N642GT

Service difficulty reports · 620

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 = 'N642GT' 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 UIEA2026100100935Drive Assy · faultedALT DISAGREE AT FL 230-270. FO AND CAPT ALTIMETER +/- 500; BELOW 10,000 NORMAL. AIRSPEED DISAGREE, CAPT & STANDBY AGREE +/-2 KNOTS. FO'S AIRSPEED +20 KTS. PITCH & POWER CROSS CHK CAPT'S ASI, BELOW 10,000 NORMAL. WXR SYS LT & RT FAILED AFTER APPROX 3 MINS OFOct 1, 2026 · N642GT · Boeing 7673Y0 · Weather Radar SystemSDR UIEA2026082600801Seat Track · corrodedMAIN DECK, BS 1590 - 1600, LBL 11 SEAT TRACK CROWN CORRODED. CORROSION REMOVED IAW SRM 51-10-02, AND PROTECTED IAW SRM 51-20-01. MEASURED L: 0.9" X W: 0.7" X D: 0.016". WITHIN SRM 53-00-52 ALLOWABLE DAMAGE 1, FIG 101, & SRM 53-00-52, ALLOWABLE DAMAGE 1, FIG 1Sep 11, 2026 · N642GT · Boeing 7673Y0 · Fuselage, Seat/Cargo Attach FittingsSDR UIEA2026082600802Seat Track · corrodedMAIN DECK, BS 1197+44, LBL 33 SEAT TRACK CROWN FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-02, AND PROTECTED IAW SRM 51-20-01. MEASURED L: 5" X W: 0.7" X D 0.010". WITHIN SRM 53-00-52 ALLOWABLE DAMAGE 1, FIG 101, & SRM 53-00-52, ALLOWABLE DAMAGE 1, FIG 10Sep 11, 2026 · N642GT · Boeing 7673Y0 · Fuselage, Seat/Cargo Attach FittingsSDR UIEA2026082600803Skin · delaminatedLEFT WING T/E OTBD FLAP LOWER SKIN, BETWEEN FLAP FAIRINGS, FOUND DELAMINATED. PERFORMED COMPOSITE HOT BOND REPAIR IAW SRM 51-70-07, PAR 5 A(1). NO FURTHER DEFECTS NOTED.Sep 11, 2026 · N642GT · Boeing 7673Y0 · Wing, Control SurfacesSDR UIEA2026082600804Seat Track · corrodedMAIN DECK, BS 1590, LBL 55 SEAT TRACK CROWN CORRODED. CORROSION REMOVED IAW SRM 51-10-02, AND PROTECTED IAW SRM 51-20-01. MEASURED L: 3" X W: 0.7" X D: 0.009". WITHIN SRM 53-00-52 ALLOWABLE DAMAGE 1, FIG 101, & SRM 53-00-52, ALLOWABLE DAMAGE 1, FIG 101, DETASep 11, 2026 · N642GT · Boeing 7673Y0 · Fuselage, Seat/Cargo Attach FittingsSDR UIEA2026082600806Seat Track · corrodedMAIN DECK, BS 1590 - 1600, LBL 33 SEAT TRACK CROWN CORRODED. CORROSION REMOVED IAW SRM 51-10-02, & PROTECTED IAW SRM 51-20-01. MEASURED L: 2.5" X W: 0.7" X D: 0.029". WITHIN SRM 53-00-52, DAMAGE 1 FIG 101, LIMITS, AND SRM 53-00-52, ALLOWABLE DAMAGE 1, FIG 101Sep 11, 2026 · N642GT · Boeing 7673Y0 · Fuselage, Seat/Cargo Attach FittingsSDR UIEA2026082600807Seat Track · corrodedMAIN DECK, BS 1590 - 1600, RBL 33 SEAT TRACK CROWN CORRODED. CORROSION REMOVED IAW SRM 51-10-02, & PROTECTED IAW SRM 51-20-01. MEASURED L: 8" X W: 0.7" X D: 0.015". IAW SRM 53-00-52, ALLOWABLE DAMAGE, FIG 101 LIMITS, & SRM 53-00-52, ALLOWABLE DAMAGE 1, FIGSep 11, 2026 · N642GT · Boeing 7673Y0 · Fuselage, Seat/Cargo Attach FittingsSDR UIEA2026082700811Skin · crackedRIGHT WING NR 9 SLAT, INBD MAIN TRACK RIB SKIN AT FASTENER HOLE, CRACKED. SKIN REPAIRED IAW SRM 57-43-01-2R-2, REPAIR 2. NO FURTHER DEFECTS NOTED.Sep 11, 2026 · N642GT · Boeing 7673Y0 · Leading Edge DevicesSDR UIEA2026082700812Skin · crackedRIGHT WING NR 10 SLAT, INBD MAIN TRACK RIB SKIN AT FASTENER HOLE, CRACKED. SKIN REPAIRED IAW SRM 57-43-01-2R-2, REPAIR 2. NO FURTHER DEFECTS NOTED.Sep 11, 2026 · N642GT · Boeing 7673Y0 · Leading Edge DevicesSDR UIEA2026082800816Skin · crackedLEFT WING, NR 4 SLAT, INBD MAIN TRACK RIB SKIN AT FASTENER HOLE, CRACKED. SKIN REPAIRED IAW SRM 57-43-01-2R-2, REPAIR 2. NO FURTHER DEFECTS NOTED.Sep 11, 2026 · N642GT · Boeing 7673Y0 · Leading Edge DevicesSDR UIEA2026082800818Skin · crackedRIGHT WING, NR 8 SLAT OTBD MAIN TRACK RIB SKIN FASTENER HOLE CRACKED. SKIN REPAIRED IAW SRM 57-43-01-2R-2, REPAIR 2. NO FURTHER DEFECTS NOTED.Sep 11, 2026 · N642GT · Boeing 7673Y0 · Leading Edge DevicesSDR UIEA2026082800819Skin · crackedLEFT WING NR 4 SLAT OTBD MAIN TRACK RIB SKIN FASTENER HOLE CRACKED. NOSE SKIN REPAIRED IAW SRM 57-43-01-2R-2, REPAIR 2. NO FURTHER DEFECTS NOTED.Sep 11, 2026 · N642GT · Boeing 7673Y0 · Leading Edge DevicesSDR UIEA2026083100830Frame · chafedNUMBER 1 ENG LT CORE COWL NR 2 FRAME MID AREA ANGLE FWD, CHAFED. FRAME REPAIRED IAW SRM 54-42-02-2R-2, REPAIR 2, & EA-1971A296, REV 0. NO FURTHER DEFECTS NOTED.Sep 11, 2026 · N642GT · Boeing 7673Y0 · Nacelle/Pylon, Frame/Spar/RibSDR UIEA2026083100831Pan · damagedWASTE SERVICE PAN FOUND TWO FASTENER HOLES WITHOUT BLANK OUT, AFTER DEACTIVATION. TWO RIVETS INSTALLED IAW DWG 146T3244, DL, & 146T3244, PL. NO FURTHER DEFECTS NOTED.Sep 11, 2026 · N642GT · Boeing 7673Y0 · Fuselage Main, StructureSDR UIEA2026083100832Frame · crackedONE CRACK FOUND ON BS 1809.5 BULKHEAD FWD OUTER FRAME BTWN STRS 6R-7R. RADIUS AREA APPROX 3/4 LENGTH. OUTER FRAME AREA REPAIRED IAW EO 6753A030, REV 16, PART 10, AND RI-53-80-18470, REV A. NO FURTHER DEFECTS NOTED.Sep 11, 2026 · N642GT · Boeing 7673Y0 · Fuselage Main, FrameSDR UIEA2026083100833Frame · crackedLEFT BS 1809.5 BULKHEAD OUTER CHORD HOLE, FOUND CRACK IN SKIN LAYER. CRACKED FASTENER HOLE, REPAIRED IAW RI-53-81-18478, REV A. NO FURTHER DEFECTS NOTED.Sep 11, 2026 · N642GT · Boeing 7673Y0 · Fuselage Main, FrameSDR UIEA2026090100844Seat Track · corrodedM/D BS 522, LBL 88, SEAT TRACK FOUND CORRODED. THE SEAT TRACK WAS REPLACED IAW SRM 51-40-05. NO FURTHER DEFECTS NOTED.Sep 11, 2026 · N642GT · Boeing 7673Y0 · Fuselage, Seat/Cargo Attach FittingsSDR UIEA2026090300847Support Rib · crackedLEFT WING, NR 3 SLAT, OTBD SUPPORT RIB FOUND CRACKED. RIB CRACK AREA REPAIRED IAW RI-57-42-18506, REV A. NO FURTHER DEFECTS NOTED.Sep 11, 2026 · N642GT · Boeing 7673Y0 · Leading Edge DevicesSDR UIEA2026090300848Ball Mat · crackedFWD CARGO BAY, BS 480 , MOT RT OTBD BALL MAT PANEL FWD MID SKIN AND SUPPORT FOUND DAMAGE. BALL MAT PANEL REPAIRED IAW RI-53-00-18499, REV A. NO FURTHER DEFECTS NOTED.Sep 11, 2026 · N642GT · Boeing 7673Y0 · Fuselage Floor PanelSDR UIEA2026090300849Slat Track · crackedLEFT WING, NR 3 SLAT, OTBD MAIN TRACK RIB SKIN FASTENER HOLE CRACKED. SKIN REPAIRED IAW SRM 57-43-01-2R-2, REPAIR 2. NO FURTHER DEFECTS NOTED.Sep 11, 2026 · N642GT · Boeing 7673Y0 · Leading Edge DevicesSDR UIEA2026090400851Stringer · crackedBS 434, STRINGER 22L FOUND ONE CRACK AT FASTENER HOLE ON VERTICAL FLANGE AREA AT 10 O'CLOCK, APPROX 3/16 LENGTH. STRINGER REPAIRED IAW IAI DOC CS-26207-005, VERSION IR. NO FURTHER DEFECTS NOTED.Sep 11, 2026 · N642GT · Boeing 7673Y0 · Fuselage Main, Longeron/StringerSDR UIEA2026090800858Track · damagedMEC ACCESS DOOR 119AL FOUND FWD ROLLER TRACK MISSING MATERIAL. THE NEW PART 1EA BOLT HOLE NOT ALIGNED. FASTENER HOLE REPAIRED, AND INSTALLED FREEZE PLUG IAW RI-52-40-18516, REV A. NO FURTHER DEFECTS NOTED.Sep 11, 2026 · N642GT · Boeing 7673Y0 · Electrical/Electronic Compartment DoorsSDR UIEA2026060500452Seal · tornL1 DOOR ELT TAMPER PROOF SEAL TORN. REMOVED AND REPLACED PORTABLE ELT BY L1 DOOR IAW AMM 25-63-03. OPS CHECKS GOOD.Jun 5, 2026 · N642GT · Boeing 7673Y0 · Emergency Locator BeaconSDR UIEA2026060400451Unknown · odorFLIGHT CREW REPORTED OIL FUMES AND RUBBER SMELL DURING TAKE OFF. PERFORMED CHAPTER 5 INSPECTION IAW AMM 05-51-56-202-001. ALSO PERFORMED REMOVAL OF OIL CONTAMINATION FROM AIR CONDITIONING AND PNEUMATIC SYSTEM IAW AMM 21-00-21-102-030, NO EVIDENCE OF OIL CONTAJun 4, 2026 · N642GT · Boeing 7673Y0 · Air Distribution SystemSDR UIEA2026050100286Oxygen Box · inoperativeSUPERNUMERARY SEAT OXY MASK INOP ( SUPERNUMERARY OXYGEN SYSTEM, OXYGEN MASKS, ASSOCIATED SEAT NOT OCCUPIED, TRANSFER TO DMI 251838 PER MEL 35-11-03-02A CAT C DUE DATE 11MAY26. R & R RH OTBD O2 MASK STOWAGE BOX IAW AMM 35-11-51. OPS & LK CHK GOOD.May 1, 2026 · N642GT · Boeing 7673Y0 · Crew Oxygen SystemSDR UIEA2026032700109Bottle · low pressureSUPERNUMERARY O2 BELOW LIMITS INOP. PLACARDS INSTALLED. SERVICED O2 TO 1710 PSI PER AMM 12-15-08. LEAK CHK GOOD. DMI 249872 CLOSED</P>)Mar 26, 2026 · N642GT · Boeing 7673Y0 · Crew Oxygen SystemSDR UIEA2026020700044Control Panel · faultedMCP ALTITUDE SELECTOR SELECTS ERRONEOUS ALTITUDES PLUS/MINUS 3000 FEET WHEN TURNING. REMOVED AND REPLACED MCP IAW AMM 22-11-02. PERFORMED MCDP GROUND TEST, 30-40 TEST PASS, NO FAULTS NOTED.Feb 7, 2026 · N642GT · Boeing 7673Y0 · Autopilot SystemSDR UIEA2026020200028Antenna · unwanted deployELT ANTENNA DEPLOYED STICKING STRAIGHT UP. REMOVED & REPLACED RT PORTABLE ELT IAW AMM 25-63-03. OPS CHK OK.Feb 1, 2026 · N642GT · Boeing 7673Y0 · Emergency Locator BeaconSDR 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 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 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 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 System
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