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 DALA2024091809137Web · damagedELONGATED HOLE ON WEB (DOOR JAMB) BTW STA Y=362 TO STA Y=370 AND L24R TO L26R AND STA Y=427 TO STA Y=434 L25R TO L26R AT FWD CARGO. SUMMARY OF NRC 00234: ELONGATED HOLE ON WEBS (DOOR JAMB) BTW STA Y=362 TO STA Y=370 AND L24R TO L26R AND STA Y=427 TO STA Y=434 Sep 12, 2024 · N990AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024091609047Shear Tie · crackedFABRICATED PARTS IN REFERENCE NRC 00592 AND PRI 620225-14 REV 0. MANUFACTURE SHEAR CLIP (AFT ACCESS). CRACK WAS FOUND ON SHEAR CLIP IN REFERENCE NRC 00592: FABRICATE SHEAR CLIP PER PRI 620225-14 REV 4 AND ER/A 620225-14 REV OROGINAL, SECTION I PERMANENT REPAIRSep 12, 2024 · N989AT · Boeing 717200 · Fuselage Internal Mounting StructureSDR DALA2024091308984Door Frame · damagedELONGATED HOLES ON WEB (DOOR JAMB) BTW STA Y=362 TO STA Y=370 AND L24R TO L26R AND STA Y=427 TO STA Y=434 L25R TO L26R AT FWD CARGO. SUMMARY OF NRC 00234: ELONGATED HOLES ON WEB (DOOR JAMB) BTW STA Y=362 TO STA Y=370 AND L24R TO L26R AND STA Y=427 TO STA Y=434Sep 12, 2024 · N990AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2024091308983Floorbeam · crackedCORROSION ON FLOOR SUPPORT ON W1 STA Y=198 TO Y=160 X=-5.5 TO X=-9 AT PAX CABIN. SUMMARY OF NRC 00748: CORROSION LEVEL 2. SUPPORT WAS REPLACED ON W1 STA Y=198 TO Y=160 X=-5.5 TO X=-9 AT PAX CABIN PER B717-200 SRM 51-41-01-0G. (LP #0552652)Sep 12, 2024 · N990AT · Boeing 717200 · Fuselage Main, Floor BeamSDR DALA2024091308982Skin · crackedCRACK ON SKIN, SHEAR CLIP, AND SHEAR TIE OUTBOARD FASTENER AT STA Y=1152 AND LONG 2L ON AFT ACCESORY COMPARTMENT (IN REFERENCE TO ERA 95-520358-14 REV ORIGINAL FIGURE 4). SUMMARY OF NRC 00592: SHEAR TIE OUTBOARD FASTENER AT STA Y=1152 AND LONG 2L ON AFT ACCESOSep 12, 2024 · N989AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2024091308981Cusp Web · crackedCRACKED CUSP WEB ON STA Y=656 X=-56 TO -60 AT PASSENGER COMPARMENT. SUMMARY OF NRC 00413: CUSP WEB ON STA Y=656 X=-56 TO -60 AT PASSENGER COMPARMENT WAS REPLACED PER B717 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4. (LP #0551885)Sep 12, 2024 · N990AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2025040402562Hinge Fitting · damagedCORROSION AND SCRATCHES ON HOLES OF OUTBRD WING FLAP HINGE FITTING AND ON SETTLEMENT AREA OF OUTBRD WING FLAP HINGE FITTING AT LH WING. SUMMARY OF NRC 00785: CORROSION LEVEL 2. OUTBRD WING FLAP HINGE FITTING AND ON SETTLEMENT AREA OF OUTB WING FLAP HINGE FITTISep 11, 2024 · N990AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2024091108922Pan · crackedCRACK ON INNER PAN FWD SIDE OF BEAM #4 AT AFT CARGO COMPARTMENT DOOR. SUMMARY OF NRC 00422: INNER PAN FWD SIDE OF BEAM #4 AT AFT CARGO COMPARTMENT DOOR WAS REPAIRED PER ERA 619283-14, REV ORIGINAL, SECTION I, PERMANENT REPAIR. (LP #0550050)Sep 11, 2024 · N717JL · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024091008882Lug · corrodedCORROSION ON OUTER/INNER LUGS (INNER PART) AND BUSHING OF LH FLAP OUTBOARD HINGE. SUMMARY OF NRC 00657: CORROSION LEVEL 2. LH FLAP OUTBOARD HINGE WAS REPAIRED PER PRI 619369-14 REV 4 & ER/A 619369-14 REV ORIG. REPAIR APPROVAL IS LIMITED TO 24 MONTHS FROM 29AUGSep 9, 2024 · N980AT · Boeing 717200 · Wing, Control Surface Attach FittingsSDR DALA2024091008881Frame · corrodedCORROSION ON FRAME BTW STA Y=1023 LONGERON 29L AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00754: CORROSION LEVEL 2. CORROSION ON FRAME BTW STA Y=1023 LONGERON 29L AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 3. (LP #0542411)Sep 6, 2024 · N989AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2026080404487Skin · corrodedCORROSION STABILIZERS RT HORIZONTAL STABILIZER UPPER AFT SKIN PANEL BARREL NUT HOLE #11. REPAIRED PER ERA 620136-14. (0541097) AIRCRAFT WAS GROUNDED.Sep 5, 2024 · N989AT · Boeing 717200 · Horizontal Stabilizer, Plate/SkinSDR DALA2024090608757Access Panel · corrodedCORROSION INSIDE HOLE #33C LWR LH INSIDE ACCESS PANEL 350AB AT STABILIZER CENTER BOX. SUMMARY OF NRC 00399: CORROSION LEVEL 2. HOLE #33C LWR LH INSIDE ACCESS PANEL 350AB AT STABILIZER CENTER BOX WAS REPAIRED PER ER/A 620168-14 REV ORIGINAL, SECTION 1: PERMANENSep 5, 2024 · N989AT · Boeing 717200 · Horizontal Stabilizer StructureSDR DALA2024090608756Barrel Nut · corrodedCORROSION IN BARREL NUT HOLE #11RH AT HORIZONTAL STABILIZER IN REF NRC 00400. SUMMARY OF NRC 00649: CORROSION LEVEL 2. BARREL NUT HOLE #11RH AT HORIZONTAL STABILIZER WAS REPAIRED PER PRI 620136-14 REV 3 & ER/A 620136-14 REV ORIG SECTION I: PERMANENT REPAIR. ASSep 5, 2024 · N989AT · Boeing 717200 · Horizontal Stabilizer StructureSDR DALA2024090608755Cable · brokenMAINTENANCE FOUND A BROKEN KEVLAR CABLE AT THE TAIL CONE SLIDE. 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 00917: THE KEVLAR CABLE AT TAIL CONE SLIDE WAS REPLACED PER B717 AMMSep 5, 2024 · N717JL · Boeing 717200 · Aerodynamic FairingsSDR DALA2024090608754Floor Support · crackedCRACK ON INTERCOSTAL BTW STA Y=636 X=0 (CEILING AREA) AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00231: INTERCOSTAL BTW STA Y=636 X=0 (CEILING AREA) AT FWD CARGO COMPARTMENT WAS REPAIRED PER B717 SRM 53-00-00-2R REPAIR 1. (LP #0540825)Sep 5, 2024 · N990AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024090508739Floorbeam · corrodedCORROSION ON FLOORBEAM STA Y=653 BTW LONG 28L AND LONG 28R AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00135: CORROSION LEVEL 2. FLOORBEAM STA Y=653 BTW LONG 28L AND LONG 28R AT FWD CARGO COMPARTMENT WAS REPLACED PER DWG 5971111 REV F AND PER B717-200 SRM 51-41-Sep 4, 2024 · N951AT · Boeing 717200 · Fuselage Main, Floor BeamSDR DALA2024090408735Light · intermittentWITH THE COCKPIT EMERGENCY LIGHT SWITCH IN THE ARM POSITION, THE CABIN EMERGENCY LIGHTS ILLUMINATE INTERMITTANTLY DURING FLIGHT. MAINTENANCE TROUBLESHOT PER B717 FIM 33-50-00 810-801 AND FAULT WAS INTERMITANT. NO 60 DAY HISTORY. AIRCRAFT OK FOR SERVICE. (LP #5Sep 4, 2024 · N930AT · Boeing 717200 · Emergency LightingSDR DALA2024090408734Hinge Fitting · corrodedWEAR AND CORROSION ON HOLES OF LH FLAP HINGE FITTING #3. SUMMARY OF NRC 0885: CORROSION LEVEL 2. LH FLAP HINGE FITTING #3 WAS REPLACED BY A SERVICEABLE PER B717 AMM 57-55-25. (LP #0537751)Sep 3, 2024 · N717JL · Boeing 717200 · Trailing Edge FlapsSDR DALA2024090408733Pan · corrodedCORROSION ON JAMB PAN (BTW LONG 25RH-29RH) LOWER EDGE AND AFT EDGE AT FWD CARGO DOOR COMPARTMENT. SUMMARY OF NRC 00144: CORROSION LEVEL 2. JAMB PAN (BTW LONG 25RH-29RH) FWD CARGO DOOR COMPARTMENT WAS REPLACED PER B717-200 SRM 53-20-15-2R PROCEDURE 6 REPAIR 6. Sep 3, 2024 · N951AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024090308638Intercostal · corrodedCORROSION ON INTERCOSTAL BTW STA 200-218, L28R-L29R AT E/E COMPARTMENT. SUMMARY OF NRC 00804: CORROSION LEVEL 2. INTERCOSTAL BTW STA 200-218, L28R-L29R AT E/E COMPARTMENT WAS REPLACED PER DRAWING 9923686 REV D AND NRC 00285. (LP #0535463)Sep 2, 2024 · N951AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024090308637Cusp Web · crackedCRACK ON CUSP WEB STA Y=645 X=44, Y=656 X=57, AND Y=633 X=44 AT LH PASSENGER CABIN (CPAX). SUMMARY OF NRC 00516: CUSP WEB STA Y=645 X=44, Y=656 X=57, AND Y=633 X=44 AT LH PASSENGER CABIN WERE FABRCATED AND REPAIRED PER DWG 9910151 REV CH, B717 SRM 51-70-10-2R Sep 2, 2024 · N989AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024090308636Former · crackedCRACK FORMER ON INTERNAL STRUCTURE BTW BEAM 4/5 FWD EDGE AT L1 DOOR. L1. SUMMARY OF NRC 00118: FORMER ON INTERNAL STRUCTURE BTW BEAM 4/5 FWD EDGE AT L1 DOOR WAS REPAIRED PER B717-200 SRM 52-10-02-2R, PROCEDURE 3, REPAIR 3. (LP #0533710)Sep 1, 2024 · N989AT · Boeing 717200 · Passenger/Crew DoorsSDR DALA2024090308635Pan · crackedCRACK ON AFT PAN INTERSECTION WITH BEAM #5, CRACK ON FWD PAN INTERSECTION WITH BEAM #3 , 3) CRACK ON FWD PAN INTERSECTION WITH BEAM #5 ON FWD CARGO DOOR. SUMMARY OF NRC 00132: AFT PAN INTERSECTION WITH BEAM #5, FWD PAN INTERSECTION WITH BEAM #3, AND FWD PAN INSep 1, 2024 · N989AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024090408732Control System · out of adjust-AD- AMDS 2740-01114-07 STEP 6: DUE RESULT OF THE STEP 6A "ADJUST THE HORIZONTAL STABILIZER TRIM SYSTEM AND SHUTOFF CONTROL SYSTEM AMM 27-40-00 820-801. SUMMARY NRC 00298: HORIZONTAL STABILIZER TRIM SYSTEM AND SHUTOFF CONTROL SYSTEM WAS ADJUSTED PER B717-200 AAug 31, 2024 · N717JL · Boeing 717200 · Stabilizer Control SystemSDR DALA2024090308634Cusp Web · corrodedCORROSION ON LH CUSP WEB UPPER/LOWER SURFACES BTW STA Y=470 AND STA Y=870-889 AT PAX CABIN. SUMMARY OF NRC 00753: CORROSION LEVEL 2. LH CUSP WEB UPPER/LOWER SURFACES BTW STA Y=470 AND STA Y=870-889 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R REPAIR Aug 31, 2024 · N951AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024090308633Doubler · corrodedCORROSION ON DOUBLER PRODUCTION OF MASTER DRAIN BTW STA Y=199 AND Y=218, L28R, AND L29R. ALSO STA Y=163, Y= 183 BTW L29L AND L30 AT E/E COMPARTMENT. SUMMARY OF NRC 00295: CORROSION LEVEL 2. PRODUCTION DOUBLER OF MASTER DRAIN BTW STA Y=199 AND Y=218 L28R AND L2Aug 30, 2024 · N951AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2024083008600Cap · crackedCRACK ON CAP STA Y=1022 & LONG 7R ON PASSENGER CABIN. SUMMARY OF NRC 00554: CAP STA Y=1022 & LONG 7R ON PASSENGER CABIN WAS REPAIRED PER ERA 620017-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 620017-14 REV 1. ASSOCIATED ER/A 14-620017 ADDED FOR AC 9527Aug 30, 2024 · N989AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2024090408731Intercostal · crackedCRACK ON INTERCOSTAL 2 (EA) STA Y=1225 LONGERON 1 AT AFT ACCESORIES COMPARTMENT. SUMMARY OF NRC 00361: INTERCOSTAL 2 (EA) STA Y=1225 LONGERON 1 AT AFT ACCESORIES COMPARTMENT WERE REPLACED PER B717-200 SRM 51- 41-02-0G AND 51-42-05-0G AND SPRINGS WERE REMOVED AAug 29, 2024 · N989AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024083008601Sign · inoperativeFOUND L/H AND R/H OVERWING EXIT DOOR SIDE PANEL IDENTIFIER SIGN INOPERATIVE. CONFIRMED NO POWER AT PIN 1 OF EITHER EEI. VERIFIED GOOD GROUND. POWER SUPPLY B5-118 TO EEI SIGNS (L2-834 AND L2-835). FOUND FUSES F3 AND F4 BLOWN IN POWER SUPPLY. REPLACED POWER SUPPAug 29, 2024 · N961AT · Boeing 717200 · Emergency LightingSDR DALA2024083008599Hinge Fitting · corrodedCORROSION WAS FOUND ON THE LH FLAP INBOARD HINGE FITTING FASTENER HOLES (8 ATTACH POINT) IN REF NRC 258. SUMMARY OF NRC 00861: LEVEL CORROSION 2. LH FLAP INBOARD HINGE FITTING WAS REPLACED PER B717 AMM 57-55-25. (LP #0528717)Aug 29, 2024 · N717JL · Boeing 717200 · Trailing Edge FlapsSDR DALA2024083008598Longeron · crackedCRACK ON LONGERONS 06R, 05R, 04R, 03R STA Y=1022 ON PASSENGER CABIN. SUMMARY OF NRC 00553: LONGERONS 06R, 05R, 04R, 03R STA Y=1022 ON PASSENGER CABIN WERE REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURE 2. (LP #0527480)Aug 29, 2024 · N989AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2024083008597Beam · crackedCRACK BULKHEAD VERTICAL BEAM STA Y=813 -X=24 AT AFT CARGO COMPARMENT. SUMMARY OF NRC 00225: BULKHEAD VERTICAL BEAM STA Y=813 -X=24 AT AFT CARGO COMPARMENT WAS REPAIRED PER B717-200 SRM 51-70-11-2R. PROCEDURE 2 REPAIR 2, FIG 201. (LP #0527465)Aug 29, 2024 · N951AT · Boeing 717200 · Fuselage Main, BulkheadSDR DALA2024083008596Cap · crackedCRACK ON UPPER CAP STA Y=1022 AND LONGERON #7 LH AT CABIN PAX. SUMMARY OF NRC 000367: UPPER CAP STA Y=1022 AND LONGERON #7 LH AT CABIN PAX WAS REPAIRED PER PRI 619642-14 REV 1 AND ER/A 619642-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-6196Aug 28, 2024 · N717JL · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024083008595Window Frame · crackedCRACK WAS FOUND ON FRAME ON CUTOUT UPPER AFTER CORNER OF RH SLIDING WINDOW. SUMMARY OF NRC 00693: FRAME ON CUTOUT UPPER AFTER CORNER OF RH SLIDING WINDOW WAS REPAIRED PER B717-200 SRM 56-10-02-2R PROCEDURE 1 REPAIR 1. (LP #0526479)Aug 28, 2024 · N951AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2024083008594Barrel Nut · corrodedCORROSION ON THE BARREL NUT HOLES #26, #27, #28, AND #30, STA HX 6.625 RIGHT, STABILIZER CENTER BOX. SUMMARY OF NRC 00407: BARREL NUT HOLES #26, #27, #28, AND #30, STA HX 6.625 RIGHT, STABILIZER CENTER BOX WERE REPAIRED PER ER/A 619552-14 REV ORIGINAL. ASSOCIAAug 28, 2024 · N717JL · Boeing 717200 · Horizontal Stabilizer Miscellaneous StructureSDR DALA2024083008593Beam · crackedCRACK BEAM #1 AFT EDGE AT L1 DOOR PTAS. SUMMARY OF NRC 00320: BEAM #1 AFT EDGE AT L1 DOOR PTAS WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 7 REPAIR 7. (LP #0526246)Aug 28, 2024 · N989AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2024082808523Web · crackedAIRCRAFT 9510, CRACK UNDER, INBD WEB RH APPROX. BEHIND FLOOR BEAM ON STA Y=715 AT CPAX. CORRECTIVE ACTION: INBD WEB RH APPROX. BEHIND FLOOR BEAM ON STA Y=715 AT CPAX WAS REPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 2 REPAIR 2. (LP 0525055)Aug 27, 2024 · N951AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024082808522Cusp Web · corrodedAIRCRAFT 9510, CORROSION OUT OF LIMITS WAS FOUND ON PASSENGER CUSP WEB STRUCTURE BTW Y=870 - 889 AND X=-54 TO X=-60 ON PASSENGER CABIN. CORRECTIVE ACTION: CORROSION LEVEL 2- CUSP WEB STRUCTURE BTW Y=870 - 889 AND X=-54 TO X=-60 ON PASSENGER CABIN WAS REPAIRED Aug 27, 2024 · N951AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024082808521Seat Track · crackedAIRCRAFT 9527, AFTER SEAT TRACK X = -44 BTW STA Y = 646 TO Y = 775 REMOVAL, CRACK ON HOLES AT WEB BTW STA 648 AND STA 650. CORRECTIVE ACTION: WEB BTW STA 648 AND STA 650 WAS REPAIRED PER B717 SRM 51-41-02-0G AND B717-200 SRM 51-70-10-2R-2. (LP 0524830)Aug 27, 2024 · N989AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2024082708491Door Frame · corrodedAIRCRAFT 9550, CORROSION ON DOOR JAMB E/E STA Y=133 BTW LONG 29 RH TO 29 LH ALSO ON STA Y=160 FOUND PREVIUOS HOLE PLUGGED LIKE REPAIR AND NO DECAL FOUND. CORRECTIVE ACTION: CORROSION LEVEL 2 // DOOR JAMB E/E STA Y=133 BTW LONG 29 RH TO 29 LH ALSO ON STA Y=160 Aug 27, 2024 · N717JL · Boeing 717200 · Fuselage Main, StructureSDR DALA2024082708490Longeron · crackedAIRCRAFT 9510, CRACK ON LONGERON END (2EAS) FROM STA 1133 BTW LONG 2 LH TO LONG 2RH OF AFT ACCESSORY COMPARTMENT. CORRECTIVE ACTION: LONGERON END FROM STA 1133 LONG 2RH OF AFT ACCESSORY COMPARTMENT WAS REPAIRED PER B-717-200 SRM 53-00-05-2R PROCEDURE 2 FIG.201Aug 27, 2024 · N951AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2024082708493Lamp · inoperativeAIRCRAFT 9576, EXT OVERHEAD IND NEEDS RELAMPED. CORRECTIVE ACTION: RELAMPED EXT IND OVERHEAD. OPS CK GOOD. (LP 5945559)Aug 26, 2024 · N608AT · Boeing 717200 · Emergency LightingSDR DALA2024082708492Lens · missingAIRCRAFT 9584, EMERGENCY LENS COVER AT 26CDE IS MISSING. CEILING EMERGENCY LIGHT. CORRECTIVE ACTION: INSTALLED EMERGENCY CEILING LENS COVER PER B717 AMM 33-51. (LP 5719964)Aug 26, 2024 · N986AT · Boeing 717200 · Emergency LightingSDR DALA2024082708489Cusp Web · corrodedAIRCRAFT 9510, CORROSIONS ON CUSP MEMBRANE (WEB) RH ON SEVERAL LOCATIONS FROM STA Y=560 TO STA Y=579 AND STA Y=503 TO STA Y=522 AND STA Y=484 TO STA Y=503 AND STA Y=446 TO STA Y=465 AT CPAX. CORRECTIVE ACTION: CUSP MEMBRANE (WEB) RH ON LOCATIONS FROM STA Y=560Aug 26, 2024 · N951AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024082708488Cusp Web · crackedAIRCRAFT 9510, INITIAL INSPECTION: CRACK ON CUSP MEMBRANE (WEB) RH BTW STA Y=389 TO STA Y=427 AT CPAX. CORRECTIVE ACTION: CUSP MEMBRANE (WEB) RH BTW STA Y=389 TO STA Y=427 AT CPAX WAS REPAIRED PER B717-200 SRM 53-00-55-2R FIGURE 223. (LP 0523259)Aug 26, 2024 · N951AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024082708487Cusp Web · crackedAIRCRAFT 9510, AFTER BLEND OUT CRACKS WERE FOUND AT LH CUSP WEB ON STATIONS Y= 813-832 AND STA Y= 832-841 AT PAX CABIN. CORRECTIVE ACTION: CUSP WEB ON STATIONS Y= 813-832 AND STA Y= 832-841 AT PAX CABIN. WAS REPAIRED PER B717-200 SRM-53-00-55-2R-4. (LP 0523187Aug 26, 2024 · N951AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024082708486Window Frame · crackedAIRCRAFT 9510, HIDDEN DISCPRECANCY; AFTER BRACKET WAS REMOVED, CRACK WAS FOUND ON FRAME ON CUTOUT UPPER AFTER CORNER OF LH SLIDING WINDOW. CORRECTIVE ACTION: FRAME ON CUTOUT UPPER AFTER CORNER OF LH SLIDING WINDOW WAS REPAIRED PER B717-200 SRM 56-10-02-2R PROCAug 26, 2024 · N951AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2024082608452Battery · inoperativeBOTH EMERGENCY LIGHTS IN CABIN ABOVE AFT OVERWING EXITS ARE INOP. CORRECTIVE ACTION: REPLACED BATTERY AT STA 426.Aug 26, 2024 · N986AT · Boeing 717200 · Emergency LightingSDR HALA20240826043Landing Gear · malfunctionedNOSE GEAR DID NO RETRACT ON DEPARTURE WHEN THE GEAR HANDLE WAS MOVED UP. NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED. COMPLETED QRH PROCEDURE. GEAR RETRACTED NORMALLY. PERFORM VISUAL INSPECTION LANDING GEAR CONTROL VALVE, RETRACT CYLINDER, BUNGEE, ALSO SERVICEAug 25, 2024 · N495HA · Boeing 717200 · Landing Gear Retraction/Extension SystemSDR DALA2024082508422Window Frame · crackedAIRCRAFT 9527, CRACK LH SLIDING WINDOW FRAME, JUST AFT UPPER CORNER OF INNER PLATE SKIN AT CREW CABIN. CPRRECTIVE ACTION: LH SLIDING WINDOW FRAME, JUST AFT UPPER CORNER OF INNER PLATE SKIN AT CREW CABIN WAS REPAIRED PER B717 SRM 56-10-02-2R-1. (LP 0519523)Aug 24, 2024 · N989AT · Boeing 717200 · Fuselage Main, Structure
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