# Service difficulty reports: N934AT

A list on [N934AT](https://openairdocs.org/aircraft/N934AT.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 · 204 reports

- [SDR DALA2026071304091](https://openairdocs.org/sdr/DALA2026071304091.md): Transceiver · faulty · Jul 10, 2026 · N934AT · Boeing 717200 · Ground Proximity System
  > ATB- RETURNED TO DTW DUE TO MULTIPLE FAULTS AFTER GEAR RETRACTION. REPLACED ALL RADIO ALTIMETER ANTENNAS AND BOTH TRANSCEIVERS. GEAR SWING AND RADIO ALTIMETER OPS CHECK GOOD. (6544512) (AIRCRAFT WAS GROUNDED)
- [SDR DALA2026070103877](https://openairdocs.org/sdr/DALA2026070103877.md): Coalescer Bag · odor · Jul 1, 2026 · N934AT · Boeing 717200 · Humidity Control System
  > BURNING SMELL WITH APU ON AND PACKS, R & R COALESCER BAGS PER B717 AMM 21-54-08. (6688572) (AIRCRAFT GROUNDED).
- [SDR DALA2026042902730](https://openairdocs.org/sdr/DALA2026042902730.md): Hinge Fitting · damaged · Apr 24, 2026 · N934AT · Boeing 717200 · Trailing Edge Flaps
  > SHIP 9565 LH WING T.E. FLAP ON FWD IDLER HINGE FITTING OUTBD LUG BORE DAMAGED. CORRECTIVE ACTION: REPAIRED PER ER/A 633228-14. (1559850) (AIRCRAFT GROUNDED)
- [SDR DALA2026041402347](https://openairdocs.org/sdr/DALA2026041402347.md): Not Reported · not reported · Apr 7, 2026 · N934AT · Boeing 717200 · Standard Practices/Structures
  > REFERENCE ER/A626909-14AD. COMPLIED WITH ER/A626909-14AD (1533159) (AIRCRAFT GROUNDED)
- [SDR DALA2025092306961](https://openairdocs.org/sdr/DALA2025092306961.md): Strap · damaged · Sep 22, 2025 · N934AT · Boeing 717200 · Wing Miscellaneous Structure
  > COMPLY WITH ER/A 626909-14AD SECTION IV LT WING REAR SPAR LOWER STRAP REPAIR. COMPLIED WITH ER/A 626909-14AD REV. E SECTION IV AND PRI 626909- 14AD REV. E REV 0 - 4. LH WING REAR SPAR LOWER STRAP REPAIR. (1212786)
- [SDR DALA2025090406564](https://openairdocs.org/sdr/DALA2025090406564.md): Spar Cap · cracked · Aug 21, 2025 · N934AT · Boeing 717200 · Wing Spar
  > LEFT WING REAR SPAR, LOWER CAP, AFT FLANGE CRACKED NEAR XRS = 164. REPAIRED PER ER/A 00-626909. (1156447)
- [SDR DALA2025062604793](https://openairdocs.org/sdr/DALA2025062604793.md): Girt Bar · detached · Jun 25, 2025 · N934AT · Boeing 717200 · Emergency Equipment
  > SHIP 9565 GIRT BAR DETACHED FROM 1R DOOR. CORRECTIVE ACTION: RE ATTACHED LANYARD ASSY. IAW 717 AMM 25-61 (6588676)
- [SDR DALA2025061504506](https://openairdocs.org/sdr/DALA2025061504506.md): Spar Cap · cracked · Jun 13, 2025 · N934AT · Boeing 717200 · Wing Spar
  > AIRCRAFT 9565, WHILE MAINTENANCE IN DTW WAS ACCOMPLISHING AA WORKCARD 5720-01103-01A, MTC DISCOVERED A CRACK COMMON TO THE LH WING LOWER SPAR CAP (P/N 5911301-507), COMMON TO THE LH WING REAR SPAR INSTL (P/N 9910010-511) AFT FLANGE NEAR XRS 164.000. CORRECTIVE
- [SDR DALA2025060604344](https://openairdocs.org/sdr/DALA2025060604344.md): Spar Cap · cracked · May 29, 2025 · N934AT · Boeing 717200 · Wing Spar
  > SHIP 9565 CRACK FOUND DURING INSPECTION OF LH WING REAR SPAR LOWER CAP AFT LEG. CONTACT LIASON ENGINEERING FOR REPAIR PROCEDURES PRIOR TO FURTHER FLIGHT. REF FC 5720-01103. BOLT LOCATION XRS158. CRACK AT 1OCLOCK POS LOOKING DOWN ON BOLT AND IS 3/8" FROM CENTER
- [SDR DALA2025012800656](https://openairdocs.org/sdr/DALA2025012800656.md): Battery Pack · inoperative · Jan 23, 2025 · N934AT · Boeing 717200 · Emergency Lighting
  > THE EMERGENCY LIGHTS ARE INOPERATIVE AT THE FWD LIGHT ATTENDANT STATION. MAINTENANCE REPLACED THE BATTERY PACK FOR THE EMERGENCY LIGHTS IN THE AFT CARGO COMPARTMENT PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #6733983)
- [SDR DALA2024022702692](https://openairdocs.org/sdr/DALA2024022702692.md): Control Valve · malfunctioned · Feb 24, 2024 · N934AT · Boeing 717200 · Leading Edge Slat Control System
  > SHIP 9565 -ATB/DE- THE CREW PERFORMED AN AIR TURNBACK AND DECLARED AN EMERGENCY WITH ATC DUE TO A SLAT DISAGREE. THE AIRCRAFT REQUIRED SIGNIFICANT AILERON CORRECTION FOR WINGS LEVEL ATTITUDE. THE QRH WAS COMPLIED WITH, AND THE RESULT WAS A NORMAL SLAT EXTENSIO
- [SDR DALA2023120609979](https://openairdocs.org/sdr/DALA2023120609979.md): Unknown · unknown · Dec 5, 2023 · N934AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > ELONGATED HOLES ON FUSELAGE BTW CANTED STA Y=1178 AND LOG PROJECT 14L AT AFT FUSELAGE. (IN REF TO NRC: 00238). SUMMARY OF NRC 00298: FUSELAGE BTW CANTED STA Y=1178 AND LOG PROJECT 14L AT AFT FUSELAGE WAS REPAIRED PER ER/A 613199-14 REV ORIGINAL, SECTION I: PER
- [SDR DALA2023120409900](https://openairdocs.org/sdr/DALA2023120409900.md): Unknown · unknown · Dec 2, 2023 · N934AT · Boeing 717200 · Trailing Edge Flaps
  > WEAR ON LEADING EDGE OF UPPER FLAP ON STA CW 61 AT RH WING. SUMMARY OF NRC00114: LEADING EDGE OF UPPER FLAP ON STA CW 61 AT RH WING WAS REPAIRED PER ER/A 613673-14 REV ORG SECTION I: PERMANENT REPAIR. (LP #0092117)
- [SDR DALA2024022002333](https://openairdocs.org/sdr/DALA2024022002333.md): Skin · corroded · Dec 1, 2023 · N934AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CORROSION ON UPPER SKIN OF CENTER WING AREA BTW STA 710 TO STA 756 AND X=-40 TO X=-56 AT CPAX. SUMMARY OF NRC 00354: CORROSION LEVEL 2. UPPER SKIN OF CENTER WING AREA BTW STA 710 TO STA 756 AND X=-40 TO X=-56 WAS REPAIRED PER ERA 613363-14 REV ORIGINAL SECTION
- [SDR DALA2023113009839](https://openairdocs.org/sdr/DALA2023113009839.md): Unknown · unknown · Nov 29, 2023 · N934AT · Boeing 717200 · Fuselage Main, Structure
  > INAPPROPRIATE HOLES ON VERTICAL BEAMS STA Y=817 AND STA X=0, X=13, 25, X=-13, -25 AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00184: VERTICAL BEAMS ON STA Y=817, X=13, X=25, X=-13, X=-25 AT AFT CARGO COMPARTMENT WERE REPAIRED PER B717 SRM 51-70-11-2R-2. BEAM
- [SDR DALA2023113009838](https://openairdocs.org/sdr/DALA2023113009838.md): Unknown · unknown · Nov 29, 2023 · N934AT · Boeing 717200 · Fuselage Main, Structure
  > CRACK FRAME ON AFT FACE OF AFT LAVATORY ENGINE PYLON SUPPORT BULKHEAD, STA 1022 AND LONGERON 7R. SUMMARY OF NRC 00259: PERMANENT REPAIR ON FRAME ON AFT FACE OF AFT LAVATORY ENGINE PYLON SUPPORT BULKHEAD, STA 1022 AND LONGERON 7R WAS PERFORMED PER PRI 613338-14
- [SDR DALA2023113009837](https://openairdocs.org/sdr/DALA2023113009837.md): Unknown · unknown · Nov 29, 2023 · N934AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACK AT FUSELAGE SKIN ON AFT CORNER OF LH SLIDING WINDOW CUTOUT IN COCKPIT. SUMMARY OF NRC 00583: FUSELAGE SKIN ON AFT CORNER OF LH SLIDING WINDOW CUTOUT WAS REPAIRED PER ERA 613859-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-613859 ADDED
- [SDR DALA2023113009836](https://openairdocs.org/sdr/DALA2023113009836.md): Unknown · unknown · Nov 29, 2023 · N934AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RH TIE TRACK BTW STA Y=813/954 AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00215: CORROSION LEVEL 2. RH TIE TRACK BTW STA Y=813/954 WAS REPLACED PER B717 SRM 51-41-05-0G PAR 8 AND 51-41-01-0G PAR 9. (LP #0087493)
- [SDR DALA2023112909802](https://openairdocs.org/sdr/DALA2023112909802.md): Unknown · unknown · Nov 29, 2023 · N934AT · Boeing 717200 · Fuselage Main, Structure
  > CORROSION ON LOWER EDGE OF BULKHEAD EMERGENCY EXIT DOOR JAMB ON STA Y=1053 AND X=-15 AT AFT PAX CABIN. SUMMARY OF NRC 00250: CORROSION LEVEL 2. LOWER EDGE OF BULKHEAD EMERGENCY EXIT DOOR JAMB ON STA Y=1053 AND X=-15 WAS REPAIRED PER ER/A 613464-14 REV ORIGINAL
- [SDR DALA2023112909801](https://openairdocs.org/sdr/DALA2023112909801.md): Unknown · unknown · Nov 29, 2023 · N934AT · Boeing 717200 · Fuselage, Door Hinge
  > WEAR ON AFT HINGE. ALSO WEAR ON INTERNAL SKIN (BELOW HINGE) AT FWD CARGO COMP DOOR. SUMMARY OF NRC 00075: INTERNAL SKIN (BELOW HINGE) AT FWD CARGO COMP DOOR WAS REPAIRED PER ERA 613609-14 REV ORIGINAL. SECTION 1 PERMANENT REPAIR AND PRI 613609-14 REV 1. AFT HI
- [SDR DALA2023112809762](https://openairdocs.org/sdr/DALA2023112809762.md): Unknown · unknown · Nov 28, 2023 · N934AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LH TIE TRACK BTW STA Y=813/1022 AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC S/N 00217: CORROSION LEVEL 2. LH TIE TRACK BTW STA Y=813/1022 AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-01-0G AND 51-41-05-0G PAR 8. (LP #0084915)
- [SDR DALA2023112809756](https://openairdocs.org/sdr/DALA2023112809756.md): Unknown · unknown · Nov 27, 2023 · N934AT · Boeing 717200 · Rudder, Tab Structure
  > DENT FOUND ON RUDDER CONTROL TAB, RH SURFACE BTW STA ZR=43 TO ZR=52 9.5" FROM T/E. SUMMARY OF NRC 00614: RUDDER CONTROL TAB RH SURFACE BTW STA ZR=43 TO ZR=52 9.5" FROM T/E WAS REPAIRED PER B717-200 SRM 51-70-02-0G WITH REFERENCE TO 55-41-01-2R-1 PAR 5 B (1) AN
- [SDR DALA2023112709719](https://openairdocs.org/sdr/DALA2023112709719.md): Unknown · unknown · Nov 22, 2023 · N934AT · Boeing 717200 · Trailing Edge Flaps
  > AFTER PADS WERE REMOVED, PUNCTURE AND CRACKS WERE FOUND ON LOWER MOVABLE FLAP VANE UPPER SKIN AT RH WING. SUMMARY OF NRC 00407: MOVABLE FLAP VANE OF RH WING WAS REPAIRED PER ER/A 613241-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-613241 ADD
- [SDR DALA2023112709716](https://openairdocs.org/sdr/DALA2023112709716.md): Unknown · unknown · Nov 22, 2023 · N934AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION FOUND OUT OF LIMITS ON RH SEAT TRACK (X=-54) STA Y=395-397, Y=748-755, AND Y=765-773 AT PAX CABIN. SUMMARY OF NRC 00555: CORROSION LEVEL 2. RH SEAT TRACK (X=-54) STA Y=395-397 WAS REPAIRED WITH PLUG PER B717 53-20-52-2R-1 REPAIR 1. SECTION SEAT TRACK
- [SDR DALA2023112109570](https://openairdocs.org/sdr/DALA2023112109570.md): Unknown · unknown · Nov 19, 2023 · N934AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CUSP WEB BTW STA Y=715 TO STA Y=756 AND X=-40 TO X=-56 AT PAX CABIN WAS NOTED TO HAVE CRACKS IN THE WEB. SUMMARY OF NRC 00613: CUSP WEB BTW STA Y=715 TO STA Y=756 AND X=-40 TO X=-56 WAS REPAIRED PER B717 SRM 53-00-55-2R PROCEDURE 4 FIG 211. (LP #0072824)
- [SDR DALA2023112209653](https://openairdocs.org/sdr/DALA2023112209653.md): Unknown · unknown · Nov 18, 2023 · N934AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON RH CUSP MEMBRANE WEB BTW STA 484 TO STA 503, ALSO BTW STA 655 TO STA 725 AT PAX CABIN. SUMMARY OF NRC 00331: RH CUSP MEMBRANE WEB ON STA 655 TO STA 715 WAS REPAIRED PER B717 SRM 53-00-55-2R REPAIR 4 FIG 204. ON STA 484 TO STA 503 GVI WAS PERFORMED AND
- [SDR DALA2023112009526](https://openairdocs.org/sdr/DALA2023112009526.md): Unknown · unknown · Nov 18, 2023 · N934AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK WAS FOUND AT CUSP WEB ON FUSELAGE STA 218, X= 56. SUMMARY OF NRC 00609: LH CUSP WEB ON FUSELAGE STA 218, X=56 WAS REPAIRED PER B717 SRM 51-70-10-2R PROCEDURE 2 PAR 4 FIG 201. (LP #0071687)
- [SDR DALA2023112009523](https://openairdocs.org/sdr/DALA2023112009523.md): Unknown · unknown · Nov 18, 2023 · N934AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK CUSP WEB BTW STA Y 256 BTW -X=-44 TO -X=56 AT CABIN PAX. SUMMARY OF NRC 00598: CUSP WEB BTW STA Y 256 BTW -X=-44 TO -X =56 WAS REPAIRED PER B717 SRM 53-00-55-2R PROCEDURE 4 FIG 211. (LP #0070354)
- [SDR DALA2023112009522](https://openairdocs.org/sdr/DALA2023112009522.md): Unknown · unknown · Nov 17, 2023 · N934AT · Boeing 717200 · Cargo/Baggage Doors
  > WEAR ON AFT EDGE NEAR OF AFT LATH ON AFT CARGO DOOR. SUMMARY OF NRC 00083: AFT EDGE (INNER PAN) NEAR OF AFT LATH ON AFT CARGO COMPARTMENT DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R, PROCEDURE 8, REPAIR 8. (LP #0070156)
- [SDR DALA2023112009521](https://openairdocs.org/sdr/DALA2023112009521.md): Unknown · unknown · Nov 17, 2023 · N934AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON LH CUSP MEMBRANE WEB STA 597. SUMMARY OF NRC 00603: LH CUSP MEMBRANE WEB STA 597 WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 PAR. 5, FIGURE 211. (LP #0070121)
- [SDR DALA2023112009519](https://openairdocs.org/sdr/DALA2023112009519.md): Unknown · unknown · Nov 17, 2023 · N934AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON LH CUSP WEBS STA Y=292 TO 294 AT PAX CABIN. SUMMARY OF NRC 00494: CORROSION LEVEL 2. LH CUSP WEB STA Y=292 TO 294 WAS REPAIRED PER B717 SRM 53-00-55-2R-4 FIG 211. (LP #0068683)
- [SDR DALA2023112009516](https://openairdocs.org/sdr/DALA2023112009516.md): Unknown · unknown · Nov 16, 2023 · N934AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON LH CUSP MEMBRANE WEB BTW STA Y=891 TO Y=908 AT PAX CABIN WAS FOUND OUT OF LIMITS PER B717 SRM 53-00-55-1A PROCEDURE 1 PAR 4 FIG 101. (ORIGINAL THICKNESS 0.020 IN AND MINIMUM REMAINING THICKNESS IS 0.008 IN). SUMMARY OF NRC 00589: CORROSION LEVEL 2
- [SDR DALA2023112009515](https://openairdocs.org/sdr/DALA2023112009515.md): Unknown · unknown · Nov 16, 2023 · N934AT · Boeing 717200 · Fuselage Floor Panel
  > CORROSION ON FLOOR SUPPORTS IS OUT LIMITS AT STA Y=148 BTW X=-44 AND X=-51, STA Y=200 BTW X=-9 AND X=-44, STA Y=173 TO STA Y=191 AND X=55, AND STA Y=210 AND X=-10. SUMMARY OF NRC 00561: CORROSION LEVEL 2. FLOOR SUPPORTS STA Y=148 BTW X=-44 AND X=-51, STA Y=200
- [SDR DALA2023111609441](https://openairdocs.org/sdr/DALA2023111609441.md): Unknown · unknown · Nov 16, 2023 · N934AT · Boeing 717200 · Fuselage Main, Structure
  > CORROSION WAS FOUND AT JAMB WEB BETWEEN STA 200 TO STA 208 ON L 18 LH. SUMMARY NRC 00604: CORROSION LEVEL 2. JAMB WEB BETWEEN STA 200 TO STA 208 ON L 18 WAS REPAIRED PER B717 SRM 53-00-00-2R PROCEDURE 2 REPAIR 2, PAR 4 FIG 201. (LP #0067252)
- [SDR DALA2023111509408](https://openairdocs.org/sdr/DALA2023111509408.md): Unknown · unknown · Nov 15, 2023 · N934AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON CUSP WEBS RH STA Y=953 TO Y=955 AND Y=958 TO Y=963. SUMMARY OF NRC 00489: CORROSION LEVEL 2. CORROSION ON CUSP WEBS RH STA Y=953 TO Y=970 WAS REPAIRED PER B717 SRM 53-00-55-2R REPAIR 4 FIG 223. (LP #0065452)
- [SDR DALA2023111509406](https://openairdocs.org/sdr/DALA2023111509406.md): Unknown · unknown · Nov 14, 2023 · N934AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON RH CUSP WEBS STA Y=580 TO 590 AND STA Y=597 IN REF NRC 00551. SUMMARY OF NRC 00573: CORROSION LEVEL 2. CORROSION ON RH CUSP WEBS STA Y=580 TO 590 AND STA Y=597 WAS REPAIRED PER B717 SRM 53-00-55-2R REPAIR 4 FIG 216. (LP #0065239)
- [SDR DALA2023111509405](https://openairdocs.org/sdr/DALA2023111509405.md): Unknown · unknown · Nov 14, 2023 · N934AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR MEMBRANES STA Y=198 X=-15, Y=198 X=-20, Y=180 X=-15, Y=184 X=-20, Y=183 X=-6, AND Y=197 X=50. SUMMARY OF NRC 00547: CORROSION LEVEL 2. CORROSION ON FLOOR MEMBRANES STA Y= 198 X=-15, Y=198 X=-20, Y=180 X=-15, Y=184 X=-20, Y=183 X=-6, AND Y= 1
- [SDR DALA2023111409353](https://openairdocs.org/sdr/DALA2023111409353.md): Unknown · unknown · Nov 14, 2023 · N934AT · Boeing 717200 · Fuselage Main, Floor Beam
  > CRACK FLOOR BEAM STA Y=737 AND X=53 APROX AT PAX CABIN. SUMMARY OF NRC 00262: FLOOR BEAM STA Y=737 AND X=53 APROX WAS REPLACED PER B717 SRM 51-41-02-0G & 51-41-05-0G. (LP #0063896)
- [SDR DALA2023111309308](https://openairdocs.org/sdr/DALA2023111309308.md): Unknown · unknown · Nov 13, 2023 · N934AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > OUT OF LIMITS CUSP MEMBRANE WEB STA 944, X=58 AND STA 948, X=50 AT CABIN PAX. SUMMARY OF NRC 00564: CORROSION LEVEL 2. CUSP MEMBRANE WEB STA 944, X=58 AND STA 948, X=50 WERE REPAIRED PER B717 SRM 53-00-55-2R-4 FIG 215. (LP #0062291)
- [SDR DALA2023111309307](https://openairdocs.org/sdr/DALA2023111309307.md): Unknown · unknown · Nov 13, 2023 · N934AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON LH CUSP MEMBRANE WEB BTW STA 655 TO STA 674 AT PAX CABIN. SUMMARY OF NRC 00327: LH CUSP MEMBRANE WEB BTW STA 655 TO STA 674 WAS REPAIRED PER B717 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4. (LP #0062288)
- [SDR DALA2023111309304](https://openairdocs.org/sdr/DALA2023111309304.md): Unknown · unknown · Nov 10, 2023 · N934AT · Boeing 717200 · Fuselage Main, Structure
  > CRACK ON PAN BTW BEAM 1-3 STA 160 AT FWD PASS DOOR. SUMMARY OF NRC 00050: PAN WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 3 REPAIR 3. (LP #0059117)
- [SDR DALA2023111309302](https://openairdocs.org/sdr/DALA2023111309302.md): Unknown · unknown · Nov 10, 2023 · N934AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON WEB BTW STA Y=190 TO 180 X=55 APROX AT CABIN PAX. SUMMARY OF NRC 00574: WEB BTW STA Y=190 TO 180 X=55 APROX WAS REPAIRED PER B717 SRM 51-70-10-2R REPAIR 2 PAR 4 AND FIGURE 201. (LP #0058091)
- [SDR DALA2023111309301](https://openairdocs.org/sdr/DALA2023111309301.md): Unknown · unknown · Nov 10, 2023 · N934AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION LH CUSP MEMBRANE WEB BTW STA Y=562 TO Y=579 IS OUT OF LIMITS. SUMMARY OF NRC 00570: CORROSION LEVEL 2. MEMBRANE WEB BTW STA Y=562 TO Y=579 WAS REPAIRED PER B717 SRM 53-00-55-2R-4, PAR 5, FIGURE 216. (LP #0058082)
- [SDR DALA2023110909224](https://openairdocs.org/sdr/DALA2023110909224.md): Unknown · unknown · Nov 8, 2023 · N934AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON CUSP WEBS RH STA Y=1026 TO Y=1030. SUMMARY OF NRC 00490: CORROSION LEVEL 2. CUSP WEB RH STA Y=1026 TO Y=1030 WAS REPLACED PER B717 SRM 51-41-02-0G & 51-41-01-0G. (LP #0055282)
- [SDR DALA2023110809200](https://openairdocs.org/sdr/DALA2023110809200.md): Unknown · unknown · Nov 7, 2023 · N934AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK ON FRAME BTW STA Y=1037 AND LONG 17L AT AFT PAX CABIN. SUMMARY OF NRC 00269: FRAME BTW STA Y=1037 AND LONG 17L AT AFT PAX CABIN WAS REPAIRED PER B717 SRM 53-20-07-2R PROCEDURE 4 REPAIR 4. (LP #0054020)
- [SDR DALA2023110709162](https://openairdocs.org/sdr/DALA2023110709162.md): Unknown · unknown · Nov 7, 2023 · N934AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > BROKEN UPPER SURFACE JAMB BTW STA Y=170-200 APPROX AT PASSENGER DOOR (L1). SUMMARY OF NRC 00383: UPPER SURFACE JAMB BTW STA Y=170-200 APPROX AT PASSENGER DOOR WAS REPAIRED PER B717 SRM 53-00-00-2R-1. (LP #0053120)
- [SDR DALA2023040502674](https://openairdocs.org/sdr/DALA2023040502674.md): Unknown · unknown · Mar 31, 2023 · N934AT · Boeing 717200 · Fuselage Main, Frame
  > AFT CARGO DOOR FRAME STRUCK BY BELT LOADER IN MSP. REMOVED DAMAGE DOUBLER, DAMAGE CONTAINED. ACCOMPLISHED HFEC INSPECTION OF CUT-OUT IAW NDT SPM 06-10-01.01. NO CRACKS NOTED. REMOVED DAMAGE SEAL DEPRESSOR. DAMAGE CONTAINED. REPAIRED SKIN PER B717 SRM 53-20-15
- [SDR DALA2022121308026](https://openairdocs.org/sdr/DALA2022121308026.md): Light · inoperative · Dec 12, 2022 · N934AT · Boeing 717200 · Emergency Lighting
  > THE OVER WING EMERGENCY EXIT LIGHTS IN THE CABIN WERE FOUND TO BE INOPERATIVE (FWD LIGHTS). MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK AND THE EMERGENCY BATTERY POWER SUPPLY UNIT PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD PER B717 AMM 33-51. (LP
- [SDR DALA2021112307180](https://openairdocs.org/sdr/DALA2021112307180.md): None · none · Nov 22, 2021 · N934AT · Boeing 717200 · Emergency Lighting
  > THE FLIGHT ATTENDANT REPORTED THAT THE EMERGENCY EXIT SIGN COVER IS MISSING AT DOOR 1R. MAINTENANCE INSTALLED EXIT SIGN COVER. OPERATIONAL CHECK WAS GOOD. (LP #2026799)
- [SDR DALA2021102606607](https://openairdocs.org/sdr/DALA2021102606607.md): None · none · Oct 18, 2021 · N934AT · Boeing 717200 · Fuselage Floor Panel
  > FLOOR SUPPORT AT RBL 12 AND STA 160 TO STA 200 HAS AREAS OF LIGHT CORROSION. SUMMARY SEE NRC 061-0023:5310-2005/006 00477: REMOVED CORROSION ON SUPPORT AND FOUND IT TO BE OUT OF LIMITS. REMOVED, FABRICATED, AND INSTALLED A NEW SUPPORT PER B717 SRM 53-00 -00-1A

Next page: https://openairdocs.org/aircraft/N934AT/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 = 'N934AT' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N934AT/reports

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OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.