# Service difficulty reports: N445MA, cancelled Sep 30, 2005 A list on [N445MA, cancelled Sep 30, 2005](https://openairdocs.org/deregistered/N445MA-2005-09-30.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR I7WAB1536](https://openairdocs.org/sdr/I7WAB1536.md): Line · cracked · Jan 3, 2001 · N445MA · Swrngn SA227AC · Hydraulic System, Main > LOSS OF HYDRULIC FLUID. CAUSE:HARD LINE CRACKED, GEAR UP PRESSURE LINE. PART CRACKED AT 90 DEGREE BEND. REPLACED LINE. - [SDR 20010530CW003](https://openairdocs.org/sdr/20010530CW003.md): Spar · cracked · Dec 22, 2000 · N445MA · Swrngn SA227AC · Wing Spar > CRACKS FOUND IN WEB CUTOUTS. DURING INSPECTION CRACKS WERE FOUND. AIRCRAFT WILL BE FERRIED TO LOCATION TO BE REPAIRED. - [SDR MALA965027](https://openairdocs.org/sdr/MALA965027.md): Dir Gyro · internal fault · Jun 11, 1996 · N445MA · Swrngn SA227AC · Directional Gyro and Indicating System > FLT 3310 - AFTER TAKEOFF FROM DTW, THE CAPTAINS DIRECTIONAL GYRO WOULD INTERMITTENTLY FREEZE. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED THE NR 1 DIRECTIONAL GYRO. ALL CHECKS SATISFACTORY. (M) - [SDR MALA4896](https://openairdocs.org/sdr/MALA4896.md): Hyd Line · chafed · Mar 3, 1996 · N445MA · Swrngn SA227AC · Hydraulic System, Main > FLT NR 3285 - AFTER DEPARTURE FROM MLI, BOTH HYDRAULIC PRESSURE CAUTION LIGHTS ILLUMINATED AND THE HYDRAULIC PRESSURE DROPPED TO ZERO. THE CREW ELECTED TO RETURN TO MLI AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED A HYDRAULIC PUMP - [SDR MALA964887](https://openairdocs.org/sdr/MALA964887.md): Tq Signal Cond · failed · Feb 22, 1996 · N445MA · Swrngn SA227AC · Engine BMEP/Torque Indicating > FLT NR 3416 - ON CLIMB-OUT FROM DTW, THE LEFT ENGINES TORQUE INDICATION BEGAN TO FLUCTUATE AND THEN FAILED. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED THE NR 1 TORQUE SIGNAL CONDITIONER. ALL SYSTEMS OPERATED SATISFACTORILY. (M) - [SDR MALA964886](https://openairdocs.org/sdr/MALA964886.md): Tq Ring · failed · Feb 20, 1996 · N445MA · Swrngn SA227AC · Engine BMEP/Torque Indicating > FLT NR 3334 - ON CLIMB-OUT FROM DTW, THE NR 1 TORQUE GAUGE BEGAN TO FLUCTUATE BETWEEN ZERO AND 120 PERCENT. ALL OTHER ENGINE INDICATORS WERE NORMAL. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED THE LEFT TORQUE RING. SYSTEM OPERATED SATISFACTORILY. ( - [SDR MALA964836](https://openairdocs.org/sdr/MALA964836.md): Hts Switch · failed · Jan 23, 1996 · N445MA · Swrngn SA227AC · Propeller Controlling System > FLT 3269 - ON DESCENT TO MSP, THE LEFT OIL PRESSURE WARNING LIGHT ILLUMINATED AND THE LEFT OIL PRESSURE GAUGE INDICATED DECLINING PRESSURE. THE CREW SHUT THE ENGINE DOWN AND CONTINUED TO MSP. MAINTENANCE REPLACED THE NEGATIVE TORQUE SENSOR SWITCH. SYSTEM OP - [SDR MALA964801](https://openairdocs.org/sdr/MALA964801.md): Switch · failed · Jan 6, 1996 · N445MA · Swrngn SA227AC · Landing Gear Position and Warning > BRD - FLT 3236 - AFTER TAKEOFF, THE NLG RED INTRANSIT LIGHT DID NOT ILLUMINATE UPON GEAR RETRACTION. THE AIRCRAFT CONTINUED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED THE LT NLG UPLOCK SWITCH. ALL SYSTEMS OPERATED SATISFACTORILY. (X - [SDR MALA964802](https://openairdocs.org/sdr/MALA964802.md): Switches · out of adjust · Jan 5, 1996 · N445MA · Swrngn SA227AC · Landing Gear Retraction/Extension System > GFK - FLT 3253 - AFTER DEPARTURE, THE NOSE GEAR WOULD CYCLE IN THE GEAR WELL AFTER RETRACTION. THE CREW CYCLED THE GEAR SEVERAL TIMES AND THE CYCLING STOPPED. THE AIRCRAFT CONTINUED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL ADJUSTED THE RIGG - [SDR MALA954749](https://openairdocs.org/sdr/MALA954749.md): Switch · dirty · Dec 9, 1995 · N445MA · Swrngn SA227AC · Landing Gear Position and Warning > FLT NR 3065 - INBOUND TO DTW, THE NOSE GEAR GREEN LIGHT DID NOT ILLUMINATE WHEN THE GEAR HANDLE WAS SELECTED DOWN. THE CREW RECYCLED THE GEAR AND THE LIGHT ILLUMINATED. THE AIRCRAFT CONTINUED TO DTW WITHOUT INCIDENT. MAINTENANCE PERSONNEL CLEANED THE DOWN P - [SDR MALA954718](https://openairdocs.org/sdr/MALA954718.md): Brake System · req'd service · Nov 23, 1995 · N445MA · Swrngn SA227AC · Landing Gear Brake System > FLT NR 3141 - DURING TAXI AT DTW, THE CREW HAD TO PUMP THE BRAKE PEDALS TO GET ANY BRAKE EFFECTIVENESS. MAINTENANCE PERSONNEL BLED THE BRAKES AND SERVICED THE BRAKE RESERVOIR. ALL SYSTEMS OPERATED SATISFACTORILY. (M) - [SDR MALA954607](https://openairdocs.org/sdr/MALA954607.md): Door Frame · cracked · Aug 27, 1995 · N445MA · Swrngn SA227AC · Fuselage Miscellaneous Structure > MSP - DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND THE AFT CARGO DOOR FRAME AT FS 491.00 HAD A RADIAL CRACK IN THE GAS STRUT ATTACH HOLE AREA. REPAIRS WERE COMPLETED BY INSTALLING A REPAIR ANGLE, FILLER AND DOUBLER IAW ARP 53-20-9503. (X) - [SDR MALA954606](https://openairdocs.org/sdr/MALA954606.md): Angle · cracked · Aug 27, 1995 · N445MA · Swrngn SA227AC · Nacelle/Pylon Structure > MSP - DURING SCHEDULED INSPECTION, MAINTENANCE FOUND THE LEFT NACELLE INBOARD WING TO NACELLE ATTACH ANGLE CRACKED AT THE 9TH RIVET HOLE OF THE FORWARD END. REPAIRS WERE COMPLETED BY INSTALLING A REPAIR DOUBLER IAW FAC ARP 54-20-9101. (X) - [SDR MALA954605](https://openairdocs.org/sdr/MALA954605.md): Angle · cracked · Aug 27, 1995 · N445MA · Swrngn SA227AC · Nacelle/Pylon Structure > DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND THE RIGHT NACELLE INBOARD UPPER WING SKIN TO NACELLE ATTACH ANGLE CRACKED AT THE 10TH RIVET HOLE OF THE FORWARD END. REPAIRS WERE COMPLETED BY INSTALLING A DOUBLER IAW FAC ARP 54-20-9101. (X) - [SDR MALA954604](https://openairdocs.org/sdr/MALA954604.md): Corner · cracked · Aug 27, 1995 · N445MA · Swrngn SA227AC · Passenger/Crew Doors > MSP - DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND THE PASSENGER DOOR LOWER FORWARD CORNER CRACKED AT THE NUTPLATE GAS SPRING ATTACH PLATE. REPAIRS WERE COMPLETED BY REPLACING THE LOWER FORWARD PASSENGER DOOR CORNER IAW FAC MM 51-00-00 AND MM 51-40-01. ( - [SDR MALA954532](https://openairdocs.org/sdr/MALA954532.md): Dir Gyro · malfunctioned · Jul 10, 1995 · N445MA · Swrngn SA227AC · Directional Gyro and Indicating System > FLT 3213 - ON CLIMB-OUT FROM MSP, THE FIRST OFFICERS HSI AND CAPTAINS RMI HEADING INDICATOR STUCK. THE AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED THE NR 2 DIRECTIONAL GYRO. SYSTEM OPERATED SATISFACTORILY. (M) - [SDR MALA954373](https://openairdocs.org/sdr/MALA954373.md): Door Cable · failed · Mar 11, 1995 · N445MA · Swrngn SA227AC · Passenger/Crew Doors > FLT 3140 - ON CLIMB-OUT FROM DTW, THE AIRCRAFT WOULDN'T PRESSURIZE. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE FOUND THE PASSENGER DOOR CABLE WEDGED BETWEEN THE DOOR AND THE FRAME. MAINTENANCE REPLACED THE FORWARD CABLE RETRACTOR ASSY. SYSTEMS OPERATED SATI - [SDR MALA954351](https://openairdocs.org/sdr/MALA954351.md): Tray · cracked · Feb 28, 1995 · N445MA · Swrngn SA227AC · Battery Box Structure > MSP - DURING A SCHEDULED INSPECTION, MECHANICS FOUND RT BATTERY SUPPORT TRAY ASSEMBLY (PN 27-82366-904) CRACKED. COMPLETED REPAIR BY THE PART FOR PART REPLACEMENT OF THE BATTERY SUPPORT TRAY ASSEMBLY IAW THE FAIRCHILD SRM. (X) - [SDR MALA954350](https://openairdocs.org/sdr/MALA954350.md): Skin · dented · Feb 28, 1995 · N445MA · Swrngn SA227AC · Fuselage Main, Plate/Skin > MSP - DURING A MAINTENANCE INSPECTION, MECHANICS FOUND LOWER AFT FUSELAGE SKIN PANEL (PN 27-23000-011) DENTED BETWEEN STA NR 530.810 AND STA NR 548.810. COMPLETED REPAIR TO THE LOWER AFT SKIN PANEL IAW THE FAIRCHILD SRM. (X) - [SDR MALA954349](https://openairdocs.org/sdr/MALA954349.md): Rib · cracked · Feb 28, 1995 · N445MA · Swrngn SA227AC · Wing, Rib/Bulkhead > MSP - DURING A MAINTENANCE INSPECTION, MECHANICS FOUND TRAILING EDGE OF RT WING RIB (PN 27-31241-076) AT WS 66.58, CRACKED. COMPLETED REPAIR TO THE TRAILING EDGE OF THE RT WING RIB IAW FAIRCHILD LAR 95-MALA-064 AND SRM. (X) - [SDR MALA954345](https://openairdocs.org/sdr/MALA954345.md): Doubler · worn · Feb 27, 1995 · N445MA · Swrngn SA227AC · Trailing Edge Flaps > MSP - DURING SCHEDULED MAINTENANCE INSPECTION, MECHANICS FOUND THE RT SUPPORT DOUBLER (PN 27-31141-001) FOR THE FLAP WALKING BEAM ROLLER BEARING WORN. COMPLETED REPAIR BY REPLACEMENT OF THE SUPPORT DOUBLER IAW FAIRCHILD SRM AND ARP 57-20-9424. (X) ## 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 = 'N445MA' AND deregistration_id = 'N445MA-2005-09-30' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N445MA-2005-09-30/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.