# Service difficulty reports: N935AT

A list on [N935AT](https://openairdocs.org/aircraft/N935AT.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 · 219 reports

- [SDR DALA2026050502818](https://openairdocs.org/sdr/DALA2026050502818.md): Elec Connector · loose · May 1, 2026 · N935AT · Boeing 717200 · Light System Wiring
  > SEVERAL EMERGENCY LIGHTS DO NOT TURN ON, ALONG CPAX INCLUDING DOORS AND CEILING PANELS ALSO 2 UPPER LIGHTS ON AFT ACCESORIES COMPARTMENT. CONNECTOR P1-1217 AND LINE ( C9318-51-18) OF (L2-787) AND LINE (C9318-64-20) OF (L2-506) WERE FOUND LOOSE AND WAS CONNEC
- [SDR DALA2025121009013](https://openairdocs.org/sdr/DALA2025121009013.md): Housing · dirty · Dec 8, 2025 · N935AT · Boeing 717200 · Cabin Cooling System
  > ATB, CREW REPORTED CABIN ODOR IN AFT CABIN ON TAKEOFF CLIMB. BORESCOPE BOTH ENGINES, NO DEFECTS NOTED. INSPECTED THE BOTH PACKS COALESCER BAGS AND FOUND THE HOUSING DIRTY. PERFORMED HIGH POWER RUNS WITH SNIFFER, NTF.
- [SDR DALA2025120508919](https://openairdocs.org/sdr/DALA2025120508919.md): Unknown · odor · Dec 4, 2025 · N935AT · Boeing 717200 · Air Distribution System
  > RETURNED TO STL DUE TO BURNT OIL SMELL AT 300FT AFTER GEAR RETRACTION. UNABLE TO DUPLICATE ODOR AT GATE RUNNING APU OR ENGINES. GATHERING PARTS AND P-TRACK FROM CARGO TO BEGIN FURTHER EVALUATION. FOUND GLYCOL IN RAM AIR INLET. REPLACED COALESCER BAGS AND DUC
- [SDR DALA2024040804184](https://openairdocs.org/sdr/DALA2024040804184.md): Lens · wrong part · Apr 8, 2024 · N935AT · Boeing 717200 · Emergency Lighting
  > PASSENGER EXIT SIGN IS MISSING THE WORD "EXIT". MISSING FROM LIGHT NEAREST CLOSET. MAINTENANCE FOUND THAT THE SIGN HAD BEEN INSTALLED BACKWARDS. ADJUSTED FWD CABIN EXIT SIGN PER B717 AMM 33-51. (LP #4601783)
- [SDR DALA2024032703839](https://openairdocs.org/sdr/DALA2024032703839.md): Cusp Web · corroded · Mar 25, 2024 · N935AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON RH CUSP ANGLE BTW STA Y=160-169 AND STA Y=200 AT PAX CABIN. SUMMARY OF NRC 00489: CORROSION LEVEL 2. CUSP ANGLE BTW STA Y=160-169 AND STA Y=200 AT PAX CABIN WAS REPAIRED PER ER/A 616043-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A
- [SDR DALA2024032503736](https://openairdocs.org/sdr/DALA2024032503736.md): Skin · debonded · Mar 24, 2024 · N935AT · Boeing 717200 · Trailing Edge Flaps
  > TWO DISBONDS WERE FOUND OF: 0.500 IN LENGTH.X 0.500 IN. WIDTH. ON DENTS LOWER SKIN AT LH CENTER FLAP VANE 26.500 IN. INBOARD EDGE, 12.500 IN. TRAILING EDGE AND 28.000 IN. INBOARD EDGE, 12.500 IN. TRAILING EDGE. (IN REFERENCE JOB# 020-0001) SUMMARY OF NRC 0065
- [SDR DALA2024032503735](https://openairdocs.org/sdr/DALA2024032503735.md): Frame · corroded · Mar 24, 2024 · N935AT · Boeing 717200 · Fuselage Main, Frame
  > CORROSION ON FRAME FROM STA 1022 LONGERON 30 CORDENATED X=-4 TO X=4. SUMMARY OF NRC 00708: CORROSION LEVEL 2. FRAME FROM STA 1022 LONGERON 30 CORDENATED X=-4 TO X=4 WAS REPAIRED PER B717 SRM 53-20-07-2R-3, 51-41-02-0G, AND 51-41-05-0G. PERFORM AN INITIAL VISUA
- [SDR DALA2024032503734](https://openairdocs.org/sdr/DALA2024032503734.md): Skin · cracked · Mar 23, 2024 · N935AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACK ON SKIN STA Y=370 BTW L20 AND L22 APROX AT FWD DOOR CARGO COMPARMENT. SUMMARY OF NRC 00227: SKIN STA Y=370 BTW L20 AND L22 APROX AT FWD DOOR CARGO COMPARMENT WAS REPAIRED PER PRI 616337-14 REV 0 AND ERA 616337-14 REV ORIG SECTION I: PERMANENT REPAIR. ASS
- [SDR DALA2024050805016](https://openairdocs.org/sdr/DALA2024050805016.md): Web · damaged · Mar 22, 2024 · N935AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > ELONGATED HOLES ON WEB BTW STA 370 TO 360 AND LONGERONS 24 RH TO 26 RH AT CUT OUT FORWARD CARGO COMPARTMENT DOOR (CCD). SUMMARY OF NRC 00131: WEB BTW STA 370 TO 360 AND LONGERONS 24 RH TO 26 RH AT CUT OUT FORWARD CARGO COMPARTMENT DOOR (CCD) WAS REPAIRED PER B
- [SDR DALA2024032303702](https://openairdocs.org/sdr/DALA2024032303702.md): Rib · worn · Mar 22, 2024 · N935AT · Boeing 717200 · Wing, Rib/Bulkhead
  > WEAR ON RIBS (3 EA) BETWEEN STA XIS 174 TO XIS 186 INSIDE FIXED LEADING-EDGE AT LH WING. SUMMARY OF NRC 00621: RIBS (3 EA) BETWEEN STA XIS 174 TO XIS 186 INSIDE FIXED LEADING-EDGE AT LH WING WERE REPAIRED PER ERA 616112-14 REV ORIG SECTION 1 PERMANENT REPAIR.
- [SDR DALA2024032203635](https://openairdocs.org/sdr/DALA2024032203635.md): Seat Track · corroded · Mar 21, 2024 · N935AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RH SEAT TRACKS X-54.0 BTW STA Y=200-256 AT PAX CABIN. SUMMARY OF NRC 00493: CORROSION LEVEL 2. RH SEAT TRACKS X-54.0 BTW STA Y=200-256 AT PAX CABIN WAS REPAIRED PER B717 SRM 53-20-52-2R PROCEDURE 5. (LP #0256135)
- [SDR DALA2024032103594](https://openairdocs.org/sdr/DALA2024032103594.md): Diaphragm · corroded · Mar 21, 2024 · N935AT · Boeing 717200 · Fuselage Main, Structure
  > CORROSION ON RIGHT DIAPHRAGM ON STA X=-44 AND X=-56 FROM STA Y 200 TO Y 218 AT W1 AREA. SUMMARY OF NRC 00697: CORROSION LEVEL 2. RIGHT DIAPHRAGM ON STA X=-44 AND X=-56 FROM STA Y 200 TO Y 218 AT W1 AREA WAS REPLACED PER DWG 9936535 REV CS, PER B717-200 SRM 51-
- [SDR DALA2024032103593](https://openairdocs.org/sdr/DALA2024032103593.md): Guide Vane · punctured · Mar 21, 2024 · N935AT · Boeing 717200 · Trailing Edge Flaps
  > PUNCTURE ON AFT MOVABLE GUIDE VANE AT RH WING. SUMMARY OF NRC 00042: AFT MOVABLE GUIDE VANE AT RH WING WAS REPAIRED PER B717-200 SRM 57-53-01-2R PROCEDURE 1 REPAIR 1 AND 51-70-02-0G PROCEDURE GENERAL. (LP #0254635)
- [SDR DALA2024032103591](https://openairdocs.org/sdr/DALA2024032103591.md): Skin · cracked · Mar 21, 2024 · N935AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACKS ON FUSELAGE SKIN STA 1076.0 AND STA 1087 OVER LONGERON 14 RH. FUSELAGE SKIN STA 1076.0 AND STA 1087 OVER LONGERON 14 RH WAS REPAIRED PER ERA 616042-14 REV ORIGINAL SECTION 1 PERMANENT REPAIR. ASSOCIATED ERA 14-616042 ADDED FOR AC 9564. (LP #0254610)
- [SDR DALA2024032103577](https://openairdocs.org/sdr/DALA2024032103577.md): Diaphragm · cracked · Mar 16, 2024 · N935AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK AND PUNCTURE ON DIAPHRAGM BTW STA X=-44 AND X=-56 FROM STA Y=257 APPROX AT PASSENGER CABIN. SUMMARY OF NRC 00707: DIAPHRAGM BTW STA X=-44 AND X=-56 FROM STA Y=257 APPROX AT PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 REPAIR 4 AND 53-00-00
- [SDR DALA2024031503376](https://openairdocs.org/sdr/DALA2024031503376.md): Floor Support · corroded · Mar 15, 2024 · N935AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON CABIN FLOOR SUPPORTS AT X=-53, STA Y=160 TO 200; X=-15 TO -40, STA Y=180; STA Y=200, X=-44.5 TO -55; AND X=-12 STA Y=210. SUMMARY OF NRC 00677: CORROSION LEVEL 2. FLOOR SUPPORTS AT X=-53, STA Y=160 TO 200; X=-15 TO -40, STA Y=180; STA Y=200, X=-44
- [SDR DALA2024031503375](https://openairdocs.org/sdr/DALA2024031503375.md): Frame · cracked · Mar 14, 2024 · N935AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK ON FRAME STA Y=64 APPROX AND X=18 LH SIDE AT NLG W/W. SUMMARY OF NRC 00705: FRAME STA Y=64 APPROX AND X=18 LH SIDE AT NLG W/W WAS REPAIRED PER B717-200 SRM 53-00-00-2R REPAIR 1. (LP #0245021)
- [SDR DALA2024031403329](https://openairdocs.org/sdr/DALA2024031403329.md): Web · corroded · Mar 14, 2024 · N935AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON DIAPHRAGM MEMBRANE APPROX -X=53 STA Y=156 AT PAX CABIN. SUMMARY OF NRC 00488: CORROSION LEVEL 2. DIAPHRAGM MEMBRANE APPROX -X=53 STA Y=156 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 1 REPAIR 1. (LP #0243883)
- [SDR DALA2024031403328](https://openairdocs.org/sdr/DALA2024031403328.md): Tee Angle · corroded · Mar 13, 2024 · N935AT · Boeing 717200 · Fuselage Main, Attach Fittings
  > CORROSION ON ANGLE "TEE" STA 1053 LONGERON 30 AT AFT CARGO COMPARMENT. SUMMARY OF NRC 00559: CORROSION LEVEL 2. ANGLE "TEE" STA 1053 LONGERON 30 AT AFT CARGO COMPARMENT WAS REPLACED PER B717-200 SRM 51-41-05-0G. (LP #0242409)
- [SDR DALA2024031303281](https://openairdocs.org/sdr/DALA2024031303281.md): Pan · cracked · Mar 13, 2024 · N935AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON PAN BTW STA Y=427 AND BEAM 5 APROX AT FWD DOOR CARGO COMPARMENT. SUMMARY OF NRC 00226: PAN BTW STA Y=427 AND BEAM 5 APROX AT FWD DOOR CARGO COMPARMENT WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1. (LP #0242328)
- [SDR DALA2024031303279](https://openairdocs.org/sdr/DALA2024031303279.md): Frame · cracked · Mar 12, 2024 · N935AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK ON CANTED FRAME ON STA 1200 APROX. BTW L-17L AND L-18L AT AFT INTERNAL FUSELAGE. SUMMARY OF NRC 00232: CANTED FRAME ON STA 1200 APROX. BTW L-17L AND L-18L AT AFT INTERNAL FUSELAGE WAS REPAIRED PER B717-200 SRM 53-00-00-2R-1. (LP #0241299)
- [SDR DALA2024030803184](https://openairdocs.org/sdr/DALA2024030803184.md): Seat Track · corroded · Mar 8, 2024 · N935AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LH OTBD SEAT TRACK ON STA Y=636 AT CABIN PAX. SUMMARY OF NRC 00605: LH OTBD SEAT TRACK ON STA Y=636 AT CABIN PAX WAS REPAIRED PER B717-200 SRM 53-20-52-2R PROCEDURE 5, REPAIR 5. (LP #0235072)
- [SDR DALA2024030803183](https://openairdocs.org/sdr/DALA2024030803183.md): Longeron · corroded · Mar 7, 2024 · N935AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CORROSION ON LONGERON END STA Y=1050, LONG 28RH AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00654: CORROSION LEVEL 2. LONGERON END STA Y=1050, LONG 28RH AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-05-0G. (LP #0234611)
- [SDR DALA2024030703126](https://openairdocs.org/sdr/DALA2024030703126.md): Cusp Web · corroded · Mar 6, 2024 · N935AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON RH CUSP WEB UPPER AND LOWER SUARFACE FROM STA Y=489 TO STA Y=494 COORDINATES X=-44 TO COORDINATES X=-60 (CAB PAX). SUMMARY OF NRC 00668: CORROSION LEVEL 2. RH CUSP WEB UPPER AND LOWER SURFACE FROM STA Y=489 TO STA Y=494 COORDINATES X=-44 TO COORDI
- [SDR DALA2024030603062](https://openairdocs.org/sdr/DALA2024030603062.md): Intercostal · cracked · Mar 5, 2024 · N935AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK INTERCOSTAL ON INNER STRUCTURE STA 184 BTW BEAMS #4 AND 5 AT PASSENGER DOOR 1L. SUMMARY OF NRC 00144: INTERCOSTAL ON INNER STRUCTURE STA 184 BTW BEAMS #4 AND 5 AT PASSENGER DOOR 1L WAS FABRICATED PER DOUGLAS DWG 9955763 REV K AND REPLACED PER B717-200 SR
- [SDR DALA2024030503005](https://openairdocs.org/sdr/DALA2024030503005.md): Cusp Web · cracked · Mar 4, 2024 · N935AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON LH CUSP WEB LOCATED ON OUTB SEAT TRACK SPLICE AREA STA 595 AT PASSENGER CABIN. SUMMARY OF NRC 00639: LH CUSP WEB STA 595 AT PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4. (LP #0229779)
- [SDR DALA2024030402943](https://openairdocs.org/sdr/DALA2024030402943.md): Doubler · corroded · Mar 3, 2024 · N935AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CORROSION ON DOUBLER BELOW TEE FITTING STA 1053 LONGERON 30 AT AFT BULKHEAD. SUMMARY OF NRC 00562: CORROSION LEVEL 2. DOUBLER BELOW TEE FITTING STA 1053 LONGERON 30 AT AFT BULKHEAD WAS FABRICATED AND REPLACED PER B717-200 SRM 51-41-05-0G PAR 8 AND 51-41-02-0G
- [SDR DALA2024030402941](https://openairdocs.org/sdr/DALA2024030402941.md): Cusp Web · dented · Mar 3, 2024 · N935AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > DENT ON RH CUSP WEB APPROX STA Y=355, Y=441 AND X-44/-60 AT PAX CABIN. SUMMARY OF NRC 00400: RH CUSP WEB APPROX STA Y=355, Y=441 AND X-44/-60 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4 PAR 5 FIGURE 213. (LP #0227465)
- [SDR DALA2024030402938](https://openairdocs.org/sdr/DALA2024030402938.md): Cusp Web · corroded · Mar 2, 2024 · N935AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON LH CUSP WEB STA Y 636 AT PASSENGER CABIN. SUMMARY OF NRC 00640: CORROSION LEVEL 2. LH CUSP WEB STA Y 636 AT PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 51-70-10-2R REPAIR 2 PAR 4. (LP #0227124)
- [SDR DALA2024030402934](https://openairdocs.org/sdr/DALA2024030402934.md): Web · corroded · Mar 1, 2024 · N935AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON WEB (2 EA) OF STA Y=1053 LONGERON 30 AT AFT COMPARTMENT (C2). SUMMARY OF NRC 00638: CORROSION LEVEL 2. SECTIONS OF THE WEB (PREVIOUSLY REPAIRED) WERE REPLACED PER B717-200 SRM 51-41-02-0G STEP 8 A, 51-41-05-0G STEP 8, AND 51-70-10-2R. (LP #0225822
- [SDR DALA2024030402931](https://openairdocs.org/sdr/DALA2024030402931.md): Beam · cracked · Mar 1, 2024 · N935AT · Boeing 717200 · Fuselage Main, Structure
  > CRACK ON BEAM #1 ON STA 197 AT PASSENGER DOOR 1L. SUMMARY OF NRC 00138: BEAM #1 ON STA 197 AT PASSENGER DOOR 1L WAS REPAIRED PER B717-200 SRM 52-10-02-2R, PROCEDURE 7, REPAIR 7, FIGURE 201. (LP #0225315)
- [SDR DALA2024022802765](https://openairdocs.org/sdr/DALA2024022802765.md): Frame · cracked · Feb 27, 2024 · N935AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK ON FRAME STA Y1037 OVER LONG 17 RH AT CPAX. SUMMARY OF NRC 00409: FRAME STA 1037 OVER LONG 17 RH AT CPAX WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 4. (LP #0221351)
- [SDR DALA2024022602641](https://openairdocs.org/sdr/DALA2024022602641.md): Beam · cracked · Feb 25, 2024 · N935AT · Boeing 717200 · Fuselage Main, Structure
  > CRACK ON BEAM #2 ON STA 197 AT PASSENGER DOOR 1L. SUMMARY OF NRC 00139: BEAM #2 ON STA 197 AT PASSENGER DOOR 1L WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 8 REPAIR 8. (LP #0218077)
- [SDR DALA2024022602639](https://openairdocs.org/sdr/DALA2024022602639.md): Cusp Web · cracked · Feb 24, 2024 · N935AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON LH CUSP WEB STA 716 AND X44/60 AT CAB PAX. SUMMARY OF NRC 00399: CUSP WEB STA 716 AND X44/60 AT CAB PAX WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 (FIG.221). (LP #0216965)
- [SDR DALA2024022602635](https://openairdocs.org/sdr/DALA2024022602635.md): Seat Track · corroded · Feb 23, 2024 · N935AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK -X=22 BTW STA Y=215-256 PAX CABIN. SUMMARY OF NRC 00580: CORROSION LEVEL 2. SEAT TRACK -X=22 BTW STA Y=215-256 PAX CABIN WAS REPAIRED PER B717-200 53-20-52-2R PROCEDURE 5. (LP #0215602)
- [SDR DALA2024022202462](https://openairdocs.org/sdr/DALA2024022202462.md): Frame · cracked · Feb 22, 2024 · N935AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK ON FRAME STA Y1037 OVER LONG 17 LH AT CPAX. SUMMARY OF NRC 00408: FRAME STA Y1037 OVER LONG 17 LH AT CPAX WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 4. PERFORM AN GVI ON FRAME STA Y=1037 OVER LONG 17 LH AT CPAX EVERY "C" CHECK PER B717 SRM 53-20
- [SDR DALA2023083107086](https://openairdocs.org/sdr/DALA2023083107086.md): Unknown · unknown · Aug 31, 2023 · N935AT · Boeing 717200 · Emergency Lighting
  > THE FORWARD OVERWING EMERGENCY EXIT LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY B5-121 PER B717 AMM 33-51. OPERATIONAL TEST WAS GOOD. (LP #4094980)
- [SDR DALA2023081406583](https://openairdocs.org/sdr/DALA2023081406583.md): Unknown · unknown · Aug 11, 2023 · N935AT · Boeing 717200 · Emergency Lighting
  > THE OVERHEAD LIGHT FIXTURE IN THE FWD GALLEY AT R1 DOOR WITH BUILT-IN EMERGENCY LIGHTING IS MISSING LENS COVER. MAINTENANCE INSTALLED THE MISSING OVERHEAD LIGHT FIXTURE LENS IN FWD GALLEY ABOVE R1 DOOR IN REF WITH B717 AMM 33-23. THIS ACTION ALSO CLEARS NEF 33
- [SDR DALA2023080806441](https://openairdocs.org/sdr/DALA2023080806441.md): Unknown · unknown · Aug 5, 2023 · N935AT · Boeing 717200 · Emergency Lighting
  > THE EMERGENCY EXIT COVER DIFFUSER LENS FELL OFF AT AFT CABIN. MAINTENANCE RESECURED LENS COVER PER B717 AMM 33-51. OK FOR SERVICE. (LP #2902779)
- [SDR DALA2023021701234](https://openairdocs.org/sdr/DALA2023021701234.md): None · none · Feb 16, 2023 · N935AT · Boeing 717200 · Emergency Lighting
  > THE F/O SIDE EXIT SIGN AT THE EMERGENCY ROW FELL OFF DURING TURBULENCE. MAINTENANCE RESECURED THE EXIT SIGN LENSE COVER AT THE EMERGENCY EXIT ROW CROWN. (LP #8566510)
- [SDR DALA2023012400523](https://openairdocs.org/sdr/DALA2023012400523.md): Splice · cracked · Jan 20, 2023 · N935AT · Boeing 717200 · Vertical Stabilizer
  > NOTED CRACK ON RT SIDE 2ND SCREW HOLE BELOW SPLICE 4NE 52.267. AFTER ACCOMPLISHMENT OF SEPARATION OF LAYERS, PERFORMED BHEC IAW STEP 14 OF AA5530-01048-02 AD 2618-10-08 & NOTED CRACK APPEARED TO BE IN SPAR RUNNING TOWARD 7 O'CLOCK. REMOVED VERTICAL STAB LEADI
- [SDR DALA2022100406445](https://openairdocs.org/sdr/DALA2022100406445.md): None · none · Oct 3, 2022 · N935AT · Boeing 717200 · Emergency Lighting
  > THE OVERWING EMERGENCY LIGHTS WERE DISCOVERED INOPERATIVE. MAINTENANCE FOUND A FAULTY POWER SUPPLY. THE POWER SUPPLY B5-125 WAS REPLACED PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #9062743)
- [SDR DALA2022083005818](https://openairdocs.org/sdr/DALA2022083005818.md): None · none · Aug 30, 2022 · N935AT · Boeing 717200 · Emergency Lighting
  > AIRCRAFT 9564, BOTH OVERWING EMERGENCY LIGHTS DO NOT ILLUMINATE. CORRECTIVE ACTION: REPLACED EMERGENCY LIGHTS OVERWING BATTERY. LP 9128322
- [SDR DALA2022061004080](https://openairdocs.org/sdr/DALA2022061004080.md): Battery · inoperative · Jun 9, 2022 · N935AT · Boeing 717200 · Emergency Lighting
  > THE EXTERIOR EMERGENCY LIGHT IS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY POWER SUPPLY AND REPLACED THE BATTERY REF B717 AMM 33-51-01. (LP #9247536)
- [SDR DALA2022051303315](https://openairdocs.org/sdr/DALA2022051303315.md): None · none · May 13, 2022 · N935AT · Boeing 717200 · Emergency Lighting
  > DURING THE SERVICE CHECK, SEVEN EMERGENCY LIGHTS IN THE CABIN WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED SEVEN EMERGENCY LIGHT BATTERIES IN THE CABIN. OPERATIONAL CHECK WAS NORMAL. (LP #8635234)
- [SDR DALA2022031601715](https://openairdocs.org/sdr/DALA2022031601715.md): None · none · Mar 12, 2022 · N935AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > FOUND CORROSION ON INTERCOSTAL AFT CARGO BILGE AREA, AFT OF STA 1022, L29R. REPLACED PER BOEING DRAWING 9936718. CORROSION LEVEL 2. (LP #2154330)
- [SDR DALA2022031501676](https://openairdocs.org/sdr/DALA2022031501676.md): None · none · Mar 11, 2022 · N935AT · Boeing 717200 · Fuselage Main, Keel
  > FOUND LIGHT CORROSION BILGE AREA AFT CARGO, STA 1022, FWD AND AFT OF STRINGER, L29 R. "M". SUMMARY SEE NRC 045-0008:5331-2001/001 00357: REPLACED LONGERON AT BILGE AREA AFT CARGO, STA 1022, STRINGER, L30 PER B712 DRAWING #5911425. CORROSION LEVEL:2. (LP #2153
- [SDR DALA2022031401646](https://openairdocs.org/sdr/DALA2022031401646.md): None · none · Mar 10, 2022 · N935AT · Boeing 717200 · Escape Slide
  > TAILCONE SLIDE DATA TAG STATES SLIDE IS OUT OF DATE. OVERHAUL WAS DUE IN DECEMBER 2020. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY SEE NRC 001-0261:2000-1002/021 00462: MAINTENANCE REPLA
- [SDR DALA2022031001550](https://openairdocs.org/sdr/DALA2022031001550.md): None · none · Feb 20, 2022 · N935AT · Boeing 717200 · Trailing Edge Flaps
  > RT WING UPPER TRAILING EDGE PANEL DAMAGED FWD OF THE OUTBRD SPOILER OUTBRD HINGE. REMOVED DAMAGED "T" AND WEB ASSY FROM AFT WING SPAR. REPLACED THE "T" AND WEB ASSY PER LONG BEACH DWG 9957465, 975008, AND 57-51-09 BOEING 717 SRM. RIB INSTALLATION INSP: QC5312.
- [SDR DALA2019110606423](https://openairdocs.org/sdr/DALA2019110606423.md): Light · disconnected · Nov 5, 2019 · N935AT · Boeing 717200 · Emergency Lighting
  > ROW 20D CEILING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE FOUND THE LIGHT ASSEMBLY DISCONNECTED. ONCE THE LIGHT WAS RECONNECTED THE OPERATION CHECKED GOOD REF B717 WDM 33-51 AND THE AIRCRAFT RETURNED TO SERVICE. (LP #6370942)

Next page: https://openairdocs.org/aircraft/N935AT/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 = 'N935AT' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N935AT/reports

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