# Service difficulty reports: N947AT

A list on [N947AT](https://openairdocs.org/aircraft/N947AT.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 · 231 reports

- [SDR DALA2026062903844](https://openairdocs.org/sdr/DALA2026062903844.md): Accumulator · leaking · Jun 28, 2026 · N947AT · Boeing 717200 · Hydraulic Power Accumulator, Main
  > ATB- RETURNED TO DTW DUE TO A LEFT HYDRAULIC QUANTITY LOW MESSAGE. MAINTENANCE FOUND THE LEFT SYSTEM ACCUMULATOR LEAKING AND REPLACED SAME. ALL OPERATIONAL AND LEAK CHECKS NORMAL. (8424352) (AIRCRAFT GROUNDED).
- [SDR DALA2026020900904](https://openairdocs.org/sdr/DALA2026020900904.md): Sign · damaged · Feb 1, 2026 · N947AT · Boeing 717200 · Emergency Lighting
  > EMERGENCY EXIT SIGN ON CEILING BETWEEN 1B AND 1C IS DAMAGED. REPLACED DAMAGED EXIT SIGN IAW AMM 33-51. (8182268)
- [SDR DALA2025111808424](https://openairdocs.org/sdr/DALA2025111808424.md): Latch · dirty · Nov 16, 2025 · N947AT · Boeing 717200 · Emergency Equipment
  > GIRT BAR BRACKETS HARD TO OPERATE / LOCATIONS:601. CLEANED AND LUBED DOOR 1L GIRT BAR LATCH CHECKS GOOD REF B717 MM 25-61 OK FOR SVC (1306981).
- [SDR DALA2025111108258](https://openairdocs.org/sdr/DALA2025111108258.md): Skin · cracked · Nov 6, 2025 · N947AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACK ON EXTERNAL SKIN, BS 1087, BTW L-13R AND L-14R AT AFT FUSELAGE. PERMANENT REPAIR AND PRI 630164-14 REV. 3. (1291355)
- [SDR DALA2025110708141](https://openairdocs.org/sdr/DALA2025110708141.md): Skin · cracked · Nov 4, 2025 · N947AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > SHIP 9507 FUSELAGE / SKIN / STA Y=1087, L=13R & L=14R / CRACK. CORRECTIVE ACTION: ACCOMPLISH ER/A 630164-14 (1290083)
- [SDR DALA2025110708135](https://openairdocs.org/sdr/DALA2025110708135.md): Slide · unpacked · Oct 31, 2025 · N947AT · Boeing 717200 · Escape Slide
  > IN REF. TO AMDS 5211-4001: EMERGENCY SLIDE PACK WAS FOUND UNFOLDED, DOOR L1 WAS REPLACED UNDER AMDS 97-2561-9-0003 AND AMDS 2561- 9004 (1281137)
- [SDR DALA2025110708139](https://openairdocs.org/sdr/DALA2025110708139.md): Skin · cracked · Oct 29, 2025 · N947AT · Boeing 717200 · Vertical Stabilizer, Plate/Skin
  > CRACK SKIN INSIDE OF ACCESS PANEL 370BL FWD /UPPER CORNER AT VERTICAL STABILIZER DORSAL FIN. CORRECTIVE ACTION: UPPER CORNER AT VERTICAL STABILIZER DORSAL FIN WAS REPAIRED PER B717 SRM 55-30-01 (1278507)
- [SDR DALA2025103107965](https://openairdocs.org/sdr/DALA2025103107965.md): Vane · punctured · Oct 29, 2025 · N947AT · Boeing 717200 · Wing Main, Frame Structure
  > INSPECTION: PUNCTURE ON FWD MOVABLE VANE LOWER SURFACE AT LT WING. FWD MOVABLE VANE LOWER SURFACE AT LH WING WAS REPAIRED IAW SRM 57-53-01 (1277612).
- [SDR DALA2025103107963](https://openairdocs.org/sdr/DALA2025103107963.md): Wire · broken · Oct 27, 2025 · N947AT · Boeing 717200 · Equipment/Furnishings Wiring
  > BROKEN WIRES ON ESCAPE SLIDE LANYARD ASSEMBLY (2 EA) AT R1 & L1 DOOR. LANYARDS ASSEMBLIES AT L1 DOOR AND R1 DOOR WERE REPLACED & VERIFIED IAW AIPC 25-61-01-01 TEM 95 & AIPC 25-61-03 (1275291).
- [SDR DALA2025102407793](https://openairdocs.org/sdr/DALA2025102407793.md): Roller · faulted · Oct 20, 2025 · N947AT · Boeing 717200 · Main Landing Gear
  > RETURNED TO ATLANTA DUE TO A LEFT GEAR UNSAFE INDICATION. PERFORMED TROUBLE SHOOT PER B717 FIM 32-60. REPLACED EMERGENCY RELEASE ROLLER FOR LEFT GEAR. TEST GOOD.(7707462)
- [SDR DALA2025102207719](https://openairdocs.org/sdr/DALA2025102207719.md): Sensor · faulted · Oct 19, 2025 · N947AT · Boeing 717200 · Landing Gear Position and Warning
  > RETURNED TO AGS DUE TO A LEFT GEAR UNSAFE INDICATION. MAINTENANCE REPLACED THE LEFT DOOR UP AND LATCHED SENSOR. CYCLED GEAR OPS CHECK NORMAL.(7707452)
- [SDR DALA2025050603514](https://openairdocs.org/sdr/DALA2025050603514.md): Battery Pack · inoperative · Apr 23, 2025 · N947AT · Boeing 717200 · Emergency Lighting
  > AFT OVERWING (L&R) EXIT LIGHT IS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACKS B5-119 & B5-230. OPERATIONAL CHECK IS NOW NORMAL REF B717 AMM 33-51. (LP #6520466)
- [SDR DALA2025041502917](https://openairdocs.org/sdr/DALA2025041502917.md): Not Reported · cracked · Apr 14, 2025 · N947AT · Boeing 717200 · Wing Structure
  > -AD- DUE TO CRACK INDICATION FOUND DURING INSP, COMPLIED WITH AMDS CARD 5720-01103-01B. REQUIRES COMPLETION OF PRI 624259-14. COMPLIED WITH PRI 624259-14AD REV 0, 1, & 2. COMPARED PRI 324259-14AD REV 0, 1, & 2 WITH ERA 624259-14AD REV ORIG AND ALL ITEMS MATCH.
- [SDR DALA2025041502916](https://openairdocs.org/sdr/DALA2025041502916.md): Spar Cap · cracked · Apr 14, 2025 · N947AT · Boeing 717200 · Wing Spar
  > -AD- CRACK WAS FOUND IN LOWER SPAR CAP NEAR XRS=164 DURING INSP OF LT WING REAR SPAR INSP AMDS 5720-01103-01A. "CONTACT LIAISON ENGINEERING FOR REPAIR PRIOR TO FURTHER FLIGHT" FC 5720-01103. COMPLIED WITH PRI 624256-14AD REVS 0, 1, 2, 3, 4, & 5. COMPARED PRI 6
- [SDR DALA2025020400814](https://openairdocs.org/sdr/DALA2025020400814.md): None · none · Feb 3, 2025 · N947AT · Boeing 717200 · Standard Practices/Structures
  > -AD- COMPLY WITH ERA 623716-14AD REV ORIGINAL. SUMMARY NRC 002-0001:0514-2001/008 00009: COMPLIED WITH ER/A 623716-14AD REV 0, PRI REV 0, 1, AND 2. ENSURED PRI AND FINAL ERA MATCH. (LP #0794140)
- [SDR DALA2025010800157](https://openairdocs.org/sdr/DALA2025010800157.md): Stab System · out of adjust · Jan 2, 2025 · N947AT · Boeing 717200 · Flight Control System
  > WHILE PERFORMING W/C 2740-01114-07, THE JACKSCREW DID NOT STOP AUTOMATICALLY AND CONTACTED THE UPPER STOP. HORIZ STAB ADJ REQUIRED PER B717 AMM 27-40-00 820-801 & INSPECTION OF THE JACK SCREW REQUIRED PER B717 AMM 27-41-04 220-802. C/W INSPECTION OF JACKSCREW
- [SDR DALA2024112711256](https://openairdocs.org/sdr/DALA2024112711256.md): Light · sparks · Nov 25, 2024 · N947AT · Boeing 717200 · Flight Compartment Lighting
  > F/O BRIEFCASE LIGHT IS SPARKING INTERNALLY. MAINTENANCE REPLACED THE F/O BRIEFCASE LIGHT IAW B717 AMM 33-16. OPERATIONAL CHECK WAS GOOD. AIRCRAFT IS OK FOR SERVICE. (LP #6723386)
- [SDR DALA2024042304671](https://openairdocs.org/sdr/DALA2024042304671.md): Limit Switch · out of adjust · Apr 22, 2024 · N947AT · Boeing 717200 · Flight Control System
  > WHILE WORKING A.A. WORKCARD 2740-01114-07 HORIZONTAL JACK SCREW INSPECTION FAILED ONLY DURING ALTERNATE NOSE UP. HITS THE UPPER STOP. WITH PRIMARY SWITCH WORKS OK REF B717 AMM 27-40-00-820-801. ADJUSTED HORIZONTAL STABILIZER TRIM SYS & SHUT OFF CONTROLS PER B7
- [SDR DALA2024041804531](https://openairdocs.org/sdr/DALA2024041804531.md): Skin · damaged · Apr 16, 2024 · N947AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > REF LOG #0286119: C/W ER/A 617263-14 REV ORIG. C/W ER/A 617263-14 REV ORIG SECTION II STEPS 1 AND 2. NO FURTHER DEFECTS NOTED. CUT OUT DAMAGED SKIN AND DRILLED REPAIR DOUBLER PER ER/A 617263-14 REV ORIG SECTION II STEP 3. C/W DVI OF DENTS REF STEP 4 SECTION II
- [SDR DALA2024011700681](https://openairdocs.org/sdr/DALA2024011700681.md): Door Frame · cracked · Jan 16, 2024 · N947AT · Boeing 717200 · Fuselage Main, Structure
  > RT MAIN GEAR WHEEL WELL DOOR JAMB FWD CHANNEL WAS FOUND CRACKED / DAMAGED. MAINTENANCE CLEANED UP DAMAGE AND INSPECTED PER B717 SRM 53-20-02-2R PROC 3. CRACK IN UPPER CHANNEL AREA MEASURED APPROX. 0.25IN. STOP DRILLED CRACK PER B717 SRM 53-20-02-2R REPAIR 3. C
- [SDR DALA2023091107389](https://openairdocs.org/sdr/DALA2023091107389.md): Unknown · unknown · Sep 9, 2023 · N947AT · Boeing 717200 · Emergency Lighting
  > LIGHTS OF WALKWAY PATH DO NOT TURN ON AT AFT ACCESORIES COMPARTMENT. SUMMARY OF NRC 00214: CONNECTOR R5-1211 WAS CONNECTED CORRECTLY PER B717 WDM 33-51-14. THEN OPERATIONAL TEST WAS PERFORMED PER B717 AMM 33-51-00 710-801. SATISFACTORY TEST. LIGHTS OF WALKWAY
- [SDR DALA2025090206466](https://openairdocs.org/sdr/DALA2025090206466.md): Skin · dented · Sep 8, 2023 · N947AT · Boeing 717200 · Wing, Plate/Skin
  > ER/A 611604-14; WINGS / OUTER WING / L.E. RHS / SKIN XOS 250-260 / DENT. ER/A 611604-14 HAS BEEN REVISED CURRENT STATUS IS REV. A. (2960169)
- [SDR DALA2023091107388](https://openairdocs.org/sdr/DALA2023091107388.md): Unknown · unknown · Sep 8, 2023 · N947AT · Boeing 717200 · Emergency Lighting
  > OUT SERVICE CEILING EMERGENCY LIGHT AT ROWS 29, 26, 22, 20, 19, 15, AND 12. ALSO OUT SERVICE LOWER EMERGENCY SIGN OF AFT RH OVERWING EXIT DOOR. SUMMARY OF NRC 00208: OPERATIONAL TEST OF THE EMERGENCY LIGHTING SYSTEM B717 AMM 33-51-00 710-801 FIGURE 501 (SHEET
- [SDR DALA2023091107385](https://openairdocs.org/sdr/DALA2023091107385.md): Unknown · unknown · Sep 7, 2023 · N947AT · Boeing 717200 · Emergency Lighting
  > DURING PC POWER SYSTEM OPERATIONAL TEST AT EMERGENCY EXITS; SEAT RH AND LH WAS FOUND TURNED OFF. STATUS LEDS (GREEN LIGHT) OF MOUNTED OUTLED UNID (OU) AT PASSENGER SEAT ROW 20 LH. SUMMARY OF NRC 00195: MOUNTED OUTLED UNID (OU) AT PASSENGER SEAT ROW 20 LH WAS I
- [SDR DALA2023090607279](https://openairdocs.org/sdr/DALA2023090607279.md): Unknown · unknown · Sep 6, 2023 · N947AT · Boeing 717200 · Fuselage Main, Frame
  > CORROSION ON FRAME STA Y=889 LONG 29LH-29RH AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 0185: CORROSION LEVEL 2. FRAME STA Y=889 LONG 29LH-29RH AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 3. THE REPAIR'S SPECIFIED MAINTENANCE REQU
- [SDR DALA2023090607276](https://openairdocs.org/sdr/DALA2023090607276.md): Unknown · unknown · Sep 6, 2023 · N947AT · Boeing 717200 · Fuselage Main, Frame
  > CORROSION WAS FOUND ON FRAME STA Y=1022 BTW LONG 29LH-29RH AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 0183: CORROSION LEVEL 2. FRAME STA Y=1022 BTW LONG 29LH-29RH AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 3 REPAIR 3. PERFORM AN
- [SDR DALA2023090607275](https://openairdocs.org/sdr/DALA2023090607275.md): Unknown · unknown · Sep 6, 2023 · N947AT · Boeing 717200 · Fuselage Main, Frame
  > CORROSION ON FRAME STA Y=889 LONG 29LH-29RH AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 0185: CORROSION LEVEL 2. FRAME STA Y=889 LONG 29LH-29RH AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 3. (LP #2955290)
- [SDR DALA2023090607272](https://openairdocs.org/sdr/DALA2023090607272.md): Unknown · unknown · Sep 5, 2023 · N947AT · Boeing 717200 · Fuselage Structure (General)
  > CORROSION ON FRAME CLIP AT STA Y=1022 BTW LONG 30 AND LONG 29L. AREA EXCEEDS MORE THAN 50 PERCENT OF THE ALLOWED DAMAGE PER B717-200 SRM 53-00-00-1A PAR 4. SUMMARY OF NRC 00180: CORROSION LEVEL 2. FRAME CLIP AT STA Y=1022 BTW LONG 30 AND LONG 29L AT AFT CARGO
- [SDR DALA2023090507191](https://openairdocs.org/sdr/DALA2023090507191.md): Unknown · unknown · Sep 3, 2023 · N947AT · Boeing 717200 · Escape Slide
  > TORN KEVLAR CABLE OF SLIDE RELEASE MECHANISM INSIDE TAILCONE. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY OF NRC 00138: KEVLAR CABLE OF RELEASE MECHANISM INSIDE TAILCONE WAS REPLACED PER
- [SDR DALA2023090507184](https://openairdocs.org/sdr/DALA2023090507184.md): Unknown · unknown · Sep 1, 2023 · N947AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON GUSSET OF DOOR JAMB PAN BTW STA Y=994 AND LONG 29R AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00122: CORROSION LEVEL 2. GUSSET OF DOOR JAMB PAN BTW STA Y=994 AND LONG 29R AT AFT CARGO COMPARTMENT WAS REPLACED PER DWG 5913537 REV D AND B717 SRM 51-41
- [SDR DALA2023062705159](https://openairdocs.org/sdr/DALA2023062705159.md): Unknown · unknown · Jun 26, 2023 · N947AT · Boeing 717200 · Emergency Lighting
  > UPPER EMERGENCY LIGHTS OVER WING EXITS ARE INOPERATIVE. MAINTENANCE RPLACED THE EMERGENCY LIGHT BATTERY PACK STA 726 PER B717 33-51. OPERATIONAL CHECK WAS GOOD. (LP #4703548)
- [SDR DALA2023060904691](https://openairdocs.org/sdr/DALA2023060904691.md): Unknown · unknown · May 24, 2023 · N947AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > ON WALK-AROUND FOUND AFT CARGO DOOR FRAME DAMAGE JAMB AREA. INSPECTED DAMAGE AREA. BLENDED IAW SRM 52-30-02-R PROCEDURE 8. PERFORMED TEMP REPAIR IAW ERA 609141-14 SECTION I. ENGR APPROVED PER DAL PS 500-5-1-NO 04. ASSOCIATED ER/A 14-609141 ADDED FOR AC 9507. C
- [SDR DALA2023030201557](https://openairdocs.org/sdr/DALA2023030201557.md): None · none · Mar 1, 2023 · N947AT · Boeing 717200 · Emergency Lighting
  > CABIN STANDBY EMERGENCY LIGHTING IS MISSING TWO LENS COVERS (LOC ROW 22 AND 26). FORWARD MISSING CABIN STANDBY EMERGENCY LIGHTING TO MEL 33-52-01. PLACARDS INSTALLED. (LP #4154618)
- [SDR DALA2022053103725](https://openairdocs.org/sdr/DALA2022053103725.md): Lens · missing · May 27, 2022 · N947AT · Boeing 717200 · Emergency Lighting
  > THE OVERHEAD EMERGENCY LIGHT LENS COVER IS MISSING AT SEAT ROWS 24 AND 27. MAINTENANCE INSTALLED NEW OVERHEAD EMERGENCY LIGHT LENS COVERS FOR SEAT ROWS 24 AND 27 PER AMM 33-51. OK FOR SERVICE. (LP #8293852)
- [SDR DALA2021110906895](https://openairdocs.org/sdr/DALA2021110906895.md): None · none · Nov 8, 2021 · N947AT · Boeing 717200 · Escape Slide
  > THE R1 DOOR SLIDE PRESSURE GAUGE INDICATION IS IN THE RED ZONE. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE SLIDE AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE REPLACED THE R1 DOOR SLIDE PER AMDS 2561-9005. COMPLETED RII STEPS PER AMD
- [SDR DALA2021090705225](https://openairdocs.org/sdr/DALA2021090705225.md): Tail Cone · out of adjust · Sep 3, 2021 · N947AT · Boeing 717200 · Aerodynamic Fairings
  > MULTIPLE WIRTEUPS FOR TAIL CONE CAM RIGGING. RAM 1. PLEASE REMOVE TAIL CONE AND INSPECT ALL ATTACH FITTINGS CABLES BRACKETS AND CAMS PER AMDS WORK CARD 5352-4013. 00-0000-3-0001. ADJUSTED TAILCONE RELEASE CAM REF B717 AMM 53-52-03. (LP #1935731)
- [SDR DALA2021090305223](https://openairdocs.org/sdr/DALA2021090305223.md): Cam · cocked · Sep 2, 2021 · N947AT · Boeing 717200 · Aerodynamic Fairings
  > THE TAILCONE RELEASE CAM IS CLOCKED WRONG. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY SEE NRC 001-0115:5352-4002/002 00349: ADJUSED TAILCONE RELEASE CAM REF B717 AMM 53-52-03. (LP #19344
- [SDR DALA2021090305221](https://openairdocs.org/sdr/DALA2021090305221.md): Conduit · dented · Sep 2, 2021 · N947AT · Boeing 717200 · Aerodynamic Fairings
  > THE CONDUIT FOR TAILCONE RELEASE CABLE IS DENTED, RT SIDE LOWER AREA (MARKED). THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY SEE NRC 001-0265:5300-2004/007 00082: REPLACED CONDUIT AND TAILC
- [SDR DALA2021083105135](https://openairdocs.org/sdr/DALA2021083105135.md): Cam · out of position · Aug 28, 2021 · N947AT · Boeing 717200 · Aerodynamic Fairings
  > THE TAILCONE RELEASE CAM IS CLOCKED WRONG AND OUT OF ADJUSTMENT. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY NRC 001-0115:5352-4002/001 00303: ADJUSTED TAILCONE RELEASE MECHANISM CAM REF
- [SDR DALA2021052702916](https://openairdocs.org/sdr/DALA2021052702916.md): Battery · inoperative · May 26, 2021 · N947AT · Boeing 717200 · Emergency Lighting
  > THE EMERGENCY EXIT SIGN AT ROW 19 WOULD NOT LIGHT UP WHEN THE EMERGENCY LIGHTS WERE TURNED ON. MAINTENANCE REPLACED THE EMERGENCY BATTERY B5-120. OPERATIONAL CHECK WAS GOOD PER B717 AMM 33-51. OK FOR SERVICE. (LP #7374124)
- [SDR DALA2021083005089](https://openairdocs.org/sdr/DALA2021083005089.md): Frame · damaged · Apr 10, 2021 · N947AT · Boeing 717200 · Fuselage Main, Frame
  > ER/A 581113-14 REV A WAS ISSUED FOR DAMAGE AT STA 1037, L-14L. FOLLOW ON ACTION IS REQUIRED. ACCOMPLISH ER/A 581113-14 REV A, SECTION II WITHIN 3,500FC FOLLOWING THE COMPLETION OF SECTION I (ACCOMPLISHED AT 36,606FC). ASSOCIATED ER/A 95-581113 ADDED FOR AC 950
- [SDR DALA2021042902459](https://openairdocs.org/sdr/DALA2021042902459.md): Skin · damaged · Apr 9, 2021 · N947AT · Boeing 717200 · Vertical Stabilizer, Plate/Skin
  > ER/A 560974-14AD REV D ISSUED FOR REPAIRS TO LOWER FIXED LE ON VERTICAL STAB. ACCOMPLISH ER/A 560974-14AD REV D SECTION III REPEAT INSPECTIONS EVERY 3,000FC FOLLOWING THE ACCOMPLISHMENT OF SECTION II (ACCOMPLISHED AT 53,271HRS AND 36,606CYC). ASSOCIATED ER/A 9
- [SDR DALA2025060704356](https://openairdocs.org/sdr/DALA2025060704356.md): Spar Cap · cracked · Apr 8, 2021 · N947AT · Boeing 717200 · Vertical Stabilizer, Spar/Rib
  > AIRCRAFT 9507, STABILIZERS / VERTICAL / APPROX. ZFS =62 - 44 / RH SPAR CAP, AND FORWARD SPAR WEB / CRACKS / AMOC 21-151. CORRECTIVE ACTION: COMPLIED WITH ER/A 561912-14AD SECTION III. (LP 1776790)
- [SDR DALA2021042902458](https://openairdocs.org/sdr/DALA2021042902458.md): Skin · damaged · Apr 8, 2021 · N947AT · Boeing 717200 · Vertical Stabilizer, Plate/Skin
  > VERTICAL STABILIZER LH LOWER FIXED LEADING EDGE SKIN FASTENER HOLES / BUSHING REPAIR / AD RELATED. REF PREVIOUS LOG 1263304. ER/A 562080-14 REV C ISSUED AND IS CURRENT REVISION. SECT III INSPECTIONS TBA WITHIN 3000FC AFTER SECT II, AND AT EVERY 3000FC REPEATIN
- [SDR DALA2020060802451](https://openairdocs.org/sdr/DALA2020060802451.md): Power Supply · inoperative · Jun 5, 2020 · N947AT · Boeing 717200 · Emergency Lighting
  > THE CEILING EMERGENCY LIGHTS IN THE FIRST CLASS CABIN TO ROW 14 ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY POWER SUPPLY B5-227 IAW B717 AMM 33-51. PERFORMED OPERATIONAL CHECK AND ALL LIGHTS CHECK GOOD.
- [SDR DALA2019091105260](https://openairdocs.org/sdr/DALA2019091105260.md): Retainer · cracked · Sep 10, 2019 · N947AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON RETAINER INTERNAL WINDOW SKIN RT SIDE OF COCKPIT AREA (SM). NRC 00720: RETAINER INTERNAL WINDOW SKIN RT SIDE OF COCKPIT AREA WAS REPAIRED PER ER/A 581231-14 REV ORIGINAL (SECTION I: PERMANENT REPAIR) AND ETI-17-19-172 REV 1 ASSOCIATED ER/A 14-581231 A
- [SDR DALA2019091005239](https://openairdocs.org/sdr/DALA2019091005239.md): Longeron Splice · corroded · Sep 10, 2019 · N947AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CORROSION ON SPLICE BTW STA 650 AND 660 LONGERON 30 C1 AREA (SM). NRC 00490: SPLICE BTW STA 650 AND 660 LONGERON 30 C1 WAS REPAIRED PER ETI-17-19-168 REV 2 AND ER/A 581203-14 REV ORIGINAL. ASSOCIATED ER/A 14-581203 ADDED FOR AC 9507. (LP #1263609)
- [SDR DALA2021041202110](https://openairdocs.org/sdr/DALA2021041202110.md): Skin · damaged · Sep 9, 2019 · N947AT · Boeing 717200 · Vertical Stabilizer, Plate/Skin
  > ERA 560974-14AD REV C ISSUED FOR REPAIRS TO LOWER FIXED LE ON VE RTICAL STAB. DTA / DTE IS REQUIRED. ASSOCIATED AA 5530-01048 ADDED FOR AC 9507. ASSOCIATED ER/A 00-560974 ADDED FOR AC 9507. DTE HAS BEEN ACCOMPLISHED. FOLLOW ON INSPECTIONS ARE REQUIRED. SECTION
- [SDR DALA2019091005238](https://openairdocs.org/sdr/DALA2019091005238.md): Support · cracked · Sep 9, 2019 · N947AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON AREA AND HOLES OF SETTLEMENT THE SUPPORT AT AFT UPPER CORNER OF COCKPIT RT SLINDING WINDOW CUT OUT (SM). NRC 00654: AFT UPPER CORNER OF COCKPIT RT SLINDING WINDOW CUT OUT WAS REPAIRED PER SRM 56-10-02-2R AND ER/A 581052-14 REV ORIGINAL ASSOCIATED ER/A
- [SDR DALA2019090905216](https://openairdocs.org/sdr/DALA2019090905216.md): Rub Strip · corroded · Sep 8, 2019 · N947AT · Boeing 717200 · Aerodynamic Fairings
  > CORROSION AT SEVERAL FILLET FAIRING RUBSTRIPS BTW STA Y=560 TO STA Y=848 AND STA Y=858 TO STA Y=917 BOTH SIDES (FUS). NRC 00520: CORROSION LEVEL 2, RUBSTRIPS (8 EA) BTW STA Y=560 TO STA Y=848 AND STA Y=858 TO STA Y=917 BOTH SIDES WERE REPLACED PER SRM 51-20-05

Next page: https://openairdocs.org/aircraft/N947AT/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 = 'N947AT' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N947AT/reports

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