# N622VA: Vector HD 580 - Status: Valid registration - Airframe: [Vector HD 580](https://openairdocs.org/model/vector-hd-580) (registry code 06102LZ) - Serial number: 5358C73E - Type: Rotorcraft - Engine type: Electric - Certificate issued: July 17, 2026 - Expires: July 31, 2033 - Mode S code: A81F87 - Registered owner: [Horizon Ag Application Inc](https://openairdocs.org/faa-owner/HORIZON%20AG%20APPLICATION%20INC) - Location: [Milford, IL](https://openairdocs.org/faa-place/IL/Milford) - Owner type: Corporation - Owner's area on the map: 40.6290° N, 87.6902° W: Placed by OpenAirDocs at the center of ZIP code 60953, within about 7 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=622VA - Page: https://openairdocs.org/aircraft/N622VA From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. ## ADs that may apply (OpenAirDocs): 0 in force ### Matched by airframe (Vector HD 580) None in force. ## Information bulletins (advisory) None matched. ## NTSB investigations None matched to N622VA. ## FAA accident and incident reports None matched to N622VA. ## Service difficulty reports None filed for this aircraft. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. ## Service difficulty reports on N622VA not matched to an aircraft (19) They name N622VA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR ASAA2020112533619](https://openairdocs.org/sdr/ASAA2020112533619), Nov 25, 2020: FLOORBOARD. DELAMINATED. MAIN CABIN FLOOR PANEL 242KF DELAMINATED AROUND MOUNT POINT. GROUNDED-YES. FABRICATED NEW MAIN CABIN FLOOR PANEL 242KF, IAW A320 SRM 53-02-283-001 & MCG IRM 970 - [SDR ASAA2020110533528](https://openairdocs.org/sdr/ASAA2020110533528), Nov 5, 2020: SKIN. DENTED. DENT OBSERVED FORWARD OF THE POTABLE WATER SERVICE DOOR. GROUNDED-YES. REPAIRED DENTED AREA WITH DOUBLER BETWEEN FR 64 AND FR 65 AND STR 36L AND STR 39L, REF A3 - [SDR ASAA2020110133529](https://openairdocs.org/sdr/ASAA2020110133529), Nov 1, 2020: SKIN. DENTED. LT INBOARD FLAP DENTED 24 INCHES FROM INBOARD AND .5 INCHES FROM TRAILING EDGE. GROUNDED-YES. REPAIRED DENT ON LT INBOARD FLAP UPPER SURFACE 24 IN FROM INBOARRD - [SDR ASAA2019081430533](https://openairdocs.org/sdr/ASAA2019081430533), Aug 14, 2019: SUPPORT WEB. CORRODED. AFT CABIN RT UNDER LAV LATERAL SHEAR PLATE, SUPPORT WEB CORRODED GROUNDED - YES. REMOVED AND REPLACED SUPPORT WEB IAW SRM 51-42-11 AND DWG D53474180. NOTE: NO A - [SDR ASAA2019081330542](https://openairdocs.org/sdr/ASAA2019081330542), Aug 13, 2019: SHEAR PLATE. CORRODED. AFT CABIN RT LAV, LATERAL SHEAR PLATE HAS CORROSION ON THE WEB GROUNDED - YES. REMOVED AND REINSTALLED MOTOR STARTER RELAY IAW AMM 38-31-36 & ESPM 20-33-11, OPS - [SDR ASAA2018112427159](https://openairdocs.org/sdr/ASAA2018112427159), Nov 24, 2018: SKIN. DENTED. LOWER LT SKIN IS DENTED AT FR61 TO FR62 S36L GROUNDED - YES. ACCOMPLISHED REPAIR TO 2 EA DENTED AREAS BETWEEN FR61 TO FR62 STR 35L TO 37L PER SRM 53-00-11-300-0 - [SDR ASAA2018091826155](https://openairdocs.org/sdr/ASAA2018091826155), Sep 13, 2018: WIRE. DETACHED. EMER ROW LIGHTS INOP AT ROWS 22 & 23. GROUNDED - YES. REATTACHED WIRES IN CONNECTOR PER AMM AWM 33-51-07 P 0249, SHT 2. OPS CHECK GOOD. - [SDR VQI2017F00014](https://openairdocs.org/sdr/VQI2017F00014), Mar 25, 2017: BUSHING. WORN. MX FOUND THE R1 DOOR GUST LOCK STICKING DUE TO WORN BUSHINGS. MX REPLACED THE BUSHINGS IAW AMM 52-11-12 AND TBN 52-10-01. OPS CHECKED GOOD. - [SDR VQIA2016011200004](https://openairdocs.org/sdr/VQIA2016011200004), Jan 31, 2016: PROXIMITY SENSOR. FAILED. AIRPLANE WAS RELEASED FROM HEAVY MAINTENANCE. THE ACFT THEN TOOKOFF, AFTER TAKEOFF, THE CREW ATTEMPTED TO RETRACT THE GEARS AND RECEIVED, DOORS UNLOCKED MESSAGE - [SDR VQI2015F00009](https://openairdocs.org/sdr/VQI2015F00009), Mar 11, 2015: SLIDE. LOW PRESSURE. R2 DOOR SLIDE PRESSURE GUAGE WAS FOUND IN THE RED BAND DURING PREFLIGHT CHECKS BY INFLIGHT TEAM. MAINTENANCE WAS SENT WITH SERVICEABLE SLIDE AND SLIDE WAS REPLA - [SDR VQI2014F00035](https://openairdocs.org/sdr/VQI2014F00035), Nov 17, 2014: HOSE. LEAKING. DURING APPROACH, REPORTED LOSS OF GREEN SYSTEM HYDRAULIC FLUID. MAINTENANCE DISCOVERED A MLG DOOR ACTUATOR HOSE ON THE LT SIDE LEAKING. R & R IAW AMM 32-31-39-4 - [SDR VQIA2013112200033](https://openairdocs.org/sdr/VQIA2013112200033), Oct 24, 2013: FAN. FAILED. PLASTIC BURNING ODOR DETECTED IN COCKPIT WITH AMBER FAN ANNUNCIATED ON THE COND PAGE. MX ACCOMPLISHED TSM 24-00-00810-823A FOR BURNING ODOR WITH NO DEFECTS FOUN - [SDR VQI2012F00009](https://openairdocs.org/sdr/VQI2012F00009), Apr 19, 2012: SWITCH. DEFECTIVE. ACFT WAS ON A TURN, AFTER FLIGHT. DURING THE PREFLIGHT, THE FLIGHT CREW NOTED THAT THE EMERGENCY EXIT LIGHTS STAYED ILLUMINATED WITH THE SWITCH IN THE "ARMED" P - [SDR VQI2011F00027](https://openairdocs.org/sdr/VQI2011F00027), Dec 5, 2011: PIN. UNSERVICEABLE. UPON ARRIVAL, A LOG ENTRY WAS MADE NOTING THAT THE L2 DOOR INDICATED DISARMED ON THE LOWER ECAM PAGE DURING CRUISE FLIGHT. THIS WAS AREPEAT ITEM BEING MONITORED - [SDR VQI2011F00031](https://openairdocs.org/sdr/VQI2011F00031), Nov 17, 2011: FLOOR SUPPORT. CORRODED. REMOVED CORROSION AT CABIN FLOOR PANEL SUPPORT UPPER SURFACE BETWEEN FRAMES 68-70, RBL 6" IAW SRM 51-74-00. PERFORMED UT THICKNESS INSP OF REWORKED AREA, FOUND - [SDR VQI2011F00030](https://openairdocs.org/sdr/VQI2011F00030), Nov 11, 2011: FLOOR SUPPORT. CORRODED. REMOVED CORROSION AT MAIN CABIN FLOOR SUPPORT UPPER SURFACE BETWEEN FR 67 TO 68, LBL 46" REF SRM 51-74-00. ACCOMPLISHED A UT THICKNESS INSP AFTER REWORK MAX 0, - [SDR VQI2011F00028](https://openairdocs.org/sdr/VQI2011F00028), Nov 8, 2011: FLOOR SUPPORT. CORRODED. REMOVED CORROSION AT CABIN FLOOR SUPPORT UPPER SURFACE BETWEEN FR 68 AND 69, LBL 66. FOURN OUT OF LIMITS IAW SRM 53-00-14. R & R FLOORBEAM SUPPORT IAW SRM 53-00 - [SDR VQI2011F00029](https://openairdocs.org/sdr/VQI2011F00029), Oct 31, 2011: FLOOR PANEL. CORRODED. CABIN FLOOR PANEL 262FF HAS CORROSION SPOTS NEAR R-2 DOOR ENTRANCE AND AROUND FWD GIRT BAR LATCH. (REMOVED CORROSION, ACCOMPLISHED AUT THICKNESS. FOUND OUT OF L - [SDR VQI2009F00002](https://openairdocs.org/sdr/VQI2009F00002), Oct 22, 2009: COMPUTER. MALFUNCTIONED. FLIGHT DEPARTED 3 MINUTES EARLY AT 0422Z, WITH T/O AT 0433Z. ALSO AT 0433Z THE ACFT REPORTED ELAC 1 AND 2 AILERON ORDER DISAGREE THRU EFCS 1 AND 2 AS FAILURE ME ## STCs that may be installed (OpenAirDocs) None matched to this aircraft's models. ## Related - Other Vector HD 580 aircraft: https://openairdocs.org/model/vector-hd-580/aircraft.md --- 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.