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 COMPLETED - [SDR UIEA2019120906032](https://openairdocs.org/sdr/UIEA2019120906032.md): Splice Plate · corroded · Dec 4, 2019 · N656GT · Boeing 767281 · Fuselage Miscellaneous Structure > THE RIGHT OVERWING LONGERON HAS A LARGE AREA OF CORROSION NEAR THE AFT END.(
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 DOCU - [SDR UIEA2019120906033](https://openairdocs.org/sdr/UIEA2019120906033.md): Web · corroded · Dec 4, 2019 · N656GT · Boeing 767281 · Fuselage Miscellaneous Structure > CORROSION IN SEVERAL AREAS OF KEEL WEB IN RWW (M), JUST INBD OF BODY DOOR AT STA 955-1021.(
REPAIRED DAMAGE IAW AMES DOCUMENT 47389REA09 AND 47389REA07. SEE PARTIAL WORK ACCOMPLISHED AND PARTIAL WORKSHEET #10 PAGES 1-9 FOR WORK COMPLETED AND 47389REA10.
< - [SDR UIEA2019120906034](https://openairdocs.org/sdr/UIEA2019120906034.md): Rib · corroded · Dec 4, 2019 · N656GT · Boeing 767281 · Wing, Rib/Bulkhead > RW LES 477 LOWER AIR LOAD RIB CORRODED.(REMOVED AND REPLACED AIR LOAD RIB RW LES 477 IAW B767 SRM 51-40-02 PARAGRAPH 9. SEE PARTIAL WORK ACCOMPLISHED.
) - [SDR UIEA2019120906035](https://openairdocs.org/sdr/UIEA2019120906035.md): Web · corroded · Dec 4, 2019 · N656GT · Boeing 767281 · Fuselage Miscellaneous Structure > CORROSION IN SEVERAL AREAS ON UPPER SURFACE OF KEEL WEB, STA 970-1021 APPROX.(REPAIRED DAMAGE IAW AMES DOCUMENTS 47389REA09 AND 47389REA07, SEE PARTIAL WORK ACCOMPLISHED AND PARTIAL WORKSHEET #7 PAGES 1-8.
PN: 145T8612- - [SDR UIEA2019120906036](https://openairdocs.org/sdr/UIEA2019120906036.md): Longeron · corroded · Dec 4, 2019 · N656GT · Boeing 767281 · Fuselage Main, Structure > LEFT SIDE OVERWING LONGERON CORRODED.(
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.
) - [SDR UIEA2019120906037](https://openairdocs.org/sdr/UIEA2019120906037.md): Door Frame · corroded · Dec 4, 2019 · N656GT · Boeing 767281 · Fuselage Main, Structure > ALC DOOR CUTOUT, FWD EDGE FRAME STRAP UPPER SURFACE IS CORRODED AT STA 1270, S32R.(REPAIRED FRAME IAW B767-200 SRM 51-40-02 AND AMES 47389REA06. SEE PARTIAL WORK ACCOMPLISHED AND PWS 46.
) - [SDR UIEA2019120906038](https://openairdocs.org/sdr/UIEA2019120906038.md): Support · corroded · Dec 4, 2019 · N656GT · Boeing 767281 · Fuselage Miscellaneous Structure > ROLLER TRAY FRAME SUPPORT IS CORRODED AT STA 720, S 33R. (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.0 - [SDR ABXR2019112700322](https://openairdocs.org/sdr/ABXR2019112700322.md): Floorbeam · corroded · Nov 27, 2019 · N656GT · Boeing 767281 · Fuselage Main, Floor Beam > FLOOR FRAME UPPER CHORD CORRODED - [SDR ABXR2019112700321](https://openairdocs.org/sdr/ABXR2019112700321.md): Failsafe · corroded · Nov 27, 2019 · N656GT · Boeing 767281 · Fuselage Main, Structure > FAILSAFE STRAP ON FRAME AT ALC DOOR CUTOUT WAS CORRODED - [SDR ABXR2019112700320](https://openairdocs.org/sdr/ABXR2019112700320.md): Splice Plate · corroded · Nov 27, 2019 · N656GT · Boeing 767281 · Fuselage Miscellaneous Structure > LEFT OVERWING SPLICE PLATE CORRODED. - [SDR ABXR2019112700319](https://openairdocs.org/sdr/ABXR2019112700319.md): Keel · corroded · Nov 27, 2019 · N656GT · Boeing 767281 · Fuselage Main, Keel > KEEL CORRODED AT STA 970-1021 - [SDR ABXR2019112700318](https://openairdocs.org/sdr/ABXR2019112700318.md): Rib · corroded · Nov 27, 2019 · N656GT · Boeing 767281 · Wing, Rib/Bulkhead > RT WING AIRLOAD RIB CORRODED - [SDR ABXR2019112700317](https://openairdocs.org/sdr/ABXR2019112700317.md): Web · corroded · Nov 27, 2019 · N656GT · Boeing 767281 · Fuselage Main, Keel > KEEL WEB IN RWW CORRODED - [SDR ABXR201911270316](https://openairdocs.org/sdr/ABXR201911270316.md): Stringer Splice · corroded · Nov 27, 2019 · N656GT · Boeing 767281 · Fuselage Main, Longeron/Stringer > RT OVERWING LONGERON SPLICE PLATE CORRODED - [SDR ABXR2019112700315](https://openairdocs.org/sdr/ABXR2019112700315.md): Bushing · worn · Nov 27, 2019 · N656GT · Boeing 767281 · Wing Structure > RT WING SUMP DRAIN LEAKING AT BUSHING - [SDR UIEA2017121102385](https://openairdocs.org/sdr/UIEA2017121102385.md): Actuator · leaking · Dec 11, 2017 · N656GT · Boeing 767281 · Landing Gear Actuator > RH LANDING GEAR AFT SIDE BRACE ACTUATOR LEAKING.(
REMOVED AND REPLACED RH MLG SIDE BRACE ACTUATOR ASS. OPS CHECK NORMAL IAW AMM 32-32-02
) - [SDR UIEA2017121102387](https://openairdocs.org/sdr/UIEA2017121102387.md): Control Unit · leaking · Nov 11, 2017 · N656GT · Boeing 767281 · Hydraulic System, Main > LEFT STCM INPUT SHAFT SEAL HAS HYDRAULIC LEAK.(REMOVED AND REPLACED LEFT STCM. OPS CHECK NORMAL IAW AMM 27-41-00-715-014 TASK.
) - [SDR UIEA2017121102386](https://openairdocs.org/sdr/UIEA2017121102386.md): Starter · damaged · Nov 11, 2017 · N656GT · Boeing 767281 · Engine Starter > NO 2 ENGINE STARTER WITH METAL FRAGMENT LARGER THAN 0-1 INCH.(REMOVED AND REPLACED THE #2 ENGINE STARTER IAW AMM 80-11-01. OPS CHECK NORMAL.
) - [SDR UIEA2017080601420](https://openairdocs.org/sdr/UIEA2017080601420.md): Hydraulic System · low · Aug 6, 2017 · N656GT · Boeing 767281 · Hydraulic System, Main > LEFT HYD SYSTEM QTY WENT TO 0. C/W MTX PROCEDURES DISPATCH YK AT 1849Z DUE DATE 16AUG17. - [SDR UIEA2017040900531](https://openairdocs.org/sdr/UIEA2017040900531.md): Line · loose · Apr 7, 2017 · N656GT · Boeing 767281 · Fuel Controlling System > DURING 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 INDICATION - [SDR UIEA2017022000205](https://openairdocs.org/sdr/UIEA2017022000205.md): Housing · corroded · Mar 1, 2017 · N656GT · Boeing 767281 · Fuel Boost Pump > LEFT 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. - [SDR UIEA2017022000206](https://openairdocs.org/sdr/UIEA2017022000206.md): Housing · corroded · Mar 1, 2017 · N656GT · Boeing 767281 · Fuel Boost Pump > RIGHT WING BOOST PUMP HOUSING SHUT OFF SLEEVE HAS CORROSION. - [SDR UIEA2017022000207](https://openairdocs.org/sdr/UIEA2017022000207.md): Rod · corroded · Mar 1, 2017 · N656GT · Boeing 767281 · Horizontal Stabilizer Structure > APU 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. - [SDR UIEA2017022000210](https://openairdocs.org/sdr/UIEA2017022000210.md): Shim · corroded · Mar 1, 2017 · N656GT · Boeing 767281 · Cargo/Baggage Doors > FWD 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. - [SDR UIEA2017022000211](https://openairdocs.org/sdr/UIEA2017022000211.md): Tee Fitting · corroded · Mar 1, 2017 · N656GT · Boeing 767281 · Horizontal Stabilizer Structure > LEFT 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. - [SDR UIEA2017022000213](https://openairdocs.org/sdr/UIEA2017022000213.md): Attach Fitting · corroded · Mar 1, 2017 · N656GT · Boeing 767281 · Horizontal Stabilizer Structure > RIGHT 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. - [SDR UIEA2017022000214](https://openairdocs.org/sdr/UIEA2017022000214.md): Attach Fitting · corroded · Mar 1, 2017 · N656GT · Boeing 767281 · Horizontal Stabilizer Structure > RIGHT 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. - [SDR UIEA2017022000215](https://openairdocs.org/sdr/UIEA2017022000215.md): Attach Fitting · corroded · Mar 1, 2017 · N656GT · Boeing 767281 · Horizontal Stabilizer Structure > RIGHT 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. - [SDR UIEA2017022000216](https://openairdocs.org/sdr/UIEA2017022000216.md): Window Frame · corroded · Mar 1, 2017 · N656GT · Boeing 767281 · Fuselage Main, Structure > CABIN 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. - [SDR UIEA2017022000227](https://openairdocs.org/sdr/UIEA2017022000227.md): Lock · corroded · Mar 1, 2017 · N656GT · Boeing 767281 · Fuselage Main, Attach Fittings > MAIN 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. - [SDR UIEA2017022000226](https://openairdocs.org/sdr/UIEA2017022000226.md): Lock · corroded · Mar 1, 2017 · N656GT · Boeing 767281 · Fuselage Main, Attach Fittings > MAIN 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. - [SDR UIEA2017022000225](https://openairdocs.org/sdr/UIEA2017022000225.md): Attach Fitting · corroded · Mar 1, 2017 · N656GT · Boeing 767281 · Fuselage Main, Attach Fittings > MAIN 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. - [SDR UIEA2017022000224](https://openairdocs.org/sdr/UIEA2017022000224.md): Attach Fitting · corroded · Mar 1, 2017 · N656GT · Boeing 767281 · Fuselage Main, Attach Fittings > MAIN 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. - [SDR UIEA2017022000223](https://openairdocs.org/sdr/UIEA2017022000223.md): Attach Fitting · corroded · Mar 1, 2017 · N656GT · Boeing 767281 · Fuselage Main, Attach Fittings > MAIN 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 25-50-9 - [SDR UIEA2017022000222](https://openairdocs.org/sdr/UIEA2017022000222.md): Attach Bracket · corroded · Mar 1, 2017 · N656GT · Boeing 767281 · Fuselage Main, Attach Fittings > MAIN 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. - [SDR UIEA2017022000221](https://openairdocs.org/sdr/UIEA2017022000221.md): Fitting · corroded · Mar 1, 2017 · N656GT · Boeing 767281 · Fuselage Main, Attach Fittings > MAIN 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. TREA - [SDR UIEA2017022000220](https://openairdocs.org/sdr/UIEA2017022000220.md): Attach Bracket · corroded · Mar 1, 2017 · N656GT · Boeing 767281 · Fuselage Main, Attach Fittings > MAIN 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. - [SDR UIEA2017022000219](https://openairdocs.org/sdr/UIEA2017022000219.md): Fitting · corroded · Mar 1, 2017 · N656GT · Boeing 767281 · Fuselage Miscellaneous Structure > MAIN 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. - [SDR UIEA2017022000218](https://openairdocs.org/sdr/UIEA2017022000218.md): Inlet · corroded · Mar 1, 2017 · N656GT · Boeing 767281 · Turbine Engine Air Inlet Section > NR 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. - [SDR UIEA2017022000217](https://openairdocs.org/sdr/UIEA2017022000217.md): Support Channel · corroded · Mar 1, 2017 · N656GT · Boeing 767281 · Wing Main, Frame Structure > RT 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. - [SDR UIEA2016092000763](https://openairdocs.org/sdr/UIEA2016092000763.md): Engine · power loss · Sep 20, 2016 · N656GT · Boeing 767281 · Engine (Turbine/Turboprop) > RTO 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 73-21-01 - [SDR UIEA2016011800021](https://openairdocs.org/sdr/UIEA2016011800021.md): Escape Rope · unserviceable · Jan 18, 2016 · N656GT · Boeing 767281 · Emergency Equipment > COCKPIT DESCENT DEVICE CABLE EXTENDED. R & R DEFECTIVE DESCENT DEVICE IAW AMM 25-61-03. - [SDR UIEA2015121100722](https://openairdocs.org/sdr/UIEA2015121100722.md): Warning System · false activation · Dec 11, 2015 · N656GT · Boeing 767281 · Trailing Flap Position Indicating System > TRAILING 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. - [SDR UIEA2015081400410](https://openairdocs.org/sdr/UIEA2015081400410.md): Strap · cracked · Aug 13, 2015 · N656GT · Boeing 767281 · Fuselage Main, Frame > LEFT FAILSAFE CRACKED AT STATION 955. REPAIRED IAW EO 06753A070, TRIMMED. - [SDR UIEA2015081400411](https://openairdocs.org/sdr/UIEA2015081400411.md): Frame · damaged · Aug 13, 2015 · N656GT · Boeing 767281 · Fuselage Main, Frame > ELONGATED HOLE THROUGH FAILSAFE STRAP & FRAME CHORD. REPAIRED IAW REA 47169 REA 10. - [SDR UIEA2015081400412](https://openairdocs.org/sdr/UIEA2015081400412.md): Failsafe · cracked · Aug 13, 2015 · N656GT · Boeing 767281 · Fuselage Main, Frame > RIGHT SIDE FAILSAFE CRACKED AT STATION 955. REPAIRED IAW EO 06753A070, TRIMMED. Next page: https://openairdocs.org/aircraft/N656GT/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 = 'N656GT' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N656GT/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.