Boeing 717-200

Service difficulty reports · 18,756

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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 DALA2024121711773Skin · damaged-AD- FUEL LEAK FOUND DURING INSPECTION OF LH WING AFT LOWER SKIN AT XRS=164. CONTACT LIAISON ENGINEERING FOR REPAIR PROCEDURES PRIOR TO FURTHER FLIGHT PER A.A. #FC5720-01103-01A. REFER TO NRC 0714281 FOR COMPLETION OF ERA 622950-14AD. NO LEAKS NOTED. OK FOR SEDec 17, 2024 · N942AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2024121711772Skin · damaged-AD- REF TO LOG PAGE #6930830. ORIGINAL WRITE UP: FUEL LEAK FOUND DURING INSPECTION OF LH WING AFT LOWER SKIN AT XRS+164. CONTACT LIAISON ENGINEERING FOR REPAIR PROCEDURES PRIOR TO FURTHER FLIGHT PER A.A #FC5720-0110-01A. ALL WORK COMPLETED PER ERA 622950AD REDec 17, 2024 · N942AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2024121711768Skin · damaged-AD- WEAR AND ELONGATED COUNTERSINK OF FASTENERS ON REMOVABLE VERTICAL STABILIZER LEADING EDGE. SUMMARY OF NRC 00053: COUNTERSINK OF FASTENERS ON REMOVABLE VERTICAL STABILIZER LEADING EDGE WERE REPAIRED PER ERA 621994-14AD REV ORIGINAL. ASSOCIATED ER/A 14-6219Dec 17, 2024 · N978AT · Boeing 717200 · Vertical Stabilizer, Plate/SkinSDR DALA2024121711771Tank · not reported-AD- STEP 16 OF ER/A 622950-14AD REV 0 PRI REV 2. C/W STEP 16 A&B PR1422A2 USED AT 1700 13DEC24. C/W STEP 16 STEP B PR1422B1/2 USED 0100 15DEC24. C/W STEP 16 STEP C UP TO LT TANK LEAK CHECK. LEAK CHECK COMPLETED. SENT TO REFUEL FOR LEAK CHECK. TANK FILLED WITHDec 16, 2024 · N942AT · Boeing 717200 · Fuel StorageSDR DALA2024121711770Support Fitting · cracked-AD- FOUND CRACK INDICATION OF L/H INBOARD FLAP FORWARD HINGE SUPPORT FITTING #8 OPEN BUSHING HOLE DURING BHEC PER PRI 622950-14AD (REV 1) STEP 12 QC2013. REINSPECTED INBD FLAP HINGE SUPPORT FITTING #8 BHEC INSPECTION IAW NDTSPM PY6 06-10-01-003 NO CRACK INDICDec 16, 2024 · N942AT · Boeing 717200 · Wing Miscellaneous StructureSDR DALA2024121711769Support Fitting · cracked-AD- FOUND CRACK INDICATION OF L/H INBOARD FLAP FORWARD HINGE SUPPORT FITTING #1 OPEN BUSHING HOLE DURING BHEC PER PRI 622950-14AD (REV 1) STEP 12 QC 2013. REINSPECTED FWD HINGE SUPPORT FITTING BHEC INSPECTION IAW PY6 06-10-01-003 WITH FS STANDARD NO CRACKS NODec 16, 2024 · N942AT · Boeing 717200 · Wing Miscellaneous StructureSDR DALA2024121711767Cusp Web · corrodedCORROSION ON LH CUSP WEB BTW STA Y=908 TO STA Y=927. SUMMARY OF NRC 00725: CORROSION LEVEL 2. CORROSION ON LH CUSP WEB BTW STA Y=908 TO STA Y=927 WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4, REPAIR 4, PAR 6 FIG 208. (LP #0713769)Dec 16, 2024 · N979AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024121711766Retainer · crackedCRACK INNER RETAINER OF COCKPIT WINDOW FRAME, UNDER BRACKET, UPPER AFT LH SIDE ON FLIGHT COMPARTMENT. SUMMARY OF NRC 00782: CRACK INNER RETAINER OF COCKPIT WINDOW FRAME, UNDER BRACKET, UPPER AFT LH SIDE ON FLIGHT COMPARTMENT WAS REPAIRED PER ER/A 622289-14 REVDec 16, 2024 · N981AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2025011500349Door · missingEXTERNAL POWER RECEPTACLE DOOR MISSING. FWD TO CDL 52-47-01 ON 15DEC24 IN LEX. FLIGHT CREW PLACARD INSTALLED. ON 14JAN25 MAINTENANCE INSTALLED A NEW DOOR ASSY PER B717 AMM 24-24. OPERATIONAL CHECK WAS GOOD. CDL & PLACARDS REMOVED. (LP #0711663)Dec 15, 2024 · N961AT · Boeing 717200 · Accessory Compartment DoorsSDR DALA2024121611740Battery Pack · inoperativeTHE EMERGENCY LIGHTS POWERED BY BATTERIES B5-235 AND B5-118 ARE INOPERATIVE. MAINTENANCE REPLACED EMERGENCY BATTERY PACKS B5-235 AND B5-118 PER B717 AMM 33-51. OK FOR SERVICE. (LP #6519628)Dec 15, 2024 · N966AT · Boeing 717200 · Emergency LightingSDR DALA2024121611739Wire · shortedTHE FWD EXIT SIGN OVER FWD F/A SEAT IS INOPERATIVE. ALSO, 4 EXIT LIGHTS ON AFT CATWALK ARE INOPERATIVE. MAINTENANCE REPLACED THE FWD EMERGENCY EXIT SIGN (L2-790). ALL LIGHTS ASSOCIATED WITH BATTERY PACK B5-260 ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY Dec 14, 2024 · N943AT · Boeing 717200 · Light System WiringSDR DALA2024121611737Frame · crackedCRACK ON FRAME STA Y=1037 BTW L-17L AND L-18L AT PASSENGER COMPARTMENT (CPAX). SUMMARY OF NRC 00579: FRAME STA Y=1037 BTW L-17L AND L-18L AT PASSENGER COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-20-07-0G PROCEDURE 4 REPAIR 4. (LP #0709303)Dec 14, 2024 · N979AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2024121611736Pan · gougedGOUGE ON INNER PAN AFT EDGE, 2 INCHES BELLOW BEAM #1 AFT EDGE, ON AFT CARGO DOOR (C2). SUMMARY OF NRC 00321: INNER PAN ON AFT LOWER CORNER CLOSE TO BEAM #1 AT AFT CARGO DOOR (C2) WAS REPAIRED PER ER/A 621854-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI Dec 13, 2024 · N981AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024121611735Longeron · corrodedCORROSION ON LONGERON 29L UPPER/LOWER SURFACE BTW STA Y=900-946 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00630: CORROSION LEVEL 2. LONGERON 29L BTW STA Y= 898 TO 964 AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-02-0G, 51-41-05-0G, AND PER B717-Dec 13, 2024 · N981AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2024121611734Skin · crackedELONGATED HOLES AND CRACKS ON COUNTERSINK OF PANEL 370CR. SUMMARY OF NRC 00658: PANEL 370CR WAS REPAIRED PER ERA 622046-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 622046-14 REV 1. ASSOCIATED ER/A 14-622046.Dec 12, 2024 · N978AT · Boeing 717200 · Vertical Stabilizer, Plate/SkinSDR DALA2024121311704Retainer · crackedCRACK INNER RETAINER OF COCKPIT WINDOW FRAME, UNDER BRACKET, UPPER AFT RH SIDE ON FLIGHT COMPARTMENT. SUMMARY OF NRC 00663: CRACK ON INNER RETAINER OF COCKPIT WINDOW FRAME, UNDER BRACKET, UPPER AFT RH SIDE ON FLIGHT COMPARTMENT WAS REPAIRED B717-200 SRM 56-10-Dec 12, 2024 · N978AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2024121311703Skin · dentedDAMAGE T: ELONGATE HOLES, PROTRUDING DENTS, AND GOUGES ON FUSELAGE SKIN STA Y 1037 BTW LONG 7R-13R. SUMMARY OF NRC 00627: ELONGATED HOLES, PROTRUDING DENTS, AND GOUGES ON FUSELAGE SKIN STA Y 1037 BTW LONG 7R-13R WERE REPAIRED PER PRI 622118-14 REV 3 AND ER/A 6Dec 12, 2024 · N981AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2024121311702Frame · wornWEAR AT FRAME OF STA Y=598 LH SIDE WAS FOUND OUT OF LIMITS. SUMMARY OF NRC 00716: FRAME OF STA Y=598 LH SIDE WAS REPAIRED PER ER/A 622297-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PER PRI 622297-14 REV 4. ASSOCIATED ER/A 14-622297 ADDED FOR AC 9543. (LP Dec 12, 2024 · N978AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2024121311701Longeron · crackedCRACKED LONGERONS L-3R, L-4R, L-5R, AND L-8R ON STA Y=1022 AT PASSENGER COMPARTMENT. (CPAX). SUMMARY OF NRC 00580: LONGERONS L-3R, L-4R, L-5R, AND L-8R ON STA Y=1022 AT PASSENGER COMPARTMENT WERE REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURE 2 REPAIR 2. (LP Dec 12, 2024 · N979AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2024121211665Floor Support · corrodedCORROSION OUT OF LIMITS ON FLOOR SUPPORTS ON STA Y=157-200 AND X=45 (1 EA) PER B717-200 SRM 53-00-00-1A PROCEDURE, ALLOWABLE DAMAGE GENERAL, PAR 4.C, FIG 103. SUMMARY OF NRC 00821: CORROSION LEVEL 2. FLOOR SUPPORT ON STA Y=157-200 AND X=45 WAS REPLACED PER B71Dec 12, 2024 · N981AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024121611738Hinge Fitting · corrodedCORROSION ON ALL INNER CAVITY LUGS (9 EA) OF THE INBOARD WING FLAP HINGE FITTING AT LH WING, AND WEAR ON FAIRING SUPPORTS OF THE INBOARD WING FLAP HINGE FITTING AT LH WING. ALSO WEAR ON INNER CAVITY (4 EA) SUPPORT AT LH WING. CORROSION ON ACTUATOR SUPPORT LUGSDec 11, 2024 · N981AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2024121211664Skin · crackedCRACK AND WEAR AT SKIN CUTOUT STA Y 994 AT LONGERON 25R AT AFT CARGO COMPARMENT. SUMMARY OF NRC 00774: CRACK AND WEAR AT SKIN CUTOUT STA Y 994 AT LONGERON 25R AT AFT CARGO COMPARMENT WAS REPAIRED PER B717-200 SRM 53-20-15-2R, PROCEDURE 12, REPAIR 12, FIG 201. Dec 11, 2024 · N978AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2024121111616Lug · wornWEAR ON HOLES AND INTERNAL FACE LUGS OF LH HINGE #3 OF LH WING. SUMMARY OF NRC 00803: HOLES AND INTERNAL FACE LUGS OF LH HINGE #3 OF LH WING WERE REPAIRED PER PRI 622848-14 REV 0 & ER/A 622848-14 REV ORIG. ASSOCIATED ER/A 14-622848 ADDED FOR AC 9548. (LP #0703Dec 11, 2024 · N981AT · Boeing 717200 · Wing, Control Surface Attach FittingsSDR DALA2024123112106None · none-AD- OVERWEIGHT LANDING. LW - 110.1. MAX 110.0. VERTICAL SPEED AT TOUCHDOWN ~ 50 FT/MN. WT EXITING RUNWAY INDICATED 109.8. PERFORMED B717 AMM 05-51-04 210-801 A-1 CHECK INSP FOR HARD OR OVERWEIGHT LANDING. FLOW CHART FIGURE 602 USED FOR OVERWEIGHT LANDING ONLYDec 10, 2024 · N964AT · Boeing 717200 · Standard Practices/StructuresSDR DALA2024121111615Cusp Web · crackedCRACK ON CUSP WEB STA Y=815 X=44 AT PASSENGER CABIN (CPAX). SUMMARY OF NRC 00606: CUSP WEB STA Y=815 X=44 AT PASSENGER CABIN (CPAX) WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4 FIG 221. (LP #0703712)Dec 10, 2024 · N979AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024121111614Beam · crackedCRACK ON INTERNAL STRUCTURE LL BEAM #1 STA 195 AT PASSENGER DOOR. SUMMARY OF NRC 00293: BEAM #1 ON INTERNAL STRUCTURE STA 195 AT PASSENGER DOOR (L1) WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 7 REPAIR 7. (LP #0703468)Dec 10, 2024 · N979AT · Boeing 717200 · Passenger/Crew DoorsSDR DALA2024121111613Longeron · crackedCRACKED LONGERONS L-4L AND L-5L ON STA Y=1022 AT PASSENGER COMPARTMENT. (CPAX) SUMMARY OF NRC 00581: LONGERONS L-4L AND L-5L ON STA Y=1022 AT PASSENGER COMPARTMENT WERE REPAIRED PER B717-200 SRM 53-00-05-2R REPAIR 2. (LP #0703457)Dec 10, 2024 · N979AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2024121111612Frame Angle · crackedCRACK ON FRAME CLIP (ENGINE PYLON SUPPORT BULKHEAD) IN STA Y=1022 AT L7 LH. SUMMARY OF NRC 00536: FRAME CLIP (ENGINE PYLON SUPPORT BULKHEAD) IN STA Y=1022 AT L7 LH WAS REPAIRED PER ERA 622468-14 REV ORIGINAL. (LP #0703045)Dec 10, 2024 · N979AT · Boeing 717200 · Nacelle/Pylon, Main FrameSDR DALA2025010500069Fuel Cell · leaking-AD- FUEL LEAK FOUND DURING INSPECTION OF THE RH WING THROUGH FLAP FITTING BOLTS (4 EA WET LEAK) AT XRS=164 LOWER SURFACE (OUTB BOLTS). CONTACT LIAISON ENGINEERING FOR REPAIR PROCEDURES PRIOR TO FURTHER FLIGHT. SUMMARY OF NRC 00002: RH WING THROUGH FLAP FITTINDec 9, 2024 · N967AT · Boeing 717200 · Fuel StorageSDR DALA2024121011569Wire · damagedSHIP 9501 -ATB/FUME- THE FLIGHT CREW RETURNED THE AIRCRAFT TO ATL DUE TO AN ACRID BURNING SMELL IN THE CABIN. CORRECTIVE ACTION: MAINTENANCE REPAIRED DAMAGED WIRES AND RING TERMINALS AT THE SERVICE DOOR OVERHEAD LIGHT ASSEMBLY. AIRCRAFT RETURNED TO SERVICE. (LDec 9, 2024 · N940AT · Boeing 717200 · Light System WiringSDR 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 DALA2024120911540Power Supply · faultedSEVERAL EMERGENCY LIGHTS ARE INOPERATIVE NEAR FWD SERVICE DOOR. MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY UNIT AT CANNON PLUG P1-259 PER B717 AMM 22-51. OPERATIONAL CHECK WAS GOOD. (LP #6556658)Dec 8, 2024 · N940AT · Boeing 717200 · Emergency LightingSDR DALA2024120911539Cusp Web · damagedTOOL MARK ON CUSP WEB AND SPLICE BTW STA Y=794, X44 TO X54 AT CABIN PASENGER. SUMMARY OF NRC 00547: CUSP WEB ON STA 796 X44 TO X54 WAS REPAIRED PER B717 SRM 53-00-55-2R. (LP #0700055)Dec 8, 2024 · N979AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024120911538Doubler · crackedCRACK ON EXTERNAL DOUBLER OF CUTOUT CLOSE/OPEN HANDLE AT FWD CARGO DOOR (C1). SUMMARY OF NRC 00088: EXTERNAL DOUBLER OF CUTOUT CLOSE/OPEN HANDLE AT FWD CARGO DOOR (C1) WAS FABRICATED AND REPLACED PER B717-200 SRM 52-30-01-2R PROCEDURE 1 REPAIR 1 PAR. 4B (9), (Dec 6, 2024 · N979AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2024120911537Longeron · crackedCRACK ON LONGERON 17 LH, LONGERON 8 LH, AND LONGERON 13 LH BTW STA Y=1020 AND STA Y=1023 LH SIDE. SUMMARY OF NRC 537: LONGERON 17 LH AND LONGERON 8 LH BTW STA Y=1020 AND STA Y=1023 LH WERE REPAIRED PER B717-200 SRM 53-00-05-2R REPAIR 2. AND LONGERON 13 LH HAD Dec 6, 2024 · N979AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2024120911536Angle · corrodedCORROSION ON CUSP ANGLE OF FWD SERVICE DOOR JAMB AT FOUR POINTS; THE FIRST ONE, FORWARD OF STA Y=167; THE SECOND ONE, UNDER THE PAN AFT OF STA Y=167; THE THIRD ONE, ALSO UNDER THE PAN FORWARD OF STA Y=200; AND THE FOURTH ONE, AFT OF STA Y=200. SUMMARY OF NRC 0Dec 6, 2024 · N978AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024120911542Control Unit · faultedSHIP 9536 -MISC/DE- FLIGHT CREW NOTED THE "LEFT GENERATOR OFF" MESSAGE WITH A POSSIBLE ELECTRICAL SMELL IN THE CABIN. THE PILOT DECLARED AN EMERGENCY WITH ATC AND WAS MET BY ARFF AFTER A NORMAL SAFE LANDING. CORRECTIVE ACTION: MAINTENANCE REPLACED THE EPCU, L Dec 5, 2024 · N974AT · Boeing 717200 · AC Generator-AlternatorSDR DALA2024120911535Seat Track · corrodedCORROSION ON SEAT TRACK X=56 AND STA 996 IN PAX CABIN. SUMMARY OF NRC 723: CORROSION LEVEL 2. SEAT TRACK X=56 AND STA 996 IN PAX CABIN WAS REPAIRED PER B717 SRM 53-20-52-2R PROCEDURE 1 REPAIR 1 FIGURE 201. PERFORM DECAL INSPECTION CONDITION EVERY C-CHECK PER TDec 5, 2024 · N979AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2024120911534Pan · corrodedCORROSION ON SEVERAL POINTS OF FORWARD CARGO DOOR JAMB PAN LOWER SECTION AT FORWARD CARGO COMPARTMENT. SUMMARY OF NRC 00224: CORROSION LEVEL 2. FORWARD CARGO DOOR JAMB PAN LOWER SECTION AT FORWARD CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-20-15-2R, REDec 5, 2024 · N978AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024120911530Floor Support · corrodedCORROSION ON FLOOR SUPPORTS (8 EA) X=-53.5, BTW STA Y=160 TO Y=200; STA X=44.5, BTW STA Y=160 TO Y=196; STA X=56, BTW STA Y=160 TO Y=196; STA Y=180.5, BTW STA X=13 TO X=38.25; STA Y=196, BTW STA X=15.5 TO X=44.5; STA Y=200, BTW STA X=-7 TO X=-44.5; STA Y=200, Dec 5, 2024 · N978AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024121111611Unknown · not reported-AD- MONITOR LOG REQUIRES PERMANENT REPAIR INSTRUCTIONS FOR ER/A 542233-14AD SECTION IV PRIOR TO 30-NOV-2025. CONTACT LIAISON ENGINEERING, DEP 555, FOR INSTRUCTIONS. DISCONTINUE REVENUE SERVICE ON OR PRIOR TO 30-NOV-25. PERMANENT REPAIR REQUIRED PER ERA 542233Dec 4, 2024 · N946AT · Boeing 717200 · Standard Practices/StructuresSDR DALA2024120911543Battery · inoperativeBOTH OVER-WING EMERGENCY EXIT LIGHTS ARE OUT. ALL OTHER EMERGENCY LIGHTS ARE GOOD. MAINTENANCE REPLACED THE OVER-WING EMERGENCY LIGHT BATTERY PER B717 AMM 31-51-06-401. BOTH OVER-WING EMERGENCY LIGHTS NOW ILLUMINATE PROPERLY. (LP #6931002)Dec 4, 2024 · N922AT · Boeing 717200 · Emergency LightingSDR DALA2025030601774Access Door · missing-PDA- THE LEFT ELEVATOR LEFT CENTER HINGE NUT ACCESS LOWER DOOR IS MISSING. DISPATCH APPROVAL VALIDATION IS ACCOMPLISHED. FWD TO CDL 55-25-01, PLACARD INSTALLED. SUMMARY NRC 00528: NUTS OF ELEVATOR HINGE ACCESS DOORS WERE INSTALLED PER B717 AMM 20-50-01. (LP #Dec 3, 2024 · N998AT · Boeing 717200 · Elevator, Plate/SkinSDR DALA2024122411974Pump · failedSHIP 9536 -MISC/DE- DECLARED AN EMERGENCY DUE TO LEFT HYDRAULIC PUMP FAIL MESSAGE AND LEFT GENERATOR OFF MESSAGE. CORRECTIVE ACTION: MAINTENANCE REPLACED THE LEFT ENGINE DRIVEN HYDRAULIC PUMP AND THE LEFT IDG. ALL RETURN TO SERVICE TEST PASSED. (LP #0690281)Dec 3, 2024 · N974AT · Boeing 717200 · Hydraulic Pump (Electric/Engine), MainSDR DALA2024120911529Web · crackedCRACK WAS FOUND ON WEB IN STA Y=247 AND X-44.5 APPROX IN AREA OF X-44.5 (MEDIUM) AT STA Y=200 TO STA Y=266 RH SIDE. SUMMARY OF NRC 00671: CRACK ON WEB IN STA Y=247 AND X-44.5 APPROX WAS REPAIRED PER B717-200 SRM 53-00-55-2R REPAIR 4 FIG 215. (LP #0691502)Dec 3, 2024 · N978AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024120911528Seat Track · corrodedCORROSION ON LH SEAT TRACK X=22 BTW STA Y=200-214 AT PASSENGER CABIN. SUMMARY OF NRC 00660: CORROSION LEVEL 2. LH SEAT TRACK X=22 BTW STA Y=200-214 AT PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 53-20-52-2R PROCEDURE 5 REPAIR 5. (LP #0691470)Dec 3, 2024 · N978AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2024120911527Fuel Tank · corroded-AD- CORROSION ON CENTER TANK UPPER SURFACE, AFT BULKHEAD STA Y=747 X=39 TO X=44 AT CENTER WING (LH WHELL WELL AREA). SUMMARY OF NRC 00678: CORROSION LEVEL 2. CORROSION ON CENTER TANK UPPER SURFACE, AFT BULKHEAD STA Y=747 X=39 TO X=44 AT CENTER WING (LH WHELL Dec 3, 2024 · N978AT · Boeing 717200 · Fuel StorageSDR DALA2024120911526Cusp Web · corrodedCORROSION ON CUSP WEB STA X=-44.5 TO X=-56 AND STA Y=313 AT CPAX. SUMMARY OF NRC 00738: CORROSION LEVEL 2. CUSP WEB STA X=-44.5 TO X=-56 AND STA Y=313 AT CPAX WAS REPAIRED PER B717-200 SRM 51-70-10-2R, PROCEDURE 2, REPAIR 2. (LP #0691024)Dec 3, 2024 · N978AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024120311395Cusp Web · corrodedCORROSION WAS FOUND ON LH CUSP ANGLE BTW STA Y=200-207 AT PASSENGER CABIN. SUMMARY OF NRC 00630: CORROSION LEVEL 2. LH CUSP ANGLE BTW STA Y=200-207 WAS REPAIRED PER B717 SRM 53-00-55-2R REPAIR 3. (LP #0690306)Dec 3, 2024 · N978AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2024120311394Cusp Web · crackedCRACKED IN FIVE PLACES OF THE CUSP WEB MEMBRANE AT STA Y=266, STA X=-44.5; STA Y=589, STA X=-44.5; STA Y= 663, STA X=-44.5; STA Y=716, STA X=-44.5; AND STA Y=1012, STA X=-56. SUMMARY OF NRC 00472: (ET) (HFEC) INSPECTION WAS ACCOMPLISHED ONLY ON STA Y=663, STA Dec 3, 2024 · N978AT · Boeing 717200 · Fuselage Main, Frame
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