# N762NA: Hylio HYL-150 - Status: Valid registration - Airframe: [Hylio HYL-150](https://openairdocs.org/model/hylio-hyl-150) (registry code 06102IX) - Serial number: 17906110536 - Type: Rotorcraft - Engine type: Electric - Certificate issued: January 8, 2026 - Expires: January 31, 2033 - Mode S code: AA4A23 - Registered owner: [Hylio Inc](https://openairdocs.org/faa-owner/HYLIO%20INC) - Location: [Richmond, TX](https://openairdocs.org/faa-place/TX/Richmond) - Owner type: Corporation - Owner's area on the map: 29.4914° N, 95.7021° W: Placed by OpenAirDocs at the center of ZIP code 77469, within about 6 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=762NA - Page: https://openairdocs.org/aircraft/N762NA 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 (Hylio HYL-150) None in force. ## Information bulletins (advisory) None matched. ## NTSB investigations None matched to N762NA. ## FAA accident and incident reports None matched to N762NA. ## 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 N762NA not matched to an aircraft (21) They name N762NA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR NOCA00113](https://openairdocs.org/sdr/NOCA00113), Nov 29, 2012: BALLAST. FAULTY. EMERGENCY PATH LIGHTING INOP. RECONNECTED CONNECTORS AND REPLACED BALLAST. - [SDR NOCA09712](https://openairdocs.org/sdr/NOCA09712), Aug 17, 2012: CABLE. INOPERATIVE. PASSENGER CABIN ESCAPE PATH LIGHTING AT LEFT O/B DOES NOT ILLUMINATE IN SECTION BETWEEN SEATS 1 AND 8. REMOVED AND REPLACED TWO EACH LAMP ASSY AND CABLE SECTION - [SDR NOCA09612](https://openairdocs.org/sdr/NOCA09612), Aug 14, 2012: FLASHLIGHT. INOPERATIVE. MID CABIN LC EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED LC EMERGENCY LIGHT AND BATTERY PER MM 25-64-00, OPS CHECK NORMAL. - [SDR NOCA05912](https://openairdocs.org/sdr/NOCA05912), Jul 7, 2012: BATTERY PACK. DISCHARGED. CAPT'S AND F/O'S DETACHABLE EMERGENCY FLASHLIGHT BATTERY CHARGER INDICATOR LIGHT NOT FLASHING. REMOVED AND REPLACED FLASHLIGHT BATTERY PACK, OPS CHECK NORMAL RE - [SDR NOCA04412](https://openairdocs.org/sdr/NOCA04412), Jun 5, 2012: CONTROLLER. INOPERATIVE. AIRCRAFT HAD A 2ND AIR TURNBACK FOR THE HPSOV EICAS MSG REF SDR NOCA04212 EICAS MSG RIGHT ENGINE HPSOV DISPLAYED RIGHT ENG BLEED ILLUMINATED STEADY AT CRUISE TH - [SDR NOCA04212](https://openairdocs.org/sdr/NOCA04212), Jun 3, 2012: SHUTOFF VALVE. INOPERATIVE. A/C HAD AN AIR-TURNBACK DUE TO RIGHT ENGINE 'HPRSOV' EICAS MSG ON AND OFF FOR 4 TIMES THEN STAYED WITH LIGHT ON. PLACED ON MEL 36-11-02-01. REMOVED AND REPLACED - [SDR NOCA04112](https://openairdocs.org/sdr/NOCA04112), May 23, 2012: BRAKE ASSY. DAMAGED. ON WALK AROUND FOUND NR 7 BRAKE DAMAGED. REMOVED AND REPLACED NR 7 BRAKE PER MM 32-41-08. OPS CHECK AND LEAK CHECK OK. - [SDR NOCA201205024012](https://openairdocs.org/sdr/NOCA201205024012), May 2, 2012: BATTERY. DISCHARGED. F/A FLASHLIGHT IS INOP AT DOOR L1 FWD POSITION. REMOVED AND REPLACED BATTERY. - [SDR NOCA03612](https://openairdocs.org/sdr/NOCA03612), Apr 20, 2012: FLASHLIGHT. INOPERATIVE. EMERGENCY FLASHLIGHT INOP AT THE L1 F/A JUMPSEAT. REMOVED AND REPLACED EMERGENCY FLASHLIGHT AT L1 F/A JUMPSEAT PER IPC 25-64-50. - [SDR NOCA2012042003512](https://openairdocs.org/sdr/NOCA2012042003512), Apr 20, 2012: LIGHT. INOPERATIVE. E-PATH LIGHT LEFT SIDE AFT GALLEY INOP. REMOVED AND REPLACED E-PATH LIGHT ASSY PER MM 33-51-10, OPS CHECK GOOD. - [SDR NOCA2012010300112](https://openairdocs.org/sdr/NOCA2012010300112), Jan 3, 2012: INSULATOR. DAMAGED. F/D FLAG IN VIEW AND NO COMMAND BARS ON F/O ADI. INDICATION NORM WITH INSTR SOURCE SELECTOR SWITCH "C" INTERMITTENT, BURNT SMELL IN COCKPIT AFTER THIS FAULT. NO - [SDR NOCA20121229611](https://openairdocs.org/sdr/NOCA20121229611), Dec 29, 2011: LIGHT. INOPERATIVE. RIGHT SIDE EMERGENCY LIGHT INOPERATIVE, BETWEEN SEAT 10GH-13GH. REPLACED LIGHT PER AMM 33-51-10. - [SDR NOCA12411](https://openairdocs.org/sdr/NOCA12411), Dec 28, 2011: FIRE BOTTLE. DISCHARGED. DURING TROUBLESHOOTING APU FIRE BOTTLE DISCHARGED. REASON FOR DISCHARGE UNKNOWN. ASSIGNED CI 26-06. REMOVED AND REPLACED APU FIRE BOTTLE PER TASK 26-22-02 TEST - [SDR NOCA11511](https://openairdocs.org/sdr/NOCA11511), Dec 9, 2011: UNKNOWN. UNKNOWN. AIRCRAFT HAD AN AIR TURNBACK DUE TO UNCOMMANDED RAPID LEFT RIGHT YAW MOVEMENT FOR APPROX 3 SEC NO EICAS OR WARNING LIGHTS OR INDICATIONS ON STATUS PAGE NOTICED - [SDR NOCA11111](https://openairdocs.org/sdr/NOCA11111), Nov 5, 2011: PCA. MALFUNCTIONED. A/C REQUIRES 4 1/2 LEFT RUDDER TRIM FOR STRAIGHT AND LEVEL FLT WITH CONTROL WHEEL AT 0 IN CRUISE AT FL 340 MACH .80. REPLACED ALL 3 RUDDER POWER CONTROL ACTUATO - [SDR NOCA20111011411](https://openairdocs.org/sdr/NOCA20111011411), Oct 11, 2011: YAW DAMPER. DAMAGED. FIVE UNITS RUDDER TRIM REQUIRED IN NOSE LEFT DIRECTION WHILE IN CRUISE AT FL370 OAT -52 AND LEFT CROSSWIND OF 75 KTS. DURING THIRD ENCOUNTER WITH LIGHT TURBULEN - [SDR NOCA10211](https://openairdocs.org/sdr/NOCA10211), Oct 9, 2011: FRAME. DAMAGED. STA 1702 FRAME AND PLATFORM DAMAGED AFT OF SECTION 48 ENTERY DOOR - DAMAGED RIGHT AFT. REMOVED DAMAGED PLATFORM AND CUT OUT DAMAGE SECTION OF WEB DAMAGE ON UPPE - [SDR NOCA09111](https://openairdocs.org/sdr/NOCA09111), Sep 18, 2011: CONNECTOR. LOOSE. A/C HAD AN AIR TURNBACK TO LEJ DUE TO NR 1 ENGINE EGT OVERTEMP DURING CLIMBOUT EGT PEAKED AT 1071. VISUALLY INSPECTED THERMAL COUPLES WIRING AND JUCTION BOX FOU - [SDR NOCA08211](https://openairdocs.org/sdr/NOCA08211), Aug 25, 2011: ACTUATOR. INOPERATIVE. UNCOMMANDED LEFT AILERON INPUT. REQUIRED 4-5 LEFT RUDDER TRIM TO COMPENSATE. DISTINCT DUTCH ROLL TENDENCY FELT IN CPT AND AFT CABIN. AIR SPEED FLUCTUATES (+-) . - [SDR NOCA08011](https://openairdocs.org/sdr/NOCA08011), Aug 24, 2011: LIGHT. INOPERATIVE. THREE EXTERIOR EMERGENCY LIGHTS DO NOT OPERATE RIGHT SIDE FWD OF AFT CARGO DOOR, LEFT SIDE OVER HYD ADP AND LEFT FWD MAIN ENTRY DOOR. REPLACED LIGHTS AND CHARGE - [SDR NOCA07911](https://openairdocs.org/sdr/NOCA07911), Aug 14, 2011: BATTERY. DISCHARGED. EMERGENCY LIGHTS INOP ROW 15 A, B. REPLACED BATTERY PACK AT ROW 15 A, B AS PER MM 33-51-07 OPS CHECK GOOD. ## STCs that may be installed (OpenAirDocs) None matched to this aircraft's models. ## Related - Other Hylio HYL-150 aircraft: https://openairdocs.org/model/hylio-hyl-150/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.