N1381A

Service difficulty reports · 382

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N1381A' AND registry_match = 'registration'
  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 UIEA2025032300377Retainer · corrodedCORROSION ON THE PLATE LOCATED IN THE FRAME UPPER PART (INNER STRUCTURE) WHICH IT IS SUPPORTING THE ACCESS PANEL 447BL, RIGHT ENGINE, AFT NACELLE STRUT FAIRINGS.(<P>PLATE OF THE ACCESS PANEL 447BL WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9 REV 52. NO FURTHER DEApr 5, 2025 · N1381A · Boeing 767316 · Nacelle/Pylon, Main FrameSDR UIEA2025032300378Retainer · corrodedCORROSION ON THE PLATE LOCATED IN THE FRAME UPPER PART (INNER STRUCTURE) WHICH IT IS SUPPORTING THE ACCESS PANEL 447BR, RIGHT ENGINE, AFT NACELLE STRUT FAIRINGS.(<P>PLATE OF THE ACCESS PANEL 447BR WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9 REV 52. NO FURTHER DEFApr 5, 2025 · N1381A · Boeing 767316 · Nacelle/Pylon, Main FrameSDR UIEA2025032300379Skin · gougedGOUGE AT INTERIOR SKIN OF FWD CARGO DOOR LWR FWD FRAME, STA 494.(<P>REWORKED AND INSPECTED PER TRE6752058 (BOEING MESSAGE CMA-TLS-25-0024). NO FURTHER DEFECTS NOTED.</P>)Apr 5, 2025 · N1381A · Boeing 767316 · Cargo/Baggage DoorsSDR UIEA2025032700392Computer · leakingELEVATOR FEEL COMPUTER, WITH HYDRAULIC LEAK.(<P>ELEVATOR FEEL COMPUTER HYDRAULIC LINES WERE RE-TORQUED IAW AMM 27-31-19-424-015 REV. 144 22DEC24. TORQUE APPLIED 270 IN/LB AND 170 IN/LB, TORQUES WRENCH DATA S/N: 0422127314 D/D: 17SEP25 AND S/N: 1123126519 D/D: Apr 5, 2025 · N1381A · Boeing 767316 · Elevator Control SystemSDR UIEA2025040100423Skin · crackedLH SIDE, FORWARD ENTRY DOOR CUTOUT AFT LOWER CORNER, WAS FOUND CRACK INDICATION, ON OPEN HOLE # 4 POSITION 5 O'CLOCK AT SKIN AND 10 O'CLOCK POSITION BEAR STRAP.(<P>LH SIDE, FORWARD ENTRY DOOR CUTOUT AFT LOWER CORNER, ON OPEN HOLE # 4 POSITION 5 O'CLOCK AT SKINApr 5, 2025 · N1381A · Boeing 767316 · Fuselage Main, Plate/SkinSDR UIEA2025040100424Skin · crackedRH SIDE, FORWARD SERVICE DOOR CUTOUT AFT LOWER CORNER, WAS FOUND CRACK INDICATION, ON OPEN HOLE # 4 POSITION 1 O'CLOCK AT SKIN APPROX.(<P>RH SIDE, FORWARD SERVICE DO OR CUTOUT AFT LOWER CORNER, ,ON OPEN HOLE # 4 POSITION 1 O'CLOCK AT SKIN CRACK WAS REPAIRED IAApr 5, 2025 · N1381A · Boeing 767316 · Fuselage Main, Plate/SkinSDR UIEA2025040100425Torsion Box · corrodedCORROSION ON TORSION BOX TOP SKIN BTW RBL 13.83 AND RBL 41.50, STGR 3 AT HORIZONTAL STABILIZER CENTER SECTION.(<P>ON TORSION BOX TOP SKIN BTW RBL 13.83 AND RBL 41.50, STGR 3 AT HORIZONTAL STABILIZER CENTER SECTION, CORROSION LEVEL 2 WAS REPAIRED IAW TRE6755083Apr 5, 2025 · N1381A · Boeing 767316 · Horizontal Stabilizer StructureSDR UIEA2025040100426Fuel Cell · leakingFUEL LEAK AT LOWER SIDE AREA OF LT WING LWR REAR SPAR SPLICE FITTING.<BR>(<P>LOWER SIDE AREA OF LT WING LWR REAR SPAR SPLICE FUEL LEAK WAS REPAIRED AND TEST WAS SATISFACTORY IAW AMM 28-11-00-308-013 REV 144 22/DEC/24. NO FURTHER DEFECTS NOTED.</P>)Apr 5, 2025 · N1381A · Boeing 767316 · Fuel StorageSDR UIEA2025040300428Blocker Door · crackedENG. 1, RIGHT T/R BLOCKER DOOR NO. 9 WITH A CRACK.(<P>ENG. 1, RIGHT T/R BLOCKER DOOR NO. 9 WAS REPLACED IAW AMM TASK 78-31-14-404-008-H00. NO FURTHER DEFECTS NOTED.</P>)Apr 5, 2025 · N1381A · Boeing 767316 · Engine Thrust ReverserSDR UIEA2025040300429Apu · inoperativeAPU INOP (AUXILIARY POWER UNIT) ER OPERATIONS NOT ALLOWED (NOTIFY DISPATCH) R60).(<P>APU INOP (AUXILIARY POWER UNIT) ER OPERATIONS NOT ALLOWED (NOTIFY DISPATCH) R60) WAS REPLACED WITH TASK CARD 8027 A-49-999-00-01. NO FURTHER DEFECTS NOTED.</P>)Apr 5, 2025 · N1381A · Boeing 767316 · Airborne Auxiliary Power Unit (APU) SystemSDR UIEA2025040300430Seal · brokenWING RH, BROKEN SEAL ON ACCESS PANELS 661 LB AND 661 CB.(<P>WING RH SEAL WAS REPLACED ON ACCESS PANEL 661LB, WING RH SEAL WAS REPLACED ON ACCESS PANEL 661CB IAW SRM 51-10-02-0G-0 PAR 9. NO FURTHER DEFECTS NOTED</P>)Apr 5, 2025 · N1381A · Boeing 767316 · Wing Main, Frame StructureSDR UIEA2025040300431Metering Valve · leakingLH WHEEL WELL AREA FWD BULKHEAD LH BRAKE METERING VALVE ASSY WITH HYDRAULIC LEAK.(<P>LH BRAKE METERING VALVE ASSY WAS INSTALLED IAW 32-41-02-424-002-003. STEP D1 STEP D10 TORQUE APPLIED S/N 0422127314 DUE DATE 17SEP25, TORQUE APPLIED 85 IN LBS, 140 IN LB, 200 Apr 5, 2025 · N1381A · Boeing 767316 · Landing Gear Brake SystemSDR UIEA2025040300432Pca · leakingRH WING, REAR SPAR, INBOARD AILERON, BOTH PCA´S WITH HYDRAULIC LEAK.(<P>AILERON PCAS (2 EAS) WERE REPLACED (SN: 1133 PN: 282800-1009 & SN: 1196 PN: 282800-1009). CHECKED FOR LEAKS & NO LEAK FOUND. ADJUSTMENT AND TESTS WERE SATISFACTORY. ALL WORKS IAW AMM 27-11Apr 5, 2025 · N1381A · Boeing 767316 · Aileron Control SystemSDR UIEA2025040400433Union · brokenRIGHT ENGINE STRUT 2 AFT NACELLE STRUT FAIRINGS IN ACCESS PANEL 447BL INTERNAL PART IN HYDRAULIC SHUT OFF VALVE WITH BROKEN CONNECTOR.(<P>CONNECTOR OF HYDRAULIC SHUTOFF VALVE AND BACKSHELL WERE REPLACED (PN: BACC63BW14SC5S & PN: BACC10HV14) INSTALLATION TEST WApr 5, 2025 · N1381A · Boeing 767316 · Hydraulic System, MainSDR UIEA2025040400434Pbe · leakingWING LH, INBOARD AILERON, BOTH PCA'S WITH LEAK.(<P>BOTH PCA'S, WERE REPLACED, ADJUSTED AND TESTED. (SN: 0683 PN: 282800-1011 & SN: 280 PN: 282800-1007) TEST WAS SATISFACTORY AND NO LEAK FOUND. ALL WORK IAW AMM: 27-11-48-022-003, AMM 27-11-48-422-040 AND 27-11-Apr 5, 2025 · N1381A · Boeing 767316 · Aileron Control SystemSDR UIEA2025040400436Fuse · leakingHYDRAULIC LEAK AT RH ANTISKID MODULE FUSE.(<P>IN RH ANTISKID MODULE FUSE WAS REPLACED IAW AMM 32-42-02-404-014, CHECK FOR LEAK, NO LEAK FOUND, OPERATION OF BRAKES WAS SATISFACTORY, IAW AMM 32-42-03-404-033.</P>)Apr 5, 2025 · N1381A · Boeing 767316 · Landing Gear Brake SystemSDR UIEA2025040400437Seal · brokenLH WING ACCESS PANEL 561BB WITH BOTH BULB SEAL BROKEN.(<P>BROKEN SEAL REPLACED AND CORRECTLY INSTALLED PER SRM 51-10-02-0G-0 PARA 9 REV 51. NO FURTHER DEFECTS NOTED.</P>)Apr 5, 2025 · N1381A · Boeing 767316 · Wing Miscellaneous StructureSDR UIEA2025040400439Pad · brokenLEFT WING LOWER SURFACE AREA MIDBODY INTEGRAL JACK PAD BROKEN.(<P>LEFT WING LOWER SURFACE AREA MIDBODY INTEGRAL JACK PAD WAS REPLACED IAW AMM 57-54-06-914-002 REV 144 DATE 22DEC24. NO FURTHER DEFECT NOTED.</P>)Apr 5, 2025 · N1381A · Boeing 767316 · Wing Miscellaneous StructureSDR UIEA2025040400440Proximity Sensor · damagedBROKEN TAG WASHER SUPPORT ON INBOARD AUX TRACK AT SLAT NO. 9.(<P>LEADING EDGE SENSOR SWITCH ON INBOARD AUX TRACK AT SLAT NO. 9 WAS REPLACED IAW AMM 27-88-01-902-001 REV 144 22DEC24. NO FURTHER DEFECTS NOTED.</P>)Apr 5, 2025 · N1381A · Boeing 767316 · Leading Edge Slat Position Indicating SystemSDR UIEA2025040400441Cover · dentedDURING RAM AIR TURBINE DEPLOYMENT TEST BY TASK CARD 8017-0101, FOUND A DENT ON RAM AIR TURBINE COVER SURFACE; IT WAS EVALUATED AND FOUND OUT OF LIMITS. L= 2.400 IN, W= 1.100 IN, D= 0.075 IN.(<P>N/R 00278 THE COVER WAS REMOVED FROM THE RAM AIR TURBINE IAW CMM 2Apr 5, 2025 · N1381A · Boeing 767316 · Fuselage Main, StructureSDR UIEA2025040400442Skin · dentedVERTICAL STABILIZER LH PANEL ASSEMBLY OUTER SKIN WITH DENT.(<P>DENT ON VERTICAL STABILIZER, LH PANEL ASSEMBLY, OUTER SKIN, WAS EVALUATED AND FOUND WITHIN ALLOWABLE DAMAGE LIMITS I.A.W. SRM 55-30-01-1A-1 AD.1 FIG. 101, DETAIL III. REV. 52 15APR25. DENT DOT 9025Apr 5, 2025 · N1381A · Boeing 767316 · Vertical Stabilizer, Plate/SkinSDR UIEA2025040400443Skin · debondedLH VERTICAL STABILIZER SKIN PANEL BTW FSS 270.784 TO FSS 118.75 PANEL WITH DISBONDED.(<P>LH VERTICAL STABILIZER SKIN PANEL WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9 REV 52 15-APR-25. NO FURTHER DEFECTS NOTED.</P>)Apr 5, 2025 · N1381A · Boeing 767316 · Vertical Stabilizer, Plate/SkinSDR UIEA2025040400444Pump · faultedLH WING THE FUEL BOOST PUMP LH FWD, TEST OPERATIONAL NOT SATISFACTORY. LT FWD BOOST PUMP LIGHT IN PANEL "P5" WAS INSTALLED CORRECTLY. IAW SWPM 20-84, REV 88, DATE 15-FEB-2025. TEST RESULT SATISFACTORY.Apr 5, 2025 · N1381A · Boeing 767316 · Fuel Boost PumpSDR UIEA2025011000027Control Unit · damagedPERFORMED TURNBACK TO IAH, DUE TO ELECTRICAL FUMES SMELL.(<P>FOUND M00897 ELECTRICAL LOAD CONTROL UNIT WITH LOOSE HARDWARE AND BURNT PLASTIC COVERING. REMOVED AND REPLACED ELCU IAW B767 AMM 29-11-14, OPS CHECK GOOD. SMELL IS NOW FAINT AND GOING AWAY. IPC 29-11Jan 11, 2025 · N1381A · Boeing 767316 · Hydraulic Power System WiringSDR UIEA2024123001192Escape Reel · missingEMERGENCY DESCENT DEVICES MISSING ONE.(<P>INSTALLED ONE EMERGENCY DESCENT DEVICE PER AMM 25-61-03. NO DEFECTS NOTED. PART EFFECTIVITY VERIFIED PER IPC 25-61-03-02.</P>)Dec 30, 2024 · N1381A · Boeing 767316 · Emergency EquipmentSDR UIEA2024111701095Warning Light · abnormalLOW-SPEED RTO DUE TO CONFIG WARN FLASPS M/S SET WITH FLAPS RESET SYS OPS NORMAL(<P>PERFORMED FLAPS SYS TEST PER 767 AMM 27-51-00, OPS CKS NORMAL, NO FAULTS NOTED </P>)Nov 17, 2024 · N1381A · Boeing 767316 · Trailing Edge Flap Control SystemSDR UIEA2023112600971Idg · unknown"L GEN DRIVE" EICAS AT FL240, MESSAGE BLANKED BEFORE PERFORMING ENG CHECKLISTS STEPS. (APU WAS PREVIOUSLY PLACED ON DEFERRAL)(<P>REMOVED AND REPLACED LH RNG IDG IAW AMM 24-11-01. NO FURTHER DEFECTS NOTED.</P>)Nov 25, 2023 · N1381A · Boeing 767316 · AC Generator-AlternatorSDR UIEA2023111400940Support · unknownFUDELAGE BULK CARGO COMPARTMENT LOWER SILL INNER CHORD BETWEEN STA 1417 / STA 1461 WITH CORROSION.(<P>INNER CHORD WAS REPLACED PER BOEING DWG 146T8210. NO FURTHER DEFECTS NOTED.</P>)Nov 16, 2023 · N1381A · Boeing 767316 · Fuselage Miscellaneous StructureSDR UIEA2023111400942Floor Support · unknownFUSELAGE BULK CARGO COMPARTMENT FLOOR PANEL SUPPORT BETWEEN  STA 1540 & STGR 34 / 35 RH CORROSION DAMAGE.(<P>FUESELAGE BULK CGO COMPARTMENT FLOOR PANEL SUPPORT WAS REPLACED PER DWG 146T5004. NO FURTHER DEFECTS NOTED.</P>)Nov 16, 2023 · N1381A · Boeing 767316 · Fuselage Miscellaneous StructureSDR UIEA2023111400943Unknown · unknownLEFT SKIN PANEL 175T2001-3 OF VERTICAL STABILIZER LOCATED BETWEEN AUXILIARY SPAR AND FRONT SPAR AND FSS 92.5 / FSS 270 DELAMINATION.(<P>LH VERTICAL STABILIZER WAS REPAIRED PER CMA-TLS-23-0150-15B. NO FURTHER DEFECTS NOTED</P>)Nov 16, 2023 · N1381A · Boeing 767316 · Vertical Stabilizer, Plate/SkinSDR UIEA2023111400944Unknown · unknownRIGHT SKIN PANEL 175T2001-4 OF VERTICAL STABILIZER LOCATED BETWEEN AUXILIARY SPAR AND FRONT SPAR AND FSS 92.5 / FSS 270.(<P>VERTICAL STABILIZER WAS REPAIRED PER CMA-TLS-0150-15B. NO FURTHER DEFECTS NOTED.</P>)Nov 16, 2023 · N1381A · Boeing 767316 · Vertical Stabilizer, Plate/SkinSDR UIEA2023111400945Unknown · unknownAFT CARGO COMPT DOOR LOCKOUT TORQUE TUBE WITH CORROSION.(<P>CORROSION WAS CLEANED PER AMM 52-35-00-622-074 REV. NO FURTHER DEFECTS NOTED.</P>)Nov 16, 2023 · N1381A · Boeing 767316 · Cargo/Baggage DoorsSDR UIEA2023111400946Floorbeam · unknownBULK CARGO COMPARTMENT RIGHT SIDE, STA 1480 BETWEEN STGR29 RH & STGR32 RH SUPPORTS FLOOR PANEL(<P>SUPPORT FLOOR PANEL WAS REPLACED PER DWG 146T1032. NO FURTHER DEFECTS NOTED</P>)Nov 16, 2023 · N1381A · Boeing 767316 · Fuselage Main, Floor BeamSDR UIEA2023111400947Floor Support · unknownBULK CARGO COMPARTMENT RIGHT SIDE, STA 1502 & STGR32 RH SUPPORT FLOOR PANEL(<P>SUPPORT FLOOR PANEL WAS REPLACED PER SRM 51-10-02-0G-0. NO FURTHER DEFECTS NOTED.</P>)Nov 16, 2023 · N1381A · Boeing 767316 · Fuselage Miscellaneous StructureSDR UIEA2023111400948Floorbeam · unknownAFT CARGO COMPARTMENT RH, INTERNAL STRUCTURE BTW STA 1417 AND STGR 27RH, SUPPORT FLOOR PANEL WITH CORROSION.(<P>SUPPORT FLOOR PANEL WAS REPLACED PER DWG 146T1032. NO FURTHER DEFECTS NOTED</P>)Nov 16, 2023 · N1381A · Boeing 767316 · Fuselage Main, Floor BeamSDR UIEA2023111400949Floorbeam · unknownAFT CARGO COMPARTMENT RH, INTERNAL STRUCTURE STA 1395 BETWEEN STGR 28RH & STGR 26RH, SUPPORT FLOOR PANEL WITH CORROSION.(<P>SUPPORT FLOOR PANEL WAS REPLACED PER DWG 453T1031. NO FURTHER DEFECTS NOTED.</P>)Nov 16, 2023 · N1381A · Boeing 767316 · Fuselage Main, Floor BeamSDR UIEA2023111400950Unknown · unknownRH WING BS 486.2 LOWER SURFACE CORROSION.(<P>DAMAGES WAS REWORKED PER TRE6757220. NO FURTHER DEFECTS NOTED.</P>)Nov 16, 2023 · N1381A · Boeing 767316 · Wing, Plate/SkinSDR UIEA2023111400951Nut · unknownLH WING FILL PORT ADAPTER NUT WITH GALVANIC CORROSION(<P>ADAPTER NUT WAS REPLACED PER AMM TASK 28-11-01-404-019. NO FURTHER DEFECTS NOTED.</P>)Nov 16, 2023 · N1381A · Boeing 767316 · Aircraft Fuel SystemSDR UIEA2023111400952Nut · unknownLH WING FILL PORT ADAPTER NUT WITH GALVANIC CORROSION(<P>ADAPTER NUT WAS REPLACED PER AMM TASK 28-11-04-404-019. NO FURTHER DEFECTS NOTED.</P>)Nov 16, 2023 · N1381A · Boeing 767316 · Wing StructureSDR UIEA2023111740953Failsafe · unknownLOWER FUSELAGE LOBE INTERIOR, EXFOLATION ON FAIL SAFE CHORD AFT FRAME WEB AT STA 1562 BL 0.(<P>FAIL-SAFE LOWER CHORD WAS REPLACED PER DWG 146T1223. NO FURTHER DEFECTS NOTED</P>)Nov 16, 2023 · N1381A · Boeing 767316 · Fuselage Main, StructureSDR UIEA2023111740954Failsafe · unknownTHE FAIL-SAFE STRAP UNDER THE T-FITTING ON THE RIGHT SIDE WITH CRACK INDICATION(<P>FAIL-SAFE STRAP WAS REPAIRED PER EO 6753A070/001. NO FURTHER DEFECTS NOTED.</P>)Nov 16, 2023 · N1381A · Boeing 767316 · Fuselage Main, StructureSDR UIEA2023111740955Unknown · unknownCANTED AREA STA. 955 BETWEEN LBL 87/LBL 91 UPPER SKIN EXTERIOR SIDE(<P>DAMAGE WAS REPAIRED PER CMA-TLS-23-0154-04B. NO FURTHER DEFECTS NOTED.</P>)Nov 16, 2023 · N1381A · Boeing 767316 · Wing, Plate/SkinSDR UIEA2023111740956Unknown · unknownAFT FUSELAGE STA 1725.5 CRACK FOUND ON THE BULKHEAD OUTER CHORD STRAP AND SKIN ABOVE STR-7R(<P>DAMAGE WAS REPAIRED PER SRM 53-80-01-2R-5. NO FURTHER DEFECTS NOTED.</P>)Nov 16, 2023 · N1381A · Boeing 767316 · Fuselage Miscellaneous StructureSDR UIEA2023111400957Unknown · unknownMAIN DECK CARGO DOOR AFT FRAME MID SPAN LATCH CAM WITH WEAR.(<P>DAMAGE WAS REPAIRED PER CMA-TLS-23-0164-02B. NO FURTHER DEFECTS NOTED.</P>)Nov 16, 2023 · N1381A · Boeing 767316 · Cargo/Baggage DoorsSDR UIEA2023111400958Unknown · unknownLH WING PUNCTURE IN LOWER SKIN SPOILER # 6.(<P>DAMAGE WAS REPAIRED PER CMA-TLS-23-0162-05B. NO FURTHER DEFECTS NOTED</P>)Nov 16, 2023 · N1381A · Boeing 767316 · SpoilersSDR UIEA2023111400959Floorbeam · unknownSECTION 41 FLOOR STRUCTURE, CRACK ON STIFFENER LOCATED ON REAR FACE OF FLOOR BEAM STA 246 APROX LBL 48.(<P>ANGLE WAS REPLACED PER FCVI EO 23214-1. NO FURTHER DEFECTS NOTED.</P>)Nov 16, 2023 · N1381A · Boeing 767316 · Fuselage Main, Floor BeamSDR UIEA2023082400796Unknown · unknownRED EICAS WARNING CAME ON FOR A SECOND WITH THE BELL. WE WERE UNABLE TO READ WHAT THE WARNING WAS. WHEN I OPENED THE FLIGHT DECK CARGO ACCESS DOOR, I SAW WHITE BILLOWING SMOKE (NOT CONDENSATION) & DECLARED AN EMERGENCY(<P>UPON BLOCK IN OF A/C, NO INDICATIONS OAug 24, 2023 · N1381A · Boeing 767316 · Fire Protection SystemSDR UIEA2023013070088Lamp · inoperativeEMERGENCY LIGHT BY FWD OF L1 DOOR INOP.(<P>RELAMPED, OPS CHECK NORMAL IAW AMM 33-51-03. </P>)Jan 27, 2023 · N1381A · Boeing 767316 · Emergency LightingSDR UIEA2022050200427Keelbeam · corrodedKEELBEAM ON HYD GROUND SERVICE DISCONNECT CENTER RETURN DOUBLER HAS CORROSION(<P>REMOVED, FABRICATED NEW, AND INSTALLED NEW <SPAN>KEEL BEAM ON HYD GROUND SERVICE DISCONNECT CENTER RETURN DOUBLER IAW B767 SRM 51-40-02, 51-40-05, </SPAN><SPAN>ATLAS GMM 3.39.2, AMay 3, 2022 · N1381A · Boeing 767316 · Fuselage Structure (General)SDR UIEA2021102202274None · none"L ENG FUEL VALVE" EICAS AFTER ENGINE SHUTDOWN.(<P>PERFORMED SPAR OPS CHECK SYSTEM, NO DEFECT NOTED AT THIS TIME AND ENGINE VALVE NO DEFECTS NOTED IAW AMM 28-22-01.</P>)Oct 22, 2021 · N1381A · Boeing 767316 · Fuel Boost Pump
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