# Service difficulty reports: N967AT

A list on [N967AT](https://openairdocs.org/aircraft/N967AT.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 · 197 reports

- [SDR DALA2026102305841](https://openairdocs.org/sdr/DALA2026102305841.md): Skin · debonded · Oct 22, 2026 · N967AT · Boeing 717200 · Ailerons
  > DISBOND ON LOWER SKIN TRIM TAB RH WING AILERON, CORRECTIVE ACTION: R/R TRIM TAB RH AILERON PER B717 AMM 27-10-05-000-801. (1879775) (AIRCRAFT GROUNDED).
- [SDR DALA2026102305837](https://openairdocs.org/sdr/DALA2026102305837.md): Beam · cracked · Oct 22, 2026 · N967AT · Boeing 717200 · Passenger/Crew Doors
  > FOUND CRACK ON LL BEAM N 2 ON STA=161.375 AND STA 197.750 AT L1 PASSENGER ENTRANCE DOOR, REPAIRED BEAM PER B717-200 SRM 52-10-02-2R. (1880039) (AIRCRAFT GROUNDED).
- [SDR DALA2026102205828](https://openairdocs.org/sdr/DALA2026102205828.md): Duct · cracked · Oct 21, 2026 · N967AT · Boeing 717200 · Vertical Stabilizer, Plate/Skin
  > CRACK ON LEADING EDGE OF RAM AIR ILNET DUCT LH SIDE AT VERTICAL STABILIZER, COMPLIED WITH ER/A 382101- 14MA. (1878155) (AIRCRAFT GROUNDED).
- [SDR DALA2026093005424](https://openairdocs.org/sdr/DALA2026093005424.md): Sign · detached · Sep 29, 2026 · N967AT · Boeing 717200 · Emergency Lighting
  > FORWARD CABIN EXIT SIGN FELL OFF, RESECURED THE EXIT SIGN OK FOR SVC. (9488778) (AIRCRAFT GROUNDED).
- [SDR DALA2026082004757](https://openairdocs.org/sdr/DALA2026082004757.md): Localizer · faulted · Aug 17, 2026 · N967AT · Boeing 717200 · Localizer/VOR System
  > FOUND A NON-COMPLIANCE ISSUE RELATED TO SATELLITE-BASED AUGMENTATION SYSTEM (SBAS) MESSAGE TYPE 6, COMPLIED WITH ER/A 636183-14. (6771160) (AIRCRAFT GROUNDED).
- [SDR DALA2026030201422](https://openairdocs.org/sdr/DALA2026030201422.md): Ils System · unreliable · Feb 15, 2026 · N967AT · Boeing 717200 · Localizer/VOR System
  > ILS IS SOMEWHAT NOT RELIABLE, THEREFORE, AN STC FOR "ILS LOOK-ALIKE" LPV IS BEING DEVELOPED AS A BACK UP FOR ILS. ACCOMPLISHED ER/A 632398-14 (1452682)
- [SDR DALA2026020200757](https://openairdocs.org/sdr/DALA2026020200757.md): Mmr · not reported · Jan 31, 2026 · N967AT · Boeing 717200 · Navigation System
  > REMOVED MMR 2 IAW ER/A 625937-14. INSTALLED MMR 2 PER ER/A 625937-14 REV. B (1428881)
- [SDR DALA2025110708144](https://openairdocs.org/sdr/DALA2025110708144.md): Sign · damaged · Nov 1, 2025 · N967AT · Boeing 717200 · Emergency Lighting
  > SHIP 9526 FORWARD CENTER OVERHEAD EXIT SIGN DAMAGED. CORRECTIVE ACTION: R/R FWD ISLE EMERGENCY LIGHT SIGN IAW B717 AMM 33-51. OPS CHECK GOOD. (7608370)
- [SDR DALA2025080205799](https://openairdocs.org/sdr/DALA2025080205799.md): Fan · odor · Jul 28, 2025 · N967AT · Boeing 717200 · Air Distribution Fan
  > SMOKE & FUMES, THE CREW REPORTED ELECTRICAL SMELL IN THE CABIN DURING PUSHBACK AND START OF NR 2 ENGINE. MAINTENANCE REPLACED GASPER BOOSTER FAN.
- [SDR DALA2025010500069](https://openairdocs.org/sdr/DALA2025010500069.md): Fuel Cell · leaking · Dec 9, 2024 · N967AT · Boeing 717200 · Fuel Storage
  > -AD- FUEL LEAK FOUND DURING INSPECTION OF THE RH WING THROUGH FLAP FITTING BOLTS (4 EA WET LEAK) AT XRS=164 LOWER SURFACE (OUTB BOLTS). CONTACT LIAISON ENGINEERING FOR REPAIR PROCEDURES PRIOR TO FURTHER FLIGHT. SUMMARY OF NRC 00002: RH WING THROUGH FLAP FITTIN
- [SDR DALA2024121611733](https://openairdocs.org/sdr/DALA2024121611733.md): Repair · unknown · Jan 30, 2024 · N967AT · Boeing 717200 · Standard Practices/Structures
  > ERA 615468-14 SECTION I REPAIR REQUIRES DTE WITHIN 12 MONTHS OF AIRCRAFT RETURN TO SERVICE. ADDED FOR AC 9526. REDEFERRED LOG TO QC, ESTAB MON INSP. ER/A 615468-14 REV A, DTE STAGE 2 AND 3 ACCOMPLISHED ON 11DEC24. ER/A SECTION II FOLLOW-ON INSPECTIONS ARE REQU
- [SDR DALA2024020101442](https://openairdocs.org/sdr/DALA2024020101442.md): Skin · cracked · Jan 28, 2024 · N967AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACK AT FWD UPPER CORNER OF R1 DOOR ON FUSELAGE SKIN. REMOVED PAINT AND FASTENER FOR FURTHER EVALUATION PER B717 SRM 51-22-01 AND SRM 51-40-02-06. VERIFIED CRACK PER BHEC AND HFEC INSPECTION, NDTSPM PART 06-10-01.003 AND PART 06-10-01.001. TWO CRACKS MARKED A
- [SDR DALA2024112711264](https://openairdocs.org/sdr/DALA2024112711264.md): Frame · corroded · Jun 29, 2023 · N967AT · Boeing 717200 · Fuselage Main, Frame
  > CORROSION ON FRAME CHANNEL BTW LONGS 29L / 29R STA Y=1037 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00311: CORROSION LEVEL 2. FRAME CHANNEL BTW LONGS 29L / 29R STA Y=1037 AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 3 REPAIR 3 TA
- [SDR DALA2023031501885](https://openairdocs.org/sdr/DALA2023031501885.md): Unknown · unknown · Mar 11, 2023 · N967AT · Boeing 717200 · Fuselage Main, Frame
  > NLG WHEEL WELL AFT FRAME FOR GEAR DOOR CUTOUT DAMAGED 2 PLACES. (MARKED) SUMMARY SEE NRC 005-0003:3221-4001/002 00005: REPLACED NLG WHEEL WELL AFT FRAME FOR GEAR DOOR CUT OUT FRAME PER B717 SRM 53-10-15-2. AND DAC DWG 5913421. (LP #2665497)
- [SDR DALA2023031001761](https://openairdocs.org/sdr/DALA2023031001761.md): None · none · Mar 10, 2023 · N967AT · Boeing 717200 · Fuselage, Landing Gear Attach Fittings
  > LMLG FIXED STRUT O/B ATTACH FITTING WORN ON FWD AND AFT FACES. SUMMARY SEE NRC 008-0003:3211-4001/001 00006: REPAIRED PER CMM 57-40-1. (LP #2663943)
- [SDR DALA2023031001760](https://openairdocs.org/sdr/DALA2023031001760.md): None · none · Mar 10, 2023 · N967AT · Boeing 717200 · Fuselage, Landing Gear Attach Fittings
  > RMLG FIXED STRUT O/B ATTACH FITTING WORN ON FWD AND AFT FACES. SUMMARY SEE NRC 006-0003:3211-4004/001 00007: REPAIRED PER CMM 57-40-1. (LP #2663936)
- [SDR DALA2023020300858](https://openairdocs.org/sdr/DALA2023020300858.md): Not Entered · not entered · Feb 2, 2023 · N967AT · Boeing 717200 · Escape Slide
  > MAINTENANCE FOUND THE R1 DOOR SLIDE PARTIALLY DEPLOYED. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. THE R1 DOOR SLIDE WAS REPLACED PER AMDS CARD 2561-9005. (LP #4153514)
- [SDR DALA2023010600090](https://openairdocs.org/sdr/DALA2023010600090.md): Skin · damaged · Jan 5, 2023 · N967AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKE ON FUSELAGE SKIN LEFT SIDE AT FS 325, STR 10L, BETWEEN 2 FASTNERS. REMOVED DAMAGED SKIN PER B717 SRM 53-03-01-2R-1 FIG 205 SHEET 5. FABRICATED & DRILLED EXTERNAL REPAIR DOUBLER IAW B717 SRM 53-03-01-2R-1 FIG 205 SHEET 5. TREATED, PRIMED, AND I
- [SDR DALA2022112107448](https://openairdocs.org/sdr/DALA2022112107448.md): Angle · corroded · Nov 17, 2022 · N967AT · Boeing 717200 · Fuselage Main, Frame
  > EXFOLATION CORROSION ON RH ANGLE CUSP STA 200 TO 206 AT CPAX (CFS). SUMMARY OF NRC 00441: CORROSION LEVEL 2. RH ANGLE CUSP STA 168 TO 218 WAS REPAIRED PER PRI 603031-14 PRI REV 3 AND ER/A 603031- 14 REV. ORIGINAL SECTION I: PERMANENT REPAIR ASSOCIATED ER/A 14-
- [SDR DALA2022111707401](https://openairdocs.org/sdr/DALA2022111707401.md): Intercostal · corroded · Nov 16, 2022 · N967AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTAL OVER LONG 30 BTW STA Y=1022 AND Y=1037 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00310: CORROSION LEVEL 2. INTERCOSTAL OVER LONG 30 BTW STA Y=1022 AND Y=1037 AT AFT CARGO COMPARTMENT WAS REPLACED PER B-717 200 SRM 51-41-02-0G PAR 4 (A),
- [SDR DALA2022110907242](https://openairdocs.org/sdr/DALA2022110907242.md): None · none · Nov 8, 2022 · N967AT · Boeing 717200 · Wing, Control Surface Attach Fittings
  > FREEPLAY ON LH WING FLAP OUTBD HINGES PIVOT AREA (STA 331.1). SUMMARY OF NRC 00186: LH WING FLAP OUTBD HINGES PIVOT AREA WAS REPAIRED PER PRI 603178-14 REV 2 & ERA 603178-14 REV. ORIG. ASSOCIATED ER/A 14-603178 ADDED FOR AC 9526. (LP #2487822)
- [SDR DALA2022110907241](https://openairdocs.org/sdr/DALA2022110907241.md): None · none · Nov 8, 2022 · N967AT · Boeing 717200 · Wing, Control Surface Attach Fittings
  > FREEPLAY ON RH WING FLAP OUTBD HINGES PIVOT AREA (STA 331.1). SUMMARY OF NRC 00188: RH WING FLAP OUTBD HINGES PIVOT AREA WAS REPAIRED PER PRI 603122-14 REV 3 & ER/A 603122-14 REV ORIG. (LP #2488108)
- [SDR DALA2022110807205](https://openairdocs.org/sdr/DALA2022110807205.md): None · none · Nov 7, 2022 · N967AT · Boeing 717200 · Fuselage Main, Frame
  > CORROSION ON FRAME CHANNEL BTW LONGS 29L / 29R STA Y=1037 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00311: CORROSION LEVEL 2. FRAME CHANNEL BTW LONGS 29L / 29R STA Y=1037 AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 3 REPAIR 3 TA
- [SDR DALA2022110807204](https://openairdocs.org/sdr/DALA2022110807204.md): None · none · Nov 7, 2022 · N967AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK ON BRACKET UPPER CORNER AFT SIDE OF CUT OUT AT RH SLIDING CLEARVIEW WINDOW COCKTPIT (CPIL) IN REF NRC 00019. SUMMARY OF NRC 00073: CORNER AFT SIDE OF CUT OUT AT RH SLIDING CLEARVIEW WINDOW WAS REPAIRED PER B717-200 SRM 56-10-02-2R PROCEDURE 1 REPAIR 1, P
- [SDR DALA2022110807203](https://openairdocs.org/sdr/DALA2022110807203.md): None · none · Nov 7, 2022 · N967AT · Boeing 717200 · Fuselage Main, Frame
  > CORROSION ON FRAME CHANNEL BTW LONGS 29L / 29R STA Y=1037 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00311: CORROSION LEVEL 2. FRAME CHANNEL BTW LONGS 29L / 29R STA Y=1037 AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 3 REPAIR 3 TA
- [SDR DALA2022110807202](https://openairdocs.org/sdr/DALA2022110807202.md): None · none · Nov 4, 2022 · N967AT · Boeing 717200 · Fuselage Floor Panel
  > FOUND CORROSION ON FLOOR SUPPORTS STA Y=160-200 AND X=-53 AT CPAX (CFS)(W1)(IN REF NRC NBR 00468). SUMMARY OF NRC 00613: CORROSION LEVEL 2 IS OUT OF LIMITS. SUPPORTS BTW STA Y=160-200 AND X=-53 AT CPAX WERE REPLACED PER B717-200 SRM 51-41-01-0G. (LP #2482688)
- [SDR DALA2022110207099](https://openairdocs.org/sdr/DALA2022110207099.md): Web · cracked · Oct 31, 2022 · N967AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACKS (2 PLACES) ON UPPER WEB OF AFT CABIN BULKHEAD DOOR. SUMMARY OF NRC 00063: UPPER WEB OF AFT CABIN BULKHEAD DOOR WAS REPLACED PER B717 SRM 51-41-05-0G PAR. 8 AND SRM 51-40-02-0G. (LP #2477471)
- [SDR DALA2022110107061](https://openairdocs.org/sdr/DALA2022110107061.md): Angle · cracked · Oct 31, 2022 · N967AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON CLIP ANGLE NEAR TO UPPER BELLCRANK OF AFT CABIN BULKHEAD DOOR. SUMMARY OF NRC 00065: CLIP ANGLE (FITTING ASSY) NEAR TO UPPER BELLCRANK OF AFT CABIN BULKHEAD DOOR WAS FABRICATED AND REPLACED PER DWG 3917863 REV B AND B717-200 SRM 51-41-05-0G. (LP #2477
- [SDR DALA2022110107060](https://openairdocs.org/sdr/DALA2022110107060.md): Seat Track · corroded · Oct 31, 2022 · N967AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > EXFOLATION RH SEAT TRACK X=-22 STA 200 TO 206 AT CPAX (CFS). SUMMARY OF NRC 00446: CORROSION LEVEL 2. RH SEAT TRACK SECTION X=-22 BTW STA 200 TO STA 265 WAS REPLACED PER B717-200 SRM 51-41-01-0G AND B717-200 SRM 51-41-05-0G. (LP #2475977)
- [SDR DALA2022110107059](https://openairdocs.org/sdr/DALA2022110107059.md): Seat Track · corroded · Oct 29, 2022 · N967AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > AFTER RH SEAT TRACK REMOTION, CORROSION WAS FOUND ON DIAPHRAGM BTW Y=200 AND Y=206 X-22 IN REF NRC 00446. SUMMARY OF 00573: CORROSION LEVEL 2. DIAPHRAGM (WEB) BTW Y=200 AND Y=218 X-17 TO X-25 WAS REPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 1. (LP #2474250)
- [SDR DALA2022110107058](https://openairdocs.org/sdr/DALA2022110107058.md): Longeron · corroded · Oct 28, 2022 · N967AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CORROSION ON LONG 29LH STA Y=908 TO 927 AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00260: CORROSION LEVEL 2. LONG 29LH BTW STA Y=908 TO 927 AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53 -20-05-2R-1, REPAIR 1 FIGURE 201 AND B717-200 SRM 53-00-06-
- [SDR DALA2022102706965](https://openairdocs.org/sdr/DALA2022102706965.md): None · none · Oct 26, 2022 · N967AT · Boeing 717200 · Fuselage Floor Panel
  > CORROSION ON L1 DOOR JAMB SUPPORT STA Y=160-200 AT PAX CABIN (W1). SUMMARY OF NRC 00470: CORROSION LEVEL 2. L1 DOOR JAMB SUPPORTS, 2 EA, STA Y=160-200 AT PAX CABIN WAS REPLACED PER B717-200 SRM-51-41-05-0G. (LP #2469122)
- [SDR DALA2022102606953](https://openairdocs.org/sdr/DALA2022102606953.md): Membrane · corroded · Oct 23, 2022 · N967AT · Boeing 717200 · Fuselage Floor Panel
  > CORROSION ON CUSP MEMBRANES BTW X=-54-X=-60 AND BTW STA Y=408-427, 506, 525, 598. ORIGINAL THICKNESS IS 0.020 IN AND MINIMUM REMAINING THICKNESS IS 0.010 IN, THEREFORE THE AREA IS OUT OF LIMITS IN REF NRC 00453 AT PAX CABIN. SUMMARY OF NRC 00621: CORROSION LEV
- [SDR DALA2022102606952](https://openairdocs.org/sdr/DALA2022102606952.md): Floor Support · corroded · Oct 22, 2022 · N967AT · Boeing 717200 · Fuselage Floor Panel
  > CORROSION ON FLOOR SUPPORT BTW STA Y=1024 TO Y=1054 RBL 56 AT RH LAVATORY AFT PASSENGER CABIN (W2). SUMMARY OF NRC 00491: CORROSION LEVEL 2. FLOOR SUPPORT BTW STA Y=1024 TO Y=1054 RBL 56 AT RH LAVATORY AFT PASSENGER CABIN WAS REPLACED PER B717-200 SRM 51-41-02
- [SDR DALA2022102606951](https://openairdocs.org/sdr/DALA2022102606951.md): Floor Support · corroded · Oct 21, 2022 · N967AT · Boeing 717200 · Fuselage Floor Panel
  > EXFOLATION ON FLOOR SUPPORT STA Y=160-200 X=-44 (CAPX)(W1). SUMMARY OF NRC 00482: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=160- 200 X=-44 WAS REPLACED PER B717-200 SRM 51-41-01-0G AND B717-200 SRM 51-41-05-0G. (LP #2462423)
- [SDR DALA2022102606950](https://openairdocs.org/sdr/DALA2022102606950.md): Floor Support · corroded · Oct 21, 2022 · N967AT · Boeing 717200 · Fuselage Floor Panel
  > CORROSION ON FLOOR SUPPORT STA Y=200 BTW X=-9 AND X=-46 (CAPX)(W1). SUMMARY OF NRC 00472: CORROSION LEVEL 2. FLOOR SUPPORT AT STA Y= 200 BTW X=-9 AND X=-46 WAS REPLACED PER B717-200 SRM 51-41-01-0G AND B717-200 SRM 51-41-05-0G. (LP #2462418)
- [SDR DALA2022102606949](https://openairdocs.org/sdr/DALA2022102606949.md): Floor Support · corroded · Oct 21, 2022 · N967AT · Boeing 717200 · Fuselage Floor Panel
  > CORROSION ON FLOOR SUPPORT BTW STA Y=1024 TO Y=1055 RBL 48 AT RH LAVATORY AFT PASSENGER CABIN (W2). SUMMARY OF NRC 00492: CORROSION LEVEL 2. FLOOR SUPPORT BTW STA Y=1024 TO Y=1055 RBL 48 AT RH LAVATORY AFT PASSENGER CABIN WAS REPLACED PER DWG 9981474-82 AND B7
- [SDR DALA2022102606948](https://openairdocs.org/sdr/DALA2022102606948.md): Floor Support · corroded · Oct 21, 2022 · N967AT · Boeing 717200 · Fuselage Floor Panel
  > EXFOLATION ON FLOOR SUPPORT STA Y=180 BTW X=-9 - X=-43 (CAPX)(W1). SUMMARY OF NRC 00481: CORROSION LEVEL 2. SUPPORT STA Y=180 BTW X =-9 - X=-43 WAS REPLACED PER B717-200 SRM 51-41-02-0G AND B717- 200 SRM 51-41-05-0G. (LP #2461817)
- [SDR DALA2022101806740](https://openairdocs.org/sdr/DALA2022101806740.md): Floorbeam · corroded · Oct 18, 2022 · N967AT · Boeing 717200 · Fuselage Main, Floor Beam
  > AIRCRAFT 9526, INITIAL INSPECTION:CORROSION ON FLOOR SUPPORT STA Y=200 BTW X=9 AND X=13 (CAPX)(W1). CORRECTIVE ACTION: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=200 BTW X=9 AND X=13 WAS REPLACED PER B717-200 SRM 51-41-05-0G PAR. 8. LP 2457059
- [SDR DALA2022101806739](https://openairdocs.org/sdr/DALA2022101806739.md): Floorbeam · corroded · Oct 18, 2022 · N967AT · Boeing 717200 · Fuselage Main, Floor Beam
  > AIRCRAFT 9526, INITIAL INSPECTION:CORROSION ON FLOOR SUPPORT STA Y=200 BTW X=5 AND X=-5 (CAPX)(W1). CORRECTIVE ACTION: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=200 BTW X=5 AND X=-5 WAS REPLACED PER B717-200 SRM 51-41-05-0G PAR. 8. LP 2457001
- [SDR DALA2022101806738](https://openairdocs.org/sdr/DALA2022101806738.md): Cusp Web · corroded · Oct 16, 2022 · N967AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > AIRCRAFT 9526, INITIAL INSPECTION: CORROSION ON PREVIOUSLY REPAIR DOUBLER RH CUSP WEB BTW X=-54 - X=-60 AND STA Y=446-465. CORRECTIVE ACTION: DOUBLER RH CUSP WEB BTW X=-54 - X=-60 AND STA Y=446-465 WAS REPLACED PER B717-200 SRM 53-00-55-2R-4 REPAIR 4 FIGURE 2
- [SDR DALA2022101606676](https://openairdocs.org/sdr/DALA2022101606676.md): Hinge · damaged · Oct 14, 2022 · N967AT · Boeing 717200 · Doors
  > AIRCRAFT 9526, INITIAL INSPECTION. WEAR ON INTERNAL DOUBLER BTW LOWER HINGE AND LOWER PAN OF AFT CABIN BULKHEAD DOOR. CORECTIVE ACTION: PAN OF AFT CABIN BULKHEAD DOOR WAS REPAIRED PER B-717 SRM 52-10-02-2R PROCEDURE 16, REPAIR 16, PAR 4. A. LP 2450898
- [SDR DALA2022101406662](https://openairdocs.org/sdr/DALA2022101406662.md): Longeron Splice · corroded · Oct 13, 2022 · N967AT · Boeing 717200 · Fuselage Main, Frame
  > AIRCRAFT 9526, INITIAL INSPECTION:CORROSION ON LONG SPLICE 30 BTW STA Y=889-908 AT AFT CARGO COMPARTMENT (C2). CORRECTIVE ACTION: LONG SPLICE 30 BTW STA Y=889-908 AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-01-0G PAR. 6 & 51-41-05-0G PAR. 8. L
- [SDR DALA2019082644954](https://openairdocs.org/sdr/DALA2019082644954.md): Slide · no test · Aug 24, 2019 · N967AT · Boeing 717200 · Escape Slide
  > THE R1 DOOR SLIDE FAILED THE DEPLOYMENT TEST PER AMDS CARD #2561-9002 FORECAST #95-0525-8-0121. MAINTENANCE REMOVED AND INSTALLED A NEW SERVICEABLE R1 DOOR SLIDE REF AMDS CARD #2561-9005. ICR HAS BEEN SUBMITTED USING DOC/WORKCARD #2560-9352 -95 (QC5126/376046)
- [SDR DALA2019062703887](https://openairdocs.org/sdr/DALA2019062703887.md): Battery Pack · inoperative · Jun 27, 2019 · N967AT · Boeing 717200 · Emergency Lighting
  > THE EXIT SIGN ABOVE THE AFT BULKHEAD DOOR IS INOPERATIVE (EMERGENCY LIGHT). MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY IAW B717 AMM 33-57-03. OPERATIONAL CHECK WAS GOOD. (LP #5759650)
- [SDR DALA2018100205846](https://openairdocs.org/sdr/DALA2018100205846.md): Battery Pack · discharged · Sep 30, 2018 · N967AT · Boeing 717200 · Emergency Lighting
  > THE FORWARD EMERGENCY EXIT SIGN IS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK B5-235 REF AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #3914354)
- [SDR DALA2018092005666](https://openairdocs.org/sdr/DALA2018092005666.md): Door Frame · corroded · Sep 18, 2018 · N967AT · Boeing 717200 · Fuselage Main, Structure
  > CORROSION WAS FOUND ON THE FORWARD CARGO DOOR JAMB. REPLACED DOOR JAMB IN STEPS 1 THRU 5 REF SRM 53-20-15-2R PROC 6.
- [SDR DALA2018091805643](https://openairdocs.org/sdr/DALA2018091805643.md): Mechanism · out of adjust · Sep 14, 2018 · N967AT · Boeing 717200 · Aerodynamic Fairings
  > TAILCONE RELEASE CAM MECHANISM IS CLOCKED WRONG. CHECKED CLOCKING AND ADJUSTED, REF BAC DWG 5961568 & AMM 53-52-03.
- [SDR DALA2018082705270](https://openairdocs.org/sdr/DALA2018082705270.md): Lens · missing · Aug 25, 2018 · N967AT · Boeing 717200 · Emergency Lighting
  > THE FLIGHT ATTENDANT DISCOVERED THE OVERWING EXIT EMERGENCY SIGN COVER WAS MISSING. MAINTENANCE REPLACED THE LENS ASSEMBLY AND THE AIRCRAFT RETURNED TO SERVICE.
- [SDR DALA2018052103460](https://openairdocs.org/sdr/DALA2018052103460.md): Power Supply · contaminated · May 20, 2018 · N967AT · Boeing 717200 · Emergency Lighting
  > THE EMERGENCY EXIT LIGHTS WOULD NOT TURN OFF. MAINTENANCE FOUND THE POWER SUPPLY ABOVE THE AFT F/A SEAT TO BE SATURATED WITH WATER. MAINTENANCE REPLACED POWER SUPPLY AND BATTERY IAW AMM 33-51. OPS CHECKED NORMAL.

Next page: https://openairdocs.org/aircraft/N967AT/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 = 'N967AT' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N967AT/reports

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