# N997AM: Boeing 737-76Q - Status: Valid registration - Airframe: [Boeing 737-76Q](https://openairdocs.org/model/boeing-737-76q) (registry code 13845AA, 149 seats) - Serial number: 30283 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Certificate issued: September 4, 2019 - Expires: September 30, 2029 - Mode S code: ADECB0 - Registered owner: [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%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 is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=997AM - Page: https://openairdocs.org/aircraft/N997AM From the FAA registry file of October 22, 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 (Boeing 737-76Q) None in force. ## Information bulletins (advisory) None matched. ## NTSB investigations None matched to N997AM. ## FAA accident and incident reports None matched to N997AM. ## Service difficulty reports (61, newest 50) As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ASMF202101023](https://openairdocs.org/sdr/ASMF202101023), Jan 22, 2021: SKIN. CRACKED. DURING 8A-P CHECK AT MEX STATION, IT WAS DETECTED SEVERAL CRACKS AT BOTH HORIZONTAL STABILIZERS. MAINTENANCE PERSONNEL PERFORMED A REVISION, DETECTING A CRACK O - [SDR ASMF202101013](https://openairdocs.org/sdr/ASMF202101013), Dec 17, 2020: FILTER. LEAKING. DURING TRANSIT CHECK, A HYDRAULIC LEAK WAS DETECTED IN THE HYDRAULIC SYSTEM B. MAINTENANCE PERSONNEL PERFORMED REVISION DETECTING HYDRAULIC LEAK AT IN ACOUSTIC - [SDR ASMF202011015](https://openairdocs.org/sdr/ASMF202011015), Oct 1, 2020: ACOUSTIC PANEL. DAMAGED. DURING TRANSIT CHECK, IT WAS DETECTED SEVERAL NICKS ON RIGHT ENGINE INNER BARREL ACOUSTIC PANEL. MAINTENANCE PERSONNEL PERFORMED A REVISION, DETECTING A NICK OF - [SDR ASMF202011012](https://openairdocs.org/sdr/ASMF202011012), Sep 29, 2020: ACOUSTIC PANEL. DAMAGED. DURING OVERNIGHT CHECK AT MEX STATION, IT WAS DETECTED SEVERAL DENTS AND A NICK ON BOTH ENGINES INNER BARREL ACOUSTIC PANEL INLET COWL. MAINTENANCE PERSONNEL PE - [SDR ASMF2019100909](https://openairdocs.org/sdr/ASMF2019100909), Aug 23, 2019: DRAIN LINE. LEAKING. DURING RIGHT ENGINE TEST RUNNING, MAINTENANCE PERSONNEL DETECTED AN OIL LEAK AT RIGHT ENGINE. PERFORMED REVISION, DETECTING A RIGHT ENGINE OIL LEAK ON AGB/TGB D - [SDR ASMF201910004](https://openairdocs.org/sdr/ASMF201910004), Jul 24, 2019: BLEED AIR SYS. TRIPPED. AIRCRAFT PERFORMED AN UNSCHEDULED LANDING AT GDL DUE TO DURING DESCENT AT 14,000 FEET, THE RH PACK AND LH BLEED TRIP OFF LIGHTS TURNED ON AND OXYGEN MASK DEPLOY - [SDR ASMF2018101509024](https://openairdocs.org/sdr/ASMF2018101509024), Sep 28, 2018: SEAL. LEAKING. FUEL LEAK ON LT ENGINE. DURING TRANSIT CHECK, A FUEL LEAK WAS DETECTED ON LT ENGINE. MAINTENANCE PERSONNEL PERFORMED LEAKING ENGINE INSPECTION IAW AMM 71-00-00- - [SDR ASMF20180927020](https://openairdocs.org/sdr/ASMF20180927020), Sep 13, 2018: MONITOR. FAILED. AIRCRAFT RETURNED TO PLATFORM DUE THAT DURING TAXING THE RT ENGINE VIBRATION REACHED 5.2 UNITS. MAINTENANCE PERSONNEL PERFORMED VIBRATION ANALYSIS IAW FIM 77-31 - [SDR ASMF20180927019](https://openairdocs.org/sdr/ASMF20180927019), Sep 12, 2018: TRANSMITTER. FAILED. CAPTAIN REPORTED THAT DURING LANDING, THE FLAPS TRAILING EDGE DOESN´T OPERATE WITH PRIMARY CONTROL. FLIGHT CREW ACCOMPLISHED THE QRH 9.18 PROCEDURE CONTINUING T - [SDR ASMF20171005004](https://openairdocs.org/sdr/ASMF20171005004), Sep 11, 2017: ACTUATOR. LEAKING. DURING OVERNIGHT CHECK, IT WAS DETECTED A LEAKAGE IN HYDRAULIC LOWER ACTUATOR AT ENGINE 1, THEREFORE MAINTENANCE PERSONNEL REPLACED LEFT ENGINE THRUST REVERSER - [SDR ASMF201612018](https://openairdocs.org/sdr/ASMF201612018), Dec 25, 2016: BATTERY PACK. DISCHARGED. DURING TRANSIT CHECK, FLOOR EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE DETECTED THE BATTERY PACK DISCHARGED IAW AMM 33-51-00. THE BATTERY PACK WAS CHARGED I - [SDR ASMF2016072600007](https://openairdocs.org/sdr/ASMF2016072600007), May 20, 2016: ENGINE. MAKING METAL. DURING TRANSIT CHECK, THE APU SHUTDOWN SUDDENLY, THE APU FAIL LIGHT TURNED ON AND FAILURE CODE 49-94299. MAINTENANCE PERSONNEL PERFORMED FIM 49-90 TASK 809 PROC - [SDR ASMF201605012](https://openairdocs.org/sdr/ASMF201605012), Apr 9, 2016: PIN. DAMAGED. AIRCRAFT RETURNED OF FLIGHT DUE TO DURING CLIMB, WHEN ACTION TO LG UP LEVER IT WAS NOT UNABLE TO MOVE UP THE LEVER & THE PSEU LIGHT TURNED ON. ACCOMPLISHED THE - [SDR ASMF201605011](https://openairdocs.org/sdr/ASMF201605011), Apr 8, 2016: CIRCUIT BREAKER. FAILED. AIRCRAFT RETURNED OF FLIGHT DUE TO DURING CLIMB, THE CONFIGURATION ALARM WAS ACTIVE, TAKEOFF CONFIGURATION LIGHT TURNED ON & TAKEOFF WARNING HORN SOUNDED. PERFO - [SDR ASMF201605010](https://openairdocs.org/sdr/ASMF201605010), Apr 7, 2016: WARNING SYSTEM. FALSE ACTIVATION. DURING CRUISE THE TAKEOFF CONFIGURATION LIGHT TURNED ON & TAKEOFF WARNING HORN SOUNDED. PERFORMED TAKEOFF WARNING SYS TEST IAW AMM 31-51-00-730-803 & FIM 31-51 - [SDR ASMF201511010](https://openairdocs.org/sdr/ASMF201511010), Nov 16, 2015: BATTERY PACK. DISCHARGED. DURING TRANSIT CHECK, SOME FLOOR EMER LIGHTS WERE OUT OF SERVICE. PERFORMED REVISION DETECTING THE BATTERY PACK FAILED. THE BATTERY PACK WAS REPLACED IAW AMM 33 - [SDR ASMF201511007](https://openairdocs.org/sdr/ASMF201511007), Nov 7, 2015: UNKNOWN. MALFUNCTIONED. CAPTAIN REPORTED THAT DURING CLIMB, WHEN ACTION TO LG UP LEVER, IT WAS UNABLE TO MOVE UP POSITION THE LEVER BEING NECESSARY MOVE UP WITH OVERRIDE LOCK. ACFT WAS - [SDR ASMF201507021](https://openairdocs.org/sdr/ASMF201507021), Jul 17, 2015: PRESSURE SWITCH. FAILED. DURING TRANSIT CHECK, DURING PREFLIGHT PROCEDURE THE FLIGHT CONTROL LOW PRESSURE LIGHT TURNED OFF IN THE CHANNEL B. PERFORMED FIM 27-21 TASK 814 PROCEDURE, DETE - [SDR ASMF201506004](https://openairdocs.org/sdr/ASMF201506004), Apr 28, 2015: FUEL FILTER. FAILED. AIRCRAFT RETURNED TO PLATFORM DUE TO DURING TAXING, THE RT ENG OIL FILTER BY PASS LIGHT TURNED ON & THE LT ENG CONTROL LIGHT TURNED ON. PERFORMED BITE TO EEC IA - [SDR ASMF201503029](https://openairdocs.org/sdr/ASMF201503029), Mar 19, 2015: MOTOR. FAILED. AIRCRAFT REJECTED TAKEOFF AT 65 KNOTS DUE TO AUTO THROTTLE OSCILLATIONS IN THRUST LEVER 1. AT PLATFORM, AUTO THROTTLES TEST WAS PERFORMED IAW FIM 22-31 TASK 801 - [SDR ASMF201409007](https://openairdocs.org/sdr/ASMF201409007), Aug 15, 2014: TRANSCEIVER. DAMAGED. CAPTAIN REPORTED THAT BOTH DME’S OUT OF SERVICE. PERFORMED REVISION DETECTING A LIGHTNING STRIKE IN THE DME ANTENNA & A LIGHTNING STRIKE INSPECTION WAS PERFORME - [SDR ASMF2014061806015](https://openairdocs.org/sdr/ASMF2014061806015), May 13, 2014: LINKAGE. OUT OF ADJUST. CAPTAIN REPORTED THAT DURING DESCENT TO EXTEND THE SPEED BRAKES, THE RT SPOILERS HIGHER THAN LT SPOILERS. ACFT WAS SENT TO THE HANGAR & PERFORMED ADJUSTMENT OF - [SDR ASMF2014061706006](https://openairdocs.org/sdr/ASMF2014061706006), Apr 15, 2014: BATTERY PACK. BURNED. AIRCRAFT RETURNED TO PLATFORM DUE TO AFTER ENGS START, THE CB P18-3 POS A11 WAS POPPED & AN ELEC CABLE BURNED ODOR WITH NO EVIDENCE OF SMOKE. DURING REVISION, T - [SDR ASMF201403011](https://openairdocs.org/sdr/ASMF201403011), Feb 28, 2014: SPOILER. OUT OF ADJUST. CAPTAIN REPORTED THAT DURING DESCENT, TO EXTEND THE SPEED BRAKES ACFT ROLLED APPROXIMATELY 2 UNITS TO RT. ACFT SENT TO THE HANGAR & MX PERFORMED ADJUSTMENT OF S - [SDR ASMF201310009](https://openairdocs.org/sdr/ASMF201310009), Sep 28, 2013: PUMP. LEAKING. DURING RT ENGINE TEST, MAINTENANCE DETECTED FUEL LEAK OF 80 DROPS PER MINUTE IN THE FUEL PUMP PAD DRAIN DURING IDLE POWER OPERATION; SO THE RT ENGINE FUEL PUMP - [SDR ASMF201310006](https://openairdocs.org/sdr/ASMF201310006), Sep 20, 2013: WARNING LIGHT. ILLUMINATED. CAPTAIN REPORTED THAT BEFORE TAXING, STANDBY RUDDER LIGHT ILLUMINATED. MAINTENANCE PERFORMED THE FIM 27-21-94, TASK 817 PROCEDURE, NO FAILURE FOUND. STANDBY RUD - [SDR ASMF201305004](https://openairdocs.org/sdr/ASMF201305004), Apr 25, 2013: WARNING LIGHT. FALSE ACTIVATION. CAPTAIN REPORTED THAT DURING TAKEOFF ROLL, THE PSEU LIGHT TURNED ON. MX PERSONNEL PERFORMED THE FIM 32-09, TASK 801 PROCEDURE, NO FAILURE WAS FOUND. CIRCUIT BRA - [SDR ASMF201301002](https://openairdocs.org/sdr/ASMF201301002), Jan 2, 2013: SNUBBER. BENT. DURING TRANSIT CHECK, TECH DETECTED FORWARD ENTRY DOOR WITH DIFFICULT TO CLOSE DUE TO A BEND IN THE LOWER PERIPHERY OF THE CAVITY ACTUATOR; SO THE FORWARD ENTRY - [SDR ASMF201212014](https://openairdocs.org/sdr/ASMF201212014), Dec 27, 2012: PACKING. DAMAGED. AIR RETURN, DURING CLIMB, RT ENGINE LOW OIL QTY AND LOW OIL PRESS INDICATIONS. RT ENGINE SHUTDOWN AND ACCOMPLISHED QRH 7.21 PROCEDURE. REPLACED RT ENGINE CRACKI - [SDR ASMF201212010](https://openairdocs.org/sdr/ASMF201212010), Dec 23, 2012: VALVE. LEAKING. DURING LT ENGINE START, A FUEL LEAK WAS DETECTED WITH 52 DROPS PER MINUTE. MX PERFORMED REVISION DETECTING THE HPTCCV VALVE DRAIN WITH LEAK WITHIN OPERATION LIM - [SDR ASMF201208002](https://openairdocs.org/sdr/ASMF201208002), Aug 1, 2012: SHUTOFF VALVE. MALFUNCTIONED. DURING FUELING, A FUEL SPILLAGE IN THE LT TANK WAS DETECTED DUE TO THE SHUTOFF VALVE FAILURE. PLATFORM WAS CLEANED AND MX CLOSED THE VALVE MANUALLY. SHUTOFF VAL - [SDR ASMF20111209004](https://openairdocs.org/sdr/ASMF20111209004), Dec 9, 2011: ACTUATOR. LEAKING. DURING TRANSIT CHECK, DETECTED A FUEL LEAK IN RT ENGINE WITH 94 DROPS PER MINUTE. MX DETECTED ACTUATOR DRAIN LINE VSVS WITHIN OPERATION LIMITS IAW MM 75-31-00. - [SDR ASMF201110004](https://openairdocs.org/sdr/ASMF201110004), Oct 14, 2011: PUMP. LEAKING. DURING TRANSIT CHECK, A FUEL LEAK IN THE RT ENGINE WITH 60 DROPS PER MINUTE. MX PERSONNEL PERFORMED REVISION DETECTING THE RT FUEL PUMP WITH LEAK WITHIN OPERATI - [SDR ASMF201110003](https://openairdocs.org/sdr/ASMF201110003), Oct 9, 2011: BLEED VALVE. LEAKING. DURING TRANSIT CHECK, DETECTED A FUEL LEAK IN THE RT ENGINE WITH 60 DROPS PER MINUTE. MX PERSONNEL PERFORMED REVISION DETECTING THE TRANSIENT BLEED VALVE WITH L - [SDR ASMF201108003](https://openairdocs.org/sdr/ASMF201108003), Aug 13, 2011: SKIN. DENTED. ACFT ARRIVED WITH A DENT AFT OF CARGO DOOR ON FUSELAGE SKIN AT BS 842, BETWEEN STRINGERS 18 AND 19 RT. INSP PERSONNEL EVALUATED THE DAMAGE AND FOUND IT WITHIN L - [SDR ASMF201009010](https://openairdocs.org/sdr/ASMF201009010), Sep 25, 2010: TRANSMITTER. DAMAGED. DURING APPROACH, THE T/E FLAPS ASYMMETRY LIGHT TURNED ON WHEN FLIGHT CREW SELECTED FLAPS 5 GRADE, DISCONNECTING THE YAW DAMPER; SO THE FLIGHT CREW PERFORMED THE - [SDR ASMF201009009](https://openairdocs.org/sdr/ASMF201009009), Sep 19, 2010: FSEU. DAMAGED. DURING APPROACH, THE L/E FLAPS TRANSIT LIGHT WAS SHOWN WHEN FLIGHT CREW SELECTED FLAPS 1 GRADE, SO THE FLIGHT CREW PERFORMED THE QRH 9.12 PROCEDURE LANDING WITH - [SDR ASMF201009006](https://openairdocs.org/sdr/ASMF201009006), Sep 14, 2010: VALVE. DAMAGED. DURING APPROACH, THE T/E FLAPS ASYMMETRY LIGHT WAS SHOWN WHEN FLIGHT CREW SELECTED FLAPS 1 GRADE, DISCONNECTING THE YAW DAMPER, SO THE FLIGHT CREW PERFORMED THE - [SDR ASMF201004004](https://openairdocs.org/sdr/ASMF201004004), Apr 20, 2010: HEATER. LEAKING. DURING TRANSIT CHECK, A FUEL LEAK WAS DETECTED IN THE RT ENGINE. ACFT WAS SENT TO THE HANGAR AND MX PERSONNEL PERFORMED AN ENGINE RUN TEST IAW MM 71-00-00, CONF - [SDR ASMF201002002](https://openairdocs.org/sdr/ASMF201002002), Jan 29, 2010: WARNING LIGHT. ILLUMINATED. CAPTAIN REPORTED THAT DURING CLIMB THE LT "BLEED TRIP OFF" LIGHT TURNED ON, SO IT TURNED OFF AFTER ABNORMAL PROCEDURE WAS ACCOMPLISHED. THE OVER SPEED WARNING A - [SDR ASMF200910003](https://openairdocs.org/sdr/ASMF200910003), Oct 12, 2009: DOOR. UNKNOWN. ACFT RETURNED DUE TO A HEAVY NOISE IN THE FWD ENTRY DOOR AND THE ACFT DID NOT PRESSURIZE; ADDITIONALLY, THE FWD ENTRY DOOR LIGHT DOES NOT TURNED ON. MX PERFORME - [SDR ASMF20090904](https://openairdocs.org/sdr/ASMF20090904), Sep 21, 2009: VALVE. FAILED. DURING TRANSIT CHECK, MX DETECTED A FUEL LEAK IN THE DRAIN OF THE RT ENGINE. THE FUEL LEAK INSP WAS PERFORMED DETECTING THE LEAK AT THE VALVE HPTCC, SO IT WAS P - [SDR ASMF200909003](https://openairdocs.org/sdr/ASMF200909003), Sep 4, 2009: WHEEL. DAMAGED. CAPTAIN REPORTED THAT AFTER LANDING ROLL THE AIRCRAFT WAS UNABLE TO MOVE BEING NECESSARY TO ADD THRUST, HEARING A STRONG NOISE. AT PLATFORM, MAINTENANCE PERSONN - [SDR ASMF200805003](https://openairdocs.org/sdr/ASMF200805003), May 23, 2008: SELECTOR VALVE. FAILED. CAPTAIN REPORTED THAT DURING CRUISE AT 39,000 FEET, THE MAIN LANDING GEAR RED LIGHT TURNED ON AND MAIN LANDING GEAR GO DOWN WITH LEVER IN OFF POSITION, THEN LEV - [SDR ASMF200805002](https://openairdocs.org/sdr/ASMF200805002), May 20, 2008: SENSOR. FAILED. AIRCRAFT RETURNED TO PLATFORM, DUE TO LE FLAPS TRANSIT LIGHT TURNED ON AND TAKEOFF WARNING ACTIVATED. MAINT PERFORMED BITE TO PSEU AND FSEU IAW FIM 32-09 TASK 8 - [SDR ASMF200804001](https://openairdocs.org/sdr/ASMF200804001), Apr 6, 2008: SKIN. DENTED. DURING TRANSIT CHECK, A BIRD STRIKE WAS DETECTED IN THE LT WING LEADING EDGE. MAINT PERFORMED A BIRD STRIKE INSPECTION IAW MM 05-51-18 DETECTING A DENT OF 0.562 - [SDR ASMF200710006](https://openairdocs.org/sdr/ASMF200710006), Oct 22, 2007: PITOT HEAD. WARNING MESSAGE. AIRCRAFT RETURNED TO PLATFORM, THE RT ELEVATOR PITOT LIGHT TURNED ON. MAINTENANCE PERSONNEL REPLACED THE PITOT PROBE RT ELEVATOR IAW MM 27-31-94 AND TESTED CORR - [SDR ASMF200709009](https://openairdocs.org/sdr/ASMF200709009), Sep 23, 2007: WINDOW. CRACKED. DURING TRANSIT CHECK, THE RT FIRST OFFICER LATERAL WINDOW GLASS CRACKED AND IT WAS EXTREMELY HOT. MAINTENANCE PERSONNEL REPLACED THE WINDOW IAW MM 56-12-11, TES - [SDR ASMF200709006](https://openairdocs.org/sdr/ASMF200709006), Sep 21, 2007: SLEEVE. DAMAGED. CAPTAIN REPORTED LIGHTNING ACTIVITY NEAR TO THE AIRCRAFT DURING FLIGHT; AT GDL PLATFORM, TECHNICAL PERSONNEL DETECTED A LIGHTNING STRIKE DAMAGE IN THE LT ENGINE - [SDR ASMF200704007](https://openairdocs.org/sdr/ASMF200704007), Apr 10, 2007: VALVE. FAILED. AIRCRAFT AIR-TURNED BACK DUE TO RT ENGINE BLEED TRIP OFF LIGHT, TURNED ON. AT CUU, TECH PERSONNEL DEFERRED REPORT IAW MEL 36-8. DURING OVERNIGHT CHECK; RT HIGH All 61: https://openairdocs.org/aircraft/N997AM/reports.md ## STCs that may be installed (OpenAirDocs) None matched to this aircraft's models. ## Related - Other Boeing 737-76Q aircraft: https://openairdocs.org/model/boeing-737-76q/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.