# Service difficulty reports: N954AT

A list on [N954AT](https://openairdocs.org/aircraft/N954AT.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 · 163 reports

- [SDR DALA2026080604549](https://openairdocs.org/sdr/DALA2026080604549.md): Ils System · malfunctioned · Aug 6, 2026 · N954AT · Boeing 717200 · Auto Flight System
  > ILS 28C STARTED LOSING THE LOCATION INTERMITTENTLY ON THE CAPTAIN`S SIDE ON SHORT FINAL, 1500 THE AUTOPILOT 1 DISCONNECTED UNCOMMON, FO'S FD WENT OFF, SCREEN INTERMITTENTLY AFTER LOSSING AP1, T/S IAW FRM/FIM 22-10-00-810-802 & 22-10-00-810-809. NO FAULTS FOUN
- [SDR DALA2026073004420](https://openairdocs.org/sdr/DALA2026073004420.md): Light · inoperative · Jul 29, 2026 · N954AT · Boeing 717200 · Passenger Compartment Lighting
  > FOUND FWD AISLE LIGHT INOP. R & R AISLE LIGHT PER AMM 33-21. OP CKS GOOD. ACFT OK FOR SVC. (9223777) AIRCRAFT GROUNDED.
- [SDR DALA2025111808425](https://openairdocs.org/sdr/DALA2025111808425.md): Power Supply · faulted · Nov 17, 2025 · N954AT · Boeing 717200 · Emergency Lighting
  > EXTERIOR OVERWING EMERGENCY LIGHT WON'T EXTINGUISH. T/S OVERWING EMERGENCY LIGHTS PER B717 FIM 33-50-00-810-801. R & R EMERGENCY LIGHT POWER SUPPLY AT LOC B5-125 PER AMM 33-51. OPS CKD GOOD. (7844834).
- [SDR DALA2023121310203](https://openairdocs.org/sdr/DALA2023121310203.md): Unknown · unknown · Dec 12, 2023 · N954AT · Boeing 717200 · Airfoil Anti/De-ice System
  > SHIP 9513 -MISC/DE- THE CREW DECLARED AN EMERGENCY WHILE IN ICING CONDITIONS IN ORDER TO RAPIDLY DESCEND OUT OF ICING CONDITIONS AFTER RECEIVING A "WING MANIFOLD FAIL" MESSAGE. CORRECTIVE ACTION: MAINTENANCE REPLACED THE PODS PROCESSOR, REPAIRED A BLOWN DUCT,
- [SDR DALA2023100308100](https://openairdocs.org/sdr/DALA2023100308100.md): Unknown · unknown · Sep 29, 2023 · N954AT · Boeing 717200 · Emergency Equipment
  > THE CREW DISCOVERED THAT THE 1L GIRT BAR CABLE WAS DETACHED. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. CONTRACT MAINTENANCE REATTACHED THE GIRT BAR LANYARD PER B717 AMM 25-61. THE AIRCRAFT IS O
- [SDR DALA2023080806440](https://openairdocs.org/sdr/DALA2023080806440.md): Unknown · unknown · Aug 4, 2023 · N954AT · Boeing 717200 · Emergency Equipment
  > THE PILOT NOTICED THE 1L DOOR GIRT BAR TETHER STRAP WAS LOOSE. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE REATTACHED THE STRAP BUCKLE. OPERATIONAL CHECK WAS GOOD. (LP #4498172)
- [SDR DALA2023070705489](https://openairdocs.org/sdr/DALA2023070705489.md): Unknown · unknown · Jul 6, 2023 · N954AT · Boeing 717200 · Emergency Equipment
  > THE MAIN CABIN DOOR GIRT BAR STRAP NOT ATTACHED. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE REATTACHED THE GIRT BAR STRAP AS PER B717 AMM 25-61. (LP #4951546)
- [SDR DALA2023060604562](https://openairdocs.org/sdr/DALA2023060604562.md): Unknown · unknown · Jun 4, 2023 · N954AT · Boeing 717200 · Escape Slide
  > AFTER PARKING AT GATE IT WAS DISCOVERED THAT METAL LANYARD AND BRACKET WAS DISCONNECTED FROM FWD MAIN CABIN DOOR SLIDE. THIS WOULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. REINSTALLED 1L DOOR SLIDE LANYA
- [SDR DALA2023041302903](https://openairdocs.org/sdr/DALA2023041302903.md): Unknown · unknown · Apr 11, 2023 · N954AT · Boeing 717200 · Escape Slide
  > IN REFERANCE TO AMDS 5352-4002: DURING INSTALLATION OF TAILCONE SLIDE, THE RESTRAINT STRAPS WERE FOUND MISSING. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY OF THE NRC 712: STRAP (2 EAS) W
- [SDR DALA2023041002742](https://openairdocs.org/sdr/DALA2023041002742.md): Unknown · unknown · Apr 7, 2023 · N954AT · Boeing 717200 · Fuselage Floor Panel
  > CRACK ON FWD PAN NEAR TO BEAM 1 OF AFT CARGO CAMPARTMENT DOOR. (C2) SUMMARY OF NRC 00639: FWD PAN NEAR TO BEAM 1 OF AFT CARGO CAMPARTMENT DOOR (C2) WAS REPAIRED PER ER/A 606786-14 REV ORIGINAL SECTION I PERMANENT REPAIR AND PRI 606786-14 REV 2. (LP #2708762)
- [SDR DALA2023041002741](https://openairdocs.org/sdr/DALA2023041002741.md): Unknown · unknown · Apr 7, 2023 · N954AT · Boeing 717200 · Fuselage Floor Panel
  > CORROSION ON WEB OF AFT CUT OUT DOOR JAMB LOWER SECTION AT ENTRY DOOR (L1). SUMMARY OF NRC 00408: CORROSION LEVEL 2. REPAIR ON WEB OF AFT CUT OUT DOOR JAMB LOWER SECTION AT ENTRY DOOR (L1) WAS PERFORMED PER PRI ER/A606769-14 REV. 0 AND ER/A 606769-14 REV. ORIG
- [SDR DALA2023041002738](https://openairdocs.org/sdr/DALA2023041002738.md): Unknown · unknown · Apr 6, 2023 · N954AT · Boeing 717200 · Fuselage Main, Frame
  > CRACKED FRAME BTW BEAMS 4 AND 5 AT MAIN ENTRY DOOR. LOCATED JUST ON HANDLE HOUSING AREA. SUMMARY OF NRC 00075: FRAME (INTERCOSTAL) BTW BEAMS 4 AND 5 AT MAIN ENTRY DOOR ON HANDLE HOUSING AREA WAS FABRICATED AND REPLACED PER DWG 9955763 REV K AND B717-200 SRM 51
- [SDR DALA2023041002737](https://openairdocs.org/sdr/DALA2023041002737.md): Unknown · unknown · Apr 6, 2023 · N954AT · Boeing 717200 · Fuselage Main, Frame
  > CRACKED BEAM #6 (CENTER SECTION) AT MAIN ENTRY DOOR. SUMMARY OF NRC 00077: BEAM #6 (CENTER SECTION) AT MAIN ENTRY DOOR WAS REPAIRED PER B717-200 SRM 51-70-11-2R REPAIR 1. (LP #2706615)
- [SDR DALA2023040602681](https://openairdocs.org/sdr/DALA2023040602681.md): Unknown · unknown · Apr 5, 2023 · N954AT · Boeing 717200 · Fuselage Floor Panel
  > CORROSION ON CUSP ANGLE BTW STA Y=170 TO Y=203 AND X=-60 BELOW SERVICE DOOR SURROUND. SUMMARY OF NRC 00553: CORROSION LEVEL 2. CUSP ANGLE BTW STA Y=170 TO Y=203 AND X=-60 BELOW SERVICE DOOR SURROUND WAS REPAIRED PER PRI 606633-14 REV.2 AND ER/A 606633-14 REV.
- [SDR DALA2023033102476](https://openairdocs.org/sdr/DALA2023033102476.md): Unknown · unknown · Mar 30, 2023 · N954AT · Boeing 717200 · Aerodynamic Fairings
  > AIRCRAFT 9513, AFTER TAILCONE SLIDE REMOVAL, IT WAS FOUND UNPACKED. CORRECTIVE ACTION: TAILCONE SLIDE WAS REMOVED P/N: D29984-213 S/N: 1539 PER AMM 25-61-02-000-801 AND SERVICEABLE TAILCONE SLIDE P/N: D29984-213 S/N: 1561RP WAS REPLACED. (LP 2695495)
- [SDR DALA2023032902432](https://openairdocs.org/sdr/DALA2023032902432.md): Unknown · unknown · Mar 28, 2023 · N954AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > AIRCRAFT 9513, CORROSION ON INTERCOSTAL STA 814 BTW LONGERON 24 LH TO 23LH AT FWD CARGO COMPARTMENT. CORRECTIVE ACTION: INTERCOSTAL STA 814 BTW LONGERON 24 LH TO 23LH AT AFT CARGO COMPARTMENT WAS REPLACE PER B717 SRM 51-41-05-0G. AND PER DRAWING 9971095 ITEM 5
- [SDR DALA2023032802389](https://openairdocs.org/sdr/DALA2023032802389.md): Unknown · unknown · Mar 28, 2023 · N954AT · Boeing 717200 · Fuselage Main, Frame
  > AIRCRAFT 9513, CRACK ON OVERWING FRAME STA Y=674 LH SIDE AT WING BOX AREA. CORRECTIVE ACTION: OVERWING FRAME STA Y=674 LH WAS REPLACED PER CARD 5310-01436-03A. (LP 2691308)
- [SDR DALA2023032802388](https://openairdocs.org/sdr/DALA2023032802388.md): Unknown · unknown · Mar 27, 2023 · N954AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > AIRCRAFT 9513, INITIAL INSPECTION: CRACK 3EA S BTW STA 1087 AND 1076 ABOVE LONG 14 RH AT EXTERNAL FUSELAGE SKIN. CORRECTIVE ACTION: CRACK 3EA S BTW STA 1087 AND 1076 ABOVE LONG 14 RH WERE REPAIRED PER PRI 606376-14 REV. 1 AND ER/A 606376-14 REV. ORIGINAL SECTI
- [SDR DALA2023032702356](https://openairdocs.org/sdr/DALA2023032702356.md): Unknown · unknown · Mar 27, 2023 · N954AT · Boeing 717200 · Fuselage Main, Frame
  > AIRCRAFT 9513, INITIAL INSPECTION: CORROSION AT CUSP ANGLE LOWER SURFACE ON STA=560 TO STA =579 ON FWD CARGO COMPARTMENT RH SIDE. CORRECTIVE ACTION: CUSP ANGLE LOWER SURFACE ON STA =560 TO STA=579 ON FWD CARGO COMPARTMENT RH SIDE WAS REPAIRED PER B717 200 SRM
- [SDR DALA2023032702355](https://openairdocs.org/sdr/DALA2023032702355.md): Unknown · unknown · Mar 27, 2023 · N954AT · Boeing 717200 · Fuselage Main, Frame
  > AIRCRAFT 9513, AFTER REMOVAL WEB BTW STA Y=200 TO 208 AND STRINGERS L13 TO L18 CORROSION WAS FOUND AT CUSP ANGLE AT STA Y-200 ON STRINGER L18. CORRECTIVE ACTION: CUSP ANGLE AT STA Y-200 ON STRINGER L18 WAS REPAIRED PER B717-200 SRM 53-00-55-2 REPAIR 3 PAR. 5.
- [SDR DALA2023032602318](https://openairdocs.org/sdr/DALA2023032602318.md): Unknown · unknown · Mar 25, 2023 · N954AT · Boeing 717200 · Fuselage Floor Panel
  > AIRCRAFT 9513, INITIAL INSPECTION: CORROSION ON FLOOR SUPPORTS BTW STA Y=148 TO STA Y= 200 AND BTW X=-43 TO X=-54. CORRECTIVE ACTION: FLOOR SUPPORTS BTW STA Y=148 TO STA Y= 200 AND BTW X=-43 TO X=-54 WERE REPLACED PER B717-200 SRM 51-41-02-0G. (LP 2686942)
- [SDR DALA2023032602316](https://openairdocs.org/sdr/DALA2023032602316.md): Unknown · unknown · Mar 24, 2023 · N954AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > AIRCRAFT 9513, INITIAL INSPECTION: CORROSION ON LONGERON END 24RH STA Y 944 AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: CLIP ON LONGERON END 24RH STA Y 944 AT AFT CARGO COMPARTMENT WAS REPLACED PER B-717-200 SRM 51-40-02-0G. AND SRM 51-41-05-0G. (LP 2686715)
- [SDR DALA2023032602313](https://openairdocs.org/sdr/DALA2023032602313.md): Unknown · unknown · Mar 24, 2023 · N954AT · Boeing 717200 · Fuselage Main, Frame
  > AIRCRAFT 9513, INITIAL INSPECTION: CORROSION ON RH CUSP WEB STA. Y= 198 TO Y=202 (R1) RBL50 AT PASSENGER CABIN. CORRECTIVE ACTION: RH CUSP WEB STA. Y=200 TO Y=218 (R1) RBL50 AT PASSENGER CABIN WAS FABRICATED AND REPLACED PER DWG 9936535 REV. CS ITEM: -95 AND B
- [SDR DALA2023032402308](https://openairdocs.org/sdr/DALA2023032402308.md): Unknown · unknown · Mar 24, 2023 · N954AT · Boeing 717200 · Fuselage Floor Panel
  > AIRCRAFT 9513, CORROSION ON DIAPHRAGM STA Y=200 RBL45 - 55 (UNDER R1) VIEW FROM E/E COMPARTMENT. CORRECTIVE ACTION: REPAIR ON DIAPHRAGM STA Y=200 RBL45 - 55 (UNDER R1) VIEW FROM E / E COMPARTMENT WAS PERFORMED PER B-717-200 SRM 51-70-10 REPAIR 2 PAR. 4 FIG. 20
- [SDR DALA2023032402307](https://openairdocs.org/sdr/DALA2023032402307.md): Unknown · unknown · Mar 24, 2023 · N954AT · Boeing 717200 · Fuselage Main, Frame
  > AIRCRAFT 9513, CUSP ANGLE ON R1 DOOR JAMB WAS FOUND CORROSION ON CUSP WEB TO BTW STA 218 TO STA 237 RH. CORRECTIVE ACTION: CUSP WEB TO BTW STA 218 TO STA 237 RH WAS FABRCATED AND REPAIRED PER B 717-200 SRM 53-00-55-2R-4 FIG 226, DWG 9930538-109 REV. CC AND WAS
- [SDR DALA2023032402306](https://openairdocs.org/sdr/DALA2023032402306.md): Unknown · unknown · Mar 24, 2023 · N954AT · Boeing 717200 · Fuselage Main, Frame
  > AIRCRAFT 9513, CUSP ANGLE ON R1 DOOR JAMB WAS FOUND CORROSION ON ANGLE SUPPORT BTW STA 137 TO STA 160. CORRECTIVE ACTION: ANGLE WAS FABRICATED PER DWG 5910085 REV DE. (LP 2685491)
- [SDR DALA2023032402305](https://openairdocs.org/sdr/DALA2023032402305.md): Unknown · unknown · Mar 24, 2023 · N954AT · Boeing 717200 · Fuselage Main, Frame
  > AIRCRAFT 9513, CUSP ANGLE ON R1 DOOR JAMB WAS FOUND CORROSION ON ANGLE SUPPORT BTW STA 200 TO STA 210. CORRECTIVE ACTION: ANGLE SUPPORT WAS REPLACED PER DRAWING 5910085 ITEM 15 REV. DJ. (LP 2685489)
- [SDR DALA2023032402304](https://openairdocs.org/sdr/DALA2023032402304.md): Unknown · unknown · Mar 24, 2023 · N954AT · Boeing 717200 · Fuselage Floor Panel
  > AIRCRAFT 9513, CORROSION ON FLOOR SUPPORTS BTW STA Y=148 TO STA Y= 200 AND BTW X=-9 TO X=-42. CORRECTIVE ACTION: FLOOR SUPPORTS WERE REPLACED PER DWG 9936534 REV. BW AND PER B717-200 SRM-51-41-02-0G PAR. 4. (LP 2685485)
- [SDR DALA2023032402303](https://openairdocs.org/sdr/DALA2023032402303.md): Unknown · unknown · Mar 23, 2023 · N954AT · Boeing 717200 · Fuselage Main, Frame
  > AIRCRAFT 9513, CRACKS (2EAS) AND ELONGATED HOLES ON LH CUSP WEB BTW STA=656 TO STA=715 AND X=44 TO X=60 AT PAX CABIN. CORRECTIVE ACTION: CUSP WEB BTW STA=656 TO STA=715 AND X=44 TO X=60 AT PAX CABIN WAS FABRICATED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAI
- [SDR DALA2023032202171](https://openairdocs.org/sdr/DALA2023032202171.md): Unknown · unknown · Mar 21, 2023 · N954AT · Boeing 717200 · Cargo/Baggage Doors
  > AIRCRAFT 9513, CRACK ON FITTING ON FWD PAN NEAR TO BEAM 1 OF AFT CARGO COMPARTMENT DOOR WAS FOUND. CORRECTIVE ACTION: FITTING ON FWD PAN NEAR TO BEAM 1 OF AFT CARGO COMPARTMENT DOOR WAS FABRICATED AND REPLACED PER B717-200 SRM 51-41-01-0G, SRM 51-41-05-0G AND
- [SDR DALA2023032202170](https://openairdocs.org/sdr/DALA2023032202170.md): Unknown · unknown · Mar 21, 2023 · N954AT · Boeing 717200 · Fuselage Floor Panel
  > AIRCRAFT 9513, INITIAL INSPECTION: CORROSION ON FLOOR SUPPORT BTW STA Y= 200 TO STA Y=218 AND X=-11 AT CABIN PAX. CORRECTIVE ACTION: FLOOR SUPPORT BTW STA Y= 200 TO STA Y=218 AND X=-11 AT CABIN PAX WAS REPLACED PER B717-200 SRM 51-41-05-0G. PAR.8. (LP 2681442)
- [SDR DALA2023032202169](https://openairdocs.org/sdr/DALA2023032202169.md): Unknown · unknown · Mar 21, 2023 · N954AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > AIRCRAFT 9513, INITIAL INSPECTION: CRACK ON FRAME BTW STA=1037 BTW LONGERON 17RH AND LONGERON #18RH OF PAX CABIN. CORRECTIVE ACTION: REPAIR WAS PERFORMED PER B717-200 SRM 53- 20-07-2R PROCEDURE 4 REPAIR 4. (LP2680687)
- [SDR DALA2023032202168](https://openairdocs.org/sdr/DALA2023032202168.md): Unknown · unknown · Mar 20, 2023 · N954AT · Boeing 717200 · Cargo/Baggage Doors
  > AIRCRAFT 9513, INITIAL INSPECTION: CRACK ON UPPER PAN STA Y 389 AT FWD CARGO COMPARTMENT DOOR. CORRECTIVE ACTION: UPPER PAN ON STA Y 389 AT FWD CARGO COMPARTMENT DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1, REPAIR 1 PAR. (LP2680219)
- [SDR DALA2023031802045](https://openairdocs.org/sdr/DALA2023031802045.md): Unknown · unknown · Mar 18, 2023 · N954AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > AIRCRAFT 9513, INITIAL INSPECTION: CORROSION AND CRACK ON LH CUSP WEB (UPPER-LOWER SURFACE) STA. Y= 636 TO Y=655 AT PASSENGER CABIN. CORRECTIVE ACTION: LH CUSP WEB ON STA. Y=636 TO Y=655 AT PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4
- [SDR DALA2023031802044](https://openairdocs.org/sdr/DALA2023031802044.md): Unknown · unknown · Mar 18, 2023 · N954AT · Boeing 717200 · Cargo/Baggage Doors
  > AIRCRAFT 9513, INITIAL INSPECTION: CRACK ON INNER AFT PAN ABOVE BEAM 5 AT FWD CARGO DOOR. CORRECTIVE ACTION: INNER AFT PAN ABOVE BEAM 5 AT FWD CARGO DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1, REPAIR 1. (LP 2675859)
- [SDR DALA2023031802043](https://openairdocs.org/sdr/DALA2023031802043.md): Unknown · unknown · Mar 17, 2023 · N954AT · Boeing 717200 · Fuselage Floor Panel
  > AIRCRAFT 9513, INITIAL INSPECTION: CORROSION ON LUGS (FLOOR SUPPORT) STA=147 BTW RBL=30 TO RBL=50 AT COCKPIT. CORRECTIVE ACTION: FLOOR SUPPORT ON STA=147 BTW RBL=30 TO RBL=50 AT COCKPIT FABRICATED PER DWG 9936533-89 REV. CM AND WAS REPLACED PER B717-200 SRM 51
- [SDR DALA2023031802042](https://openairdocs.org/sdr/DALA2023031802042.md): Unknown · unknown · Mar 17, 2023 · N954AT · Boeing 717200 · Passenger/Crew Doors
  > AIRCRAFT 9513, INITIAL INSPECTION: CRACK ON BEAM NBR 1, (FWD EDGE) OF L1 PASSENGER ENTRANCE DOOR. CORRECTIVE ACTION: ENTRANCE DOOR L1 WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 7 REPAIR 7. (LP 2675276)
- [SDR DALA2023031802041](https://openairdocs.org/sdr/DALA2023031802041.md): Unknown · unknown · Mar 17, 2023 · N954AT · Boeing 717200 · Cargo/Baggage Doors
  > AIRCRAFT 9513, INITIAL INSPECTION: CRACK INTERCOSTAL ATTACH LOWER PAN STA Y 389 AT FWD CARGO COMPARTMENT DOOR. CORRECTIVE ACTION: INTERCOSTAL ATTACH LOWER PAN STA Y 389 AT FWD CARGO COMPARTMENT DOOR WAS REPLACED PER B717-200 SRM 51-41-02-0G AND SRM 51-41-05-0G
- [SDR DALA2023031802040](https://openairdocs.org/sdr/DALA2023031802040.md): Unknown · unknown · Mar 17, 2023 · N954AT · Boeing 717200 · Cargo/Baggage Doors
  > AIRCRAFT 9513, INITIAL INSPECTION: CRACK ON CLIP ON LOWER PAN SECTION STA Y 389 AT FWD CARGO COMPARTMENT DOOR. CORRECTIVE ACTION: CLIP OF LOWER PAN SECTION STA Y 389 AT FWD CARGO COMPARTMENT DOOR WAS REPLACED PER B717-200 SRM 51-41-02-0G AND SRM 51-41-05-0G. (
- [SDR DALA2023031702017](https://openairdocs.org/sdr/DALA2023031702017.md): Unknown · unknown · Mar 17, 2023 · N954AT · Boeing 717200 · Fuselage Floor Panel
  > AIRCRAFT 9513, INITIAL INSPECTION: CRACKED RH CUSP WEB STA. Y=389 (UNDER SEAT TRACK) AT PASSENGER CABIN. CORRECTIVE ACTION: RH CUSP WEB STA. Y=389 (UNDER SEAT TRACK) AT PASSENGER CABIN. WAS REPAIRED PER B717-200 SRM 53-00-55-2R. REP. 4. (LP2674411)
- [SDR DALA2023031702016](https://openairdocs.org/sdr/DALA2023031702016.md): Unknown · unknown · Mar 17, 2023 · N954AT · Boeing 717200 · Cargo/Baggage Doors
  > AIRCRAFT 9513, INITIAL INSPECTION: CRACK ON CLIP ON LOWER PAN SECTION STA Y 427 AT FWD CARGO COMPARTMENT DOOR. MAINTENANCE ACTION: CLIP ON LOWER PAN SECTION STA Y 427 WAS REPLACED PER B717-200 SRM 51-41-02-0G AND SRM 51-41-05-0G. (LP 2674408)
- [SDR DALA2023031702015](https://openairdocs.org/sdr/DALA2023031702015.md): Unknown · unknown · Mar 16, 2023 · N954AT · Boeing 717200 · Cargo/Baggage Doors
  > AIRCRAFT 9513, INITIAL INSPECTION: CRACK ON FITTING ATTACH UPPER PAN STA Y 389 AT FWD CARGO COMPARTMENT DOOR. MAINTENANCE ACTION: UPPER FITTING STA Y 389 WAS REPLACED PER B717-200 SRM 51-41-02-0G AND SRM 51-41-05-0G. (LP 2673904)
- [SDR DALA2023031702008](https://openairdocs.org/sdr/DALA2023031702008.md): Unknown · unknown · Mar 16, 2023 · N954AT · Boeing 717200 · Fuselage Main, Frame
  > AIRCRAFT 9513, INITIAL INSPECTION: CRACKED RH CUSP WEB (2 EA) STA. Y= 655 TO Y=674 AT PASSENGER CABIN. CORRECTIVE ACTION: CUSP WEB RH (2 EA) STA. Y= 655 TO Y=674 AT PASSENGER CABIN WERE REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4. CONFIGURATION 7003 CUSP
- [SDR DALA2023031501886](https://openairdocs.org/sdr/DALA2023031501886.md): Unknown · unknown · Mar 15, 2023 · N954AT · Boeing 717200 · Fuselage Main, Frame
  > IN REF NRC 00485 CORROSION ON RH CUSP WEB BTW STA Y=600 TO Y=615 AT PAX CABIN. SUMMARY OF NRC 00640: CORROSION LEVEL 2. CUSP WEB BTW STA Y=600 TO Y=615 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 FIGURE 216. (LP #2671432)
- [SDR DALA2023031401853](https://openairdocs.org/sdr/DALA2023031401853.md): Unknown · unknown · Mar 13, 2023 · N954AT · Boeing 717200 · Fuselage Floor Panel
  > CRACK ON INTERNAL ANGLE ON AFT PAN MIDDLE SECTION AT LH FWD OVERWING EMERGENCY EXIT DOOR. (PTAS) SUMMARY OF NRC 00073: INTERNAL ANGLE AT LH FWD OVERWING EMERGENCY EXIT DOOR WAS FABRICATED AND REPLACED PER DWG 9957735 REV G, B717-200 SRM 51-41-02-0G AND 51-41-0
- [SDR DALA2023031401850](https://openairdocs.org/sdr/DALA2023031401850.md): Unknown · unknown · Mar 12, 2023 · N954AT · Boeing 717200 · Fuselage Floor Panel
  > CRACKED ON FWD PAN OF LH FWD OVERWING EMERGENCY EXIT DOOR. SUMMARY OF NRC 00655: FWD PAN OF LH FWD OVERWING EMERGENCY EXIT DOOR WAS REPAIRED PER B717-200 SRM 52-20-02-2R. (LP #2667352)
- [SDR DALA2023031001759](https://openairdocs.org/sdr/DALA2023031001759.md): None · none · Mar 8, 2023 · N954AT · Boeing 717200 · Fuselage Main, Frame
  > CRACKED RH CUSP WEB BTW STA Y=918-925 AND Y=935-942 AT PASSENGER CABIN. SUMMARY OF NRC 00489: CORROSION LEVEL 2. CUSP WEB RH BTW STA Y=918-925 AND Y=935-942 WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 REPAIR 4 PAR 5 B FIG 216. (LP #2661740)
- [SDR DALA2022122008239](https://openairdocs.org/sdr/DALA2022122008239.md): Pseu · failed · Dec 19, 2022 · N954AT · Boeing 717200 · Leading Edge Slat Position Indicating System
  > SHIP 9513- MISC/DE - WHILE ON APPROACH FOR LANDING THE CREW NOTED THE MASTER CAUTION WITH EICAS MESSAGE OF "PSEU FAIL". WHICH REQUIRED A NO SLAT / NO FLAP LANDING BE ACCOMPLISHED. THE CREW DID DECLARE AN EMERGENCY WITH ATC AND COMPLIED WITH THE QRH. CORRECTIVE
- [SDR DALA2022031601718](https://openairdocs.org/sdr/DALA2022031601718.md): None · none · Mar 15, 2022 · N954AT · Boeing 717200 · Emergency Lighting
  > DURING CHECK THE OPERATION OF THE EMERGENCY LIGHTING SYSTEM, LEFT AND RIGHT OVER-WING EMERGENCY EXTERIOR LIGHTS DON'T ILLUMINATE IN REFERENCE CARD 0514-2001 STEP 8. SUMMARY OF NRC 00110: OVERWING EMERGENCY EVACUATION BATTERY POWER SUPPLY WAS REPLACED PER B717-
- [SDR DALA2023041302904](https://openairdocs.org/sdr/DALA2023041302904.md): Unknown · unknown · Mar 14, 2022 · N954AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > ER/A 597798-14, FUSELAGE / SKIN / LH WINDOW BELT PANEL / Y=522-541 / LIGHTNING STRIKE. SUBJECT REPAIR REQUIRES FOLLOW-ON REPETITIVE INSPECTION AND PERMANENT REPAIR. ACCOMPLISH ER/A 597798-14, SECTION II REPETITIVE INSPECTION WITHIN EVERY 24 MONTHS OF SECTION I

Next page: https://openairdocs.org/aircraft/N954AT/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 = 'N954AT' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N954AT/reports

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