N656GT

Service difficulty reports · 71

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 = 'N656GT' 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 PCSA202110150184Control Panel · intermittentAS THE CREW WERE APPROACHING TOP CLIMB OF FLIGHT LEVEL 380, THE CREW RECEIVED A MASTER WARNING,FOLLOWED BY A FIRE BELL, EICAS MESSAGE OF "MAIN DECK CARGO FIRE" AND THE MAIN DECK ZONES THAT WERE SENSING SMOKE ENUNCIATED. THE CREW PROCEEDED TO COMMENCE THE QRH Oct 12, 2021 · N656GT · Boeing 767281 · Fire Protection SystemSDR UIEA2020100902198Escape Reel · unsecureESCAPE REEL NOT SECURED. RESECURED DESCENT DEVICE, IAW AIA 25-61-03.Oct 9, 2020 · N656GT · Boeing 767281 · Emergency EquipmentSDR UIEA2020012310103Engine · vibrationHEARD SEVERAL BANGS AND FELT THE AIRFRAME SHUDDER EACH TIME FOLLOWED BY ABNORMAL ENGINE INDICATIONS ON RIGHT ENGINE, WHICH RESULTED IN THE ENGINE SHUTTING DOWN IN FLIGHT. NR 2 ENG REMOVED & REPLACED IAW WORK CARD A-71-999-03-01.Jan 20, 2020 · N656GT · Boeing 767281 · Engine (Turbine/Turboprop)SDR UIEA2019120906031Bushing · leakingRW MAIN TANK SUMP DRAIN LEAKING.(<P>REMOVED AND REPLACED SUMP DRAIN & SUMP DRAIN BUSHING IAW B767 AMM 28-11-05 AND AMES ENGINEERING 47389REA03. LEAK CHECK GOOD IAW B767 AMM 28-11-00-206. SEE PARTIAL WORK ACCOMPLISHED AND PARTIAL WORKSHEET 45 FOR WORK COMPLETEDDec 4, 2019 · N656GT · Boeing 767281 · Fuel StorageSDR UIEA2019120906032Splice Plate · corrodedTHE RIGHT OVERWING LONGERON HAS A LARGE AREA OF CORROSION NEAR THE AFT END.(<P>AREA OF CORROSION FOUND TO BE OUT OF LIMITS IAW B767-200 SRM 53-50-05. AREA BEYOND LIMITS, THEREFORE REPLACEMENT OF R/H EXTERIOR LONGERON SPLICE PLATE WAS ACCOMPLISHED IAW AMES DOCUDec 4, 2019 · N656GT · Boeing 767281 · Fuselage Miscellaneous StructureSDR UIEA2019120906033Web · corrodedCORROSION IN SEVERAL AREAS OF KEEL WEB IN RWW (M), JUST INBD OF BODY DOOR AT STA 955-1021.(<P>REPAIRED DAMAGE IAW AMES DOCUMENT 47389REA09 AND 47389REA07. SEE PARTIAL WORK ACCOMPLISHED AND PARTIAL WORKSHEET #10 PAGES 1-9 FOR WORK COMPLETED AND 47389REA10.</P><Dec 4, 2019 · N656GT · Boeing 767281 · Fuselage Miscellaneous StructureSDR UIEA2019120906034Rib · corrodedRW LES 477 LOWER AIR LOAD RIB CORRODED.(<P>REMOVED AND REPLACED AIR LOAD RIB RW LES 477 IAW B767 SRM 51-40-02 PARAGRAPH 9. SEE PARTIAL WORK ACCOMPLISHED.</P>)Dec 4, 2019 · N656GT · Boeing 767281 · Wing, Rib/BulkheadSDR UIEA2019120906035Web · corrodedCORROSION IN SEVERAL AREAS ON UPPER SURFACE OF KEEL WEB, STA 970-1021 APPROX.(<P>REPAIRED DAMAGE IAW AMES DOCUMENTS 47389REA09 AND 47389REA07, SEE PARTIAL WORK ACCOMPLISHED AND PARTIAL WORKSHEET #7 PAGES 1-8.</P><P><BR DATA-MCE-BOGUS="1" /></P><P>PN: 145T8612-Dec 4, 2019 · N656GT · Boeing 767281 · Fuselage Miscellaneous StructureSDR UIEA2019120906036Longeron · corrodedLEFT SIDE OVERWING LONGERON CORRODED.(<P>REMOVED CORROSION ON LEFT SIDE OVERWING LONGERON IAW B767-200 SRM 51-10-02 AND REPAIRED IAW AMES NO. #47389REA05. SEE PARTIAL WORK ACCOMPLISHED AND PARTIAL WORKSHEET #9, PGS 1 & 2.</P>)Dec 4, 2019 · N656GT · Boeing 767281 · Fuselage Main, StructureSDR UIEA2019120906037Door Frame · corroded ALC DOOR CUTOUT, FWD EDGE FRAME STRAP UPPER SURFACE IS CORRODED AT STA 1270, S32R.(<P>REPAIRED FRAME IAW B767-200 SRM 51-40-02 AND AMES 47389REA06. SEE PARTIAL WORK ACCOMPLISHED AND PWS 46.</P>)Dec 4, 2019 · N656GT · Boeing 767281 · Fuselage Main, StructureSDR UIEA2019120906038Support · corrodedROLLER TRAY FRAME SUPPORT IS CORRODED AT STA 720, S 33R. (<P>BLENDED CORROSION ON FLOOR FRAME UPPER CHORD @ STA 720 ST 33R IAW B767 SRM 53-00-07 FIG 101 DET VIII. FOUND TO BE OUT OF LIMITS. ORIGINAL THICKNESS 103". MATERIAL REMAINING .036". MATERIAL REMOVED .0Dec 4, 2019 · N656GT · Boeing 767281 · Fuselage Miscellaneous StructureSDR ABXR2019112700322Floorbeam · corrodedFLOOR FRAME UPPER CHORD CORRODEDNov 27, 2019 · N656GT · Boeing 767281 · Fuselage Main, Floor BeamSDR ABXR2019112700321Failsafe · corrodedFAILSAFE STRAP ON FRAME AT ALC DOOR CUTOUT WAS CORRODEDNov 27, 2019 · N656GT · Boeing 767281 · Fuselage Main, StructureSDR ABXR2019112700320Splice Plate · corrodedLEFT OVERWING SPLICE PLATE CORRODED.Nov 27, 2019 · N656GT · Boeing 767281 · Fuselage Miscellaneous StructureSDR ABXR2019112700319Keel · corrodedKEEL CORRODED AT STA 970-1021Nov 27, 2019 · N656GT · Boeing 767281 · Fuselage Main, KeelSDR ABXR2019112700318Rib · corrodedRT WING AIRLOAD RIB CORRODEDNov 27, 2019 · N656GT · Boeing 767281 · Wing, Rib/BulkheadSDR ABXR2019112700317Web · corrodedKEEL WEB IN RWW CORRODEDNov 27, 2019 · N656GT · Boeing 767281 · Fuselage Main, KeelSDR ABXR201911270316Stringer Splice · corrodedRT OVERWING LONGERON SPLICE PLATE CORRODEDNov 27, 2019 · N656GT · Boeing 767281 · Fuselage Main, Longeron/StringerSDR ABXR2019112700315Bushing · wornRT WING SUMP DRAIN LEAKING AT BUSHINGNov 27, 2019 · N656GT · Boeing 767281 · Wing StructureSDR UIEA2017121102385Actuator · leakingRH LANDING GEAR AFT SIDE BRACE ACTUATOR LEAKING.(<P>REMOVED AND REPLACED RH MLG SIDE BRACE ACTUATOR ASS. OPS CHECK NORMAL IAW AMM 32-32-02</P>)Dec 11, 2017 · N656GT · Boeing 767281 · Landing Gear ActuatorSDR UIEA2017121102387Control Unit · leakingLEFT STCM INPUT SHAFT SEAL HAS HYDRAULIC LEAK.(<P>REMOVED AND REPLACED LEFT STCM. OPS CHECK NORMAL IAW AMM 27-41-00-715-014 TASK .</P>)Nov 11, 2017 · N656GT · Boeing 767281 · Hydraulic System, MainSDR UIEA2017121102386Starter · damagedNO 2 ENGINE STARTER WITH METAL FRAGMENT LARGER THAN 0-1 INCH.(<P>REMOVED AND REPLACED THE #2 ENGINE STARTER IAW AMM 80-11-01. OPS CHECK NORMAL.</P>)Nov 11, 2017 · N656GT · Boeing 767281 · Engine StarterSDR UIEA2017080601420Hydraulic System · lowLEFT HYD SYSTEM QTY WENT TO 0. C/W MTX PROCEDURES DISPATCH YK AT 1849Z DUE DATE 16AUG17.Aug 6, 2017 · N656GT · Boeing 767281 · Hydraulic System, MainSDR UIEA2017040900531Line · looseDURING TAKE OFF AT 80 KTS, THE RT ENGINE ROLLED BACK TO 96.8 N1, UNABLE TO PUSH BACK TO MATCH, LT ENGINE AT 100.4. ACCOMPLISHED EEC BITE IAW FIM 71-01, 804, NO FAULTS NOTED. FOUND LOOSE CBT LINE ON MEC. RAN ENGINE TO POWER IAW AMM 71-01-00, ALL INDICATIONApr 7, 2017 · N656GT · Boeing 767281 · Fuel Controlling SystemSDR UIEA2017022000205Housing · corrodedLEFT WING BOOST PUMP HOUSING SHUT OFF SLEEVE HAS CORROSION TO THE INSIDE FUEL PATH SURFACE. REMOVED AND REPLACED THE BOOST FUEL PUMP HOUSING IAW AMM 28-92-03-404-027.Mar 1, 2017 · N656GT · Boeing 767281 · Fuel Boost PumpSDR UIEA2017022000206Housing · corrodedRIGHT WING BOOST PUMP HOUSING SHUT OFF SLEEVE HAS CORROSION.Mar 1, 2017 · N656GT · Boeing 767281 · Fuel Boost PumpSDR UIEA2017022000207Rod · corrodedAPU BLEED AIR DUCT SUPPORT ROD FACING LEFT & RIGHT CORRODED LOCATED IN AFT HORIZONTAL STAB ACCESS AREA. REMOVED APU BLEED AIR DUCT SOPPORT ROD AND INSTALLED A NEW ONE IAW AMM 20-11-00.Mar 1, 2017 · N656GT · Boeing 767281 · Horizontal Stabilizer StructureSDR UIEA2017022000210Shim · corrodedFWD CARGO DOOR AFT HOOK APPEARS TO HAVE CORROSION UNDER MOUNT SURFACE. INSPECTION REVEALED CORROSION IS ON LIMITED SHIMS. REPLACED AND REMOVED THE HOOK IAW SRM 51-20-11-0G-0, AND AMM 20-11-00-910-802.Mar 1, 2017 · N656GT · Boeing 767281 · Cargo/Baggage DoorsSDR UIEA2017022000211Tee Fitting · corrodedLEFT HORIZONTAL STAB, OTBD END RIB 17, UPPER ATTACH TEE FITTING FOR STAB TIP HAS CORROSION AT THE FWD END, BOTH INBD AND OTBD SIDES, FWD 3 INCHES. REMOVED CORROSION IAW AMM 51-10-02-0G-0. FOUND TO BE IN LIMITS IAW SRM 55-10-09-1A-1, FIGURE 101, DETAIL 1.Mar 1, 2017 · N656GT · Boeing 767281 · Horizontal Stabilizer StructureSDR UIEA2017022000213Attach Fitting · corrodedRIGHT HORIZONTAL STAB INBD END, INBD ATTACH FLANGE FOR PANEL 345CB HAS CORROSION ON THE UPPER & LOWER SURFACE OF HORIZONTAL FLANGE. REMOVED CORROSION IAW SRM 55-10-09 AND REINSTALLED IAW SRM 51-40-02- & 02.Mar 1, 2017 · N656GT · Boeing 767281 · Horizontal Stabilizer StructureSDR UIEA2017022000214Attach Fitting · corrodedRIGHT HORIZONTAL STAB OTBD END, AFT OTBD CHORDWISE ATTACH FLANGE FOR THE STAB TIP HAS CORROSION ON THE UPPER SURFACE. REMOVED AND REPLACED THE ATTACH FLANGE IAW SRM 51-40-2, PARAGRAPH 4.Mar 1, 2017 · N656GT · Boeing 767281 · Horizontal Stabilizer StructureSDR UIEA2017022000215Attach Fitting · corrodedRIGHT HORIZONTAL STAB OTBD END, AFT SPANWISE ATTACH FLANGE FOR THE HORIZONTAL TIP HAS CORROSION ON THE TOP SURFACE. REMOVED CORROSION IAW51-10-02-OG-0 PARA 14 & 15, FIG 1. FOUND TO BE WITHIN LIMITS IAW SRM 55-10-09 .Mar 1, 2017 · N656GT · Boeing 767281 · Horizontal Stabilizer StructureSDR UIEA2017022000216Window Frame · corrodedCABIN WINDOW FRAME, STRINGER 16R, IS CORRODED AT LOWER EDGE. REMOVED AND REPLACED THE WINDOW FRAME IAW SRM 51-40-02-0G-0 AND DRAWING 143T3410.Mar 1, 2017 · N656GT · Boeing 767281 · Fuselage Main, StructureSDR UIEA2017022000227Lock · corrodedMAIN DECK CARGO BS 1480 - 1500, LBL 48 - 72. TWO BROKEN BAT WING CARGO LOCKS ARE CORRODDED, REMOVED CORROSION AND FOUND OUT OF LIMITS IAW CMM 25-50-99.Mar 1, 2017 · N656GT · Boeing 767281 · Fuselage Main, Attach FittingsSDR UIEA2017022000226Lock · corrodedMAIN DECK CARGO BS 1307 - 1327, LBL 48 - 72. FOUR BAT WINGS CARGO LOCKS CORRODDED. REMOVED THE CORROSION IAW SRM 51-10-02, AND FOUND TO BE IN LIMITS IAW CMM 25-50-99.Mar 1, 2017 · N656GT · Boeing 767281 · Fuselage Main, Attach FittingsSDR UIEA2017022000225Attach Fitting · corrodedMAIN DECK CARGO BS 1177 - 1197, LBL 48 AND 72, FOUR BAT WING CARGO LOCK FITTINGS ARE CORRODED. CLEANED & EVALUATED THE AREAS UNDER CARGO LOCKS IAW SRM 51-10-02. FOUND IN LIMITS IAW CMM 25-50-94.Mar 1, 2017 · N656GT · Boeing 767281 · Fuselage Main, Attach FittingsSDR UIEA2017022000224Attach Fitting · corrodedMAIN DECK CARGO BS 1349 - 1369, LBL 48 - 70. FOUR BAT WINGS CARGO LOCKS ATTACH FITTINGS FOUND CORRODED AFTER REMOVAL OF BAT WING CARGO LOCKS. CLEANED & EVALUATED THE AREAS UNDER CARGO LOCKS ATTACH FITTING IAW SRM 51-10-02, FOUND IN LIMITS IAW CMM 25-50-94.Mar 1, 2017 · N656GT · Boeing 767281 · Fuselage Main, Attach FittingsSDR UIEA2017022000223Attach Fitting · corrodedMAIN DECK CARGO BS 1437 TO 1461, LBL 48 TO 72. FOUR BAT WINGS CARGO LOCKS ATTACH FITTINGS FOUND CORRODED AFTER REMOVAL OF BAT WING CARGO LOCKS. CLEANED & EVALUATED THE AREAS UNDER CARGO LOCKS ATTACH FITTINGS IAW SRM 51-10-02. FOUND IN LIMITS IAW CMM 25-50-9Mar 1, 2017 · N656GT · Boeing 767281 · Fuselage Main, Attach FittingsSDR UIEA2017022000222Attach Bracket · corrodedMAIN DECK CARGO BS 1510 TO 1570, LBL 4. ONE BUMPER RAIL ATTACH BRACKET CORRODED. REMOVED & REINSTALLED THE BUMPER RAIL IAW SRM 51-40-02. CLEANED THE BUMPER RAIL IAW SOPM 20-30-03, NO CORROSION NOTED.Mar 1, 2017 · N656GT · Boeing 767281 · Fuselage Main, Attach FittingsSDR UIEA2017022000221Fitting · corrodedMAIN DECK CARGO BS1395 TO 1417, LBL 72, FOUR BAT WING CARGO LOCKS ATTACH FITTINGS FOUND CORRODED. FITTINGS LOCATED UNDER REMOVED BAT WING CARGO LOCKS. REF NRI 3280. CLEANED AND EVALUATED MAIN DECK CARGO IAW SRM 51-10-02. FOUND IN LIMITS IAW CMM 25-50-94. TREAMar 1, 2017 · N656GT · Boeing 767281 · Fuselage Main, Attach FittingsSDR UIEA2017022000220Attach Bracket · corrodedMAIN DECK CARGO BS 1257 TO 1277 LBL 48 TO 72. FOUR EACH BAT WING CARGO LOCKS ATTACH BRACKETS CORRODED. CLEANED & EVALUATED IAW SRM 51-10-02. FOUND TO BE IN LIMITS IAW CMM 25-50-94.Mar 1, 2017 · N656GT · Boeing 767281 · Fuselage Main, Attach FittingsSDR UIEA2017022000219Fitting · corrodedMAIN DECK CARGO BAY BS 1237 - 1217, LBL 48 TO 72. FITTING LOCATED UNDER REMOVED BATWINGS CORRODED. CLEANED & EVALUATED IAW SRM 51-10-02. FOUND IN LIMITS IAW CMM 25-50-94. TREATED & PRIMED IAW SRM 51-20-01-OG-0.Mar 1, 2017 · N656GT · Boeing 767281 · Fuselage Miscellaneous StructureSDR UIEA2017022000218Inlet · corrodedNR 2 ENGINE INLET LOWER TWO BOLT HOLES HAVE CORROSION. FREEZE PLUGS FABRICATED AND INSTALLED IAW SRM 51-20-07, PARA B, FIG 5 & FIG C, AND PARA 3B AND RDR PMO-TLS-17-007-14B.Mar 1, 2017 · N656GT · Boeing 767281 · Turbine Engine Air Inlet SectionSDR UIEA2017022000217Support Channel · corrodedRT WINE TE PANEL SUPPORT CHANNEL AT PANEL 661PB HAS CORROSION BETWEEN NUT PLATE HOLES. REMOVED AND REPLACED THE SUPPORT CHANNEL IAW SRM 51-40-05 & DWG 113T1912, SHEET 1, REV D.Mar 1, 2017 · N656GT · Boeing 767281 · Wing Main, Frame StructureSDR UIEA2016092000763Engine · power lossRTO ON TAKEOFF RT ENGINE DID NOT PRODUCE TAKEOFF THRUST, RTO BELOW 80 KNOTS. COMPLIED WITH GROUND TEST NR 4 VERIFIED BOTH ENGINE MAKE T/O POWER 108.6 NO THROTTLE SPLIT ELECTRONIC ENGINE CONTROL OFF REF AMM 71-00-00. TRANSFERED TO MDDR 70393 IAW MEL 73-21-01Sep 20, 2016 · N656GT · Boeing 767281 · Engine (Turbine/Turboprop)SDR UIEA2016011800021Escape Rope · unserviceableCOCKPIT DESCENT DEVICE CABLE EXTENDED. R & R DEFECTIVE DESCENT DEVICE IAW AMM 25-61-03.Jan 18, 2016 · N656GT · Boeing 767281 · Emergency EquipmentSDR UIEA2015121100722Warning System · false activationTRAILING EDGE FLAP DISAGREE MSG DISPLAYED & APPROACH LANDING FLAPS 20. TROUBLE SHOT IAW FIM 27-51 FIM FAULT TREE, NO FAULTS NOTED. PERFORMED BITE CHECK OF FSEU, NO FAULTS REPORTED, OK FOR SERVICE.Dec 11, 2015 · N656GT · Boeing 767281 · Trailing Flap Position Indicating SystemSDR UIEA2015081400410Strap · crackedLEFT FAILSAFE CRACKED AT STATION 955. REPAIRED IAW EO 06753A070, TRIMMED.Aug 13, 2015 · N656GT · Boeing 767281 · Fuselage Main, FrameSDR UIEA2015081400411Frame · damagedELONGATED HOLE THROUGH FAILSAFE STRAP & FRAME CHORD. REPAIRED IAW REA 47169 REA 10.Aug 13, 2015 · N656GT · Boeing 767281 · Fuselage Main, FrameSDR UIEA2015081400412Failsafe · crackedRIGHT SIDE FAILSAFE CRACKED AT STATION 955. REPAIRED IAW EO 06753A070, TRIMMED.Aug 13, 2015 · N656GT · Boeing 767281 · Fuselage Main, Frame
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