Chrysler Aviation Inc
Also recorded as: CHRYSLER AVIATION INC, CHRYSLER AVIATION, INC., Chrysler Aviation 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
Sanction: $9,000 · case closed 2014-02-07
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 1995–2018. Most-reported systems: Flight controls (27) — 1; Navigation (34) — 1; Nacelles / pylons (54) — 1; Engine (72) — 1. Most-common natures of condition, as filed: OTHER — 2; NO WARNING INDICATION — 1; WARNING INDICATION — 1.
4 reports on file.
Part: DISPLAY — POWER LOSS (COCKPIT) · airframe 8,319 hrs · 5,674 cycles
PILOTS SIDE EFIS INTERMITTENTLY LOST POWER.
Part: PEDAL — BROKEN (CAPT RT RUDDER)
DURING TAXI IN FROM FLT NR 4453 - THE CAPTAINS RIGHT RUDDER PEDDLE ARM BROKE OFF. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT, AND FOUND ARM HAD FAILED AT PEDAL PIVOT POINT. THE ARM WAS REPLACED AND THE AIRCRAFT WAS RELEASED TO SERVICE. (M)
Part: KEEL WEB — CRACKED (LT NACELLE)
DURING INSPECTION THE LEFT ENGINE NACELLE OUTBOARD UPPER KEEL WEB (P/N 114-980022-1) WAS FOUND TO HAVE TWO CRACKS ON THE FORWARD FLANGE. BOTH CRACKS RAN VERTICALLY ON THE FLANGE. ONE CRACK WAS BETWEEN THE TWO CENTER ATTACH RIVETS APPROXIMATELY 1 INCH IN LENGTH. THE 2ND CRACK WAS LOCATED NEXT TO THE THREE LOWER HI-LOCK ATTACH FASTENERS APPROXIMATELY 3 INCHES IN LENGTH. THE KEEL WAS REPAIRED IAW AERODESIGN ENGINEERING REPORT NR 1507, DATED 6/2/95 AND FAA FORM 8110-3. THE KEEL WEB IS TO BE REPLACED NO LATER THAN 1/4/96 WITH REINSPECTIONS EVERY 45 DAYS UNTIL REPLACEMENT. (M)
Part: SUNGEAR — SHEARED (LT ENGINE)
PVD - ON TAKEOFF ROLL, THE LT ENGINE EXPERIENCED A LOSS OF POWER AND OIL PRESSURE. THE TAKEOFF WAS ABORTED, ENGINE WAS SHUTDOWN AND ACFT RETURNED TO GATE. INITIAL ON SITE INVESTIGATION REVEALED LOSS OF POWER TURBINE BLADES, PUNCTURED EXHAUST DUCTS AND DEBRIS IN EXHAUST AREA. INSPECTION OF MAIN ENGINE OIL FILTER REVEALED HEAVY METAL PARTICLE CONTAMINATION. COMPLETE ENGINE CHANGE OUT WAS ACCOMPLISHED ON SITE, WITH FAILED ENGINE AND PROPELLER RETURNED TO PSM. ENGINE TO BE DIRECTED TO O/H FACILITY FOR FURTHER INVESTIGATION. S/D - THE POWERPLANT REFERENCE ABOVE EXPERIENCED A POWER SECTION FAILURE OF THE SUNGEAR. (Z)
Linked aircraft
| N-number | Make / model | Year | Status | Link basis |
|---|---|---|---|---|
| N14TX | CESSNA 150C | 1963 | Valid Registration | Operator named in NTSB report |
| N404HG | ZIPLINE INTERNATIONAL INC P2 ZIP | — | Valid Registration | Matched by certificate designator |
| N54DD | CESSNA 560 | 1990 | Valid Registration | Matched by certificate designator |
| N560PA | CESSNA 560 | 1991 | Valid Registration | Matched by certificate designator |
| N561SR | CESSNA 560 | 1991 | Valid Registration | Matched by certificate designator |
| N810BE | CESSNA 560 | 1990 | Valid Registration | Matched by certificate designator |
| N904LR | CESSNA 560 | 1992 | Valid Registration | Matched by certificate designator |
| N968SR | CESSNA 560 | — | 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.
- N14TX (CESSNA 150C) — records 1996 · registered to MCBRIDE ROBERT W JR (owner ≠ operator)