# Service difficulty reports: N957AT

A list on [N957AT](https://openairdocs.org/aircraft/N957AT.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 · 187 reports

- [SDR DALA2026021801178](https://openairdocs.org/sdr/DALA2026021801178.md): Hydraulic Line · leaking · Feb 17, 2026 · N957AT · Boeing 717200 · Hydraulic System, Main
  > ATB, THE FLIGHT CREW PERFORMED AN AIR TURNBACK DUE TO A RIGHT HYDRAULIC SYSTEM QUANTITY LOW MESSAGE. MAINTENANCE FOUND A LT MAIN LANDING GEAR HYDRAULIC LINE LEAKING, REPLACED SAME OK FOR SERVICE. (LP 8408166)
- [SDR DALA2025081105989](https://openairdocs.org/sdr/DALA2025081105989.md): Frame · damaged · Aug 7, 2025 · N957AT · Boeing 717200 · Fuselage Main, Frame
  > SHIP 9516 FRAME AND FASTENERS DAMAGED AT 6 O'CLOCK POSITION ON CANTED. CORECTIVE ACTION: COMPLIED WITH ER/A 627973-14 (1130003)
- [SDR DALA2025080205797](https://openairdocs.org/sdr/DALA2025080205797.md): Pan · corroded · Jul 27, 2025 · N957AT · Boeing 717200 · Fuselage Main, Structure
  > SEVERAL AREAS OF CORROSION AROUND FASTENES. REPLACED FORWARD CARGO DOOR LOWER JAMB PAN IAW B717-200 SRM 53- 20-15-2R (1108952)
- [SDR DALA2025080205798](https://openairdocs.org/sdr/DALA2025080205798.md): Pin · cocked · Jul 27, 2025 · N957AT · Boeing 717200 · Aerodynamic Fairings
  > TAIL CONE RELEASE CAM PIN CLOCKED INCORRECTLY. ADDED WASHERS AND SHIMS WHICH WAS MISSING FROM THE TAIL CONE RELEASE CAM PIN TO CORRECT EXCESSIVE FORWARD AND AFT PLAY IN TAIL MECHANISM RELEASE CAM ASSEMBLY REF B717 AMM 53-52-03.
- [SDR DALA2025061504507](https://openairdocs.org/sdr/DALA2025061504507.md): Compressor · stalled · Jun 13, 2025 · N957AT · Boeing 717200 · Turbine Engine Compressor Section
  > SHIP 9516 - DIV - DIVERSION TO ORD DUE TO LEFT ENGINE COMPRESSOR STALL ON CLIMB. CORRECTIVE ACTION: PERFORMED BORESCOPE INSPECTION AND FOUND SEVERAL HPC BLADES DAMAGED. REPLACED NBR 1 ENGINE. (LP 7264142)
- [SDR DALA2025030401652](https://openairdocs.org/sdr/DALA2025030401652.md): Pcdu · faulted · Mar 1, 2025 · N957AT · Boeing 717200 · Electrical Power System
  > SHIP 9516 -MISC/DE- THE FLIGHT CREW DECLARED AN EMERGENCY WITH ATC FOLLOWING A "RIGHT DC BUS FAILURE" INDICATION. THE RESULT OF THAT WAS A NO FLAP, NO SLAT LANDING. CORRECTIVE ACTION: MAINTENANCE REPLACED THE RIGHT PCDU AND THE LEFT POWER CONTACTOR RELAY. PERF
- [SDR DALA2024103010506](https://openairdocs.org/sdr/DALA2024103010506.md): Battery Pack · inoperative · Oct 30, 2024 · N957AT · Boeing 717200 · Emergency Lighting
  > THE OVERWING EXIT LIGHT IS INOPERATIVE. MAINTENANCE REPLACED THE OVERWING EXIT LIGHT BATTERY PACK PER B717 AMM 33-51. THE AIRCRAFT IS OK FOR SERVICE. (LP #6703153)
- [SDR DALA2024080507766](https://openairdocs.org/sdr/DALA2024080507766.md): Power Supply · no test · Aug 3, 2024 · N957AT · Boeing 717200 · Emergency Lighting
  > DURING SERVICE CHECK, THE EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE FROM THE FLIGHT ATTENDANT PANEL. MAINTENANCE FOUND THAT THE CABIN EMERGENCY LIGHTS WOULD WORK WITH COCKPIT SWITCH ARMED AND FLIGHT ATTENDANT SWITCH SET TO "ON" ONLY, BUT NOT FROM FLIGHT AT
- [SDR DALA2024072407443](https://openairdocs.org/sdr/DALA2024072407443.md): Circuit Breaker · tripped · Jul 23, 2024 · N957AT · Boeing 717200 · Electrical Power System
  > SHIP 9516 -MISC/DE- THE "DC R BUS OFF" WARNING ILLUMINATED IN CRUISE FLIGHT, ALONG WITH MANY OTHER ASSOCIATED MESSAGES. THE FLIGHT CREW DECLARED AN EMERGENCY INTO MKE DUE TO LOSS OF RIGHT DC BUS, BUT LANDED UNEVENTFULLY. CORRECTIVE ACTION: MAINTENANCE FOUND TH
- [SDR DALA2024040504129](https://openairdocs.org/sdr/DALA2024040504129.md): Battery · inoperative · Apr 3, 2024 · N957AT · Boeing 717200 · Emergency Lighting
  > TAIL CONE INTERIOR EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY AND POWERPACK REF B717 AMM 33-51-04. OPERATIONAL CHECK WAS GOOD. (LP #0275902)
- [SDR DALA2024040404052](https://openairdocs.org/sdr/DALA2024040404052.md): Battery · inoperative · Apr 3, 2024 · N957AT · Boeing 717200 · Emergency Lighting
  > ON SERVICE CHECK, FOUND AFT OVERWUNG EXIT SIGNS ABOVE DOOR TO BE INOPERATIVE. MAINTENANCE FOUND THE BATTERY CASE CRACKED. INSTALLED NEW BATTERY IAW B717 AMM 33-51-04. REPLACED POWER PACK ASSY PER B717 AMM 33-51-04. OPERATIONAL CHECK WAS GOOD. (LP #0275763)
- [SDR DALA2024010210751](https://openairdocs.org/sdr/DALA2024010210751.md): Unknown · unknown · Dec 27, 2023 · N957AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > GOUGES FOUND AT FUSELAGE BELLY SKIN FOR #1 RAD ALT TRANS ANTENNA. SUMMARY NRC 003-0001:0514-2001/001 00011: C/W ERA 614660-14 REV ORIG REPAIR INSTRUCTIONS. CHECKED TO ENSURE ALL PRI'S MATCH ERA 614660-14 REV ORIG. REPAIRED SKIN PER ERA 614660-14 REV ORIG. (LP
- [SDR DALA2023122110466](https://openairdocs.org/sdr/DALA2023122110466.md): Unknown · unknown · Dec 20, 2023 · N957AT · Boeing 717200 · Emergency Lighting
  > AFT OVERWING EMERGENCY EXIT SIGN IS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT IS OK FOR SERVICE. (LP #5513464)
- [SDR DALA2023081106541](https://openairdocs.org/sdr/DALA2023081106541.md): Unknown · unknown · Aug 10, 2023 · N957AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK ON DOOR BEAM #1 STA Y=198 AT PASSENGER ENTRANCE DOOR L1. SUMMARY OF NRC 00141: DOOR BEAM #1 STA Y=198 AT PASSENGER ENTRANCE DOOR L1 WAS REPAIRED PER B717-200 SRM 52-10-02-2R REPAIR 7. (LP #2911591)
- [SDR DALA2023081006498](https://openairdocs.org/sdr/DALA2023081006498.md): Unknown · unknown · Aug 9, 2023 · N957AT · Boeing 717200 · Aerodynamic Fairings
  > OUTER EMERGENCY TAILCONE HANDLE IS ARMED INCORRECTLY. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY OF NRC 00731: EMERGENCY TAILCONE HANDLE WAS REINSTALLED CORRECTLY PER B717-200 AMM 53-52-
- [SDR DALA2023080806439](https://openairdocs.org/sdr/DALA2023080806439.md): Unknown · unknown · Aug 7, 2023 · N957AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTAL (2 EA) BTW LONGERON 22 AND 21 LH FROM FRAME 1037 TO 1058 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00201: CORROSION LEVEL 2. INTERCOSTALS (2 EA) BTW LONGERON 22 AND 21 LH FROM FRAME 1037 TO 1058 AT AFT CARGO COMPARTMENT WERE REPLACED PE
- [SDR DALA2023080806438](https://openairdocs.org/sdr/DALA2023080806438.md): Unknown · unknown · Aug 7, 2023 · N957AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CORROSION DAMAGE TO INTERNAL SKIN BETWEEN LONGERON 21-22L, FRAMES Y1037- Y1058 AT AFT CARGO COMPARTMENT, DAMAGE IS ESTIMATED TO EXCEED THE ALLOWABLE LIMITS. SUMMARY OF NRC 00656: CORROSION LEVEL 2. INTERNAL SKIN BETWEEN LONGERON 21-22L BTW FRAMES STA Y=1037 -
- [SDR DALA2023080806436](https://openairdocs.org/sdr/DALA2023080806436.md): Unknown · unknown · Aug 4, 2023 · N957AT · Boeing 717200 · Cargo/Baggage Doors
  > WEAR ON FWD/AFT LATCH FITTINGS AT AFT CARGO DOOR. SUMARY OF NRC 00135: THE LATCH FITTINGS AT AFT/FWD AT AFT CARGO DOOR WERE REPLACED PER BOEING CMM 52-30-2. (LP #2901739)
- [SDR DALA2023080406295](https://openairdocs.org/sdr/DALA2023080406295.md): Unknown · unknown · Aug 3, 2023 · N957AT · Boeing 717200 · Fuselage Main, Frame
  > CORROSION ON FRAME STA 1037 BETWEEN LONGERON 24 TO LONGERON 21 LH AT AFT CARGO COMPARTMENT IS OUT LIMITS WITH 0.040 IN PER B717-200 SRM 53-00-00-1A ALLOWABLE DAMAGE GENERAL PAR. 4. C. FIGURE 103. SUMMARY OF NRC 00660: CORROSION LEVEL 2. FRAME STA 1037 BTW LONG
- [SDR DALA2023080306280](https://openairdocs.org/sdr/DALA2023080306280.md): Unknown · unknown · Aug 2, 2023 · N957AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGERS 22L, 23L, 24L, 26L, AND 27L FROM STA Y=898.5 TO Y=STA 1053 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00667: CORROSION LEVEL 2. STRINGERS 22L, 23L, 24L, 26L, AND 27L FROM STA Y=898.5 TO Y=STA 1053 AT AFT CARGO COMPARTMENT WERE REPLACED PER
- [SDR DALA2023080206248](https://openairdocs.org/sdr/DALA2023080206248.md): Unknown · unknown · Aug 1, 2023 · N957AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CORROSION ON LONGERONS END (28 Y 27) LH AND LONGERONS END (23 Y 26) LH AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00641: CORROSION LEVEL 2. LONGERONS END (28,27,26,23) LH AT AFT CARGO COMPARTMENT WERE REPLACED PER B-717-200 SRM 51-41-05-0G PAR 8.B. (LP #2896107
- [SDR DALA2023080206247](https://openairdocs.org/sdr/DALA2023080206247.md): Unknown · unknown · Jul 31, 2023 · N957AT · Boeing 717200 · Fuselage Main, Frame
  > CORROSION WAS FOUND ALONG FRAME SPLICE REPAIR AT STA 908 BTW L29-L AND L29 -R. SUMMARY OF NRC 00561: CORROSION LEVEL 2. REPAIR SPLICE AT FRAME STA 908 BTW LONGERON 27R TO LONGERON 28L WERE FABRICATED AND REPLACED PER B717-200 SRM 53-20-07-2R PROCEDURE 3 REPAIR
- [SDR DALA2023080106208](https://openairdocs.org/sdr/DALA2023080106208.md): Unknown · unknown · Jul 31, 2023 · N957AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CORROSION ON LON-30, LON-28L, AND LON-29L BTW STA 905 TO STA 1053 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00158: CORROSION LEVEL 2. LON-30, LON-28LH, AND LON-29LH BTW STA 905 TO STA 1053 WERE REPLACED PER B717-200 SRM 51-41-01-0G PAR 6, 51-41-02-0G PAR 4, AND
- [SDR DALA2023080106207](https://openairdocs.org/sdr/DALA2023080106207.md): Unknown · unknown · Jul 31, 2023 · N957AT · Boeing 717200 · Fuselage Main, Frame
  > CORROSION ON ANGLE OF FRAME BTW LON 27R TO LON 28L STA 908 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00161: CORROSION LEVEL 2. ANGLE OF FRAME BTW LONG 26L TO LONG 26R STA 908 AT AFT CARGO COMPARTMENT WAS FABRICATED AND REPLACED PER DWG 9975524 REV P AND B717-20
- [SDR DALA2023080106204](https://openairdocs.org/sdr/DALA2023080106204.md): Unknown · unknown · Jul 30, 2023 · N957AT · Boeing 717200 · Fuselage Main, Frame
  > CORROSION WAS FOUND ALONG FRAME SPLICE REPAIR AT STA 927 BTW L26-L AND L26-R. SUMMARY OF NRC 00560: CORROSION LEVEL 2. FRAME SPLICE REPAIR AT STA 927 BTW L26-L AND L26-R WERE FABRICATED AND REPLACED PER B717-200 SRM 53-20-07-2R PROCEDURE 3 PAR 5, 51- 41-02-0G,
- [SDR DALA2023080106203](https://openairdocs.org/sdr/DALA2023080106203.md): Unknown · unknown · Jul 29, 2023 · N957AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CORROSION WAS FOUND ON LONGERON 22LH END FORWARD SECTION AT STA Y=1053 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00679: CORROSION LEVEL 2. LONGERON END 22LH WAS FABRICATED AND REPLACED PER DWG 4914954 REV A. (LP #2891485)
- [SDR DALA2023080106202](https://openairdocs.org/sdr/DALA2023080106202.md): Unknown · unknown · Jul 29, 2023 · N957AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON ANGLE BTW LONGERON 29 RH TO 28 LH AND FRAME 950 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00233: CORROSION LEVEL 2. ANGLE BTW LONGERON 29 RH TO 28 LH AND FRAME 950 AT AFT CARGO COMPARTMENT WAS FABRICATED AND REPLACED PER DWG 995814-39 REV CC AND B7
- [SDR DALA2023072806112](https://openairdocs.org/sdr/DALA2023072806112.md): Unknown · unknown · Jul 27, 2023 · N957AT · Boeing 717200 · Rudder, Tab Structure
  > DISBOND ON RUDDER TAB LH SIDE OF 1.7000IN LENGTH X 0.500IN WIDTH AT DENT #2, (9" ABOVE #2 HINGE 3"AFT L/E RUDDER TAB) IN REF MON JOB 029-0001, LOG 1488874. SUMMARY OF NRC 00564: DENT #2 AT RUDDER TAB LH SIDE WAS REPAIRED PER ER/A 609491-14 REV ORIGINAL SECTION
- [SDR DALA2023072706097](https://openairdocs.org/sdr/DALA2023072706097.md): Unknown · unknown · Jul 26, 2023 · N957AT · Boeing 717200 · Fuselage Structure (General)
  > CORROSION ON FRAME CLIP BTW LONGERON 26LH TO 26 RH STA Y=1022 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00710: CORROSION LEVEL 2. FRAME CLIP STA Y=1022 BTW STR 26RH TO STR 26LH WAS FABRICATED AND REPLACED PER DWG 9912243 REV JS AND PER B717-200 SRM 51-41-02-0G.
- [SDR DALA2023072505978](https://openairdocs.org/sdr/DALA2023072505978.md): Unknown · unknown · Jul 22, 2023 · N957AT · Boeing 717200 · Fuselage Main, Structure
  > CORROSION ON LOWER CUTOUT BTW FRAME 990 TO 950 AFT DOOR CARGO. SUMMARY OF NRC 00240: CORROSION LEVEL 2. LOWER DOOR JAMB WAS REPLACED PER B-717-200 SRM 51-41-02-0G PAR 4 AND 51-41-05-0G PAR 8. (LP #2879720)
- [SDR DALA2023072105927](https://openairdocs.org/sdr/DALA2023072105927.md): Unknown · unknown · Jul 20, 2023 · N957AT · Boeing 717200 · Fuselage Floor Panel
  > CORROSION ON FLOOR PANELS 222XF, 222NF, 223EF, 221SF, 221XF, 222HF, 222MF, 223AF, 222AQF, 222AWF, 222AJF, 222ASF, 222ZF, 222ALF, AND 222EF AT PASSENGER CABIN. SUMMARY OF NRC 00503: FLOOR PANELS 222XF, 222NF, 221XF, 222HF, 222MF, 223AF, 222AWF, 222ALF WERE REPA
- [SDR DALA2023072505975](https://openairdocs.org/sdr/DALA2023072505975.md): Unknown · unknown · Jul 19, 2023 · N957AT · Boeing 717200 · Fuselage Internal Mounting Structure
  > CORROSION ON TRACK BTW FRAME 950 TO 884 RH AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00242: CORROSION LEVEL 2. TIE TRACK BTW FRAME 884 TO 950 RH AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-01-0G PAR 6 AND 51-41-05-0G PAR 8. (LP #2874605)
- [SDR DALA2023072105920](https://openairdocs.org/sdr/DALA2023072105920.md): Unknown · unknown · Jul 19, 2023 · N957AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CARGO DOOR JAMB LOWER PAN SPLICE BTW STA 954 TO 994 AND L-27R AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00563: CORROSION LEVEL 2. AFT CARGO DOOR JAMB LOWER PAN SPLICE BTW STA 954 TO 994 AND L-27R AT AFT CARGO COMPARTMENT WAS FABRICATED PER B717
- [SDR DALA2023072105919](https://openairdocs.org/sdr/DALA2023072105919.md): Unknown · unknown · Jul 19, 2023 · N957AT · Boeing 717200 · Fuselage Main, Frame
  > CORROSION ON ANGLE OF FRAME STA 927 BTW L29R TO L27L AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00166: CORROSION LEVEL 2. ANGLE OF FRAME STA 927 BTW L29R TO L27L WAS FABRICATED PER DWG 9915524 REV M. NEW ANGLE OF FRAME STA 927, STRAP STA 908 STR 28RH AND 29RH, S
- [SDR DALA2023072105922](https://openairdocs.org/sdr/DALA2023072105922.md): Unknown · unknown · Jul 19, 2023 · N957AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON TRACKS RBL16 AND LBL16 BTW STA 810 TO STA 895 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00167: CORROSION LEVEL 2. TIE TRACKS RBL16 AND LBL16 BTW STA 810 TO STA 895 AT AFT CARGO COMPARTMENT WERE REPLACED PER B717-200 SRM 51-41-01-0G. (LP #2874607)
- [SDR DALA2023072105921](https://openairdocs.org/sdr/DALA2023072105921.md): Unknown · unknown · Jul 19, 2023 · N957AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON TRACK BTW FRAME 1022 TO 884 LH AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00241: CORROSION LEVEL 2. TIE TRACK BTW FRAME 884 TO 1022LH AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-01-0G. (LP #2874544)
- [SDR DALA2023071905862](https://openairdocs.org/sdr/DALA2023071905862.md): Unknown · unknown · Jul 18, 2023 · N957AT · Boeing 717200 · Fuselage Main, Frame
  > CORROSION ON SPLICE (4 EA) BTW FRAME 990 TO 950 FROM LONGERON 30 AND 27 LH AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00227: CORROSION LEVEL 2. SPLICE (4 EA) L-28 LH AND L-27 BTW STA Y=974 TO STA Y=994 AND SPLICE L-29 BTW STA Y=954 TO Y=974 LH WERE REPLACED PER
- [SDR DALA2023071405738](https://openairdocs.org/sdr/DALA2023071405738.md): Unknown · unknown · Jul 14, 2023 · N957AT · Boeing 717200 · Emergency Equipment
  > CORROSION ON GIRT BAR FITTINGS AT R1 DOOR. SUMMARY OF NRC 00691: CORROSION LEVEL 2. GIRT BAR FITTINGS (2 EA) WERE REPLACED PER B717 SRM 51-40-08-0G. (LP #2865125)
- [SDR DALA2023071405737](https://openairdocs.org/sdr/DALA2023071405737.md): Unknown · unknown · Jul 13, 2023 · N957AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > AFTER LONGERON 26 LH BTW STA Y=900 TO STA Y=1053 REMOVAL, CORROSION WAS FOUND AT FUSELAGE SKIN BTW STA 1000 TO STA 1006 L-26 LH. SUMMARY OF NRC 00688: CORROSION LEVEL 2. FINGER DOUBLER AT STA 946 TO 1006 LONGERON 26 LH WAS REPLACED PER B717-200 SRM 51-41-02-0G
- [SDR DALA2023071405736](https://openairdocs.org/sdr/DALA2023071405736.md): Unknown · unknown · Jul 13, 2023 · N957AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON TRIM PANELS (2 EA) FROM SERVICE DOOR STA Y=148 - Y=200. SUMMARY OF NRC 00472: CORROSION LEVEL 2. TRIM PANELS (2 EA) FROM SERVICE DOOR STA Y=148 - Y=200 WERE REPLACED PER B717 SRM 51-40-08-0G AND DWG 957828 REV AB. (LP #2863315)
- [SDR DALA2023071205664](https://openairdocs.org/sdr/DALA2023071205664.md): Unknown · unknown · Jul 11, 2023 · N957AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON WEBS BTW STA Y=148/218 AND BTW STA X=-60/60 AT PAX CABIN (W1). SUMMARY OF NRC 00373: CORROSION LEVEL 2. WEB STA Y=158/200 AND BTW X=-3.5/-60 AND Y=158/200 AND BTW X 48/60 WAS REPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 1 REPAIR 1. (LP #2861223
- [SDR DALA2023071205660](https://openairdocs.org/sdr/DALA2023071205660.md): Unknown · unknown · Jul 8, 2023 · N957AT · Boeing 717200 · Fuselage Structure (General)
  > CORROSION ON CUSP ANGLE BTW STA Y=158/171 APROX, BTW STA Y=195/207 APROX AND BTW RBL=54/60 AT PAX CABIN (W1). SUMMARY OF NRC 00413: CORROSION LEVEL 2. CUSP ANGLE BTW STA Y=158/171 APROX, BTW STA Y=195/207 APROX AND BTW RBL=54/60 WAS REPAIRED PER ER/A 609285-14
- [SDR DALA2023070705488](https://openairdocs.org/sdr/DALA2023070705488.md): Unknown · unknown · Jul 7, 2023 · N957AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK ON FRAMES STA=680 AND 715 AND LONGERON 26RH UNDER WING BARREL KEEL BEAMS AND CANTED KEEL INTERNAL STRUCTURE FUSELAGE. SUMMARY OF NRC 00291: FRAMES STA=680 AND 715 AND LONGERON 26RH UNDER WING BARREL KEEL BEAMS AND CANTED KEEL INTERNAL STRUCTURE FUSELAGE
- [SDR DALA2023070605438](https://openairdocs.org/sdr/DALA2023070605438.md): Unknown · unknown · Jul 5, 2023 · N957AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORTS BTW STA Y=197/158 AND LBL=54 AND FLOOR SUPPORTS STA Y=200 AND BTW RBL=44/54 AT PAX CABIN WERE FOUND OUT OF LIMITS (W1). SUMMARY OF NRC 00676: CORROSION LEVEL 2. FLOOR SUPPORTS BTW STA Y=197/158 AND LBL=54 AND FLOOR SUPPORTS STA Y=20
- [SDR DALA2023070605437](https://openairdocs.org/sdr/DALA2023070605437.md): Unknown · unknown · Jul 5, 2023 · N957AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORTS STA Y=197 AND BTW LBL=15/43 WAS FOUND OUT LIMITS AT PAX CABIN (W1). SUMMARY OF NRC 00677: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=197 BTW LBL=15/43 WAS FABRICATED AND REPLACED PER DWG 99365534 REV BW AND B717-200 SRM 51-41-02-0G AND
- [SDR DALA2023070505393](https://openairdocs.org/sdr/DALA2023070505393.md): Unknown · unknown · Jul 4, 2023 · N957AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT STA Y=200 LBL=6 WAS FOUND CORRODED OUT OF LIMITS AT PAX CABIN (W1). SUMMARY OF NRC 00678: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=200 LBL=6 TO RBL=6 WAS REPLACED PER B-717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP #2849660)
- [SDR DALA2023070305310](https://openairdocs.org/sdr/DALA2023070305310.md): Unknown · unknown · Jul 3, 2023 · N957AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CORROSION ON LONGERON END 24 RH BTW FRAME 1022 TO 1002 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00212: CORROSION LEVEL 2. LONGERON END 24 RH BTW STA Y=1022-Y=1002 WAS REPLACED PER B717-200 SRM 51-41-05-0G. (LP #2846590)
- [SDR DALA2023070305307](https://openairdocs.org/sdr/DALA2023070305307.md): Unknown · unknown · Jul 3, 2023 · N957AT · Boeing 717200 · Fuselage Floor Panel
  > CORROSION ON FLOOR SUPPORTS BTW STA Y=158/200 AND RBL=44, STA Y=179 AND BTW RBL=8/43, STA Y=200 AND BTW RBL=8/44. SUMMARY OF NRC 00604: CORROSION LEVEL 2. FLOOR SUPPORTS (3 EA) WERE REPLACED PER B717-200 SRM 51-40-02-0G AND 51-41-05-0G PAR 8.A. (LP #2846527)
- [SDR DALA2023070305299](https://openairdocs.org/sdr/DALA2023070305299.md): Unknown · unknown · Jun 30, 2023 · N957AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK -X=22.0 BTW STA Y=200 TO STA Y=270. SUMMARY OF NRC 00603: CORROSION LEVEL 2. SEAT TRACK SECTION X=-22.0 BTW STA Y=200 TO STA Y=270 WAS REPLACED PER B717-200 SRM 51-41-01-0G AND B717-200 SRM 51-41-05-0G. (LP #2842925)
- [SDR DALA2023063005263](https://openairdocs.org/sdr/DALA2023063005263.md): Unknown · unknown · Jun 30, 2023 · N957AT · Boeing 717200 · Fuselage Main, Frame
  > SEVERAL CRACKS ON CUSP WEB LH SIDE LOWER SIDE STA Y=586 BTW X=+60 AT PAX CAB. SUMMARY OF NRC 00520: CUSP WEB LH STA 579 TO STA 598 WAS FABRICATED PER B717-200 SRM 53-00-55-2R-4 AND DWG: 9910151 REV CH AND REPLACED PER B-717-200 SRM 51-41-02-0G AND 51-41-05-0G.

Next page: https://openairdocs.org/aircraft/N957AT/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 = 'N957AT' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N957AT/reports

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