Boeing 717-200

Service difficulty reports · 18,756

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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 aircraft_model_key = '717200'
  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 DALA2023092908006Unknown · unknownCORROSION ON FRAME CLIP STA Y=974 BTW STRG 26L/25L AT AFT CARGO COMPARMENT. SUMMARY OF NRC 0345: CORROSION LEVEL 2. FRAME CLIP STA Y=974 BTW STRG 26L/25L AT AFT CARGO COMPARTMENT WAS REPLACED PER DWG 9958215 REV AM. (LP #2992309)Sep 29, 2023 · N966AT · Boeing 717200 · Fuselage Internal Mounting StructureSDR DALA2023092908005Unknown · unknownCRACK ON UPPER FITTING AT AFT CABIN COMPARTMENT IN LONGERON 2L AT STA 1116. SUMMARY OF NRC 00224: UPPER FITTING AT AFT CABIN COMPARTMENT IN LONGERON 2L AT STA 1116 WAS REPAIRED PER B717 SRM 53-00-05-2R REPAIR 2 FIG 201 SHEET 2. (LP #2992175)Sep 29, 2023 · N966AT · Boeing 717200 · Fuselage Structure (General)SDR DALA2023092908007Unknown · unknownTHE EMERGENCY CEILING LIGHTS ROW 24-27 ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY BATTER PACK AT SEAT 25 PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #4480888)Sep 28, 2023 · N945AT · Boeing 717200 · Emergency LightingSDR DALA2023092908004Unknown · unknownCORROSION ON INTERCOSTAL STA Y=916 OVER STRG 28R AT AFT CARGO COMPARMENT. SUMMARY OF NRC 00328: CORROSION LEVEL 2. INTERCOSTAL ON STA Y=908 TO Y=927 STGR 28 RH WAS REPLACED PER DWG 9957704 REV M, B717 SRM 51-41-02-0G, AND 51-41-05-0G. (LP #2991968)Sep 28, 2023 · N966AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023092908003Unknown · unknownCRACK ON FUSELAGE SKIN BTW STA Y=1076 AND LONGERON 14L. SUMMARY OF NRC 00036: CRACK ON FUSELAGE SKIN BTW STA Y=1076 AND LONGERON 14L.WAS REPAIRED PER PRI 611843-14 REV 2 AND ERA 611843-14 REV ORIGINAL. SECTION I PERMANENT REPAIR.TIME COTROLLED ITEMS: SEC II COSep 28, 2023 · N961AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2023092908002Unknown · unknownCORROSION ON INNER DOUBLER AT AFT FUSELAGE PRESSURE BULKHEAD LOWER AREA STA Y=1053 BTW LONG 29LH-29RH AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00231: CORROSION LEVEL 2. INNER DOUBLER AT AFT FUSELAGE PRESSURE BULKHEAD LOWER AREA STA Y=1053 BTW LONG 29LH-29Sep 28, 2023 · N920AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2023092908001Unknown · unknownBROKEN INTERCOSTAL OF FLOOR CPAX STA 1022 AND BL=0 AT AFT CARGO. SUMMARY OF NRC 00214: INTERCOSTAL OF FLOOR CPAX STA 1022 AND BL= 0 AT AFT CARGO WAS REPAIRED B717-200 SRM 51-70-11-2R-1 REPAIR 1. (LP #2991792)Sep 28, 2023 · N920AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023092908000Unknown · unknownCORROSION ON CUSP WEB STA Y=370 X=-54 AT CPAX. SUMMARY OF NRC 00668: LEVEL CORROSION 2. CUSP WEB STA Y=370 X=-54 AT CPAX WAS REPAIRED PER B717 SRM-53-00-55-2R PROCEDURE 4 AND 51-41-05-0G PAR 8. (LP #2991582)Sep 28, 2023 · N961AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023092907999Unknown · unknownCRACKS (2 EA) ON PAN (AFT EDGE) BTW STOP #2 AND #4 OF AFT CARGO COMPARTMENT DOOR. SUMMARY OF NRC 00445: PAN (AFT EDGE) BTW STOP #2 AND #4 OF AFT CARGO COMPARTMENT DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 6 REPAIR 6. (LP #2990723)Sep 28, 2023 · N961AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023092807974Unknown · unknownCRACK ON BEAM 1 BELOW FWD UPPER CORNER AT PASSENGER DOOR (L1). SUMMARY OF NRC 00152: BEAM NBR 1 BELOW FWD UPPER CORNER AT PASSENGER DOOR (L1) WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 7 REPAIR 7. (LP #2990273)Sep 27, 2023 · N920AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2023092807973Unknown · unknownCORROSION ON FRAME CLIP STA Y=1022 BTW LONGERON 26 RH TO LONGERON 26 LH AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00499: CORROSION LEVEL 2. FRAME CLIP STA Y=1022 BTW LONGERON 26 RH TO LONGERON 26 LH WAS REPLACED AND INSTALLED PER DWG 9912243 TEM 383 REV JMSep 27, 2023 · N960AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023092807972Unknown · unknownCRACK ON SKIN ON STA Y=1133 AND BTW LONG 2R AND LONG 3R AT AFT FUSELAGE. SUMMARY OF NRC 00077: CRACK ON SKIN ON STA Y=1133 AND BTW LONG 2R AND LONG 3R AT AFT FUSELAGE WAS REPAIRED PER PRI 612145-14 REV 5 AND ER/A 612142-14AD REV ORIGINAL. SECTION I: PERMANENT Sep 27, 2023 · N989AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2023092807971Unknown · unknownCORROSION ON WEB BTW STA 940 TO 950 AND L25R TO L26R AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00139: CORROSION LEVEL 2. WEB BTW STA 940 TO 950 AND L25R TO L26R AFT CARGO COMPARTMENT WAS REPAIRED PER B717 SRM 51-70-10-2R PROCEDURE 1, REPAIR 1. (LP #2990111)Sep 27, 2023 · N966AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023092707959Unknown · unknownCORROSION ON REPAIR DOUBLERS BTW STA Y=991 / 998, BTW STA Y=743 / 751, AND BTW STA X=54 / 60 AT LH WEBS (PAX CABIN). SUMMARY OF NRC 00405: CORROSION LEVEL 2. DOUBLERS BTW STA Y=991 / 998, BTW STA Y=743 / 751, AND BTW STA X=54 / 60 AT LH WEBS WERE REPLACED PER Sep 27, 2023 · N961AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023092707958Unknown · unknownCORROSION ON FRAMES STA 1022 BTW LONG 27R-29R AND AT STA 1037 BTW LONG 29R-29L AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00622: CORROSION LEVEL 2. FRAMES STA 1022 BTW LONG 27R-29R AND AT STA 1037 BTW LONG 29R-29L AT AFT CARGO COMPARTMENT WERE REPAIRED PER Sep 27, 2023 · N960AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023092707957Unknown · unknownCORROSION ON FRAME BOTH SIDES, STA 908 BTW L-28R TO L-28L BILGE AREA AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00103: CORROSION LEVEL 2. FRAME BOTH SIDES, STA 908 BTW L-28R TO L-28L BILGE AREA AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-05-0G PSep 27, 2023 · N961AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023092707960Unknown · unknownCEILING MOUNTED EMERGENCY EXIT LIGHT AT ROW 1 DOES NOT ILLUMINATE WHEN EMERGENCY LIGHTS ARE ACTIVATED. MAINTENANCE REPLACED THE FWD EMERGENCY LIGHT BATTERY ASSY PER B-717 AMM 35-51. ALL LIGHTS OPERATE NORMAL NOW. AIRCRAFT OK FOR SERVICE. (LP #9986094)Sep 26, 2023 · N942AT · Boeing 717200 · Emergency LightingSDR DALA2023092707956Unknown · unknownCORROSION ON CUSP WEB FROM Y=160 TO Y=200 -X8 TO -X37 AT PAX CABIN IN REF NRC 00538. SUMMARY OF NRC 00614: CORROSION LEVEL 2. CUSP WEB FROM Y=160 TO Y=200 -X8 TO -X37 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 1 PAR 4 FIG 201 SHEET 1. (LPSep 26, 2023 · N920AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023092707955Unknown · unknownCRACK ON WEB (BELOW FLOOR BEAM) STA Y=696 AND X=56 LH ADJACENT TO FRAME. (WINGBOX AREA). SUMMARY OF NRC 00118: CRACK ON WEB (BELOW FLOOR BEAM) STA Y=696 AND X=56 LH ADJACENT TO FRAME WAS REPAIRED PER PRI 612213-14 REV 2 AND ER/A 612213-14 REV ORIGINAL SECTION Sep 26, 2023 · N989AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023092707954Unknown · unknownCRACK ON LH CUSP WEB STA Y=696 X=54 AT PAX CABIN. SUMMARY OF NRC 00135: CUSP WEB FROM STA Y=655 TO STA Y=715 X=54 WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4. (LP #2988642)Sep 26, 2023 · N989AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023092707953Unknown · unknownCRACKS ON AFT PAN UPPER SECTION AT L1 DOOR. SUMMARY OF NRC 00603: AFT PAN UPPER SECTION AT L1 DOOR WAS REPAIRED PER B717-200 SRM 52-10-02-2R REPAIR 3. (LP #2988599)Sep 26, 2023 · N966AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023092707952Unknown · unknownCORROSION ON CABIN FLOOR WEB DOUBLER BTW STA=641 TO 646 X=-58. CORROSION ON WEB DOUBLER BTW STA=476 TO STA=498 RH SIDE AT PAX CABIN. SUMMARY OF NRC 00542: CORROSION LEVEL 1. CORROSION ON CABIN FLOOR WEB DOUBLER (SPLICE ANGLE) BTW STA=641 TO 646 X=-58 WAS REMOVSep 26, 2023 · N966AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023092707951Unknown · unknownCORROSION FOUND ON AFT CARGO LOWER DOOR JAMB BTW STA Y-954 TO Y-994 AND LONGERONS 27R AND 28R. SUMMARY OF NRC 0163: CORROSION LEVEL 2. LOWER DOOR JAMB WAS REPLACED PER B717-200 SRM 51-41-02-0G, 51-41-05-0G, AND 53-20-15-2R-7 REPAIR 7. (LP #2987631)Sep 26, 2023 · N989AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023092707950Unknown · unknownCORROSION ON FLOOR SUPPORT Y=180 FROM X=-10 TO X=-43, FROM Y=162 TO Y=198 X=-45 AT W-1 AREA CPAX IN REF NRC 00541. SUMMARY OF NRC 00610: CORROSION LEVEL 2. FLOOR SUPPORTS Y=180 FROM X=-10 TO X=-43 AND FLOOR SUPPORT FROM Y=162 TO Y=198 X=-45 AT W-1 AREA CPAX WESep 26, 2023 · N920AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023092607924Unknown · unknownCRACK ON EXTERNAL FUSELAGE SKIN BTW STA Y=1087 AND STR L14. SUMMARY OF NRC 00024: CRACK ON EXTERNAL FUSELAGE SKIN BTW STA Y=1087 AND STR L14 WAS REPAIRED PER ER/A 612108-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 612108-14 REV 2. REPETITIVE INSPECTIONSep 25, 2023 · N989AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2023092507867Unknown · unknownCORROSION OUT OF LIMITS ON CUSP WEB RBL=57 AND STA 266, 331, 926, 935, AND 944. WITH AN ORIGINAL THICKNESS OF 0.020 INCHES AND REMAINING THICKNESS OF 0.007 INCHES, THE AREAS ARE OUT OF LIMITS PER B717-200 SRM 53-00-55-1A PROCEDURE 1, ALLOWABLE DAMAGE 1, PAR 4 Sep 24, 2023 · N966AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023092507866Unknown · unknownCORROSION ON WEB STA Y=200 TO 218 BTW X=-42 TO X=-54 SIDE RH AT CPAX. SUMMARY OF NRC 00311: CORROSION LEVEL 2. WEB STA Y=200 TO 218 BTW X=-42 TO X=-54 SIDE RH AT CPAX WAS REPLACED PER B717-200 SRM 53-10-51-0I PROCEDURE 2 ITEM 32 AND DWG: 9936535 REV CS. (LP #2Sep 24, 2023 · N961AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023092507865Unknown · unknownCORROSION ON FLOOR SUPPORT FROM Y=148 TO Y=200 X=8 W-1 AREA AT CPAX. SUMMARY OF NRC 00324: CORROSION LEVEL 2. FLOOR SUPPORT FROM Y=148 TO Y=200 X=8 W-1 AREA AT CPAX WAS REPLACED PER B717-200 SRM 51-41-01-0G. (LP #2984541)Sep 24, 2023 · N920AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023092507864Unknown · unknownCRACK ON FRAME STA Y=275 BTW STRG 15L/14L AT CPAX. SUMMARY OF NRC 00286: FRAME STA Y=275 BTW STRG 15L/14L AT CPAX WAS REPAIRED PER B-717-200 SRM 53-20-07-2R REPAIR 1. (LP #2984454)Sep 24, 2023 · N920AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023092507863Unknown · unknownCORROSION ON EXTERNAL SKIN BTW STA Y=1037 TO Y=1022, L-29R TO L-28R AT LOWER FUSELAGE. SUMMARY OF NRC 00085: CORROSION LEVEL 2. EXTERNAL SKIN BTW STA Y=1037 TO Y=1022, L-29R TO L-28R AT LOWER FUSELAGE WAS REPAIRED PER ERA 612001-14 REV. ORIGINAL SECTION I: PERSep 24, 2023 · N607AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2023092507862Unknown · unknownCORROSION ON GENERATION FLOOR PANEL FLOOR PANELS WERE FABRICATED AND REPLACED PER DWG 9952521 REV BB, DWG 9956320 REV G, DWG 9956336 REV G AND B717-200 SRM 51-20-05-0G. (LP #2984188)Sep 23, 2023 · N961AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2023092507861Unknown · unknownCORROSION ON DOOR JAMB LOWER EDGE BTW LONG PROJECT 26R AND LONG PROJECT 28R AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00148: CORROSION LEVEL 2. PAN JAMB LOWER WAS REPLACED PER B-717-200 SRM 53-20-15 PROCEDURE 7 REPAIR 7, 51-41-02-0G PAR 4 B, AND 51-41-05-0G PARSep 23, 2023 · N607AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2023092507860Unknown · unknownCORROSION ON CUSP WEB STA Y=680 X=-50, AT CABIN PAX. SUMMARY OF NRC 00619: CORROSION LEVEL 2. CUSP WEB BTW STA 655 TO STA 684 X=-50 AT CABIN PAX WAS REPAIRED PER B717 SRM 53-00-55-2R-4 PAR 4 AND 5 FIGURE 223. (LP #2983819)Sep 23, 2023 · N966AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023092507859Unknown · unknownCORROSION ON CABIN FLOOR CUSP WEB UPPER AND LOWER FACE BTW STA=541 TO 560 FROM X=-58 TO X=-54, STA=598 TO 617 FROM X=-58 TO X=-54, STA=620 TO 630 FROM X=-58 TO X=-54, STA=636 TO 655 FROM X=-55 TO X=-46, AND BTW STA=655 TO STA=674 FROM X=-55 TO X=-46 RH SIDE ATSep 23, 2023 · N966AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023092507858Unknown · unknownCORROSION ON CUSP WEB DOUBLERS (5 EA) RH SIDE; (4 EA) BTW STA Y=503 AND STA Y=579 ON X=-56 AND (1 EA) BTW STA Y=794 AND STA Y=813 ON X=-56 AT PAX CABIN. SUMMARY OF NRC 00323: CORROSION LEVEL 2. CUSP WEB DOUBLERS (5 EA) RH SIDE; (4 EA) BTW STA Y=503 AND STA Y=5Sep 23, 2023 · N961AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023092507868Unknown · unknownTHE DOOR R1 EMERGENCY EXIT TOP SIGN IS INOPERATIVE. MAINTENANCE FOUND A BROKEN PIN IN THE IN-LINE JUNCTION. REPINNED AND REPLACED THE IN-LINE JUNCTION REF BOEING SWPM CHP 20-20-02. EMERGENCY LIGHT OPS NORMAL AS PER B717 AMM 33-51. (LP #4782462)Sep 22, 2023 · N939AT · Boeing 717200 · Emergency LightingSDR DALA2023092507857Unknown · unknownCRACK ON WEB INSIDE UPPER STA Y=1076 AT AFT BULKHEAD DOOR. SUMMARY OF NRC 00093: WEB INSIDE UPPER STA Y=1076 AT AFT BULKHEAD DOOR WAS FABRICATED AND REPLACED PER DRAWING 9929480-49 REV BW, B717-200 SRM 51-41-02-0G, AND 51-41-05-0G PAR 8. (LP #2982829)Sep 22, 2023 · N966AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023092507856Unknown · unknownCORROSION ON LONGERON 30 BTW STA 909 TO STA 912, STA 921 TO STA 922, STA 962 TO STA 968, STA 998 TO STA 1000, LONGERON 29L STA 910 TO STA 912, STA 940 TO STA 950, STA 952 TO STA 955, AND LONGERON 29R STA 924 TO STA 928, STA 1005 TO STA 1006 AT AFT CARGO COMPARSep 22, 2023 · N607AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2023092507855Unknown · unknownCORROSION ON CUSP WEB STA FROM Y=860 TO Y=870 X=- 58, AT CABIN PAX. SUMMARY OF NRC 00621: CORROSION LEVEL 2. CUSP WEB STA FROM Y=860 TO Y=870 X=- 58 WAS REPAIRED PER B717 SRM 53-00-55-2R REPAIR 4 FIGURE 216. (LP #2982286)Sep 22, 2023 · N966AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023092507854Unknown · unknownFOUND INTERCOSTAL CRACKED BETWEEN STA 946.5 AND 954. FABBED NEW INTERCOSTAL PER DWG 9915578 AND SRM 53-20-51-0I PROC 7. INSTALLED INTERCOSTAL PER B717 SRM 51-41. (LP #2980699)Sep 21, 2023 · N979AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023092207784Unknown · unknownDOOR R1 EXIT SIGN IS MISSING. MAINTENANCE REPLACED AND INSTALLED THE MISSING LENS COVER IAW B717 AMM 33-51. LIGHT OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT IS OK FOR SERVICE. (LP #4579222)Sep 21, 2023 · N894AT · Boeing 717200 · Emergency LightingSDR DALA2023092207783Unknown · unknownAFTER INNER SKIN REMOVAL, A CRACK WAS FOUND ON BEAM #1 AFT SECTION OF L1 DOOR. SUMMARY OF NRC 00647: BEAM #1 AFT SECTION OF L1 DOOR WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 7 REPAIR 7. (LP #2981121)Sep 21, 2023 · N966AT · Boeing 717200 · Passenger/Crew DoorsSDR DALA2023092207782Unknown · unknownA.D. CRACK WAS FOUND ON RH UPPER RADIUS OF THE FRAME TAB OF THE OVERWING FRAME STA Y=674.000 IN REFERENCE CARD 5310-01436-01D JOB #044-0004 STEP 7. SUMMARY OF NRC 00112: RH FRAME OF THE OVERWING FRAME STA Y=674.000 WAS REPLACED UNDER AMDS 5310-01436-03B. (LP #Sep 21, 2023 · N989AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023092107773Unknown · unknownSHIP 9523 -HYD/DE- THE CREW RECEIVED A "HYD R QTY LOW" MESSAGE AT TOP OF CLIMB. THEY WERE UNABLE TO REPRESSURIZE THE SYSTEM. THE QRH WAS COMPLIED WITH AND PERFORMED THE ALTERNATE GEAR EXTENSION (DUE TO A RIGHT HYDRAULIC SYSTEM LOW QUANTITY). AN EMERGENCY WAS DSep 21, 2023 · N964AT · Boeing 717200 · Hydraulic System, MainSDR DALA2023092107772Unknown · unknownBROKEN FINGER DOUBLER ON INTERNAL FUSELAGE SKIN BTW STA Y 294-300 AND LONG L 11R. SUMMARY OF NRC 00578: FINGER DOUBLER ON INTERNAL FUSELAGE SKIN BTW STA Y 294-300 AND LONG L 11R WAS REPAIRED PER PRI 611539-14 REV 3 AND ERA 611539-14AD REV ORIGINAL, SECTION I PSep 21, 2023 · N960AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2023092107771Unknown · unknownCRACK ON PRESSURE BULKHEAD EMERGENCY EXIT DOOR JAMB (RH EDGE) ON STA Y=1053 BTW LONG PROJECTION 14R AND 16R AT AFT CPAX. SUMMARY OF NRC 00285: PRESSURE BULKHEAD EMERGENCY EXIT DOOR JAMB (RH EDGE) ON STA Y=1053 BTW LONG PROJECTION 14R AND 16R AT AFT CPAX WAS RESep 20, 2023 · N960AT · Boeing 717200 · Fuselage Main, BulkheadSDR DALA2023092107770Unknown · unknownCORROSION ON FLOOR SUPPORTS (3 EA) VERTICAL AND HORIZONTAL BTW STA 200 TO STA 160 BTW LBL15, LBL45, AND LBL55 AT CPAX. SUMMARY OF NRC 00437: CORROSION LEVEL 2. FLOOR SUPPORTS (3 EA) VERTICAL AND HORIZONTAL BTW STA 200 TO STA 160 BTW LBL15, LBL45, AND LBL55 AT Sep 20, 2023 · N920AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023092107769Unknown · unknownCRACK ON RH CUSP WEB STA Y=655 AND Y=715 AND X=54. SUMMARY OF NRC 00145: RH CUSP WEB BETWEEN STA Y=655 AND Y=715 AND BETWEEN X=40 AND X=54 WAS REPAIRED PER B-717 SRM 53-00-55-2R-4 REPAIR 4. (LP #2979411)Sep 20, 2023 · N989AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023092107768Unknown · unknownCRACK ON WEB ON STA Y=579 AND X=-44 AT PAX CABIN. SUMMARY OF NRC 00389: WEB ON STA Y=579 AND X=-44 AT PAX CABIN WAS REPAIRED PER B 717-200 SRM 53-00-55-2R REPAIR 4. (LP #2979222)Sep 20, 2023 · N920AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023092007728Unknown · unknownCORROSION ON CUSP WEB STA Y=256 X=-58. SUMMARY OF NRC 00618: CORROSION LEVEL 2. CUSP WEB STA 256 X=-58 WAS REPAIRED PER B717 SRM 53-00-55-2R REPAIR 4 FIGURE 220. (LP #2978269)Sep 20, 2023 · N966AT · Boeing 717200 · Fuselage Miscellaneous Structure
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