Capital City Jet Center, Inc.
Also recorded as: CAPITAL CITY JET CENTER INC, CAPITAL CITY JET CENTER, INC., Capital City Jet Center, Inc.
Accident & enforcement record
Events that happened, regardless of the operator's own reporting. Each links to its public source.
NTSB accidents & incidents
Operated by CAPITAL CITY JET CENTER INC (per NTSB report)
The flight crew’s decision to attempt an engine start in conditions that exceeded the engine's maximum allowable ground start crosswind component limitation.
FAA enforcement actions
Sanction: $8,000 · case closed 2016-03-14
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 2015–2026. Most-reported systems: Fire protection (26) — 4; Landing gear (32) — 2; Engine (72) — 2. Most-common natures of condition, as filed: FALSE WARNING — 3; OTHER — 3; F.O.D. — 1; SMOKE/FUMES/ODORS/SPARKS; FALSE WARNING — 1.
8 reports on file.
Part: COMPRESSOR — DAMAGED (ENGINE) · airframe 9,106 hrs · 6,600 cycles
WILLIAMS INTERNATIONAL ENGINE MODEL FJ44-3A, SERIAL NUMBER 141186, FROM AIRCRAFT 525B-0088 (N525MP) WAS RETURNED TO OUR REPAIR STATION FOR UNSCHEDULED REPAIR. N525MP IS OPERATED UNDER FAR PART-135. ACCORDING TO THE WILLIAMS INTERNATIONAL OEM PRODUCT SUPPORT TEAM, ONE OF THEIR AUTHORIZED SERVICE CENTERS WAS PERFORMING REPLACEMENT OF THE NO. 1 CARBON SEAL TO RESOLVE AN OIL LEAK SQUAWK ON SUBJECT ENGINE, AND DURING THAT PROCESS, DISCOVERED A LIBERATED BLADE ON THE INTERMEDIATE PRESSURE (I.P.) COMPRESSOR ROTOR. DUE TO THIS FINDING, W.I. OEM PRODUCT SUPPORT DIRECTED THE PART-145 SERVICE CENTER TO REASSEMBLE THE ENGINE (TO FACILITATE SHIPMENT), REMOVE IT FROM THE AIRFRAME, AND RETURN IT TO OUR REPAIR STATION FOR REPAIR. AFTER INDUCTION INTO OUR REPAIR STATION, WE DISASSEMBLED THE ENGINE AND CONFIRMED ONE LIBERATED 3RD-STAGE I.P. COMPRESSOR ROTOR BLADE. NOTE: THE I.P. COMPRESSOR ROTOR IS A THREE-STAGE AXIAL COMPRESSOR. FURTHER INSPECTIONS REVEALED A CRACK IN THE INTERSTAGE HOUSINGâS BEARING CAVITY, WHICH IS DEEMED TO BE ROOT-CAUSE OF THE OIL LEAK ORIGINALLY SQUAWKED BY THE AIRCRAFT OPERATOR.
Part: SMOKE DETECTOR — FALSE ACTIVATION (ZONE 100) · airframe 8,712 hrs · 6,323 cycles
BAGGAGE SMOKE DETECTOR WARNING CAME ON DURING DESCENT INTO KAPA.
Part: TIRE — FAILED (ZONE 700) · airframe 8,273 hrs · 6,014 cycles
AIRCRAFT HIT POTHOLE ON TAKE OFF TIRE BLEW.
Part: TIRE — FAILED (ZONE 700) · airframe 10,799 hrs · 7,985 cycles
UPON LANDING THEY RAN OFER SOMETHING ON RUNWAY THAT PUNCTURED THE TIRE.
Part: SMOKE DETECTOR — WARNING MESSAGE (CARGO) · airframe 8,067 hrs · 5,882 cycles
DURING TAKEOFF ROLL ON GROUND BAGGAGE SMOKE DETECTOR WARNING LIGHT CAME ON PILOT ABORTED TAKE OFF AND DECLARED AN EMERGENCY AND TAXIED BACK TO RAMP. FIRE DEPARTMENT LOOKED IN BOTH BAGGAGE AREAS AND FOUND NO EVIDENCE OF FIRE OR SMOKE. HAD A MECHANIC INSPECT BOTH BAGGAGE AREAS AND FOUND NO EVIDENCE OF FIRE OR SMOKE, I HAD THEM VACUUM AROUND DETECTORS TO REMOVE ANY DUST PARTICLES THAT MIGHT HAVE SET OFF THE DETECTORS. THE AIRCRAFT WAS RETURNED TO SERVICE. IT WAS A PART 91 FLIGHT.
Part: SMOKE DETECTOR — FALSE ACTIVATION (CARGO BAY) · airframe 4,352 hrs · 3,375 cycles
BAGGAGE SMOKE ANNUNCIATOR IN DESCENT TO HOU. DECLARED EMERGENCY FOR EXPEDITED LANDING AT HOU. NO SMOKE NOTICED BY TOWER SO TURNED OFF THE RUNWAY FOR FIRE RESCUE TO DO A QUICK WALK AROUND. NO INDICATIONS OF FIRE OR SMOKE SO AIRCRAFT CONTINUED TO RAMP FOR NORMAL DEPLANING. MAINTENANCE INSPECTED FORWARD AND AFT BAGGAGE AREAS WITH NO ISSUES AND RETURNED TO SERVICE. ANNUNCIATOR DOES NOT DIFFERENTIATE BETWEEN FWD OR AFT. THIS SEEMS TO HAPPEN TO OUR FLEET A FEW TIMES PER YEAR.
Part: SENSOR — DIRTY (SMOKE DETECTOR) · airframe 1,234 hrs · 1,015 cycles
PILOT DECLARED AN EMERGENCY AND LANDED, DUE TO A FORWARD BAGGAGE COMPARTMENT SMOKE DETECTOR LIGHT AND AUREL WARNING. AFTER LANDING AND EVACUATING AIRPLANE THE FORWARD BAGGAGE AREA WAS OPENED UP AND INSPECTED FOR SMOKE OR THE ODOR OF SMOKE, NONE WAS FOUND. HAD A LOCAL A&P ALSO CHECK IT OUT, IT WAS CLEANED AROUND THE SENSOR WITH A VACUUM CLEANER AND THE FAULT COULD NOT BE DUPLICATED. THE A&P SIGNED IT OFF AS COULD NOT DUPLICATE AND THE FLIGHT CONTINUED AS PLANNED. THERE WERE NO MORE INCIDENTS OF THIS NATURE ON THE REMAINING FLIGHT.
Part: BLADE — MISSING (ENGINE)
DURING OPERATION A "HOOTING" SOUND WAS PRESENT FROM IDLE THOUGH MCT POWER SETTING. A FIELD BORESCOPE INSPECTION REVEALED 1 OF THE IP COMPRESSOR BLADES HAD LIBERATED. THE REPAIR STATION INVESTIGATION HAS CONFIRMED THE FIELD FINDINGS. THERE WAS NO EVIDENCE OF UPSTREAM FOREIGN OBJECT DAMAGE (FOD).
Linked aircraft
| N-number | Make / model | Year | Status | Link basis |
|---|---|---|---|---|
| N39DJ | CESSNA 525B | 2006 | Valid Registration | Matched by certificate designator |
| N525MP | CESSNA 525B | 2006 | Valid Registration | Matched by certificate designator |
| N53NW | CESSNA 525B | 2005 | Valid Registration | Matched by certificate designator |
| N718MV | — | — | Operator named in NTSB report |
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.
- N718MV — records 2014–2016 · no longer on the FAA registry