N657GT
Service difficulty reports · 49
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 = 'N657GT' 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 = 'N657GT' 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 UIEA2020081711749Sensor · failedL ENG HI STAGE EICAS MSG DURING CLIMB. REMOVED AND REPLACED FAN AIR TEMP SENSOR IAW AMM 36-11-17. OPS CK GOOD.SDR ABXR2020070200034Trunnion · corrodedRT MLG FORWARD TRUNNION WAS CORRODED IN THE LOWER SUPPORT ASSEMBLY BUSHING SHOULDER. REMOVED CORROSION AND INSTALLED OVERSIZED BUSHING PER 47401REA18 WITH 8100-9 BY AR-831084. REFERENCE NR 123447.0007SDR UIEA2020050100925Panel · bulgedLH WING UPPER T/E PANEL SURFACE BULGED BEYOND LIMITS.(<P>REPAIRED DAMAGED CHORD IAW REA 47401 REV. 3 AND B767 SRM 57-20-10.</P>)SDR UIEA2020050100926Skin · corrodedSTA 1065 LOWER INTERNAL SKI AND STRINGERS HAVE SURFACE CORROSION.(<P>REMOVED CORROSION. DID SCAN INSPECTION, FOUND SKIN TO BE OUT OF LIMITS. INSTALLED DOUBLER AND TRIPLER IAW REA 47401 REV A.</P>)SDR UIEA2020050100927Keelbeam · corrodedKEEL PANEL CROSS MEMBER CORROSION UNDER NUT PLACES.(<P>REPLACED KEEL PANEL IAW B767 SRM 51-10-02.</P>)SDR UIEA2020050100929Skin · delaminatedRT SIDE VERTICAL STAB SKIN DELAMINATED.(<P>REMOVED AND REPAIRED SKIN PANEL AND INSTALLED STAB SKIN WITH INTERIM FASTENERS PER 47401REA15.</P>)SDR UIEA2020050100930Stringer · corrodedH2 STAB STRINGER 11 CORRODED.(<P>REPLACED STRINGER PER 767-200 SRM 51-40-02 AND REA 47401FAB03.</P>)SDR UIEA2020050100931Stringer · corrodedH2 STAB STRINGER 8 CORRODED.(<P>REPAIRED WITH SPLICE PER B767-200 SRM 55-10-03 AND REA 47401FAB</P>)SDR ABXR2020042400024Stringer · corrodedHORIZONTAL STAB STRINGER 11 CORRODED. REPLACE STRINGER PER B767-200 SRM 51-40-02 AND REA 47401FAB03.SDR ABXR2020042400023Stringer · corrodedHORIZONTAL STAB STRINGER 8 CORRODED. REPAIRED WITH SPLICE PER B767-200 SRM 55-10-03SDR ABXR2020042300020Skin · corrodedALC 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 DAMAGSDR ABXR2020042300000Panel · corrodedTHE 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 ABXR2020042300019Attach Fitting · corrodedKEEL 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 14SDR UIEA2020010206167Escape Reel · unwanted deployEMERGENCY INERTIAL ESCAPE REELS AT POSITION 2, 4, AND 7 DEPLOYED AND REMOVED.(<P>TRANSFERRED TO MDDR 122754 AS PER DDG 25-61-01-01, CAT 'C'.</P><P>LP <SPAN>1112482 - </SPAN>INSTALLED GALLEY EMERGENCY DESCENT DEVICES IAW AMM 25-61-02.</P><P>POS. #7 - PN OFF 379SDR UIEA2019120635987Adc · malfunctionedLEAVING 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.(<P>PERFORMED PITOT HSDR UIEA201904223911Display · failedDURING CLIMB, CAPTAINS EHSI TURNED INTO PINK TINT, SHORTLY FOLLOWED BY F/O'S EHSI FAILING (BLANK). THIS WAS FOLLOWED BY SCENT OF BURNING.(<P>PERFORMED INSP. OF CAPT'S & FO'S EHSI IAW BOEING 767 AMM 20-60-00. CLEAN FILTERS AND VERIFIED AIR COOLING. NO DISCREPSDR UIEA2018122432905Pump · faultedAFTER GEAR SELECTED UP GEAR DISAGREE & GEAR DOOR EICAS ALSO DOOR LT NEXT TO GEAR INDICATOR LTS STAYED ON, RAN CHECKLIST , RETURNED TO CVG (<P>FOUND CENTER HYD SYSTEM ADP AT FAULT , REPLACED ADP ( LP 1018242 ITEM # 5 ) AND ASSOCIATED COMPONENTS I.A.W AMM 29-11-SDR UIEA2018112102664Circuit Card · failedFWD CABIN TEMP CAUTION MSG(<P>REMOVED AND REPLACED L/H PACK FLOW CONTROL CARD IAW B767 AMM 20-41-01 OPS GOOD AT THIS TIME </P>)SDR UIEA2018112102665Wire · corruptedDURING CRUISE FLT DECK TEMP REACHED 36 C PER QRH TURNED OFF TRIM AIR STILL COULD NOT CONTROL FLT DECK TEMP (<P>FOUND POORLY CONNECTED WIRE TO PIN 2 CONNECTOR D490 RETERMINATED WIRE IAW B767 SWPM 20-60-00 SYSTEM OPS CHECKS GOOD AT THIS TIME </P>)SDR UIEA2018111632587Adi · inoperativeDURING 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 (<P>REMOVED ADI & HSI(CAPT) FOUND WATER BLOWING INTO DISPLAYS. REMOVED & RESEATED EICAS-DISPLAY OPERATSDR UIEA2018091101942Doubler · chafedCHAFING 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 UIEA2017122102423Warning Message · illuminatedMAIN CARGO DOOR WARNING ANNUNCIATED DURING CLIMB PASSING FL240.SDR UIEA2017091101630Warning Message · illuminatedRIGHT EEC EICAS MESSAGE AT 240 KTS.SDR UIEA2017072101263Unknown · odorPASSING 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 LANDSDR UIEA2017072101262Display · inoperativeDURING 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 UIEA2017072101260Fmc · failedDURING TAXI OUT, RT FMC WENT BLANK WITH ELECTRICAL SMOKE ODOR. REMOVED AND REPLACED RT CDU IAW AMM 34-61-02, OPS CHECKED NORMAL.SDR UIEA2017070301109Circuit Breaker · trippedDURING 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 UIEA2017061301015Frame · crackedFRAME BS 883.5, LBL 89, BELOW WL 200, TRANSITION RADIUS HAS A .5 INCH CRACK. REPAIRED THE FRAME IAW SB 767-53A-0209.SDR UIEA2017061301016Stringer · crackedAFT CARGO BAY STRINGER 29R, BS 1083 IS CRACKED AT THE END OF THE FITTING. REMOVED AND REPLACED THE STRINGER IAW EA 17076PI.SDR UIEA2017061301017Skin · damagedNR 1 PYLON BLEND DAMAGE UNDER THE 431 BT PANEL INBD OF SUPPORT FITTING. REPAIRED THE PYLON IAW EA 170189.SDR UIEA2017061301018Frame · crackedFRAME BS 859.5, RBL 89, BELOW 200, TRANSITION RADIUS HAS .5 INCH CRACK. REPAIRED THE FRAME IAW SB 767-534-0209.</P>)SDR UIEA2017021300179Unknown · smokeON SHUTDOWN OF ENGINES SMOKE FILLED THE COCKPIT, APU SHUTOFF ON ITS OWN. PERFORMED CHAPTER 5 INSPECTION IAW AMM 21-00-21-862-051.SDR UIEA2016092200767Module · faultyREJECTED 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 UIEA2015110900615Support · damagedNUMBER 1 FLAP SUPPORT, NR 2 HOLE HAS A DEFECT INDICATION WITH HFEC ROTARY SCAN. REAMED NR 1 & 2 HOLES IAW 47177REA04.SDR UIEA2015110900616Support · damagedNUMBER 1 FLAP SUPPORT, NR 1 HOLE HAS A DEFECT INDICATION WITH HFEC ROTARY SCAN. REAMED NR 1 & 2 HOLES IAW 47177REA04.SDR UIEA2015110900617Support · damagedNUMBER 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 UIEA2015110900619Doubler · crackedINBOARD THRUST REVERSER ON NR 2 ENG HAD CRACKED DOUBLER. REPLACED DOUBLER IAW 47177REA02.SDR UIEA2015110900620Panel · corrodedRIGHT WING OTBD FLAP CORRODED. BLENDED & REPAIRED ON NR-0713 REFERENCING REA 47177REA03.SDR UIEA2015110900621Stringer · corrodedCORROSION, HORIZONTAL STAB BOX, CTR INTERIOR, OTBD RIB 2L, UPPER NR 6 STRINGER, AFT HORIZONTAL LEG UPPER. R & R STRINGER NR 6, DOCUMENT 47177FAB08.SDR UIEA2015111000622Skin · crackedRIGHT WING LE SKIN CLOSE CUT CRACKED AT LES 446. REPAIRED IAW SRM 51-70-11 FIG.SDR UIEA2015111000623Support Beam · damagedNUMBER 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 UIEA2015111000625Stringer · corrodedHORIZONTAL STAB BOX STRINGER U3, BETWEEN RIBS 1L & 2L, CORRODED ON AFT FLANGE. REMOVED CORROSION & BLENDED AREA.SDR UIEA2015111000626Support · damagedNUMBER 1 FLAP, NR 3 TENSION BOLT HOLE HAS DEFECT INDICATION. REAMED HOLES OVERSIZE IAW RFA 47177 REA 04.SDR UIEA2015111000627Support · damagedNUMBER 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 UIEA2015111000628Support · damagedNUMBER 8 FLAP SUPPORT, NR 2 TENSION BOLT HOLE HAS A DEFECT INDICATION WITH HFEC ROTARY SCAN. REAMED SUPPORT HOLES IAW REA 47177REA04.SDR UIEA2015111000629Beam · corrodedRIGHT 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 UIEA2015111000630Rib · damagedTHE 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 UIEA2015111000631Support · damagedNUMBER 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 UIEA2015111000632Panel · corrodedRIGHT 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.
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