# N851AM: 2003 Boeing 737-752, registration cancelled 2018-09-21 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: September 21, 2018 - Exported to: Bermuda - Status when cancelled: Valid registration - Airframe: [Boeing 737-752](https://openairdocs.org/model/boeing-737-752) (registry code 13844C3) - Engine: [CFM International CFM56 series](https://openairdocs.org/engine/cfm-international-cfm56-series) (registry code 13802) - Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (OpenAirDocs) - Serial number: 29363 - Year built: 2003 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: May 5, 2005 - Certificate issued: March 6, 2013 - Last registry action: December 5, 2015 - Mode S code: ABAB1B - Owner when cancelled: [Wilmington Trust Co Trustee](https://openairdocs.org/faa-owner/WILMINGTON%20TRUST%20CO%20TRUSTEE) - Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington) - Owner type: Corporation - Owner's area on the map: 39.7357° N, 75.5321° W: Placed by OpenAirDocs: center of Wilmington, DE, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N851AM - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=851AM - Page: https://openairdocs.org/deregistered/N851AM-2018-09-21 From the FAA registry file of October 29, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Boeing 737-752: https://openairdocs.org/model/boeing-737-752.md ## Service difficulty reports (41) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ASMF20180821002](https://openairdocs.org/sdr/ASMF20180821002), Jun 3, 2018: COMPUTER. FAILED. DURING TRANSIT CHECK, A HYDRAULIC LEAK WAS DETECTED IN THE HYDRAULIC SYSTEM B ON THE FEEL ELEVATOR COMPUTER. MAINTENANCE PERFORMED A REVISION, DETECTING A HYDRA - [SDR ASMF201706003](https://openairdocs.org/sdr/ASMF201706003), Jun 11, 2017: TIRE. PUNCTURED. AIRCRAFT RETURNED TO PLATFORM DURING PUSH BACK, THE NLG WHEEL NUMBER 2 WAS PUNCTURED. MAINTENANCE PERFORMED REVISION IAW AMM 32-45-00, DETECTING NLG WHEEL NUMBE - [SDR ASMF201611013](https://openairdocs.org/sdr/ASMF201611013), Sep 18, 2016: FUEL HEATER. LEAKING. AIRCRAFT RETURNED TO PLATFORM DURING TAXING, A FUEL LEAK WAS DETECTED IN THE LEFT ENGINE. MAINTENANCE PERSONNEL PERFORMED REVISION, DETECTING THE FUEL SERVO HEA - [SDR ASMF201610022](https://openairdocs.org/sdr/ASMF201610022), Sep 18, 2016: FUEL HEATER. LEAKING. AIRCRAFT RETURNED TO PLATFORM DUE TO DURING TAXING, A FUEL LEAK WAS DETECTED IN THE LEFT ENGINE. MAINTENANCE PERSONNEL PERFORMED REVISION, DETECTING THE FUEL SE - [SDR ASMF2016072600001](https://openairdocs.org/sdr/ASMF2016072600001), May 8, 2016: ACTUATOR. LEAKING. DURING TRANSIT CHECK, IT WAS DETECTED A HYDRAULIC LEAK IN THE SPOILER ACTUATOR NUMBER 12. MAINTENANCE PERSONNEL PERFORMED REVISION DETECTING HYDRAULIC LEAK AT S - [SDR ASMF201602002](https://openairdocs.org/sdr/ASMF201602002), Dec 23, 2015: WARNING SYSTEM. FALSE ACTIVATION. AIRCRAFT RETURNED TO PLATFORM DUE TO AFTER START ENGS, THE ELEC LIGHT TURNED ON. PERFORMED ELEC SYS AUTO TEST IAW FIM 34-31 TASK 801, CONFIRMING THE FAILURE, SO - [SDR ASMF201510025](https://openairdocs.org/sdr/ASMF201510025), Sep 30, 2015: WARNING SYSTEM. FALSE ACTIVATION. AIRCRAFT RETURNED TO PLATFORM DUE TO DURING TAXING, THE ELEC LIGHT TURNED ON. PERFORMED RESEAT TO STANDBY POWER IAW AMM 24-21-00, NO CONFIRMING FAILURE, TESTED - [SDR ASMF201510003](https://openairdocs.org/sdr/ASMF201510003), Aug 5, 2015: WARNING SYSTEM. FALSE ACTIVATION. DURING APPROACH WITH FLAPS & LANDING GEARS UP, THE RED LIGHT OF NLG TURNED ON BRIEFLY & ALARM WAS ACTIVE RETURNED TO NORMAL CONDITION AFTER THE EVENTS. PERFORME - [SDR ASMF201509008](https://openairdocs.org/sdr/ASMF201509008), Jul 29, 2015: WINDSHIELD. CRACKED. DURING TRANSIT CHECK, IT WAS DETECTED THE RT WINDSHIELD NR 1 CRACKED. PERFORMED REVISION, DETECTING CRACKS OUT OF LIMITS IAW AMM 56-11-00-210-007. THE RT WINDSH - [SDR ASMF201507013](https://openairdocs.org/sdr/ASMF201507013), Jun 21, 2015: HYDRAULIC LINE. LEAKING. DURING TRANSIT CHECK, A HYD LEAK WAS DETECTED IN THE HYD SYS B OF THE ENG DRIVEN PUMP. PERFORMED REVISION DETECTING HYD LEAK AT HYD SYS B OF THE ENG DRIVEN PUMP - [SDR ASMF201503004](https://openairdocs.org/sdr/ASMF201503004), Jan 18, 2015: HEAT EXCHANGER. LEAKING. AIRCRAFT RETURNED TO PLATFORM DUE TO DURING RT ENG START, AN OIL LEAK WAS DETECTED. PERFORMED REVISION, DETECTING OIL LEAK IN THE OIL & FUEL HEAT EXCHANGER DRAI - [SDR ASMF2014061706014](https://openairdocs.org/sdr/ASMF2014061706014), May 10, 2014: PUMP. LEAKING. DURING OVERNIGHT CHECK, A FUEL LEAK WAS DETECTED IN RT ENG FUEL PUMP OF 40 DROPS PER MINUTE. THE FUEL PUMP WAS REPLACED IAW AMM 73-11-01, TESTED CORRECT. - [SDR ASMF201308017](https://openairdocs.org/sdr/ASMF201308017), Jul 27, 2013: WARNING LIGHT. FALSE ACTIVATION. ACFT RETURNED DUE TO DURING CLIMB THE "EQUIP" LIGHT TURNED ON CROSSING OF 12,000 FT TO 13,000 FT. MX PERSONNEL PERFORMED REVISION TO ELECTRONIC EQUIPMENT ACCESS - [SDR ASMF201306005](https://openairdocs.org/sdr/ASMF201306005), Jun 12, 2013: APU. DAMAGED. DURING TRANSIT CHECK, DETECTED SMOKE AND STRONG NOISE WAS HEARD IN THE APU. MX PERSONNEL PERFORMED REVISION DETECTING INTERNAL DAMAGES IN THE APU; SO THE REPORT - [SDR ASMF201210001](https://openairdocs.org/sdr/ASMF201210001), Sep 11, 2012: ACTUATOR. DAMAGED. CAPTAIN REPORTED THAT DURING APPROACH, THE AILERONS CONTROL FELT HARD. MX PERSONNEL PERFORMED FLIGHT CONTROL TEST, DETECTING THAT THE AILERONS CONTROL DID NOT R - [SDR ASMF201207008](https://openairdocs.org/sdr/ASMF201207008), Jul 26, 2012: ENGINE. MAKING METAL. CAPTAIN REPORTED THAT DURING DESCENT, THE RT ENGINE OIL FILTER BYPASS LIGHT TURNED ON. MX PERSONNEL REMOVED THE FILTER ASSY AND CHIP DETECTOR ABG/TGB, DETECTED - [SDR ASMF201111010](https://openairdocs.org/sdr/ASMF201111010), Nov 14, 2011: SLIDE. UNWANTED DEPLOY. DURING TRANSIT CHECK, A F/A ACTIVATED THE RT DOOR SLIDE. MX REPLACED THE RT DOOR SLIDE IAW MM 25-66-01, ALL CORRECT. - [SDR ASMF201111001](https://openairdocs.org/sdr/ASMF201111001), Oct 23, 2011: CARBON SEAL. LEAKING. DURING TRANSIT CHECK,DETECTED AN OIL LEAK IN THE RT ENGINE HYD PUMP SEAL WITH 118 DROPS PER MINUTE. ACFT WAS SENT TO THE HANGAR AND THE RT ENGINE HYD PUMP CARBO - [SDR ASMF201107004](https://openairdocs.org/sdr/ASMF201107004), Jun 27, 2011: SKIN. DENTED. DURING TRANSIT CHECK, MX DETECTED ONE DENT IN THE RT HORIZ STABILIZER L/E AT STATION 233.30 OF 5.50 X 2.00 INCHES WITH 0.208 INCH DEPTH. INSPECTION PERSONNEL CO - [SDR ASMF201012007](https://openairdocs.org/sdr/ASMF201012007), Dec 6, 2010: BRAKE. DAMAGED. DURING TRANSIT CHECK, TECH DETECTED THE MLG BRAKE NR 2 WITH THE INNER BEARING SEPARATED OF THEIR RETAINING RING AND HUBCAP; ALSO, MLG BRAKE BUSHING DID OUT OF P - [SDR ASMF201012002](https://openairdocs.org/sdr/ASMF201012002), Nov 28, 2010: SHUTOFF VALVE. LEAKING. DURING TRANSIT CHECK, TECH DETECTED A FUEL LEAK IN RT FUELING SHUTOFF VALVE; SO MX CLOSED THE VALVE. MX REPLACED THE RT FUELING SHUTOFF VALVE IAW MM 28-21-51-00 - [SDR ASMF201010006](https://openairdocs.org/sdr/ASMF201010006), Oct 19, 2010: ACTUATOR. LEAKING. CAPTAIN REPORTED THAT DURING CRUISE AND DESCENT, THE CONTROL COLUMN WITH AFT AND FWD MOVEMENT ABOUT 2 INCHES. ACFT WAS SENT TO THE HANGAR AND MX PERFORMED A CON - [SDR ASMF 20081101](https://openairdocs.org/sdr/ASMF%2020081101), Nov 17, 2008: WINDSHIELD. CRACKED. AIRCRAFT RETURNED DUE TO THE LT WINDOW NR 1 CRACKED. MAINT REPLACED THE LT WINDSHIELD ASSY NR 1 AND WINDOW HEAT CONTROL UNIT IAW AMM 56-11-11 AND AMM 30-41-11, - [SDR ASMF200804004](https://openairdocs.org/sdr/ASMF200804004), Apr 22, 2008: CONTROL MODULE. FAILED. CAPTAIN REPORTED THAT LANDING GEAR LEVER DID NOT MOVE UP AFTER TAKE OFF, SO HE PERFORMED ABNORMAL PROCEDURE QRH PAGE 14.4. AIRCRAFT WAS SENT TO THE HANGAR AND M - [SDR ASMF200804002](https://openairdocs.org/sdr/ASMF200804002), Apr 17, 2008: MODULE. FAILED. DURING TAKEOFF, THE (3) LIGHTS OF LANDING GEAR TURNED ON; CAPTAIN PERFORMED AN ADDITIONAL LANDING GEAR CYCLE AND LIGHTS TURNED OFF. MAINT PERFORMED FIM 32-61 TA - [SDR ASMF200803002](https://openairdocs.org/sdr/ASMF200803002), Mar 14, 2008: WINDSHIELD. SCRATCHED. CAPTAIN REPORTED SEVERAL SCRATCHES ON RT WINDSHIELD NR 1. RT WINDSHIELD NR 1 WAS REPLACED IAW MM 56-11-11, TESTED CORRECT. - [SDR ASMF200712003](https://openairdocs.org/sdr/ASMF200712003), Dec 18, 2007: SKIN. DAMAGED. DURING TRANSIT CHECK THE AIRCRAFT WAS HIT BY A BAGGAGE CONVEYOR IN THE LOWER FUSELAGE SKIN AT STATION 807 BETWEEN STRINGER 26R AND 27R; CAUSING A DAMAGE OUT OF - [SDR ASMF200712001](https://openairdocs.org/sdr/ASMF200712001), Dec 9, 2007: WINDOW. CRACKED. CAPTAIN REPORTED THAT LT WINDOW NR 4, CRACKED DURING DESCENT. MAINTENANCE PERSONNEL REPLACED THE WINDOW IAW MM 56-11-31, TESTED CORRECT. - [SDR ASMF200609001](https://openairdocs.org/sdr/ASMF200609001), Sep 1, 2006: CONTROL BOX. FAILED. AIRCRAFT RETURNED TO PLATFORM DURING TAXING ANTISKID INOP LIGHTS TURNED ON. ANTISKID CONTROL BOX DELETED PROCEDURE WAS PERFORMED BUT FAIL CONTINUED AND VALVES C - [SDR ASMF200608010](https://openairdocs.org/sdr/ASMF200608010), Aug 13, 2006: RADOME. DAMAGED. DURING FINAL APPROACH, A HAIL STORM WAS REPORTED BY CAPTAIN AND A MISSED APPROACH WAS PERFORMED. DURING MAINTENANCE REVIEW, THE RADOME WAS DETECTED DAMAGED AND - [SDR ASMF200607013](https://openairdocs.org/sdr/ASMF200607013), Jul 18, 2006: STRUCTURE. GROUND DAMAGE. DURING OVERNIGHT CHECK, AIRCRAFT WAS HIT BY A CARGO CONTAINER, BETWEEN LT LONGERONS 25 AND 26 PRODUCING A DENT OF 5 INCHES OF DIAMETER AND CRACK IN THE CENTER O - [SDR ASMF20060508](https://openairdocs.org/sdr/ASMF20060508), May 17, 2006: SENSOR. FAULTY. AIRCRAFT RETURNED TO PLATFORM, APU WITH LOW PRESSURE. ENGINES WERE STARTED WITH GROUND EQUIPMENT. DURING OVERNIGHT SERVICE, SENSORS P2, PT AND DP WERE REPLACED - [SDR ASMF200604018](https://openairdocs.org/sdr/ASMF200604018), Apr 27, 2006: BLADES. BROKEN. CAPTAIN REPORTED THAT DURING FINAL APPROACH AT VSA IT WAS A BIRD STRIKE ON THE RIGHT SIDE OF THE AIRCRAFT. THE RT ENGINE WAS INSPECTED, CLEANED AND OPERATIONAL - [SDR ASMF200603004](https://openairdocs.org/sdr/ASMF200603004), Mar 9, 2006: WARNING LIGHT. ILLUMINATED. AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURING TAXI, PSEU LIGHT TURNED ON. BREAKERS P6-3, D1 AND D2 WERE RESEATED AND LIGHT TURNED OFF. DURING RIGHT E - [SDR ASMF200601013](https://openairdocs.org/sdr/ASMF200601013), Jan 19, 2006: BLEED AIR SYS. MALFUNCTIONED. AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURING PUSH BACK, THE BLEED APU WITH 12 PSI INDICATION. THE ENGINES WERE STARTED WITH EXTERNAL PNEUMATIC PLANT - [SDR ASMF200601005](https://openairdocs.org/sdr/ASMF200601005), Jan 12, 2006: APU. FAILED. AIRCRAFT RETURNED TO PLATFORM DURING ENGINES STARTING, LOW PNEUMATIC INDICATION PRESSURE IN THE APU. THE ENGINES WERE STARTED WITH EXTERNAL PNEUMATIC PLANT IAW - [SDR ASMF200601002](https://openairdocs.org/sdr/ASMF200601002), Jan 4, 2006: HYDRAULIC SYSTEM. LEAKING. CAPTAIN REPORTED THAT DURING TAKE OFF WHEN THE LANDING GEARS WAS RETRACTED, THE LT HYDRAULIC QUANTITY INDICATION FELT FROM 105 PERCENT TO 74 PERCENT; REDUCING D - [SDR ASMF200511004](https://openairdocs.org/sdr/ASMF200511004), Nov 5, 2005: APU. FAILED. DURING ENGINES STARTING, THE PNEUMATIC AUXILIARY POWER UNIT FAILED. THE ENGINES WERE STARTED WITH EXTERNAL PNEUMATIC PLANT IAW MM 49-11-00, TESTED CORRECT. THE - [SDR ASMF200510014](https://openairdocs.org/sdr/ASMF200510014), Oct 29, 2005: PUMP. FAILED. CAPTAIN REPORTED LOSS OF HYDRAULIC FLUID IN LT SIDE. DURING REVISION DETECTED A LEAK IN LT MAIN PUMP, SO IT WAS REPLACED IAW MM 29-11-11 AC WAS DISPATCHED. AC R - [SDR ASMF200506018](https://openairdocs.org/sdr/ASMF200506018), Jun 17, 2005: EEC. FAILED. ACFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURING RT ENGINE STARTING, ENGINE SHUT OFF BY ITSELF AT 20 PERCENT, STAR VALVE INDICATION FLASHING AND LOW OIL PRE - [SDR ASMF200506008](https://openairdocs.org/sdr/ASMF200506008), Jun 5, 2005: WARNING LIGHT. ILLUMINATED. AIRCRAFT RETURNED TO PLATFORM, RT ENGINE LOW OIL PRESSURE INDICATION DURING TAXING. RAN ENG CONNECTOR AND SWAP / CHANGE TRANSMITTER CHANNEL WERE CLEANED IAW MM ## Other aircraft with N851AM - [Registered now](https://openairdocs.org/aircraft/N851AM): Amazon.Com Services MK30, S/N 178650109P --- 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.