# N906AM: 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: 1786501101 - Type: Rotorcraft - Engine type: Electric - Certificate issued: July 18, 2025 - Expires: July 31, 2032 - Mode S code: AC8582 - 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=906AM - Page: https://openairdocs.org/aircraft/N906AM 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 N906AM. ## FAA accident and incident reports None matched to N906AM. ## 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 N906AM not matched to an aircraft (33) They name N906AM, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR ASMF20180821005](https://openairdocs.org/sdr/ASMF20180821005), Jun 17, 2018: ACTUATOR. LEAKING. DURING A PERIODIC CHECK, DETECTED A HYDRAULIC LEAK THROUGH THE BODY OF LEFT MAIN LANDING GEAR RETRACT ACTUATOR. MAINTENANCE REPLACED THE LEFT MLG RETRACT ACTUAT - [SDR ASMF201801006](https://openairdocs.org/sdr/ASMF201801006), Dec 3, 2017: WINDOW. CRACKED. DURING A TRANSIT CHECK, FOUND THE RIGHT SIDE WINDOW CRACKED. MAINTENANCE PERFORMED AMM 56-12-11, CONFIRMING THE RIGHT SIDE WINDOW CRACKED AND OPERATIONAL OUT OF - [SDR ASMF201710090001](https://openairdocs.org/sdr/ASMF201710090001), Sep 24, 2017: STATIC INVERTER. FAILED. CAPTAIN REPORTED THAT DURING TAXING TO PLATFORM, THE ELEC LIGHT TURNED ON. MAINTENANCE PERFORMED ELECTRICAL SYSTEM AUTO TEST IAW FIM 24-31, TASK 801 PROCEDURE, - [SDR ASMF201611022](https://openairdocs.org/sdr/ASMF201611022), Oct 8, 2016: BLEED VALVE. LEAKING. DURING TRANSIT CHECK, IT WAS DETECTED A FUEL LEAK IN THE RIGHT ENGINE. THE PLATFORM WAS CLEANED AND MAINTENANCE PERFORMED REVISION, DETECTING FUEL LEAK IN THE T - [SDR ASMF201606002](https://openairdocs.org/sdr/ASMF201606002), Apr 17, 2016: UNKNOWN. MALFUNCTIONED. CAPTAIN REPORTED THAT DURING CLIMB, THE MAIN AND NOSE LANDING GEARS WERE NOT RETRACTED WHEN LANDING GEAR LEVER MOVED TO UP POSITION AFTER TAKEOFF. THE FLIGHT CR - [SDR ASMF201510020](https://openairdocs.org/sdr/ASMF201510020), Sep 15, 2015: SENSOR. FAILED. DURING START ENGINES, THE LE FLAPS TRANSIT LIGHT TURNED ON. PERFORMED BITE TO FSEU IAW FIM 27-88 TASK 810 PROCEDURE, SHOWING FAILURE CODE 27-81215 SL8 PROX INBD - [SDR ASMF201507015](https://openairdocs.org/sdr/ASMF201507015), Jun 23, 2015: WINDOW. CRACKED. CAPTAIN REPORTED THAT AT 39,000 FEET, THE LT WINDOW NR 1 CRACKED. ACCOMPLISHED THE QRH 1.14 PROCEDURE, CONFIRMING THE FAILURE & CONTINUING TO DESTINATION. REPLA - [SDR ASMF201503019](https://openairdocs.org/sdr/ASMF201503019), Feb 28, 2015: ACTUATOR. FAILED. AIRCRAFT RETURNED TO PLATFORM DUE TO TAKEOFF CONFIGURATION ALARM WAS ACTIVE. PERFORMED BITE TO FSEU IAW FIM 31-51 TASK 801, NO CONFIRMING FAILURE, TESTED CORREC - [SDR ASMF201503016](https://openairdocs.org/sdr/ASMF201503016), Feb 19, 2015: PUMP. LEAKING. AIRCRAFT RETURNED TO PLATFORM DUE TO DURING RT ENG START, A FUEL LEAK WAS DETECTED. THE PLATFORM WAS CLEANED BY FIREMEN & MX PERFORMED REVISION, DETECTING FUEL - [SDR ASMF201503015](https://openairdocs.org/sdr/ASMF201503015), Feb 18, 2015: STATIC INVERTER. FAILED. AIRCRAFT RETURNED TO PLATFORM DUE TO DURING TAXING, THE ELEC LIGHT TURNED ON. PERFORMED ELEC SYS AUTO TEST IAW FIM 34-31 TASK 801, DETECTING THE STATIC INVERTER - [SDR ASMF201501025](https://openairdocs.org/sdr/ASMF201501025), Jan 2, 2015: O-RING. DAMAGED. AIRCRAFT RETURNED TO PLATFORM DUE TO DURING RT ENG START, A FUEL & HYD LEAKS WERE DETECTED. THE PLATFORM WAS CLEANED. PERFORMED REVISION, DETECTING FUEL LEAK IN - [SDR ASMF201409004](https://openairdocs.org/sdr/ASMF201409004), Aug 2, 2014: TRANSCEIVER. FAILED. CAPTAIN REPORTED THAT DURING CRUISE, THE WXR FAIL ON BOTH SIDES LIGHT TURNED ON WITH INTERMITTENT FAULT. PERFORMED REVISION DETECTING THE RADAR FAILED, SO THE W - [SDR ASMF201409003](https://openairdocs.org/sdr/ASMF201409003), Aug 1, 2014: TRANSCEIVER. FAILED. AIRCRAFT PERFORMED AN UNSCHEDULED LANDING DUE TO EICAS MSGS. PWS FAIL & WXR FAIL. PERFORMED REVISION DETECTING THE TRANSCEIVER FAILED, SO THE WEATHER RADAR TRAN - [SDR ASMF2014061706009](https://openairdocs.org/sdr/ASMF2014061706009), Apr 26, 2014: WINDSHIELD. ABNORMAL. DURING TRANSIT CHECK, IT WAS DETECTED SCRATCHES IN BOTH COCKPIT WINDSHIELD. PERFORMED REVISION DETECTING SCRATCHES OUT OF LIMITS SO BOTH COCKPIT WINDSHIELDS WER - [SDR ASMF201403004](https://openairdocs.org/sdr/ASMF201403004), Feb 15, 2014: BLADE. LACK OF LUBE. AIRCRAFT RETURNED TO PLATFORM DUE TO DURING TAXING, THE RT ENG VIBRATION REACHED 0.5 UNITS. ACFT WAS SENT TO THE HANGAR & MX PERFORMED LUBRICATION OF THE RT ENG - [SDR ASMF201403003](https://openairdocs.org/sdr/ASMF201403003), Feb 11, 2014: WINGLET. DAMAGED. DURING TRANSIT CHECK, A LIGHTNING STRIKE WAS DETECTED IN RT WINGLET TE. MXL PERFORMED A LIGHTNING STRIKE INSPECTION IAW MM 05-51-19 DETECTING DAMAGES OUT OF LIM - [SDR ASMF201402006](https://openairdocs.org/sdr/ASMF201402006), Dec 31, 2013: NOSE COWL. SCRATCHED. DURING TRANSIT CHECK, DETECTED A SCRATCH IN THE LT NOSE COWLING AT 05:30 HRS POSITION. MX PERSONNEL PERFORMED REVISION DETECTING A SCRATCH OF 2” LENGTH IN THE L - [SDR ASMF201301004](https://openairdocs.org/sdr/ASMF201301004), Jan 6, 2013: SEAL. LEAKING. AIRCRAFT RETURNED TO PLATFORM, NLG SHOCK STRUT HYD LEAK. ACFT WAS SENT TO THE HANGAR AND MX PERSONNEL REPLACED THE ACTIVE SEALS IAW MM 32-21-11, TESTED CORRECT. - [SDR ASMF201211001](https://openairdocs.org/sdr/ASMF201211001), Oct 21, 2012: REGULATOR. DAMAGED. REJECTED TAKEOFF AT 60 KNOTS DUE TO LT ENGINE PRESSURE DROP OF 15 PSI IN PNEUMATIC DUCT AND LT OVER WING LIGHT TURNED ON. MX PERSONNEL REPLACED THE BLEED AIR RE - [SDR ASMF201112003](https://openairdocs.org/sdr/ASMF201112003), Dec 2, 2011: SKIN. DENTED. DURING OVERNIGHT CHECK, MX DETECTED A DENT IN THE RT HORIZONTAL STAB L/E AT STA 181.23 OF 4.150" LONG AND 0.270" DEPTH, IT WAS CONFIRMED THAT DENT WAS OUT OF LI - [SDR ASMF201108010](https://openairdocs.org/sdr/ASMF201108010), Aug 19, 2011: DOOR. OUT OF ADJUST. ACFT RETURNED TO DEPARTURE DURING CLIMB, THE ACFT DID NOT PRESSURIZE WITH DOOR TOTALLY CLOSED AND PRESSURE LIGHT REMAINING OFF. DURING MX REVISION, THE FORWARD - [SDR ASMF20110712](https://openairdocs.org/sdr/ASMF20110712), Jul 24, 2011: MANIFOLD. LEAKING. DURING FUELING SERVICE, DETECTED A FUEL LEAK THROUGH THE ACFT FUEL MANIFOLD, MX TIGHTEN THE SCREWS IAW AMM 28-21-11 CORRECTING THE LEAK. - [SDR ASMF201010003](https://openairdocs.org/sdr/ASMF201010003), Oct 3, 2010: CARBON SEAL. DAMAGED. DURING TRANSIT CHECK, TECH DETECTED AN OIL LACK IN THE IDG GEARBOX CARBON SEAL IN THE LT ENGINE. ACFT WAS SENT; SO IT WAS REPLACED AND LEAK TEST WAS PERFORMED I - [SDR ASMF201009008](https://openairdocs.org/sdr/ASMF201009008), Sep 19, 2010: SEAL. OUT OF POSITION. ACFT RETURNED, DURING TAKEOFF AND INITIAL CLIMB, A FUEL LEAK WAS FOUND ON RT WING. MX PERFORMED FUSELAGE AND WING INSP DETECTING FUEL LEAK ON RT LOWER WING DUE - [SDR ASMF201009005](https://openairdocs.org/sdr/ASMF201009005), Sep 11, 2010: SKIN. DENTED. DURING TRANSIT CHECK A BIRD STRIKE WAS DETECTED ON THE RT SIDE HORIZONTAL STABILIZER L/E. MX PERFORMED A BIRD STRIKE INSP IAW 05-51-18 DETECTING DENT OF 12.00 X - [SDR ASMF200904004](https://openairdocs.org/sdr/ASMF200904004), Apr 24, 2009: ENGINE. FAILED. CAPTAIN REPORTED THAT DURING CRUISE THE RT ENGINE LOW OIL PRESS ALERT CAME ON, SO THEY PERFORMED THE SPECIAL ENGINE OIL PRESS PROCEDURE AND SHUTDOWN THE ENGINE. - [SDR ASMF20090404](https://openairdocs.org/sdr/ASMF20090404), Apr 24, 2009: ENGINE. FAILED. CAPTAIN REPORTED THAT DURING CRUISE, IN THE ENG, NR 2 THE LOW OIL PRESS ALERT CAME ON, THE QRH PROCEDURE WAS FOLLOWED BY AN ENGINE FAILURE OR SHUTDOWN PROCEDURE - [SDR ASMF200710007](https://openairdocs.org/sdr/ASMF200710007), Oct 22, 2007: ENGINE. LOW PRESSURE. CAPTAIN REPORTED LT ENGINE WITH LOW PNEUMATIC PRESSURE INDICATION, RT ENGINE 40 PSI AND LT 20 PSI. MAINTENANCE PERSONNEL PERFORMED THE FIM PROCEDURE 36-10, TEST - [SDR ASMF200708004](https://openairdocs.org/sdr/ASMF200708004), Aug 15, 2007: EEC. FAILED. AIRCRAFT RETURNED TO PLATFORM DURING TAXI, LT ENGINE CONTROL LIGHT TURNED ON AND STAY ILLUMINATED. MAINTENANCE CLEANED PS3 AIR TUBE WITH HIGH PRESSURE NITROGEN, - [SDR ASMF200606014](https://openairdocs.org/sdr/ASMF200606014), Jun 23, 2006: ENGINE. FOD. AIRCRAFT RETURNED TO PLATFORM, THE RT ENGINE INGESTED A PLASTIC BAG DURING TAXING. RT ENGINE WAS INSPECTED IAW MM 71-00-00, SECONDARY FLOW AREA WAS CLEANED AND - [SDR ASMF200602005](https://openairdocs.org/sdr/ASMF200602005), Feb 17, 2006: UNKNOWN. UNKNOWN. AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF THE 3 LAVATORIES WERE INOPERATIVE WITH NO FAILURE INDICATIONS. DURING CHECK WAS DETECTED THE BLOWER VACUUM INO - [SDR ASMF200503015](https://openairdocs.org/sdr/ASMF200503015), Mar 15, 2005: ENGINE. MALFUNCTIONED. AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURING RIGHT ENGINE STARTED, N1 WAS INCREASED SLOWLY AFTER EGT INDICATION. THE FAULT ISOLATION PROCEDURE 80-07 - [SDR ASMF200503007](https://openairdocs.org/sdr/ASMF200503007), Mar 9, 2005: MODULE. FAILED. CAPTAIN REPORTED THAT MESSAGE (SPD LIM FLAG IN PFD) WAS SHOWN. REPORT WAS DEFERRED IAW MEL 34-2-1. AIRCRAFT RETURNED TO PLATFORM BECAUSE OF MACH TRIM, AUTO SLAT ## STCs that may be installed (OpenAirDocs) None matched to this aircraft's models. ## 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.