# Service difficulty reports: N997AM

A list on [N997AM](https://openairdocs.org/aircraft/N997AM.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 2 · 61 reports

- [SDR ASMF202101023](https://openairdocs.org/sdr/ASMF202101023.md): Skin · cracked · Jan 22, 2021 · N997AM · Boeing 73776Q · Horizontal Stabilizer, Plate/Skin
  > DURING 8A-P CHECK AT MEX STATION, IT WAS DETECTED SEVERAL CRACKS AT BOTH HORIZONTAL STABILIZERS. MAINTENANCE PERSONNEL PERFORMED A REVISION, DETECTING A CRACK OF 3.5" LENGTH AT STAB STA 101.90 AND 0.5" DISTANCE FROM REAR SPAR; A CRACK OF 1.00" LENGTH AT STAB S
- [SDR ASMF202101013](https://openairdocs.org/sdr/ASMF202101013.md): Filter · leaking · Dec 17, 2020 · N997AM · Boeing 73776Q · Hydraulic System, Main
  > DURING TRANSIT CHECK, A HYDRAULIC LEAK WAS DETECTED IN THE HYDRAULIC SYSTEM B. MAINTENANCE PERSONNEL PERFORMED REVISION DETECTING HYDRAULIC LEAK AT IN ACOUSTIC FILTER. SO THE ACOUSTIC FILTER P/N 1013983-1, S/S, MANUFACTURER SUNDSTRAND WAS REPLACED, IAW AMM B
- [SDR ASMF202011015](https://openairdocs.org/sdr/ASMF202011015.md): Acoustic Panel · damaged · Oct 1, 2020 · N997AM · Boeing 73776Q · Nacelle/Pylon, Main Frame
  > DURING TRANSIT CHECK, IT WAS DETECTED SEVERAL NICKS ON RIGHT ENGINE INNER BARREL ACOUSTIC PANEL. MAINTENANCE PERSONNEL PERFORMED A REVISION, DETECTING A NICK OF 0.187 LENGTH, 0.046 WIDTH FROM 2.5" DISTANCE OF AFTER EDGE OF INNER BARREL ACOUSTIC PANEL AT 12 HR
- [SDR ASMF202011012](https://openairdocs.org/sdr/ASMF202011012.md): Acoustic Panel · damaged · Sep 29, 2020 · N997AM · Boeing 73776Q · Nacelle/Pylon, Main Frame
  > 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 PERFORMED A REVISION, DETECTING A DENT OF 0.0110" DEPTH, 1.000" WIDTH, A DENT OF 0.0012" DEPTH, 0.125
- [SDR ASMF2019100909](https://openairdocs.org/sdr/ASMF2019100909.md): Drain Line · leaking · Aug 23, 2019 · N997AM · Boeing 73776Q · Turbine Engine Oil System
  > 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 DRAIN LINE OF FUEL PUMP PAD DRAIN WITH 12 DROPS PER MINUTE WITHIN OF LIMITS IAW AMM 71-71-00-200-80
- [SDR ASMF201910004](https://openairdocs.org/sdr/ASMF201910004.md): Bleed Air Sys · tripped · Jul 24, 2019 · N997AM · Boeing 73776Q · Engine Bleed Air System
  > 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 DEPLOYED; SO THE FLIGHT CREW ACCOMPLISHED THE QRH 2.7 PROCEDURE, CONFIRMING THE FAILURE. MAINTENANCE PERSO
- [SDR ASMF2018101509024](https://openairdocs.org/sdr/ASMF2018101509024.md): Seal · leaking · Sep 28, 2018 · N997AM · Boeing 73776Q · Fuel Controlling System
  > FUEL LEAK ON LT ENGINE. DURING TRANSIT CHECK, A FUEL LEAK WAS DETECTED ON LT ENGINE. MAINTENANCE PERSONNEL PERFORMED LEAKING ENGINE INSPECTION IAW AMM 71-00-00-800-811-F00; IT WAS DETECTING LEAK ON SEAL BETWEEN FUEL PUMP AND HMU; IT WAS REPLACED SEAL P/N 9057M
- [SDR ASMF20180927020](https://openairdocs.org/sdr/ASMF20180927020.md): Monitor · failed · Sep 13, 2018 · N997AM · Boeing 73776Q · Engine Vibration Analyzer
  > 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 TASK 803 PROCEDURE, SHOWING FAILURE CODE 43 ON AVM. AVM WAS REPLACED IAW AMM 77-31-03, SHOWING FEWE
- [SDR ASMF20180927019](https://openairdocs.org/sdr/ASMF20180927019.md): Transmitter · failed · Sep 12, 2018 · N997AM · Boeing 73776Q · Trailing Flap Position Indicating System
  > CAPTAIN REPORTED THAT DURING LANDING, THE FLAPS TRAILING EDGE DOESN´T OPERATE WITH PRIMARY CONTROL. FLIGHT CREW ACCOMPLISHED THE QRH 9.18 PROCEDURE CONTINUING TO LANDING. AIRCRAFT WAS SENT TO THE HANGAR AND MAINTENANCE PERSONNEL PERFORMED BITE TO FSEU IAW FIM
- [SDR ASMF20171005004](https://openairdocs.org/sdr/ASMF20171005004.md): Actuator · leaking · Sep 11, 2017 · N997AM · Boeing 73776Q · Engine Thrust Reverser
  > DURING OVERNIGHT CHECK, IT WAS DETECTED A LEAKAGE IN HYDRAULIC LOWER ACTUATOR AT ENGINE 1, THEREFORE MAINTENANCE PERSONNEL REPLACED LEFT ENGINE THRUST REVERSER INBOARD LOWER ACTUATOR IAW AMM 78-31-03, TESTED CORRECT.
- [SDR ASMF201612018](https://openairdocs.org/sdr/ASMF201612018.md): Battery Pack · discharged · Dec 25, 2016 · N997AM · Boeing 73776Q · Emergency Lighting
  > DURING TRANSIT CHECK, FLOOR EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE DETECTED THE BATTERY PACK DISCHARGED IAW AMM 33-51-00. THE BATTERY PACK WAS CHARGED IAW AMM 33-51-00, TESTED CORRECT.
- [SDR ASMF2016072600007](https://openairdocs.org/sdr/ASMF2016072600007.md): Engine · making metal · May 20, 2016 · N997AM · Boeing 73776Q · APU Core Engine
  > 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 PROCEDURE, REVISION TO CHIP DETECTOR IAW AMM 49-91-81-200-801, DETECTING SILVER COLOR PARTICLES, THIS CO
- [SDR ASMF201605012](https://openairdocs.org/sdr/ASMF201605012.md): Pin · damaged · Apr 9, 2016 · N997AM · Boeing 73776Q · Instrument System Wiring
  > 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 QRH 14.6 PROCEDURE. PERFORMED BITE TO PSEU IAW FIM 31-51 TASK 801 PROCEDURE, SHOWING FAILURE CODE
- [SDR ASMF201605011](https://openairdocs.org/sdr/ASMF201605011.md): Circuit Breaker · failed · Apr 8, 2016 · N997AM · Boeing 73776Q · Central Warning
  > AIRCRAFT RETURNED OF FLIGHT DUE TO DURING CLIMB, THE CONFIGURATION ALARM WAS ACTIVE, TAKEOFF CONFIGURATION LIGHT TURNED ON & TAKEOFF WARNING HORN SOUNDED. PERFORMED TAKEOFF WARNING SYS TEST IAW AMM 31-51-00-730-803, DETECTING THE CB CO1398 FAILED. CB CO1398
- [SDR ASMF201605010](https://openairdocs.org/sdr/ASMF201605010.md): Warning System · false activation · Apr 7, 2016 · N997AM · Boeing 73776Q · Central Warning
  > 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 TASKS 803 STEP E & 822 STEP B PROCEDURES, SHOWING FAILURE CODE 31-53010. SO THE FIM 32-09 TASK 812
- [SDR ASMF201511010](https://openairdocs.org/sdr/ASMF201511010.md): Battery Pack · discharged · Nov 16, 2015 · N997AM · Boeing 73776Q · Emergency Lighting
  > 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 33-51-06, TESTED CORRECT.
- [SDR ASMF201511007](https://openairdocs.org/sdr/ASMF201511007.md): Unknown · malfunctioned · Nov 7, 2015 · N997AM · Boeing 73776Q · Landing Gear Retraction/Extension System
  > 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 SENT TO THE HANGAR & PERSONNEL PERFORMED BITE TO PSEU IAW AMM 32-09-10, NO CONFIRMING FAILURE. AS
- [SDR ASMF201507021](https://openairdocs.org/sdr/ASMF201507021.md): Pressure Switch · failed · Jul 17, 2015 · N997AM · Boeing 73776Q · Flight Control System
  > 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, DETECTING THE LOW PRESSURE WARNING SWITCH OF SYS B WITH FAILURE. THE LOW PRESSURE WARNING SWITCH WAS RE
- [SDR ASMF201506004](https://openairdocs.org/sdr/ASMF201506004.md): Fuel Filter · failed · Apr 28, 2015 · N997AM · Boeing 73776Q · Engine Fuel Distribution
  > 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 IAW AMM 73-21-00, SHOWING RT ENG FAILURE CODE 73-31072 & LT ENG FAILURE CODE 73-31321, THE ACFT WAS S
- [SDR ASMF201503029](https://openairdocs.org/sdr/ASMF201503029.md): Motor · failed · Mar 19, 2015 · N997AM · Boeing 73776Q · Auto Throttle System
  > 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 WITH FAIL CODE ASM1. DIFFERED AUTO THROTTLE IAW MEL 22-15-3 C. HIGH ENERGY STOP INSPECTION WAS PE
- [SDR ASMF201409007](https://openairdocs.org/sdr/ASMF201409007.md): Transceiver · damaged · Aug 15, 2014 · N997AM · Boeing 73776Q · DME/TACAN System
  > CAPTAIN REPORTED THAT BOTH DME’S OUT OF SERVICE. PERFORMED REVISION DETECTING A LIGHTNING STRIKE IN THE DME ANTENNA & A LIGHTNING STRIKE INSPECTION WAS PERFORMED IAW AMM 05-51-19, DETECTING BOTH DME’S TRANSCEIVERS DAMAGES, SO BOTH DME’S TRANSCEIVERS WERE REPL
- [SDR ASMF2014061806015](https://openairdocs.org/sdr/ASMF2014061806015.md): Linkage · out of adjust · May 13, 2014 · N997AM · Boeing 73776Q · Drag Control Actuator
  > 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 SPOILERS ACTUATORS SYS LINKAGES IAW AMM 27-61-00-820-801 & FLIGHT SPOILERS SYS TEST WAS PERFORMED IA
- [SDR ASMF2014061706006](https://openairdocs.org/sdr/ASMF2014061706006.md): Battery Pack · burned · Apr 15, 2014 · N997AM · Boeing 73776Q · Emergency Lighting
  > 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, THE EMER LIGHTS BATTERY PACK NR M1674 WAS FOUND BURNED. THE EMER LIGHTS BATTERY PACKS NR M1674 & M1
- [SDR ASMF201403011](https://openairdocs.org/sdr/ASMF201403011.md): Spoiler · out of adjust · Feb 28, 2014 · N997AM · Boeing 73776Q · Drag Control System
  > 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 SPOILERS NR 4 & 9 IAW AMM 27-61-00, THE AILERON CABLES ADJUSTMENT WAS CHECKED IAW AMM 27-11-00 & SPE
- [SDR ASMF201310009](https://openairdocs.org/sdr/ASMF201310009.md): Pump · leaking · Sep 28, 2013 · N997AM · Boeing 73776Q · Engine Fuel Pump
  > 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 WAS REPLACED IAW AMM 73-11-01, TESTED CORRECT.
- [SDR ASMF201310006](https://openairdocs.org/sdr/ASMF201310006.md): Warning Light · illuminated · Sep 20, 2013 · N997AM · Boeing 73776Q · Rudder Control System
  > CAPTAIN REPORTED THAT BEFORE TAXING, STANDBY RUDDER LIGHT ILLUMINATED. MAINTENANCE PERFORMED THE FIM 27-21-94, TASK 817 PROCEDURE, NO FAILURE FOUND. STANDBY RUDDER PCU VALVE WAS REPLACED AS PRECAUTION IAW AMM 27-21-94, TESTED CORRECT.
- [SDR ASMF201305004](https://openairdocs.org/sdr/ASMF201305004.md): Warning Light · false activation · Apr 25, 2013 · N997AM · Boeing 73776Q · Central Warning
  > 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 BRAKE WAS RESEATED IAW AMM 32-09-10, PAGE 501, NO CONFIRMING FAILURE, TESTED CORRECT.
- [SDR ASMF201301002](https://openairdocs.org/sdr/ASMF201301002.md): Snubber · bent · Jan 2, 2013 · N997AM · Boeing 73776Q · Passenger/Crew Doors
  > 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 DOOR SNUBBER WAS REPLACED IAW MM 52-11-51 AND IT WAS ADJUSTED IAW MM 52-11-00, TESTED CORRECT.
- [SDR ASMF201212014](https://openairdocs.org/sdr/ASMF201212014.md): Packing · damaged · Dec 27, 2012 · N997AM · Boeing 73776Q · Turbine Engine Oil System
  > 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 CRACKING DRIVE COVER PACKING'S IAW MM 72-63-01 AND OPS TEST WAS PERFORMED IAW MM 79-00-00 AND DRY MOTOR
- [SDR ASMF201212010](https://openairdocs.org/sdr/ASMF201212010.md): Valve · leaking · Dec 23, 2012 · N997AM · Boeing 73776Q · Engine Fuel and Control
  > 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 LIMITS IAW MM 71-71-00 PAGE 606; SO THE LEFT ENGINE START WAS PERFORMED AGAIN ELIMINATING THE FUEL LEA
- [SDR ASMF201208002](https://openairdocs.org/sdr/ASMF201208002.md): Shutoff Valve · malfunctioned · Aug 1, 2012 · N997AM · Boeing 73776Q · Aircraft Fuel Distribution System
  > 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 VALVE WAS RESET IAW MM 28-21-00, TESTED CORRECT.
- [SDR ASMF20111209004](https://openairdocs.org/sdr/ASMF20111209004.md): Actuator · leaking · Dec 9, 2011 · N997AM · Boeing 73776Q · Compressor Bleed Governor
  > 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. MX REPLACED THE ACTUATOR VSVS IAW MM 71-00-00 PAGE 501, TESTED CORRECT.
- [SDR ASMF201110004](https://openairdocs.org/sdr/ASMF201110004.md): Pump · leaking · Oct 14, 2011 · N997AM · Boeing 73776Q · Engine Fuel Pump
  > 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 OPERATION LIMITS IAW MM 71-71-00 DISPATCHING THE ACFT IN SUCH CONDITION. MX PERSONNEL REPLACED THE RT FUEL
- [SDR ASMF201110003](https://openairdocs.org/sdr/ASMF201110003.md): Bleed Valve · leaking · Oct 9, 2011 · N997AM · Boeing 73776Q · Compressor Bleed Valve
  > 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 LEAK WITHIN OPERATION LIMITS IAW MM 71-71-00 PAGE 6, DISPATCHING THE AIRCRAFT IN SUCH CONDITION. AT
- [SDR ASMF201108003](https://openairdocs.org/sdr/ASMF201108003.md): Skin · dented · Aug 13, 2011 · N997AM · Boeing 73776Q · Fuselage Main, Plate/Skin
  > 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 LIMITS IAW SRM 53-60-15.
- [SDR ASMF201009010](https://openairdocs.org/sdr/ASMF201009010.md): Transmitter · damaged · Sep 25, 2010 · N997AM · Boeing 737705 · Trailing Flap Position Indicating System
  > 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 QRH 9.28 AND 9.40 PROCEDURES, LANDING WITH T/E FLAPS UP. DURING MX REVISION, THE FIM PROCEDURES 27-
- [SDR ASMF201009009](https://openairdocs.org/sdr/ASMF201009009.md): Fseu · damaged · Sep 19, 2010 · N997AM · Boeing 73776Q · Trailing Edge Flap Control System
  > 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 NO ADDITIONAL PROBLEMS. DURING MX, REVISIONS WERE DETECTED, THE FSEU AND FLIGHT CONTROLS MODULE DAM
- [SDR ASMF201009006](https://openairdocs.org/sdr/ASMF201009006.md): Valve · damaged · Sep 14, 2010 · N997AM · Boeing 737705 · Trailing Edge Flap Control System
  > 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 QRH 9.28 AND 9.40 PROCEDURES, LANDING WITH T/E FLAPS UP AND REFERENCE SPEED OF 161 KNOTS AND MAXIM
- [SDR ASMF201004004](https://openairdocs.org/sdr/ASMF201004004.md): Heater · leaking · Apr 20, 2010 · N997AM · Boeing 73776Q · Engine (Turbine/Turboprop)
  > 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, CONFIRMING THAT THE FUEL LEAK WAS WITHIN LIMITS IAW MM 71-71-00. ADDITIONALLY, AN OIL LEAK WAS FOUND IN
- [SDR ASMF201002002](https://openairdocs.org/sdr/ASMF201002002.md): Warning Light · illuminated · Jan 29, 2010 · N997AM · Boeing 73776Q · Central Warning
  > 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 ALARM WAS ACTIVATED DUE TO A CHANGE ON SPEED OF THE WIND. AT PLATFORM, MX PERSONNEL PERFORMED FIM 36
- [SDR ASMF200910003](https://openairdocs.org/sdr/ASMF200910003.md): Door · unknown · Oct 12, 2009 · N997AM · Boeing 73776Q · Passenger/Crew Doors
  > 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 PERFORMED FWD ENTRY DOOR OPS CHECK IAW MM 52-10-00, ALL CORRECT. THE OVERWEIGHT INSP WAS NOT NECESSARY DUE
- [SDR ASMF20090904](https://openairdocs.org/sdr/ASMF20090904.md): Valve · failed · Sep 21, 2009 · N997AM · Boeing 73776Q · Engine Fuel and Control
  > 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 PERFORMED AN ENGINE START AND CHECK FOR LEAK IAW MMA 71-71-00, IT WAS FOUND ALL CORRECT. ADDITIONAL
- [SDR ASMF200909003](https://openairdocs.org/sdr/ASMF200909003.md): Wheel · damaged · Sep 4, 2009 · N997AM · Boeing 73776Q · Wheel/Ski/Float
  > CAPTAIN REPORTED THAT AFTER LANDING ROLL THE AIRCRAFT WAS UNABLE TO MOVE BEING NECESSARY TO ADD THRUST, HEARING A STRONG NOISE. AT PLATFORM, MAINTENANCE PERSONNEL DETECTED THE MLG WHEEL AND BRAKE ASSY POSITION 2 DAMAGED, SO THEY WERE REPLACED IAW AMM 32-45-11
- [SDR ASMF200805003](https://openairdocs.org/sdr/ASMF200805003.md): Selector Valve · failed · May 23, 2008 · N997AM · Boeing 73776Q · Landing Gear Retraction/Extension System
  > 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 LEVER WAS POSITIONED ON UP POSITION AND LIGHT TURNED OFF. MAINTENANCE PERSONNEL REPLACED THE LANDING G
- [SDR ASMF200805002](https://openairdocs.org/sdr/ASMF200805002.md): Sensor · failed · May 20, 2008 · N997AM · Boeing 73776Q · Leading Edge Slat Position Indicating System
  > 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 801 AND FIM 27-51 TASK 801 INDICATING FAIL OF SLAT NR1 SENSOR. FSEU WAS REPLACED BUT FAIL CONTINUED,
- [SDR ASMF200804001](https://openairdocs.org/sdr/ASMF200804001.md): Skin · dented · Apr 6, 2008 · N997AM · Boeing 73776Q · Wing, Plate/Skin
  > 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 INCH DEPTH, 11.5 INCH LENGTH AND 3.5 INCH WIDTH AT STATION WS 192, OUT OF LIMITS IAW SRM 57-41-01.
- [SDR ASMF200710006](https://openairdocs.org/sdr/ASMF200710006.md): Pitot Head · warning message · Oct 22, 2007 · N997AM · Boeing 73776Q · Pitot/Static System
  > 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 CORRECT IAW MM 27-31-17 AND FIM PROCEDURE 30-31 TASKS 808-809.
- [SDR ASMF200709009](https://openairdocs.org/sdr/ASMF200709009.md): Window · cracked · Sep 23, 2007 · N997AM · Boeing 73776Q · Flight Compartment Windows
  > 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, TESTED CORRECT. WINDOWS HEATER WAS DEFERRED IAW MEL 30-11 CATEGORY C. LATER, FIM 30-41 TASK 813 PROCED
- [SDR ASMF200709006](https://openairdocs.org/sdr/ASMF200709006.md): Sleeve · damaged · Sep 21, 2007 · N997AM · Boeing 73776Q · Engine Thrust Reverser
  > CAPTAIN REPORTED LIGHTNING ACTIVITY NEAR TO THE AIRCRAFT DURING FLIGHT; AT GDL PLATFORM, TECHNICAL PERSONNEL DETECTED A LIGHTNING STRIKE DAMAGE IN THE LT ENGINE THRUST REVERSER TRANSLATING SLEEVE PANEL, 10 INCHES FROM THE TRAILING EDGE OF PANEL, WITH LOSS OF M
- [SDR ASMF200704007](https://openairdocs.org/sdr/ASMF200704007.md): Valve · failed · Apr 10, 2007 · N997AM · Boeing 737* · Pneumatic Distribution System
  > 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 STAGE PRECOOLER VALVE WAS REPLACED IAW MM 36-11-06, TESTED CORRECT. OVERWEIGHT INSPECTION WAS NOT RE

Next page: https://openairdocs.org/aircraft/N997AM/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N997AM' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N997AM/reports

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