# N806AM: Amazon.Com Services MK30 - Status: Valid registration - Airframe: [Amazon.Com Services MK30](https://openairdocs.org/model/amazon-com-services-mk30) (registry code 06102FK) - Serial number: 178650109L - Type: Rotorcraft - Engine type: Electric - Certificate issued: July 18, 2025 - Expires: July 31, 2032 - Mode S code: AAF833 - Registered owner: [Amazon.Com Services LLC](https://openairdocs.org/faa-owner/AMAZON.COM%20SERVICES%20LLC) - Location: [Seattle, WA](https://openairdocs.org/faa-place/WA/Seattle) - Owner type: LLC - Owner's area on the map: 47.6306° N, 122.3456° W: Placed by OpenAirDocs at the center of ZIP code 98109, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=806AM - Page: https://openairdocs.org/aircraft/N806AM 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 (Amazon.Com Services MK30) None in force. ## Information bulletins (advisory) None matched. ## NTSB investigations None matched to N806AM. ## FAA accident and incident reports None matched to N806AM. ## 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 N806AM not matched to an aircraft (25) They name N806AM, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR ASMF200604009](https://openairdocs.org/sdr/ASMF200604009), Apr 16, 2006: SLIDE. UNWANTED DEPLOY. AT PLATFORM, GROUND PERSONNEL DEPLOYED THE R1 DOOR RAFT-SLIDE. DURING REVIEW, IT WAS DETECTED THE BAR IN ARMED POSITION. THE RAFT-SLIDE AND POWER RESERVOIR WERE - [SDR ASMF200601008](https://openairdocs.org/sdr/ASMF200601008), Jan 14, 2006: WARNING LIGHT. ILLUMINATED. AIRCRAFT RETURNED TO PLATFORM AS CONSEQUENCE OF OIL LOW PRESSURE AND HIGH EGT INDICATIONS DURING THE LEFT ENGINE STARTING. AT PLATFORM, THE TECHNICAL PERSONNEL - [SDR ASMF200512004](https://openairdocs.org/sdr/ASMF200512004), Nov 28, 2005: ENGINE. FLAMED OUT. AC PERFORMED AN UNSCHEDULED LANDING, FWD AND AFT FUEL PUMP LIGHTS TURNED ON AND RT ENGINE FLAMED OUT ON FLIGHT AND DURING LANDING THE TIRES POSITION 4 AND 8 WAS - [SDR ASMF200512003](https://openairdocs.org/sdr/ASMF200512003), Nov 28, 2005: ENGINE. NONE. AIRCRAFT RETURNED TO PLATFORM, DURING TAXING THE LT ENGINE WAS SHUTOFF WITH 420 OF EGT. DURING MAINTENANCE REVISION, THE LT ENGINE PARAMETERS WAS VERIFIED FINDI - [SDR ASMF200511003](https://openairdocs.org/sdr/ASMF200511003), Nov 4, 2005: PRESSURE SWITCH. FAILED. AIRCRAFT RETURNED OF FLIGHT AS A CONSEQUENCE OF EICAS MESSAGE -L ENG FUEL FILT- WAS SHOWN. THE FUEL PUMP FILTER AND DEFERENTIAL PRESSURE SWITCH WERE REPLACED IA - [SDR ASMF200509006](https://openairdocs.org/sdr/ASMF200509006), Sep 13, 2005: EEC. FAILED. CAPTAIN REPORTED RT ENGINE EGT INDICATION WITH OSCILLATIONS OF 100 GRADES IN EICAS. THE RT EEC EBG AND THERMOCOUPLE HARNESS JUNCTION BOX WERE REPLACED IAW MM 73 - [SDR ASMF200507013](https://openairdocs.org/sdr/ASMF200507013), Jul 17, 2005: WINDOW. OPEN. AIRCRAFT REJECTED TAKEOFF AT 90 KTS AS A CONSEQUENCE OF LT WINDSHIELD OPENED WITHOUT APPARENT REASON. WINDSHIELD ADJUSTMENT CHECKED IAW MM56-11-01, TESTED CORRE - [SDR ASMF200503020](https://openairdocs.org/sdr/ASMF200503020), Mar 27, 2005: INLET GUIDE VANE. FAILED. AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF CAPTAIN REPORTED APU PNEUMATIC PRESSURE DOWN TO 8 PSI WHEN LEFT ENGINE STARTED INSULATION VALVE WAS OPENED. EN - [SDR ASMF200503014](https://openairdocs.org/sdr/ASMF200503014), Mar 14, 2005: CONTROL VALVE. FAILED. AIRCRAFT RETURNED TO PLATFORM AFTER ENGINES STARTED WITH CROSSED FEEDING, EICAS MESSAGES R HYD R SUR PRESS, R ENG REV CONE, L ENG REV CONE, L ENG FIRE LOOP 2, E - [SDR ASMF200501006](https://openairdocs.org/sdr/ASMF200501006), Jan 12, 2005: VALVE. LEAKING. DURING FUEL SERVICE WAS DETECTED HIGH SUPPLY PRESSURE ON FUEL DISPENSER (80 PSI), PROMOTING FUEL LEAK ON RT CENTRAL TANK VALVE. AIRCRAFT WAS FUELED THROUGH LT V - [SDR ASMF200412003](https://openairdocs.org/sdr/ASMF200412003), Dec 15, 2004: SHUTOFF VALVE. FAILED. CAPTAIN REPORTED THAT WHEN LEFT THRUST LEVER WAS LOCATED IN IDLE POSITION THE AIR-CONDITIONING PACK WAS SHUTDOWN AND "HI STAGE" LIGHT TURNED ON. DUAL VALVE WAS - [SDR ASMF200410017](https://openairdocs.org/sdr/ASMF200410017), Oct 23, 2004: MECHANISM. OUT OF ADJUST. AIRCRAFT REJECTED TAKEOFF AT 80 KTS, AFT CABIN DOOR LIGHT TURNED ON. CAPTAIN REPORTED THAT DURING TAXING, LIGHT TURNED OFF AND TURNS ON AGAIN AT PLATFORM. CAPTA - [SDR ASMF200408009](https://openairdocs.org/sdr/ASMF200408009), Aug 9, 2004: A/C PACK. INOPERATIVE. CAPTAIN REPORTED, AFTER ENGINE STARTED (LT ENGINE BLEED) LIGHT TURNED ON AND LT AIR CONDITIONING PACKAGE WAS INOPERATIVE. ENGINE WAS ACCELERATED, BLEED SWITCH W - [SDR ASMF200407028](https://openairdocs.org/sdr/ASMF200407028), Jul 24, 2004: CONTROLLER. FAILED. CAPTAIN REPORTED RT AIR CONDITIONING (PACK OFF) LIGHT TURNED ON CONTINUALLY AFTER ENGINE START AND WHEN ENGINE WAS IN IDLE POSITION, PNEUMATIC BLEED OF RT ENGIN - [SDR ASMF200406028](https://openairdocs.org/sdr/ASMF200406028), Jun 23, 2004: CIRCUIT BREAKER. TRIPPED. AIRCRAFT RETURNED TO PLATFORM, "CTL HYDRAULIC PUMP" LIGHT TURNED ON AND EICAS MESSAGE, ENGINES WERE SHUTDOWN. DURING MAINTENANCE CHECK, HYDRAULIC PUMP BREAKER K - [SDR MEX2004040](https://openairdocs.org/sdr/MEX2004040), Jan 30, 2004: LINE. LEAKING. DURING PUSH BACK, FOUND HYDRAULIC LEAKAGE ON THE LT ENGINE WHEN IT WAS STARTED. AT REVISION WAS FOUND A BROKEN HYDRAULIC LINE, SUCH LINE WAS REPLACED BY AN ALTE - [SDR MEX2003530](https://openairdocs.org/sdr/MEX2003530), Nov 22, 2003: LIGHT. INOPERATIVE. AIRCRAFT RETURNED TO PLATFORM DURING TAXIING RT AFT SLIDE ARMED LIGHT DID NOT TURN ON. AT PLATFORM, TECH PERSONNEL SWAPPED BOTH AFT SLIDE LIGHTS, AND CLEANED PR - [SDR MEX2003360](https://openairdocs.org/sdr/MEX2003360), Aug 13, 2003: SHUTOFF VALVE. FAILED. AIRCRAFT RETURN TO PLATFORM AFTER LEFT ENGINE WAS STARTED. THE LT FUEL SPAR VALVE LIGHT COME ON AND THE LEFT ENGINE SHUTDOWN WITH CODE 282209. DURING REVISION, - [SDR MEX2003220](https://openairdocs.org/sdr/MEX2003220), Jun 9, 2003: BYPASS VALVE. LEAKING. FLT 494 - MID-MEX - AIRCRAFT RETURN TO GATE, HYDRAULIC LEAK AT LEFT COMPARTMENT RESERVOIR AND DURING ENGINES STARTING THE 'LIGHT RUDDER PCU' EICAS STATUS MESSAG - [SDR MEX2003155](https://openairdocs.org/sdr/MEX2003155), May 3, 2003: ACTUATOR. INOPERATIVE. AIRCRAFT RETURN TO PLATFORM DUE TO RUDDER PCA EICAS MESSAGE. THE RUDDER MODULE WAS VERIFIED AND THE ALARM WAS FOUND IN RIGHT RUDDER RATIO. IN HANGER THE FIM 27- - [SDR MEX2002367](https://openairdocs.org/sdr/MEX2002367), Dec 18, 2002: INDICATOR. FAILED. AIRCRAFT RETURNED DUE TO FIRST OFFICER AIRSPEED INDICATOR OUT OF SERVICE, CAPTAIN PERFORMED ABNORMAL PROCEDURES AND FAIL CONTINUED DURING DESCENT, AIRSPEED INDI - [SDR MEX2002347](https://openairdocs.org/sdr/MEX2002347), Nov 22, 2002: PANEL. FAILED. CAPTAIN REPORTED THAT THE RT ENGINE BLEED VALVE SWITCH WAS OUT OF SERVICE PANEL WAS REMOVED AND SWITCH WAS UNCLOGGED AND PNEUMATIC SYSTEM WAS LET OUT OF SERVICE - [SDR MEX2002266](https://openairdocs.org/sdr/MEX2002266), Aug 14, 2002: WARNING SYSTEM. ACTIVATED. AT START OF RT ENGINE, ALL THE FIRE ALARMS ACTIVATED. FUEL CONTROL WAS DISCONNECTED AND MASTER WARNING WAS ADJUSTED, CREW REQUESTED TO PERFORM A VISUAL INSPECTI - [SDR MEX2002123](https://openairdocs.org/sdr/MEX2002123), Apr 25, 2002: PANEL. FAILED. FLT 902 - MEX-MTY - AIRCRAFT GOT PLATFORM WITHOUT AUDIBLE FIRE ALARMS. PERFORMED A FIRE DETECTION TEST IAW FIM 26-11-00 AND WEU AUDIBLE SYSTEM TEST IAW FIM 31-5 - [SDR MEX2002067](https://openairdocs.org/sdr/MEX2002067), Mar 3, 2002: PANEL. FAILED. FLT 941 - MTY-MEX - CABIN CREW REPORTED OTU OF SERVICE THE LANDING ALTITUDE SELECTOR, AS CONSEQUENCE OF SPARE PARTS MISSING IN MTY, MEX SENT SUCH PARTS IN FLT 9 ## STCs that may be installed (OpenAirDocs) None matched to this aircraft's models. ## Earlier aircraft with N806AM The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N806AM before. - [Cancelled 2017-03-03](https://openairdocs.org/deregistered/N806AM-2017-03-03): Hexacrafter HC-800, S/N 2013804. Assigned, pending cancellation ## Related - Other Amazon.Com Services MK30 aircraft: https://openairdocs.org/model/amazon-com-services-mk30/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.