# N756NA: Hylio HYL-150

- Status: Registration pending
- Airframe: [Hylio HYL-150](https://openairdocs.org/model/hylio-hyl-150) (registry code 06102IX)
- Serial number: 17906110554
- Type: Rotorcraft
- Engine type: Electric
- Mode S code: AA3180
- Location: [Frederick, OK](https://openairdocs.org/faa-place/OK/Frederick)
- Owner type: Individual
- Owner's area on the map: 34.3980° N, 98.9359° W: Placed by OpenAirDocs at the center of ZIP code 73542, within about 10 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=756NA
- Page: https://openairdocs.org/aircraft/N756NA

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 N756NA.

## FAA accident and incident reports

None matched to N756NA.

## Reports on N756NA not matched to an aircraft (1)

They name N756NA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 20080809849659I](https://openairdocs.org/incident/20080809849659I), Aug 9, 2008: Boeing 75728A (N756NA), Fort Lauderdal, FL, No damage, 1 fatal. (-23) Turbulence encountered during descent into fort Lauderdale airport. Three flight attendants treated at a local hospital and released. Two passengers…

## 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 N756NA not matched to an aircraft (63, newest 50)

They name N756NA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR NOCA02309](https://openairdocs.org/sdr/NOCA02309), Apr 17, 2009: SLIDE. UNSERVICEABLE. FOUND L4 DOOR SLIDE PRESSURE INDICATION NEEDLE IN RED ZONE. REMOVED AND REPLACED L4 DOOR SLIDE AS PER AMM 25-66-01.
- [SDR NOCA02209](https://openairdocs.org/sdr/NOCA02209), Apr 16, 2009: LIGHT. INOPERATIVE. FLOOR PATH EMERGENCY LIGHTS INOP BETWEEN ROWS 10 - 15. REMOVED AND REPLACED FOUR EMERGENCY LIGHT ASSY'S FOR THE FLOOR PATH EMERGENCY LIGHTS SYSTEM BETWEEN ROWS 
- [SDR NOCA00409](https://openairdocs.org/sdr/NOCA00409), Jan 8, 2009: PSEU. INOPERATIVE. EICAS : FLAPS, CAPT PITOT, TAT PROBE .5 LOW LIGHT ILLUMINATED WHILE GEAR WAS UP. FOUND EICAS AND STATU MESSAGES DISPLAYED R,N,L GEAR DOWN, AIR / GD DISAGREE NOS
- [SDR NOCA00109](https://openairdocs.org/sdr/NOCA00109), Jan 1, 2009: LIGHT. INOPERATIVE. 1 ABC EMERGENCY EXIT LIGHT INOP. RELAMPED 1ABC EMERGENCY EXIT LIGHT. OPS CK OK IAW MM 33-51-00.
- [SDR NOCA02208](https://openairdocs.org/sdr/NOCA02208), Apr 17, 2008: POWER SUPPLY. DISCHARGED. R2 DOOR INTERIOR EMERGENCY LIGHTS INOP AT THE MIDDLE OF THE DOOR. FOUND POWER SUPPLY M732 AT FAULT. REMOVED AND REPLACED POWER SUPPLY BY R2 DOOR (M732) IAW MM 3
- [SDR NOCA01908](https://openairdocs.org/sdr/NOCA01908), Mar 15, 2008: PANEL. CORRODED. RIGHT HAND TRANSITION PANEL HAS CORROSION ALONG TAPE LINE FROM STA 800-850. REMOVED AND REPLACED TRANSITION PANEL AS PER SRM 51-10-02.
- [SDR NOCA01508](https://openairdocs.org/sdr/NOCA01508), Feb 26, 2008: COVER. MISSING. R4 EMERGENCY EXIT SIGN COVER MISSING. REPLACED EXIT LIGHT ASSY AT R4 DOOR.
- [SDR NOCA16707](https://openairdocs.org/sdr/NOCA16707), Nov 13, 2007: SIGN. MALFUNCTIONED. EMERGENCY EXIT SIGN ABOVE R-1 FADING STILL READABLE. REPLACED EMERGENCY EXIT SIGN PER MM 33-51-09.
- [SDR NOCA15807](https://openairdocs.org/sdr/NOCA15807), Oct 20, 2007: FIRE LOOP. MALFUNCTIONED. RIGHT ENG 1 EICAS STATUS MSG. REMOVED AND REPLACED NR 4 DETECTOR ON THE NR 2 ENG PER AA E58 CARD 9325657 PER MM 26-11-01. OPS CHECK NORMAL, NO EICAS MSG. 
- [SDR NOCA15707](https://openairdocs.org/sdr/NOCA15707), Oct 9, 2007: LAMP. INOPERATIVE. EMERGENCY EXIT PATH LIGHTING INOP AT SEAT 28ABC. RELAMPED AS REQUIRED.
- [SDR NOCA10507](https://openairdocs.org/sdr/NOCA10507), May 31, 2007: BATTERY. INOPERATIVE. L-2 OUTBOARD EMERGENCY FLASHLIGHT INOP. DEFERRED PER MEL 25-63-4. FLIGHT ATTENDANT MUST HAVE OWN FLASHLIGHT. REMOVED AND REPLACED L-2 OUTBOARD EMERGENCY FLASHLI
- [SDR NOCA10707](https://openairdocs.org/sdr/NOCA10707), May 5, 2007: BATTERY. INOPERATIVE. FLIGHT ATTENDANT FLASHLIGHT AT DOOR 2L INOP. REPLACED FLASHLIGHT BATTERY AS REQ'D, OPS CHECKS NORMAL.
- [SDR NOCA09507](https://openairdocs.org/sdr/NOCA09507), Apr 30, 2007: SLIDE. ACTIVATED. L1 SLIDE INOP, FOUND L1 DOOR 1/4 OPENED. THE EVAC SLIDE HALF OUT OF CONTAINER CASE WITH THE GIRT BAR STILL ATTACHED TO THE DOOR FRAME. THE EVACUATION SLIDE HAND
- [SDR NOCA08407](https://openairdocs.org/sdr/NOCA08407), Apr 15, 2007: PRESSURE SWITCH. MALFUNCTIONED. AUTO-BRAKE DISENGAGE ON LANDING CORRECTIVE ACTION REPLACED PRESSURE SWITCHES S282 AND S283 PER MM 32-42-00, OPS CHECK OK.
- [SDR NOCA08007](https://openairdocs.org/sdr/NOCA08007), Apr 9, 2007: OVERHEAT LOOP. MALFUNCTIONED. EICAS STATUS MESSAGE L TURB OH DET 2. REMOVED AND REPLACED L ENG OVERHEAT DET 2 IAW MM 26-13-01. OPS CK NORMAL.
- [SDR NOCA04907](https://openairdocs.org/sdr/NOCA04907), Feb 27, 2007: IRU. MALFUNCTIONED. AUTOBRAKES DISARMED ON LANDING. PERFORMED ANTI-SKID AUTOBRAKES BITE PER FIM 32-42-00 FOUND IRS R AT FAULT REMOVED AND REPLACED R IRU PER MM 34-21-01, OPS CHECKE
- [SDR NOCA03207](https://openairdocs.org/sdr/NOCA03207), Feb 3, 2007: FUSE. BLOWN. FOUND EMERGENCY EXIT FLOOR LIGHTING IS INOP FROM ROW 28ABC TO ROW 32ABC. REMOVED AND REPLACED THE POWER SUPPLY FUSE PER TASK 33-51-07-962-071. OPS CHECKS GOOD.
- [SDR NOCA02807](https://openairdocs.org/sdr/NOCA02807), Jan 30, 2007: CONTROL MODULE. MALFUNCTIONED. SPOILER EICAS MESSAGE. FOUND SCM MS30 AT FAULT. REMOVED AND REPLACED SPOILER CONTROL MODULE PER MM 27-09-00. OPS CHECKS OK, NO FAULTS NOTED.
- [SDR NOCA22506](https://openairdocs.org/sdr/NOCA22506), Dec 15, 2006: BOTTLE. LOW. L4 DOOR POWER ASSIST BOTTLE PRESSURE BELOW LIMITS. REMOVED AND REPLACED L4 DOOR EMERGENCY POWER RESERVOIR PER MM 52-11-30, OPS CHECKS OK.
- [SDR NOCA21806](https://openairdocs.org/sdr/NOCA21806), Nov 26, 2006: EADI. MALFUNCTIONED. CAPTAINS DISPLAY UNIT (PRIMARY FLIGHT DISPLAY) CHANGES COLOR AND FLICKERS OCCASIONALLY. REMOVED AND REINSTALLED CAPT`S EAID IAW AMM 34-22-03. INSPECTED COOLING 
- [SDR NOCA20306](https://openairdocs.org/sdr/NOCA20306), Nov 18, 2006: BULB. INOPERATIVE. R-4 DOOR SLIDE INDICATOR LIGHT INOP. RELAMPED R-4 DOOR SLIDE INDICATOR LIGHT. OPS CHECKS NORMAL, SYSTEM CHECKS NORMAL AS PER AMM 25-66-01.
- [SDR NOCA20106](https://openairdocs.org/sdr/NOCA20106), Nov 15, 2006: AUTOBRAKE SYS. INOPERATIVE. AUTO BRAKES KICKED OFF DURING LANDING. AUTOBRAKES WERE SET AT 2. PLACARDED AUTOBRAKES SYSTEM INOP IAW DDG 32-32-4 ASSIDNED CI 32-78. REMOVED AND REPLACED AUTO B
- [SDR NOCA18606](https://openairdocs.org/sdr/NOCA18606), Nov 3, 2006: ALTIMETER. UNKNOWN. F/O RADIO ALTIMETER FLAG RA VISIBLE ON EADI, ITEM DEFERRED PER MEL 34-33-1B.
- [SDR NOCA17906](https://openairdocs.org/sdr/NOCA17906), Oct 23, 2006: INDICATOR. INOPERATIVE. RT RMI NR 2 VOR INOP. FLAG IN VIEW. REMOVED AND REPLACED RIGHT RDMI PER MM 34-22-05, OPS CHECK NORMAL.
- [SDR NOCA17806](https://openairdocs.org/sdr/NOCA17806), Oct 23, 2006: TRANSCEIVER. MALFUNCTIONED. LEFT F/D FAILED IN FLIGHT "NO LAND 3" DISPLAY ON AUTO LAND STATUS IND. PERFORMED AUTO FLT FAULT BITE PROCEDURE PER 22-00-02 RIGHT RA FAULT. REMOVED AND REPLACED
- [SDR NOCA17206](https://openairdocs.org/sdr/NOCA17206), Oct 18, 2006: COMPUTER. INOPERATIVE. LEFT FLIGHT DIRECTOR INOP ( F/D BARS NOT IN VIEW ). ACCOMPLISHED OPERATIONAL CHECK OF FLIGHT DIRECTOR PER MM 22-10-00. OPS CHECKED NORMAL AND PERFORMED AFDS SYS
- [SDR NOCA16806](https://openairdocs.org/sdr/NOCA16806), Oct 18, 2006: SHUTOFF VALVE. MALFUNCTIONED. LE SLAT ASYM EICAS MSG AND LEADING EDGE LIGHT ON DEPARTURE UPON FLAP ACTUATION. ALSO C HYD SYS WHITE LIGHT ON P61 PANEL. PERFORMED FIM TASK 32-09-03 FIG 103PSEU
- [SDR NCOA16506](https://openairdocs.org/sdr/NCOA16506), Oct 5, 2006: MEGAPHONE. FAULTY. MEGAPHONE IN BIN 1 ABC IS INOP. REINSTALLED TRIGGER SET SCREW AND REPLACED BATTERIES, OPS CHECK GOOD.
- [SDR NCOA16606](https://openairdocs.org/sdr/NCOA16606), Oct 4, 2006: SMOKE DETECTOR. INOPERATIVE. RIGHT MID LAV SMOKE DETECTOR INOP. GREEN PAIR LT IS ON, INSTALLED SMOKE DETECTOR, OP CHECK GOOD.
- [SDR NCOA16706](https://openairdocs.org/sdr/NCOA16706), Oct 3, 2006: BULB. INOPERATIVE. EMERGENCY AISLE LIGHTING BETWEEN SEAT ROWS 27 AND 28 LEFT, NEXT TO LFT LAV, HAS 5 LIGHTS INOPERATIVE. REPLACED LIGHTS IN EMERGENCY AISLE LIGHTING BETWEEN SEAT R
- [SDR NOCA15006](https://openairdocs.org/sdr/NOCA15006), Sep 29, 2006: FLOOR SUPPORT. CORRODED. LIGHT CORROSION FLOOR RAILS AT INDENTS STA 1470. REMOVED CORROSION FROM FLOOR RAILS PER SRM 51-10-02, REINSPECT AND EVALUATE FOR CORROSION LEVEL, TREATED AND PR
- [SDR NOCA14706](https://openairdocs.org/sdr/NOCA14706), Sep 29, 2006: PANEL. CORRODED. FOUND LEFT TRANSITION PANEL CORRODED AT STATION 1530 TO 1610. REMOVED CORROSION PER SRM 51-10-02. REINSPECT AND EVALUATED FOR CORROSION, ALODINED AND PRIMED TRA
- [SDR NOCA16406](https://openairdocs.org/sdr/NOCA16406), Sep 29, 2006: PANEL. CORRODED. RIGHT TRANSITION PANEL TIEDOWN LUG AT STA 760 HAS CORROSION, BLENDED OUT CORROSION PER SRM 51-10-02. REINSPECT AND EVALUATE FOR CORROSION LEVEL, TREATED, PRIMED
- [SDR NOCA16306](https://openairdocs.org/sdr/NOCA16306), Sep 29, 2006: ATTACH ANGLE. CORRODED. FOUND CORROSION ON SIDEWALL 2-ANGLE. REMOVED CORROSION IAW SRM 51-10-02. REINSPECT AND EVALUATE FOR CORROSION LEVEL, TREATED, PRIMED AND PAINTED AREA PER SRM 51
- [SDR NOCA16206](https://openairdocs.org/sdr/NOCA16206), Sep 29, 2006: ATTACH ANGLE. CORRODED. FOUND CORROSION ON SIDEWALL 2-ANGLE, FROM STA 560 TO 640. REMOVED CORROSION IAW SRM 51-10-02. REINSPECT AND EVALUATE FOR CORROSION LEVEL. TREATED, PRIMED AND PA
- [SDR NOCA16106](https://openairdocs.org/sdr/NOCA16106), Sep 29, 2006: ATTACH ANGLE. CORRODED. FOUND CORROSION ON SIDEWALL 2-ANGLE. REMOVED CORROSION IAW SRM 51010-02. REINSPECT AND EVALUATE FOR CORROSION LEVEL. REPLACED 2 ANGLE FROM STA 640 THRU STA 765 
- [SDR NOCA16006](https://openairdocs.org/sdr/NOCA16006), Sep 29, 2006: PANEL. CORRODED. AFT CARGO LEFT TRANSITION PANEL CORRODED FROM STA 1200 - 1330. REMOVED CORROSION PER SRM 51-10-03. REINSPECT AND EVALUATE FOR CORROSION LEVEL, BLENDED OFF CORRO
- [SDR NOCA15906](https://openairdocs.org/sdr/NOCA15906), Sep 29, 2006: PAN. CORRODED. MAIN ETE AREA AT FWD LAV SERVICE PAN CORRODED AT TUBE CONNECTION. REMOVED 2 CORRODED DOUBLERS ON TOP OF LAV PAN. REINSPECT AND EVALUATE FOR CORROSION LEVEL. REM
- [SDR NOCA15806](https://openairdocs.org/sdr/NOCA15806), Sep 29, 2006: ATTACH FITTING. CORRODED. FWD CARGO DOOR SILL AREA HAS CORROSION ON 2 AFT FITTING. REMOVED CORROSION IAW SRM 51-10-02. REINSPECT AND EVALUATE FOR CORROSION LEVEL. INSTALLED NEW FITTING N
- [SDR NOCA15706](https://openairdocs.org/sdr/NOCA15706), Sep 29, 2006: ANGLE. CORRODED. FOUND CORROSION ON SIDE OF ALL PANEL 2-ANGLE. REMOVED CORROSION IAW SRM 51-10-02. REINSPECT AND EVALUATE FOR CORROSION LEVEL. REMOVED AND REPLACED TRANSITION AN
- [SDR NOCA15606](https://openairdocs.org/sdr/NOCA15606), Sep 29, 2006: THRESHOLD. CORRODED. AFT CARGO DOOR THRESHOLD CORRODED AT STA 1380 TO 1440 RIGHT SIDE. REMOVED RIGHT TRANSITION PANEL FROM STA 13809 TO 1440. REINSPECT AND EVALUATE FOR CORROSION LE
- [SDR NOCA15506](https://openairdocs.org/sdr/NOCA15506), Sep 29, 2006: FLOORBEAM. CORRODED. AFT CARGO FLOORBOARD TIEDOWN CONNECTION STRIP ON FLOORBEAMS CORRODED. REMOVED CORROSION FROM FLOORBEAMS, CONNECTON STRIP OUT OF LIMITS PER SRM 51-10-02. REINSPE
- [SDR NOCA15406](https://openairdocs.org/sdr/NOCA15406), Sep 29, 2006: PANEL. CORRODED. AFT CARGO LEFT TRANSITION PANEL STA 1330 TO 1410 CORRODED. REINSPECT AND EVALUATE FOR CORROSION LEVEL, BLENDED OFF CORROSION AND ALODINED AND PAINTED LEFT TRANS
- [SDR NOCA15306](https://openairdocs.org/sdr/NOCA15306), Sep 29, 2006: PANEL. CORRODED. AFT CARGO RIGHT HAND TRANSITION PANEL CORRODED FROM STA 1330 TO 1380. REMOVED CORROSION FROM RIGHT HAND TRANSITION PANEL FROM STA 1330 TO 1380. REINSPECT AND EV
- [SDR NOCA15206](https://openairdocs.org/sdr/NOCA15206), Sep 29, 2006: PANEL. CORRODED. AFT CARGO RIGHT TRANSITION PANEL CORRODED FROM STA 1330 TO 1380. REMOVED CORROSION FROM RIGHT TRANSITION PANEL FROM STA 1330 TO 1380. REINSPECT AND EVALUATE FOR
- [SDR NOCA15106](https://openairdocs.org/sdr/NOCA15106), Sep 29, 2006: PANEL. CORRODED. AFT CARGO RIGHT TRANSIITION PANEL CORRODED FROM STA 1200 TO 1330. REMOVED CORROSION FROM RIGHT TRANSITION PANEL FROM STA 1200 TO 1330 PER SRM 51-10-02. REINSPEC
- [SDR NOCA14906](https://openairdocs.org/sdr/NOCA14906), Sep 29, 2006: PANEL. CORRODED. LEFT TRANSITION PANEL CORRODED STA 1410-1530, REMOVED CORROSION IAW SRM 51-10-02. REINSPECTED AND EVALUATED FOR CORROSION LEVEL, BLENDED OFF CORROSION AND ALODI
- [SDR NOCA14806](https://openairdocs.org/sdr/NOCA14806), Sep 29, 2006: PANEL. CORRODED. LEFT TRANSITION PANEL CORRODED STA 1440-1530, REMOVED CORROSION IAW SRM 51-10-02. REINSPECTED AND EVALUATED FOR CORROSION LEVEL. REPLACED TRANSITION PANEL PER A
- [SDR NOCA14606](https://openairdocs.org/sdr/NOCA14606), Sep 29, 2006: PANEL. CORRODED. RIGHT TRANSINTION PANEL CORRODED STA 6530-1640, REMOVED CORROSION IAW SRM 51-10-02. REINSPECTED AND EVALUATED FOR CORROSION LEVEL. REPLACED RIGHT TRANSITION PAN
- [SDR NOCA13906](https://openairdocs.org/sdr/NOCA13906), Sep 23, 2006: FRAME. MISSING. AFTER TAKEOFF RIGHT ENGINE EGT CLIMBED O 863 DEGREES CELCIUS. UPDATED (10/04/06) PERFORMED FIM TASK 71-03-00 FIG 116 AND NO FAULTS FOUND IN INSP, PERFORMED TEST

All 63: https://openairdocs.org/aircraft/N756NA/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

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