# Service difficulty reports: N659GT

A list on [N659GT](https://openairdocs.org/aircraft/N659GT.md).

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

- [SDR FIKA2021051200045](https://openairdocs.org/sdr/FIKA2021051200045.md): Connector · loose · May 12, 2021 · N659GT · Boeing 767281 · Flight Control System Wiring
  > THIS MORNING GOING INTO CVG FROM IAH (AIRCRAFT 659GT) ON DECENT THE TE FLAPS GAVE A DISAGREE MSG THE FLAPS WERE AT 5 DEGREES AND WOULD NOT COME DOWN. THE CREW USED THE ALT SYSTEM BROUGHT THE FLAPS UP AND DID A GO AROUND. THEY DID ANOTHER APPROACH AND LANDED W
- [SDR ABXR2020042400022](https://openairdocs.org/sdr/ABXR2020042400022.md): Skin Panel · delaminated · Apr 24, 2020 · N659GT · Boeing 767281 · Vertical Stabilizer, Plate/Skin
  > RIGHT SIDE VERTICAL STAB SKIN DELAMINATED. REMOVED AND REPAIRED SKIN PANEL AND INSTALLED STAB SKIN WITH INTERIM FASTENERS.
- [SDR UIEA2020030900407](https://openairdocs.org/sdr/UIEA2020030900407.md): Angle · corroded · Mar 4, 2020 · N659GT · Boeing 767281 · Fuselage Main, Keel
  > CORROSION ON ANGLE THAT ATTACHES FRAME AT STR 997 TO KEEL WEB.(<P>BLENDED CORROSION IAW B767 SRM 53-50-12 FIG 1001 DETAIL II. FOUND TO BE OUT OF LIMITS, COMPLIED WITH ENGINEERING DOC #47396REA07.</P>)
- [SDR UIEA2020030900409](https://openairdocs.org/sdr/UIEA2020030900409.md): Keelbeam · corroded · Mar 4, 2020 · N659GT · Boeing 767281 · Fuselage Main, Keel
  > LLW - CORROSION ON KEEL WEB AT STA 1002 LBL 5. (<P><SPAN>BLENDED CORROSION IAW B767 SRM 53-50-12-1A, REPAIRED IAW ENGINEERING DOCUMENT 47396REA04 DUE TO BLEND BEING OUT OF LIMITS.</SPAN><BR /></P>)
- [SDR UIEA2020030900410](https://openairdocs.org/sdr/UIEA2020030900410.md): Splice Plate · corroded · Mar 4, 2020 · N659GT · Boeing 767281 · Wing Miscellaneous Structure
  > CORROSION AROUND GROUNDING JACK ON FRONT SPAR UPPER CHORD AFT OF NUMBER 3 SLAT OUTBOARD DRIVE ROD ACTUATOR.(<P>COMPLETED REPAIR IAW REA: 47396REA05 AND 47396REA06. REMOVED AND REPLACED SLICE PLATE L/W LES 745-807 IAW REA 47396REA05 & 47396REA06. </P>)
- [SDR UIEA2020030900411](https://openairdocs.org/sdr/UIEA2020030900411.md): Skin · cracked · Mar 4, 2020 · N659GT · Boeing 767281 · Fuselage Main, Plate/Skin
  > UPPER L/H FUSELAGE STA 1654.5 BETWEEN STRINGERS 4L-5L EXTERNAL SKIN IS CRACKED.(<P>REPAIRED L/H FUSELAGE SKIN AT STA 1654.5 IAW B767 SRM 53-80-01-2R-4 REPAIR 4.</P>)
- [SDR UIEA2020030900412](https://openairdocs.org/sdr/UIEA2020030900412.md): Spar · corroded · Mar 4, 2020 · N659GT · Boeing 767281 · Wing Spar
  > CORROSION AROUND RIVET ON FRONT SPAR UPPER CHORD AT LES 730.(<P>BLENDED CORROSION. 0.013" MATERIAL REMOVED. BEYOND LIMITS. REPAIRED IAW AMES DOCUMENT 47396REA01.</P>)
- [SDR UIEA2020030900413](https://openairdocs.org/sdr/UIEA2020030900413.md): Rib · corroded · Mar 4, 2020 · N659GT · Boeing 767281 · Ailerons
  > UPPER TRAILING EDGE PANEL ATTACH CHORD AT WS 434, 22 INCHES AFT OF REAR SPAR HAS CORROSION AROUND NUTPLATE.(<P>BLENDED CORROSION ON UPPER CHORD ON AILERON RIB AT WS 434 TO DEPTH OF.017", MAX DEPTH ALLOWED.008" IAW B767 SRM 57-51-02-1A-1 DETAIL 19. OUT OF LIMI
- [SDR UIEA2020030900414](https://openairdocs.org/sdr/UIEA2020030900414.md): Attach Bracket · cracked · Mar 4, 2020 · N659GT · Boeing 767281 · Fuselage Miscellaneous Structure
  > ATTACHED BRACKET BEHIND AFT LOWER CORNER SEAL DEPRESSOR IS CRACKED ON UPPER CARGO DOOR.(<P>REMOVED AND REPLACED CORNER SEAL DEPRESSOR IAW B767 SRM 51-40-02.</P>)
- [SDR UIEA2020030900415](https://openairdocs.org/sdr/UIEA2020030900415.md): Structure · corroded · Mar 4, 2020 · N659GT · Boeing 767281 · Horizontal Stabilizer Miscellaneous Structure
  > FLANGE UNDER PANEL 335AT HAS CORROSION ON UPPER SURFACE.(<P>REMOVED CORROSION IAW B767 SRM 55-10-09. FOUND TO BE OUT OF LIMITS OT.090" R.T.077. INSTALLED UPPER CHORD IAW B767 SRM 51-40-02.</P>)
- [SDR UIEA2020030900416](https://openairdocs.org/sdr/UIEA2020030900416.md): Rib · cracked · Mar 4, 2020 · N659GT · Boeing 767281 · Horizontal Stabilizer, Spar/Rib
  > L HORIZONTAL LEADING EDGE INBD END RIB IS CRACKED.(<P>CUT OUT DAMAGE AND REPAIRED IAW B767 SRM 55-10-09 REPAIR 1.</P>)
- [SDR UIEA2020030900417](https://openairdocs.org/sdr/UIEA2020030900417.md): Angle · cracked · Mar 4, 2020 · N659GT · Boeing 767281 · Rudder Miscellaneous Structure
  > CLOSE OUT ANGLE UNDER RUDDER HAS CRACK AT LEFT END OF ANGLE.(<P>REMOVED AND REPLACED CRACKED CLOSE OUT ANGLE UNDER RUDDER IAW BOEING DOCUMENT #173T1215 AND B767-200 SRM 51-40-02.</P>)
- [SDR UIEA2020030900418](https://openairdocs.org/sdr/UIEA2020030900418.md): Structure · corroded · Mar 4, 2020 · N659GT · Boeing 767281 · Horizontal Stabilizer Miscellaneous Structure
  > L HORIZ STAB UPPER CHORD ATTACH FITTING UNDER PANEL 335AT HAS CORROSION UNDER NUT PLATES, AND ALSO CORRODED NUT PLATES. (<P><SPAN>CORROSION BENEATH 335AT FOUND TO BE OUT OF LIMITS. REMOVED, FABRICATED, AND REPLACED CORRODED CHORD IAW BOEING DWG 182T7103.</SPAN
- [SDR UIEA2020030900419](https://openairdocs.org/sdr/UIEA2020030900419.md): Attach Bracket · cracked · Mar 4, 2020 · N659GT · Boeing 767281 · Fuselage Miscellaneous Structure
  > ATTACH BRACKET BEHIND FWD LOWER CORNER SEAL DEPRESSOR IS CRACKED.(<P>REMOVED AND REPLACED ATTACH BRACKET BEHIND FWD LOWER CORNER SEAL DEPRESSOR IAW B767 SRM 51-40-02.</P>)
- [SDR UIEA2019121876093](https://openairdocs.org/sdr/UIEA2019121876093.md): Escape Reel · unwanted deploy · Dec 17, 2019 · N659GT · Boeing 767281 · Emergency Equipment
  > 4 EACH GALLEY DESCENT DEVICES DEPLOYED; 3 EACH AVAILABLE.(<P>TRANSFERRED TO DMI 122134 IAW MEL 25-61-01-01, CAT 'C'.</P><P>LP 1084472 - M5: REMOVED AND REPLACED 4 EACH EMERGENCY DESCENT DEVICES IAW AMM 25-61-03. NO DISCREPANCIES NOTED AT THIS TIME. THIS CLEARS
- [SDR UIEA2019121606086](https://openairdocs.org/sdr/UIEA2019121606086.md): Escape Reel · unwanted deploy · Dec 16, 2019 · N659GT · Boeing 767281 · Emergency Equipment
  > 4EA GALLEY DESCENT DEVICES DEPLOY; 3EA AVAILABLE.(<P>TRANSFERRED TO MDDR 122134 IAW MEL 25-61-01-01, CAT 'C'.</P>)
- [SDR UIEA2019021303210](https://openairdocs.org/sdr/UIEA2019021303210.md): Control Panel · smoke · Feb 13, 2019 · N659GT · Boeing 767281 · Central Display
  > AIR TURN BACK ELECTRICAL SMELL MCP STOPPED WORKING(<P>REPLACED MCP PER AMM 22-11-02. INSTALLATION CHECKS GOOD' OPS CHECKS GOOD IAW 22-00-00. A/C STILL REMAINS CAT 3 B<BR /></P>)
- [SDR UIEA2018102602361](https://openairdocs.org/sdr/UIEA2018102602361.md): Switch · faulty · Oct 26, 2018 · N659GT · Boeing 767281 · Landing Gear Position and Warning
  > RED "CONFIG" LIGHT ILLUMINATED IN FLIGHT ACCOMPANIED BY EICAS "FLAPS" WARNING. WARNING SIREN. UNABLE TO CANCEL. PERFORMED FIM 31-51 FT 808 PER BLOCK 3 PSEU BITE FAULTS S266 NOSE GEAR NOT COMPRESSED SWITCH. R&R S266 IAW AMM 32-09-08, ADJUSTMENT AND OPS CHECKS O
- [SDR UIEA2017101201958](https://openairdocs.org/sdr/UIEA2017101201958.md): Terminal · arced · Oct 12, 2017 · N659GT · Boeing 767281 · Ice/Rain Protection System Wiring
  > VERY STRONG ODOR OF ELECTRICAL FUMES AFTER TAKEOFF, TURNED OFF RIGHT FORWARD WINDOW HEAT, ODOR DISSIPATED IMMEDIATELY. FOUND THE LOWER RIGHT TERMINAL LOOSE AND ARCING, CLEANED THE TERMINAL AND REINSTALLED. OPS CHECKED GOOD IAW AMM 56-11-00.
- [SDR UIEA2017093001907](https://openairdocs.org/sdr/UIEA2017093001907.md): Engine · odor · Sep 25, 2017 · N659GT · Boeing 767281 · Engine (Turbine/Turboprop)
  > STRONG ELECTRICAL ODOR DETECTED WHIILE CLIMBING THROUGH FL 320 AND UNTIL A RETURN LANDING, THE ODOR DISSIPATED AT 4000 FT, NO SMOKE OR OTHER ABNORMALLY OBSERVED. REMOVED AND REPLACED THE NR 2 ENGINE IAW 71-00-00, PERFORMED REQUIRED TEST 1, 3, 4, 7, AND 12.
- [SDR UIEA2017040500518](https://openairdocs.org/sdr/UIEA2017040500518.md): Structure · cracked · Apr 3, 2017 · N659GT · Boeing 767281 · Fuselage Main, Structure
  > BS 859.5, LBL 89, BELOW WL 200 STRUCTURE BETWEEN BOTTOM TWO FASTENERS CRACKED. REPAIRED IAW BULLETIN 76753A0209, REV 2, FIGURE 7.
- [SDR UIEA2017040500519](https://openairdocs.org/sdr/UIEA2017040500519.md): Skin · corroded · Apr 3, 2017 · N659GT · Boeing 767281 · Cargo/Baggage Doors
  > FORWARD CARGO DOOR, INTERIOR SIDE, 82 INCHES FROM LEADING EDGE AT LOWER DOOR FRAME WEB GAS SURFACE CORRODED. REMOVED AND REPLACED THE FWD CARDO DOOR LOWER SKIN PANEL IAW SRM 51-40-02-0G-0, AND DWG 140T2340, SHEET 2, REV.
- [SDR UIEA2017040500520](https://openairdocs.org/sdr/UIEA2017040500520.md): Skin · corroded · Apr 3, 2017 · N659GT · Boeing 767281 · Cargo/Baggage Doors
  > FWD CARGO DOOR INSIDE UPPER AREA CORRODED, APPROXIMATELY 24 INCHES FROM AFT EDGE. REMOVED AND REPLACED FWD CARGO DOOR SKIN IAW SRM 51-40-02-0G-0, AND DRAWING 140T2640, SHEET 2, REV.
- [SDR UIEA2017040500521](https://openairdocs.org/sdr/UIEA2017040500521.md): Keelbeam · corroded · Apr 3, 2017 · N659GT · Boeing 767281 · Fuselage Main, Keel
  > LEFT KEEL BEAM CORRODED ON LOWER SURFACE OF INBOARD LOWER FLANGE, BS 990 - 1015, LBL 10. REPAIRED THE KEEL BEAM IAW EA 170090, REV IR, AND EO 6753A408.
- [SDR UIEA2017040500522](https://openairdocs.org/sdr/UIEA2017040500522.md): Floor Panel · gouged · Apr 3, 2017 · N659GT · Boeing 767281 · Fuselage Floor Panel
  > MAIN CARGO DECK FLOOR PANEL 2420 IS GOUGE ON TOP. REPAIRED THE FLOOR PANEL IAW EA 170084, REV A, AND EO 6753A414.
- [SDR UIEA2016062800535](https://openairdocs.org/sdr/UIEA2016062800535.md): Light · inoperative · May 28, 2016 · N659GT · Boeing 767281 · Emergency Lighting
  > L1 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. RELAMPED L1 DOOR EXTERIOR EMERGENCY LIGHT. OPS OK IAW AMM 33-51-00.
- [SDR UIEA2016021500097](https://openairdocs.org/sdr/UIEA2016021500097.md): Escape Rope · damaged · Feb 14, 2016 · N659GT · Boeing 767281 · Emergency Equipment
  > MAIN DECK FWD CARGO, DESCENT DEVICE F UNRAVELED, PN 379103D-29. R & R MAIN DECK DESCENT DEVICE F IAW AMM 25-61-00.
- [SDR UIEA2015091700535](https://openairdocs.org/sdr/UIEA2015091700535.md): Structure · corroded · Sep 14, 2015 · N659GT · Boeing 767281 · Horizontal Stabilizer Miscellaneous Structure
  > CORROSION STAB CTR BOX INTERIOR, UPPER STRUCTURE NR 11, FWD VERTICAL LEG. BLENDED AREA, FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 55-10-03 & FIG 201 DETAIL 1 REPAIR 1.
- [SDR UIEA2015091700538](https://openairdocs.org/sdr/UIEA2015091700538.md): Skin Panel · corroded · Sep 14, 2015 · N659GT · Boeing 767281 · Wing, Plate/Skin
  > LEFT WING UPPER SKIN CORRODED AROUND OVERWING FILL PART ADAPTER. REPAIRED IAW DOC 47172REA12 REV 1R & REA 47172REA08 REV 1R.
- [SDR UIEA2015091700539](https://openairdocs.org/sdr/UIEA2015091700539.md): Skin · corroded · Sep 14, 2015 · N659GT · Boeing 767281 · Wing, Plate/Skin
  > RIGHT WING UPPER SKIN IS CORRODED AROUND THE OVERWING FILL PORT ADAPTER. REMOVED CORROSION IAW SRM 57-20-01. FOUND TO BE OUT OF LIMITS. REPAIRED AREA IAW REA 47172 REA 10 REV IR.
- [SDR UIEA2015091700540](https://openairdocs.org/sdr/UIEA2015091700540.md): Support · corroded · Sep 14, 2015 · N659GT · Boeing 767281 · Trailing Edge Flaps
  > LEFT WING NR 1 FLAP SUPPORT 1, 2 & 3 BEAM, OTBD STUD HOLE HAS CORROSION. REAMED HOLE & COMPLIED WITH REA 47172 REA07 REV IR.
- [SDR UIEA2015091500530](https://openairdocs.org/sdr/UIEA2015091500530.md): Rib · damaged · Sep 14, 2015 · N659GT · Boeing 767281 · Trailing Edge Flaps
  > NUMBER 8 FLAP SUPPORT, OTBD RIB NR 2 HOLE OF THE ROTARY ACTUATOR MOUNT, HAS A HFEC INDICATION. REPAIRED DEFECTIVE HOLE IN THE NR 8 FLAP SUPPORT OTBD RIB IAW REA 47172REA11.
- [SDR UIEA2015091500526](https://openairdocs.org/sdr/UIEA2015091500526.md): Support · corroded · Sep 14, 2015 · N659GT · Boeing 767281 · Trailing Edge Flaps
  > LEFT WING NR 1 FLAP SUPPORT 1, 2 & 3 BEAM INBD HANGER LOCATION, AFT UPPER HOLE HAS CORROSION. REAMED HOLE & COMPLIED WITH REA 47172REA01 REV IR.
- [SDR UIEA2015091500527](https://openairdocs.org/sdr/UIEA2015091500527.md): Panel · corroded · Sep 14, 2015 · N659GT · Boeing 767281 · Trailing Edge Flaps
  > LEFT WING OTBD FLAP, LOWER STRESS PANEL LE CORRODED, REPLACED FLAP.
- [SDR UIEA2015091500528](https://openairdocs.org/sdr/UIEA2015091500528.md): Rib · damaged · Sep 14, 2015 · N659GT · Boeing 767281 · Trailing Edge Flaps
  > LEFT WING NR 2 FLAP SUPPORT, NR 3 HOLE HAS HFEC DEFECT INDICATION. REAMED NR 2 FLAP SUPPORT, NR 3 & 4 HOLES IAW REA 47172REA09.
- [SDR UIEA2015091500529](https://openairdocs.org/sdr/UIEA2015091500529.md): Rib · damaged · Sep 14, 2015 · N659GT · Boeing 767281 · Trailing Edge Flaps
  > NUMBER 1 FLAP SUPPORT OUTER RIB HAS 5 HOLES THAT SHOW DEFECTS. REPAIRED DEFECTIVE HOLES IN THE NR 1 FLAP SUPPORT OUTER RIB IAW REA 4717REA11.
- [SDR UIEA2015021600124](https://openairdocs.org/sdr/UIEA2015021600124.md): Spar · corroded · Feb 14, 2015 · N659GT · Boeing 767281 · Wing Spar
  > CORROSION ON RT WING AFT SPAR AT WS 920. REPAIRED RT WING TE IAW REA 47142REA01. SEE REA NR 547810000 0151 & PARTIAL WORK SHEET NR 3, IN WORK ORDER 9607 FOR WORK PERFORMED.

## 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 = 'N659GT' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N659GT/reports

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