- Registered owner
- Finke Aviation LLC
- Location
- Charleston, MS
- Owner type
- LLC
- Serial number
- 802-0540
- Year built
- 2014
- Type
- Fixed wing single engine
- Engine
- Turbo-prop
- Airworthiness
- Restricted, agriculture and pest control, forest
- Airworthiness date
- January 7, 2014
- Certificate issued
- May 5, 2020
- Expires
- May 31, 2027
- Mode S code
- AAE957
Air Tractor AT-802TCDS A19SWAirframe · Air Tractor AT-802TCDS E26NEEngine · Pratt & Whitney Canada PT6A-67AG
From the FAA registry file of October 21, 2026.
On this page
Airworthiness directives that may apply · 15
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1996 | 1 |
|---|---|
| 1997 | 2 |
| 2001 | 2 |
| 2002 | 3 |
| 2004 | 1 |
| 2005 | 1 |
| 2006 | 4 |
| 2007 | 1 |
| 2008 | 1 |
| 2009 | 2 |
| 2010 | 2 |
| 2011 | 1 |
| 2014 | 1 |
| 2016 | 1 |
| 2021 | 1 |
| 2023 | 1 |
| 2024 | 2 |
| 2026 | 1 |
See all 28 ADs
Information bulletins that may apply · 12
Advisory, not mandatory.
Airframe · Air Tractor AT-802
SAIB 2024-03Rudder Control SystemSAIB CE-19-21Flap Motor Mounting StudsSAIB CE-18-06Flight Controls, Rudder Control SystemSAIB CE-17-22Flight Controls, Aileron Control SystemSAIB CE-17-03Flight Controls, Rudder Control SystemSAIB CE-16-27Flight Controls, Trailing Edge (TE) Flap Control SystemSAIB CE-16-10Stabilizers, Rudder StructureSAIB CE-16-07Powerplant, Engine Mount SectionSAIB CE-11-49Flight Controls, Elevator Tab Control SystemSAIB CE-11-30Aircraft StructuresSAIB CE-09-28Fuselage Main, Longeron/Stringer: Float Equipped Air Tractor AT-802 and AT-802A Airplanes - Periodic Inspection and Repair for Aft Fuselage Diagonal TubesSAIB CE-04-23NTSB investigations
No NTSB investigations matched to N802AMMatched by N-number and event date. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Air Tractor AT-802 aircraft
FAA incident reports
No FAA accident or incident reports matched to N802AMMatched by N-number and event date. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Air Tractor AT-802 aircraft
Service difficulty reports · 11
SDR ASMF200405005Warning Light · illuminatedAIRCRAFT SUSPENDED TAKE OFF AT 70 KTS AND RETURNED TO PLATFORM BECAUSE (L ENG BLEED OFF) LIGHT TURNED ON. (L ENG BLEED OFF) LIGHT WAS DEFERRED IAW MEL 36-11-1. FIM 36-10-00 PROCEDURE WAS PERFORMED AND SUSPENDED TAKE OFF INSPECTION WAS ACCOMPLISHED IAW MM 05-5SDR ASMF200404021Idg · failedAIRCRAFT PERFORMED AN UNSCHEDULED LANDING AT MTY AS A CONSEQUENCE OF APU WAS SHUTDOWN IN FLIGHT AND LT IDG WAS PREVIOUSLY DEFERRED. BITE TO ECU WAS PERFORMED IAW FIM 49-11-00 AND "NO FAME" MESSAGE WAS SHOWN IN FAULT DISPLAY. APU OIL LEVEL WAS VERIFIED AND FOUNSDR MEX2004026Skin · damagedDURING OVERNIGHT SERVICE, IT WAS DETECTED THAT THE SLAT NR 5 HAD DAMAGES AND MATERIAL LOST IN A 20 X 10 INCH AREA, AND THE WING LEADING EDGE HAD DAMAGES TOO. SLAT NR 5 WAS REPLACED AND THE WING LEADING EDGE WAS REPAIRED IAW MM, ALL CORRECT.SDR MEX2003325Turbine · damagedMEX-TIJ - FLT 176 - AIRTURN BACK, DURING TAKEOFF RIGHT ENGINE HAD 600 DEGREES CELSIUS REDUCING THRUST TO MAINTAIN TEMPERATURE ON LIMITS. DURING EHM ANALYSIS WAS DETECTED R EGT YELLOW MESSAGE AND AIRCRAFT WAS SENT TO THE HANGAR. DURING REVISION DETECTED MISINGSDR MEX2003212Inlet · damagedFLT 6444 - MEX-HMO - DURING TRANSIT CHECK, DETECTED FAN INLET GUIDE DAMAGED BY AND FOD. IN THE HANGAR THE FAN INLET GUIDE WAS REWORKED, TEST PERFORMED IAW 72-00-00, ALL CORRECT. (M)SDR MEX2003137Arm · jammedCAPTAIN REPORTED THAT WAS NOT POSSIBLE TO ARM THE EMERGENCY SLIDE OF DOOR NR 4 IT WAS JAMMED. AIRCRAFT WAS SENT TO THE HANGAR WHERE WAS TESTED AND ADJUSTED THE MECHANISM WAS ADJUSTED IAW MM 52-11-20, ALL CORRECT. (M)SDR MEX2003055Girt Bar · stuckAIRCRAFT RETURNED TO PLATFORM DUE TO LEFT AFT SLIDE DOOR NR 4 WAS NOT ARMED, ARMED AND DISARMED SYSTEM, AFT SLIDE DOOR 4 WAS CHECKED AND IT WAS STUCK. AIRCRAFT WAS SENT TO THE HANGAR. EMERGENCY MECHANISM WAS ADJUSTED IAW MM, TEST CORRECT.SDR MEX2003029Slide · stuckAIRCRAFT RETURNED TO PLATFORM, LEFT AFT SLIDE WAS NOT ARMED. ARMED AND DISARMED MECHANISM OF LEFT AFT SLIDE WAS CHECKED, IT WAS STUCK. BAR WAS REMOVED AND REINSTALLED IAW MM, TESTS CORRECT.SDR MEX2002216Fan · malfunctionedFLT 490 - MEX-LAX - CAPTAIN ABORTED TAKEOFF, RADAR FAILED, OVERHEAT LIGHT WAS ON AND BURNING SMELL WAS DETECTED. DURING CHECK RADAR AND EICAS MESSAGES WERE OK AND BURNING SMELL DISAPPEARED. AIR CONDITIONING PACKS, TRIM VALVES WERE CHECKED, ALL OK. AIRCRAFT SDR MEX2002027Actuator · failedFLT 402 - MEX-NYC - DURING TRANSIT CHECKED ENGINE NR 1 AND THE REVERSER WAS FOUND DEACTIVATED. THE WIRE BUNDLE OF THE REVERSER CONTROL VALVE WAS CHAFED AGAINST THE WIRE BUNDLE OF THE FIRE DETECTOR. WIRE BUNDLES WERE ISOLATED, REVERSERS WORKED OK AND NO SCREESDR MEX2002024Valve · leakingFLT 913 - MTY-MEX - AIRCRAFT ARRIVED TO PLATFORM WITH HYDRAULIC FLUID LEAK IN THE LEFT WING. IT WAS CHECKED AND THE LEAK WAS FOUND AT SPOILER PCA NR 3 LEFT SIDE, EHSV BODY. CANCELLED THE PRESSURE AND RETURN PORTS AND DISCONNECTED THE ELECTRIC CONNECTOR OF TH