# Service difficulty reports: N953AT

A list on [N953AT](https://openairdocs.org/aircraft/N953AT.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 3 · 137 reports

- [SDR DALA2026090905048](https://openairdocs.org/sdr/DALA2026090905048.md): Oxygen Mask · inoperative · Sep 9, 2026 · N953AT · Boeing 717200 · Crew Oxygen System
  > FO'S OXYGEN MASK HARNESS DOES NOT INFLATE, R & R HARNESS PER AMM 35-12. (9096980) (AIRCRAFT GROUNDED).
- [SDR DALA2025060604346](https://openairdocs.org/sdr/DALA2025060604346.md): Door · open · Jun 5, 2025 · N953AT · Boeing 717200 · Landing Gear Doors
  > SHIP 9512 -ATB/GEAR- RETURNED MSP DUE TO RUMBLING NOISE IN NOSE GEAR AREA AFTER GEAR RETRACTION. GEAR CYCLED BACK DOWN SHOWING LOCKED WITH 3 GREEN. NLG DOORS FOUND OPEN. NO DAMAGE NOTED. CLOSED DOORS, OPS CHECKS GOOD.
- [SDR DALA2025060604343](https://openairdocs.org/sdr/DALA2025060604343.md): Battery Pack · inoperative · Jun 1, 2025 · N953AT · Boeing 717200 · Emergency Lighting
  > SHIP 9512 DURING SVC CHK FOUND ENERGENCY LIGHTS SEAT ROW 25 TO AFT OF CABIN INOP. T/S REF B717 SSM 33-51 REPLACED BATTERY PACK B5-231 REF B717 AMM 33-51. CHECKS GOOD (7262863)
- [SDR DALA2024061105984](https://openairdocs.org/sdr/DALA2024061105984.md): Doubler · damaged · Jun 8, 2024 · N953AT · Boeing 717200 · Wing Main, Frame Structure
  > RT WING LE REFUEL PANEL DOOR CUTOUT JAMB DOUBLER DAMAGED AT BOTH CENTER LATCH LAND LOCATIONS. CUTOUT DAMAGED AT BOTH CENTER LATCH LAND LOCATIONS PER B717 SRM 57-40-01-2R PROCEDURE 3 FIG 3 SHT 1. PERFORMED HFEC IAW B717 PER B717 SRM 57-40-01-2R PROCEDURE 3 AND
- [SDR DALA2024061005958](https://openairdocs.org/sdr/DALA2024061005958.md): Door · bent · Jun 8, 2024 · N953AT · Boeing 717200 · Fluid Service Doors
  > ON ARRIVAL FOUND FUEL SELECTOR PANEL DOOR BENT OPEN. DAMAGE TO THE SLAT SEAL, DAMAGE TO FUEL SELECTOR PANEL, AND DAMAGE TO THE GUARDED SWITCHES. ALL REFUEL ASSOCIATED LATCHES WERE FOUND OPEN / UNLATCHED. REPLACED GUARDED SWITCHES IAW B717 AMM 28-21-14. REPAIRE
- [SDR DALA2024011500580](https://openairdocs.org/sdr/DALA2024011500580.md): Unknown · unknown · Jan 14, 2024 · N953AT · Boeing 717200 · Emergency Lighting
  > DURING SERVICE CHECK, MAINTENANCE FOUND THE FORWARD OVERWING EXIT LIGHT AND ISLE OVERWING EXIT LIGHT TO BE INOPERATIVE. MAINTENANCE REPLACED 2 EACH BATTERIES, AT ROWS 18 & 19, IAW B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. ALL LIGHTS ILLUMINATE. AIRCRAFT IS O
- [SDR DALA2023061504881](https://openairdocs.org/sdr/DALA2023061504881.md): Unknown · unknown · Jun 11, 2023 · N953AT · Boeing 717200 · Flight Compartment Windows
  > AT CRUISE, MULTIPLE SPARKS ON CENTER WINDSHIELD AND CRACK FORMED. TURNED ANTI-ICE OFF PER QRH PROCEDURE. REMOVED CENTER WINDSHIELD IAW B717 AMM 56-11-01. REPLACED CENTER WINDOW HEAT CONTROLLER IAW AMM 30-41-01 A2-10. REPLACED THE CENTER WINDOW PER B717 AMM 56-
- [SDR DALA2023042003112](https://openairdocs.org/sdr/DALA2023042003112.md): Unknown · unknown · Apr 19, 2023 · N953AT · Boeing 717200 · Hydraulic Pump, Auxiliary
  > SHIP 9512 -HYD/DE- THE RIGHT HYDRAULIC SYSTEM EXPERIENCED A COMPLETE LOSS OF FLUID WHILE ON APPROACH FOR LANDING. THE CREW DECLARED AN EMERGENCY WITH ATC AND THE ALTERNATE GEAR EXTENSION PROCEDURES WERE COMPLIED WITH. THE LANDING WAS UNEVENTFUL EXCEPT FOR THE
- [SDR DALA2023031802046](https://openairdocs.org/sdr/DALA2023031802046.md): Unknown · unknown · Mar 17, 2023 · N953AT · Boeing 717200 · Hydraulic System, Main
  > SHIP 9512 - MISC/HYD - DECLARED EMERGENCY FOR THE RIGHT HYDRAULIC SYSTEM QUANTITY DROPPING. CORRECTIVE ACTION: FOUND RUDDER LIMITER ACTUATOR LINE LEAKING. FOUND LEAK ON PIPE ASSY CONNECTED TO RUDDER LIMITER CONTROL. PIPE WAS CHAFING AGAINST WORN ADEL CLAMP (91
- [SDR DALA2023040402603](https://openairdocs.org/sdr/DALA2023040402603.md): Unknown · unknown · Mar 16, 2023 · N953AT · Boeing 717200 · Hydraulic System, Main
  > SHIP 9512 -HYD/MISC- THE FLIGHT CREW DECLARED AN EMERGENCY FOLLOWING THE ILLUMINATION OF THE "RIGHT HYD LO" MESSAGE AND THE RIGHT HYDRAULIC SYSTEM QUANTITY DROPPING. THE QRH WAS COMPLIED WITH AND THE LANDING WAS UNEVENTFUL. CORRECTIVE ACTION: MAINTENANCE FOUND
- [SDR DALA2023022001260](https://openairdocs.org/sdr/DALA2023022001260.md): None · none · Feb 17, 2023 · N953AT · Boeing 717200 · Landing Gear Position and Warning
  > SHIP 9512 -ATB/GEAR/DE- DURING CLIMB OUT AFTER TAKEOFF, THE RIGHT MAIN LANDING GEAR "UNSAFE" LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. THE CREW COMPLIED WITH THE QRH AND ATTEMPTED ANOTHER RETRACTION. WHEN IT WAS DETERMINED THAT THE RIGHT LANDING GEAR W
- [SDR DALA2023011800364](https://openairdocs.org/sdr/DALA2023011800364.md): Structure · cracked · Jan 17, 2023 · N953AT · Boeing 717200 · Passenger/Crew Doors
  > DURING PRESSURE SEAL REMOVAL, CRACK WAS FOUND ON PASSENGER DOOR FWD UPPER CORNER. PASSENGER DOOR FWD WAS REPLACED FOR THE SERVICIABLE DOOR AND A NEW BRACKET WAS REPLACED PER AMM 52-11-01.
- [SDR DALA2023011700313](https://openairdocs.org/sdr/DALA2023011700313.md): Skin · cracked · Jan 16, 2023 · N953AT · Boeing 717200 · Cargo/Baggage Doors
  > CRACK ON FWD SKIN PAN UPPER CORNER SIDE AT AFT CARGO COMPARTMENT DOOR (PTAS). SKIN PAN UPPER CORNER SIDE AT AFT CARGO COMPARTMENT DOOR WAS REPAIRED PER ER/A 604439-14 REV. ORIGINAL SECTION I PERMANENT REPAIR.
- [SDR DALA2023011000171](https://openairdocs.org/sdr/DALA2023011000171.md): Frame · cracked · Jan 8, 2023 · N953AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK ON FRAME STA Y=674, 696, & 715 BTW RH LONG 26 AND 28 AT CANTED KEEL. SUMMARY OF NRC 00332: FRAMES ON STA Y=674, 696, & 715 BTW RH LONG 26 AND 28 AT CANTED KEEL WERE REPAIRED PER B717-200 SRM 51-70-11-2R, REPAIR 1. (LP #2573068)
- [SDR DALA2023011000169](https://openairdocs.org/sdr/DALA2023011000169.md): Floorbeam · corroded · Jan 8, 2023 · N953AT · Boeing 717200 · Fuselage Main, Floor Beam
  > CORROSION ON FLOOR SUPPORT STA Y=200 BTW X=-9 AND X=-46 (CPAX)(W1). SUMMARY OF NRC 00334: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=200 BTW X=-9 AND X=-46 WAS REPLACED PER DWG 9936534 REV. BW AND B717-200 SRM 51-41-05-0G AND B717-200 SRM 51-41-02-0G. (LP #2572323
- [SDR DALA2023011000168](https://openairdocs.org/sdr/DALA2023011000168.md): Frame · cracked · Jan 7, 2023 · N953AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK ON FRAME BS 674, 696, & 715 BTW LH LONG 26 AND 28 AT CANTED KEEL. SUMMARY OF NRC 00331: FRAMES ON STA Y=674, 696, & 715 BTW LH LONG 26 AND 28 AT CANTED KEEL WERE REPAIRED PER B717-200 SRM 51-70-11 -2R, REPAIR 1. (LP #2571796)
- [SDR DALA2023010308523](https://openairdocs.org/sdr/DALA2023010308523.md): Web · corroded · Dec 30, 2022 · N953AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON WEB AT LWR SILL AREA BTW STA Y=946-954 PROJECTION LONG 28R-29R OF AFT CARGO COMPARTMENT. CORROSION LEVEL 2. WEB AT LWR SILL AREA BTW STA 946 TO STA 1002 PROJECTION LONG 28R-29R OF AFT CARGO WAS REPLACED IAW SRM 51-41-01-0G, SRM 51-41-02-0G PAR 4,
- [SDR DALA2022123008501](https://openairdocs.org/sdr/DALA2022123008501.md): Door Frame · corroded · Dec 30, 2022 · N953AT · Boeing 717200 · Fuselage Main, Structure
  > CORROSION ON LOWER DOOR JAMB AT AFT CARGO COMPARTMENT DOOR (C2). LOWER DOOR JAMB AT AFT CARGO COMPARTMENT DOOR WAS REPLACED IAW SRM 53-20-15- 2R REPAIR 7, SRM 51-40-02-0G, SRM 51-41-05-0G, AND SRM 51-41-01- 0G.
- [SDR DALA2022123008500](https://openairdocs.org/sdr/DALA2022123008500.md): Seat Track · corroded · Dec 29, 2022 · N953AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK SECTION X=-56 BTW STA=479 WAS FOUND CORRODED OUT LIMITS. SEAT TRACK SECTION X=-56 BTW STA=479 WAS REPAIRED IAW SRM 53-20-52-2R REP. 1 FIG. 201.
- [SDR DALA2022122908460](https://openairdocs.org/sdr/DALA2022122908460.md): Seat Track · corroded · Dec 29, 2022 · N953AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT SEAT TRACK SECTION X=-44 BTW STA Y=210 TO Y=275 WAS FOUND CORRODED OUT LIMITS. SUMMARY OF NRC 00503: CORROSION LEVEL 2. RH SEAT TRACK SECTION X =-44 BTW STA Y=218 TO Y=342 WAS REPAIRED PER B717-200 SRM 53-20 -52-2R PROCEDURE 5.
- [SDR DALA2022122908459](https://openairdocs.org/sdr/DALA2022122908459.md): Seat Track · cracked · Dec 29, 2022 · N953AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > AFTER REMOVAL RH SEAT TRACK SECTION X=-44 BTW STA Y= 218 TO Y=342 A CRACK WAS FOUND IN THE CUSP WEB AT STA Y=294 TO Y=300. SUMMARY OF NRC 00516: CUSP WEB STA Y=294 TO Y=300 WAS PERMANENTLY REPAIRED PER B717-200 SRM 53-00-55-2R-4 FIG. 222. (LP #2558235)
- [SDR DALA2022122908458](https://openairdocs.org/sdr/DALA2022122908458.md): Seat Track · corroded · Dec 29, 2022 · N953AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > IN REF TO NRC 00325: SEAT TRACK SECTION X=-56 BTW STA=920 TO STA=922 WAS FOUND CORRODED OUT LIMITS. SUMMARY OF NRC 00496: CORROSION LEVEL 2. SEAT TRACK SECTION X=- 56 BTW STA=920 TO STA=922 WAS REPAIRED PER ER/A 604805-14 SECTION I PERMANENT REPAIR REV ORIGINA
- [SDR DALA2022122908461](https://openairdocs.org/sdr/DALA2022122908461.md): Pan · worn · Dec 28, 2022 · N953AT · Boeing 717200 · Cargo/Baggage Doors
  > WEAR ON SKIN PAN NEAR TO AFT LATCH FITTING AT AFT CARGO COMPARTMENT DOOR (PTAS). SUMMARY OF NRC 00061: SKIN PAN NEAR TO AFT LATCH FITTING AT AFT CARGO COMPARTMENT DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 8, REPAIR 8. FIG. 206.
- [SDR DALA2022122908457](https://openairdocs.org/sdr/DALA2022122908457.md): Longeron · cracked · Dec 28, 2022 · N953AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CRACK ON LOGERON 2LH ON STA Y=1144 AT AFT ACCESSORIES COMPARTMENT (CAT). SUMMARY OF NRC 00469: LONGERON 2LH ON STA Y=1144 AT AFT ACCESSORIES COMPARTMENT WAS REPAIRED PER B717 SRM 53-00-05-2R PROCEDURE 2.
- [SDR DALA2022122708378](https://openairdocs.org/sdr/DALA2022122708378.md): Web · corroded · Dec 24, 2022 · N953AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON WEB BS 256, X=49. THE WEB WAS REPAIRED IAW SRM 53-00-55-2R-4R.
- [SDR DALA2022122708377](https://openairdocs.org/sdr/DALA2022122708377.md): Cusp Web · cracked · Dec 24, 2022 · N953AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON LT CUSP WEB INNER FACE AT BS 898, X=44. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R, REPAIR 4.
- [SDR DALA2022122708376](https://openairdocs.org/sdr/DALA2022122708376.md): Cusp Web · cracked · Dec 23, 2022 · N953AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK IN RT CUSP WEB BTW BS 617-636, X=-53 TO X=-59 IN PASSENGER CABIN. CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R-4, REPAIR 4.
- [SDR DALA2022122708375](https://openairdocs.org/sdr/DALA2022122708375.md): Seat Track · corroded · Dec 23, 2022 · N953AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK X=-22 BTW BS 200-266 WAS FOUND CORRODED OUT LIMITS. SEAT TRACK REPLACED IAW SRM 51-41-01-0G & SRM 51-41-05-0G.
- [SDR DALA2022122308316](https://openairdocs.org/sdr/DALA2022122308316.md): Angle · corroded · Dec 23, 2022 · N953AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORRODED OUT OF LIMITS AT CLIPS STA Y=829, Y=875, Y=912. ORIGINAL THICKNESS IS 0.032 IN AND MINIMUM REMAINING THICKNESS IS 0.10 IN, THEREFORE THE AREA IS OUT OF LIMITS IN REF NRC 00376 AT PAX CABIN. CLIPS STA Y=829, Y=875, Y=912 AT PAX CABIN WERE REPLACED PER
- [SDR DALA2022122308313](https://openairdocs.org/sdr/DALA2022122308313.md): Angle · cracked · Dec 22, 2022 · N953AT · Boeing 717200 · Cargo/Baggage Doors
  > AFTER SEAL RETAINER REMOVAL, CRACKED INTERNAL ANGLE WAS FOUND ON APROX STA Y=390 AT FWD CARGO DOOR. INTERNAL ANGLE ON AFT LOWER EDGE APROX STA Y=390 AT FWD CARGO DOOR WAS FABRICATED AND REPLACED PER DWG 9957664 REV N, B717-200 SRM 51-30-07-0G, SRM 51-41-05-0G
- [SDR DALA2022122308312](https://openairdocs.org/sdr/DALA2022122308312.md): Fitting · cracked · Dec 22, 2022 · N953AT · Boeing 717200 · Cargo/Baggage Doors
  > AFTER SEAL RETAINER REMOVAL, CRACK WAS FOUND ON FITTING. FITTING ON AFT LOWER EDGE AT FWD CARGO DOOR WAS REPLACED IAW SRM 51-41-01-0G AND SRM 51-41-02-0G.
- [SDR DALA2022122208293](https://openairdocs.org/sdr/DALA2022122208293.md): Web · cracked · Dec 22, 2022 · N953AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK ON LH CUSP WEB EDGE AT STA Y=717 AND X =56. SUMMARY OF NRC 00373: LH CUSP WEB EDGE AT STA Y=717 AND X=56 WAS PERMANENTLY REPAIRED PER B717-200 SRM 53-00-55-2R-4 REPAIR 4 FIGURE 203. (LP #2548917)
- [SDR DALA2022122208292](https://openairdocs.org/sdr/DALA2022122208292.md): Angle · cracked · Dec 21, 2022 · N953AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK ON INTERNAL ANGLE LOWER EDGE STA Y=389 APROX AT FWD CARGO COMPARTMENT. (CCD). SUMMARY OF NRC 00048: INTERNAL ANGLE LOWER EDGE STA Y=389 APROX AT FWD CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 52-30-02 -2R PROCEDURE 1 REPAIR 1. (LP #2548249)
- [SDR DALA2022122108269](https://openairdocs.org/sdr/DALA2022122108269.md): Floor Support · corroded · Dec 21, 2022 · N953AT · Boeing 717200 · Fuselage Floor Panel
  > CORROSION ON FLOOR SUPPORT STA Y=218 - X=0 (CPAX)(W1). SUMMARY OF NRC 00363: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=218 - X=0 WAS REPLACED PER B717-200 SRM 51-41-02-0G. (LP #2547442)
- [SDR DALA2022122108268](https://openairdocs.org/sdr/DALA2022122108268.md): Floor Support · corroded · Dec 21, 2022 · N953AT · Boeing 717200 · Fuselage Floor Panel
  > CORROSION ON FLOOR SUPPORT STA Y=200 BTW X=5 AND X=-5 (CPAX)(W1). SUMMARY OF NRC 00335: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=200 BTW X=5 AND X=-5 WAS FABRICATED AND REPLACED PER DWNG 936534 REV BW AND B717-200 SRM 51-41-02-0G. (LP #2547431)
- [SDR DALA2022122108267](https://openairdocs.org/sdr/DALA2022122108267.md): Support · corroded · Dec 21, 2022 · N953AT · Boeing 717200 · Fuselage Floor Panel
  > CORROSION ON GALLEY SUPPORT STA Y=210 & STA Y=217 - X=-11 (CPAX)(W1). SUMMARY OF NRC 00361: CORROSION LEVEL 2. GALLEY SUPPORT STA Y=210 & STA Y=217 - X=-11 WERE REPLACED PER B717-200 SRM 51-41-02- 0G. (LP #2547311)
- [SDR DALA2022122008238](https://openairdocs.org/sdr/DALA2022122008238.md): Web · punctured · Dec 20, 2022 · N953AT · Boeing 717200 · Fuselage Main, Frame
  > PUNCTURE ON WEB STA Y=217 - X=-11 WAS FOUND DURING REMOVAL OF GALLEY SUPPORT ON NRC 00361. (CPAX)( W1). SUMMARY OF NRC 00456: WEB STA Y=217 - X=-11 WAS REPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 2. PAR 4 FIG. 201. (LP #2545920)
- [SDR DALA2022122008237](https://openairdocs.org/sdr/DALA2022122008237.md): Floor Support · corroded · Dec 20, 2022 · N953AT · Boeing 717200 · Fuselage Floor Panel
  > SECONDARY NRC, IN REF NRC 00364: AFTER REMOVAL PARTS TO ATTEND DISCREPANCY, CORROSION ON FLOOR SUPPORT STA Y=200 AND X=-55 WAS FOUND AT PASSENGER CABIN FLOOR AREA. SUMMARY OF NRC 00462: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=200 AND X=-55 WAS REPLACED PER B717
- [SDR DALA2022121908173](https://openairdocs.org/sdr/DALA2022121908173.md): Floor Support · corroded · Dec 19, 2022 · N953AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORT STA Y=180 BTW X=-9 - X=-42. CORROSION LEVEL 2. FLOOR SUPPORT WAS REPLACED IAW SRM 51-41-02-0G AND B717-200 SRM 51-41-05-0G.
- [SDR DALA2022121908176](https://openairdocs.org/sdr/DALA2022121908176.md): Floor Support · corroded · Dec 18, 2022 · N953AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORT STA Y=160-200 X=-44 (CPAX)(W1). SUMMARY OF NRC 00338: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=160-200 X=-44 (CPAX)(W1) WAS FABRICATED AND REPLACED PER DWG 9936534 -71 AND B717-200 SRM 51-41-02-0G PAR 4 AND SRM 51-41-05-0G PAR 8. (LP #
- [SDR DALA2022121908175](https://openairdocs.org/sdr/DALA2022121908175.md): Floor Support · corroded · Dec 17, 2022 · N953AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION OUT OF LIMITS ON FLOOR SUPPORT AT STA Y=160-195. ORIGINAL THICKNESS IS 0.071 IN AND MINIMUM REMAINING THICKNESS IS 0.025 IN, THEREFORE THE AREA IS OUT OF LIMITS IN REF NRC 00352 AT PAX CABIN (CPAX)(W1). SUMMARY OF NRC 00457: CORROSION LEVEL 2. FLOOR
- [SDR DALA2022122008236](https://openairdocs.org/sdr/DALA2022122008236.md): Doubler · corroded · Dec 16, 2022 · N953AT · Boeing 717200 · Fuselage Floor Panel
  > CORROSION ON RH REPAIR DOUBLER BTWN STA 908 TO STA 927 AND FROM X=44 TO X=59 OF PASSENGER CABIN FLOOR. SUMMARY OF NRC 00333: CORROSION LEVEL 2. PREVIOS REPAIR DOUBLER BTW STA 908 TO STA 927 AND FROM X=-44 TO X=-59 OF FLOOR CABIN PASSENGER WAS REPLACED PER B-71
- [SDR DALA2022082405714](https://openairdocs.org/sdr/DALA2022082405714.md): None · none · Aug 23, 2022 · N953AT · Boeing 717200 · Emergency Lighting
  > THE EMERGENCY LIGHTS OVER THE EMERGENCY EXIT WINDOWS AND ALL OF THE CEILING LIGHTS AFT OF THE OVER WING EMERGENCY EXITS CAME ON IN FLIGHT. MAINTENANCE COULD NOT DUPLICATE THE PROBLEM. THE SYSTEM WAS RESET AND THE OPERATIONAL CHECK WAS GOOD PER B717 AMM 33-51-0
- [SDR DALA2022081605532](https://openairdocs.org/sdr/DALA2022081605532.md): None · none · Aug 16, 2022 · N953AT · Boeing 717200 · Steering Unit
  > SHIP 9512 -HYD/GEAR- AN EMERGENCY WAS DECLARED FOR THE APPROACH AND LANDING IN BTR FOLLOWING THE LOSS OF THE RIGHT HYDRAULIC SYSTEM FLUID. THE ALTERNATE GEAR EXTENSION PROCEDURES WERE NECESSARY AND UTILIZED. THE LANDING WAS UNEVENTFUL. CORRECTIVE ACTION: MAINT
- [SDR DALA2022051603342](https://openairdocs.org/sdr/DALA2022051603342.md): None · none · May 16, 2022 · N953AT · Boeing 717200 · Emergency Lighting
  > THE AFT LOWER OVERWING EMERGENCY EXIT LIGHTS WERE DISCOVERED AS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY POWER SUPPLY, PER B717 AMM 33-51. THE OPERATIONAL CHECK WAS GOOD. (LP #8505194)
- [SDR DALA2022051603341](https://openairdocs.org/sdr/DALA2022051603341.md): None · none · May 16, 2022 · N953AT · Boeing 717200 · Emergency Lighting
  > THE AFT OVERWING EMERGENCY EXIT LIGHTS ARE INOPERATIVE. THE BATTERY POWER SUPPLY WAS REPLACED BY MAINTENANCE PER B717 AMM 33-51. OPERATIONAL WAS CHECK GOOD. (LP #8505193)
- [SDR DALA2022051603340](https://openairdocs.org/sdr/DALA2022051603340.md): None · none · May 16, 2022 · N953AT · Boeing 717200 · Emergency Lighting
  > THE AFT BULKHEAD EMERGENCY EXIT LIGHT WAS DISCOVERED TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY POWER SUPPLY, PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #8505192)
- [SDR DALA2021113007344](https://openairdocs.org/sdr/DALA2021113007344.md): None · none · Nov 28, 2021 · N953AT · Boeing 717200 · Aerodynamic Fairings
  > TAIL CONE EXTERNAL RELEASE CLAMP OUT OF RIG LEFT AND RIGHT CLAMPS. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY SEE NRC 001-0113:5352-4002/003 00423: RIGGED CLAMPS PER B717 AMM 53-52-01. O
- [SDR DALA2021112907291](https://openairdocs.org/sdr/DALA2021112907291.md): None · none · Nov 24, 2021 · N953AT · Boeing 717200 · Fuselage Main, Frame
  > THE AFT CABIN EMERGENCY EXIT DOOR FRAME HAS TWO LARGE CRACKS. RIGHT HAND MID AREA. -M- SUMMARY SEE NRC 001-0308:5212-2001/001 00084: REPAIRED DAMAGE TO AFT CABIN EMERGENCY EXIT DOOR FRAME IAW PRI 595460-14 REV 0 THROUGH REV 4, AND ER/A 595460-14 REV ORIGINAL.
- [SDR DALA2021112407219](https://openairdocs.org/sdr/DALA2021112407219.md): None · none · Nov 23, 2021 · N953AT · Boeing 717200 · Escape Slide
  > THE LEFT HAND FORWARD ENTRY DOOR SLIDE HAS THE PARACHUTE PIN ROUTED INCORRECTLY. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY SEE NRC 001-0025:5211-4002/002 00405: THE LEFT HAND FORWARD EN

Next page: https://openairdocs.org/aircraft/N953AT/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 = 'N953AT' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N953AT/reports

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