Boeing 767-3Y0

Service difficulty reports · 1,443

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 = '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 UIEA2024120301164Shutoff Valve · faultedLEFT TR INOP(<P>REMOVED DEFECTIVE REVERSER PRSOV REF 767-300 M/M 78-34-05-004-001-H00. OK TO INSTALL SERVICEABLE UNIT.</P> / <P>INSTALLED SERVICEABLE PRSOV REF 767-300 M/M 78-34-05-404-009-H00. INDICATOR AND OPERATION GOOD WITHOUT ENGINE OPERATING REF 767-300 Dec 3, 2024 · N642GT · Boeing 7673Y0 · Engine Thrust ReverserSDR UIEA2024112801118Shutoff Valve · faultedDURING CRUISE, RECEIVED A MASTER WARNING "CABIN ALT". COMPLIED W/ QRH. FL380. CABIN ALT 11,000' DPSI 7.0. USED MANUAL PRESSURIZATION MODE TO CONTROL & STABILIZED CABIN ALT. "CABIN AUTO INOP" CAUTION MSG. COMPLIED W/ QRH PROC. "CABIN ALT AUTO 1" AND "CABINov 28, 2024 · N642GT · Boeing 7673Y0 · Cabin Pressure Control SystemSDR UIEA2024111501092Lamp · burned outEMERGENCY LIGHTS "UNARMED" DISCRETE LIGHT HAS BURNED OUT LIGHT BULB(<P>RELAMPED EMERGENCY UNARMED LIGHT PER AMM 33-10-00. OPS CHECK NORMAL</P>)Nov 15, 2024 · N1619A · Boeing 7673Y0 · Emergency LightingSDR UIEA2024101801052Screen · cloggedATB - FWD EQUIP OVHT EICAS MSG. WENT TO STBY IAW QRH, DID NOT CLEAR. WENT TO OVRD IAW QRH, EICAS MSG CLEARED. DID NOT ENTER ETOPS(<P>FOUND EQPT COOL SUPPLY AIR INLET GRILL DIRTY AND PARTIALLY BLOCKED. CLEANED PER AMM 21-58-10. FOUND SUPPLY FAN SCREEN EQUIPMENTOct 18, 2024 · N1619A · Boeing 7673Y0 · Air Distribution SystemSDR UIEA2024101501005Attach Fitting · corrodedLH UPPER HORIZONTAL STABILIZER PIVOT FITTING ATTACHMENT WITH CORROSION(<P><SPAN DATA-OLK-COPY-SOURCE="MESSAGEBODY">REMOVE FASTENERS FROM ALTERNATE ROWS, REAM THE AFFECTED HOLES THRU THE ENTIRE STACK-UP IN 1/64 INCH INCREMENTS UNTIL FASTENER HOLE IS CLEAN, ROUNOct 17, 2024 · N642GT · Boeing 7673Y0 · Horizontal Stabilizer StructureSDR UIEA2024101501008Fuse Pin · crackedSUPPORT #6 INBOARD FLAP - FUSE PIN - UNDERWING FITTING TO FOWARD TO TENSION LINK, WITH CRACK INDICATION FOUND AND CORROSION.(<P>FUSE PIN WAS REPLACED AND TORQUE WAS APPLIED IAW AMM 27-51-02-004-001. NO FURTHER DEFECTS NOTED</P>)Oct 17, 2024 · N642GT · Boeing 7673Y0 · Trailing Edge FlapsSDR UIEA2024101501010Fuse Pin · crackedSUPPORT #3 INBOARD FLAP - FUSE PIN - UNDERWING FITTING TO FOWARD TO TENSION LINK, WITH CRACK INDICATION FOUND AND CORROSION.(<P>FUSE PIN WAS REPLACED AND TORQUE WAS APPLIED IAW AMM 27-51-02-004-001. NO FURTHER DEFECTS NOTED</P>)Oct 17, 2024 · N642GT · Boeing 7673Y0 · Trailing Edge FlapsSDR UIEA2024101501011Panel · damagedEVALUATE AND REPAIR AS REQUIRED, INDUCED DAMAGE TO RH HORIZONTAL STABILIZER T/E PANEL(<P>RH HORIZONTAL STABILIZER T/E PANEL WAS REPAIRED IAW SRM 55-10-01-2R-1 FIG 201 SHEET 4 PAGE 1-5 AND SRM 51-70-07- 0G-0 PAR 5.D FIG 11 PAG 16,37 REV 126 15/AUG/24</P>)Oct 17, 2024 · N642GT · Boeing 7673Y0 · Horizontal Stabilizer Miscellaneous StructureSDR UIEA2024101501012Pivot Assy · corrodedHORIZONTAL STABILIZER - PIVOT FITTING - UPPER ATTACHMENT - MOST OUTBOARD REAR BOLT HOLE WITH INDICATION OF CORROSION(<P>TRE6755057 WAS PERFORMED AND NIL DAMAGE FOUND, TRE6755057 WAS BASED ON OEM MESSAGES CMA-PAO-24-0103</P>)Oct 17, 2024 · N642GT · Boeing 7673Y0 · Horizontal Stabilizer Miscellaneous StructureSDR UIEA2024101501014Support Fitting · wornFLAP SUPPORT #1 FITTING OUTBOARD ACTUATOR SPAR FITTING WEAR FOUND 3 HOLES WITH CORROSION INDICATION (LOCATED 12:00, 08:00 AND 10:00 O´CLOCK)(<P>CORROSION WAS REMOVED, REAMING THE AFFECTED HOLES AND FREEZE PLUGS WERE INSTALLED. THIS REPAIR WAS BASED ON CMA-PAOct 17, 2024 · N642GT · Boeing 7673Y0 · Trailing Edge FlapsSDR UIEA2024101501017Pin · corrodedLEFT 6-6 PIN FLAP SUPPORT #4 WITH CORROSION(<P>PIN WAS REPLACED AND TORQUE WAS APPLIED IAW AMM 27-51-04-402-135. NO FURTHER DEFECTS NOTED</P>)Oct 17, 2024 · N642GT · Boeing 7673Y0 · Trailing Edge FlapsSDR UIEA2024101701042Transmitter · failedLEFT WING TRANSMITTER FLAP POSITION #1 WITH FAIL(<P>LEFT WING TRANSMITTER FLAP POSITION #1 WAS REPLACED AND TESTED IAW AMM TASK 27-51-45-422-030 REV 143 DATE 22 AUG 24, TEST OK, 50 IN LB WERE APPLIED. S/N 0818911494 DUE DATE 04 APR 25</P>)Oct 17, 2024 · N642GT · Boeing 7673Y0 · Trailing Flap Position Indicating SystemSDR UIEA2024101701050Packing · leakingFUEL LEAK IN MAIN FUEL BOOST PUMP WING RH(<P>THE PACKING AT THE MAIN FUEL BOOST PUMP WING RH WAS REPLACED. NO LEAKS WERE FOUND IAW AMM 24-22-03-004-001 AND 28-22-03-404-027 REV. 143 DATE: 22 AUG 24. TORQUE APPLIED: 55 LB-IN AND 35 LB-IN. S/N: 0821902601 DATE: Oct 17, 2024 · N642GT · Boeing 7673Y0 · AC InverterSDR UIEA2024101701051Union · leakingFUEL LEAK IN THE DENSITOMETER CONNECTOR PUMP QTY WING LH(<P>FUEL LEAK IN THE DENSITOMETER CONNECTOR PUMP QTY WING LH WAS R/R & NO LEAKS WERE FOUND IN IAW AMM 28-41-09-004-001-002 AND 28-41-09-404-028-002 REV. 143 DATE: 22 AUG 24. TORQUE APPLIED: 240 LB-IN S/N:Oct 17, 2024 · N642GT · Boeing 7673Y0 · Aircraft Fuel Distribution SystemSDR UIEA2024092400931Pdu · leakingRIGHT WING, SLAT PDU INBOARD, WITH EVIDENCE OF HYD LEAK(<P>RIGHT WING, SLAT PDU INBOARD WERE REPLACED IAW AMM 27-81-10-424-023 AND AMM 27-81-10-024-001, LEAK CHECK WERE PERFORMED, NO LEAK WAS FOUND.</P>)Sep 29, 2024 · N1619A · Boeing 7673Y0 · Hydraulic System, MainSDR UIEA2024092400932Skin · detachedRH WING, SLAT #7, SURFACE INNER SIDE, UPPER AND LOWER AREA WITH SEVERAL POINTS OF DETACHED.(<P>RH WING, SLAT #7, WAS REPLACED IAW AMM 27-81-01-024-001 AND AMM 27- 81-01-424-143. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED</P>)Sep 29, 2024 · N1619A · Boeing 7673Y0 · AileronsSDR UIEA2024092400933Skin · corrodedRH WING, SLAT #7, SURFACE INNER SIDE, AREA UPPER MIDDLE, WITH TWO POINTS OF CORROSION EVIDENCE.(<P>RH WING, SLAT #7, WAS REPLACED IAW AMM 27-81-01-024-001 AND AMM 27-81- 01-424-143. OPS CHECK GOOD</P>)Sep 29, 2024 · N1619A · Boeing 7673Y0 · Leading Edge DevicesSDR UIEA2024092400934Pca · leakingLEFT WING, OUTER AILERON, INNER PCA, WITH EVIDENCE OF HYD LEAKAGE(<P>LEFT WING, OUTER AILERON, INNER PCA, WAS REPLACED, ADJUSTED AND LEAK TEST WAS PERFORMED IAW AMM 27-11- 49-422-028 AND AMM 27-11-49-022-014. NO LEAKS WERE FOUND.</P>)Sep 29, 2024 · N1619A · Boeing 7673Y0 · Hydraulic System, MainSDR UIEA2024092400935Skin · detachedLEFT WING, LEFT INBOARD AILERON, LEADING EDGE MIDDLE AREA DETACHED.(<P>LEFT WING, INBOARD AILERON, LEADING EDGE MIDDLE AREA WAS REPAIRED IAW SRM 57-60-01-2R-1 FIG 201 SHEET 9 PAG 1-10 AND SRM 51-70-17-0G-0 PAR 4G FIG 15</P>)Sep 29, 2024 · N1619A · Boeing 7673Y0 · AileronsSDR UIEA2024092400936Fuel Cell · leakingRH WING, FUEL LEAK ON LOWER SKIN AND SPLICE BTW WBL 97.95. TO WS 226.3 AND BTW STGR L7 TO L15(<P>FUEL LEAK WAS REPAIRED AND LEAK TEST WAS SATISFACTORY IAW AMM 28-11-00-308-013</P>)Sep 29, 2024 · N1619A · Boeing 7673Y0 · Fuel StorageSDR UIEA2024092400937Fire Bottle · expiredENG 2 BOTTLE EXTINGUISHER #2 DATE OFF(<P>ENG 2 BOTTLE EXTINGUISHER #2 WAS REPLACED AND TEST WAS SATISFACTORY IAW AMM 26-21-03-424-095</P>)Sep 29, 2024 · N1619A · Boeing 7673Y0 · Fire Bottle, FixedSDR UIEA2024092400938Skin · crackedDOUBLER INSTALLED ON EMERGENCY LIGHT OF THE MCD SURROUND SKIN CIRCUMFERENTIAL SPLICE STA 654+22 AT AFT FASTENER ROW IN THE SECOND LOWER FASTENER HOLE WITH CRACK INDICATION.(<P>THE SECOND LOWER FASTENER HOLE WAS ENLARGE UP TO SECOND OVERSIZE AND WAS REPAIRED IASep 29, 2024 · N1619A · Boeing 7673Y0 · Fuselage Main, Plate/SkinSDR UIEA2024092400939Skin · crackedAT FWD ENTRY DOOR CUTOUT AFT LOWER CORNER ONE HOLE WITH CRACK INDICATION ON BOTH STRUCTURES FUSELAGE SKIN AND BEAR STRAP APPROX TO THE 10 O´CLOCK.(<P>HOLE INDICATION ON BOTH STRUCTURES FUSELAGE SKIN AND BEAR STRAP APPROX TO THE 10 O´CLOCK. CRACK WAS REPAIREDSep 29, 2024 · N1619A · Boeing 7673Y0 · Fuselage Main, Plate/SkinSDR UIEA2024092400940Skin · crackedAT FWD SERVICE DOOR CUTOUT AFT LOWER CORNER TWO HOLES WITH CRACK INDICATION ON FUSELAGE SKIN APPROX 10 O´CLOCK.(<P>AT FWD SERVICE DOOR CUTOUT AFT LOWER CORNER ON FUSELAGE SKIN APPROX 10 O´CLOCK DAMAGES WERE REPAIRED IAW FVCI #24153-2 A FAA FORM 8110-3 (09/20Sep 29, 2024 · N1619A · Boeing 7673Y0 · Fuselage Main, Plate/SkinSDR UIEA2024092400941Skin · wornLH WING, AT WBL 97.5 , BTW STA 785.9 AND STA 830 WING LOWER SKIN WITH WEAR.(<P>LH WING, AT WBL 97.5 , BTW STA 785.9 AND STA 830 WING LOWER SKIN DAMAGE WAS REPAIRED IAW FVCI #24153-3 AN APPROVAL FORM FAA 8110-3 WAS ISSUED. NO FURTHER DEFECTS NOTED</P>)Sep 29, 2024 · N1619A · Boeing 7673Y0 · Wing, Plate/SkinSDR UIEA2024092400942Seal · wornLEFT WING, OUTBD WING TIP, ANTI-COLLISION LIGHT WITH WORN SEAL(<P>THE WORN SEAL ON LEFT WING, OUTBD WING TIP, ANTI-COLLISION LIGHT WAS REPLACED IAW AMM 33-44-01-002-017. NO FURTHER DEFECTS NOTED</P>)Sep 29, 2024 · N1619A · Boeing 7673Y0 · Exterior LightingSDR UIEA2024092400943Frame · corrodedFWD CARGO COMPARTMENT, EVIDENCE OF CORROSION ON WEB FRAME AT BS 764 BTW S37L AND S38L.(<P>WEB FRAME AT BS 764 BTW S37L AND S38L. PAINT WAS REMOVED, REWORKED, INSPECTED AND ALLOWABLE LIMITS FOUND. ALLODINE, PRIMER AND PAINT WAS RESTORED IAW SRM 53-00-07-1A-1. NSep 29, 2024 · N1619A · Boeing 7673Y0 · Fuselage Main, FrameSDR UIEA2024092400944Jumper · brokenRH WING, FUEL TANK, INSIDE ACCESS PANEL 632DB, BROKEN BONDING JUMPER (2E/A'S) BTW RIB 6/7.(<P>THE BROKEN BONDING JUMPER (2E/A'S) ON RH WING, FUEL TANK, INSIDE ACCESS PANEL 632DB, BTW RIB 6/7 WERE REPLACED IAW SWPM 20-20-10 REV</P>)Sep 29, 2024 · N1619A · Boeing 7673Y0 · Wing System WiringSDR UIEA2024092400945Sealant · missingRH WING, INSIDE FUEL TANK REAR SPAR, MISSING FILLET SEALANT ON SHUT OFF VALVE (2 E/A'S) BTW RIB 1/6.(<P>RH WING, INSIDE FUEL TANK REAR SPAR, FILLET SEALANT ON SHUT OFF VALVE WAS APPLIED IAW AMM TASK 28-21-02-404-021. NO FURTHER DEFECT NOTED</P>)Sep 29, 2024 · N1619A · Boeing 7673Y0 · Wing Main, Frame StructureSDR UIEA2024092400946Actuator · leakingLH WING, LATERAL CENTRAL CONTROL ACTUATORS UPPER AND LOWER (M274 AND M276) LCCA WITH HYDRAULIC LEAK.(<P>LH WING, LATERAL CENTRAL CONTROL ACTUATORS UPPER AND LOWER (M274 AND M276) LCCA LEAK CHECK WAS PERFORMED, NO LEAKS WERE FOUND</P>)Sep 29, 2024 · N1619A · Boeing 7673Y0 · Hydraulic System, MainSDR UIEA2024092500948Access Panel · puncturedSYS LH HYD BAY, (ACCESS PANEL 437BL), SURFACE INERSIDE AREA LOWER RIGH TSIDE, ANGLE WITH PUNCTURE.(<P>SURFACE INERSIDE AREA LOWER RIGHTSIDE, ANGLE WAS REPAIRED IAW TRE 6754195 ISSUED DATE 13/SEP/24 & CMA-TLS-24-0190, RDR WAS ISSUED. NO FURTHER DEFECTS NOTED</PSep 29, 2024 · N1619A · Boeing 7673Y0 · Nacelle/Pylon, Plate/SkinSDR UIEA2024092500949Access Panel · wornSYST LH HYD BAY, (ACCESS PANEL: 437BL) INNER RIGHTSIDE, LOWER REAR CORNER AREA, PLATE-STRICKER WITH WORN.(<P>LOWER REAR CORNER AREA, PLATE ASSY WAS REPLACED SRM 51-10-02-0G-0. NO FURTHER DEFECTS NOTED</P>)Sep 29, 2024 · N1619A · Boeing 7673Y0 · Fuselage Main, Plate/SkinSDR UIEA2024092500950Fire Seal · detachedENGINE ONE NACELLE STRUT FIRE SEAL DETACHED ON FWD CORNER LH AND RH SIDE(<P>ENGINE ONE NACELLE STRUT FWD CORNER LH AND RH SIDE; SEAL WAS REPAIRED IAW AMM 54-54-03-308-014. NO FURTHER DEFECTS NOTED</P>)Sep 29, 2024 · N1619A · Boeing 7673Y0 · Nacelle/Pylon, Main FrameSDR UIEA2024092500951Fill Port · corrodedRH WING, UPPER SURFACE, BASE OF OVERWING FILL PORT ADAPTER WITH EVIDENCE OF CORROSION(<P>OVERWING FILL PORT ADAPTER. CORROSION LEVE 1 WAS REWORKED, INSPECTED AND ALLOWABLE LIMITS FOUND IAW SRM 57-20-01-1A-1</P>)Sep 29, 2024 · N1619A · Boeing 7673Y0 · Wing Main, Frame StructureSDR UIEA2024092500952Bracket · corrodedBULK CARGO COMPARTMENT, AFT BULKHEAD, AFT STA 1540, BTW S-38R, AND S-39R, BRACKET WITH EVIDENCE OF CORROSION.(<P>BRACKET WAS REPLACED IAW SRM 51-10-02-0G-0. NO FURTHER DEFECTS NOTED</P>)Sep 29, 2024 · N1619A · Boeing 7673Y0 · Fuselage Miscellaneous StructureSDR UIEA2024092500953Bulkhead · corrodedBULK CARGO COMPARTMENT, AFT BULKHEAD, BTW STA 1540 AND STA 1581, S-38R WITH EVIDENCE OF CORROSION.(<P>BULK CARGO COMPARTMENT, AFT BULKHEAD, BTW STA 1540 AND STA 1581, S-38R WAS REPAIRED IAW SRM 53-00-03-2R-2. NO FURTHER DEFECTS NOTED</P>)Sep 29, 2024 · N1619A · Boeing 7673Y0 · Fuselage Main, BulkheadSDR UIEA2024092500954Bulkhead · corrodedBULK CARGO COMPARTMENT, AFT BULKHEAD, BTW STA 1540 AND STA 1581, S-38L WITH EVIDENCE OF CORROSION.(<P>BULK CARGO COMPARTMENT, AFT BULKHEAD, BTW STA 1540 AND STA 1581, S-38L WAS REPAIRED IAW SRM 53-00-03-2R-2</P>)Sep 29, 2024 · N1619A · Boeing 7673Y0 · Fuselage Main, BulkheadSDR UIEA2024092500955Fire Seal · brokenENG 2, RIGHT T/R DOOR, UPPER AFTER SECTION, FIRE SEAL BROKEN(<P>FIRE SEAL WAS REPAIRED IAW AMM 78-00-00-038-001-N00. NO FURTHER DEFECTS NOTED</P>)Sep 29, 2024 · N1619A · Boeing 7673Y0 · Engine Thrust ReverserSDR UIEA2024092500956Seal · damagedENG 2, RIGHT T/R DOOR, UPPER SECTION, FIRE SEAL, RESTORE SEALANT (THE ENTIRE PERIPHERY)(<P>FIRE SEAL WAS REPAIRED IAW AMM 78-00-00-038-001-N00. NO FURTHER DEFECTS NOTED</P>)Sep 29, 2024 · N1619A · Boeing 7673Y0 · Engine Thrust ReverserSDR UIEA2024092500957Fire Seal · damagedENG 2, LEFT T/R DOOR, UPPER SECTION, FIRE SEAL, RESTORE SEALANT (THE ENTIRE PERIPHERY)(<P>FIRE SEAL WAS REPAIRED IAW AMM 78-00-00-038-001-N00. NO FURTHER DEFECTS NOTED</P>)Sep 29, 2024 · N1619A · Boeing 7673Y0 · Engine Thrust ReverserSDR UIEA2024092500958Display · inoperativeFLIGHT MANAGEMENT COMPUTER SYSTEM, ASSY-FLIGHT PANEL P9, MCDU RIGHT SIDE INOPERATIVE(<P>MCDU RIGHT WAS REPLACED IAW AMM 34-61-02-400-802. OPS CHECK GOOD</P>)Sep 29, 2024 · N1619A · Boeing 7673Y0 · Indicating/Recording SystemSDR UIEA2024092700960Fuel Cell · leakingRH WING, LOWER SKIN BETWEEN WBL 97.95 TO WS 226.3 AND STGR 10 WITH EVIDENCE OF FUEL LEAK(<P>FUEL LEAK WAS REPAIRED IAW AMM 28-11-00-308-013. LEAK CHECK GOOD</P>)Sep 29, 2024 · N1619A · Boeing 7673Y0 · Fuel StorageSDR UIEA2025081501124Warning Light · false activationMAIN CARGO DOOR DISCRETE LIGHT ON AFTER 2ND ENGINE START(<P>MDC CHECKED IAW AMM 52-31-00. OPENED & INSPECTION CHECKED GOOD. THIS CLOSES MDDR 236249 </P>)Aug 16, 2024 · N642GT · Boeing 7673Y0 · Door Warning SystemSDR UIEA2025081501125Starter · failedJUST BEFORE ENGINE START, A VERY STRONG ELECTRICAL SMELL OVERWHELMED THE FLIGHT DECK. SMELL GOES AWAY AFTER PACKS ARE SHUT OFF(<P>APU STARTER WAS BURNT AND WAS DETERMINED TO BE THE CAUSE OF THE SMOKE SMELL. R/R APU STARTER PER AMM 49-41-01. OPS CHK OK. NO DEFEAug 16, 2024 · N642GT · Boeing 7673Y0 · APU Start/Ignition SystemSDR UIEA2024080500789Rvdt · out of rigCLIMBING OUT OF RFD, WE WENT FLAPS UP AND THEN GOT LE SLAT DISAGREE MSG. PERFORMED FSEU BITE CHECK IAW FIM 27-51 FT 809. FOUND FAULT CODE 27-S1040 FOR LVR 1 NOT IN DETENT, CHECKED RIGGING OF FLAP LEVER RVDT IAW AMM 27-51-26. FOUND RVDT 1 OUT OF LIMITS IN UP PAug 5, 2024 · N1619A · Boeing 7673Y0 · Leading Edge Slat Control SystemSDR UIEA2024072400743Escape Reel · unwanted deploy1 EA ESCAPE INERTIAL REEL DEVICE FULL OUT(<P>TRANSFER TO DMI 213408 PER MEL 25-61-01-01 CAT C DUE DATE 4AUG2024. PN 379103D-29</P> / <P>LP 1239968 ITEM 5 / ONT / 27JUL24: INSTALLED 1 EA INERTIA REEL IAW B767 AMM 25-61-01. NO FUTHER DEFECTS NOTED. THIS CLEARS MJul 24, 2024 · N1181A · Boeing 7673Y0 · Emergency EquipmentSDR UIEA2024062700570Harness · malfunctionedTHREE ESCAPE HARNESSES INOP. INSTALLED SAFETY HARNESS IAW AMM 25-61-05. MCC NOTIFIED, PLACARDS REMOVED. THIS CLOSES DMI #211594.</P>)Jun 27, 2024 · N1619A · Boeing 7673Y0 · Emergency EquipmentSDR UIEA2024062200564Elevator System · noneCAN'T GET FULL TRAVEL WITH FWD ELEVATOR(<P>PERFORMED OPS CHECK OF ELEVATOR POSITION INDICATION SYSTEM IAW AMM 27-38-00. VERIFIED ALL INDICATIONS WITHIN LIMITS. AC OKAY FOR SERVICE.</P>)Jun 22, 2024 · N1619A · Boeing 7673Y0 · Elevator Control SystemSDR UIEA2024060700500Control Panel · faultedFO SIDA UNABLE TO TURN VOR EMERGENCYIN MANUAL MODE(<P>REMOVED AND REPLACED VOR CONTROL PANEL IAW AMM 34-51-02. NO DEFECTS NOTED AT THIS TIME. VERIFIED PART EFFECTIVITY IAW IPC 31-11-11-17</P>)Jun 7, 2024 · N642GT · Boeing 7673Y0 · DME/TACAN SystemSDR UIEA2024060500494Stowage Box · unknown/FO OXYGEN STOWAGE BOX REQ REPLACEMENT(<P>R/R F/O'S OXYGEN STOWAGE BOX REF 35-11-51 LEAK CHECK GOOD OPS CHECK GOOD. PART EFFECTIVITY VERIFIED IAW AIPC 35-11-52-15</P>)Jun 5, 2024 · N642GT · Boeing 7673Y0 · Crew Oxygen System
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