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 DALA2023061304795Unknown · unknownCRACKED MEMBRANE BTW STA Y=172 AND Y=187 APROX AND X54 AT CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00577: MEMBRANE BTW STA Y=172 AND Y=200 APROX AND X54 AT CABIN FLOOR STRUCTURE WAS REPLACED PER DRAWING 9936534-5 REV BW AND PER B717-200 SRM 51-41-05-0G AND 51-41-Jun 13, 2023 · N899AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2023061604906Unknown · unknownSHIP 9547 -ATB/GEAR/DE- THE FLIGHT CREW RETURNED THE AIRCRAFT TO ATL FOLLOWING A "RIGHT GEAR DOOR OPEN" INDICATION AND A "RIGHT GEAR UNSAFE" LIGHT ON CLIMB OUT. AN EMERGENCY WAS DECLARED BY THE CREW. THE GEAR POSITION SHOWED GOOD DOWN AND LOCKED INDICATIONS ANJun 12, 2023 · N998AT · Boeing 717200 · Landing Gear SystemSDR 2023F00200Disc · crackedMULTIPLE MICRO CRACKS FOUND ON OUTER AIR SEAL F THE LONGEST ONE HAS A RADIAL LENGTH 0.021 INCHES.Jun 12, 2023 · N991AT · Boeing 717200 · Turbine SectionSDR DALA2023061304794Unknown · unknownCORROSION ON INTERNAL REPAIR DOUBLERS BTW STA 966/1000 AND BTW STR 28L/25L APROX AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00158: CORROSION LEVEL 2. REPAIR WAS PERFORMED PER PRI 525610-14 REV 2 AND ERA 525610-14 REV A. SECTION II PERMANENT REPAIR. ACCOMPLIJun 12, 2023 · N926AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2023061504881Unknown · unknownAT CRUISE, MULTIPLE SPARKS ON CENTER WINDSHIELD AND CRACK FORMED. TURNED ANTI-ICE OFF PER QRH PROCEDURE. REMOVED CENTER WINDSHIELD IAW B717 AMM 56-11-01. REPLACED CENTER WINDOW HEAT CONTROLLER IAW AMM 30-41-01 A2-10. REPLACED THE CENTER WINDOW PER B717 AMM 56-Jun 11, 2023 · N953AT · Boeing 717200 · Flight Compartment WindowsSDR DALA2023061504876Unknown · unknownCORROSION ON FLOOR SUPPORT STA Y=215 TO 157 X54, X44, X7, X-7, X-44, X-54, X-55 CPAX (W1). SUMMARY OF NRC 00409: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=215 TO 157 X54, X44, X7, X-7, X-44, X-54, X-55 CPAX (W1) WERE REPLACED PER DWG 9936534 REV BW AND PER B717-2Jun 11, 2023 · N899AT · Boeing 717200 · Fuselage Floor PanelSDR HALA2023061200032Unknown · unknownBRAKE PRES LO INDICATED WHEN SETTING THE PARKING BRAKE W/ HYD AUX AND TRANS PUMPS IN THE OFF POSITION AT THE GATE. REMOVED AND REPLACED THE LEFT BRAKE ACCUMULATOR PER TASK 32-44-01. OPS CHECKED NORMAL AND OK FOR SERVICE.Jun 11, 2023 · N483HA · Boeing 717200 · Landing Gear SystemSDR DALA2023061304796Unknown · unknownBOTH OVER-WING EMERGENCY EXIT LIGHTS ONLY ILLUMINATE FOR A FEW SECONDS BEFORE GOING OUT. MAINTENANCE REPLACED THE OVERWING EMERGENCY EVACUATION LIGHT BATTERY PER B717 AMM 33-51-06-401. BOTH OVERWING EMERGENCY LIGHTS NOW WORK CORRECTLY. (LP #9963359)Jun 10, 2023 · N998AT · Boeing 717200 · Emergency LightingSDR DALA2023061304793Unknown · unknownCORROSION ON FLOOR SUPPORT BTW L28R TO L28L STA 375 AT FWD CARGO COMPARTMENT C-1. SUMMARY CORROSION LEVEL 2. FLOOR SUPPORT BTW L28R TO L28L STA 375 AT FWD CARGO COMPARTMENT C-1 WAS REPLACED PER B717-200 SRM 51-40-02-0G. (LP #2809951)Jun 10, 2023 · N924AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2023061304792Unknown · unknownCRACK ON DOOR BEAM #1 STA Y=162 AT PASSENGER ENTRANCE DOOR L1. SUMMARY OF NRC 00140: DOOR BEAM #1 STA Y=162 AT PASSENGER ENTRANCE DOOR L1 WAS REPAIRED PER B717-200 SRM 52-10-02-2R REPAIR 7. (LP #2809935)Jun 10, 2023 · N957AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023061304791Unknown · unknownCORRODED OUT OF LIMITS IN REF TO NRC 339: CORROSION ON FLOOR SUPPORT BTW STA 200 AND -X=46 TO -X=57 AT PAX CAB. SUMMARY OF NRC 00584: NEW FLOOR SUPPORT BTW STA 200 AND -X=46 TO -X=57 WAS INSTALLED, ADJUSTED, AND DRILLED PER B717-200 SRM 51-40-08- 0G GENERAL ANJun 10, 2023 · N899AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023061304790Unknown · unknownCORROSION ON SUPPORT ANGLES ON STA 271.5, 291, 305, 311, 539, 647, 847, 874, 883, AND 924 AT CUSP WEB LH. SUMMARY OF NRC 00143: CORROSION LEVEL 2. NEW CLIPS WERE INSTALLED PER B717-200 SRM 51-41-02-0G. (LP #2808532)Jun 9, 2023 · N924AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023061304789Unknown · unknownCORROSION ON WEB FROM STA Y 155 TO 200 AND FROM X 20 TO X-60 AT R1 DOOR LOWER DOOR JAMB. IN REF NRC 00531. SUMMARY OF NRC 00549: CORROSION LEVEL 2. WEB FROM STA Y 155 TO 200 AND FROM X 20 TO X-60 AT WAS REPLACED PER B717-200 SRM 51-41 -02-0G AND 51-41-05-0G. (Jun 9, 2023 · N899AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023061304788Unknown · unknownAFTER CORROSION REMOVAL ON OTBD SEAT TRACK LH ON STA Y:577 TO 578 AT PAX CABIN, THE TRACK WAS FOUND OUT OF LIMITS. SUMMARY OF NRC 00500: CORROSION LEVEL 2. SEAT TRACK LH OUT OF LIMITS ON STA Y:577 TO 578 AT CABIN PAX WAS REPAIRED PER B717-200 SRM 53-20-52-2R PJun 9, 2023 · N919AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR 2023F00187Gearshaft · abnormalON FEBRUARY 10, 2023 THIS AGB WAS RECEIVED BY STS MAINTENANCE ORGANIZATION (EASA FR.145.0229) FOR AN OVERHAUL (NOT RELATED TO THIS EVENT) FROM CUSTOMER ROLLS-ROYCE NORTH AMERICA. THIS AGB WAS NEVER SERVICED BY STS BEFORE. DURING DISASSEMBLY, IT WAS OBSERVED TJun 9, 2023 · Boeing 717200 · Engine (Turbine/Turboprop)SDR DALA2023060904690Unknown · unknownCRACK INDICATION ON L/H VERT STAB ON HOLE 5 FROM BOTTOM -MARKED-. CONFIRMED CRACK IS IN SKIN LAYER ONLY QC5253. REMOVED LEADING EDGE VERTICAL STAB REF. B717, AMM 55-32-01. C/W ERA 609501-14AD REV ORIGINAL PERMANENT REPAIR SECTION I QC5270. REINSTALLED LEADING Jun 8, 2023 · N977AT · Boeing 717200 · Vertical Stabilizer, Plate/SkinSDR DALA2023060904689Unknown · unknownCRACK INDICATION ON L/H VERT STAB ON HOLES 5 FROM BOTTOM -MARKED-. C/W PRI 609501-14AD REV 0 AND 1 QC 5270. C/W PRI 609501-14AD REV 2 QC 5270. FINAL ERA 609501-14AD REV ORIGINAL MATCHES ALL STEPS OF PRI 609501-14AD REV 0, 1, AND 2 QC 5270. ASSOCIATED ER/A 14-6Jun 8, 2023 · N977AT · Boeing 717200 · Vertical Stabilizer, Plate/SkinSDR DALA2023060904692Unknown · unknownRAMP REPORTED DAMAGE TO AFT CARGO DOOR CUTOUT. FOUND DAMAGE TO PREVIOUS REPAIR SPLICE ONLY. REMOVED SPLICE TO PREPARE FOR REPLACEMENT. NO OPEN HOLE REQUIRED. INSTALLED REPAIR PER B717 SRM 53-20-15-2R PROC 4 PERMENANT REPAIR. (LP #4798350)Jun 7, 2023 · N988AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2023060804667Unknown · unknownCORROSION ON WEB FROM STA 218 TO 237, X -55 TO 44:5 AT W1 IN REF NRC 531. CPAX. SUMMARY OF NRC 00546: CORROSION LEVEL 2. WEB FROM STA 218 TO 237, X -55 TO 44:5 AT W1 WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4 FIG 226 AND SRM 51-41-02-0G. (LJun 7, 2023 · N899AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023060804666Unknown · unknownCORROSION ON INTERCOSTAL BTW STR 30 AND STR 29RH FROM STA Y=946 TO 954 AT AFT CARGO. SUMMARY OF NRC 00275: CORROSION LEVEL 2. NEW INTERCOSTAL WAS REPLACED PER B717 SRM 51-41-02-0G PAR 4. (LP #2804838)Jun 7, 2023 · N924AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2023060804665Unknown · unknownCRACK INDICATION AT OVERWING FRAME TAB STA 674 RT SIDE, MARKED (FLOOR LEVEL). SUMMARY SEE NRC 073-0004:5310-01436-01D/002 00055: REPLACED DAMAGED FRAME ON WC 5310-01436-03B. (LP #2804708)Jun 7, 2023 · N951AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023060804664Unknown · unknownERODED MATERIAL ON FUSELAGE SKIN BTW STA 992 AND LONGERON 25R APPROX (DOOR CUTOUT). SUMMARY OF NRC 00214: FUSELAGE SKIN BTW STA 992 AND LONGERON 25R APPROX (DOOR CUTOUT) WAS REPAIRED PER B717-200 SRM 53-20-15-2R PROCEDURE 12 REPAIR 12 PAR 6 OPTION 1, FIGURE 20Jun 7, 2023 · N899AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2023060704647Unknown · unknownEXIT SIGN AT FRONT OF CABIN IS BROKEN OFF FROM THE CEILING AND IS HANGING BY THE WIRES. MAINTENANCE REPLACED THE FWD CABIN SIGN PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. AIRCRAFT IS OK FOR SERVICE. (LP #9962890)Jun 6, 2023 · N925AT · Boeing 717200 · Emergency LightingSDR DALA2023060704645Unknown · unknownTHE EMERGENCY BATTERY PACK B5-120 DIES. MAINTENANCE REPLACED THE B5-120 EMERGENCY LIGHT BATTERY PACK PER B717 AMM 33-51. (LP #4688714)Jun 6, 2023 · N981AT · Boeing 717200 · Emergency LightingSDR DALA2023060704644Unknown · unknownCRACK FRAME OF LH AFT LAVATORY ENGINE PYLON SUPPORT BULKHEAD, STA 1022 AND LONGERON 7 LH. SUMMARY OF NRC 00231: FRAME OF LH AFT LAVATORY ENGINE PYLON SUPPORT BULKHEAD, STA 1022 AND LONGERON 7 LH WAS REPAIRED PER PRI 608989-14 REV. 0 AND ER/A 608989-14 REV ORIGJun 6, 2023 · N899AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023060704643Unknown · unknownCORROSION ON WEB PRODUCTION DOUBLER FROM STA 157 TO 178 AT R1 DOOR LOWER JAMB. W1. SUMMARY OF NRC 00550: CORROSION LEVEL 2. WEB PRODUCTION DOUBLER FROM STA 157 TO 178 AT R1 DOOR LOWER JAMB W1 WAS REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP #2803Jun 6, 2023 · N899AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2023060604564Unknown · unknownFOUND THAT THE EMERGENCY LIGHT IN ROW 20 WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK B5-230. OPERATIONAL CHECK WAS GOOD PER B717 AMM 33-51. (LP #9964533)Jun 6, 2023 · N943AT · Boeing 717200 · Emergency LightingSDR DALA2023060704646Unknown · unknownSHIP 9543 -DIV/DE- THE CREW DIVERTED THE AIRCRAFT TO MEM AND DECLARED AN EMERGENCY ON APPROACH DUE TO THE RIGHT GENERATOR FAILING AND THE APU ALREADY ON MEL DEFERRAL. CORRECTIVE ACTION: MAINTENANCE REPLACED THE APU ECU, THE RIGHT PCDU, THE LEFT & RIGHT BUS TIEJun 5, 2023 · N978AT · Boeing 717200 · Airborne Auxiliary Power Unit (APU) SystemSDR DALA2023060704642Unknown · unknownLONGERON AT 11R FWD OF FRAME STA 674" REQUIRES REMOVAL FOR ACCESS TO MAKE FRAME REPLACEMENT AT STA. 674". SUMMARY SEE NRC 129-0002:5310-01436-03B/003 00293: COMPLIED WITH ERA 530437-14MA REV ORIG FOR REPAIR OF LONGERON AT 11R FWD OF FRAME STA 674". (LP #280181Jun 5, 2023 · N951AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023060604563Unknown · unknownSHIP 9543 -DIV/DE- THE CREW DIVERTED THE AIRCRAFT TO MEM AND DECLARED AN EMERGENCY ON APPROACH DUE TO THE RIGHT GENERATOR FAILING AND THE APU ALREADY ON MEL DEFERRAL. CORRECTIVE ACTION: MAINTENANCE REPLACED THE APU ECU, THE RIGHT PCDU, THE LEFT & RIGHT BUS TIEJun 5, 2023 · N978AT · Boeing 717200 · AC Generator-AlternatorSDR DALA2023060604561Unknown · unknownAFTER P DOME STIFFENER REMOVAL, 4 HOLE LOCATIONS WERE NOTED TO BE MISSDRILED. IN REF TO NRC 00209. SUMMARY OF NRC 00566: HOLES (4 LOCATIONS) WERE REPAIRED PER PRI 608965-14 REV. 1 AND ER/A 608965-14AD REV. ORIGINAL, SECTION I: PERMANENT REPAIR. (LP #2802136)Jun 5, 2023 · N926AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023060804663Unknown · unknownCRACK ON FLOOR PANEL OF FWD CARGO COMPARTMENT. SUMMARY OF NRC 00499: FLOOR PANEL OF FWD CARGO COMPARTMENT WAS MANUFACTURED PER ER/A 591778-14TR REV ORIGINAL SECTION I PERMANENT REPAIR. PANEL INSTALLED PER AMDS 2040-0006. ASSOCIATED ER/A 14-591778 ADDED FOR AC Jun 4, 2023 · N924AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2023060604562Unknown · unknownAFTER PARKING AT GATE IT WAS DISCOVERED THAT METAL LANYARD AND BRACKET WAS DISCONNECTED FROM FWD MAIN CABIN DOOR SLIDE. THIS WOULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. REINSTALLED 1L DOOR SLIDE LANYAJun 4, 2023 · N954AT · Boeing 717200 · Escape SlideSDR DALA2023060604560Unknown · unknownCRACK ON DOOR BEAM #2 STA Y=163 AT PASSENGER DOOR 1 LEFT. SUMMARY OF NRC 00163: BEAM #2 STA Y=163 AT PASSENGER DOOR 1 LEFT WAS REPAIRED PER B717-200 SRM 52-10-02-2R REPAIR 8. (LP #2800335)Jun 4, 2023 · N919AT · Boeing 717200 · Passenger/Crew DoorsSDR DALA2023060604559Unknown · unknownCRACK ON FRAME ANGLE BTW STA Y=1022 AND L-12RH TO L-14RH AT PASSENGER CABIN. SUMMARY OF NRC 592: FRAME ANGLE BTW STA Y=1022 AND L-12RH TO L-14RH WAS REPLACED PER DWG 9912243 REV JS. (LP #2800077)Jun 4, 2023 · N924AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2023060604558Unknown · unknownCORROSION ON FWD AND AFT REPAIRS SPLACE DOUBLERS DOOR JAMB AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00100: CORROSION LEVEL 2. FWD AND AFT REPAIR SPLICE DOUBLERS AT AFT CARGO COMPARTMENT DOOR JAMB (C2) WERE REPLACED PER B717-200 SRM 53-20-15-2R-7, 51-41-05Jun 3, 2023 · N919AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2023060604557Unknown · unknownGOUGE WAS FOUND ON PERMANENT REPAIR BTW STA Y=243 AND 3" ABOVE OF LONGERON 17L AT FUSELAGE. SUMMARY OF NRC 00283: DOUBLER ON PERMANENT REPAIR BTW STA Y=243 AND 3" ABOVE OF LONGERON 17L AT FUSELAGE WAS REPLACED PER B717 SRM 53-00-01-2R PROCEDURE 6. PERFORM A GVJun 3, 2023 · N919AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2023060604556Unknown · unknownCORROSION ON LH/RH CUPS WEB MEMBRANE AT STA Y=1045 AT CPAX CABIN. SUMMARY OF NRC 00369: CORROSION LEVEL 2. LH/RH CUPS WEB MEMBRANE AT STA Y=1045 AT CPAX CABIN WERE REPLACED PER DWG 9981474 REV L AND B717-200 SRM 51-41-01-0G, 51-41-02-0G, AND 51-41 -05-0G. (LP Jun 3, 2023 · N924AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023060604555Unknown · unknownCORROSION ON CHORD ANGLE AT AFT PRESSURE BULKHEAD LOWER AREA (FWD FACE) STA Y=1053 BTW LONG 28LH-28RH AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00208: CORROSION LEVEL 2. ANGLE AT AFT PRESSURE BULKHEAD LOWER AREA (FWD FACE) STA Y=1053 BTW LONG 28LH-28RH WERJun 2, 2023 · N926AT · Boeing 717200 · Nacelle/Pylon StructureSDR DALA2023060204426Unknown · unknownCRACK ON CUSP MEMBRANE (WEB) X=56 AND STA 611 AT CPAX. CRACK WAS REPAIRED PER B-717-200 SRM 53-00-55-2R PROCEDURE 4 PAR 5 FIG 204. (LP #2795916)Jun 2, 2023 · N919AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023060204427Unknown · unknownSHIP 9522 -MISC/DE- DURING APPROACH FOR LANDING, THE "BUS DC R OFF" INDICATION ILLUMINATED. WHICH WAS FOLLOWED BY 15 OTHER DISCREPANCY INDICATIONS. THE QRH WAS COMPLIED WITH AND THE CREW DECLARED EMERGENCY DUE TO THE IMPENDING NO FLAP AND NO SLAT LANDING. A HOJun 1, 2023 · N963AT · Boeing 717200 · Electrical Power SystemSDR DALA2023060204425Unknown · unknownDELAMINATION AND BROKEN COMPOSITE MATERIAL AND SHEET ON FWD CARGO FLOOR PANEL 121CF AND 121NF (C1). SUMMARY OF NRC 00376: FWD CARGO FLOOR PANEL 121CF AND 121NF WERE MANUFACTURED PER ERA 544901-14 REV A PAR 6. AND FIGURE 5 AND ERA 591778-14TR REV ORIGINAL SECTIJun 1, 2023 · N899AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2023060104390Unknown · unknownCRACK ON FRAME STA 1037 BTW LONG-16 LH TO LONG-17 AT PAX CABIN. SUMMARY OF NRC 00534: FRAME STA 1037 BTW LONG-16 LH TO LONG-17 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 4, REPAIR 4. (LP #2794265)Jun 1, 2023 · N899AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023060104389Unknown · unknownCORROSION ON CUSP WEB BTW STA=201 TO STA=220 RH SIDE AT CABIN PAX. SUMMARY OF NRC 00422: CORROSION LEVEL 2. CUSP WEB WAS REPLACED PER B717 SRM 53-10-51-0I FIG 1 SHEET 2 ITEM 32. (LP #2794167)Jun 1, 2023 · N926AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023060104388Unknown · unknownSEVERE CORROSION ON GALLEY SERVICE DOOR CUSP ANGLE STA 168 TO 201 X=-44 TO X=-60. SUMMARY OF NRC 374: CORROSION LEVEL 2. CUSP ANGLE OF GALLEY SERVICE DOOR STA 168 TO 201 X=-44 TO X=-60 WAS REPAIRED PER PRI 608340-14 REV 1 AND ER/A 608340-14 REV ORIGINAL. (LP #Jun 1, 2023 · N926AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023060104387Unknown · unknownCRACK ON FRAME CLIP OVER STA Y=1022 AND LONGERON 7LH AT CPAX (CPAX). SUMMARY OF NRC 00215: FRAME CLIP OVER STA Y=1022 AND LONGERON 7LH WAS REPAIRED PER PRI 608496-14 REV 0 AND ER/A 608496-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-608496 AJun 1, 2023 · N926AT · Boeing 717200 · Fuselage Structure (General)SDR DALA2023060104386Unknown · unknownCRACK ON FRAME CLIP OVER STA Y=1022 AND LONGERON 7 RH AT CPAX (CPAX). SUMMARY OF NRC 00210: FRAME CLIP OVER STA Y=1022 AND LONGERON 7 RH WAS REPAIRED PER PRI 608496-14 REV 0 AND ER/A 608496-14 REV ORIGINAL, SECTION I: PERMANENT REPAIR. (LP #2794144)Jun 1, 2023 · N926AT · Boeing 717200 · Fuselage Structure (General)SDR DALA2023060104385Unknown · unknownCRACK ON CUSP MEMBRANE (WEB) X=44 AND STA 636 AT CPAX. SUMMARY OF NRC 00431: CRACK ON CUSP MEMBRANE (WEB) X=44 AND STA 636 AT CPAX WAS REPAIRED PER B717-200 SRM 55-00-55-2R PROCEDURE 4 PAR 5 FIG 217. (LP #2793591)May 31, 2023 · N919AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023060104384Unknown · unknownCORROSION ON FLOOR SUPPORT RBL 54 STA Y=1050 AND Y=1054 AT CPAX CABIN. SUMMARY OF NRC 00374: CORROSION LEVEL 2. FLOOR SUPPORT RBL 54 STA Y=1050 AND Y=1054 AT CPAX CABIN WAS REPLACED PER DWG 9981474 REV L AND B717-200 SRM 51-41-05-0G. (LP #2793392)May 31, 2023 · N924AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023053104339Unknown · unknownNOTED CRACK INDICATIONS IN 6 HOLES BELOW EXISTING REPAIR (MARKED). REF AA 5530-01048-02 STEP 8, AA 2018-10 -08. SEPARATED LAYERS REF STEP 9 OF AA CARD 5530-01048-02. CONFIRMED CRACKS ARE IN SKIN ONLY (7 EA). INSTALLED REPAIR DOUBLER PER ERA 609262-14 AD REV ORMay 31, 2023 · N980AT · Boeing 717200 · Vertical Stabilizer, Plate/Skin
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