Boeing 767-281

Service difficulty reports · 1,831

Newest first. General aviation reporting is voluntary.

Query with SQL
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 = '767281'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR ABXA030025Shear Tie · corrodedFORWARD CARGO LOWER LOBE, CORRODED SHEAR TIE AT STA 412, BETWEEN STRINGERS 39 LEFT - 39 RIGHT. CORRODED SHEAR TIE REMOVED AND INSTALLED NEW SHEAR TIE IAW SRM.Jan 6, 2003 · N795AX · Boeing 767281 · Fuselage Main, StructureSDR ABXA030024Shear Tie · corrodedFORWARD CARGO LOWER LOBE, CORRODED SHEAR TIE AT STA 742, BETWEEN STRINGERS 36 - 37 LEFT. CORRODED SHEAR TIE REMOVED, NEW SHEAR TIE INSTALLED IAW SRM.Jan 6, 2003 · N795AX · Boeing 767281 · Fuselage Main, StructureSDR ABXA030023Shear Tie · corrodedFORWARD CARGO LOWER LOBE, STA. 742, CORRODED SHEAR TIE, BETWEEN STR 38 - 39 LEFT. CORRODED SHEAR TIE REMOVED, NEW SHEAR TIE INSTALLED IAW SRM.Jan 6, 2003 · N795AX · Boeing 767281 · Fuselage Main, StructureSDR ABXA030022Panel · scratchedFORWARD CARGO LOWER LOBE, DEEP SCRATCHES ON SHEAR PANEL BETWEEN STA 610 - 632, LBL 45. DAMAGED SHEAR PANEL REMOVED AND NEW SHEAR PANEL INSTALLED IAW SRM.Jan 6, 2003 · N795AX · Boeing 767281 · Fuselage Miscellaneous StructureSDR ABXA030021Panel · corrodedFORWARD CARGO LOWER LOBE BETWEEN STA 577 - 610, LBL - RBL 15, CORRODED SHEAR PANEL. CORRODED SHEAR PANEL REMOVED, NEW SHEAR PANEL INSTALLED IAW SRM 51-40-02.Jan 6, 2003 · N795AX · Boeing 767281 · Fuselage Miscellaneous StructureSDR ABXA030020Shear Tie · corrodedFORWARD CARGO LOWER LOBE CORRODED SHEAR TIES AT STA 434, BETWEEN LONG 36-37 LEFT AND RIGHT. CORRODED SHEAR TIE REPLACED WITH NEW SHEAR TIE IAW SRM.Jan 6, 2003 · N795AX · Boeing 767281 · Fuselage Main, StructureSDR ABXA030019Frame · damagedFORWARD CARGO LOWER LOBE EXISTING REPAIRS ON UPPER CHORD OF BEAM AT STA 588, BL 45, FOUND DAMAGE. DAMAGED CHORD REMOVED AND NEW FRAME INSTALLED IAW SRM.Jan 6, 2003 · N795AX · Boeing 767281 · Fuselage Main, FrameSDR ABXA030018Shear Tie · corrodedFORWARD CARGO LOWER LOBE STA 742, CORRODED SHEAR TIE, BETWEEN STRINGER 39 LEFT - 39 RIGHT. CORRODED SHEAR TIE REMOVED, NEW SHEAR TIE INSTALLED IAW SRM.Jan 6, 2003 · N795AX · Boeing 767281 · Fuselage Main, StructureSDR ABXA030017Panel · crackedFORWARD CARGO LOWER LOBE, CORRODED SHEAR PANEL, BETWEEN STA 544-610, LBL 20 - 30 AND CRACKED. CORRODED AND CRACKED SHEAR PANEL. REMOVED AND REPLACED SHEAR PANEL IAW SRM.Jan 6, 2003 · N795AX · Boeing 767281 · Fuselage Miscellaneous StructureSDR ABXA030050Skin · corrodedLT WING SLAT NR 3 OSS 756.50, LE SKIN FOUND CORRODED ON FASTENER HEAD ATTACHING SKIN TO FORMER. REPAIRED AREA IAW REA B657-45505MR.Dec 11, 2002 · N795AX · Boeing 767281 · Leading Edge DevicesSDR ABXA030051Skin · corrodedLT WING UPPER SKIN PANEL NR 1 AFT OF REAR SPAR ATTACHMENT, WHERE THE TRAILING EDGE PANELS ARE INSTALLED, FOUND CORROSION AT WING STATIONS 534.27 & 554, 811.20 & 852. REPAIRED AREA IAW REA B657-45500MR.Dec 8, 2002 · N795AX · Boeing 767281 · Wing, Plate/SkinSDR ABXA030052Stringer · crackedDURING CHECK, 0.5 INCH LONG CRACK WAS FOUND AT SEC. 43 RT, STR. 17 RT, STA. 434. THE CRACK ORIGINATED AT THE FORWARD FASTENER HOLE IN STR. VERTICAL FLANGE. REPAIRED AREA IAW REA B653-45486MR.Nov 28, 2002 · N795AX · Boeing 767281 · Fuselage Main, Longeron/StringerSDR ABXA030016Tee Fitting · crackedFORWARD FUSELAGE CABIN RIGHT SIDE, WL 251.8, STA 287, FOUND CRACK ON TEE CONNECT TO FRAME. CRACKED TEE REMOVED AND INSTALLED NEW TEE. REF SRM 53-10-16, FIGURE 1 AND BAC DWG NR 141T8330/-6 INSTALLATION.Nov 28, 2002 · N795AX · Boeing 767281 · Fuselage Miscellaneous StructureSDR ABXA030015Tee Fitting · crackedFORWARD FUSELAGE CABIN LEFT SIDE, WL 251.8, STA 287. FOUND CRACK ON TEE CONNECT TO FRAME. CRACKED TEE REMOVED AND INSTALLED NEW TEE, FASTENERS IAW SRM, INSTALLATION.Nov 28, 2002 · N795AX · Boeing 767281 · Fuselage Miscellaneous StructureSDR ABXA030014Floorbeam · corrodedCABIN RIGHT SIDE STA 287 FLOORBEAM, RBL 73, FOUND CORROSION ON UPPER FLANGE OF FLOORBEAM, WL 199.5. PERFORMED FLOORBEAM UPPER CHORD REPAIR IAW SRM 53-00-51, FIGURE 201, REF SRM 53-10-51 AND DWG NR 141T5111. INSTALLED IAW SRM 51-40-02.Nov 20, 2002 · N796AX · Boeing 767281 · Fuselage Main, Floor BeamSDR ABXA030013Stringer · crackedSTRINGER 19L, BETWEEN STA 632 AND STA 654, AFT SIDE OF EXISTING LAMP HAD CRACKS ON STRINGER. THE CRACKS LENGTH WERE APPROXIMATELY .5 INCHES FROM THE EDGE OF STRINGER. PERFORMED STRINGER REPAIR IAW SRM 53-30-03 AND SRM 53-00-03, FIGURE 201. PART OF STRINGER WNov 18, 2002 · N795AX · Boeing 767281 · Fuselage Main, Longeron/StringerSDR ABXA030049Skin · gougedNR 1 ENGINE STRUT UNDER WING FAIRING FOUND DEEP GOUGE ON SKIN AT NAC STATION 258 RT SIDE. REPAIRED AREA IAW REA B654-45455MR.Nov 10, 2002 · N795AX · Boeing 767281 · Nacelle/Pylon, Main FrameSDR ABXA020119Latch · dirtyUPON DEPARTURE, WHEN LANDING GEAR WAS RAISED, A LOUD NOISE WAS HEARD AND A LARGE AMOUNT OF VIBRATION WAS FELT. LANDING GEAR WAS EXTENDED AND THREE GREEN INDICATED. AIRCRAFT LANDED UNEVENTFULLY. FOUND LEFT FORWARD NOSE LANDING GEAR DOOR OPEN. MANUALLY CLOSEAug 26, 2002 · N784AX · Boeing 767281 · Landing Gear Door Retract SectionSDR ABXA020005Sensor · defectiveLt eng hi stage displayed. Lt hi stage light illuminated. Per non-normal check list the left pneumatic switch was cycled on/off with oily fumes coming into the cabin. Note: The remainder of the flight was operated with left engine bleed and left A/C pack off. Jun 25, 2002 · N788AX · Boeing 767281 · Pneumatic Distribution SystemSDR ABXA010901Battery · dischargedDURING PREDEPARTURE CHECK, FOUND COCKPIT OVER THE DOOR REMOVABLE EMERGENCY LIGHT BARELY GLOWING WHEN TESTED. REPLACED INTERNAL BATTERIES IN EMERGENCY EXIT LIGHT. OPS CHECKED GOOD IAW B767 MM 33-51-0.Jun 3, 2002 · N791AX · Boeing 767281 · Emergency LightingSDR ABXA010876Battery Pack · dischargedDURING MAINTENANCE TEST OF EMERGENCY LIGHTING SYSTEM, FOUND STANDBY BATTERY INOPERATIVE. INSTALLED NEW BATTERY PACK IAW B767 MM 33-51-07-02. OPS CHECKED GOOD.May 13, 2002 · N774AX · Boeing 767281 · Emergency LightingSDR ABXA010875Power Supply · dischargedDURING MAINTENANCE INSPECTION, FOUND BOTH EMERGENCY LIGHTS INOPERATIVE. REPLACED PRIMARY EMERGENCY LIGHT POWER SUPPLY AND TESTED IAW B767 MM 33-51-07. PRIMARY SUPPLY OPS CHECKED GOOD. LIGHTS ILLUMINATED.May 11, 2002 · N774AX · Boeing 767281 · Emergency LightingSDR ABXA020084Panel · corrodedCORRODED SHEAR PANEL BETWEEN STATIONS 544-610, LEFT BUTT LINE - RIGHT BUTT LINE - 20. REPLACED PANEL IAW B767 AMM.Apr 9, 2002 · N793AX · Boeing 767281 · Fuselage Miscellaneous StructureSDR ABXA010804Odor · detectedAT TAKEOFF AND THROUGHOUT CLIMB, THERE WAS AN OIL SMELL COMING FROM THE ENVIRONMENTAL SYSTEM. RAN BOTH PACKS ON GROUND, NO SMELL NOTICED. OPS CHECKED GOOD.Mar 27, 2002 · N769AX · Boeing 767281 · Air Distribution SystemSDR ABXA010758Computer · defectiveDURING DESCENT, OBSERVED FUEL DISAGREE PROGRAM 2/2 AND VERIFIED FUEL IMBALANCE. LEFT FUEL QUANTITY LOWER THAN THE RIGHT BY APPROXIMATELY 1,400 LBS. ACCOMPLISHED THE QUICK REFERENCE HANDBOOK PROCEDURES AND SECURED THE LEFT ENGINE IAW THE QRH. PERFORMED FIM PMar 7, 2002 · N773AX · Boeing 767281 · Fuel Indicating SystemSDR ABXA010653Motor · leakingAN OIL ODOR WAS DETECTED IN THE AIR CONDITIONING SYSTEM DURING TAKEOFF. RAN UP PACKS WITH APU. SUSPECT ODOR FROM THE RIGHT PACK. FOUND EVIDENCE OF HYDRAULIC LEAK. SKYDROL AROUND THE PNEUMATIC DUCT CONNECTION IN THE KEEL AREA, RIGHT SIDE OF AIRCRAFT. REPLADec 18, 2001 · N787AX · Boeing 767281 · Leading Edge Slat ActuatorSDR ABXA010615Switch · wornDURING TAXI INTO GATE, THE NR 2 THRUST REVERSER DEPLOYED UNCOMMANDED, WOULD NOT STOW. DFDR DATA WAS REVIEWED AND THE DATA SHOWED THAT THE REVERSER DID NOT STOW AFTER LANDING. THE THROTTLE MICROSWITCH PACK WAS FOUND WORN WHICH PREVENTED THE THRUST REVERSER FRNov 29, 2001 · N769AX · Boeing 767281 · Power LeverSDR ABXA010627Frame · damagedENGINE NR 2 RIGHT CORE COWL FRAME NAC STA 304.60, NAC WL 75, FOUND DAMAGE ON FRAME. FABRICATED REPAIR PARTS, INSTALLED AND REPAIRED AREA IAW REA B671-42172MR.Nov 18, 2001 · N791AX · Boeing 767281 · Engine Cowling SystemSDR ABXA010630Skin · damagedDAMAGED AREA NEAR AN EXISTING FASTENER HOLE AT STATION 435, BETWEEN STR 13 LEFT TO STR 14 LEFT, LEFT SIDE ON OUTER SKIN. REPAIRED AREA IAW REA B653-41430MR.Oct 31, 2001 · N791AX · Boeing 767281 · Fuselage Main, Plate/SkinSDR ABXA010628Skin · gougedENGINE NR 1 STRUT, RIGHT SKIN PANEL OUTER SURFACE, DEEP GOUGE WITH SKIN PUNCTURE WAS FOUND NEAR AN ACCESS DOOR CUT OUT, STA 237, WL 135. FABRICATED REPAIR PARTS AND INSTALLED IAW REA B654-42153MR.Oct 31, 2001 · N791AX · Boeing 767281 · Nacelle/Pylon, Plate/SkinSDR ABXA010634Skin · dentedDENT WAS FOUND ON FUSELAGE SKIN BETWEEN STATION 1373 TO STATION 1395 AND BETWEEN STRINGER 25 LEFT TO STRINGER 26 LEFT AT LONGITUDINAL LAP SPLICE, LEFT SIDE. REPAIRED AREA IAW REA B653-41399MR.Oct 30, 2001 · N791AX · Boeing 767281 · Fuselage Main, Plate/SkinSDR ABXA010641Skin · crackedGOUGE AND CRACK ON P/N 313T1200-3 FAIRING SKIN PYLON NR 1 RIGHT SIDE. FABRICATED REPAIR PARTS AND REPAIRED AREA IAW REA B654-42136MR.Oct 22, 2001 · N791AX · Boeing 767281 · Nacelle/Pylon, Plate/SkinSDR ABXA010644Bolt · improperSTRUT FASTENERS INSTALLATION GRIP LENGTH NOT PER DRAWING, RIGHT STRUT. REPAIRED AREA IAW REA B654-42146MR.Oct 21, 2001 · N791AX · Boeing 767281 · Nacelle/Pylon, Main FrameSDR ABXA010629Bolt · improperSTRUT FASTENERS INSTALLATION GRIP LENGTH NOT PER DWG, LEFT STRUT. REPAIRED AREA IAW REA B654-42145MR.Oct 21, 2001 · N791AX · Boeing 767281 · Nacelle/Pylon, Main FrameSDR ABXA010638Channel · corrodedFORWARD CARGO LOWER LOBE BETWEEN STATION 610 AND STATION 632, LEFT BUTT LINE 6.5, CORRODED FLOOR CHANNEL, P/N 143T5000-80, LEFT SIDE. FABRICATED NEW PART AND REPAIRED AREA IAW REA B653-41896MR.Oct 8, 2001 · N791AX · Boeing 767281 · Fuselage Miscellaneous StructureSDR ABXA010631Stringer · damagedAFTER REMOVAL OF 140T015-22 SPLICE FITTING, STRINGER 34 RIGHT AT STATION 434, DAMAGE WAS FOUND ON TWO ENDS OF STRINGER 34 RIGHT. FABRICATED NEW PART AND REPAIRED AREA IAW REA B653-41910MR.Oct 3, 2001 · N791AX · Boeing 767281 · Fuselage Main, Longeron/StringerSDR ABXA010640Skin · crackedUPPER LINK PITCH FITTING REWORK. UPPER WING SKIN CRACKS, RIGHT WING. REPAIRED AREA IAW REA B657-41905MR.Oct 1, 2001 · N791AX · Boeing 767281 · Wing, Plate/SkinSDR ABXA010643Fitting · damagedDURING THE SIDE LINK FITTING REPLACEMENT ON THE RIGHT WING, DISCOVERED THAT TWO EXISTING ATTACHMENT HOLES WERE ALREADY SECOND OVERSIZED, WHILE SERVICE BULLETIN ALLOWED THE HOLES TO BE ENLARGED (AFTER COLDWORK) TO A MAXIMUM OF SECOND OVERSIZE. ONE OF THE HOLESSep 30, 2001 · N791AX · Boeing 767281 · Wing, Attach FittingsSDR ABXA010525Seal · wornA MEDIUM FREQUENCY LOUD TONE ACCOMPANIED BY AIRFRAME VIBRATION WAS FELT IN THE YOKE AND RUDDER PEDALS, WHILE CLIMBING THROUGH 12000 ACCELERATING TO 280 KNOTS. THE TONE CONTINUED UNTIL FL310. THE TONE CEASED UPON LEVAL OFF AT FL350. MAINTENANCE INSPECTED THE LESep 28, 2001 · N787AX · Boeing 767281 · Landing Gear DoorsSDR ABXA010524Indicator · malfunctionedBOTH LEFT AND RIGHT GLIDE SLOPES WERE FLAGGED. MAINTENANCE PERFORMED B767 FIM 22-00-02, FIG 113. A CAT III EVALUATION APPROACH WAS COMPLETED WITH SATISFACTORY RESULTS.Sep 26, 2001 · N787AX · Boeing 767281 · Glide Slope SystemSDR ABAX010461Door · out of adjDURING CLIMB, THERE WAS A LOUD NOISE AND AIRFRAME VIBRATION AT SPEEDS ABOVE 280 KTS BETWEEN 15,000 TO 20,000 FEET. NO LOUD NOISE OR VIBRATION DURING CRUISE OR DESCENT. VISUALLY INSPECTED UPPER AND LOWER FUSELAGE AND ALL CONTROL SURFACES. NO DEFECTS NOTED. Aug 31, 2001 · N787AX · Boeing 767281 · Landing Gear DoorsSDR ABXA010460Structure · vibrationTHERE WAS A LOUD NOISE ON BOTH SIDES OF THE COCKPIT AND AIRFRAME VIBRATION AT AIRSPEEDS ABOVE 310 AT 10,000 TO 20,000 FOOT ALTITUDES. INSPECTED FLAPS, GEAR WELL AREAS, FLIGHT CONTROLS. RAN FLIGHT CONTROLS THRU. PRESSURIZED AIRCRAFT TO 6 PSI. INSPECTED MEC Aug 30, 2001 · N787AX · Boeing 767281 · Fuselage Structure (General)SDR ABXA010639Frame · damagedTHREE OVAL HOLES WERE FOUND IN THE 143T1052-29 FRAME AND IN THE EXISTING ANGLE AT THE AFT SIDE OF FRAME, AT STATION 456, BETWEEN STRINGER 7 RIGHT AND STRINGER 8 RIGHT. FABRICATED NEW PART AND REPAIRED AREA IAW REA B653-41426DE.Aug 21, 2001 · N791AX · Boeing 767281 · Fuselage Main, FrameSDR ABXA010632Stringer · damagedONE ELONGATED HOLE WAS FOUND AT STATION 434, STRINGER 9, LEFT SIDE ON STRINGER, LOWER SIDE. FABRICATED REPAIR PART AND REPAIRED AREA IAW REA B653-41421MR.Aug 21, 2001 · N791AX · Boeing 767281 · Fuselage Main, Longeron/StringerSDR ABXA010447Engine · vibrationCLIMB READING WAS 2.7, CRUISE READING WAS 1.3, ENGINE PARAMETERS NORMAL. OTHER INDICATION WAS AUDIBLE NOISE AND VIBRATION FOLLOWING THRUST CHANGE. CLEANED AND INSPECTED HOLD OPEN RODS FOR FAN COWL IAW B767 MM 77-11-10-2. VIBRATION LEVELS WERE FOUND TO BE WIAug 17, 2001 · N786AX · Boeing 767281 · Engine (Turbine/Turboprop)SDR ABXA010436Valve · defectiveFLIGHT DECK TEMP. CONTROL FAILED TO CONTROL DESIRED TEMP. IN AUTO OR MANUAL. ALSO NO TEMP. CONTROL WITH ANY SELECTOR. DURING APPROACH, NAV EQUIPMENT BEGAN ERONEOUS INDICATIONS, AUTO PILOT DISENGAGED, F/O'S DU-1 FAILED, THEN F/O'S DU-2 FAILED. F/O'S FMC FAILED,Aug 9, 2001 · N783AX · Boeing 767281 · Cabin Temperature Control SystemSDR ABXA010647Skin · gougedA GOUGE WAS FOUND IN THE 146T6334-1 INNER SKIN, NEAR STATION 1439, WATER LINE 131, LOWER SIDE ON BULK CARGO DOOR INNER SKIN. REPAIRED THE AREA IAW REA B652-41387MR.Aug 6, 2001 · N791AX · Boeing 767281 · Cargo/Baggage DoorsSDR ABXA010413Odor · detectedTHERE WAS AN OIL SMELL FROM THE ENVIRONMENTAL SYSTEM ON TAKEOFF. REMOVED LEFT AND RIGHT CHECK VALVES (ENGINE SUPPLY) AND INSPECTED FOR OIL CONTAMINATION, NONE FOUND. REINSTALLED VALVES IAW B767 MM 36-20. RAN BOTH PACKS ON ENGINE PNEUMATICS, FULL HOT AND COLJul 27, 2001 · N787AX · Boeing 767281 · Air Distribution SystemSDR ABXA010407Light · inoperativeRIGHT GEAR GREEN DOWN LIGHT FAILED TO ILLUMINATE WITH GEAR HANDLE DOWN. EICAS MESSAGE NOT DISPLAYED. DOOR AND GEAR AMBER LIGHTS WERE EXTINGUISHED. CREW ELECTED TO DO A GO-AROUND AND A GEAR RECYCLE. RELAMPED RIGHT GEAR DOWN AND LOCKED. INDICATION OPS CHECKJul 25, 2001 · N788AX · Boeing 767281 · Landing Gear Position and WarningSDR ABXA010402Light · intermittentPORTABLE EMERGENCY EXIT LIGHT ASSEMBLY WAS FLICKERING ABOVE THE CREW DOOR. REPLACED THE PORTABLE EMERGENCY EXIT LIGHT ASSEMBLY IAW B767 AMM 33-51-00. OPS CHECKED GOOD.Jul 18, 2001 · N767AX · Boeing 767281 · Emergency Lighting
Back to Boeing 767-281