# Service difficulty reports: N642GT

A list on [N642GT](https://openairdocs.org/aircraft/N642GT.md).

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

Page 1 of 13 · 620 reports

- [SDR UIEA2026100100935](https://openairdocs.org/sdr/UIEA2026100100935.md): Drive Assy · faulted · Oct 1, 2026 · N642GT · Boeing 7673Y0 · Weather Radar System
  > ALT 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 OF
- [SDR UIEA2026082600801](https://openairdocs.org/sdr/UIEA2026082600801.md): Seat Track · corroded · Sep 11, 2026 · N642GT · Boeing 7673Y0 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN 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 1
- [SDR UIEA2026082600802](https://openairdocs.org/sdr/UIEA2026082600802.md): Seat Track · corroded · Sep 11, 2026 · N642GT · Boeing 7673Y0 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN 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 10
- [SDR UIEA2026082600803](https://openairdocs.org/sdr/UIEA2026082600803.md): Skin · delaminated · Sep 11, 2026 · N642GT · Boeing 7673Y0 · Wing, Control Surfaces
  > LEFT 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.
- [SDR UIEA2026082600804](https://openairdocs.org/sdr/UIEA2026082600804.md): Seat Track · corroded · Sep 11, 2026 · N642GT · Boeing 7673Y0 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN 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, DETA
- [SDR UIEA2026082600806](https://openairdocs.org/sdr/UIEA2026082600806.md): Seat Track · corroded · Sep 11, 2026 · N642GT · Boeing 7673Y0 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN 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 101
- [SDR UIEA2026082600807](https://openairdocs.org/sdr/UIEA2026082600807.md): Seat Track · corroded · Sep 11, 2026 · N642GT · Boeing 7673Y0 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN 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, FIG
- [SDR UIEA2026082700811](https://openairdocs.org/sdr/UIEA2026082700811.md): Skin · cracked · Sep 11, 2026 · N642GT · Boeing 7673Y0 · Leading Edge Devices
  > RIGHT 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.
- [SDR UIEA2026082700812](https://openairdocs.org/sdr/UIEA2026082700812.md): Skin · cracked · Sep 11, 2026 · N642GT · Boeing 7673Y0 · Leading Edge Devices
  > RIGHT 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.
- [SDR UIEA2026082800816](https://openairdocs.org/sdr/UIEA2026082800816.md): Skin · cracked · Sep 11, 2026 · N642GT · Boeing 7673Y0 · Leading Edge Devices
  > LEFT 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.
- [SDR UIEA2026082800818](https://openairdocs.org/sdr/UIEA2026082800818.md): Skin · cracked · Sep 11, 2026 · N642GT · Boeing 7673Y0 · Leading Edge Devices
  > RIGHT 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.
- [SDR UIEA2026082800819](https://openairdocs.org/sdr/UIEA2026082800819.md): Skin · cracked · Sep 11, 2026 · N642GT · Boeing 7673Y0 · Leading Edge Devices
  > LEFT 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.
- [SDR UIEA2026083100830](https://openairdocs.org/sdr/UIEA2026083100830.md): Frame · chafed · Sep 11, 2026 · N642GT · Boeing 7673Y0 · Nacelle/Pylon, Frame/Spar/Rib
  > NUMBER 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.
- [SDR UIEA2026083100831](https://openairdocs.org/sdr/UIEA2026083100831.md): Pan · damaged · Sep 11, 2026 · N642GT · Boeing 7673Y0 · Fuselage Main, Structure
  > WASTE SERVICE PAN FOUND TWO FASTENER HOLES WITHOUT BLANK OUT, AFTER DEACTIVATION. TWO RIVETS INSTALLED IAW DWG 146T3244, DL, & 146T3244, PL. NO FURTHER DEFECTS NOTED.
- [SDR UIEA2026083100832](https://openairdocs.org/sdr/UIEA2026083100832.md): Frame · cracked · Sep 11, 2026 · N642GT · Boeing 7673Y0 · Fuselage Main, Frame
  > ONE 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.
- [SDR UIEA2026083100833](https://openairdocs.org/sdr/UIEA2026083100833.md): Frame · cracked · Sep 11, 2026 · N642GT · Boeing 7673Y0 · Fuselage Main, Frame
  > LEFT 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.
- [SDR UIEA2026090100844](https://openairdocs.org/sdr/UIEA2026090100844.md): Seat Track · corroded · Sep 11, 2026 · N642GT · Boeing 7673Y0 · Fuselage, Seat/Cargo Attach Fittings
  > M/D BS 522, LBL 88, SEAT TRACK FOUND CORRODED. THE SEAT TRACK WAS REPLACED IAW SRM 51-40-05. NO FURTHER DEFECTS NOTED.
- [SDR UIEA2026090300847](https://openairdocs.org/sdr/UIEA2026090300847.md): Support Rib · cracked · Sep 11, 2026 · N642GT · Boeing 7673Y0 · Leading Edge Devices
  > LEFT WING, NR 3 SLAT, OTBD SUPPORT RIB FOUND CRACKED. RIB CRACK AREA REPAIRED IAW RI-57-42-18506, REV A. NO FURTHER DEFECTS NOTED.
- [SDR UIEA2026090300848](https://openairdocs.org/sdr/UIEA2026090300848.md): Ball Mat · cracked · Sep 11, 2026 · N642GT · Boeing 7673Y0 · Fuselage Floor Panel
  > FWD 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.
- [SDR UIEA2026090300849](https://openairdocs.org/sdr/UIEA2026090300849.md): Slat Track · cracked · Sep 11, 2026 · N642GT · Boeing 7673Y0 · Leading Edge Devices
  > LEFT 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.
- [SDR UIEA2026090400851](https://openairdocs.org/sdr/UIEA2026090400851.md): Stringer · cracked · Sep 11, 2026 · N642GT · Boeing 7673Y0 · Fuselage Main, Longeron/Stringer
  > BS 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.
- [SDR UIEA2026090800858](https://openairdocs.org/sdr/UIEA2026090800858.md): Track · damaged · Sep 11, 2026 · N642GT · Boeing 7673Y0 · Electrical/Electronic Compartment Doors
  > MEC 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.
- [SDR UIEA2026060500452](https://openairdocs.org/sdr/UIEA2026060500452.md): Seal · torn · Jun 5, 2026 · N642GT · Boeing 7673Y0 · Emergency Locator Beacon
  > L1 DOOR ELT TAMPER PROOF SEAL TORN. REMOVED AND REPLACED PORTABLE ELT BY L1 DOOR IAW AMM 25-63-03. OPS CHECKS GOOD.
- [SDR UIEA2026060400451](https://openairdocs.org/sdr/UIEA2026060400451.md): Unknown · odor · Jun 4, 2026 · N642GT · Boeing 7673Y0 · Air Distribution System
  > FLIGHT 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 CONTA
- [SDR UIEA2026050100286](https://openairdocs.org/sdr/UIEA2026050100286.md): Oxygen Box · inoperative · May 1, 2026 · N642GT · Boeing 7673Y0 · Crew Oxygen System
  > SUPERNUMERARY 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.
- [SDR UIEA2026032700109](https://openairdocs.org/sdr/UIEA2026032700109.md): Bottle · low pressure · Mar 26, 2026 · N642GT · Boeing 7673Y0 · Crew Oxygen System
  > SUPERNUMERARY O2 BELOW LIMITS INOP. PLACARDS INSTALLED. SERVICED O2 TO 1710 PSI PER AMM 12-15-08. LEAK CHK GOOD. DMI 249872 CLOSED</P>)
- [SDR UIEA2026020700044](https://openairdocs.org/sdr/UIEA2026020700044.md): Control Panel · faulted · Feb 7, 2026 · N642GT · Boeing 7673Y0 · Autopilot System
  > MCP 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.
- [SDR UIEA2026020200028](https://openairdocs.org/sdr/UIEA2026020200028.md): Antenna · unwanted deploy · Feb 1, 2026 · N642GT · Boeing 7673Y0 · Emergency Locator Beacon
  > ELT ANTENNA DEPLOYED STICKING STRAIGHT UP. REMOVED & REPLACED RT PORTABLE ELT IAW AMM 25-63-03. OPS CHK OK.
- [SDR UIEA2026012900019](https://openairdocs.org/sdr/UIEA2026012900019.md): Tape · damaged · Jan 29, 2026 · N642GT · Boeing 7673Y0 · Emergency Locator Beacon
  > FIRST OBSERVER ELT TAPE IS DAMAGED(<P>RESECURED TAPE AS PER HONEYWELL CMM JOB TASK 25-60-10. NO FURTHER DEFECTS NOTED</P>)
- [SDR UIEA2026012900020](https://openairdocs.org/sdr/UIEA2026012900020.md): Fitting · wrong part · Jan 28, 2026 · N642GT · Boeing 7673Y0 · Portable Oxygen System
  > LAVATORY 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>)
- [SDR UIEA2025121501345](https://openairdocs.org/sdr/UIEA2025121501345.md): Stowage Box · no test · Dec 11, 2025 · N642GT · Boeing 7673Y0 · Crew Oxygen System
  > DURING 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.
- [SDR UIEA2025112601326](https://openairdocs.org/sdr/UIEA2025112601326.md): Elec Connector · damaged · Nov 26, 2025 · N642GT · Boeing 7673Y0 · Landing Gear System Wiring
  > GEAR 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 BR
- [SDR UIEA2025112501325](https://openairdocs.org/sdr/UIEA2025112501325.md): Pseu · faulted · Nov 22, 2025 · N642GT · Boeing 7673Y0 · Landing Gear Position and Warning
  > RH 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 MO
- [SDR UIEA2025090801169](https://openairdocs.org/sdr/UIEA2025090801169.md): Hook And Loop · damaged · Sep 8, 2025 · N642GT · Boeing 7673Y0 · Emergency Equipment
  > HOOK 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 NOTED
- [SDR UIEA2025030600213](https://openairdocs.org/sdr/UIEA2025030600213.md): Structure · damaged · Mar 24, 2025 · N642GT · Boeing 7673Y0 · Cargo/Baggage Doors
  > DAMAGE 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>)
- [SDR UIEA2025030600214](https://openairdocs.org/sdr/UIEA2025030600214.md): Actuator · out of limits · Mar 24, 2025 · N642GT · Boeing 7673Y0 · Elevator Control System
  > DURING 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>)
- [SDR UIEA2025030600217](https://openairdocs.org/sdr/UIEA2025030600217.md): Actuator · out of limits · Mar 24, 2025 · N642GT · Boeing 7673Y0 · Elevator Control System
  > DURING 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>)
- [SDR UIEA2025030600219](https://openairdocs.org/sdr/UIEA2025030600219.md): Actuator · leaking · Mar 24, 2025 · N642GT · Boeing 7673Y0 · Drag Control Actuator
  > RH 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>)
- [SDR UIEA2025030600220](https://openairdocs.org/sdr/UIEA2025030600220.md): Skin · cracked · Mar 24, 2025 · N642GT · Boeing 7673Y0 · Fuselage Main, Plate/Skin
  > FWD 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 51
- [SDR UIEA2025030600221](https://openairdocs.org/sdr/UIEA2025030600221.md): Skin · cracked · Mar 24, 2025 · N642GT · Boeing 7673Y0 · Fuselage Main, Plate/Skin
  > SERVICE 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>)
- [SDR UIEA2025030600222](https://openairdocs.org/sdr/UIEA2025030600222.md): Lamp · inoperative · Mar 24, 2025 · N642GT · Boeing 7673Y0 · Emergency Lighting
  > EMERGENCY 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>)
- [SDR UIEA2025030800224](https://openairdocs.org/sdr/UIEA2025030800224.md): Sign · loose · Mar 24, 2025 · N642GT · Boeing 7673Y0 · Emergency Lighting
  > EMERGENCY 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>
- [SDR UIEA2025030800225](https://openairdocs.org/sdr/UIEA2025030800225.md): Actuator · leaking · Mar 24, 2025 · N642GT · Boeing 7673Y0 · Drag Control Actuator
  > LH 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>)
- [SDR UIEA2025030800226](https://openairdocs.org/sdr/UIEA2025030800226.md): Skin · corroded · Mar 24, 2025 · N642GT · Boeing 7673Y0 · Trailing Edge Flaps
  > RH 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>)
- [SDR UIEA2025030800227](https://openairdocs.org/sdr/UIEA2025030800227.md): Feel Unit · leaking · Mar 24, 2025 · N642GT · Boeing 7673Y0 · Elevator Control System
  > LEAKAGE 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 27-31-19-424-015
- [SDR UIEA2025030800229](https://openairdocs.org/sdr/UIEA2025030800229.md): Fuel Tank · leaking · Mar 24, 2025 · N642GT · Boeing 7673Y0 · Fuel Storage
  > LH 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 SATISFACT
- [SDR UIEA2025030800231](https://openairdocs.org/sdr/UIEA2025030800231.md): Fuel Tank · leaking · Mar 24, 2025 · N642GT · Boeing 7673Y0 · Fuel Storage
  > LH 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 SATIS
- [SDR UIEA2025030800236](https://openairdocs.org/sdr/UIEA2025030800236.md): Fuel Tank · leaking · Mar 24, 2025 · N642GT · Boeing 7673Y0 · Fuel Storage
  > LH 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 SATIS
- [SDR UIEA2025030800239](https://openairdocs.org/sdr/UIEA2025030800239.md): Skin · corroded · Mar 24, 2025 · N642GT · Boeing 7673Y0 · Fuselage Main, Plate/Skin
  > UPPER 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-COR
- [SDR UIEA2025030800242](https://openairdocs.org/sdr/UIEA2025030800242.md): Transmitter · faulted · Mar 24, 2025 · N642GT · Boeing 7673Y0 · Trailing Flap Position Indicating System
  > TRANSMITER 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.</P

Next page: https://openairdocs.org/aircraft/N642GT/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/aircraft/N642GT/reports

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