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 DALA2025010700129Frame · cracked-AD- CRACK OF 1.00 IN ON UPPER RADIUS OF THE FRAME TAB OF THE OVERWING FRAME AT STA Y=696.000 RH (REF CARD 5310-01436-01D). SUMMARY OF NRC 0470: OVERWING FRAME AT STA Y=696.000 RH WAS REPLACED PER B717-200 SRM 51-41-05-0G, 51-41-02-0G, 51-41-01-0G, AND CARD 53Jan 6, 2025 · N979AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2025010700131Power Supply · no testTHE AFT EMERGENCY EXIT DOORS OVERWING LIGHTS, LT AND RT, ARE NOT COMING ON WHEN TESTED AT ROW 20. MAINTENANCE REPLACED THE B5-119 EMERGENCY POWER SUPPLY PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #6967194)Jan 5, 2025 · N603AT · Boeing 717200 · Emergency LightingSDR DALA2025010500067Cargo Track · corrodedCORROSION ALONG CARGO TRACK RH AT AFT CARGO COMPARTMENT. SUMMARY: CORROSION LEVEL 2. CORROSION ALONG TRACK RH BTW STA Y=813 TO STA Y=954, AT AFT CARGO COMPARTMENT WAS REMOVED PER B717-200 SRM 51-10-04-0G. (UT) THICKNESS MEASUREMENT WAS ACOMPLISHED WITH ORIGINAJan 4, 2025 · N979AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2025010700132Light · arcedLIGHT PRODUCES AN ELECTRICAL ARC WHEN THE ATTACHMENT BOLT TOUCHES THE SCREW NEXT TO THE LIGHT ATTACHMENT SOCKET. MAINTENANCE REPLACED THE F/O LIGHT ASSEMBLY PER B717 AMM 33-16. THE OPERATIONAL CHECK WAS GOOD AND THERE WAS NO LONGER ANY ARCHING. (LP #6555658)Jan 3, 2025 · N717JL · Boeing 717200 · Flight Compartment LightingSDR DALA2025020500872Spar Cap · cracked-AD- LEFT WING REAR SPAR LOWER CAP IB OF FLAP TRACK. CRACK INDICATION IN HOLE THAT IS 2 HOLES IB OF EXISTING CRACK, XRS 164. REF PRI 621050-14 REV 1 STEP 11 AND FIGURE 3. SUMMARY SEE NRC 006-0001:10-0557-8-8910/002 00039: REFERENCED PRI 621050-14 ALL REVISIONSJan 2, 2025 · N949AT · Boeing 717200 · Wing SparSDR DALA2025020500871Spar · cracked-AD- VISIBLE CRACK FOUND ON LEFT WING REAR SPAR LOWER CAP IB OF FLAP TRACK, OB OF THE TE RIB CLIP BETWEEN XRS 150.450 AND XRS 164.000. SUMMARY SEE NRC 006-0001:10-0557-8-8910/001 00017: COMPLIED WITH PRI 621050-14 REV 0, REV 1, REV 2, REV 3, REV 4, REV 5, REV Jan 2, 2025 · N949AT · Boeing 717200 · Wing SparSDR DALA2025020500870None · none-AD- WHILE IN MAINTENANCE, AA WORK CARD 5720-01103-01B RH WING XRS 164, REAR SPAR AND LWR SKIN INSPECTION WAS COMPLETED WITH NO FINDINGS. DAL BELIEVES ADDITIONAL INSPECTIONS BEYOND THE SCOPE OF AA WC 5720-01103-01B ARE NECESSARY TO VERIFY NO DAMAGE IS PRESENT Jan 2, 2025 · N949AT · Boeing 717200 · Standard Practices/StructuresSDR DALA2025010800157Stab System · out of adjustWHILE PERFORMING W/C 2740-01114-07, THE JACKSCREW DID NOT STOP AUTOMATICALLY AND CONTACTED THE UPPER STOP. HORIZ STAB ADJ REQUIRED PER B717 AMM 27-40-00 820-801 & INSPECTION OF THE JACK SCREW REQUIRED PER B717 AMM 27-41-04 220-802. C/W INSPECTION OF JACKSCREW Jan 2, 2025 · N947AT · Boeing 717200 · Flight Control SystemSDR DALA2025010300046Power Supply · faultedFOUND ROW 21 EMERGENCY EXIT LIGHT B5-230/P9 TO BE INOPERATIVE. MAINTENANCE TRIED A NEW EMERGENCY LIGHT BATTERY. NO HELP, REINSTALLED ORIGINAL. REPLACED POWER SUPPLY B5-230 PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #6733147)Jan 2, 2025 · N930AT · Boeing 717200 · Emergency LightingSDR DALA2025010300045Door Frame · corrodedCORROSION ON DOOR JAMB PAN. ALSO ON PREVIOUS REPAIR DOUBLER AT AFT CARGO COMPARMENT BTW STA Y=954 TO STA Y=994 APROX C2. SUMMARY OF NRC 00133: CORROSION LEVEL 2. DOOR JAMB PAN AT AFT CARGO COMPARTMENT BTW STA Y=954 TO STA Y=994 APPROX C2 WAS REPLACED PER B717-Jan 2, 2025 · N979AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2025010300047Battery Pack · inoperativeOVERHEAD EMERGENCY LIGHTS FROM ROW 15 TO 19 ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHTS BATTERY PACK FOR CORRESPONDING LIGHTS PER B717 AMM 33-51. OPERATIONAL CHECK WAS NORMAL. OK FOR SERVICE. (LP #6601810)Jan 1, 2025 · N961AT · Boeing 717200 · Emergency LightingSDR DALA2025010500068Unknown · fumesSHIP 9502 -FUMES/DE- THE FLIGHT ATTENDANT REPORTED A "RUBBER SMELL" COMING FROM ROW 26 IN THE CABIN. SMELL STAYED FAIRLY CONTAINED BUT DID MIGRATE TO OTHER ROWS. THE SOURCE COULD NOT BE IDENTIFIED SO THE PILOT DECLARED AN EMERGENCY WITH ATC. A FOLLOW-UP LOG PADec 31, 2024 · N942AT · Boeing 717200 · Air Distribution SystemSDR DALA2025010300044Skin · damagedSKIN AT FWD LOWER CORNER OF LAV WASTE DUMP CUT OUT PUSHED OUT APPROX .75" FWD LAV WASTE BOX. CREASE IN SKIN APPROX 4" LONG. MAX DEEP IN GAP BETWEEN SKIN AND WASTE BOX APPROX 1". PERFORMED EXTERNAL DOUBLER AND TRIPLER REPAIR IAW ER/A 622994-14 REV O. FOLLOW ON Dec 31, 2024 · N943AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2024123112105Spar · crackedCRACK AT LEFT WING REAR SPAR, PRI 623253-14 REV 0 ISSUED. REMOVE TANK PLATES 520FT, 520CB, AND TWO FUEL LINES FOR MAINTENANCE. REMOVED AND REINSTALLED L/H OVER WING BOOST PUMP PANEL TO F.O.M. PER B717 AMM 28-00. RE-INSTALLED TANK PLATE 520CB PER B717 AMM 28-00Dec 30, 2024 · N950AT · Boeing 717200 · Wing SparSDR DALA2024123112104Floor Support · corrodedCORROSION ON FLOOR SUPPORTS (3 EA), FROM STA Y=1022 TO STA Y=1063 ON X=44, X=52, AND X=-44 AT AFT PAX CABIN FLOOR. SUMMARY OF NRC 00459: CORROSION LEVEL 2. FLOOR SUPPORTS (3 EA), FROM STA Y=1022 TO STA Y=1063 ON X=44, X=52, AND X=-44 AT AFT PAX CABIN FLOOR WERDec 30, 2024 · N995AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024123112103Cusp Web · crackedCRACK ON CUSP WEB (LOWER SIDE) BTW X=47 AND STA 591 AT CPAX. SUMMARY OF NRC 00467: CUSP WEB (LOWER SIDE) BTW X=47 AND STA 591 AT CPAX WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 FIG 221 AND 51-41-02-0G. (LP #0736473)Dec 30, 2024 · N995AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024123012068Skin · crackedCRACK ON AFT UPPER CORNER SKIN OF RH SLIDING WINDOW FRAME AT COCKPIT. SUMMARY OF NRC 00707: AFT UPPER CORNER SKIN OF RH SLIDING WINDOW FRAME AT COCKPIT WAS REPAIRED PER B717-200 SRM 56-10-02-2R REPAIR 1 AND FIXED UPPER FLIGHT COMPARTMENT WINDOW RH WAS INSTALLEDec 29, 2024 · N979AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2024123012067Pan · crackedCRACK ON OUTER PAN AT FWD EDGE ON BEAM #3 WAS FOUND AT FWD CARGO COMPARTMENT DOOR. SUMMARY OF NRC 00405: CRACK ON OUTER PAN AT FWD EDGE ON BEAM #3 AT FWD CARGO DOOR COMPARTMENT WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1. (LP #0734792)Dec 29, 2024 · N995AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR HALA20241230082Light · inoperativeEVERY OTHER OVERHEAD EMERGENCY LIGHT IS INOP IN CABIN. REMOVED AND REPLACED EMER. LTS PER AMM 33-51-08/401. OPS CHECK OK. SECURITY CHECK OK. OK TO CONTINUE SERVICE.Dec 28, 2024 · N491HA · Boeing 717200 · Emergency LightingSDR DALA2024123012066Vane · dentedSEVERAL DENTS ON LOWER SKIN LH AFT MOVEABLE FLAP VANE. SUMMARY OF NRC 00250: DENTS (8 EA) ON LOWER SKIN LH AFT MOVABLE FLAP VANE WERE EVALUATED AND DENTS #1 TO #7 ARE OUT OF LIMITS PER B717-200 SRM 57-53-01-1A PROCEDURE 1 ALLOWABLE DAMAGE 1 PAR 3. A. AND WERE Dec 27, 2024 · N995AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2024122712036Reservoir · leakingSHIP 9573 -MISC- THE FLIGHT CREW DECLARED AN EMERGENCY DUE TO RIGHT HYDRAULIC SYSTEM PRESSURE LOSS AFTER GEAR EXTENSION. CORRECTIVE ACTION: MAINTENANCE FOUND THAT THE RIGHT HYDRAULIC RESERVOIR WAS LEAKING. THE RESERVOIR WAS REPLACED PER B717 AMM. OPERATION ANDDec 27, 2024 · N926AT · Boeing 717200 · Hydraulic Reservoir, MainSDR DALA2024122712034Pan · crackedCRACK ON PAN OF FWD AND AFT EDGE AT FWD CARGO DOOR BELOW BEAM 5. SUMMARY OF NRC-00143: PAN OF FWD AND AFT EDGE AT FWD CARGO DOOR BELOW BEAM 5 WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1. (LP #0730599)Dec 27, 2024 · N995AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024123012069Wire · overtempSHIP 9536 -DIV/DE- THE FLIGHT CREW DIVERTED THE AIRCRAFT TO DTW AND DECLARED AN EMERGENCY WITH ATC DUE TO BURNING SMELL IN THE CABIN AROUND ROW 17. AN OVERWEIGHT LANDING RESULTED BUT WAS UNEVENTFUL. CORRECTIVE ACTION: MAINTENANCE FOUND THAT THE PED POWER OUTLEDec 25, 2024 · N974AT · Boeing 717200 · Electrical Power System WiringSDR DALA2024122712035Battery Pack · inoperativeTHE FOUR LOWER OVERWING EXIT LIGHTS, LEFT AND RIGHT, ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND BATTERY R5-119 PER B717 AMM 33-51-03. SYSTEM NOW OPERATIONALLY CHECKS GOOD. THE AIRCRAFT IS OK FOR SERVICE. (LP #6976208)Dec 25, 2024 · N923AT · Boeing 717200 · Emergency LightingSDR DALA2024123012065Seat Track · corrodedCORROSION ON LH INB SEAT TRACK (X=22) ON STA Y=200-205 AT CPAX. SUMMARY OF NRC 00482: CORROSION LEVEL 2. CORROSION AT LH INB SEAT TRACK (X=22) ON STA Y=200-205 AT CPAX WAS REPAIRED PER B717-200 SRM 53-20-52-2R PROCEDURE 5 REPAIR 5. (LP #0726955)Dec 24, 2024 · N995AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2024122712033Angle · corrodedCORROSION ON CUSP ANGLE FROM STA Y=157 TO STA Y=200 BTW -X=61.5 TO -X=66 INNER STRUCTURE OF SERVICE DOOR JAMB AT CPAX. SUMMARY OF NRC 00506: CORROSION LEVEL 2. CORROSION ON CUSP ANGLE FROM STA Y=157 TO STA Y=200 BTW -X=61.5 TO -X=66 INNER STRUCTURE OF SERVICE Dec 24, 2024 · N981AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024122712032Pan · corrodedCORROSION ON E/E DOOR JAMB PAN STA Y=160 BTW LONG 29LH TO 29RH. SUMMARY OF NRC 00644: CORROSION LEVEL 2. CORROSION ON E/E DOOR JAMB PAN STA Y=160 BTW LONG 29LH TO 29RH WAS REPAIRED PER ER/A 623018-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 623018-14 RDec 24, 2024 · N978AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2024122712031Beam · crackedCRACK ON BEAM #1 APROX STA Y=190 AT PASSENGER ENTRANCE DOOR (L1). SUMMARY OF NRC 00255: BEAM #1 APROX STA Y=190 AT PASSENGER ENTRANCE DOOR (L1) WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 7 REPAIR 7. (LP #0726863)Dec 24, 2024 · N995AT · Boeing 717200 · Passenger/Crew DoorsSDR DALA2024122411973Cargo Track · corrodedCORROSION ON TRACK OF AFT CARGO COMPARTMENT STA Y=994 (DOOR JAMB AREA). SUMMARY OF NRC 00722: CORROSION LEVEL 2. TRACK OF AFT CARGO COMPARTMENT STA Y=994 (DOOR JAMB AREA) WAS REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-01-0G. (LP #0725967)Dec 24, 2024 · N979AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2024122712030Spar Cap · crackedCRACKS FOUND DURING INSPECTION OF LH WING REAR SPAR LOWER CAP RADIUS. CONTACT LIASON ENGINEERING FOR REPAIR PROCEDURES PRIOR TO FURTHER FLIGHT. FC 5720-01103 2ND FASTENER INBOARD OF FLAP HINGE FITTING EXTERIOR FROM TRAILING EDGE THROUGH FASTENER INTO RADIUS. MDec 23, 2024 · N950AT · Boeing 717200 · Wing SparSDR DALA2024122712029Pin · out of positionTHE INFLATION CABLE PIN WAS OUT OF PLACE. ALSO MISSING THE VALVE LOCK PIN ON THE FWD PASSENGER ENTRANCE DOOR SLIDE (L1). 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 00065: SLIDDec 23, 2024 · N979AT · Boeing 717200 · Escape SlideSDR HALA2024122380Unknown · noiseDURING TAKEOFF ROLL AT ABOUT 70 KNTS LOUD BANG ON THE RIGHT SIDE OF AC ALL SYSTEM INDICATIONS APPEAR TO BE NORMAL TKAEOFF ROLL ABORTED TAKEOFF AND BTB. PERFORMED INSPECTIONS OF LANDING GEAR HYD INLET OUTLET FLIGHT CTLS ENGINEERING REPORTED NO DEFECTS FAULTS ONDec 22, 2024 · N483HA · Boeing 717200 · Standard Practices/StructuresSDR DALA2024122311966Cusp Web · crackedCRACK ON CUSP WEB BTW STA Y=636-655 X=- 44 TO X=-60 AT PASSENGER CABIN (CPAX). SUMMARY OF NRC 826: CUSP WEB BTW STA Y=636-655 X=-44 TO X=-60 AT PASSENGER CABIN WAS REPAIRED PER B717 SRM 53-00-55-2R-4. (LP #0721136)Dec 21, 2024 · N979AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024122311963Support · crackedCRACK ON LH TRACK SUPPORT STA Y=918-915, STA Y=879-876, AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00252: LH TRACK SUPPORT STA Y=876 TO 1022 AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-20-52-2R- PROCEDURE 4 REPAIR 4. (LP #0721119)Dec 21, 2024 · N978AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2025010800167Blades · damagedSHIP 9502 -ATB- THE CREW RETURNED THE AIRCRAFT TO PHL DUE TO MULTIPLE COMPRESSOR STALLS DURING CLIMB OUT. CORRECTIVE ACTION: INSPECTION PERFORMED BORESCOPE INSPECTION AND FOUND NUMEROUS HPC STAGE 1 BLADES DAMAGED. THE POWERPLANT WAS REPLACED. (LP #6930842)Dec 20, 2024 · N942AT · Boeing 717200 · Turbine Engine Compressor SectionSDR DALA2024122311964Skin · damagedFUSELAGE DAMAGE AFT OF L1 DOOR. REPAIRED A/C PER ER/A 542469-14 REV A. REF 001-0002:0514-2000 NRC 6 FOR DOCUMENTATION OF WORK PERFORMED. (LP #6956730)Dec 20, 2024 · N992AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2024122311962Skin · ground damageAIRCRAFT SUSTAINED DAMAGE FROM JETWAY CONTACT AT LH FRAME STATION BS 237 BETWEEN STR 18L AND STR 17LH. SUMMARY NRC 001-0002:0514-2001/006 00006: COMPLIED WITH ER/A 542469-14 REV A. ENSURED PRI 542469-14 REV 0 MATCHES FINAL ERA. (LP #0719406)Dec 20, 2024 · N992AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2024122311965None · noneDTE TRACKING PER ER/A 542469-14 REV A. REPAIR APPROVAL IS LIMITED TO 12 MONTHS OF SERVICE. ER/A REVISION REQUIRED FOR SERVICE BEYOND THIS LIMIT. DTA REQUIRED IN ACCORDANCE WITH FAA AC 120-93. REPAIR APPROVAL LIMITED TO 12 MONTHS OF SERVICE AFTER ACCOMPLISHMENTDec 19, 2024 · N992AT · Boeing 717200 · Standard Practices/StructuresSDR DALA2024122311961Pan · crackedCRACK ON INNER PAN AT FWD EDGE BTW BEAM 1 AND 2 WAS FOUND ON AFT CARGO DOOR. SUMMARY OF NRC 00442: OUTER PAN FWD EDGE BTW BEAM 1 AND 2 WAS BLENDED OUT AND MEASURED AS FOLLOW: MINIOR DAMAGED TO SKIN EDGE NO MORE THAN 0.380" DEEP: BLEND OUT IS 0.125". REWORK AREDec 19, 2024 · N995AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024122311960Structure · corrodedCORROSION ON BARREL NUTS HOLES XH=-7 RH [7, 8, 11, 12, 16, 18, 21, 26, 28] AND XH=7 LH [10, 18, 26, 27, 29] AT HORIZONTAL STABILIZER CENTER BOX. SUMMARY OF NRC 00407: CORROSION LEVEL 2. BARREL NUTS HOLES XH=-7 RH [7, 8, 11, 12, 16, 18, 21, 26, 28] AND XH=7 LH Dec 19, 2024 · N978AT · Boeing 717200 · Horizontal Stabilizer StructureSDR DALA2024122311959Structure · corrodedCORROSION ON BARREL NUTS HOLES XH=-7 RH [7, 8, 11, 12, 16, 18, 21, 26, 28] AND XH=7 LH [10, 18, 26, 27, 29] AT HORIZONTAL STABILIZER CENTER BOX. SUMMARY OF NRC 00407: CORROSION LEVEL 2. CORRODED BARREL NUTS HOLES XH=-7 RH [7, 8, 11, 12, 16, 18, 21, 26, 28] ANDDec 19, 2024 · N978AT · Boeing 717200 · Horizontal Stabilizer StructureSDR DALA2024122311958Structure · wornFOUND WEAR ON BARREL NUT HOLE #30 AT LH HORIZONTAL STABILIZER CENTER. SUMMARY OF NRC 00754: BARREL NUT HOLE #30 AT LH HORIZONTAL STABILIZER CENTER WAS REPAIRED PER ER/A 622465-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. REPAIR APPROVAL IS LIMITED TO 24 MONTHSDec 19, 2024 · N978AT · Boeing 717200 · Horizontal Stabilizer StructureSDR DALA2024121911830Idg · failedSHIP 9579 -MISC/DE- THE FLIGHT CREW DECLARED AN EMERGENCY WITH ATC FOLLOWING THE "LEFT GENERATOR FAIL" MESSAGE DURING APPROACH INTO PHL. THE APU WAS ALREADY ON MEL. CORRECTIVE ACTION: MAINTENANCE REPLACED THE LEFT IDG, PERFORMED ALL OPERATIONAL CHECKS, AND RETDec 19, 2024 · N919AT · Boeing 717200 · AC Generator-AlternatorSDR DALA2024121911829Frame · corrodedCORROSION ON FRAME STA Y=908 FROM LONG 26LH TO LONG 29RH AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00609: CORROSION LEVEL 2. CORROSION ON FRAME STA Y=908 FROM LONG 26LH TO LONG 29RH AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 3 Dec 19, 2024 · N981AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2024121911828Cover · brokenBROKEN PLASTIC COVER OF TAIL CONE EXTENSION PULL LEVER 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: 00326 PLASTIC COVER OF TAIL CONE EXTENSION PULL Dec 19, 2024 · N995AT · Boeing 717200 · Aerodynamic FairingsSDR DALA2024121911827Bearing · wornWORN BEARING OF FLAP AND ELONGATED HOLES ON OUTB HINGE OF LH FLAP WERE FOUND. SUMMARY OF NRC 00684: OUTB HINGE OF LH FLAP WAS REPAIRED PER ER/A 622136-14 REV ORIG, SECTION I: PERMANENT REPAIR. "DTE" TIME CONTROLLED ITEM WITH LOG PAGE #0701683. ASSOCIATED ER/A Dec 19, 2024 · N978AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2024121911826Stop Fitting · crackedDOOR STOP FITTING #4 WAS FOUND CRACK ON INNER PAN FWD SIDE OF AFT CARGO DOOR. SUMMARY OF NRC 00716: INNER PAN ON FWD SIDE STOP #4 AT AFT CARGO COMPARTMENT DOOR WAS REPAIRED PER ER/A 622684-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 622684-14 REV 1. ASDec 18, 2024 · N979AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2024121811803Union · leakingSHIP 9538 -MISC/DE- THE FLIGHT CREW DECLARED AN EMERGENCY WITH ATC FOLLOWING THE RIGHT HYDRAULIC SYSTEM SHOWING A LOSS IN QUANTITY. THE QRH WAS COMPLIED WITH, BUT AN ALTERNATE GEAR EXTENSION WAS NOT REQUIRED. CORRECTIVE ACTION: MAINTENANCE CYCLED THE MLG DOORSDec 18, 2024 · N993AT · Boeing 717200 · Hydraulic System, MainSDR DALA2024121811802Battery Pack · inoperativeBOTH OF THE AFT EMERGENCY OVERWING EXIT DOOR LIGHTS ARE INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY (B5-230) PER B717 AMM 33-51-04. LIGHT OPERATIONS CHECK GOOD. OK FOR SERVICE. (LP #6930841)Dec 18, 2024 · N942AT · Boeing 717200 · Emergency LightingSDR DALA2024121811801Skin · crackedCRACKS ON EXTERNAL SKIN STA Y 1153, BTW LONGERON 3L/4L AND BTW LONGERON 2R/3R AT AFT FUSELAGE. SUMMARY OF NRC 00050: EXTERNAL SKIN STA Y 1153, BTW LONGERON 3L/4L AND BTW LONGERON 2R/3R AT AFT FUSELAGE WAS REPAIRED PER ER/A 621926-14 REV ORIG SECTION I PERMANENDec 18, 2024 · N978AT · Boeing 717200 · Fuselage Main, Plate/Skin
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