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 DALA2025051203682Battery · no testDURING TESTING FOUND 1EA LIGHT IN CEILING AT AFT EXIT / FA SEAT AREA TO BE INOPERATIVE. REPLACED BATTERY AT B5-116. NOW LIGHT TEST GOOD REF B717 AMM 33-51-00. (LP #0957765)May 9, 2025 · N959AT · Boeing 717200 · Emergency LightingSDR DALA2025051203679Skin · crackedCRACKS ON FUSELAGE SKIN ON STA Y=1087 AND LONG 14R AT AFT FUSELAGE. SUMMARY OF NRC 00025: FUSELAGE SKIN ON STA Y=1087 AND LONG 14R AT AFT FUSELAGE WAS REPAIRED PER ER/A 625728-14 REV ORIG SECTION I: PERMANENT REPAIR AND PER PRI 625728-14 REV 3. TIME CONTROLLEDMay 9, 2025 · N921AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2025051403726Spar Cap · crackedDUE TO CRACK IN LH WING LOWER SPAR CAP, COMPLY WITH PRI 621443-14. CRACKED SPAR CAP REPLACED ON PRI 621443-14 REVS 0 THRU 24. COMPARED PRI 621443-14 REVS 0 THRU 24 WITH ERA 621443-14 REV A. ALL ITEMS MATCH. COMPLIED WITH ERA 621443-14 REV A. ALL RII ITEMS C/W.May 8, 2025 · N959AT · Boeing 717200 · Wing SparSDR DALA2025051203678Cable · wornTAILCONE EMERGENCY RELEASE HANDLE CABLE ASSEMBLY WAS FOUND WORN. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY OF NRC 00623: RELEASE HANDLE CABLE ASSEMBLY WAS REPLACED PER B717 AMM 20-0May 8, 2025 · N921AT · Boeing 717200 · Aerodynamic FairingsSDR DALA2025050803559Cusp Web · corrodedCORROSION ON PASSENGER CABIN CUSP WEB PREVIOUS REPAIR LOCATED Y=541 - 580; X=-56. SUMMARY OF NRC 00768: CORROSION LEVEL 2. PREVIOUS REPAIR LOCATED ON PASSENGER CABIN CUSP WEB STA Y=541 - 580; X=-56, WAS REPLACED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 PAR 5, May 7, 2025 · N921AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2025051903830Tab · delaminatedSHIP 9568 INITIAL INSPECTION: DELAMINATED CONTROL TAB OF AILERON AT LH WING. CORRECTIVE ACTION: AILERON CONTROL TAB WAS REMOVED (PN: UNK, SN: 5106) AND SERVICEABLE AILERON CONTROL TAB (P/N: 5910047-501 S/N: 5029) WAS INSTALLED AT LH WING PER B717-200 AMM 27-10May 6, 2025 · N932AT · Boeing 717200 · AileronsSDR DALA2025050803558Cusp Web · corrodedCORROSION OUT LIMITS ON PASSENGER CABIN CUSP WEB PREVIOUS REPAIR LOCATED Y=256; X=-56. SUMMARY OF NRC 00770: PREVIOUS REPAIR ON CUSP WEB LOCATED Y=256; X=-56 AT PASSENGER CABIN WAS REPLACED DUE CORROSION LEVEL 2 PER B717-200 SRM 53-00-55-2R PROCEDURE 4 PAR 5, May 6, 2025 · N921AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2025051203683Window · crackedDURING CRUISE, THE CA NOTED AN ARC AND THE WINDSHIELD DEVELOPED A CRACK. MAINTENANCE REPLACED THE CAPT FWD WINDSHIELD REF B717 AMM 56-11. ALL CHECKS WERE GOOD. WINDOW HEAT TEST GOOD REF B717 AMM 30-41. INSTALLED WINDOW WIPER REF B717 AMM 30-42. AIRCRAFT IS OK May 5, 2025 · N939AT · Boeing 717200 · Flight Compartment WindowsSDR DALA2025050603512Floor Support · corrodedCORROSION ON PASSENGER CABIN FLOOR SUPPORTS (2 EA) BETWEEN Y=148 - 200, X=7 AND X=-7. SUMMARY OF NRC 00637: CORROSION LEVEL 2. FLOOR SUPPORTS (2 EA) BETWEEN Y=148 - 200, X=7 AND X=-7, WERE FABRICATED PER DWG 9936534 REV BW, AND REPLACED PER B717-200 SRM 51-41-May 5, 2025 · N921AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2025050503409Cargo Track · corrodedCORROSION ON TIE TRACK STA 898.5-954 L27R TO L28R IN AFT CARGO COMPARTMENT. ORIGINAL THICKNESS 0.060IN AND MINIMUM REMAINING THICKNESS 0.05IN; FLANGE AREA IS OUT OF LIMITS. SUMMARY OF NRC 00771: CORROSION LEVEL 2. AFT CARGO COMPARTMENT TIE TRACK STA 898.5-954 May 3, 2025 · N921AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2025050503410Spar · cracked-AD- LH WING SPAR CRACK. LEFT WING SPAR REPARED PER ERA 621363-14AD REV ORG. FINAL ERA REV ORG HAS BEEN RECEIVED AND MATCHES PRI REV. 21. ASSOCIATED ER/A 14-621363 ADDED FOR AC 9572. (LP #6377060)May 2, 2025 · N927AT · Boeing 717200 · Wing SparSDR DALA2025050503408Floor Support · corrodedCORROSION PER (UT) MEASUREMENT THICKNESS WAS ACCOMPLISHED PER DC/MD/BOEING NDT SPM, PART 4 04- 00-07, PAR 4 FIG 9, FLOORS SUPPORT AT LAVATORIES ZONES: [1 EA; BETWEEN Y=1053 - 1022, X=-44]. WITH ORIGINAL THICKNESS =0.125" AND MINIMUM REMAINING THICKNESS =0.062"May 2, 2025 · N921AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2025050503407Cusp Web · corrodedCORROSION ON PASSENGER CABIN CUSP WEB PREVIOUS REPAIR LOCATED Y=503 - 522; X=-56. SUMMARY OF NRC 00767: CORROSION LEVEL 2. PREVIOUS REPAIR LOCATED Y=503 - 522; X=-56 ON PASSENGER CABIN CUSP WAS REPLACED PER B717-200 SRM 53-00-55-2R PROCEDURE 4. (LP #0945857)May 2, 2025 · N921AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2025050503406Frame · damagedSTA 1053.00 PRESSURE BULKHEAD LOWER Y CHORD DAMAGED BETWEEN LONGERON 26L-LONGERON 28L. SUMMARY SEE NRC 001-0575:5300-2013/024 01395: COMPLIED WITH E/RA 625071-14 REV ORIG. PRI REV 0, 1, 2, 3, 4, 5, 6. REPAIR INSTRUCTIONAL STEPS. ENSURED ALL E/RA 625071-14 REMay 2, 2025 · N925AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2025051403731None · none-AD- PER ERA 621363-14 AD REV 0 STAGE VIII STEP 9, PRIOR TO ACCESS CLOSE-UP, PERFORM A GENERAL VISUAL INSPECTION OF THE AREA FOR CLEANLINESS, AS DEFINED IN TOPP 40-10-10. A) ENSURE ALL TOOLS, RAGS, SHAVINGS, DEBRIS, ETC. HAVE BEEN REMOVED. B) PAY PARTICULAR ATMay 1, 2025 · N927AT · Boeing 717200 · Standard Practices/StructuresSDR DALA2025051403725None · none-AD- PER ERA 621441-14AD REV ORIG STEP 25, PERFORM GVI OF RH WING AREA BEFORE ACCESS CLOSE UP. STEP 25 OF ERA 621441-14AD REV O WAS COMPLIED WITH ON NRC 11 DURING OK TO CLOSE FUEL PANELS. GVI OF RH WING ACCESS AREA WAS COMPLIED WITH ON NON ROUTINE 11, DURING OMay 1, 2025 · N927AT · Boeing 717200 · Standard Practices/StructuresSDR DALA2025051403724Spar · cracked-AD- DUE TO CRACK INDICATION, COMPLY WITH RH WING SPAR REPAIR PER ERA 621441-14AD REV ORIG. SPAR REPAIRED PER PRI 621441-14AD REVS 0 THRU 8. COMPARED PRI 621441-14 REVS 0 THRU 8 WITH ERA 621441-14 REV ORIG. ALL ITEMS MATCH. COMPLIED WITH ERA 621441-14 REV ORIGMay 1, 2025 · N927AT · Boeing 717200 · Wing SparSDR DALA2025051403723Hinge Fitting · worn-AD- LH WING, OUTBOARD FLAP HINGE POINT AC SIDE, IB FITTING WORN. COMPLIED WITH ERA 623200-14AD REV ORG. REPAIRED LH WING OUBOARD FLAP HINGE POINT AC SIDE PER ERA 623200-14AD REV ORIG. REWORKED AND BUSHED LH WING OUTBOARD FLAP HINGE POINT, INBOARD FITTING PER May 1, 2025 · N927AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2025050503411Handle · damagedTHE CABIN CREW REPORTS THAT THE 1L DOOR INTERIOR HANDLE ROTATES FREELY WITHOUT OPENING THE DOOR. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE FOUND THAT THE HANDLE BOLT HAD SHEAREDMay 1, 2025 · N922AT · Boeing 717200 · Passenger/Crew DoorsSDR DALA2025050103360Cusp Web · corrodedCORROSION IN REFERENCE TO (UT) MEASUREMENT THICKNESS WAS ACCOMPLISHED ON CUSP MEMBRANE WEB X=58, STA Y=340, STA Y=868 C PAX (LH). ORIGINAL THICKNESS IS 0.020IN AND MINIMUM REMAINING THICKNESS IS 0.012IN., THEREFORE IT IS OUT LIMITS PER B717-200 SRM 53-00-55-1AApr 30, 2025 · N921AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2025050103359Spar Web · damagedLEFT WING AFT SPAR WEB O/B LOWER HOLE HAS DAMAGE (1 EA), LABELED AS B1. NO DAMAGE FOUND IAW DELTA ER/A 623679-14AD REV 0, PRI REV 7 SECTION 4 STEP #1 AND TABLE 2. ASSOCIATED ER/A 14-623679 ADDED FOR AC 9541. (LP #0941455)Apr 30, 2025 · N977AT · Boeing 717200 · Wing SparSDR DALA2025050103358Skin · damagedLEFT WING LOWER SURFACE AFT SPAR HOLES HAVE DAMAGE FROM STA XRS 111 TO XRS 137 (7 EA) MARKED AS A1 THRU A7. DAMAGE WAS REMOVED IAW DELTA ER/A 623679-14AD REV 0 PRI REV 7 SECTION IV STEP # 5, #6, AND #7. ASSOCIATED ER/A 14-623679 ADDED FOR AC 9541. (LP #0941448Apr 30, 2025 · N977AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2025043003319Cusp Web · corrodedCORROSION ON PASSENGER CABIN CUSP WEB PREVIOUS REPAIR LOCATED Y=484 - 503; X=-56. SUMMARY OF NRC 00766: CORROSION LEVEL 2. PASSENGER CABIN CUSP WEB PREVIOUS REPAIR LOCATED Y=484 - 503; X=-56 WAS REPLACED PER B717-200 SRM 53-00-55-2R, REPAIR 4. (LP #0940885)Apr 30, 2025 · N921AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2025043003318Cusp Web · corrodedCORROSION ON PASSENGER CABIN CUSP WEB PREVIOUS REPAIR LOCATED Y=465 - 484; X=-56. SUMMARY OF NRC 00765: CORROSION LEVEL 2. PASSENGER CABIN CUSP WEB PREVIOUS REPAIR LOCATED Y=465 - 484; X=-56 WAS REPLACED PER B717-200 SRM 53-00-55-2R, REPAIR 4. (LP #0940877)Apr 30, 2025 · N921AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2025043003317Doubler · crackedDOUBLER CRACKED. AFT LOWER CORNER OF AFT CARGO DOOR. MARKED NRC 455. REMOVED EXISTING REPAIR & REPLACED DOUBLER REF B717 SRM 53-20-15-2R PROCEDURE 12 REPAIR 12. AFT CARGO DOOR JAMB EDGE SKIN REP- AIR. (LP #0940824)Apr 30, 2025 · N926AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2025043003316Cusp Web · corrodedCORROSION ON PASSENGER CABIN CUSP WEB PREVIOUS REPAIR LOCATED Y=446 - 465; X=-56. SUMMARY OF NRC 00764: CORROSION LEVEL 2. CABIN CUSP WEB (PREVIOUS REPAIR) LOCATED Y=446 - 465; X=-56 WAS REPLACED PER B717-200 SRM 53-00-55-2R REPAIR 4. (LP #0940714)Apr 30, 2025 · N921AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2025043003322Holder · sparksWHILE MOVING CAPT NOTE PAD HOLDER HAD SPARKS BEHIND THE HOLDER & ALL MAP LIGHTS WENT OUT. ALSO, CIRCUIT BREAKER W29 TRIPPED. MAINTENANCE REPAIRED BARE WIRES PER B717 SWPM 20-10-03. NO FURTHER ISSUES. OPERATIONAL CHECK WAS NORMAL ON CHART HOLDER. (LP #7237748)Apr 29, 2025 · N915AT · Boeing 717200 · Flight Compartment LightingSDR DALA2025043003320Battery Pack · inoperativeEMERGENCY LIGHTS (3 EA) LOCATED AT CEILING PANEL IN FRONT OF FWD LAVATORY, EXIT SIGN AT TOP OF COW 1 AND ABOVE THE SERVICE DOOR DOES NOT OPERATE. THE POWER ASSEMBLY BATTERY PACK WAS REPLACED PER B717-200 AMM 33-51-04. TEST OK. (LP #6915838)Apr 29, 2025 · N938AT · Boeing 717200 · Emergency LightingSDR DALA2025043003315Repair · not reported-AD- EXISTING REPAIR FOUND, CONTACT LIAISON ENGINEERING FOR REPAIR PROCEDURE PRIOR TO FURTHUR FLIGHT REF. FC5720-01103. AMOC 24-160 TO AD 2024-21-01 PARA(G) W/C 5720-01103-01B AND ERA 621136-14AD REV ORIGINAL ALREADY APPROVED AND PROVIDE AMOC TO SUBJECT AD FORApr 29, 2025 · N986AT · Boeing 717200 · Wing StructureSDR DALA2025043003313Battery · inoperativeTHE OVERHEAD CEILING EMERGENCY LIGHTS ARE INOPERATIVE AT ROWS 24-28. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY ASSEMBLY B5-231 PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #7173431)Apr 29, 2025 · N985AT · Boeing 717200 · Emergency LightingSDR DALA2025043003321Repair · not reported-AD- EXISTING REPAIR FOUND, CONTACT LIASON ENGINEERING FOR REPAIR PROCEDURES PRIOR TO FUTHER FLIGHT. FC 5720-01103-01A. OK TO CONT THE WC INSP AS AUTHORIZED BY THE TIME CONT ITEMS STATEMENT FOR SEC II OF ERA 621176-14AD REV A. (LP #7184928)Apr 28, 2025 · N980AT · Boeing 717200 · Standard Practices/StructuresSDR DALA2025043003314Repair · not reported-AD- EXISTING REPAIR FOUND, OK TO CONT THE WC INSP AS AUTHORIZED BY THE TIME CONT ITEMS STATEMENT FOR SEC I OF ERA 619064-14AD REV B. (LP #7184929)Apr 28, 2025 · N980AT · Boeing 717200 · Wing StructureSDR DALA2025043003312Hinge Fitting · wornLH WING OUTBOARD FLAP HINGE POINT AC SIDE, IB FITTING WORN. MACHINED IB AND OB LUGS TO REMOVE DAMAGE. OB LUG BORE FINAL SIZE IS .533. IB LUG FINAL SIZE IS .594. INNER FACE OF IB LUG SPOTFACED .880 DIAMETER WITH .060 RADIUS TO A DEPTH OF .076. REMAINING LUG THIApr 25, 2025 · N927AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2025100807320Hinge Fitting · corrodedCORROSION ON FLAP FWD HINGE FITTING XRS=267 OF REAR SPAR AREA AT LH WING. REPLACED PER SERVICEABLE LT CENTER WING FLAP HINGE FITTING (0931308)Apr 24, 2025 · N921AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2025042503241Longeron · crackedCRACKED LONGERONS 6R, 4L, AND 8R LOCATED AT RH LAVATORY ZONE Y=1022. SUMMARY OF NRC 00417: LONGERON 6R AND 8R STA Y=1022 AT RH AFT LAVATORY ZONE WERE REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURE 2 REPAIR 2 FIG 201. NO CRACKS WERE FOUND ON LONGERON 4L PER DCApr 24, 2025 · N921AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2025050603514Battery Pack · inoperativeAFT OVERWING (L&R) EXIT LIGHT IS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACKS B5-119 & B5-230. OPERATIONAL CHECK IS NOW NORMAL REF B717 AMM 33-51. (LP #6520466)Apr 23, 2025 · N947AT · Boeing 717200 · Emergency LightingSDR DALA2025042403190Cusp Web · crackedCRACK ON CUSP WEB RH BTW STA Y=715 AT PASSENGER CABIN. CUSP WEB RH BTW STA Y=715 AT PASSENGER CABIN WAS REPAIRED PER B-717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4 FIG 203.Apr 23, 2025 · N921AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2025050803560Door Sill · corrodedAFT CARGO DOOR SILL HAS EVIDENCE OF CORROSION IN TWO AREAS. REPAIRED PER REF B717-200 SRM 53-20-15-2R PROCEDURE 7 REPAIR 7. AFT CARGO DOOR JAMB LOWER PAN CORROSION DAMAGE SPLICE REPAIR CHECKED AND REPLACED HI-SHEAR FASTENERS PER REF B717-200 SRM 51-41-04-0G ANApr 22, 2025 · N948AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2025042403189Skin · wornWEAR ON SKIN BTW STA Y=994 L24R TO L26R (AFT EDGE CUT OUT) AT AFT CARGO DOOR. WORN SKIN BTW STA Y=994 L24R TO L26R (AFT EDGE CUT OUT) AT AFT CARGO DOOR WAS REPAIRED PER PRI 625059-14 REV 7 AND ER/A 625059-14 REV ORIGINAL SECTION I: PERMANENT REPAIR.Apr 22, 2025 · N938AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2025042303171Door Sill · corrodedAFT CARGO DOOR SILL HAS EVIDENCE OF CORROSION IN TWO AREAS. MARKED. SUMMARY SEE NRC 001-0319:5231-2002/001 00174: REPAIRED PER B717-200 SRM 53-20-15-2R PROCEDURE 7 REPAIR 7. AFT CARGO DOOR JAMB LOWER PAN, CORROSION DAMAGE SPLICE REPAIR. CHECKED AND REPLACED HIApr 22, 2025 · N948AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2025042303170Wire · damagedSEAT EMERGENCY PATH LIGHTS ARE INOPERATIVE. SUMMARY SEE NRC 087-0001:3351-2001/001 00359: REPAIRED WIRE E9405-7-16N REF B717 SWPM 20-10-03. REPLACED POWER SUPPLY AND BATTERY PACK REF B717 AMM 33-51-03 AND CHECKED OPERATION. (LP #0927540)Apr 22, 2025 · N926AT · Boeing 717200 · Light System WiringSDR DALA2025042303169Doubler · corrodedCORROSION ON INTERNAL DOUBLER AND ON INNER SIDE OF WASTE SERVICE PANEL BTW STA Y=1022 AND STA Y=1037 BTW LONG 23L AND LONG 25L AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00232: CORROSION LEVEL 2. INTERNAL DOUBLER AT INNER SIDE OF WASTE SERVICE PANEL BTW STA Y=10Apr 22, 2025 · N921AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR HALA20250421024Battery Pack · inoperativeCABIN EMERGENCY LIGHTS INTERMITTENT. REPLACED EMERGENCY LIGHT BATTERY AT ROW 7 (B5-227) PER AMM 31-51-03. OPS CHECK GOOD, OK FOR SVC.Apr 19, 2025 · N495HA · Boeing 717200 · Emergency LightingSDR DALA2025042103076Cable · out of trackGOT A TAILCONE UNLOCK MSG DURING TAXI IN TO GATE. WHILE VERIFYING M PROCEDURES FOR MEL 53-52-018, FOUND LOCKING CABLE LEADS LOOSE, MEL STATES LEADS SHOULD BE TIGHT/NO EVIDENCE OF SLACK. FOUND CABLE OUT OF T FITTING. THE KEVLAR CABLE FOR THE TAIL CONE EMERGENCYApr 19, 2025 · N919AT · Boeing 717200 · Aerodynamic FairingsSDR DALA2025042103075Spar · corrodedLH AUX SPAR WEB 9919401-3 HAS CORROSION ON IB LWR FWD SURFACE. SUMMARY SEE NRC 002-0001:0514-2001/207 01575: REPLACED PER B717 DWG 9919401. (LP #0921231)Apr 19, 2025 · N925AT · Boeing 717200 · Wing SparSDR DALA2025042103074Stiffener · corrodedLH AUX SPAR WEB STIFFENER 9919401-5 HAS CORROSION ON IB LWR FWD SURFACE. SUMMARY SEE NRC 002-0001:0514-2001/209 01577: REPLACED PER B717 DWG 9919401. (LP #0921228)Apr 19, 2025 · N925AT · Boeing 717200 · Wing Miscellaneous StructureSDR DALA2025042103073Pan · crackedCRACK ON UPPER PAN. ALSO FWD EDGE PAN ON BEAM #2 CRACKED AT LH FWD EMERGENCY EXIT. SUMMARY OF NRC-00781: UPPER PAN AND ALSO FWD EDGE PAN CRACKS ON BEAM #2 AT LH FWD EMERGENCY EXIT WERE REPAIRED PER B717-200 SRM 52-20-02-2R PROCEDURE 1 REPAIR 1. (LP #0919966)Apr 18, 2025 · N998AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2025042103072Skin · damagedWORN AND BENT ON PREVIOUS REPAIR OF PASSENGER ENTRANCE DOOR SKIN L1. ALSO LOOSE RIVETS ON PREVIOUS REPAIR OF PASSENGER ENTRANCE DOOR SKIN L1 (LOWER REAR AREA). SUMMARY OF NRC 00238: REPAIR DOUBLER OF PASSENGER ENTRANCE DOOR SKIN L1 (LOWER REAR AREA) WAS FABRICApr 18, 2025 · N998AT · Boeing 717200 · Passenger/Crew DoorsSDR DALA2025042103070Warning Message · illuminatedSHIP 9510 -ATO- THE CREW SAFELY ABORTED THE TAKEOFF AT 110 KTS DUE TO RECEIVING AN AURAL "SLAT CONFIGURATION" MESSAGE. CORRECTIVE ACTION: MAINTENANCE (LP #7507750)Apr 16, 2025 · N951AT · Boeing 717200 · Leading Edge Slat Position Indicating SystemSDR DALA2025042103071Skin · crackedDAMAGE T: CRACK ON FUSELAGE LOWER SKIN BTW STA 1048 - 1053 AND LONG 30. SUMMARY OF NRC 00136: FUSELAGE LOWER SKIN BTW STA 1048 - 1053 AND LONG 30 WAS REPAIRED PER PRI 625673-14 REV 2 AND ERA 625673 -14 REV ORIGINAL. SECTION I: PERMANENT REPAIR. MAINTENANCE REQApr 16, 2025 · N895AT · Boeing 717200 · Fuselage Main, Plate/Skin
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