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 DALA2023080806440Unknown · unknownTHE PILOT NOTICED THE 1L DOOR GIRT BAR TETHER STRAP WAS LOOSE. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE REATTACHED THE STRAP BUCKLE. OPERATIONAL CHECK WAS GOOD. (LP #4498172)Aug 4, 2023 · N954AT · Boeing 717200 · Emergency EquipmentSDR DALA2023080806436Unknown · unknownWEAR ON FWD/AFT LATCH FITTINGS AT AFT CARGO DOOR. SUMARY OF NRC 00135: THE LATCH FITTINGS AT AFT/FWD AT AFT CARGO DOOR WERE REPLACED PER BOEING CMM 52-30-2. (LP #2901739)Aug 4, 2023 · N957AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2023080706365Unknown · unknownNICKS ON DOUBLER REPAIR BTW STA Y=996 TO Y=1002. SUMMARY OF NRC 099: 2ND. DOUBLER WAS REPLACED PER B717-200 SRM 53-20-15-2R PROCEDURE 10 FIGURE 202. PERFORM VISUAL INSPECTION EACH 8000 CYCLES PER B 717-200 SRM 53-20-15-2R PROCEDURE 10 PAR 7 TABLE 202. (LP #290Aug 4, 2023 · N959AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023080706364Unknown · unknownCRACK ON WEB INSIDE STRUCTURE AFT EMERGENCY DOOR AT CABIN PAX. SUMMARY OF NRC 0170: WEB INSIDE STRUCTURE AFT EMERGENCY DOOR AT CABIN PAX WAS REPAIRED PER B-717-200 SRM 55-00-00-2R REPAIR 1 FIG 201. (LP #2901626)Aug 4, 2023 · N959AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023080706363Unknown · unknownCORROSION OUT OF LIMITS ON STA=994 TO STA=1053. ORIGINAL THICKNESS OF 0.052 IN. AND MINIMUM REMAINING THICKNESS IS 0.009 IN ON SIDE PARTS, THEREFORE AREAS ARE OUT OF LIMITS PER B717 SRM 53-20-52-1A PROCEDURE 2 ALLOWABLE DAMAGE 2 PAR 4 FIG 101 AND PER DC-MD/BOEAug 4, 2023 · N922AT · Boeing 717200 · Fuselage Structure (General)SDR DALA2023080706362Unknown · unknownDAMAGE T: DURING JACK REACTION AND CENTER OF GRAVITY FOR NOSE LANDING GEAR STRUT SEAL REPLACEMENT, CRACK WAS FOUND FROM STA Y=371 TO Y=375 BTW LONG 30 TO LONG 29 RH AT EXTERNAL FUSELAGE SKIN IN REF AMDS 3221-4002. SUMMARY OF NRC 00084: EXTERNAL FUSELAGE SKIN FAug 4, 2023 · N978AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2023080706361Unknown · unknownCORROSION ON FLOORS SUPPORTS (9 EA) LH SIDE: #1 FROM STA Y=160 TO STA Y=197 AND +X=55, #2 FROM STA Y=200 AND +X 55, #3 FROM STA Y=186 TO STA Y=195 AND +X=52, #4 FROM STA Y=160 TO STA Y=197 AND +X44, #5 FROM STA Y=180 AND +X=25, #6 FROM STA Y=195 TO STA Y=200 AAug 4, 2023 · N922AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023080406302Unknown · unknownHOLE AT UPPER SKIN AND PROTUBERANCE AT LOWER SKIN OF RH ELEVATOR BETWEEN XHS 122.241 AND XHS 104.000 (ER/A RELATED 610064-14). SUMMARY OF NRC 00460: UPPER SKIN AND PROTUBERANCE AT LOWER SKIN OF RH ELEVATOR BETWEEN XHS 122.241 AND XHS 104.000 WAS REPAIRED PER BAug 4, 2023 · N922AT · Boeing 717200 · Elevator, Plate/SkinSDR DALA2023080406301Unknown · unknownCRACK ON AFT BULKHEAD DOOR JAMB (UPPER AREA) STA Y=1060 PROJECTION LONGERON 1 AT AFT PAX CABIN. SUMMARY OF NRC 00286: AFT BULKHEAD DOOR JAMB (UPPER AREA) STA Y=1060 PROJECTION LONGERON 1 AT AFT PAX CABIN WAS REPAIRED PER ER/A 610327-14 REV ORIGINAL SECTION I: Aug 4, 2023 · N603AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2024080807883Unknown · unknownDTE REQUIRED WITHIN 12 MONTHS OF ER/A 610692-14 ACCOMPLISHMENT ASSOCIATED ER/A 00-610692 ADDED FOR AC 9543. ER/A 610692-14, REV IR. DTE RESTRICTION IS FOR 12 MONTHS OF SERVICE. RTS DATE AT TIME OF REPAIR ACCOMPLISHMENT WAS 10AUG23. THEREFORE, THIS LP IS UPDATEAug 3, 2023 · N978AT · Boeing 717200 · Standard Practices/StructuresSDR DALA2023080406303Unknown · unknownTHE CENTER AISLE OVERHEAD RED EXIT SIGN IS BROKEN AND MISSING THE BACK HALF OF THE SIGN. MAINTENANCE REPLACED THE SIGNAGE. OPERATIONAL CHECK OF THE SIGN WAS NORMAL. THE AIRCRAFT IS OK FOR SERVICE. (LP #4398332)Aug 3, 2023 · N963AT · Boeing 717200 · Emergency LightingSDR DALA2023080406300Unknown · unknownCORROSION ON INTERNAL SKIN BTW STA 655 TO 658 AND LONG 29LH TO 29RH BILGE AREA AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00611: CORROSION LEVEL 2. CORROSION ON INTERNAL SKIN BTW STA 655 TO 658 AND LONG 29LH TO 29RH BILGE AREA AT FWD CARGO COMPARTMENT WAS REPAIRAug 3, 2023 · N603AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2023080406295Unknown · unknownCORROSION ON FRAME STA 1037 BETWEEN LONGERON 24 TO LONGERON 21 LH AT AFT CARGO COMPARTMENT IS OUT LIMITS WITH 0.040 IN PER B717-200 SRM 53-00-00-1A ALLOWABLE DAMAGE GENERAL PAR. 4. C. FIGURE 103. SUMMARY OF NRC 00660: CORROSION LEVEL 2. FRAME STA 1037 BTW LONGAug 3, 2023 · N957AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023080406297Unknown · unknownCRACK ON ANGLE BTW XRS 189 TO 200 APPROX AT LH WING REAR SPAR. SUMMARY OF NRC 00198: ANGLE BTW XRS 189 TO 200 APPROX AT LH WING REAR SPAR WAS REPLACED PER DWG 4981366 REV ORIGINAL AND PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G. ALSO TO GET ACCESS TO AREA THEAug 2, 2023 · N608AT · Boeing 717200 · Wing Miscellaneous StructureSDR DALA2023080306284Unknown · unknownCORROSION ON INTERNAL DOUBLER BTW LOWER DOOR JAMB AND EXTERNAL SKIN FROM STA Y 954 TO 994 AT AFT CARGO. IN REF NRC0337. C2. SUMMARY OF NRC 00664: CORROSION LEVEL 2. CORROSION ON INTERNAL DOUBLER BTW LOWER DOOR JAMB AND EXTERNAL SKIN FROM STA Y 954 TO 994 AT AFAug 2, 2023 · N603AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2023080306283Unknown · unknownCRACK ON FLAP VANE INBOARD SIDE STA XFLS 127 APPROX AT RIGHT WING. (AD) SUMMARY OF NRC 00051: FLAP VANE INBOARD SIDE STA XFLS 127 APPROX AT RIGHT WING WAS REPAIRED PER ER/A 610662-14 REV. ASSOCIATED ER/A 14-610662 ADDED FOR AC 9576. (LP #2898258)Aug 2, 2023 · N608AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2023080306282Unknown · unknownCORROSION ON LOWER JAMB PAN INTERNAL AND EXTERNAL STRUCTURE STA 946 TO STA 1002 AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00337: DOOR JAMB WAS REPLACED PER B717-200 SRM 51 -41-01-0G, 51-41-02-0G, AND 51-41-05-0G. (LP #2898062)Aug 2, 2023 · N603AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023080306281Unknown · unknownCORROSION ON INTERNAL DOUBLER OF AFT CARGO COMPARTMENT LWR DOOR JAMB BTW STA Y 954-994. SUMMARY OF NRC 00180: INTERNAL DOUBLER OF AFT CARGO COMPARTMENT LWR DOOR JAMB BTW STA Y 954-994 WAS REPAIRED ER/A 610521-14 REV ORIG, SECTION 1 PERMANENT REPAIR. ASSOCIATEDAug 2, 2023 · N608AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023080306280Unknown · unknownCORROSION ON STRINGERS 22L, 23L, 24L, 26L, AND 27L FROM STA Y=898.5 TO Y=STA 1053 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00667: CORROSION LEVEL 2. STRINGERS 22L, 23L, 24L, 26L, AND 27L FROM STA Y=898.5 TO Y=STA 1053 AT AFT CARGO COMPARTMENT WERE REPLACED PERAug 2, 2023 · N957AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2023080306279Unknown · unknownDENT ON INBD LH FLAP FIXED VANE, BTW XRS 162 TO 166 AT LH WING. SUMMARY OF NRC 00104: INBD LH FLAP FIXED VANE, BTW XRS 162 TO 166 AT LH WING, WAS REPAIRED PER B717-200 SRM 57-53-01-2R-1 REPAIR 1. (LP #2897695)Aug 2, 2023 · N978AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2023080306278Unknown · unknownCORROSION ON WEB ON X=-44 STA Y=160 AND X=54 BTW STA Y=160 AND STA Y=180 AT FWD PAX CABIN FLOOR. SUMMARY OF NRC 00179: CORROSION LEVEL 2. WEB ON X=-44 STA Y=160 AND X=54 BTW STA Y=160 AND STA Y=180 AT FWD PAX CABIN FLOOR WERE REPAIRED PER B717-200 SRM 51-70-10Aug 2, 2023 · N959AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023080306277Unknown · unknownCORROSION ON FLOOR SUPPORTS (4 EA) ON STA 466, STA 426, STA 371, AND STA 332 BTW LONG 28RH AND 28LH BILGE AREA AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00317: LEVEL CORROSION 2. FLOOR SUPPORTS (4 EA) ON STA 466, STA 426, STA 371, AND STA 332 BTW LONG 28RH AND Aug 2, 2023 · N603AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023080206249Unknown · unknownCORROSION ON DOOR JAMB AFT CARGO (C2) STA=954 TO STA=980 APROX. SUMMARY OF NRC 00031: CORROSION LEVEL 2. DOOR JAMB AFT CARGO C2 STA=954 TO STA=980 APROX WAS REPLACED PER B717 SRM 51-41-02-0G, 51-41-04-0G, AND 51-41-05-0G. (LP #2896570)Aug 1, 2023 · N978AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2023080206248Unknown · unknownCORROSION ON LONGERONS END (28 Y 27) LH AND LONGERONS END (23 Y 26) LH AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00641: CORROSION LEVEL 2. LONGERONS END (28,27,26,23) LH AT AFT CARGO COMPARTMENT WERE REPLACED PER B-717-200 SRM 51-41-05-0G PAR 8.B . (LP #2896107Aug 1, 2023 · N957AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2023080106212Unknown · unknownDENT ON LOWER SURFACE OF AFT MOVABLE VANE AT LH FLAP. SUMMARY OF THE NRC 00359: AFT MOVABLE VANE AT LH FLAP WAS REMOVED PER B717 AMM 27-50-03 AND DENT REPAIRED PER B717 SRM 51-70-02-0G PROCEDURE GENERAL AND SRM 57-53-01 FIG 201. REFER TO AMDS 2750-4007 FOR COMAug 1, 2023 · N922AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2023080206247Unknown · unknownCORROSION WAS FOUND ALONG FRAME SPLICE REPAIR AT STA 908 BTW L29-L AND L29 -R. SUMMARY OF NRC 00561: CORROSION LEVEL 2. REPAIR SPLICE AT FRAME STA 908 BTW LONGERON 27R TO LONGERON 28L WERE FABRICATED AND REPLACED PER B717-200 SRM 53-20-07-2R PROCEDURE 3 REPAIRJul 31, 2023 · N957AT · Boeing 717200 · Fuselage Main, FrameSDR HALA2023080100036Support Fitting · damagedATB - ON GEAR RETRACTION, LEFT AND RIGHT MAIN GEAR LIGHTS WENT FROM GREEN TO DARK. NOSE GEAR LIGHT WENT FROM GREEN TO RED AND REMAINED RED. LOUD NOISE HEARD FROM FLIGHT DECK. QRH COMPLETE, GEAR EXTENDED AND SHOWED THREE GREEN. FOUND NLG CYLINDER SUPPORT FITTINJul 31, 2023 · N483HA · Boeing 717200 · Landing Gear SystemSDR HALA2023080100035Unknown · unknownATB - NOSE GEAR WOULD NOT RETRACT AFTER TAKE OFF. PERFORMED B717 FIM TASK 32-30 TASK 802. NO DAMAGE, NO LEAKS NOTED. NFT. PER FIM 32-30 TASK 802 FAULTS WAS INTERMERITTENT. CYCLED GEAR 6 TIMES. NO FAULTS FOUND. OK FOR SVCJul 31, 2023 · N483HA · Boeing 717200 · Nose/Tail Landing GearSDR DALA2023080106211Unknown · unknownCORROSION ON GENERATION FLOOR ACCESS PANELS 221SF, 222EF, 221NF, 222AWF, AND 222SF. SUMMARY OF NRC 00283: CORROSION LEVEL 2. FLOOR ACCESS PANELS 222EF AND 222SF WAS REPAIRED PER B717-200 SRM 53-00-00-2R PROCEDURE 2 REPAIR 2, FLOOR PANELS 221SF AND 221NF WERE FJul 31, 2023 · N959AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2023080106210Unknown · unknownDISBOND ON RH CENTER FIXED VANE, UPPER SURFACE OF 0.700IN LENGTH X 0.600IN WIDTH AT DENT #1, (53.25" FROM IB EDGE, 5" FROM TE) IN REF MON JOB 032-0001 LOG 1549344. SUMMARY OF NRC 00407: RH CENTER FIXED VANE, UPPER SURFACE WAS REPAIRED PER B717-200 SRM 57-53-01Jul 31, 2023 · N959AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2023080106209Unknown · unknownCORROSION ON LOWER SILL STRUCTURE BTW STA 954 TO STA 994 OF AFT DOOR AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00089: CORROSION LEVEL 2. LOWER SILL STRUCTURE (DOOR JAMB) BTW STA 954 TO STA 994 OF AFT DOOR AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 5Jul 31, 2023 · N608AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023080106208Unknown · unknownCORROSION ON LON-30, LON-28L, AND LON-29L BTW STA 905 TO STA 1053 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00158: CORROSION LEVEL 2. LON-30, LON-28LH, AND LON-29LH BTW STA 905 TO STA 1053 WERE REPLACED PER B717-200 SRM 51-41-01-0G PAR 6, 51-41-02-0G PAR 4, ANDJul 31, 2023 · N957AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2023080106207Unknown · unknownCORROSION ON ANGLE OF FRAME BTW LON 27R TO LON 28L STA 908 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00161: CORROSION LEVEL 2. ANGLE OF FRAME BTW LONG 26L TO LONG 26R STA 908 AT AFT CARGO COMPARTMENT WAS FABRICATED AND REPLACED PER DWG 9975524 REV P AND B717-20Jul 31, 2023 · N957AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023080106206Unknown · unknownCRACKS ON STRINGERS 6LH, 8LH AND 6RH STA Y=1022 AT INTERNAL FUSELAGE (PAX CABIN). SUMMARY OF NRC 00153: REPAIR ON STRINGERS 6LH, 8LH AND 6RH STA Y = 1022 AT INTERNAL FUSELAGE WAS PERFORMED PER B717-200 SRM 53-00-05-2R PROCEDURE 2 PAR 5 FIG 201. (LP #2891854)Jul 30, 2023 · N922AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2023080106205Unknown · unknownCRACK WAS FOUND ON LH OVERWING FRAME STA Y=696, GREATER THAN 0.125IN IN REF TASK CARD 5310-01436-01B JOB #078-0002 STEP 10. SUMMARY OF NRC 00181: LH OVERWING FRAME STA Y=696 WAS REPLACED PER B717-200 TASK CARD 5310-01436-03A JOB 107-0001. ASSOCIATED AA 5310-01Jul 30, 2023 · N608AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023080106204Unknown · unknownCORROSION WAS FOUND ALONG FRAME SPLICE REPAIR AT STA 927 BTW L26-L AND L26-R. SUMMARY OF NRC 00560: CORROSION LEVEL 2. FRAME SPLICE REPAIR AT STA 927 BTW L26-L AND L26-R WERE FABRICATED AND REPLACED PER B717-200 SRM 53-20-07-2R PROCEDURE 3 PAR 5, 51- 41-02-0G,Jul 30, 2023 · N957AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023080106203Unknown · unknownCORROSION WAS FOUND ON LONGERON 22LH END FORWARD SECTION AT STA Y=1053 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00679: CORROSION LEVEL 2. LONGERON END 22LH WAS FABRICATED AND REPLACED PER DWG 4914954 REV A. (LP #2891485)Jul 29, 2023 · N957AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2023080106202Unknown · unknownCORROSION ON ANGLE BTW LONGERON 29 RH TO 28 LH AND FRAME 950 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00233: CORROSION LEVEL 2. ANGLE BTW LONGERON 29 RH TO 28 LH AND FRAME 950 AT AFT CARGO COMPARTMENT WAS FABRICATED AND REPLACED PER DWG 995814-39 REV CC AND B7Jul 29, 2023 · N957AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023080106201Unknown · unknownCORROSION ON FLOOR PANEL 211AMF AT COCKPIT. SUMMARY OF NRC 00299: CORROSION LEVEL 2. PANEL (SKIN) OF FLOOR PANEL 211AMF AT COCKPIT WAS FABRICATED AND REPLACED PER DWG 9957826 REV AA, B717-200 SRM 51-20-05-0G AND 51-41-02-0G. (LP #2891380)Jul 29, 2023 · N959AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2023080106200Unknown · unknownCRACK ON FRAME BTW STA Y=1037 AND LONG 17LH AT AFT PAX CABIN. SUMMARY OF NRC 00289: FRAME BTW STA Y=1037 AND LONG 17LH AT AFT PAX CABIN WAS REPAIRED PER B717 SRM-53-20-07-2R-4 (PERMANENT REPAIR). (LP #2890030)Jul 28, 2023 · N959AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023072806114Unknown · unknownCORROSION ON TIE TRACK LH SIDE STA 813 TO STA 1022 AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00306: CORROSION LEVEL 2. TIE TRACK LH SIDE STA 813 TO STA 1022 AT AFT CARGO COMPARTMENT (C2) WAS REPLACED PER DWG 5936663, B717-200 SRM 51-40-04-0G AND 51-41-05-0Jul 28, 2023 · N603AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2023072806113Unknown · unknownCORROSION ON RH CTR SEAT TRACK FROM STA Y=216 TO STA Y=245 AT FWD PAX CABIN FLOOR. SUMMARY OF NRC 0174: CORROSION LEVEL 2. SECTION SEAT TRACK FROM STA Y=200 TO STA Y=245 AT FWD PAX CABIN WAS REPLACED PER B717-200 SRM 51-41-01-0G PAR 6 AND 51-41-05-0G PAR 8. (LJul 28, 2023 · N959AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2023080406296Unknown · unknownWEB-CORRODED FS 1053 AFT SIDE AT STR 28 LH (P DOME AREA). SUMMARY NRC 096-0022:5310-2014/003 00258: CLEANED AREA CHECKED LIMITS REF B717-200 SRM 53-00-00-1A. REPLACE FASTENERS AS REQUIRED REF B717-200 SRM 51-40-02-0G. SUMMARY NRC 096-0022:5310-2014/003 00258: Jul 27, 2023 · N944AT · Boeing 717200 · Fuselage Main, BulkheadSDR DALA2023072806112Unknown · unknownDISBOND ON RUDDER TAB LH SIDE OF 1.7000IN LENGTH X 0.500IN WIDTH AT DENT #2, (9" ABOVE #2 HINGE 3"AFT L/E RUDDER TAB) IN REF MON JOB 029-0001, LOG 1488874. SUMMARY OF NRC 00564: DENT #2 AT RUDDER TAB LH SIDE WAS REPAIRED PER ER/A 609491-14 REV ORIGINAL SECTIONJul 27, 2023 · N957AT · Boeing 717200 · Rudder, Tab StructureSDR DALA2023072806111Unknown · unknownCORROSION ON LOWER DOOR JAMB AT FWD CARGO COMPARTMENT BTW STA Y370 AND STA Y427 (INNER AND OUTER SIDE). SUMMARY OF NRC 00081: CORROSION LEVEL 2. LOWER DOOR JAMB AT FWD CARGO COMPARTMENT BTW STA Y370 AND STA Y427 WAS REPLACED AND INSTALLED PER B717-200 SRM 51-4Jul 27, 2023 · N608AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023072806110Unknown · unknownCORROSION ON FITTINGS (2 EA) OF FWD SERVICE DOOR JAMB AT FWD PAX CABIN FLOOR. SUMMARY OF NRC 0180: CORROSION LEVEL 2. FITTINGS (2 EA) WERE REPLACED PER B717-200 SRM 51-41-02-0G. (LP #2887630)Jul 27, 2023 · N959AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023072706099Unknown · unknownCORROSION AT ANGLES (2 EA) WAS FOUND DURING DOOR JAMB DISASSEMBLY. SUMMARY OF NRC 00196: CORROSION LEVEL 2. ANGLES (2 EA) WERE FABRICATED AND INSTALLED PER B717-200 SRM 53-20-15-2R PROCEDURE 7 REPAIR 7 AND 51-41-05-0G. (LP #2886801)Jul 27, 2023 · N608AT · Boeing 717200 · Fuselage Structure (General)SDR DALA2023072706098Unknown · unknownCORROSION ON FRAME STA 870 AND LONGERON L30 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00645: CORROSION LEVEL 2. FRAME STA 870 AND LONGERON L30 AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 3. (LP #2886682)Jul 27, 2023 · N603AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023072706097Unknown · unknownCORROSION ON FRAME CLIP BTW LONGERON 26LH TO 26 RH STA Y=1022 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00710: CORROSION LEVEL 2. FRAME CLIP STA Y=1022 BTW STR 26RH TO STR 26LH WAS FABRICATED AND REPLACED PER DWG 9912243 REV JS AND PER B717-200 SRM 51-41-02-0G.Jul 26, 2023 · N957AT · Boeing 717200 · Fuselage Structure (General)SDR DALA2023072606038Unknown · unknownCRACKS (3 EA) ON INTERNAL STRUCTURE BEAM #3 STA 370 AND BEAM #5 STA 370, STA 427 AT FWD CARGO DOOR. SUMMARY OF NRC 00264: CRACKS (3 EA) ON INTERNAL STRUCTURE BEAM #3 STA 370 AND BEAM #5 STA 370, STA 427 AT FWD CARGO DOOR WERE REPAIRED PER B717-200 SRM 52-30-02Jul 25, 2023 · N603AT · Boeing 717200 · Fuselage Main, Structure
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