# N776AS: 2016 Air Tractor AT-802A

- Status: Valid registration
- Airframe: [Air Tractor AT-802A](https://openairdocs.org/model/air-tractor-at-802a) (registry code 0390308, 2 seats)
- Engine: [Pratt & Whitney Canada PT6A-67F](https://openairdocs.org/engine/pratt-whitney-canada-pt6a-67f) (registry code 52290)
- Data sheets: [TCDS A19SW](https://openairdocs.org/tcds/A19SW) (Air Tractor Inc.), [TCDS E26NE](https://openairdocs.org/tcds/E26NE) (Pratt & Whitney Canada Corp.) (OpenAirDocs)
- Serial number: 802A-0648
- Year built: 2016
- Type: Fixed wing single engine
- Engine type: Turbo-prop
- Airworthiness: Restricted, agriculture and pest control, forest
- Airworthiness date: April 18, 2016
- Certificate issued: December 20, 2019
- Expires: December 31, 2029
- Mode S code: AA7F62
- Registered owner: [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE)
- Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City)
- Owner type: Corporation
- Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=776AS
- Page: https://openairdocs.org/aircraft/N776AS

From the FAA registry file of October 22, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination.

## ADs that may apply (OpenAirDocs): 14 in force

### Matched by airframe (Air Tractor AT-802A)

- [AD 2026-16-12](https://openairdocs.org/ad/2026-16-12): Horizontal stabilizer structure; Horizontal stabilizer miscellaneous structure; Vertical stabilizer structure · Air Tractor AT-802 and AT-802A. Effective Aug 31, 2026
- [AD 2021-05-14](https://openairdocs.org/ad/2021-05-14): TE flap control system · Air Tractor AT-250, AT-300, AT-301 and 19 more. Effective Apr 29, 2021
- [AD 2014-16-17](https://openairdocs.org/ad/2014-16-17): Wings · Air Tractor AT-802 and AT-802A. Effective Sep 29, 2014
- [AD 2009-18-04](https://openairdocs.org/ad/2009-18-04): Rudder-aileron interconnect · Air Tractor AT-802 and AT-802A. Effective Oct 1, 2009
- [AD 2009-11-05](https://openairdocs.org/ad/2009-11-05): Cracks in the engine mount · Air Tractor AT-400, AT-400A, AT-402 and 9 more. Effective Jun 1, 2009
- [AD 2008-26-01](https://openairdocs.org/ad/2008-26-01): Overturn skid plate kit · Air Tractor AT-250, AT-300, AT-301 and 15 more. Effective Jan 28, 2009
- [AD 2006-23-14](https://openairdocs.org/ad/2006-23-14): Rudder and vertical fin hinge attaching structure · Air Tractor AT-502, AT-502A, AT-502B and 3 more. Effective Dec 21, 2006
- [AD 2006-20-10](https://openairdocs.org/ad/2006-20-10): Attach angles on the firewall mounted  
 hopper rinse tank shelf · Air Tractor AT-802 and AT-802A. Effective Nov 3, 2006
- [AD 2005-13-12](https://openairdocs.org/ad/2005-13-12): Front and rear spar of the horizontal stabilizer · Air Tractor AT-300, AT-301, AT-302 and 11 more. Effective Aug 5, 2005
- [AD 2004-15-15](https://openairdocs.org/ad/2004-15-15): Aft Fuselage Upper Longeron · Air Tractor AT-401, AT-401B, AT-402 and 10 more. Effective Sep 7, 2004
- [AD 2002-15-06](https://openairdocs.org/ad/2002-15-06): Rudder control cable · Air Tractor AT-802 and AT-802A. Effective Sep 13, 2002
- [AD 97-04-11](https://openairdocs.org/ad/97-04-11): Tail Landing Gear Spring · Air Tractor AT-802 and AT-802A. Effective Apr 4, 1997
- [AD 96-04-08](https://openairdocs.org/ad/96-04-08): Main Landing Gear Legs · Air Tractor AT-802 and AT-802A. Effective Apr 12, 1996

### Matched by engine (Pratt & Whitney Canada PT6A-67F)

- [AD 2024-04-51](https://openairdocs.org/ad/2024-04-51): Turbine Section · Pratt & Whitney Canada PT6A-64, PT6A-66, PT6A-66A and 17 more. Effective Mar 28, 2024

### Historical (superseded or no longer in force)

- [AD 2024-16-06](https://openairdocs.org/ad/2024-16-06) (historical): Horizontal Stabilizer Structure; Horizontal stabilizer, Spar/Rib; Horizontal Stabilizer Miscellaneous Structure;  Vertical Stabilizer Structure · Air Tractor AT-802 and AT-802A. Effective Sep 4, 2024
- [AD 2023-15-07](https://openairdocs.org/ad/2023-15-07) (historical): Horizontal Stabilizer Structure; Horizontal stabilizer, Spar/Rib; Horizontal Stabilizer Miscellaneous Structure; Vertical Stabilizer Structure · Air Tractor AT-802 and AT-802A. Effective Aug 9, 2023
- [AD 2010-17-18 R1](https://openairdocs.org/ad/2010-17-18-R1) (historical): Wings · Air Tractor AT-802 and AT-802A. Effective Jan 14, 2011
- [AD 2010-17-18](https://openairdocs.org/ad/2010-17-18) (historical): Wings · Air Tractor AT-802 and AT-802A. Effective Sep 9, 2010
- [AD 2010-13-08](https://openairdocs.org/ad/2010-13-08) (historical): Wing main spar lower caps · Air Tractor AT-802 and AT-802A. Effective Jul 28, 2010
- [AD 2008-11-17](https://openairdocs.org/ad/2008-11-17) (historical): Overturn skid plate in the cockpit area · Air Tractor AT-250, AT-300, AT-301 and 14 more. Effective Jul 7, 2008
- [AD 2008-10-12](https://openairdocs.org/ad/2008-10-12) (historical): Cracks in the engine mount · Air Tractor AT-400, AT-400A, AT-402 and 9 more. Effective Jun 12, 2008
- [AD 2007-13-17](https://openairdocs.org/ad/2007-13-17) (historical): Cracked engine mounts · Air Tractor AT-602, AT-802 and AT-802A. Effective Aug 10, 2007
- [AD 2006-22-08](https://openairdocs.org/ad/2006-22-08) (historical): Inspect engine mount · Air Tractor AT-602, AT-802 and AT-802A. Effective Dec 1, 2006
- [AD 2006-08-09](https://openairdocs.org/ad/2006-08-09) (historical): Main spar lower caps · Air Tractor AT-802 and AT-802A. Effective Apr 21, 2006
- [AD 2002-19-10](https://openairdocs.org/ad/2002-19-10) (historical): Upper longeron and upper diagonal tube · Air Tractor AT-402, AT-402A, AT-402B and 3 more. Effective Nov 15, 2002
- [AD 2002-11-05](https://openairdocs.org/ad/2002-11-05) (historical): Wing Lower Spar Cap · Winglets (Aero Spraying Service STC SA00490LA). Effective Jul 12, 2002
- [AD 2001-10-04 R1](https://openairdocs.org/ad/2001-10-04-R1) (historical): Wing Lower Spar Cap · Air Tractor AT-400, AT-400A, AT-401 and 11 more. Effective Jun 8, 2001
- [AD 2001-10-04](https://openairdocs.org/ad/2001-10-04) (historical): Wing Lower Spar Cap · Air Tractor AT-400, AT-401, AT-401B and 10 more. Effective Jun 8, 2001

## Information bulletins (advisory) (11 in force)

- [SAIB CE-19-21](https://openairdocs.org/saib/CE-19-21): Flap Motor Mounting Studs. Issued Dec 9, 2019
- [SAIB CE-18-06](https://openairdocs.org/saib/CE-18-06): Flight Controls, Rudder Control System. Issued Dec 1, 2017
- [SAIB CE-17-22](https://openairdocs.org/saib/CE-17-22): Flight Controls, Aileron Control System. Issued Aug 22, 2017
- [SAIB CE-17-03](https://openairdocs.org/saib/CE-17-03): Flight Controls, Rudder Control System. Issued Dec 16, 2016
- [SAIB CE-16-27](https://openairdocs.org/saib/CE-16-27): Flight Controls, Trailing Edge (TE) Flap Control System. Issued Oct 31, 2016
- [SAIB CE-16-10](https://openairdocs.org/saib/CE-16-10): Stabilizers, Rudder Structure. Issued Dec 1, 2015
- [SAIB CE-16-07](https://openairdocs.org/saib/CE-16-07): Powerplant, Engine Mount Section. Issued Nov 20, 2015
- [SAIB CE-11-49](https://openairdocs.org/saib/CE-11-49): Flight Controls, Elevator Tab Control System. Issued Aug 26, 2011
- [SAIB CE-11-30](https://openairdocs.org/saib/CE-11-30): Aircraft Structures. Issued May 9, 2011
- [SAIB CE-09-28](https://openairdocs.org/saib/CE-09-28): Fuselage Main, Longeron/Stringer: Float Equipped Air Tractor AT-802 and AT-802A Airplanes - Periodic Inspection and Repair for Aft Fuselage Diagonal Tubes. Issued May 12, 2009
- [SAIB CE-04-23](https://openairdocs.org/saib/CE-04-23): . Issued Dec 2, 2003

## NTSB investigations

None matched to N776AS.

## FAA accident and incident reports (2)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20220614005119I](https://openairdocs.org/incident/20220614005119I), Jun 14, 2022: Air Tractor Inc AT-802A (N776AS), Toppenish, WA, Minor damage. Amphibian fire fighting airplane lost power due to fuel starvation while enroute to contract base airport. Aircraft made an emergency landing in rangeland…
- [Incident 20180628008809I](https://openairdocs.org/incident/20180628008809I), Jun 28, 2018: Air Tractor Inc AT-802A (N776AS), Dallesport, WA, Minor damage. At the end of water scoop on Columbia river (aftr 3-4 scouting passes) aircraft hit 2 roller type waves in quick succession. After climb out noticed wrinkle on…

## Reports on N776AS not matched to an aircraft (1)

They name N776AS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 20090113025029I](https://openairdocs.org/incident/20090113025029I), Jan 13, 2009: Boeing 737-4Q8 (N776AS), Kodiak, AK, Minor damage. The anchorage FSDO incident number is: IAL0320090010THE pilot stated: we were unable to fly the 'rwy 25 ils' approach into adq due to tailwind limits. We…

## Service difficulty reports

None filed for this aircraft. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

## Service difficulty reports on N776AS not matched to an aircraft (110, newest 50)

They name N776AS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR ASAA0944356](https://openairdocs.org/sdr/ASAA0944356), Feb 4, 2009: JAM-NUT. LOOSE. R 1 DOOR HARD TO CLOSE FROM INSIDE CABIN. PERFORMED INSPECTION OF R 1 DOOR MECHANISM PER AMM 52 41 00 206 001. FOUND JAM NUT ON TOP HINGE GUIDE ARM LOOSE. COMPL
- [SDR ASAA0843345](https://openairdocs.org/sdr/ASAA0843345), Aug 15, 2008: NUT. LOOSE. L1 DOOR VERY STIFF HARD TO OPEN. PERFORMED VISUAL INSP OF L1 DOOR FOUND GUIDE ARM LOCK NUT LOOSE. TIGHTENED LOCK NUT IAW AMM 52 11 00 705 007 B00. PERFORMED FWD
- [SDR ASAA0843328](https://openairdocs.org/sdr/ASAA0843328), Jul 28, 2008: BEAM. CRACKED. BS 601, STUB BEAM INNER HORD LOWER FASTENER HOLE CRACKED REPAIRED IAW EA 5310-02807.
- [SDR ASAA0843327](https://openairdocs.org/sdr/ASAA0843327), Jul 21, 2008: SKIN. CORRODED. EXFOLIATION CORROSION FOUND ON UPPER WING SKIN AT FS 608.5 RBL 62 REPAIRED IAW EA 5710 01153.
- [SDR ASAA0843326](https://openairdocs.org/sdr/ASAA0843326), Jul 21, 2008: SKIN. CORRODED. EXFOLIATION CORROSION FOUND ON UPPER WING SKIN AT FS 592 RBL 63 REPAIRED IAW EA 5710 01153.
- [SDR ASAA0843325](https://openairdocs.org/sdr/ASAA0843325), Jul 21, 2008: SKIN. CORRODED. EXFOLIATION CORROSION FOUND ON UPPER WING PLANK AT FS591, RBL67 REPAIRED IAW EA 5710 01153.
- [SDR ASAA0843324](https://openairdocs.org/sdr/ASAA0843324), Jul 21, 2008: SKIN. CORRODED. EXFOLIATION CORROSION FOUND ON UPPER WING PLANK AT FS 661, RBL 57 REPAIRED IAW EA-5710 01153.
- [SDR ASAA0741629](https://openairdocs.org/sdr/ASAA0741629), May 2, 2007: SHEAR TIE. CRACKED. SHEAR TIE CRACKED. CUT OUT DAMAGED SECTION OF FRAME (SHEAR TIE) FABRICATED AND INSTALLED A REPAIR SHEAR TIE DOUBLER AND RADIUS FILLERS IAW SRM 53 00 07 FIG 201 
- [SDR ASAA0741628](https://openairdocs.org/sdr/ASAA0741628), May 2, 2007: SKIN. PUNCTURED. THE IB FORE FLAP IS PUNCTURED NEAR THE CENTER TRACK. REMOVED THE DAMAGED AREA OF LWR SKIN FABRICATED AND INSTALLED A SKIN FILLER AND A REPAIR DOUBLER IAW SRM 51
- [SDR ASAA0741627](https://openairdocs.org/sdr/ASAA0741627), May 2, 2007: SKIN. CHAFED. THE RT OB MID FLAP IS CHAFED ON AN EXITING LE DOUBLER AT THE IB END. REMOVED THE EXITING REPAIR DOUBLER FABRICATED AND INSTALLED A REPAIR DOUBLER IAW SRM 57 53 
- [SDR ASAA0741626](https://openairdocs.org/sdr/ASAA0741626), May 2, 2007: SKIN. CRACKED. NR 2 SLAT SKIN LWR LIP IS CRACKED AROUND FASTENER HOLES JUST BELOW THE O B AUX TRACK. CUT OUT THE DAMAGED AREA OF SKIN FABRICATED AND INSTALLED A SKIN FILLER AN
- [SDR ASAA0741625](https://openairdocs.org/sdr/ASAA0741625), May 2, 2007: SKIN. DAMAGED. OUTWARD DING IN FUSELAGE SKIN REMOVED SKIN DAMAGE BY DRILLING A 0.1935" HOLE INSTALLED A BACR15BB6 RIVET IAW ASA EA 5330 02205 REV NEW AND AAR EA 112004 REV IR.
- [SDR ASAA0741623](https://openairdocs.org/sdr/ASAA0741623), May 2, 2007: DOUBLER. CHAFED. RT IB FORE FLAP CHAFED ON AN EXITING REPAIR DOUBLER ON THE UPPER SIDE. REMOVED THE EXITING REPAIR DOUBLER AND FILLER FABRICATED AND INSTALLED A REPLACEMENT DOUB
- [SDR ASAA0741622](https://openairdocs.org/sdr/ASAA0741622), May 2, 2007: SKIN. DENTED. LT IB FOR FLAP DENTED OUT OF LIMITS NEAR CENTER TRACK. REMOVED THE DAMAGED AREA OF LOWER SKIN FABRICATED AND INSTALLED A SKIN FILLER AND REPAIR DOUBLER IAW SRM 
- [SDR ASAA0741621](https://openairdocs.org/sdr/ASAA0741621), May 2, 2007: SKIN. DELAMINATED. LT ELEV TAB UPPER SURFACE T E IS SPLIT 51" FROM I B END. PREPPED THE TAB UPPER SKIN SURFACE FOR BONDING CUT AND APPLIED REPAIR PLIES IAW SRM 51 70 05 PAPR 3.
- [SDR ASAA0640270](https://openairdocs.org/sdr/ASAA0640270), Mar 16, 2006: SKIN. DENTED. SKIN DENTED. FABRICATED AND INSTALLED REPAIR PARTS PER EA 5330 02061 AND ER 06 1486.
- [SDR ASAA0640265](https://openairdocs.org/sdr/ASAA0640265), Mar 15, 2006: SKIN. DENTED. FUSELAGE SKIN DENT. REPAIRED PER EA 5330 02064 AND EO 06 1319.
- [SDR ASAA0640260](https://openairdocs.org/sdr/ASAA0640260), Mar 15, 2006: DOOR FRAME. CRACKED. L1 DOOR FRAME CRACKED AT LOWER STOP FITTING FWD SIDE. REPAIRED PER EA 5310 02594.
- [SDR ASAA0640254](https://openairdocs.org/sdr/ASAA0640254), Mar 13, 2006: SKIN. CHAFED. CHAFE MARKS ON SKIN. INSTALLED REPAIR PER ASA EA 5360 01055.
- [SDR ASAA0640255](https://openairdocs.org/sdr/ASAA0640255), Mar 13, 2006: FLOORBEAM. CORRODED. FLOORBEAM CORRODED. REMOVED CORRODED AREA AND INSTALLED REPAIR PER EA 5310 02591.
- [SDR ASAA0640234](https://openairdocs.org/sdr/ASAA0640234), Mar 8, 2006: FLOORBEAM. CORRODED. FOUND CORROSION ON FLOORBEAM. REPAIRED PER GOODRICH ER 06 1383 AND ASA EA 5310 02585.
- [SDR ASAA0640229](https://openairdocs.org/sdr/ASAA0640229), Mar 7, 2006: FLOORBEAM. CORRODED. FOUND TOP FLANGE OF FLOORBEAM CORRODED. REPAIRED PER SRM 51 70 11.
- [SDR ASAA0640228](https://openairdocs.org/sdr/ASAA0640228), Mar 7, 2006: FRAME. CRACKED. FOUND BSTA 907 STR 8L FRAME CRACKED. REPAIRED PER SRM 53 00 07.
- [SDR ASAA0640225](https://openairdocs.org/sdr/ASAA0640225), Mar 4, 2006: FLOORBEAM. CORRODED. FOUND TOP FLANGE OF FLOORBEAM AT BSTA 360 RBL 12 TO 25 WL 208 CORRODED. REPAIRED FLOORBEAM PER SRM 51 70 11.
- [SDR ASAA0640221](https://openairdocs.org/sdr/ASAA0640221), Feb 28, 2006: SILL. CORRODED. AFT SERVICE DOOR CREASE BEAM MOPSILL CORRODED. REMOVED AND REPLACED AFT SVC DOOR MOPSILL PER SRM 51 40 02.
- [SDR ASAA0640207](https://openairdocs.org/sdr/ASAA0640207), Feb 28, 2006: WEB. CRACKED. FOUND FLOOR WEB IS CRACKED. REMOVED AND REPLACED WEB.
- [SDR ASAA0640199](https://openairdocs.org/sdr/ASAA0640199), Feb 23, 2006: CREASE BEAM. CORRODED. FOUND CREASE BEAM CORRODED. REPLACED CREASE BEAM PER SRM 51 40 02.
- [SDR ASAA0640198](https://openairdocs.org/sdr/ASAA0640198), Feb 22, 2006: FRAME. CHAFED. FOUND FRAME FLANGE CHAFED. REPAIRED PER SRM 51 70 11.
- [SDR ASAA0640195](https://openairdocs.org/sdr/ASAA0640195), Feb 22, 2006: ANGLE. CORRODED. CORROSION ON THRESHOLD Z ANGLE. REMOVED AND REPLACED PER SRM 51 40 02.
- [SDR ASAA0640193](https://openairdocs.org/sdr/ASAA0640193), Feb 21, 2006: FRAME. CRACKED. CRACKED FRAME AT BIN RAIL ATTACHMENT. REPAIRED PER SRM 53 00 07
- [SDR ASAA0640194](https://openairdocs.org/sdr/ASAA0640194), Feb 21, 2006: STRINGER CLIP. CRACKED. CRACKED STRINGER CLIP. REMOVED AND REPLACED PER SRM 51 40 02.
- [SDR ASAA0640192](https://openairdocs.org/sdr/ASAA0640192), Feb 20, 2006: SHEAR TIE. CORRODED. CORRODED SHEAR TIE. REPAIRED PER SRM 53 00 07.
- [SDR ASAA0640191](https://openairdocs.org/sdr/ASAA0640191), Feb 20, 2006: SHEAR TIE. CORRODED. CORRODED SHEAR TIE. REPAIRED PER SRM 53 00 07.
- [SDR ASAA0640190](https://openairdocs.org/sdr/ASAA0640190), Feb 20, 2006: SHEAR TIE. CORRODED. CORRODED SHEAR TIE. REPAIRED PER SRM 53 00 07.
- [SDR ASAA0640189](https://openairdocs.org/sdr/ASAA0640189), Feb 20, 2006: SHEAR TIE. CORRODED. CORRODED SHEAR TIE. REPAIRED PER SRM 53 00 07.
- [SDR ASAA0640188](https://openairdocs.org/sdr/ASAA0640188), Feb 20, 2006: SHEAR TIE. CORRODED. CORROSION ON SHEAR TIE. REMOVED AND REPAIRED PER SRM 53 00 07.
- [SDR ASAA0640187](https://openairdocs.org/sdr/ASAA0640187), Feb 19, 2006: CREASE BEAM. CORRODED. CORROSION AT RT SIDE CREASE BEAM. REMOVED AND REPLACED OUT OF LIMITS CORRODED CREASE BEAM PER SRM 57 48 02.
- [SDR ASAA0640186](https://openairdocs.org/sdr/ASAA0640186), Feb 19, 2006: STRINGER CLIP. CHAFED. STRINGER CLIP CHAFED. REMOVED AND REPLACED STRINGER CLIP PER SRM 51 40 02.
- [SDR ASAA0640166](https://openairdocs.org/sdr/ASAA0640166), Feb 17, 2006: FLOORBEAM. CORRODED. CORRODED FLOOR BEAM.
- [SDR ASAA0640165](https://openairdocs.org/sdr/ASAA0640165), Feb 16, 2006: FLOORBEAM. CORRODED. FLOOR BEAM FASTENER HOLES HAVE CORROSION.
- [SDR ASAA0640164](https://openairdocs.org/sdr/ASAA0640164), Feb 16, 2006: STRINGER CLIP. CRACKED. STRINGER CLIP CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM 51 40 02.
- [SDR ASAA0540278](https://openairdocs.org/sdr/ASAA0540278), Jun 6, 2005: SKIN. DENTED. DENT FOUND AT LT WING IB T/E FORE FLAP. REPAIRED LT WING IB T/E FORE FLAP IAW SRM. (K)
- [SDR ASAA0540277](https://openairdocs.org/sdr/ASAA0540277), May 30, 2005: SKIN. GOUGED. LT WING UPPER SKIN GOUGED AT WING STA 223 BETWEEN STA 12 AND 13. BLENDED AREA, TREATED AND PRIMED IAW EA. (K)
- [SDR ASAA0540276](https://openairdocs.org/sdr/ASAA0540276), May 28, 2005: SKIN. CHAFED. NR 4 SLAT IB T/E CHAFED. REMOVED DAMAGE, FABRICATED FILLER SKIN AND DOUBLER AND INSTALLED REPAIR IAW SRM. (K)
- [SDR ASAA0540268](https://openairdocs.org/sdr/ASAA0540268), May 26, 2005: SKIN. DELAMINATED. LT WING OB FORE FLAP DELAMINATED AT IB END. REMOVED DAMAGED AREA OF LT OB FORE FLAP IAW SRM. (K)
- [SDR ASAA0540267](https://openairdocs.org/sdr/ASAA0540267), May 26, 2005: SKIN. DELAMINATED. RT WING OB AFT FLAP DELAMINATED AT IB TRAILING EDGE. REMOVED DAMAGED MATERIAL, INSTALLED CORE, SKIN, AND DOUBLER IAW SRM. (K)
- [SDR ASAA0540266](https://openairdocs.org/sdr/ASAA0540266), May 26, 2005: SKIN. DELAMINATED. NR 2 SLAT HAS DELAMINATED AT IB TRAILING EDGE. REPAIRED DAMAGED AREA OF NR 2 SLAT IAW SRM. (K)
- [SDR ASAA0540269](https://openairdocs.org/sdr/ASAA0540269), May 25, 2005: SHEAR TIE. CRACKED. SHEAR TIE CRACKED AND CORRODED AT STR 28L B-STA 500G. FABRICATED SHEAR TIE, REMOVED AND REPLACED SHEAR TIE IAW SRM AND MFG DWG. (K)
- [SDR ASAA0540265](https://openairdocs.org/sdr/ASAA0540265), May 25, 2005: SHEAR TIE. CORRODED. SHEAR TIE BETWEEN STR 26L AND 25R, B-STA 947 HAS SURFACE CORROSION. REMOVED FABRICATED AND INSTALLED SHEAR TIE AND CLIP IAW SRM . (K)
- [SDR ASAA0540264](https://openairdocs.org/sdr/ASAA0540264), May 25, 2005: SKIN. CORRODED. NR 5 SLAT IB TRAILING EDGE CHAFED. REMOVED DAMAGE, BONDED FILLER SKIN AND DOUBLER IAW SRM. (K)

All 110: https://openairdocs.org/aircraft/N776AS/unmatched-reports.md

## STCs that may be installed (OpenAirDocs) (75, first 50)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the airframe (Air Tractor AT-802A)

- [STC SA04484CH](https://openairdocs.org/stc/SA04484CH): Installation of a Reabe Aircraft Improvement Power Gate Control System. Reabe Design LLC
- [STC SA01800SE](https://openairdocs.org/stc/SA01800SE): Fabrication and installation of new or replacement of existing instrument panel lights dimmer control. TCW Technologies, LLC
- [STC SA01861SE](https://openairdocs.org/stc/SA01861SE): Fabrication and installation of Landing Light Controller. TCW Technologies, LLC
- [STC SA01844WI](https://openairdocs.org/stc/SA01844WI): Installation of Garmin GFC 600 Automatic Flight Control System. Garmin International Inc
- [STC SA04837NY](https://openairdocs.org/stc/SA04837NY): Installation of AeroLED's Holdings, LLC., position lights, navigation lights, strobe lights and beacon lights. AeroLED's Holdings, LLC
- [STC SA01795CH](https://openairdocs.org/stc/SA01795CH): For Model AT-802A: Installation of Wipaire Model 10000 Amphibious Floats in accordance with Wipaire, Inc. Installation Drawing No. 7D1-4251, No Revision, dated January 13, 2003, or later FAA approved revisions. Operations with the floats removed are permitted when the aircraft is modified in accordance with Wipaire, Inc. Installation Drawing No. 7D1-4405, No Revision, dated January 13, 2003, or later FAA approved revisions. For Model AT-802: Installation of Wipaire Model 10000 Amphibious Floats in accordance with Wipaire, Inc. Installation Drawing No. 1003231, Revision A, dated June 12, 2008, or later FAA approved revisions. Operations with the floats removed are permitted when the aircraft is modified in accordance with Wipaire, Inc. Installation Drawing No. 1003406, Revision 01, dated July 15, 2008, or later FAA approved revisions. Wipaire Inc
- [STC SA02019SE-D](https://openairdocs.org/stc/SA02019SE-D): Installation of Garmin Model GTN 625/635/650; 725/750 Navigation System. Garmin International Inc
- [STC SA12386AK](https://openairdocs.org/stc/SA12386AK): Increase of the engine power of the PT6A-67F engine to 1600 SHP for takeoff power and 1550 SHP for maximum continuous power. Momentum Aeronautics Holdings, LLC
- [STC SA12204WI](https://openairdocs.org/stc/SA12204WI): Wing Spar Cap manufacturing process change. Air Tractor Inc
- [STC SA03040CH](https://openairdocs.org/stc/SA03040CH): Installation of a digital payload hopper quantity and spray boom pressure indicating system. Reabe Design LLC
- [STC SA12187AK](https://openairdocs.org/stc/SA12187AK): Installation of Momentum Aeronautics Holdings LLC. Model 11600 Amphibious Floats. Momentum Aeronautics Holdings, LLC
- [STC SA09946AC](https://openairdocs.org/stc/SA09946AC): Installation of a single point fueling system. Texas Transland LLC
- [STC SA02031WI](https://openairdocs.org/stc/SA02031WI): Installation of a True Blue Power TB60 Lithium ION Battery to replace the existing lead-acid battery. Wipaire Inc
- [STC SA12057IB](https://openairdocs.org/stc/SA12057IB): Substitution of basic instrumentation by an electronic display PFD/MFD Garmin GDU 1060 (G600 Txi). Aeronautics Solutions Europe S.L
- [STC SA02603SE](https://openairdocs.org/stc/SA02603SE): Installation of a Supplemental Lighting System manufactured and installed. Aviation Specialties Unlimited Inc
- [STC SA02738CH](https://openairdocs.org/stc/SA02738CH): Installation of L-3 Communications Avionics Systems. Acron Aviation Inc
- [STC SA11868WI](https://openairdocs.org/stc/SA11868WI): Increased Altitude Limitation. CO Fire Aviation Inc
- [STC SA01240SE](https://openairdocs.org/stc/SA01240SE): Installation of secondary voltage indication system. Visual Instruments LLC
- [STC SA01995WI](https://openairdocs.org/stc/SA01995WI): Spray System Installation. See attached FAA Approved Model List (AML) SA01995WI for required data. Aeronautix, LLC
- [STC SA39CH](https://openairdocs.org/stc/SA39CH): Installation of an Amphibian Landing Gear Position Advisory System/Laser Gear Advisory System. Wipaire Inc
- [STC SA04676CH](https://openairdocs.org/stc/SA04676CH): Installation of a True Quantity Gauge System. Reabe Design LLC
- [STC SA04568CH](https://openairdocs.org/stc/SA04568CH): Installation of the uAvionix tailBeaconX, a tail mounted position light with integrated Automatic Dependent Surveillance - Broadcast (ADS-B) Out and 1090MHz Mode-S transponder functionality. uAvionix Corporation
- [STC SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc
- [STC SA01851WI](https://openairdocs.org/stc/SA01851WI): Installation of a Hydraulic Actuator and Auger. Texas Transland LLC
- [STC SA04526NY](https://openairdocs.org/stc/SA04526NY): Installation of MT-Propeller Entwicklung GmbH model MTV-27-1-( )-C-F-R(P)-J/CFR300-82( ) 5-blade, full feathering, constant speed, counterweighted, reversing propellers and spinners. MT- Propeller Entwicklung GmbH
- [STC SA02266SE](https://openairdocs.org/stc/SA02266SE): Installation of a Lever Throttle Quadrant. Kawak Aviation Technologies Inc
- [STC SA01801SE](https://openairdocs.org/stc/SA01801SE): Installation of a Kawak Aviation Technologies auxiliary system, and optional ancillary equipment. Air Repair Inc
- [STC SA02444AK](https://openairdocs.org/stc/SA02444AK): Approval of the L-3 Communications NGT 9000/9000R ADS-B system installed. ADS-B Technologies LLC
- [STC SA02265SE](https://openairdocs.org/stc/SA02265SE): Installation of a camera housing. Airborne Sensor LLC
- [STC SA02430SE](https://openairdocs.org/stc/SA02430SE): Fabrication and installation of a camera housing. Airborne Sensor LLC
- [STC SA04514NY](https://openairdocs.org/stc/SA04514NY): Single/Dual Transponder System ADS-B Upgrade. Scandinavian Avionics Design ApS
- [STC SA01756WI](https://openairdocs.org/stc/SA01756WI): Installation of a Tail Wheel Modification. Turbine Conversions Ltd
- [STC SA02535AK](https://openairdocs.org/stc/SA02535AK): Fabrication of Fire Retardant Dispersal System, GEN III. Trotter Controls Inc
- [STC SA01714WI](https://openairdocs.org/stc/SA01714WI): Installation of a Garmin transponders: (a) GTX 330/330D/33/33D with ADS-B Out functionality; (b) GTX 335/335R/345/345R with ADS-B Out and In functionality; or (c) GTX 335R/345R with ADS-B Out functionality in select airplanes installed with G950/G1000 systems. Garmin International Inc
- [STC SA00344BO PAGE 2](https://openairdocs.org/stc/SA00344BO%20PAGE%202): Installation of Parmetheus Plus LED PAR36 and PAR46 taxi and landing lights. Whelen Aerospace Technologies
- [STC SA02135SE](https://openairdocs.org/stc/SA02135SE): Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data). Electronics International Inc
- [STC SA04165NY](https://openairdocs.org/stc/SA04165NY): Installation of Latitude Technologies Skynode S200 Satcom system must be performed. Latitude Technologies Corporation
- [STC SA01323CH](https://openairdocs.org/stc/SA01323CH): Installation of a ground single point fueling system. Turbine Conversions Ltd
- [STC SA04145NY](https://openairdocs.org/stc/SA04145NY): Installation of the Flight Data Acquisition Storage and Transmission System (Fast). Amtech Aeronautical Limited
- [STC SA01560SE](https://openairdocs.org/stc/SA01560SE): Install modified engine cowl per Cascade Flying Service LLC data. Cascade Flying Service LLC
- [STC SA02205SE](https://openairdocs.org/stc/SA02205SE): Installation of a replacement airframe fuel pump in accordance with Cascade Flying Service Master Drawing List FW-CFS545-90, Rev. B, dated October 19, 2011, or later FAA approved revision. Cascade Aircraft conversions LLC
- [STC SA01745WI](https://openairdocs.org/stc/SA01745WI): Installation of a Cable Cutter System on the Main Landing Gear. Hershey Flying Service Inc
- [STC SA09743AC-D](https://openairdocs.org/stc/SA09743AC-D): Installation of an S-TEC 3100 (01326) Digital Flight Control System (DFCS). S-TEC Corporation
- [STC SA04398AT](https://openairdocs.org/stc/SA04398AT): Installation of a Manual Dump Gate Box. Texas Transland LLC
- [STC SA01845WI](https://openairdocs.org/stc/SA01845WI): Installation of a Center Windshield. Hershey Flying Services
- [STC SA00382BO](https://openairdocs.org/stc/SA00382BO): Installation of Globalstar Antenna and Cradle provisions to support a Globalstar GPS-1700 in non-composite airplanes. Avidyne Corporation
- [STC SA02276AK](https://openairdocs.org/stc/SA02276AK): Installation of AMSAFE Aviation Inflatable Restraints. AMSAFE Inc
- [STC SA09866AC](https://openairdocs.org/stc/SA09866AC): Installation of a Fire Gel tank and associated systems. Pays Air Service Pty LTD
- [STC SA02119SE PAGE 1](https://openairdocs.org/stc/SA02119SE%20PAGE%201): Installation of Garmin GDL 88 ADS-B UAT Transceiver System. Garmin International Inc
- [STC SA01969SE](https://openairdocs.org/stc/SA01969SE): Installation of a Mid-Continent MD302 Standby Attitude Module. Mid-Continent Instruments and Avionics

All 75: https://openairdocs.org/aircraft/N776AS/stcs.md

## Related

- Other Air Tractor AT-802A aircraft: https://openairdocs.org/model/air-tractor-at-802a/aircraft.md
- The Pratt & Whitney Canada PT6A-67F engine: https://openairdocs.org/engine/pratt-whitney-canada-pt6a-67f.md

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