# Service difficulty reports: N950AM A list on [N950AM](https://openairdocs.org/aircraft/N950AM.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR ASMF202508040001](https://openairdocs.org/sdr/ASMF202508040001.md): Shutoff Valve · faulty · Jul 28, 2025 · N950AM · Boeing 737852 · Pneumatic Distribution System > DUCT PRESSURE INDICATION LOW DURING TAKEOFF, CLIMB AND CRUISE, ENGINE IS THE BLEED SOURCE. FRM 361 040 00 - [SDR 2025FA0000340](https://openairdocs.org/sdr/2025FA0000340.md): Valve · malfunctioned · Apr 28, 2025 · N950AM · Boeing 737852 · Pneumatic Distribution System > DUCT L INDICATION PRESSURE IS LOW - [SDR M17F202401170001](https://openairdocs.org/sdr/M17F202401170001.md): Duct · damaged · Dec 21, 2023 · N950AM · Boeing 737852 · Engine Thrust Reverser > WHEN READY FOR PUSHBACK DURING BEFORE START CHECKLIST A VEHICLE CRASH THE AIRCRAFT FROM THE RIGHT SIDE OF THE AIRPLANE GOING THRU THE LEFT SIDE STOPPING THE MOVEMENT ON THE LEFT ENGINE, CAUSING SEVERE DAMAGE TO THE ENGINE AND FUSELAGE. - [SDR 2022FA0000253](https://openairdocs.org/sdr/2022FA0000253.md): Pneumatic System · secondary damage · May 9, 2022 · N950AM · Boeing 737 · Pneumatic System > BLEED TRIP OFF EN ESTATUS DURANTE DESPEGUE (REGRESO DE VUELO) / LEED TRIP OFF IN STATUS DURING TAKEOFF (FLIGHT RETURN) - [SDR ASMF202101011](https://openairdocs.org/sdr/ASMF202101011.md): Skin · corroded · Nov 18, 2020 · N950AM · Boeing 737852 · Fuselage Main, Plate/Skin > REVISION, DETECTING A BULGE OF 2.00" LENGTH, 0.875" WIDTH AND 0.1875" DEPTH AND A DENT OF 1.3125" LENGTH, 1.0625" WIDTH AND 0.021" DEPTH WITH THREE FASTENERS DAMAGES IN FUSELAGE SKIN RIGHT COUNTER FRAME APU ACCESS DOOR. APU COWL DOOR WAS REMOVED, IAW AMM 52-4 - [SDR ASMF202011009](https://openairdocs.org/sdr/ASMF202011009.md): Acoustic Panel · dented · Sep 27, 2020 · N950AM · Boeing 737852 · Nacelle/Pylon, Main Frame > DURING TRANSIT CHECK, IT WAS DETECTED A SEVERAL DENTS ON LEFT ENGINE INNER BARREL ACOUSTIC PANEL INLET COWL. MAINTENANCE PERSONNEL PERFORMED A REVISION, DETECTING A DENT OF 0.281" WIDTH AND 0.013" DEPTH, TWO DENTS OF 0.500" WIDTH AND 0.006" DEPTH, A DENT OF 0 - [SDR ASMF2020090710](https://openairdocs.org/sdr/ASMF2020090710.md): Proximity Sensor · malfunctioned · Jul 13, 2020 · N950AM · Boeing 737852 · Trailing Flap Position Indicating System > CAPTAIN REPORTED THAT DURING APPROACH FLAP POSITION INDICATOR HAS NEEDLE SPLIT, AFTER 2 MINUTES IT TURNED TO A TRAILING EDGE FLAP LEVER DISAGREE CONDITION. MAINTENANCE PERSONNEL PERFORMED THE BITE TO FSEU IAW FIM 27-51 TASK 801 PROCEDURE, DETECTING FAILURE CO - [SDR ASMF2020090709](https://openairdocs.org/sdr/ASMF2020090709.md): Flap System · malfunctioned · Jul 10, 2020 · N950AM · Boeing 737852 · Trailing Edge Flap Control System > CAPTAIN REPORTED THAT DURING APPROACH THE FLAPS WERE NOT OPERATING CORRECTLY, REMAINING IN FLAPS 10 WHEN THE LEVER WAS PUT ON FLAPS 15. MAINTENANCE PERSONNEL PERFORMED BITE TO FSEU IAW FIM 27-51 TASK 803 PROCEDURE, SHOWING FAILURE CODES 27-81224, 27-81203, 27 - [SDR ASMF2020090703](https://openairdocs.org/sdr/ASMF2020090703.md): Module · failed · Jun 20, 2020 · N950AM · Boeing 737852 · Drag Control System > CAPTAIN REPORTED THAT DURING LANDING AUTO BRAKE DISARM LIGHT TURNED ON. MAINTENANCE PERSONNEL PERFORMED REVISION TO SYSTEM, DETECTING LEFT ANTI-SKID VALVE WITH FAILURE. THE S2 AND S3 SWITCH PACK M1766 AND M 1767 WERE CHECKED, IAW FIM 32-42 TASK 828 PROCEDURE - [SDR ASMF2019042317](https://openairdocs.org/sdr/ASMF2019042317.md): Bolt · loose · Mar 4, 2019 · N950AM · Boeing 737852 · Trailing Edge Flaps > DURING TRANSIT CHECK, IT WERE DETECTED SUPPORT BOLT OF LH AND RH INBOARD FLAP AFT LOOSED. AIRCRAFT WAS SENT TO THE HANGAR TO REVISION; THEY WERE ISSUED WO´S 5273684 AND 5273713 TO PERFORM TASKS; MAINTENANCE PERSONNEL PREFORMED REPLACEMENT OF BEARINGS I.A.W. AM - [SDR ASMF2019042301](https://openairdocs.org/sdr/ASMF2019042301.md): Warning Message · false activation · Jan 8, 2019 · N950AM · Boeing 737852 · Central Warning > AIRCRAFT RETURN TO PLATFORM DUE TO DURING TAKEOFF, IT WAS ACTIVE “TAKE OFF CONFIGURATION ALARM”; FLIGHT CREW ACCOMPLISHED THE QRH 15.2 PROCEDURES; MAINTENANCE PERSONNEL PERFORMED TAKE OFF WARNING SYSTEM TEST IAW FIM 31-51 TASK 803, NO FAILURE WAS FOUND, TEST - [SDR ASMF201901017](https://openairdocs.org/sdr/ASMF201901017.md): Warning System · false activation · Jan 8, 2019 · N950AM · Boeing 737852 · Central Warning > AIRCRAFT RETURN TO PLATFORM DUE TO DURING TAKEOFF, IT WAS ACTIVE “TAKE OFF CONFIGURATION ALARM”; FLIGHT CREW ACCOMPLISHED THE QRH 15.2 PROCEDURES; MAINTENANCE PERSONNEL PERFORMED TAKE OFF WARNING SYSTEM TEST IAW FIM 31-51 TASK 803, NO FAILURE WAS FOUND, TEST - [SDR ASMF20180515001](https://openairdocs.org/sdr/ASMF20180515001.md): Warning Light · false activation · Mar 10, 2018 · N950AM · Boeing 737852 · Central Warning > AIRCRAFT RETURNED TO PLATFORM DUE TO DURING ENGINE START THE LOW OIL PRESSURE LIGHTS ILLUMINATED. MAINTENANCE PERFORMED FIM 49-90-803, TESTED CORRECT. - [SDR ASMF201802002](https://openairdocs.org/sdr/ASMF201802002.md): Valve · leaking · Feb 3, 2018 · N950AM · Boeing 737752 · Aircraft Fuel Distribution System > DURING FUELING, A FUEL LEAK IN THE LEFT TANK OCCURRED DUE TO THE SHUTOFF VALVE DID NOT CLOSE. MAINTENANCE PERFORMED A FUEL TRANSFER TO AVOID THE SPILL IAW AMM 28-21-00 AND THE VALVE WAS REPLACED IAW AMM 28-21-32, ALL TESTED CORRECT. - [SDR ASMF201801009](https://openairdocs.org/sdr/ASMF201801009.md): Line · leaking · Dec 8, 2017 · N950AM · Boeing 737852 · Landing Gear Brake System > DURING TRANSIT CHECK, A HYDRAULIC LEAK WAS FOUND IN THE MLG WHEEL BRAKE LINE NUMBER 3. MAINTENANCE ADJUSTED THE MLG WHEEL BRAKE LINE IAW AMM 32-41-00, AND THE MLG WHEEL NUMBERS 3 AND 4 WERE INSPECTED IAW AMM 32-45-00-700-803, TESTED CORRECT. - [SDR ASMF20170424002](https://openairdocs.org/sdr/ASMF20170424002.md): Fan · fod · Mar 16, 2017 · N950AM · Boeing 737800* · Turbine Engine Air Inlet Section > DURING TRANSIT CHECK, DETECTED FOREIGN OBJECT DAMAGE AT INLET CASE FAN OF THE LEFT ENGINE. MAINTENANCE PERSONNEL PERFORMED A REVISION TO LEFT ENGINE IAW AMM 71-00-00, DETECTING TWO DENTS OF 3/4"LENGTH, 3/8"DEPTH AND 2 1/2"LENGTH, 9/16"DEPTH IN THE ABRADABLE SH - [SDR ASMF20170216001](https://openairdocs.org/sdr/ASMF20170216001.md): Warning System · false activation · Feb 16, 2017 · N950AM · Boeing 737800* · Engine Thrust Reverser > AIRCRAFT REJECTED TAKE OFF AT 90 KNOTS DUE TO TAKE OFF CONFIG AND REVERSE ENG 1 INDICATION. MAINTENANCE PERSONNEL PERFORMED REVISION AND OPERATIONAL TEST IAW AMM 78-31-200, TESTED CORRECT. THE HIGH ENERGY STOP INSPECTION WAS NOT NECESSARY DUE TO THE MAXIMUM GR - [SDR ASMF201612017](https://openairdocs.org/sdr/ASMF201612017.md): Solenoid · failed · Dec 19, 2016 · N950AM · Boeing 737800* · Emergency Exits > AIRCRAFT REJECTED TAKEOFF AT 45 KNOTS DUE TO RIGHT FORWARD EMERGENCY OVERWING DOOR WARNING ANNUNCIATOR ILLUMINATED. MAINTENANCE PERFORMED REVISION IAW AMM 52-20-00. THE RIGHT FORWARD EMERGENCY OVERWING WARNING DOOR SOLENOID WAS REPLACED IAW AMM 52-22-41 AND T - [SDR ASMF201611024](https://openairdocs.org/sdr/ASMF201611024.md): Shutoff Valve · malfunctioned · Oct 15, 2016 · N950AM · Boeing 737800* · Fuel Selector/Shut-Off Valve > DURING FUELING, A FUEL SPILLAGE IN THE RIGHT TANK OCCURRED DUE TO THE SHUTOFF VALVE DID NOT CLOSE. THE PLATFORM WAS CLEANED AND MAINTENANCE CLEANED THE SELECTOR. THE SHUTOFF VALVE WAS RESEATED AND TESTED SEVERAL TIMES IAW MM 28-21-00, NO LEAKS WERE DETECTED - [SDR ASMF201611017](https://openairdocs.org/sdr/ASMF201611017.md): Wire Harness · damaged · Sep 29, 2016 · N950AM · Boeing 737800* · Fire Protection System Wiring > DURING TRANSIT CHECK, THE RIGHT ENGINE FIRE HANDLE LIGHT WAS NOT ILLUMINATED DURING FIRE DETECTION TEST AND LOOP B OF RIGHT ENGINE WITH FAULT. MAINTENANCE PERSONNEL PERFORMED RIGHT ENGINE FIRE DETECTION TEST IAW AMM 26-10-00, DETECTING LINE OPEN AT MW0326 WIR - [SDR ASMF201608006](https://openairdocs.org/sdr/ASMF201608006.md): Engine · damaged · Jul 3, 2016 · N950AM · Boeing 737800* · Engine (Turbine/Turboprop) > IAW REMOTE DIAGNOSTIC SYSTEM, THE RT ENGINE HAD A SHARP DECREASE IN TAKEOFF, EGT MARGIN AND CORE SPEED AS WELL AS IN INCREASE IN EGT AND FUEL FLOW. MAINTENANCE PERSONNEL PERFORMED THE RT BORESCOPE INSPECTION OF THE HIGH PRESSURE TURBINE AND COMBUSTION SECTION - [SDR ASMF20160620010](https://openairdocs.org/sdr/ASMF20160620010.md): Engine · damaged · May 4, 2016 · N950AM · Boeing 737800* · Engine (Turbine/Turboprop) > IAW REMOTE DIAGNOSTIC SYSTEM, THE LT ENGINE HAD A SHARP DECREASE OF EGT HOT DAY MARGIN, AS WELL AS AN INCREASE OF EGT AND FUEL CONSUMPTION. MAINTENANCE PERSONNEL PERFORMED THE LT ENGINE BORESCOPE INSPECTION OF THE HIGH PRESSURE TURBINE AND COMBUSTION SECTION - [SDR ASMF201605003](https://openairdocs.org/sdr/ASMF201605003.md): Warning Light · false activation · Mar 4, 2016 · N950AM · Boeing 737800* · Door Warning System > AIRCRAFT REJECTED TAKEOFF DUE TO FWD OVERWING DOOR LIGHT TURNED ON BEFORE RESIZING 80% OF N1. DEFERRED THE FWD OVERWING DOOR LIGHT IAW MEL 52-3 2 CAT C. HIGH ENERGY STOP INSPECTION WAS PERFORMED IAW MM 05-51-07, NO DAMAGES WERE FOUND. THE FIM 52-20 TASK 801 - [SDR ASMF201601002](https://openairdocs.org/sdr/ASMF201601002.md): Fuel Heater · leaking · Nov 29, 2015 · N950AM · Boeing 737800* · Fuel Heater > DURING TRANSIT CHECK, A FUEL LEAK WAS DETECTED IN THE LT ENG. PERFORMED REVISION, DETECTING THE FUEL SERVO HEATER & HPTCC VLV LEAKING, SO THE LT FUEL SERVO HEATER & HPTCC VLV WERE REPLACED IAW AMM 73-11-07 & AMM 75-21-01, TESTED CORRECT. - [SDR ASMF201511011](https://openairdocs.org/sdr/ASMF201511011.md): Transmitter · failed · Nov 19, 2015 · N950AM · Boeing 737800* · Engine Oil Indicating System > AIRCRAFT RETURNED TO PLATFORM DUE TO DURING TAXING, THE RT ENG OIL FILTER BY PASS LIGHT TURNED ON. PERFORMED REVISION TO CHIP DETECTOR IAW AMM 79-00-00, NO METAL PARTICLES WERE FOUND. PERFORMED FIM 79-05 TASK 817 PROCEDURE, DETECTING THE SCAVENGE OIL FILTER - [SDR ASMF201510009](https://openairdocs.org/sdr/ASMF201510009.md): Sensor · failed · Aug 23, 2015 · N950AM · Boeing 737800* · Trailing Flap Position Indicating System > DURING APPROACH, FLAPS DID NOT EXTEND. ACFT WAS SENT TO THE HANGAR & MX PERFORMED BITE TO FSEU IAW FIM 27-51 TASK 801 PROCEDURE, SHOWING FAILURE CODE 27-53252 FLAP 3 SKEW, SO THE SENSOR T527 OF FLAP 3 WAS REPLACED IAW FIM 27-59 TASK 803 PROCEDURE, TESTED CORR - [SDR ASMF201510008](https://openairdocs.org/sdr/ASMF201510008.md): Fan · lack of lube · Aug 21, 2015 · N950AM · Boeing 737800* · Turbine Engine Compressor Section > DURING CLIMB, THE RT ENG VIBRATION REACHED 2.5 UNITS. ACFT WAS SENT TO THE HANGAR & MX PERFORMED REVISION TO CHIP DETECTOR IAW AMM 79-00-00, NO METAL PARTICLES WERE FOUND. A BORESCOPE INSPECTION TO LPT STAGES 1 - 3 IAW AMM 72-00-00, NO DAMAGES WERE FOUND. L - [SDR ASMF201509004](https://openairdocs.org/sdr/ASMF201509004.md): Warning System · false activation · Jul 25, 2015 · N950AM · Boeing 737800* · Engine Vibration Analyzer > CAPTAIN REPORTED THAT DURING CLIMB, THE LT ENG VIBRATION REACHED 4.2 UNITS. PERFORMED FIM 77-31 TASK 801 & FIM 78-01 TASK PROCEDURES, NO DAMAGES WERE FOUND, TESTED CORRECT. AS PRECAUTIONARY ACTION, REPLACED THE VIBRATION MONITOR IAW AMM 77-31-01. TRIM BALAN - [SDR ASMF201507009](https://openairdocs.org/sdr/ASMF201507009.md): Wire Harness · damaged · Jun 10, 2015 · N950AM · Boeing 737800* · Pneumatic System Wiring > AIRCRAFT RETURNED TO PLATFORM, AFTER LT ENG START, THE BLEED DUCT PRESS INDICATOR SHOWED 5 PSI & IT WAS STABILIZED AT 10 PSI. PERFORMED REVISION, DETECTING THE ELEC HARNESS NR MW0311 DAMAGED. THE LT ELEC HARNESS NR MW0311, BLEED AIR REGULATOR & TUBE WERE REP - [SDR ASMF201506009](https://openairdocs.org/sdr/ASMF201506009.md): Window · cracked · May 11, 2015 · N950AM · Boeing 737832 · Flight Compartment Windows > AIRCRAFT RETURN TO PLATFORM AS A CONSEQUENCE OF THE LT WINDOW NR 2 CRACKED. REPLACED THE LT WINDOW NR 2 & WINDOW HEAT CONTROLLER MODULE IAW AMM 56-12-11 & AMM 30-41-11, TESTED CORRECT. - [SDR ASMF201503022](https://openairdocs.org/sdr/ASMF201503022.md): Hmu · failed · Mar 5, 2015 · N950AM · Boeing 737800* · Fuel Control/Turbine Engines > AIRCRAFT RETURNED TO PLATFORM DUE TO DIFFERENCE OF ONE INCH BETWEEN THRUST LEVERS AT IDLE & THE RT ENG WITH OSCILLATIONS. PERFORMED BITE TO RT EEC IAW FIM 73-00 TASK 801 PROCEDURE, NO FAILURE DETECTED. BOTH ENGS WERE STARTED DETECTING THE LT ENG WAS 67.9% AT - [SDR ASMF201501024](https://openairdocs.org/sdr/ASMF201501024.md): Radome · dented · Dec 30, 2014 · N950AM · Boeing 737800* · Aerodynamic Fairings > DURING TRANSIT CHECK, IT WAS DETECTED A DENT IN RADOME BETWEEN 4:00 AND 5:00 HRS POSITION OF 4.0 INCHES IN LENGTH & 3.0 INCHES WIDE. EVALUATED THE DAMAGE & FOUND OUT OF LIMITS IAW SRM 53-52-00. ACFT WAS SENT TO THE HANGAR & ISSUED THE NON-ROUTINE CARDS A0223 - [SDR ASMF201501014](https://openairdocs.org/sdr/ASMF201501014.md): Warning System · false activation · Nov 14, 2014 · N950AM · Boeing 737800* · Brake Anti-Skid Section > DURING TRANSIT CHECK, THE ANTI-SKID LIGHT TURNED ON WAS DETECTED ON CABIN CREW. PERFORMED FIM 32-42 TASK 829 PROCEDURE, CONFIRMING THE FAILURE, SO THE ANTI-SKID SYS WAS DEFERRED IAW MEL 32-2-2 CAT C. ACFT PERFORMED AN UNSCHEDULED LANDING DUE TO RAIN IN THE D - [SDR ASMF201402010](https://openairdocs.org/sdr/ASMF201402010.md): Warning System · false activation · Jan 23, 2014 · N950AM · Boeing 737832 · Door Warning System > AIRCRAFT REJECTED TAKE OFF AT 40 KNOTS, DUE TO RT FWD OVERWING LIGHT TURNED ON. PERFORMED A REVISION AT THE FWD OVERWING DOOR IAW AMM 52-20-00, DETECTING THE FWD OVERWING DOOR WAS LOCKED CORRECTLY. FWD OVERWING DOOR DEFERRED IAW MEL 52-3-2 CAT C. THE HIGH - [SDR ASMF201312012](https://openairdocs.org/sdr/ASMF201312012.md): Warning System · false activation · Dec 16, 2013 · N950AM · Boeing 737800* · Door Warning System > AIRCRAFT REJECTED TAKE OFF AT 80 KNOTS DUE TO RIGHT FWD OVERWING LIGHT TURNED ON. PERFORMED THE QRH 1.14 PROCEDURE, NO CONFIRMING THE FAILURE & INITIATING AGAIN SEQUENCE OF TAKEOFF. AT MEX, AS PRECAUTIONARY ACTION, PERFORMED BITE TO OVERWING EXIT DOOR FLIGH - [SDR ASMF201308007](https://openairdocs.org/sdr/ASMF201308007.md): Unknown · odor · Jul 10, 2013 · N950AM · Boeing 737800* · Air Distribution System > ACFT RETURNED TO PLATFORM AFTER ENGINES START. A RUBBER BURNING ODOR WITH NO EVIDENCE TO SMOKE. MX PERSONNEL PERFORMED SMOKE OR FUMES IN CABIN CONDITIONAL INSPECTION IAW MM 05-51-56 AND FIM 21-00 TASK 806 PROCEDURE, NO ODOR OR SMOKE EVIDENCES WERE FOUND. TH - [SDR ASMF201303020](https://openairdocs.org/sdr/ASMF201303020.md): Pump · leaking · Feb 25, 2013 · N950AM · Boeing 737800* · Fuel Boost Pump > DURING TRANSIT CHECK, A FUEL LEAK WAS DETECTED. MAINTENANCE PERSONNEL DETECTED THE FUEL PUMP SEAL DAMAGED ON RT ENGINE, FUEL PUMP WAS REPLACED IAW AMM 73-11-01 AND TESTED IAW AMM 71-00-00, ALL CORRECT. - [SDR ASMF201303006](https://openairdocs.org/sdr/ASMF201303006.md): Connector · out of position · Jan 19, 2013 · N950AM · Boeing 737800* · Buffet/Galleys > CAPTAIN REPORTED THAT DURING CLIMB AN ELECTRICAL CABLE BURNED ODOR WITH NO EVIDENCE OF SMOKE, DISAPPEARING DURING CLIMB. MX PERSONNEL PERFORMED FIM 21-00, TASK 806 PROCEDURE AND SMOKE OR FUMES IN CABIN CONDITIONAL INSPECTION IAW MM 05-51-56, DETECTING A FORWA - [SDR ASMF201211011](https://openairdocs.org/sdr/ASMF201211011.md): Case · damaged · Nov 20, 2012 · N950AM · Boeing 737832 · Turbine Engine Air Inlet Section > DURING TRANSIT CHECK, IT WAS DETECTED SCRATCH ON RT ENGINE FAN INLET CASE. ACFT WAS SENT TO THE HANGAR AND MX PERSONNEL PERFORMED AN ENGINE REVISION IAW MM 72-24-01, DETECTING SCRATCH AND GROOVE ON RT ENGINE FAN INLET CASE OUT OF LIMITS; SO THE RT ENGINE WAS - [SDR ASMF201211009](https://openairdocs.org/sdr/ASMF201211009.md): Blade · dented · Nov 19, 2012 · N950AM · Boeing 737832 · Turbine Engine Air Inlet Section > CAPTAIN REPORTED THAT DURING TAKEOFF AT ROTATION SPEED A BIRD STRIKE ON RT ENGINE; FLIGHT CREW CONTINUED TO DESTINATION DUE TO RT ENGINE PARAMETERS WERE NORMAL AND VIBRATION REACHED 2.9 OF N2.. MX PERSONNEL PERFORMED A BIRD STRIKE CONDITIONAL INSPECTION IAW M - [SDR ASMF201210006](https://openairdocs.org/sdr/ASMF201210006.md): Windshield · leaking · Sep 21, 2012 · N950AM · Boeing 737* · Flight Compartment Windows > CAPTAIN REPORTED THAT DURING CLIMB AT 3.8 PSI’S OF DIFFERENTIAL PRESSURE, A STRONG NOISE IN CREW CABIN WAS HEARD. FLIGHT CREW ACCOMPLISHED THE QRH 2.1 PROCEDURE, NO CONFIRMED FAILURE, CONTINUED TO DESTINATION. MX PERSONNEL REPLACED THE LT WINDSHIELD NR 2 IAW - [SDR ASMF201207002](https://openairdocs.org/sdr/ASMF201207002.md): Line · leaking · Jun 25, 2012 · N950AM · Boeing 737800* · Hydraulic System, Main > DURING PUSH BACK, DETECTED A HYD LEAK IN THE RT MLG. ACFT WAS SENT TO THE HANGAR AND MX PERSONNEL REPLACED FLEXIBLE BRAKE LINE NR 4 IAW MM 32-41-00, TESTED CORRECT. ## 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 = 'N950AM' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N950AM/reports --- 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.