N835MA
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
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
7 reports on file, 1997-02-20 – 2026-08-15.
Part: WING — DAMAGED (ZONE 500)
LEFT WING SUFFERED MAJOR DAMAGE FROM WINDS. WILL REMOVE AND REPLACE WING
Part: UNKNOWN — MALFUNCTIONED · airframe 3,404 hrs · 6,399 cycles
AIRCRAFT WAS BEING FLOWN BY PIC & SIC AT APPROX 400 FT, PILOT FELT A JOLT & OBSERVED ITT AT 720 THEN JUMPED TO 805. THE PILOT REPORTED THE POWER LEVER & EMER POWER LEVER WAS UNRESPONSIVE & UNABLE TO REGULATE FUEL FLOW TO ENG.
Part: FUEL CONTROL — FAULTY (ENGINE) · airframe 1,100 hrs · 1,954 cycles
WHILE FLYING, POWER LEVER WAS MOVED TO IDLE POSITION BUT THERE WAS NO CHANGE IN ENG POWER. TORQUE STAYED BETWEEN 1250 & 1400 FLB.
Part: SCAVENGE PUMP — FLUCTUATES (LT ENGINE)
COMMANDED IN-FLIGHT SHUTDOWN OF LT ENGINE DUE TO FLUCTUATING OIL PRESSURE. UNEVENTFUL SINGLE ENGINE LANDING. ENGINE LOST OIL. OIL EXITED ENGINE FROM TURBINE AIR/OIL SEAL AS A RESULT OF TURBINE SCAVENGE PUMP FAILURE. RECOMMEND COMPLIANCE WITH SB 72-2074R1. (K)
Part: SKIN — CORRODED (RT WING) · airframe 3,320 hrs
FOUND FUEL LEAK COMING FROM BEHIND THE RT WING DE-ICE BOOT. AFTER PEELING BACK BOOT TO LOCATE LEAK, NOTED SEVERAL AREAS OF HEAVY CORROSION ON LEADING EDGE. FERRIED AIRCRAFT TO FACILITY FOR LEADING EDGE REPLACEMENT. SUSPECT DE-ICE BOOT WAS INSTALLED USING IMPROPER PRACTICES ALLOWING MOISTURE TO GET IN BEHIND BOOT AND BECOME TRAPPED.
Part: BOOT — LEAKING (RT WING) · airframe 3,320 hrs · 2,908 cycles
NOTED FUEL LEAK FROM BEHIND RT WING DE-ICE BOOT. AFTER PEELING BOOT BACK TO RESEARCH LEAK, NOTED NUMEROUS AREAS OF HEAVY CORROSION. AIRCRAFT WAS FERRIED TO FACILITY FOR REPLACEMENT OF LEADING EDGE ASSEMBLY.
Part: RIB — CRACKED (RT WING)
DURING A PHASE INSPECTION, FOUND A CRACK IN THE RT WING CANTED RIB TOP CAP. CRACK STARTS AT AFT SIDE OF FORWARD WING SPAR AND RUNS AFT PARALLEL TO THE BEND RADIUS, APPROXIMATELY 1 INCH IN LENGTH. STOP-DRILLED ENDS OF CRACK PER CESSNA INSTRUCTIONS.