N159MC

Service difficulty reports · 54

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 = 'N159MC' 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 DUFA20080001Overheat Sensor · defectiveWHILE ON CLIMB OUT, THE PILOT NOTICED THAT THE LT WING OVERHEAT LIGHT ILLUMINATED. FOLLOWING PROCEDURE, THE LT GENERATOR WAS SHUTDOWN, BLEED AIR TURNED OFF AND THE LANDING GEAR EXTENDED. AFTER 3 MINUTES THE LIGHT WAS STILL ILLUMINATED AND PROCEDURES CALL OUT FJan 3, 2008 · N159MC · Swrngn SA227AC · Overheat DetectionSDR EAC0705Overheat Sensor · defectiveWHILE ON CLIMB OUT, THE PILOT NOTICED THAT THE LT WING OVERHEAT LIGHT ILLUMINATED. FOLLOWING PROCEDURE, THE LT GENERATOR WAS SHUTDOWN, BLEED AIR TURNED OFF AND THE LANDING GEAR EXTENDED. AFTER 3 MINUTES THE LIGHT WAS STILL ILLUMINATED AND PROCEDURES CALL OUT FJan 3, 2008 · N159MC · Swrngn SA227AC · Overheat DetectionSDR DUFA010308001Warning Light · false activationWHILE ON CLIMB OUT, THE PILOT NOTICED THAT THE LT WING OVERHEAT LIGHT ILLUMINATED. FOLLOWING PROCEDURE, THE LT GENERATOR WAS SHUTDOWN, BLEED AIR TURNED OFF AND THE LANDING GEAR EXTENDED. AFTER 3 MINUTES THE LIGHT WAS STILL ILLUMINATED AND PROCEDURES CALL OUT FJan 3, 2008 · N159MC · Swrngn SA227AC · Overheat DetectionSDR DUFA20070003Overheat Sensor · defectiveSHORTLY AFTER DEPARTURE, THE LT WING OVERHEAT LIGHT ILLUMINATED. FOLLOWING PROCEDURE, THE PILOT SHUTDOWN THE LT GENERATOR, LT BLEED AIR AND EXTENDED THE LANDING GEAR. THE LIGHT REMAINED ILLUMINATED SO THE LT ENGINE WAS SHUTDOWN AS A PRECAUTIONARY MEASURE AND TApr 17, 2007 · N159MC · Swrngn SA227AC · Overheat DetectionSDR DUFA041707Overheat Sensor · defectiveSHORTLY AFTER DEPARTURE, THE LT WING OVERHEAT LIGHT ILLUMINATED. FOLLOWING PROCEDURE, THE PILOT SHUTDOWN THE LT GENERATOR, LT BLEED AIR AND EXTENDED THE LANDING GEAR. THE LIGHT REMAINED ILLUMINATED SO THE LT ENGINE WAS SHUTDOWN AS A PRECAUTIONARY MEASURE AND TApr 17, 2007 · N159MC · Swrngn SA227AC · Overheat DetectionSDR MR0510Line · crackedJUST BEFORE LANDING, HYDRAULIC VAPOR/SMOKE NOTED IN CABIN AND COCKPIT. AIRCRAFT LANDED WITHOUT INCIDENT, ENGINES SHUTDOWN AND PAX DEPLANED. MAINTENANCE FOUND FAILED HYDRAULIC LINE IN WING ROOT THAT SPRAYED FLUID INTO AIR CYCLE MACHINE INTAKE WHICH TRANSFERREMar 28, 2005 · N159MC · Frchld SA227CC · Hydraulic System, MainSDR 2005FA0000053Line · leakingMRR-M04-11, ENGINE RPM ONLY WENT TO 97 PERCENT DURING TAKEOFF ROLL AND TORQUE WAS ALSO LOW, ALSO, THERE WAS LITTLE RESPONSE TO POWER LEVER MOVEMENT. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. INITIALLY SUSPECTED FCU FAILURE, BUT UPON INSPECTION FOUND FCUJun 2, 2004 · N159MC · Swrngn SA227AC · Engine Fuel DistributionSDR 2005FA0000048Handle · incorrectTHE CARGO DOOR WARNING LIGHT CAME ON DURING CLIMBOUT, CREW RETURNED TO STATION. ONE OF THE FOLLOWING: DOOR CLOSING PROCEDURES, DOOR HARD TO CLOSE, DOOR CLICKCLACK RIGGING/ LUBRICATION, OR SWITCH RIGGING. MAINTENANCE FOUND HANDLE NOT FULLY ROTATED TO CLOSED May 3, 2004 · N159MC · Swrngn SA227AC · Cargo/Baggage DoorsSDR 2005FA0000046Door · out of alignmentCARGO DOOR WARNING LIGHT CAME ON AS POWER WAS BEING APPLIED FOR TAKEOFF, CREW DISCONTINUED TAKEOFF ROLL AND RETURNED TO GATE. ONE OF THE FOLLOWING: DOOR CLOSING PROCEDURES, DOOR HARD TO CLOSE, DOOR CLICKCLACK RIGGING/ LUBRICATION, OR SWITCH RIGGING. CLICK CLMar 22, 2004 · N159MC · Swrngn SA227AC · Cargo/Baggage DoorsSDR 2005FA0000042Squat Switch · damagedLANDING GEAR WOULD NOT RETRACT DURING CLIMBOUT, WHEN CREW WAS RETURNING FOR LANDING, GPWS GAVE (TO LOW GEAR) ALERT. THE CREW THEN INITIATED A GO-AROUND, ASKED TOWER TO CONFIRM, THREE GEAR DOWN, DID CONFIRM. CREW DECLARED EMERGENCY, MADE NORMAL LANDING, DURINMar 3, 2004 · N159MC · Swrngn SA227AC · Landing Gear Position and WarningSDR 2002F00418Handle · stuckCARGO DOOR LIGHT CAME ON DURING TAKEOFF ROLL AT APPROXIMATELY 50 KTS. CREW RETURNED TO GATE. STICKING DOOR HANDLE OR CLICK CLACKS. CLEANED AND LUBED CLICK CLACKS. (M)Jan 31, 2002 · N159MC · Swrngn SA227AC · Door Warning SystemSDR 2002F00352Latch · stuckCARGO DOOR LIGHT CAME ON DURING TAKEOFF ROLL AT APPROXIMATELY 50 KTS. CREW RETURNED TO GATE. STICKING DOOR HANDLE OR CLICK CLACKS. CLEANED AND LUBED CLICK CLACKS. (M)Jan 30, 2002 · N159MC · Swrngn SA227AC · Cargo/Baggage DoorsSDR 20010511SG003Warning Light · false activationFOUND CARGO DOOR WARNING LIGHT CAME ON IN FLIGHT DURING CLIMB-OUT AT ABOUT 10,000 FEET MSL. CREW RETURNED TO STATION WITHOUT INCIDENT. INSPECTED CARGO DOOR CLICK-CLACKS, CLEANED AND LUBED SWITCHES, GROUND OPS CHECK GOOD. NO FURTHER PROBLEMS NOTED. (M)Feb 25, 2001 · N159MC · Swrngn SA227AC · Door Warning SystemSDR 20001005AP011Moisture Vapor · detectedFLT 1308 - DFW - PASSENGERS REPORTED SMOKE IN THE CABIN TO THE CREW. CREW SHUT DOWN AIRCRAFT AND EVACUATED PASSENGERS. THE HUMIDITY WAS EXTREMELY HIGH, WITH A VERY SMALL TEMPERATURE SPREAD BETWEEN DEWPOINT AND TEMPERATURE. THIS CAUSED THE RESIDUAL MOISTURE May 10, 2000 · N159MC · Swrngn SA227AC · Air Distribution SystemSDR 20000614SH005Smoke · detectedDFW - FLT 1308 - PASSENGERS REPORTED SMOKE IN THE CABIN TO THE CREW. CREW SHUT DOWN AIRCRAFT AND EVACUATED PASSENGERS. THE HUMIDITY WAS EXTREMELY HIGH WITH A VERY SMALL TEMPERATURE SPREAD BETWEEN DEWPOINT AND TEMPERATURE. THIS CAUSED THE RESIDUAL MOISTURE IMay 10, 2000 · N159MC · Swrngn SA227AC · Air Distribution SystemSDR MALA975354Temp Contl Valve · failedFLT 3049 - EN ROUTE TO LNK, THE CABIN AND COCKPIT FILLED WITH SMOKE, CREW AND PASSENGERS ON OXYGEN. FLIGHT WAS DIVERTED TO OMA, LANDED WITH NO INCIDENTS. MAINTENANCE REMOVED AND REPLACED TEMPERATURE CONTROL MASTER VALVE. OPS CHECK GOOD. (M)Mar 26, 1997 · N159MC · Swrngn SA227AC · Cabin Temperature Control SystemSDR MALA975344Rib · crackedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND A CRACK IN THE LEFT FLAP S/N 1159 OUTBOARD FLAP NOSE RIB. REMOVED AND REPLACED FLAP NOSE RIB P/N 27-36015-009 AND HINGE ARM P/N 27-36044-003 IAW FAIRCHILD SRM 57-90-60 PAGES 43-46. (M)Mar 8, 1997 · N159MC · Swrngn SA227AC · Trailing Edge FlapsSDR MALA975342Frame · crackedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND A .25 INCH CRACK IN RIGHT SIDE OF LOWER CONSTANT SECTION RELIEF RADIUS AT FUSELAGE FRAME STATION 377. COMPLETED REPAIR TO RIGHT LOWER CONSTANT SECTION FRAME IAW AERO TECH DESIGNS EA01-96136. (M)Mar 4, 1997 · N159MC · Swrngn SA227AC · Fuselage Main, FrameSDR MALA975341Frame · crackedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND A .25 INCH CRACK IN LEFT SIDE OF LOWER CONSTANT SECTION RELIEF RADIUS AT FUSELAGE FRAME STATION 287. COMPLETED REPAIR TO LEFT LOWER CONSTANT SECTION IAW AERO TECH DESIGNS EA01-96136. (M)Mar 4, 1997 · N159MC · Swrngn SA227AC · Fuselage Main, FrameSDR MALA975296Switch · failedFLT 3332 - IN FLIGHT, AIRCRAFT IS TRIMMED OUTSIDE GREEN ARC ON TRIM INDICATOR, ORAL OUT OF TRIM WARNING SOUNDS WITH GEAR RETRACTED. CREW CYCLED GEAR, NO CHANGE. AIRCRAFT TRIMS NORMALLY AND WARNING STILL SOUNDS. AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACEJan 22, 1997 · N159MC · Swrngn SA227AC · Landing Gear Position and WarningSDR MALA965236Skin · crackedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND A CRACK IN RT FLAP SKIN S/N RPL 1688. CRACK IS APPROXIMATELY 1 INCH IN LENGTH. COMPLETED REPAIR TO FLAP IAW FAIRCHILD SRM 57-90-60 PAGES 19-21. (M)Dec 7, 1996 · N159MC · Swrngn SA227AC · Trailing Edge FlapsSDR MALA965235Rib · crackedMALA - DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND A CRACK IN RT FLAP, S/N RPL1688, OUTBOARD FLAP NOSE RIB. REMOVED AND REPLACED FLAP NOSE RIB, P/N 27-36015-002 IAW FAIRCHILD SRM 57-90-60 PAGES 43-46. (M)Dec 7, 1996 · N159MC · Swrngn SA227AC · Trailing Edge FlapsSDR MALA964995Brake Line · out of positionFLT N3393 - ON CLIMB-OUT FROM MSP, THE CREW NOTED A LIGHT RUBBER BURNING SMELL THAT DISSIPATED IN APPROXIMATELY 5 MINUTES. UPON POST FLIGHT INSPECTION, THE LEFT MAIN GEAR INBOARD BRAKE LINE WAS FOUND TO BE RUBBING ON THE TIRE. MX INSPECTED THE LINE AND FOUNDMay 16, 1996 · N159MC · Swrngn SA227AC · Landing Gear Brake SystemSDR MALA964940Door Frame · crackedMSP - DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND A CRACK IN THE FUSELAGE FORWARD CARGO DOOR FRAME (PN 27-22085) AT FS 438. REPAIRS WERE COMPLETED BY REMOVING THE CRACKED AREA AND INSTALLING REPAIR DOUBLERS IAW FAC ARP 53-20-5503. (X)Apr 1, 1996 · N159MC · Swrngn SA227AC · Fuselage Miscellaneous StructureSDR MALA964939Intercostal · crackedMSP - DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND THE LEFT LOWER FUSELAGE INTERCOSTAL, AT FS 212.37 (PN 27-22104), CRACKED IN THE FLANGE RELIEF RADIUS. REPAIRS WERE COMPLETED BY STOP DRILLING THE CRACK AND INSTALLING A REPAIR DOUBLER AND STIFFENER IAW FAApr 1, 1996 · N159MC · Swrngn SA227AC · Fuselage Miscellaneous StructureSDR MALA964938Corner · crackedMSP - DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND THE LOWER AFT PASSENGER DOOR CORNER, PN 27-24044, CRACKED AT SNUBBER ATTACH NUTPLATE. REPAIRS WERE COMPLETED BY REPLACING THE CORNER IAW FAC SRM'S 51-00-00, 51-30-02, 51-30-04, AND 51-40-00. (X)Apr 1, 1996 · N159MC · Swrngn SA227AC · Passenger/Crew DoorsSDR MALA964937Skin · crackedMSP - DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND THE PASSENGER DOOR LOWER SKIN EDGE CRACKED OFF AT THE FORWARD HINGE RECESS. REPAIRS WERE COMPLETED BY INSTALLING A REPAIR DOUBLER IAW ARP 52-10-8701, SRM 51-30-04 AND SRM 51-40-01. (X)Apr 1, 1996 · N159MC · Swrngn SA227AC · Passenger/Crew DoorsSDR MALA964936Skin · crackedMSP - DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND THE PASSENGER DOOR LOWER SKIN EDGE CRACKED OFF AT THE AFT HINGE RECESS. REPAIRS WERE COMPLETED BY INSTALLING A REPAIR DOUBLER IAW ARP 52-10-8701, SRM 51-30-04, AND SRM 51-40-01. (X)Apr 1, 1996 · N159MC · Swrngn SA227AC · Passenger/Crew DoorsSDR MALA964935Angle · crackedMSP - DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND THE RIGHT INBOARD LOWER WING TO NACELLE TRANSIT/ATTACH ANGLE CRACKED APPROXIMATELY .750 INCHES AT THE FORWARD END. REPAIRS WERE COMPLETED BY INSTALLING A REPAIR DOUBLER IAW FAC SRM 51-00-00 AND ARP 54-20-Apr 1, 1996 · N159MC · Swrngn SA227AC · Wing Miscellaneous StructureSDR MALA964934Sill Frame · crackedMSP - DURING A SCHEDULED INSPECTION, THE CARGO DOOR SILL FRAME AT FS 438 WAS FOUND TO HAVE A .25 INCH CRACK. REPAIRS WERE COMPLETED BY STOP DRILLING THE CRACK, ENLARGING THE CUT OUT IN THE SILL, AND WET INSTALLING TWO DOUBLERS IAW FAC ARP 53-30-5507. (X)Apr 1, 1996 · N159MC · Swrngn SA227AC · Fuselage Miscellaneous StructureSDR MALA964847Switch · failedFLT 3202 - ON CLIMB-OUT FROM MSP, THE CABIN DOOR ANNUNCIATOR LIGHT ILLUMINATED. AFTER THE CREW TURNED OFF THE BLEEDS AND DEPRESSURIZED THE CABIN, THE LIGHT EXTINGUISHED. THE AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED THE UPPER CENTER PASSENGER DOOR SWITJan 28, 1996 · N159MC · Swrngn SA227AC · Door Warning SystemSDR MALA964829Frame · crackedDURING A SCHEDULED INSPECTION MSP, MAINTENANCE PERSONNEL NOTED A CRACK IN THE FUSELAGE FRAME AT FS 174. THEY STOP DRILLED THE CRACK AND FABRICATED AND INSTALLED A REPAIR DOUBLER IAW FAC SRM 53-90-20. (M)Jan 20, 1996 · N159MC · Swrngn SA227AC · Fuselage Main, FrameSDR MALA954786Nut · malfunctionedFLT 3237 - DURING APPROACH TO BJI, CREW NOTED AN EXCESSIVE PITCH DOWN WHEN POWER WAS REDUCED. AFTER PERFORMING A GO-AROUND, ACFT RETURNED TO BJI AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL FOUND UPPER ELEVATOR STOP BOLT HAD MIGRATED OUT RESULTING IN IDec 28, 1995 · N159MC · Swrngn SA227AC · Elevator Control SystemSDR MALA954783Skin · crackedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED A CRACK IN THE LEFT VERTICAL STABILIZER SKIN. STOP DRILLED THE CRACK AND INSTALLED A REPAIR DOUBLER IAW FAC SRM 55-90-30. (M)Dec 26, 1995 · N159MC · Swrngn SA227AC · Vertical Stabilizer, Plate/SkinSDR MALA954744Seat Track · crackedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND CRACKS AT THE LEFT OUTBOARD SEAT TRACK ATTACH HOLES ON FS 116.56. REPAIRS WERE COMPLETED BY INSTALLING A REPAIR ANGLE IAW AERO TECH DESIGNS EA 01-95032. (M)Dec 9, 1995 · N159MC · Swrngn SA227AC · Fuselage, Seat/Cargo Attach FittingsSDR MALA954743Seat Channel · crackedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND CRACKS AT THE NUT PLATE ATTACH RIVET HOLES ON THE RIGHT INBOARD SEAT CHANNEL LOCATED APPROXIMATELY 4 INCHES AFT OF FS 107. REPAIRS WERE COMPLETED BY INSTALLING A DOUBLER IAW FAC ARP 53-10-9322. (M)Dec 9, 1995 · N159MC · Swrngn SA227AC · Fuselage, Seat/Cargo Attach FittingsSDR MALA954666Seal · failedFLT NR 3487 - IN CRUISE FLIGHT TO MSP, THE CREW NOTED THAT SMOKE WAS NOTED WITH THE BLEED AIR ON. THE CREW TURNED OFF THE BLEED AIR SYSTEMS AND CONTINUED TO MSP. MAINTENANCE REPLACED THE RIGHT COMPRESSOR SEAL. ALL CHECKS WERE SATISFACTORILY. (M)Oct 16, 1995 · N159MC · Swrngn SA227AC · Turbine Engine Compressor SectionSDR MALA954602Oil Press Trans · malfunctionedFLT NR 3075 - ON CLIMB-OUT FROM MSP, THE CREW NOTED THAT THE RIGHT OIL PRESSURE GAUGE WAS FLUCTUATING ERRATICALLY BETWEEN 10 PSI AND 100 PSI. ALL OTHER INDICATIONS WERE NORMAL. THE AIRCRAFT RETURNED TO MSP. MAINTENANCE COMPLETED GROUND RUNS AT CRUISE POWER Aug 24, 1995 · N159MC · Swrngn SA227AC · Engine Oil PressureSDR MALA954594Bellcrank · wornFLT NR 3213 - ON CLIMB-OUT FROM MSP, THE CABIN DOOR WARNING LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED THE LEFT AND RIGHT UPPER BAYONET BELLCRANK ASSY. SYSTEM OPERATED SATISFACTORILY. (M)Aug 21, 1995 · N159MC · Swrngn SA227AC · Passenger/Crew DoorsSDR MALA954587Bushing · wornFLT 3220 - ON CLIMB-OUT FROM MSP, THE CABIN DOOR WARNING LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO MSP. REPAIRS WERE COMPLETED BY REPLACING THE BUSHING FOR THE UPPERMOST BAYONET. SYSTEM OPERATED SATISFACTORILY. (M)Aug 20, 1995 · N159MC · Swrngn SA227AC · Passenger/Crew DoorsSDR MALA954389Switch · out of adjustFLT 3218 - IN CRUISE FLIGHT FROM MSP, THE PRIMARY AND SECONDARY CARGO DOOR WARNING LIGHTS ILLUMINATED. THE AIRCRAFT RETURNED TO MSP WITHOUT FURTHER INCIDENT. MAINTENANCE ADJUSTED THE CARGO DOOR HANDLE WARNING SWITCH. SYSTEM OPERATED SATISFACTORILY. (W)Mar 28, 1995 · N159MC · Swrngn SA227AC · Door Warning SystemSDR MALA954382Skin · damagedDURING A SCHEDULED MAINTENANCE INSPECTION IN MSP, MECHANICS FOUND THE UPPER ATTACHMENT SCREWS FOR RT WING EXTENSION SKIN PANEL (P/N 27-31361-332) TO BE PULLING THROUGH THE SKIN PANEL, ALONG WS 266.0. COMPLETED REPAIR TO THE UPPER RT WING SKIN IAW THE FAIRCHILMar 15, 1995 · N159MC · Swrngn SA227AC · Wing, Plate/SkinSDR MALA954381Skin · damagedDURING A SCHEDULED INSPECTION IN MSP, MECHANICS FOUND THE UPPER ATTACHMENT SCREWS FOR LEFT WING EXTENSION SKIN PANEL (P/N 27-31361-331) TO BE PULLING THROUGH THE SKIN PANEL ALONG WSL 266.0. COMPLETED REPAIR TO THE LEFT UPPER WING SKIN IAW THE FAIRCHILD SRM. Mar 15, 1995 · N159MC · Swrngn SA227AC · Wing, Plate/SkinSDR MALA954380Frame · crackedDURING A SCHEDULED MAINTENANCE INSPECTION IN MSP, MECHANICS FOUND THE RT LOWER BELT FRAME P/N 27-22104-047 TO BE CRACKED AT THE UPPER, OUTBOARD RELIEF RADIUS OF FS 212.27. COMPLETED REPAIR TO THE LOWER BELT FRAME IAW THE FAIRCHILD SRM. (W)Mar 15, 1995 · N159MC · Swrngn SA227AC · Fuselage Main, FrameSDR MALA954379Frame · crackedDURING A SCHEDULED MAINTENANCE INSPECTION, MECHANICS FOUND THE LEFT LOWER BELT FRAME, P/N 27-22100-036, TO BE CRACKED AT THE UPPER, OUTBOARD FLANGE RELIEF RADIUS OF FS 242.27. COMPLETED REPAIR TO THE LOWER BELT FRAME IAW THE FAIRCHILD SRM. (W)Mar 15, 1995 · N159MC · Swrngn SA227AC · Fuselage Main, FrameSDR MALA954378Frame · crackedDURING A SCHEDULED MAINTNENANCE INSPECTION IN MSP, MECHANICS FOUND THE REAR FUSELAGE MOUNTED FRAME OF THE AFT CARGO DOOR (P/N 27-0085) TO BE CRACKED AT THE GAS STRUT ATTACHMENT HOLE. COMPLETED REPAIR TO THE FRAME IAW FAIRCHILD ARP 53-20-9503 AND THE FAIRCHILDMar 15, 1995 · N159MC · Swrngn SA227AC · Fuselage Main, FrameSDR MALA954377Intercostal · crackedDURING A SCHEDULED MAINTENANCE INSPECTION IN MSP, MECHANICS FOUND THE RT LOWER INTERCOSTAL P/N 27-22108-035 TO BE CRACKED AT THE LOWER, CENTER AISLE SUPPORT FLANGE RELIEF RADIUS OF FS 287.27. COMPLETED REPAIR TO THE INTERCOSTAL FRAME IAW THE FAIRCHILD SRM. (Mar 15, 1995 · N159MC · Swrngn SA227AC · Fuselage Miscellaneous StructureSDR MALA954376Support · crackedDURING A SCHEDULED MAINTENANCE INSPECTION IN MSP, MECHANICS FOUND THE FORWARD FUSELAGE BELLY SUPPORT CHANNEL (P/N 27-31110-033) AT BL 0.00 TO BE CRACKED. COMPLETED REPAIR TO THE SUPPORT CHANNEL IAW THE FAIRCHILD SRM. (W)Mar 15, 1995 · N159MC · Swrngn SA227AC · Fuselage Miscellaneous StructureSDR MALA954358Frame · crackedDURING AN INSPECTION IN MSP, MAINTENANCE REPAIRED A .250 INCH CRACK TO FUSELAGE FRAME P/N 27-22093-106, FS 144.24 IAW FAC ARP 53-20-9148, REV A AND LAR 95-MALA-072 AND SRM 51-00-00 STANDARD PRACTICES. (W)Mar 6, 1995 · N159MC · Swrngn SA227AC · Fuselage Main, FrameSDR MALA954357Frame · crackedMSP - DURING INSPECTION, MAINTENANCE REPAIRED A .500 INCH CRACK ON FUSELAGE FRAME, FS 174.24, IAW FAC SRM 53-90-20, REPAIR NR 20, AND SRM 51-00-00. (X)Mar 6, 1995 · N159MC · Swrngn SA227AC · Fuselage Main, Frame
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