N993AT

Service difficulty reports · 210

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 = 'N993AT' 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 DALA2026090805037Slat · damagedDAMAGE TO LEFT WING SLAT DUE TO BIRD STRIKE. PERFORMED A BIRD STRIKE INSP PER B717 AMM 05-62 FOUND NO OTHER DAMAGE. REPLACED #3 WING SLAT IAW AMDS JOB CARD 2780-4000-LH-3. A/C OK FOR SERVICE. (9189256) AIRCRAFT WAS GROUNDED.Sep 7, 2026 · N993AT · Boeing 717200 · Leading Edge DevicesSDR DALA2026060903438Wing · no discrepancyACFT DUE LT AND RT WING INSPECTIONS AD 2024-21-01. C/W WORKCARDS 5720-01103-01A, AND 5720-01103-01B, FCN'S 95-0557- 8-0032, AND 95-0557-8-0035. OK FOR SVC. (8357674) (AIRCRAFT GROUNDED)Jun 2, 2026 · N993AT · Boeing 717200 · Wing StructureSDR DALA2026060203339Skin · crackedCRACKS ON FUSELAGE OUTER SKIN, BS 1095 BTW LONGERON 3R AND 4R & BS 1095 BTW LONGERON 2R AND 3R. REPAIRED IAW PRI 634353-14 (1621163) (AIRCRAFT GROUNDED)May 30, 2026 · N993AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2026052903260Skin · crackedCRACK ON EXTERNAL FUSELAGE SKIN STA Y=1037 BTW. REPAIRED PER ER/A NO. 634335-14 (1618251) (AIRCRAFT GROUNDED)May 28, 2026 · N993AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2026052903258Skin · crackedCRACK ON EXTERNAL FUSELAGE SKIN STA Y= 1022 BTW. REPAIRED PER ER/A 634381 (1616802) (AIRCRAFT GROUNDED)May 28, 2026 · N993AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2026052903257Skin · crackedCRACK ON EXTERNAL FUSELAGE SKIN STA Y= 1022 BTW LONG 13RH & 14RH. REPAIRED IAW PRI 634340 (1616686) (AIRCRAFT GROUNDED)May 28, 2026 · N993AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2026060203342Skin · damagedERA 634353-14 ISSUED FOR REPAIR TO FUSELAGE SKIN AT STA 1152, L2 TO L4. ACCOMPLISH ERA 634353-14 (1616414) (AIRCRAFT GROUNDED)May 26, 2026 · N993AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2026052903255Door Frame · corrodedCORROSION AROUND LOWER DOOR JAMB AT AFT CARGO COMPARTMENT. REPAIRED IAW SRM 51-41-02-0G AND SRM 51-41-05-0G AND PER B717-200 SRM 53-20-15. (1614443) (AIRCRAFT GROUNDED)May 26, 2026 · N993AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2026052903253Skin · crackedCRACK ON EXTERNAL FUSELAGE SKIN STA Y=1076 BTW LONG 13LH & 14LH. REPAIR AND PRI 634388-14 (1613658) (AIRCRAFT GROUNDED)May 26, 2026 · N993AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2026052903252Skin · crackedCRACK ON EXTERNAL FUSELAGE SKIN STA Y= 1087 BTW LONG 13RH & 14RH. REPAIRED PER ER/A NO. 634338-14 (1612208) (AIRCRAFT GROUNDED)May 25, 2026 · N993AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2026052803221Cusp Web · crackedIAW TASK 310-01436-01 STEP 5 AFTER REMOVAL CUSP MEMBRENE CRACK WAS FOUND AT CUSP WEB. FUSELAGE STA 674 LH SIDE. CORRECTIVE ACTION: REPAIRED PER B717-200 SRM 53-00-55 (1606106) (AIRCRAFT GROUNDED)May 22, 2026 · N993AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2026052903261Skin · crackedCRACK AND WEAR EXTERNAL SKIN ON AFT CARGO DOOR CUTOUT AFT EDGE BTW LONG 24RH TO LONG 26RH AT LOWER FUSELAGE SECTION. REPAIRED PER B717-200 SRM 53-20-15 (1605105) (AIRCRAFT GROUNDED)May 21, 2026 · N993AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2025120808961Unknown · odorFWD FAS SAYS THAT GOT A GOOD WIFT OF THE DIRTY SOCK SMELL ON CLIMB OUT. NO OTHER COMPLAINTS ON ACFT. FUME WAS SHORT TERM MAYBE A MINUTE OR TWO. TROUBLESHOT ODOR SMELL PER NO GO ODI PREVENTION REF TO LOG 1327715 FOR CORRECTIVE ACTION (7952142)Nov 30, 2025 · N993AT · Boeing 717200 · Air Distribution SystemSDR DALA2025120508917Pin · brokenATO- APPROX 80KTS DUE TO PREDICTIVE WINDSHEAR WARNING. FOUND COAXIAL CABLE PIN BROKEN. REPLACED SAME. OPS NORMAL.(7952152)Nov 30, 2025 · N993AT · Boeing 717200 · Navigation System WiringSDR DALA2025091606813Lanyard · unsecureDOOR 1R EMERGENCY SLIDE ARMING BAR DETACHED AND BROKEN. MEM DELTA MX NOTIFIED. REINSTALLED GIRT BAR LANYARD ON 1R EMERGENCY SLIDE IAW AMM 25-61 (7587364)Sep 6, 2025 · N993AT · Boeing 717200 · Emergency EquipmentSDR DALA2025030601744Battery Pack · no testTHE EMERGENCY LIGHT SERVICE CHECK FOUND THE LIGHTED SIGNS ABOVE THE AFT OVERWING EXITS ON LEFT & RIGHT SIDES TO BE INOPERATIVE. MAINTENANCE TROUBLESHOT IN REF WITH B717 WDM 33-51-11 PG 4 SHEET 3 OF 3, DELTA AVIONICS JOB AIDS TO EMERGENCY LIGHT BATTERY PACK B5-Mar 5, 2025 · N993AT · Boeing 717200 · Emergency LightingSDR DALA2025021801200Oven · contaminatedSHIP 9538 -DIV/SMK/DE- THE FLIGHT CREW NOTED SMOKE IN COCKPIT WHILE ENROUTE TO MCI. AN EMERGENCY WAS DECLARED, AND THE AIRCRAFT WAS DIVERTED TO A NORMAL SAFE LANDING IN ORD. CORRECTIVE ACTION: MAINTENANCE INSPECTED THE GALLEY OVEN CONNECTOR, AND NO TROUBLE WASFeb 13, 2025 · N993AT · Boeing 717200 · Buffet/GalleysSDR DALA2024121811803Union · leakingSHIP 9538 -MISC/DE- THE FLIGHT CREW DECLARED AN EMERGENCY WITH ATC FOLLOWING THE RIGHT HYDRAULIC SYSTEM SHOWING A LOSS IN QUANTITY. THE QRH WAS COMPLIED WITH, BUT AN ALTERNATE GEAR EXTENSION WAS NOT REQUIRED. CORRECTIVE ACTION: MAINTENANCE CYCLED THE MLG DOORSDec 18, 2024 · N993AT · Boeing 717200 · Hydraulic System, MainSDR DALA2024120911541Battery Pack · inoperativeDURING THE SERVICE CHECK THE FWD OVERWING EMERGENCY EXIT UPPER DOOR LIGHTS ON BOTH LT & RT SIDE WERE FOUND NOT ILLUMINATED. MAINTENANCE REPLACED THE B5-121 BATTERY PACK PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. OK FOR SERVICE. (LP #6930904)Dec 8, 2024 · N993AT · Boeing 717200 · Emergency LightingSDR DALA2024120911531None · none-AD- ACCOMPLISH ER/A 622306-14AD SECTION I B717 FUSELAGE STA 1178.558 ALTERNATIVE INSPECTION FOR PREVIOUS REPAIR. ACCOMPLISH ER/A 622306-14AD SECTION I FOR THE INSPECTION OF THE REAR CANTED BULKHEAD REPAIR. THIS IS AD RELATED. INSPECTIONS CANNOT BE PUSHED PASTNov 12, 2024 · N993AT · Boeing 717200 · Standard Practices/StructuresSDR DALA2024062706579Hpc · damagedSHIP 9538 -ATO- ABORTED TAKEOFF AT APPROXIMATELY 80 KNOTS DUE TO SUSPECTED RIGHT ENGINE SUSPECTED COMPRESSOR STALL. CORRECTIVE ACTION: PERFORMED BORESCOPE INSPECTION AND FOUND DAMAGE TO 3RD AND 4TH STAGE HPC. REPLACED RIGHT ENGINE. (LP 5271438)Jun 25, 2024 · N993AT · Boeing 717200 · Turbine Engine Compressor SectionSDR DALA2024052105381Power Supply · inoperativeTHE AFT ACCESORY COMPARTMENT EMERGENCY LIGHTS ARE INOPERATIVE. THE EMERGENCY LIGHT BATTERY POWER SUPPLY WAS REPLACED PER B717 AMM 33-51-03. OPERATIONAL TESTS ARE GOOD. THE AIRCRAFT HAS RETURNED TO SERVICE. (LP #5731034)May 20, 2024 · N993AT · Boeing 717200 · Emergency LightingSDR DALA2024052105376Release Cable · misroutedIMPROPER ROUTING OF MANUAL RELEASE CABLE FOR SLIDE AT FORWARD SERVICE DOOR. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY OF NRC 00695: MANUAL INFLATION CABLE FOR SLIDE AT FORWARD SERVIMay 19, 2024 · N993AT · Boeing 717200 · Escape SlideSDR DALA2024052005345Pan · crackedCRACK ON PAN LOWER EDGE INTERNAL STRUCTURE BTW STA 403 TO 413 FWD CARGO DOOR. SUMMARY OF NRC 00212: INNER AND OUTER PAN ON LOWER EDGE INTERNAL STRUCTURE BTW STA 403 TO 413 AT FWD CARGO COMPARTMENT DOOR WERE REPAIRED PER ER/A 617729-14 REV ORIGINAL SECTION I: PMay 18, 2024 · N993AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024052005342Slide · damagedDURING FWD PASSENGER SLIDE DOOR COVER INSTALLATION, THE SLIDE PACKAGE WAS FOUND UNSAFE. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY OF NRC SERIAL 00682: FORWARD ENTRY PASSENGER DOOR SMay 17, 2024 · N993AT · Boeing 717200 · Escape SlideSDR DALA2024052005340Slide · damagedDURING FWD PASSENGER SLIDE DOOR COVER INSTALLATION, THE SLIDE PACKAGE WAS FOUND UNSAFE. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY OF NRC 682: FORWARD ENTRY PASSENGER DOOR SLIDE ASSYMay 17, 2024 · N993AT · Boeing 717200 · Escape SlideSDR DALA2024051705296Strap · corrodedCORROSION ON WEB STRAP BTW STA Y=200/208 AND LONGERON 18L. (PAX CAB). SUMMARY OF NRC 00409: CORROSION LEVEL 2. WEB STRAP BTW STA Y=200/208 AND LONGERON 18L WAS REPAIRED PER ER/A 617656-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 617656-14 REV 0. ASSOCIMay 16, 2024 · N993AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024051705294Hinge · excess playFREEPLAY ON JOINT BTW FLAP AND FLAP OUTBD HINGE AT LH WING. LT WING FLAP OUTBD HINGE WAS REPAIRED IN ACCORDANCE WITH PRI 617504-14 REV 2 AND ER/A 617504-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. REPAIR APPROVAL IS LIMITED TO 24 MONTHS FROM 09MAY24. ADDITIMay 16, 2024 · N993AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2024051605253Structure · corrodedCORROSION WAS FOUND ON HSTB HOLE #27 RH. SUMMARY OF NRC 00650: RH HORIZONTAL STABILIZER BARREL NUT HOLE #27 WAS REPAIRED IN ACCORDANCE WITH ER/A 617762-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. TIME CONTROLLED ITEMS: REPAIR APPROVAL IS LIMITED TO 24 MONTHS May 16, 2024 · N993AT · Boeing 717200 · Horizontal Stabilizer Miscellaneous StructureSDR DALA2024051505224Intercostal · crackedCRACK ON INTERCOSTAL BTW STA Y=636 AND X=0 AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00679: CRACK ON INTERCOSTAL BTW STA Y=636 AND X=0 AT FWD CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-00-00-2R PROCEDURE 1 REPAIR 1. (LP #0343135)May 15, 2024 · N993AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024051505223Vane · dentedDENTS ON AFT MOVEABLE VANE LOWER SKIN AT RIGHT WING. SUMMARY OF NRC 00238: AFT MOVEABLE VANE LOWER SKIN AT RIGHT WING WAS REPAIRED PER ER/A 617597-14 REV ORIGINAL. ASSOCIATED ER/A 14-617597 ADDED FOR AC 9538. (LP #0342649)May 14, 2024 · N993AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2024051505221Doubler · corrodedCORROSION ON INTERNAL DOUBLER BTW STA Y 617-636 AND LONG L27L TO L28L AT FWD CARGO COMPARTEMENT. SUMMARY OF NRC 00631: CORROSION LEVEL 2. CORROSION ON INTERNAL DOUBLER BTW STA Y 617-636 AND LONG L27L TO L28L AT FWD CARGO COMPARTMENT WAS REPAIRED PER ER/A 61763May 14, 2024 · N993AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2024051405175Support Angle · crackedCRACKS (2 EA) ON ANGLE STRUCTURE SUPPORT BULKHEAD BTW LONGERON 5L AND 6L ALSO 7L STA=Y 1022 AT AFT LAVATORY ENGINE PYLON AREA. SUMMARY OF NRC 00400: CRACK ON ANGLE STRUCTURE SUPPORT BULKHEAD BTW LONGERON 7L STA=Y 1022 AT AFT LAVATORY ENGINE PYLON AREA WAS REPAMay 13, 2024 · N993AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024051405172Scuff Plate · crackedCRACK ON AFT SCUFF PLATE AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 0002: SCUFF PLATE AT AFT CARGO COMPARTMENT WAS REPAIRED PER ER/A 542149-14TR REV B, SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-542149 ADDED FOR AC 9538. (LP #0339236)May 12, 2024 · N993AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024051405171Pan · crackedCRACKS ON PAN FWD EDGE AND AFT EDGE BETWEEN BEAM #2 AND #3 AT AFT CARGO DOOR. SUMMARY OF NRC 00366: AFT CARGO DOOR ASSY WAS REMOVED PER AMDS 5231-4002, WAS REPLACED WITH SERVICEABLE AFT CARGO DOOR ASSY, AND WILL BE INSTALLED WITH AMDS 5231-4004. (LP #0336365)May 10, 2024 · N993AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024051305131Frame · corrodedCORROSION ON PREVIOUS REPAIR DOUBLER ON FRAME Y=870 BTW LONGERONS 29L AND 29R AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00299: CORROSION LEVEL 2. PREVIOUS REPAIR DOUBLER ON FRAME Y=870 BTW LONGERONS 29L AND 29R AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200May 9, 2024 · N993AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2024050905041Angle · corrodedCORROSION ON CUSP ANGLE AT FORWARD GALLEY SERVICE DOOR JAMB STA Y=157-200. SUMMARY OF NRC 00345: CORROSION LEVEL 2. CUSP ANGLE AT FORWARD GALLEY SERVICE DOOR JAMB STA Y=157-200 WAS REPAIRED PER PRI 617406-14 REV 2 AND ER/A 617406-14 REV ORIGINAL, SECTION I: PEMay 8, 2024 · N993AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024050805022Floor Support · corrodedCORROSION ON FLOOR SUPPORT BTW STA Y 157 TO 200 AND X=-43 AT PAX CABIN. SUMMARY OF NRC 00407: CORROSION LEVEL 2. FLOOR SUPPORT BTW STA Y 157 TO 200 AND X=-43 AT PAX CABIN WAS REPLACED AND INSTALLED PER DWG S2929169 REV WB AND B717 SRM 51-41-02-0G AND 51-41-05-May 7, 2024 · N993AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024050704974Floorbeam · corrodedCORROSION ON FLOOR SUPPORT STA 180 FROM X=-7 TO X=-44 AT PAX CABIN. SUMMARY OF NRC 00415: CORROSION LEVEL 2. FLOOR SUPPORT STA 180 FROM X=-7 TO X=-44 AT PAX CABIN WAS REPLACED AND INSTALLED PER DWG S2929169 REV B AND B717 SRM 51-41-02-0G AND 51-41-05-0G. (LP #May 7, 2024 · N993AT · Boeing 717200 · Fuselage Main, Floor BeamSDR DALA2024050604954Frame · crackedCRACK ON FRAME STA=Y 1178 APPROX BTW LONGERON 1L AND 2L AT AFT ACCESORY COMPARTMENT AREA. SUMMARY OF NRC 00401: FRAME STA=Y 1178 APPROX BTW LONGERON 1L AND 2L AT AFT ACCESORY COMPARTMENT AREA WAS REPAIRED PER B717 SRM 53-30-08-2R. PERFORM A VISUAL INSPECTION EMay 3, 2024 · N993AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2024050304920Skin · crackedCRACK INTERNAL FUSELAGE SKIN JUST AFT UPPER CORNER AT RH SLIDING WINDOW AREA. CPIL. SUMMARY OF NRC 00524: FUSELAGE SKIN JUST AFT UPPER CORNER AT RH SLIDING WINDOW AREA WAS REPAIRED PER PRI 617480-14 REV 1 AND ERA 617480-14 REV ORIGINAL SECTION I: PERMANENT REPMay 2, 2024 · N993AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2024050204890Bulkhead Web · crackedCRACKED BULKHEAD WEB STA Y=218, X=-8 AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00647: BULKHEAD WEB STA Y=218, X=-8 AT FWD CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 2. (LP #0321848)May 1, 2024 · N993AT · Boeing 717200 · Fuselage Main, BulkheadSDR DALA2024050204887Cusp Web · corrodedCORROSION ON RH CUSP WEB UPPER AND LOWER BTW STA 217-237 AT PAX CAB. SUMMARY OF NRC 00346: CORROSION LEVEL 2. RH CUSP WEB UPPER AND LOWER BTW STA 217-237 AT PAX CAB WAS FABRICATED PER B717-200 SRM 53-00-55-2R-4 REPAIR 4 FIG 209. REPLACED PER B717-200 SRM 53-00Apr 30, 2024 · N993AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024043004795Cusp Web · corrodedCORROSION ON LH CUSP WEB ALSO WITH OIL SCAN ON THE SAME CUSP WEB BTW STA 889 TO STA 908 X=58 AT PAX CABIN. SUMMARY OF NRC 00396: CORROSION LEVEL 2. LH CUSP WEB ALSO WITH OIL SCAN ON THE SAME CUSP WEB BTW STA 889 TO STA 908 X=58 AT PAX CABIN WAS REPLACED PER B7Apr 27, 2024 · N993AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024043004792Skin · damagedELONGATED HOLE ON VERTICAL STABILIZER LEADING EDGE LEFT SIDE, JUST ON THE CORNER WAS FOUND STA ZFS=52.267 IN REF NRC 0525. SUMMARY OF NRC 00611: HOLE ON VERTICAL STABILIZER LEADING EDGE LEFT SIDE, JUST ON THE CORNER WAS REPAIRED PER B717-200 SRM 55-30-01-2R PRApr 27, 2024 · N993AT · Boeing 717200 · Vertical Stabilizer, Plate/SkinSDR DALA2024042304669Cusp Web · crackedCRACK LH CUSP WEB STA 657 TO 663 X=55 AT PAX CABIN. SUMMARY OF NRC 00394: CRACK LH CUSP WEB STA 657 TO 663 X=55 AT PAX CABIN WAS REPAIRED PER B717 SRM-53-00-55-2R-4. (LP #0307832)Apr 23, 2024 · N993AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024042304665Longeron · crackedCRACKS ON LONGERON (3 EA) 5L, 5R, AND 17L STA=Y 1022 AT AFT LAVATORY ENGINE PYLON SUPPORT BULKHEAD AREA. SUMMARY OF NRC 0245: LONGERON (2 EA) 5L & 5R AT AFT LAVATORY ENGINE PYLON SUPPORT BULKHEAD AREA WERE REPAIRED PER B-717-200 SRM 53-00-05-2R REPAIR 2 AND LOApr 22, 2024 · N993AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2024041904571Membrane · corrodedCORROSION ON LEFT MEMBRANE STA 200 TO 207 X=54 AT PAX CABIN IN REFERENCE NRC 00391. SUMMARY OF NRC 00591: CORROSION LEVEL 2. LEFT MEMBRANE STA 200 TO 207 X=54 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 2 REPAIR 2. (LP #0301180)Apr 19, 2024 · N993AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024041904567Cusp Web · crackedCRACK LH CUSP WEB STA 606 X=59 AT PAX CABIN PAX. SUMMARY OF NRC 00393: CRACK LH CUSP WEB STA 606 X=59 AT PAX CABIN, WAS REPAIRED PER B717 SRM-53-00-55-2R-4. (LP #0300915)Apr 18, 2024 · N993AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024041504424Bulkhead Web · crackedCRACKED BULKHEAD WEB SYA Y=218, X=-8 AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00283: BULKHEAD WEB STA Y=218, X=-8 AT FWD CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 2. (LP #0290830)Apr 12, 2024 · N993AT · Boeing 717200 · Fuselage Main, Bulkhead
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