Boeing 767-300

Service difficulty reports · 2,161

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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 = '767300'
  ORDER BY difficulty_date DESC"

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SDR HALA0600618Floorbeam · damagedDOUBLE HOLE IN FLOORBEAM AT NUT PLATE, HOLE AT STA 1502 RBL WL 200. DOUBLE HOLE NOT ALLOWED IN FLOORBEAM, STA 1502, WL 200. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51-1A-1. REMOVED DAMAGE IAW SRM 53-00-51-2R-2. RECEIVED NEW -1 ANGLE LOT NR 665417, EXTENSIOJun 30, 2006 · N598HA · Boeing 767300 · Fuselage Main, Floor BeamSDR HALA0600613Floor Support · crackedFWD CARGO COMPT FLOOR SUPPORT LOWER SURFACE ATTACH ANGLE CRACKED BS 478 LBL 47, WL 125. ATTACH ANGLE AT BS 478 LBL 47 WL 125 CRACKED 100 PERCENT ACROSS MATERIAL OUT OF LIMITS, IAW SRM 53-00-04-1A-1, NOTE (B) CRACKS ARE NOT PERMITTED. FABRICATED NEW ATTACH ANJun 30, 2006 · N598HA · Boeing 767300 · Fuselage Miscellaneous StructureSDR HALA0600468Structure · ground damagePER BOARDING AGENT, JET BRIDGE CONTACTED BOTTOM OF MED. LOWER FWD OF DOORS EDGE DAMAGE 1/8 DEEP BY 10" LONG. OK TO CONTINUE PER M105FILE NR 486050. XCRIBED TO DPM P14542367Jun 28, 2006 · N486HA · Boeing 767300 · Standard Practices/StructuresSDR HALA060465Processor · malfunctionedETOPS SIGNIFICANT ITEM T/CAS INOP, OFF AND ON IN CLIMB UNTIL CRUISE. REPLACED TCAS PROCESSOR. OPS CHECK OK PER MM 34-45-00.Jun 28, 2006 · N584HA · Boeing 767300 · Air Collision Avoidance SystemSDR NOCA9606Lamp · burned outRED EMERGENCY EXIT FLOOR LIGHT INOP AT DOOR 2R.Jun 28, 2006 · N760NA · Boeing 767300 · Emergency LightingSDR NOCA9306Lamp · burned outDOOR R2 FLOOR PROXIMITY 2 RED EMERGENCY LIGHTS INOP.Jun 28, 2006 · N760NA · Boeing 767300 · Emergency LightingSDR HALA0600707Intercostal · crackedCRACKED INTERCOSTAL UPPER ANGLE STA 566-588 RBL 39 WL 200. NO CRACKS PERMITTED ON FLANGE OF INTERCOSTAL STA 566-588 RBL 39 WL 200, OUT OF LIMITS, IAW SRM 55-00-04-1A-1. REMOVED UPPER CORD ANGLE IAW SRM 51-40-02 1801 DETAIL 1 AND DETAIL 2. INSTALLED NEW UPPEJun 27, 2006 · N598HA · Boeing 767300 · Fuselage Miscellaneous StructureSDR HALA0600810Support Angle · crackedVERTICAL SUPPORT ANGLE CRACKED STA 325 RBL 22 WL 199. REMOVED AND INSTALLED NEW VERICAL SUPPORT ANGLE IAW SRM 51-40-05, SRM 51-20-01-0G-0 AND SRM 51-40-02-60-0.Jun 26, 2006 · N589HQ · Boeing 767300 · Fuselage Miscellaneous StructureSDR HALA0600476Skin · maint errorWHILE INSTALLING RUDDER, MECHANIC DROPPED A WRENCH PUNCTURING LEFT I/B ELEVATOR UPPER SKIN APPROX 18 INCHES FROM I/B END. REPAIR ACCOMPLISHED ON LEFT ELEVATOR UPPER SKIN APPROXIMATELY 18 INCHES FROM I/B END IAW SRM 55-20-01-1, SRM 55-20-1A1, SRM 55-20-2R-1, SJun 26, 2006 · N594HA · Boeing 767300 · Elevator StructureSDR NOCA9206Light · inoperativeO/H EMERGENCY LIGHT INOP BY SEAT 34BJun 26, 2006 · N768NA · Boeing 767300 · Emergency LightingSDR UPS06647394Flap · delaminatedFOUND RT I/B AFT FLAP HAS 3.5" DENT WITH DELAMINATED. REPAIRED IAW 51-20-10-2 AND 51-70-10-2R.Jun 25, 2006 · N320UP · Boeing 767300 · Trailing Edge FlapsSDR HALA0600477Angle · crackedNR 1 ENGINE PYLON O/B SKIRT FAIRING 2ND ANGLE FWD OF AFT ENG MOUNT CRACKED PAST STOP DRILL. REMOVED CRACKED SKIRT FAIRING ANGLE, 2ND FROM FWD OF AFT ENGINE MOUNT ON NR 1 ENGINE PYLON O/B SIDE AND INSTALLED NEW ANGLE PER SRM 51-40-04 AND SRM 51-40-02.Jun 24, 2006 · N594HA · Boeing 767300 · Nacelle/Pylon, Attach FittingsSDR HALA0600479Angle · crackedNR 1 ENGINE PYLON O/B SKIRT FAIRING 3RD ANGLE FWD OF THE AFT ENGINE MOUNT CRACKED. REMOVED CRACKED SKIRT O/B SIDE OF PYLON AND INSTALLED NEW ANGLE PER SRM 51-40-04, AND SRM 51-40-02.Jun 24, 2006 · N594HA · Boeing 767300 · Nacelle/Pylon, Main FrameSDR HALA0600720Support Channel · crackedBIN SUPPORT CHANNEL CRACKED STA/ 1197+88 BETWEEN STR 11L AND 12L. REMOVED DAMAGE BIN SUPPORT CHANNEL AND INSTALLED WITH NEW IAW SRM 51-40-02, FIG.8 AND STEP 4.8.Jun 23, 2006 · N598HA · Boeing 767300 · Fuselage Miscellaneous StructureSDR HALA0600482Static Wick · looseRT STAB FIXED T/E MIDDLE STATIC DISCHARGER WICK BASE IS LOOSE, FOUND FASTENERS TO BASE WORKED HOLES OUT OF USEABLE SIZE. REPAIRED RT STAB FIXED T/E MIDDLE STATIC DISCHARGER WICK BASE AND WORKED HOLES OUT OF USEABLE SIZE IAW SRM 51-20-17, MM 51-21-10.Jun 23, 2006 · N594HA · Boeing 767300 · Static Discharge SystemSDR NOCA9106Light · inoperativeEMERGENCY LIGHT STRIP AT R4 DOOR INOP.Jun 23, 2006 · N768NA · Boeing 767300 · Emergency LightingSDR HALA0600500Rib · corrodedFOUND CORROSION ON LEFT WING AT LES 485 UPPER RIB FLANGE. REMOVED CORROSION AT LES 485 UPPER RIB FLANGE 16 INCH BY .75" WIDE AND .002" DEEP. FOUND TO BE WITHIN LIMITS PER SRM 57-41-09/101. ALODINED AND APPLIED DECORATIVE FINISH IAW MM 51-21-04-377-001 AND MJun 22, 2006 · N598HA · Boeing 767300 · Wing, Rib/BulkheadSDR HALA0600502Rib · corrodedFOUND CORROSION ON LT WING AT LES 456, UPPER RIB FLANGE. REMOVED CORROSION ON UPPER FLANGE LES 456 15" LONG .75" WIDE .003" DEEP. FOUND TO BE WITHIN LIMITS PER SRM 57-41-09/101. ALODINED AND RESTORED FINISH IAW MM51-21-04-377-001 AND MM51-221-10-307-020.Jun 22, 2006 · N598HA · Boeing 767300 · Wing, Rib/BulkheadSDR HALA0600501Support Angle · corrodedFOUND CORROSION ON LT WING AT LES 475 LWR LE SUPPORT ANGLE FWD END. REMOVED CORROSION AT LES 475 LWR LE SUPPORT ANGLE FWD END. .50" BY .50" AND 001 DEEP AT TOP AND .50" BY .50" AND .001" DEEP AT BOTTOM. FOUND TO BE WITHIN LIMITS PER SRM 57-41-09/101. ALODINJun 22, 2006 · N598HA · Boeing 767300 · Wing Miscellaneous StructureSDR HALA0600480Skin · lightning strikeWHILE WORKING TAIL 5033 DISCOVERED FIN LEADING EDGE PANEL 326A HAS LIGHTING STRIKE DAMAGE AT LEADING EDGE 7" FROM TIP. REMOVED AND REPLACED FIN LEADING EDGE PANEL 326A REF, SOPM 20-50-01.Jun 21, 2006 · N594HA · Boeing 767300 · Vertical Stabilizer, Plate/SkinSDR HALA0600729Pump · failedAFTER ENGINE START EICAS R FWD FUEL PUMP ILLUMINATED ALONG W/PRESS LIGHT IN SWITCH. "R FWD FUEL BOOST PUMP" CN POPPED. PERFORMED FIM 28-22-00 FIGURE 106A. NO FAULTS FOUND OK FOR SERVICE. REMOVED AND REPLACED RF FWD FUEL BOOST PUMP PER MM 28-22-03 OP AND LKJun 16, 2006 · N585HA · Boeing 767300 · Fuel Boost PumpSDR HALA0600461Valve · malfunctionedETOPS SIGNIFICANT SYSTEM - MID CABIN TRIM AIR VALVE VERY SLOW TO RESPOND TO COMMAND CHANGES. FUNCTIONAL TESTED VALVE PER MM 21-61-07 VALVE CHECKED NORMAL. OK FOR SERVICE.Jun 16, 2006 · N586HA · Boeing 767300 · Cabin Temperature Control SystemSDR HALA0600457Gps · malfunctionedL GPS EICAS MESSAGE. RAN A GROUND OPS TEST ON THE L GPS SYSTEM AS PER 34-58-00 GRD OPS CK SAT OK TO CONTINUE.Jun 14, 2006 · N590HA · Boeing 767300 · Global Positioning SystemSDR HALA0600481Skin · debondedLT I/B AILERON TE IS DISBONDED AND HAS SEVERAL IMPROPER FASTENERS. REMOVED, REPAIRED AND REINSTALLED LT WING I/B AILERON IAW SRM 51-40-02, BAC DWG 11376100, AMM27-11-01-024-051, AMM 27-11-01-424-031. REPAIR ACCOMPLISHED ON ID NR 00774. ADJUSTMENT AND FUNCTIJun 13, 2006 · N594HA · Boeing 767300 · AileronsSDR HALA0600456Gps · malfunctionedBTB ETOPS SIGNIFICANT SYSTEM - RIGHT AFTER ENGINE START AND BEFORE COMMENCING TAXI RECEIVED EICAS AMBER MESSAGE -UNABLE RNP- FOLLOWED SHORTLY BY EICAS AMBER MESSAGE -L GPS- CHECK POS PAGE 3, CONFIRMED GPS FUNCTION WAS SWITCHED ON; NO GPS POSITIONS SHOWN. RESEJun 13, 2006 · N583HA · Boeing 767300 · Global Positioning SystemSDR HALA0600455Switch · malfunctionedETOPS SIGNIFICANT SYSTEM--REPEAT- LEFT PACK AUTO SHUT DOWN. AFTER APPROX 5 MIN OF OPERATION LEFT PACK DISPLAYED -INOP ANNUN LIGHT- AND THEN SHUTDOWN. PERFORMED BITE OF PACK CONTROL PER 21-51-00 FIG 103, CHECKED GOOD, PERFORMED FIM 21-51-00 FIG 104B CHECKED GJun 13, 2006 · N586HA · Boeing 767300 · Cabin Cooling SystemSDR HALA0600458Radar · inoperativeETOPS SIGNIFICANT SYSTEM - WX RADAR (LT SIDE) INOP. PERFORM FIM 34-43-00-1 CHECK OK ON GND. OK FORSERVICE.Jun 13, 2006 · N586HA · Boeing 767300 · Weather Radar SystemSDR HALA0600459Warning System · activatedETOPS SIGNIFICANT SYSTEM - FOUND -FUEL QTY BITE- MSG ON MTC ECS PAGE. TS PER FIM 28 41 00 FIG 108 SHT 22 COULD NOT LOCATE CONNECTOR D08380P ON RACK AE 0320 AS PER WDM 28-41-22 E2 RACK CONNECTOR VISIBLY CHECKS GOOD OUT OF TIME SUPPLEMENT TSI.Jun 12, 2006 · N587HA · Boeing 767300 · Fuel Quantity IndicatorSDR HALA0600533Skin · crackedCRACK ON STRAP AFT OF STA 1725.5, STR-7R. INVESTIGATED DAMAGE AND FOUND CHORD STRAP AND SKIN TO BE CRACKED AT BS 1725.5, STR 7R. CUT OUT DAMAGE AND REPAIRED IAW ER 06-2425 DTD 25JUL 06, FILE NO. 594011.Jun 11, 2006 · N594HA · Boeing 767300 · Fuselage Main, Plate/SkinSDR HALA0600449Apu · malfunctionedETOPS SIGNIFICANT SYSTEM - APU AIR TOO LOW FOR ENGINE START. OK TO CONTINUE PER C 49-11-1-1.Jun 11, 2006 · N586HA · Boeing 767300 · APU Bleed Air SystemSDR HALA0600450Charger · failedETOPS SIGNIFICNAT SYSTEM - MAIN BATTERY CHARGER STATUS MESSAGE INDICATED ON STATUS PAGE. MAIN BATTERY DISCH ARGE LIGHT EXTINGUISHED. REPLACED MAIN BATTERY CHARGER PER MM 24-31-02. REPLACED MAIN BATTERY PER MM 24-31-01. CHARGING NORMAL. AMP AND VOLTAGE NORMJun 11, 2006 · N582HA · Boeing 767300 · Battery/Charger SystemSDR HALA0600448Idg · malfunctionedETOPS SIGNIFICANT SYSTEM - EICAS MSG LT GEN DRIVE DISPLAYED, GEN DRIVE LIGHT ILLUMINATED, GEN DRIVE DISCONNECTED. REMOVED AND INSTALLED LEFT IDG PER 767-3-405001 AND AMM 24-11-01. ON ENGINE RUN-UP LEFT GEN OPS NORMAL, NO LEAKS NOTED.Jun 10, 2006 · N580HA · Boeing 767300 · AC Generator-AlternatorSDR HALA0600451Skin · dentedTWO EA DENTS BELOW L4 DOOR ON FUSELAGE STATIONS 1480 AND 1540. PER DRM 53-00-01/101 DENTS ARE WITH IN OPERATIONAL LIMITS FWD DENT .875 X .008 INCH AND AFT 1.1875 X .012 INCH.Jun 10, 2006 · N590HA · Boeing 767300 · Fuselage Main, Plate/SkinSDR HALA0600447Skin · dentedON WALKAROUND FOUND DENT AFT OF FWD CARGO DOOR APPROX STATION 615, LONGERON 25R. DAMAGE WITHIN LIMITS PER SRM 53-00-01 FIGURE 101. NO CRACKS NOTED EDDY CURRENT AREA SILVER DOT INSTALLED.Jun 10, 2006 · N585HA · Boeing 767300 · Fuselage Main, Plate/SkinSDR HALA0600453Controller · malfunctionedLT PACK INOP LIGHT ON AFTER PACK SHUT DOWN. RAN BITE ON LT PACK, CONTROLLER SHOWS TEMP CONT VLV. RERACKED CONTROLLER AND RAN BITE AGAIN, NO FAULTS SHOWN, OPS CHECKS GOOD PER FIM 21-51-00 FIG 103.Jun 9, 2006 · N592HA · Boeing 767300 · Cabin Cooling SystemSDR HALA0600499Door Frame · corrodedFOUND CORROSION ON BULK CARGO DOOR CUTOUT FWD FRAME AT NUTPLATES ABOVE AND BELOW BOTTOM STOP FITTING BS 1417. REMOVED BOTTOM STOP FITTING AT BS 1417, IN BULK CARGO DOOR CUTOUT. BLENDED CORROSION OUT TO A DEPTH OF .004". MAX ALLOWABLE IS 10% (ORIG THICKENSS Jun 8, 2006 · N594HA · Boeing 767300 · Fuselage Main, StructureSDR HALA0600673Connector · unsecureETOPS SIGNIFICANT SYSTEM, PRIMARY ENG EGT IND FLUCTUATES STBY ENG IND ALSO ABNORMAL HAPPENED INTERMITTENTLY DURING CRUISE SEEMED TO GET WORSE LATER IN FLT. CHECKED CONTINUITY FROM JUNCTION BOX D932 TO FIREWALL PLUG P4208 NO OPENS OR SHORTS CHKD CONTINUITY FROJun 7, 2006 · N594HA · Boeing 767300 · Engine EGT/TIT Indicating SystemSDR HALA0600532Skin · damagedRIGHT WING FIXED LEADING EDGE SKIN IS DAMAGED AT NR 9 SLAT IB ROTARY ACTUATOR AND IB MAIN TRACK CUTOUT RESIDUE MOTOR.// REPAIRED THE RT WING L/E SKIN AT NR 9 SLAT I/B ROTARY ACTUATOR AND I/B MAIN TRACK CUTOUT IAW SRM 57-41-01 AND SRM 51-70-07.Jun 7, 2006 · N594HA · Boeing 767300 · Leading Edge DevicesSDR HALA0600442Warning System · malfunctionedETOPS SIGNIFICANT SYSTEM - EICAS STATUS MSG ELEV FEEL DISPLAYED. T/S PER FIM 27-31-00 FIG 106. OPS NORMAL. MSG ERASED.Jun 7, 2006 · N583HA · Boeing 767300 · Elevator Control SystemSDR HALA0600443Depressor · gougedUPON ACFT ARRIVAL WHILE PERFORMING WALKAROUND WAS ALERTED BY RAMP AGENT/STATION MGR, AFT CARGO DOOR SEAL DEPRESSOR AT FWD LOWER CORNER WAS GOUGED. INSPECTED AND FOUND WHAT APPEARED TO BE OLD DAMAGE. INFO SENT TO MOC. SMOOTHED GOUGE PER SRM 53-00-15 FIG 101 Jun 7, 2006 · N585HA · Boeing 767300 · Fuselage Miscellaneous StructureSDR HALA0600571Panel · damagedFIXED LEADING EDGE COMPOSITE PANEL IS DAMAGED OB OF NR 9 SLAT IB CONTROL ROD AND IB MAIN TRACK CUTOUT. REMOVED AND REINSTALLED FIXED LEADING EDGE COMPOSITE PANEL OB OF NR 9 SLAT BIG CONTROL ROD REPAIRED ON STRB CARD 5027 TO INCLUDE MISSING FASTENER REFERENCEDJun 6, 2006 · N594HA · Boeing 767300 · Leading Edge DevicesSDR HALA0600439Seal · wornETOPS SIGNIFICANT SYSTEM - AFTER ENGINE IDLE RUN FOUND OIL PUDDLE UNDER NR 2 ENGINE. ACCOMPLISHED AMM 71-71-00 EXAMINED THE VENTS AND DRAINS ON NR 2 ENGINE, FOUND GEARBOX STARTER DRIVE PAD DRAIN PORT OUT OF LIMITS. REPLACED STARTER DRIVE OIL SEAL PER AMM 72-Jun 6, 2006 · N583HA · Boeing 767300 · Turbine Engine Oil SystemSDR HALA0600437Intercostal · crackedINTERCOSTAL WEB CRACKED AT BS 287, RBL 25, WL 157. REPLACED INTERCOSTAL WEB AT BS 287, RBL 25, WL 157. FABRICATED WEB FROM 2024T3.040 PER DWG 284T0040, AND DWG 289T0039, SRM 51-30-01. ALODINED AND PRIMED PER 51-20-01. INSTALLED PER SRM 51-40-02.Jun 4, 2006 · N585HA · Boeing 767300 · Fuselage Miscellaneous StructureSDR HALA0600433B-Nut · looseETOPS SIGNIFICANT SYSTEM - RT OIL CONSUMPTION HIGH, ABOUT 2 QT PER HR. JUST PRIOR DESCENT 4 QTS ON DESCENT 1 QT, ON LANDING 3 QTS, ON SHUTDOWN 11 QT. FOUND B-NUT ON EEC OIL TEMP THERMOCOUPLE PROBE LOOSE. TIGHTENED AND RESAFTIED B-NUT. RESERVICED TO ENGINE Jun 4, 2006 · N583HA · Boeing 767300 · Engine Oil TemperatureSDR HALA0600436Stiffener · crackedCRACK NOTED IN NLG WHEEL WELL BULKHEAD VERTICAL CHORD RADIUS AT BS 287, LBL 25, WL 179. REPAIRED NLG BULKHEAD VERTICAL CHORD AT BS 287, LBL 25, WL 179.Jun 3, 2006 · N585HA · Boeing 767300 · Fuselage Main, BulkheadSDR HALA0600438Stiffener · crackedCRACK NOTED IN NLG WHEEL WELL BULKHEAD VERTICAL CHORD RADIUS AT BS 287, RBL 25, WL 179. REPAIRED NLG AFT BULKHEAD VERTICAL CHORD AT BS 287, RBL 25, WL 179, PER SRM 51-70-12-06-0.Jun 3, 2006 · N585HA · Boeing 767300 · Fuselage Main, BulkheadSDR HALA0600498Bulkhead · puncturedAFT CARGO BAY BULKHEAD RT CENTER PANEL PUNCTURED LWR EDGE. REPAIRED AFT CARGO BAY FWD BULK HEAD RT CENTER PANEL IAW SRM 51-70-03-06 PARA 4C STEPS (A)-(F), PARA 4D STEP (2) AND (3), PARA 4E STEP (1)-(4) AND PARA 4H STEPS (1)-(2).Jun 2, 2006 · N594HA · Boeing 767300 · Fuselage Main, BulkheadSDR HALA0600428Scuff Plate · ground damageBULK CARGO DOOR DAMAGED BY GROUND SERVICE EQUIPMENT. BULK CARGO DOOR SCUFF PLATE REMOVED, NO DAMAGE NOTED TO AIRFRAME. REPAIR SCUFF PLATE DENT PER COLD WORK BAC5300 AND CRACK PER BAC5975 613. INSTALLED SCUFF PLATE PER AMM 53-13-02, SECURITY CONDITION GOOD.Jun 2, 2006 · N588HA · Boeing 767300 · Fuselage Miscellaneous StructureSDR HALA0600426Warning System · activatedETOPS SIGNIFICANT SYSTEM - AFT CARGO AFT DETECTION FAN MESSAGE ON EICAS. OK TO CONTINUE PER MEL 21-51-01.Jun 1, 2006 · N588HA · Boeing 767300 · Air Distribution SystemSDR HALA0600423Depressor · crackedFWD CARGO DOOR SEAL DEPRESSOR CRACKED AT STATION 478 AT S32R. ACCOMPLISHED TEMP REPAIR PER HAL M105 FILE NR 582080. TO BE REINSPECTED ONCE DAILY FOR SMOOTHNESS. PERMANENT REPAIR TO BE ACCOMPLISHED WITHIN 50 FLT CYCLES.Jun 1, 2006 · N592HA · Boeing 767300 · Fuselage Miscellaneous Structure
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