# Service difficulty reports: N710SY, cancelled Aug 21, 2021 A list on [N710SY, cancelled Aug 21, 2021](https://openairdocs.org/deregistered/N710SY-2021-08-21.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 3 · 119 reports - [SDR SCNA2019100197177](https://openairdocs.org/sdr/SCNA2019100197177.md): Connector · dirty · Sep 27, 2019 · N710SY · Boeing 73773V · Trailing Flap Position Indicating System > LEADING EDGE FLAP TRANSIT LIGHT ILLUMINATED BETWEEN 5-15 PERFORMED QRH 9.14. CREW INITIATED GO AROUND AND DECLARED EMERGENCY, AND FLIGHT LANDED SAFELY ON SECOND APPROACH. PERFORMED FIM TASK 27-51 #830, TASK #803 & TASK 820. PERFORMED LEADING EDGE CONTROL SYSTE - [SDR SCNA20190907176](https://openairdocs.org/sdr/SCNA20190907176.md): Screw · unsecure · Sep 10, 2019 · N710SY · Boeing 73773V · Trailing Edge Flap Control System > #3 SPOILER DAMAGED DUE TO SCREW POPPED OUT FROM THE TRAILING EDGE OUTBOARD FLAP. REMOVED #3 SPOILER IAW AMM 27-61-11. INTERFACE INSPECTION OF #3 SPOILER COMPLIED WITH, OK TO INSTALL. INSTALLED #3 SPOILER IAW AMM 27-61-11. PERFORMED SPOILER SYSTEM TEST AND ADJU - [SDR SCNA20190907175](https://openairdocs.org/sdr/SCNA20190907175.md): Skin Panel · worn · Sep 10, 2019 · N710SY · Boeing 73773V · Trailing Edge Flaps > RIGHT WING OUTBOARD TRAILING EDGE MAIN FLAP TOP PANELS ARE WORN. REMOVED OUTBOARD TRAILING EDGE FLAP PER AMM 27-51-21-000-801. INTERFACE INSPECTION OF RT OTBD TRAILING EDGE FLAP AND AFT FLAP SECTION COMPLIED WITH. OK TO INSTALL. INSTALLED RT OB FLAP REF AMM 27 - [SDR SCNA20190907174](https://openairdocs.org/sdr/SCNA20190907174.md): Screw · broken · Sep 10, 2019 · N710SY · Boeing 73773V · Trailing Edge Flap Control System > TE OB FWD FLAP DAMAGED DUE TO SCREW BROKEN FROM 10FT OB OF THE FLAP. DAMAGE PAST LIMITS FOR SRM 57-53-01-01-03. REMOVED LT OUTBOARD FLAP PER AMM 27-51-22. INSTALLED SERVICEABLE LT OB MAIN FLAP REF AMM 27-51-21-400-801. FLAP ADJUSTMENT PERFORMED PER AMM 27-51-2 - [SDR SCNA20190907173](https://openairdocs.org/sdr/SCNA20190907173.md): Intercostal · cracked · Sep 10, 2019 · N710SY · Boeing 73773V · Fuselage Miscellaneous Structure > THE WEB LOCATED AT EMPENAGE STATION 1040 HAS A.6 INCH LONG CRACK AT THE MOST LEFT LIGHTENING HOLE. DRILLED A.128" DIA STOP HOLE AT END OF CRACK. OPEN HOLE NDT ACCOMPLISHED AND NO CRACK BEYOND STOP DRILL HOLE. REMOVED DAMAGE FROM INTERCOSTAL WEB IAW SRM 53-00 - [SDR SCNA20181128125](https://openairdocs.org/sdr/SCNA20181128125.md): Flap · damaged · Nov 28, 2018 · N710SY · Boeing 73773V · Trailing Edge Flaps > BOTTOM OUTBOARD FLAP AT CANOE 7 OUTBOARD SIDE HAS WEAR AND MISSING PAINT FROM CANOE FLAP SURFACE. WEAR WAS FOUND TO BE ON RIGHT OUTBOARD AFT FLAP LOWER SURFACE ON A PREVIOUS REPAIR DOUBLER THAT IS WORN THROUGH DOUBLER IN THE CRITICAL AREA. DAMAGE IS OUT OF LIM - [SDR SCNA2018111309118](https://openairdocs.org/sdr/SCNA2018111309118.md): Landing Gear · malfunctioned · Nov 9, 2018 · N710SY · Boeing 73773V · Landing Gear Retraction/Extension System > WHEN GEAR HANDLE WAS MOVED FROM UP TO OFF POSITION, NOSE GEAR EXTENDED TO DOWN AND LOCKED POSITION. MX NOTIFIED. PERFORMED FIM TASK AND AMM. MULTIPLE GEAR SWINGS WITH NO FAULTS NOTED. OPS CHECKS GOOD. - [SDR SCNA201808132102](https://openairdocs.org/sdr/SCNA201808132102.md): Stiffener · broken · Aug 12, 2018 · N710SY · Boeing 73773V · Wing Miscellaneous Structure > DURING REPAIR OF UPPER LT WING SKIN, FOUND A STIFFINER AT THE WING LE TO PYLON RIB WS 204 WAS BROKEN. REMOVED THE DAMAGED STIFFENER. NDT INSPECTION PERFORMED. NO CRACKS NOTED. INSTALLED THE NEW STIFFENER. OK FOR SERVICE. - [SDR SCNA201808130101](https://openairdocs.org/sdr/SCNA201808130101.md): Skin · damaged · Aug 10, 2018 · N710SY · Boeing 73773V · Wing, Plate/Skin > LEFT WING UPPER SURFACE L/E. OTBD OF KRAS 206. THE LAST 18 OTBD AFT RIVETS ARE LOOSE AND WORKING. REMOVE 29 FASTNERS. FOUND L/E SKIN DAMAGED IN THE FORM OF OVERSIZED COUNTER SINKS IN THE SKIN. MOST OBRD FASTNER PULLED THROUGH THE SKIN. REMOVED PNEU. DUCT BY TH - [SDR SCNA201805232093](https://openairdocs.org/sdr/SCNA201805232093.md): Turnbuckle · cracked · May 22, 2018 · N710SY · Boeing 73773V · Wing Main, Frame Structure > RIGHT WING TRAILING EDGE TURNBUCKLE BRACKET INBD OF DEFLECTION RIB WAS CRACKED. REMOVED AND REPALCED THE TURNBUCKLE. - [SDR SCNA201805232092](https://openairdocs.org/sdr/SCNA201805232092.md): Mount · corroded · May 22, 2018 · N710SY · Boeing 73773V · Fuselage Main, Attach Fittings > AFT LAVATORY AFT INBD MOUNT HAD CORROSION EVIDENCE. REPAIRED THE MOUNT. - [SDR SCNA201805232091](https://openairdocs.org/sdr/SCNA201805232091.md): Plate · corroded · May 22, 2018 · N710SY · Boeing 73773V · Fuselage Miscellaneous Structure > AFT CARGO PANEL "HOCKEY STICK" AND A SPLICE PLATE CORRODED, BOTHSIDE OF PLATES. REMOVED AND REPLACED AFT PIT PANEL HOCKEY STICK AND SPLICE PLATE. - [SDR SCNA20180301069](https://openairdocs.org/sdr/SCNA20180301069.md): Charger · inoperative · Mar 1, 2018 · N710SY · Boeing 73773V · Emergency Lighting > ON RON CHECK FOUND THE FWD EMG FLOOR LIGHT INOP. DEACTIVATED THE FWD LEFT WIND SCREEN PROX LIGHT. PLACED DEACTIVATION OF LT FWD PROX LIGHT ON GMM/MTI FOR TRACKING PURPOSES. R&R FWD LEFT EMERG LIGHT BATT CHARGER. OP CHKS GOOD. OK FOR SVC, THIS CLEARS MTI/GMM. - [SDR SCNA20180301068](https://openairdocs.org/sdr/SCNA20180301068.md): Power Supply · inoperative · Mar 1, 2018 · N710SY · Boeing 73773V · Emergency Lighting > R2 DOOR EMERGENCY LIGHT SIGN DOES NOT ILLUMINATE. REMOVED AND REPLACED R2 DOOR EMERGENCY LIGHT POWER SUPPLY. OPS CK'D OK. A/C OK FOR SERVICE. - [SDR SCNA20170817159](https://openairdocs.org/sdr/SCNA20170817159.md): Connector · disconnected · Aug 17, 2017 · N710SY · Boeing 73773V · Light System Wiring > ON LT FORWARD WINDSCREEN, LOWER PROXIMITY LIGHT IS INOPERATIVE. CONNECTED EXIT LIGHT BATTERY PACK M1675 CONNECTOR D10750P AND CONNECTED D12350 TO FWD LEFT WINDSCREEN PROXIMITY LIGHT RECEPTICLE D92352. OP CHECKED GOOD. ACFT IS OK FOR SERVICE. - [SDR SCNA20170702154](https://openairdocs.org/sdr/SCNA20170702154.md): Attach Fitting · loose · Jul 2, 2017 · N710SY · Boeing 73773V · Wing Main, Frame Structure > RIGHT WING UPPER FIXED TRAILING EDGE PANEL ATTACH FITTING LOOSE. REPAIRED. - [SDR SCNA20170509057](https://openairdocs.org/sdr/SCNA20170509057.md): Connector · defective · May 9, 2017 · N710SY · Boeing 73773V · Flight Control System Wiring > FLAP ASYMMETRY OFF OF "UP" AT GATE. REMOVED AND REPLACED SKEW NR 5 CONNECTOR D11822. COMPLETED FLAP SKEW FUNCTIONAL TEST. OPS TEST NORMAL. - [SDR SCNA20161112299](https://openairdocs.org/sdr/SCNA20161112299.md): Cowling · dented · Nov 12, 2016 · N710SY · Boeing 73773V · Engine Cowling System > FOUND DENT AT 7 O'CLOCK POSITION ON NR 2 ENG INLET COWL, 11" X 8" BY.5". DENT OUT OF LIMITS. REMOVE AND REPLACED NR 2 ENGINE INLET COWL. - [SDR SCNA20160916189](https://openairdocs.org/sdr/SCNA20160916189.md): Window Frame · cracked · Sep 16, 2016 · N710SY · Boeing 73773V · Fuselage Main, Structure > DURING DVI AND NDT INSPECTION OF RT NR 1 FLIGHT DECK WINDOW FRAME, FOUND FRAME CRACKED AT UPPER OTBD CORNER. VERIFIED WITH HFEC AND MARKED CRACK END IN BLACK. INSTALLED REPAIR. REPAIRED NR 1 RT FLIGHT DECK WINDOW AT UPPER OTBD CORNER. REMOVED AND REINSTALL - [SDR SCNA20160916188](https://openairdocs.org/sdr/SCNA20160916188.md): Window Frame · cracked · Sep 16, 2016 · N710SY · Boeing 73773V · Fuselage Main, Structure > DURING DVI AND NDT INSPECTION OF LT NR 1 FLIGHT DECK WINDOW FRAME, FOUND FRAME CRACKED AT UPPER OTBD CORNER. VERIFIED WITH HFEC AND MARKED CRACK END IN BLACK. INSTALLED REPAIR. GAINED AND RESTORED ACCESS TO THE LT NR 1 FLIGHT DECK WINDOW FRAME BY REMOVING A - [SDR SCNA20160916187](https://openairdocs.org/sdr/SCNA20160916187.md): Spar · damaged · Sep 16, 2016 · N710SY · Boeing 73773V · Horizontal Stabilizer, Spar/Rib > WHILE ACCOMPLISHING LT HORIZONTAL STABILIZER LOWER SKIN MODIFICATION, FASTENER HOLE IN THE FRONT LOWER SPAR WAS ELONGATED AT STA 142. FASTENER HOLE WAS CLEANED TO A.277" DIA, NDT ACCOMPLISHED WITH NO DEFECTS. - [SDR SCNA20160916185](https://openairdocs.org/sdr/SCNA20160916185.md): Support Bracket · broken · Sep 16, 2016 · N710SY · Boeing 73773V · Fuselage Miscellaneous Structure > LOWER CENTER PANEL SUPPORT BRACKET BROKEN ON RIGHT SIDE. MARKED WITH A DOT. KEELBEAM BETWEEN A/C ACCESS PANELS. REMOVED AND REPLACED LOWER CENTER PANEL SUPPORT BRACKET A/C ACCESS PANEL. - [SDR SCNA20160916184](https://openairdocs.org/sdr/SCNA20160916184.md): Rib · damaged · Sep 16, 2016 · N710SY · Boeing 73773V · Horizontal Stabilizer, Spar/Rib > ELONGATED HOLE ON RIB 120.3 OUTBOARD LOWER FLANGE RT. REPAIRED ELONGATED FASTNER HOLE ON RT HORIZONTAL STAB AT RIB STA 120.3. - [SDR SCNA20160916183](https://openairdocs.org/sdr/SCNA20160916183.md): Rib · cracked · Sep 16, 2016 · N710SY · Boeing 73773V · Horizontal Stabilizer, Spar/Rib > WHILE ACCOMPLISHING LT HORIZONTAL STAB LOWER SKIN MODIFICATION, CRACK FOUND AT FASTENER HOLE ON RIB, STA 138.7, 12" FROM AFT SPAR ON THE OTBD HORZ FLANGE. DAMAGE HAS BEEN REMOVED AND 4 FASTENERS ON EITHER SIDE OF THE CUTOUT HAS BEEN NDT FOR CRACKS WITH NO DEF - [SDR SCNA20160916182](https://openairdocs.org/sdr/SCNA20160916182.md): Stiffener · cracked · Sep 16, 2016 · N710SY · Boeing 73773V · Horizontal Stabilizer Miscellaneous Structure > RIGHT HORIZONTAL STABILIZER LOWER SIDE NR 1 RIB STIFFINER CRACKED MARKED. VERIFIED CRACK ON RT HORIZONTAL STABILIZER LOWER SIDE NR 1 RIB STIFFINER. REPAIRED CRACKED. - [SDR SCNA20160916181](https://openairdocs.org/sdr/SCNA20160916181.md): Rib · damaged · Sep 16, 2016 · N710SY · Boeing 73773V · Horizontal Stabilizer, Spar/Rib > RIGHT HORIZONTAL STABILIZER LOWER NR 5 RIB HAS BAD HOLE MARKED. CUTOUT DAMAGE HOLE ON RT HORIZONTAL STABILIZER NR 5 RIB. FABRICATED AND INSTALLED REPAIR. - [SDR SCNA20160916180](https://openairdocs.org/sdr/SCNA20160916180.md): Keelbeam · corroded · Sep 16, 2016 · N710SY · Boeing 73773V · Fuselage Main, Keel > KEELBEAM FORWARD AREA LT SIDE EYE BOLT CORRODED. R & R KEELBEAM FORWARD AREA LT SIDE EYE BOLT WITH NEW. - [SDR SCNA20160916179](https://openairdocs.org/sdr/SCNA20160916179.md): Skin · cracked · Sep 16, 2016 · N710SY · Boeing 73773V · Horizontal Stabilizer, Plate/Skin > LEFT HORIZONTAL STABILIZER L/E LOWER SKIN, STA 138.7 28" AFT LOWER RIB FLANGE OTBD FASTENER HOLE CRACKED. REPAIRED LT HORIZONTAL STABILIZER L/E LOWER SKIN STA 138.7, 28" AFT LOWER RIB FLANGE OTBD FASTENER. - [SDR SCNA20160916178](https://openairdocs.org/sdr/SCNA20160916178.md): Skin · damaged · Sep 16, 2016 · N710SY · Boeing 73773V · Horizontal Stabilizer, Plate/Skin > LEFT HORIZONTAL STABILIZER L/E LOWER SKIN, STA 138.7, 18" AFT LOWER RIB FLANGE INBD ROW FASTENER HOLE ELONGATED. REAMED HOLE TO FINAL SIZE OF.193 HOLE CLEAN AND ROUND. NO DEFECTS NOTED. - [SDR SCNA20160916177](https://openairdocs.org/sdr/SCNA20160916177.md): Skin · damaged · Sep 16, 2016 · N710SY · Boeing 73773V · Horizontal Stabilizer, Plate/Skin > LEFT HORIZONTAL STABILIZER L/E LOWER SKIN, STA 138.7 AFT 4" LOWER RIB FLANGE HAS ELONGATED OTBD HOLE. REPAIRED LT HORIZONTAL STABILIZER L/E LOWER SKIN AT STA 138.7, AFT 4" LOWER RIB FLANGE ELONGATED FASTENER HOLE. - [SDR SCNA20160916176](https://openairdocs.org/sdr/SCNA20160916176.md): Skin · damaged · Sep 16, 2016 · N710SY · Boeing 73773V · Horizontal Stabilizer, Plate/Skin > LT HORIZONTAL STABILIZER L/E LOWER SKIN, STA 142 LOWER CORD HAS ELONGATED FASTENER HOLE. REPAIRED LT HORIZONTAL STABILIZER L/E LOWER SKIN AT STA 142, LOWER CHORD. - [SDR SCNA20160916175](https://openairdocs.org/sdr/SCNA20160916175.md): Skin · damaged · Sep 16, 2016 · N710SY · Boeing 73773V · Horizontal Stabilizer, Plate/Skin > LEFT HORIZON STABILIZER L/E LOWER SKIN, STA 157, 7"AFT INBD FASTENER ROW HAS ELONGATED HOLE. REMOVED HOLE TO FINAL SIZE OF.193. HOLE CLEAN AND ROUND. NO DEFECTS NOTED. - [SDR SCNA20160916174](https://openairdocs.org/sdr/SCNA20160916174.md): Hinge Fitting · cracked · Sep 16, 2016 · N710SY · Boeing 73773V · Landing Gear Doors > LEFT MLG INBD HINGED DOOR, AFT HINGE FITTING ON INBD DOOR, CRACK IN FITTING AT AFT OTBD ATTACH BOLT HOLE, END OF CRACK MARKED IN BLACK, VERIFIED BY NDT INSP. ACCOMPLISH TASK CARD FOR REPAIRS. R & R -1 & -2 HINGES. - [SDR SCNA20160916173](https://openairdocs.org/sdr/SCNA20160916173.md): Mount · corroded · Sep 16, 2016 · N710SY · Boeing 73773V · Fuselage, Equipment Attach Fittings > G4 GALLEY CENTER DIVIDER FLOOR MOUNT CORRODED. REPLACED G4 GALLEY CENTER DIVIDER FLOOR MOUNT THAT WAS CORRODED. - [SDR SCNA20160916172](https://openairdocs.org/sdr/SCNA20160916172.md): Floorboard · damaged · Sep 16, 2016 · N710SY · Boeing 73773V · Fuselage Floor Panel > AFT WET AREA FLOORBOARD, PN147A58140-76 DELAMINATED AND FIBERS SHOWING. REPAIRED AFT WET AREA FLOORBOARD, PN 147A58140-76. - [SDR SCNA20160916171](https://openairdocs.org/sdr/SCNA20160916171.md): Insert · corroded · Sep 16, 2016 · N710SY · Boeing 73773V · Fuselage Floor Panel > AFT WET AREA FLOORBOARD, PN 147A5810-171 HAS 4 CORRODED INSERTS. R & R 4 EA DAMAGED INSERT IN PANEL 3-147A5810-171. - [SDR SCNA20160916170](https://openairdocs.org/sdr/SCNA20160916170.md): Insert · corroded · Sep 16, 2016 · N710SY · Boeing 73773V · Fuselage Floor Panel > AFT WET AREA CABIN FLOORBOARD, PN147A5810-288 HAS 3 CORRODED INSERTS. INSTALLED 3 INSERTS. - [SDR SCNA20160916169](https://openairdocs.org/sdr/SCNA20160916169.md): Insert · corroded · Sep 16, 2016 · N710SY · Boeing 73773V · Fuselage Floor Panel > AFT WET AREA CABIN FLOORBOARD HAS CORRODED INSERTS AND ONE MISSING INSERT. REMOVED & REPLACED THE INSERTS. - [SDR SCNA20160916168](https://openairdocs.org/sdr/SCNA20160916168.md): Floorboard · delaminated · Sep 16, 2016 · N710SY · Boeing 73773V · Fuselage Floor Panel > AFT WET AREA CABIN FLOORBOARD HAS MINOR DELAMINATION ON TOP. REPAIRED THE FLOORBOARD. - [SDR SCNA20160916167](https://openairdocs.org/sdr/SCNA20160916167.md): Insert · corroded · Sep 16, 2016 · N710SY · Boeing 73773V · Fuselage Floor Panel > AFT WET AREA FLOORBOARD HAS SEVERAL CORRODED INSERTS. REPLACED THE INSERTS. - [SDR SCNA20160916166](https://openairdocs.org/sdr/SCNA20160916166.md): Floorboard · delaminated · Sep 16, 2016 · N710SY · Boeing 73773V · Fuselage Floor Panel > FWD WET AREA FLOORBOARD 221BF RT CORNER IS DELAMINATED. REPAIRED THE FLOORBOARD. - [SDR SCNA20160916165](https://openairdocs.org/sdr/SCNA20160916165.md): Floorboard · damaged · Sep 16, 2016 · N710SY · Boeing 73773V · Fuselage Floor Panel > FWD CABIN FLOORBOARD 221GF HAS DAMAGE WHERE INSERT WAS PULLED. REPAIRED THE FLOORBOARD. - [SDR SCNA20160916164](https://openairdocs.org/sdr/SCNA20160916164.md): Insert · corroded · Sep 16, 2016 · N710SY · Boeing 73773V · Fuselage Floor Panel > FWD CABIN FLOORBOARD 222BF HAS 1 MISSING INSERT AND SEVERAL CORRODED INSERTS. REMOVED AND REPLACED THE INSERTS. - [SDR SCNA20160916163](https://openairdocs.org/sdr/SCNA20160916163.md): Floorboard · delaminated · Sep 16, 2016 · N710SY · Boeing 73773V · Fuselage Floor Panel > FWD WET AREA FLOORBOARD 221CF HAS CORNER DELAMINATED AND ONE INSERT MISSING. REPAIRED THE FLOORBOARD. - [SDR SCNA20160916162](https://openairdocs.org/sdr/SCNA20160916162.md): Floorboard · delaminated · Sep 16, 2016 · N710SY · Boeing 73773V · Fuselage Floor Panel > FWD CABIN FLOORBOARD 222DF CORNER IS DELAMINATED. REPAIRED THE FLOORBOARD. - [SDR SCNA20160916161](https://openairdocs.org/sdr/SCNA20160916161.md): Insert · corroded · Sep 16, 2016 · N710SY · Boeing 73773V · Fuselage Floor Panel > FWD WET AREA FLOORBOARD 222AF HAS SEVERAL CORRODED INSERTS. REMOVED AND REPLACED THE INSERTS. - [SDR SCNA20160916160](https://openairdocs.org/sdr/SCNA20160916160.md): Floorbeam · corroded · Sep 16, 2016 · N710SY · Boeing 73773V · Fuselage Main, Floor Beam > BS 986 FLOORBEAM UPPER TEE PREVIOUS REPAIR IS CORRODED AT SEVERAL AREAS ON UPPER AND LOWER SURFACES FROM LBL 14 TO RBL 45. REPAIRED. - [SDR SCNA20160916159](https://openairdocs.org/sdr/SCNA20160916159.md): Floorbeam · corroded · Sep 16, 2016 · N710SY · Boeing 73773V · Fuselage Main, Floor Beam > BS 986 UPPER TEE, FORWARD FLANGE, LOWER SURFACE COMMON TO FASTENER HOLE IS CORRODED AT LBL 30. REMOVED CORROSION. - [SDR SCNA20160916158](https://openairdocs.org/sdr/SCNA20160916158.md): Crease Beam · corroded · Sep 16, 2016 · N710SY · Boeing 73773V · Fuselage Main, Structure > LEFT CREASE BEAM IS CORRODED IN SEVERAL AREAS ON UPPER SURFACE FROM BS 967+10 - 986+6. FOUND CORROSION TO BE OUT OF LIMITS. REMOVED AND REPLACED THE CREASE BEAM. - [SDR SCNA20160916157](https://openairdocs.org/sdr/SCNA20160916157.md): Crease Beam · corroded · Sep 16, 2016 · N710SY · Boeing 73773V · Fuselage Main, Structure > RIGHT CREASE BEAM IS CORRODED IN SEVERAL AREAS ON UPPEER SURFACE FROM BS 947+9 - 986+7. REMOVED AND REPLACED THE CREASE BEAM. Next page: https://openairdocs.org/deregistered/N710SY-2021-08-21/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 = 'N710SY' AND deregistration_id = 'N710SY-2021-08-21' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N710SY-2021-08-21/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.