# N861AM: 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: 178650109Q - Type: Rotorcraft - Engine type: Electric - Certificate issued: July 18, 2025 - Expires: July 31, 2032 - Mode S code: ABD29A - 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=861AM - Page: https://openairdocs.org/aircraft/N861AM 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 N861AM. ## FAA accident and incident reports None matched to N861AM. ## 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 N861AM not matched to an aircraft (40) They name N861AM, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR ASMF20180327001](https://openairdocs.org/sdr/ASMF20180327001), Mar 7, 2018: SENSOR. FAILED. DURING A TRANSIT CHECK, DETECTED AN LE SLAT NR 6 LIGHT TURNED ON. MAINTENANCE PERFORMED A BITE TO FSEU IAW FIM 27-51 / 801, SHOWING FAILURE CODES 27-81211, FIM - [SDR ASMF201704019](https://openairdocs.org/sdr/ASMF201704019), Apr 28, 2017: BRAKE. LEAKING. DURING TRANSIT CHECK, A HYDRAULIC LEAK WAS DETECTED FROM THE RIGHT MAIN LANDING GEAR. MAINTENANCE PERFORMED AN INSPECTION IAW AMM 32-11-21, LEAKAGE WAS OUT OF L - [SDR ASMF201704008](https://openairdocs.org/sdr/ASMF201704008), Apr 6, 2017: RESERVOIR. LOW QUANTITY. DURING TRANSIT CHECK, IT WAS DETECTED EVIDENCE OF HYDRAULIC LEAKAGE IN THE LEFT MAIN LANDING GEAR AND AN INDICATION IN COCKPIT OF LOW LEVEL OF HYDRAULIC IN THE - [SDR ASMF20170301001](https://openairdocs.org/sdr/ASMF20170301001), Feb 16, 2017: GLAND NUT. CORRODED. DURING TRANSIT CHECK, IT WAS DETECTED CORROSION ON THE SHOCK STRUT GLAND NUT AND CYLINDER OF THE LEFT MAIN LANDING GEAR; THEREFORE THE LEFT MAIN LANDING ASSY WA - [SDR ASMF20170301002](https://openairdocs.org/sdr/ASMF20170301002), Feb 12, 2017: WARNING SYSTEM. ACTIVATED. AIRCRAFT RETURNED OF FLIGHT DUE TO DURING CRUISE, THE RIGHT SIDE WING BODY OVERHEATS LIGHT TURNED ON AND RIGHT PACK AIR CONDITIONED WAS DEFERRED, SHOWING BETWEE - [SDR ASMF201611008](https://openairdocs.org/sdr/ASMF201611008), Sep 7, 2016: HINGE FITTING. DAMAGED. CAPTAIN REPORTED THAT DURING CRUISE, A STRONG NOISE IN THE FWD ENTRY DOOR WAS LISTENED; AT THE GATE THE FLIGHT ATTENDANT DETECTED THAT THE HINGE OF THE DOOR WAS - [SDR ASMF201610017](https://openairdocs.org/sdr/ASMF201610017), Sep 7, 2016: HINGE FITTING. DAMAGED. CAPTAIN REPORTED THAT DURING CRUISE, A STRONG NOISE IN THE FWD ENTRY DOOR WAS LISTENED; AT THE GATE THE FLIGHT ATTENDANT DETECTED THAT THE HINGE OF THE DOOR WAS - [SDR ASMF201610007](https://openairdocs.org/sdr/ASMF201610007), Aug 13, 2016: ACTUATOR. LEAKING. DURING TRANSIT CHECK, A FUEL LEAK WAS DETECTED IN THE RIGHT ENGINE. MAINTENANCE PERSONNEL PERFORMED REVISION, DETECTING FUEL LEAK IN THE TRANSIENT BLEED VALVE D - [SDR ASMF201610002](https://openairdocs.org/sdr/ASMF201610002), Aug 7, 2016: MODULE. INTERMITTENT. AIRCRAFT RETURNED TO PLATFORM DURING TAXING, THE RIGHT SIDE WING BODY OVERHEATS LIGHT TURNED ON. MAINTENANCE PERSONNEL PERFORMED BITE TO WHEEL WELL FIRE, WING A - [SDR ASMF201605013](https://openairdocs.org/sdr/ASMF201605013), Apr 9, 2016: PRESSURE VALVE. FAILED. AIRCRAFT RETURNED TO PLATFORM DUE TO DUCT PRESS LOW INDICATION IN THE LT ENG, SHOWING 5 PSI. PERFORMED REVISION IAW 36-11-00, DETECTING A PNEUMATIC LEAK IN THE - [SDR ASMF201605001](https://openairdocs.org/sdr/ASMF201605001), Feb 25, 2016: VALVE. STUCK. AIRCRAFT REJECTED TAKE OFF AT 40 KNOTS, DUE TO DURING TAKEOFF ROLL THE RT BLEED TRIP OFF LIGHT TURNED ON. THE FLIGHT CREW ACCOMPLISHED THE QRH 2.6 PROCEDURE, CO - [SDR ASMF201510016](https://openairdocs.org/sdr/ASMF201510016), Sep 5, 2015: TRANSMITTER. FAILED. AIRCRAFT RETURNED TO PLATFORM DUE TO, AFTER START ENGINES & DURING FLAPS EXTENSION, THE LT & RT FLAP INDICATION SHOWN ASYMMETRY WITH LEVER DID NOT COMMAND. PERF - [SDR ASMF201510015](https://openairdocs.org/sdr/ASMF201510015), Sep 4, 2015: INDICATION SYS. MALFUNCTIONED. AIRCRAFT RETURNED TO PLATFORM DUE TO AFTER START ENGINES, THE LE FLAP EXTEND INDICATION WAS SHOWN WITHOUT MOVEMENT. PERFORMED THE FIM 27-51 TASK 820 PROCEDURE, - [SDR ASMF201509009](https://openairdocs.org/sdr/ASMF201509009), Jul 31, 2015: LINE. LEAKING. DURING TRANSIT CHECK, IT WAS DETECTED A HYD LEAK IN THE MAIN BRAKE NR 1. PERFORMED REVISION IAW AMM 31-40-00, DETECTING A HYD LEAK IN QUICK CONNECTION LINE OF T - [SDR ASMF201509006](https://openairdocs.org/sdr/ASMF201509006), Jul 28, 2015: CAP. LOOSE. AIRCRAFT RETURNED TO PLATFORM, DUE TO DURING TAXING, IT WAS DETECTED AN ELEC CABLE BURNED ODOR WITH EVIDENCE OF WHITE SMOKE. PERFORMED FIM 21-00 TASK 806 PROCED - [SDR ASMF201509005](https://openairdocs.org/sdr/ASMF201509005), Jul 25, 2015: HEAT EXCHANGER. DAMAGED. AIRCRAFT RETURNED TO PLATFORM DUE TO DURING TAXING, THE EECS ALT MODE & RT WINDOW HEAT PANEL LIGHTS TURNED ON. PERFORMED BITE TO BOTH EEC IAW AMM 73-21-00, NO F - [SDR ASMF201509003](https://openairdocs.org/sdr/ASMF201509003), Jul 24, 2015: LINE. LEAKING. DURING TRANSIT CHECK, TECHNICAL PERSONNEL DETECTED SMOKE IN THE LT MLG. PERFORMED REVISION, DETECTING HYD LEAK IN THE LINE MAIN TO BRAKE NR 1. LINE MAIN TO BRAK - [SDR ASMF201509001](https://openairdocs.org/sdr/ASMF201509001), Jul 24, 2015: LINE. LOOSE. DURING TRANSIT CHECK, TECHNICAL PERSONNEL DETECTED SMOKE IN THE LT MLG. PERFORMED REVISION, DETECTING HYD LEAK IN THE LINE MAIN TO BRAKE NR 1. LINE MAIN TO BRAK - [SDR ASMF201506011](https://openairdocs.org/sdr/ASMF201506011), May 14, 2015: WARNING SYSTEM. FALSE ACTIVATION. AIRCRAFT REJECTED TAKEOFF AT 30 KNOTS, DUE TO PSEU LIGHT TURNED ON. ACCOMPLISHED THE QRH 15.4 PROCEDURE & RETURNED TO PLATFORM. PERFORMED RESEAT PSEU TEST IAW A - [SDR ASMF201506008](https://openairdocs.org/sdr/ASMF201506008), May 6, 2015: WARNING SYSTEM. FALSE ACTIVATION. DURING TRANSIT CHECK, AFTER CLOSE THE DOORS, THE RT WING BODY OVERHEATS LIGHT TURNED ON, SO THE FLIGHT CREW ACCOMPLISHED THE QRH 2.23 PROCEDURE, NO CONFIRMING F - [SDR ASMF201503030](https://openairdocs.org/sdr/ASMF201503030), Mar 20, 2015: INDICATION SYS. FAULTY. AIRCRAFT PERFORMED AN UNSCHEDULED LANDING DUE TO LOW FUEL INDICATION. DETECTED FUEL LEAKS IN BOTH ENGS WITHIN LIMITS IAW MM71-71-00. DURING OVERNIGHT CHECK, PER - [SDR ASMF201501003](https://openairdocs.org/sdr/ASMF201501003), Oct 5, 2014: TIP CAP. DAMAGED. DURING TRANSIT CHECK DETECTED DAMAGE IN LE OF THE HORIZONTAL STABILIZER & RETRACTABLE LANDING LIGHT RIGHT, THE ACFT WAS SENT TO HANGAR, REPLACED THE LE OF THE H - [SDR ASMF201407006](https://openairdocs.org/sdr/ASMF201407006), Jun 24, 2014: FILTER. FAILED. DURING TRANSIT CHECK, CAPTAIN REPORTED AN ABNORMAL SMOKE FROM LT WING. PERFORMED REVISION DETECTING CONTAMINATED WITH HYD LIQUID THE LT ENG AIR PURGE SYS PNEUMA - [SDR ASMF201407005](https://openairdocs.org/sdr/ASMF201407005), Jun 23, 2014: RELIEF VALVE. LEAKING. DURING TRANSIT CHECK, CAPTAIN REPORTED AN ABNORMAL FUME & ODOR WITH NO EVIDENCE OF SMOKE IN CABIN CREW. PERFORMED SMOKE OR FUMES IN CABIN CONDITIONAL INSPECTION - [SDR ASMF201312008](https://openairdocs.org/sdr/ASMF201312008), Dec 13, 2013: SHUTOFF VALVE. FAILED. AIRCRAFT REJECTED TAKE OFF AT 50 KNOTS, DUE TO DURING TAKEOFF ROLL THE LT BLEED TRIP OFF LIGHT TURNED ON, SO THE FLIGHT CREW ACCOMPLISHED THE QRH 2.6 PROCEDURE, - [SDR ASMF20131108004](https://openairdocs.org/sdr/ASMF20131108004), Oct 2, 2013: BATTERY PACK. DAMAGED. AIRCRAFT RETURNED TO PLATFORM DUE TO EMERGENCY EXIT LIGHTS TURNED ON WITH SWITCH IN ARM POSITION AND CIRCUIT BREAKER A-11 TRIPPED. DURING MAINTENANCE REVISION, - [SDR ASMF201308002](https://openairdocs.org/sdr/ASMF201308002), Jul 2, 2013: SHUTOFF VALVE. DAMAGED. DURING CLIMB, AIRCRAFT RETURNED, THE LEFT AIR CONDITIONING PACK AND ALL TOILETS OUT OF SERVICE, FLIGHT CREW ACCOMPLISHED THE QRH 2.10 PROCEDURE. MX PERSONNEL RE - [SDR ASMF201306007](https://openairdocs.org/sdr/ASMF201306007), Jun 14, 2013: SKIN. DENTED. DURING TRANSIT CHECK, THE RT FWD SERVICE DOOR WAS DAMAGED, PROMOTING A DENT OF 1.5" LENGTH, 0.020" DEPTH, AT BS 343.2, ON STRINGER 13R. MX PERSONNEL ISSUED THE - [SDR ASMF201306002](https://openairdocs.org/sdr/ASMF201306002), May 31, 2013: LINE. LEAKING. DURING PUSH BACK, DETECTED A HYDRAULIC LEAK IN THE RT MLG LINE, THE LINE WAS TIGHTENED IAW MM 20-10-51, ALL CORRECT. - [SDR ASMF201303001](https://openairdocs.org/sdr/ASMF201303001), Jan 10, 2013: SENSOR. OUT OF LIMITS. ACFT RETURNED TO PLATFORM DUE TO FLAPS WITHOUT MOVEMENT WITH INDICATION LEVER OF 5 UNITS. MX PERSONNEL PERFORMED BITE TO FSEU IAW FIM 27-51 TASK 801 PROCEDURE, - [SDR ASMF201211008](https://openairdocs.org/sdr/ASMF201211008), Nov 18, 2012: SEAL. LEAKING. DURING TRANSIT CHECK, TECH PERSONNEL DETECTED A NLG SHOCK STRUT HYD LEAK; SEALS REPLACED IAW MM 32-21-11, TESTED CORRECT. - [SDR ASMF201211002](https://openairdocs.org/sdr/ASMF201211002), Nov 5, 2012: ENGINE. VIBRATION. CAPTAIN REPORTED THAT DURING ENGINES START, LT ENGINE VIBRATION REACHED 5.01. MX PERSONNEL PERFORMED BITE TO AIRBORNE VIBRATION MONITORING SYSTEM; THE LT ENGINE - [SDR ASMF201203001](https://openairdocs.org/sdr/ASMF201203001), Mar 2, 2012: SWITCH. OUT OF ADJUST. ACFT RETURNED TO DEPARTURE, DURING CLIMB, THE MLG DID NOT RETRACT; SO FLIGHT CREW ACCOMPLISHED THE QRH 14.16 PROCEDURE, CONFIRMING THE FAILURE. ACFT WAS SENT TO - [SDR ASMF201202005](https://openairdocs.org/sdr/ASMF201202005), Feb 11, 2012: BELLCRANK. BROKEN. CAPTAIN REPORTED THAT DURING TAKEOFF, THE ACFT REQUIRED 3 UNITS TO THE LEFT OF RUDDER TRIM. DURING MX REVIEW, THE RT OTBD FLAP, INBD BELLCRANK WAS FOUND BROKEN. - [SDR ASMF201202004](https://openairdocs.org/sdr/ASMF201202004), Feb 5, 2012: FSEU. DAMAGED. CAPTAIN REPORTED THAT DURING APPROACH, FLAPS DID NOT EXTEND, FLIGHT CREW ACCOMPLISHED QRH 9.4 PROCEDURE, CONFIRMING THE FAILURE. MX REPLACED THE FLAP SLAT ELECT - [SDR ASMF201109006](https://openairdocs.org/sdr/ASMF201109006), Sep 13, 2011: PUMP. DAMAGED. CAPTAIN REPORTED THAT DURING APPROACH LANDING GEAR HANDLE HAD NOT MOVED EVEN THROUGH LOCK OVERRIDE HANDLE WAS MOVED; FLIGHT CREW ACCOMPLISHED THE QRH 14.10 PROC - [SDR ASMF201109003](https://openairdocs.org/sdr/ASMF201109003), Sep 3, 2011: ACTUATOR. LEAKING. DURING OVERNIGHT CHECK, A HYD LEAK WAS DETECTED IN THE LT ELEVATOR TAB LOCK ACTUATOR. THE LT ELEVATOR TAB LOCK ACTUATOR WAS REPLACED IAW MM 27-31-34 AND OPS TES - [SDR ASMF201107011](https://openairdocs.org/sdr/ASMF201107011), Jul 18, 2011: STRUCTURE. DAMAGED. DURING TRANSIT CHECK, THE LT AFT CABIN DOOR WAS DAMAGED. MX PERFORMED VISUAL INSPECTION TO LT AFT ENTRY STRUCTURE DOOR IAW MM 52-13-00 DETECTING DAMAGES OUT OF - [SDR ASMF201107009](https://openairdocs.org/sdr/ASMF201107009), Jul 12, 2011: PUMP. DAMAGED. ACFT REJECTED TAKEOFF AT LESS THAN 70 KNOTS WITH GROSS WEIGHT OF 58764 KG DUE TO LEFT ENGINE NOT REACHING THRUST, 101PERCENT REQUIRED, ONLY IT REACHED 90 PERCEN - [SDR ASMF201107008](https://openairdocs.org/sdr/ASMF201107008), Jul 10, 2011: ENGINE. MALFUNCTIONED. ACFT REJECTED TAKEOFF AT 80 KNOTS AND GROSS WEIGHT OF 67 870 KG DUE TO THRUST ASYMMETRY OF 97 PERCENT N2 ON LT ENGINE AND 103 PERCENT N2 ON RT ENGINE AND LT THR ## 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.