# N423AM: 2004 Boeing 737-73V, registration cancelled 2019-05-13 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: May 13, 2019 - Status when cancelled: Valid registration - Airframe: [Boeing 737-73V](https://openairdocs.org/model/boeing-737-73v) (registry code 1384540) - Engine: [CFM International CFM56-7B22 series](https://openairdocs.org/engine/cfm-international-cfm56-7b22-series) (registry code 13043) - Serial number: 32423 - Year built: 2004 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: February 25, 2011 - Certificate issued: February 25, 2011 - Last registry action: October 26, 2018 - Mode S code: A506D0 - Owner when cancelled: [Wells Fargo Trust Co Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20TRUST%20CO%20NA%20TRUSTEE) - Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City) - Owner type: Corporation - Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N423AM - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=423AM - Page: https://openairdocs.org/deregistered/N423AM-2019-05-13 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 737-73V: https://openairdocs.org/model/boeing-737-73v.md ## Service difficulty reports (23) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ASMF20180918001](https://openairdocs.org/sdr/ASMF20180918001), Jul 8, 2018: WARNING SYSTEM. FALSE ACTIVATION. AIRCRAFT RETURNED OF FLIGHT DUE TO DURING CLIMB MAP FLAG AND TCAS OFF APPEARED ON MFD. MAINTENANCE PERSONNEL PERFORMED FAULT ISOLATION PROCEDURE TO TCAS IAW FIM - [SDR ASMF20180821004](https://openairdocs.org/sdr/ASMF20180821004), Jun 14, 2018: WARNING MESSAGE. ILLUMINATED. AIRCRAFT REJECTED TAKEOFF WHEN TO/GA WAS PRESSED, THE TAKEOFF CONFIGURATION SOUNDS AND PSEU LIGHTTURNED ON. MAINTENANCE PERSONNEL PERFORM THE FIM 32-09 TASK 801 - [SDR ASMF20180625002](https://openairdocs.org/sdr/ASMF20180625002), Apr 22, 2018: HMU. LEAKING. DURING RIGHT ENGINE RUN DURING OVERNIGHT CHECK, A FUEL LEAK WAS DETECTED ON THE RIGHT ENGINE, BETWEEN FUEL PUMP AND HMU. THE FUEL PUMP AND HMU WERE REPLACED IAW - [SDR ASMF20180515011](https://openairdocs.org/sdr/ASMF20180515011), Apr 22, 2018: FUEL. LEAKING. DURING RIGHT ENGINE RUN IN OVERNIGHT CHECK, A FUEL LEAK WAS DETECTED. MAINTENANCE PERSONNEL PERFORMED A REVISION DETECTING FUEL LEAK ON RIGHT ENGINE BETWEEN FUE - [SDR ASMF20180515009](https://openairdocs.org/sdr/ASMF20180515009), Apr 7, 2018: WIRE HARNESS. DAMAGED. AIRCRAFT RETURNED DURING CLIMB AT FL 300 FT, THE RIGHT ENGINE REACHED 934 CELSIUS WITH AN EGT AMBER LIGHT AND VIBRATION IN THE AIRCRAFT. PERFORMED THE MCDU /EEC - [SDR ASMF20170630007](https://openairdocs.org/sdr/ASMF20170630007), Jun 25, 2017: TRANSMITTER. FAILED. CAPTAIN REPORTED THAT DURING APPROACH, TRAILING EDGE FLAP ASYMMETRY OCCURED WITH FLAP LEVER AT 30 AND FLAP INDICATION 25, FLIGHT CREW ACCOMPLISHED THE QRH 9.28 - [SDR ASMF201606007](https://openairdocs.org/sdr/ASMF201606007), Apr 30, 2016: ACTUATOR. LOOSE. CAPTAIN REPORTED THAT DURING CRUISE, THE ACFT REQUIRED 4 UNITS OF COMPENSATION TO LT FOR MAINTAINING THE ACFT STRAIGHT AND LEVEL. MAINTENANCE PERSONNEL PERFORME - [SDR ASMF201510030](https://openairdocs.org/sdr/ASMF201510030), Oct 13, 2015: SKIN. DENTED. DURING OVERNIGHT CHECK, IT WAS DETECTED A BIRD STRIKE IN THE RT HORIZONTAL STABILIZER LE. PERFORMED A BIRD STRIKE CONDITIONAL INSPECTION IAW AMM 05-51-18, DETEC - [SDR ASMF201507017](https://openairdocs.org/sdr/ASMF201507017), Jun 28, 2015: IDG. FAILED. AIRCRAFT RETURNED TO PLATFORM, AFTER BOTH ENG STARTS, THE RT ENG GEN DID SHUTDOWN. REVISION DETECTING RT IDG FAILED, SO THE RT IDG WAS DEFERRED IAW MEL 24-1-2 C - [SDR ASMF201507007](https://openairdocs.org/sdr/ASMF201507007), Jun 6, 2015: IGNITER BOX. FAILED. CAPTAIN REPORTED THAT DURING START ENGINES, THE LT ENGINE IGNITION FAILED WITHOUT EGT. DURING TRANSIT CHECK THE LT ENGINE IGNITION BOX WAS REPLACED IAW AMM 74-2 - [SDR ASMF201403008](https://openairdocs.org/sdr/ASMF201403008), Feb 24, 2014: UNKNOWN. VIBRATION. CAPTAIN REPORTED THAT DURING TAKEOFF, A VIBRATION WAS HAD IN THE NLG. MX PERFORMED A NLG REVISION IAW MM 32-00-00, NO FAILURES DETECTED. AS A PRECAUTIONARY ACTI - [SDR ASMF201312006](https://openairdocs.org/sdr/ASMF201312006), Dec 3, 2013: WARNING SYSTEM. FALSE ACTIVATION. AIRCRAFT REJECTED TAKE OFF AT 70 KNOTS WITH 51,000 KG WEIGHT, DUE TO CONFIGURATION ALARM SHOWED. PERFORMED BITE TO PSEU IAW AMM 32-09-10, NO FAILURE CODE WAS SH - [SDR ASMF20130523006](https://openairdocs.org/sdr/ASMF20130523006), Apr 29, 2013: WARNING MESSAGE. FALSE ACTIVATION. AIRCRAFT RETURNED TO PLATFORM, TAKEOFF CONFIGURATION ALARM WAS ACTIVE. MX PERSONNEL PERFORMED TAKEOFF WARNING SYSTEM TEST IAW AMM 31-51-00-730-803, SHOWING FAIL - [SDR ASMF201305002](https://openairdocs.org/sdr/ASMF201305002), Apr 19, 2013: SENSOR. DAMAGED. CAPTAIN REPORTED THAT DURING APPROACH, T/E FLAPS ASYMMETRY LEVER DID NOT COMMAND, FLIGHT CREW ACCOMPLISHED QRH 9.28 PROCEDURE, LANDING WITH SLATS DOWN AND FLAPS - [SDR ASMF201303022](https://openairdocs.org/sdr/ASMF201303022), Mar 8, 2013: WARNING LIGHT. FALSE ACTIVATION. ACFT REJECTED TAKEOFF AT 75 KNOTS DUE TO LT OVERWING DOOR LIGHT ILLUMINATED. NO DAMAGE FOUND TO AIRCRAFT. - [SDR ASMF201303018](https://openairdocs.org/sdr/ASMF201303018), Feb 15, 2013: GEARBOX. DAMAGED. CAPTAIN REPORTED THAT FLAPS AND SLATS DO NOT RETRACT. MX PERSONNEL DETECTED THE RT FLAPS ANGLE GEAR BOX DAMAGED. THE GEAR BOX WAS REPLACED IAW AMM 27-51-55 AND - [SDR ASMF201303002](https://openairdocs.org/sdr/ASMF201303002), Jan 12, 2013: UNKNOWN. VIBRATES. THE ACFT TO LANDING DUE TO A STRONG NOISE AND VIBRATION IN THE NLG AND RT TREND. MX PERSONNEL PERFORMED A NLG REVISION IAW MM 32-00-00, NO DETECTING FAILURE. AS - [SDR ASMF20121012003](https://openairdocs.org/sdr/ASMF20121012003), Sep 15, 2012: ACTUATOR. LEAKING. CAPTAIN REPORTED THAT DURING TAXING AFTER LANDING, THE NOSE STEERING WAS PARTIALLY BLOCKED. MX PERSONNEL PERFORMED THE FIM 32-51 TASKS 807 AND 808 PROCEDURE, DE - [SDR ASMF201205008](https://openairdocs.org/sdr/ASMF201205008), May 17, 2012: SKIN. DAMAGED. DURING TRANSIT CHECK WAS DETECTED A LIGHTNING STRIKE IN RT ENGINE. MX PERSONNEL PERFORMED A LIGHTNING STRIKE CONDITIONAL INSPECTION IAW MM 05-51-19, FOUND DAMAG - [SDR ASMF2011102811004](https://openairdocs.org/sdr/ASMF2011102811004), Oct 28, 2011: PITOT TUBE. OBSTRUCTED. ACFT REJECTED TAKEOFF AT 105 KNOTS DUE TO DIFFERENCE OF 55 KNOTS BETWEEN THE AIRSPEED INDICATORS OF THE CREW. ACFT WAS SENT TO THE HANGAR AND DURING MX REVISION - [SDR ASMF201105002](https://openairdocs.org/sdr/ASMF201105002), Apr 30, 2011: PUMP. DAMAGED. CAPTAIN REPORTED THAT BEFORE ENGINES WERE STARTED, WHEN SWITCH TURNED ON, THE LT CTR FUEL PUMP LOW PRESSURE LIGHT TURNED ON. AFT WAS SENT TO THE HANGAR AND MX P - [SDR ASMF201104003](https://openairdocs.org/sdr/ASMF201104003), Apr 7, 2011: WINDSHIELD. CRACKED. ACFT PERFORMED AN UNSCHEDULED LANDING, DUE TO RT FWD WINDSHIELD BROKEN. FLIGHT CREW PERFORMED THE QRH 1.14 PROCEDURE, CONFIRMING THE FAILURE. MX PERSONNEL REPLA - [SDR ASMF201103001](https://openairdocs.org/sdr/ASMF201103001), Mar 7, 2011: MOTOR. DAMAGED. CAPTAIN REPORTED THAT DURING CRUISE THE STAB OUT OF TRIM LIGHT TURNED ON MOMENTARY, LATER DURING DESCENT IT CAME ON STEADY, HAVING THE ELECTRICAL MOTOR ACTUATOR ## Other aircraft with N423AM - [Registered now](https://openairdocs.org/aircraft/N423AM): Amazon.Com Services MK30, S/N 178650107P --- 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.