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 DALA2024050905042Support Fitting · corrodedCORROSION ON R1 DOOR SLIDE GIRT BAR SUPPORT FITTINGS. ALSO CORROSION ON PANEL LOCATED BELOW FITTINGS. SUMMARY OF NRC 00426: CORROSION LEVEL 2. R1 DOOR SLIDE GIRT BAR SUPPORT FITTINGS AND PANEL LOCATED BELOW FITTINGS PANEL WERE FABRICATED AND REPLACED PER DRAWIMay 8, 2024 · N983AT · Boeing 717200 · Emergency EquipmentSDR DALA2024050905041Angle · corrodedCORROSION ON CUSP ANGLE AT FORWARD GALLEY SERVICE DOOR JAMB STA Y=157-200. SUMMARY OF NRC 00345: CORROSION LEVEL 2. CUSP ANGLE AT FORWARD GALLEY SERVICE DOOR JAMB STA Y=157-200 WAS REPAIRED PER PRI 617406-14 REV 2 AND ER/A 617406-14 REV ORIGINAL, SECTION I: PEMay 8, 2024 · N993AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024050805024Cusp Web · corrodedCORROSION ON LOWER SURFACE OF CUSP WEB AT STA Y 940 AND -X56 IN PAX CABIN. SUMMARY OF NRC 00594: CORROSION LEVEL 2. CORROSION ON CUSP WEB AT STA Y 940 AND -X56 IN PAX CABIN WAS REPAIRED PER B717 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4 FIGURE 209 CONFIGURATION-701May 8, 2024 · N974AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024050805023Intercostal · crackedCRACK ON INTERCOSTAL STA Y=636, X=0 AT C1. SUMMARY OF NRC 00183: INTERCOSTAL STA Y=636, X=0 AT C1 WAS REPAIRED PER B717-200 SRM 53-00-00-2R PROCEDURE 1. (LP #0331871)May 8, 2024 · N983AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024050805022Floor Support · corrodedCORROSION ON FLOOR SUPPORT BTW STA Y 157 TO 200 AND X=-43 AT PAX CABIN. SUMMARY OF NRC 00407: CORROSION LEVEL 2. FLOOR SUPPORT BTW STA Y 157 TO 200 AND X=-43 AT PAX CABIN WAS REPLACED AND INSTALLED PER DWG S2929169 REV WB AND B717 SRM 51-41-02-0G AND 51-41-05-May 7, 2024 · N993AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024050805021Seat Track · corrodedCORROSION ON SEAT TRACKS X=-22, X=-44.5 BTW STA Y=200 TO Y=215. SUMMARY OF NRC 00343: SEAT TRACKS X=-22, X=-44.5 BTW STA Y=200 TO Y=215 WERE REPAIRED PER B717-200 SRM 53-20-52-2R PROCEDURE 5 REPAIR 5. (LP #0331571)May 7, 2024 · N983AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2024050805020Cusp Web · corrodedCORROSION ON CUSP WEB LOWER AND UPPER SIDE IN SECTION STA Y: 832 TO 845 X: 56, PAX CABIN. SUMMARY OF NRC 00784: CORROSION LEVEL 2. CORROSION ON CUSP WEB STA Y: 832 TO 845 X: 56, PAX CABIN WAS REPAIRED PER B717 SRM 53-00-55-2R REPAIR 4, FIGURE 215. (LP #0331554May 7, 2024 · N974AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024050805019Frame · crackedCRACK ON FRAME CANTED KEEL BEAM AREA BTW STA Y 715, 674, AND 696 - L24R/26R AT LOWER FUSELAGE. SUMMARY OF NRC 00494: FRAMES CANTED KEEL BEAM AREA BTW STA Y 715, 674, AND 696 - L24R/26R AT LOWER FUSELAGE WERE REPAIRED PER B717 SRM 51-70-11-2R PROCEDURE 1 REPAIRMay 7, 2024 · N974AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2024050704974Floorbeam · corrodedCORROSION ON FLOOR SUPPORT STA 180 FROM X=-7 TO X=-44 AT PAX CABIN. SUMMARY OF NRC 00415: CORROSION LEVEL 2. FLOOR SUPPORT STA 180 FROM X=-7 TO X=-44 AT PAX CABIN WAS REPLACED AND INSTALLED PER DWG S2929169 REV B AND B717 SRM 51-41-02-0G AND 51-41-05-0G. (LP #May 7, 2024 · N993AT · Boeing 717200 · Fuselage Main, Floor BeamSDR DALA2024050704973Cusp Web · corrodedCORROSION ON CUSP WEB LOWER AND UPPER SIDE STA Y=526 AND Y=571 APPROX X=58 LH SIDE AT PAX CABIN (CPAX). SUMMARY OF NRC 00728: CORROSION LEVEL 2. CUSP WEB STA Y=526 AND X=58 WAS MEASURED ON LIGHTENING HOLE AND MATERIAL REMOVAL IS 0.100IN THERFORE IS WITHIN LIMIMay 6, 2024 · N974AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024050704972Cusp Web · crackedCRACK ON LOWER SURFACE OD CUSP WEB ON STAY 655 UNDER SEAT TRACK -X44 AT PAX CABIN. SUMMARY OF NRC 00591: CUSP WEB ON STAY 655 UNDER SEAT TRACK -X44 AT CABIN PAX WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4. (LP #0329495)May 6, 2024 · N974AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024050704971Cusp Web · crackedTWO CRACKS WERE FOUND ON RH CUSP WEB BTW STA Y=715 TO Y=737 AND -X=45 TO -X=60 IN PAX CABIN. SUMMARY OF NRC 00534: RH CUSP WEB BTW STA Y=715 TO Y=737 AND -X= 45 TO -X=60 IN CABIN PAX WAS REPAIRED PER B717 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4. (LP #0329432)May 6, 2024 · N974AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024050604957Cusp Web · corrodedCORROSION OUT OF LIMITS IN REF NRC 298, CUSP WEB BTW X=-56 TO -60 AND Y=294-313 AND STA 420 TO 437, STA 674, STA 889 ALSO ON RH CUSP WEB BTW STA X=-44 TO -56 WITH ORIGINAL THICKNESS IS 0.020" AND MINIMUM REMAINING THICKNESS IS 0.08". THEREFORE IT IS OUT OF LIMMay 4, 2024 · N983AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024050604958Heater · inoperativeLT WINDSHIELD ARCING. WINDOW HEAT INOP. REPLACED LEFT FLIGHT COMPARTMENT WINDSHIELD PER B717 AMM 56-11-02 420-801. (LP #5893976)May 3, 2024 · N929AT · Boeing 717200 · Windshield/Door Rain/Ice RemovalSDR DALA2024050604956Cusp Web · crackedCRACK ON CUSP WEB STA Y=225 AND X=56 AT PAX CABIN. SUMMARY OF NRC 00567: CUSP WEB STA Y=225 AND X=56 AT PAX CABIN WAS REPAIRED PER B717 SRM 53-00-55-2R-PROCEDURE 4 FIG 216. (LP #0325208)May 3, 2024 · N974AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024050604955Cusp Web · crackedCRACK ON CUSP WEB STA Y=657 AND Y=715 LH SIDE AT PAX CABIN. SUMMARY OF NRC 00599: CUSP WEB STA Y=657 AND Y=715 LH SIDE AT PAX CABIN WAS REPAIRED PER B717 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4. (LP #0325055)May 3, 2024 · N974AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024050604954Frame · crackedCRACK ON FRAME STA=Y 1178 APPROX BTW LONGERON 1L AND 2L AT AFT ACCESORY COMPARTMENT AREA. SUMMARY OF NRC 00401: FRAME STA=Y 1178 APPROX BTW LONGERON 1L AND 2L AT AFT ACCESORY COMPARTMENT AREA WAS REPAIRED PER B717 SRM 53-30-08-2R. PERFORM A VISUAL INSPECTION EMay 3, 2024 · N993AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2024050304923Battery Pack · faultedEXIT LIGHT OVER 1R DOOR AND EXIT LIGHT IN FRIST CLASS CABIN INTERMITIELY FLASHING. REPLACE THE EMERGENCY BATTERY & POWER SUPPLY UNIT LOCTION AT 247L PER B717 AMM 33-51. OPERATIONAL TEST WAS GOOD. (LP #5824217)May 3, 2024 · N922AT · Boeing 717200 · Emergency LightingSDR DALA2024050304922Floorbeam · crackedCRACK ON FLOOR BEAM STA Y=737 BELOW X=54 RH/LH AT PASSENGER FLOOR CABIN. SUMMARY OF NRC 00438: FLOOR BEAM STA Y=737 BELOW X=54 RH/LH AT PASSENGER FLOOR CABIN WERE REPLACED PER B717 SRM 51-41-02-0G, 51-41-05-0G, AND 51-41-08-0G. (LP #0323733)May 2, 2024 · N974AT · Boeing 717200 · Fuselage Main, Floor BeamSDR DALA2024050304921Floor Support · corrodedCORROSION ON FLOOR SUPPORT STA Y=150-200 X=7 RH, STA Y=200 X=7LH TO 7RH, AND STA Y=160 X=5LH TO 5RH AT PASSENGER CABIN (W1). SUMMARY OF NRC 00700: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=150-200 X=7 RH, STA Y=200 X=7LH TO 7RH, AND STA Y=160 X=5LH TO 5RH AT PASSMay 2, 2024 · N974AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2024050304920Skin · crackedCRACK INTERNAL FUSELAGE SKIN JUST AFT UPPER CORNER AT RH SLIDING WINDOW AREA. CPIL. SUMMARY OF NRC 00524: FUSELAGE SKIN JUST AFT UPPER CORNER AT RH SLIDING WINDOW AREA WAS REPAIRED PER PRI 617480-14 REV 1 AND ERA 617480-14 REV ORIGINAL SECTION I: PERMANENT REPMay 2, 2024 · N993AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2024052005348Flap System · malfunctionedSHIP 9558 -MISC/DE- FLIGHT TEST. EXPERIMENTAL TEST FLIGHT FOR FLAP 25 LANDINGS. FLIGHT PLANNED FOR ATL-HSV-ATL. BOEING TEST ENGR/PILOT IN LEFT SEAT AND DELTA LLCP IN RIGHT SEAT AT INITIAL TIME OF EVENT. CREW EXECUTED SIX APPROACHES AND THREE TOUCH AND GOES IN May 1, 2024 · N922AT · Boeing 717200 · Trailing Flap Position Indicating SystemSDR DALA2024050204890Bulkhead Web · crackedCRACKED BULKHEAD WEB STA Y=218, X=-8 AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00647: BULKHEAD WEB STA Y=218, X=-8 AT FWD CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 2. (LP #0321848)May 1, 2024 · N993AT · Boeing 717200 · Fuselage Main, BulkheadSDR DALA2024050204889Not Reported · scratched-AD- SCRATCHES WERE FOUND AT FWD/LH BARREL NUT HOLE HORIZONTAL STABILIZER. SUMMARY OF NRC 00666: FWD/LH BARREL NUT HOLE HORIZONTAL STABILIZER (HOLE #19) WAS REPAIRED PER PRI 617393-14 REV 1 AND ER/A 617393AD REV ORIG SECTION I: PERMANENT REPAIR. REPAIR APPROVAMay 1, 2024 · N923AT · Boeing 717200 · Horizontal Stabilizer Miscellaneous StructureSDR DALA2024050204888Pan · crackedCRACK ON AFT PAN ABOVE BEAM 1 OF FWD CARGO DOOR. SUMMARY OF NRC 00247: AFT PAN ABOVE BEAM 1 OF FWD CARGO DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1. (LP #0321706)May 1, 2024 · N983AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024050104840Battery Pack · no testON SERVICE CHECK THE EMERGENCY EXIT SIGN ABOVE THE L1 DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND POWER SUPPLY B5-235 PER B717 AMM 33-51. LIGHT OPERATION NOW CHECKS GOOD. THE AIRCRAFT IS OK FOR SERVICE. (LP #5307990)May 1, 2024 · N970AT · Boeing 717200 · Emergency LightingSDR DALA2024050204887Cusp Web · corrodedCORROSION ON RH CUSP WEB UPPER AND LOWER BTW STA 217-237 AT PAX CAB. SUMMARY OF NRC 00346: CORROSION LEVEL 2. RH CUSP WEB UPPER AND LOWER BTW STA 217-237 AT PAX CAB WAS FABRICATED PER B717-200 SRM 53-00-55-2R-4 REPAIR 4 FIG 209. REPLACED PER B717-200 SRM 53-00Apr 30, 2024 · N993AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024050104838Cusp Web · corrodedCORROSION CUSP WEB PREVIOUS REPAIR LOWER SIDE STA Y=471 LH SIDE AT PAX CABIN. SUMMARY OF NRC 00598: CORROSION LEVEL 2. PREVIOUS REPAIR PART (RING DOUBLER) WAS REPLACED PER B717 SRM 53-00-55-2R-4 REPAIR 4, PAR. 5, FIGURE 216 AND 51-41-02-0G. (LP #0320091)Apr 30, 2024 · N974AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024050104835Skin · corrodedCORROSION ON SETTLEMENT AREA OF RUB STRIP FUSELAGE SKIN BTW STA Y=870 RH TO 896.5 RH AND LONGERON 27RH FUSELAGE. SUMMARY OF NRC 00737: CORROSION LEVEL 2. FUSELAGE SKIN BTW STA Y=870RH TO 896.5RH AND LONGERON 27RH WAS REPAIRED PER B717 SRM 53-20-70-2R PROCEDUREApr 30, 2024 · N988AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2024050104834Computer · faultedBOTH FCC FAULTING BOTH REDUNDANT STOP SWITCHES ON DESCENT MULTIPLE FLIGHTS. VERIFY CONDITION AND SECURITY OF REDUNDANT RUDDER LIMITER RETURN SPRINGS. FOUND RUDDER LIMITER PUH ROD BINDING. REMOVED ROD AND REPLACED BOTH BEARINGS REF P.S. 900-9-1 #06. INSTALLRD RApr 30, 2024 · N899AT · Boeing 717200 · Flight Control SystemSDR DALA2024050104839Seal · cutSHIP 9569 -ATB- CABIN CREW STATED THAT THERE WAS A SLOW DEPRESSURIZATION OCCURRING DURING THE CLIMB OUT AFTER TAKEOFF. THE LEAD F/A PASSED OUT (REGAINED CONSCIOUSNESS LATER) AND ANOTHER FELT LIGHTHEADED. THE OXYGEN MASKS AT ROW 24DEF DID AUTOMATICALLY DEPLOY BApr 29, 2024 · N607AT · Boeing 717200 · Passenger/Crew DoorsSDR DALA2024050805018Intercostal · crackedCRACK ON INTERCOSTAL OF MECHANISM BTW BEAM #4 AND BEAM #5 OF L1 DOOR. SUMMARY OF NRC 00086: INTERCOSTAL OF MECHANISM BTW BEAM #4 AND BEAM #5 OF L1 DOOR WAS FABRICATED PER DOUGLAS AIRCRAFT COMPANY DWG 9955763 REV M AND REPLACE PER B717-200 SRM 51-41-02-0G. (LP Apr 28, 2024 · N983AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024043004795Cusp Web · corrodedCORROSION ON LH CUSP WEB ALSO WITH OIL SCAN ON THE SAME CUSP WEB BTW STA 889 TO STA 908 X=58 AT PAX CABIN. SUMMARY OF NRC 00396: CORROSION LEVEL 2. LH CUSP WEB ALSO WITH OIL SCAN ON THE SAME CUSP WEB BTW STA 889 TO STA 908 X=58 AT PAX CABIN WAS REPLACED PER B7Apr 27, 2024 · N993AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024043004794Floor Panel · corrodedCORROSION ON FLOOR PANEL 121TF, 121CF, AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00411: CORROSION LEVEL 2. CORROSION WAS FOUND ON FLOOR PANEL 121TF, 121CF, AT FWD CARGO COMPARTMENT. IN ACCORDANCE B717-200 SRM 51-10-04-0G PROCEDURE GENERAL FIG 2 THE PANELS WERE Apr 27, 2024 · N983AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2024043004793Angle · damagedCORROSION ON CLIP STA Y=1072 AND X=-16 LONGERON PROJECTION 18RH AT AFT EMERGENCY EXIT DOOR JAMB AREA. SUMMARY OF NRC 00381: CORROSION LEVEL 2. CLIP (GUSSET) STA Y=1072 AND X=-16 LONGERON PROJECTION 18RH AT AFT EMERGENCY EXIT DOOR JAMB AREA WAS REPLACED PER B71Apr 27, 2024 · N974AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024043004792Skin · damagedELONGATED HOLE ON VERTICAL STABILIZER LEADING EDGE LEFT SIDE, JUST ON THE CORNER WAS FOUND STA ZFS=52.267 IN REF NRC 0525. SUMMARY OF NRC 00611: HOLE ON VERTICAL STABILIZER LEADING EDGE LEFT SIDE, JUST ON THE CORNER WAS REPAIRED PER B717-200 SRM 55-30-01-2R PRApr 27, 2024 · N993AT · Boeing 717200 · Vertical Stabilizer, Plate/SkinSDR DALA2024043004791Cusp Web · corrodedCORROSION ON LOWER SURFACE OF LH CUSP WEB BTW STA 359-382. ALSO UPPER SURFACE BTW 660-664 PAX CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00315: CORROSION LEVEL 2. CUSP WEB ON STA 660-664 PAX CABIN FLOOR STRUCTURE WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 REPAIR 4Apr 26, 2024 · N983AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024043004790Release Cable · corrodedRUSTED CABLES AND ALL PINS ON TAILCONE RELEASE CABLE AND PULLEY MECHANISMS. ALSO BROKEN STRANDS OF CABLE AT 10 HRS POSITION. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY NRC 00180: CABApr 26, 2024 · N974AT · Boeing 717200 · Aerodynamic FairingsSDR DALA2024042604729Frame · corrodedCORROSION AT FRAME STA 869 BETWEEN L29L AND L29R AFT CARGO COMPARTMENT. SUMMARY OF NRC 00298: CORROSION LEVEL 2. FRAME STA 869 BETWEEN L29L AND L29R AFT CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-20-07-2R REPAIR 3. PERFORM VISUAL INSPECTION INITIAL 25,Apr 26, 2024 · N988AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2024042604728Pan · crackedCRACKS WERE FOUND ON PAN, BTW BEAMS 3/4 AND AFT SIDE AT AFT CARGO DOOR (C2). SUMMARY OF NRC 00348: AFT INNER PAN ON BEAM #3 AND BEAM #4 AT AFT CARGO COMPARTMENT DOOR WAS REPAIRED PER ER/A 617066-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 617066-14 REVApr 26, 2024 · N923AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024050104837None · none-AD- AMOC ER/A 617393-14AD MONITOR LOG REQUIRES DTA WITH NEW AMOC ON OR BEFORE THE NEXT 24 MONTHS AFTER 25-APR-2024. CONTACT LIAISON ENGINEERING, DEPT 555 FOR RESULTS. NOTE TO MONITOR RECORDS / PLANNING. DISCONTINUE REVENUE SERVICE ON OR BEFORE THE NEXT 24 MApr 25, 2024 · N923AT · Boeing 717200 · Standard Practices/StructuresSDR DALA2024050104836None · none-AD- DTA ER/A 616393-14AD MONITOR LOG REQUIRES DTA APPROVAL ON OR BEFORE THE NEXT 24 MONTHS AFTER 25-APR-2024. CONTACT LIAISON ENGINEERING, DEPT 555 FOR RESULTS. NOTE TO MONITOR RECORDS / PLANNING . DISCONTINUE REVENUE SERVICE ON OR BEFORE THE NEXT 24 MONTHSApr 25, 2024 · N923AT · Boeing 717200 · Standard Practices/StructuresSDR DALA2024043004789Cusp Web · corrodedCORROSION ON CUSP WEB BTW STA Y 188\X=58, Y257/X=59, Y275/X=59, Y313/X=59 AT LH CABIN PAX. SUMMARY OF NRC 00650: CORROSION LEVEL 2. CUSP WEB BTW STA Y257/X=59, Y275/X=59, Y313/X=59 AT LH CABIN PAX WERE REPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 2 REPAIR 2Apr 25, 2024 · N983AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024042604727Pan · crackedCRACK ON FWD PAN ABOVE BEAM 3 OF FWD CARGO DOOR. SUMMARY OF NRC 00246: FWD PAN ABOVE BEAM 3 OF FWD CARGO DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1. (LP #0312268)Apr 25, 2024 · N983AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024042504694Power Supply · no testDURING THE SERVICE CHECK, THE EMERGENCY LIGHTS AT THE CATWALK WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY B5-237 PER B717 AMM 33-51-03. (LP #5853294)Apr 25, 2024 · N943AT · Boeing 717200 · Emergency LightingSDR DALA2024042604730Cover · missingTHE CABIN CEILING EMERGENCY STANDBY LIGHT LENS COVER IS MISSING AT SEAT ROW 3. MAINTENANCE FORWARDED IT TO NEF 33-21-02. CABIN LIGHT LENS MISSING SEAT ROW 3. (LP #0309494)Apr 24, 2024 · N938AT · Boeing 717200 · Emergency LightingSDR DALA2024042504693Floor Support · corrodedCORROSION ON FLOOR SUPPORTS AT STA Y=177 TO 200 X=9 AND STA Y=200 X=11 AT PAX CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00626: CORROSION LEVEL 2. FLOOR SUPPORTS AT STA Y=177 TO 200 X=9 AND STA Y=200 X=11 AT PAX CABIN FLOOR STRUCTURE WERE FABRICATED PER B717 DWG 99Apr 24, 2024 · N988AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024042504692Window Frame · crackedCRACK ON AFT UPPER CORNER OF RH SLIDING WINDOW FRAME AT FLIGHT DECK INTERNAL SKIN. SUMMARY OF NRC 00692: AFT UPPER CORNER OF RH SLIDING WINDOW FRAME AT FLIGHT DECK INTERNAL SKIN WAS REPAIRED PER B717-200 SRM 56-10-02-2R PROCEDURE.1. PERFORM VISUAL INSPECTION EApr 24, 2024 · N988AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2024042504691Window Frame · crackedCRACK ON AFT UPPER CORNER OF RH SLIDING WINDOW FRAME AT FLIGHT DECK INTERNAL SKIN. SUMMARY OF NRC 00692: AFT UPPER CORNER OF RH SLIDING WINDOW FRAME AT FLIGHT DECK INTERNAL SKIN WAS REPAIRED PER B717-200 SRM 56-10-02-2R PROCEDURE.1. PERFORM VISUAL INSPECTION EApr 24, 2024 · N988AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2024042404676Lens · missingTHE CABIN CREW NOTED THAT THE AFT TAIL COMPT EMERGENCY EXIT LIGHT LENS IS MISSING. MAINTENANCE INSTALLED THE MISSING LIGHT COVER AT AFT TAIL OF AIRCRAFT. THE AIRCRAFT IS NOW OK FOR SERVICE. (LP #5829167)Apr 24, 2024 · N928AT · Boeing 717200 · Emergency Lighting
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