Boeing 717-200

Service difficulty reports · 18,771

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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 DALA2019083105116Not Reported · crackedCRACK AT L=4 LT STA Y=1022 (CPAX). NRC 00532: L=4 LT STA Y=1022 WAS REPAIRED PER SRM 53-00-05-2R-2- FIG. 201. (LP #1248630)Aug 30, 2019 · N947AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2019082905054Longeron · crackedCRACK AT LONGERON 5 LT, BS 1022. THE LONGERON WAS REPAIRED IAW SRM 53-00-05-2R.Aug 29, 2019 · N947AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2019082805007Gusset · crackedCRACK GUSSET AT L=7 RH STA Y=1022 (CPAX). NRC 00537: GUSSET AT L=7 RH STA Y=1022 WERE REPAIRED PER ER/A 580881-14 REV. ORIGINAL SECTION I: PERMANENT REPAIR AND ETI-17-19-154 REV. ORIGINAL. ASSOCIATED ER/A 14-580881 ADDED FOR AC 9507. (LP #1243761)Aug 27, 2019 · N947AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2019082805006Skin · crackedCRACK AT FUSELAGE SKIN STA Y=1095 BTW L=13/14 LH (FUS). NRC 00039: FUSELAGE SKIN STA Y=1095 BTW L=13/14 LH WAS REPAIRED PER ER/A 580773-14 REV. ORIGINAL (PERMANENT REPAIR) AND ETI-17-19-155 REV. 1. WILL BE MONITORED BY LOG PAGE #1241544 PER ER/A NO 580773-14 RAug 27, 2019 · N947AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2019082805005Former · crackedCRACK ON KEEL BEAM FORMER LH SIDE STA Y=696 AND X=30 (CPAX). NRC 00590: KEEL BEAM FORMER LH SIDE STA Y=696 AND X=30 WAS REPAIRED PER B717-200 SRM 51-70-11-2R-1 FIG 201. (LP #1243383)Aug 27, 2019 · N947AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2019082805004Longeron · crackedCRACK AT L=6 LH STA Y=1022 (CPAX). NRC 00534: LONGERON 6 LH STA Y=1022 WAS REPAIRED PER B717-200 SRM 53-00-05-2R. (LP #1243376)Aug 27, 2019 · N947AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2019082805003Access Panel · corrodedCORROSION IN ACCESSES #520CT AND 620CT ON AREA SETTLEMENT AND COUNTERSINK AT FUEL TANK (AI) (AD). NRC 00549: CORROSION LEVEL 2, FUEL ACCESS PLATE #520CT AND 620CT WERE REPLACED PER AMDS 2040-0012, 2040-0010, AND VERIFIED PER B717-200 IPC 57-22- 01-01. (LP #124Aug 27, 2019 · N947AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2019082704976Former · crackedCRACK ON KEEL BEAM FORMER RH SIDE STA Y=715 AND X=-37. NRC 00595: CRACK ON KEEL BEAM FORMER RH SIDE STA Y=715 AND X=-37 WAS REPAIRED PER B717-200 SRM 51-70-11-2R-1 FIG. 201. (LP #1242493)Aug 27, 2019 · N947AT · Boeing 717200 · Fuselage Main, FrameSDR HALA2019090500368Valve · corrodedNR00112 - RIGHT FUEL VENT VALVE CORRODED (M). REMOVED AND REPLACED THE RIGHT WING FUEL VENT VALVE PER AMM 28-12-04. OP'S AND LEAK CHECK GOOD.Aug 26, 2019 · N491HA · Boeing 717200 · Fuel StorageSDR DALA2019082704974Keelbeam · crackedCRACK ON KEEL BEAM FORMER RH SIDE STA Y=679 AND X=-43 (FUS). NRC 00649: CRACK ON KEEL BEAM FORMER RH SIDE STA Y=679 AND X=-43 WAS REPAIRED PER B717-200 SRM 51-70-11-2R-1 FIG. 201. (LP #1241655)Aug 26, 2019 · N947AT · Boeing 717200 · Fuselage Main, KeelSDR DALA2019082704973Former · crackedCRACK ON KEEL BEAM FORMER RH SIDE STA Y=696 AND X=-30 (FUS). NRC 00591: CRACK ON KEEL BEAM FORMER RH SIDE STA Y=696 AND X=-30 CRACK ON KEEL BEAM FORMER RH SIDE STA Y=696 AND X=-30 WAS REPAIRED PER B717-200 SRM 51-70-11-2R-1 FIG. 201. (LP #1241629)Aug 26, 2019 · N947AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2019082604960Floor Support · corrodedCORROSION ON FLOOR SUPPORT STA X=07 FROM Y=160 TO Y=200 AT FWD WET AREA IN REF NRC 00587 (W1). NRC 00680: CORROSION LEVEL 2, FLOOR SUPPORT STA X=07 FROM Y=160 TO Y=200 AT FWD WET AREA (W1) WAS REPLACED PER B717- 200 SRM 53-10-51-0I-2 AND 51-41-01-0G. (LP #1240Aug 26, 2019 · N947AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2019082604959Floor Support · corrodedCORROSION ON FLOOR SUPPORT STA X=-05 FROM Y=200 TO Y=160 AT FWD WET AREA IN REF NRC 00588 (W1). NRC 00679: CORROSION LEVEL 2, FLOOR SUPPORT STA X=-05 FROM Y=200 TO Y=160 WAS REPLACED PER B717-200 SRM 53-10-51-0I -2 AND SRM 51-41-01-0G.Aug 26, 2019 · N947AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR HALA2019090600378Bracket · corrodedS/M AFT ACCESSORY COMPARTMENT: CATWALK PANEL RETAINING BRACKET RIGHT SIDE SURFACE CORROSION AND LOOSE RIVET. (AFT PANEL) (MARKED) 1. REMOVED AFT ACCRY CATWALK PANEL RETAINING BRACKET ON RT SIDE AND FABRICATED NEW BRACKET PER DWG 5991251-25.2. PRIME PER SRMAug 25, 2019 · N491HA · Boeing 717200 · Fuselage Miscellaneous StructureSDR HALA2019090600377Tee Fitting · corrodedMODERATE CORROSION ON TEE FITTING IN APU ENCLOSURE AT STA 1095. 1. CUT-OUT CORROSION DAMAGE PER SRM 51-70-11-2R-2. HFEC CHECK OK NO CRACK NOTED. FABRICATED ANGLES 1 & 2 PER SRM 51-70-11-2R-2 REPAIR 2 STEPS 1 THRU 4B(4). FABRICATED FILLER 0.075-T6, 0.090 PEAug 25, 2019 · N491HA · Boeing 717200 · Fuselage Miscellaneous StructureSDR HALA2019090600376Spar · corrodedLEFT WING REAR SPAR LOWER TANG SERVERE CORROSION STATION 360 - 366 (M) O/B OF O/B FLAP HINGE. 1. REPAIRED PER E105-491102-PERM VER A.Aug 25, 2019 · N491HA · Boeing 717200 · Wing SparSDR HALA2019090600375Spar · corrodedLEFT WING REAR SPAR LOWER TANG MODERATE CORROSION STATION XRS 184 - 188 (M) 1. REMOVED CORROSION PER SRM 51-10-04. 2. HFEC OK. CHORD 1.0 SPAN 3.75 ADJ .173 REM .119, M66 SUBMITTED 3. COMPLETED REPAIR PER E105-491103-PERM.Aug 25, 2019 · N491HA · Boeing 717200 · Wing SparSDR HALA2019090600374Former · crackedKEEL AREA - RIGHT SIDE - UNDERWING BARREL KEEL BEAMS AND CANTED KEEL - FORMER CRACKED AT STA Y = 694.500 (FORMER INSL 9923453-509) REPAIRED PER E105-491104-PERM ITEM 9-14.Aug 25, 2019 · N491HA · Boeing 717200 · Fuselage Main, FrameSDR HALA2019090600373Fitting · crackedFORWARD CARGO COMPARTMENT BULKHEAD FITTING CRACKED ALONG LONGERON 24 RIGHTHAND SIDE, FITTING P/N 3971162-2. 1) REMOVED FITTING AS REQUIRED. PICKED UP HOLES ON NEW FITTING PER DWG 5971094. OKAY FOR INSTALL. 2) INSTALLED FITTING PER DWG 5971094. TREATED ANDAug 25, 2019 · N491HA · Boeing 717200 · Fuselage Main, BulkheadSDR HALA2019090600372Fitting · corrodedAFT ACCY MODERATE CORROSION ON LONGERON END FITTING PN 3914653-1 STA 1054 AT L24L. REMOVED END FITTING 8-5-19 NEW FITTING PILOT HOLES DO NOT LINE UP WITH EXISTING. 3 EACH HOLES O/S 1 HOLE TO .2450 AND 2 EA HOLES TO .2910 SUB M66 FOR STANDARD BUSHING REPAIR 8Aug 25, 2019 · N491HA · Boeing 717200 · Fuselage Main, Longeron/StringerSDR HALA2019090600371Bracket · corrodedAFT ACCY COMP.FWD CATWALK LOWER BRACKET MOD CORROSION//1. REMOVED AND INSTALLED NEW CATWALK LOWER SUPPORT BRACKET P/N 9915537-25 PER DRAWING# 9915537.Aug 25, 2019 · N491HA · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2019082604958Keelbeam · crackedCRACK ON KEEL BEAM FORMER LH SIDE STA Y=679 AND X=43 (FUS). NRC 00648: CRACK ON KEEL BEAM FORMER LH SIDE STA Y=679 AND X=43 WAS REPAIRED PER B717-200 SRM 51-70-11 FIG 201 REP 1. (LP #1240605)Aug 25, 2019 · N947AT · Boeing 717200 · Fuselage Main, KeelSDR DALA2019082604957Keelbeam · crackedCRACK ON KEEL BEAM FORMER LH SIDE STA Y=715 AND X=37 (FUS). NRC 00594: CRACK ON KEEL BEAM FORMER LH SIDE STA Y=715 AND X=37 WAS REPAIRED PER B717-200 SRM 51-70-11 FIG 201 REP 1. (LP #1240592)Aug 25, 2019 · N947AT · Boeing 717200 · Fuselage Main, KeelSDR DALA2019082654956Charger · inoperativeTHE EMERGENCY LIGHT BATTERY CHARGER AT 25E WENT INOPERATIVE. MAINTENANCE REPLACED THE BATTERY CHARGER IAW B717 AMM 33-51. OPERATIONAL CHECK IS GOOD. (LP #6141432)Aug 24, 2019 · N993AT · Boeing 717200 · Emergency LightingSDR DALA2019082654955Skin · dentedSEVERAL DENTS ON LOWER AREA FWD FLAP MOVABLE VANE LEFT WING (AI). NRC 00247: LH WING FWD FLAP MOVABLE VANE WAS REPAIRED PER B 717-200 SRM 57-53-01-2R PROCEDURE 1 REPAIR 1 PARAGRAPH 4 FIGURE 202.Aug 24, 2019 · N947AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2019082644954Slide · no testTHE R1 DOOR SLIDE FAILED THE DEPLOYMENT TEST PER AMDS CARD #2561-9002 FORECAST #95-0525-8-0121. MAINTENANCE REMOVED AND INSTALLED A NEW SERVICEABLE R1 DOOR SLIDE REF AMDS CARD #2561-9005. ICR HAS BEEN SUBMITTED USING DOC/WORKCARD #2560-9352 -95 (QC5126/376046)Aug 24, 2019 · N967AT · Boeing 717200 · Escape SlideSDR DALA2019082644953Longeron · crackedCRACK AT LONGERON 4R, BS 1022, THE LONGERON WAS REPAIR IAW SRM 53-00-05-2R-2, FIG 201.Aug 24, 2019 · N947AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2019082654961Cable · misroutedTAIL CONE LOCK IS CABLE ROUTED INCORRECTLY TO THE EXTERIOR RELEASE HANDLE. MAINTENANCE REROUTED THE LOCKING CABLE CORRECTLY TO EXTERIOR HANDLE ASSEMBLY IAW B717 AMM 53-52-01 830-802. RII COMPLETED BY QC2045. (LP #1236960 )Aug 23, 2019 · N945AT · Boeing 717200 · Aerodynamic FairingsSDR DALA2019082304923Cusp Web · crackedCRACK ON RH CUSP MEMBRANE STA 620 BTW X=- 44.5 AND X=-54.5 AT PAX CABIN. (CPAX). NRC 00396: RH CUSP MEMBRANE STA 620 BTW X=-44.5 AND X=-54.5 WERE REPAIRED PER B717-200 SRM 53-00-55-2R- 4 FIG. 215. (LP #1236084)Aug 23, 2019 · N947AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR HALA2019082600355Probe · malfunctionedINFLIGHT, RT ENG SYS FAIL. TROUBLESHOT FAULT THROUGH MCDU EEC-2 AND FOUND FAULT TO BE N2 PROBE ELECTRICAL CH-B. REMOVED AND REPLACED N2 SPEED PROBE PER FIM 77-12 TASK802. PERFORMED ENGINE AND LEAK CHECK. NO LEAKS/NO FAULTS. FAULT CODE; 771202Aug 22, 2019 · N494HA · Boeing 717200 · Fuel Control/Reciprocating EnginesSDR DALA2019082304922Cusp Web · crackedCRACK ON RH CUSP MEMBRANE STA 536 BTW X=- 44.5 AND X=-54.5 AT PAX CABIN. RH CUSP MEMBRANE STA 536 BTW X=-44.5 AND X=-54.5 WERE REPAIRED PER B717-200 SRM 53-00-55-2R- 4- FIG.219.Aug 22, 2019 · N947AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR HALA2019082200351Fire Loop · faultedFIRE L-A FAULT SHOWS ON STATUS PAGE. REMOVED AND REPLACED NR 1 ENG FIRE LOOP A PER AMM 26-11-00. TEST GOOD. OK FOR SERVICE.Aug 21, 2019 · N481HA · Boeing 717200 · Fire DetectionSDR DALA2019082104885Frame · crackedCRACK AT LH RING PAN FWR LOWER SECTION BTW STA Y=889. LH RING PAN FWR LOWER SECTION BTW STA Y=889 WAS REPAIRED PER B717-200 SRM 56-20-02-2R-1 FIG. 202.Aug 21, 2019 · N947AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2019082104884Frame · crackedCRACK AT LH RING PAN FWD LOWER SECTION BTW Y=636. LH RING PAN FWD LOWER SECTION BTW Y=636 WAS REPAIRED PER B717-200 SRM 56-20-02-2R-1- FIG. 202.Aug 21, 2019 · N947AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2019082104883Frame · crackedCRACK AT RH RING PAN AT STA Y=870. RH RING PAN AT STA Y=870 WAS REPAIRED PER B717-200 SRM 56-20-02-2R-1- FIG. 202.Aug 21, 2019 · N947AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2019082104882Frame · crackedCRACK AT LH RING PAN FWD LOWER SECTION BTW Y=794. LH RING PAN FWD LOWER SECTION BTW Y=794/ 813 WAS REPAIRED PER B-717-200 SRM 56-20-02-2R-1 FIG. 202.Aug 20, 2019 · N947AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2019082004881Lens · missingTHE FORWARD FACING LENS FROM THE CENTER AISLE EMERGENCY EXIT SIGN AT THE OVERWING EXIT IS MISSING. MAINTENANCE INSTALLED THE CENTER AISLE FORWARD FACING LENS AT THE OVERWING EXITS PER B717 AMM 33-51. (LP #6167025)Aug 19, 2019 · N930AT · Boeing 717200 · Emergency LightingSDR DALA2019081900003Panel · crackedHIDDEN CRACK ON O/B SPOILER PANEL NEAR TO HINGE FITTING.Aug 19, 2019 · N608AT · Boeing 717200 · SpoilersSDR DALA2019081904853Hinge · crackedCRACK CUTOUT ON AFT HINGE AT RH/LH FIXED NLG DOOR (FUS). NRC 00136: CRACK CUTOUT ON AFT HINGE AT RH/LH FIXED NLG DOOR WAS REPAIRED PER B717-200 SRM 53-10-01-2R PROCEDURE 11 FIG. 201. (LP #1229158)Aug 18, 2019 · N947AT · Boeing 717200 · Fuselage, Door HingeSDR DALA2019081904854Power Supply · malfunctionedTHE AFT CABIN EMERGENCY LIGHTS ARE FLASHING IN THE ARMED POSITION. MAINTENANCE REPLACED THE AFT CABIN EMERGENCY LIGHT BATTERY AND POWER SUPPLY PER B717 AMM 33-51. OPERATIONAL CHECK IS NORMAL. (LP #6142124)Aug 16, 2019 · N961AT · Boeing 717200 · Emergency LightingSDR DALA2019081704852Skin · damagedFUSELAGE SKIN DAMAGE AT STA 256, 2 INCHES BELOW L17LT. NRC 011-0001:0514-2001/001 00001: COMPLIED WITH ER/A 580474-14 REV O. ASSOCIATED ER/A 14-580474 ADDED FOR AC 9570. NRC 16: COMPLIED WITH ER/A 580474-14 REV ORIG. PRI 580474-14 REV 0 MATCHES ER/A 580474-14 Aug 16, 2019 · N929AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2019081764823Bearing · frozenATTACH BEARINGS FROZEN/WORN, PAINT ERODED. REPLACED BEARINGS REF. CMM 27-10-1 DAL. REV. 12, PAINTED PER AMDS WORKCARD 1120-2004 AND BALANCED PER 717 SRM 51-60-01. WEIGHT AND BALANCE -264.8 IN/LBS. REPLACED BEARINGS REF. CMM 27-10-1 DAL. REV. 12, PAINTED PER Aug 14, 2019 · Boeing 717200 · AileronsSDR DALA2019081504764Doubler · corrodedCORROSION ON INTERNAL PRODUCTION DOUBLER BTW STA 1022 AND LONG 29RH AT AFT CARGO COMPARTMENT. THE DOUBLER WAS REPAIRED PER ER/A 580391-14 REV ORIG AND ETI -17-19-122 REV 2.Aug 14, 2019 · N945AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2019081504763Tray · corrodedSPOTS OF CORROSION ON WASTE SRVC TRAY PANEL. CORROSION WAS REMOVED PER B717-200 SRM 51-10-04-0G AND REMAINING THICKNESS IS 0.030"; OUT OF LIMITS IAW SRM 53- 00-00-1A ALLOWABLE DAMAGE PAR. 4 FIG-.103. WASTE SRVC TRAY PANEL WAS REPLACED IAW DWG 5965767-7, SRAug 14, 2019 · N945AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2019081764824Bearing · frozenPD: ATTACH BEARINGS FROZEN/WORN, PAINT ERODED. CA: REPLACED BEARINGS REF. CMM 27-10-1 DAL. REV. 12, PAINTED PER AMDS WORKCARD 1120-2004 AND BALANCED PER 717 SRM 51-60-01. WEIGHT AND BALANCE -262.00 IN/LBS. REPLACED BEARINGS REF. CMM 27-10-1 DAL. REV. 12, PAINAug 13, 2019 · Boeing 717200 · AileronsSDR DALA2019081404755Sliding Window · crackedCRACK ON UPPER AFT CORNER SLIDING WINDOW LEFT SIDE (CPIL). NRC 00575: CRACK ON UPPER AFT CORNER SLIDING WINDOW LEFT SIDE WAS REPAIRED PER B717-200 SRM 56-10-02-2R-1.Aug 13, 2019 · N945AT · Boeing 717200 · Flight Compartment WindowsSDR DALA2019081434753Frame Angle · crackedCRACKED FRAME CLIP ON STA 1152 AND X=9 CROWN AREA, AFT ACCESORY COMPARTMENT (CAT). NRC 00422: AREA WAS REPAIRED PER ER/A 580410-14 REV ORIG AND ETI-17-19-141 REV 1. ASSOCIATED ER/A 14-580410 ADDED FOR AC 9505. (LP #1219535)Aug 12, 2019 · N945AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2019081204733Frame · corrodedCORROSION ON FRAME ON BS 890, STRINGER 25L IS OUT OF LIMITS AT AFT CARGO COMPARTMENT, MINIMUM REMAINING THICKNNES IS 0.032" AND OUT OF LIMITS IAW SRM 53-00-00-1A, ALLOWABLE DAMAGE 1, PAR 4, FIG 103. DUE TO FRAME OUT LIMITS, THE FRAME WAS REPAIRED IAW SRM 53Aug 11, 2019 · N945AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2019081204732Door · damagedELONGATED SCREW HOLES ON LH FWD OVERWING EMERGENCY EXIT DOOR FROM PASSENGER INNER SKIN AND PAN AT LH FWD OVERWING EMERGENCY EXIT DOOR REPAIRED IAW ETI-17-19-134 REV 2, AND ER/A 580350-14, REV ORIGINAL, SECTION I, PERMANENT REPAIR.Aug 10, 2019 · N945AT · Boeing 717200 · Emergency ExitsSDR DALA2019081204731Battery Pack · failedROW 26C EMERGENCY LIGHT IS NOT ILLUMINATING. MAINTENANCE SUSPECTS A BAD EMERGENCY BATTERY POWER SUPPLY PACK, REPLACED THE BATTERY PACK IAW AMM 33-51-03. EEPL SYSTEM NOW OK FOR SERVICE.Aug 10, 2019 · N961AT · Boeing 717200 · Emergency Lighting
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