Holman Leasing Systems, Inc.
Also recorded as: HOLMAN LEASING SYSTEMS, INC., Holman Leasing Systems, Inc., PRIVATE JET CENTER
Accident & enforcement record
Events that happened, regardless of the operator's own reporting. Each links to its public source.
NTSB accidents & incidents
No NTSB accidents or incidents linked to this operator.
FAA enforcement actions
No FAA enforcement actions linked to this operator.
Maintenance disclosure history
Service Difficulty Reports are self-reported maintenance findings. The NUMBER of reports is not a measure of reliability — diligent operators file more, not fewer. These are shown for transparency, not as a negative signal. To verify a report, search its control number at the FAA SDRS site.
Reports span 2006–2024. Most-reported systems: Landing gear (32) — 1; Lights (33) — 1; Navigation (34) — 1; Stabilizers (55) — 1; Engine (72) — 1. Most-common natures of condition, as filed: OTHER — 3; MULTIPLE FAILURE — 1; NO TEST — 1.
5 reports on file.
Part: COMPRESSOR — DAMAGED (ENGINE) · airframe 7,574 hrs · 5,586 cycles
ENGINE EXHIBITED AN OIL LEAK WHICH WAS SUBSEQUENTLY TRACED TO A CRACK IN ENGINE GEARBOX HOUSING. ENG OEM DIRECTED TROUBLESHOOTING INCLUDING A VIBRATION SURVEY GROUND-RUN, REVEALED ENG VIBRATION LEVELS BEYOND LIMITS IAW ICA. ENGINE OEM. BORESCOPE INSPECTION OF ENG COMPRESSOR SECTION, REVEALED DAMAGE TO THE HPC BLADES & 1 LIBERATED 3RD-STAGE INTERMEDIATE IPC ROTOR BLADE. DISASSEMBLY OF ENGINEâS COMPRESSOR SECTION CONFIRMED 1 LIBERATED 3RD-STAGE IPC BLADE. IPC ROTOR IS A THREE-STAGE AXIAL COMPRESSOR. FURTHER DISASSEMBLY OF THE ENGINE REVEALED DOWNSTREAM SECONDARY DAMAGE TO HPC BLADES & OTHER ENG COMPONENTS.
Part: PROCESSOR — MALFUNCTIONED (TCAS)
HAD 3 TCAS PROCESSORS FAIL WITHIN A YEAR AND 4 MONTHS. THEY KEEP SHOWING TCAS FAIL ON THE PILOTS PFD. MANUFACTURER COULD NOT GET THE UNIT TO FAIL.
Part: SCREW — DAMAGED (ZONE 300) · airframe 4,031 hrs · 3,166 cycles
DUAL AHRS FAILURE DURING CRUISE. MADE AN EMERGENCY DESCENT. AFTER TESTING, FOUND NO PROBLEM WITH AHRS BOXES. ON FURTHER INVESTIGATION, ORIGINAL SCREWS THAT HOLD THE INSPECTION PANEL TO THE FLUX VALVES BECAME MAGNETIZED. MFG RECOMMENDED INSTALLING NEW SCREWS. PERFORMED LEAKS TESTS ON THE AIR DATA SYSTEM. NO DEFECTS WERE FOUND AFTER THE TEST FLIGHT.
Part: LAMP — BURNED OUT (TAIL)
THE MALFUNCTION OF THE BEACON ASSY IS THAT IT KEEPS BURNING OUT THE LAMPS, SOMETIMES 2 TO 3 TIMES A MONTH. PROBABLE IS VIBRATION INTHE TAIL CAUSING ELEMENT TO BURN OUT. RECOMMENDATION TO INSTALL LED LIGHTING FOR TAIL BEACON ASSY
Part: PIN — FAILED (NLG TORQUE LINKS)
NOSE LANDING GEAR TORQUE LINKS CONNECTED BY QUICK RELEASE PIN. QUICK RELEASE PIN FELL APART WHILE TAXIING ON ACTIVE TAXI WAY DISCONNECTING NOSE WHEEL STEARING. AIRCRAFT TOWED FROM TAXI WAY. NO DAMAGE NOTED. (K)
Linked aircraft
| N-number | Make / model | Year | Status | Link basis |
|---|---|---|---|---|
| N179ER | CESSNA 525B | 2009 | Valid Registration | Matched by certificate designator |
| N379DB | — | — | Matched by certificate designator | |
| N632XL | CESSNA 560XL | 2006 | Valid Registration | Matched by certificate designator |
| N803SD | CESSNA 525B | 2010 | Valid Registration | Matched by certificate designator |
| N808SD | TEXTRON AVIATION INC 560XL | 2017 | Valid Registration | Matched by certificate designator |
| N811CE | CESSNA 560XL | 2007 | Valid Registration | Matched by certificate designator |
| N924TG | BOMBARDIER INC BD-100-1A10 | 2006 | Valid Registration | Matched by certificate designator |
Aircraft with earlier records under this certificate
Maintenance and accident records on this page also cover aircraft that are not in this operator's current FAA fleet list. Charter and management fleets change — owners switch management companies, sell, or export aircraft. Where the registry shows what became of a tail, it is noted below.
- N424HH — records 2006 · no longer on the FAA registry