N659GT
Service difficulty reports · 37
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 = 'N659GT' 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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR FIKA2021051200045Connector · looseTHIS 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 WSDR ABXR2020042400022Skin Panel · delaminatedRIGHT SIDE VERTICAL STAB SKIN DELAMINATED. REMOVED AND REPAIRED SKIN PANEL AND INSTALLED STAB SKIN WITH INTERIM FASTENERS.SDR UIEA2020030900407Angle · corrodedCORROSION 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 UIEA2020030900409Keelbeam · corrodedLLW - 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 UIEA2020030900410Splice Plate · corrodedCORROSION 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 UIEA2020030900411Skin · crackedUPPER 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 UIEA2020030900412Spar · corrodedCORROSION 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 UIEA2020030900413Rib · corrodedUPPER 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 LIMISDR UIEA2020030900414Attach Bracket · crackedATTACHED 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 UIEA2020030900415Structure · corrodedFLANGE 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 UIEA2020030900416Rib · crackedL HORIZONTAL LEADING EDGE INBD END RIB IS CRACKED.(<P>CUT OUT DAMAGE AND REPAIRED IAW B767 SRM 55-10-09 REPAIR 1.</P>)SDR UIEA2020030900417Angle · crackedCLOSE 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 UIEA2020030900418Structure · corrodedL 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.</SPANSDR UIEA2020030900419Attach Bracket · crackedATTACH 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 UIEA2019121876093Escape Reel · unwanted deploy4 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 CLEARSSDR UIEA2019121606086Escape Reel · unwanted deploy4EA GALLEY DESCENT DEVICES DEPLOY; 3EA AVAILABLE.(<P>TRANSFERRED TO MDDR 122134 IAW MEL 25-61-01-01, CAT 'C'.</P>)SDR UIEA2019021303210Control Panel · smokeAIR 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 UIEA2018102602361Switch · faultyRED "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 OSDR UIEA2017101201958Terminal · arcedVERY 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 UIEA2017093001907Engine · odorSTRONG 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 UIEA2017040500518Structure · crackedBS 859.5, LBL 89, BELOW WL 200 STRUCTURE BETWEEN BOTTOM TWO FASTENERS CRACKED. REPAIRED IAW BULLETIN 76753A0209, REV 2, FIGURE 7.SDR UIEA2017040500519Skin · corrodedFORWARD 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 UIEA2017040500520Skin · corrodedFWD 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 UIEA2017040500521Keelbeam · corrodedLEFT 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 UIEA2017040500522Floor Panel · gougedMAIN CARGO DECK FLOOR PANEL 2420 IS GOUGE ON TOP. REPAIRED THE FLOOR PANEL IAW EA 170084, REV A, AND EO 6753A414.SDR UIEA2016062800535Light · inoperativeL1 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. RELAMPED L1 DOOR EXTERIOR EMERGENCY LIGHT. OPS OK IAW AMM 33-51-00.SDR UIEA2016021500097Escape Rope · damagedMAIN DECK FWD CARGO, DESCENT DEVICE F UNRAVELED, PN 379103D-29. R & R MAIN DECK DESCENT DEVICE F IAW AMM 25-61-00.SDR UIEA2015091700535Structure · corrodedCORROSION 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 UIEA2015091700538Skin Panel · corrodedLEFT WING UPPER SKIN CORRODED AROUND OVERWING FILL PART ADAPTER. REPAIRED IAW DOC 47172REA12 REV 1R & REA 47172REA08 REV 1R.SDR UIEA2015091700539Skin · corrodedRIGHT 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 UIEA2015091700540Support · corrodedLEFT WING NR 1 FLAP SUPPORT 1, 2 & 3 BEAM, OTBD STUD HOLE HAS CORROSION. REAMED HOLE & COMPLIED WITH REA 47172 REA07 REV IR.SDR UIEA2015091500530Rib · damagedNUMBER 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 UIEA2015091500526Support · corrodedLEFT 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 UIEA2015091500527Panel · corrodedLEFT WING OTBD FLAP, LOWER STRESS PANEL LE CORRODED, REPLACED FLAP.SDR UIEA2015091500528Rib · damagedLEFT 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 UIEA2015091500529Rib · damagedNUMBER 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 UIEA2015021600124Spar · corrodedCORROSION 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.
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