Boeing 767-304

Service difficulty reports · 89

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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 = '767304'
  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 IPXA2026092037107Seal · brokenFOUND DURING PS1 CHECK EMERGENCY DECENT DEVICE NR 6 WITH BROKEN SEAL. REPLACED BY SERVICEABLE IAW AMM 25-61-00/401 REV 149.Sep 20, 2026 · N391UP · Boeing 767304 · Emergency EquipmentSDR IPXA2026091803535Door · leakingPRESSURE LEAK MAIN DOOR ALONG FLOOR AREA CENTER. ENTERY/SERVICE DOOR SEAL CHECKED AND CLEANED, NO DAMAGED FAUND. IAW AMM:52-11-00-206-001 REV:149 CONFIRMED ALL TOOLS AND PARTS REMOVED FROM AIRCRAFT. Q9DY421Y CR102006933 KISISep 17, 2026 · N391UP · Boeing 767304 · Passenger/Crew DoorsSDR IPXA2026082983908Evas Unit · damagedCAPTAIN`S EVAS UNABLE TO DO BATTERY & BLOWER CHECK DUE TO TEST BUTTON SEEMS TO BE LOOSE INSIDE BOX. THE EVAS WAS REPLACED IAW AMM 25-69-00 PB. 401, REV 05-03-21. REF AIPC 25-69-00-01-001 REV. 05-03-21.Aug 29, 2026 · N391UP · Boeing 767304 · Emergency EquipmentSDR IPXA2026040806493Battery · dischargedAVI- COCKPIT EMERGENCY LIGHT FAIL TEST. ATA 33-51. REPLACED BATTERY ASSEMBLY IAW B767 AMM 33-51-07-022-003-002, B767 AMM 33-51-07-422-007. OPS CHECK GOOD.Apr 8, 2026 · N392UP · Boeing 767304 · Emergency LightingSDR IPXA2026020377596Window · warning messageLEFT FWD WINDOW EICAS MSG W/ WINDOW SW IN ON POSITION PERFORMED WINDSHIELD HEAT CONTROLLER BITE PER AMM 30-41-00, SENSOR WAS FAULTED. SWAPPED TO SPARE SENSOR USING TB322 PER AMM 30-41-00-801, OPS CHECK GOOD. ETOPS CERTIFIED MECH.Feb 1, 2026 · N392UP · Boeing 767304 · Windshield/Door Rain/Ice RemovalSDR IPXA2026020277596Sensor · faultedLEFT FWD WINDOW EICAS MESSAGE WITH WINDOW SWITCH IN THE -ON- POSITION. PERFORMED WINDSHIELD HEAT CONTROLLER BITE IAW AMM 30-41-00, SENSOR WAS FAULTED. SWAPPED TO SPARE SENSOR USING TB322 IAW AMM 30-41-00-801, OPS CHECKED GOOD.Feb 1, 2026 · N392UP · Boeing 767304 · Windshield/Door Rain/Ice RemovalSDR IPXA2025121171825Landing Gear · faultedATB, AFTER T/O WHEN RETRACTING THE L/G THE RIGHT REMAINED DOWN AND LOCKED. GEAR DISAGREE EICAS MESSAGE.RETURNED TO SNN AND REMAINING TWO GEARS EXT NORMALLY FOR LANDING. FLAPS OPERATED NORMALLY.Dec 10, 2025 · N391UP · Boeing 767304 · Landing Gear Retraction/Extension SystemSDR IPXA2025120950228Warning Light · illuminatedATB, C HYD DEM PUMP EICAS MESSAGE FLASHED BRIEFLY AFTER START.C HYD DEM PUMP EICAS MESSAGE CAME BACK ON DURING CLIMB AND GEAR DISAGREE EICAS MESSAGE. RIGHT GEAR REMAINED DOWN. GEAR EXT NORM ON LANDING TO CONFIRM NO FURTHER ISSUES WITH THE GEAR THE AIRCRAFT WASDec 9, 2025 · N391UP · Boeing 767304 · Hydraulic Pump (Electric/Engine), MainSDR IPXA2025110656340Beam · crackedA 0.3125 INCH CRACK WAS FOUND ON THE BEAM AT THE FORWARD-LOWER CORNER OF THE L1 DOOR. IAW AMM 52-11-01-404-018, REV 59. INSTALLED L1 DOOR. CONDITION CHECK NORMAL.Oct 26, 2025 · N391UP · Boeing 767304 · Passenger/Crew DoorsSDR IPXA2025110325464Skin Panel · crackedCRACK, L1 DOOR AFT LOWER CORNER SKIN. (REPAIR) COMPLETED REPAIR I.A.W SRM 53-10-01-2R-1 REV.129 AND EGAT WORK SHEET NO. 50805 WORK INSTRUCTIONS<BR>STEP D.26(5) SAND THE OUTER SURFACES AND EDGES OF THE SCUFF PLATE AS NECESSARY TO GET A SMOOTH SURFACE.<BR>STEP DOct 24, 2025 · N391UP · Boeing 767304 · Fuselage Main, Plate/SkinSDR IPXA2025110331356Skin Panel · crackedCRACK, R1 DOOR AFT LOWER CORNER SKIN. (REPAIR) COMPLETED REPAIR I.A.W SRM 53-10-01-2R-1 REV.129 AND EGAT WORK SHEET NO. 50807 WORK INSTRUCTIONS, STEP D.26 (5) SAND THE OUTER SURFACES AND EDGES OF THE SCUFF PLATE AS NECESSARY TO GET A SMOOTH SURFACE.<BR>STEP DOct 24, 2025 · N391UP · Boeing 767304 · Fuselage Main, Plate/SkinSDR IPXA2025100641817Hydraulic System · leakingATB AFTER TAKEOFF WHILE RETRACTING FLAPS FROM F5 TO F1 WE RECEIVED C HYD QTY ABD STATUS PAGE SHOWED QUANTITY DECREASING #8 SPOILER ACTUATOR REPLACED IAW AMM 26-61-02-401. LEAK CHECK PERFORMED AND NOT FOUND LEAKS. SPOILER OPTS PERFORMED IAW AMM 27-61-00 AND SYSOct 1, 2025 · N391UP · Boeing 767304 · Hydraulic System, MainSDR IPXA2025100241817Warning Message · illuminatedAIR TURNBACK. AFTER TAKEOFF WHILE RETRACTING FLAPS FROM F5 TO F1 WE RECEIVED C HYD QTY ABD STATUS PAGE SHOWED QUANTITY DECREASINGOct 1, 2025 · N391UP · Boeing 767304 · Hydraulic System, MainSDR IPXA2025071171812Unknown · odorWITH LEFT PACK ON AND ONLY APU PNEUMATICS, STRONG SMELL OF JET FUEL IN FLIGHT DECK. PERFORMED 20 MINS OF APU OPERATION BOTH AC NO FUMES EVIDENT I.A.W AMM 21-00-21-102-030 REB 145.00. TXFRD TO MAINTENIX TASK ID T3F18E006ZXJX FOR DEFECT RECTIFICATION.Jul 4, 2025 · N392UP · Boeing 767304 · Air Distribution SystemSDR IPXA202507071812A/C Pack · odorWITH LEFT PACK ON AND ONLY APU PNEUMATICS, STRONG SMELL OF JET FUEL IN FLIGHT DECK. TXFRD TO MAINTENIX TASK ID T3F18E006ZXJX FOR DEFECT RECTIFICATION.Jul 4, 2025 · N392UP · Boeing 767304 · Cabin Cooling SystemSDR IPXA2025022789366None · none**SUPPLEMENTAL SDR** ADD SDR FOR EO-82173-JIC001 (FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R). PERFORM MODIFICATION PER UPS EO-82173-JIC001. COMPLETED SDR.Feb 22, 2025 · N392UP · Boeing 767304 · Standard Practices/StructuresSDR IPXA2025022289366None · none**SDR FILED OPEN** ADD SDR FOR EO-82173-JIC001 (FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R)Feb 22, 2025 · N392UP · Boeing 767304 · Standard Practices/StructuresSDR IPXA2025030651444Bear Strap · crackedMAJOR REPAIR, FOUND CRACK ON THE NO.1 FWD ENTRY DOOR LH AFT LOWER CORNER BEAR STRIP. (REPAIR) INSTALL SCUFF PLATE I.A.W AMM 53-13-01-424-005 REV.144 AND EGAT WORK SHEET NO: 50133 REPAIR INSTRUCTIONS STEP D.25(7).(8).(9).(10). INSTALL DOOR WAY LINING I.A.W AMMFeb 20, 2025 · N392UP · Boeing 767304 · Fuselage Main, Plate/SkinSDR IPXA2025022747627Skin · crackedCRACK - SKIN, FWD LOWER FACE OF L/H WING NO.5 SLAT L/E NOSE SKIN OSS 492.953, NEAR OUTBD TRACK.I.A.W AMM 27-81-02-024-001 REV.144 REMOVED LH WING NO.5 SLAT.I.A.W. AMM 06-44-00-992-002 REV.144 REMOVED THE PANEL NO.522CB.I.A.W. AMM 30-11-05-004-001 REV.144 REMOVFeb 20, 2025 · N392UP · Boeing 767304 · Leading Edge DevicesSDR IPXA2025022747635Skin · crackedCRACK - SKIN, FWD LOWER FACE OF L/H WING NO.4 SLAT L/E NOSE SKIN OSS 568.149, NEAR INBD TRACK. I.A.W AMM 27-81-02-024-001 REV.144 REMOVED LH WING NO.4 SLAT. I.A.W. AMM 06-44-00-992-002 REV.144 REMOVED THE PANEL NO.523CB.COMPLETED REPAIR I.A.W SRM 57-43-01-2R-2Feb 20, 2025 · N392UP · Boeing 767304 · Leading Edge DevicesSDR IPXA2025022200461Skin Panel · dentedDENT - SKIN, L/H FORWARD LOWER FUSELAGE, NEAR CREW ENTRY DOOR, STA 315, S-30L~S-31L. (REPAIR). ENSURE ALL DATA REQUIRED IN GMM-MTX 03.43.01.04 HAS BEEN CORRECTLY DOCUMENTED. A. ORIGINAL SKIN (P/N:141T3231-7) MADE FROM 2024-T3 CLAD REPAIR AREA THICKNESS 0.07Feb 18, 2025 · N392UP · Boeing 767304 · Fuselage Main, Plate/SkinSDR IPXA2024121143530Lamp · inoperativeP6 OVHD PANEL EMERGENCY LIGHTS UNARMED LIGHT INOP FOUND CAP ASSY BROKEN. CAP ASSY AND LAMPS REPLACED IAW IPC 33-51-08-30BDec 11, 2024 · N392UP · Boeing 767304 · Emergency LightingSDR IPXA2024091974562Seal · dirtyLOUD NOISE FROM AIR LEAK AFTER TAKEOFF GOING THRU ABOUT 3000 FT UNTIL 11,000 FT. SUSPECT CREW ENTRY DOOR. NOISE WENT AWAY AFTER. PRESSURIZATION REMAINED NORMAL. CHECKED CREW ENTRY DOOR AND SEAL IAW AMM 52-12-00-601 REV.143, FOUND NO DAMAGE AT CREW ENTRY DOOR, Sep 18, 2024 · N392UP · Boeing 767304 · Passenger/Crew DoorsSDR IPXA2024091491233Drive Shaft · brokenENG #1 INBOARD REVERSER HALF PARTIAL OPEN WITH GAP ON UPPER SIDE INSPECTION C?O O.K AND FOUND UPPER FLEXIBLE SHAFT DRIVE BROKEN. #1 ENG INBOARD T/R UPPER AND LOWER (AS A PRECAUTION) FLEXIBLE SHAFT DRIVES REPLACED BY SERVICEABLE I.A.W AMM 78-31-18/401 REV 142. Sep 13, 2024 · N392UP · Boeing 767304 · Engine Thrust ReverserSDR IPXA2024052846775Warning Message · illuminated*DIVERSION* AIR/GND DISAGREE STATUS MESSAGE T/S C/O IAW FIM 32-09 FAULT TREE 810 REV142. PSEU BITE PROCEDURE C/O IAW FIM 32-09 FAULT TREE 803 AND FOUND FAULT CODE "S244" NOT COMPRESSED SENSOR OF NLG. DURING CHECK, S244 SENSOR TARGET FOUND LOOSE. SENSOR TARGET May 24, 2024 · N391UP · Boeing 767304 · Landing Gear Position and WarningSDR 2024FA0000323Window · crackedDURING FUNCTIONAL CHECK FLIGHT AFTER BDSF CONVERSION WINDOW R1 (RIGHT WINDSHEILD) CRACKEDApr 18, 2024 · N292CR · Boeing 767304 · Flight Compartment WindowsSDR 2024FA0000319Pressure Blkhd · dentedFOUND DENT WITH CREASE ON AFT PRESSURE BULKHEAD WEB, STA 1582, WL 235, RBL 75.Apr 17, 2024 · N292CR · Boeing 767304 · Fuselage Main, BulkheadSDR IPXA2023111554296Hinge · brokenDURING WAI FOUND INSPECTIONPANEL, 2 FEET OUTBOARD OF RIGHT ENGINE, HINGES BROKEN BUT PANEL STILL ATTACHED. INSTALLED TAI SEAL DOOR PANEL ON RH WING OUTB OF ENG IAW AMM 57-41-58/401 REV 140 THIS CLOSED DMINov 1, 2023 · N391UP · Boeing 767304 · Wing, Attach FittingsSDR IPXA2023110154296Unknown · unknown*SDR FILED OPEN* DURING WAI FOUND INSPECTIONPANEL, 2 FEET OUTBOARD OF RIGHT ENGINE, HINGES BROKEN BUT PANEL STILL ATTACHED. PANEL REMOVED AND PANEL DEFERRED IAW CDL 57-41-2.<BR>PLACKARD INSTALLED.Nov 1, 2023 · N391UP · Boeing 767304 · Wing, Fuselage Attach FittingsSDR IPXA2023102376262Landing Gear · warning messageEICAS GEAR DISAGREE. AFTER T/O LANDING GEAR LEVER UP RIGHT MAIN GEAR WOULD NOT RETRACT. REVERSED DMP PER MEL 32-30-1. R+R RH MAIN LANDING GEAR SIDE BRACE LOCK ACTUATOR PER AMM 32-32-02 PB 401 REV140. TEST PASS. LEAK CHECK SATIS. CHECKED LOCK LINKS, JURY STRUT Oct 20, 2023 · N391UP · Boeing 767304 · Landing Gear SystemSDR IPXA2023071979142Charger · inoperativeDURING PS1 CHECK,FOUND 2 OF 4 EMERGENCY LIGHTS IN THE FLIGHT DECK ARE NOT ILLUMINATING ++ TROUBLESHOTING C/OUT IAW FIM 33-51 FT 803 REV:139 AND FOUND ONE BATTERY AND ONE POWER SUPPLY (CHARGER) FAULTY. POWER SUPPLY (CHARGER) AND BATTERY REPLACED IAW AMM 33-51-Jul 19, 2023 · N392UP · Boeing 767304 · Emergency LightingSDR IPXA20230719142Unknown · unknown*** SDR FILED OPEN *** DURING PS1 CHECK,FOUND 2 OF 4 EMERGENCY LIGHTS IN THE FLIGHT DECK ARE NOT ILLUMINATINGJul 19, 2023 · N392UP · Boeing 767304 · Emergency LightingSDR MK1Y20230719005Unknown · unknownFLOOR TRUSS ASSY PN 145T5300-947: THERE IS 1 ELONGATED FASTENER HOLE AND 1 DRILL START ADJACENT TO AN EXISTING HOLE DIA ¼ ON THE FLOOR TRUSS ASSY. P/N 145T5300-947. THE PART CANNOT BE REPAIRED OR PROCURED IN A FAIR TIME FRAME.Jul 19, 2023 · N291CR · Boeing 767304 · Fuselage Main, Floor BeamSDR MK1Y20230719004Unknown · unknownSTA 1351, LBL 49.0: DURING MAINTENANCE INSPECTION A CRACK WAS FOUND ON THE SIDE GUIDE RAIL IN AFT CARGO AT LENGTH OF THE CRACK IS ABOUT 1.7”. THE DATUM RAIL MADE OF 7075-T73511 BAC 1520-2199 EXTRUSION PER SRM 53-60-53, IDENT 1.Jul 19, 2023 · N291CR · Boeing 767304 · Standard Practices/StructuresSDR MK1Y20230719003Unknown · unknownL/H WING, LOWER SKIN, CORROSION DAMAGE WAS FOUND ON THE LOWER SKIN PANEL (P/N 112T4703-1) AROUND FUEL SUMP DRAIN VALVE HOLE BETWEEN STRINGERS L-11 AND L-12 NEAR SIDE OF BODY.Jul 19, 2023 · N291CR · Boeing 767304 · Fuselage Main, Plate/SkinSDR MK1Y20230719002Unknown · unknownSTA 933 ABOVE STR 19R INNER CHORD FRAME: DURING CONVERSION AT IAI FACILITIES, MTX FOUND CORROSION ON INNER CHORD FRAME AT STA 933 ABOVE STR 19R. THE CORROSION WAS REMOVED PER SRM PRACTICES. J/C MF02920R0217-01 WAS REISED AND FURTHER INSPECTIONS WERE PERFORMEDJul 19, 2023 · N291CR · Boeing 767304 · Fuselage Structure (General)SDR MK1Y20230719001Unknown · unknownSTA 871.5 ABOVE STR 19R INNER CHORD FRAME: DURING CONVERSION AT IAI FACILITIES, MTX FOUND CORROSION ON INNER CHORD FRAME AT STA 871.5 ABOVE STR 19R. THE CORROSION WAS REMOVED PER SRM PRACTICES. J/C MF02920R0218-01 WAS REISED AND FURTHERJul 19, 2023 · N291CR · Boeing 767304 · Fuselage Structure (General)SDR IPXA2023070402978Fmc · frozenAIRTURN BACK DUE TO BOTH FMC UNRESPONSIVE IN LEGS + ROUTE PAGES ENTIRE ROUTE WAS ERASED. BOTH FMC IN STANDBY ONE. REPLACED BOTH FMC IAW AMM: 34-61-02/401, REV: 139. OPS TEST SATIS, VERIFIRED CORRECT SOFTWARE P/N ARE INSTALLED IAW SOFTWARE MATRIX, REV: 130.<BR>Jul 4, 2023 · N391UP · Boeing 767304 · Flight Management Computing Hardware SystemSDR IPXA2023030691557Stiffener · crackedINSPECTION TYPE:C14*MAJOR REPAIR* CRACK ON THE STIFFENER ( P/N:141T5814-176) OF THE FLOOR BEAM ASSEMBLY AT STA 246, LBL 40REPAIR I.A.W 767-300 SRM 53-10-51-2R-4 REV.121.01Feb 23, 2023 · N392UP · Boeing 767304 · Fuselage Structure (General)SDR IPXA2023030591523Skin · crackedINSPECTION TYPE:C14*MAJOR REPAIR* CRACK ON NOSE SKIN (P/N:114T4103-4) OF NO.10 SLAT AT OSS 723.94REPAIR I.A.W 767-300 SRM 57-43-01-2R-2 REV 121.01.Feb 23, 2023 · N392UP · Boeing 767304 · Wing StructureSDR IPXA2022111688163Power Supply · inoperativeINSPECTION TYPE:N/ARH DOME EMERGENCY LT AND THRESHOLD EMER LT NOT WORKINGT/S'D IAI WDM 33-51-11. FOUND EMER LT BATT SUPPLY U/S R/R EMER PWR BATT SUPPLY IAW IAI AMM 33-51-00. P/N ON/OFF 3013-1A S/N ON 67960 S/N OFF 119067 TAG 965757. REF IAI AIPC 33-51-00-01N-4Nov 16, 2022 · N391UP · Boeing 767304 · Emergency LightingSDR IPXA2022070583807Door · inoperativeINSPECTION TYPE:N/AUNABLE TO OPEN UP MAIN CARGO DORAFTER CYCLING OF GROUND HANDLING BUS NORMAL MAIN DECK CARGO DOOR OPS ESTABLISHED IAW AMM 52-10-00Jul 5, 2022 · N391UP · Boeing 767304 · Passenger/Crew DoorsSDR IPXA2022060282759Eicas · activation errorINSPECTION TYPE:NA***MX REROUTE*** UNSCHD STAB TRIM MESSAGE ONCE AT 1000 FT CLIMBING AND THEN AGAIN AT FL 320 - 360. CENTER AP ENGAGED.T/S PERF IAW FIM 27-09-00-815-813 REV 136.00 REF ALERT T204080, REPLACED L STCM, STAB TRIM POS XMTRS M519 & M520 & FLAP SLAT Jun 2, 2022 · N391UP · Boeing 767304 · Stabilizer Control SystemSDR IPXA2022031580121Light · faultedENTRY DOOR LIGHT ON OVERHEAD PANEL INTERMITTENT IN CRUISE FLT. NO EICAS MESSAGE. NOTE: LIGHT CHOP AT FLIGHT LEVEL 350. LATCH PIN AND LATCH PIN CABLE ADJUSTED IAW AMM 52-11-00-501-825-018 REV 135.05. OPS TEST SATIS. THIS CLOSES 775704.Mar 15, 2022 · N391UP · Boeing 767304 · Passenger/Crew DoorsSDR IPXA2022031380060None · noneINSPECTION TYPE:N/AENTRY DOOR LIGHT ON OVHD PNL INTERMITTENT ON IN CRUISE FLIGHT. NO EICAS MSG.OPS CHECK ON CREW ENTRY DOOR IAW AMM 52-11-00-715-128 REV 135.05 TESTED SATIS. THIS CLEARS M775632Mar 13, 2022 · N391UP · Boeing 767304 · Passenger/Crew DoorsSDR IPXA2022011377830None · noneINSPECTION TYPE:ETOP*ETOPS FILED OPEN*A/C OOS* R ENG BLEED OFF SHOWS & R ENG BLEED OFF LT ILLUM AFTER ENG START. QRH PROCEDURE DID NOT FIX ISSUE.RH ENG PRV & PRV CONTROLLER REPLACED IAW AMM 36-11-18-401 REV. 135.02 & AMM 36-11-19-401 REV. 135.02, NO HELP. OPCJan 12, 2022 · N391UP · Boeing 767304 · Pneumatic Distribution SystemSDR IPXA2021121977078Warning Message · false activationDURING TAKEOFF AND DURING FLAP RETRACTION, FLAPS STOPPED AT JUST THAN 5 AND THE TE FLAP ASYM EICAS MSG ILLUMINATED. RAN THE CHECKLIST IAW QRH, CONSULTED WITH DISPATCH AND BURNED DOWN FUEL.FIM TASK 27-51 815-810 APPLIED. FLAP PDU BY-PASS LEVER CHECKED WITH ALT Dec 19, 2021 · N391UP · Boeing 767304 · Trailing Edge Flap Control SystemSDR IPXA2021103175473None · noneINSPECTION TYPE:C13DAMAGE ON MAIN DECK FLOOR PANEL ASSY (P/N:368-53-16-94477-127) BETWEEN LBL 11.0 AND RBL 11.0.FABRICATE A NEW FLOOR PANEL I.A.W UPS EO B767-5320-82003-AOct 21, 2021 · N391UP · Boeing 767304 · Fuselage Structure (General)SDR IPXA2021060370142Warning Message · false activationDIVERSION-NO EMERG DECL'D & NO EQUIP USED-LANDED UNEVENTFULLY-AC TAKEN OOS** AFTER SUCCESSFUL GRND TEST OF WX RDR, AFTER AIRBOURNE WX RDR NEVER WORKED. "WXR SYS" STATUS MSG DISPLAYED. AT NO TIME WAS THERE EVER ANY INDICATION OF A WX SWEEP ON THE HSI. INFLT TEJun 3, 2021 · N391UP · Boeing 767304 · Weather Radar SystemSDR IPXA2021040967978Fuel Filter · contaminatedINSPECTION TYPE:NA**ATB - NO EMERGENCY DECLARED, NO EMERG EQUIP USED.** DURING CLIMB L ENG FUEL FILT EICAS DISPLAYED AFTER PERFORMING QRH PROCEDURE EICAS MSG WAS GONE BUT STATUS MSG STILL DISPLAYED.T/S PERFOMRED IAW FIM 73-11-00-815-803-H00 REV 132.00 FOUND CApr 9, 2021 · N391UP · Boeing 767304 · Engine Fuel Distribution
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