Boeing 717-200

Service difficulty reports · 18,756

Newest first. General aviation reporting is voluntary.

Query with SQL
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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR HALA20240524026Compressor · stalledENG L COMP STALL ON TAKE OFF @ 1600' (ATB). PERFORMED EEC 1 BITE - FC 801105 STARTER AIR VALVE OUT OF POSITION. REPLACED #1 ENGINE START VALVE PER AMM 80-11-03. OPS CHECK & LEAK CHECK NEED TO BE ACCOMPLISHED. BORESCOPE INSP PERFORMED NO FINDINGS AMM 72-33-00-2May 23, 2024 · N492HA · Boeing 717200 · Turbine Engine Compressor SectionSDR DALA2024052305457Connector · damagedDURING EMERGENCY LIGHTS CHECK, THE EXTERIOR EMERGENCY LIGHTS TURN ON WITH FLIGHT CABIN SWITCH IN ARM POSITION. SUMMARY OF NRC00627: CONTINUITY WAS PERFORMED PER B717-200 WDM 33-51-11 IN CONNECTOR (P1-125) OF EMERGENCY EVACUATION BATTERY POWER SUPPLY. A MELTED May 22, 2024 · N983AT · Boeing 717200 · Light System WiringSDR DALA2024052205414Skin · dentedDENT ON FUSELAGE SKIN STA 205, 1" ABOVE LONGERON 17L WITH DIMENSIONS AS A FOLLOW D (WIDTH)=1.300, X (DEPTH)=0.110, D/X=11.81 IS OUT OF LIMITS PER B717 SRM 53-01-01-1A, PROCEDURE 3 ALLOWABLE DAMAGE 3 PAR 4. C CONDITION 1B. SUMMARY OF NRC 00388: PREVIOUS REPAIR May 22, 2024 · N974AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2024052205413Door Frame · damagedELONGATED HOLE ON DOOR JAMB STA Y=427 AND LONGERON 25R. SUMMARY OF NRC 00173: DOOR JAMB STA Y=427 AND LONGERON 25R WAS REPAIRED PER PRI 617550-14 REV 3 AND ER/A 617550-14 REV 0, SECTION I: REPAIR. ASSOCIATED ER/A 14-617550 ADDED FOR AC 9536. (LP #0353594)May 21, 2024 · N974AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2024052205412Fuel Tank · corroded-AD- CORROSION ON CENTER WING TANK LOWER SKIN BOTTOM SURFACE STA 747 BETWEEN XCW 27-32 AT LH MLG WHEEL WELL (AREA UNDER MLG CABLE FITTING). SUMMARY OF NRC 00775: CORROSION LEVEL 1. CORROSION ON CENTER WING TANK LOWER SKIN BOTTOM SURFACE STA 747 BETWEEN XCW 27-May 20, 2024 · N988AT · Boeing 717200 · Fuel StorageSDR HALA20240521025Compressor · stalledATB - ENG L. COMP STALL @ APPX 1500' ON CLIMBOUT. CONDITION IMPROVED ON POWER REDUCTION. NORMAL LANDING PERFORMED. COMPLETED INSPECTION OF THE ENGINE AFTER HIGH POWER SURGE AMM 72-00-200-801 UP TO STEP 2.E. (7) -N. DAMAGE FOUND NO DAMAGE NOTED. ENG 1 ON COMPREMay 20, 2024 · N492HA · Boeing 717200 · Turbine Engine Compressor SectionSDR DALA2024052105381Power Supply · inoperativeTHE AFT ACCESORY COMPARTMENT EMERGENCY LIGHTS ARE INOPERATIVE. THE EMERGENCY LIGHT BATTERY POWER SUPPLY WAS REPLACED PER B717 AMM 33-51-03. OPERATIONAL TESTS ARE GOOD. THE AIRCRAFT HAS RETURNED TO SERVICE. (LP #5731034)May 20, 2024 · N993AT · Boeing 717200 · Emergency LightingSDR DALA2024052105380Skin · scratchedSCRATCH ON LOWER SKIN, SLAT PANEL #1 LH WS 168.0. SUMMARY OF NRC 00610: SCRATCH ON LOWER SKIN, SLAT PANEL #1 LH WS 168.0 WAS REPAIRED PER ER/A 618009-14 REV ORIG. SECTION I PERMANENT REPAIR AND PER PRI 618009-14 REV 1. ASSOCIATED ER/A 14-618009 ADDED FOR AC 95May 20, 2024 · N983AT · Boeing 717200 · Leading Edge DevicesSDR DALA2024052105379Skin · crackedCRACK ON FUSELAGE SKIN LOCATED Y=1022 AND Y=1076 ON LONGERON L-14R. SUMMARY OF NRC 00164: FUSELAGE SKIN LOCATED Y=1022 AND Y=1076 ON LONGERON L-14R WAS REPAIRED PER ER/A 617295-14 REV O, SECTION I: PERMANENT REPAIR. PERFORM SECTION II: REPETITIVE INSPECTIONS WMay 20, 2024 · N974AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2024052105378Skin · crackedCRACK ON FUSELAGE SKIN LOCATED Y=1087 BETWEEN L-13 AND LONGERON L-14R. SUMMARY OF NRC 00165: FUSELAGE SKIN LOCATED Y=1087 BETWEEN L-13 AND LONGERON L-14R WAS REPAIRED PER ER/A 617295-14 REV O, SECTION I: PERMANENT REPAIR. PERFORM SECTION II: REPETITIVE INSPECTMay 20, 2024 · N974AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2024052105377Beam · crackedCRACK ON BEAM #1 AT AFT CARGO DOOR. SUMMARY OF NRC 00575: BEAM #1 AT AFT CARGO DOOR WAS REPAIRED PER ER/A 617654-14 REV ORIGINAL. ASSOCIATED ER/A 14-617654 ADDED FOR AC 9560. (LP #0351759)May 20, 2024 · N983AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2024052105376Release Cable · misroutedIMPROPER ROUTING OF MANUAL RELEASE CABLE FOR SLIDE AT FORWARD SERVICE 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 NRC 00695: MANUAL INFLATION CABLE FOR SLIDE AT FORWARD SERVIMay 19, 2024 · N993AT · Boeing 717200 · Escape SlideSDR DALA2024052005347Battery · failedTHE FWD L1 DOOR EMERGENCY LIGHT IS INOPERATIVE. CONDITION WAS FOUND ON SERVICE CHECK. MAINTENANCE FOUND THE BATTERY ASSEMBLY BAD AND REPLACED IT IN REF TO B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #5308068)May 18, 2024 · N891AT · Boeing 717200 · Emergency LightingSDR DALA2024052005346Structure · corrodedCORROSION ON HOLE 18 CENTER BOX LH SIDE AT HORIZONTAL STABILIZER. SUMMARY OF NRC 00589: CORROSION LEVEL 2. HOLE 18 CENTER BOX LH SIDE AT HORIZONTAL STABILIZER WAS REPAIRED PER PRI 617688-14 REV 3 AND ER/A 617688-14 REV ORIG SECTION I: TIME LIMITED REPAIR DTE RMay 18, 2024 · N983AT · Boeing 717200 · Horizontal Stabilizer StructureSDR DALA2024052005345Pan · crackedCRACK ON PAN LOWER EDGE INTERNAL STRUCTURE BTW STA 403 TO 413 FWD CARGO DOOR. SUMMARY OF NRC 00212: INNER AND OUTER PAN ON LOWER EDGE INTERNAL STRUCTURE BTW STA 403 TO 413 AT FWD CARGO COMPARTMENT DOOR WERE REPAIRED PER ER/A 617729-14 REV ORIGINAL SECTION I: PMay 18, 2024 · N993AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024052005344Floorbeam · damaged-AD- REWORK ON WEB BELOW FLOOR BEAM DOES NOT MEET WITH EDGE DISTANCE REQUIREMENTS AT STA 696 X=56 LH. SUMMARY OF NRC 00439: WEB BELOW FLOOR BEAM ON STA 696 X=56 LH WAS REPAIRED PER ER/A 617901-14AD REV ORIGINAL, SECTION I: PERMANENT REPAIR. REPAIR APPROVAL IS May 17, 2024 · N974AT · Boeing 717200 · Fuselage Main, Floor BeamSDR DALA2024052005343Frame · crackedCRACK ON MAIN FRAME STA 1037 LONGERON 17L AND LONGERON 17R AT PAX CABIN. SUMMARY OF NRC 00459: MAIN FRAME STA 1037 LONGERON 17L WAS REPAIRED PER ER/A 617631-14 REV ORIGINAL, SECTION I: PERMANENT REPAIR AND MAIN FRAME STA 1037 LONGERON 17R WAS REPAIRED PER B717May 17, 2024 · N974AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2024052005342Slide · damagedDURING FWD PASSENGER SLIDE DOOR COVER INSTALLATION, THE SLIDE PACKAGE WAS FOUND UNSAFE. 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 SERIAL 00682: FORWARD ENTRY PASSENGER DOOR SMay 17, 2024 · N993AT · Boeing 717200 · Escape SlideSDR DALA2024052005341Pan · crackedCRACK WAS FOUND ON PAN IN BEAM #2 AT FWD CARGO COMPARTMENT DOOR (FWD EDGE). SUMMARY OF NRC 00610: INNER PAN IN BEAM #2 AT FWD CARGO COMPARTMENT DOOR (FWD EDGE) WAS REPAIRED PER ER/A 617689-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 617689-14 REV 2. ASMay 17, 2024 · N974AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024052005340Slide · damagedDURING FWD PASSENGER SLIDE DOOR COVER INSTALLATION, THE SLIDE PACKAGE WAS FOUND UNSAFE. 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 682: FORWARD ENTRY PASSENGER DOOR SLIDE ASSYMay 17, 2024 · N993AT · Boeing 717200 · Escape SlideSDR DALA2024052005339Structure · corrodedCORROSION ON HOLES 27 AND 28, CENTER BOX RH, AT HORIZONTAL STABILIZER. SUMMARY OF NRC 00581: HOLES 27 AND 28 CENTER BOX RH AT HORIZONTAL STABILIZER. WERE REPAIRED PER PRI 617657-14 REV 1 AND ER/A 617657-14 REV ORIG SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A May 17, 2024 · N983AT · Boeing 717200 · Horizontal Stabilizer StructureSDR DALA2024051705298Doubler · damagedMISSING MATERIAL IN ONE HOLE WAS FOUND AT INNER DOUBLER. SUMMARY OF NRC 00583: AREA WAS REPAIRED PER ER/A 617844-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-617844 ADDED FOR AC 9560. (LP #0346414)May 17, 2024 · N983AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2024051705297Door Frame · corrodedCORROSION ON DOOR JAMB BTW L24 AND L24 LOWER AREA AFT CARGO. SUMMARY OF NRC 00205: CORROSION LEVEL 2. DOOR JAMB AND REPAIR DOUBLERS (ANGLES) BTW L24 AND L24 LOWER AREA AFT CARGO WERE REPLACED PER B717 SRM 53-20-15-2R REP 7.May 17, 2024 · N974AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2024051705296Strap · corrodedCORROSION ON WEB STRAP BTW STA Y=200/208 AND LONGERON 18L. (PAX CAB). SUMMARY OF NRC 00409: CORROSION LEVEL 2. WEB STRAP BTW STA Y=200/208 AND LONGERON 18L WAS REPAIRED PER ER/A 617656-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 617656-14 REV 0. ASSOCIMay 16, 2024 · N993AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024051705295Cargo Track · corrodedCORROSION WAS FOUND ON TIE TRACK LOCATED BETWEEN Y=1002 AND Y=1022 RH SIDE, CORROSION LEVEL 2. TIE TRACK LOCATED BETWEEN Y=1002 AND Y=1022 RH SIDE WAS REPLACED PER B717 SRM 51-41-01-0G. (LP #0345653)May 16, 2024 · N974AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2024051705294Hinge · excess playFREEPLAY ON JOINT BTW FLAP AND FLAP OUTBD HINGE AT LH WING. LT WING FLAP OUTBD HINGE WAS REPAIRED IN ACCORDANCE WITH PRI 617504-14 REV 2 AND ER/A 617504-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. REPAIR APPROVAL IS LIMITED TO 24 MONTHS FROM 09MAY24. ADDITIMay 16, 2024 · N993AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2024051605256Battery Pack · faultedAFT, CENTER EMERGENCY EXIT SIGN BECOMES ILLUMINATED THEN EXTIGUISHES INTERMITENTLY. REPLACED POWER SUPPLY ASSEMBLY AND BATTERY PACK AT B5-230 PER B717 AMM 33-51. ONCE BATTERY CHARGED, THE OPERATIONAL CHECK WAS GOOD. (LP #5822592)May 16, 2024 · N980AT · Boeing 717200 · Emergency LightingSDR DALA2024051605253Structure · corrodedCORROSION WAS FOUND ON HSTB HOLE #27 RH. SUMMARY OF NRC 00650: RH HORIZONTAL STABILIZER BARREL NUT HOLE #27 WAS REPAIRED IN ACCORDANCE WITH ER/A 617762-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. TIME CONTROLLED ITEMS: REPAIR APPROVAL IS LIMITED TO 24 MONTHS May 16, 2024 · N993AT · Boeing 717200 · Horizontal Stabilizer Miscellaneous StructureSDR DALA2024051605251Door Frame · corrodedCORROSION ON DOOR JAMB BTW STA Y=370-427 AND LONGERON 28R-24R AT FWD CARGO COMPARMENT. SUMMARY OF NRC 00172: CORROSION LEVEL 2. DOOR JAMB BTW STA Y =370-427 AND LONGERON 28R-24R AT FWD CARGO COMPARMENT WAS REPLACED PER B717-200 SRM 53-20-15-2R-REP 6, PAR 6. (LMay 16, 2024 · N974AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2024051605250Skin · crackedCRACK ON FUSELAGE SKIN LOCATED AT Y=1037 AND LONGERON L-14L. SUMMARY OF NRC 00162: FUSELAGE SKIN LOCATED AT Y=1037 AND LONGERON L-14L WAS REPAIRED PER ER/A 617297-14 REV ORIGINAL, SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-617297 ADDED FOR AC 9536. (LP #0May 16, 2024 · N974AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2024051605249Intercostal · crackedCRACK ON INTERCOSTAL X=0 BTW STA Y=832 AND Y=851 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00509: INTERCOSTAL X=0 BTW STA Y=832 AND Y=851 AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717 SRM 51-70-11-2R PROCEDURE 1 REPAIR 1 PAR. 4. (LP #0344606)May 15, 2024 · N974AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024051605254Pin · out of positionINCORRECT HRS POSITION OF TAILCONE RELEASE MECHANISM CAM PIN STA Y=1225 CANT 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 NRC 00817: TAILCONE RELEASE MECMay 15, 2024 · N974AT · Boeing 717200 · Aerodynamic FairingsSDR DALA2024051505224Intercostal · crackedCRACK ON INTERCOSTAL BTW STA Y=636 AND X=0 AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00679: CRACK ON INTERCOSTAL BTW STA Y=636 AND X=0 AT FWD CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-00-00-2R PROCEDURE 1 REPAIR 1. (LP #0343135)May 15, 2024 · N993AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024051605255Attach Fitting · corrodedRUSTED ON LUG AT ATTACH FIXED STRUT, ALSO ON FITTING TO RH LANDING GEAR. SUMMARY OF NRC 00731: RUSTED ON FITTING TO RH LANDING GEAR WAS REMOVED PER BOEING OM 57-40-1 REPAIR PAR 2 G (6) (B), (UT) THICKNESS MEASUREMENT WAS ACCOMPLISHED ON FITTING TO RH LANDING GMay 14, 2024 · N923AT · Boeing 717200 · Fuselage, Landing Gear Attach FittingsSDR DALA2024051505223Vane · dentedDENTS ON AFT MOVEABLE VANE LOWER SKIN AT RIGHT WING. SUMMARY OF NRC 00238: AFT MOVEABLE VANE LOWER SKIN AT RIGHT WING WAS REPAIRED PER ER/A 617597-14 REV ORIGINAL. ASSOCIATED ER/A 14-617597 ADDED FOR AC 9538. (LP #0342649)May 14, 2024 · N993AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2024051505222Skin · crackedDENT WITH CRACK (1 EA) 19" FROM OTBD EDGE AND 5.500" FROM LEADING EDGE AND DENT WITH DISBOND (1 EA) 34" FROM OUTBD EDGE AND 4" FROM TRALING EDGE ON LOWER SURFACE AT AFT FLAP MOVABLE VANE AT RIGHT WING. SUMMARY OF NRC 00563: LOWER SURFACE AT AFT FLAP MOVABLE VAMay 14, 2024 · N983AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2024051505221Doubler · corrodedCORROSION ON INTERNAL DOUBLER BTW STA Y 617-636 AND LONG L27L TO L28L AT FWD CARGO COMPARTEMENT. SUMMARY OF NRC 00631: CORROSION LEVEL 2. CORROSION ON INTERNAL DOUBLER BTW STA Y 617-636 AND LONG L27L TO L28L AT FWD CARGO COMPARTMENT WAS REPAIRED PER ER/A 61763May 14, 2024 · N993AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2024051405176Bottle · low pressurePRESSURE WAS FOUND TO BE OUT OF RANGE ON 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 00519: TAIL CONE SLIDE WAS REMOVED UNDER AMDS 5352-4001 AND REPLACED PMay 13, 2024 · N983AT · Boeing 717200 · Escape SlideSDR DALA2024051405175Support Angle · crackedCRACKS (2 EA) ON ANGLE STRUCTURE SUPPORT BULKHEAD BTW LONGERON 5L AND 6L ALSO 7L STA=Y 1022 AT AFT LAVATORY ENGINE PYLON AREA. SUMMARY OF NRC 00400: CRACK ON ANGLE STRUCTURE SUPPORT BULKHEAD BTW LONGERON 7L STA=Y 1022 AT AFT LAVATORY ENGINE PYLON AREA WAS REPAMay 13, 2024 · N993AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024051405174Longeron Splice · corrodedCORROSION ON LOWER SPLICE (BELOW CUSP WEB) BTW STA Y=908 AND Y=889 APPROX LONG 18RH AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00514: CORROSION LEVEL 2. SPLICE (BELOW CUSP WEB) BTW STA Y=908 AND Y=889 APPROX LONG 18RH AT AFT CARGO COMPARTMENT WAS REPLACED PER DWMay 13, 2024 · N974AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2024051405173Skin · crackedCRACK WAS FOUND OVER THE VERTICAL STABILIZER DORSAL FIN LEADING EDGE RAM AIR SCOOP. SUMMARY OF NRC 00469: CRACK ON VERTICAL STABILIZER DORSAL FIN LEADING EDGE RAM AIR SCOOP WAS REPAIRED (WELDED) PER ER/A 382101-14MA REV H. SECTION I: PERMANENT REPAIR. ASSOCIATMay 12, 2024 · N974AT · Boeing 717200 · Vertical Stabilizer, Plate/SkinSDR DALA2024051405172Scuff Plate · crackedCRACK ON AFT SCUFF PLATE AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 0002: SCUFF PLATE AT AFT CARGO COMPARTMENT WAS REPAIRED PER ER/A 542149-14TR REV B, SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-542149 ADDED FOR AC 9538. (LP #0339236)May 12, 2024 · N993AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024051305135Pump · leakingSHIP 9542 -HYD/DE- LOSS OF RIGHT HYDRAULIC SYSTEM ON APPROACH REQUIRING A MANUAL GEAR EXTENSION. CORRECTIVE ACTION: MAINTENANCE DETERMINED THAT THE HYDRAULIC REVERSABLE PUMP (PTU) WAS LEAKING INTERNALLY AND REPLACED IT ALONG WITH THE RIGHT SYSTEM RESERVOIR. (LMay 12, 2024 · N996AT · Boeing 717200 · Hydraulic Pump (Electric/Engine), MainSDR DALA2024051305134Frame · crackedCRACK ON FRAME STA Y=1116 LONGERON 21R AT RH AFT ACCESSORIES COMPARTMENT. SUMMARY OF NRC 00238: FRAME STA Y=1116 LONGERON 21R AT RH AFT ACCESSORIES COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-00-07-2R REPAIR 1 FIG 201. (LP #0337618)May 11, 2024 · N983AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2024051305133Doubler · corrodedCORROSION ON DOUBLER BTW L29R-L28R STA Y=199-119 AT E&E. SUMMARY OF NRC 00186: CORROSION LEVEL 2. DOUBLER BTW L29R-L28R STA Y=199-119 AT E&E WAS REPLACED PER B717-200 DWG 9923686 REV D AND PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G. FORWARD WATER DRAIN MAST May 11, 2024 · N983AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2024051405171Pan · crackedCRACKS ON PAN FWD EDGE AND AFT EDGE BETWEEN BEAM #2 AND #3 AT AFT CARGO DOOR. SUMMARY OF NRC 00366: AFT CARGO DOOR ASSY WAS REMOVED PER AMDS 5231-4002, WAS REPLACED WITH SERVICEABLE AFT CARGO DOOR ASSY, AND WILL BE INSTALLED WITH AMDS 5231-4004. (LP #0336365)May 10, 2024 · N993AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2024051405170Jackscrew · nicked-AD- A NICK WAS FOUND ON THREAD OF THE ACME SCREW AT THE HORIZONTAL STAB. SUMMARY OF NRC 00485: HORIZONTAL STABILIZER ACTUATOR JACKSCREW ASSY WAS REPLACED FOR SERVICEABLE ACTUATOR JACKSCREW. WAS INSTALLED PER B717 AMM 27-41-04 AND TESTED OK. ALSO, TRIM GEARBOXMay 10, 2024 · N923AT · Boeing 717200 · Stabilizer ActuatorSDR DALA2024051305132Door Frame · damagedBENT AND MISSING MATERIAL ON AFT EDGE OF FWD CARGO DOOR CUTOUT AT EXTERNAL FUSELAGE. SUMMARY OF NRC 00008: AFT EDGE OF FWD CARGO DOOR CUTOUT AT EXTERNAL FUSELAGE WAS REPAIRED PER ERA 617722-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-617722May 10, 2024 · N983AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2024051305131Frame · corrodedCORROSION ON PREVIOUS REPAIR DOUBLER ON FRAME Y=870 BTW LONGERONS 29L AND 29R AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00299: CORROSION LEVEL 2. PREVIOUS REPAIR DOUBLER ON FRAME Y=870 BTW LONGERONS 29L AND 29R AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200May 9, 2024 · N993AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2024050905043Lug · crackedCRACK ON OVERWING FRAME LUG STA Y=715.000, X=-54 RH AT PASSENGER CABIN FLOOR. OVERWING FRAME STA Y=715.000, X=-54 RH AT PASSENGER CABIN FLOOR WAS REPLACED PER AMDS 5310-01436-03B. ASSOCIATED AA 5310-01436 ADDED FOR AC 9536.May 8, 2024 · N974AT · Boeing 717200 · Fuselage Main, Attach Fittings
Back to Boeing 717-200