N934AT

Service difficulty reports · 204

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR DALA2026071304091Transceiver · faultyATB- 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)Jul 10, 2026 · N934AT · Boeing 717200 · Ground Proximity SystemSDR DALA2026070103877Coalescer Bag · odorBURNING SMELL WITH APU ON AND PACKS, R & R COALESCER BAGS PER B717 AMM 21-54-08. (6688572) (AIRCRAFT GROUNDED).Jul 1, 2026 · N934AT · Boeing 717200 · Humidity Control SystemSDR DALA2026042902730Hinge Fitting · damagedSHIP 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)Apr 24, 2026 · N934AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2026041402347Not Reported · not reportedREFERENCE ER/A626909-14AD. COMPLIED WITH ER/A626909-14AD (1533159) (AIRCRAFT GROUNDED)Apr 7, 2026 · N934AT · Boeing 717200 · Standard Practices/StructuresSDR DALA2025092306961Strap · damagedCOMPLY 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)Sep 22, 2025 · N934AT · Boeing 717200 · Wing Miscellaneous StructureSDR DALA2025090406564Spar Cap · crackedLEFT WING REAR SPAR, LOWER CAP, AFT FLANGE CRACKED NEAR XRS = 164. REPAIRED PER ER/A 00-626909. (1156447)Aug 21, 2025 · N934AT · Boeing 717200 · Wing SparSDR DALA2025062604793Girt Bar · detachedSHIP 9565 GIRT BAR DETACHED FROM 1R DOOR. CORRECTIVE ACTION: RE ATTACHED LANYARD ASSY. IAW 717 AMM 25-61 (6588676)Jun 25, 2025 · N934AT · Boeing 717200 · Emergency EquipmentSDR DALA2025061504506Spar Cap · crackedAIRCRAFT 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. CORRECTIVEJun 13, 2025 · N934AT · Boeing 717200 · Wing SparSDR DALA2025060604344Spar Cap · crackedSHIP 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 CENTERMay 29, 2025 · N934AT · Boeing 717200 · Wing SparSDR DALA2025012800656Battery Pack · inoperativeTHE 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)Jan 23, 2025 · N934AT · Boeing 717200 · Emergency LightingSDR DALA2024022702692Control Valve · malfunctionedSHIP 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 EXTENSIOFeb 24, 2024 · N934AT · Boeing 717200 · Leading Edge Slat Control SystemSDR DALA2023120609979Unknown · unknownELONGATED 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: PERDec 5, 2023 · N934AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2023120409900Unknown · unknownWEAR 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)Dec 2, 2023 · N934AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2024022002333Skin · corrodedCORROSION 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 SECTIONDec 1, 2023 · N934AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2023113009839Unknown · unknownINAPPROPRIATE 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. BEAMNov 29, 2023 · N934AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2023113009838Unknown · unknownCRACK 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 613338-14Nov 29, 2023 · N934AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2023113009837Unknown · unknownCRACK 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 Nov 29, 2023 · N934AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2023113009836Unknown · unknownCORROSION 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)Nov 29, 2023 · N934AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2023112909802Unknown · unknownCORROSION 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 ORIGINALNov 29, 2023 · N934AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2023112909801Unknown · unknownWEAR 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 HINov 29, 2023 · N934AT · Boeing 717200 · Fuselage, Door HingeSDR DALA2023112809762Unknown · unknownCORROSION 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)Nov 28, 2023 · N934AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2023112809756Unknown · unknownDENT 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) ANNov 27, 2023 · N934AT · Boeing 717200 · Rudder, Tab StructureSDR DALA2023112709719Unknown · unknownAFTER 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 ADDNov 22, 2023 · N934AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2023112709716Unknown · unknownCORROSION 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 TRACKNov 22, 2023 · N934AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2023112109570Unknown · unknownCUSP 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)Nov 19, 2023 · N934AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023112209653Unknown · unknownCRACK 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 ANDNov 18, 2023 · N934AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023112009526Unknown · unknownCRACK 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)Nov 18, 2023 · N934AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023112009523Unknown · unknownCRACK 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)Nov 18, 2023 · N934AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023112009522Unknown · unknownWEAR 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)Nov 17, 2023 · N934AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2023112009521Unknown · unknownCRACK 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)Nov 17, 2023 · N934AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023112009519Unknown · unknownCORROSION 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)Nov 17, 2023 · N934AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023112009516Unknown · unknownCORROSION 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 2Nov 16, 2023 · N934AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023112009515Unknown · unknownCORROSION 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=200Nov 16, 2023 · N934AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2023111609441Unknown · unknownCORROSION 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)Nov 16, 2023 · N934AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2023111509408Unknown · unknownCORROSION 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)Nov 15, 2023 · N934AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023111509406Unknown · unknownCORROSION 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)Nov 14, 2023 · N934AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023111509405Unknown · unknownCORROSION 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= 1Nov 14, 2023 · N934AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023111409353Unknown · unknownCRACK 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)Nov 14, 2023 · N934AT · Boeing 717200 · Fuselage Main, Floor BeamSDR DALA2023111309308Unknown · unknownOUT 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)Nov 13, 2023 · N934AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023111309307Unknown · unknownCRACK 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)Nov 13, 2023 · N934AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023111309304Unknown · unknownCRACK 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)Nov 10, 2023 · N934AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2023111309302Unknown · unknownCRACK 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)Nov 10, 2023 · N934AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023111309301Unknown · unknownCORROSION 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)Nov 10, 2023 · N934AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023110909224Unknown · unknownCORROSION 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)Nov 8, 2023 · N934AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023110809200Unknown · unknownCRACK 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)Nov 7, 2023 · N934AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023110709162Unknown · unknownBROKEN 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)Nov 7, 2023 · N934AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023040502674Unknown · unknownAFT 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 Mar 31, 2023 · N934AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2022121308026Light · inoperativeTHE 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. (LPDec 12, 2022 · N934AT · Boeing 717200 · Emergency LightingSDR DALA2021112307180None · noneTHE 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)Nov 22, 2021 · N934AT · Boeing 717200 · Emergency LightingSDR DALA2021102606607None · noneFLOOR 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 -00-1AOct 18, 2021 · N934AT · Boeing 717200 · Fuselage Floor Panel
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