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 DALA2025040802707Cable · brokenTHE FLIGHT ATTENDANT FOUND THAT THE FRONT SERVICE DOOR EMERGENCY CABLE TO BAR WAS BROKEN. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE INSTALLED A NEW 1R DOOR SLIDE LATCH/LANYARD AMar 27, 2025 · N961AT · Boeing 717200 · Emergency EquipmentSDR DALA2025040802696Lanyard · severedFOUND R1 DOOR SLIDE RELEASE LANYARD CABLE SEVERED. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE REPLACED THE R1 DOOR SLIDE RELEASE LANYARD ASSEMBLY REF B717 AMM 25-61-03. (LP #6874Mar 27, 2025 · N945AT · Boeing 717200 · Emergency EquipmentSDR DALA2025040102422Structure · cracked-AD- COMPLIED WITH AMDS CARD 5720-01103-01B. REQUIRES COMPLETION OF PRI 623843-14AD DUE TO CRACK INDICATION FOUND DURING INSP. COMPLIED WITH PRI 623843-14AD REV 0,1,2, & 3. COMPARED PRI 623843-14AD REV 0,1,2, & 3 WITH ERA 623843-14AD REV ORIG AND ALL ITEMS MATMar 27, 2025 · N937AT · Boeing 717200 · Wing StructureSDR HALA20250331022Bracket · corrodedSURFACE CORROSION ON "L" BRACKET UNDER MAINT PLATFORM STATION 1095 . MARKED. 1. REMOVED TEE EXTRUSION FROM WALKWAY STRUCTURE. FABRICATED NEW TEE PER BOEING DRAWING# 9915537. TREATED, PRIMED AND PAINTED PER SRM 51-22-01. INSTALLED NEW TEE PER BOEING DRAWING# 9Mar 27, 2025 · N486HA · Boeing 717200 · Fuselage Miscellaneous StructureSDR HALA20250331021Frame · corrodedNUMEROUS CORROSION ON FRAME 1138 (M). CUTOUT APPROX 4 INCHES OF OUT OF LIMITS CORROSION ON STA 1138 FRAME BETWEEN LEFT L29 AND L30, HFC CUTOUT NO CRACKS NOTED. REMOVED REMAINING S/C AT STA 1138 FRAME , CLEANED AND TREATED PRIME AND PAINTED PER SRM 51-10-04 MMar 27, 2025 · N486HA · Boeing 717200 · Fuselage Main, FrameSDR DALA2025033102349Spar · cracked-AD- CRACK FOUND IN LWR AFT LEG OF LWR REAR SPAR JUST OB OF FLAP FITTING @ XRS170 DURING LT WING REAR SPAR INSP AMDS #5720-01103-01A. COMPLIED WITH PRI 623680-14AD REVS 0,1,2,3,4,5,6, & 7. COMPARED PRI 623680-14AD REVS 0,1,2,3,4,5,6, & 7 WITH ERA 623680-14AD RMar 27, 2025 · N937AT · Boeing 717200 · Wing SparSDR DALA2025033102348Skin · dentedPERFORM REPAIR TO DENT ON EXTERNAL FUSELAGE SKIN BTW STA 237-256 BTW LONG 15RH TO 16RH JUST BELOW THE BEAUTY STRAP. SUMMARY OF NRC 00637: SKIN BTW STA 237-256 BTW LONG 15RH TO 16RH JUST BELOW THE BEAUTY STRAP WAS REPAIRED PER ER/A 624583-14AD REV ORIGINAL SECTMar 27, 2025 · N998AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2025040102468Frame · corrodedFS 1022, LOWER PRIOR FRAME REPAIR AT STR 29LT-30 IS CORRODED. SUMMARY SEE NRC 001-0545:5331-2001/010 01244: CORROSION LEVEL 2. REPAIRED 3 ROLLED Z-FRAME REPAIR SPLICE PER B717-200 SRM 53-20-07-2R. (LP #0879160)Mar 26, 2025 · N925AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2025033102347Skin · dentedSEVERAL DENTS ON EXTERNAL SKIN OF FWD CARGO DOOR. SUMMARY OF NRC 00025: EXTERNAL SKIN OF FWD CARGO DOOR WAS REPAIRED PER B717-200 SRM 52-00-01-2R PROCEDURE 8 REPAIR 8. PERFORM AN EXTERNAL GVI OF THE REPAIR DOUBLERS ON FWD CARGO DOOR EVERY C-CHECK PER B717-200 Mar 26, 2025 · N940AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2025033102346Longeron · crackedCRACK LONGERON #2RH AT STA Y=1133 AT 12HRS POSITION AT AFT ACCESORY COMPARTMENT. SUMMARY OF NRC 00456: LONGERON #2RH AT STA Y=1133 AT 12HRS POSITION AT AFT ACCESORY COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURE 2 REPAIR 2 FIG 201. (LP #087885Mar 26, 2025 · N998AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2025032502209Longeron · corrodedCORROSION ON END-LONGERON BTW STA 1002 LONGERON 27RH AT AFT CARGO COMPARTMENT. SUMMARY OF THE NRC 00284: CORROSION LEVEL 2. END-LONGERON BTW STA 1002 LONGERON 27RH AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-05-0G. (UT) THICKNESS MEASURED WAS Mar 24, 2025 · N998AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2025032402192Pump · leakingSHIP 9573 -ATB- ON ROTATION, THE CREW RECEIVED A "HYD R LO PRESS" MESSAGE AND THE INABILITY TO RETRACT THE GEAR. THEY MOVED THE GEAR SELECTION LEVER DOWN AND RECEIVED THREE GREEN "GEAR SAFE" INDICATIONS. AN EMERGENCY WAS DECLARED WITH ATC, THE FLIGHT RETURNED Mar 23, 2025 · N926AT · Boeing 717200 · Hydraulic Pump (Electric/Engine), MainSDR DALA2025032402191Skin · dentedDENT ON UPPER MID AREA NEAR L/E AT LH WING FWD MOVABLE VANE. SUMMARY OF NRC 00554: AREA DAMAGE WAS REPAIRED ON UPPER MID AREA NEAR L/E AT LH WING FWD MOVABLE VANE PER B717-200 SRM 57-53-01-2R PROCEDURE 1 REPAIR 1 PAR 4. (LP #0873498)Mar 23, 2025 · N938AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2025032402190Support · corrodedCORROSION ON INNER STRUCTURE OF RUDDER YOKE BEARING SUPPORT HOUSING. SUMMARY OF NRC 00770: CORROSION LEVEL 2. AREA ON INNER STRUCTURE OF RUDDER YOKE BEARING SUPPORT HOUSING WAS REPAIRED PER ER/A 619864-14TR REV ORIGINAL SECTION I PERMANENT REPAIR. ASSOCIATED EMar 23, 2025 · N998AT · Boeing 717200 · Rudder StructureSDR DALA2025040802695Release Mech · out of adjustTHE TAILCONE RELEASE MECHANISM CAM WAS FOUND TO BE INCORRECTLY ADJUSTED: PIN ALIGMENT IS MORE THAN 38.5. 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 00166: TAILCONE RELEASE MECMar 22, 2025 · N940AT · Boeing 717200 · Aerodynamic FairingsSDR DALA2025032402189Pan · crackedCRACKED PAN ON AFT EDGE OF AFT CARGO COMPARMENT DOOR BTW BEAM 1-2. SUMMARY OF NRC 00096: PAN ON AFT EDGE OF AFT CARGO COMPARMENT DOOR BTW BEAM 1-2 WAS REPAIRED PER B717-200 SRM 52-30-02-2R REPAIR 8 FIGURE 202, 51-41-02-0G PROCEDURE GENERAL, AND 51-41-05-0G. (LMar 22, 2025 · N938AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2025032402188Beam · crackedCRACK ON BEAM #8 AFT SIDE AT PASSENGER DOOR. SUMMARY OF NRC 00083: BEAM #8 AFT SIDE AT PASSENGER DOOR WAS REPAIRED PER B717-200 SRM 52-10-02-2R REPAIR 14 PAR 6. (LP #0871639)Mar 22, 2025 · N938AT · Boeing 717200 · Passenger/Crew DoorsSDR DALA2025032402187Pan · crackedA CRACK WAS FOUND ON THE #2 INNER PAN AT AFT EDGE OF THE FWD CARGO COMPARMENT DOOR. SUMMARY OF NRC 00598: INNER PAN ON AFT EDGE BEAM #2 AT FWD CARGO COMPARTMENT DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R-3 PROCEDURE 3 REPAIR 3. (LP #0871599)Mar 22, 2025 · N938AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2025032402186Door Frame · crackedCRACK ON BEAM #1 AFT EDGE AT PASSENGER ENTRANCE DOOR (L1). SUMMARY OF NRC 00290: BEAM #1 AFT EDGE AT PASSENGER ENTRANCE DOOR WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 7 REPAIR 7. (LP #0871550)Mar 22, 2025 · N938AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2025032402185Intercostal · corrodedCORROSION ON INTERCOSTALS (2 EA) AND INTERNAL DOUBLER BTW STA Y=196/212 AND BTW LONGERONS 28R/29R AT E/E COMPARTMENT. SUMMARY OF NRC 00077: CORROSION LEVEL 2. REPAIR DOUBLER WAS REPLACED PER DWG 9923686-25 REV D, PER B717 SRM 51-41-02-0G AND 51-41-05-0G. CORROMar 22, 2025 · N940AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2025032402184Access Panel · corrodedCORROSION ON CONTACT AREA OF FUEL ACCESS PLATE 620QB. ALSO, CORROSION ON FASTENER HOLES OF PLATE 620JB AT RH WING. SUMMARY OF NRC 00604: CORROSION LEVEL 2. ACCESS PLATE 620JB WAS REPLACED AND VERIFIED FOR A NEW ACCESS PLATE PER B717-200 AIPC 57-23-01-01 ITEM 2Mar 21, 2025 · N998AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2025032402183Access Panel · corrodedCORROSION ON COUNTERSINK ON FUEL ACCESS PLATES 620GB, 620HB, 620CB, 620FT, 620DB, AND ARB0872-535 AT RH WING WAS FOUND. SUMMARY OF NRC 00602: CORROSION LEVEL 2. FUEL ACCESS DOORS 620FT AND 620DB WERE REPAIRED PER B717-200 SRM 57-10-01-2R PROCEDURE 2. FUEL ACCEMar 21, 2025 · N998AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2025032102134Frame · crackedCRACK OF 0.093 IN LENGTH WAS FOUND ON THE UPPER RADIUS OF FRAME TAB ON THE OVERWING FRAME AT STA Y=696.000 RH. (IN REF CARD 5310-01436-04D, JOB #090-0004, STEP 10). SUMMARY OF NRC 00281: FRAME TAB ON THE OVERWING FRAME AT STA Y= 696.000 RH WAS REPAIRED PER CARMar 21, 2025 · N938AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2025032102133Barrel Nut · corrodedCORROSION ON HORIZONTAL STAB BARREL NUTS RH SIDE #13 AND #27. SUMMARY OF NRC 00800: LEVEL CORROSION 2. BARREL NUTS HORIZONTAL STAB RH SIDE #13 AND 27 WERE REPAIRED PER PRI 624606-14 REV 1 & ER/A 624606-14 REV ORIG. SECTION I: PERMANENT REPAIR APPROVAL IS LIMITMar 20, 2025 · N998AT · Boeing 717200 · Horizontal Stabilizer Miscellaneous StructureSDR DALA2025032102132Cusp Web · crackedCRACK ON CUSP WEB BTW STA Y=655 TO STA Y=670 LH SIDE AT CABIN PASSENGER. SUMMARY OF NRC 00338: CRACK ON CUSP WEB BTW STA Y=655 TO STA Y=670 LH SIDE AT CABIN PASSENGER WAS REPAIRED PER B717-200 SRM 53- 00-55-2R PROCEDURE 4 REPAIR 4 FIGURE 203. (LP #0868343)Mar 20, 2025 · N938AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2025032102131Lamp · inoperativeTHE EMERGENCY LIGHTS FOR THE RH AFT EMERGENCY EXIT AND THE LH AFT LAVATORY WERE FOUND INOPERATIVE. SUMMARY OF NRC 00168: THE LAMPS FOR THE EMERGENCY LIGHTS AT THE RH AFT EMERGENCY EXIT AND LH AFT LAVATORY WERE REPLACED PER B717 AMM 33-52-18. THE SYSTEM NOW OPEMar 20, 2025 · N891AT · Boeing 717200 · Emergency LightingSDR DALA2025032002096Frame · crackedCRACK ON FRAME STA Y=1037 LONG 17L AT PASSENGER CABIN. SUMMARY OF NRC 00360: CRACK ON FRAME STA Y=1037 LONG 17L AT PASSENGER CABIN WAS REPAIRED PER B717-200 53-20-07-2R REPAIR 4. (LP #0866910)Mar 19, 2025 · N938AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2025032002095Pan · crackedCRACK ON PAN NEXT TO AFT HINGE DOOR (UPPER AREA) AT FWD CARGO DOOR. SUMMARY OF NRC 00193: PAN NEXT TO AFT HINGE DOOR (UPPER AREA) OF FWD CARGO DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1. (LP #0866764)Mar 19, 2025 · N955AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2025032002094Cusp Web · damagedELONGATED HOLE ON CUSP WEB LH BTW STA Y=696 X=56 AT CABIN PASSENGER. SUMMARY OF NRC 00339: ELONGATED HOLE ON CUSP WEB LH BTW STA Y=696 X=56 AT CABIN PASSENGER WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 REP 4. (LP #0866724)Mar 19, 2025 · N938AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2025032002093Pan · crackedCRACK ON OUTER PAN BTW BEAM 1 AND 2 (AFT EDGE) OF FWD CARGO DOOR WAS FOUND. SUMMARY OF NRC 00552: OUTER PAN AND INNER PAN BTW BEAM #1 AND BEAM #2 (AFT EDGE) AT FWD CARGO DOOR WERE REPAIRED PER ER/A 624433-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 624Mar 19, 2025 · N955AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2025032002092Pan · crackedCRACK WAS FOUND ON INNER PAN AT AFT CARGO DOOR AT STOP FITTING ON BEAM 5 AFT EDGE. SUMMARY OF NRC 00577: INNER PAN ON BEAM 5 AFT EDGE OF AFT CARGO DOOR WAS REPAIRED PER ER/A 566665-14 REV A SECTION II: PERMANENT REPAIR AND PRI 566665-14 REV 4. ASSOCIATED ER/A Mar 19, 2025 · N955AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2025031902066Floor Support · corrodedCORROSION ON FLOOR SUPPORTS BTW STA Y=210 TO STA Y=218 X=-11, Y=180 TO STA Y=190 X=-56, STA Y=190 TO STA Y=198 X=54, STA Y=197 X=22 TO X=42 AND STA Y=180 X=-22 TO X=-42, STA X=7RH BTW Y=148-200, IS OUT OF LIMITS PER B717-200 SRM 53-00-00-1A PROCEDURE ALLOWABLEMar 19, 2025 · N998AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2025031902065Frame · corrodedCORROSION FOUND ON FRAME AT F.S. 889 BETWEEN STRINGER 29L. SUMMARY SEE NRC 001-0508:2550-2001/008 01228: CLEANED UP FRAME REF B717-200 SRM 53-00-00-1A ALLOWABLE DAMAGE GENERAL. FOUND TO BE OUT OF LIMITS. REPAIRED REF B717-200 SRM 53-20-07-2R REPAIR 3 ROLLED Z-Mar 19, 2025 · N925AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2025031902064Beam · crackedCRACK WAS FOUND ON INNER/OUTER PAN BEAM 2 AND INNER PAN BEAM 1 FWD EDGE AT AFT CARGO DOOR. SUMMARY OF NRC 00578: INNER/OUTER PAN BEAM 2 AND INNER PAN BEAM 1 FWD EDGE AT AFT CARGO DOOR WAS REPAIRED PER PRI 624376-14 REV 2 AND ERA 624376-14 REV ORIGINAL SECTION Mar 19, 2025 · N955AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2025031902063Cusp Web · crackedCRACK ON CUSP WEB RH SIDE BTW STA Y=674 X-56 AT CABIN PASSENGER. SUMMARY OF NRC 00330: CRACK ON CUSP WEB RH SIDE BTW STA Y=674 X-56 AT CABIN PASSENGER WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4, PAR 5, FIG 223, AND FIG 226. (LP #0864855)Mar 18, 2025 · N938AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2025031902062Pan · crackedCRACK ON INNER PAN AFT UPPER CORNER AT PASSENGER ENTRANCE DOOR (L1). SUMMARY OF NRC 00532: INNER PAN AFT UPPER CORNER AT PASSENGER ENTRANCE DOOR (L1) WAS REPAIRED PER B717-200 SRM 52-10-02-2R REPAIR 3. (LP #0864707)Mar 18, 2025 · N998AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2025031702029Frame · crackedCRACK ON FRAME STA Y=1037 LONG 17R AT PASSENGER CABIN. SUMMARY OF NRC 00361: FRAME STA Y=1037 LONG 17R AT PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 4 REPAIR 4. (LP #0861190)Mar 16, 2025 · N938AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2025031702030Battery Pack · faultedTHE AFT EMERGENCY EXIT LIGHT IS FLICKERING. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY POWER SUPPLY AT STA 1050. OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT RETURNED TO SERVICE. (LP #7236550)Mar 15, 2025 · N607AT · Boeing 717200 · Emergency LightingSDR DALA2025031702028Pan · crackedCRACKS (2 EA) WERE FOUND ON INNER PAN AT AFT CARGO DOOR STOP FITTING ON BEAM 1 STA Y=990. SUMMARY OF NRC 00589: INNER PAN ON AFT SIDE BETWEEN STOP #1 AND STOP #2 AT AFT CARGO DOOR WAS REPAIRED PER ER/A 624383-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRIMar 15, 2025 · N955AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2025031702027Vane · crackedCRACK ON UPPER SURFACE OF FLAP MOVABLE VANE AT LH WING. SUMMARY OF NRC 00063: FLAP MOVABLE VANE AT LH WING WAS REPAIRED PER B717-200 SRM 51-70-02-0G PROCEDURE GENERAL IN REFERENCE WITH B717-200 SRM 57-53-01-2R PROCEDURE 1 REPAIR 1. (LP #0859916)Mar 15, 2025 · N891AT · Boeing 717200 · Leading Edge DevicesSDR DALA2025031702026Seat Track · corrodedRIGHT MID SEAT TRACK CORRODED AT FORWARD END. MARKED. SUMMARY SEE NRC 001-0550:5300-2010/013 00986: REPAIRED PER B717 SRM 53-20-52 REPAIR 5 (CP LEVEL 2) CLOSING REQUIREMENTS RII: INSPECTOR 00316969. CORROSION LEVEL CHANGED FROM 1 TO: 2. (LP #0859488)Mar 15, 2025 · N925AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR HALA20250317019Cylinder · bypassingATB! NOSE GEAR WOULD NOT RETRACT AFTER T/O. DURING RETRACT TEST. FOUND RETRACT CYCLINDER BYPASSING. REMOVED AND REPLACED NLG RETRACT CYCLINDER PER AMM 32-35-01.OPS CHECK GOOD. LEAK CHECK GOOD. OK FOR SVCMar 14, 2025 · N495HA · Boeing 717200 · Landing Gear Retraction/Extension SystemSDR DALA2025031702025Longeron · crackedCRACK ON INTERNAL AREA OF LONGERON 7R, 8R, 5R, STA Y=1022 AT PASSENGER CABIN. SUMMARY OF NRC 00363: LONGERON 8R, 5R, STA Y=1022 AT PASSENGER CABIN WERE REPAIRED PER B717-200 SRM 53-00-05-2R REPAIR 2 AND LONGERON 7R NO DAMAGE WAS FOUND PER DC-MD/BOEING NDTSPM PMar 14, 2025 · N938AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2025031702024Seat Track · corrodedRIGHT I/B SEAT TRACK CORRODED AT FORWARD END. MARKED. SUMMARY SEE NRC 001-0550:5300-2010/012 00985: REPAIRED PER B717 SRM 53-20-52-2R PROCEDURE 5 (CPCP LEVEL 1). (LP #0858357)Mar 14, 2025 · N925AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2025031702023Intercostal · crackedCRACK ON INTERCOSTAL STA Y=636 APPROX BL=0 AT FOWARD CARGO COMPARMENT WAS FOUND. SUMMARY OF NRC 00146: INTERCOSTAL ON STA Y=636 APPROX BL=0 AT FOWARD CARGO COMPARMENT WAS REPAIRED PER B717-200 SRM 53-00-00-2R PROCEDURE 1. (LP #0858310)Mar 14, 2025 · N891AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2025031702022Seat Track · corrodedCORROSION ON RH SEAT TRACK STA Y=236-238 -X=22 AT PAX CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00398: CORROSION LEVEL 2. CORROSION ON RH SEAT TRACK STA Y=236-238 -X=22 AT PAX CABIN FLOOR STRUCTURE WAS REPAIRED PER B717-200 SRM 53-20-52-2R. PROC 1, REPAIR 1. (LP #Mar 14, 2025 · N938AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2025031702021Fitting · corrodedSTR 25R END FITTING CORRODED (MKD). SUMMARY SEE NRC 001-0467:2000-1002/567 01398: CORROSION LEVEL 2. CLEANED UP STRINGER END FITTING REF B717-200 SRM 53-00-00-1A. ALLOWABLE DAMAGE GENERAL. RESTORED FINISH REF B717-200 SRM 51-10-04. (LP #0858004)Mar 14, 2025 · N925AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2025031702020Stringer · corrodedSTR 26R END FITTING CORRODED (MKD). SUMMARY SEE NRC 001-0467:2000-1002/566 01397: CORROSION LEVEL 2. CLEANED UP STRINGER END FITTING REF B717-200 SRM 53-00-00-1A. ALLOWABLE DAMAGE GENERAL. RESTORED FINISH REF B717-200 SRM 51-10-04. (LP #0858003)Mar 14, 2025 · N925AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2025031702019Pan · crackedCRACKS (2 EA) ON OUTER PAN IN BEAM 5 AT AFT CARGO DOOR FWD AND AFT EDGES. SUMMARY OF NRC 00111: DAMAGED AREA OF OUTER PAN IN BEAM 5 AT AFT CARGO DOOR FWD AND AFT EDGES WERE REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 6 REPAIR 6. (LP #0857625)Mar 14, 2025 · N955AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2025031401970Cusp Web · crackedCRACK ON CUSP WEB BTW STA Y=672 -X=56 RH SIDE AT MID PASSENGER CABIN. SUMMARY OF NRC 00649: CUSP WEB BTW STA Y=672 -X=56 RH SIDE AT MID CABIN PASSENGER WAS REPAIRED PER B-717-200 SRM 53-00-55-2R REP 4, PAR 5, FIG 212. (LP #0856963)Mar 14, 2025 · N998AT · Boeing 717200 · Fuselage Miscellaneous Structure
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