2023051103711.md): Unknown · unknown · May 10, 2023 · N970AT · Boeing 717200 · Vertical Stabilizer, Plate/Skin
  > IN REF TO CARD AD A.A. 5530-01048-03: PERFORM PERMANENT REPAIR (VERTICAL STABILIZER SPLICE BAND). SUMMARY OF NRC-00504: 48 HOLES OF VERTICAL STABILIZER LEADING EDGE STA ZFS=52.267. WERE MEASURED AND 26 HOLES OF 1/4" DIAMETER AND 5 HOLES OF 3/16" DIAMETER WERE
- [SDR DALA2023051003665](https://openairdocs.org/sdr/DALA2023051003665.md): Unknown · unknown · May 9, 2023 · N970AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CORROSION ON FRAME CLIP STA Y=1028 AFT CARGO. SUMMARY OF NRC 00566: CORROSION LEVEL 2. FRAME CLIP STA Y=1028 AFT CARGO WAS REPLACED PER B717-200 SRM 53-00-06-2R PROCEDURE 2 REPAIR 2 AND SRM 51-41-05-0G PAR 8 AND 51-41-02-0G. ALSO WAS FABRICATED PER DWG 9912243
- [SDR DALA2023050903614](https://openairdocs.org/sdr/DALA2023050903614.md): Unknown · unknown · May 9, 2023 · N970AT · Boeing 717200 · Escape Slide
  > CUT ON LANYARD ASSY CABLE OF DOOR 1 LEFT ESCAPE SLIDE (L1). THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY OF NRC 00568: LANYARD ASSY CABLE OF DOOR 1 LEFT ESCAPE SLIDE WAS REPLACED PER B717-
- [SDR DALA2023050803568](https://openairdocs.org/sdr/DALA2023050803568.md): Unknown · unknown · May 6, 2023 · N970AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > ELONGATED HOLES ON CARGO TRACK BTW STA Y408 TO Y427, LONGERONS 27L AND 28L AT FWD CARGO COMPARTMENT (C1). SUMMARY OF NRC 00200: CARGO TRACK BTW STA Y408 TO Y427, LONGERONS 27L AND 28L AT FWD CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-20-52-2R PROCEDURE
- [SDR DALA2023050403459](https://openairdocs.org/sdr/DALA2023050403459.md): Unknown · unknown · May 4, 2023 · N970AT · Boeing 717200 · Fuselage Main, Frame
  > CORROSION ON LOWER SKIN OF CUSP ANGLE FROM STA 200 TO 218 AND -X=56 AT PASSENGER CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00489: LOWER SKIN OF CUSP ANGLE FROM STA 200 TO 218 AND -X=56 AT PASSENGER CABIN FLOOR STRUCTURE WAS REPAIRED PER ER/A 607622-14 REV. ORIGINA
- [SDR DALA2023050203393](https://openairdocs.org/sdr/DALA2023050203393.md): Unknown · unknown · May 1, 2023 · N970AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CORROSION ON LONGERON END RH L24 APROX STA Y=1002 OF AFT CARGO COMPARTMENT. SUMMARY OF NRC 00256: CORROSION LEVEL 2. LONGERON END RH L24 APROX STA Y=1002 OF AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-05-0G PAR. 8. (LP #2745776)
- [SDR DALA2023050203391](https://openairdocs.org/sdr/DALA2023050203391.md): Unknown · unknown · Apr 28, 2023 · N970AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > DENTS ON EXTERNAL SKIN BTW STA Y=218 TO 245 AND L-17L TO L-18L AT FUSELAGE, IN REFERENCE TO LP 1614671 AND LP 1614671. SUMMARY OF NRC 00535: FUSELAGE EXTERNAL SKIN BTW STA Y=229 TO 237 AND L-17L TO L-18L WAS PERMANENT REPAIRED PER B717-200 SRM 53-10-01-2R REPA
- [SDR DALA2023050203390](https://openairdocs.org/sdr/DALA2023050203390.md): Unknown · unknown · Apr 28, 2023 · N970AT · Boeing 717200 · Fuselage Floor Panel
  > CRACKS (3 EA) ON AFT PAN OF FROM BEAM #3 TO BEAM #5 AND CRACKS (3 EA) ON FWD PAN FROM BEAM #1 AND BEAM #4 OF FWD CARGO DOOR. ALSO CRACK (1 EA) ON UPPER PAN CLOSE OF AFT HINGE. SUMMARY OF NRC 00093: CRACKS (3 EA) ON AFT PAN OF FROM BEAM #3 TO BEAM #5 AND CRACKS
- [SDR DALA2023042803322](https://openairdocs.org/sdr/DALA2023042803322.md): Unknown · unknown · Apr 27, 2023 · N970AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > DENTS ON EXTERNAL SKIN BTW STA Y=218 TO 245 AND L-17L TO L-18L AT FUSELAGE. SUMMARY OF NRC 00525: DENTS ON EXTERNAL SKIN BTW STA Y=218 TO 229 AND L-17L TO L-18L AT FUSELAGE WAS ATTENDENTED WITH LOG 1614618, 1614633, & 1614629 AND FOUND WITHIN ALLOWABLE LIMITS
- [SDR DALA2023042603250](https://openairdocs.org/sdr/DALA2023042603250.md): Unknown · unknown · Apr 26, 2023 · N970AT · Boeing 717200 · Fuselage Floor Panel
  > DURING ATTENTION OF NRC 00399, FLOOR SUPPORTS (2 EA) ON STA 148 TO 200 X=-54 WERE FOUND CORRODED OUT OF LIMITS. SUMMARY OF NRC 00491: CORROSION LEVEL 2. FLOOR SUPPORTS (2 EA) ON STA 148 TO 200 X=-54 WERE FABRICATED AND REPLACED PER B717-200 SRM 51-30-07-0G FIG
- [SDR DALA2023042603248](https://openairdocs.org/sdr/DALA2023042603248.md): Unknown · unknown · Apr 25, 2023 · N970AT · Boeing 717200 · Fuselage Main, Frame
  > CORROSION ON FLOOR ANGLE BTW STA Y=200 AND STA Y=210 AND X=-54 OF AFT DOOR JAMB AT FWD SERVICE DOOR. SUMMARY OF NRC 00397: CORROSION LEVEL 2. FLOOR ANGLE BTW STA Y=200 AND STA Y=210 AND X=-54 OF AFT DOOR JAMB AT FWD SERVICE DOOR WAS REPLACED PER B717-200 SRM 5
- [SDR DALA2023042503243](https://openairdocs.org/sdr/DALA2023042503243.md): Unknown · unknown · Apr 25, 2023 · N970AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK ON FRAME STA Y=1022 AND LONGERON 7RH AT PAX CABIN. SUMMARY OF NRC 00402: CRACK ON FRAME STA Y=1022 AND LONGERON 7RH AT PAX CABIN WAS REPAIRED PER ER/A 607699-14 REV ORIGINAL SECTION I, PERMANENT REPAIR AND PRI 607699-14 REV 0. ASSOCIATED ER/A 14-607699 A
- [SDR DALA2023042503242](https://openairdocs.org/sdr/DALA2023042503242.md): Unknown · unknown · Apr 24, 2023 · N970AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK ON FRAME STA Y=1022 AND LONGERON 7LH AT PAX CABIN. SUMMARY OF NRC 00299: CRACK ON FRAME STA Y=1022 AND LONGERON 7LH AT PAX CABIN WAS REPAIRED PER ER/A 607681-14 REV ORIGINAL SECTION I, PERMANENT REPAIR AND PRI 607681-14 REV 0. ASSOCIATED ER/A 14-607681 A
- [SDR DALA2023042503238](https://openairdocs.org/sdr/DALA2023042503238.md): Unknown · unknown · Apr 22, 2023 · N970AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR ANGLE CLIP APPROX STA Y=168 AND X=-56 AT W1. SUMMARY OF NRC 00400; CORROSION LEVEL 2. FLOOR ANGLE CLIP APPROX STA Y=168 AND X=-56 AT W1 WAS FABRICATED PER DWG 5910085 REV DJ AND REPLACED PER B717-200 SRM 51-41-05-0G. (LP #2732197)
- [SDR DALA2023042503237](https://openairdocs.org/sdr/DALA2023042503237.md): Unknown · unknown · Apr 22, 2023 · N970AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON MEMBRANE FROM STA Y=150 TO Y=218 AND -X=47 TO -X=60 AT PAX CABIN (CPAX). SUMMARY OF NRC 00389: CORROSION LEVEL 2. MEMBRANE FROM STA Y=150 TO Y=218 AND -X=47 TO -X=60 AT PAX CABIN (CPAX) WAS REPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 2 FIG. 20
- [SDR DALA2023042003110](https://openairdocs.org/sdr/DALA2023042003110.md): Unknown · unknown · Apr 20, 2023 · N970AT · Boeing 717200 · Fuselage Floor Panel
  > CORROSION ON UPPER MEMBRANE FROM STA Y=150 TO Y=170 AND -X=47 TO -X=60 AT PASSENGER CABIN. SUMMARY OF NRC 00528: CORROSION LEVEL 2. WEB FROM STA Y=150 TO Y=170 AND -X=47 TO -X=60 AT PASSENGER CABIN WAS REPLACED PER B717-200 SRM 51-41-02-0G AND SRM 51-41-05-0G
- [SDR DALA2023041803050](https://openairdocs.org/sdr/DALA2023041803050.md): Unknown · unknown · Apr 17, 2023 · N970AT · Boeing 717200 · Fuselage Main, Frame
  > AD. CRACK WAS FOUND ON RH OVERWING FRAME, LENGTH=0.600 IN IN REF TASK CARD 5310-01436-01D JOB #084-0004 STEP 7. SUMMARY OF NRC 00322: OVERWING FRAME RH LENGTH=0.600 IN. IN REF TASK CARD 5310-01436-01D JOB #084-0004 STEP 7 WAS REPLACED PER B717-200 TASK CARD 53
- [SDR DALA2023041803048](https://openairdocs.org/sdr/DALA2023041803048.md): Unknown · unknown · Apr 16, 2023 · N970AT · Boeing 717200 · Fuselage Main, Frame
  > REWRITE. SECONDARY NRC IN REF NRC 311: CORROSION ON CUSP MEMBRANE (WEB) RH STA Y=427 AT PAX CABIN. SUMMARY OF NRC 00525: CORROSION LEVEL 2. REPAIR DOUBLER WAS FABRICATED AND REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4, REPAIR 4, PAR. 5B (9), FIG: 211, GE
- [SDR DALA2023041803047](https://openairdocs.org/sdr/DALA2023041803047.md): Unknown · unknown · Apr 16, 2023 · N970AT · Boeing 717200 · Fuselage Main, Frame
  > CORROSION ON FWD FACE BELOW FLOOR BULKHEAD RBL 20 AND LBL 20 STA 1053 AT PAX CABIN. SUMMARY OF NRC 00429: CORROSION LEVEL 2. GUSSETS ON FWD FACE BELOW FLOOR BULKHEAD RBL 20 AND LBL 20 STA 1053 AT PAX CABIN WERE REPLACED PER DWG 3925389 ITEM 1 & 2 AND B717-200
- [SDR DALA2023041402966](https://openairdocs.org/sdr/DALA2023041402966.md): Unknown · unknown · Apr 14, 2023 · N970AT · Boeing 717200 · Fuselage Floor Panel
  > DENT ON LH CUSP MEMBRANE STA Y=927 AT PAX CABIN. SUMMARY OF NRC 00419: DENT ON LH CUSP MEMBRANE STA Y=927 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4, REPAIR 4. (LP #2718821)
- [SDR DALA2023041202862](https://openairdocs.org/sdr/DALA2023041202862.md): Unknown · unknown · Apr 11, 2023 · N970AT · Boeing 717200 · Fuselage Floor Panel
  > CRACK ON CUSP WEB MEMBRANE (2EA) BTW STA Y636 AND Y655, LONGERONS 18L AND 18R AT FWD CARGO COMPARTMENT (C1). SUMMARY OF NRC 00287: CRACK ON CUSP WEB MEMBRANE (2EA) BTW STA Y636 AND Y655 LONGERONS AND 18R AT FWD CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 5
- [SDR DALA2023041002744](https://openairdocs.org/sdr/DALA2023041002744.md): Unknown · unknown · Apr 8, 2023 · N970AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CRACK ON INTERCOSTAL BTW STA Y617 TO STA Y636 LONGERONS 18L AND 18R AT FWD CARGO COMPARTMENT (C1). SUMMARY OF NRC 00291: INTERCOSTAL BTW STA Y617 TO STA Y636 LONGERONS 18L AND 18R AT FWD CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-00-00-2R PROCEDURE 1.
- [SDR DALA2023040502677](https://openairdocs.org/sdr/DALA2023040502677.md): Unknown · unknown · Apr 4, 2023 · N970AT · Boeing 717200 · Vertical Stabilizer, Plate/Skin
  > SECONDARY NRC IN REF AMDS 5530-01048-02: "AA 5530-01048" AND "AD 2018-10-08". LOOSE FASTENERS OF RH VERTICAL STABILIZER LEADING EDGE STRUCTURE SPLICE (STA ZFS=52.267). SUMMARY OF NRC 00428: FASTENERS HOLES COUNTER SINK AND DIAMETER ON RH VERTICAL STABILIZER LE
- [SDR DALA2023040502676](https://openairdocs.org/sdr/DALA2023040502676.md): Unknown · unknown · Apr 4, 2023 · N970AT · Boeing 717200 · Vertical Stabilizer, Plate/Skin
  > SECONDARY NRC IN REF AMDS 5530-01048-02: "AA 5530-01048" AND "AD 2018-10-08". LOOSE FASTENERS OF LH VERTICAL STABILIZER LEADING EDGE STRUCTURE SPLICE (STA ZFS=52.267). SUMMARY OF NRC 00427: FASTENERS HOLES COUNTER SINK AND DIAMETER ON LH VERTICAL STABILIZER LE
- [SDR DALA2023030101526](https://openairdocs.org/sdr/DALA2023030101526.md): None · none · Feb 25, 2023 · N970AT · Boeing 717200 · Passenger/Crew Doors
  > FOUND LOWER AFT CORNER OF L1 DOOR DAMAGED AFTER AIRCRAFT ARRIVAL. INSPECTED DAMAGE AREA. REMOVED REQ FASTENERS AND CUT OUT DAMAGE PER B717 SRM 52-10-01-2R-1. PREFORMED DAMAGE CONTAINMENT REF NDT SPM 06.10.01.001 PROCEDURE 1 NO DEFECTS AND OPEN HOLE REF NDTSPM
- [SDR DALA2022070504625](https://openairdocs.org/sdr/DALA2022070504625.md): None · none · Jul 3, 2022 · N970AT · Boeing 717200 · Emergency Lighting
  > THE EMERGENCY LIGHTS AT LOCATIONS POWERED BY B5-123 BATTERY PACK ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY BATTERY PACK PER B717 AMM 33-51, AT THE B5-123 LOCATION. THE EMERGENCY LIGHTS OPERATIONAL CHECK WAS GOOD. (LP #9217075)
- [SDR DALA2022050103044](https://openairdocs.org/sdr/DALA2022050103044.md): Light · inoperative · May 1, 2022 · N970AT · Boeing 717200 · Exterior Lighting
  > THE AFT OVERWING EXIT LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY TRAY FOR EXIT LIGHT POSITION B5-230 IAW B717 AMM 33-51-00. OPERATIONAL CHECK WAS GOOD. (LP #6884529)
- [SDR DALA2022042903014](https://openairdocs.org/sdr/DALA2022042903014.md): None · none · Apr 27, 2022 · N970AT · Boeing 717200 · Wing, Plate/Skin
  > CORROSION UPPER WING SURFACE AT STA 324 & STR 5 (RIGHT WING). BLENDED CORROSION AT STA 324 STR 5 RH WING UPPER SURFACE PER B717 SRM 51-10-04. C/W HFEC INSPECTION PER ERA 598953- 14 REV 0. NO INDICATIONS NOTED. C/W UT REMAINING THICKNESS CHECK PER ERA 598953-14
- [SDR DALA2022032401938](https://openairdocs.org/sdr/DALA2022032401938.md): Unknown · unknown · Mar 24, 2022 · N970AT · Boeing 717200 · Emergency Lighting
  > THE EMERGENCY EXIT SIGN ABOVE THE FWD FLIGHT ATTENDANT SEAT IS INOPERATIVE. MAINTENANCE REPLACED THE #2 EMERGENCY LIGHT BATTERY ASSEMBLY PER B717 AMM 35-51. OPERATIONAL CHECK WAS GOOD. (LP #8250120)
- [SDR DALA2022031801806](https://openairdocs.org/sdr/DALA2022031801806.md): None · none · Mar 17, 2022 · N970AT · Boeing 717200 · Tire
  > FLIGHT CREW DECLARED AN EMERGENCY DUE TO A REPORT OF A SEPERATED TIRE. THE AIRCRAFT MADE A NORMAL SAFE LANDING AND UN-EVENTFUL TAXI AT ATL. MAINTENANCE INSPECTED ALL TIRE/WHEEL ASSEMBLIES PER B717 AMM 32-41. NO DAMAGE WAS FOUND AND EVERYTHING WAS IN GOOD CONDI
- [SDR DALA2021062203376](https://openairdocs.org/sdr/DALA2021062203376.md): Lens · detached · Jun 21, 2021 · N970AT · Boeing 717200 · Emergency Lighting
  > THE FORWARD EXIT SIGN COVER FELL OF ON LANDING AND COULD NOT BE FOUND. LATER, MAINTENANCE REINSTALLED THE EMERGENCY EXIT COVER. OPERATIONAL CHECK WAS OK. EMERGENCY LIGHTS OPERATE OK PER B717-AMM 33-50. (LP #7568382)
- [SDR DALA2021050302491](https://openairdocs.org/sdr/DALA2021050302491.md): Battery Pack · inoperative · May 2, 2021 · N970AT · Boeing 717200 · Emergency Lighting
  > THE EXTERIOR OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE OVERWING EMERGENCY EVACUATION LIGHTS BATTERY PACK, B5-125, PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #7603721)
- [SDR DALA2022110207101](https://openairdocs.org/sdr/DALA2022110207101.md): None · none · Mar 23, 2021 · N970AT · Boeing 717200 · Standard Practices/Structures
  > DAMAGE TOLERANCE EVALUATION REQUIRED FOR ERA 590529-14. REPAIR APPROVAL IS LIMITED TO 24 MONTHS SERVICE FROM DATE OF APPROVAL ONLY (23 MAR 2023). ADDITIONAL ENGINEERING AUTHORIZATION (ER/A REVISION) IS REQUIRED FOR CONTINUED SERVICE BEYOND THIS LIMIT. NOTE TO
- [SDR DALA2021032401733](https://openairdocs.org/sdr/DALA2021032401733.md): Hinge · excess play · Mar 21, 2021 · N970AT · Boeing 717200 · Trailing Edge Flaps
  > THE LT O/B FLAP HINGE HAS EXCESSIVE PLAY AT HINGE BOLT. DEFERRED FOR SDR REPORTING. NRC 331: REPAIRED PER PRI 590529-14 REV 0,1,2,3,&4 AND ER/A 590529-14 REV ORIG. (LP #1761231)
- [SDR DALA2021032301673](https://openairdocs.org/sdr/DALA2021032301673.md): Ring · detached · Mar 20, 2021 · N970AT · Boeing 717200 · Escape Slide
  > THE R1 SLIDE PACK MANUAL DEPLOYMENT RING IS NOT ATTACHED TO THE CABLE. MAINTENANCE REPLACED THE R-1 DOOR SLIDE REF ROUTINE TASK CARD 2561-9005. (LP #1760202)

Next page: https://openairdocs.org/aircraft/N970AT/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 = 'N970AT' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N970AT/reports

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