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 DALA2025020400815Battery Pack · inoperativeTHE FWD EXIT SIGN IS NOT ILLUMINATING. MAINTENANCE REPLACED THE BATTERY PACK AT THE FWD OVERHEAD EQUIPMENT F5-259 COMPARTMENT PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #6858025)Feb 4, 2025 · N943AT · Boeing 717200 · Emergency LightingSDR DALA2025020400814None · none-AD- COMPLY WITH ERA 623716-14AD REV ORIGINAL. SUMMARY NRC 002-0001:0514-2001/008 00009: COMPLIED WITH ER/A 623716-14AD REV 0, PRI REV 0, 1, AND 2. ENSURED PRI AND FINAL ERA MATCH. (LP #0794140)Feb 3, 2025 · N947AT · Boeing 717200 · Standard Practices/StructuresSDR DALA2025020600922None · none-AD- EXISTING REPAIR FOUND. CONTACT LIAISON ENGINEERING FOR REPAIR PROCEDURE PRIOR TO FURTHER 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 FOR Feb 1, 2025 · N986AT · Boeing 717200 · Standard Practices/StructuresSDR DALA2025020600921Attach Bracket · cracked-AD- DURING BHEC ON PRI 622371-14AD, REV 2 HOLE #2 ON INBOARD FLAP FAIRING ATTACH BRACKET HAS A CRACK INDICATION. FLAP FAIRING ATTACH BRACKET REPLACED DURING LEFT WING LOWER SKIN DOUBLER REPAIR ON ER/A 622371-14AD, REV O. JOB COMPLETE. A/C OK FOR SERVICE. (LP Feb 1, 2025 · N932AT · Boeing 717200 · Wing, Attach FittingsSDR DALA2025020600920Support Fitting · damaged-AD- ON LEFT WING XRS 164.00 LOWER FLAP HINGE SUPPORT FITTING 2ND NUT FORWARD ON INBOARD SIDE IS LOOSE. FASTENER REPLACED DURING LEFT WING LOWER SKIN REPAIR ON ER/A 622371-14AD, REV O. JOB COMPLETE. A/C OK FOR SERVICE. (LP #0791075)Feb 1, 2025 · N932AT · Boeing 717200 · Wing, Attach FittingsSDR DALA2025020600919Attach Bracket · damaged-AD- DURING BHEC ON PRI 622371-14AD, REV 2 HOLE #4 ON INBOARD FLAP FAIRING ATTACH BRACKET HAS CRACK INDICATION. HOLE #4 OVERSIZED TO 0.363" ON STEP 41 OF PRI 622371-14AD, REV 9. FREEZE PLUG INSTALLED ON PART C, STEP 12 OF PRI 622371-14AD, REV 13. HOLE WILL BE Feb 1, 2025 · N932AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2025020600918Attach Bracket · damaged-AD- DURING BHEC ON PRI 622371-14AD, REV 2 HOLE #3 ON INBOARD FLAP FAIRING ATTACH BRACKET HAS 2 CRACK INDICATIONS. HOLE #3 OVERSIZED TO 0.547" ON STEP 41 OF PRI 622371-14AD, REV 9. FREEZE PLUG INSTALLED IN HOLE #3 ON STEP 12, PART C OF PRI 622371-14AD, REV 13.Feb 1, 2025 · N932AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2025020600917Spar Cap · damaged-AD- ON UPPER LEG OF LEFT WING AFT SPAR LOWER SPAR CAP XRS 164.00 FASTENER ABOVE INBOARD LOWER FLAP FITTING ATTACH BOLT IS LOOSE AND SPINNING. THIS FASTENER REPLACED WITH OVERSIZE FASTENER DURING LEFT WING SKIN DOUBLER RFEPAIR ON ER/A 622371-14AD, REV O. JOB CFeb 1, 2025 · N932AT · Boeing 717200 · Wing SparSDR DALA2025020300803Retainer · crackedCRACK AROUND DRAIN OF RH SLIDING WINDOW RETAINER AT COCKPIT. SUMMARY OF NRC 00468: CRACK AROUND DRAIN OF RH SLIDING WINDOW RETAINER AT COCKPIT WAS REPAIRED PER PRI 622332-14 REV 1 AND ER/A 622332-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-Feb 1, 2025 · N979AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2025020300802Cargo Track · corrodedCORROSION WAS FOUND ON THE AFT CARGO COMP TIE TRACK LOCATED BETWEEN Y=995 TO Y=1022. SUMMARY OF NRC 00133: CORROSION LEVEL 2. THE TIE TRACK LOCATED BETWEEN Y=995 TO Y=1022 WAS FABRICATED PER DWG S2922357 AND REPLACED PER B717 SRM 51-41-01-OG. (LP #0790027)Feb 1, 2025 · N893AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR HALA20250204003Manifold · failed"DIVERSION TO HNL" TAIL ANTI-ICE MANIFOLD FAILED IN ICING CONDITIONS, FLAP 25 LANDING AS PER QRH. FOUND "PODS SYSTEM FAULT" ON FAULT REVIEW. REMOVED AND REPLACED PODS PER AMM 36-23-01. RTS TEST "PASS". NO FAULTS FOUND. A/C OK FOR SVCJan 31, 2025 · N478HA · Boeing 717200 · Airfoil Anti/De-ice SystemSDR DALA2025020300804Computer · faultedSHIP 9556 -MISC/DE- THE FLIGHT CREW NOTICED THAT THE AIRCRAFT WAS FLYING UNCOORDINATED DURING THE DESCENT AND THEN THEY RECEIVED "RUDDER RESTRICTED" MESSAGE ON APPROACH. AN EMERGENCY WAS THEN DECLARED WITH ATC. THE LANDING WAS UNEVENTFUL. CORRECTIVE ACTION: MAJan 31, 2025 · N896AT · Boeing 717200 · Rudder Control SystemSDR DALA2025020300801Spar Cap · crackedCRACK ON RH WING LOWER REAR SPAR CAP AROUND SECOND FASTENER FROM FLAP HING FITTING STA XW=154 OUTBOARD TO INBOARD DIRECTION. SUMMARY OF NRC 00347: CRACK ON RH WING LOWER REAR SPAR CAP AROUND SECOND FASTENER FROM FLAP HING FITTING STA XW=154 OUTBOARD TO INBOARDJan 31, 2025 · N980AT · Boeing 717200 · Wing SparSDR DALA2025013000725Drain · crackedCRACK AROUND DRAIN OF LH SLIDING WINDOW RETAINER AT COCKPIT. SUMMARY OF NRC 00027: CRACK AROUND DRAIN OF LH SLIDING WINDOW RETAINER AT COCKPIT WAS REPAIRED PER PRI 622331-14 REV 1 AND ER/A 622331-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-Jan 29, 2025 · N979AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2025013000724Safety Pin · missingMISSING SAFETY PIN OF SLIDE R1 DOOR. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY OF THE NRC 00084: SAFETY PIN WAS INSTALLED ON SLIDE R1 DOOR PER B717-200 AMM 25-61-03-000-801 STEP B.(Jan 29, 2025 · N952AT · Boeing 717200 · Escape SlideSDR DALA2025012900689Doubler · corrodedCORROSION ON DOUBLER REPAIR, BTW PROJECTION LONGS 26/27RH AT AFT CARGO DOOR, FWD JAMB C2. SUMMARY OF NRC 00010: CORROSION LEVEL 2. DOUBLER REPAIR BTW PROJECTION LONGS 26/27RH AT AFT CARGO DOOR, FWD JAMB C2 WAS MANUFACTURED AND REPLACED PER B717-200 SRM 53-20-1Jan 29, 2025 · N952AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2025012800654Battery Pack · inoperativeTHE EMERGENCY LIGHTS AT ROW 20 ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK AT B5-230 PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #6384488)Jan 27, 2025 · N986AT · Boeing 717200 · Emergency LightingSDR DALA2025012800656Battery Pack · inoperativeTHE EMERGENCY LIGHTS ARE INOPERATIVE AT THE FWD LIGHT ATTENDANT STATION. MAINTENANCE REPLACED THE BATTERY PACK FOR THE EMERGENCY LIGHTS IN THE AFT CARGO COMPARTMENT PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #6733983)Jan 23, 2025 · N934AT · Boeing 717200 · Emergency LightingSDR DALA2025012800655Lens · detachedTHE EMERGENCY EXIT COVER DIFFUSER LENS IS MISSING AT LOCATION 600. THE EXIT SIGN COVER FELL OFF. MAINTENANCE RESECURRED THE LENS COVER. OPERATIONAL CHECK WAS NORMAL. OK FOR SERVICE. (LP #776098)Jan 23, 2025 · N986AT · Boeing 717200 · Emergency LightingSDR DALA2025100807325Access Panel · out of limitsELONGATED HOLES (11 EA) WERE FOUND ON ACCESS PANEL OF LIGHT ASSY MB LOWER ARE OUT OF LIMITS PER DWG 5925039 REV. F. HOLES OUT OF LIMITS WERE REPAIRED PER ER/A 623283-14 REV. (0773037)Jan 22, 2025 · N995AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2025012400583Light · inoperativeTHE EXTERIOR EMERGENCY LIGHT DOESN'T TURN ON. THE OVERWING EMERGENCY LIGHT WAS REPLACED PER B717-200 AMM 33-51-05. ALL TEST OK. (LP #6552182)Jan 22, 2025 · N995AT · Boeing 717200 · Emergency LightingSDR DALA2025012100470Doubler · wornWEAR ON REPAIR DOUBLER BTW STA Y=954 L24R TO L27R AT EXTERNAL FUSELAGE. SUMMARY OF NRC 00011: PREVIOUS REPAIR DOUBLER BTW STA Y=954 L24R TO L27R AT EXTERNAL FUSELAGE WAS REPLACED PER PRI 562383-14 REV 3 AND ERA 562383-14 REV B SECTION III: PERMANENT REPAIR. PEJan 20, 2025 · N995AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2025012100469Frame · bentBENT FRAME STA Y=465 BTW LONG 26L AND LONG 27L AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00279: FRAME STA Y=465 BTW LONG 26L AND LONG 27L AT FWD CARGO COMPARTMENT WAS REPAIRED PER PRI 623357-14 REV 2 AND ERA 623357-14 REV ORIGINAL, SECTION I: PERMANENT REPAIR. Jan 20, 2025 · N995AT · Boeing 717200 · Fuselage Main, FrameSDR HALA20250121002Pump · faultedBTB "HYD L PUMP FIL" AFTER ENG START . PERFORMED FAULT ISOLATION PROCEDURE 29-10 TASK 801, UP TO ND INCLUDING STEP 801. F. (3) 01/19/2025. REMOVED AND REPLACED #1 ENG ENGINE DRIVEN HYDRAULIC PUMP PER AMM 29-11-01/401. OPS CHECK GOOD. LEAK CHECK GOOD. NO FAULTSJan 19, 2025 · N493HA · Boeing 717200 · Hydraulic Pump (Electric/Engine), MainSDR HALA20250121001Wheel · abnormalLOW SPEED REJECTED TAKEOFF. EXCESSIVE NOSEWHEEL SHIMMY. REMOVED AND REPLACED BOTH NLG WHEEL/TIRE ASSEMBLYS PER AMM 32-42-01. SPIN AND SECURITY CHECK GOOD. OK FOR SERVICE. NO BRAKE OVERHEAT AFTER RTO. NO INSPECTION REQUIRED PER AMM 05-53-01-200-801Jan 19, 2025 · N488HA · Boeing 717200 · Wheel/Ski/FloatSDR DALA2025012000466Frame · crackedCRACK ON FRAME DOUBLER STA Y=1178 CANT BTW LONGERON 2-3LH AT AFT ACCESSORY COMPARTMENT. SUMMARY OF NRC 264: FRAME DOUBLER STA Y=1178 CANT BTW LONGERON 2-3LH AT AFT ACCESSORY COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-30-08-2R PROCEDURE 7 REPAIR 7. (LP #07673Jan 18, 2025 · N979AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2025012000465Door Frame · corrodedCORROSION ON CARGO DOOR JAMB BTW STA Y=954 TO Y=988 AND LONGERON 28R (LOWER SIDE) AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00154: CORROSION LEVEL 2. CARGO DOOR JAMB CORROSION BTW STA Y=954 TO Y=988 AND LONGERON 28R (LOWER SIDE) AT AFT CARGO COMPARTMENT WAS REPJan 17, 2025 · N995AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2025012000464Skin · corroded-AD- CORROSION ON UPPER SKIN BTW XRS 360 TO XRS 380 AT LH WING. SUMMARY OF NRC 0015: CORROSION LEVEL 2. CORROSION ON UPPER SKIN BTW XRS 360 TO XRS 380 AT LH WING WAS REAPAIRED PER PRI 623423-14 REV 2 AND ERA 623423-14AD REV ORIGINAL. ASSOCIATED ER/A 14-623423 Jan 17, 2025 · N896AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2025012000463Pan · crackedCRACKS ON PAN OF INTERNAL STRUCTURE AT AFT EDGE OF AFT CARGO COMPARMENT DOOR BTW BEAM 2/3 AND BTW BEAM 4/5. ALSO ON FWD EDGE BTW BEAM 3/4. SUMMARY OF NRC 00135: AFT CARGO COMPARMENT DOOR WAS REMOVED AND A SERVICEALBE AFT CARGO COMPARMENT DOOR WAS INSTALLED PERJan 15, 2025 · N995AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2025011600360Frame · corrodedCORROSION ON FRAME BTW STA Y=851 BTW L29L TO L29R, AND STA Y=870 BTW L29L TO L29R AT AFT CARGO COMPARMENT. SUMMARY OF NRC 00839: CORROSION LEVEL 2. CORROSION ON FRAME BTW STA Y=851 BTW L29L TO L29R, AND STA Y=870 BTW L29L TO L29R AT AFT CARGO COMPARMENT WERE RJan 15, 2025 · N979AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2025011600359Beam · crackedCRACK ON BEAM 6 APROX STA Y=180 AT PASSENGER ENTRANCE DOOR (L1). SUMMARY OF NRC 00256: BEAM 6 APROX STA Y=180 AT PASSENGER ENTRANCE DOOR (L1) WAS REPAIRED PER ER/A: 623355-14 REV ORIGINAL SECTION I PERMANENT REPAIR AND PRI 623355-14 REV 0. ASSOCIATED ER/A 14-6Jan 15, 2025 · N995AT · Boeing 717200 · Passenger/Crew DoorsSDR DALA2025011500348Battery Pack · inoperativeMAINTENANCE FOUND ROW 19 LT & RT EMERGENCY EXIT SIGN LIGHTS WERE INOPERATIVE. THEY REPLACED THE EMERGENCY LIGHT BATTERY PACK LOC B5-121 PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #6776224)Jan 14, 2025 · N974AT · Boeing 717200 · Emergency LightingSDR DALA2025011400313Pan · wornWEAR ON INNER PAN FWD LOWER CORNER OF FWD CARGO DOOR. SUMMARY OF NRC 00083: INNER AND OUTER PAN FWD EDGE LOWER CORNER OF FWD CARGO DOOR WAS REPAIRED PER PRI 622673-14 REV 4 AND ERA 622673-14, SECTION I, PERMANENT REPAIR, REV ORIGINAL. ASSOCIATED ER/A 14-622673Jan 13, 2025 · N979AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2025011400312Skin · nickedNICK BETWEEN STA 994 AND STGR 24-26 RH AT EXTERNAL FUSELAGE SKIN. SUMMARY OF NRC 00007: EXTERNAL SKIN BETWEEN STA 994 AND STGR 24-26 RH WAS REPAIRED PER B717-200 SRM 53-20-15-2R PROCEDURE 12, REPAIR 12. PERFORM INITIAL GENERAL VISUAL INSPECTION AT 8,000 CYCLESJan 13, 2025 · N896AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2025011300273Longeron · corrodedCORROSION ON LONGERON 29L BTW STA Y=946 TO Y=1007 AT AFT CARGO COMPARMENT. SUMMARY OF NRC 00651: CORROSION LEVEL 2. LONGERON 29L BTW STA Y=946 TO Y=1007 AT AFT CARGO COMPARMENT WAS REPAIRED DUE CORROSION PER B717-200 SRM 53-00-05-2R REPAIR 3 PAR 4. (1) FIGURE Jan 11, 2025 · N995AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2025011300272Spar Cap · cracked-AD- CRACKS FOUND DURING INSPECTION OF LH WING REAR SPAR LOWER CAP RADIUS. CONTACT LIASON ENGINEERING FOR REPAIR PROCEDURES PRIOR TO FURTHER FLIGHT REF FC5720-01103. CRACK IS LOCATED INBD OF XRS 164 AT RIVET HEAD 1/2 INCH ABOVE LWR RADIUS. DISCREPANCY TRANSFERJan 10, 2025 · N977AT · Boeing 717200 · Wing SparSDR DALA2025011300271Frame · cracked-AD- CRACK ON UPPER RADIUS OF THE FRAME TAB ON THE OVERWING FRAME AT STA Y=715 LH WAS FOUND IN REF TASK CARD 5310-01436-04B JOB #079-0002, STEP 13. SUMMARY OF NRC 00397: FRAME WAS REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G UNDER AMDS 5310-01436-03A.Jan 10, 2025 · N995AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2025021201088Fuel Sys · leakingFUEL LEAK FOUND DURING INSP OF LH WING AFT LOWER SKIN DOUBLER AT XRS 164. ACCOMPLISHED PRI 623309-14 REV O THROUGH 3 REMAINING FUEL SEE POST PRI'S WITHIN B717 AMM 28-11-00 GROUP A ALLOWANCE. FORWARD TO MON PER ER/A 623309-14 AD REV O REPETITIVE INSP REQ DAILY Jan 9, 2025 · N974AT · Boeing 717200 · Fuel StorageSDR DALA2025011300270Skin · damaged-AD- ELONGATED HOLES (3 EA) ON CENTER WINGBOX UPPER SKIN STA Y=750 BTW X=44 AND X=50, ALSO ON SAME ANGLE BTW X=44 AND X=50 (4 EA) AT WINGBOX AREA. (CPAX). SUMMARY OF NRC 00750: ELONGATED HOLES (3 EA) ON CENTER WINGBOX UPPER SKIN STA Y=750 BTW X=44 AND X=50 AT Jan 9, 2025 · N979AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2025011300269Doubler · damagedWEAR AND GOUGES ON PREVIOUS REPAIR DOUBLER OF FIXED LEADING EDGE PANEL ON XIS=120 AT RH WING. SUMMARY OF NRC 00057: PREVIOUS REPAIR DOUBLER OF FIXED LEADING EDGE PANEL ON XIS=120 AT RH WING WAS REPLACED PER B717-200 SRM 57-40-01-2R REPAIR 7 FIG 202, 51-41-05-0Jan 9, 2025 · N995AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2025011300268Skin · damagedCORROSION AND TOOL MARKS WERE FOUND ON INNER HOLE #27 AND WEAR ON UPPER SKIN AROUND FROM #27 AT RH HORIZONTAL STAB. SUMMARY OF NRC 00735: CORROSION LEVEL 2. CORROSION IN HOLE #27 AT RH HORIZONTAL STAB WAS REPAIRED PER PRI 622779-14 REV 2 & ER/A 622779-14 REV OJan 9, 2025 · N979AT · Boeing 717200 · Horizontal Stabilizer, Plate/SkinSDR DALA2025011300267Structure · damagedCORROSION AND SCRATCHES ON INNER BOLT HOLE AND HOLE OF BARREL NUT (HOLE #26) AT HORIZONTAL STAB. SUMMARY OF NRC 00742: LEVEL CORROSION 2. CORROSION IN INNER BOLT HOLE AND HOLE OF BARREL NUT (HOLE #26) AT HORIZONTAL STAB WAS REPAIRED PER PRI 622843-14 REV 1 & EJan 9, 2025 · N979AT · Boeing 717200 · Horizontal Stabilizer StructureSDR DALA2025011300266Floor Support · corrodedCORROSION ON FLOOR SUPPORTS OF STA 157-210 -X=45, STA 256 -X=44-24L, STA 174-176 BTW -X=10- 49, STA 200-157 X=10, STA 200-157 -X=10, STA 157-200 BTW X=44, STA 200 BTW X=44-42, AND STA 200-203 BTW -X=5 TO -X=43 AT PAX CABIN. SUMMARY OF NRC 00671: CORROSION LEVEJan 9, 2025 · N995AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2025011300265Bulkhead · corroded-AD- CORROSION ON FWD BULKHEAD OF LH WHEEL WELL BTW STA Y737 AND X=18 TO X=30 (UNDER SLANT PANELS). SUMMARY OF NRC 00140: CORROSION LEVEL 2. CORROSION ON FWD BULKHEAD OF LH WHEELL WELL BTW STA Y737 AND X=18 TO X=30 (UNDER SLANT PANELS) WAS REPAIRED PER PRI 622Jan 9, 2025 · N979AT · Boeing 717200 · Fuselage Main, BulkheadSDR DALA2025011300264Structure · damagedSCRATCHES AND MISSING MATERIAL WERE FOUND ON INTERIOR DIAMETER OF ATTACHMENT AREA AT RUDDER. SUMMARY OF NRC 00729: INTERIOR DIAMETER OF ATTACHMENT AREA AT RUDDER WAS REPAIRED PER PRI 622781-14 REV 2 & ER/A 622781-14 REV ORIGINAL. ASSOCIATED ER/A 14-622781 ADDEJan 9, 2025 · N979AT · Boeing 717200 · Rudder StructureSDR DALA2025011300274Skin · dentedDENT #4, XF=89.250" DAE=13.500"; DENT #5, XF=86.500" DAE=11.500"; DENT#6. XF=88.375" DAE=14"; AND DENT#26, XF=81.250" DAE=4.500" WERE FOUND OUT OF LIMITS ON LOWER SURFACE ON AFT MOVABLE FLAP VANE AT RH WING. SUMMARY OF NRC 00592: RIGHT WING AFT MOVABLE FLAP VAJan 9, 2025 · N995AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2025010900178Cusp Web · crackedCRACK ON CUSP WEB STA Y:715 X:60 IN PAX CABIN. SUMMARY OF NRC 00567: CUSP WEB STA Y:715 X:60 IN PAX CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 REPAIR 4, FIG 223 AND DWG 9910151-5. (LP #0752185)Jan 8, 2025 · N995AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2025010900177Pin · out of positionTAIL CONE EXIT RELEASE CAM PIN IS NOT 34.5 TO 38.5 DEGREES FROM THE CENTERLINE OF THE BASE AT AFT ACCESORIES COMPARTMENT. 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 00899: RELJan 8, 2025 · N981AT · Boeing 717200 · Aerodynamic FairingsSDR DALA2025010800158Rod End · damagedDAMAGED DURING ADJUSTMENT OF RH INBD SPOILER PANEL. THE HOLDDOWN ACTUATOR ROD-END INADVERTENTLY EXTENDED CAUSING A PUNCTURE ON RH INBD GUIDE VANE. SUMMARY OF NRC 00886: THE RH INBD GUIDE VANE WAS REPAIRED PER B717 SRM 51-70-02-0G PROCEDURE GENERAL AND IN REFERJan 7, 2025 · N981AT · Boeing 717200 · Drag Control SystemSDR DALA2025010700130Angle · crackedUPPER ANGLE COMMON TO FUSELAGE SKIN AND RH PYLON UPPER SKIN LOCATED AT Y=1178 CANTED WAS REMOVED. LOWER ANGLE COMMON TO REMOVED ANGLE WAS FOUND CRACKED. SUMMARY OF NRC 00820: LOWER ANGLE COMMON TO FUSELAGE SKIN AND RH PYLON UPPER SKIN LOCATED AT Y=1178 CANTED Jan 7, 2025 · N981AT · Boeing 717200 · Fuselage Miscellaneous Structure
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