Boeing 717-200

Service difficulty reports · 18,771

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  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 DALA2016121409834Structure · crackedAFT CARGO DOOR CRACKED AT UPPER FWD AND AFT DOOR STOPS. FABBED DOUBLERS FROM 2024-0-.050, HEAT TREATED TO 2024-T42, AND INSTALLED DOUBLERS AT UPPER FWD AND AFT STOPS IAW SRM 52-30-02 REPAIR 6 ON AFT CARGO DOOR.Dec 8, 2016 · N985AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2016120909746Pan · crackedCRACKED RT RING PAN UPPER AFT CORNER BS 832. REPAIRED THE RING PAN IAW SRM 56-20-02 FIG. 202.Dec 8, 2016 · N975AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016120909745Pan · crackedCRACKED RT RING PAN UPPER FWD CORNER BS 696. REPAIRED THE RING PAN WAS REPAIRED IAW SRM 56-20-02 FIG. 202.Dec 8, 2016 · N975AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016120909744Pan · crackedCRACKED RT RING PAN LOWER FWD CORNER BS 889. REPAIRED THE RING PAN IAW SRM 56-20-02 FIG. 202.Dec 8, 2016 · N975AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016120909743Pan · crackedCRACKED RT RING PAN UPPER & LOWER AFT CORNERS BS 851. REPAIRED THE RING PAN IAW SRM 56-20-02 FIG 202.Dec 8, 2016 · N975AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016120909742Pan · crackedCRACKED RT RING PAN LOWER FWD CORNER BS 794. REPAIRED THE RING PAN IAW SRM 56-20-02 FIG 202.Dec 8, 2016 · N975AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016120909741Pan · crackedCRACKED RT RING PAN UPPER AFT CORNER BS 832. REPAIRED THE RING PAN IAW SRM 56-20-02 FIG. 202.Dec 8, 2016 · N937AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016120909722Pan · crackedCRACK ON LOWER FWD CORNER AT RING PAN WINDOW LT SIDE BTW STA Y 598-617. CRACKED RING PAN LOWER FWR CORNER BTW STA Y=598-617 LT, WAS REPAIRED PER SRM 56-20-02 FIG 202.Dec 8, 2016 · N975AT · Boeing 717200 · Passenger Compartment WindowsSDR DALA2016120909721Cusp Web · puncturedPUNCTURES ON RT CUSP WEB BTW STA Y=974 TO Y=975 AND BTW Y=989 TO Y=990, X=49R. PUNCTURE WAS DRILLED, DAMAGE WAS REMOVED PER SRM 53-00-00 PAR 2, AND FASTENERS WERE INSTALLED PER SRM 51-41-02.Dec 8, 2016 · N975AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016120909720Fitting · crackedCRACKED FITTINGS (4EA) ON AFT VENTRAL DOOR JAMB STA Y=1076. FITTINGS WERE REMOVED (4EA). NEW FITTINGS DRILLED, TREATED, PAINTED, AND INSTALLED PER SRM 51-41-01, 51-41-02, 51-10-04, PAR 15 & 24, AND 51-40-08.Dec 8, 2016 · N607AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016120909719Channel · crackedFLOOR PANEL 222AFF HAT CHANNEL IS CRACKED. FABRICATED HAT CHANNEL REPAIR SECTION IAW SRM 53-20-50 REPAIR NR 5 FIG 202, HEAT TREATED TO T-6 CONDITION IAW DPS 900-4-1 NR 1 PAGES 16 AND 18. INSTALLED REPAIR IAW SRM 53-20-50 REPAIR NR 5 FIG 202.Dec 8, 2016 · N985AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2016120909718Seat Track · corrodedLEFT OUTBD SEAT TRACK LBL 56 HAS CORROSION DISCREPANCIES FROM FUSELAGE STATION 982-986. REPAIRED LEFT OUTBD SEAT TRACK LBL56 FUSELAGE STATION 982-986 IAW SRM 53-20-52 REPAIR 1.Dec 8, 2016 · N985AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016120909717Shear Tie · crackedUPPER FUSELAGE, PASSENGER CABIN, STA 1022 L12R TO L14R, CRACKS. STA 1022 L12R TO L14R CRACKED SHEAR TIE. REMOVED CRACKED SHEAR TIE AND INSTALLED REPLACEMENT IAW SRM 51-41-05 AND 51-41-05.Dec 8, 2016 · N985AT · Boeing 717200 · Fuselage Internal Mounting StructureSDR DALA2016120909716Stiffener · crackedUPPER CABIN FLOOR PANEL 222 AJF HAS A CRACKED STIFFENER AND DISBONDED STIFFENER END. REPAIRED CRACKED STIFFENER IAW SRM 53-20-50 REPAIR 5 FIG 202. REPAIRED DISBONDED STIFFENER IAW SRM 51-20-05 REPAIR SEALING.Dec 8, 2016 · N985AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2016120909715Floor Panel · delaminatedNR 3 AFT LAV FLOOR PANEL HAS DELAMINATED CORNER AND EDGE SEAL MISSING. REPAIRED LAV FLOOR PANEL IAW SRM 52-20-50 REPAIR 4.Dec 8, 2016 · N985AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2016120909714Shear Tie · corrodedSHEAR TIE CORRODED IN AFT BAG BIN STA 908 BETWEEN LONGERON 29L-30. SHEAR TIE FOUND TO BE CORRODED THROUGH. 100% MATERIAL LOSS. REPAIRED CORRODED SHEAR TIE SECTION IAW SRM 53-20-06 REPAIR 1.Dec 8, 2016 · N985AT · Boeing 717200 · Fuselage Internal Mounting StructureSDR DALA2016120909713Stringer · corrodedAFT CARGO L30 IS CORRODED BETWEEN STA 920 - STA 994. BLENDED CORROSION ON STR 30 FROM STA 920 TO 965 IAW SRM 51-10-04 SECTION 26. .115 REMAINING OF .125 FOUND TO BE IN LIMITS IAW SRM 53-00-60 FIG 103. BLENDED STR 30 FROM STA 975 TO 994 IAW SRM 51-10-04 SECTIONDec 8, 2016 · N985AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2016120909712Frame · crackedCRACKED FRAME AT STA Y=1133 AND LONGERON 2R IN THE AFT ACCESSORY COMPARTMENT. FRAME WAS REPLACED PER SRM 51-41-02 AND DRAWING 5913595 REV AP.Dec 8, 2016 · N607AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2016120809801Floor Panel · delaminatedDELAMINATED FLOOR PANEL 222JF. THE FLOOR PANEL WAS FABRICATED AND REPLACED IAW SRM 53-20-50.Dec 7, 2016 · N607AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2016120709657Lamp · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT LEFT EXTERIOR EMERGENCY FLOOD LIGHT WAS INOPERATIVE. REPLACED THE LAMP AND THE OPERATIONAL CHECKED GOOD.Dec 7, 2016 · N953AT · Boeing 717200 · Emergency LightingSDR DALA2016121309813Shear Tie · corrodedAFT CARGO SHEAR TIE AND FRAME IS CORRODED AT BS 1002 BETWEEN LONGERSONS 29 - 30L. REPLACED THE SHEAR TIE IAW DWG 9957739, SRM 53-00-00 FIG 103 & SRM IN 51-41-05 PGS 1-5.Dec 6, 2016 · N985AT · Boeing 717200 · Fuselage Internal Mounting StructureSDR DALA2016120709693Skin · dentedFWD CARGO DOOR EXTERNAL SKIN EDGE AT THE AFT LOWER CORNER AREA HAS TWO DENTS. REMOVED AND REPLACED THE SKIN.Dec 6, 2016 · N985AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2016120709692Pan · crackedCRACKED FWD CARGO DOOR PAN UPPER EDGE BS 389 - 408. THE DOOR PAN WAS REPAIRED IAW SRM 52-30-02 FIG. 201 REP 1.Dec 6, 2016 · N607AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016120709653Door Frame · crackedNOSE LANDING GEAR WHEEL WELL DOOR FRAME BEAM CRACKED . REPAIRED IAW SRM 53-10-14 FIGURE 201 REPAIR 2.Dec 6, 2016 · N607AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016120709652Door Frame · crackedNOSE LANDING GEAR WHEEL WELL DOOR FRAME BEAM CRACKED. THE BEAM WAS REPAIRED IAW SRM 53-10-14 FIGURE 201 REPAIR 2.Dec 6, 2016 · N607AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016120709651Pan · crackedCRACKED FWD CARGO DOOR PAN BETWEEN STOP FITTINGS 1 & 2. HFEC INSPECTION WAS ACCOMPLISHED AND THE CRACKS WERE CONFIRMED IN FWD SECTION OF 1.625", AND AFT SECTION OF 1.5" IAW NDTSPM 06-10-01.001. STOP DRILLED IAW SRM 52-30-02 FIGURE 201 SHEET 3 OF 3, HFEC INSDec 6, 2016 · N607AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016120709650Angle · crackedCRACKED INTERNAL ANGLE ON LT FWD EMERGENCY EXIT DOOR. THE ANGLE WAS REPLACED IAW SRM 51-41-02, AND 51-41-05.Dec 6, 2016 · N607AT · Boeing 717200 · Emergency ExitsSDR DALA2016120609592Light · intermittentTHE PILOT DISCOVERED THAT THE EMERGENCY EXIT LIGHTS AT THE GALLEY DOOR AND THE FRONT OF THE FIRST CLASS SECTION OF THE CABIN WERE INTERMITTENT IN OPERATION. MAINTENANCE COULD NOT DUPLICATE THE PROBLEM AND SIGNED IT OFF AS NTF.Dec 6, 2016 · N989AT · Boeing 717200 · Emergency LightingSDR DALA2016121409841Intercostal · crackedFORWARD CARGO CEILING STRUCTURE INTERCOSTAL CRACKED AT STA 636 BL 0. REPAIRED CRACKED INTERCOSTAL AT STA 636 BL 0 IAW SRM 53-00-00 REP 1 FIG 201.Dec 5, 2016 · N933AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016120609591Skin · wornWEAR ON RT FLAP AFT MOVEABLE VANE UPPER SURFACE OUTBOARD EDGE NEAR TO STA XRS 111. RT MOVEABLE VANE WAS REPAIRED PER SRM 57-53-01 REPAIR 1. PARAGRAPH 4.Dec 5, 2016 · N607AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2016120609590Beam · crackedCRACKED BEAM NR 1 AT AFT END, ALSO BEAM CLIP SAME AREA, AT FWD SERVICE DOOR. BEAM NR 1 AND CLIP AFT EDGE WERE REPLACED PER SRM 51-41-02, 51-41-05.Dec 5, 2016 · N607AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016120509515Light · missingDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHT STRIP WAS MISSING. MAINTENANCE INSTALLED AND OPS CHECKED GOOD.Dec 5, 2016 · N945AT · Boeing 717200 · Emergency LightingSDR DALA2016120509514Cusp Web · crackedCRACK ON RT CUSP WEB BS 655 - 715 AND RBL 44 TO 60. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55 FIG 223 REPAIR 4.Dec 4, 2016 · N607AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016120509513Doubler · corrodedCORROSION ON PRODUCTION DOUBLER OF FWD E/E BAY MAST DRAIN. THE DOUBLER WAS REPLACED IAW SRM 51-41-02.Dec 4, 2016 · N607AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016120509512Cusp Web · crackedCRACK ON THE LEFT CUSP WEB BS 672 BETWEEN LBL 60 AND 54. THE DAMAGE WAS REMOVED IAW SRM 53-00-55 REPAIR 4, HFEC WAS ACCOMPLISHED AND NO CRACKS WERE FOUND IAW NDT SPM 06-10-01.001. A REPAIR WAS FABRICATED IAW SRM 53-00-55 REPAIR 4 FIG 215, AND INSTALLED IAW SRDec 4, 2016 · N607AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016120509511Angle · crackedCRACK ON AFT EDGE ANGLE BETWEEB BEAM NR 5 AND 6. THE ANGLE WAS REPLACED IAW SRM 51-41-01, 51-41-02, AND DWG 5914121 REV: AV.Dec 4, 2016 · N607AT · Boeing 717200 · Passenger/Crew DoorsSDR DALA2016120509510Floor Panel · puncturedPUNCTURED FLOOR PANEL. FLOOR PANEL REPAIRED IAW AMM 20-60-10 340-801.Dec 4, 2016 · N607AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2016120509509Floor Panel · crackedCRACK ON COCKPIT FLOOR PANEL P/N 9957824-3 (CPIL) (NRC 00465). HFEC WAS ACCOMPLISHED ON COCKPIT FLOOR PANEL P/N 9957824-3 (CPIL) NO CRACKS WERE FOUND AFTER STOP DRILL PER MD-DC/BOEING NDT SPM 06-10-01.001 EQUIPMENT: MENTOR C/N 1205 EXP DATE: 24AGO17 FLOOR PANEDec 4, 2016 · N607AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2016120509508Cusp Web · corrodedCORROSION OUT LIMITS ON LH CUSP WEB UPPER AND LWR SURFACE BTW X:60 AND X:44 STAY:544-551 IN REF NRC. S/N. 00329 (CPAX) (NRC 00499). SEAT TRACK ON STA 541 TO 588 LH WAS REMOVED PER B-717 SRM 51-41-01 AREA OUT LIMITS WAS CUT OUT ON STA. 544 TO 556, X=60 AND X=44Dec 4, 2016 · N607AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016120509588Floor Support · corrodedCORROSION ON FLOOR SUPPORT X=-52 BTW STA Y=132 TO Y=-148. AT COCKPIT FLOOR STRUCTURE. FLOOR SUPPORT WAS REPLACED PER DRAWING 9936533 ITEM 35 REV CM AND SRM 51-41-02.Dec 3, 2016 · N969AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016120409507Longeron · crackedAFT ACCESSORY COMPARTMENT: CRACKED LONGERONS 2LH AND 2RH AT STA Y=1133 (AMDS 5300-2004) (NRC 00343). LONGERONS 2 LH AND 2 RH AT STA Y=1133 WERE REPAIRED PER B-717 SRM 53-00-05 REPAIR 2. (LP #2793607)Dec 3, 2016 · N607AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2016120409506Skin · damagedCRACK ON INNER SKIN BESIDE LATCH LINK ON LT MLG DOOR. INNER SKIN BESIDE LATCH LINK ON LH MLG DOOR X=55 APROXIMATELY WAS REPAIRED PER B-717 SRM 52-82-01 FIG 201 REPAIR 3, 51-41-08, AND 51-41-05. REQUIRED VISUAL INSPECTION EVERY 3000 CYCLES PER SRM B717 REPAIR 3Dec 3, 2016 · N607AT · Boeing 717200 · Landing Gear DoorsSDR DALA2016120509587Attach Fitting · wornINSPECTION OF THE TAILCONE LOCKING MECHANISM CABLE DISCOVERED A WORN CABLE SLIDE ATTACHMENT WHICH MAY PREVENT THE SLIDE FROM DEPLOYING. THE ATTACHMENT WAS REPLACED, THE SYSTEM WAS RETURNED OPERATIONAL STATUS, AND THE RII WAS COMPLETED.Dec 2, 2016 · N985AT · Boeing 717200 · Aerodynamic FairingsSDR DALA2016120709655Cusp Web · crackedRIGHT CUSP WEB CRACKED AT BS 218. REPLACED THE CUSP WEB IAW SRM 51-41-02.Dec 1, 2016 · N985AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016120209462Lens · unknownTHE FLIGHT ATTENDANT DISCOVERED THAT THE OVERWING EXIT PATH AT 29C EMERGENCY EXIT SIGN HAD A DAMAGED OR MISSING LENS/COVER. MAINTENANCE INSTALLED THE LENS/COVER AND THE OPERATIONAL CHECK WAS GOOD.Dec 1, 2016 · N921AT · Boeing 717200 · Emergency LightingSDR DALA2016120209461Cusp Web · crackedCRACKED RT CUSP WEB STA Y=218 BELOW SEAT TRACK X.-44. DAMAGE WAS TRIMMED OUT PER SRM 53-00-55 REPAIR 4 FIG 210. HFEC INSP WAS ACCOMPLISHED ON RT CUSP WEB STA Y=218 BELOW SEAT TRACK X.-44. NO CRACKS WERE FOUND AFTER TRIM OUT PER NDT SPM 06-10-01.001. REPAIR PARDec 1, 2016 · N607AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016120109460Doubler · corrodedAFT CARGO INTERNAL DOUBLER IS CORRODED AT STA 1025, BETWEEN L29L-L30. REPLACED INTERNAL DOUBLER IAW SRM 53-02-01 REPAIR 1 2024-T3 -.025.Nov 30, 2016 · N985AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016120109418Fitting · crackedCRACKED INTERNAL CLIP ON RT FWD EMERGENCY EXIT DOOR. CLIP WAS REPLACED PER SRM 51-41-02 AND 51-41-05 DWG 9957735 REV G.Nov 30, 2016 · N607AT · Boeing 717200 · Emergency ExitsSDR DALA2016120709656Skin · damagedRIGHT FLAP INBD LOWER WEDGE HAS A HOLE. REMOVED DAMAGED AREA IAW SRM 51-70-13 REPAIR 1 FIG 202. FABRICATED A REPAIR IAW SRM 51-70-13 REPAIR 1 AND INSTALLED IAW SRM 51-70-13 REPAIR 1 FIG 202.Nov 29, 2016 · N985AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2016113009393Fitting · crackedCRACKED LT FRAME CLIP STA Y1022 BTW LONG 14-13L. FRAME CLIP WAS REPLACED PER SRM 51-41-02, 51-41-05 AND DWG 9912243-197 REV JS.Nov 29, 2016 · N607AT · Boeing 717200 · Fuselage Main, Frame
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