N950AT

Service difficulty reports · 215

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 = 'N950AT' 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 DALA2026090204949Threshold · damagedAFT CARGO THRESHOLD FWD INBD CORNER STICKING UP AND DAMAGED, COMPLIED WITH ERA 636705-14. (9622032) (AIRCRAFT GROUNDED).Sep 2, 2026 · N950AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2026080604547Skin · dentedDENT FOUND ON THE FUSELAGE BTWN BS 218 - 229, COMPLIED WITH ER/A 636117-14. (1734913) (AIRCRAFT GROUNDED).Aug 2, 2026 · N950AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2026072204285Battery Pack · inoperativeOVERHEAD EXIT EMERGENCY LIGHT SIGN AND EMERGENCY LIGHT IN FWD GALLEY INOPERATIVE, R & R EMERGENCY BATTERY B5-259 IAW AMM 33- 51. (9127379) (AIRCRAFT GROUNDED).Jul 21, 2026 · N950AT · Boeing 717200 · Emergency LightingSDR DALA2026072004263Relay · faultedDIVERTED TO CVG DUE TO MULTIPLE FLIGHT DECK EFFECTS AFTER TAKEOFF. REPLACED LT PCDU, EMERGENCY POWER SWITCH AND EMERGENCY DC POWER RELAY. PERFORMED VERIFICATION FLIGHT. ALL OPS GOOD. (9127356) AIRCRAFT GROUNDED.Jul 18, 2026 · N950AT · Boeing 717200 · Integrated Flight SystemSDR DALA2026041702450Engine · fireFIRE- DURING RIGHT ENGINE START, TGT ROSE RAPIDLY ALONG WITH AUDIBLE STALL. ENGINE SHUTDOWN AND FIRE BOTTLE DISCHARGED. PERFORMED BORESCOPE INSPECTION OF LPC AND HPC, NO LIMITING DAMAGE FOUND. REPLACED NO.1 FIRE BOTTLE AND RETURNED TO SERVICE.(8685546) (AIRCRApr 14, 2026 · N950AT · Boeing 717200 · Engine (Turbine/Turboprop)SDR DALA2025120108775None · noneSHIP 9509 ER/A 623425-14AD REV C REQUIRES STAGE 2 DTA APRPOVAL. C/W ER/A 623425-14AD. (1321407)Nov 25, 2025 · N950AT · Boeing 717200 · Wing StructureSDR DALA2025070805067Pan · crackedSHIP 9509 INITIAL INSPECTION: CRACK ON FWD EDGE INNER AND OUTER PAN DOOR BTW BEAM 1 AT AFT CARGO DOOR COMPARMENT. CORRECTIVE ACTION: FWD EDGE INNER AND OUTER PAN DOOR BTW BEAM 1 AT AFT CARGO DOOR COMPARMENT WERE REPAIRED PER ERA 626981-14 REV. ORIGINAL, SECTIOJul 2, 2025 · N950AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2025062504749Frame Angle · corrodedCORROSION ON FRAME ANGLES BTW LONG 28L & 28R AT STA Y=927 AFT CARGO COMPARTMENT. CORROSION LEVEL 2. FRAME ANGLES BTW LONG 28L & 28R AT STA Y=927 AFT CARGO COMPARTMENT. WERE REPLACED PER DWG 9919605-15.Jun 24, 2025 · N950AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2025062504748Intercostal · corrodedCORROSION ON INTERCOSTALS BTW STA Y=1022 & Y =1037 AT LONG 30 & LONG 29R BILGE AREA AT AFT CARGO COMPARTMENT. DAMAGED AREA REPAIRED PER B717-200 SRM 51-41-05- 0G AND SRM 51-41-02 .Jun 24, 2025 · N950AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2025062504746Guide Vane · wornWEAR ON GUIDE VANE BEHIND HINGUE FLAP 1 AT RH WING. CORRECTIVE ACTION: GUIDE VANE WAS REPAIRED PER B717-200 SRM 57-53-01.Jun 23, 2025 · N950AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2025062104660Skin · dentedDENT OUT OF LIMITS, AT LOWER SURFACE ON LH AFT MOVABLE FLAP VANE AT STA XF74 APROX (2 INCHES FROM T.E. AND 12 INCH FROM L.E.): W=WIDTH, Y =DEPTH (NO MORE 0.060 INCH), RATIO W/Y= MUST BE 10 OR MORE, DENT #17: W=2.0 INCH, Y=0.090 INCH AND W/Y= 22.22 PER B717-200Jun 20, 2025 · N950AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2025062004658Skin · corrodedAIRCRAFT 9509, CORROSION AT LOWER SKIN DOOR JAMB ON MIDDLE DOORSTOP (AFT CARGO COMPARTMENT). CORRECTIVE ACTION: (CORROSION LEVEL 2) DOOR JAMB ON MIDDLE DOOR TOP (AFT CARGO COMPARTMENT) WAS REPLACED PER B717-200 SRM 51-41-02-0G, B717-200 SRM 51-41-05-0G AND B71Jun 20, 2025 · N950AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2025062004657Frame · crackedAIRCRAFT 9509, CRACK ON FRAME STA Y1037 AND L13L AT PAX CABIN. CORRECTIVE ACTION: CRACK ON FRAME STA Y1037 AND L13L AT PAX CABIN. WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 1. (LP 1034104)Jun 19, 2025 · N950AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2025062004656Frame · crackedAIRCRAFT 9509, CRACK ON FRAME STA Y1037 AND L13R AT PAX CABIN. CORRECTIVE ACTION: CRACK ON FRAME STA Y1037 AND L13R AT PAX CABIN. WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 1. (LP 1033875)Jun 19, 2025 · N950AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2025061904606Pan · crackedAIRCRAFT 9509, CRACK ON PAN NEAR TO BEAM NBR 2 AFT EDGE AT PASSENGER ENTRANCE DOOR. CORRECTIVE ACTION: PASSENGER ENTRANCE DOOR WAS REPAIRED PER B717-200 SRM 52-10-02-2R REPAIR 3. (LP 1032719)Jun 19, 2025 · N950AT · Boeing 717200 · Passenger/Crew DoorsSDR DALA2025061904605Door Frame · corrodedAIRCRAFT 9509, CORROSION WAS FOUND ON DOUBLERS REPAIR STA 954 AND 994 BTW S-26R TO S-27R AT LOWER SKIN DOOR JAMB ON AFT CARGO COMPARTMENT. CORRECTIVE ACTION: DOUBLERS REPAIR STA 954 AND 994 BTW S-26R TO S-27R AT LOWER SKIN DOOR JAMB ON AFT CARGO COMPARTMENT. WJun 18, 2025 · N950AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2025061904604Seat Track · corrodedAIRCRAFT 9509, CORROSION ON LH INB SEAT TRACK BTW STA 256 TO 200 AT CABIN PAX. CORRECTIVE ACTION: CORROSION LEVEL 2 // LH INB SEAT TRACK BTW STA 256 TO 200 AT CABIN PAX. WAS REPLACED PER B717-200 SRM 51-41-05-0G AND 51-41-01-0G. (LP 1029594)Jun 17, 2025 · N950AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2025061904603Seat Track · corrodedAIRCRAFT 9509, CORROSION ON INBD RH SEAT TRACK BTW STA 256 TO 200 AT CABIN PAX. CORRECTIVE ACTION: CORROSION LEVEL 2 // INBD RH SEAT TRACK BTW STA 256 TO 200 AT CABIN PAX WAS REPLACED PER B717-200 SRM 51-41-05-0G AND 51-41-01-0G. (LP 1029591)Jun 17, 2025 · N950AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2025061504505Longeron · crackedAIRCRAFT 9509, CRACK ON LONGERON 3(EAS) LONGERON 4, 5, AND 6 RH SIDE STA Y=1022 AT PASSENGER CABIN (CPAX). CORRECTIVE ACTION: LONGERON 3(EAS) LONGERON 4, 5, AND 6 RH SIDE STA Y=1022 AT PASSENGER CABIN (CPAX) WERE REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDUREJun 13, 2025 · N950AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2025060904376Pan · crackedAIRCRAFT 9509, AFTER SEAL RETAINERS REMOVAL, CRACK ON INNER PAN BTW STOP FITTING #1 AND #2 AFT EDGE, AT FWD CARGO DOOR WAS FOUND. CORRECTIVE ACTION: INNER PAN BTW STOP FITTING #1 AND #2 AFT EDGE, AT FWD CARGO DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R REPAJun 8, 2025 · N950AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2025060804360Cusp Web · corrodedAIRCRAFT 9509, CORROSION ON RH CUSP WEB UPPER & LOWER FACE ON STA Y=373 AT CABIN PAX. CORROSION LEVEL 2, CUSP WEB ON STA Y=373 AT CABIN PAX WAS REAPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 2 REPAIR 2. (LP1011516)Jun 7, 2025 · N950AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2025052704024Inspection · noneSHIP 9509 COMPLY WITH ERA 623616-14AD RH WING/ REAR SPAR/ LOWER CAP CRACK. CORRECTIVE ACTION: COMPLIED WITH ERA 623616-14AD (0978229)May 21, 2025 · N950AT · Boeing 717200 · Standard Practices/StructuresSDR DALA2025052704022None · noneSHIP 9509 INSTALL LH INBOARD AND CENTER BUTE DOORS. CORRECTIVE ACTION: C/W ER/A 623425-14AD (0972844)May 18, 2025 · N950AT · Boeing 717200 · Standard Practices/StructuresSDR DALA2025052704021Structure · wornSHIP 9509 LT WING OUTBD-AIRFRAME-HINGE BOLT HOLE IS WORN. CORRECTIVE ACTION: ALL WORK C/W ON ERA 625207 -14 REV ORG. (0973047)May 18, 2025 · N950AT · Boeing 717200 · Fuselage, Wing Attach FittingsSDR DALA2024123112105Spar · crackedCRACK AT LEFT WING REAR SPAR, PRI 623253-14 REV 0 ISSUED. REMOVE TANK PLATES 520FT, 520CB, AND TWO FUEL LINES FOR MAINTENANCE. REMOVED AND REINSTALLED L/H OVER WING BOOST PUMP PANEL TO F.O.M. PER B717 AMM 28-00. RE-INSTALLED TANK PLATE 520CB PER B717 AMM 28-00Dec 30, 2024 · N950AT · Boeing 717200 · Wing SparSDR DALA2024122712030Spar Cap · crackedCRACKS FOUND DURING INSPECTION OF LH WING REAR SPAR LOWER CAP RADIUS. CONTACT LIASON ENGINEERING FOR REPAIR PROCEDURES PRIOR TO FURTHER FLIGHT. FC 5720-01103 2ND FASTENER INBOARD OF FLAP HINGE FITTING EXTERIOR FROM TRAILING EDGE THROUGH FASTENER INTO RADIUS. MDec 23, 2024 · N950AT · Boeing 717200 · Wing SparSDR DALA2023081406584Unknown · unknownPUNCTURE IN FUSELAGE RT SIDE AFT OF FORWARD CARGO DOOR. THIS WAS ORIGINALLY DOCUMENTED IN LP #4849328 AND TRANSFERRED TO THIS LOG PAGE. MAINTENANCE REMOVED THE DAMAGE, DRILLED DOUBLER REF B717 53-03-01-2R PROCEDURE 1 REPAIR 1 CLASS 2 FIG 202 SHT 3, FABRICATED Aug 13, 2023 · N950AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2023070405377Unknown · unknownTHE CEILING EMERGENCY EXIT LIGHT COVER FELL OFF AT ROW 22. MAINTENANCE RESECURED THE LIGHTING COVER. THE AIRCRAFT IS NOW OK FOR SERVICE. (LP #8310082)Jul 3, 2023 · N950AT · Boeing 717200 · Emergency LightingSDR DALA2023022501422None · noneLT SLANT PANEL HAS CORROSION ON IT AT NUT PLATE LOCATION SEEN FROM THE INSIDE. BOTTOM ROW APPROX. LBL27. SUMMARY SEE NRC 001-0196:5300-2005/001 00276: COMPLIED WITH ER/A PRI 606032-14 REV "0","1" INSTRUCTIONAL STEPS. ENSURED FINAL ER/A 606032-14 REV ORIG SECTIFeb 23, 2023 · N950AT · Boeing 717200 · Fuselage Internal Mounting StructureSDR DALA2023021401131Unknown · unknownC/W ERA 597013-14 REV A FUSELAGE SKIN REPAIR AT LAV WASTE VENT. SUMMARY NRC 001-0002:2040-0015/001 00026: COMPLIED WITH ERA 597013-14 REV A FUSELAGE SKIN REPAIR AT LAV WASTE VENT. (LP #2621093)Feb 9, 2023 · N950AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2022051003229Door Sill · damagedFORWARD EDGE OF AFT CARGO DOOR FRAME SILL WAS DAMAGED BY BAGGAGE CREW WITH BELT LOADER. MAINTENANCE REMOVED DAMAGED SCUFF PLATE AND REFORMED PER B717 SRM 51-20-09-0G. INSPECTED SCUFF PLATE, NO CRACKS NOTED. COMPLIED WITH B717 SRM 53-00-15-2R. REINSTALLED SCUFFMay 6, 2022 · N950AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2022042903018None · noneSHIP 9509 - THE FLIGHT CREW DECLARED AN EMERGENCY DURING LANDING DUE TO THE RIGHT HYDRAULIC QUANTITY SHOWING A LOW INDICATION (BUT NOT EMPTY). CORRECTIVE ACTION: MAINTENANCE FOUND THAT THE #3 BRAKE PRESSURE LINE HAD BEEN DAMAGED BY A BIRD STRIKE AND WAS LEAKINApr 28, 2022 · N950AT · Boeing 717200 · Hydraulic System, MainSDR DALA2022021500951None · noneFUSELAGE CROWN LIGHTNING STRIKE DAMAGE AT PREVIOUS BLEND OUT. NO REPAIR TAG PRESENT. -M-. SUMMARY SEE NRC 001-0249:5300-2018/003 00365: REPAIRED LIGHTNING STRIKE DAMAGE ON CROWN PER ER/A 597099-14 PRI REV. 0 THROUGH REV 1. AND ER/A 597099-14AD REV. ORIGINAL. (Feb 12, 2022 · N950AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2022021500949None · noneCORROSION AROUND EXTERIOR SIDE OF VACUUM BLOWER FOR LAV TANK EXHAUST VENT -M-. SUMMARY SEE NRC 001-0247:2550-2003/001 00405: REPAIRED AREA AROUND VENT PER ER/A 597013-14 PRI REV 0 THROUGH REV 3 AND ER/A 597013-14 REV ORIGINAL. (LP #2118994)Feb 12, 2022 · N950AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2022021500945None · noneWHILE PERFORMING INSPECTION OF APU ENCLOSURE FWD SKIN ASSY. STA 1064 FOUND -2 REPAIR DOUBLER TO BE MISSING UPPER RH FASTENER PER ERA 540237-14 REV. O FIG. 2. SUMMARY SEE NRC 007-0001:21-0553-8- 7617/001 00320: REPAIRED PER ERA 540237-14 AND UPDATED LOG 2167684Feb 4, 2022 · N950AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2019020500805Fitting · corrodedCORROSION ON FLOOR FITTINGS G-7 (CPAX). CORROSION LEVEL 2, FLOOR FITTING OF G-7 WAS REPLACED PER ER/A 535099-14MA REV H AND CMM 25-30-16 REPAIR SECTION.Feb 4, 2019 · N950AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2019020400713Cargo Track · corrodedSEVERAL POINTS OF CORROSION ON LH TIE TRACK BTW STA 813 TO 1022 AT AFT CARGO COMPARTMENT (CCT). NRC 00271: CORROSION LEVEL 2, CORROSION ON TIE TRACK BTW STA 813 TO 1022 AT AFT CARGO COMPARTMENT WAS REMOVED PER B717-200 SRM 51-10-04-0G PAR 26. (UT) WAS ACCOMPLIFeb 3, 2019 · N950AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2019020400711Cargo Track · corrodedSEVERAL POINTS OF CORROSION ON RH TIE TRACK BTW STA 813 TO 954 AT AFT CARGO COMPARTMENT (CCT). NRC 00272: CORROSION LEVEL 2, ON RH TIE TRACK BTW STA 813 TO 954 AT AFT CARGO COMPARTMENT (CCT), TIE TRACK WAS REPLACED PER B717-200 SRM 51-40-08-0G AND B717-200 SRMFeb 3, 2019 · N950AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2019020430710Doubler · corrodedDURING INSPECTION OF A REPAIRED AREA AT FUSELAGE SKIN STA 851; L29L-29R, SOME CORROSION WAS FOUND. NRC 00225: REPAIR DOUBLER WAS REPLACED PER ER/A 540245-14 REV. ORIGINAL. ASSOCIATED ER/A 14-540245 ADDED FOR AC 9509. (LP #0929471)Feb 2, 2019 · N950AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2019020200708Access Panel · corrodedCORROSION ON LAVATORY SERVICE ACCESS INNER PANE AT FUSELAGE. (FUS). NRC 00059: LAVATORY SERVICE ACCESS INNER PANE AT FUSELAGE WAS REPLACED PER B717-200 SRM 51-41-02 AND 51-41-05. (LP #0928367)Feb 2, 2019 · N950AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2019020430706Skin · corrodedCORROSION WAS FOUND AT FUSELAGE SKIN STA 851; L29L-29R. NRC 00225: REPAIR DOUBLER WAS REPLACED PER ER/A 540245-14 REV. ORIGINAL. PERFORM ACOMPLISH ER/A 540245-14 REV. ORIGINAL SECTION I. ASSOCIATED ER/A 14-540245 ADDED FOR AC 9509. (LP #0929473)Feb 2, 2019 · N950AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2019013100635Floor Support · corrodedEXFOLIATION TYPE CORROSION ON FLOOR SUPPORT STA 655 BTW L28L TO L28R 5331-2007 (CCD). NRC 00291: CORROSION LEVEL 2, SUPPORT WAS REPLACED PER SRM 51-41-02-0G AND DWG #5971111 REV. F. (LP #0925601)Jan 30, 2019 · N950AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2019013000624Doubler · corrodedCORROSION ON PRODUCTION DOUBLER OF INNER SKIN FUSELAGE BTW STA Y=974 TO 954 AND L30 TO L29R AT AFT CARGO COMPARTMENT 5331-2001. NRC 00224: CORROSION LEVEL 2, PRODUCTION DOUBLER OF INNER SKIN FUSELAGE BTW STA Y=974 TO 954 AND L30 TO L29R WAS REPAIRED PER ETI-17Jan 29, 2019 · N950AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2019012901848Window Frame · crackedCRACK ON LT SLIDE WINDOW FRAME UPPER AFT CORNER STA 120. NRC 00500: LT SLIDE WINDOW STIFFENER (BRACKET) UPPER AFT CORNER STA 120 WAS REPLACED PER SRM 51-41-01-0G, 51-41-02-0G, AND 51-41-05-0G. DOUBLER WAS INSTALLED PER SRM 51-41-05-0G AND 56-10-02-2R. (ET) HFEJan 28, 2019 · N950AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2019030601500Skin · crackedTWO CRACKS ON FWD TOP SKIN AND ONE CRACK ON UPPER RIGHT EDGE AT FWD WALL OF APU COMPARTMENT IN REF NRC 00369. (CAT). NRC 00513: CRACKS (2) ON FWD TOP SKIN AND CRACK (1) ON UPPER RIGHT EDGE AT FWD WALL OF APU COMPARTMENT IN REF NRC 00369 WERE REPAIRED PER ETI-1Jan 28, 2019 · N950AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2019012900620Longeron · not reportedREMOVE LONGERON 25L BETWEEN STA 974/994 (IN REF NRC 00059) FOR SPLICE REPAIR PER SRM 53-00-05-2R-2. LONGERON 25L WAS REPAIRED PER SRM 53-00-05-2R-2. (LP #0922514)Jan 28, 2019 · N950AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2019012800571Bracket · crackedCRACK ON RT SLIDE WINDOW FRAME UPPER AFT CORNER STA 120. NRC 00499: RT SLIDE WINDOW STIFFENER (BRACKET) UPPER AFT CORNER STA 120 WAS REPLACED PER SRM 51-41-01-0G, 51-41-01-02-0G, AND 51-41-05-0G. (ET)(HFEC) WAS ACCOMPLISHED ON RT SLIDE WINDOW FRAME UPPER AFT CJan 27, 2019 · N950AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2019012800570Floor Panel · corrodedCORROSION ON FLOOR PANEL STA 120 (CPAX). NRC 00514: CORROSION LEVEL 2, FLOOR PANEL STA 120 WAS REPLACED PER DWG #9957828 REV: Y. (UT) ACCOMPLISHED PER NDT 04-00-07 PAR. 5 FIG. 3 SHEET 1 AND 2 ON FLOOR PANEL STA 120. ORIGINAL THICKNESS IS 0.100" AND MAXIMUM REMJan 27, 2019 · N950AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2019012800569Splice · corrodedCORROSION TYPE EXFOLIATION ON SPLICE STA Y=898.500 BTW L27R TO L26L AT AFT CARGO COMPARTMENT AMDS 5331-2001. (CCT). NRC 00165: CORROSION LEVEL 2. SPLICE STA Y=898.500 BTW L27R TO L26L WAS REPLACED PER SRM 51-41-05. (UT) WAS ACCOMPLISHED PER NDT SPM 04-00-07 PAJan 27, 2019 · N950AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2019012900621Beam · crackedCRACK ON RT NLG DOOR JAMB BEAM STA Y=40. (NLG). NRC 00155: RT NLG DOOR JAMB BEAM STA Y=40 WAS REPAIRED PER ER/A 495600-14MA REV. C.(ET)(HFEC) WAS ACCOMPLISHED ON RT NLG DOOR JAMB BEAM STA Y=40.(NLG) AND CRACK WAS DIMENSIONED WITH 1.500" LENGTH PER NDTSPM 06-10Jan 26, 2019 · N950AT · Boeing 717200 · Fuselage Main, Structure
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