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 DALA2024100709734Lens · missingTHE OVERHEAD EMERGENCY EXIT LIGHT DIFFUSER IS MISSING AT 25/26DEF. DEFERRED 25/26DEF OVERHEAD EMERGENCY EXIT LIGHT DIFFUSER PER NEF 33-51-02. DEFERRAL REMARKS NOTED. MAINTENANCE REPLACED THE MISSING COVER ASSEMBLY REF B717 AMM 33-51. THIS ACTION CLEARS NEF 33-Oct 7, 2024 · N940AT · Boeing 717200 · Emergency LightingSDR DALA2024100709751Compressor Wheel · damagedSHIP 9577 -FUME/DE- ON CLIMB OUT THROUGH FL200, AN ODOR SIMILAR TO MELTING PLASTIC WAS BRIEFLY NOTED. ABOUT ONE MINUTE LATER THE CREW EXPERIENCED SOME ENGINE VIBRATION ON THE LEFT SIDE AND AT THE SAME TIME, THE "ENG COMP L STALL" MESSAGE ILLUMINATED. SHORTLY TOct 5, 2024 · N921AT · Boeing 717200 · Turbine Engine Compressor SectionSDR DALA2024100709733Frame · crackedCRACK ON FRAME BTW STA Y=1037 AND LONG 17R AT PAX CABIN RH SIDE. SUMMARY OF NRC 00287: FRAME BTW STA Y=1037 AND LONG 17R AT PAX CABIN RH SIDE WAS REPAIRED PER B717 SRM 53-20-07-2R-4. PERFORM A GENERAL VISUAL INSPECTION EVERY C-CHECK PER B717-200 SRM 53-20-07-2Oct 5, 2024 · N991AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2024100709732Longeron · crackedCRACK ON LONGERON L10L STA Y=908 AT CPAX CABIN. SUMMARY OF NRC 00268: LONGERON L10L STA Y=908 AT CPAX CABIN WAS REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURE 2 REPAIR 2. PERFORM DECAL INSPECTION CONDITION EVERY "C" CHECK PER TOPP 30-10-70 PAGE 14 PAR I. (LP Oct 4, 2024 · N991AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2024100709731Floor Support · corrodedCORROSION ON FLOOR SUPPORT X=-22 BTW STA Y=1022 TO STA Y=1053 WAS FOUND OUT LIMITS AT PASSENGER CABIN (W2). SUMMARY OF NRC 00715: CORROSION LEVEL 2. FLOOR SUPPORT X=-22 BTW STA Y=1022 TO STA Y=1053 AT PASSENGER CABIN (W2) WAS REPLACED AND INSTALLED PER B717-20Oct 4, 2024 · N991AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024100409702Frame · wornWEAR ON PREVIOUS DOUBLER REPAIR ON INTERNAL LOWER FRAME AT AFT BULKHEAD DOOR. SUMMARY OF NRC 00363: REPAIR DOUBLER ON INTERNAL LOWER FRAME AT AFT BULKHEAD DOOR WAS FABRICATED AND REPLACED PER B717-200 SRM 52-10-02-2R PROCEDURE 16 REPAIR 16. (LP #0590940)Oct 3, 2024 · N991AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2024100409701Angle · corrodedCORROSION ON DOOR JAMB ANGLE AND DOOR JAMB WEB BTW STA Y=200-210 AND X=56 AT FWD PASSENGER DOOR JAMB (L1). SUMMARY OF NRC 00450: CORROSION LEVEL 2. DOOR JAMB ANGLE WAS REPLACED AND DOOR JAMB WEB BTW STA Y=200-210 AND X=56 AT FWD PASSENGER DOOR JAMB WAS REPAIREOct 3, 2024 · N990AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024100409700Barrel Nut · corrodedCORROSION ON BARREL NUTS 3 (UPPER RH), 27 (UPPER LH), 28 (LOWER LH), AND 29 (LOWER RH) AT HORIZONTAL STABILIZER CENTER BOX. SUMMARY OF NRC 00544: CORROSION LEVEL 2. BARREL NUTS 3 (UPPER RH), 27 (UPPER LH), 28 (LOWER LH) CLEANED PER DAL P.S. 900-1-2-1 NO 01 ANDOct 3, 2024 · N951AT · Boeing 717200 · Horizontal Stabilizer StructureSDR HALA20241004047Lamp · inoperativeCOCKPIT EMERGENCY LIGHT INOP. RELAMPED CP EMERGENCY LIGHTS AND INSTALLED NEW BATTERY PACK AT B5-123, OPS TEST PER AMM 33-51-03 OK.Oct 3, 2024 · N492HA · Boeing 717200 · Emergency LightingSDR HALA20241004046Battery · inoperativeCOCKPIT EMER LT COMES ON MOMENTARILY THEN TURNS OFF. REMOVE/REPLACE FLT COMPT. OVERHEAD LIGHT BATTERY B5-123. OPS CHECK GOOD OK FOR SVC.Oct 3, 2024 · N476HA · Boeing 717200 · Emergency LightingSDR DALA2024100409699Door Frame · corrodedCORROSION ON PREVIOUS REPAIR DOUBLER OF DOOR JAMB FWD SECTION AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00145: CORROSION LEVEL 2. PREVIOUS REPAIR DOUBLER OF DOOR JAMB FWD SECTION AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 53-20-15-2R-7. (LP #0588555Oct 2, 2024 · N991AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2024103010525Access Door · detachedHORIZONTAL STABILIZER BEARING AND CENTER SECTION ACCESS DOORS WERE DISCOVERED MISSING DURING POSTFLIGHT INSPECTION. MEL NUMBER ADDED FOR DISPATCH RELEASE, LOG REDEFERRAL REQUIRED. DISPATCH APPROVAL VALIDATION IS ACCOMPLISHED PANEL 370SL BEARING COVER PANEL MISOct 1, 2024 · N983AT · Boeing 717200 · Horizontal Stabilizer, Plate/SkinSDR DALA2024100209620Spar Cap · crackedCRACK IN LH WING REAR SPAR LOWER CAP RADIUS. REFERENCE AA NUMBER FC 5720-01103. CRACK LOCATION IS XRS 156.950. SUMMARY NRC 010-0001:5720-01103-01A/001 00001 COMPLIED WITH PRI 621210-14 REV 0 AND REV 1 AND ENSURED IT MATCHES ERA 621210-14 REV ORIG SECTION 1 STESep 30, 2024 · N927AT · Boeing 717200 · Wing SparSDR DALA2024100209619Vane · dentedDENTS ON LH WING INBOARD FIXED FLAP VANE INTRADOS BETWEEN XV1=119 AND XV1=119+11, XV1=211-24, XV1=211-26. SUMMARY OF NRC 00172: DENTS (16 EA) ON LH WING INBOARD FIXED FLAP VANE INTRADOS BETWEEN XV1=119 AND XV1=119+11, XV1=211-24, AND XV1=211-26 WERE EVALUATED Sep 29, 2024 · N717JL · Boeing 717200 · Trailing Edge FlapsSDR DALA2024100209618Skin · corroded-AD- CORROSION ON UPPER SKIN BTW STA Y=740 AND -XCW=0-10 AT LH/RH MLG WELL. SUMMARY OF NRC 00216: CORROSION LEVEL 2. UPPER SKIN BTW STA Y=740 AND -XCW=0-10 AT LH/RH MLG WELL WAS REPAIRED PER PRI 620162-14 REV 8 AND ER/A 620162-14AD REV ORIGINAL SECTION I: PERMSep 28, 2024 · N951AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2024100209617Longeron · crackedCRACKED LONGERON 17 RH AT STA Y=408 PAX CABIN. SUMMARY OF NRC 00259: LONGERON 17 RH AT STA Y=408 PAX CABIN WAS REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURE 2 REPAIR 2. PERFORM AN EXTERNAL GVI OF THE REPAIR EVERY C-CHECK PER B717 SRM 53-00-05-2R PROCEDURE 2 Sep 28, 2024 · N991AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2024100209616Skin · cracked-AD- CRACK ON EXTERNAL FUSELAGE SKIN Y=1037 LONG 14 LH (FUS). SUMMARY OF NRC 00348: CRACK ON EXTERNAL FUSELAGE SKIN Y=1037 LONG 14 LH WAS REPAIRED PER ER/A 619986-14AD REV ORIGINAL SECTION I: PERMANENT REPAIR. REPAIR APPROVAL IS LIMITED TO 24 MONTHS FROM 23-SESep 27, 2024 · N951AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2024100209615Unknown · no discrepancy-AD RELATED- AMDS 5720-01103-01A: PERFORM STEP 13. SUMMARY NRC 00919: (ET) HFEC INSPECTION WAS PERFORMED. NO CRACKS WERE FOUND PER B717 CARD 5720-01103-01A, STEP 13 AND B717 DC/MD NDT SPM PART 6, 06-10-01.001. ASSOCIATED AA 5720-01103 ADDED FOR AC 9546. (LP #0Sep 26, 2024 · N980AT · Boeing 717200 · Standard Practices/StructuresSDR DALA2024100209614Unknown · no discrepancy-AD RELATED- AMDS 5720-01103-01A: PERFORM STEP 15 AND 16. SUMMARY NRC 00921: SEALANT WAS REMOVED AND APPLIED PER B717 AMM 20-60-01 PER AMDS 5720-01103-01A ALSO (ET) HFEC INSPECTION WAS PERFORMED. NO CRACKS WERE FOUND PER B717 CARD 5720-01103-01A, STEP 16 AND BSep 26, 2024 · N980AT · Boeing 717200 · Standard Practices/StructuresSDR DALA2024100209613Unknown · no discrepancy-AD RELATED- AMDS 5720-01103-01A: PERFORM STEP 14. SUMMARY NRC 00920: (ET) HFEC INSPECTION WAS PERFORMED. NO CRACKS WERE FOUND PER B717 CARD 5720-01103-01A, STEP 14 AND B717 DC/MD NDT SPM PART 6, 06-10-01.001. ASSOCIATED AA 5720-01103 ADDED FOR AC 9546. (LP #0Sep 26, 2024 · N980AT · Boeing 717200 · Standard Practices/StructuresSDR DALA2024092609432Skin · crackedCRACKS ON FUSELAGE SKIN BTW STA Y=1087 AND LONGERON 13R-14R AT AFT FUSELAGE. SUMMARY OF NRC 00020: FUSELAGE SKIN BTW STA Y=1087 AND LONGERON 13R-14R AT AFT FUSELAGE WAS REPAIRED PER PRI 620514-14 REV 5 AND ER/A 620514-14 REV ORIGINAL, SECTION I: PERMANENT REPASep 26, 2024 · N990AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2024092609433Connector · not seatedTHE AFT EMERGENCY CEILING LIGHT REMAINED ON IN THE ARM POSITION. MAINTENANCE RESEATED THE CANNON PLUG ON THE AFT CABIN EMERGENCY LIGHT BATTERY IAW B717 AMM 33-51. PERFORMED OPERATIONAL CHECK OF THE EMERGENCY LIGHT SYSTEM. ALL LIGHTS OPERATE NORMALLY. OK FOR SESep 25, 2024 · N929AT · Boeing 717200 · Light System WiringSDR DALA2024092609431Skin · crackedCRACK ON FUSELAGE SKIN BTW STA Y=1022 AND LONGERON 13L-14L AT AFT FUSELAGE. SUMMARY OF NRC 00049: FUSELAGE SKIN BTW STA Y=1022 AND LONGERON 13L-14L AT AFT FUSELAGE WAS REPAIRED PER ER/A 620582-14 REV ORIG. SECTION I PERMANENT REPAIR PERFORM A GENERAL VISUAL INSep 25, 2024 · N990AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2024092509407Longeron · crackedCRACK ON LONGERON 5LH, 8LH, 16LH, 5RH, 7RH, AND 9RH STA 1022 AT PAX CABIN. SUMMARY OF NRC 00404: LONGERONS 5LH, 8LH, 16LH, 5RH, AND 7RH STA 1022 AT PAX CABIN WERE REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURE 2 REPAIR 2 FIG 201. ON LONGERON 9RH STA 1022 (ET)Sep 24, 2024 · N990AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2024092509408Battery Pack · inoperativeFOUND THE LEFT FORWARD ENTRY EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE REPLACED THE FORWARD OVERHEAD EMERGENCY LIGHT BATTERY PACK IAW B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #6464450)Sep 24, 2024 · N895AT · Boeing 717200 · Emergency LightingSDR DALA2024092509406Floor Support · corrodedCORROSION ON FLOOR SUPPORTS (2 EA) BTW STA=1022 TO STA=1053 ON X=56, AND -X=20 AT PAX CABIN. SUMMARY OF NRC 00835: CORROSION LEVEL 2. FLOOR SUPPORTS (2 EA) BTW STA=1022 TO STA=1053 ON X=56, AND -X=20 AT PAX CABIN WERE REPLACED PER B717 SRM 51-30-07-0G FIG 9, DSep 23, 2024 · N990AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024092309315Lens · missingTHE 1AB EMERGENCY LIGHT LENSE IS MISSING. MAINTENANCE REPLACED THE EMERGENCY LIGHT COVER AT 1AB AS REQUIRED. OK FOR SERVICE. (LP #0569847)Sep 22, 2024 · N977AT · Boeing 717200 · Emergency LightingSDR DALA2024092309314Cusp Web · crackedCRACK ON LH CUSP WEB (LOWER SURFACES) STA 718 X=44 AT PAX CABIN. SUMMARY OF NRC 00509: LH CUSP WEB (LOWER SURFACES) STA 718 X=44 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4. (LP #0568424)Sep 21, 2024 · N990AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024092309313Pan · crackedCRACK ON PAN AROUND BEAM #1 AFT EDGE OF PASSENGER DOOR. SUMMARY OF NRC 00301: PAN AROUND BEAM #1 AFT EDGE OF PASSENGER DOOR WAS REPAIRED PER B717-200 SRM 52-10-02-2R, PROCEDURE 3, REPAIR 3. (LP #0566607)Sep 20, 2024 · N990AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024092009272Cusp Web · crackedCRACK ON BELOW CUSP WEB BTW STA Y=520 LOWER FACE X=-44 AND STA Y=650 X=-46 AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00230: CUSP WEB BTW STA Y=520 LOWER FACE X=-44, WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4, PAR 5, FIG 216. THE CUSP WEB ON Sep 19, 2024 · N990AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024091909180Pseu · failedSHIP 9580 -MISC/DE- THE FLIGHT CREW DECLARED AN EMERGENCY DUE TO A "PSEU FAIL" MESSAGE. THE QRH WAS COMPLIED WITH AND THE LANDING GEAR POSITION INDICATIONS WERE NORMAL FOLLOWING GEAR EXTENSION FOR LANDING. HOWEVER, THE LEADING EDGE SLATS FAILED TO EXTEND RESULSep 19, 2024 · N915AT · Boeing 717200 · Landing Gear Position and WarningSDR DALA2024091909181Control Unit · failedSHIP 9519 -MISC/DE- THE FLIGHT CREW RECEIVED AN "ANTI-SKID FAIL" MESSAGE WHEN TRANSITIONING FLAPS FROM 18 TO 40 WITH THE GEAR EXTENDED. THE CREW PERFORMED A GO-AROUND. ONCE STABLE, THE CREW COMPLIED WITH THE QRH AND REFERENCED THE ODM FOR LANDING PERFORMANCE DSep 18, 2024 · N960AT · Boeing 717200 · Brake Anti-Skid SectionSDR DALA2024091809141Floorbeam · corrodedCORRODED HORIZONTAL FLOOR SUPPORTS AT W1 ON STA Y=180 X-9 TO X-43 WITH ORIGINAL THICKNESS WAS 0.070" AND REMAINING THICKNESS IS 0.044", STA Y=196 X 16 TO X 43 WITH ORIGINAL THICKNESS WAS 0.070" AND REMAINING THICKNESS IS 0.044", STA Y=200 X 5 TO X-5 WITH ORIGISep 18, 2024 · N990AT · Boeing 717200 · Fuselage Main, Floor BeamSDR DALA2024091909182Actuator · leakingSHIP 9585 -DIV/FUME/DE- ENROUTE TO MDT THE FLIGHT WAS DIVERTED TO IAD FOLLOWING STRONG SULFUR FUMES THROUGHOUT THE COCKPIT AND CABIN. MAINTENANCE FOUND THE NOSE LANDING GEAR RETRACT ACTUATOR LEAKING HYDRAULIC FLUID. THE ACTUATOR WAS REPLACED AND THE AIRCRAFTSep 17, 2024 · N985AT · Boeing 717200 · Landing Gear ActuatorSDR DALA2024091809140Hinge · excess playFREEPLAY WAS FOUND ON RH WING FLAP OUTBD HINGE AREA. SUMMARY OF NRC 00781: RH WING FLAP OUTBD HINGE WAS REPAIRED PER ER/A 620752-14 REV ORIGINAL AND PRI 620752-14 REV 2 AND WAS INSTALLED PER B717-200 AMM 27-55-03 400-801. ASSOCIATED ER/A 14-620752 ADDED FOR ACSep 17, 2024 · N989AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2024091809139Pan · crackedCRACK ON PAN INTERNAL EDGE BTW BEAM #1 AND #2 AT AFT CARGO DOOR AFT EDGE. SUMMARY OF NRC 00126: INNER PAN ON INTERNAL AFT EDGE BTW BEAM #1 AND #2 AT AFT CARGO COMPARTMENT DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R REPAIR 8. (LP #0561817)Sep 17, 2024 · N990AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024091809138Skin · crackedCRACK ON FUSELAGE EXTERNAL SKIN STA Y=1087 BTW L=13R AND L=14R. SUMMARY OF NRC 00047: CRACK ON FUSELAGE EXTERNAL SKIN STA Y=1087 BTW L=13R AND L=14R WAS REPAIRED PER ERA 619868-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ACCOMPLISH SECTION II. ACCOMPLISH REPESep 17, 2024 · N951AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2024091809136Pan · crackedCRACK ON PAN FWD EDGE IN LOWER SIDE AT FWD CARGO COMPARTMENT DOOR. RE-WRITE REASON: TECHNICAL REFERENCE USED DOES NOT APPLY TO FWD CARGO COMPARTMENT. ALSO, AFTER DOUBLERS REMOVED CRACKS WERE FOUND ON PAN BTW BEAM 1 AND 2 AND ELONGATED HOLES ON INNER/OUTER PAN.Sep 17, 2024 · N989AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024091809135Fastener · shearedFASTENER SHEARED OFF ON FRAME REAR SIDE STA Y=1152 AT AFT ACCESORY COMPARTMENT. SUMMARY OF NRC 00441: FRAME REAR SIDE STA Y=1152 AT AFT ACCESSORY COMPARTMENT WAS REPAIRED PER PRI 619773-14 REV 3 AND ERA 619773-14 REV ORIGINAL, SECTION I: PERMANENT REPAIR. ACCOSep 16, 2024 · N980AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2024091809134Fastener · shearedFASTENER SHEARED OFF ON FRAME REAR SIDE STA Y=1152 AT AFT ACCESORY COMPARTMENT. SUMMARY OF NRC 00441: FRAME REAR SIDE STA Y=1152 AT AFT ACCESSORY COMPARTMENT WAS REPAIRED PER PRI 619773-14 REV 3 AND ERA 619773-14 REV ORIGINAL, SECTION I: PERMANENT REPAIR. ACCOSep 16, 2024 · N980AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2024091609052Doubler · wornWEAR ON INTERNAL DOUBLER BETWEEN LOWER HINGE AND LOWER PAN OF AFT CABIN BULKHEAD DOOR. SUMMARY OF NRC 00289: INTERNAL DOUBLER BETWEEN LOWER HINGE AND LOWER PAN OF AFT CABIN BULKHEAD DOOR WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 16 REPAIR 16. (LP #05Sep 16, 2024 · N990AT · Boeing 717200 · Fuselage Main, StructureSDR HALA20240917046Unknown · odorPRIOR TO PUSH, BURNING RUBBER SMELL FROM CEILING VENT BEHIND COCKPIT DOOR. AWAITING MORE INFORMATION AND RESOLUTION.Sep 15, 2024 · N483HA · Boeing 717200 · Air Distribution SystemSDR DALA2024091609051Pan · crackedCRACK ON AFT PAN WAS FOUND BTW BEAM 1 AND 2 AT AFT CARGO DOOR (REF NRC NBR 00640). SUMMARY OF NRC 00693: AFT INNER PAN BTW BEAM 1 AND 2 AT AFT CARGO COMPARTMENT DOOR WAS REPAIRED PER ER/A 620224-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 620224-14 REVSep 15, 2024 · N989AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2025042003033Pan · damagedPD: INNER PAN DAMAGED AT UPPER FWD CORNER HINGE ATTACH POINT / CA: REPAIRED INNER PAN PER ERA 623397-14 REV ORIG REPAIRED INNER PAN PER ERA 623397-14 REV ORIG. (NO LP)Sep 14, 2024 · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024091809133Angle · crackedANGLE BRACKET AT STATION 1178.255 ABOVE L-9L CRACKED. REPLACED ANGLE BRACKET AT STATION 1178.255 ABOVE L-9L IAW B717 SRM 51-40-02 AND B DRAWING 5420838. INSTALLED LT & RT LOUVER PANELS. COMPLIED WITH INSP PER B717 W/C 5312-01194-01.Sep 14, 2024 · N943AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024091609050Longeron · crackedCRACK ON LONGERON 17LH SIDE STA=1022 AFT OF BULKHEAD. CRACK ON LONGERON 12RH SIDE STA=1022 FWD OF BULKHEAD. CRACK ON LONGERON 14 RH STA=1022 FWD OF BULKHEAD AT PAX CABIN. SUMMARY OF NRC 00380: LONGERON 17LH SIDE STA=1022 AFT OF BULKHEAD WAS REPAIRED PER B717-2Sep 14, 2024 · N990AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2024091809142Windshield · arcedENROUTE F/O WINDSHIELD WAS ARCING. FOLLOWED BY A "LEVEL 1 WSHLD HEAT FAIL" MESSAGE. RAN QRH CHECK LED US TO "WINDSHIELD CRACKED OR ARCING" CHECKLIST ON PAGE 3.13. PULLED CB Z-24. LOOKS LIKE A HAIRLINE CRACK ON OUTER PANE - UPPER PORTION OF WINDSHIELD. MAINTENASep 13, 2024 · N899AT · Boeing 717200 · Flight Compartment WindowsSDR DALA2024091609049Frame · crackedCRACKED FRAME (BOTH FACES) STA=1037 LONGERON 17 LH SIDE AT CPAX. SUMMARY OF NRC 00386: FRAME (BOTH FACES) STA=1037 LONGERON 17 LH SIDE AT CPAX WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 4 REPAIR 4. (LP #0554632)Sep 13, 2024 · N990AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2024091609048Doubler · corrodedCORROSION ON REPAIR DOUBLER OF JAMB WEB STA Y=954 AND LONG 29R AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00264: CORROSION LEVEL 2. JAMB WEB STA Y=954 AND LONG 29R AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 51-70-10-2R PRUCEDURE 2 REPAIR 2. (LP #0554Sep 13, 2024 · N990AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2024091308985Skin · crackedCRACKS WERE FOUND ON SKIN AT COCKPIT ON AFT UPPER CORNER CUTOUT SLIDING WINDOW. SUMMARY OF NRC 00718: CRACKS ON AFT UPPER CORNER CUTOUT SLIDING WINDOW ON SKIN AT COCKPIT WERE REPAIRED PER B-717-200 SRM 56-10-02-2R PROCEDURE 1 REP 1 FIG 201. PERFORM EXTERNAL GVSep 13, 2024 · N990AT · Boeing 717200 · Fuselage Main, Plate/Skin
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