REMOVED AND REPLACED DOOR INSTALLATION S.O.B. IAW AMM 27-51-03. NO FURTHER DEFECTS NOTED
) - [SDR UIEA2026030600077](https://openairdocs.org/sdr/UIEA2026030600077.md): Oxygen Mask · unsecure · Mar 6, 2026 · N663GT · Boeing 767324 · Crew Oxygen System > CAPT, FIRST OFFICER, OBSERVER SEAT, & NR 1 SUPERNUMERARY OXYGEN MASK NEED TO BE STOWED. STOWED THE CREW OXYGEN MASK "4 TOTAL" IAW B767AMM 35-11-51. OPS CHECK GOOD, NO DEFECTS NOTED.) - [SDR UIEA2025121701350](https://openairdocs.org/sdr/UIEA2025121701350.md): Tamper Strip · missing · Dec 17, 2025 · N663GT · Boeing 767324 · Emergency Equipment > ELT -DO NOT REMOVE- TAPE WAS REMOVED. R &R ELT IAW AMM 25-63-03. OPS CHECKED GOOD. - [SDR UIEA2025082801145](https://openairdocs.org/sdr/UIEA2025082801145.md): Seal · broken · Aug 28, 2025 · N663GT · Boeing 767324 · Emergency Equipment > CAPTAIN EVAS TAMPER SEAL BROKEN(INSTALLED NEW SEAL & NO FURTHER DEFECTS NOTED PER STC ST00892LA. DMI 237059 CLOSED
) - [SDR UIEA2025062200790](https://openairdocs.org/sdr/UIEA2025062200790.md): Panel · corroded · Jun 30, 2025 · N663GT · Boeing 767324 · Fuselage Main, Structure > AFT CARGO BAY TORQUE BOX PANEL BETWEEN STATION 1262 AND STATION 1285 RBL6 TO RBL 10 FOUND WITH SURFACE CORROSION. WEB REMOVED AND REPLACED AS PER B767-300BCF SRM 51-40-02 REV 52. NO FURTHER DEFECTS NOTED. - [SDR UIEA2025062200791](https://openairdocs.org/sdr/UIEA2025062200791.md): Panel · corroded · Jun 30, 2025 · N663GT · Boeing 767324 · Fuselage Main, Structure > AFT CARGO BAY TORQUE BOX PANEL AT STATION 1280 RBL 29 FOUND WITH SURFACE CORROSION. WEB REMOVED AND REPLACED AS PER SRM 51-40-02 REV 52. NO FURTHER DEFECTS NOTED. - [SDR UIEA2025062200792](https://openairdocs.org/sdr/UIEA2025062200792.md): Shear Tie · corroded · Jun 30, 2025 · N663GT · Boeing 767324 · Fuselage Internal Mounting Structure > FWD CARGO BAY SHEAR CLIP AT STATION 742 BETWEEN S35L AND S36L FOUND WITH SURFACE CORROSION. NEW SHEAR CLIP (P/N:140T2101Y21) AND SHEAR TIE (P/N:140T2102U243) INSTALLED AS PER SRM 51-40-02 REV 52. NO FURTHER DEFECTS NOTED. - [SDR UIEA2025062200793](https://openairdocs.org/sdr/UIEA2025062200793.md): Shear Tie · corroded · Jun 30, 2025 · N663GT · Boeing 767324 · Fuselage Internal Mounting Structure > FWD CARGO BAY- SHEAR CLIP AT STATION 742 BETWEEN S37R AND S38R FOUND WITH SURFACE CORROSION. NEW SHEAR CLIP (P/N:140T2102U252) INSTALLED AS PER SRM 51-40-02 REV52. NO FURTHER DEFECTS NOTED. - [SDR UIEA2025062300795](https://openairdocs.org/sdr/UIEA2025062300795.md): Web · corroded · Jun 30, 2025 · N663GT · Boeing 767324 · Fuselage Miscellaneous Structure > FWD CARGO COMPT WEB AT STATION 742 ABOVE S35L AND S36L FOUND WITH SURFACE CORROSION. REPAIR CARRIED OUT AS PER EN #3218-25. NO FURTHER DEFECTS NOTED. - [SDR UIEA2025062300796](https://openairdocs.org/sdr/UIEA2025062300796.md): Web · corroded · Jun 30, 2025 · N663GT · Boeing 767324 · Fuselage Miscellaneous Structure > FWD CARGO COMPT WEB AT STATION 742 ABOVE S36L FOUND WITH SURFACE CORROSION. REPAIR CARRIED OUT AS PER EN #3218-25. NO FURTHER DEFECTS NOTED. - [SDR UIEA2025062300797](https://openairdocs.org/sdr/UIEA2025062300797.md): Skin · cracked · Jun 30, 2025 · N663GT · Boeing 767324 · Fuselage Main, Plate/Skin > DURING HFEC OPEN HOLE INSPECTION ON RH FWD ENTRY DOOR CUTOUT AFT LOWER CORNER. FOUND SECOND HOLE FROM BOTTOM WITH CRACK INDICATION AT 1 O'CLOCK POSITON VIEW LOOKING INBOARD. REPAIR CARRIED OUT IAW SRM 53-10-01 REPAIR 1 REV. 52. NO FURTHER DEFECTS NOTED. - [SDR UIEA2025062300798](https://openairdocs.org/sdr/UIEA2025062300798.md): Skin · cracked · Jun 30, 2025 · N663GT · Boeing 767324 · Fuselage Main, Plate/Skin > DURING HFEC OPEN HOLE INSPECTION ON LT FWD ENTRY DOOR CUTOUT AFT LOWER CORNER FOUND SECOND HOLE FROM BOTTOM WITH CRACK INDICATION AT 10 O'CLOCK & 4 O'CLOCK POSITION VIEW LOOKING INBOARD. REPAIR CARRIED OUT IAW SRM 53-10-01 REPAIR 1 REV. 52. NO FURTHER DEFECTS - [SDR UIEA2025062400799](https://openairdocs.org/sdr/UIEA2025062400799.md): Shear Tie · corroded · Jun 30, 2025 · N663GT · Boeing 767324 · Fuselage Internal Mounting Structure > FWD CGO COMP'T - SHEAR CLIP AT STATION 742 S34L FOUND WITH SURFACE CORROSIONS AS MARKED. SHEAR CLIP (P/N: 140T2101Y21) AND SHEAR TIE (P/N: 140T2102U203) REMOVED AND REPLACED AS PER B767-300BCF SRM 51-40-02 REV 52. NO FUTHER DEFECTS NOTED. - [SDR UIEA2025062400800](https://openairdocs.org/sdr/UIEA2025062400800.md): Shear Tie · corroded · Jun 30, 2025 · N663GT · Boeing 767324 · Fuselage Internal Mounting Structure > FWD CGO COMP - SHEAR CLIP AT STATION 742 S37L FOUND WITH SURFACE CORROSIONS AS MARKED. SHEAR CLIP REMOVED AND REPLACED AS PER B767-300BCF SRM 51-40-02 REV 52. NO FURTHER DEFECTS NOTED. - [SDR UIEA2024122201180](https://openairdocs.org/sdr/UIEA2024122201180.md): Fuel Filter · warning message · Dec 23, 2024 · N663GT · Boeing 767324 · Engine Fuel Distribution > RIGHT ENGINE FUEL FILTER EICAS MESSAGE.(REMOVED AND REPLACED RIGHT ENGINE FUEL FILTER AND THEN RIGHT ENGINE RUN CHECKED OK WITH NO LEAKEAGE FOUND, NO FAULT MESSAGE FOUND PER AMM 73-11-03/401.
) - [SDR UIEA2024092100913](https://openairdocs.org/sdr/UIEA2024092100913.md): Adc · faulted · Sep 21, 2024 · N663GT · Boeing 767324 · Airspeed/Mach Indicator > AT 40,000' IN LEVEL FLIGHT, IAS DISAGREE MSG ON EICAS. CAPT'S AIRSPEED IND MAINTAINED 0.807M WHILE FO'S VARIED BY AS MUCH AS 0.03M & 12 KIAS. STBY A/S IND WAS CONCURRENT. FO'S A/S IND & CA'S A/S DETERMINED AS UNRELIABLE. ASSOC AIL LOCKOUT & RUDDER RATIO MS - [SDR UIEA2024090400884](https://openairdocs.org/sdr/UIEA2024090400884.md): Controller · faulted · Sep 4, 2024 · N663GT · Boeing 767324 · Cabin Pressure Controller > CABIN ALT AUTO 2 EICAS MSG, CHANGE IN PRESSURIZATION, BRIEFLY DONNED OXYGEN MASKS(TRANSFER TO DMI 215993 PER MEL 21-31-01A CAT C DUE DATE 13SEP24 REMOVED AND REPLACED CABIN PRESSURE CONTROLLER #2 IAW AMM 21-31-02 BITE CHECK PASSED THIS CLEARS MDDR 215993 - [SDR UIEA2024021500087](https://openairdocs.org/sdr/UIEA2024021500087.md): Spar · corroded · Feb 22, 2024 · N663GT · Boeing 767324 · Wing Spar > RH WING INSPAR LOWER SURFACE WS 720.2 & STRINGER L-9 EVIDENCE OF CORROSION(
RH WING INSPAR LOWER SURFACE AT WS 720.2 & STRINGER L-9 WAS REPAIRED PER CMA-TLS 24-0108-01C * CMA-TLS 24-0108. NO FURTHER DEFECTS NOTED
) - [SDR UIEA2024021500088](https://openairdocs.org/sdr/UIEA2024021500088.md): Skin · delaminated · Feb 22, 2024 · N663GT · Boeing 767324 · Trailing Edge Flaps > RH WING OUTBOARD FLAP LOWER SKIN EXISTING REPAIR WITH DELAMINATION (23 IN FROM L/E & 48 IN FROM LH EDGE)(RH WING OUTBOARD FLAP LOWER SKIN PANEL WAS REPAIRED PER SRM 57-53-01-2R-1 & SRM 51-70-10-2R-4. NO FURTHER DEFECTS NOTED.
) - [SDR UIEA2024021600089](https://openairdocs.org/sdr/UIEA2024021600089.md): Skin · damaged · Feb 22, 2024 · N663GT · Boeing 767324 · Spoilers > RH WING SPOILER NO 7 HOLE (7 IN FROM LH EDGE & 5 IN FROM T/E)(RH WING SPOILER #7 (AT 7" FROM INBD & 5" FROM T/E) LOWER SKIN WAS REPAIRED PER SRM 57-70-01-2R-1 & SRM 51-70-17-0G-0. NO FURTHER DEFECTS NOTED.
) - [SDR UIEA2024022000095](https://openairdocs.org/sdr/UIEA2024022000095.md): Valve · leaking · Feb 22, 2024 · N663GT · Boeing 767324 · Landing Gear Brake System > MLG, LH MLG WHEEL WELL, VALVE MODULE SHUTTLE AUTOBRAKE WITH LEAK(PART WAS REPLACED PER AMM 32-42-10-404-015. OPS CHK GOOD.
) - [SDR UIEA2024022100109](https://openairdocs.org/sdr/UIEA2024022100109.md): Skin · corroded · Feb 22, 2024 · N663GT · Boeing 767324 · Wing, Plate/Skin > LH WINGLET WEB SKIN (STA ZERO) CORROSION EVIDENCE(LH WINGLET RIB 1 WEB SURFACE (STA ZERO) WAS REPAIRED PER CMA-TLS 24-0107-07B & CMA-TLS 24-0107-12B. NO FURTHER DEFECTS NOTED.
) - [SDR UIEA2024022100110](https://openairdocs.org/sdr/UIEA2024022100110.md): Skin · corroded · Feb 22, 2024 · N663GT · Boeing 767324 · Wing, Plate/Skin > RH WINGLET WEB SKIN (STA ZERO) EVIDENCE OF CORROSION(RH WINGLET RIB 1 WEB SURFACE (STA ZERO) WAS REPAIRED PER CMA-TLS 24-0105-03B. NO FURTHER DEFECTS NOTED.
) - [SDR UIEA2023120400974](https://openairdocs.org/sdr/UIEA2023120400974.md): Idg · unknown · Dec 3, 2023 · N663GT · Boeing 767324 · AC Generator-Alternator > TWO LOWSPEED RTO'S PERFORMED DUE TO L GEN OFF, L/R UTILITY BUS OFF SHORTLY AFTER APPLYING T/O POWER(TRANSFER TO DMI 198358 PER MEL 24-00-01-01 CAT B DUE 06DEC2023. MX ACTIONS COMPLIED WITH VIA DISCONNECTION. PLACARDS INSTALLED. DISPATCH NOTIFIED. PERFORMED - [SDR UIEA2023101200902](https://openairdocs.org/sdr/UIEA2023101200902.md): Unknown · unknown · Oct 12, 2023 · N663GT · Boeing 767324 · Emergency Equipment > L1 ENTRY DOOR WILL NTO CLOSE DUE TO EMERGENCY ESCAPE ROPE FALLING OUT OF CONTAINMENT POUCH(
STOWED EMERGENCY ROPE IAW AMM 25-61-04-402-010-001. L1 DOOR OPS CHECK NORMAL.
) - [SDR UIEA2023080800773](https://openairdocs.org/sdr/UIEA2023080800773.md): Unknown · unknown · Aug 8, 2023 · N663GT · Boeing 767324 · Aileron Control System > FLIGHT CONTROL FLUTTER ON LANDING(PER ATLAS SAFETY DATA RETRIEVED INDICATED NO FLIGHT CONT ISSUES ON LANDING OR FLAIR. ACCOMPLISHED FLIGHT CONT/AILERON OPS TEST IAW AMM 27-11-00-215. NO DEFECTS NOTED.
) - [SDR UIEA2023060700598](https://openairdocs.org/sdr/UIEA2023060700598.md): Control Rod · unknown · Jun 7, 2023 · N663GT · Boeing 767324 · Flight Control System > UPON TAKEOFF, LE SLAT DISAGREE MESSAGE APPEARED ON EICAS. FOLLOWED QRH PROCEDURES. FLAPS WILL NOT MOVE TO UP POSITION. DIVERSION BACK TO SCK.(REMOVED AND REPLACED #6 SLAT OB SLAT CONTROL ROD REF AMM 27-81-04-434-036 AND AMM 27-81-00-825-437. OPS CHECK SATIS - [SDR UIEA2023012200072](https://openairdocs.org/sdr/UIEA2023012200072.md): Aileron · cracked · Jan 24, 2023 · N663GT · Boeing 767324 · Aileron Control System > LH O/B AILERON I/B TRAILING EDGE NEAR FUEL DUMP TUBE REQUIRES EVALUATION FOR POSSIBLE CRACK (REPAIRED AILERON IAW B767-300 SRM BCG D634T210 REV121, 51-70-17-0G-0) - [SDR UIEA2023010300001](https://openairdocs.org/sdr/UIEA2023010300001.md): Extinguisher · leaking · Dec 30, 2022 · N663GT · Boeing 767324 · Passenger Compartment Equipment > FIRE BANE LIFE KIT FIRE EXTINGUISHER AGENT FOUND LEAKING. R & R FIREBANE LIFE KIT EXTINGUISHER IN OVERHEAD BIN IAW AMM 25-60-01. MCC NOTIFIED, PLACARDS REMOVED. NEW PART FILLED IN, OLD PART PREVIOUSLY REMOVED. MB 1757Z
) - [SDR UIEA2022122871218](https://openairdocs.org/sdr/UIEA2022122871218.md): Warning Message · illuminated · Dec 27, 2022 · N663GT · Boeing 767324 · Pneumatic Distribution System > DURING CLIMBOUT, EICAS MSG DISPLAYED DURING HIGH POWER SETTING. RAN QRH CHECKLIST. L ENG HPSOV. TRANSFER TO MDDR 177720 IAW MEL 36-11-02-02 CAT C. - [SDR UIEA2022110301187](https://openairdocs.org/sdr/UIEA2022110301187.md): None · none · Nov 3, 2022 · N663GT · Boeing 767 · Aircraft Fuel Distribution System > AT CRUISE PRIOR TO ETOPS ENTRY: RECEIVED "FUEL CONFIG" EICAS MSG. FUEL SUSEPTED. TOTALIZER & CALCULATED FUEL WERE 1500 LBS DEFFERENCE & INCREASING. FUEL QUANTITY INDICATING A 2,300 LBS SPLIT & INCREASING. COMPLIED WITH QRH, 1 ENG SHUT DOWN MANDAY RETURN TO HNL - [SDR UIEA2022073000792](https://openairdocs.org/sdr/UIEA2022073000792.md): Valve · leaking · Aug 12, 2022 · N663GT · Boeing 767324 · Aircraft Fuel Distribution System > LH WING, REAR SPAR RIB 2 AT FUEL SHUT-OFF VALVE APU WITH EVIDENCE OF LEAK FUEL(LH WING REAR SPAR RIB 2 AT FUEL SHUT OFF VALVE APU WAS REPLACED IAW AMM 28-25-02-404-008 REV 136 DATE 22 APR 2022
) - [SDR UIEA2022073000788](https://openairdocs.org/sdr/UIEA2022073000788.md): Panel · burned · Aug 12, 2022 · N663GT · Boeing 767324 · Fuselage Miscellaneous Structure > LH FUSELAGE AFT STATIC PORT THREE BURN MARKS NEAR LH STATIC PORT(BURN MARKS WERE REPAIRED BY BLENDING OPERATIONS AND APPROVED BY BOEING IAW TRE6753549 DATE JUL 22, 2022
) - [SDR UIEA2022073000789](https://openairdocs.org/sdr/UIEA2022073000789.md): Apu · leaking · Aug 12, 2022 · N663GT · Boeing 767324 · APU Engine Fuel and Control > EVIDENCE OF FUEL LEAK AROUND ELECTRICAL WIRING CTR AUX FUEL QTY (M1934) LOCATED BETWEEN WBL 121 AND WBL 97.9566 AT REAR SPAR OF LH WING(JAM NUT WAS TIGHTENED AND SEALANT WAS APPLIED AND CHEKED FOR LEAKS. TEST SATISFACTORY IAW AMM 28-41-04-404-028-002
) - [SDR UIEA2022073000790](https://openairdocs.org/sdr/UIEA2022073000790.md): Panel · dented · Aug 12, 2022 · N663GT · Boeing 767324 · Aileron Control System > RH WING, BOTH OUTBOARD AILERON ACTUATORS (PCA) WITH EVIDENCE OF HYDRAULIC LEAK(HYDRAULIC SYSTEM EXTERNAL LEAKAGE CHECK WERE PERFORMED. NO LEAKING EVIDENCE FOUND IAW AMM 29-11-00-796-053 REV 136
) - [SDR UIEA2022073000791](https://openairdocs.org/sdr/UIEA2022073000791.md): Hose Connector · leaking · Aug 12, 2022 · N663GT · Boeing 767324 · Pneumatic Distribution System > NLG HYDRAULIC ACTUATOR, HOSE ASSY RH WITH SWEVEL LEAK(NLG HYDRAULIC ACTUATOR, HOSE ASSY RH (P/N LPS14-49C8S) WAS REPLACED IAW AMM 32-34-01-004-027 & 32-34-01-404-010 REV 136
) - [SDR UIEA2022073000793](https://openairdocs.org/sdr/UIEA2022073000793.md): Panel · delaminated · Aug 12, 2022 · N663GT · Boeing 767324 · Nacelle/Pylon, Main Frame > ENGINE 1, ACOUSTIC SHROUD WITH SEVERAL DENTS BETWEEN 4 AND 7 HRS(INLET COWL ACOUSTIC PANEL DENTS WERE REPAIR IAW EO 1971A286
) - [SDR UIEA2022073000794](https://openairdocs.org/sdr/UIEA2022073000794.md): Radome · delaminated · Aug 12, 2022 · N663GT · Boeing 767324 · Fuselage Structure (General) > RADOME OUTER SKIN, HONEYCOMB AREA WITH IMPACT(RADOME WAS REPLACED (NEW RADOME P/N 284T0052-39 S/N 000673) IAW AMM 53-12-01-A02-054
) - [SDR UIEA2022080900843](https://openairdocs.org/sdr/UIEA2022080900843.md): Elt · broken · Aug 12, 2022 · N663GT · Boeing 767324 · Emergency Equipment > CONTROL CABIN, RH SIDE, LATERAL WALL OF LAVATORY, ELT WITH BROKEN SEAL(EMERGENCY LOCATOR TRANSMITTER WAS REPLACED IAW AMM 25-63-03-000-802 & 25-63-03-400-802 REV 136
) - [SDR UIEA2022081000850](https://openairdocs.org/sdr/UIEA2022081000850.md): Door · dented · Aug 12, 2022 · N663GT · Boeing 767324 · Passenger/Crew Doors > DENT WITH PREVIOUS REWORK AND ELONGATED HOLE AT STA 654+85 AND BEAM #3 OF LH MID ENTRY DOOR - OUTER SKIN(DENT, PREVIOUS REWORK AND ELONGATED FASTENER HOLE WERE REPAIRED IAW TRE6752035
) - [SDR UIEA2022081000853](https://openairdocs.org/sdr/UIEA2022081000853.md): Skin Panel · burned · Aug 12, 2022 · N663GT · Boeing 767324 · Fuselage Main, Plate/Skin > LH FUSELAGE AFT STATIC PORT THREE BURN MARKS(BURN MARKS WERE REPAIR BY BLENDING OPERATIONS IAW TRE6753549 REV 0
) - [SDR UIEA2022060600571](https://openairdocs.org/sdr/UIEA2022060600571.md): Bleed Air Sys · not seated · Jun 6, 2022 · N663GT · Boeing 767324 · Pneumatic Indicating System > L ENG BLEED OFF RTB KONT DUE TO PRESSUERIZATION/BLEED ISSUE. PERF AIR SUPPLY BITE PER FIM 36-20 FT 804.BITE FAULTED TEST FAILED WITH LIGHT TEST AND FAULTED MULTIPLE FAULTS ON BOTH L&R ENG. R&R SUPPLY BOX PER AMM 36-23-01. UPON FUTHER INSPECTION FOUND L ENG BLE - [SDR UIEA2021110102311](https://openairdocs.org/sdr/UIEA2021110102311.md): None · none · Oct 26, 2021 · N663GT · Boeing 767324 · Engine Fuel/Oil Cooler > L ENG FUEL FILTER STATUS MSG(INSPECTED FUEL FILTER ELEMENT IAW AMM 73-11-02-216-001-H00, NO CONTAMINATION FOUND. INSTALLED NEW FILTER ELEMENT IAW AMM 73-11-02-404-008-H00, RAN ENG IAW AMM 71-00-00-995-229-H03, NO LEAKS NOTED AND NO MSG ON EICAS DURING RUN.< - [SDR UIEA2021102002261](https://openairdocs.org/sdr/UIEA2021102002261.md): None · none · Oct 20, 2021 · N663GT · Boeing 767324 · Oxygen System > FWD E&E COMPT CREW OXYGEN NEED SERVICE TO FULL(
REMOVED, SERVICED & REINSTALLED CREW OXYGEN CYLINDER AS PER B767-300 AMM 12-15-08
/AMM 35-00-00-012-005, AMM 35-11-00-206 AND AC 43.13-1B PAR 9-46 THRU 9-51 & NO LEAKS NOTED - [SDR UIEA2021102002262](https://openairdocs.org/sdr/UIEA2021102002262.md): None · none · Oct 20, 2021 · N663GT · Boeing 767324 · Engine Air Baffle Section > #2 ENG O/B FAN COWL IS DELAMINATED(
ACCOMPLISHED HOT BONDED PERMANENT REPAIR ON #2 ENG O/B FAN COWL PER 54-22-00-0G-0
/54-21-01-0I-1, 54-21-01-01A-1; 54-21-01-2R-1 REPAIR 1
/51-70-04-0G-0, WORK ACCOMPLISHED PER - [SDR UIEA2021100802204](https://openairdocs.org/sdr/UIEA2021100802204.md): None · none · Oct 7, 2021 · N663GT · Boeing 767324 · Doppler System > "WX SYS" STATUS MSG AFTER TAKEOFF (REMAINED ENTIRE FLT)(
PERFORMED FIM TASK 34-43 TASK 801. FAULT CLEARED. WEATHER RADAR SYSTEM OPS CHECKS GOOD.
) - [SDR UIEA2021091102010](https://openairdocs.org/sdr/UIEA2021091102010.md): Warning Message · false activation · Sep 11, 2021 · N663GT · Boeing 767324 · Weather Radar System > ON TAXI IN THE "WXR SYS" STATUS MESSAGE DISPLAYED(C/W WEATHER RADAR SYSTEM OPERATIONAL TEST IAW AMM 34-43-00-715-026-002. OPS CHECK GOOD.
) Next page: https://openairdocs.org/aircraft/N663GT/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 = 'N663GT' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N663GT/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.