# N813PH: Island Time AIRCAM - Status: Valid registration - Airframe: [Island Time AIRCAM](https://openairdocs.org/model/island-time-aircam) (registry code 05636SO, 2 seats) - Engine: [Rotax 912ULS series](https://openairdocs.org/engine/rotax-912uls-series) (registry code 55572) - Serial number: AC240 - Type: Fixed wing single engine - Engine type: 4 cycle - Kit: Lockwood Aircraft Corp AIRCAM - Airworthiness: Experimental, amateur built - Airworthiness date: October 25, 2017 - Certificate issued: July 26, 2021 - Expires: July 31, 2028 - Mode S code: AB15CE - Registered owner: [Island Time LLC](https://openairdocs.org/faa-owner/ISLAND%20TIME%20LLC) - Location: [Holiday, FL](https://openairdocs.org/faa-place/FL/Holiday) - Owner type: LLC - Owner's area on the map: 28.1926° N, 82.7704° W: Placed by OpenAirDocs at the center of ZIP code 34691, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=813PH - Page: https://openairdocs.org/aircraft/N813PH 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. The registry lists only the engine series, so ADs for every Rotax 912ULS model are included. ## ADs that may apply (OpenAirDocs): 0 in force ### Matched by airframe (Island Time AIRCAM) None in force. ### Matched by engine (Rotax 912ULS series) None in force. ## Information bulletins (advisory) None matched. ## NTSB investigations None matched to N813PH. ## NTSB investigations on N813PH not matched to an aircraft (1) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB SEA87IA119](https://openairdocs.org/ntsb/SEA87IA119), Jun 19, 1987: de Havilland DHC-8-101 (N813PH), Seattle, WA, incident, minor damage ## FAA accident and incident reports None matched to N813PH. ## Reports on N813PH not matched to an aircraft (2) They name N813PH, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [Incident 19871002069759I](https://openairdocs.org/incident/19871002069759I), Oct 2, 1987: Dhav DHC8101 (N813PH), Great Falls, MT. The number 2 engine failed on takeoff. The aircraft safely returned. An electronic fuel control plug was oil soaked - [Incident 19870619041209I](https://openairdocs.org/incident/19870619041209I), Jun 19, 1987: Dhav DHC8101 (N813PH), Seattle, WA, Minor damage. Explosion and fire in right engine on climbout. Used fire bottles and shut down. Fuel line near fcu had burst. ## 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 N813PH not matched to an aircraft (17) They name N813PH, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR SABA020034](https://openairdocs.org/sdr/SABA020034), Mar 13, 2002: BULB. ircraft 813 following flight 5057 ALH to CLT. during post flight inspection the left forward exterior emergency light was found inoperative. Maintgenance remove - [SDR SABA010045](https://openairdocs.org/sdr/SABA010045), Aug 28, 2001: POWER SUPPLY. INOPERATIVE. Aircraft 813 prior to flight 5099 CLT to PGV. During preflight the aft overhead emergency lights were inoperative. No emergency procedures were used. Maintenanc - [SDR QXEA9801284](https://openairdocs.org/sdr/QXEA9801284), Sep 13, 1998: BULB. FAILED. COCKPIT EMERGENCY OVERHEAD LIGHT INOP. RELAMPED, PERFORMED OPERATIONAL CHECK OF EMERGENCY LIGHTS SYSTEM. ALL LIGHTS OPERATE NORMALLY. - [SDR QXEA9800523](https://openairdocs.org/sdr/QXEA9800523), Apr 12, 1998: TSCU. MALFUNCTION. AUTOFEATHER SYSTEM DOES NOT ARM. ABORTED TAKEOFF AND RETURNED TO THE GATE. SYSTEM ARMED AND TESTED NORMALLY ON THE GROUND DURING TEST MODE. REPLACED POWER LEVER - [SDR QXEA9800241](https://openairdocs.org/sdr/QXEA9800241), Mar 6, 1998: RELAY. MALFUNCTION. AUTOFEATHER FAILED TO ARM. INSPECTED AND CLEANED POWER LEVER SWITCHES AND REPLACED 6121-K2 RELAY, OPERATIONAL CHECKS GOOD. - [SDR QXEA9800069](https://openairdocs.org/sdr/QXEA9800069), Feb 14, 1998: HYD LINE. CRACKED. EN ROUTE, NR 2 HYDRAULIC QUANTITY AND PRESSURE DROPPED TO ZERO WITH ASSOCIATED CAUTION LIGHTS. NR 1 HYDRAULIC QUANTITY DROPPED TO .5 QUARTS (PRESSURE ON NR 1 SY - [SDR QXEA9700867](https://openairdocs.org/sdr/QXEA9700867), Dec 1, 1997: BATTERY. DISCHARGED. PDX - RIGHT HAND FORWARD EGRESS LIGHTS INOP. REPLACED BATTERY, OPERATIONAL CHECK GOOD. - [SDR QXEA9700773](https://openairdocs.org/sdr/QXEA9700773), Nov 22, 1997: BULB. FAILED. PDX - NR 1 TEST POSITION OF THE BAGGAGE SMOKE DETECTOR INOP. REPLACED LAMP IN NR 1 SMOKE DETECTOR. OPERATIONAL CHECK GOOD. - [SDR QXEA9700771](https://openairdocs.org/sdr/QXEA9700771), Nov 20, 1997: SWITCH. DIRTY. SEA- ABORTED TAKEOFF NO AUTO FEATHER ARM LIGHT. CLEANED POWER LEVER SWITCH QUADRANT, NO PARTS REPLACED AND OPERATIONAL CHECK GOOD. - [SDR QXEA9700462](https://openairdocs.org/sdr/QXEA9700462), Aug 7, 1997: LIGHT. INOPERATIVE. SEA - COCKPIT CEILING EMERGENCY LIGHT INOP. REPLACED LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. - [SDR QXEA9700215](https://openairdocs.org/sdr/QXEA9700215), May 31, 1997: SMOKE DETECTOR. NO TEST. NR 1 BAGGAGE SMOKE DETECTOR WILL NOT TEST. REPLACED TEST LAMPS, OPERATIONAL CHECKS GOOD. - [SDR QXEA9700124](https://openairdocs.org/sdr/QXEA9700124), Apr 11, 1997: CABLE. BROKEN. UNABLE TO OPEN MAIN CABIN DOOR UPON ARRIVAL AT GATE. AIRCRAFT FERRIED FROM LWS TO PDX FOR REPAIRS. REPLACED PASSENGER DOOR CABLE AND RIGGED DOOR BALANCE SYSTEM, - [SDR QXEA9600301](https://openairdocs.org/sdr/QXEA9600301), Aug 13, 1996: SENSOR. CRACKED. ON CLIMBOUT THROUGH 12,000 FT, A THUMP WAS HEARD FOLLOWED BY NOSE GEAR INTRANSIT LIGHT. INTRANSIT LIGHT EXTINGUISHED ON ITS OWN AFTER AWHILE. AIRCRAFT LANDED IN - [SDR QXEA9600227](https://openairdocs.org/sdr/QXEA9600227), Jun 29, 1996: CONTROL BOX. MALFUNCTIONED. FCA - CABIN EMERGENCY LIGHTS WILL NOT SHUT OFF WHEN SELECTED OFF. EMERGENCY LIGHT CONTROL BOX REPLACED AND LIGHTS OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE - [SDR QXEA9600033](https://openairdocs.org/sdr/QXEA9600033), Jan 29, 1996: CIRCUIT BREAKER. INTERMITTENT. PDX - EMERGENCY LIGHTS FLICKER ON TAKEOFF ABOUT THE SAME TIME STANDBY HYDRAULIC SWITCHES ARE TURNED OFF. POWER SUPPLY PS1 AND PS2, CONTROL BOX AND CIRCUIT BREAK - [SDR QXEA9600029](https://openairdocs.org/sdr/QXEA9600029), Jan 24, 1996: SWITCH PANEL. MALFUNCTIONED. PDX - ALL EMERGENCY LIGHTS IN CABIN FLICKER DURING FLIGHT. FLIGHT ATTENDANTS SWITCH PANEL REPLACED AND LIGHTS OPS CHECKED GOOD. - [SDR QXEA9600012](https://openairdocs.org/sdr/QXEA9600012), Jan 5, 1995: CONTROL BOX. MALFUNCTIONED. PDX - ON CLIMBOUT, WHEN GEAR IS RAISED CABIN EMER LIGHTS FLICKER. CONTROL BOX AND BATTERY PACKS PS3 AND PS4 REPLACED. EMER LIGHTS OPS CHECKED GOOD AND AIRCRAFT ## STCs that may be installed (OpenAirDocs) None matched to this aircraft's models. ## Related - Other Island Time AIRCAM aircraft: https://openairdocs.org/model/island-time-aircam/aircraft.md - The Rotax 912ULS series engine: https://openairdocs.org/engine/rotax-912uls-series.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.