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 DALA2016062304859Skate Angle · deformedRT SIDE VERTICAL STABILIZER ATTACH SKATE ANGLE IS DEFORMED. REPAIRED IAW ER/A 547541-14, REV ORIGINAL ER/A MATCHES ALL PRIS.Jun 22, 2016 · N939AT · Boeing 717200 · Fuselage, Stabilizer Attach FittingsSDR DALA2016062304858Frame · dentedCANTED FRAME 1189 IS DENTED AT SKIN CUTOUT FOR REPAIR OF DAMAGE AT STR-11R. REPAIRED IAW ER/A 547985-14, REV A, SECTION 2, FRAME DAMAGE PERMANENT REPAIR.Jun 22, 2016 · N939AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2016062404890Door Frame · corrodedFWD CARGO DOOR JAMB IS CORRODED IN SEVERAL PLACES, MARKED. REPLACED DOOR JAMB IAW SRM 51-41-02 AND 51-41-05 AND 51-41-02.Jun 21, 2016 · N920AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016062304861Pan · crackedLEFT MLG BODY DOOR CRACKED ON FWD SIDE APPROXIMATELY MIDWAY DOWN, MARKED. REMOVED AND REINSTALLED MLG DOOR IAW 32-14-00, INSTALLED NEW DOOR PAN IAW ERA 545687-14 AND DWG 5910782. ASSOCIATED ER/A 00-545687, ADDED FOR AC 9578.Jun 21, 2016 · N920AT · Boeing 717200 · Landing Gear DoorsSDR DALA2016062304860Pan · crackedRIGHT MLG BODY DOOR CRACKED AT FORWARD DOOR PAN, MARKED. REMOVED AND REINSTALLED MLG DOOR IAW 32-14-01, INSTALLED NEW DOOR PAN IAW ER/A 545687-14 AND DWG NR 5910782. ASSOCIATED ER/A 54-568814, ADDED FOR AC 9578.Jun 21, 2016 · N920AT · Boeing 717200 · Landing Gear DoorsSDR DALA2016062104803Cusp Web · corrodedUNDER FLOOR SUPPORT, CUSP WEB 219-237, RBL 44-RBL HAS CORROSION. REPLACED CUSP WEB AT FS 218 TO 237, RBL 44 TO 56 IAW SRM 51-41-02, 51-41-05.Jun 20, 2016 · N920AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016062004763Battery Pack · dischargedDURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY PATHWAY LIGHTING AT PANELS 11, 12, AND 13 WERE INOPERATIVE. MAINTENANCE FOUND THAT THE BATTERY PACK WAS NOT CHARGING AND REPLACED IT ALONG WITH THE BATTERIES IN THE POWER SUPPLY. THE LIGHTS RETJun 19, 2016 · N952AT · Boeing 717200 · Emergency LightingSDR DALA2016061904762Web · damagedTOOL MARK ON WEB STA Y=674 BETWEEN LONGERON 11RT TO 10RT AND LONGERON 14RT TO 15RT AT CPAX, SM, CARD 6, ZONE 201. WEB WAS REPAIR IAW ER/A 547802-14, REV ORIGINAL AND ETI 17-16-064, SRM 51-40-08, 51-20-09 AND 51-10-04, PAR 15/21.Jun 18, 2016 · N915AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016061804761Cusp Web · crackedRIGHT CUSP MEMBRANE IS CRACKED AT STA 384. REPAIRED RT CUSP MEMBRANE AT STA 384 IAW SRM 53-00-55, REPAIR 4, FIG 224.Jun 17, 2016 · N920AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR HALA2016061600239Hydraulic System · contaminatedLT HYD TEMP HI, ABORT ON TAKEOFF. BLEED LEFT HYD SYS AND QTY CK OK TO CONTINUE IAW AMM 12-13-01, AND AMM 29-00-00, BOTH HYD SYST. CK OK FOR SERVICE.Jun 16, 2016 · N477HA · Boeing 717200 · Hydraulic System, MainSDR DALA2016061704730Cusp Web · corrodedCORROSION ON RT CUSP WEB AT STA 655 TO 674 IS OUT OF LIMITS. INSTALLED REPAIR DOUBLER ON RT CUSP WEB AT STA 655-674 IAW SRM 53-00-55, REPAIR 4.Jun 16, 2016 · N920AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016061704729Cusp Web · crackedRIGHT CUSP MEMBRANE CRACKED AT STA 943. REMOVED CRACK DAMAGE AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 53-00-55, REPAIR 4, FIG 216.Jun 16, 2016 · N920AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016061704728Skin · corrodedCORROSION AT WING BOX REAR SPAR UPPER SKIN LOWER SURFACE. RIGHT WHEEL WELL AREA, ZONE 144, CARD 1. REPAIR WAS ACCOMPLISHED IAW ER/A 546499-14, REV ORIGINAL, HFEC ON BLENDED AREAS WAS PERFORMED AND NO ADDITIONAL DAMAGE WAS FOUND.Jun 16, 2016 · N961AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016061704727Skin · corrodedCORROSION AT WING BOX REAR SPAR UPPER SKIN LOWER SURFACE LT WHEEL WELL AREA, ZONE 145, CARD 1. CORROSION WAS REMOVED, REWORKED AREA WAS TREATED, PAINTED IAW ER/A 546499-14, REV ORIGINAL. HFEC BLENDED AREA AND NO ADDITIONAL DAMAGE WAS FOUND. ASSOCIATED ER/AJun 16, 2016 · N961AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016061704726Cusp Web · crackedRIGHT CUSP MEMBRANE CRACKED AT BS 435. REPAIRED CRACKED MEMBRANE AT BS 434 RT IAW SRM 53-00-55, REPAIR 4.Jun 16, 2016 · N920AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016061604672Strap · crackedCRACK ON FWD STRAP AT BEAM NR 6 L1 PASSEGER DOOR. STRAP WAS REPLACED IAW SRM 51-41-02, 51-41-05, 51-40-08, 51-10-04 PAR 15 AND 21, AND DWG 9955750, REV. U. CRACK LENGTH .500".Jun 15, 2016 · N915AT · Boeing 717200 · Passenger/Crew DoorsSDR DALA2016061604671Angle · corrodedCORROSION ON CUSP ANGLE AT LBL 60 BETWEEN BS 157 AND 218. DUE TO EXCESSIVE DAMAGE BY CORROSION. CUSP ANGLE WAS REPAIRED IAW ETI 17-16-054, REV 1 AND ER/A 547810-14, REV ORIGINAL.Jun 15, 2016 · N915AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016F00141Spoiler · dentedDURING NON-ROUTINE CHECK, UNSCHEDULED INSPECTION, RT OTBD SPOILER FOUND DENTED.Jun 15, 2016 · N925AT · Boeing 717200 · SpoilersSDR DALA2016061604670Skin · crackedVERTICAL STABILIZER L/E HAS A 3" CRACK & FASTENERS PULLED INTO THE SKIN & ELONGATED HOLES BY LWR VOR ACCESS PANELS, REMOVED DAMAGE, FABRICATED FILLERS AND DOUBLERS USING 7075-0 HEAT TREATED TO 7075-T6 2090. INSTALLED REPAIR PARTS IAW ER/A 545681-14AD REPETITIJun 14, 2016 · N966AT · Boeing 717200 · Vertical Stabilizer, Plate/SkinSDR DALA2016061504668Longeron · corrodedLONGERON 30 AND SPLICE CORRODED FROM BS 927-946. BLENDED CORROSION ON L30 SPLICE AT BS 927 TO BS 946 ORIGINAL THICKNESS .250 REMAINING .245 FOUND TO BE WITHIN LIMITS IAW 53-00-00 AND 53-00-05, REPAIR 2, FIG 201, TAG 1768. BLENDED L30 BETWEEN BS 927 AND BS 94Jun 14, 2016 · N966AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2016061504667Structure · bentBEND ON FWD/AFT LOWER CORNER AT EXTERNAL SURFACE PASSENGER L1 DOOR. LOWER CORNER AT EXTENAL SURFACE PASSENGER ENTRANCE DOOR WAS REPAIRED IAW SRM 52-10-01, FIG 201, REP 2. WEIGHT IS 1.52 LB. RII INSPECTOR EVP 200801883 TECHOPS.Jun 14, 2016 · N915AT · Boeing 717200 · Passenger/Crew DoorsSDR DALA2016061504666Doubler · crackedCRACK ON DOUBLER FWD/AFT END AT BEAM NR 1 L1 DOOR. FWD/AFT END AT BEAM NR 1 WERE REPIRED IAW SRM 52-10-02, FIG 201, REPAIR 7. CRACKS LONG .656 AND .468".Jun 14, 2016 · N915AT · Boeing 717200 · Passenger/Crew DoorsSDR DALA2016061504665Doubler · crackedCRACK ON DOUBLER AFT END AT BEAM NR 7 L1 DOOR. AFT END AT BEAM NR 7 WAS REPAIRED IAW SRM 52-10-02, FIG 201, REPAIR 13. CRACK LONG 0.812".Jun 14, 2016 · N915AT · Boeing 717200 · Passenger/Crew DoorsSDR DALA2016061504664Doubler · wornWEAR ON DOUBLER PRODUCTION AT INNER RT PAN A SIDE LOWER HINGE AFT EMERGENCY EXIT. DOUBLER PRODUCTION WAS REPAIRED IAW SRM 52-10-02, FIG 201, REP 16. MEASURE: OT IS 0.050" AND REMAINING THICKNESS IS 0.028". THEREFORE OUT LIMITS. EQ: DIGITAL ULTRASONIC THICKJun 14, 2016 · N915AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016061504663Doubler · crackedCRACK ON PRODUCTION DOUBLER BS 1178 CANT BETWEEN LONGERON NR 1 AND NR 2 LT AT AFT ACCESSORY COMPARTMENT, SM. PRODUCTION DOUBLER WAS REPAIRED IAW ER/A 546495-14, REV ORIGINAL, PERFORM REPETITIVE INSPECTIONS AT EVERY, C-CHECK OR 3000 CYCLES WHICHEVER COME FIRSTJun 14, 2016 · N961AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016061504662Skin · crackedCRACKED FUSELAGE SKIN ON CUTOUT OF RT/LT NLG AFT DOOR AFT HINGE. SKIN WAS REPLACED IAW SRM 53-10-01, 51-41-02, 51-41-05, 51-10-3 P. 21, 15.Jun 14, 2016 · N915AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016061504661Cusp Web · corrodedCORROSION ON CUSP WEB UPPER/LOWER SURFACE AT BS 157 TO 187 BETWEEN X=-54 AND X=-60 LOWER AREA OF R1 DOOR JAMB. W1, SM, CARD 87, ZONE 200. SERVICE DOOR JAMB PAN AND CUSP ANGLE WERE REPAIRED IAW ER/A 546506-14, REV ORIGINAL.Jun 14, 2016 · N961AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016061504660Cusp Web · corrodedRT CUSP MEMBRANE AT BS 943 HAS CORROSION. REMOVED CRACK DAMAGE AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 53-00-55, REPAIR 4, FIG 216.Jun 14, 2016 · N920AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016103107962Access Panel · corrodedCORROSION ON SETTLEMENT AND COUNTERSINK AREA OF WING ACCESS PANEL 620KB. THE ACCESS PANEL WAS REPLACED AND A LEAK CHECK WAS PERFORMED.Jun 13, 2016 · N961AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016103107961Access Panel · corrodedCORROSION ON SETTLEMENT AND COUNTERSINK AREA OF WING ACCESS PANEL 620HB. THE ACCESS PANEL WAS REPLACED AND A LEAK CHECK WAS PERFORMED.Jun 13, 2016 · N961AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016103107960Access Panel · corrodedCORROSION ON SETTLEMENT AND COUNTERSINK AREA OF WING ACCESS PANEL. THE ACCESS PANEL WAS REPLACED AND A. LEAK CHECK WAS PERFORMED.Jun 13, 2016 · N961AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016103107959Access Panel · corrodedCORROSION ON SETTLEMENT AND COUNTERSINK AREA OF WING ACCESS PANEL 620QB. ACCESS PANEL WAS REPLACED AND LEAK CHECKED.Jun 13, 2016 · N961AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016061504669Door Frame · corrodedR1 DOOR JAMB HAS CORROSION VISIBLE IN FWD AND AFT LOWER CORNER POCKETS OF JAMB AND IN LOWER POCKET OF AFT DOOR FRAME MARKED WITH ARROW. REMOVED CORROSION FROM LWR AND AFT LWER POCKETS AT R1 DOOR JAMB AREA AND LOWER POCKET OF AFT DOOR FRAME. INSTALLED REPLACEMJun 13, 2016 · N966AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016061404601Cargo Track · corrodedCORROSION ON RT CARGO TRACK UPPER & LOWER SURFACE BETWEEN BS 900-954. DUE TO EXCESSIVE DAMAGE, CARGO TRACK SECTION WAS REPLACED IAW SRM 51-41-05 AND 51-41-02.Jun 13, 2016 · N915AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016061404600Angle · crackedCRACK ON ANGLE OF WING BOX FLOOR STRUCTURE BS 712 TO 714 X -20 AND Z -8. ANGLE WAS REPLACED IAW SRM 51-41-02 AND SRM 51-41-05 AND DWG 5910464, REV "DE" ITEM 24.Jun 13, 2016 · N915AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016061404599Access Panel · corrodedCORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS DOOR 520EB AT LT WING. CORROSION ON COUNTERSINK OF ACCESS DOOR 520EB WAS REMOVED IAW SRM 51-10-04 AND WAS MEASURED AND FOUND OUT OF LIMITS WITH 3 ADJACENT HOLES 0.545", 0.555", AND 0.540" AND WAS REPJun 13, 2016 · N915AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016061404598Cargo Track · corrodedCORROSION ON LT CARGO TRACK BETWEEN BS 900 TO 1022. THE CARGO TRACK WAS REWORKED IAW SRM 51-10-04 PAR. 26. FOUND TO BE OUT OF LIMITS IAW SRM 53-20-52. A NEW CARGO TRACK WAS INSTALLED IAW SRM 51-41-05 AND 51-41-01.Jun 13, 2016 · N961AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016061404597Cargo Track · corrodedCORROSION ON LEFT CARGO TRACK FROM BS 817 TO 900. CARGO TRACK WAS REPLACED IAW SRM 53-20-52, 51-41-05 AND 51-41-01.Jun 13, 2016 · N961AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016061404596Skin · damagedENLONGATED HOLES ON FUSELAGE SKIN AND LONGERON 26 LT FROM BS 1004 TO 1045. SKIN REPAIRED IAW ETI-17-16-060, REV. 2 AND ER/A 546557-14, REV. ORIGINAL.Jun 13, 2016 · N961AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016061404595Skin · crackedCRACK ON SKIN BS 1133 BETWEEN LONGERON 2-3R AT OUTER FUSELAGE SKIN AREA. SKIN WAS REPAIRED IAW ETI-17-16-035, ER/A 546487-14AD, REV. ORIGINAL. ASSOCIATED ER/A 00-546487 ADDED FOR AC 9520.Jun 13, 2016 · N961AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016061404592Support · crackedLOWER FUSELAGE, UNDER WING BARREL KEELBEAM BS 606 CRACKED KEELBEAM SUPPORT, MARKED. REMOVED DAMAGED FORMER LT KEEL BS 606. REPAIRED FORMER IAW ER/A 545683-14MA. REINSTALLED FORMER IAW ER/A 545683-14MA, STEPS 1 THRU 10.Jun 13, 2016 · N966AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016061304548Longeron · corrodedCORROSION ON LONGERON 29 LT BELOW OF SPLICE BS 960 IN AFT CARGO COMPARTMENT. DAMAGE ON SECTION LONGERON WAS REMOVED AND WAS REPAIRED IAW SRM 51-10-04 AND 53-20-05, FIG 201.Jun 12, 2016 · N915AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2016061304547Access Panel · corrodedCORROSION ON COUNTERSINKS AND SETTLEMENT AREA OF FUEL ACCESS DOOR 620EB AT RT WING. CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS 620EB WERE REMOVED AND FOUND OUT LIMITS WITH 3 ADVANCED HOLES .545, .549, .544 THEREFORE WAS REPLACED IAW SRM 57-10Jun 12, 2016 · N915AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016061304546Frame · corrodedCORROSION ON FRAME ANGLE BS 908 BETWEEN LONGERON 29 AND 30L IN AFT CARGO COMPARTMENT. FRAME ANGLE WAS REPAIRED IAW SRM 53-00-06, FIG 201.Jun 12, 2016 · N915AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2016061304545Finger Doubler · corrodedCORROSION ON INTERNAL STRUCTURE BETWEEN BS 1002 TO 1022, LONGERON 26L AT AFT CARGO COMPARTMENT. FINGER DOUBLER WAS REPLACED BY EXCESSIVE CORROSION IAW SRM 53-03-07, FIG 212 AND 51-41-02.Jun 12, 2016 · N961AT · Boeing 717200 · Fuselage Main, StructureSDR HALA2016061100233Battery Pack · dischargedAFTER EMERGENCY POWER TEST WE HAVE EMERGENCY POWER TEST FAIL. GATE EXTERNAL POWER DROPPED OFF WHILE PLUGGED IN. BATTERY NEEDS CHARGING. CHARGED BATTERY EMERGENCY POWER TEST PASSED.Jun 11, 2016 · N488HA · Boeing 717200 · Emergency LightingSDR DALA2016061304549Battery Pack · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING IN THE FIRST CLASS SECTION OF THE CABIN HAD FAILED. MAINTENANCE REPLACED THE BATTERY PACK FOR THE NOTED LIGHTED AREA AND THE OPS CHECK WAS GOOD.Jun 11, 2016 · N987AT · Boeing 717200 · Emergency LightingSDR DALA2016061304544Bracket · crackedLEFT WING, L/E, STATION 164, CRACKED. REMOVED DAMAGED BRACKET, FABRICATED NEW BRACKET. TREAT AND PRIME BRACKET IAW SRM 51-22-01. INSTALLED FABRICATED BRACKET IAW SRM 51-40-02 AND 51-41-05 PARA 10,Jun 11, 2016 · N920AT · Boeing 717200 · Wing Miscellaneous StructureSDR DALA2016061204543Access Panel · corrodedCORROSION ON SETTLEMENT AREA AND COUNTERSINK OF WING ACCESS PLATE NR 520CB. CARD 38, ZONE 500. BECAUSE ACCESS PANEL WAS OUT OF LIMITS IAW SRM 57-10-01. ACCESS PLATE WAS REPLACED FOR A SERVICEABLE ONE.Jun 11, 2016 · N961AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016061204542Access Panel · corrodedCORROSION ON SETTLEMENT AREA AND COUNTERSINK OF FUEL ACCESS PLATE 620LB. ZONE 600, CARD 35. BECAUSE ACCESS PANEL WAS OUT OF LIMITS IAW SRM SRM 57-10-01. ACCESS PLATE WAS REPLACED FOR A SERVICEABLE ONE.Jun 11, 2016 · N961AT · Boeing 717200 · Wing, Plate/Skin
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