# Service difficulty reports: N130HQ A list on [N130HQ](https://openairdocs.org/aircraft/N130HQ.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 · 104 reports - [SDR R61A2025060900284](https://openairdocs.org/sdr/R61A2025060900284.md): Skin · damaged · May 29, 2025 · N130HQ · Emb ERJ170100LR · Fuselage Main, Plate/Skin > LIGHTNING STRIKE AT FIVE AREAS AFT OF RIGHT UPPER RADOME LATCH AT FR 2-3 AND STGR 12R-13R. PERFORMED FORWARD FUSELAGE - RH SKIN - LIGHTNING STRIKE - PERMANENT REPAIRS IAW ETD2025-170-921445 REV.: B AFT OF RIGHT UPPER RADOME LATCH AT FR2-3 AND STGR 12R-13R. REI - [SDR R61A2025060600283](https://openairdocs.org/sdr/R61A2025060600283.md): Frame · cracked · May 24, 2025 · N130HQ · Emb ERJ170200LR · Fuselage Main, Frame > WHILE IN HEAVY CHECK - FRAME 89 CRACKED AT STRINGER 28R. REPAIRED FRAME 89 AT STRINGER 28R IN ACCORDANCE WITH ETD2025-170-921863 REV A. - [SDR R61A2025060600282](https://openairdocs.org/sdr/R61A2025060600282.md): Doubler · corroded · May 19, 2025 · N130HQ · Emb ERJ170200LR · Fuselage Main, Plate/Skin > WHILE IN HEAVY CHECK - CORROSION FOUND ON INTERNAL DOUBLER BY WASTE ACCESS PANEL. REMOVE AND REPLACE INTERNAL WASTE DOUBLER RREF SRM 51-40-08. - [SDR R61A2025060600281](https://openairdocs.org/sdr/R61A2025060600281.md): Plate · chafed · May 19, 2025 · N130HQ · Emb ERJ170200LR · Engine Thrust Reverser > WHILE IN HEAVY CHECK - L/H ENGINE I/B TR CENTER BLANKET IS CHAFE. REMOVE DAMAGED CHAFE PLATE, FABRICATE REPAIR PATCH FROM.003" S/ S P.O.# 97613. SPOT WELDED REPAIR PATCH IN PLACE OVER DAMAGED AREA CREATED FROM REMOVING CHAFE PLATE. INSTALLED NEW CHAFE PLATE - [SDR R61A2025032900170](https://openairdocs.org/sdr/R61A2025032900170.md): Pressure Switch · faulted · Mar 29, 2025 · N130HQ · Emb ERJ170200LR · Landing Gear Brake System > PARKING BRAKE NOT RELEASED MSG INFLIGHT. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. REPLACED EMERGENCY BRAKE PRESSURE SWITCH. - [SDR R61A2025032700169](https://openairdocs.org/sdr/R61A2025032700169.md): Valve · faulted · Mar 27, 2025 · N130HQ · Emb ERJ170200LR · Landing Gear Brake System > PARKING BRAKE NOT RELEASED MSG AFTER TAKEOFF. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. REPLACED EMERGENCY PARKING BRAKE VALVE. - [SDR R61A2024100400455](https://openairdocs.org/sdr/R61A2024100400455.md): Slide · partial deploy · Oct 2, 2024 · N130HQ · Emb ERJ170200LR · Escape Slide > R1 DOOR SLIDE DEPLOYED PARTIALLY. R&R FWD SERVICE DOOR EMERGENCY EVACUATION SLIDE ASSEMBLY. - [SDR R61A2022061900399](https://openairdocs.org/sdr/R61A2022061900399.md): Stringer · corroded · Jun 19, 2022 · N130HQ · Emb ERJ170200LR · Fuselage Main, Longeron/Stringer > STRINGER 21L AT FR 89/90 HAS SPOTS OF CORROSION AROUND 2EA FASTENERS. CUT OUT CORRODED SECTION OF STRINGER 21L FRAME 88/91 AND INSTALL NEW SECTION PER EMB ETD2022-170-019794. RESTORE FINISH REF EMB SRM 51-23-05 & 51-23-06. - [SDR R61A2022061900398](https://openairdocs.org/sdr/R61A2022061900398.md): Beam · corroded · Jun 19, 2022 · N130HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure > FWD CARGO DOOR LOWER BEAM HAS CORROSION AT AFT LATCH FITTING FR 26-27 STGR 25R-26R. REMOVED AND REPLACED FWD CARGO DOOR LOWER BEAM EMB REF SRM 51-40-08 - [SDR R61A2022011700042](https://openairdocs.org/sdr/R61A2022011700042.md): Sensor · inoperative · Jan 13, 2022 · N130HQ · Emb ERJ170200LR · Airfoil Anti/De-ice System > ANTI-ICE WING 2 LEAK PASSING 13.5. ANTI-ICE WING TEST COMPLETED, THEN VALVES CLOSED, THEN MESSAGE DISPLAYED. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. R&R WING 2 SLAT 4 OUTBOARD WING ANTI-ICE TEMP SENSOR AND HARNESS TO TEMP SENSOR. - [SDR R61A2021111800911](https://openairdocs.org/sdr/R61A2021111800911.md): Fuse · blown · Nov 14, 2021 · N130HQ · Emb ERJ170200LR · Emergency Lighting > L1 DOOR EMERGENCY LIGHT 'EXIT' INOP. R&R F3 FUSE IN ELPU 2. - [SDR R61A2021082700673](https://openairdocs.org/sdr/R61A2021082700673.md): Windshield · cracked · Aug 24, 2021 · N130HQ · Emb ERJ170200LR · Flight Compartment Windows > RETURN TO FIELD FOR CAPTAIN'S WINDSHIELD CRACKED AFTER TAKE-OFF. R/R CAPTAIN'S WINDSHIELD. - [SDR R61A2020020410148](https://openairdocs.org/sdr/R61A2020020410148.md): Battery · inoperative · Feb 1, 2020 · N130HQ · Emb ERJ170200LR · Emergency Lighting > EMERGENCY LIGHT ABOVE ROW 20/21 INOP. R&R EMERGENCY LIGHT POWER UNIT IN RH AFT GALLEY. - [SDR R61A201911201292](https://openairdocs.org/sdr/R61A201911201292.md): Shear Angle · corroded · Nov 20, 2019 · N130HQ · Emb ERJ170200LR · Fuselage Main, Structure > WHILE IN HEAVY CHECK - CORROSION_FR.87 ST26R TO 27R HAS HAS CORRODED SHEAR CLIP. REMOVED AND INSTALLED NEW SHEAR CLIP FR 86 STGR 26R-27R REF SRM 51-40-08 - [SDR R61A201911201291](https://openairdocs.org/sdr/R61A201911201291.md): Shear Angle · corroded · Nov 20, 2019 · N130HQ · Emb ERJ170200LR · Fuselage Main, Structure > WHILE IN HEAVY CHECK - CORROSION_CORROSION AT FR.89 STR.26-27 R.HAND SHEAR CLIP. REMOVED AND REPLACE SHEAR CLIP REF SRM 51-40-02 - [SDR R61A201911201290](https://openairdocs.org/sdr/R61A201911201290.md): Shear Angle · corroded · Nov 20, 2019 · N130HQ · Emb ERJ170200LR · Fuselage Main, Structure > WHILE IN HEAVY CHECK - CORROSION_CORROSION AT FR.88 STR.26-27 R.HAND SHEAR CLIP. REMOVED DAMAGED SHEAR CLIP REF SRM 51-40-08. LOCATED AND DRILLED NEW SHEAR CLIP REF SRM 51-40-02, SRM 51-23-04.INSTALLED SHEAR CLIP AND APPLIED TOP COAT AT FR. 88 STR.26 - 27 REF - [SDR R61A201911201289](https://openairdocs.org/sdr/R61A201911201289.md): Sill Drain · corroded · Nov 20, 2019 · N130HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure > WHILE IN HEAVY CHECK - CORROSION_PASSENGER CABIN FWD WET AREA FWD RIGHT SILL FR.13 HAS CORROSION AS MARKED. REMOVED AND REPLACED FWD WET AREA FWD RIGHT SILL REF SRM 51-40-08. - [SDR R61A201911201288](https://openairdocs.org/sdr/R61A201911201288.md): Shear Panel · corroded · Nov 20, 2019 · N130HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure > WHILE IN HEAVY CHECK - CORROSION-CENTER FUSELAGE III WET AREA 53-23 RH SHEAR PANEL FRAME 87-88. REMOVED AND REPLACE RH SHEAR PANEL FR87-88 REF. SRM 51-40-08 - [SDR R61A201911201287](https://openairdocs.org/sdr/R61A201911201287.md): Floor Support · corroded · Nov 20, 2019 · N130HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure > WHILE IN HEAVY CHECK - CORROSION-CENTER FUSELAGE III WET AREA 53-52 ON RH PANEL SUPPORT, JUST FWD OF FRAME 89 AS MARKED. REMOVED AND REPLACED RH PANEL SUPPORT PN: 170-86181-005 REF EMB SRM 51-21-01, - [SDR R61A201911201286](https://openairdocs.org/sdr/R61A201911201286.md): Shear Tie · corroded · Nov 20, 2019 · N130HQ · Emb ERJ170200LR · Fuselage Internal Mounting Structure > WHILE IN HEAVY CHECK - CORROSION_FR.87 ST26R TO 27R HAS HAS CORRODED SHEAR CLIP. REMOVED AND INSTALLED NEW SHEAR CLIP FR 86 STGR 26R-27R REF SRM 51-40-08. - [SDR R61A201911201285](https://openairdocs.org/sdr/R61A201911201285.md): Floorbeam · corroded · Nov 20, 2019 · N130HQ · Emb ERJ170200LR · Fuselage Main, Floor Beam > WHILE IN HEAVY CHECK - CORROSION- CENTER FUSELAGE III WET AREA 53-23 RH SPLICE FRAME 90 AS MARKED. REMOVED AND REPLACED SPLICE PN: 170-86119-005 REF EMB SRM 51-21-01 AND 51-40-08, - [SDR R61A2019022520199](https://openairdocs.org/sdr/R61A2019022520199.md): Battery · inoperative · Feb 22, 2019 · N130HQ · Emb ERJ170200LR · Emergency Lighting > FWD AND AFT EMERGENCY LIGHT BATTERIES INOP. R&R FWD AND AFT EMERGENCY LIGHT BATTERIES REF AMM 33-50-01. - [SDR R61A201807180798](https://openairdocs.org/sdr/R61A201807180798.md): Brake · overheated · Jul 18, 2018 · N130HQ · Emb ERJ170200LR · Brake > SHORTLY AFTER TAKEOFF DURING INITIAL CLIMB OUT, EICAS MESSAGE BRAKE OVERHEAT. DURING TAXI OUT, A/C REQUIRE MORE POWER THAN USUAL TO TAXI WITH A SLIGHT LEFT PULL, AFTER INITIAL ROTATION A/C LUNGED FORWARD. R&R NR 1 MAIN WHEEL IAW AMM 33-49-05 AND NR 1 BRAKE ASS - [SDR R61A201802230238](https://openairdocs.org/sdr/R61A201802230238.md): Girt Bar · malfunctioned · Feb 23, 2018 · N130HQ · Emb ERJ170200LR · Emergency Equipment > L2 DOOR WILL NOT DISARM. SECURED THE ANGLE ON THE GIRT BAR IAW AMM 52-11-41. - [SDR R61A201802140179](https://openairdocs.org/sdr/R61A201802140179.md): Girt Bar · out of adjust · Feb 14, 2018 · N130HQ · Emb ERJ170200LR · Emergency Equipment > R2 DOOR WILL NOT DISARM. ADJUSTED R2 DOOR GIRT BAR FLOOR PLATES IAW CMM 52-42-22. OPS CHECKED GOOD. - [SDR R61A201801010013](https://openairdocs.org/sdr/R61A201801010013.md): Plate · damaged · Jan 1, 2018 · N130HQ · Emb ERJ170200LR · Emergency Equipment > L2 DOOR WON'T ARM. HANDLE SEEMS TO BE JAMMED. FOUND FWD GIRT BAR PLATE STOPPING THE ARMING OF THE L2 GIRT BAR. ADJUSTED, OPS CHECKED GOOD IAW AMM 52-12-40. - [SDR R61A201711050814](https://openairdocs.org/sdr/R61A201711050814.md): Closeout Panel · corroded · Nov 5, 2017 · N130HQ · Emb ERJ170200LR · Cargo/Baggage Doors > WHILE IN HEAVY MX CHECK - FWD CARGO DOOR LOWER CLOSE OUT PANEL HAS 2 AREAS OF CORROSION AS MARKED. REMOVE AND REPLACE LOWER CLOSE OUT PANEL. - [SDR R61A201711050813](https://openairdocs.org/sdr/R61A201711050813.md): Bracket · corroded · Nov 5, 2017 · N130HQ · Emb ERJ170200LR · Cargo/Baggage Doors > WHILE IN HEAVY MX CHECK - FWD CARGO DOOR FR 24+2" STR 26 BRACKET IS CORRODED AS MARKED. REMOVED AND INSTALLED NEW FWD CARGO DOOR FR 24+2" STR 26 BRACKET REF SRM 51-41-01, 51-23-06 PN 170-67176-403. - [SDR R61A201711050812](https://openairdocs.org/sdr/R61A201711050812.md): Seat Track · corroded · Nov 5, 2017 · N130HQ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings > WHILE IN HEAVY MX CHECK - CORROSION ON THE RT I/B SEAT TRACK FR23-34/43. PERFORMED SEAT TRACK SPLICE REPAIR ON RT INBD AT FR 28-29 REF SRM 53-00-10/REPAIR 01 AND PERFORMED PERMANENT REPAIR IN ACCORDANCE WITH ETD2017-170-088873. - [SDR R61A201711050811](https://openairdocs.org/sdr/R61A201711050811.md): Seat Track · corroded · Nov 5, 2017 · N130HQ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings > WHILE IN HEAVY MX CHECK - CORROSION ON LT SEAT TRACK BETWEEN FR 18 - 20, Z=490.0. REMOVED AND INSTALLED NEW LT FORWARD SEAT TRACK BETWEEN FR.20 REF SRM 51-42-01, 51-43-03 P/N 170-03264-001. - [SDR R61A201711050810](https://openairdocs.org/sdr/R61A201711050810.md): Seat Track · corroded · Nov 5, 2017 · N130HQ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings > WHILE IN HEAVY MX CHECK - CORROSION ON FITTING O/B OF THE LT SEAT TRACK AFT OF FR 16, Z=490.0. REMOVED AND INSTALLED FITTING OB OF LT SEAT TRACK AFT OF FR 16 REF SRM 51-42-01, 51-43-03 PART 170-05323-005. - [SDR R61A201711050809](https://openairdocs.org/sdr/R61A201711050809.md): Seat Track · corroded · Nov 5, 2017 · N130HQ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings > WHILE IN HEAVY CHECK - CORROSION ON FLOOR DOUBLER O/B OF THE LT SEAT TRACK AT FR 16, Z=490.0. BLENDED AREAS OF CORROSION ON FLOOR DOUBLER O/B OF THE LT SEAT TRACK AT FR 16 COMPLIED WITH PERMANENT REPAIR REF ETD2017-170-088175 REV I PN 170-12118-001. - [SDR R61A201711050808](https://openairdocs.org/sdr/R61A201711050808.md): Door Sill · corroded · Nov 5, 2017 · N130HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure > DURING HEAVY MX CHECK - CORROSION ON RT SILL PLATE BETWEEN FR 13 - 14 Z=490.0. REMOVED AND INSTALLED NEW SILL PLATE BETWEEN FR 13-14 Z=490.0. REF SRM 51-23-05, 51-23-06, 51-41-02 PN 170-05663-003. - [SDR R61A201706140412](https://openairdocs.org/sdr/R61A201706140412.md): Fitting · damaged · Jun 14, 2017 · N130HQ · Emb ERJ170200LR · Fuselage Main, Attach Fittings > CREW REPORTED THE R1 DOOR DIFFICULT TO DISARM AND MOVE SLIDE HANDLE UP. FOUND FWD GIRT BAR FLOOR FITTING SPRING TAB GROOVED AND WORN CAUSING GIRT BAR DIFFICULT TRAVEL ON DISARM AND JUMPING AND JOLTING OF THE GIRT BAR. R & R FWD GIRT BAR FLOOR FITTING ASSY AND - [SDR R61A201612150736](https://openairdocs.org/sdr/R61A201612150736.md): Door · dirty · Dec 15, 2016 · N130HQ · Emb ERJ170200LR · Service Doors > CREW REPORTED THAT THE R1 DOOR SLIDE WOULD NOT ARM. MAINTENANCE CLEANED DEBRIS FROM THE DOOR IAW AMM AND OPS CHECKED GOOD. - [SDR R61A201612050704](https://openairdocs.org/sdr/R61A201612050704.md): Lever · inoperative · Dec 5, 2016 · N130HQ · Emb ERJ170200LR · Landing Gear Selector > DURING FLIGHT, CREW REPORTED THAT THE GEAR LEVER WOULD NOT MOVE. DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT AND REMOVED AND REPLACED LANDING GEAR LEVER IAW AMM AND OPS CHECKED GOOD. - [SDR R61A201611250685](https://openairdocs.org/sdr/R61A201611250685.md): Indicator · out of position · Nov 25, 2016 · N130HQ · Emb ERJ170200LR · Emergency Equipment > CREW REPORTED THE L2 DOOR WOULD NOT ARM. MAINENANCE REPOSITIONED THE DOOR INDICATOR IAW AMM AND OPS CHECKED GOOD. - [SDR R61A201608120478](https://openairdocs.org/sdr/R61A201608120478.md): Flashlight · missing · Aug 12, 2016 · N130HQ · Emb ERJ170200LR · Emergency Equipment > CREW REPORTED THAT THE AFT FLIGHT ATTENDANT FLASHLIGHT WAS MISSING. MAINTENANCE REPLACED MISSING AFT FLIGHT ATTENDANT FLASHLIGHT IAW AMM AND OPS CHECKED GOOD. - [SDR R61A201605050321](https://openairdocs.org/sdr/R61A201605050321.md): Connector · disconnected · May 5, 2016 · N130HQ · Emb ERJ170200LR · Light System Wiring > CREW REPORTED THAT THE COCKPIT EMERGENCY FLOODLIGHT WAS NOT TESTING. MAINTENANCE FOUND FLOODLIGHT ASSY NOT CONNECTED. MAINTENANCE RECONNECTED FLOODLIGHT IAW AMM AND OPS CHECKED GOOD. - [SDR R61A201605010290](https://openairdocs.org/sdr/R61A201605010290.md): Slide · unwanted deploy · May 1, 2016 · N130HQ · Emb ERJ170200LR · Escape Slide > WHILE BEING CATERED, THE L2 DOOR SLIDE HUNG UP AND PARTIALLY UNRAVELED. ACFT WAS FLOWN VIA MAINTENANCE FERRY WHERE MAINTENANCE R & R L2 DOOR SLIDE IAW AMM AND OPS CHECKED GOOD. - [SDR R61A201604210274](https://openairdocs.org/sdr/R61A201604210274.md): Firewall · cracked · Apr 21, 2016 · N130HQ · Emb ERJ170200LR · APU Cowling/Containment > DURING HEAVY CHECK, APU FIRE WALL PANEL 351AZ LOWER RADIUS IS CRACKED. MX REPAIRED IAW SRM 170 53-31-21. - [SDR R61A201604210273](https://openairdocs.org/sdr/R61A201604210273.md): Firewall · cracked · Apr 21, 2016 · N130HQ · Emb ERJ170200LR · APU Cowling/Containment > DURING HEAVY CHECK, APU FIRE WALL PANEL 351AZ UPPER RADIUS IS CRACKED. MAINTENANCE FABRICATED AND INSTALLED DOUBLER AND FILLERS IAW ETD 2016-170-038970. - [SDR R61A201604210261](https://openairdocs.org/sdr/R61A201604210261.md): Screw · corroded · Apr 21, 2016 · N130HQ · Emb ERJ170200LR · Leading Edge Devices > DURING HEAVY CHECK, RT WING INBD SLAT SEAL HARDWARE IS CORRODED. MX R & R RT WING INBD SLAT SEAL HARDWARE IAW AMM 20-10-01. PN NAS1102-06-5 SCREW. - [SDR R61A201604210260](https://openairdocs.org/sdr/R61A201604210260.md): Firewall · cracked · Apr 21, 2016 · N130HQ · Emb ERJ170200LR · APU Cowling/Containment > DURING HEAVY CHECK, APU FIRE WALL PANEL 351AZ LOWER RADIUS IS CRACKED. MX TRIMMED OUT CRACKED AREA IAW SRM 53-31-21. - [SDR R61A201604160272](https://openairdocs.org/sdr/R61A201604160272.md): Spar · cracked · Apr 16, 2016 · N130HQ · Emb ERJ170200LR · Wing Spar > DURING HEAVY CHECK, LT SPAR 3 WING STUB FASTENER HOLE HAS CRACK LIKE INDICATIONS. MAINTENANCE REPAIRED LT SPAR 3 WING STUB FASTENER HOLE IAW ETD2016-170-037169. - [SDR R61A201604160250](https://openairdocs.org/sdr/R61A201604160250.md): Spar · cracked · Apr 16, 2016 · N130HQ · Emb ERJ170200LR · Wing Spar > DURING HEAVY CHECK, RT SPAR WING STUB FASTENER HOLE HAS CRACK LIKE INDICATIONS IN FASTENER HOLE. MAINTENANCE REPAIRED RT SPAR WING STUB FASTENER HOLE IAW ETD 2016-170-037169. - [SDR R61A201604150253](https://openairdocs.org/sdr/R61A201604150253.md): Intercostal · corroded · Apr 15, 2016 · N130HQ · Emb ERJ170200LR · Fuselage Miscellaneous Structure > DURING HEAVY CHECK, RT FRAME INTERCOSTAL BETWEEN FRAMES 17-18 IS CORRODED. R & R RT FRAME INTERCOSTAL BETWEEN FRAMES 17-18 IAW SRM 51-43-02, PN 170-07304-002 BEAM. - [SDR R61A201604130243](https://openairdocs.org/sdr/R61A201604130243.md): Battery Pack · discharged · Apr 13, 2016 · N130HQ · Emb ERJ170200LR · Emergency Equipment > DURING HEAVY CHECK, MAINTENANCE REPORTED THAT THE LT COCKPIT FLASHLIGHT WAS DISCHARGING RAPIDLY. MAINTENANCE R & R FLASHLIGHT BATTERIES IAW AMM AND OPS CHECKED GOOD. - [SDR R61A201604100251](https://openairdocs.org/sdr/R61A201604100251.md): Clamp · broken · Apr 10, 2016 · N130HQ · Emb ERJ170200LR · Waste Disposal System > DURING HEAVY CHECK, WASTE VACUUM SYS TUBE AFT CABIN SECOND CLAMP FROM TANK IS CORRODED AND BROKEN. MAINTENANCE R & R WASTE VACUUM SYSTEM TUBE AFT CABIN SECOND CLAMP FROM TANK IAW EI R170EI-38-32-0004, AMM 38-32-13, PN 19000-87, SLEEVE. - [SDR R61A201604090246](https://openairdocs.org/sdr/R61A201604090246.md): Rib · cracked · Apr 9, 2016 · N130HQ · Emb ERJ170200LR · Horizontal Stabilizer, Spar/Rib > DURING HEAVY CHECK, RT HORIZONTAL STABILIZER, RIB 11 IS CRACKED 5 RIVETS BACK FROM FORWARD SPAR TOP SKIN ATTACH POINT. MAINTENANCE REPAIRED RIB 11A IAW ETD 2016-170-034759 CUTOFF CRACKED FLANGE, FABRICATED AND INSTALLED NEW ONE. Next page: https://openairdocs.org/aircraft/N130HQ/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 = 'N130HQ' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N130HQ/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.