Boeing 767-34AF

Service difficulty reports · 6,321

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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 = '76734AF'
  ORDER BY difficulty_date DESC"

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SDR UPS08653415Panel · damagedLEFT INBOARD L/E SLAT CLOSURE PANEL DAMAGED BEYOND LIMITS. REPAIRED NR 6 L/E SLAT CLOSURE PANEL TORN OFF AREA IAW SRM 57-43-01-2R, REPAIR 3 TABLE 1 WET LAYUP 200DF CURE METHOD. SLAT OPERATION TEST SATISFACTORY IAW AMM 27-81-00-05. ACFT OK FOR SERVICE.Oct 1, 2008 · N331UP · Boeing 76734AF · Leading Edge DevicesSDR UPS08653450Bracket · crackedINSPECTION TYPE:N/A RT WING NR 7 SLAT 3EA BRACKET NR 10, 11, 12 FOUND CRACK. CRACK LENGTH .5 INCH APPROX. RT WING NR 7 SLAT 3EA BRACKET NR 10, 11, 12 REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02.Sep 29, 2008 · N330UP · Boeing 76734AF · Leading Edge DevicesSDR UPS08653429Web · crackedINSPECTION TYPE:C RT WING FRONT SPAR AREA LES 680 D-NOSE WEB FOUND CRACK (CRACK LENGTH .5 INCH). D-NOSE WEB REPAIRED AS PER SRM 57-41-13-2R3 FIG 201 REPAIR 3.Sep 29, 2008 · N330UP · Boeing 76734AF · Wing Miscellaneous StructureSDR UPS08653449Bracket · crackedINSPECTION TYPE:N/A LT WING NR 6 SLAT INNER LOWER NR 5 AND NR 8 BRACKET FOUND CRACK 2EA CRACK LENGTH .5 INCH APPROX. TWO BRACKETS REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02.Sep 27, 2008 · N330UP · Boeing 76734AF · Leading Edge DevicesSDR UPS08653455Support Bracket · crackedINSPECTION TYPE:N/A EMP - JACKSCREW COMPARTMENT RT STA 1767.25 (STR 22) SUPPORT BRACKET FOUND CRACK. CRACK LENGTH .5 INCH APPROX. SUPPORT BRACKET REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02.Sep 26, 2008 · N330UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR UPS08653453Stiffener · crackedINSPECTION TYPE:N/A CABIN STA 240 LBL 25 FLOORBEAM ATT STIFFENER CRACKED. CRACK LENGTH 1 INCH. DEFECTIVE STIFFENER REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02.Sep 26, 2008 · N330UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR UPS08653452Stiffener · crackedINSPECTION TYPE:N/A CABIN STA 246 RBL 10 FLOORBEAM ATT STIFFENER CRACKED. CRACK LENGTH 1 INCH. DEFECTIVE STIFFENER REPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02.Sep 26, 2008 · N330UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR UPS08653451Stiffener · crackedINSPECTION TYPE:N/A CABIN STA 246 LBL 50 FLOORBEAM ATT STIFFENER CRACKED. CRACK LENGTH 1 INCH. DEFECTIVE STIFFENER REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02.Sep 26, 2008 · N330UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR UPS08653448Hinge Fitting · crackedINSPECTION TYPE:N/A LT WING I/B MAIN FLAP AFT FLAP I/B SUPPORT FITTING FOUND CRACK. CRACK LENGTH .5 INCH APPROX. HINGE FITTING REPAIRED AS PER SRM 57-53-02-2R1 FIG 201.Sep 26, 2008 · N330UP · Boeing 76734AF · Trailing Edge FlapsSDR UPS08653454Floor Support · crackedINSPECTION TYPE:N/A AFT CARGO COMPT STA 1324 FLOOR SUPPORT BEAM UPPER WEB FOUND CRACKED. CRACK LENGTH 1 INCH APPROX. FLOOR SUPPORT BEAM UPPER WEB REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02.Sep 25, 2008 · N330UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR UPS08653456Skin · gougedINSPECTION TYPE:N/A DMID383810 - RT WING L/E SKIN GOUGE TEMP REPAIR I/B NR 2 ENG ABOVE KRUEGER FLAP. RT WING L/E SKIN AT BETWEEN ISS337.6-345.5 AREA SKIN REPAIRED AS PER RS R57-41-36117 & UPS EO B767-5730-30466-A.Sep 24, 2008 · N330UP · Boeing 76734AF · Wing, Plate/SkinSDR UPS08653430Bracket · crackedINSPECTION TYPE:C AFT CARGO COMPT STA 1087 RBL 25 UNDER FLOOR BRACKET FOUND CRACK (CRACK LENGTH 1 INCH). BRACKET REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02.Sep 24, 2008 · N330UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR UPS08653344Support Bracket · crackedINSPECTION TYPE:C LT WING NR 6 SLAT LWR LIP NR 5, 7 & 8 SUPPORT BRACKET CRACK (CRACK LENGTH .5 INCH). THREE EA SUPPORT BRACKET REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02.Sep 14, 2008 · N332UP · Boeing 76734AF · Wing Miscellaneous StructureSDR UPS08653343Stiffener · crackedINSPECTION TYPE:C MEC CABIN FLOORBEAM STA 246 LBL 20 VERT STIFFENER CRACK (CRACK LENGTH 1 INCH). VERT STIFFENER REPLACED AS PER SRM 53-10-51-2R FIG 201 REPAIR 3. UPS MPI P19868 RAISED FOR REPEAT DVI AT 3000 CYCLES OR 24 MONTHS WHICHEVER COMES FIRST.Sep 14, 2008 · N332UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR UPS08653329Unknown · noisyINSPECTION TYPE:N/A 30 SECS AFTER GEAR RETRACTION THERE WAS A NOISE UNDER C/P SIMILAR TO A COMPRESSOR STALL WITH NO OTHER INDICATIONS. DURING DESCENT FROM FL 390 PASSING FL 390 PASSING FL 250 SAME SOUND WAS HEARD THROTTLES AT IDLE. CREW REQUESTED EMERGENCY ESep 14, 2008 · N324UP · Boeing 76734AF · Nose/Tail Landing GearSDR UPS08653345Stiffener · crackedINSPECTION TYPE:C MEC CABIN FLOORBEAM STA 246 LBL 55 VERTICAL STIFFENER FOUND CRACK (CRACK LENGTH 1 INCH). VERT STIFFENER REPLACED AS PER SRM 53-10-51-2R FIG 201 REPAIR 3 UPS MPI P19867 RAISED FOR REPEAT DVI AT 3000 CYC OR 24 MONTHS, WHICHEVER COMES FIRST.Sep 13, 2008 · N332UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR UPS08653313Window · delaminatedINSPECTION TYPE:N/A DIVERSION - R2 WINDOW HAS DELAMINATION APPROX 3 INCHES HIGH COVERING THE LOWER FORWARD HALF OF THE WINDOW. SLIGHT DISTORTION OF VIEW. DISCOVERED AFTER AIRBORNE. REVISED AND REPLACED R2 WINDOW ASSY AS REQ'D PER 50-11-02-40. OPS AND LEAK Sep 11, 2008 · N312UP · Boeing 76734AF · Flight Compartment WindowsSDR UPS08653308Bracket · crackedINSPECTION TYPE:N/A R2 WINDOW CARRIAGE ASSEMBLY BRACKET CRACKED. REMOVED AND REPLACED BALL SCREW ASSEMBLY AND CARRIAGE ASSEMBLY PER MM 56-11-04-4.Sep 9, 2008 · N306UP · Boeing 76734AF · Flight Compartment WindowsSDR UPS08653245Seat Track · wornINSPECTION TYPE:C M/D STA 754 RBL 11 SEAT TRACK CROWN WORN. M/D - CARGO TRACK SECTIONAL REPLACED FROM STA 709 TO STA 785 RBL 11 AND REPAIRED AS PER SRM 53-00-52-2R REPAIR 9 FIG 201.Aug 24, 2008 · N320UP · Boeing 76734AF · Fuselage, Seat/Cargo Attach FittingsSDR UPS08653243Stiffener · crackedINSPECTION TYPE:C FX- INTERNAL AREA STA 246 LBL 50 CABIN FLOORBEAM ATTACHMENT STIFFENER FOUND CRACK. CRACK LENGTH 0.75 INCH. FX- STA 246 LBL 50 CABIN FLOORBEAM ATTACHMENT STIFFENER REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02.Aug 21, 2008 · N320UP · Boeing 76734AF · Fuselage Main, Attach FittingsSDR UPS08653109Floorbeam · crackedINSPECTION TYPE:C FX - CABIN FLOORBEAM ATTACHMENT STIFFENER AT STA 246 LBL 50 FOUND CRACK. CRACK LENGTH 0.75 INCH. FX CABIN FLOORBEAM STA 246 LBL 50 ATTACHMENT STIFFENER WAS REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02.Aug 10, 2008 · N334UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR UPS08653110Beam · crackedINSPECTION TYPE:C LT WING LES 674 'D' NOSE SUPPORT WEB LOWER FLANGE FOUND CRACKED. CRACK LENGTH 1.125 INCH. LT WING LES 674 'D' NOSE SUPPORT WEB LOWER FLANGE REPAIRED AS PER SRM 57-41-13-2R REPAIR 3 FIG 201.Aug 8, 2008 · N334UP · Boeing 76734AF · Wing Main, Frame StructureSDR UPS08652984Engine · bird ingestionINSPECTION TYPE-ETOP ATB - ON TAKEOFF UPS 232 INGESTED A BIRD TO THE LT ENGINE CAUSING VIBRATION. THE CREW DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. THEY DID NOT SHUT DOWN THE ENGINE. COMPLETE FAN BLADE SET REPLACED IAW AMM 72-31-02-4. ENGINE VIB CHEAug 2, 2008 · N303UP · Boeing 76734AF · Engine (Turbine/Turboprop)SDR UPS08652951Pseu · faulted2ND ATB - LE FLAP ASSYMETRY. REF FIM 27-81-00 FIG 107 PSEU FAULTED S280. INSPECTED TARGET AND AFFECTED SLAT. NO DAMAGE FOUND. CLEARANCE WITHIN LIMITS AT .111 INCH. TESTED INDUCTANCE IAW FIM 32-09-03 FIG 108. FOUND S280 OUT OF LIMITS READING 5.8 MILLIHENRYS. RJul 31, 2008 · N306UP · Boeing 76734AF · Leading Edge Slat Control SystemSDR UPS08652923Indicator · malfunctionedATB - RECEIVED MESSAGE AND FLAP INDICATOR SHOWED LE FLAPS NOT UP. RAN CHECKLISTS. REMOVED AND REPLACED IAW 27-58-02-4 FLAP POSITION INDICATOR OPERATION CHECKED SATISFACTORY IAW 27-58-00-5.Jul 31, 2008 · N306UP · Boeing 76734AF · Leading Edge Slat Position Indicating SystemSDR UPS08652869Web · crackedRT WING L/E NOSE BEAM LOWER SUPPORT WEB FOUND CRACKED AT ILS 676 (CRACK LENGTH 1.25") RT WING L/E NOSE BEAM SUPPORT WEB REPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02 JUST BETWEEN OSS 648 AND OSS 694.Jul 17, 2008 · N303UP · Boeing 76734AF · Wing Miscellaneous StructureSDR UPS08652871Stiffener · crackedINSPECTION TYPE:C FX MEC STA 246 LBL 50" FLOORBEAM SUPPORT STIFFENER CRACKED (CRACK LENGTH .5" APPROX) FX MEC STA 246 LBL 50" FLOORBEAM SUPPORT STIFFENER REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02Jul 16, 2008 · N303UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR UPS08652870Stiffener · crackedINSPECTION TYPE-C, MEC STA 246 LBL 25" FLOORBEAM SUPPORT STIFFENER CRACKED (CRACK LENGTH .3750" APPROX). FX MEC STA 246 LBL 25" FLOORBEAM SUPPORT STIFFENER REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02.Jul 16, 2008 · N303UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR UPS08652866Skin · crackedNR 2 PYLON LT MOST FWD PYLON STRUT ACCESS CUTOUT CRACKED AT AFT UPPER CORNER (CRACK LENGTH 1" APPROX). NR2 PYLON LT MOST FWD PYLON STRUT ACCESS CUTOUT AFT UPPER CORNER SKIN REPAIRED IAW HX RS NR R54-51-36029 AND UPS EO NR B767-5430- 30063-A.Jul 16, 2008 · N303UP · Boeing 76734AF · Nacelle/Pylon, Plate/SkinSDR UPS08652862Stiffener · crackedFX MEC STA 246 LBL 40", FLOORBEAM SUPPORT STIFFENER CRACK. (CRACK LENGTH 1/2" APPROX). FX MEC STA 246 LBL 40" FLOORBEAM SUPPORT STIFFENER REPAIR AS IAW SRM 53-10-51-2R 4 FIG 201 THIS REPAIR IS A CATEGORY 'B' REPAIR. REPEAT INSPECTION IS REQUIRED IAW SRM 53-1Jul 16, 2008 · N303UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR UPS08652868Web · crackedLT WING L/E STA 525 FWD NOSE BEAM WEB LT WING AREA CRACK. (CRACK LENGTH .7500" APPROX). LT WING L/E FWD NOSE BEAM WEB REPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02 JUST BETWEEN OSS 499.6, AND OSS 565.9 REF HX NRC NR 50462 FOR WORKING DETAIL.Jul 15, 2008 · N303UP · Boeing 76734AF · Wing Miscellaneous StructureSDR UPS08652867Web · crackedLT WING L/E STA 504 FWD NOSE BEAM WEB LWR AREA CRACK (CRACK LENGTH 1" APPROX). LT WING L/E FWD NOSE BEAM WEB REPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02 JUST BETWEEN OSS 499.6 AND OSS 565.9.Jul 15, 2008 · N303UP · Boeing 76734AF · Wing Miscellaneous StructureSDR UPS08652673Sign · unknownEMERGENCY LIGHT ASSY REMOVED FROM CREW ENTRY DOOR HANDLE PANEL. REINSTALLED EMERGENCY EXIT SIGN AND OPS CHECK NORMAL.Jul 7, 2008 · N305UP · Boeing 76734AF · Emergency LightingSDR UPS08652642Panel · damagedL1 DOOR SIDE BUMPER AND SIDE PANEL DAMAGED. REMOVED INTERIOR PANEL FOR CREW ENTRY DOOR HANDLE AND SENT TO SM. REPAIRED SIDEWALL PANEL REF 767 AMM 25 00 00 08.Jul 7, 2008 · N305UP · Boeing 76734AF · Passenger/Crew DoorsSDR UPS08652726Skin · dentedINSPECTION TYPE-C, FX RT UPPER FUSELAGE BS 559 S4R SKIN EXTERNAL SURFACE DENT TO REPAIRED PATCH AREA. BS 553 TO 568 S3-4R TO S6R AREA APPROX SKIN REPAIRED IAW RS R53-31-36027. THIS REPAIR CLASSIFY AS CAT B WITH THE ADDITIONAL INSPECTION IAW RS R53-31-36027 AJul 2, 2008 · N301UP · Boeing 76734AF · Fuselage Main, Plate/SkinSDR UPS08652725Angle · crackedINSPECTION TYPE-C, AFT CARGO COMPT BS 1085 LBL 26 UNDER FLOOR CHORD ANGLE CRACK. CRACK LENGTH .6250", AFT CARGO COMPT BS 1085 LBL 26 UNDER FLOOR CHORD ANGLE REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02.Jul 2, 2008 · N301UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR UPS08652724Angle · crackedINSPECTION TYPE-C, AFT CARGO COMPT BS 1085 RBL 26 UNDER FLOOR CHORD ANGLE CRACK. CRACK LENGTH .7500", AFT CARGO COMPT STA1085 RBL26 UNDER FLOOR CHORD ANGLE REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02.Jul 2, 2008 · N301UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR UPS08652669Floor Support · crackedAFT OF BULK CARGO COMPT STA 1581 LBL 75 MAIN DECK FLOOR SUPPORT ATTACH SPLICE DAMAGED. (CRACK LENGTH 1" APPROX) AFT OF BULK CARGO COMPT BS 1581 LBL 75 FLOOR SUPPORT ATTACHMENT SPLICE REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02 AT MAIN DECK AREA.Jul 2, 2008 · N301UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR UPS08652668Web · crackedLT WING OSS 664 & 679 NOSE BEAM WEB LOWER AREA FOUND CRACKED. (CRACK LENGTH 2" & 3") LHW AT OSS 648 TO OSS 694 L/E NOSE BEAM SUPPORT WEB REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02.Jul 1, 2008 · N301UP · Boeing 76734AF · Leading Edge DevicesSDR UPS08652667Web · crackedRT WING L/E OSS 664 NOSE BEAM SUPPORT BEAM LOWER AREA FOUND CRACKED (CRACK LENGTH .7500"). RHW AT OSS 648 TO OSS 694 L/E NOSE BEAM SUPPORT WEB REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02.Jul 1, 2008 · N301UP · Boeing 76734AF · Leading Edge DevicesSDR UPS08652666Web · crackedRT WING L/E OSS 695 NOSE BEAM SUPPORT WEB LWR AREA FOUND CRACKED. (CRACK LENGTH 1" APPROX ) RHW AT OSS 694 TO OSS 717 L/E NOSE BEAM SUPPORT WEB REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02.Jul 1, 2008 · N301UP · Boeing 76734AF · Leading Edge DevicesSDR UPS08652624Module · malfunctionedRUDDER TRIM STUCK AT 4 UNITS. T/S IAW FIM 27-21-00 FIG 106 FOUND RUDDER TRIM CONTROL PANEL FAULT. R/R AILERON AND RUDDER TRIM CONTROL MODULE IAW MM 27-21-23-2. OPS GOOD.Jul 1, 2008 · N314UP · Boeing 76734AF · Rudder Tab Control SystemSDR UPS08652604Power Supply · dischargedINSPECTION TYPE:PS1 EMERGENCY LIGHTS ARE INOP WITH NO PWR. REMOVED AND REPLACED PWR SUPPLY UNIT IAW MM 33-51-07-2, SYSTEM OPS CHECKS NORMAL.Jun 27, 2008 · N312UP · Boeing 76734AF · Emergency LightingSDR UPS08652605Bracket · crackedINSPECTION TYPE:AD NOSE LANDING GEAR WHEEL WELL RT SENSOR BRACKET CRACK. CRACK LENGTH .375 INCH. NOSE LANDING GEAR WHEEL WELL RT SENSOR SUPPORT BRACKET REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02.Jun 23, 2008 · N325UP · Boeing 76734AF · Landing Gear Position and WarningSDR UPS08652440Cap · crackedINSPECTION TYPE:N/A RIGHT WING O/B FLAP LEADING EDGE CAP CRACKED.Jun 9, 2008 · N305UP · Boeing 76734AF · Trailing Edge FlapsSDR UPS08652424Brake · fireINSPECTION TYPE:N/A, NR 1 BRAKE FIRE ON ARRIVAL, FUSE PLUGS MELTED. CFR WAS CALLED DUE TO FIRE.Jun 4, 2008 · N323UP · Boeing 76734AF · BrakeSDR UPS08652394Fuel Sys · leakingINSPECTION TYPE:ETOP DIVERSION, FUEL DISCREPANCY WITH ASSOCIATED INSUFFICIENT FUEL LEAK.May 30, 2008 · N311UP · Boeing 76734AF · Fuel StorageSDR UPS08652348Thermal Switch · inoperativeINSPECTION TYPE:ETOP ATB - DUCT LEAK LIGHT ILLUM. EICAS MSG: LEFT BLEED DUCT LEAK DISPLAYED. FUEL DUMPED. REPLACED M691 CONTROL CARD PER MM 26-10-01-4. REPLACED S236 THERMAL SWITCH PER MM 26-18-01-4. REMOVED AND REPLACED S237 THERMAL SWITCH PER MM 26-18-May 25, 2008 · N319UP · Boeing 76734AF · Overheat DetectionSDR UPS08652342Web · crackedINSPECTION TYPE:N/A LEFT WING LES 694 FWD D-NOSE FAIRING SUPPORT WEB LOWER AREA FOUND CRACKED. CRACK LENGTH 2.5 INCHES APPROX. LEFT WING FWD D-NOSE FAIRING SUPPORT WEB REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02, JUST BETWEEN OSS648 AND 694 AREA.May 24, 2008 · N302UP · Boeing 76734AF · Wing Miscellaneous StructureSDR UPS08652341Web · crackedINSPECTION TYPE:N/A LEFT WING LES 675 FWD OF REFUEL PANEL LOWER CHORD FOUND CRACK. LEFT WING FWD D-NOSE FAIRING SUPPORT WEB REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02, JUST BETWEEN OSS648 AND 694 REFER NRC50623 FOR WORKING DETAIL.May 24, 2008 · N302UP · Boeing 76734AF · Wing Miscellaneous Structure
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