REPAIRED DAMAGED CHORD IAW REA 47401 REV. 3 AND B767 SRM 57-20-10.
) - [SDR UIEA2020050100926](https://openairdocs.org/sdr/UIEA2020050100926.md): Skin · corroded · Apr 28, 2020 · N657GT · Boeing 767281 · Fuselage Main, Plate/Skin > STA 1065 LOWER INTERNAL SKI AND STRINGERS HAVE SURFACE CORROSION.(REMOVED CORROSION. DID SCAN INSPECTION, FOUND SKIN TO BE OUT OF LIMITS. INSTALLED DOUBLER AND TRIPLER IAW REA 47401 REV A.
) - [SDR UIEA2020050100927](https://openairdocs.org/sdr/UIEA2020050100927.md): Keelbeam · corroded · Apr 28, 2020 · N657GT · Boeing 767281 · Fuselage Main, Keel > KEEL PANEL CROSS MEMBER CORROSION UNDER NUT PLACES.(REPLACED KEEL PANEL IAW B767 SRM 51-10-02.
) - [SDR UIEA2020050100929](https://openairdocs.org/sdr/UIEA2020050100929.md): Skin · delaminated · Apr 28, 2020 · N657GT · Boeing 767281 · Vertical Stabilizer, Plate/Skin > RT SIDE VERTICAL STAB SKIN DELAMINATED.(REMOVED AND REPAIRED SKIN PANEL AND INSTALLED STAB SKIN WITH INTERIM FASTENERS PER 47401REA15.
) - [SDR UIEA2020050100930](https://openairdocs.org/sdr/UIEA2020050100930.md): Stringer · corroded · Apr 28, 2020 · N657GT · Boeing 767281 · Horizontal Stabilizer, Spar/Rib > H2 STAB STRINGER 11 CORRODED.(REPLACED STRINGER PER 767-200 SRM 51-40-02 AND REA 47401FAB03.
) - [SDR UIEA2020050100931](https://openairdocs.org/sdr/UIEA2020050100931.md): Stringer · corroded · Apr 28, 2020 · N657GT · Boeing 767281 · Horizontal Stabilizer, Spar/Rib > H2 STAB STRINGER 8 CORRODED.(REPAIRED WITH SPLICE PER B767-200 SRM 55-10-03 AND REA 47401FAB
) - [SDR ABXR2020042400024](https://openairdocs.org/sdr/ABXR2020042400024.md): Stringer · corroded · Apr 24, 2020 · N657GT · Boeing 767281 · Horizontal Stabilizer Structure > HORIZONTAL STAB STRINGER 11 CORRODED. REPLACE STRINGER PER B767-200 SRM 51-40-02 AND REA 47401FAB03. - [SDR ABXR2020042400023](https://openairdocs.org/sdr/ABXR2020042400023.md): Stringer · corroded · Apr 24, 2020 · N657GT · Boeing 767281 · Horizontal Stabilizer Structure > HORIZONTAL STAB STRINGER 8 CORRODED. REPAIRED WITH SPLICE PER B767-200 SRM 55-10-03 - [SDR ABXR2020042300020](https://openairdocs.org/sdr/ABXR2020042300020.md): Skin · corroded · Apr 16, 2020 · N657GT · Boeing 767281 · Fuselage Main, Plate/Skin > ALC STA 1065 LOWER INTERNAL SKIN AND STRINGERS BETWEEN FUSELAGE DRAINS HAVE SURFACE CORROSION. BLEND OUT REQUIRED AT CORRODED AREA, REMOVED CORRODED AREA AT LOWER FUSELAGE SKIN STA 1080 TO STA 1131, STRINGER 38L TO 38R IAW B767-200 SRM 53-60-01 ALLOWABLE DAMAG - [SDR ABXR2020042300000](https://openairdocs.org/sdr/ABXR2020042300000.md): Panel · corroded · Apr 15, 2020 · N657GT · Boeing 767281 · Wing, Plate/Skin > THE LEFT WING, UPPER T/E PANEL, UPPER SURFACE IS BULGED, ON THE FWD O/B CORNER, LOCATED JUST FWD OF THE O/B AILERON'S I/B END.BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 57-20-10 DET V. REPAIRED DAMAGED UPPER CHORD IAW AMES REA # 47401 REA 03. - [SDR ABXR2020042300019](https://openairdocs.org/sdr/ABXR2020042300019.md): Attach Fitting · corroded · Mar 17, 2020 · N657GT · Boeing 767281 · Fuselage Main, Keel > KEEL PANEL ATTACH CROSS MEMBER AT STA.967 CORRODED UNDER NUT PLATES ON FORWARD AND AFT SIDES.BLENDED CORROSION AT STA 967 KEEL PANEL ATTACH CROSS MEMBER IAW B767 SRM 51-10-02 MEASURED T. 0.100. REMOVED T 0.055 FOUND TO BE OUT OF LIMITS TAG 8720 INSTALLED PN 14 - [SDR UIEA2020010206167](https://openairdocs.org/sdr/UIEA2020010206167.md): Escape Reel · unwanted deploy · Dec 30, 2019 · N657GT · Boeing 767281 · Emergency Equipment > EMERGENCY INERTIAL ESCAPE REELS AT POSITION 2, 4, AND 7 DEPLOYED AND REMOVED.(TRANSFERRED TO MDDR 122754 AS PER DDG 25-61-01-01, CAT 'C'.
LP 1112482 - INSTALLED GALLEY EMERGENCY DESCENT DEVICES IAW AMM 25-61-02.
POS. #7 - PN OFF 379 - [SDR UIEA2019120635987](https://openairdocs.org/sdr/UIEA2019120635987.md): Adc · malfunctioned · Dec 3, 2019 · N657GT · Boeing 767281 · Air Data Computer > LEAVING FL410 FOR FL390, CAUTION MSG IAS DISAGREE WAS DISPLAYED ALONG WITH L & R ENG EEC, AILERON LOCKOUT APPEARED, & RUDDER RATIO. F/O A/S INDICATION DECREASED AS WE DESCENDED, AND PASSING FL250, THE F/O A/S INDICATION RETURNED TO NORMAL.(
PERFORMED PITOT H - [SDR UIEA201904223911](https://openairdocs.org/sdr/UIEA201904223911.md): Display · failed · Apr 20, 2019 · N657GT · Boeing 767281 · Navigation System > DURING CLIMB, CAPTAINS EHSI TURNED INTO PINK TINT, SHORTLY FOLLOWED BY F/O'S EHSI FAILING (BLANK). THIS WAS FOLLOWED BY SCENT OF BURNING.(
PERFORMED INSP. OF CAPT'S & FO'S EHSI IAW BOEING 767 AMM 20-60-00. CLEAN FILTERS AND VERIFIED AIR COOLING. NO DISCREP - [SDR UIEA2018122432905](https://openairdocs.org/sdr/UIEA2018122432905.md): Pump · faulted · Dec 21, 2018 · N657GT · Boeing 767281 · Hydraulic Pump (Electric/Engine), Main > AFTER GEAR SELECTED UP GEAR DISAGREE & GEAR DOOR EICAS ALSO DOOR LT NEXT TO GEAR INDICATOR LTS STAYED ON, RAN CHECKLIST, RETURNED TO CVG (
FOUND CENTER HYD SYSTEM ADP AT FAULT, REPLACED ADP ( LP 1018242 ITEM # 5) AND ASSOCIATED COMPONENTS I.A.W AMM 29-11- - [SDR UIEA2018112102664](https://openairdocs.org/sdr/UIEA2018112102664.md): Circuit Card · failed · Nov 19, 2018 · N657GT · Boeing 767281 · Air Conditioning System Wiring > FWD CABIN TEMP CAUTION MSG(
REMOVED AND REPLACED L/H PACK FLOW CONTROL CARD IAW B767 AMM 20-41-01 OPS GOOD AT THIS TIME
) - [SDR UIEA2018112102665](https://openairdocs.org/sdr/UIEA2018112102665.md): Wire · corrupted · Nov 19, 2018 · N657GT · Boeing 767281 · Air Conditioning System Wiring > DURING CRUISE FLT DECK TEMP REACHED 36 C PER QRH TURNED OFF TRIM AIR STILL COULD NOT CONTROL FLT DECK TEMP (FOUND POORLY CONNECTED WIRE TO PIN 2 CONNECTOR D490 RETERMINATED WIRE IAW B767 SWPM 20-60-00 SYSTEM OPS CHECKS GOOD AT THIS TIME
) - [SDR UIEA2018111632587](https://openairdocs.org/sdr/UIEA2018111632587.md): Adi · inoperative · Nov 13, 2018 · N657GT · Boeing 767281 · Attitude Gyro and Indicating System > DURING TAXI OUT CA ADI BLANKED, ALTN EFI DID NOT RETURN SCREEN WE THEN HAD ELECTRICAL SMOKE / BURNING SMELL. SUBSEQUENTLY LOST CA HSI AND UPPER EICAS SCREENS (REMOVED ADI & HSI(CAPT) FOUND WATER BLOWING INTO DISPLAYS. REMOVED & RESEATED EICAS-DISPLAY OPERAT - [SDR UIEA2018091101942](https://openairdocs.org/sdr/UIEA2018091101942.md): Doubler · chafed · Sep 7, 2018 · N657GT · Boeing 767281 · Fuselage Main, Bulkhead > CHAFING FROM RT APU DOOR CATCH ON FIRE WALL IN APU COMPARTMENT LOWER AREA RIGHT OF CENTERLINE. REMOVED AND REPLACED APU FIRE WALL DOUBLER LINE IAW SRM 51-40-02 AND SRM 53-80-08-2R-5. - [SDR UIEA2017122102423](https://openairdocs.org/sdr/UIEA2017122102423.md): Warning Message · illuminated · Dec 20, 2017 · N657GT · Boeing 767281 · Door Warning System > MAIN CARGO DOOR WARNING ANNUNCIATED DURING CLIMB PASSING FL240. - [SDR UIEA2017091101630](https://openairdocs.org/sdr/UIEA2017091101630.md): Warning Message · illuminated · Sep 11, 2017 · N657GT · Boeing 767281 · Fuel Controlling System > RIGHT EEC EICAS MESSAGE AT 240 KTS. - [SDR UIEA2017072101263](https://openairdocs.org/sdr/UIEA2017072101263.md): Unknown · odor · Jul 21, 2017 · N657GT · Boeing 767281 · Air Distribution System > PASSING THRU 11K FEET ON CLIMB OUT, CAPTAINS ND BEGAN TO CYCLE ON AND OFF WITH STRONG ELECTRICAL ODOR. LEVELED OFF, TURNED BACK AND RAN- C&D SMOKE, FIRE OR FUMES QRH. MX PULLED C/B ANDTHE ODOR DIMINISHED. DURING BASE TURN, LOST THE FO'S CDU SCREEN, AFTER LAND - [SDR UIEA2017072101262](https://openairdocs.org/sdr/UIEA2017072101262.md): Display · inoperative · Jul 20, 2017 · N657GT · Boeing 767281 · Central Display > DURING TAXI IN, NOTICED A BURNING ODOR, OZONE TYPE. REMOVED THE RT FMC CDU, FOUND A SLIGHT SMOKEY ODOR. R & R THE RT CDU IAW AMM 34-61-02. OPS CHECKED NORMAL. - [SDR UIEA2017072101260](https://openairdocs.org/sdr/UIEA2017072101260.md): Fmc · failed · Jul 20, 2017 · N657GT · Boeing 767281 · Flight Management Computing Hardware System > DURING TAXI OUT, RT FMC WENT BLANK WITH ELECTRICAL SMOKE ODOR. REMOVED AND REPLACED RT CDU IAW AMM 34-61-02, OPS CHECKED NORMAL. - [SDR UIEA2017070301109](https://openairdocs.org/sdr/UIEA2017070301109.md): Circuit Breaker · tripped · Jul 4, 2017 · N657GT · Boeing 767281 · Flight Management Computing Hardware System > DURING BLOCK IN LEFT FMC CIRCUIT BREAKER TRIPPED WITH ELECTRICAL SMOKE ODOR IN THE COCKPIT. PERFORMED INSPECTION FOR SMOKE ODOR IAW AMM 05-51-56. NO DEFECTS NOTED. - [SDR UIEA2017061301015](https://openairdocs.org/sdr/UIEA2017061301015.md): Frame · cracked · Jun 13, 2017 · N657GT · Boeing 767281 · Fuselage Main, Frame > FRAME BS 883.5, LBL 89, BELOW WL 200, TRANSITION RADIUS HAS A.5 INCH CRACK. REPAIRED THE FRAME IAW SB 767-53A-0209. - [SDR UIEA2017061301016](https://openairdocs.org/sdr/UIEA2017061301016.md): Stringer · cracked · Jun 13, 2017 · N657GT · Boeing 767281 · Fuselage Main, Longeron/Stringer > AFT CARGO BAY STRINGER 29R, BS 1083 IS CRACKED AT THE END OF THE FITTING. REMOVED AND REPLACED THE STRINGER IAW EA 17076PI. - [SDR UIEA2017061301017](https://openairdocs.org/sdr/UIEA2017061301017.md): Skin · damaged · Jun 13, 2017 · N657GT · Boeing 767281 · Nacelle/Pylon, Plate/Skin > NR 1 PYLON BLEND DAMAGE UNDER THE 431 BT PANEL INBD OF SUPPORT FITTING. REPAIRED THE PYLON IAW EA 170189. - [SDR UIEA2017061301018](https://openairdocs.org/sdr/UIEA2017061301018.md): Frame · cracked · Jun 13, 2017 · N657GT · Boeing 767281 · Fuselage Main, Frame > FRAME BS 859.5, RBL 89, BELOW 200, TRANSITION RADIUS HAS.5 INCH CRACK. REPAIRED THE FRAME IAW SB 767-534-0209.
) - [SDR UIEA2017021300179](https://openairdocs.org/sdr/UIEA2017021300179.md): Unknown · smoke · Feb 13, 2017 · N657GT · Boeing 767281 · Air Distribution System > ON SHUTDOWN OF ENGINES SMOKE FILLED THE COCKPIT, APU SHUTOFF ON ITS OWN. PERFORMED CHAPTER 5 INSPECTION IAW AMM 21-00-21-862-051. - [SDR UIEA2016092200767](https://openairdocs.org/sdr/UIEA2016092200767.md): Module · faulty · Sep 22, 2016 · N657GT · Boeing 767281 · Trailing Edge Flap Control System > REJECTED T/O DUE TO T/O WARNING HORN. STATUS MESSAGE FLAP/SLAT ELECTRONIC LESS THAN 20KTS ACHIEVED. FOUND C FSPM FAULTING R & R C FSPM MODULE M839 IAW AMM 27-58-01. OPS CKS OK. - [SDR UIEA2015110900615](https://openairdocs.org/sdr/UIEA2015110900615.md): Support · damaged · Nov 6, 2015 · N657GT · Boeing 767281 · Trailing Edge Flaps > NUMBER 1 FLAP SUPPORT, NR 2 HOLE HAS A DEFECT INDICATION WITH HFEC ROTARY SCAN. REAMED NR 1 & 2 HOLES IAW 47177REA04. - [SDR UIEA2015110900616](https://openairdocs.org/sdr/UIEA2015110900616.md): Support · damaged · Nov 6, 2015 · N657GT · Boeing 767281 · Trailing Edge Flaps > NUMBER 1 FLAP SUPPORT, NR 1 HOLE HAS A DEFECT INDICATION WITH HFEC ROTARY SCAN. REAMED NR 1 & 2 HOLES IAW 47177REA04. - [SDR UIEA2015110900617](https://openairdocs.org/sdr/UIEA2015110900617.md): Support · damaged · Nov 6, 2015 · N657GT · Boeing 767281 · Trailing Edge Flaps > NUMBER 8 FLAP SUPPORT, NR 4 TENSION BOLT HOLE HAS A DEFECT INDICATION WITH HFEC ROTARY SCAN. REAMED NR 3 & 4 SUPPORT HOLES IAW 47177REA04. - [SDR UIEA2015110900619](https://openairdocs.org/sdr/UIEA2015110900619.md): Doubler · cracked · Nov 6, 2015 · N657GT · Boeing 767281 · Engine Thrust Reverser > INBOARD THRUST REVERSER ON NR 2 ENG HAD CRACKED DOUBLER. REPLACED DOUBLER IAW 47177REA02. - [SDR UIEA2015110900620](https://openairdocs.org/sdr/UIEA2015110900620.md): Panel · corroded · Nov 6, 2015 · N657GT · Boeing 767281 · Trailing Edge Flaps > RIGHT WING OTBD FLAP CORRODED. BLENDED & REPAIRED ON NR-0713 REFERENCING REA 47177REA03. - [SDR UIEA2015110900621](https://openairdocs.org/sdr/UIEA2015110900621.md): Stringer · corroded · Nov 6, 2015 · N657GT · Boeing 767281 · Horizontal Stabilizer, Spar/Rib > CORROSION, HORIZONTAL STAB BOX, CTR INTERIOR, OTBD RIB 2L, UPPER NR 6 STRINGER, AFT HORIZONTAL LEG UPPER. R & R STRINGER NR 6, DOCUMENT 47177FAB08. - [SDR UIEA2015111000622](https://openairdocs.org/sdr/UIEA2015111000622.md): Skin · cracked · Nov 6, 2015 · N657GT · Boeing 767281 · Wing, Plate/Skin > RIGHT WING LE SKIN CLOSE CUT CRACKED AT LES 446. REPAIRED IAW SRM 51-70-11 FIG. - [SDR UIEA2015111000623](https://openairdocs.org/sdr/UIEA2015111000623.md): Support Beam · damaged · Nov 6, 2015 · N657GT · Boeing 767281 · Trailing Edge Flaps > NUMBER 8 FLAPS, SUPPORT 1 - 3 BEAM HAS 2 HOLES WITH DEFECT INDICATIONS WITH HFEC ROTARY SCAN. REAMED DISCREPANT HOLES IAW SRM 51-40-02 - PAR 7D 47177 REAOG. - [SDR UIEA2015111000625](https://openairdocs.org/sdr/UIEA2015111000625.md): Stringer · corroded · Nov 6, 2015 · N657GT · Boeing 767281 · Horizontal Stabilizer, Spar/Rib > HORIZONTAL STAB BOX STRINGER U3, BETWEEN RIBS 1L & 2L, CORRODED ON AFT FLANGE. REMOVED CORROSION & BLENDED AREA. - [SDR UIEA2015111000626](https://openairdocs.org/sdr/UIEA2015111000626.md): Support · damaged · Nov 6, 2015 · N657GT · Boeing 767281 · Trailing Edge Flaps > NUMBER 1 FLAP, NR 3 TENSION BOLT HOLE HAS DEFECT INDICATION. REAMED HOLES OVERSIZE IAW RFA 47177 REA 04. - [SDR UIEA2015111000627](https://openairdocs.org/sdr/UIEA2015111000627.md): Support · damaged · Nov 6, 2015 · N657GT · Boeing 767281 · Trailing Edge Flaps > NUMBER 8 FLAP SUPPORT, NR 3 TENSION BOLT HOLE HAS A DEFECT INDICATION WITH HFEC ROTARY SCAN. REAMED NR 3 & 4 SUPPORT HOLES IAW REA47177REA04. - [SDR UIEA2015111000628](https://openairdocs.org/sdr/UIEA2015111000628.md): Support · damaged · Nov 6, 2015 · N657GT · Boeing 767281 · Trailing Edge Flaps > NUMBER 8 FLAP SUPPORT, NR 2 TENSION BOLT HOLE HAS A DEFECT INDICATION WITH HFEC ROTARY SCAN. REAMED SUPPORT HOLES IAW REA 47177REA04. - [SDR UIEA2015111000629](https://openairdocs.org/sdr/UIEA2015111000629.md): Beam · corroded · Nov 6, 2015 · N657GT · Boeing 767281 · Wing Main, Frame Structure > RIGHT WING LE NOSE BEAM FROM LES 395 - 421 IS CORRODED ON THE INBD UPPER FLANGE. REMOVED CORROSION & REPAIRED IAW SRM 57-41-13 FIG 101 & SRM 51-70-11 FIG 101 RESPECTIVELY. - [SDR UIEA2015111000630](https://openairdocs.org/sdr/UIEA2015111000630.md): Rib · damaged · Nov 6, 2015 · N657GT · Boeing 767281 · Trailing Edge Flaps > THE LT WING NR 2 FLAP SUPPORT, OTBD RIB ACTUATOR BORE UPPER FWD SURFACE HAD A DEFECT INDICATION DURING AN HFEC SURFACE SCAN. BLENDED CORROSION IAW SRM 57-51-90 FIG 101. - [SDR UIEA2015111000631](https://openairdocs.org/sdr/UIEA2015111000631.md): Support · damaged · Nov 6, 2015 · N657GT · Boeing 767281 · Trailing Edge Flaps > NUMBER 1 FLAP SUPPORT, NR 4 TENSION BOLT HOLE HAS A DEFECT INDICATION WITH HFEC ROTARY SCAN. REAMED NR 1 FLAP SUPPORT HOLES 3 & 4 IAW 4717 REA 04. - [SDR UIEA2015111000632](https://openairdocs.org/sdr/UIEA2015111000632.md): Panel · corroded · Nov 6, 2015 · N657GT · Boeing 767281 · Trailing Edge Flaps > RIGHT WING OTBD FLAP, LOWER FWD INBD STRESS PANEL HAD A SPOT OF CORROSION THAT WAS BLENDED OUT OF LIMITS ON NR-0570. REPAIRED PANEL IAW VACUUM CUT METHOD IAW SRM 57-53-01 & 51-70-01 & REA 47177REA03. ## 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 = 'N657GT' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N657GT/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.