Boeing 767-3Y0

Service difficulty reports · 1,443

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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 = '7673Y0'
  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 UIEA2026012900019Tape · damagedFIRST OBSERVER ELT TAPE IS DAMAGED(<P>RESECURED TAPE AS PER HONEYWELL CMM JOB TASK 25-60-10. NO FURTHER DEFECTS NOTED</P>)Jan 29, 2026 · N642GT · Boeing 7673Y0 · Emergency Locator BeaconSDR UIEA2026012900020Fitting · wrong partLAVATORY PORTABLE O2 BOTTLE MASK HAS INCORRECT FITTING TO ATTACH TO O2 BOTTLE.(<P>REMOVED & REPLACED O2 MASK ASSY IAW AMM 35-31-00. OPS CHK OK.THIS CLEARS MDDR 246793. </P>)Jan 28, 2026 · N642GT · Boeing 7673Y0 · Portable Oxygen SystemSDR UIEA2026012000015Elt · inoperativeELT LOCATED RT AFT OF OBSERVERS SEAT INOP. REQ REPLACEMENT(<P>R/R ELT FROM RH AFT OF OBSERVERS SEAT IAW B767 AMM 25-26-03. NO DEFECTS NOTED</P>)Jan 15, 2026 · N1619A · Boeing 7673Y0 · Emergency Locator BeaconSDR UIEA2025122701359Elt · looseELT NEAR RH CB PANEL TAPE IS LOOSE & 1 LATCH WILL NOT CLOSE. INSTALLED TAMPER TAPE ON FWD ELT IAW AMM 25-61-05-200-801. NO DEFECTS NOTED.Dec 27, 2025 · N1619A · Boeing 7673Y0 · Emergency Locator BeaconSDR UIEA2025121501345Stowage Box · no testDURING PREFLIGHT, FOUND OBS SEAT O2 MASK DOES NOT RESET DURING TEST. R & R OBSERVER'S O2 MASK ASSY IAW AMM 35-11-51 & IPC 35-11-51. OPS & LEAK CHECK GOOD AT THIS TIME.Dec 11, 2025 · N642GT · Boeing 7673Y0 · Crew Oxygen SystemSDR UIEA2025112601326Elec Connector · damagedGEAR DISAGREE, GEAR DOORS EICAS MESSAGE AFTER GEAR UP SELECTION. PERFORMED PSEU LDG SYS 1 & 2. NO FAULT FOUND IAW AMM 32-09-04-204-013. PERFORMED PSEU LDG SYS 1 & 2, NO FAULTS FOUND IAW AMM 32-09-04-204-013. INSTALLED & REMOVED RT MAIN GEAR PIN ON SIDE BRNov 26, 2025 · N642GT · Boeing 7673Y0 · Landing Gear System WiringSDR UIEA2025112501325Pseu · faultedRH LANDING GEAR TOOK EXCESSIVELY LONG TO EXTEND AND / OR RH MAIN GEAR TO ILLUMINATE, LH AND NOSE GREEN LIGHTS WERE THE ONLY LIGHTS FOR 5-6 SECONDS. AT GEAR UP SELECTION, RECEIVED GEAR DISAGREE EICAS CAUTION MSG, GEAR DOORS EICAS ADVISORY MSG, AND A LDG GEAR MONov 22, 2025 · N642GT · Boeing 7673Y0 · Landing Gear Position and WarningSDR UIEA2025102001275Engine · no discrepancyON TAKE OFF ROLL, RECEIVED LT & RT ENG BLEED EICAS MSG & MASTER CAUTION LIGHT. RTO, PERFORMED BITE TEST IAW FIM 36-20 FT 804. FOUND 0 MSG ON THIS FLT LEG. EICAS MSG CLEARED. ALSO, PERFORMED WEU TEST IAW AMM 31-51-00, OPS CHK GOOD. FOUND MSG TO BE NORMAL.Oct 20, 2025 · N1619A · Boeing 7673Y0 · Central WarningSDR UIEA2025101001264Shutoff Valve · faultedC HYD SYS PRESS EICAS MESSAGE DISPLAYED IN FLIGHT, HMG INOP. HYD PRESS INDICATION OPERATES NORMAL PER AMM 29-31-00-001. PERFORMED ADP SYS TEST PER B767 AMM 29-11-00. NO DEFECTS NOTED. TRANSFER TO DMI 239843 PER MEL 24-25-01-01D CAT A. R & R SOV PER AMM 24-2Oct 10, 2025 · N1619A · Boeing 7673Y0 · Hydraulic Indicating SystemSDR UIEA2025101001266Regulator · leakingPAX OXYGEN TANK (BOTTLE 2) REGULATOR LEAK(<P>REMOVED AND REPLACED PAX OXYGEN TANK REGULATOR IAW B767 AMM 35-11-03. LEAK & PRESSURE CHK OK</P>)Oct 9, 2025 · N1619A · Boeing 7673Y0 · Crew Oxygen SystemSDR UIEA2025090801169Hook And Loop · damagedHOOK AND LOOP FOR EVAS ON CAPT SIDE NEEDS TO BE ATTACHED. EVAS IS SECURED WITH BOLTS. NO HOOK AND LOOP ON EVAS IAW AMM 25-60-99. NO FURTHER DEFECTS NOTEDSep 8, 2025 · N642GT · Boeing 7673Y0 · Emergency EquipmentSDR 21GA20250906018Warning Message · false activationON APPROACH, SELECTED FLAPS TO 20. RECEIVED TE FLAP DISAGREE EICAS MESSAGE. DID GO AROUND, DECLARED EMERGENCY, AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED FIM PROCEDURE. NO DEFECTS NOTED.Aug 29, 2025 · N1181A · Boeing 7673Y0 · Trailing Flap Position Indicating SystemSDR UIEA2025080401084Flashlight · no discrepancyL1 DOOR ENTRY WAY EMERGENCY FLASHLIGHT INOPERATIVE. OPS CHK ENTRY WAY FLASHLIGHT IAW AMM 25-05-03, OPS CHECK GOOD.Aug 4, 2025 · N1619A · Boeing 7673Y0 · Emergency EquipmentSDR UIEA2025073001069Lens · scratchedOBSERVER SMOKE GOGGLES LENS SCRATCHED. REPLACED OBS SMOKE GOGGLE PER IPC 25-64-54-01B ITEM 30. NO FURTHER DEFECTS NOTED.Jul 30, 2025 · N1619A · Boeing 7673Y0 · Emergency EquipmentSDR UIEA2025071100925Structure · no discrepancyAT APPROXIMATELY 310 KIAS, APPROXIMATELY 10 KNOTS OVERSPEED WITH OVSPD WARNING WHILE IN DESCENT 0 FLAPS ADVISE FLT LEVEL 200. WORK WITH MCC AND PER AMM 05-51-08. COMPLETED PHASE 1 INSPECTION, NO DAMAGE WAS FOUND. LOG ITEM CLOSED.Jul 11, 2025 · N1619A · Boeing 7673Y0 · Standard Practices/StructuresSDR UIEA2025070400832Fmc · odorCAPT REPORTS ELECTRICAL ODOR IN COCKPIT AFTER BLOCK, DETERMINED CAPT FMS CDU BLANKED AND CIRCUIT BREAKER OPEN.(<P>COLLARED CIRCUIT BREAKER, PART ORDERED FOR NGO. REPLACED CA FMC CDU IAW AMM 34-61-02. CLEARED MDDR 233639. NO FURTHER DEFECTS NOTED.</P>)Jul 4, 2025 · N1619A · Boeing 7673Y0 · Flight Management Computing Hardware SystemSDR UIEA2025030600213Structure · damagedDAMAGE TO AFT LOWER CORNER OF FWD CARGO DOOR, CW SRM 5230011A1. PERMANENT REPAIR OF DOOR REQUIRED AT THE NEXT CHECK OR BEFORE 24 MONTHS.(<P>CRACK WAS REPAIRED IAW TRE6752055 & CMA-TLS-25-0009-05B. NO FURTHER DEFECTS NOTED.</P>)Mar 24, 2025 · N642GT · Boeing 7673Y0 · Cargo/Baggage DoorsSDR UIEA2025030600214Actuator · out of limitsDURING ELEVATOR SURFACE FREE PLAY FUNTIONAL CHECK, ELEVATOR RH, OUTBOARD POWER CONTROL ACTUATOR OUT OF LIMITS.(<P>POWER CONTROL ACTUATOR WAS REPLACED, TEST FOR LEAKS AND ADJUSTMENTS WAS PERFORMED IAW AMM 27-31-05-424-027 REV 144. OPS CHECK GOOD.</P>)Mar 24, 2025 · N642GT · Boeing 7673Y0 · Elevator Control SystemSDR UIEA2025030600217Actuator · out of limitsDURING ELEVATOR SURFACE FREE PLAY FUNTIONAL CHECK, ELEVATOR LH, OUTBOARD POWER CONTROL ACTUATOR OUT OF LIMITS.(<P>POWER CONTROL ACTUATOR WAS REPLACED, TEST FOR LEAKS AND ADJUSTMENT WAS PERFORMED IAW AMM 27-31-05-424-027 REV 144. OPS CHECK GOOD.</P>)Mar 24, 2025 · N642GT · Boeing 7673Y0 · Elevator Control SystemSDR UIEA2025030600219Actuator · leakingRH WING SPOILER #12 WITH LEAK.(<P>POWER CONTROL ACTUATOR SPOILER #12 WAS REPLACED IAW AMM 27-61-02-424-023 REV 144. LEAK CHECK AND ADJUSTMENT WAS PERFORMED IAW AMM 27-60-00-825-072 REV 144. NO LEAK FOUND, SPOILER 12 IS GOOD FOR SEVICE.</P>)Mar 24, 2025 · N642GT · Boeing 7673Y0 · Drag Control ActuatorSDR UIEA2025030600220Skin · crackedFWD ENTRY DOOR, AFT LOWER CORNER, HOLE 4 WITH CRACK INDICATION ON BEAR STRAP APPROX 10 O'CLOCK, AND HOLE 5 WITH CRACK INDICATION ON SKIN AND BEAR STRAP APPROX 10 O'CLOCK, 4 AND 11 O'CLOCK.(<P>CRACK WAS REPAIRED IAW 8017-0731_6753A-937_PART (1-2) REV 1 & SRM 51Mar 24, 2025 · N642GT · Boeing 7673Y0 · Fuselage Main, Plate/SkinSDR UIEA2025030600221Skin · crackedSERVICE DOOR, AFT LOWER CORNER, HOLE 5 WITH CRACK INDICATION ON SKIN AND BEAR STRAP APPROX 2 AND 8 O'CLOCK.(<P>CRACK WAS REPAIRED IAW 8017-0731_6753A-937_PART (1-2) REV 1 & SRM 51-40-02-0G-0 REV 127. NO FURTHER DEFECTS NOTED.</P>)Mar 24, 2025 · N642GT · Boeing 7673Y0 · Fuselage Main, Plate/SkinSDR UIEA2025030600222Lamp · inoperativeEMERGENCY LIGHTS OF THE CABIN LH INOP.(<P>TASK CARD A-06-040-01/002 EMERGENCY LIGHTS OF THE CABIN LH, LAMPS WERE REPLACED IAW AMM 33-22-01 DATE. 10MAY10. TEST WAS PERFORMED SATISFACTORY.</P>)Mar 24, 2025 · N642GT · Boeing 7673Y0 · Emergency LightingSDR UIEA2025030800224Sign · looseEMERGENCY LIGHT SIGN ENTERING THE CABIN, SCREWS LOOSE (2 EACH).(<P>TASK CARD A-06-040-01/004 EMERGENCY LIGHT SIGN ENTERING THE CABIN, SCREWS LOOSE. TWO SCREWS WERE INSTALLED CORRECTLY IAW AMM 33-51-01-412-003 REV 144 DATE 22DEC24. NO FURTHER DEFECTS NOTED.</P>Mar 24, 2025 · N642GT · Boeing 7673Y0 · Emergency LightingSDR UIEA2025030800225Actuator · leakingLH WING SPOILER ACTUATOR #2, WITH LEAK EVIDENCE.(<P>POWER CONTROL ACTUATOR SPOILER #2 WAS REPLACED IAW AMM 27-61-02-424-023 REV 144. LEAK CHECK AND ADJUSTMENT WAS PERFORMED IAW AMM 27-61-00-825-072 REV 144. NO LEAK FOUND, SPOILER 2 IS GOOD FOR SERVICE.</P>)Mar 24, 2025 · N642GT · Boeing 7673Y0 · Drag Control ActuatorSDR UIEA2025030800226Skin · corrodedRH WING INBOARD TE FLAP, CORROSION ON LOWER SKIN.(<P>RH WING INBOARD TE FLAP, LOWER SKIN WAS REPAIRED IAW TRE 6757282 RI ISSUED 13MAR25, AND FAA FORM 8100-9 (2-02) DATE 21MAR25. NO FURTHER DEFECTS NOTED</P>)Mar 24, 2025 · N642GT · Boeing 7673Y0 · Trailing Edge FlapsSDR UIEA2025030800227Feel Unit · leakingLEAKAGE AT ELEVATOR FEEL UNIT IN HORIZONTAL STABILIZER TORSION BOX COMPARTMENT, LH SIDE.(<P>LEAKAGE AT ELEVATOR FEEL UNIT IN HORIZONTAL STABILIZER TORSION BOX COMPARTMENT, LH SIDE. ELEVATOR FEEL UNIT WAS REPLACED AND TEST WAS PERFORMED IAW AMM 27-31-19-424-015Mar 24, 2025 · N642GT · Boeing 7673Y0 · Elevator Control SystemSDR UIEA2025030800229Fuel Tank · leakingLH WING, LOWER EXTERNAL SURFACE, BTW OUTB AND MAIN TANK, STRG 6, AT SPLICE, FUEL LEAK.(<P>MAIN TANK STRG 6 AT SPLICE LH SIDE SEALANT WAS REMOVED, AREA CLEANED AND SEALANT PS 890A2, NSL 890B 1/2 APPLIED IAW 28-11-00-308-013 REV 144. FUEL LEAK TEST WAS SATISFACTMar 24, 2025 · N642GT · Boeing 7673Y0 · Fuel StorageSDR UIEA2025030800231Fuel Tank · leakingLH WING, LOWER EXTERNAL SURFACE, BTWN OUTB AND MAIN TANK, STRG 10, AT SPLICE, FUEL LEAK.(<P>MAIN TANK STRG 10 AT SPLICE LH SIDE SEALANT WAS REMOVED, AREA CLEANED AND SEALANT NSL 890A2, NSL 890B 1/2 APPLIED IAW 28-11-00-308-013 REV 144. FUEL LEAK TEST WAS SATISMar 24, 2025 · N642GT · Boeing 7673Y0 · Fuel StorageSDR UIEA2025030800236Fuel Tank · leakingLH WING, LOWER EXTERNAL SURFACE, BTWN OUTB AND MAIN TANK, STRG 15, AT SPLICE, FUEL LEAK.(<P>MAIN TANK STRG 15 AT SPLICE LH SIDE SEALANT WAS REMOVED, AREA CLEANED AND SEALANT NSL 890A2, NSL 890B 1/2 APPLIED IAW 28-11-00-308-013 REV 144. FUEL LEAK TEST WAS SATISMar 24, 2025 · N642GT · Boeing 7673Y0 · Fuel StorageSDR UIEA2025030800239Skin · corrodedUPPER FUSELAGE SURFACE WITH CORROSION AT THE BASE OF THE TOP TCAS ANNTENA.(<P>UPPER FUSELAGE SURFACE CORROSION AT THE BASE OF THE TOP TCAS ANNTENA. REPAIR WAS PERFORMED IN ACCORDANCE WITH TRE6753716 FEB 24, 2025. FVC TITLE REPAIR- FUSELAGE SKIN- CROWN AREA-CORMar 24, 2025 · N642GT · Boeing 7673Y0 · Fuselage Main, Plate/SkinSDR UIEA2025030800242Transmitter · faultedTRANSMITER POSITION FLAPS M489 LOW INSULATION RESISTANCE.(<P>FLAP POSITION TRANSMITTER M489 WAS REPLACED IAW AMM 27-51-45-422-030 REV 144. FLAP POSITION TRANSMITTER M489 ADJUSTED AND TEST PERFORMED IAW AMM 27-51-45-822-161 REV 144. NO FURTHER DEFECTS NOTED.</PMar 24, 2025 · N642GT · Boeing 7673Y0 · Trailing Flap Position Indicating SystemSDR UIEA2025030800245Skin · dentedLOWER HALF OF FUSELAGE, BTW STA 654+44 AND 654+66, BTW STR 34L AND 33L, DENT ON SKIN.(<P>THE DENT WAS EVALUATED AND FOUND OUT OF LIMIT. IT WAS REPAIRED IAW SRM 53-00-01-2R-29 REPAIR 29. NO FURTHER DEFECTS NOTED.</P>)Mar 24, 2025 · N642GT · Boeing 7673Y0 · Fuselage Main, Plate/SkinSDR UIEA2025031100258Servo · leakingVERTICAL STABILIZER WITH EVIDENCE OF HYDRAULIC LEAK IN BOTH YAW DAMPER SERVOS.(<P>YAW DAMPER SERVOS LH AND RH WERE REPLACED IAW AMM 22-21-02-414-016 REV 144. (OFF PART RH PN: 1540500-9 SN: 973BC, LH PN: 1536600-5 SN: 1856BA) INSTALLATION TEST WAS SATISFACTORY.Mar 24, 2025 · N642GT · Boeing 7673Y0 · Autopilot SystemSDR UIEA2025031100259Actuator · leakingVERTICAL STABILIZER WITH EVIDENCE OF HYDRAULIC LEAK IN SERVO VALVE.(<P>RUDDER RATIO CHANGER ACTUATOR WAS REPLACED I.A.W AMM 27-21-15-422-024 OPERATONAL TEST WAS PERFORMED AND NO LEAKS FOUND, TORQUE APPLIED 280 LB-IN, 360 LB-IN S/N 0823114404 DATE 12DEC2026.</PMar 24, 2025 · N642GT · Boeing 7673Y0 · Rudder Control SystemSDR UIEA2025031800355Skin · corrodedVERTICAL STABILIZER TIP LEADING EDGE WITH CORROSION L=5.0" W=4.00".(<P>VERTICAL STABILIZER TIP LEADING EDGE WITH CORROSION L=5.0" W=4.00".THE VERTICAL STABILIZER LEADING EDGE TIP HAS BEEN REPLACED. NO FURTHER DEFECTS NOTED</P>)Mar 24, 2025 · N642GT · Boeing 7673Y0 · Vertical Stabilizer, Plate/SkinSDR UIEA2025031800356Skin · corrodedVERTICAL STABILIZER TIP REMOVABLE LEADING EDGE WITH CORROSION L= 4.0" W= 3.5 " (ACCESS PANEL 326A).<BR>(<P>VERTICAL STABILIZER TIP REMOVABLE LEADING EDGE WITH CORROSION L= 4.0" W= 3.5 " (ACCESS PANEL 326A) WAS REPLACED IAW SRM 51-10-02-0G-0 REV. 127 15-DEC-24.Mar 24, 2025 · N642GT · Boeing 7673Y0 · Vertical Stabilizer, Plate/SkinSDR UIEA2025032100365Stowage Box · no testDMI 225437 PASSENGER #3 OXIGEN MASK REST SWITCH DOESN'T TEST. SEAT NOT ALLOWED TO BE OCCUPIED.(<P>STOWAGE BOX WAS REPLACED IAW AMM 35-11-51-400-803-001 REV 144, 22DEC2024 AND TEST WAS SATISFACTORY. NO FOUND LEAKS.</P>)Mar 24, 2025 · N642GT · Boeing 7673Y0 · Passenger Oxygen SystemSDR UIEA2025032100366Skin · dentedRH WING, INBOARD TRAILING EDGE FLAP, LOWER SECTION, OUTER SKIN WITH DENTS.(<P>RH WING, AFT FLAP - INBOARD TRAILING EDGE FLAP, LOWER SECTION, OUTER SKIN WAS REPAIRED IAW SRM 57-53-01-2R-1 FIG.201 SHEET 4 PAG.2,5 AND SRM 51-70-10- 2R-4 FIG.201 SHEET 1 PAG.1,3,7 Mar 24, 2025 · N642GT · Boeing 7673Y0 · Trailing Edge FlapsSDR UIEA2025032100367Skin · dentedRIGHT WING INBD FLAP UPPER AND LOWER SKIN WITH SEVERAL DENTS.(<P>RH WING, AFT FLAP - INBOARD TRAILING EDGE FLAP, LOWER SECTION, OUTER SKIN WAS REPAIRED IAW SRM 57-53-01-2R-1 FIG.201 SHEET 4 PAG.2,5 AND SRM 51-70-10- 2R-4 FIG.201 SHEET 1 PAG.1,3,7 REV.127 15 DEMar 24, 2025 · N642GT · Boeing 7673Y0 · Trailing Edge FlapsSDR UIEA2025032100368Skin · delaminatedRH WING, OUTBOARD FLAP, LOWER SURFACE, 9" TO 24" FROM INBOARD EDGE AND 23.5" TO 34" FROM LEADING EDGE, DELAMINATION.(<P>RH WING, OUTBOARD FLAP, LOWER SURFACE WAS REPAIRED I.A.W B767 SRM 57-53-01-2R-1 AND SRM 51-70-10-2R-4 PAG 1,4 FIG 201 SHEET 3 REV 127 15-DECMar 24, 2025 · N642GT · Boeing 7673Y0 · Trailing Edge FlapsSDR UIEA2025032100369Fuel Line · damagedCREASE ON APU FUEL SHROUD LINE AT STA 1646, LH SIDE.(<P> APU FUEL SHROUD LINE WAS REPLACED. IAW AMM 28-25-05-404-084 REV 144. DEC 22, 2024. TORQUE APPLIED ON CLAMPS: 24 LB IN. S/N: 0224110483. DATE: 11-MAY-25 BONDI NG TEST 0.5 MILLIHOMS SN: B0005830 DATE: 04-JMar 24, 2025 · N642GT · Boeing 7673Y0 · Aircraft Fuel Distribution SystemSDR UIEA2025032100370Fuel Line · damagedCREASE ON APU FUEL SHROUD LINE AT STA 1720.5, LH SIDE.(<P>APU FUEL SHROUD LINE WAS REPL ACED. IAW AMM 28-25-05-404-084 REV 144. DEC 22, 2024. TORQUE APPLIED ON CLAMPS: 24 LB IN. S/N: 0224110483. DATE: 11-MAY-25 BONDING TEST 0.5 MILLIHOMS SN B0005830 DATE: 04-JMar 24, 2025 · N642GT · Boeing 7673Y0 · Aircraft Fuel Distribution SystemSDR UIEA2025032100371Fuel Line · bentACCESS PANEL 197DL, FUEL LINE BENT.(<P>ACCESS PANEL 197DL, FUEL LINE WAS REPLACED. IAW AMM 28-13-06-404-005. REV 144. DEC 22, 2024. NO MORE ACTIONS REQUIRED. GOOD FOR SERVICE.</P>)Mar 24, 2025 · N642GT · Boeing 7673Y0 · Aircraft Fuel Distribution SystemSDR UIEA2025032100372Anti-Skid Valve · no testMLG, WHEEL #5, BRAKE UNIT, WHEN TEST WAS BEING PERFORMED, THE RECORDED PRESSURE WAS LOWER THAN PERMITTED.(<P>ANTISKID VALVE OF BRAKE #5 WAS REPLACED. IAW AMM 32-42-03-404-017. REV 144. DEC 22, 2024. TORQUE APPLIED: 105 LB IN. S/N: 0524121903. DATE: 15-MAY-25. Mar 24, 2025 · N642GT · Boeing 7673Y0 · Brake Anti-Skid SectionSDR UIEA2025032200376Skin · corrodedRH WING INBOARD TE FLAP, CORROSION LOWER SKIN.(<P>RH WING INBOARD TE FLAP, LOWER SKIN WAS REPAIRED IAW TRE 6757282 R1 ISSUED 13MAR25, AND FAA FORM 8100-9 (2-02) DATE 21MAR25. NO FURTHER DEFECTS NOTED</P>)Mar 24, 2025 · N642GT · Boeing 7673Y0 · Trailing Edge FlapsSDR UIEA2025020500119Oxygen Mask · inoperativePASSENGER #3 OXYGEN MASK INOP.(<P>TRANSFER TO DMI 225437 PER MEL 35-11-03-02A CAT C DUE DATE 15FEB25</P> / <P>LP 1810355 ITEM M10, 21MAR25: STOWAGE BOX WAS REPLACED IAW AMM 35-11-51-400-803-001. TEST SATISFACTORY, NO FOUND LEAKS. IPC 35-11-52-15 REV 76 22FEB25Feb 5, 2025 · N642GT · Boeing 7673Y0 · Passenger Oxygen SystemSDR UIEA2025012600108Elt · abnormalELT AT ENTRANCE HAS MASKING TAPE OVER THE WATER SOLUABLE TAPE(<P>R/R L1 DOOR L1 & BRACKET STRAP OPS CHK GOOD IAW AMM 25-63-03-400-802 & AIPC 25-63-52-97. DMI 224932 CLOSED</P>)Jan 27, 2025 · N1619A · Boeing 7673Y0 · Emergency Locator BeaconSDR UIEA2024120301162Seal · damagedRIGHT O/B T/E FLAP WITH SEAL DAMAGED AT INBOARD SIDE.(<P>REMOVED DAMAGED SEAL AT R/H O/B T/E FLAP, I/B SIDE AREA, LOCATED, CLEANED, PREPARED, SECURED AND INSTALLED NEW SEAL AS REQUIRED AT R/H O/B T/E FLAP, I/B SIDE AREA PER BOEING 767-300 AMM 57-25-01-05 & AMMDec 3, 2024 · N642GT · Boeing 7673Y0 · Trailing Edge FlapsSDR UIEA2024120301163Latch · brokenENG #2 NACELLE STRUT, INBOARD ACCESS PANEL WITH LATCH BROKEN.(<P>REMOVED DAMAGED LATCH AT ENG #2, NACELLE STRUT INBOARD ACCESS PANEL AREA, LOCATED, CLEANED, TRIMMED, SECURED, ADJUSTED, SAFETY WIRE, INSTALLED NEW LATCH AS REQUIRED AT ENG #2 NACELLE STRUT, INBOADec 3, 2024 · N642GT · Boeing 7673Y0 · Nacelle/Pylon, Main Frame
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