N852AM

Service difficulty reports not matched to an aircraft · 25

They name N852AM, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. Newest first.

Query with SQL
duckdb -csv -c "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 = 'N852AM' AND registry_match IS NULL
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR EE4Y2013032000021Frame · dentedAFT CARGO COMPARTMENT ON STR 24R FRAME UPPER FLANGE WITH DENT. FRAME REPAIRED IAW MESSAGE AMX-13-0016-03B.Mar 11, 2013 · N852AM · Boeing 737752 · Fuselage Main, FrameSDR ASMF201207003Valve · leakingDURING RT ENGINE START, A FUEL LEAK WAS DETECTED. MX PERSONNEL DETECTED THE ACTUATOR DRAIN VBV WITH LEAK WITHIN OPERATION LIMITS IAW MM 71-71-00; 3A IDLE PWR LEAK TEST WAS PERFORMED IAW MM 71-71-00, WITHOUT LEAK IN THE ACTUATOR DRAIN VBV, ALL CORRECT.Jun 28, 2012 · N852AM · Boeing 737752 · Aircraft Fuel Distribution SystemSDR ASMF201205007Skin · damagedDURING TRANSIT CHECK WAS DETECTED A LIGHTNING STRIKE IN LT WINGLET T/E. MX PERSONNEL PERFORMED A LIGHTNING STRIKE INSP IAW MM 05-51-19 DETECTED A DENT OF 0.200 INCHES LONG AND 0.250" WIDE ON NEXT TO LT WINGLET T/E; SO IT WAS REPAIRED IAW SRM 57-30-01 ALLOWABLMay 14, 2012 · N852AM · Boeing 737752 · Wing, Plate/SkinSDR ASMF20120307002Pump · leakingDURING TRANSIT CHECK, A FUEL LEAK DETECTED IN THE RT ENGINE. MX PERSONNEL DETECTED THE LEAK BETWEEN FUEL PUMP AND GEAR BOX, FOUND OUT OF ITS OPERATIONAL LIMITS IAW MM 73-11-00; FUEL PUMP WAS REPLACED IAW MM 73-11-01, TESTED CORRECT.Mar 7, 2012 · N852AM · Boeing 737752 · Engine Fuel PumpSDR ASMF201108006Windshield · brokenACT PERFORMED AN UNSCHEDULED LANDING, DUE TO L1 WINDSHIELD BROKEN. THE FLIGHT CREW PERFORMED THE QRH 1.14 PROCEDURE, CONFIRMING THE FAILURE. MX REPLACED THE L1 WINDSHIELD ASSY IAW MM 56-11-11 AND WINDOW HEAT SYS TEST WAS PERFORMED IAW MM 30-41-00, ALL CORRECTAug 14, 2011 · N852AM · Boeing 737752 · Flight Compartment WindowsSDR ASMF201107013Winglet · damagedDURING TRANSIT CHECK MX DETECTED A LIGHTNING STRIKE ON THE LT WINGLET, ACFT WAS SENT TO THE HANGAR FOR ATTENTION; A LIGHTNING STRIKE CONDITIONAL INSPECTION WAS PERFORMED IAW MM 05-51-19 FOUND DAMAGES OUT OF LIMITS OF 3.5" LONG AND 0.5" WIDE, SO LEFT WINGLET WAAug 1, 2011 · N852AM · Boeing 73776N · Wing Main, Frame StructureSDR ASMF201107006Access Panel · damagedDURING OVERNIGHT CHECK, TECH DETECTED A FUEL LEAK IN LEFT WING MAIN TANK ACCESS DOOR NR 532AB; MX TIGHTEN THE SCREWS NOT CORRECTING THE LEAK, SO THEY REMOVED THE ACCESS DOOR FINDING THE RUBBER SEAL AND THE ALUMINUM GASKET DAMAGED. ACCESS DOOR, RUBBER SEAL ANDJul 5, 2011 · N852AM · Boeing 737752 · Wing, Plate/SkinSDR ASMF201107005Regulator · damagedACFT RETURNED TO DEPARTURE, DUE TO THE RIGHT PACK BLEED TRIP OFF LIGHT TURNED ON. THE FLIGHT CREW PERFORMED THE QRH 2.6 PROCEDURE, CONFIRMING THE FAILURE. MX REPLACED THE RT ENGINE BLEED AIR REGULATOR IAW MM 36-11-03 AND FIM 36-10 TASK 801 PROCEDURE WAS PERFJul 1, 2011 · N852AM · Boeing 737752 · Engine Bleed Air SystemSDR ASMF201103003Packing · damagedDURING RT ENGINE START, SMOKE WAS DETECTED AROUND COWLING AND MX PERSONNEL PERFORMED A REVISION DETECTING HYDRAULIC LEAK IN THE COUPLING OF STARTER WITH GEARBOX; SO THE PREFORMED PACKING BETWEEN STARTER AND GEARBOX WERE REPLACED IAW MM 80-11-02, TESTED CORRECTMar 24, 2011 · N852AM · Boeing 737705 · Hydraulic System, MainSDR ASMF201101003Strut · damagedDURING TRANSIT CHECK, A HYD SLIP WAS DETECTED IN THE LT MLG SHOCK ABSORBER. DURING MX REVISION, THE MLG SHOCK ABSORBERS WERE COMPRESSED; SO ACFT WAS SENT TO THE HANGAR AND MX PERSONNEL PERFORMED A MLG SERVICE IAW MM 12-15-31, ALL CORRECT AND THE MLG SHOCK STRUDec 30, 2010 · N852AM · Boeing 737752 · Main Landing Gear Strut/Axle/TruckSDR ASMF201101002Carbon Seal · damagedCAPTAIN REPORTED THAT DURING CRUISE, THE RT ENGINE OIL QUANTITY DECREASED AND THE OIL QUANTITY REACHED 1 QUARTER DURING DESCENT, SO FLIGHT CREW ACCOMPLISHED THE QRH 7.21 AND 7.14 PROCEDURES AND SHUT DOWN THE ENGINE. ACFT WAS SENT TO THE HANGAR AND DURING OVERDec 26, 2010 · N852AM · Boeing 737752 · Turbine Engine Oil SystemSDR ASMF 20081203Unknown · smokeACFT RETURNED, DUE TO SMOKE IN THE CABIN. THE ACFT WAS SENT TO THE HANGAR AND MX PERFORMED RT ENGINE CLEANING PROCEDURE IAW AMM 72-00-00 AND AIR PRESSURIZATION OPS TEST IAW AMM 21-31-00, ALL CORRECT. THE OVERWEIGHT INSP WAS NOT NECESSARY DUE TO THE ACFT LANDEDDec 21, 2008 · N852AM · Boeing 737* · Air Distribution SystemSDR ASM2008F00006Access Panel · leakingDURING FUEL SUPPLY SERVICE MX PERSONNEL DETECTED A FUEL LEAK UNDER THE RT WING. THE MAIN TANK ACCESS DOOR 632EB AND ITS RUDDER DOOR SEAL WERE REPLACED AND TESTED IAW MM 28-11-11, TASK 28-11-00-790-801 ALL CORRECT.Sep 30, 2008 · N852AM · Boeing 737* · Wing, Plate/SkinSDR ASM2008F00004Access Panel · leakingDURING WALK AROUND CAPTAIN FOUND A FUEL LEAK UNDER THE RIGHT WING AND ENGINE FUEL DRAIN. MAINT CONFIRMED THE FUEL LEAK THEN REMOVED AND REPLACED MAIN TANK RIGHT WING ACCESS PANEL SEAL. 112N51012, DOOR ASSY ON RIGHT SIDE AND TESTED IAW MM 28-11-11M ALL CORRECTSep 9, 2008 · N852AM · Boeing 737* · Wing, Plate/SkinSDR AMF200710009Generator · damagedAIRCRAFT PERFORMED AN UNSCHEDULED LANDING, DUE TO DRIVE LIGHT OF LT GENERATOR TURNED ON. CAPTAIN PERFORMED ABNORMAL PROCEDURE BUT APU DID NOT START AT FL 400, IT LANDED. MAINTENANCE PERSONNEL VERIFIED APU GENERAL CONDITION AND STARTED IT CORRECTLY; REGARDING LOct 26, 2007 · N852AM · Boeing 737* · Alternator-Generator DriveSDR ASMF200707018Unknown · unknownAIRCRAFT RETURNED OF FLIGHT DUE TO LT TANK FUEL UNBALANCED LIGHT TURNED ON WITH INDICATION OF CENTRAL TANK 2360 KGS, LT TANK 3140 KGS AND RT TANK 3750 KGS. DURING MAINTENANCE CHECK AN UNBALANCE OF 700 KGS WAS DETECTED WITH INDICATIONS OF LT TANK 3000 KGS AND RJul 28, 2007 · N852AM · Boeing 737* · Fuel Indicating SystemSDR ASMF200707003Pitot Head · damagedAIRCRAFT REJECTED TAKEOFF AT 80 KTS DUE TO CREW DETECTED A DISCREPANCY BETWEEN READINGS IN CAPTAIN (45 KNOTS) AND FIRST OFFICER’S (80 KNOTS) VELOCIMETERS. MAINTENANCE PERSONNEL DETECTED FOD ON LT PITOT CAUSED BY A BIRD STRIKE. FLUSH TO THE LT PITOT AND TESTS Jul 2, 2007 · N852AM · Boeing 737705 · Flight Environment DataSDR ASMF200609006Door · fodDURING TRANSIT CHECK, A FOD WAS DETECTED IN THE FORWARD GALLEY SERVICE DOOR ACTUATOR FAIRING, WITH .1250 INCH LONG X .1250 INCH WIDTH AND .1250 INCH DEPTH, WITH IN LIMITS. SERVICE DOOR WAS CLOSED WITH DIFFICULTY AND AIRCRAFT WAS DISPATCHED. AIRCRAFT WAS SENT Sep 16, 2006 · N852AM · Boeing 737* · Service DoorsSDR ASMF200608018Engine · unknownAIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURING RIGHT ENGINE STARTING, -ECC ALT- LIGHT TURNED ON. REPORT WAS DEFERRED IAW MEL 73-11 CATEGORY-C. DURING OVERNIGHT CHECK, FIM 73-05 PROCEDURE, TASK 811, AND ENGINE RUNNING TEST WERE PERFORMED IAW MM 71-0Aug 26, 2006 · N852AM · Boeing 737* · Engine (Turbine/Turboprop)SDR ASMF200606005Windshield · damagedAIRCRAFT RETURNED, WINDOW R1 WAS DAMAGED AND WINDSHIELD HEATER INOPERATIVE. DURING MAINTENANCE CHECK, WINDOW WAS DETECTED WITH ISSUES. DAMAGES WERE EVALUATED IAW MM 56-11-00 AND 56-11-11, PAGE 401 THROUGH 422, BEING WITHIN LIMITS; ADDITIONALLY AN OVERWEIGHT INJun 11, 2006 · N852AM · Boeing 737* · Flight Compartment WindowsSDR ASMF200603014Speed Brake · malfunctionedAIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE THAT THE SPEED BRAKES DO NOT ARM LIGHT TURNED ON WHEN THE FLAPS WERE SELECTED AT 5 DEGREES. THE REPORT WAS DEFERRED BY MEL 27-7. DURING OVERNIGHT CHECK THE FIM PROCEDURE 27-62 TASK 802 WAS ACCOMPLISHED, TESTED CMar 26, 2006 · N852AM · Boeing 737724 · Drag Control SystemSDR ASMF200603012Warning Message · false activationAIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE THAT THE SPEED BREAK DO NOT ARM LIGHT TURNED ON DURING THE AIRCRAFT TAKEOFF SET UP. THE SYSTEM WAS DEFERRED IAW MEL 27-7. DURING TRANSIT AT MEX THE SYSTEM WAS TESTED IAW M/M 27-62-00, BEING ALL CORRECT.Mar 18, 2006 · N852AM · Boeing 737* · Drag Control SystemSDR ASMF200602008Engine · bird ingestionPILOT REPORTED THAT DURING CRUISE AT 410 FLIGHT LEVEL THE VIBRATION INDICATION OF THE LEFT ENGINE WAS 0.1 AND OF THE RIGHT ENGINE WAS 1.7. THE RIGHT ENGINE WAS CHECKED IAW M/M 71-00-00 DETECTING A BIRD STRIKE. THE ENGINE WAS CHECKED IAW M/M 05-51-18, AN FOD Feb 23, 2006 · N852AM · Boeing 737 · Engine (Turbine/Turboprop)SDR ASMF200602007Switch · misalignedAIRCRAFT REJECTED TAKEOFF DUE TO TAKEOFF WARNING ALARM WAS ACTIVATED. THE FAULT CODES 31-55-008 & 31-52-004 APPEARED DURING A BITE TO THE PROXIMITY SWITCH UNIT IAW FIM 32-9. THE SWITCH S132 WAS FOUND OUT OF ACTIVATION LIMITS. THE SWITCH WAS ADJUSTED AND THEFeb 21, 2006 · N852AM · Boeing 737 · Central WarningSDR ASMF200506025Trim System · malfunctionedAIRCRAFT RETURNED TO PLATFORM, PSEU AND OVERHEAD LIGHTS TURNED ON IN UPPER PANEL. BITE TO PROXIMITY UNIT SWITCH WAS PERFORMED SHOWING STAB TRIM DISAGREE FAILURE CODE. STABILIZER WAS COMPLETELY DEPLOYED AND CONFIGURED AGAIN IN TAKEOFF MODE TURNING OFF THE LIGJun 24, 2005 · N852AM · Boeing 737500* · Stabilizer Position Indicating
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