Boeing 767-316F

Service difficulty reports · 116

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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 = '767316F'
  ORDER BY difficulty_date DESC"

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SDR UIEA2017090601606Plate · wornNR 1 NACELLE PRESSURE RELIEF DOOR CUT OUT HAD TWO STRIKER PLATES WORN. THE STRIKER PLATES WERE REMOVED AND REPLACED IAW SRM 51-40-02, REV, 29.Oct 8, 2017 · N1381A · Boeing 767316F · Nacelle/Pylon, Main FrameSDR UIEA2017090601607Stringer · crackedFASTENER HOLE FOUND CRACKED AT BS 1548, ON STRINGER 3L. REPAIRED IAW 1162-17 REV -.Oct 8, 2017 · N1381A · Boeing 767316F · Fuselage Main, Longeron/StringerSDR UIEA2017090601610Channel · crackedNR 2 NACELLE AFT HAT CHANNEL FOUND CRACKED AND EXISTING REPAIR DOUBLER WORN. THE HAT CHANNEL WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 29.Oct 8, 2017 · N1381A · Boeing 767316F · Nacelle/Pylon Miscellaneous StructureSDR UIEA2017090701611Skin · scratchedNR 1 NACELLE SKIN FOUND SCRATCHED. THE SCRATCHES WERE REMOVED AND FOUND WITHIN LIMITS IAW SRM 54-42-01-1A-1, FIGURE 101, DETAIL III, REV 29.Oct 8, 2017 · N1381A · Boeing 767316F · Nacelle/Pylon, Plate/SkinSDR UIEA2017090701612Skin · scratchedNR 1 SKIN SKIN FOUND SCRATCHED. THE SCRATCHES WERE REMOVED AND FOUND WITHIN LIMITS IAW SRM 54-42-01-1A-1, FIGURE 101, DETAIL III, REV 29.Oct 8, 2017 · N1381A · Boeing 767316F · Nacelle/Pylon, Plate/SkinSDR UIEA2017090701613Skin · scratchedNR 2 NACELLE SKIN FOUND SCRATCHED. THE SCRATCHES WERE REMOVED AND FOUND WITHIN LIMITS IAW SRM 54-42-01-1A-1, FIGURE 101, DETAIL III, REV 29.Oct 8, 2017 · N1381A · Boeing 767316F · Nacelle/Pylon, Plate/SkinSDR UIEA2017090701614Skin · scratchedNR 2 NACELLE, RT CORE COWL SKIN FOUND SCRATCHED. SCRATCHES REMOVED AND FOUND WITHIN LIMITS IAW SRM 54-42-01-1A-1, FIGURE 101. DETAIL III, REV 29.Oct 8, 2017 · N1381A · Boeing 767316F · Nacelle/Pylon, Plate/SkinSDR UIEA2017090701615Stiffener · crackedA CRACK WAS FOUND APPROXIMATELY .5 INCHES IN LENGTH FOUND DURING HFEC INSPECTION ON THE BS 287, LBL 25 NOSE WHEEL WELL BULKHEAD VERTICAL STRUCTURE. THE BULKHEAD VERTICAL STIFFENERS WERE REPAIRED IAW SRM 51-70-12-0G-0, FIGURE 1, REV 29.Oct 8, 2017 · N1381A · Boeing 767316F · Fuselage Main, BulkheadSDR UIEA2017090801616Rub Strip · wornNR 1 NACELLE, LT CORE COWL INTERIOR SURFACE UPPER AFT EDGE WEAR STRIP FOUND WORN. THE WEAR STRIP WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 29.Oct 8, 2017 · N1381A · Boeing 767316F · Nacelle/Pylon, Main FrameSDR UIEA2017090801617Rub Strip · wornNR 2 NACELLE LT CORE COWL INTERIOR SURFACE UPPER AFT EDGE WEAR STRIP FOUND WORN. WEAR STRIP WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 29.Oct 8, 2017 · N1381A · Boeing 767316F · Nacelle/Pylon Miscellaneous StructureSDR UIEA2017090801618Frame · damagedNR 2 NACELLE COWL FWD FRAME FOUND WITH A FASTENER HOLE ELONGATED, AT THE HOLD OPEN ROD END BRACKET ATTACH. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 29.Oct 8, 2017 · N1381A · Boeing 767316F · Nacelle/Pylon, Main FrameSDR UIEA2017090801619Tee Fitting · brokenNR 2 ENGINE, LT CORE COWL MOST AFT HAT CHANNEL LOWER ATTACH TEE FOUND BROKEN. THE TEE FITTING WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 29.Oct 8, 2017 · N1381A · Boeing 767316F · Nacelle/Pylon, Attach FittingsSDR UIEA2017091101628Rod · wornNR 2 ENGINE RT CORE COWL HOLD OPEN ROD FOUND WORN. THE HOLD OPEN ROD WAS REMOVED AND REPLACED IAW AMM 70-50-00, REV 122.Oct 8, 2017 · N1381A · Boeing 767316F · Nacelle/Pylon, Main FrameSDR UIEA2017091101629Rod · wornNR 1 ENGINE LT CORE COWL HOLD OPEN ROD FOUND WORN. THE HOLD OPEN ROD WAS REMOVED AND REPLACED IAW AMM 70-50-00, REV 122.Oct 8, 2017 · N1381A · Boeing 767316F · Nacelle/Pylon, Main FrameSDR UIEA2017091101635Failsafe · crackedCRACK INDICATION FOUND DURING AN ULTRASONIC INSPECTION ON THE FAILSAFE STRAP OF THE REAR SPAR BULKHEAD AT BS 955. THE FAILSAFE STRAP WAS REPAIRED IAW EN1147-17, REV -.Oct 8, 2017 · N1381A · Boeing 767316F · Fuselage Main, StructureSDR UIEA2017091401650Frame · crackedCRACK FOUND APPROXIMATELY 0.6 INCH IN LENGTH, FOUND DURING HFEC INSPECTION ON THE BS 903.5 LBL 89, BELOW WL 200 FRAME INNER TRANSITION RADIUS. REPAIRED I.AW SB767-53A0209, REV.Oct 8, 2017 · N1381A · Boeing 767316F · Fuselage Main, FrameSDR UIEA2017091401651Frame · crackedCRACK FOUND APPROXIMATELY 0.55 INCH IN LENGTH, DURING HFEC INSPECTION ON THE BS 903.5, RBL 89, BELOW WL 200 FRAME. THE FRAME WAS REPAIRED IAW 53A0209, REV.Oct 8, 2017 · N1381A · Boeing 767316F · Fuselage Main, FrameSDR UIEA2017091901701Seal · tornNR 1 ENGINE, RT FAN COWL LOWER AREA SEALS FOUND TORN. THE SEALS WERE REPLACED IAW AMM 70-50-00, REV 121.Oct 8, 2017 · N1381A · Boeing 767316F · Nacelle/Pylon, Main FrameSDR UIEA2017091901702Pin · wornNR 1 ENGINE, LEFT CORE COWL HOLD OPEN ROD STOW PIN ADAPTER FOUND WORN. THE STOWAGE PIN WAS REPLACED IAW AMM 20-11-00, REV 121.Oct 8, 2017 · N1381A · Boeing 767316F · Nacelle/Pylon, Main FrameSDR UIEA2017091901704Seal · tornNR 2 ENGINE RT FAN COWL LOWER SEAL FOUND TORN. THE SEAL WAS REPLACED IAW AMM 20-11-00, REV 121.Oct 8, 2017 · N1381A · Boeing 767316F · Nacelle/Pylon, Main FrameSDR UIEA2017091901705Check Valve · damagedLEFT ISOLATION BYPASS CHECK VALVE HOUSING FOUND CHAFED, AND FLAPPER LOOSE. THE CHECK VALVE WAS REMOVED, REPLACED AND TESTED IAW AMM 36-11-05, REV 122. FOUND SATISFACTORY.Oct 8, 2017 · N1381A · Boeing 767316F · Pneumatic Distribution SystemSDR UIEA2017091901707Check Valve · chafedRT ISOLATION BYPASS CHECK VALVE INTERNAL, FOUND THE HOUSING CHAFED AND FLAPPER LOOSE. THE ISOLATION BYPASS CHECK VALVE WAS REMOVED, REPLACED, AND TESTED IAW AMM 36-11-05, REV 122, FOUND SATISFACTORY.Oct 8, 2017 · N1381A · Boeing 767316F · Pneumatic Distribution SystemSDR UIEA2017091901708Fastener · looseFWD CARGO BAY, LT E & E COOLING DUCT SUPPORT BRACKETS AT BS 368 - 390 FOUND FASTENERS LOOSE. THE FASTENERS WERE REMOVED AND NEW FASTENERS INSTALLED IAW SRM 51-40-02, REV 29.Oct 8, 2017 · N1381A · Boeing 767316F · Fuselage Miscellaneous StructureSDR UIEA2017091901710Duct · damagedFWD CARGO BAY, LT & RT E & E COOLING DUCTINGS FOUND DAMAGED. THE DUCT WAS REPAIRED IAW AMM 21-23-07, REV 121.Oct 8, 2017 · N1381A · Boeing 767316F · Air Distribution SystemSDR UIEA2017091901711Bearing · looseNR 1 NACELLE RT CORE COWL HOLD OPEN ROD , ROD END BEARING FOUND LOOSE. ROD END BEARING REPLACED IAW AMM 70-50-00, REV 121.Oct 8, 2017 · N1381A · Boeing 767316F · Nacelle/Pylon, Main FrameSDR UIEA2017091901712Fastener · looseFWD CARGO BAY, LT E & E COOLING DUCT SUPPORTS BRACKETS AT BS 368 - 390, FASTENERS FOUND LOOSE. FASTENERS REMOVED AND NEW FASTENERS INSTALLED IAW SRM 51-40-02, REV 29.Oct 8, 2017 · N1381A · Boeing 767316F · Fuselage Miscellaneous StructureSDR UIEA2017091901714Bearing · looseNR 2 ENGINE LT CORE COWL HOLD OPEN ROD , ROD END BEARING FOUND LOOSE. THE ROD END BEARING WAS REPLACED IAW AMM 70-50-00, REV 121.Oct 8, 2017 · N1381A · Boeing 767316F · Nacelle/Pylon, Main FrameSDR UIEA2017092201770Frame · crackedCRACK FOUND APPROX 1.5 INCHES IN LENGTH. FOUND DURING HFEC INSPECTION ON FWD OUTER FRAME, BS 1809.5 BULKHEAD OUTER FRAME. REPAIR CARRIED OUT IAW SB53A0078 FIG 7 AND EO6753A019.Oct 8, 2017 · N1381A · Boeing 767316F · Fuselage Main, FrameSDR UIEA2017092401808Sleeve · tornFWD CARGO BAY, E/E COOLING DUCT FLEX SLEEVE AT BS 412 - 434 FOUND TORN. THE DUCT FLEX SLEEVE WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 29.Oct 8, 2017 · N1381A · Boeing 767316F · Air Distribution SystemSDR UIEA2017092501859Support Rod · damagedFWD CARGO BAY, E/E COOLING SUPPORT ROD FOUND DAMAGED. THE SUPPORT ROD WAS REMOVED & REPLACED IAW AMM 20-11-00, REV 122.Oct 8, 2017 · N1381A · Boeing 767316F · Fuselage Miscellaneous StructureSDR UIEA2017092501860Gasket · damagedFWD CARGO BAY E/E COOLING DUCT GASKET FOUND DAMAGE. THE GASKET WAS REMOVED & REPLACED IAW AMM 20-11-00, REV 122.Oct 8, 2017 · N1381A · Boeing 767316F · Air Distribution SystemSDR UIEA2017092501861Duct · crackedAPU PRECOOLER EXHAUST DUCT FOUND CRACKED. APU PRECOOLER EXHAUST DUCT REMOVED & REPLACED IAW AMM 20-11-00, REV 122. LEAK CHECKED GOOD.Oct 8, 2017 · N1381A · Boeing 767316F · APU Core EngineSDR UIEA2017092501862Duct · tornAPU PRECOOLER EXHAUST TWO FLEXIBLE DUCTS FOUND TORN. APU PRECOOLER EXHAUST FLEXIBLE DUCTS REMOVED & REPLACED IAW AMM 20-11-00, REV 122. LEAK CHECKED GOOD IAW AMM 36-00-00, REV 122.Oct 8, 2017 · N1381A · Boeing 767316F · APU Core EngineSDR UIEA2017092701878Fastener · looseFWD CARGO BAY, RT E/E COOLING DUCT ASSY SUPPORT BRACKETS FOUND THE FASTENERS LOOSE. FASTENERS REMOVED AND NEW INSTALLED IAW SRM 51-40-02, REV 29.Oct 8, 2017 · N1381A · Boeing 767316F · Fuselage Miscellaneous StructureSDR UIEA2017092701879Wire Harness · deterioratedWIRE ASSY FOUND DETERIORATED. REMOVED AND REPLACED IAW SWPM 20-10-11, REV 65, SWPM 20-10-12, REV 65, SWPM 20-61-11, REV 65, AND WDM 26-15-11, REV 13. APU FIRE DETECTION OPERATIONAL TEST CARRIED OUT IAW AMM 26-15-00, REV 122. FOUND SATISFACTORY.Oct 8, 2017 · N1381A · Boeing 767316F · Fire Protection System WiringSDR UIEA2017101201949Warning Message · illuminatedRIGHT PACK OVERTEMP, RT PACK RAN 5 TIMES IAW AMM 21-51-00, REV 122, FOUND SATISFACTORY.Oct 8, 2017 · N1381A · Boeing 767316F · Cabin Cooling SystemSDR UIEA2017101201950Control Panel · failedFAILED RESET, LIGHT SWITCH FOUND INTERMITTENT DURING OPS TEST, FIRE/OVERHEAT TEST PANEL REMOVED AND REPLACED AND OPS TESTED IAW AMM 26-11-01, REV 122, FOUND GOOD.Oct 8, 2017 · N1381A · Boeing 767316F · Fire DetectionSDR FDEA201708222298Electronic Unit · failedLE SLAT ASSEMBLY ON UPPER EICAS IN FLIGHT. THIS WAS PRECEDED BY THE FLAP INDICATOR NEEDLE RAPIDLY CYCLING BETWEEN UP AND THE MID RANGE POSITION BETWEEN UP AND 1. WHEN MOVED THE FLAP HANDLE FROM UP TO 1, THE LE SLAT ASSYM CAME ON UPPER EICAS WITH MASTER CAAug 22, 2017 · N68079 · Boeing 767316F · Trailing Edge Flap Control SystemSDR FDEA201707181986Skin · delaminatedRIGHT WING OTBD FLAP LOWER SURFACE ON INBD SIDE HAS AREA OF DELAMINATION. REPAIRED IAW SRM 51-70-10, REPAIR 4, MAJOR REPAIR.Jul 18, 2017 · N68077 · Boeing 767316F · Trailing Edge FlapsSDR FDEA201707081885Jack · shortedDURING FLIGHT CREW PREFLIGHT, CREW FOUND WHEN OXYGEN MASK MICROPHONES WERE TESTED THE FLIGHT INTERPHONE STARTED TO EMIT A VERY LOUD SQUEAL. TO FURTHER TROUBLESHOT, DISCONNECTED ALL MICROPHONE INPUTS INTO THE FLIGHT INTERPHONE SYSTEM. WITH SAME RESULTS. CJul 8, 2017 · N68078 · Boeing 767316F · Interphone/Passenger Announcement (PA) SystemSDR FDEA201707071879Skin · crackedLEFT WING OTB TE FLAP LOWER SURFACE FROM 41 INCHES INBD OF THE NR 1 AFT FAIRING AND 13 INCHES FROM THE TE OF THE OTBD FLAP. REPAIRED IAW SRM 57-53-01-02R, AND 51-70-07. MAJOR REPAIR.Jul 7, 2017 · N68077 · Boeing 767316F · Trailing Edge FlapsSDR FDEA201706261762Hinge Fitting · crackedDURING A NR 2 ENGINE CHANGE, FOUND A CRACK IN THE FWD PYLON CASTING. THE LINK GOES TO THE RT THRUST REVERSER COWL. VISUALLY INSPECTED THE RIGHT ENGINE PYLON WHILE THE THRUST REVERSER HALFS INSTALLED. NO FURTHER DAMAGE FOUND WITH VISUAL INSPECTION. REMOVJun 26, 2017 · N68077 · Boeing 767316F · Engine Thrust ReverserSDR FDEA201703010717Warning Message · false activationLE SLAT ASYMETRY AMBER EICAS MESSAGE AT 6000 FT AND 220 KTS, WHEN FLAP HANDLE WAS MOVED TO 1 DEGREE. DECLARED AN EMERGENCY IAW FIM 27-81, TREE 809, SHEET 2 OF 9, BLOCK 2, NO CARD FAULT INDICATED. CYCLED LE ALTERNATE ARM SWITCH, SLAT ASSYMETRY MESSAGE EXMar 1, 2017 · N68077 · Boeing 767316F · Leading Edge Slat Control SystemSDR FDEA201612024310Feel Unit · wornF/O'S CONTROL COLUMN HAS RESISTANCE WHEN APPLYING FWD (NOSE DOWN) ELEVATOR. CAPT'S CONTROL COLUMN INTERMITTENTLY SHOWS SAME. REPLACED THE ELEVATOR FEEL UNIT.Dec 2, 2016 · N68077 · Boeing 767316F · Elevator Control SystemSDR 2LCF20160922002Eadi · failedDURING TAXI OF THE AIRCRAFT. THE CREW REPORTED SMOKE IN THE CABIN. AIRCRAFT RETURNED TO THE LOADING POSITION. TROUBLESHOT AND IDENTIFIED FAILURE IN THE COMPONENT ELECTRONIC ATTITUDE INDICATOR ASSY (EADI). CAPTAIN SIDE EADI WAS REPLACED IAW AMM 34-22-03. Sep 22, 2016 · N418LA · Boeing 767316F · Attitude and Direction Data SystemSDR FDEA201608102850Computer · malfunctionedDURING CLIMB OUT, ELEVATOR FLUTTER FROM 260 KTS UP TO 300 KTS. NO CHANGE WITH AUTO PILOT ON OR OFF. R & R THE ELEVATOR FEEL COMPUTER.Aug 10, 2016 · N68079 · Boeing 767316F · Elevator Control SystemSDR FDEA201606182054Skin Panel · damagedLEFT WING, NR 5 SLAT LOWER SKIN PANEL IS DAMAGED REPAIRED LT WING NR 5 SLAT LOWER SKIN PANEL IAW LAN SRM 57-43-01-2R, TABLE 1, FIG 201 AND 51-70-17. EA TH-5750-T0326118, P1 WINGS, FLIGHT SURFACES, NR 5 SLAT, LOWER CLOSE OUT PANEL REPAIR.Jun 18, 2016 · N68077 · Boeing 767316F · Leading Edge DevicesSDR FDEA201606081889Skin · dentedHAIL DAMAGED FOUND AT NR 5 SLAT WEDGE UPPER SURFACE. EVALUATED DENTS 10 EA. 1 EA DENT LOCATED 4.5" FROM TE & 84.25" FROM OB EDGE IS OUT OF LIMITS, 9 EA DENTS ARE WITHIN LIMITS. REPAIRED OUT OF LIMITS DENT IAW SRM 57-43-02-2R, 51-70-10-2R REPAIR 2. COMPLIED Jun 8, 2016 · N68077 · Boeing 767316F · Leading Edge DevicesSDR FDEA201605281749Escape Rope · out of positionEMERGENCY ESCAPE ROPE NOT STOWED. STOWED EMER ESCAPE ROPE IAW AMM 25-61-04-2-1, OK FOR SERVICE.May 28, 2016 · N68077 · Boeing 767316F · Emergency EquipmentSDR FDEA201603311128Relay · inoperativeDURING PUSHBACK, REV ISLN, LIGHT ON THROTTLE QUADRANT ILLUMINATED. ADVISED MX THEY SAID IT WOULD EXTINGUISH AFTER TAKEOFF. AFTER TAKEOFF, REV ISLN, REMAINED ILLUMINATED. FOR SAFETY DID AN AIR TURN BACK. R & R K2157. OPENED CB AIR & GND SYS 1 & REV ISLN LMar 31, 2016 · N68079 · Boeing 767316F · Engine Thrust Reverser
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