# N765NA: Hylio HYL-150 - Status: Sale reported - Airframe: [Hylio HYL-150](https://openairdocs.org/model/hylio-hyl-150) (registry code 06102IX) - Serial number: 17906110527 - Type: Rotorcraft - Engine type: Electric - Mode S code: AA5548 - Location: [Hannibal, MO](https://openairdocs.org/faa-place/MO/Hannibal) - Owner type: Individual - Owner's area on the map: 39.6899° N, 91.4663° W: Placed by OpenAirDocs at the center of ZIP code 63401, 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=765NA - Page: https://openairdocs.org/aircraft/N765NA 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 N765NA. ## FAA accident and incident reports None matched to N765NA. ## 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 N765NA not matched to an aircraft (65, newest 50) They name N765NA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR NOCA04311](https://openairdocs.org/sdr/NOCA04311), Apr 12, 2011: SUPPORT CHANNEL. CORRODED. FOUND CORROSION ON 3 LAV THRESHOLD SUPPORT CHANNELS. REMOVED CORROSION OUT OF LIMITS. REMOVED AND REPLACED SUPPORT CHANNELS AS PER MM 51-21-03. - [SDR NOCA20110112001](https://openairdocs.org/sdr/NOCA20110112001), Apr 12, 2011: ANGLE. CRACKED. SUPPORT CAP CRACKED LEFT WING L/E CAVITY LES 550.10. REMOVED LOWER CHORD P/N 114T2207-5 AND LOWER NUT PLATE ANGLE DRILLED UP NEW ANGLE AND PRIMED. INSTALLED NEW - [SDR NOCA03511](https://openairdocs.org/sdr/NOCA03511), Apr 1, 2011: ANGLE. CRACKED. ANGLE CRACKED NR 2 ENGINE SAILBOAT FAIRING A-FRAME. REPLACED CRACKED ANGLES AS PER SRM 51-10-02. - [SDR NOCA03411](https://openairdocs.org/sdr/NOCA03411), Apr 1, 2011: ANGLE. CRACKED. LEFT WING STA 550 NR 4 SLAT INBD OF INBD TRACK ANGLE CRACKED. REMOVED OLD ANGLE PER SRM 51-10-02. DRILLED UP NEW ANGLE AND INSTALLED AS PER SRM 51-20-05. - [SDR NOCA03211](https://openairdocs.org/sdr/NOCA03211), Mar 30, 2011: ANGLE. CRACKED. LT WING STA 500 UNDER SLAT NR 5 OUTBOARD SIDE OF OUTBOARDD TRACK ANGLE CRACKED. REMOVED AND DRILLED REPLACMENT ANGLE AS PER SRM 51-10-22. - [SDR NOCA03111](https://openairdocs.org/sdr/NOCA03111), Mar 30, 2011: RIB. CRACKED. AFT END OF L/E RIB CRACKED LES 662 AFT OF NR 9 SLAT. REMOVED ANGLE DRILLED AND INSTALLED RIB ANGLE AS PER SRM 51-10-02. - [SDR NOCA03011](https://openairdocs.org/sdr/NOCA03011), Mar 30, 2011: CROSSMEMBER. CORRODED. CORROSION AT KEEL BEAM CROSS MEMBER. REMOVED CORROSION AT KEEL BEAM CROSS MEMBER 2 TEES OUT OF LIMITS. REMOVED AND REPLACED KEEL BEAM CROSS MEMBERS AS PER SRM 5 - [SDR NOCA02611](https://openairdocs.org/sdr/NOCA02611), Mar 14, 2011: SLIDE. LOW PRESSURE. R4 DOOR SLIDE PRESSURE AT EXTREME LOW END OF NORMAL OPERATIONAL RANGE. REMOVED AND REPLACED R4 DOOR SLIDE AS PER NAA JOB CARD 767-25-029-01. - [SDR NOCA01311](https://openairdocs.org/sdr/NOCA01311), Feb 20, 2011: DOOR FRAME. DAMAGED. FUSELAGE DAMAGED BY GROUND EQUIPMENT APPROXIMANT 3FT AFT OF L4 DOOR FRAME OUT OF SRM LIMITS. REMOVED DAMAGE AREA AS PER SRM 53-00-01. ACCOMPLISHED HFEC TO ENSUR - [SDR NOCA06410](https://openairdocs.org/sdr/NOCA06410), Sep 23, 2010: LIGHT. INOPERATIVE. EMERGENCY LIGHTS INOP AT ROW 14B. REPLACED EMERGENCY LIGHT STRIPS AT 14B, OPS CHECK GOOD. - [SDR NOCA06310](https://openairdocs.org/sdr/NOCA06310), Sep 18, 2010: CONNECTOR. DIRTY. RIGHT ENG FIRE LP 1 STATUS MSG. CLEANED WAFER CONNECTORS AT M683 RIGHT ENGINE FIRE DETECTION CARD, T/S PER FIM 26-11-00 FIG 104 ALL LOOPS RESISTANCE & INSULATIO - [SDR NOCA05610](https://openairdocs.org/sdr/NOCA05610), Jul 26, 2010: LIGHT. INOPERATIVE. L-3 DOOR EMERGENCY LIGHT INOP. RELAMPED AND TESTED L-3 DOOR EXTERIOR EMERGENCY LIGHT PER MM 33-51-00. - [SDR NOCA05510](https://openairdocs.org/sdr/NOCA05510), Jul 18, 2010: O-RING. LEAKING. ACFT DIVERTED, DUE TO NR 1 ENGINE IDG ON MEL INOP AND APU AUTO SHUTDOWN IN FLIGHT DUE TO LOW OIL. APU OIL LEAK FOUND ON ITEM1, LOGPAGE 86747, DUE TO FAULTY O-RI - [SDR NOCA05410](https://openairdocs.org/sdr/NOCA05410), Jul 10, 2010: SEAL. LEAKING. A/C 765 FLT 404 EN ROUTE TO FRU OUT OF LEJ, FLT CREW ADVISED THE APU OIL QUANTITY IS DECREASING AND EXPECT THE APU TO SHUT DOWN SHORTLY. WITH THE LEFT GENERATOR - [SDR NOCA05310](https://openairdocs.org/sdr/NOCA05310), Jul 9, 2010: GENERATOR. MALFUNCTIONED. A/C N765 EN ROUTE RMS TO FRU ADVISED MCC THE LEFT GENERATOR DRIVE LIGHT CAME ON. FLT CREW PERFORMED QRH PROCEDURES GENERATOR DRIVE LIGHT STAYED ON. NOTE: THE AP - [SDR NOCA03810](https://openairdocs.org/sdr/NOCA03810), May 8, 2010: FIRE LOOP. INOPERATIVE. LEFT ENG / FIRE LOOP 2 STATUS MSG SEVERAL TIMES DURING FLT. PLACARD PER MEL 26-11-1 CAT C NOTE. A/C DOWNGRADED TO 120 ETOPS DUE TO LEFT ENG FIRE LOOP 2 INOP CI - [SDR NOCA02310](https://openairdocs.org/sdr/NOCA02310), Mar 1, 2010: COMPUTER. MALFUNCTIONED. AILERON LOCKOUT EICAS MSG. ACCOMPLISHED FIM TASK 27-11-00 FIG 104. ACCOMPLISHED BITE CHECKS, ALL CHECKS OK. REF AMM 22-00-02, MCDP TST 07 ACCOMPLISHED, NO FAULT - [SDR NOCA04009](https://openairdocs.org/sdr/NOCA04009), Jun 30, 2009: LAMP. BURNED OUT. THE AIRCRAFT HAS A MISSED APPROACH / GO-AROUND ON APPROACH INTO BGR MX REP WAS CALLED TO THE FLIGHT DECK PER CAPTAINS REQUEST. MX REP RE-LAMPED THE INOP LIGHT, - [SDR NOCA02909](https://openairdocs.org/sdr/NOCA02909), May 17, 2009: LIGHT. INOPERATIVE. EMERGENCY FLOOR LIGHT STRIP (RT SIDE FWD) NEEDS TO BE RELAMPED. RELAMPED EMERGENCY FLOOR PATH STRIP IAW MM 33-51-10-402-113. OPS CHECK OK. - [SDR NOCA02709](https://openairdocs.org/sdr/NOCA02709), May 7, 2009: PCA. FAILED. RUDDERS LOCKED ON LANDING. TILLER NOSE WHEEL STEERING OK. ACCOMPLISHED ON PL 765-0905-03, PERFORMED FIM TASK 27-21-00 FIG 107. REMOVED ACCESS PANEL 324BL, 324EL - [SDR NOCA08408](https://openairdocs.org/sdr/NOCA08408), Nov 28, 2008: FLASHLIGHT. INOPERATIVE. RT OVERWING EMERGENCY EXIT F/A FLASHLIGHT STATUS LIGHT NOT BLINKING. REMOVED AND REPLACED RT OVERWING EMERGENCY EXIT F/A EMERGENCY FLASHLIGHT IAW AMM 25-64-00. - [SDR NOCA15007](https://openairdocs.org/sdr/NOCA15007), Aug 27, 2007: DETECTOR. UNKNOWN. FWD CARGO DET 1 ON STATUS PAGE ACTION T/S SYSTEM PER FIM 26-16-00 FIG 104 &108. FOUND FWD CARGO DET M324 AT FAULT. REMOVED & REPLACED PER MM 26-16-01, OPS CHECK - [SDR NOCA14707](https://openairdocs.org/sdr/NOCA14707), Aug 4, 2007: PROXIMITY SWITCH. FAULTY. ON TAKEOFF ROLL BELOW 80 KTS HAD A L1 DOOR FWD ENTRY DOOR OPEN EICAS MESSAGE A/C REJECTED TAKEOFF AT 65 KTS. ACTION DEFERRED PER MEL 52-71-1, A/C INSPECTED OK F - [SDR NOCA11007](https://openairdocs.org/sdr/NOCA11007), Jun 17, 2007: FRAME. CORRODED. FAIL SAFE STRAP ON FRAME AT STA 1346 HAS CORROSION AT FLOOR LINE BEYOND SRM LIMITS. REPAIRED FAIL SAFE STRAP CORROSION AT STA 1346 PER MRB 767-2986. - [SDR NOCA11207](https://openairdocs.org/sdr/NOCA11207), Jun 17, 2007: FLOORBEAM. CORRODED. FLOORBEAM AT STA 325 LBL 27 HAS CORROSION BEYOND SRM LIMITS. REPAIRED FLOORBEAM PER MRB CMRB-014. - [SDR NOCA12307](https://openairdocs.org/sdr/NOCA12307), Jun 17, 2007: STIFFENER. BENT. BULKHEAD STIFFENER / FLOORBEAM SUPPORT IS BENT STA 1480 LEFT LBL 24. REPLACED STIFFENER PER SRM 51-10-02. - [SDR NOCA11707](https://openairdocs.org/sdr/NOCA11707), Jun 17, 2007: STIFFENER. BENT. BULKHEAD STIFFENER / FLOORBEAM SUPPORT IS BENT AT STA 1480 LEFT BL16. REMOVED AND REPLACED STIFFENER PER SRM 51-10-02. - [SDR NOCA11407](https://openairdocs.org/sdr/NOCA11407), Jun 17, 2007: SEAT TRACK. CORRODED. SEAT TRACK CORROSION BEYOND SRM LIMITS NUMEROUS LOCATIONS 962 - 1095. REMOVED AND REPLACED SEAT TRACK AS PER SRM 53-00-52. - [SDR NOCA11307](https://openairdocs.org/sdr/NOCA11307), Jun 17, 2007: SEAT TRACK. CORRODED. CORROSION ON SEAT TRACK OUT OF SRM LIMITS AT NUMEROUS LOCATIONS FROM STA 960 - 1085. REMOVED AND REPLACED SEAT TRACK AS PER MM 53-00-52. - [SDR NOCA11607](https://openairdocs.org/sdr/NOCA11607), Jun 17, 2007: STIFFENER. BENT. BULKHEAD STIFFENER / FLOORBEAM SUPPORT IS BENT AT STA 1461. REPLACED STIFFENER AS PER SRM 51-10-02. - [SDR NOCA12107](https://openairdocs.org/sdr/NOCA12107), Jun 17, 2007: FRAME. CORRODED. AREA OF CORROSION OUTBOARD FWD SIDE OF FRAME 22 INCHES ABOVE FLOOR STA 1307. REPLACED BELLFRAME PER SRM 51-10-02. - [SDR NOCA12707](https://openairdocs.org/sdr/NOCA12707), Jun 17, 2007: STRINGER CLIP. CORRODED. STRINGER CLIP AT STA 1324 HAS CORROSION. REPLACED STRINGER CLIP PER SRM 51-10-02. - [SDR NOCA12807](https://openairdocs.org/sdr/NOCA12807), Jun 17, 2007: MOUNT. CORRODED. AFT INBOARD GALLEY FLOOR MOUNT CORRODED. REPLACED GALLEY FLOOR MOUNT PER SRM 53-11-54. - [SDR NOCA13007](https://openairdocs.org/sdr/NOCA13007), Jun 17, 2007: RIB. CRACKED. RIB CRACKED AFT OF NR 6 SLAT AT REAR SPAR. REPLACED RIB SEALED AND PAINTED AS PER 57-11-00-1. - [SDR NOCA12907](https://openairdocs.org/sdr/NOCA12907), Jun 17, 2007: RIB. CRACKED. FIXED L/E RIB CRACKED AT REAR SPAR. REPLACED AIR LOAD RIB AND SUPPORT CLIP PER SRM 51-10-02. - [SDR NOCA11507](https://openairdocs.org/sdr/NOCA11507), Jun 17, 2007: STIFFENER. BENT. BULKHEAD STIFFENER / FLOORBEAM SUPPORT IS BENT STA 1461 LEFT BL 24. REMOVED AND REPLACED STIFFENER AS PER SRM 51-10-02. - [SDR NOCA12507](https://openairdocs.org/sdr/NOCA12507), Jun 17, 2007: FLOORBEAM. CRACKED. BULK CARGO FLOORBEAM ATTACH POINT CRACKED STA1417. REPLACED FLOORBEAM ATTACH POINT AS PER SRM 51-10-02. - [SDR NOCA11807](https://openairdocs.org/sdr/NOCA11807), Jun 17, 2007: STIFFENER. CORRODED. CORROSION ON BELLFRAME J STIFFENER. REPLACED BELLFRAME J STIFFENER PER SRM 51-10-02. - [SDR NOCA12607](https://openairdocs.org/sdr/NOCA12607), Jun 17, 2007: BRACKET. CORRODED. ANGLE BRACKET HAS CORROSION STA 1330. REPLACED ANGLE BRACKET PER SRM 51-10-02. - [SDR NOCA11107](https://openairdocs.org/sdr/NOCA11107), Jun 17, 2007: STRINGER. CORRODED. CORROSION ON STRINGER 19R AT STA 1325. REMOVED CORROSION AND REPAIRED STRINGER PER MRB CMRB-015. - [SDR NOCA11907](https://openairdocs.org/sdr/NOCA11907), Jun 17, 2007: STIFFENER. CRACKED. BULKHEAD STIFFENER / FLOORBEAM SUPPORT IS CRACKED AT STA 1439 LEFT BL 16. REMOVED AND REPLACED STIFFENER AS PER SRM 51-10-02. - [SDR NOCA12407](https://openairdocs.org/sdr/NOCA12407), Jun 17, 2007: FLOORBEAM. CRACKED. BULK CARGO FLOORBEAM ATTACH POINT CRACKED STA 1417 LEFT BL 10. REPLACED FLOORBEAM ATTACH POINT PER SRM 51-10-02. - [SDR NOCA12207](https://openairdocs.org/sdr/NOCA12207), Jun 17, 2007: BRACE. CORRODED. CORROSION ON ANGLE BRACE STA 1329. REPLACED ANGLE BRACE PER SRM 53-60-07. - [SDR NOCA08107](https://openairdocs.org/sdr/NOCA08107), Apr 9, 2007: FIRE LOOP. MALFUNCTIONED. RIGHT ENGINE FIRE LOOP 1 STATUS MESSAGE ANNUNICATED IN FLIGHT. TROUBLESHOT REMOVED AND REPLACED NR 2 ENGINE FIRE LOOP 1 LOWER AFT OUTBOARD AS PER AMM 26-11-02. - [SDR NOCA07907](https://openairdocs.org/sdr/NOCA07907), Apr 6, 2007: EXCITER. FAILED. DURING RT ENG START NO LIGHT OFF RT ENG IGNITOR 2 EICAS. REMOVED AND REPLACED NR 2 EXCITER BOX, ALSO REMOVED AND REPLACED NR 1 AND 2 IGNITOR PLUGS P/N CH31772A - [SDR NOCA07607](https://openairdocs.org/sdr/NOCA07607), Mar 28, 2007: RELAY. FAILED. LEFT ENG FUEL VALVE EICAS/COCKPIT LIGHT IND AFTER PUTTING LEFT FUEL CONTROL SWITCH TO RUN. REPLACED LEFT ENG IGN CONT RELAY(K1251). ALL OPS NORMAL. - [SDR NOCA07507](https://openairdocs.org/sdr/NOCA07507), Mar 28, 2007: RELAY. FAILED. LEFT ENGINE FAILS TO START. TROUBLESHOT PER FIM 76-11-00 FIG 108. REPLACED LEFT ENG FUEL/IGN CONTROL RELAY (K1251) PER WDM 76-11-11. OPERATED LEFT ENG PER MM 71 - [SDR NOCA06807](https://openairdocs.org/sdr/NOCA06807), Mar 14, 2007: LIGHT. INOPERATIVE. EMERGENCY EXIT LIGHT IN COCKPIT ABOVE DOOR INOP. RELAMPED, OPS CHECKS OK. - [SDR NOCA06407](https://openairdocs.org/sdr/NOCA06407), Mar 14, 2007: RECEIVER. MALFUNCTIONED. RIGHT GPS EICAS MSG ILLUMINATED IN FLIGHT. REPLACED RIGHT MMR PER MM 34-3101, OPS CHECK OK. - [SDR NOCA06207](https://openairdocs.org/sdr/NOCA06207), Mar 14, 2007: SENSOR. OUT OF ADJUST. LEFT FWD ENTRY DOOR EICAS MESSAGE. ADJUSTED S194 SENSOR PER MM 52-71-00, TEST OK. All 65: https://openairdocs.org/aircraft/N765NA/unmatched-reports.md ## 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.