N808MA
Registered owner: BANK OF UTAH TRUSTEE, UT (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| SOUTHERN AIRWAYS EXPRESS, LLC (141A) | Certificate holder | — | Matched by certificate designator |
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
PIC CONTACTED ACP SABRINI FOR BRIEFING & CLARIFICATION ABOUT PROCEDURE BEFORE BEGINNING. WHILE ON THE RAMP, PIC PERFORMED LOW-SPEED BRAKE TESTS AT 5â10 KNOTS GS TO VERIFY FUNCTIONALITY. BRAKES WERE ONLY SLOWING DOWN THE ACFT, BUT IT WASNâT FIRM BRAKING AS THEY ARE STILL NEW BRAKE PADS. ATC INSTRUCTED CREW TO CONDUCT THE PROCEDURE ON RUNWAY 27 AT MEM. PIC WAS TAXING & WHILE TAXING TO RWY27 , LIGHTLY RIDING BRAKES AS PART OF BURN-IN PROCEDURE . WHILE TAXING ON RWY27 AT 30 KNOTS GS APPLYING BRAKES EVENLY, BRAKING ACTION RESULTED IN THE ACFT PULLING RIGHT WITH NO STRONG/FIRM STOPPING ACTION . MULTIPLE ATTEMPTS MADE TO COMPLETE PROCEDURE, INCLUDING USE OF BETA MODE TO ASSIST IN STOPPING. AFTER REPEATED PULLING RIGHT & LACK OF POSITIVE BRAKING, CREW ELECTED TO ABORT PROCEDURE & RETURN BACK TO RAMP. WHILE TAXIING BACK VIA TAXIWAY C, PIC EXPERIENCED COMPLETE BRAKE LOSS. ACFT MANEUVERED INTO RAMP USING BETA THRUST ONLY. UPON ENTERING THE RAMP, CREW OBSERVED SMOKE FROM LT MLG (BRAKE PADS). FO ALSO OBSERVED SMOKE FROM RT BRAKES. ACFT BROUGHT TO COMPLETE STOP USING BETA THRUST. ENGINE SHUTDOWN, SIC NOTIFIED ATC OF A BRAKE SMOKE / FIRE.
GENERATOR OFF "CASS" MESSAGE IN FLIGHT, CREW RETURNED TO FIELD
UPON LANDING IN LAF RIGHT MAIN LANDING GEAR TIRE BLEW ON THE RUNWAY. TIRE WAS FULLY DEFLATED AND WAS PARTIALLY OFF THE RIM. THE PILOT CAME TO A HALT AND AVOIDED ANY FURTHER DAMAGE TO THE WHEEL ASSEMBLY. NO INJURIES WERE REPORTED AT THE TIME.
ON CLIMB OUT, THE AIR CONDITIONER COMPRESSOR FAILED CAUSING THE DRIVE BELT TO BREAK. CREW NOTICED A BURNING ODOR AND TURNED OFF AIR CONDITIONING SYSTEM AND DID AN AIR RETURN. THE SMELL DISSIPATED UPON TURN OFF AIR CONDITIONING SYSTEM
ON TAKEOFF ROLL, FORWARD ENTRY L1 DOOR LIGHT CAME ON, HANDLE UNSEATED. ADJUSTED/TEST DOOR IAW MM 52-11-01. PRESSURIZED AIRCRAFT TO 1 PSI IAW MM 21-31-00. NO DOOR LIGHT, OPS CHECK SATISFACTORY. PERFORMED SPECIAL INSPECTION DUE HIGH SPEED ABORT 110 KNOTS, 150 LBS IAW MM 5-51-121, NO DISCREPANCIES NOTED. RETURNED AIRCRAFT TO SERVICE. (M)
DURING CRUISE FLIGHT, LOST ALL 'A' HYDRAULIC SYSTEM FLUID. ACCOMPLISHED ABNORMAL CHECKLIST. DIVERTED TO INDIANAPOLIS. FOUND NR 2 ENGINE HYDRAULIC PUMP PRESSURE HOSE CHAFED AGAINST THE 13TH STAGE CSD EJECTOR DUCT. REPLACED DAMAGED HOSE PER MM 29-10-5. SERVICED PER MM 12-4-23. LEAK CHECK ON RUNUP OK. (M)
DURING C-CHECK, FOUND AFT CARGO COMPARTMENT BS 950E AT STRINGER 29R HAS CORROSION. REMOVED CORROSION FROM STRINGER AND FOUND CRACK IN STRINGER AT STATION 950E. REMOVED AND REPLACED STRINGER FROM STATION 950 TO 1110. INSTALLED DOUBLER TRIPLER AND QUADRUPLER WITH SPLICE FROM STATION 950 TO 1110 IAW EO L-18-R01. (M)
DURING C-CHECK, FOUND SEAT TRACK LEFT, OUTBOARD OF CENTER, TRACK CORRODED AT OUTER EDGES BETWEEN BS 1030 AND 1070. REMOVED CORROSION FROM TRACK, FOUND TRACK CRACKED. REPLACED SEAT TRACK IAW SRM 51-10-2, 51-30-2 AND 53-10-5. (M)
DURING C-CHECK, FOUND SEAT TRACK LEFT OUTBOARD BETWEEN BS 1110-1130 CORRODED ON UPPER FACE. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-10-2, 51-30-2 AND 53-10-5. (M)
DURING C-CHECK, FOUND 1 INCH DAMAGE TO LEFT HORIZONTAL STAB LOWER FORWARD CHORD OF FORWARD SPAR STATION 101. CUT OUT DAMAGED SECTION OF CHORD. FABRICATED AND INSTALLED ANGLE AND FILLER IAW SRM 51-10-3, 51-10-2 AND 55-10-5 FIG 1. (M)
DURING C-CHECK, FOUND LEFT FUSELAGE STATION 1160 TO 1183 STRINGER 22L HAS SURFACE CORROSION. REMOVED AND REPLACED DAMAGED STRINGER 24.5 INCHES AT LT FS 1160-1183 IAW SRM 53-10-3 PAGE 4B AND 4A. (M)
DURING C-CHECK, FOUND FUSELAGE UPPER LOBE INTERIOR AFT LEFT FLOOR PLATE BETWEEN STATION BS 1050 AND BS 1183 AND BETWEEN LEFT OUTBOARD OF CENTER TRACK TO THE WALL, HAS CORROSION ON SEVERAL PLACES AND IS CRACKED FORWARD OF BS 1183. REMOVED CORROSION FROM FUSELAGE UPPER LOBE INTERIOR STATION 1050 TO 1183 AND FROM LEFT OUTBOARD TRACK TO WALL. FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM 51-10-6, 51-10-2, 51-40-3 AND 51-30-2. (M)
UPON REACHING CRUISE ALT FL310, AIRCRAFT EXPERIENCED TOTAL SYSTEM A HYD FAILURE. ACCOMPLISHED ''A'' SYSTEM HYDRAULIC FAILURE CHECKLIST, IAW AOM VOL 1 EMERGENCY PROCEDURES. DECLARED AN EMERGENCY AND RETURNED TO MIAMI, DID NOT DUMP FUEL. FOUND 3 WAY VALVE IN LEFT WHEEL WELL WITH ACTUATOR AND BODY SEPARATED AND THE FOUR ATTACHING SCREWS CRACKED. REPLACED 3 WAY VALVE PER MM 29-11-62. SERVICED HYDRAULIC SYSTEM PER MM 12-12-00. OPS CHECK OK. (M)
FLAPS WILL NOT RETRACT FULLY DUE TO RT. MID FLAP FAIRING BEARING WORN(I/B).
MIA - ON CLIMB-OUT, WITH AUTO PILOT ENGAGED AT 10000 PLUS 250-260 KTS RUDDER SPLIT AND AUTO PILOT COULD NOT CONTROL AIRCRAFT. DISCONNECTED AUTO PILOT AND FOUND IT TOOK 4 DEGREES RIGHT TRIM TO KEEP AIRCRAFT FROM YAWING. RETURNED TO MIA. TROUBLE SHOT SYSTEM, FOUND UPPER YAW DAMPER COUPLER AT FAULT. REMOVED AND REPLACED UPPER YAW DAMPER COUPLER. OPS CHECKED OK IAW 22-11-131. ADJUSTED LOWER RUDDER POSITION SENSOR. OPS CHECKED OK IAW 22-11-51. (M)
ON TAKEOFF FROM ACA WHILE CLIMBING THROUGH 18,000 FEET, FELT AIRCRAFT JOLT. RETURNED TO ACA FOR GROUND INSPECTION. RETURNED TO ACA AFTER DUMPING FUEL TO OBTAIN PROPER WEIGHT FOR LANDING. INSPECTED AIRCRAFT PER INSTRUCTIONS FROM MIAMI AIR MAINTENANCE CONTROL, FOUND NO DEFECTS OR MALFUNCTIONING SYSTEMS. PERFORMED LOCAL FLIGHT OF AIRCRAFT, NO ABNORMAL FLIGHT PROFILES, NO ABNORMALTIES EXPERIENCED. RETURNED AIRCRAFT TO SERVICE.
DURING P/T WALK AROUND, FOUND LEFT WING INBOARD T/E MID FLAP CARRIAGE MISSING UPPER INBOARD ECCENTRIC, LOCKING TAB WASHER AND NUT ON OUTBOARD CARRIAGE. REPLACED CARRIAGE UPPER ECCENTRIC, LOCK TAB WASHER AND NUT ON LEFT WING INBOARD TRAILING EDGE FLAP IAW 27-51-2. OPS CHECK OK. (M)
ON PREFLIGHT, TRANSIT FOUND RIGHT FORWARD OVERWING EMERGENCY LIGHT WILL NOT TURN OFF. REPLACED BATTERY PACK, OPS CHECK NORMAL IAW 33-50-00. (M)
ON 'A' SERVICE, FOUND RIGHT OVEWING EMERENCY LIGHT INOPERATIVE. TROUBLESHOT SYTEM. FOUND RIGHT OVERWING BATTERY PACK LOW CHARGE. REPLACED BATTERY PACK. OPERATIONAL CHECK GOOD IAW MM 33-50-1. (M)
PASSING THROUGH FL190 ON TAKEOFF WHEEL WELL FIRE WARNING LIGHT ILLUMINATED. FOLLOWED COMPANY EMERGENCY CHECKLIST PROCEDURES. FIRE WARNING LIGHT EXTINGUISHED WITH GEAR EXTENSION. IN MIA REMOVED AND REPLACED LEFT AND RIGHT WHEEL WELL FIRE WARNING SENSOR LOOPS IAW 26-12-1. OPS CHECK OK. CLEANED AND RESEATED NOSE WHEEL WELL SENSOR LOOP. OPS CHECK OK IAW 26-11. (M)
PASSING THROUGH FL190 WHEEL WELL FIRE WARNING LIGHT ILLUMINATED. FOLLOWED COMPANY EMERGENCY CHECKLIST PROCEDURES. FIRE WARNING LIGHT EXTINGUISHED WITH GEAR EXTENSION. ON ARRIVAL PERFORMED VISUAL INSPECTION OF DETECTOR LOOPS, SENSORS, WHEEL WELL AND LANDING GEAR AREA. NO DAMAGE OR FAULT FOUND. PERFORMED WHEEL WELL FIRE DETECTION ADJUSTMENT TEST IAW MM 26-12-00. (M)
LOG PAGE: 24839: ON PRE-FLIGHT TRANSIT, FOUND ESCAPE PATH LIGHTING R2 DOOR NOT LIGHTING. TROUBLESHOT SYSTEM. REPAIRED WIRING. OPS CHECKED OK IAW 33-50-01. (X)
LOG PAGE: 24836 - DURING CRUISE, WHEEL WELL FIRE WARNING LIGHT AND BELL CAME ON. COMPLETED AOM PROCEDURES AND INDICATION DID NOT RETURN. THE NGU TROUBLESHOT SYSTEM, INSPECTED LOOPS, WIRING, GROMMETS, AND FASTENERS IN L/R WHEELS. NO DEFECTS NOTED. REMOVED WATER CONTAMINATION FROM L/R WHEEL WELL DISCONNECT C/P. SYSTEM CHECK OK IAW MM 2612-1. LOG PAGE 24840 IN ERW R/R FIRE DETECTOR CONTROL UNIT FOR COMPANY CONVENIENCE. OPS CHECK OK IAW 26/14/11. (X)
DURING PREFLIGHT TRANSIT CHECK, FOUND EMERGENCY EXIT LIGHT LOCATED IN THE MAIN CABIN CEILING ABOVE SEAT ROW NR 4 IS INOPERATIVE. INSTALLED BATTERY PACK. (M)
IAH - RETURN FROM FLIGHT - UPON CLIMB-OUT, FOUND CABIN PRESSURIZATION UNCONTROLLABLE IN AUTO AND STANDBY. SWITCHED MANUAL DC. CABIN RATE NOT CONTROLLABLE. SHUT OFF ONE PACK. CABIN STARTED TO RISE UNCONTROLLABLE. CLOSED CARGO HEAT OUTFLOW VALVE. CABIN STARTED TO DESCEND ON DESCENT. ON POST-FLIGHT INSPECTION, FOUND STATIC FITTING ON CABIN PRESSURE CONTROLLER TO BE LOOSE. TIGHTENED. OPS CHECK IAW MM 21-30-00 NORMAL. (X)
IAH - RETURN FROM FLIGHT, UPON CLIMB-OUT, FOUND CABIN PRESSURIZATION UNCONTROLLABLE IN AUTO AND STANDBY. SWITCHED TO MANUAL DC. CABIN RATE NOT CONTROLLABLE. SHUT OFF ONE PACK. CABIN STARTED TO RISE UNCONTROLLABLE. CLOSED CARGO HEAT OUTFLOW VALVE. CABIN STARTED TO DESCEND ON DESCENT. ON POST FLT INSPECTION, FOUND FITTING ON CABIN PRESSURE CONTROLLER TO BE LOOSE, TIGHTENED. OPS CHECK IAW MM 21-30-00 NORMAL. (M)
RETURN FROM FLIGHT, AFTER TAKEOFF AT FLL, NR 1 LE SLAT WOULD NOT RETRACT. CYCLED FLAPS, NO HELP. RETURNED TO FLL. REPLACED THE NR 1 SLAT ACTUATOR IAW MM 27-81-32. OPERATIONAL CHECK GOOD.