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 DALA2016072805624Bracket · brokenLOUD VIBERATION UNDER SEAT 20B. FOUND SUPPORT BRACKET FOR OVERWING TO BODY FAIRING BROKEN BELOW AFT OVERWING EXIT DOOR. FABRICATED AND REPLACED THE BRACKET IAW DRAWING 5971068.Jul 27, 2016 · N956AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016072705623Switch · intermittentTHE PILOT REPORTED THAT SOME OF THE EMERGENCY LIGHTS IN THE AIRCRAFT HAD ILLUMINATED UNCOMMANDED. MAINTENANCE REPLACED AN INTERMITTENT EMERGENCY LIGHT SWITCH S1-177 IN THE COCKPIT AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.Jul 27, 2016 · N989DN · Boeing 717200 · Emergency LightingSDR DALA2016072805622Structure · crackedCRACK ON INTERIOR STRUCTURE OF THE FWD CARGO DOOR LWR AFT AREA. REPAIRED IAW OVERHAUL MANUAL 52-30-1.Jul 27, 2016 · N906AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2016072805620Angle · corrodedCORROSION FOUND ON CUSP WEB ANGLE IN BOTH FWD AND AFT LOWER CORNERS OF GALLEY SERVICE DOOR. REPAIRED THE ANGLE IAW SRM 53-00-55 REPAIR 3.Jul 27, 2016 · N910AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016072705588Light · malfunctionedTHE F/A REPORTED THAT THE EEPL AT THE LOWER SIDEWALL OVERWING AND THE TAIL EXIT LIGHTS HAD ILLUMINATED UNCOMMANDED DURING FLIGHT. MAINTENANCE CYCLED THE EEPL SWITCH IN THE COCKPIT AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.Jul 26, 2016 · N989DN · Boeing 717200 · Emergency LightingSDR DALA2016072705587Pan · corrodedFWD CARGO DOOR JAMB LOWER PAN IS CORRODED AT STOPS, MARKED. REPLACED FWD LOWER CARGO DOOR JAMB PAN SECTION WITH PAN SECTION IAW SRM 51-20-15, REPAIR 6, FIG 201. APPLIED LOG DECAL IAW DPS 900-5-1, NR 04.Jul 26, 2016 · N910AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016072605548Control Unit · faultyCREW DIVERTED THE ACFT TO RDU WITH THE NR 1 ENGINE SHUTDOWN FOLLOWING A FIRE WARNING INDICATION. DURING CRUISE AT FL330, THE EAD DISPLAYED NR 1 ENGINE FIRE AND IT WAS ACCOMPANIED BY THE AUDIBLE ALERT. CREW STATES THAT THE NR 1 ENGINE FIRE HANDLE WAS NOT ILLUJul 26, 2016 · N936AT · Boeing 717200 · Fire DetectionSDR DALA2016072805621Seat Track · corrodedRIGHT SEAT TRACK RBL 56 BS 200 AND END FITTING CORRODED. FABRICATED NEW SECTION OF SEAT TRACK IAW SRM 51-40-08 AND DWG 5971185.Jul 25, 2016 · N910AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016072605547Cusp Web · corrodedWEB AT BS 160-200 RBL 56 CORRODED BEYOND LIMITS. REPLACED THE WEB IAW ER/A 547495-14. A NEW CUSP WEB AND SPLICE DOUBLER WERE FABRICATED IAW ER/A 547495-14. THE TRIMMED SECTION WAS CHECKED FOR CRACKS USING HFEC IAW NDTSPM 06-10-01 .001 NO DEFECTS FOUND. ALLJul 25, 2016 · N910AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR HALA2016072500293Interface Unit · malfunctionedDURING TAKEOFF AT APPROX 70 KNTS, TAKE OFF CONFIGURATION WARNING FOR STAB TRIM ENUNCIATED. STAB TRIM WAS SET PROPERLY. PERFORMED CAWS SYSTEM TEST PER FIM 31-51 TASK 802. TEST PASSED. PERFORMED TAKE OFF CONFIGURATION WARNING TEST FOR STAB IAW FIM 31-51 TASK Jul 25, 2016 · N484HA · Boeing 717200 · Stabilizer Control SystemSDR DALA2016080105674Former · crackedRIGHT CANTED KEEL FORMERS AT STA 674, 696, AND 714 CRACKED ON OTBD END. REPAIR IAW ER/A 545683-14MA, REF ORNRC 69946-0100-0130. REMOVED FORMERS ON RT CANTED KEEL AT STA 674, 696, AND 714. FABRICATED AND INSTALLED DOUBLERS AND FILLERS TO FORMERS IAW ER/A 545Jul 24, 2016 · N910AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2016072505501Floor Support · corrodedFLOOR PANEL SUPPORT STRUCTURE STA 215, RBL11 CORRODED. BLENDED CORROSION AND CHECKED LIMITS ON FLOOR PANEL SUPPORT STRUCTURE. NOMINAL THICKNESS IS .080". REMOVED .035", REMAINING IS .045". FOUND OUT OF LIMITS IAW SRM 53-00-00, FIG 103. FABRICATED NEW FLOOJul 24, 2016 · N910AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016072305500Cusp Web · corrodedRIGHT CUSP WEB MEMBRANE, STA 200-218 RBL 56-44. CORRODED BEYOND LIMTS. REPLACED RT CUSP MEMBRANE AT STA 210-218, RBL 56-44 IAW SRM 51-41-02, PAR 2. FABRICATED IAW DWG 9936535. THE NEW PART WAS ALODINED IAW PSM 900-2-4-1, 02. THE WEB WAS THEN PRIMED IAW PJul 21, 2016 · N910AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016072105471Battery · dischargedDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGNS AT THE OVERWING HATCH WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY AND THE OPS CHECK WAS GOOD.Jul 21, 2016 · N998AT · Boeing 717200 · Emergency LightingSDR DALA2016072205470Cargo Track · corrodedRIGHT AFT CARGO SEAT TRACK, AFT OF CARGO DOOR, HAS CORROSION AND CHAFING, MARKED. RIGHT AFT SEAT TRACK CORRODED BEYOND LIMITS. REPLACED SEAT TRACK AND MATCHED DRILL TO SAMPLE IAW SRM 51-40-08.Jul 21, 2016 · N910AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016072105449Seat Track · corrodedRIGHT INBD SEAT TRACK X 22 BS 256-465 HAS THREE NOTED AREAS OF CORROSION. FOUND OUT OF LIMITS IAW SRM 53-20-52 FIG 101. REPAIRED IAW SRM 53-20-52 REPAIR 1 FIG 201.Jul 20, 2016 · N910AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA20160720152Skin · delaminatedDURING NON ROUTINE LINE CHECK, R/H I/B SPOILER FOUND DELAMINATED.Jul 20, 2016 · N965AT · Boeing 717200 · SpoilersSDR DALA2016071805437Support · crackedCRACKED BULKHEAD DIVISOR SUPPORT, STA Y=655, X=22Z=-10 AT FORWARD CARGO COMPARTMENT. BULKHEAD DIVISOR SUPPORT STA Y=655, X=22 Z=-10 WAS REPAIRED WITH ER/A 547883-14, REV ORIGINAL AND ETI-17-16-093. CRACK 0.187" WEIGHT REPAIR, PARTS 0.32LB. ASSOCIATED ER/A 0Jul 18, 2016 · N958AT · Boeing 717200 · Fuselage Main, BulkheadSDR DALA2016071905402Battery · dischargedDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING FOR THE CATWALK IN THE TAIL COMPARTMENT WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY AND CHARGER AND THE OPS CHECK WAS GOOD.Jul 18, 2016 · N895AT · Boeing 717200 · Emergency LightingSDR DALA2016071905399Pan · chafedAFT CABIN DOOR LOWER INTERIOR HAS CHAFE DAMAGE TO DOOR PAN & FRAMEWORK 8" FROM BOTTOM OF DOOR OPPOSITE HINGES. REPAIRED CHAFE DAMAGE TO DOOR PAN & FRAME WORK ON AFT CABIN EXIT DOOR IAW SRM 52-10-02, REPAIR 15.Jul 18, 2016 · N960AT · Boeing 717200 · Passenger/Crew DoorsSDR DALA2016072005438Former · cracked3 FORMERS ON LT SIDE OF FUSELAGE IN CANTED KEEL AREA AT FS 679, FS 694, AND FS 715 ARE CRACKED, MARKED. REPAIRED FORMERS AT FS 679, FS 694, AND FS 715 IAW ER/A 545683-14MA ORIGINAL REVISION.Jul 17, 2016 · N960AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2016071805349Pan · crackedCRACK ON OUTER PAN STA Y=954, BEAM 1 FORWARD EDGE AT AFT CARGO COMPARTMENT DOOR, C2, CARD 11, ZONE 810. PAN WAS REPAIRED IAW ETI-17-16-081 AND ER/A 547860-14, REV ORIGINAL. LONGERON CRACK 0.128".Jul 17, 2016 · N958AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2016071805348Beam · crackedCRACKED BEAM 1 ON FORWARD EDGE OF AFT CARGO COMPARTMENT STA Y=954, REF CARD 11, ZONE 810, CARD 45 ZONE 810. BEAM 1 WAS REPAIRED IAW ETI-17-16-081 REV 2 AND ER/A 547860-14, REV ORIGINAL. LONG CRACK 0.156".Jul 17, 2016 · N958AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016071805347Longeron · corrodedCORROSION ON LONGERON 24R AND LONGERON 24R END CAP FROM STA 1002 AND STA 1022. REPLACED LONGERON 24R F/S 1002-1022 + FWD END CAP IAW SRM 51-40-05, PG 17, NR 8, SRM 51-41-02, PARA D. NOTE 3, FASTENERS FROM F/S 1002-1022 + SHEAR TIE AT F/S 1002-1022 LT OPEN TOJul 17, 2016 · N910AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2016071805346Beam · crackedCRACKED DOOR JAMB BEAM STA Y=47, RT SIDE AT NLG WW. DOOR JAMB BEAM WAS REPAIRED. ER/A 547858-14, REV ORIGINAL.Jul 17, 2016 · N958AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016071705345Fitting · crackedCRACKED CLIP AT STA Y=1152 BETWEEN LONGERONS 3R/2R. CLIP WAS REPLACED IAW ER/A 547861-14 REV ORIGINAL.Jul 17, 2016 · N958AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016071705344Skin · wornWORN RT WING LOWER SKIN BETWEEN STA SXR 69 AND XRS 111.500. REPAIR OF WORN AREA AT RT WING LOWER SKIN WAS PERFORMED WITH ER/A 547869-14, REV ORIGINAL.Jul 17, 2016 · N958AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016071705343Door Frame · corrodedCORROSION ON LOWER DOOR JAMB FROM STA Y=954 TO Y=994 AT AFT CARGO COMPARTMENT, SM, C2, CARD 27, ZONE 810. DUE TO EXCESIVE CORROSION WAS REPLACED IAW SRM 53-20-15, FIG 201, 51-41-05, AND 51-41-02. RII COMPLETED.Jul 16, 2016 · N958AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016071705342Skin · crackedWEAR AND CRACK ON OUTER SKIN STA Y=972 BETWEEN BEAM 1 AND 2 JUST ABOVE OF HANDLE RELEASE AT AFT CARGO COMPARTMENT DOOR. SKIN STA Y=972 BETWEEN BEAM 1 AND 2 JUST ABOVE OF HANDLE RELEASE WAS REPAIRED IAW SRM 52-30-01, FIG 201, LENGTH CRACK 0.300".Jul 16, 2016 · N958AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2016071705341Longeron · corrodedEXCESSIVE CORROSION ON LONGERON 630 BETWEEN STA 960-1010, IN REF CARD 10, ZONE 180. SECTION OF LONGERON WAS REPLACED IAW SRM 53-20-05, REPAIR 1, 51-41-05, 51-40-08, AND 51-10-04, PAR 15, 21, 26, AND 37. RII COMPLETED.Jul 16, 2016 · N958AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2016071805350Battery · dischargedDURING PREFLIGHT CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY PATHWAY LIGHTING FOR THE FIRST CLASS SECTION WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY AND THE OPS CHECK WAS GOOD.Jul 15, 2016 · N945AT · Boeing 717200 · Emergency LightingSDR DALA2016071605340Channel · crackedCRACKED FORWARD CHANNEL STA Y=757 AT RT MLG DOOR LOWER SECTION SM, MLG, CARD 1, ZONE 720. CHANNEL WAS REPAIRED IAW ETI-17-16-077 REV 1 AND ER/A 547857-14, REV ORIGINAL.Jul 15, 2016 · N958AT · Boeing 717200 · Landing Gear DoorsSDR DALA2016071605339Pan · crackedCRACKED PAN BETWEEN BEAM 7/8, STA 161.3 AT FWD ENTRY DOOR, CARD 18, ZONE 820. PAN WAS REPAIRED IAW 717, ETI-17-16-073, REV 1 AND ER/A 547853-14, REV ORIGINAL.Jul 15, 2016 · N958AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016071605338Skin · crackedRIGHT FUSELAGE EXTERIOR SKIN CRACKED AROUND FASTENER HEAD STA 1095 JUST ABOVE LONGERON 14R. REPAIRED RT FUSELAGE EXTERIOR SKIN AT STA 1095 AND LONGERON 14R IAW ER/A 547486-14, ORIGINAL REV ASSOCIATED ER/A 00-547486.Jul 15, 2016 · N960AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016071605336Cusp Web · crackedRT CUSP WEB CRACKED STA 823 BETWEEN 2 RIVETS, RBL 44.5. VIEWED IN LIGHTING HOLE WITH MIRROR. REMOVED DAMAGE, FABRICATED REPAIR DOUBLER IAW SRM 53-00-55, REPAIR NR 4. INSTALLED IAW SRM 51-41-02 AND SRM 53-00-55, REPAIR 4.Jul 15, 2016 · N910AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016071605335Stop Fitting · crackedCRACK ON DOOR STOP FITTING STA, Y=994, BEAM 3 AT AFT CARGO COMPARTMENT DOOR. DOOR STOP FITTING STA Y=994, BEAM 3 AT AFT CARGO COMPARTMENT DOOR WAS REPLACED IAW SRM 51-41-01 AND 51-41-05, IPC 52-33-01-01, FIG 01.Jul 15, 2016 · N958AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2016071605334Angle · crackedCRACK ON ANGLE STA Y=994, INNER SIDE BEAM 3 AT AFT CARGO COMPARTMENT DOOR. CRACKED ANGLE STA Y994 WAS REMOVED AND NEW ANGLE WAS INSTALLED IAW SRM 51-41-05. PARA 8, LONG CRACK 0.35".Jul 15, 2016 · N958AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2016071605333Skin · wornWEAR ON FUSELAGE SKIN IN LONGERON 20RT BETWEEN STA Y=520-526, SM, CARD 27, ZONE 110. DAMAGE WAS REPAIRED IAW ETI-17-16-084, REV 1 AND ER/A 547867-14, REV ORIGINAL. RII COMPLETED.Jul 15, 2016 · N958AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016071605332Skin · wornWEAR ON FUSELAGE SKIN IN LONGERON 21RT BETWEEN STA Y=503-508,SM, CARD 28, ZONE 110. WEAR ON FUSELAGE SKIN IN LONGERON 21RT BETWEEN STA Y=503-508 OUT OF LIMITS. ORIGINAL THICKNESS 0.050" REMAINING THICKNESS 0.035", DAMAGE WAS REPAIRED IAW ETI-17-16-084, REV 1Jul 15, 2016 · N958AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016071505297Power Supply · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE CABIN SERVICE DOOR EMERGENCY LIGHT IN THE CEILING WAS INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY AND THE LIGHT RETURNED TO AN OPERATIONAL CONDITION.Jul 15, 2016 · N972AT · Boeing 717200 · Emergency LightingSDR DALA2016071905400Web · corrodedSTA 1002, HORIZONTAL CLOSEOUT WEB CORRODED NEAR PANEL ATTACH STRUCTURE. BLENDED NOTED AREA IAW SRM 51-10-02, PAR 26, ORIG .040, .026. REMAINING FOUND TO BE OUT OF LIMITS, REPAIRED AREA IAW PRI 547489-14, TAG 6785 AND ER/A 547489-14, TAG 1482284 IAW PRI 547789Jul 14, 2016 · N960AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016071505398Pan · crackedCRACK ON INNER PAN STA Y=427 BEAM 1 AT FWD CARGO COMPARTMENT DOOR, SM, C1, CARD 33, ZONE 810. INNER PAN WAS REPAIRED IAW SRM 52-30-02, REPAIR 1, FIG 1, FIG 201, LONG CRACK 1.312". RII COMPLETED.Jul 14, 2016 · N958AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2016071505296Access Panel · damagedELONGATED HOLE AND TOOL MARKS ON LOWER ACCESS 440 INBD AT RT PYLON SM, E/P, CARD 40, ZONE 000. TOOL MARKS AND ELONGATED HOLE WERE REPAIRED IAW SRM 54-00-00, FIG 201, SRM 51-10-04, PAR 15, 21.Jul 14, 2016 · N958AT · Boeing 717200 · Nacelle/Pylon, Plate/SkinSDR DALA2016071505295Angle · corrodedCUSP WEB ANGLE CORRODED IN BOTH FWD AND AFT CORNERS ON RT GALLEY SERVICE DOOR. REPAIRED CUSP WEB ANGLE IAW SRM 53-00-55, REP 3.Jul 14, 2016 · N960AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016071505294Access Panel · corrodedCORROSION ON FUEL ACCESS PLATE 520JB COUNTERSINK. 2EA IN REF ORNRC 64, ACFT ZONE 000, CARD 110, ZONE 000, CORROSION WAS REMOVED IAW SRM 54-10-01, COUNTERSINK WERE MEASURED WITH 0.610", 0.607", AND 0.610". ADJACENT HOLES THEREFORE IS OUT OF LIMITS IAW SRM 57-Jul 14, 2016 · N958AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016071505293Intercostal · crackedCRACKED INTERCOSTAL BETWEEN Y=617 TO Y=636 X=0 AT CEILING AREA OF FWD CARGO COMPARTMENT. C1, SM, CARD 26, ZONE 120 CRACK ON INTERCOSTAL WAS REPAIRED IAW SRM 53-00-00, FIG 201, CRACK LENGTH 1.093".Jul 14, 2016 · N958AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016071505292Longeron · corrodedEXCESSIVE CORROSION ON LONGERON 30 BETWEEN STA 218 TO 237 AT FWD CARGO COMPARTMENT IN REF CARD 15, ZONE 120, CARD 45, ZONE 120. DUE TO EXCESSIVE DAMAGED SECTION OF LONGERON 30 BETWEEN STA 150 TO 227 WAS REPLACED IAW SRM 53-10-05, 51-41-02, AND 51-41-05.Jul 14, 2016 · N958AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR HALA2016071400273Adiru · failedAFTER TAKE OFF, IAS-AMBER, NO COMMAND BARS ON PFD, AUTOPILOT INOPERATIVE, RUDDER LIMITER RESTRICTED, RUDDER LIMITER FAILED. REPLACED NR 1 ADIRU PER FIM 34-16- TASK 801. TESTED OK IAW 34-43-00. RTS OK IAW AMM 22-00-00-741-811. LEAK TEST OF PITOT SYSTEM OK IAJul 14, 2016 · N484HA · Boeing 717200 · Outside Air Temperature Indicator/SensorSDR DALA2017010500099Access Panel · corrodedCORROSION ON FUEL ACCESS PLATE 620PB COUNTERSINK. (2EA) CORROSION ON FUEL ACCESS PLATE 620PB COUNTERSINK WAS REMOVED AND MEASURE AND FOUND TWO HOLES OUT OF LIMITS .608" AND .613". THEREFORE WERE REPAIRED WITH BUSHINGS PER SRM 57-10-01.Jul 13, 2016 · N958AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2017010500098Access Panel · corrodedCORROSION ON FUEL ACCESS PLATE 520GB COUNTERSINK. (2EA) CORROSION ON FUEL ACCESS PLATE 520GB COUNTERSINK WAS REMOVED AND MEASURE AND FOUND TWO HOLES OUT OF LIMITS .603" AND .606". THEREFORE WAS REPAIRED WITH BUSHINGS PER SRM 57-10-01.Jul 13, 2016 · N958AT · Boeing 717200 · Wing, Plate/Skin
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