Boeing 717-200

Service difficulty reports · 18,771

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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 aircraft_model_key = '717200'
  ORDER BY difficulty_date DESC"

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SDR DALA2019020500804Skin · gougedGOUGES AND NICKS ON FUSELAGE SKIN FROM STA Y1109 TO Y1129 BTW LONGERONS 12L-14L (FUS). FUSELAGE SKIN FROM STA Y1109 TO Y1129 BTW LONGERONS 12L-14L WAS REPAIRED PER ER/A 575178-14 REV ORIG AND ETI-17-19-017 REV 3.Feb 4, 2019 · N949AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR 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 DALA2019020400712Vane · wornWEAR ON AFT MOVABLE FLAP VANE LEADING EDGE 1 INCH FROM OUTBD EDGE (AD). NRC 00085: AFT MOVABLE FLAP VANE LEADING EDGE WAS REPAIRED PER B717 SRM 57-53-01-2R PROCEDURE 1 REPAIR 1 AND S.R.M. 51-70-02-0G. (LP #0930248)Feb 3, 2019 · N949AT · Boeing 717200 · Trailing Edge FlapsSDR 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 DALA2019020500806Pin · out of positionTAILCONE SLIDE CAM PIN WAS FOUND WITH THE WRONG ORIENTATION. (IN REF 5352-4002). CAM PIN WAS ADJUSTED (ORIENTATED) CORRECTLY PER AMM 53-52-03 820-801.Feb 2, 2019 · N949AT · Boeing 717200 · Aerodynamic FairingsSDR 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 DALA2019020420709Door Frame · crackedAMDS 5310-01436-01C RIGHT OVER WING EXIT FRAME CRACKED AT STA 715. CONDITION 3 EXITS. REPLACED FRAME ON AMDS WORK CARD 5310-01436-03B. (LP #0928476)Feb 2, 2019 · N988AT · Boeing 717200 · Fuselage Main, StructureSDR 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 DALA2019020400714Battery Pack · inoperativeTHE TAIL CONE EMERGENCY EXIT LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND THE CHARGER PER B717 AMM 33-51. CHECK WAS GOOD. (LP #3790932)Feb 1, 2019 · N906AT · Boeing 717200 · Emergency LightingSDR DALA2019020410715Cover · damagedTHE TAIL-CONE SLIDE COVER HAS A BROKEN CLIP FOR THE RELEASE CABLE. MAINTENANCE INSTALLED A NEW CLIP. (LP #0926413)Jan 31, 2019 · N959AT · Boeing 717200 · Escape SlideSDR DALA2019020410707Cam · excess playTAIL CONE CAM ASSEMBLY HAS EXCESSIVE PLAY, REF NRC 186. MAINTENANCE REPLACED THE CAM ASSEMBLY REF B717 AMM 53-52-03. SEE NRC 186 FOR DETAILS. (LP #0926185)Jan 31, 2019 · N988AT · Boeing 717200 · Aerodynamic FairingsSDR DALA2019020100658Threshold · corrodedFORWARD CARGO COMPARTMENT: CORROSION AT FWD CARGO DOOR CUT OUT THRESHOLD. (MKD). NRC 001-0229:0593-2007/002 00031 REPLACED DOOR JAMB SECTION REF B717 SRM 53-20-15-2R REPAIR 6. (LP #0926097)Jan 31, 2019 · N988AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2019020100657Door Frame · corrodedCORROSION ON LOWER DOOR JAMB FROM STA Y=954 TO Y=994 AT AFT CARGO COMPARTMENT. (C2). NRC 00253: CORROSION LEVEL 2, DOOR JAM FROM STA Y=954 TO Y=994 AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP #0926752)Jan 31, 2019 · N949AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2019020100656Cargo Track · corrodedCORROSION ON RH TIE TRACK FROM STA Y=908 TO Y=954 AT AFT CARGO COMPARTMENT (AMDS 5331-2001). (CCT). NRC 00376: CORROSION LEVEL 2, SECTION ON RH TIE TRACK FROM STA Y=908 TO Y=954 AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-05-0G AND 51-41-02-0GJan 31, 2019 · N949AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2019020100655Cusp Web · crackedCRACKS ON CUSP-MEMBRANE RH SIDE BETWEEN STA 579-589. (CPAX). NRC 00241: CUSP-MEMBRANE RH SIDE BETWEEN STA 579-589 WAS REPLACED PER B717-200 SRM 51-41-02-0G. (LP #0926077)Jan 31, 2019 · N949AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR 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 DALA2019013100634Cusp Web · corrodedCORROSION ON LT CUSP WEB STA 889-908 IN PAX CABIN IN REF NRC 00238. NRC 00477: CORROSION LEVEL 2, CUSP WEB LT BTW STA 889-908 AT PAX CABIN WAS REPLACED PER SRM 51-41-02-0G. (LP #0925509)Jan 30, 2019 · N949AT · 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 DALA2019013000623Doubler · corrodedSEVERAL CORRODED AREAS ON PREVIOUS DOUBLER REPAIR SPLICE ON STA Y=954 AND Y=994 AT AFT CARGO COMPARTMENT. (C2). NRC 00254: CORROSION LEVEL 2, DOUBLERS REPAIR SPLICE ON STA Y=954 AND Y=994 AT AFT CARGO COMPARTMENT WERE REPLACED PER SRM 53-20-15-2R-7. (LP #09240Jan 29, 2019 · N949AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR 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 DALA2019012900610Cusp Web · corrodedCORROSION OUT OF LIMITS ON CUSP-MEMBRANE RT SIDE BETWEEN STA 560-636 IN REF NRC 00240. NRC 00481: CORROSION LEVEL 2, WEB WAS REPLACED PER SRM 53-00-55-2R-4 FIG 226 AND 51-41-02-0G. (LP #0923003)Jan 28, 2019 · N949AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2019012801847Vane · delaminatedDURING TAP TEST INSPECTION PER SRM 57-53-01-1A PARA 2. B DELAMINATION OF 1.625" X 0.750" WAS FOUND AT DENT NR 1 LOCATED 22" OUTBD AND 5" T/E. IN REF JOB #70. NRC 00504: FORWARD MOVABLE OUTBD VANE WAS REPAIRED PER SRM 51-70-02-0G PARAGRAPH 15. A AND SRM 57-53-0Jan 27, 2019 · N949AT · Boeing 717200 · Trailing Edge FlapsSDR 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 DALA2019012800568Cusp Web · corrodedCRACKS ON CUSP-MEMBRANE LT SIDE BETWEEN STA 655-674 AND 696-715. (CPAX). NRC 00239: WEB WAS REPLACE PER SRM 53-00-55-02R-4 FIG 226. (LP #0921069)Jan 27, 2019 · N949AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2019012800567Former · crackedCRACKED FORMER ON RT MLG FWD DOOR JAMB OUTBOARD SECTION (FYT). NRC 00184: FORMER WAS REPLACED PER SRM 51-41-05-0G AND SRM 51-41-02-0G. (LP #0920939)Jan 27, 2019 · N949AT · Boeing 717200 · Fuselage Main, FrameSDR 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, StructureSDR HALA2019012600033Bracket · corrodedRIGHT HAND FLAP UPPER MOVABLE VANE INBOARD GUIDE BRACKET HAS EXFOLIATION CORROSION. REPLACED AND PICKED UP HOLES ON RIGHT HAND FLAP UPPER MOVABLE VANE INBD GUIDE BRACKET PER DWG 4916557.Jan 26, 2019 · N484HA · Boeing 717200 · Trailing Edge FlapsSDR DALA2019012700565Skin · crackedCRACK AT FUSELAGE SKIN STA 1087 BETWEEN LONG 13/14R. (FUS). NRC 00047: CRACK AT FUSELAGE SKIN WAS REPAIRED PER ETI-17-19-001 R2 AND ER/A 574710-14 REV. ORIGINAL SECTION: I PERMANENT REPAIR. ACCOMPLISHMENT OF SECTION I: PERMANENT REPAIR FOLLOWED UNDER LOG #0914Jan 26, 2019 · N950AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2019012700564Fitting · crackedCRACKED CLIP ON STA Y=655 X=0 AT WINGBOX (WB). NRC 0273: CLIP WAS REPLACED PER SRM 51-41-05 AND DWG #S1103715 REV. A. (LP #0920065)Jan 26, 2019 · N949AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2019012700563Cargo Track · corrodedCORROSION ON RT TIE TRACK FROM STA Y-588 TO Y-653 AT FWD CARGO COMPARTMENT (CCD). NRC 0323: CORROSION LEVEL 2, RT TIE TRACK FROM STA Y-588 TO Y-653 AT FWD CARGO COMPARTMENT WAS REPLACED PER SRM 51-41-01-0G AND 51-41-02-0G. (LP #0919720)Jan 26, 2019 · N949AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2019012600572Lens · missingTHE EMERGENCY EXIT COVER DIFFUSER LENS IS MISSING AT 29B. MAINTENANCE INSTALLED THE LENS COVER. CHECK IS GOOD. (LP #0918194)Jan 25, 2019 · N947AT · Boeing 717200 · Emergency LightingSDR DALA2019012600562Battery · dischargedTHE OVERWING EXIT EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE FORWARD EMERGENCY BATTERY AND REPLACED THE AFT EMERGENCY POWER SUPPLY PER AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #4289937)Jan 25, 2019 · N980AT · Boeing 717200 · Emergency LightingSDR DALA2019012500561Release Cable · wornTHE KEVLAR CABLE FOR THE TAIL CONE EMERGENCY EXIT RELEASE IS WORN. MAINTENANCE REPLACED THE KEVLAR CABLE PER IPC 53-52-30-01. TAIL CONE RELEASE SYSTEM WAS RIGGED IAW AMDS 5352-2001 TAILCONE SERVICE. FUNCTIONAL CHECK WAS SATISFACTORY. (LP #0918007)Jan 25, 2019 · N979AT · Boeing 717200 · Aerodynamic FairingsSDR DALA2019012500560Beam · crackedCRACK BEAM #6 BTW STA 172-190 AT PASSENGER ENTRANCE DOOR L1 (PTAS). NRC 00380: BEAM #6 WAS REPAIR PER ER/A 559578-14MA REV. ORIGINAL. ASSOCIATED ER/A 17-559578 ADDED FOR AC 9500. (LP #0916770)Jan 24, 2019 · N949AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2019012500559Longeron · wornWEAR AT FRAME AND SKIN AT RT ENGINE UPPER COWLING AT HINGE AREA. NRC 209: LONGERONS WERE REPLACED PER SRM 51-41-02-0G AND 51-41-05-0G AND SKIN WAS REPAIRED PER CV19-00214, ER/A 574759-14 REV. ORIGINAL. ASSOCIATED ER/A 17-574759 ADDED FOR AC 9509. (LP #0916826)Jan 24, 2019 · N950AT · Boeing 717200 · Engine Cowling SystemSDR DALA2019012500523Longeron · corrodedCORROSION AT LONGERON 29L FROM STA 200 TO 220 (E/E). NRC 00376: CORROSION LEVEL 2, SECTION OF LONGERON 29L FROM STA 157 TO 228 WAS REPLACED PER SRM 51-41-02 AND 51-41-05. (LP #0917473)Jan 24, 2019 · N950AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2019012500522Longeron · corrodedCORROSION AT LONGERON 28L FROM STA 200 TO 220 (E/E). NRC 00377: CORROSION LEVEL 2, SECTION OF LONGERON 28L FROM STA 157 TO 228 WAS REPLACED PER SRM 51-41-02 AND 51-41-05. (LP #0917467)Jan 24, 2019 · N950AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2019012500521Gusset · crackedCRACKED GUSSET ON AFT BULKHEAD SUPPORT STA Y=1022 PROJECTION LONG 7R AT PAX CABIN. (CPAX). NRC 00482: GUSSET ON AFT BULKHEAD SUPPORT STA Y=1022 PROJECTION LONG 7R AT PAX CABIN WAS REPAIRED PER ETI-17-19-004 REV. 1 AND ER/A 574801-14 REV ORIGINAL. ASSOCIATED ERJan 24, 2019 · N950AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2019012500520Pan · crackedCRACK ON OUTBOARD PAN IN STA Y=370 AND Y=427 BEAM 3 AT FWD CARGO DOOR. (C-1). NRC 00101: CRACKS ON OUTBOARD PAN IN STA Y=370 AND Y=427 BEAM 3 WERE REPAIRED PER SRM 52-30-02-2R REPAIR 1 FIG. 201, SRM 51-41-01-0G, SRM 51-41-02-0G AND 51-41-04-0G. (LP #0916806)Jan 24, 2019 · N949AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2019012400488Fitting · crackedCRACKED FRAME CLIP ON CENTER WING STA Y=715 XCW=44 AT WINGBOX (WB). NRC 00270: FRAME CLIP (CAP) ON CENTER WING STA Y=715 XCW=44 AT WINGBOX WAS REPLACED PER SRM 51-41-05-0G AND 51-41-01-0G. (LP #0916509)Jan 24, 2019 · N949AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2019012400487Former · crackedCRACKED LT FORMERS STA Y:660.0, Y:675.5, & Y:696.0 AT UNDERWING BARREL CANTED KEEL BEAM AREA (FUS). NRC 0389: LT FORMERS STA Y:660.0, Y:675.5, & Y:696.0 WERE REPAIRED PER SRM 51-70-11-2R -1 REPAIR 1 FIG. 201. (LP #0916479)Jan 24, 2019 · N949AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2019012400481Access Panel · corrodedCORROSION ON SEVERAL HOLES AT FUEL ACCESS PANELS #620FT, 620AT, 620CT, 520CT, 141AL, 141AR, AND FUEL PANEL P/N ARB 0975-17. NRC 00445: CORROSION LEVEL 2: FUEL ACCESS PANELS #620FT, 620AT, 620CT, 520CT, 141AL, 141AR, AND FUEL PANEL P/N ARB 0975-17 WERE REPLACEDJan 24, 2019 · N949AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2019012400480Access Panel · corrodedCORROSION ON HOLE AT FUEL ACCESS PANEL #520LB, 520CB, 620PB, AND FUEL PANEL P/N ARB 0975-17-9. NRC 00444: CORROSION LEVEL 2, FUEL ACCESS PLATES WERE REPAIRED PER SRM 57-10-01 REPAIR 2 PAR. 5 CONDITION II. (LP #0916148)Jan 24, 2019 · N949AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2019012400478Angle · crackedCRACKED ANGLE ON INTERCOSTAL FROM STA Y=409 TO 407 UPPER BEAM AT FWD CARGO DOOR (C-1) IN REF NRC: 00102. NRC 00505: ANGLE WAS REPLACED PER SRM 51-41-02-0G. (LP #0916065)Jan 24, 2019 · N949AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2019012400477Intercostal · crackedCRACK INTERCOSTAL FROM STA Y=409 TO Y=407 UPPER BEAM AT FWD CARGO DOOR. (C-1). NRC 00102: INTERCOSTAL FROM STA Y=409 TO Y=407 UPPER BEAM AT FWD CARGO DOOR WAS REPLACED PER SRM 51-41-02-0G, 51-41-05-0G, 51-41-04-0G, AND DWG #9957664 REV N. (LP #0916062)Jan 24, 2019 · N949AT · Boeing 717200 · Fuselage Miscellaneous Structure
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