N426MA
Registered owner: UAS TRANSERVICES INC, FL (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| AMERIFLIGHT, LLC (JIKA) | Certificate holder | — | Matched by certificate designator |
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
DURING CLIMB THE RIGHT âHYD LOW PRESSâ ANNUNCIATOR CAME ON, THE HYDRAULIC PRESSURE GAUGE WAS READING NORMAL. PHOENIX MAINTENANCE INSPECTED AND PERFORMED RIGHT HYDRAULIC SYSTEM OPERATIONAL CHECKS, ACTUATING THE FLAPS FULL UP TO FULL DOWN REPEATEDLY RH HYDRAULIC PRESSURE WAS NORMAL NO FAULTS WERE FOUND.
ON DEPARTURE, THE PILOT REPORTED THAT THE CARGO DOOR ANNUNCIATOR ILLUMINATED JUST AT ROTATION AND DECLARED AN EMERGENCY, RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED AN INSPECTION OF THE MECHANICAL LOCKING FEATURES OF THE CARGO DOOR AND CONTINUES TO TROUBLESHOOT THE ISSUE. OPEN
ON APPROACH PILOT NOTICED HYD PRESS BOUNCING BETWEEN 1800 & 1000 PSI. SHORTLY THEREAFTER RT HYD PRESS ANNUNCIATOR ILLUMINATED. PILOT DECIDED TO PERFORM A MANUAL EXTENSION OF LG, PILOT RECEIVED THREE GREEN DOWN & LOCKED INDICATOR LIGHTS. LANDED WITHOUT FURTHER INCIDENT. TROUBLESHOOTING REVEALED A PIN HOLE IN LG SYS GEAR UP HYD LINE. R & R LINE WITH NEW FABRICATED 27-81032-081 HYD LINE & BOTH HYD PUMP DUE TO CAVITATIONâS OF PUMP IAW MM 29-00-00. OPERATIONAL CHECKS PERFORMED IAW MM 29-10-20.
THE PILOT REPORTED THAT DURING CLIMBOUT FROM LAS AND LEVELING OFF FOR 15000 FEET THE LEFT ENGINE FIRE ANNUNCIATOR LIGHT CAME ON VERY DIM TO A LOW STEADY LIGHT. THE PILOT REQUESTED RETURN TO KLAS. ON RETURN TO KLAS WITH THE BLEED AIR OFF AND THE POWER REDUCED FOR DESCENT THE LIGHT EXTINGUISHED. THE PILOT LANDED AT KLAS WITHOUT INCIDENT. PHX MAINTENANCE INSPECTED THE LEFT ENGINE, S/N P44209, AND FOUND A COMBUSTION CASE BLEED AIR PLUG GASKET, P/N 868746-6, BLOWN OUT AND LEAKING ALLOWING BLEED AIR TO BLOW ON THE FIRE DETECTOR. REMOVED AND REPLACED THE BLEED AIR GASKET WITH NEW, GROUND RUN OPS CHECK OK. LEFT ENGINE FIRE EXTINGUISHER LIGHT REMAINED EXTINGUISHED.
THE PILOT REPORTED THAT SHORTLY AFTER TAKEOFF FROM KPRC THE LEFT ENGINE FIRE WARNING LIGHT ILLUMINATED. THE PILOT NOTICED THE LIGHT WAS VERY DIM, NOT AS BRIGHT AS THE NORMAL DIM SETTING. ALL OTHER ENGINE INDICATIONS WERE NORMAL. DUE TO BOTH THE MAIN ANNUNCIATOR FIRE WARNING LIGHT AND THE FIRE EXTINGUISHER ANNUNCIATOR WARNING LIGHT BOTH GIVING A FIRE WARNING INDICATION THE PILOT ELECTED TO RETURN TO KPRC AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE LEFT ENGINE AND FOUND NO EVIDENCE OF A FIRE. THE INDIVIDUAL FIRE DETECTION SENSORS WERE INSPECTED AND THE TERMINALS WERE CLEANED AND REINSTALLED. THE FIRE DETECTION SYSTEM FUNCTIONAL CHECKED OK. THERE WERE NO DISCREPANCIES REPORTED ON SUBSEQUENT FLIGHTS.
FLT 3002 - AFTER TAKEOFF, RIGHT GENERATOR FAILED. CREW USED QUICK REFERENCE HANDBOOK AND TRIED TO RESET. GENERATOR WOULD NOT COME ON LINE. AIRCRAFT RETURNED TO MSP. MAINTENANCE REMOVED AND REPLACED RIGHT STARTER GENERATOR AND RIGHT GCU. OPS CHECK GOOD. (M)
FLT 3262 - DURING PREFLIGHT IN MSP, LEFT ENGINE DID NOT MAKE STANDARD POWER, 88 PERCENT TORQUE, 610 DEGREE MAX, NO BYPASS LIGHT, BUT FUEL LIMITED. MAINTENANCE TIGHTENED PRIMARY BLEED TUBE UPPER CLAMP. MAINTENANCE COMPLETED POWER CHECK BLEEDS, ON/OFF. OPS CHECK GOOD. (M)
FLT 2935 - DURING APPROACH TO MSP, NOSE GEAR INTRANSIT LIGHT DOES NOT ILLUMINATE WHEN GEAR SELECTED DOWN OR UP. MAINTENANCE CLEANED AND LUBED NOSE LANDING GEAR SWITCHES. PERFORMED COMPLETE FUNCTION CHECK OF GEAR. OPS CHECK GOOD. (M)
FLT 3038 - ON CLIMB-OUT FROM MSP, THE RIGHT GEAR INTRANSIT LIGHT WAS SLOW TO EXTINGUISH AFTER GEAR RETRACTION. THE AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED THE RIGHT OUTBOARD GEAR POSITION SWITCH. ALL CHECKS SATISFACTORY. (M)
FLIGHT 3330 - ON CLIMB-OUT FROM LSE, ALL THREE RED INTRANSIT LIGHTS REMAINED ILLUMINATED AFTER GEAR RETRACTION. AFTER AN EXTENDED PERIOD OF TIME, ALL GEARS SHOWED GREEN UP AND LOCKED. MAINTENANCE REPLACED THE LANDING GEAR VALVE, P/N 24600-6. ALL CHECKS SATISFACTORY. (M)
FLT 3492 - ON CLIMB-OUT FROM STC, THE LANDING GEAR DIDN'T REMAIN UP AND LOCKED AFTER GEAR RETRACTION. THE CREW CYCLED THE GEAR AND THE GEAR REMAINED UP AND LOCKED. MAINTENANCE WAS UNABLE TO DUPLICATE THE DISCREPANCY. MAINTENANCE LUBED THE GEARS AND CHANGED THE MAIN HYDRAULIC FILTER AS A PRECAUTION. (M)
DURING BLOCK INSPECTION IN MSP, MAINTENANCE FOUND A CRACK IN RIGHT INBOARD FLAP NOSE RIB. REMOVED AND REPLACED FLAP NOSE RIB P/N 27-36004-008 IAW FAIRCHILD STRUCTURAL REPAIR MANUAL 51-00-00 PAGE 4 AND FAIRCHILD SB 227-27-023. (M)
DURING A BLOCK INSPECTION IN MSP, MAINTENANCE FOUND A CRACK IN THE LEFT OUTBOARD FLAP NOSE RIB. REMOVED AND REPLACED FLAP NOSE RIB P/N 27-36015-001 IAW FAC SRM 57-90-60 PAGES 43-46. (M)
DURING A MAINTENANCE INSPECTION IN MSP, MAINTENANCE FOUND THE FORWARD CARGO DOOR FRAME AT FS 438 CRACKED AT GAS STRUT SUPPORT MOUNTING HOLE. COMPLETED REPAIR TO FUSELAGE FORWARD CARGO DOOR FRAME P/N 27-22085 AT FS 438 DUE TO REPAIR TO FUSELAGE FORWARD CARGO DOOR FRAME P/N 27-22085 AT FS 438 DUE TO .25 INCH CRACK NOTED IN AREA OF THE DOOR GAS STRUT SUPPORT LOWER MOUNT HOLE. REMOVED CRACKED AREA AND INSTALLED REPAIR DOUBLERS IAW FAC ARP 53-20-9503. (M)
DURING A BLOCK INSPECTION IN MSP, MAINTENANCE FOUND A CRACK IN RIGHT SIDE OF LOWER CONSTANT SECTION AT FUSELAGE STATION 392. COMPLETED REPAIR TO CONSTANT SECTION IAW FAC SRM 53-90-20 REPAIR NR 20. (M)
DURING A BLOCK IINSPECTION IN MSP, FOUND A CRACK IN RIGHT LOWER INBOARD WING TO NACELLE INTRANSIT ANGLE. COMPLETED REPAIR TO WING TO NACELLE ANGLE IAW FAIRCHILD ARP 54-20-9101 REV B. (M)
FLT 3430 - AFTER TAKEOFF FROM LSE, THE CARGO DOOR PRIMARY AND SECONDARY WARNING LIGHTS ILLUMINATED. THE AIRCRAFT RETURNED TO LSE. MAINTENANCE REPLACED THE OVERCENTERING SPRING, P/N 27-24010-001, AND REPLACED A BENT ROD ASSEMBLY, P/N 27-24133-155. ALL CHECKS SATISFACTORY. REFERENCE MALA965176.
FLT 3430 - AFTER TAKEOFF FROM LSE, THE CARGO DOOR PRIMARY AND SECONDARY WARNING LIGHTS ILLUMINATED. THE AIRCRAFT RETURNED TO LSE. MAINTENANCE REPLACED THE OVERCENTERING SPRING, P/N 27-24010-001, AND REPLACED A BENT ROD ASSEMBLY, P/N 27-24133-155. ALL CHECKS SATISFACTORY. (M)
FLT 3412 - AFTER TAKEOFF FROM MSP, THE CARGO DOOR ANNUNCIATOR ILLUMINATED. THE AIRCRAFT RETURNED TO MSP. MAINTENANCE FOUND HANDLE NOT FULLY SECURED. THE LATCH WAS CYCLED SEVERAL TIMES. ALL CHECKS GOOD. (M)
FLT NR 3355 - AFTER ROTATION, THE CARGO DOOR WARNING LIGHTS ILLUMINATED. THE AIRCRAFT RETURNED TO YNG. MAINTENANCE INSPECTED THE DOOR MECHANISMS. THE DISCREPANCY COULD NOT BE DUPLICATED. ALL SYSTEMS OPERATED SATISFACTORILY. (M)
FLT 3087 - ON CLIMB-OUT FROM YQT, THE CREW NOTED THAT THE NOSE GEAR CYCLED IN THE WHEEL WELL FIVE TIMES BEFORE COMING UP AND LOCKED. THE AIRCRAFT CONTNUED TO MSP WITHOUT FURTHER INCIDENT. MAINTENANCE RE-RIGGED THE UPLIMIT AND UP POSITION SWITCHES. ALL SYSTEMS OPERATED SATISFACTORILY. (M)
MSP - DURING AN INSPECTION, FOUND FUSELAGE SKIN DENTED AFT OF CARGO DOOR AT FS 493.00 AND WL 75.00. REMOVED DAMAGED AREA (8.00 INCHES BY 9.75 INCHES), FABRICATED REPAIR DOUBLER, REPAIR FILLER, AND INSTALLED IAW FAIRCHILD SRM 53-90-20, PAGES 64-65. (X)
MSP - DURING SCHEDULED MAINTENANCE, MAINTENANCE FOUND THE FUSELAGE FRAME AT FS 51.31 CRACKED AT THE RIGHT BAGGAGE DOOR LOWER LATCH RECEPTACLE CUT OUT. REPAIRS WERE COMPLETED BY STOP DRILLING THE CRACK AND INSTALLING AN INTERNAL DOUBLER IAW FAC LAR 96-MALA-057. (X)
FLT 3095 - AFTER DEPARTURE FROM DSM, THE CARGO DOOR WARNING LIGHT ILLUMINATED. THE CREW ELECTED TO RETURN TO DSM AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL FUNCTIONALLY TESTED THE CARGO DOOR WARNING SYSTEM, BUT WERE UNABLE TO DUPLICATE THE DISCREPANCY. ALL SYSTEMS OPERATED SATISFACTORILY. (X)
FLT 3297 - AFTER DEPARTURE FROM MSP, CREW NOTED A FLUCTUATION IN THE LT ENGINE TORQUE INDICATION. THEY ELECTED TO RETURN TO MSP AND THE ACFT LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL CHANGED FROM NR 1 TO NR 2 TSC BRIDGE AND CLEANED THE LT TORQUE RING CANNON PLUG. ALL SYSTEMS OPERATED SATISFACTORILY. (X)
BEH - FLT 3485 - DURING APPROACH, THE RT MAIN GEAR DOWN AND LOCKED LIGHT DID NOT ILLUMINATE. THE CREW RECYCLED THE GEAR AND THE LIGHT ILLUMINATED NORMALLY. THE AIRCRAFT CONTINUED TO BEH AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED THE RT MLG ACTUATOR, PN 27-51016-003. ALL SYSTEMS OPERATED SATISFACTORILY. (X)
FLT NR 3156 - INBOUND TO DTW, THE RIGHT MAIN GEAR DID NOT EXTEND WHEN THE GEAR HANDLE WAS SELECTED DOWN. THE CREW RECYCLED THE GEAR AND IT EXTENDED NORMALLY. THE AIRCRAFT CONTINUED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL FUNCTIONALLY TESTED THE LANDING GEAR SYSTEM, BUT WERE UNABLE TO DUPLICATE THIS DISCREPANCY. THE LANDING GEAR POSITION INDICATOR WAS REPLACED AS A PRECAUTION. (M)
FLT NR 3409 - ON APPROACH TO DTW, THE CREW DID NOT GET A GREEN DOWN AND LOCKED LIGHT FROM THE RIGHT MAIN GEAR. THEY RECYCLED THE GEAR TWICE AND THE LIGHT ILLUMINATED. THE AIRCRAFT CONTINUED TO DTW WITHOUT INCIDENT. MAINTENANCE PERSONNEL CLEANED AND LUBRICATED THE RIGHT INBOARD MLG POSITION SWITCH. ALL SYSTEMS OPERATED SATISFACTORILY. (M)
FLT NR 3359 - INBOUND TO DTW, WHEN THE CREW SELECTED GEAR DOWN, THE RIGHT MAIN GEAR INTRANSIT LIGHT REMAINED ILLUMINATED AND THE GREEN LIGHT DID NOT ILLUMINATE. THE CREW RECYCLED THE GEAR, ALL INDICATIONS WERE NORMAL. THE AIRCRAFT CONTINUED TO DTW WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED THE LOWER OUTBOARD DOWN AND LOCKED POSITION SWITCH. ALL SYSTEMS OPERATED SATISFACTORILY. (M)
FLT NR 3065 - INBOUND TO DTW, THE CREW HAD TO CYCLE THE LANDING GEAR THREE TIMES IN ORDER TO GET A GREEN LIGHT FOR THE RIGHT MAIN GEAR. THE AIRCRAFT CONTINUED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED THE RT INBOARD GEAR POSITION SWITCH. ALL SYSTEMS OPERATED SATISFACTORILY. (M)
FLT NR 3357 - EN ROUTE TO DTW, THE ELEVATOR WOULD OCCASIONALLY PITCH UP OR DOWN ABRUPTLY, GIVING UP TO AN 800 FPM VERTICAL SPEED. THE AIRCRAFT CONTINUED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED BUSHINGS AT THE LOWER PITCH TRIM ACTUATOR MOUNT LUGS. ALL SYSTEMS OPERATED SATISFACTORILY. (M)
FLT NR 3330 - DTW-SBN - EN ROUTE, THE LEFT CHIP DETECTOR LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL REMOVED A SMALL FLAKE FROM THE CHIP DETECTOR, TOOK AN OIL SAMPLE, AND PLACED A RESAMPLE WATCH ITEM ON THE ENGINE. ALL SYSTEMS OPERATED SATISFACTORILY. (M)
DURING A SCHEDULED INSPECTION IN MSP, THE LEFT OUTBOARD LOWER WING SKIN TO NACELLE ATTACH ANGLE WAS FOUND TO BE CRACKED AT THE 10TH RIVET FROM THE FORWARD END. REPAIRS WERE COMPLETED BY INSTALLING A REPAIR DOUBLER IAW ARP 54-20-9101 REVISION 10. (M)
DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE LEFT INBOARD WING TO NACELLE SKIN ATTACH ANGLE CRACKED AT THE 5TH AND 8TH RIVETS. REPAIRS WERE COMPLETED BY INSTALLING A REPAIR ANGLE IAW ARP 54-28-9101. (M)
DURING A SCHEDULED INSPECTION IN MSP, THE LEFT OUTBOARD WING SKIN TO NACELLE ATTACH ANGLE WAS FOUND TO BE CRACKED AT THE ELEVENTH RIVET. REPAIRS WERE COMPLETED BY INSTALLING A REPAIR ANGLE IAW ARP 54-20-9101, REVISION B. (M)
DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE LEFT INBOARD WING SKIN TO NACELLE ATTACH ANGLE, 5TH RIVET FROM THE FORWARD END, IS CRACKED. REPAIRS WERE COMPLETED BY INSTALLING A REPAIR ANGLE IAW ARP 54-20-9101B. (M)
DURING A SCHEDULED INSPECTION IN MSP, THE LEFT LOWER BELT FRAME AT FS 159 WAS FOUND TO BE CRACKED. REPAIRS WERE COMPLETED BY FABRICATING AND INSTALLING A REPAIR DOUBLER IAW FAC LAR 95-MALA-237 AND SRM 51-00-00. (M)
DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL FOUND THE RT FLAP WALKING BEAM ROLLER DOUBLER WORN NEAR LIMITS. THEY REPLACED THE DOUBLER IAW FAIRCHILD ARP 57-20-9424. (M)
DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL FOUND THE RT OUTBOARD UPPER FORWARD WING SKIN TO NACELLE ATTACH ANGLE CRACKED. THEY STOP DRILLED THE CRACK AND FABRICATED AND INSTALLED A REPAIR DOUBLER IAW FAIRCHILD ARP 54-20-9101. (M)
DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED THE LEFT FLAP WALKING BEAM ROLLER DOUBLER TO BE WORN NEAR LIMITS. THEY REPLACED THE DOUBLER IAW FAIRCHILD ARP 57-20-9424. (M)
DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL FOUND THE RT OUTBOARD LOWER FORWARD WING SKIN-TO-NACELLE ATTACH ANGLE CRACKED. THEY STOP DRILLED THE CRACK AND FABRICATED AND INSTALLED A REPAIR DOUBLER IAW FAIRCHILD ARP 54-20-9101. (M)
MSP - FLT 3272 - UPON CLIMBOUT, THE LT ENGINE RPM DROPPED TO 45 PERCENT, THE ENGINE STARTED TO NTS AND THE OIL PRESSURE DROPPED TO ZERO. THE ENGINE WAS SHUTDOWN THROUGH STOP AND FEATHER. THE AC RETURNED TO MSP AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE OIL PUMP. ENGINE OPERATED SATISFACTORILY. (W)
MSP - FLT 3327- IN CRUISE FLIGHT, THE ENGINE RPM DID NOT RESPOND TO POWER LEVER MOVEMENT. THE AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE CLEANED THE PROP GOVERNOR LINKAGE. THE PROBLEM COULD NOT BE DUPLICATED DURING GROUND RUNS. SYSTEM OPERATED SATISFACTORILY DURING A TEST FLIGHT. (X)
FLT NR 3316 - WHILE TAXIING THE AIRCRAFT INTO THE GATE IN CWA, SMOKE BECAME EVIDENT IN THE COCKPIT AND CABIN. MAINTENANCE REPLACED THE COOLING TURBINE. SYSTEM OPERATED SATISFACTORILY. (W)
DTW - FLT 3149 - ON APPROACH, NOSE GEAR WOULD NOT EXTEND. THE CREW PERFORMED AN EMERGENCY GEAR EXTENSION. THE AIRCRAFT LANDED WITHOUT INCIDENT IN DTW. MAINTENANCE REPLACED THE UPLOCK ROLLER, PN 5453032-1, UPLOCK ROLLER SHAFT, PN 543033-1, AND THE NOSE LANDING GEAR DOOR PICK-UP ROLLER, PN 27-52000-087, THAT WERE FOUND BINDING. SYSTEM OPERATED SATISFACTORILY. (REFERENCE CONTROL NR 95ZZZX702, AND CONTROL NR 95ZZZX703. (X)
DTW - FLT 3149 - ON APPROACH, NOSE GEAR WOULD NOT EXTEND. THE CREW PERFORMED AN EMERGENCY GEAR EXTENSION. THE AIRCRAFT LANDED WITHOUT INCIDENT IN DTW. MAINTENANCE REPLACED THE UPLOCK ROLLER, PN 5453032-1, UPLOCK ROLLER SHAFT, PN 543033-1, AND THE NOSE LANDING GEAR DOOR PICK-UP ROLLER, PN 27-52000-087, THAT WERE FOUND BINDING. SYSTEM OPERATED SATISFACTORILY. (REFERENCE CONTROL NR MALA954247, AND CONTROL NR 95ZZZX703. (X)
DTW - FLT 3149 - ON APPROACH, NOSE GEAR WOULD NOT EXTEND. THE CREW PERFORMED AN EMERGENCY GEAR EXTENSION. THE AIRCRAFT LANDED WITHOUT INCIDENT IN DTW. MAINTENANCE REPLACED THE UPLOCK ROLLER, PN 5453032-1, UPLOCK ROLLER SHAFT, PN 543033-1, AND THE NOSE LANDING GEAR DOOR PICK-UP ROLLER, PN 27-52000-087, THAT WERE FOUND BINDING. SYSTEM OPERATED SATISFACTORILY. (REFERENCE CONTROL NR MALA954247, AND CONTROL NR 95ZZZX702. (X)
FLT 3447 - ON APPROACH TO MSP, THE NOSE GEAR HAD TO BE CYCLED FOUR TIMES BEFORE A DOWN AND LOCKED INDICATION WAS RECEIVED. MAINTENANCE REPLACED THE NOSE GEAR DOWN LIMIT SWITCHES. SYSTEM OPERATED SATISFACTORILY DURING A TEST FLIGHT. (W)