# N806FT: 1985 Kaston Aloysius P THORP T-18

- Status: Valid registration
- Airframe: [Kaston Aloysius P THORP T-18](https://openairdocs.org/model/kaston-aloysius-p-thorp-t-18) (registry code 89510L6, 2 seats)
- Engine: [Lycoming O&VO-360 series](https://openairdocs.org/engine/lycoming-o-vo-360-series) (registry code 41514)
- Serial number: K80-001
- Year built: 1985
- Type: Fixed wing single engine
- Engine type: Reciprocating
- Airworthiness: Experimental, amateur built
- Airworthiness date: January 15, 1986
- Certificate issued: October 13, 2020
- Expires: October 31, 2027
- Mode S code: AAF8B6
- Registered owner: [Johnson Daniel S](https://openairdocs.org/faa-owner/JOHNSON%20DANIEL%20S)
- Location: [Louisville, KY](https://openairdocs.org/faa-place/KY/Louisville)
- Owner type: Individual
- Owner's area on the map: 38.2154° N, 85.6187° W: Placed by OpenAirDocs at the center of ZIP code 40220, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=806FT
- Page: https://openairdocs.org/aircraft/N806FT

From the FAA registry file of October 24, 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. The registry lists only the engine series, so ADs for every Lycoming O&VO-360 model are included.

## ADs that may apply (OpenAirDocs): 40 in force

### Matched by airframe (Kaston Aloysius P THORP T-18)

None in force.

### Matched by engine (Lycoming O&VO-360 series)

- [AD 2026-04-11](https://openairdocs.org/ad/2026-04-11): Engine (Reciprocating) · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 605 more. Effective Apr 8, 2026
- [AD 2022-16-03](https://openairdocs.org/ad/2022-16-03): Engine (RECIPROCATING) · Continental Aerospace Technologies GTSIO-520-C, GTSIO-520-D, GTSIO-520-F and 236 more. Effective Aug 15, 2022
- [AD 2020-25-12](https://openairdocs.org/ad/2020-25-12): Reciprocating Engine Power Section · Superior Air Parts IO-360-A1A1, IO-360-A1A2, IO-360-A2A1 and 146 more. Effective Jan 15, 2021
- [AD 2017-16-11](https://openairdocs.org/ad/2017-16-11): Reciprocating Engine Power Section · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-360-B1G6 and 93 more. Effective Aug 15, 2017
- [AD 2012-19-01](https://openairdocs.org/ad/2012-19-01): Crankshafts · Lycoming Engines AEIO-360-A1A, AEIO-360-A1B, AEIO-360-A1B6 and 321 more. Effective Oct 24, 2012
- [AD 2012-03-07](https://openairdocs.org/ad/2012-03-07): Carburetor · Lycoming Engines GO-435, GO-435-C2 (O-435-17), GO-435-C2A and 389 more. Effective Mar 27, 2012
- [AD 2010-07-08](https://openairdocs.org/ad/2010-07-08): Turbochargers · Kelly Aerospace Energy Systems HIO-360-E1AD, HIO-360-E1BD, HIO-360-F1AD and 137 more. Effective Apr 19, 2010
- [AD 2009-26-12](https://openairdocs.org/ad/2009-26-12): Cylinder assemblies · Engine Components Reciprocating Engine Cylinder Assemblies, AEIO-320-D1B, AEIO-320-D2B and 264 more. Effective Feb 4, 2010
- [AD 2007-04-19 R1](https://openairdocs.org/ad/2007-04-19-R1): SAP cylinder assemblies · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 314 more. Effective May 7, 2007
- [AD 2006-12-07](https://openairdocs.org/ad/2006-12-07): ECi cylinder assemblies · Aerostar AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 386 more. Effective Jul 11, 2006
- [AD 2006-10-21](https://openairdocs.org/ad/2006-10-21): ECi connecting rods · Engine Components Reciprocating Engine Connecting Rods, AEIO-360-B1B, AEIO-360-B1D and 171 more. Effective Jun 22, 2006
- [AD 2006-06-16](https://openairdocs.org/ad/2006-06-16): Crankshaft · Lycoming Engines AEIO-360-A1B6, AEIO-360-A1E6, IO-360-A1B6 and 18 more. Effective Apr 27, 2006
- [AD 2005-19-11](https://openairdocs.org/ad/2005-19-11): Crankshafts · Lycoming Engines AEIO-360-A1B6, AEIO-360-A1E6, AEIO-540-D4A5 and 59 more. Effective Oct 21, 2005
- [AD 2004-10-14](https://openairdocs.org/ad/2004-10-14): Crankshaft gear · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 642 more. Effective Jun 25, 2004
- [AD 2002-12-07](https://openairdocs.org/ad/2002-12-07): Oil Filter Converter Plate Gasket or the Converter Plate Kit · Lycoming Engines HIO-360-E1AD, HIO-360-E1BD, HIO-360-F1AD and 95 more. Effective Jul 3, 2002
- [AD 98-17-11](https://openairdocs.org/ad/98-17-11): Crankshafts · Continental Motors A-65-3, A-65-8, A75-8 and 90 more. Effective Oct 19, 1998
- [AD 98-02-08](https://openairdocs.org/ad/98-02-08): Crankshaft · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 216 more. Effective Mar 30, 1998
- [AD 97-15-11](https://openairdocs.org/ad/97-15-11): Cylinder kits · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 538 more. Effective Aug 12, 1997
- [AD 96-09-10](https://openairdocs.org/ad/96-09-10): Oil pump · Lycoming Engines AEIO-320-E1A, AEIO-320-E1B, AEIO-320-E2A and 334 more. Effective Jul 15, 1996
- [AD 95-26-02](https://openairdocs.org/ad/95-26-02): Aviation Gasoline · Lycoming Engines IO-320-B1A, IO-320-B1B, IO-320-B1C and 182 more. Effective Jan 24, 1996
- [AD 95-07-01](https://openairdocs.org/ad/95-07-01): Connecting Rod Bolt · Lycoming Engines AEIO-360-A1E, AEIO-360-B1G6, AEIO-360-H1A and 177 more. Effective Apr 12, 1995
- [AD 92-12-05](https://openairdocs.org/ad/92-12-05): Piston Pins · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 532 more. Effective Jul 10, 1992
- [AD 90-04-06 R1](https://openairdocs.org/ad/90-04-06-R1): Propeller Governor External Oil Line · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 427 more. Effective May 28, 1991
- [AD 87-10-06 R1](https://openairdocs.org/ad/87-10-06-R1): Rocker Arm Assembly · Lycoming Engines IO-360-B4, IVO-360-A1A, O-340-A1A and 243 more. Effective Sep 1, 1989
- [AD 89-04-02](https://openairdocs.org/ad/89-04-02): Carburetors · Continental Motors O-470-11, O-470-11-CI, O-470-11B and 175 more. Effective Mar 8, 1989
- [AD 80-04-03 R2](https://openairdocs.org/ad/80-04-03-R2): Hydraulic Lifter · Lycoming Engines LO-360-E1A6D, LTO-360-E1A6D, O-320-H1AD and 7 more. Effective Apr 25, 1988
- [AD 81-16-05](https://openairdocs.org/ad/81-16-05): Magnetos · Lycoming Engines AEIO-320-E1B, AEIO-320-E2B, AEIO-360-B1G6 and 234 more. Effective Aug 6, 1981
- [AD 80-14-07](https://openairdocs.org/ad/80-14-07): Upper Exhaust Valve Spring Seats · Lycoming Engines LO-360-E1A6D, O-320-H1AD, O-320-H1BD and 5 more. Effective Jul 7, 1980
- [AD 79-10-03 R2](https://openairdocs.org/ad/79-10-03-R2): Engine Mounting Bracket Attaching Bolts · Lycoming Engines LO-360-E1A6D, O-320-H2AD and O-360-E1A6D. Effective Jul 1, 1980
- [AD 80-06-05](https://openairdocs.org/ad/80-06-05): Magnetos · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 254 more. Effective Mar 28, 1980
- [AD 79-15-02](https://openairdocs.org/ad/79-15-02): Channel Plug In Carburetor · Lycoming Engines LO-360-A1G6D and O-360-A1G6D. Effective Jul 20, 1979
- [AD 75-08-09](https://openairdocs.org/ad/75-08-09): Oil Pump Drive Shaft · Lycoming Engines AEIO-360-A1B, AEIO-360-A1B6, AEIO-360-A1C and 365 more. Effective Aug 18, 1977
- [AD 73-23-01](https://openairdocs.org/ad/73-23-01): Piston Pin Assembly · Lycoming Engines AIO-360-A1A, AIO-360-A1B, AIO-360-A2A and 215 more. Effective Jan 13, 1977
- [AD 69-24-03](https://openairdocs.org/ad/69-24-03): Carburetors · Continental Motors A-65-1, A-65-12, A-65-12F and 321 more. Effective Nov 29, 1969
- [AD 66-06-03](https://openairdocs.org/ad/66-06-03): Connecting Rod Assemblies · Lycoming Engines GO-435-C2 (O-435-17), GO-435-C2A, GO-435-C2A2 and 317 more. Effective Jan 16, 1969
- [AD 67-01-04](https://openairdocs.org/ad/67-01-04): Oil Filters · Full flow oil filter (Superior Flow STC SA401SW or 2 others). Effective Jan 2, 1967
- [AD 66-20-04](https://openairdocs.org/ad/66-20-04): Oil Filter Adapter Gasket · Lycoming Engines IO-320-A1A, IO-320-A2A, IO-320-B1A and 121 more. Effective Aug 27, 1966
- [AD 64-16-05](https://openairdocs.org/ad/64-16-05): AC Pumps · Lycoming Engines HIO-360-B1A, HIO-360-B1B, IO-320-B1A and 86 more. Effective Jul 10, 1964
- [AD 63-22-03](https://openairdocs.org/ad/63-22-03): Carburetors · Continental Motors GO-300-A, GO-300-B, GO-300-C and 143 more. Effective Dec 2, 1963
- [AD 59-10-07](https://openairdocs.org/ad/59-10-07): Cylinder Baffle Clamps · Lycoming Engines GO-480-A1A, GO-480-B, GO-480-B1A6 and 58 more

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

- [AD 2024-21-02](https://openairdocs.org/ad/2024-21-02) (historical): Engine (Reciprocating) · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 548 more. Effective Dec 5, 2024
- [AD 2008-19-05](https://openairdocs.org/ad/2008-19-05) (historical): Parallel Valve'' reciprocating engines · Engine Components Reciprocating Engine Cylinder Assemblies, AEIO-320-D1B, AEIO-320-D2B and 262 more. Effective Oct 20, 2008
- [AD 2006-20-09](https://openairdocs.org/ad/2006-20-09) (historical): Certain crankshafts replacing · Lycoming Engines AEIO-360-A1B6, AEIO-360-A1E6, AEIO-540-D4A5 and 82 more. Effective Nov 3, 2006
- [AD 2005-26-10](https://openairdocs.org/ad/2005-26-10) (historical): ECi cylinder assemblies. · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 413 more. Effective Jan 31, 2006
- [AD 81-18-04 R2](https://openairdocs.org/ad/81-18-04-R2) (historical): Engine Oil Pump Driven Impeller and Shaft · Textron Lycoming, AVCO AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 376 more. Effective Jun 7, 1982

## Information bulletins (advisory) (9 in force)

- [SAIB NE-06-31R6](https://openairdocs.org/saib/NE-06-31R6): Engine Lubricating Oils. Issued Sep 26, 2022
- [SAIB NE-19-08](https://openairdocs.org/saib/NE-19-08): Reciprocating Engine Cylinder Section - Lycoming Engines Parallel Valve Cylinders. Issued May 2, 2019
- [SAIB NE-08-32R1](https://openairdocs.org/saib/NE-08-32R1): Propeller Governor  Idler Gear Shaft Set Screw. Issued May 13, 2016
- [SAIB NE-14-13](https://openairdocs.org/saib/NE-14-13): Reciprocating Engine - Cylinder Mounting Studs. Issued Mar 24, 2014
- [SAIB NE-13-06](https://openairdocs.org/saib/NE-13-06): Pushrod Shroud Spring Retainers, Engine Components Part No. AEL14995, for Lycoming Engines 320, 360, and 540 Series Engines. Issued Nov 21, 2012
- [SAIB NE-08-26R3](https://openairdocs.org/saib/NE-08-26R3): Magneto/Distributor. Issued Mar 31, 2011
- [SAIB NE-06-32R1](https://openairdocs.org/saib/NE-06-32R1): Reciprocating Engine - Crankshaft. Issued Sep 10, 2008
- [SAIB NE-03-18](https://openairdocs.org/saib/NE-03-18): . Issued Jan 22, 2003
- [SAIB NE-00-22](https://openairdocs.org/saib/NE-00-22): . Issued May 23, 2000
- [SAIB NE-06-31R5](https://openairdocs.org/saib/NE-06-31R5) (historical): Engine Lubricating Oils. Issued Oct 19, 2011
- [SAIB NE-06-31R4](https://openairdocs.org/saib/NE-06-31R4) (historical): Engine Lubricating Oils. Issued Jul 6, 2011
- [SAIB NE-06-31R3](https://openairdocs.org/saib/NE-06-31R3) (historical): Engine Lubricating Oils. Issued Jul 22, 2009
- [SAIB NE-06-31R2](https://openairdocs.org/saib/NE-06-31R2) (historical): Engine Lubricating Oils. Issued Apr 29, 2009
- [SAIB NE-08-26R1](https://openairdocs.org/saib/NE-08-26R1) (historical): Dual Magnetos. Issued Jul 8, 2008
- [SAIB NE-08-32](https://openairdocs.org/saib/NE-08-32) (historical): Propeller Governor Set Screw. Issued Jul 3, 2008
- [SAIB NE-06-31R1](https://openairdocs.org/saib/NE-06-31R1) (historical): . Issued Apr 18, 2006
- [SAIB NE-06-31](https://openairdocs.org/saib/NE-06-31) (historical): . Issued Feb 27, 2006

## NTSB investigations

None matched to N806FT.

## NTSB investigations on N806FT not matched to an aircraft (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB DCA84RA002](https://openairdocs.org/ntsb/DCA84RA002), Oct 11, 1983: Boeing 747-200F (N806FT), Frankfort, Germany

## FAA accident and incident reports

None matched to N806FT.

## Reports on N806FT not matched to an aircraft (2)

They name N806FT, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 19880624069519I](https://openairdocs.org/incident/19880624069519I), Jun 24, 1988: Boeing 747200F (N806FT), Los Angeles, CA. Lost nosewheel steering power. Used more power to negotiate a turn. Blew over a taxiway sign. Sign landed on runway
- [Accident 19831011075659A](https://openairdocs.org/incident/19831011075659A), Oct 11, 1983: Boeing 747* (N806FT), Frankfurt, GE, Substantial damage. Loaded pallet shifted rearward on takeoff roll. Aircraft nosed up. Flight was aborted off runway. Locks not secured

## 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 N806FT not matched to an aircraft (56, newest 50)

They name N806FT, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR P5CA0200698](https://openairdocs.org/sdr/P5CA0200698), Aug 28, 2002: GEARBOX. FAILED. SHORTLY AFTER T/O, #1 ENG. LOW OIL PRESSURE LIGHT ILLUMINATED. OIL PRESSURE DROPPED TO 10psi & WAS STEADY; OIL QTY SHOWED FULL & WAS STEADY. PERFORMED LOSS OF O
- [SDR P5CA0200686](https://openairdocs.org/sdr/P5CA0200686), Jun 30, 2002: AUTOPILOT SYS. MALFUNCTIONED. B-AUTOPILOT WILL NOT ACCEPT STEERING COMMANDS IN HDG OR INS MODE. ALSO INOP IN MANUAL. TRANSFERRED TO DEFERRED MX ITEM.
- [SDR P5CA0200685](https://openairdocs.org/sdr/P5CA0200685), Jun 30, 2002: WIRE. BROKEN. "A" AUTOPILOT WILL NOT ACCEPT STEERING COMMANDS IN HDG OR INS MODES. ALSO INOP IN MANUAL. TRANSFERRED TO DEFERRED MX ITEM ID #036042 CTR #29299 IAW MEL 02-22-2-
- [SDR P5CA0200690](https://openairdocs.org/sdr/P5CA0200690), Jun 29, 2002: ACOUSTIC PANEL. DAMAGED. APU EXHAUST ACOUSTIC LINER DAMAGED AT 01:30 O'CLOCK POSITION. APU LINER REMOVED & REPLACED IAW MM 49-81-02.
- [SDR P5CA0200689](https://openairdocs.org/sdr/P5CA0200689), Jun 29, 2002: SHROUD. CRACKED. CRACKS FOUND ON NR 1 ENG TURBINE COOLING SHROUD AT 8 & 2 O'CLOCK POSITIONS. RT (2 CRACKS) NR 1 IS 5 INCHES LONG & NR 2 IS 2 INCHES LONG. LT (4 CRACKS) NR 1 IS 3
- [SDR P5CA0200688](https://openairdocs.org/sdr/P5CA0200688), Jun 29, 2002: PANEL. CRACKED. CRACK 15" LONG FOUND RH WING UPPER SKIN LE FIXED PANEL AT WS 834 TO WS 862. PANEL SHOWS 15 X 30 IN. SQ AREA DELAMINATED. LEADING EDGE FIXED PANEL AT WS 834 TO W
- [SDR P5CA0200687](https://openairdocs.org/sdr/P5CA0200687), Jun 27, 2002: DOOR. CRACKED. A 2 INCH LONG CRACK FOUND ON APU INLET DOOR OUTSIDE LOWER FORWARD CORNER. COMPOSITE REPAIR CARRIED OUT WITH REF TO SRM 51-40-06. AREA PROTECTED WITH REF TO SRM 
- [SDR P5CA0200651](https://openairdocs.org/sdr/P5CA0200651), Feb 20, 2002: FLAP TRACK. CORRODED. FOUND LIGHT CORROSION, AREA 600, ON UPPER FLAP TRACKS AND CENTER TOGGLE ROLLERS ON NR 5, 6, 7 & 8 FLAP TRACKS. REMOVED CORROSION AND RETREATED IAW MM 27-51-22 &
- [SDR P5CA0200650](https://openairdocs.org/sdr/P5CA0200650), Feb 20, 2002: FLAP TRACK. CORRODED. LEVEL 1 CORROSION: FOUND LIGHT CORROSION, AREA 500, ON UPPER FLAP TRACKS AND CENTER TOGGLE ROLLERS ON NR 1, 2, 3 & 4 FLAP TRACKS. REMOVED CORROSION AND RETREATE
- [SDR P5CA0200649](https://openairdocs.org/sdr/P5CA0200649), Feb 20, 2002: BOLT. WORN. WORN LT WING BODY GEAR, AREA 751; SUPPORT ROD BOLT WORN. REMOVED BOLTS/BUSHINGS AND CLEANED UP. REASSEMBLED IAW MM 32-13-00 WITH LUBRICATION AND NEW WASHERS INS
- [SDR P5CA0200629](https://openairdocs.org/sdr/P5CA0200629), Jan 11, 2002: WIRE. BROKEN. RT BODY GEAR LEFT REAR (NR 11) ANTI-SKID LIGHT CAME ON AND WOULD NOT RESET. WHEEL ASSY RETORQUED FOR PRECAUTION PER MM 32-45-01. NR 11 BRAKE DEACTIVATED PER MEL
- [SDR P5CA0100613](https://openairdocs.org/sdr/P5CA0100613), Nov 18, 2001: FAIRING. DAMAGED. L/H HORIZONTAL STABILIZER STA 560 OUTBOARD TIP - AFT WEDGE 6" SECTION BROKEN OFF. REMOVED & REPLACED T/E & BOTTOM ACCESS PANELS PER SRM 51-10-01.
- [SDR P5CA0100606](https://openairdocs.org/sdr/P5CA0100606), Oct 31, 2001: WEB. CRACKED. NOSE GEAR WHEEL WELL FRAME WEB CRACKED, APPROX. 1/8" LONG, BY INSULATION HOLES FIRST & FOUR FROM FLOOR CHORD ANGLE ON RIGHT SIDE. OPENED HOLES TO 7/16", RE-INSP
- [SDR P5CA0100569](https://openairdocs.org/sdr/P5CA0100569), Jun 12, 2001: SLIDE. DEFECTIVE. RT UPPER DECK SLIDE BLOWN BY MAINTENANCE AND ONLY HALF INFLATED. REPLACED U/D RIGHT SLIDE ASSIST BOTTLE. REMOVED AND REPLACED U/D RIGHT SLIDE FOUND SHEARED CABL
- [SDR P5CA0100466](https://openairdocs.org/sdr/P5CA0100466), Feb 25, 2001: FIRE WARNING. ACTIVATED. NR 2 ENG FIRE DET LIGHT AND FAULT LIGHT CAME ON A-LOOP WITH A FIRE WARNING. ENGINE SHUT DOWN AND BOTTLE FIRED. REPLACED NR 2 LFT FIRE BOTTLE. P/N ON 33603903P, 
- [SDR P5CA0000344](https://openairdocs.org/sdr/P5CA0000344), Oct 17, 2000: SKIN. CORRODED. LEVEL 1 CORROSION FOUND RT WING I/B MID FLAP TOP SKIN PANELS FOUND WITH CORROSION IN SEVERAL PLACES ON THE UPPER T-CHORD. CORRODED TJ-CHORD REPLACED PER SRM 51-
- [SDR P5CA0000343](https://openairdocs.org/sdr/P5CA0000343), Oct 17, 2000: FRAME. CRACKED. CRACK FOUND ON FRAME 320 RHS AT WINDOW POST INTERSECTION, DURING COCKPIT WINDOW INSPECTION. FRAME 320 RHS TEE CHORD REPAIR C/OUT PER SRM 51-40-04.
- [SDR P5CA0000342](https://openairdocs.org/sdr/P5CA0000342), Oct 17, 2000: FRAME. CRACKED. CRACK FOUND ON FRAME 320 RHS AT COCKPIT WEB. WEB REPAIR C/OUT PER SRM 51-40-02.
- [SDR P5CA0000341](https://openairdocs.org/sdr/P5CA0000341), Oct 17, 2000: SKIN. DAMAGED. DAMAGE FOUND ON FUSELAGE SKIN NOT SMOOTH AT BS 1826 TO BS 1837 BETWEEN 542L AND 543L. PAINT REMOVED NDT INSPECTED AND NO CRACKS NOTED, AREA RESTORED PER SRM 51-
- [SDR P5CA0000340](https://openairdocs.org/sdr/P5CA0000340), Oct 17, 2000: PANEL. CRACKED. CRACK FOUND AT BS 1241 CANTED BULKHEAD CLOSEOUT PANELS (LHS 2.5 AT O/B LOWER CORNER, RHS 5.0 AT O/B EDGE FASTENERS). BS 1241 LT & RT CANTED BULKHEAD CLOSEOUT PA
- [SDR P5CA0000339](https://openairdocs.org/sdr/P5CA0000339), Oct 17, 2000: BOLT. BROKEN. OUTBOARD T/E AFT FLAP ATTACHMENT FITTING TO MID FLAP MOUNTING BOLTS FOUND SHEARED DURING NISPECTION. ATTACH FITTING MOUNTING BOLTS REPLACED PER MM 27-51-04.
- [SDR P5CA0000338](https://openairdocs.org/sdr/P5CA0000338), Oct 17, 2000: BOLT. BROKEN. NR 2 SEQUENCE CARRIAGE ASSY HOOK BOLT FOUND SHEARED DURING INSPECTION. BOTH HOOK BOLTS REPLACED PER MM 27-51-30.
- [SDR P5CA0000337](https://openairdocs.org/sdr/P5CA0000337), Oct 17, 2000: HOOK. LOOSE. ABNORMALITY FOUND ON RT WING NR 7 POSITION SEQUENCE CARRIAGE HOOK ASSY FOUND LOOSE. REPLACE WITH NEW TOGGLE SEQUENCE ASSY P/N 65B17198-10, INSTALLED PER MM 27-5
- [SDR P5CA0000345](https://openairdocs.org/sdr/P5CA0000345), Oct 16, 2000: SKIN. CORRODED. LEVEL 1 CORROSION FOUND ON UPPER SURFACE OF UPPER SKIN PANEL OF WING CTR TANK JUST FWD OF BS 140 BETWEEN RBL 2 AND RBL 9. CORROSION BLENDED OUT AND REPAIRED PER
- [SDR P5CA0000334](https://openairdocs.org/sdr/P5CA0000334), Oct 13, 2000: INTERCOSTAL. CRACKED. CRACK FOUND ON MAIN DECK STA 997 INTERCOSTAL AT RBL 75 FOUND ALONG FASTENER HOLE. MAIN DECK STA 997 INTERCOSTAL REPAIR C/OUT PER SRM 51-40-03.
- [SDR P5CA0000333](https://openairdocs.org/sdr/P5CA0000333), Oct 13, 2000: ROD. DAMAGED. DAMAGE FOUND L/E SUPPORT ROD ASSY FOR RIB AT WING STA 878.55 FOUND CHAFED THRU. SUPPORT ROD ASSY REPLACED PER SRM 51-30-04.
- [SDR P5CA0000332](https://openairdocs.org/sdr/P5CA0000332), Oct 13, 2000: DRAIN VALVE. CRACKED. CRACK FOUND ON 13 OFF DRAIN VALVE ASSY AT BELLY FUSELAGE BS 2160 TO BS 2180. ALL 13 DRAIN VALVE ASSY REPLACED PER MM 51-41-03.
- [SDR P5CA0000331](https://openairdocs.org/sdr/P5CA0000331), Oct 13, 2000: FITTING. DAMAGED. ABNORMALITY FOUND ON RT WING I/B FOREFLAP O/B SEQ CARRIAGE ATTACHMENT FITTING BEARING FOUND MIGRATED. NEW FITTING P/N 65B39025-34 INSTALLED PER MM 27-51-02.
- [SDR P5CA0000330](https://openairdocs.org/sdr/P5CA0000330), Oct 13, 2000: BEAM. CRACKED. CRACK FOUND ON NOSE WHEEL WELL VERTICAL BEAM WEB AT STA 320 LHS, FOUND 2 CRACKS APPROX .75 & .1875 INCH LENGTH NDT REPORT POLAR/4284/00 REFERS. STA 320 LHS VERT
- [SDR P5CA0000329](https://openairdocs.org/sdr/P5CA0000329), Oct 13, 2000: STRUCTURE. CORRODED. LEVEL 1 CORROSION FOUND ON VERTICAL FIN 4TH BALANCE WEIGHT (COUNTING FROM TOP TO BOTTOM). CORROSION TREATMENT PER CPM PART 1, 20-40-00 P.24 C/OUT WEIGHT REINSTA
- [SDR 20000919SH015](https://openairdocs.org/sdr/20000919SH015), Aug 26, 2000: DUCT. BROKEN. NR 3 ENGINE FIRE WARNING ON TAKEOFF. BOTTLE DISCHARGED. ENGINE SHUT DOWN. AIRCRAFT RETURNED TO AKL. FOUND BROKEN 8TH STAGE ANTI-ICE DUCT THROTTLE CABLE MELTED A
- [SDR P5CA0000335](https://openairdocs.org/sdr/P5CA0000335), Jul 24, 2000: PANEL. CRACKED. CRACK FOUND AT BS 1240 RBL 5.0 CLOSURE PANEL AT CANTED BULKHEAD COMMON TO APU FUEL FEED LINE/SHROUD FOUND CRACKED AROUND FASTENER LOCATION. CLOSURE PANEL REMOVE
- [SDR P5CA9900633](https://openairdocs.org/sdr/P5CA9900633), Jun 29, 1999: WEB. CRACKED. FOUND WEB CRACKED AT BS 434L NR 1 MED. TRIMMED AREA AND FABRICATED PART FOR REPAIR PER SRM 53-10-04 AND 51-30-02.
- [SDR P5CA9900632](https://openairdocs.org/sdr/P5CA9900632), Jun 29, 1999: ANGLE. CRACKED. FOUND 1.6 INCH CRACK ON RADIUS OF ANGLE FWD OF BS 434 UNDER STR 26. FABRICATED PARTS AND REPLACED PER SRM 51-30-02.
- [SDR P5CA9900631](https://openairdocs.org/sdr/P5CA9900631), Jun 29, 1999: VERTICAL BEAM. CRACKED. FOUND INDICATION OF CRACKS AT HOLE ON VERTICAL BEAM AT BS 30L. STOP DRILLED AND FABRICATED REPAIR PER SRM 53-10-04 FIG 94 PG 8 DETAIL 5.
- [SDR P5CA9900630](https://openairdocs.org/sdr/P5CA9900630), Jun 29, 1999: BULKHEAD. CRACKED. CRACKS FOUND ON BS 1000 IN THE RADIUS BETWEEN STR 46 AND 47 LEFT AND RIGHT SIDES. STOP DRILLED, EDDY CURRENT PER SB 530-2316R1 AND SRM 51-10-01 FIG 2.
- [SDR P5CA9900629](https://openairdocs.org/sdr/P5CA9900629), Jun 29, 1999: BULKHEAD FLANGE. CRACKED. FOUND CRACK ON FLANGE OF PRESSURE BULKHEAD AT BS 140 WL 280 BL 10L. TRIMMED DAMAGED AREA AND FABRICATED NEW ANGLE PER SRM 51-40-03 AND 51-10-02.
- [SDR P5CA9900628](https://openairdocs.org/sdr/P5CA9900628), Jun 29, 1999: CLIPS. CRACKED. FOUND CRACKS ON CLIPS AT NOSE WHEEL WELL VERTICAL BEAM WEB AT BS 340 R. REPLACED CLIPS PER SRM 51-30-02.
- [SDR P5CA9900627](https://openairdocs.org/sdr/P5CA9900627), Jun 29, 1999: FLOORBEAM. DAMAGED. FOUND SHEARED RIVETS AT BS 400 ON FLOORBEAM LEFT SIDE. REPLACED RIVETS PER SRM 51-30-02.
- [SDR P5CA9900423](https://openairdocs.org/sdr/P5CA9900423), Mar 10, 1999: SKIN. DAMAGED. DURING CLOSING LOWER FWD CARGO DOOR, AEROGROUND HIGH LOADER HIT DOOR AND CAUSED DAMAGE TO LOWER AFT CORNER. REWORKED LOWER CORNER OF FWD CARGO DOOR PER SRM 51-1
- [SDR P5CA9900192](https://openairdocs.org/sdr/P5CA9900192), Feb 19, 1999: ANGLE. CRACKED. AFT PIT STAT 1726 BL 30L ANGLE FOUND CRACKED JUST BELOW TRACK. REMOVED AND FABRICATED NEW ANGLE AND INSTALLED PER SRM 51-10-01, 51-10-03 AND 51-30-02.
- [SDR P5CA9900191](https://openairdocs.org/sdr/P5CA9900191), Feb 15, 1999: KEEL BEAM. CORRODED. LEVEL 1 CORROSION FOUND ON KEEL BEAM AFT END LEFT AND RIGHT SIDE BS 1100 TO 1300. REMOVED CORROSION, TREATED AND PRIMED PER SRM 53-10-01 AND 53-10-02.
- [SDR P5CA9801614](https://openairdocs.org/sdr/P5CA9801614), Dec 4, 1998: FAIRING. DELAMINATED. NR 8 FIXED FAIRING TAIL CONE LOWER SKIN FOUND DELAMINATED. SANDED DOWN DELAMINATION AREA AND REPARIED PER SRM 51-40-09.
- [SDR P5CA9801221](https://openairdocs.org/sdr/P5CA9801221), Aug 3, 1998: PANEL. CRACKED. RIGHT WING GEAR FLYING DOOR PANEL CRACKED. REPAIRED PANEL IAW 747 SRM 51-40-09.
- [SDR P5CA9801216](https://openairdocs.org/sdr/P5CA9801216), Aug 3, 1998: PANEL. DELAMINATED. RIGHT WING UPPER SURFACE OF FLYING PANEL HAS A 2X2 AREA OF DELAMINATION AT TITANIUM COFFIN DOUBLER. REMOVED AND REPLACED RIGHT HAND WING FLYING PANEL IAW SRM 57
- [SDR P5CA9801219](https://openairdocs.org/sdr/P5CA9801219), Aug 2, 1998: FLOOR. DELAMINATED. LEVEL 1 CORROSION ON FLOOR PANEL UNDER LT UPPER DECK SLIDE CARRIAGE DELAMINATED AND MINOR CORROSION. FOUND MINOR SURFACE CORROSION, REMOVED IAW SRM 51-10-06 AND
- [SDR P5CA9801223](https://openairdocs.org/sdr/P5CA9801223), Aug 1, 1998: SUPPORT. DAMAGED. FWD LOWER CARGO COMPARTMENT STA 860 CENTER GUIDE FLOOR SUPPORT DAMAGED. REMOVED DAMAGED FLOOR SUPPORT AND WEB REINSTALLED PERMANENT REPAIR IAW SRM 51-40-02.
- [SDR P5CA9801217](https://openairdocs.org/sdr/P5CA9801217), Aug 1, 1998: SKIN. CORRODED. LEVEL 1 CORROSION UNDER THE ATC ANTENNAS. REMOVED CORROSION FROM UNDER A/C ATC ANTENNAS WITH MINIMAL MATERIAL LOSS IAW SRM 51-10-01.
- [SDR P5CA9801220](https://openairdocs.org/sdr/P5CA9801220), Jul 31, 1998: ANTENNA. CORROSION. LEVEL 1 CORROSION ON THE NR 1 AND NR 2 ANTENNA BODY. REPLACED NR 1 AND NR 2 ATC ANTENNAS IAW MM 34-53-03.
- [SDR P5CA9801218](https://openairdocs.org/sdr/P5CA9801218), Jul 31, 1998: EXHAUST SLEEVE. DELAMINATED. NR 4 ENGINE EXHAUST SLEEVE INNER SKIN DELAMINATED AT 6 O'CLOCK POSITION. REMOVED AND REPLACED NR 4 ENG EXHAUST SLEEVE ASSY IAW MM 78-11-02.

All 56: https://openairdocs.org/aircraft/N806FT/unmatched-reports.md

## STCs that may be installed (OpenAirDocs) (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 engine (Lycoming O&VO-360 series)

- [STC SE04651CH](https://openairdocs.org/stc/SE04651CH): To allow use of l00R grade aviation fuel meeting Swift Fuel, LLC specification SPEC-l00R-22. Swift Fuels LLC. Lists O-360-A1A
- [STC SE00825WI](https://openairdocs.org/stc/SE00825WI): Installation of Specialty Products Spin-on oil filter on Lycoming Engines. B & C Specialty Products Inc. Lists O-360-A1A
- [STC SE208SO](https://openairdocs.org/stc/SE208SO): Installation of ice indicator in the carburetor. LegacySTC.com
- [STC SE04349CH](https://openairdocs.org/stc/SE04349CH): Installation of SureFly electronic ignition. SureFly Partners Ltd. Lists O-360-A1A
- [STC SE01954SE](https://openairdocs.org/stc/SE01954SE): Installation of engine crankcase seal. Ly-Con Rebuilding Company. Lists O-360-A1A
- [STC SE02352CH](https://openairdocs.org/stc/SE02352CH): Installation of Challenger cleanable oil filter assembly. Challenger Aviation Products Inc. Lists O-360-A1A
- [STC SE00939WI](https://openairdocs.org/stc/SE00939WI): Installation of B&C Specialty Products Model BC 315-( ) Starter on Lycoming engines. B & C Specialty Products Inc. Lists O-360-A1A
- [STC SE2390CE](https://openairdocs.org/stc/SE2390CE): Installation of B & C Speciality Products. B & C Specialty Products Inc
- [STC SE03232CH](https://openairdocs.org/stc/SE03232CH): Installation of Engine Preheat Kit p/n TA2925-1 for 115 volt application. Hartzell Propeller Inc. Lists O-360-A1A
- [STC SE154SO](https://openairdocs.org/stc/SE154SO): Installation of one Roto-Master Turbocharger P/N's 600573-00 (RJ0326-1, RJ0326) or 600576-00 (RJ0326-2, RJ0325. TALCO Aviation. Lists O-360-A1A
- [STC SE04577CH](https://openairdocs.org/stc/SE04577CH): Install an electronic engine ignition system. Electroair Acquisition Corp. Lists O-360-A1A
- [STC SE01966WI](https://openairdocs.org/stc/SE01966WI): Use of GAMI G100UL High Octane Unleaded Avgas in spark ignition piston aircraft engines. General Aviation Modifications Inc. Lists O-360-A1A
- [STC SE4408SW](https://openairdocs.org/stc/SE4408SW): Miscellaneous engine cylinder replacement parts. Continental Motors, Inc
- [STC SE8776SW](https://openairdocs.org/stc/SE8776SW): Installation of coated cylinders and piston rings. Continental Motors, Inc
- [STC SE00218NY](https://openairdocs.org/stc/SE00218NY): Replacement of Lycoming starter with SKY-TEC 12 volt starter installed. Hartzell Engine Technologies, LLC
- [STC SE00226NY](https://openairdocs.org/stc/SE00226NY): Replacement of Lycoming starter with SKY-TEC 24-volt starter Models 149-24HT and 122-24HT. Approval limited to 24-volt DC source available to the starter. Hartzell Engine Technologies, LLC. Lists O-360-A1A
- [STC SE00357NY](https://openairdocs.org/stc/SE00357NY): Replacement of Lycoming starter with SKY-TEC 24-volt starter installed. Hartzell Engine Technologies, LLC
- [STC SE03495NY](https://openairdocs.org/stc/SE03495NY): Installation of an electronic ignition system, an air conditioning compressor, and an oil filter adapter. Helicopteres Guimbal S.A. Lists O-360-J2A
- [STC SE2901NM](https://openairdocs.org/stc/SE2901NM): Lycoming valve cover gasket. Real Gaskets Tennessee. Lists O-360-A1A
- [STC SE02291AT](https://openairdocs.org/stc/SE02291AT): Conversion of the engine from a carburetor fuel system and magneto ignition system to a full authority digital electronic control (FADEC) system for fuel injection and ignition. Continental Motors, Inc. Lists O-360-A1A
- [STC SE01524CH](https://openairdocs.org/stc/SE01524CH): Replace Slick 6000, 6100, 6200, 6300, 4000, 4100, 4200, and 4300 series magnetos and TCM/Bendix S6-20, S6-200, S6-1200, S-20, S-200, and S-1200 series magnetos with Champion Limited Authority Spark Advance Regulator (LASAR ) Model 4755 and 6755 bush kit ignition systems. Champion Aerospace LLC. Lists O-360-A1A
- [STC SE1017GL](https://openairdocs.org/stc/SE1017GL): Removal of the Type certificated Bendix magnetos and ignition harnesses followed by the installation of Slick magneto Models 4250 and 4251 with Slick ignition harnesses. Champion Aerospace LLC. Lists O-360-A1A
- [STC SE524CH](https://openairdocs.org/stc/SE524CH): Replace Slick 4000, 4100, 4200, and 4300 series magnetos and TCM/Bendix S-20, S-200, and S-1200 series magnetos with the Champion Limited Authority Spark Advance Regulator (LASAR ). Champion Aerospace LLC. Lists O-360-A1A
- [STC SE8193SW](https://openairdocs.org/stc/SE8193SW): Grind nitriden high compression cylinder barrles to plus .010 oversize and install SL75089 P10 piston, SL74242 P10 compression ring, and SL73857 P10 oil ring. Superior Air Parts Inc. Lists O-360-A1A
- [STC SE927GL](https://openairdocs.org/stc/SE927GL): Installation of a Shadin Co. fuel flow transducer. Shadin Avionics. Lists O-360-A1A
- [STC SE02285AT](https://openairdocs.org/stc/SE02285AT): Data pertaining to this modification are considered to be inadequate for duplication in other engines. This modification is applicable to Lycoming engine Serial Number L-31403-36A only. Glidden Dennis C. Lists O-360-C1E
- [STC SE1779NM](https://openairdocs.org/stc/SE1779NM): Installation of Precise Flight, Inc. Standby Vacuum System SVS III. Precise Flight Inc. Lists O-360-A1A
- [STC SE5743NM](https://openairdocs.org/stc/SE5743NM): Intallation of adapter for externally mounted oil filter. Aviation Development Corporation. Lists O-360-A1A
- [STC SE00889LA](https://openairdocs.org/stc/SE00889LA): Installation of Nickson's cylinder barrels on Lycoming reciprocating engine models. Nickson's Machine Shop Inc. Lists O-360-A1A
- [STC SE2563CE](https://openairdocs.org/stc/SE2563CE): Leaded and unleaded automotive gasoline, 91 minimum antiknock index (RON+MON) /2 per ASTM spec D-439. Intermixing with aviation gasoline also approved. Petersen Aviation Inc. Lists O-360-A1A
- [STC SE1-201](https://openairdocs.org/stc/SE1-201): Installation of the Richter Aero Equipment Type B-4 or B-5 Temperature Probe. (O-360 SERIES (excl. A1C, C2B, C2D)). MidContinent Instru Co Inc
- [STC SE09492SC](https://openairdocs.org/stc/SE09492SC): Installation and usage of Exxon 20W50 multigrade aircraft engine oil conforming to Exxon Oil formulation WS-3013. Exxon Company USA
- [STC SE00687CH](https://openairdocs.org/stc/SE00687CH): Modify by removing oil sump and vertical carburetor and installing a Facet model HA-6 carburetor(P/N 10-5045) and Lycoming oil sump (P/N 77159). (O-360-C1A 5632-36). Macy Roger F. Lists O-360-C1A
- [STC SE00350SE](https://openairdocs.org/stc/SE00350SE): Installation of sump mounted chip detector. Aviation Development Corporation. Lists O-360-A1A
- [STC SE8023SW](https://openairdocs.org/stc/SE8023SW): Installation and usage of AEROSHELL. Shell Development Co
- [STC SE702NE](https://openairdocs.org/stc/SE702NE): Modification of crankcase tappet bores to accommodate large tappets. Mattituck Airbase, Inc. Lists O-360-E1A6D
- [STC SE370NE](https://openairdocs.org/stc/SE370NE): Installation of 'Auto-Vac 2' auxiliary vacuum system. Raymond Ives. Lists O-360-A1A
- [STC SE5870SW](https://openairdocs.org/stc/SE5870SW): Installation of turbosupercharger. FliteCraft Turbo. Lists O-360-F1A6
- [STC SE738NE](https://openairdocs.org/stc/SE738NE): Installation of 'Auto-Vac-4' primary vacuum system. Raymond Ives. Lists O-360-A3A
- [STC SE2574CE](https://openairdocs.org/stc/SE2574CE): Add unleaded automotive gasoline87 minimum antiknock index and and leaded automotive gasoline, 88 minimum antiknock index (RON+ MON)/2 per ASTM Specification D-439. Petersen Aviation Inc. Lists O-360-B1A
- [STC SE4153NM](https://openairdocs.org/stc/SE4153NM): Installation of a Marvel Model MA-4-5 carburetor and associated parts. Big Bend Community College. Lists O-360-A4K
- [STC SE452NE](https://openairdocs.org/stc/SE452NE): Installation and usage of 'Mobil AV 1' aviation oil. Mobil Research & Development Corp
- [STC SE5879SW](https://openairdocs.org/stc/SE5879SW): Use of Phillips X/C II 20W-50 and25W-60 oil (OSS 55875) in all Avco reciprocating aircraft engines from 65 to 450 BHP. Phillips Petroleum Co
- [STC SE3309NM](https://openairdocs.org/stc/SE3309NM): Installation of Airesearch Model TA04 Turbosupercharger. Seaplane Flying Inc. Lists O-360-A4K
- [STC SE2574NM](https://openairdocs.org/stc/SE2574NM): Installation of updraft carburetor and associated induction system. Michael Parfit. Lists O-360-F1A6
- [STC SE5924SW](https://openairdocs.org/stc/SE5924SW): Installation of stainless steel replacement exhaust studs on AVCO engines. Perrigo & Steele Aircraft Engr Company
- [STC SE244NE](https://openairdocs.org/stc/SE244NE): Installation of Mattituck plasma flame sprayed cylinder barrels in Teledyne reciprocating engines. Mattituck Airbase, Inc
- [STC SE80NE](https://openairdocs.org/stc/SE80NE): Installation and usage of Bel-Ray synthetic aviation oil, Bel-Ray Aero 1, (nonsupercharged), horizontally opposed direct drive, aircraft engines of 350 hp. or less. Bel-Ray Company, Inc
- [STC SE128NE](https://openairdocs.org/stc/SE128NE): Use of AMS/OIL 15W 50 synthetic piston aircraft oil in Avco engines. AMS/OIL
- [STC SE2887SW](https://openairdocs.org/stc/SE2887SW): Install Bendix PS-5C carburetor. Swick Aircraft. Lists O-360-A1A

## Related

- Other Kaston Aloysius P THORP T-18 aircraft: https://openairdocs.org/model/kaston-aloysius-p-thorp-t-18/aircraft.md
- The Lycoming O&VO-360 series engine: https://openairdocs.org/engine/lycoming-o-vo-360-series.md

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