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 DALA2019070204004Light · disconnectedTHE CABIN CEILING EMERGENCY LIGHTS AT ROW 1 & 24 ARE INOPERATIVE. ONE LIGHT AT EACH LOCATION IS INOPERATIVE, LIGHTS ARE NOT ADJACENT. EACH WAS RELAMPED, BUT DID NOT CORRECT THE PROBLEM. THE LIGHTS WERE PLACED ON MEL 33-51-01A AND PLACARDS INSTALLED. MAINTENACEJun 21, 2019 · N947AT · Boeing 717200 · Emergency LightingSDR DALA2019062543826Door Frame · crackedCRACKED RH NOSE LANDING GEAR JAMB BEAM AROUND STA Y-47. RT NOSE LANDING GEAR JAMB BEAM AROUND STA Y-47 WAS REPAIRED PER ER/A 495600-14MA REV C.Jun 21, 2019 · N936AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2019062423783Floorbeam · corrodedCORROSION ON FLOOR SUPPORT STA 145 BETWEEN X=- 44 TO X=-53 RH SIDE. FLOOR SUPPORT WAS REPLACED PER B717-200 SRM 51-40-05 AND DWG #9936533 REV CM.Jun 21, 2019 · N948AT · Boeing 717200 · Fuselage Main, Floor BeamSDR DALA2019062423782Floor Panel · corrodedCORROSION ON FLOOR PANEL, BETWEEN STA 148 AND 200, BETWEEN STA X=-50 AND X=-56. FLOOR PANEL BETWEEN STA 148 AND 200, BETWEEN STA X=-50 AND X=-56 WAS REPLACED PER B737-200 SRM 51-40-08-0G AND SRM 51-10-04-0G PAR 21 AND 15.Jun 21, 2019 · N948AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2019062423781Floor Support · corrodedCORROSION ON FLOOR SUPPORT BETWEEN STA. 120 AND 148, X= -24 AND X= -36. (CPIL) LOG-PAGE UPDATED @ 21JUN19 2310 UTC 02 CORR BY MEJORADA G 00289765 QRO 21JUN19 ATA 5321 FLOOR SUPPORT BTW STA 120 AND 148, X=-24 AND X-36 WAS REPLACED PER B717-200 SRM 51-41- 02-0Jun 21, 2019 · N948AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2019062423780Cusp Web · corrodedCORROSION ON CUSP MEMBRANE BETWEEN STA RH SIDE IN STA 799 IS 0.010" REWORKED AREA IS OUT LIMITS. NRC 00606: CORROSION LEVEL 2, OUT OF LIMITS AREA WITH CORROSION CUSP MEMBRANE STA 799 WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 REPAIR 4 FIG 216.Jun 21, 2019 · N948AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2019062423779Beam · crackedCRACK BEAM #4 FWD EDGE AT GALLEY SERVICE DOOR (R1) (PTAS). NRC 00144: BEAM #4 AT GALLEY SERVICE DOOR (R1) WAS REPLACED PER SRM 51-41-02-0G AND 51-41-05-0G.Jun 21, 2019 · N948AT · Boeing 717200 · Galley DoorsSDR DALA2019062423778Beam · crackedCRACKED LH NOSE LANDING GEAR JAMB BEAM AROUND STA: Y-47 (FYT). NRC 00569: LH NOSE LANDING GEAR JAMB BEAM AROUND STA Y-47 WAS REPAIRED PER B-717-200 SRM 53-10-14-2R FIG. 201 REP. 2.Jun 21, 2019 · N936AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2019062423777Channel · crackedCRACKED CHANNEL BTW BEAM #1 AND #2 ON FWD PASSENGER DOOR FWD EDGE. (L1) (PTAS). CHANNEL BTW BEAM #1 AND #2 ON FWD PASSENGER DOOR FWD EDGE WAS REPAIRED IAW SRM 52-10-02- 2R REPAIR 3.Jun 21, 2019 · N943AT · Boeing 717200 · Passenger/Crew DoorsSDR DALA2019062103704Power Supply · inoperativeTHE AFT BULKHEAD DOOR EXIT MARKER SIGN IS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY BATTERY POWER SUPPLY B5-260 PER B717 AMM 33-50. THE AFT BULKHEAD DOOR EXIT SIGN NOW OPERATES NORMALLY. (LP #5359820)Jun 21, 2019 · N957AT · Boeing 717200 · Emergency LightingSDR DALA2019062103703Pan · crackedCRACK ON PAN BTW BEAM 1 TO BEAM 2 AND STA 994 AT AFT CARGO DOOR (C2). NRC 00439: AREA WAS REPAIRED PER ER/A 579043-14 REV. ORIG. AND ETI-17-19-074, REV 2. (LP #1133339)Jun 21, 2019 · N936AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2019070604058Torque Tube · corrodedINITIAL INSPECTION: CORROSION ON RUDDER CONTROL TAB TORQUE TUBE IN REF 2720-2004 JOB #001-0259. RUDDER TORQUE TUBE ASSY P/N 5912802-507 S/N: UNK WAS REPLACED FOR SERVICEABLE P/N: 5912802-507 S/N: DL16 AND WAS INSTALLED UNDER 2720-2004 JOB# 001-0259. TUBE, TORQJun 20, 2019 · N948AT · Boeing 717200 · Rudder Control SystemSDR DALA2019070304026Housing · corrodedCORROSION ON RUDDER YOKE BEARING SUPPORT HOUSING (AMDS 2720-2004). NRC 00379: CORROSION LEVEL 2, BEARING SUPPORT HOUSING WAS REPLACED PER SRM 51-41-02-0G AND 51-41-01- 0G. (LP #1132426)Jun 20, 2019 · N943AT · Boeing 717200 · Rudder Miscellaneous StructureSDR DALA2019062603875Doubler · corrodedEXFOLATION DOUBLER ON LOWER CUT OUT DOOR JAMB STA Y=972 AT AFT CARGO COMPARTMENT. NR 00325: CORROSION LEVEL 2, EXFOLATION CORROSION ON DOUBLER AT LOWER CUT OUT DOOR JAMB STA Y=972 AT AFT CARGO COMPARTMENT WAS ATTENDED PER ER/A 578898-14 REV. ORIGINAL. ASSOCIATJun 20, 2019 · N936AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2019062103702Cusp Web · corrodedCORROSION ON CUSP MEMBRANE BETWEEN STA 408 TO 427 RH SIDE. (CPAX). NRC 00302: CORROSION LEVEL 2, CUSP MEMBRANE BETWEEN STA Y=408 TO Y=427 RH SIDE WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 FIG.203. (LP #1132920)Jun 20, 2019 · N948AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2019062103701Intercostal · corrodedCORROSION ON INTERCOSTAL STA Y=1032 AND LONG 25LH AT AFT CARGO COMPARTMENT. NRC 00317: CORROSION LEVEL 2, INTERCOSTAL STA Y=1032 AND LONG 25LH AT AFT CARGO COMPARTMENT WAS REPLACED PER DWG #5936071 REV. W AND PER B717-200 SRM 51-41-02-0G. (LP #1132805)Jun 20, 2019 · N936AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2019062103700Finger Doubler · corrodedCORROSION ON FINGER DOUBLER FROM STA Y=943 TO 960 AND Y=1005 TO Y=1044 BELOW LH LONGERON AT AFT CARGO COMPARTMENT WAS FOUND OUT OF LIMITS. NRC 00691: CORROSION LEVEL 2, SECTION OF FINGER DOUBLERS STA Y=943 TO Y=960 AND Y=1005 TO Y=1044 BELOW LH LONGERON AT AFTJun 20, 2019 · N936AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2019062103699Cusp Web · corrodedCORROSION ON CUSP MEMBRANE (BULGING MEMBRANE) BETWEEN STA Y=460 TO Y=465 RH SIDE WAS FOUND OUT OF LIMITS IN REF NRC 00303. NRC 00596: CORROSION LEVEL 2, CUSP MEMBRANE (BULGING MEMBRANE) BETWEEN STA Y=460 TO Y=465 RH SIDE WAS REPAIRED PER B717-200 SRM 53-00-55-Jun 20, 2019 · N948AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2019062103698Frame Angle · corrodedEXFOLATION ON FRAME CLIP STA Y=1037 BTW LONG 25RH TO LONG 25LH AT AFT CARGO COMPARTMENT. NRC 0316: CORROSION LEVEL 2, FRAME CLIP FROM STA Y=1037 BTW LONG 25RH TO LONG 25LH AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-02-0G AND DWG #9958238-85 RJun 20, 2019 · N936AT · Boeing 717200 · Fuselage Main, FrameSDR 2019F00226Spoiler · delaminatedSPOILER HAD DELAMINATION.Jun 20, 2019 · N969AT · Boeing 717200 · SpoilersSDR DALA2019062003670Lens · missingTHE AFT DOOR EMERGENCY LIGHT LESN MISSING. MAINTENANCE REPLACED THE LENS IAW B717 AMM 33-51.Jun 20, 2019 · N923AT · Boeing 717200 · Emergency LightingSDR DALA2019070304025Splice · corrodedEXFOLATION ON SPLICE CLIP STA Y=898.500 BTW LONG 25L TO LONG 25R AT AFT CARGO COMPARTMENT. NRC 00171: CORROSION LEVEL 2, SPLICE CLIP STA Y= 898.500 BTW LONG 25L TO LONG 25R AT AFT CARGO WAS REPLACED PER SRM 53-20-01-0I AND 51-41-05-0G. (LP #1131371)Jun 19, 2019 · N936AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA201906253809Cusp Web · corrodedCORROSION ON CUSP MEMBRANE BETWEEN STA 851 TO 870. (CPAX). NRC 00296: CORROSION LEVEL 2, CUSP MEMBRANE BETWEEN STA 851 TO 870 LH WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 FIG. 215. (LP #1130929)Jun 19, 2019 · N948AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA201906213697Doubler · corrodedCORROSION ON DOUBLER STA 1053 OVER PROJECTION STG 30 ON LOWER BULHEAD AREA AT AFT CARGO COMPARTMENT. THE DOUBLER WAS REPLACED PER B717-200 SRM 51-41-05-0G AND SRM 53-20-08-0I- 2 FIG. 1.Jun 19, 2019 · N936AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2019062003669Floor Panel · debondedDEBONDED FLOOR PANEL #221LF PAX CABIN (CPAX). NRC 00403: FLOOR PANEL #221LF WAS FABRICATED, REPLACED, AND IDENTIFIED PER B-717-200 SRM 53-20-50-2R-3. (LP #1131537)Jun 19, 2019 · N943AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2019062003668Pan · corrodedCORROSION ON FWD CARGO COMPARTMENT LOWER DOOR JAMB PAN, BTW STA Y=370 TO Y=427 REASON FOR RE-WRITE WRONG MEASSUREMENT. (CCD). NRC 00679: CORROSION LEVEL 2, FWD CARGO COMPARTMENT LOWER DOOR JAMB PAN, BTW STA Y=370 TO Y=427 WAS REPLACED PER B717-200 SRM 53-20-15Jun 19, 2019 · N936AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2019062003667Door Frame · corrodedCORROSION ON LOWER DOOR JAMB FROM STA Y=954 TO Y=994 AT AFT CARGO COMPARTMENT. NRC 00324: LOWER DOOR JAMB AND SPLICES WERE REPLACED PER B717-200 SRM 53-20-15-2R REPAIR 7 AND 51-41-02-0G, 51-41-04-0G, AND 51-41-05-0G. (LP #1131248)Jun 19, 2019 · N936AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2019062003666Reinforcement · crackedCRACK ON LH SLINDING WINDOW REINFORCEMENT CUTOUT, AFT UPPER CORNER AT FLIGHT COMPARTMENT (CPIL). NRC 00475: BRACKET LH SLINDING WINDOW REINFORCEMENT CUTOUT, AFT UPPER CORNER WAS REPLACED PER B717-200 SRM 51-41-01-0G, 51-41-02-0G, AND 51-41-05-0G. (LP #1130511)Jun 19, 2019 · N936AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2019061903652Beam · crackedCRACK ON BEAM STA Y=737, X= 54 AND Z=-2 LH SIDE AT WING BOX. NRC 00467: FLOOR BEAM WAS REPLACED PER B717-200 SRM 51-41-02-0G AND SRM 51-41-05-0G .Jun 19, 2019 · N936AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2023052504150Unknown · unknownTHIS ER/A 527176-14 INCORPORATES FAA FORM 8110-3. ACCOMPLISH SECTION II INSPECTION INSTRUCTIONS. THE SUBJECT ER/A IS NOW AT REV A. AT OR PRIOR TO 35,500 TOTAL AIRCRAFT FLIGHT CYCLES, AND REPETITIVELY THEREAFTER EVERY 4,000 FLIGHT CYCLES, ACCOMPLISH SECTION II Jun 18, 2019 · N960AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2019061903651Pan · crackedCRACK ON INNER PAN STA Y=370 IN BEAM 3 AT FWD CARGO COMPARTMENT DOOR (C1). NRC 00127: CRACK ON INNER PAN STA Y=370 IN BEAM 3 AT FWD CARGO COMPARTMENT DOOR WAS REPAIRED REPAIR PER B717-200 SRM 52-30-02-2R REPAIR 1 FIG. 201. (LP #1129505)Jun 18, 2019 · N948AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2019061983650Longeron · corrodedCORROSION ON LONGERON END 23RH STA Y=1003 AT AFT CARGO COMPARTMENT. NRC 0304: CORROSION LEVEL 2, DUE TO CORROSION OUT OF LIMITS LONGERON END 23RH STA Y=1003 AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-05-0G. (LP #1127877)Jun 17, 2019 · N936AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2019061803628Engine · odorTHE FLIGHT CREW DIVERTED DUE TO ODOR CIRCULATING IN THE FLIGHT DECK AND CABIN AFTER ROTATION. THE FLIGHT ATTENDANTS REPORTED THE SMELL AND HAZE DURING CLIMB AFTER TAKEOFF. CORRECTIVE ACTION: MAINTENANCE REPLACED THE #1 ENGINE.Jun 17, 2019 · N990AT · Boeing 717200 · Engine (Turbine/Turboprop)SDR DALA2019061803624Cusp Web · crackedCRACKED CUSP WEB ON STA Y=355 X=57 LH AT PASSENGER COMPARTMENT (CPAX). NRC 00452: AREA WAS REPAIRED PER B717-200 SRM 53-00- 55-2R-4 FIG. 215.Jun 17, 2019 · N948AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2019061803623Frame Angle · corrodedEXFOLATION ON FRAME CLIP STA Y=908 BTW LONGERON 26LH TO LONGERON 28RH BOTH FACES AT AFT CARGO COMPARTMENT. NRC 0174: CORROSION LEVEL 2, FRAME CLIP STA Y=908 BTW LONG 26LH TO LONG 28RH AT AFT CARGO COMPARTMENT WAS REPLACED PER B-717-200 SRM 51-41-02-0G. (LP #11Jun 17, 2019 · N936AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2019061803621Frame · crackedCRACK ON RH WINDOW RING PAN STA Y=889 AT PAX CABIN. NRC 00197: CRACK ON RH WINDOW RING PAN STA Y=889 WAS REPAIRED PER B717-200 SRM 56-20-02-2R-1.Jun 17, 2019 · N943AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2019061703620Cusp Web · crackedCRACK ON LH CUSP WEB BETWEEN STA 655/653 IN REF NRC 00647. (CPAX). NRC 00675: LH CUSP WEB BETWEEN STA 655/653 WAS REPLACED PER B717-200 SRM 53-00-55-2R-4, 51-41-02-0G, AND 51-41-05-0G.Jun 16, 2019 · N936AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2019061703619Cusp Web · crackedCRACK ON LH CUSP WEB STA 655 UNDER PRODUCTION DOUBLER. (CPAX). NRC 00647: LH CUSP WEB STA 655 UNDER PRODUCTION DOUBLER WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 FIG. 211.Jun 16, 2019 · N936AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2019061703618Frame Angle · crackedCRACK ON CLIP FRAME LONG 14RH STA 1022 AT FWD FACE OF BULKHEAD (CPAX). NRC 00401: FRAME CLIP WAS REPLACED PER B717-200 SRM 51-41-05-0G.Jun 16, 2019 · N936AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2019061703617Gusset · crackedCRACK ON GUSSET PROJECTION LONGERON 7RH STA 1022 AT AFT FACE OF BULKHEAD (CPAX). NRC 00397: GUSSET PROJECTION LONG 7RH STA 1022 AT AFT FACE OF BULKHEAD WAS REPAIRED PER ER/A 578999-14 REV.ORIGINAL (SECTION I: PERMANENT REPAIR) AND ETI-17-19-076 REV. 1. ASSOCIAJun 16, 2019 · N936AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2019061703616Web · crackedCRACK ON WEB FROM STA 161 BTW X=-42 TO X=-44 (FUS). NRC 0366: WEB FROM STA 161 BTW X=-42 TO X=-44 WAS REPAIRED PER B717 SRM 53-00-00-2R-1 FIG. 201. (LP #1126059)Jun 16, 2019 · N943AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2019061763615Gusset · crackedCRACK ON GUSSET PROJECTION LONGERON 7LH STA 1022 (CPAX). NRC 00398: GUSSET PROJECTION LONG 7LH STA 1022 WAS REPAIRED PER ER/A 57899-14 REV. ORIGINAL (SECTION I: PERMANENT REPAIR) AND ETI-17-19-076 REV. 1. ASSOCIATED ER/A 14-578999 ADDED FOR AC 9563. (LP #11249Jun 16, 2019 · N936AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2019061763614Access Panel · corrodedEXCESSIVE CORROSION ON FUEL ACCESS PLATE #520LB.(AI). NRC 00666: CORROSION LEVEL 2, CORROSION ON FUEL TANK ACCESS DOOR #520LB OF LH WING FUEL TANK WAS REMOVED PER B717-200 SRM 51-10-04-0G PAR 26 AND B717-200 SRM 57-10-01- 2R REPAIR 2 PAR. 5.; DIAMETER OF COUNTJun 16, 2019 · N936AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2019061763613Frame · crackedCRACK ON FRAME, LONG 17RH STA 1037 (CPAX). NRC 00404: FRAME, LONG 17RH STA 1037 WAS REPAIRED PER B717-200 SRM 53-20-07-2R-4. (LP #1124857)Jun 16, 2019 · N936AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2019061703592Tire · failedTHE CREW RETURNED TO THE DEPARTURE AIRPORT FOLLOWING THE #2 TIRE FAILURE ON TAKEOFF ROTATION. CORRECTIVE ACTION: MAINTENANCE REPLACED BOTH THE #1 AND #2 TIRES. THERE WAS SOME DAMAGE FOUND ON LMLG WHEEL WELL DOWN LOCK CONDUIT, LMLG DOWN/UP LOCK SENSORS, AND LMLJun 15, 2019 · N958AT · Boeing 717200 · TireSDR DALA2019061763591Longeron · crackedCRACK ON LONGERON 6RH STA 1022 AT AFT FACE OF BULKHEAD (CPAX). NRC 00396: SECTION OF LONGERON 6RH BTW STA 996 TO 1053 WAS REPAIRED PER B717-200 SRM 53-00-05-2R. (LP #1124449)Jun 15, 2019 · N936AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2019061763590Cusp Web · canningOIL CANING ON CUSP WEB AT BTW STA 889/908 LH X= 44/60 (FUS). NRC 00361: CUSP WEB DAMAGED BTW STA 889 TO 908 LH, X =-44 TO X=-60, WAS REPLACED PER B-717-200 SRM 51-41-02-0G AND SRM 51-41-05-0G. (LP #1124292)Jun 15, 2019 · N936AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2019061753589Longeron · crackedCRACK ON LONGERON 4LH STA 1022 (CPAX). NRC 00388: SECTION LONGERON 4 LH FROM STA. 1010 TO STA. 1053 WAS REPAIRED PER B-717-200 SRM 53-00-05-2R.Jun 14, 2019 · N936AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2019061753588Frame · crackedCRACK INDICATION OF THE UPPER RADIUS OF THE FRAME TAB. CRACK LENGTH APPROXIMATELY 1/8 IN. NRC 066-0002:5310-01436-01B/001 00042: REPLACED LT OVER-WING FRAME AT STA 696 PER AMDS WORK CARD 5310- 01436-03A.Jun 14, 2019 · N990AT · Boeing 717200 · Fuselage Main, FrameSDR DALA201906203671Light · damagedEMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE AT 19B. 19B EMERGENCY LIGHT DAMAGED OR INOPERATIVE LIGHT ASSY - PHOTO LUMINESCENT [LENGTH 23.90 INCHES] REF IPC 33-51-12-01 ITEM 55. MAINTENANCE REINSTALLED PHOTO LUMINESCENT STRIP REF LOG PAGE #5917548. (LP #112Jun 13, 2019 · N979AT · Boeing 717200 · Emergency Lighting
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