PLATE OF THE ACCESS PANEL 447BL WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9 REV 52. NO FURTHER DE - [SDR UIEA2025032300378](https://openairdocs.org/sdr/UIEA2025032300378.md): Retainer · corroded · Apr 5, 2025 · N1381A · Boeing 767316 · Nacelle/Pylon, Main Frame > CORROSION 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.(
PLATE OF THE ACCESS PANEL 447BR WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9 REV 52. NO FURTHER DEF - [SDR UIEA2025032300379](https://openairdocs.org/sdr/UIEA2025032300379.md): Skin · gouged · Apr 5, 2025 · N1381A · Boeing 767316 · Cargo/Baggage Doors > GOUGE AT INTERIOR SKIN OF FWD CARGO DOOR LWR FWD FRAME, STA 494.(
REWORKED AND INSPECTED PER TRE6752058 (BOEING MESSAGE CMA-TLS-25-0024). NO FURTHER DEFECTS NOTED.
) - [SDR UIEA2025032700392](https://openairdocs.org/sdr/UIEA2025032700392.md): Computer · leaking · Apr 5, 2025 · N1381A · Boeing 767316 · Elevator Control System > ELEVATOR FEEL COMPUTER, WITH HYDRAULIC LEAK.(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: - [SDR UIEA2025040100423](https://openairdocs.org/sdr/UIEA2025040100423.md): Skin · cracked · Apr 5, 2025 · N1381A · Boeing 767316 · Fuselage Main, Plate/Skin > LH 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.(
LH SIDE, FORWARD ENTRY DOOR CUTOUT AFT LOWER CORNER, ON OPEN HOLE # 4 POSITION 5 O'CLOCK AT SKIN - [SDR UIEA2025040100424](https://openairdocs.org/sdr/UIEA2025040100424.md): Skin · cracked · Apr 5, 2025 · N1381A · Boeing 767316 · Fuselage Main, Plate/Skin > RH SIDE, FORWARD SERVICE DOOR CUTOUT AFT LOWER CORNER, WAS FOUND CRACK INDICATION, ON OPEN HOLE # 4 POSITION 1 O'CLOCK AT SKIN APPROX.(
RH SIDE, FORWARD SERVICE DO OR CUTOUT AFT LOWER CORNER,,ON OPEN HOLE # 4 POSITION 1 O'CLOCK AT SKIN CRACK WAS REPAIRED IA - [SDR UIEA2025040100425](https://openairdocs.org/sdr/UIEA2025040100425.md): Torsion Box · corroded · Apr 5, 2025 · N1381A · Boeing 767316 · Horizontal Stabilizer Structure > CORROSION ON TORSION BOX TOP SKIN BTW RBL 13.83 AND RBL 41.50, STGR 3 AT HORIZONTAL STABILIZER CENTER SECTION.(
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 TRE6755083
- [SDR UIEA2025040100426](https://openairdocs.org/sdr/UIEA2025040100426.md): Fuel Cell · leaking · Apr 5, 2025 · N1381A · Boeing 767316 · Fuel Storage
> FUEL LEAK AT LOWER SIDE AREA OF LT WING LWR REAR SPAR SPLICE FITTING.
(
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.
) - [SDR UIEA2025040300428](https://openairdocs.org/sdr/UIEA2025040300428.md): Blocker Door · cracked · Apr 5, 2025 · N1381A · Boeing 767316 · Engine Thrust Reverser > ENG. 1, RIGHT T/R BLOCKER DOOR NO. 9 WITH A CRACK.(ENG. 1, RIGHT T/R BLOCKER DOOR NO. 9 WAS REPLACED IAW AMM TASK 78-31-14-404-008-H00. NO FURTHER DEFECTS NOTED.
) - [SDR UIEA2025040300429](https://openairdocs.org/sdr/UIEA2025040300429.md): Apu · inoperative · Apr 5, 2025 · N1381A · Boeing 767316 · Airborne Auxiliary Power Unit (APU) System > APU INOP (AUXILIARY POWER UNIT) ER OPERATIONS NOT ALLOWED (NOTIFY DISPATCH) R60).(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.
) - [SDR UIEA2025040300430](https://openairdocs.org/sdr/UIEA2025040300430.md): Seal · broken · Apr 5, 2025 · N1381A · Boeing 767316 · Wing Main, Frame Structure > WING RH, BROKEN SEAL ON ACCESS PANELS 661 LB AND 661 CB.(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
) - [SDR UIEA2025040300431](https://openairdocs.org/sdr/UIEA2025040300431.md): Metering Valve · leaking · Apr 5, 2025 · N1381A · Boeing 767316 · Landing Gear Brake System > LH WHEEL WELL AREA FWD BULKHEAD LH BRAKE METERING VALVE ASSY WITH HYDRAULIC LEAK.(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 - [SDR UIEA2025040300432](https://openairdocs.org/sdr/UIEA2025040300432.md): Pca · leaking · Apr 5, 2025 · N1381A · Boeing 767316 · Aileron Control System > RH WING, REAR SPAR, INBOARD AILERON, BOTH PCA´S WITH HYDRAULIC LEAK.(
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 27-11 - [SDR UIEA2025040400433](https://openairdocs.org/sdr/UIEA2025040400433.md): Union · broken · Apr 5, 2025 · N1381A · Boeing 767316 · Hydraulic System, Main > RIGHT ENGINE STRUT 2 AFT NACELLE STRUT FAIRINGS IN ACCESS PANEL 447BL INTERNAL PART IN HYDRAULIC SHUT OFF VALVE WITH BROKEN CONNECTOR.(
CONNECTOR OF HYDRAULIC SHUTOFF VALVE AND BACKSHELL WERE REPLACED (PN: BACC63BW14SC5S & PN: BACC10HV14) INSTALLATION TEST W - [SDR UIEA2025040400434](https://openairdocs.org/sdr/UIEA2025040400434.md): Pbe · leaking · Apr 5, 2025 · N1381A · Boeing 767316 · Aileron Control System > WING LH, INBOARD AILERON, BOTH PCA'S WITH LEAK.(
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- - [SDR UIEA2025040400436](https://openairdocs.org/sdr/UIEA2025040400436.md): Fuse · leaking · Apr 5, 2025 · N1381A · Boeing 767316 · Landing Gear Brake System > HYDRAULIC LEAK AT RH ANTISKID MODULE FUSE.(
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.
) - [SDR UIEA2025040400437](https://openairdocs.org/sdr/UIEA2025040400437.md): Seal · broken · Apr 5, 2025 · N1381A · Boeing 767316 · Wing Miscellaneous Structure > LH WING ACCESS PANEL 561BB WITH BOTH BULB SEAL BROKEN.(BROKEN SEAL REPLACED AND CORRECTLY INSTALLED PER SRM 51-10-02-0G-0 PARA 9 REV 51. NO FURTHER DEFECTS NOTED.
) - [SDR UIEA2025040400439](https://openairdocs.org/sdr/UIEA2025040400439.md): Pad · broken · Apr 5, 2025 · N1381A · Boeing 767316 · Wing Miscellaneous Structure > LEFT WING LOWER SURFACE AREA MIDBODY INTEGRAL JACK PAD BROKEN.(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.
) - [SDR UIEA2025040400440](https://openairdocs.org/sdr/UIEA2025040400440.md): Proximity Sensor · damaged · Apr 5, 2025 · N1381A · Boeing 767316 · Leading Edge Slat Position Indicating System > BROKEN TAG WASHER SUPPORT ON INBOARD AUX TRACK AT SLAT NO. 9.(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.
) - [SDR UIEA2025040400441](https://openairdocs.org/sdr/UIEA2025040400441.md): Cover · dented · Apr 5, 2025 · N1381A · Boeing 767316 · Fuselage Main, Structure > DURING 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.(N/R 00278 THE COVER WAS REMOVED FROM THE RAM AIR TURBINE IAW CMM 2 - [SDR UIEA2025040400442](https://openairdocs.org/sdr/UIEA2025040400442.md): Skin · dented · Apr 5, 2025 · N1381A · Boeing 767316 · Vertical Stabilizer, Plate/Skin > VERTICAL STABILIZER LH PANEL ASSEMBLY OUTER SKIN WITH DENT.(
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 9025 - [SDR UIEA2025040400443](https://openairdocs.org/sdr/UIEA2025040400443.md): Skin · debonded · Apr 5, 2025 · N1381A · Boeing 767316 · Vertical Stabilizer, Plate/Skin > LH VERTICAL STABILIZER SKIN PANEL BTW FSS 270.784 TO FSS 118.75 PANEL WITH DISBONDED.(
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.
) - [SDR UIEA2025040400444](https://openairdocs.org/sdr/UIEA2025040400444.md): Pump · faulted · Apr 5, 2025 · N1381A · Boeing 767316 · Fuel Boost Pump > LH 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. - [SDR UIEA2025011000027](https://openairdocs.org/sdr/UIEA2025011000027.md): Control Unit · damaged · Jan 11, 2025 · N1381A · Boeing 767316 · Hydraulic Power System Wiring > PERFORMED TURNBACK TO IAH, DUE TO ELECTRICAL FUMES SMELL.(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 29-11 - [SDR UIEA2024123001192](https://openairdocs.org/sdr/UIEA2024123001192.md): Escape Reel · missing · Dec 30, 2024 · N1381A · Boeing 767316 · Emergency Equipment > EMERGENCY DESCENT DEVICES MISSING ONE.(
INSTALLED ONE EMERGENCY DESCENT DEVICE PER AMM 25-61-03. NO DEFECTS NOTED. PART EFFECTIVITY VERIFIED PER IPC 25-61-03-02.
) - [SDR UIEA2024111701095](https://openairdocs.org/sdr/UIEA2024111701095.md): Warning Light · abnormal · Nov 17, 2024 · N1381A · Boeing 767316 · Trailing Edge Flap Control System > LOW-SPEED RTO DUE TO CONFIG WARN FLASPS M/S SET WITH FLAPS RESET SYS OPS NORMAL(PERFORMED FLAPS SYS TEST PER 767 AMM 27-51-00, OPS CKS NORMAL, NO FAULTS NOTED
) - [SDR UIEA2023112600971](https://openairdocs.org/sdr/UIEA2023112600971.md): Idg · unknown · Nov 25, 2023 · N1381A · Boeing 767316 · AC Generator-Alternator > "L GEN DRIVE" EICAS AT FL240, MESSAGE BLANKED BEFORE PERFORMING ENG CHECKLISTS STEPS. (APU WAS PREVIOUSLY PLACED ON DEFERRAL)(REMOVED AND REPLACED LH RNG IDG IAW AMM 24-11-01. NO FURTHER DEFECTS NOTED.
) - [SDR UIEA2023111400940](https://openairdocs.org/sdr/UIEA2023111400940.md): Support · unknown · Nov 16, 2023 · N1381A · Boeing 767316 · Fuselage Miscellaneous Structure > FUDELAGE BULK CARGO COMPARTMENT LOWER SILL INNER CHORD BETWEEN STA 1417 / STA 1461 WITH CORROSION.(INNER CHORD WAS REPLACED PER BOEING DWG 146T8210. NO FURTHER DEFECTS NOTED.
) - [SDR UIEA2023111400942](https://openairdocs.org/sdr/UIEA2023111400942.md): Floor Support · unknown · Nov 16, 2023 · N1381A · Boeing 767316 · Fuselage Miscellaneous Structure > FUSELAGE BULK CARGO COMPARTMENT FLOOR PANEL SUPPORT BETWEENÂ STA 1540 & STGR 34 / 35 RH CORROSION DAMAGE.(FUESELAGE BULK CGO COMPARTMENT FLOOR PANEL SUPPORT WAS REPLACED PER DWG 146T5004. NO FURTHER DEFECTS NOTED.
) - [SDR UIEA2023111400943](https://openairdocs.org/sdr/UIEA2023111400943.md): Unknown · unknown · Nov 16, 2023 · N1381A · Boeing 767316 · Vertical Stabilizer, Plate/Skin > LEFT SKIN PANEL 175T2001-3 OF VERTICAL STABILIZER LOCATED BETWEEN AUXILIARY SPAR AND FRONT SPAR AND FSS 92.5 / FSS 270 DELAMINATION.(LH VERTICAL STABILIZER WAS REPAIRED PER CMA-TLS-23-0150-15B. NO FURTHER DEFECTS NOTED
) - [SDR UIEA2023111400944](https://openairdocs.org/sdr/UIEA2023111400944.md): Unknown · unknown · Nov 16, 2023 · N1381A · Boeing 767316 · Vertical Stabilizer, Plate/Skin > RIGHT SKIN PANEL 175T2001-4 OF VERTICAL STABILIZER LOCATED BETWEEN AUXILIARY SPAR AND FRONT SPAR AND FSS 92.5 / FSS 270.(VERTICAL STABILIZER WAS REPAIRED PER CMA-TLS-0150-15B. NO FURTHER DEFECTS NOTED.
) - [SDR UIEA2023111400945](https://openairdocs.org/sdr/UIEA2023111400945.md): Unknown · unknown · Nov 16, 2023 · N1381A · Boeing 767316 · Cargo/Baggage Doors > AFT CARGO COMPT DOOR LOCKOUT TORQUE TUBE WITH CORROSION.(CORROSION WAS CLEANED PER AMM 52-35-00-622-074 REV. NO FURTHER DEFECTS NOTED.
) - [SDR UIEA2023111400946](https://openairdocs.org/sdr/UIEA2023111400946.md): Floorbeam · unknown · Nov 16, 2023 · N1381A · Boeing 767316 · Fuselage Main, Floor Beam > BULK CARGO COMPARTMENT RIGHT SIDE, STA 1480 BETWEEN STGR29 RH & STGR32 RH SUPPORTS FLOOR PANEL(SUPPORT FLOOR PANEL WAS REPLACED PER DWG 146T1032. NO FURTHER DEFECTS NOTED
) - [SDR UIEA2023111400947](https://openairdocs.org/sdr/UIEA2023111400947.md): Floor Support · unknown · Nov 16, 2023 · N1381A · Boeing 767316 · Fuselage Miscellaneous Structure > BULK CARGO COMPARTMENT RIGHT SIDE, STA 1502 & STGR32 RH SUPPORT FLOOR PANEL(SUPPORT FLOOR PANEL WAS REPLACED PER SRM 51-10-02-0G-0. NO FURTHER DEFECTS NOTED.
) - [SDR UIEA2023111400948](https://openairdocs.org/sdr/UIEA2023111400948.md): Floorbeam · unknown · Nov 16, 2023 · N1381A · Boeing 767316 · Fuselage Main, Floor Beam > AFT CARGO COMPARTMENT RH, INTERNAL STRUCTURE BTW STA 1417 AND STGR 27RH, SUPPORT FLOOR PANEL WITH CORROSION.(SUPPORT FLOOR PANEL WAS REPLACED PER DWG 146T1032. NO FURTHER DEFECTS NOTED
) - [SDR UIEA2023111400949](https://openairdocs.org/sdr/UIEA2023111400949.md): Floorbeam · unknown · Nov 16, 2023 · N1381A · Boeing 767316 · Fuselage Main, Floor Beam > AFT CARGO COMPARTMENT RH, INTERNAL STRUCTURE STA 1395 BETWEEN STGR 28RH & STGR 26RH, SUPPORT FLOOR PANEL WITH CORROSION.(SUPPORT FLOOR PANEL WAS REPLACED PER DWG 453T1031. NO FURTHER DEFECTS NOTED.
) - [SDR UIEA2023111400950](https://openairdocs.org/sdr/UIEA2023111400950.md): Unknown · unknown · Nov 16, 2023 · N1381A · Boeing 767316 · Wing, Plate/Skin > RH WING BS 486.2 LOWER SURFACE CORROSION.(DAMAGES WAS REWORKED PER TRE6757220. NO FURTHER DEFECTS NOTED.
) - [SDR UIEA2023111400951](https://openairdocs.org/sdr/UIEA2023111400951.md): Nut · unknown · Nov 16, 2023 · N1381A · Boeing 767316 · Aircraft Fuel System > LH WING FILL PORT ADAPTER NUT WITH GALVANIC CORROSION(ADAPTER NUT WAS REPLACED PER AMM TASK 28-11-01-404-019. NO FURTHER DEFECTS NOTED.
) - [SDR UIEA2023111400952](https://openairdocs.org/sdr/UIEA2023111400952.md): Nut · unknown · Nov 16, 2023 · N1381A · Boeing 767316 · Wing Structure > LH WING FILL PORT ADAPTER NUT WITH GALVANIC CORROSION(ADAPTER NUT WAS REPLACED PER AMM TASK 28-11-04-404-019. NO FURTHER DEFECTS NOTED.
) - [SDR UIEA2023111740953](https://openairdocs.org/sdr/UIEA2023111740953.md): Failsafe · unknown · Nov 16, 2023 · N1381A · Boeing 767316 · Fuselage Main, Structure > LOWER FUSELAGE LOBE INTERIOR, EXFOLATION ON FAIL SAFE CHORD AFT FRAME WEB AT STA 1562 BL 0.(FAIL-SAFE LOWER CHORD WAS REPLACED PER DWG 146T1223. NO FURTHER DEFECTS NOTED
) - [SDR UIEA2023111740954](https://openairdocs.org/sdr/UIEA2023111740954.md): Failsafe · unknown · Nov 16, 2023 · N1381A · Boeing 767316 · Fuselage Main, Structure > THE FAIL-SAFE STRAP UNDER THE T-FITTING ON THE RIGHT SIDE WITH CRACK INDICATION(FAIL-SAFE STRAP WAS REPAIRED PER EO 6753A070/001. NO FURTHER DEFECTS NOTED.
) - [SDR UIEA2023111740955](https://openairdocs.org/sdr/UIEA2023111740955.md): Unknown · unknown · Nov 16, 2023 · N1381A · Boeing 767316 · Wing, Plate/Skin > CANTED AREA STA. 955 BETWEEN LBL 87/LBL 91 UPPER SKIN EXTERIOR SIDE(DAMAGE WAS REPAIRED PER CMA-TLS-23-0154-04B. NO FURTHER DEFECTS NOTED.
) - [SDR UIEA2023111740956](https://openairdocs.org/sdr/UIEA2023111740956.md): Unknown · unknown · Nov 16, 2023 · N1381A · Boeing 767316 · Fuselage Miscellaneous Structure > AFT FUSELAGE STA 1725.5 CRACK FOUND ON THE BULKHEAD OUTER CHORD STRAP AND SKIN ABOVE STR-7R(DAMAGE WAS REPAIRED PER SRM 53-80-01-2R-5. NO FURTHER DEFECTS NOTED.
) - [SDR UIEA2023111400957](https://openairdocs.org/sdr/UIEA2023111400957.md): Unknown · unknown · Nov 16, 2023 · N1381A · Boeing 767316 · Cargo/Baggage Doors > MAIN DECK CARGO DOOR AFT FRAME MID SPAN LATCH CAM WITH WEAR.(DAMAGE WAS REPAIRED PER CMA-TLS-23-0164-02B. NO FURTHER DEFECTS NOTED.
) - [SDR UIEA2023111400958](https://openairdocs.org/sdr/UIEA2023111400958.md): Unknown · unknown · Nov 16, 2023 · N1381A · Boeing 767316 · Spoilers > LH WING PUNCTURE IN LOWER SKIN SPOILER # 6.(DAMAGE WAS REPAIRED PER CMA-TLS-23-0162-05B. NO FURTHER DEFECTS NOTED
) - [SDR UIEA2023111400959](https://openairdocs.org/sdr/UIEA2023111400959.md): Floorbeam · unknown · Nov 16, 2023 · N1381A · Boeing 767316 · Fuselage Main, Floor Beam > SECTION 41 FLOOR STRUCTURE, CRACK ON STIFFENER LOCATED ON REAR FACE OF FLOOR BEAM STA 246 APROX LBL 48.(ANGLE WAS REPLACED PER FCVI EO 23214-1. NO FURTHER DEFECTS NOTED.
) - [SDR UIEA2023082400796](https://openairdocs.org/sdr/UIEA2023082400796.md): Unknown · unknown · Aug 24, 2023 · N1381A · Boeing 767316 · Fire Protection System > RED 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(UPON BLOCK IN OF A/C, NO INDICATIONS O - [SDR UIEA2023013070088](https://openairdocs.org/sdr/UIEA2023013070088.md): Lamp · inoperative · Jan 27, 2023 · N1381A · Boeing 767316 · Emergency Lighting > EMERGENCY LIGHT BY FWD OF L1 DOOR INOP.(
RELAMPED, OPS CHECK NORMAL IAW AMM 33-51-03.
) - [SDR UIEA2022050200427](https://openairdocs.org/sdr/UIEA2022050200427.md): Keelbeam · corroded · May 3, 2022 · N1381A · Boeing 767316 · Fuselage Structure (General) > KEELBEAM ON HYD GROUND SERVICE DISCONNECT CENTER RETURN DOUBLER HAS CORROSION(REMOVED, FABRICATED NEW, AND INSTALLED NEW KEEL BEAM ON HYD GROUND SERVICE DISCONNECT CENTER RETURN DOUBLER IAW B767 SRM 51-40-02, 51-40-05, ATLAS GMM 3.39.2, A
- [SDR UIEA2021102202274](https://openairdocs.org/sdr/UIEA2021102202274.md): None · none · Oct 22, 2021 · N1381A · Boeing 767316 · Fuel Boost Pump
> "L ENG FUEL VALVE" EICAS AFTER ENGINE SHUTDOWN.( PERFORMED SPAR OPS CHECK SYSTEM, NO DEFECT NOTED AT THIS TIME AND ENGINE VALVE NO DEFECTS NOTED IAW AMM 28-22-01.