N425MA

Service difficulty reports · 64

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. 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 = 'N425MA' AND registry_match = 'registration'
  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 MALA954433Squat Sw · malfunctionedFLT 3017 - ON CLIMB-OUT FROM MKG, THE GEAR DOOR POSITION ANNUNCIATOR LIGHT ILLUMINATED. THE CREW CYCLED THE GEAR AND THE LIGHT RE-ILLUMINATED. THE LIGHT EXTINGUISHED WITH THE GEAR FULLY RETRACTED OR EXTENDED. THE AIRCRAFT CONTINUED TO DTW. MAINTENANCE WAS Apr 26, 1995 · N425MA · Swrngn SA227AC · Landing Gear Position and WarningSDR MALA954417Door Light · illuminatedDTW - FLT 3452 - ON CLIMBOUT, GEAR DOOR POSITION LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE WAS UNABLE TO DUPLICATE THE DISCREPANCY. SYSTEM OPERATED SATISFACTORILY DURING A TEST FLIGHT. (X)Apr 18, 1995 · N425MA · Swrngn SA227AC · Landing Gear Position and WarningSDR MALA954406Egt Indicator · failedFLIGHT NR 3218 - IN CRUISE FLIGHT FROM MSP, THE RIGHT EGT READ 150 DEGREES LOWER THAN THE LEFT EGT. THE AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED THE RIGHT EGT INDICATOR. SYSTEM OPERATED SATISFACTORILY. (W)Apr 8, 1995 · N425MA · Swrngn SA227AC · Engine EGT/TIT Indicating SystemSDR MALA954401Door Sill · oversized holeMSP - DURING A SCHEDULED INSPECTION, MAINTENANCE COMPLETED A REPAIR TO THE FUSELAGE PASSENGER DOOR SILL DUE TO OVERSIZED RIVET HOLES AT HINGE ATTACHMENT. REMOVED AND RPELACED DOOR SILL IAW FAC LAR 95-MALA-105. ALSO, INSTALLED MOD KIT 27K24182 ON FUSELAGE ANDApr 5, 1995 · N425MA · Swrngn SA227AC · Fuselage Miscellaneous StructureSDR MALA954400Te Skin · wornMSP - DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND THE RIGHT INBOARD FOREFLAP TRAILING EDGE WORN. REPLACED THE RT INBOARD FOREFLAP, PN 27-36000-006. (X)Apr 5, 1995 · N425MA · Swrngn SA227AC · Trailing Edge FlapsSDR MALA954399Stiffener · crackedMSP - DURING A SCHEDULED INSPECTION, MAINTENANCE REPAIRED THE BELLY FAIRING CENTER CHANNEL STIFFENER AT BL 0.00, PN 27-31110-032, DUE TO CRACKING. REPLACED ASSEMBLY, INSTALLED DOUBLER IAW FAC SRM 57-90-30 REPAIR NR 1 AND ADDED TEE ANGLES TO REDUCE POSSIBILITYApr 5, 1995 · N425MA · Swrngn SA227AC · Fuselage Miscellaneous StructureSDR MALA954398Corner · crackedMSP - DURING A SCHEDULED INSPECTION, REPAIRS WERE COMPLETED TO THE PASSENGER DOOR BY REPLACING THE FOLLOWING PARTS DUE TO CRACKING AT NUT PLATE AREA, LOWER FORWARD DOOR FRAME CORNER, PN 27-24044-010, AND LOWER FORWARD DOOR FRAME ASSEMBLY, PN 27-244150-0734, DOApr 5, 1995 · N425MA · Swrngn SA227AC · Fuselage Miscellaneous StructureSDR MALA954397Frame · crackedMSP - DURING SCHEDULED INSPECTION, FOUND FUSELAGE FRAME FS 332.27, PN 27-22093-104, HAD A .125 INCH CRACK AT RELIEF RADIUS IN LOWER BELT FRAME OF CONSTANT SECTION. REPAIRS WERE COMPLETED IAW SRM 53-90-20, REPAIR NR 19. (X)Apr 5, 1995 · N425MA · Swrngn SA227AC · Fuselage Main, FrameSDR MALA954396Frame · crackedDURING SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND FUSELAGE FRAME FS 159.247 P/N 27-22093-105 CRACKED AT THE INNER FLANGE OF CONSTANT SECTION .005 INCH LONG. REPAIRS WERE COMPLETED IAW FAC SRM 53-90-20 REPAIR NR 20. (W)Apr 5, 1995 · N425MA · Swrngn SA227AC · Fuselage Main, FrameSDR 95ZZZX1995Door Frame · crackedMSP - DURING A SCHEDULED INSPECTION, REPAIRS WERE COMPLETED TO THE PASSENGER DOOR BY REPLACING THE FOLLOWING PARTS DUE TO CRACKING AT NUT PLATE AREA, LOWER FORWARD DOOR FRAME CORNER, PN 27-24044-010, AND LOWER FORWARD DOOR FRAME ASSEMBLY, PN 27-244150-0734, DOApr 5, 1995 · N425MA · Swrngn SA227AC · Fuselage Miscellaneous StructureSDR MALA954356Frame · crackedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE FORWARD FUSELAGE FRAME OF THE AFT CARGO DOOR (P/N 27-20085) AT FS 491 CRACKED AT THE GAS STRUT ATTACHMENT HOLE. COMPLETED REPAIR TO THE FRAME IAW FAIRCHILD ARP 53-20-9503 AND SRM. (W)Mar 1, 1995 · N425MA · Swrngn SA227AC · Fuselage Main, FrameSDR MALA954238Doubler · wornDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE LEFT FLAP ROLLER DOUBLER WAS WORN. REPAIRS WERE COMPLETED THROUGH A PART FOR PART REPLACEMENT OF THE DOUBLER IAW FAC SRM 57-90-10 PAGES 45 AND 46 AND ARP 57-20-9424. (Z)Jan 11, 1995 · N425MA · Swrngn SA227AC · Trailing Edge FlapsSDR MALA954237Doubler · wornDURING A SCHEDULED INSPECTION IN MSP, THE RIGHT FLAP ROLLER DOUBLER WAS WORN. REPAIRS WERE COMPLETED IAW FAC MM PAGES 201-202. (Z)Jan 11, 1995 · N425MA · Swrngn SA227AC · Trailing Edge FlapsSDR MALA954234Light Relay · inopFLT 3074 - ON APPROACH TO MSP, THE GEAR DOOR POSITION LIGHT ILLUMINATED. THE LIGHT EXTINGUISHED WHEN THE GEAR WAS DOWN AND LOCKED. MAINTENANCE REPLACED A RELAY. SYSTEM OPERATED SATISFACTORILY. (Z)Jan 10, 1995 · N425MA · Swrngn SA227AC · Landing Gear Position and Warning
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