JET AIR INC.
Also recorded as: JET AIR INC, JET AIR INC., Jet Air Inc.
Accident & enforcement record
Events that happened, regardless of the operator's own reporting. Each links to its public source.
NTSB accidents & incidents
FAA enforcement actions
FAA enforcement records haven't been loaded into GroundCheck yet, so none can be shown — a gap in our data, not evidence of a clean enforcement history.
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.
4 reports on file.
DURING A PRE-BUY INSPECTION OF THE LT AND RT ENGINES ON THIS AIRCRAFT, A BORESCOPED WAS PERFORMED. FOUND THAT THE SOME OF THE DIFFUSER ATTACHING HARDWARE INSIDE THE CASE LINER WERE LOOSE OR MISSING FROM THEIR RESPECTIVE HOLES AND LAYING IN THE BOTTOM OF THE ENGINE CASE LINER ON BOTH ENGINES. NO LOSS OF ENGINE PERFORMANCE OR INDICATION DURING PREVIOUS OPERATION WAS NOTED.
DURING A SCHEDULED PHASE 5 INSPECTION, FOUND FITTING CRACKED IN THE VERTICAL STAB. THE CRACK WAS FOUND USING EDDY CURRENT INSPECTION METHODS.
UPON REMOVING THE LT NACELLE FUEL TANK, WE NOTED A TOP WING SKIN CRACK ABOUT 3.5 INCHES LONG. FROM LOOKING UNDERNEATH IN THE GEAR WELL, JUST ABOVE THE MLG SIDE BRACE, YOU COULD SEE THE CRACK RUNNIING PARRALLEL WITH THE ANGLE STIFFENER. INSPECTED THE RIGHT GEAR FROM UNDERNEATH AND NOTED NOTHING. UPON REMOVAL OF THE RT NACELLE TANK WE FOUND THE SAME AREA CRACKED. THIS CRACK MUST BE JUST INWARD ENOUGH THAT FROM LOOKING UNDERNEATH THIS CRACK MUST BE JUST INWARD OF THE ANGLE STIFFENER BEING NOT VISIBLE. COULD BE THAT THE PN 502210021 ANGLE, FWD SIDE BRACE, AND PN 502210023 ANGLE, AFT SIDE BRACE WERE INSTALLED CORRECTLY IAW SK414-8E AND ME76-2 BUT BY THIS INSTALLATION THESE ANGLES ARE NOT CONNECTEDTO THE SIDE BRACE, BUT JUST ATTACH TO THE GEAR WELL TOP SKIN AND ARE PUTTING A LOAD ON THE SKIN. THESE ANGLES SHOULD ATTACH TO THE PARALLEL STIFFENER ANGLE/SIDE BRACE TO DISPENSE THE LOAD. THIS WAS COMPLIED WITH IAW BULLETIN. THE GAP BETWEEN THE FWD/AFT ANGLES AND THE ANGLE STIFFENER ARE CAUSING THE TOP GEAR WELL SKIN TO FLEX UP/DOWN. AFTER A PERIOD OF TIME THIS CAUSES THE SKIN TO CRACK PARALLEL ALONG THE STIFFENER ANGLE. (K)
LEFT ENGINE FIRE WARNING LIGHT FLICKERED ON INTERMITTENTLY. INSPECTION FOUND LOOP CHAFING AGINST OTHER WIRING AND TUBING ON THE ENGINE AND A MINOR LEAK IN A BLEED AIR LINE COUPLING.
Linked aircraft
| N-number | Make / model | Year | Status | Link basis |
|---|---|---|---|---|
| N101JL | CESSNA 550 | 2001 | Valid Registration | Matched by certificate designator |
| N328PF | — | — | Matched by certificate designator | |
| N333AE | BRENT E HOSKINS JUST ACFT HIGHLANDER | 2014 | Valid Registration | Operator named in NTSB report |
| N497MN | TEXTRON AVIATION INC 560XL | 2019 | Valid Registration | Matched by certificate designator |
| N533JR | — | — | Operator named in NTSB report | |
| N550TN | CESSNA 550 | 2001 | Valid Registration | Matched by certificate designator |
| N562VP | CESSNA 560XL | 2006 | Valid Registration | Matched by certificate designator |
| N579M | CESSNA 550 | 2006 | Valid Registration | Matched by certificate designator |
| N740SP | CESSNA 172S | 2000 | Valid Registration | Operator named in NTSB report |
| N800WT | CESSNA 550 | 1998 | Valid Registration | Matched by certificate designator |
| N824PM | CESSNA AIRCRAFT CO 560XLS | 2005 | Valid Registration | Matched by certificate designator |
| N97VS | CESSNA 560XL | 2001 | Valid Registration | Matched by certificate designator |