# N604TW: 2025 John T Stearman VANS ACFT RV-10

- Status: Valid registration
- Airframe: [John T Stearman VANS ACFT RV-10](https://openairdocs.org/model/john-t-stearman-vans-acft-rv-10) (registry code 05642Z0, 4 seats)
- Engine: [Lycoming IO-540-C4B5](https://openairdocs.org/engine/lycoming-io-540-c4b5) (registry code 41651)
- Data sheets: [TCDS 1E4](https://openairdocs.org/tcds/1E4) (Lycoming Engines) (OpenAirDocs)
- Serial number: 0002
- Year built: 2025
- Type: Fixed wing single engine
- Engine type: Reciprocating
- Kit: Vans Aircraft Inc RV-10
- Airworthiness: Experimental, amateur built
- Airworthiness date: March 28, 2025
- Certificate issued: March 19, 2025
- Expires: March 31, 2032
- Mode S code: A7D7D9
- Registered owner: [Chrysalide LLC](https://openairdocs.org/faa-owner/CHRYSALIDE%20LLC)
- Location: [Oklahoma City, OK](https://openairdocs.org/faa-place/OK/Oklahoma%20City)
- Owner type: LLC
- Owner's area on the map: 35.5467° N, 97.5646° W: Placed by OpenAirDocs at the center of ZIP code 73116, 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=604TW
- Page: https://openairdocs.org/aircraft/N604TW

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.

## ADs that may apply (OpenAirDocs): 35 in force

### Matched by airframe (John T Stearman VANS ACFT RV-10)

None in force.

### Matched by engine (Lycoming IO-540-C4B5)

- [AD 2026-17-10](https://openairdocs.org/ad/2026-17-10): Reciprocating Engine Cylinder Section · Lycoming Engines O-235, O-235-A, O-235-AP and 159 more. Effective Sep 14, 2026
- [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 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 2015-19-07](https://openairdocs.org/ad/2015-19-07): Fuel injector fuel lines · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1B and 187 more. Effective Nov 3, 2015
- [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 2012-03-06](https://openairdocs.org/ad/2012-03-06): Fuel servo diaphragm · Continental Motors 6-260-A, 6-285-A, 6-285-B and 482 more. Effective Feb 24, 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 2009-02-03](https://openairdocs.org/ad/2009-02-03): Fuel injection servos · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 261 more. Effective Feb 9, 2009
- [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 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 2005-12-06](https://openairdocs.org/ad/2005-12-06): Riveted-impulse coupling assemblies and snap-ring coupling assemblies · Lycoming Engines AEIO-540-D4A5, AEIO-540-D4B5, AEIO-540-D4C5 and 154 more. Effective Jul 19, 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 2004-05-24](https://openairdocs.org/ad/2004-05-24): Zinc-plated Crankshaft Gear Retaining Bolts · Lycoming Engines AEIO-540-D4A5, AEIO-540-D4B5, AEIO-540-D4C5 and 161 more. Effective Mar 30, 2004
- [AD 2003-14-03](https://openairdocs.org/ad/2003-14-03): Rotary fuel pumps · Lycoming Engines AEIO-540-D4A5, AEIO-540-D4B5, AEIO-540-D4C5 and 262 more. Effective Aug 14, 2003
- [AD 2002-19-03](https://openairdocs.org/ad/2002-19-03): Crankshaft · Lycoming Engines IO-540-A1A5, IO-540-AA1A5, IO-540-AA1B5 and 81 more. Effective Sep 20, 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 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 96-23-03](https://openairdocs.org/ad/96-23-03): High pressure fuel pumps · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 174 more. Effective Dec 23, 1996
- [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 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 79-04-05](https://openairdocs.org/ad/79-04-05): Regulator Diaphragm Stem Assembly · Lycoming Engines AEIO-320-D1B, AEIO-320-E1A, AEIO-320-E1B and 215 more. Effective Sep 26, 1979
- [AD 78-23-10](https://openairdocs.org/ad/78-23-10): Center Body Bellows Seal Assembly · Lycoming Engines AEIO-320-D1B, AEIO-320-E1A, AEIO-320-E1B and 218 more. Effective Nov 7, 1978
- [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 75-09-15](https://openairdocs.org/ad/75-09-15): Fuel Starvation To The Engine · Lycoming Engines AIO-320-A1A, AIO-320-A1B, AIO-320-A2A and 130 more. Effective Apr 30, 1975
- [AD 73-10-02](https://openairdocs.org/ad/73-10-02): Bendix Fuel Injectors · Bendix Fuel Injectors, AIO-320-A1A, AIO-320-A1B and 88 more. Effective May 16, 1973
- [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 67-22-06](https://openairdocs.org/ad/67-22-06): Fuel Injectors · Lycoming Engines HIO-360-A1A, HIO-360-B1A, HIO-360-B1B and 28 more. Effective Aug 9, 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

### 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 2011-26-04](https://openairdocs.org/ad/2011-26-04) (historical): Externally mounted fuel injector fuel lines · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1B and 186 more. Effective Jan 25, 2012
- [AD 2011-15-10](https://openairdocs.org/ad/2011-15-10) (historical): Fuel servos · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 256 more. Effective Aug 16, 2011
- [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 2008-14-07](https://openairdocs.org/ad/2008-14-07) (historical): Externally mounted fuel injector fuel lines · Textron Lycoming, AVCO AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1B and 185 more. Effective Aug 14, 2008
- [AD 2008-08-14](https://openairdocs.org/ad/2008-08-14) (historical): Fuel injection servo plugs · Superior Air Parts AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 242 more. Effective Apr 29, 2008
- [AD 2008-06-51](https://openairdocs.org/ad/2008-06-51) (historical): Fuel injection servo plugs · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 235 more
- [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 2002-26-01](https://openairdocs.org/ad/2002-26-01) (historical): Fuel injector fuel lines · Textron Lycoming, AVCO IGO-480-A1B6, IGO-540-B1A, IGO-540-B1C and 178 more. Effective Jan 31, 2003
- [AD 98-18-12](https://openairdocs.org/ad/98-18-12) (historical): Fuel Pump · Textron Lycoming, AVCO AEIO-540-D4A5, AEIO-540-D4B5, AEIO-540-D4C5 and 249 more. Effective Sep 28, 1998
- [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) (6 in force)

- [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-09-04](https://openairdocs.org/saib/NE-09-04): Fuel Control/Reciprocating Engines. Issued Jan 10, 2009
- [SAIB NE-06-32R1](https://openairdocs.org/saib/NE-06-32R1): Reciprocating Engine - Crankshaft. Issued Sep 10, 2008
- [SAIB NE-08-32](https://openairdocs.org/saib/NE-08-32) (historical): Propeller Governor Set Screw. Issued Jul 3, 2008

## NTSB investigations

None matched to N604TW.

## FAA accident and incident reports

None matched to N604TW.

## Reports on N604TW not matched to an aircraft (2)

They name N604TW, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 19960603021769I](https://openairdocs.org/incident/19960603021769I), Jun 3, 1996: Boeing 767231 (N604TW), Los Angeles, CA, Minor damage. Narrative: pilot report on log page 60253: loud noise like a compressor stall sounded shortly after starting taxi with both engines running. Aft flight…
- [Incident 19850514025309I](https://openairdocs.org/incident/19850514025309I), May 14, 1985: Boeing 767231 (N604TW), Bangor, ME. During climb to FL410 nr 1 engine had a compressor stall. Engine shutdown. Safe landing. Replaced engine.

## 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 N604TW not matched to an aircraft (29)

They name N604TW, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR TWAA0101127](https://openairdocs.org/sdr/TWAA0101127), Jan 15, 2001: SKIN. DELAMINATED. DURING CHECK-C MAINT THE RT WING OUTBOARD AILERON AT OUTBOARD END, BOTTOM 4 INCH BY 6 INCH AREA DELAMINATED. CLEANED AND BONDED FWD EDGE OF CONDUCTIVE FRAME WIT
- [SDR TWAA0019101](https://openairdocs.org/sdr/TWAA0019101), Dec 8, 2000: LIGHT. INOPERATIVE. THE EGRESS LAMP LEFT SIDE OF THE MID GALLEY, AND THE OVERWING ESCAPE SLIDE LIGHT AFT OF THE CARGO DOOR, WERE INOPERATIVE. REPLACED THE EGRESS FLEX LAMP, PN 3636
- [SDR TWAA0014301](https://openairdocs.org/sdr/TWAA0014301), Sep 13, 2000: SKIN. CORRODED. DURING CHECK-C MAINT, FOUND CORROSION ON LOWER AFT FUSELAGE SKIN, STA 1329, UNDER AFT VHF ANTENNA. FABRICATED CHANNEL, REMOVED AND TREATED CORROSION, INSTALLED 
- [SDR TWAA0015003](https://openairdocs.org/sdr/TWAA0015003), Sep 8, 2000: SKIN. DELAMINATED. DURING CHECK-C MAINT, THE NUMBER 8 L/E SLAT, I/B END T/E WEDGE REPAIR I/B EDGE HAD DELAMINATED. RE-BONDED EDGES ON SLAT PER SRM 51-70-03, PAGE 27 TO 48.
- [SDR TWAA0014101](https://openairdocs.org/sdr/TWAA0014101), Sep 8, 2000: SKIN. DELAMINATED. DURING CHECK-C MAINT, THE LEFT WING L/E SLAT NUMBER 2, THE I/B CORNER OF THE AFT WEDGE HAD DELAMINATION. INSTALLED A 3 INCH BY 3.5 INCH METAL BOND REPAIR PER SR
- [SDR TWAA0013614](https://openairdocs.org/sdr/TWAA0013614), Aug 19, 2000: SKIN. CRACKED. THE RT FUSELAGE SKIN SUFFERED A 2.25 INCH CRACK INSIDE 8 INCH BY 8 INCH DENT IN PREVIOUS DOUBLER REPAIR AT STA 462, 3 INCHES BELOW STRINGER 33R. REMOVED AND REP
- [SDR TWAA0013613](https://openairdocs.org/sdr/TWAA0013613), Aug 19, 2000: STRINGER. DAMAGED. STRINGER 33R WAS BROKEN AT STA 459 AT FWD END OF PREVIOUS STRINGER REPAIR. REPLACED DAMAGED SECTION OF STRINGER FROM STA 434 TO 468, STRINGER 33 TO EXISTING SPL
- [SDR TWAA0013612](https://openairdocs.org/sdr/TWAA0013612), Aug 19, 2000: STRINGER. DAMAGED. STRINGER 34R WAS BROKEN AT STA 404 AND CRACKED AT STA 413. REMOVED DAMAGED SECTION OF STRINGER. INSTALLED NEW SECTION OF STRINGER BETWEEN STA 401 TO 434 AT STRI
- [SDR TWAA0013611](https://openairdocs.org/sdr/TWAA0013611), Aug 19, 2000: STRINGER. DAMAGED. STRINGER 33R WAS BROKEN AT STA 403 AND 408. REMOVED DAMAGED SECTION OF STRINGER. INSTALLED NEW SECTION OF STRINGER BETWEEN STA 401 AND 434 AT STRINGER SPLICE PE
- [SDR TWAA0013610](https://openairdocs.org/sdr/TWAA0013610), Aug 19, 2000: SKIN. PUNCTURED. THE RT FUSELAGE SKIN SUFFERED A 3 BY 12 INCH PUNCTURE IN A DENTED AREA 17 INCHES HIGH BY 12 INCHES WIDE, STA 400 TO 412, STRINGER 32R TO 2 INCHES BELOW 34R. CUT
- [SDR TWAA0011001](https://openairdocs.org/sdr/TWAA0011001), Jul 12, 2000: LIGHT. INOPERATIVE. THE EGRESS LIGHT WAS INOPERATIVE BY THE FIRST CLASS CLOSET. REPLACED THE LIGHT STRIP. CHECK-C 6-25-00 LAX.
- [SDR TWAA0009101](https://openairdocs.org/sdr/TWAA0009101), Jun 9, 2000: LIGHT. INOPERATIVE. THE CABIN EGRESS LIGHTS ON RT SIDE OF CABIN, ROWS 11 TO 16, WERE REPORTED ILLUMINATED WITH THE SWITCH IN THE ARM POSITION. ACCOMPLISHED OPERATIONAL CHECK AND FO
- [SDR TWAA0003701](https://openairdocs.org/sdr/TWAA0003701), Mar 5, 2000: LIGHT. INOPERATIVE. THE AFT GALLEY EGRESS LIGHTS WERE INOPERATIVE. SPLICED IN NEW CONNECTOR PINS FOR THE JUMPER CABLE. CHECK-C 12-15-99 LAX.
- [SDR TWAA0001601](https://openairdocs.org/sdr/TWAA0001601), Jan 25, 2000: WIRE. WORN. THE FWD CABIN EGRESS LIGHTS WERE INOPERATIVE. REPLACED THE JUMPER CABLE BETWEEN THE FWD CLOSET AND CABIN ROW 1. CHECK-C 12-15-99 LAX.
- [SDR TWAA9913701](https://openairdocs.org/sdr/TWAA9913701), Sep 28, 1999: BATTERY. DISCHARGED. THE CABIN EMERGENCY EXIT SIGN ABOVE THE DOOR AT ROW 18, LEFT SIDE, AND THE EMERGENCY AISLE LIGHTS AT ROWS 18 TO 22, ALL ILLUMINATED WITH THE SWITCH IN THE ARMED
- [SDR TWAA9910102](https://openairdocs.org/sdr/TWAA9910102), Jul 16, 1999: FIRE LOOP. FAILED. EICAS MSG LT ENG FIRE LP2 AND LT ENG FIRE LP1 DISPLAYED. ALSO FIRE PROT SYS FAIL LIGHT ILLUMINATED. FLIGHT RETURNED TO POP. PLACARDED THE NUMBER 2 LOOP INOPERAT
- [SDR TWAA9908802](https://openairdocs.org/sdr/TWAA9908802), Jun 23, 1999: CART. FAILED. WIRE ON A GALLEY CART WAS REPORTED BURNING UNTIL THE CART WAS DISCONNECTED ELECTRICALLY. REPLACED THE CART. CHECK-C 4-18-99 LAX.
- [SDR TWAA9905501](https://openairdocs.org/sdr/TWAA9905501), Apr 15, 1999: SKIN. MISREPAIRED. DURING CHECK-C, MAINT FOUND NUMBER 9 LE SLAT WITH A REPAIR HAVING SEALANT PEELING OFF. INSTALLED A 7 IN BY 3 IN HOT BOND REPAIR PER SRM 51-70-10.
- [SDR TWAA9810102](https://openairdocs.org/sdr/TWAA9810102), Jun 19, 1998: SKIN. DELAMINATED. LAX - DURING CHECK-C, MAINTENANCE FOUND APPROXIMATELY A 5 INCH BY 5 INCH DELAMINATION ON UPPER LEADING EDGE AFT OF NR 6 LE SLAT, APPROXIMATELY 5 FEET OTBD OF IN
- [SDR TWAA9807101](https://openairdocs.org/sdr/TWAA9807101), May 4, 1998: SENSOR. WORN. SDQ - FLT 149 - AFTER FLAPS RETRACTED, GOT EICAS MESSAGE, LE SLAT ASYM WAS DISPLAYED WITH LEADING EDGE LIGHT ILLUMINATED. REPLACED NR 4 LE SLAT PROXIMITY SENSOR
- [SDR TWAA9713201](https://openairdocs.org/sdr/TWAA9713201), Nov 5, 1997: CONNECTOR. DIRTY. STL - FLT 720 - DURING CLIMB, THE NR 2 ENGINE, S/N 4603, INDICATED HIGH OIL PRESSURE. CLEANED CONNECTOR AND CHECKED PIN GRIP ON THE OIL PRESSURE TRANSMITTER, RA
- [SDR TWAA9711504](https://openairdocs.org/sdr/TWAA9711504), Sep 19, 1997: POWER CHORD. FAILED. JFK - FLT 149 - DURING CRUISE, THE AFT GALLEY FOOD CART EMITTED SMOKE DUE TO A BAD POWER CHORD. REMOVED AND REPLACED THE POWER CHORD. FUNCTIONAL CHECK NORMAL. R
- [SDR TWAA9776001](https://openairdocs.org/sdr/TWAA9776001), Jul 9, 1997: EVBC. FAILED. CDG - FLT 917 - DURING CLIMB AT FL 350, NR 2 ENGINE, SN 4613, EXPERIENCED COMPRESSOR STALL IN CLEAR AIR. REMOVED AND REPLACED EVBC, MFG PN 766555-7, MANUFACTURE
- [SDR TWAA9804704](https://openairdocs.org/sdr/TWAA9804704), Mar 25, 1997: SKIN. DISBONDED. MCI - DURING OP 16 MAINTENANCE CHECK, FOUND DISBONDING ON UPPER SKIN OF NR 4 LE SLAT. INSTALLED TWO EACH FIELD REPAIR PATCHES PER SRM 51-70-10. (M)
- [SDR TWAA9804703](https://openairdocs.org/sdr/TWAA9804703), Mar 25, 1997: SKIN. DISBONDING. MCI - DURING OP 16 MAINTENANCE CHECK, FOUND DISBONDING ON TOP SKIN OF NR 2 LE SLAT. INSTALLED TWO REPAIR DOUBLERS PER SRM 51-70-10. (M)
- [SDR TWAA9803707](https://openairdocs.org/sdr/TWAA9803707), Mar 25, 1997: STRINGER. CORRODED. MCI - DURING OP 16 MAINTENANCE CHECK, AT C-1 CARGO COMPT STRINGER 33L AT FS 390 WAS FOUND FOUND CORRODED. REMOVED CORROSION PER SRM 51-10-00. REPLACED STRINGER 
- [SDR TWAA9704001](https://openairdocs.org/sdr/TWAA9704001), Jan 6, 1997: SERVING CART. FAILED. JFK - FLT 843 - DURING CRUISE SINGLE SERVE FOOD CART, MFG P/N 88801-1, EMITTEDSMOKE WHEN TURNED ON. REMOVED AND REPLACED CART WITH A SERVICEABLE CART. (M)
- [SDR TWAA9613002](https://openairdocs.org/sdr/TWAA9613002), Oct 27, 1996: RETRACT MECH. MALFUNCTIONED. LAX - DURING TAKEOFF LEADING EDGE FLAPS WOULD NOT RETRACT. PERFORMED BITE CHECK, CHECKED ALL 24 LEADING EDGE FLAP SENSORS, OPERATED FLAPS SEVERAL CYCLES. ALL CH
- [SDR 96ZZZX2828](https://openairdocs.org/sdr/96ZZZX2828), Mar 29, 1996: DOOR LIGHT. MALFUNCTIONED. SJU - FLT 11 - DURING CLIMB, A NOSE GEAR DOOR LIGHT FAULT INDICATION WAS OBSERVED. NOSE GEAR PROXIMITY SWITCHES WERE CHECKED, OPERATION NORMAL. OP-15 - 12-29-95

## STCs that may be installed (OpenAirDocs) (47)

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 IO-540-C4B5)

- [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
- [STC SE00825WI](https://openairdocs.org/stc/SE00825WI): Installation of Specialty Products Spin-on oil filter on Lycoming Engines. B & C Specialty Products Inc
- [STC SE04349CH](https://openairdocs.org/stc/SE04349CH): Installation of SureFly electronic ignition. SureFly Partners Ltd
- [STC SE01954SE](https://openairdocs.org/stc/SE01954SE): Installation of engine crankcase seal. Ly-Con Rebuilding Company
- [STC SE02352CH](https://openairdocs.org/stc/SE02352CH): Installation of Challenger cleanable oil filter assembly. Challenger Aviation Products Inc
- [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
- [STC SE2387CE](https://openairdocs.org/stc/SE2387CE): Installation of B & C Speciality Products lightweight (10.2 pounds) engine starter P/N BC 315-100-1(12 volt) or P/N BC 315-100-3(24 volt). B & C Specialty Products Inc. Lists IO-540 Series
- [STC SE03309CH](https://openairdocs.org/stc/SE03309CH): Installation of Engine Preheat Kit, p/n TSP6CYL-2927-115 for 115 volt application. Hartzell Propeller Inc
- [STC SE6WE](https://openairdocs.org/stc/SE6WE): Installation of two Roto-Master Turbochargers Model No. 3DT5FF10J2, P/N 600572-00 (formerly Rajay Model 315F10, P/N RJ0080-100, or 102). TALCO Aviation
- [STC SE01436LA](https://openairdocs.org/stc/SE01436LA): Installation of Firewall Forward Technologies LLC modified camshaft. Centri-lube Technologies LLC
- [STC SE04577CH](https://openairdocs.org/stc/SE04577CH): Install an electronic engine ignition system. Electroair Acquisition Corp
- [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
- [STC SE8628SW](https://openairdocs.org/stc/SE8628SW): Installation of oil nozzles for lubrication of cam and filters. Cygnet Aerospace Corp
- [STC SE09445SC](https://openairdocs.org/stc/SE09445SC): Installation of fuel injector nozzles. General Aviation Modifications Inc. Lists IO-540 Series
- [STC SE4408SW](https://openairdocs.org/stc/SE4408SW): Miscellaneous engine cylinder replacement parts. Continental Motors, Inc. Lists IO-540 Series
- [STC SE7509SW](https://openairdocs.org/stc/SE7509SW): Installation of any or all parts listed on Airmotive Engineering Drawing List No. 852-1, Rev. 1, dated 10/4/88, or later FAA approved revision. Continental Motors, Inc. Lists IO-540 Series
- [STC SE7667SW](https://openairdocs.org/stc/SE7667SW): Installation of parts listed on Drawing List No. 8810-3, Rev 6. Continental Motors, Inc. Lists IO-540 Series
- [STC SE8776SW](https://openairdocs.org/stc/SE8776SW): Installation of coated cylinders and piston rings. Continental Motors, Inc. Lists IO-540 Series
- [STC SE00218NY](https://openairdocs.org/stc/SE00218NY): Replacement of Lycoming starter with SKY-TEC 12 volt starter installed. Hartzell Engine Technologies, LLC. Lists IO-540 Series
- [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
- [STC SE00357NY](https://openairdocs.org/stc/SE00357NY): Replacement of Lycoming starter with SKY-TEC 24-volt starter installed. Hartzell Engine Technologies, LLC. Lists IO-540 Series
- [STC SE2901NM](https://openairdocs.org/stc/SE2901NM): Lycoming valve cover gasket. Real Gaskets Tennessee
- [STC SE2902NM](https://openairdocs.org/stc/SE2902NM): Lycoming valve cover gasket. Real Gaskets Tennessee
- [STC SE00768CH](https://openairdocs.org/stc/SE00768CH): Replace Slick 6000, 6100, 6200 and 6300 series magnetos and TCM/Bendix S6-20, S6-200 and S6-1200 series magnetos with the Champion Limited Authority Spark Advance Regulator (LASARTM) ignition system. Champion Aerospace LLC. Lists IO-540 Series
- [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
- [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
- [STC SE611GL](https://openairdocs.org/stc/SE611GL): Incorporation of a fuel flow transducer. Shadin Avionics
- [STC SE01930NY](https://openairdocs.org/stc/SE01930NY): Installation of Casper Labs 90 degree oil filter housing adapter. Casper Labs Inc
- [STC SE7734SW](https://openairdocs.org/stc/SE7734SW): Modification of engine for operation with ethanol fuel. Shauck Dr Maxwell E Jr
- [STC SE1779NM](https://openairdocs.org/stc/SE1779NM): Installation of Precise Flight, Inc. Standby Vacuum System SVS III. Precise Flight Inc
- [STC SE21WE](https://openairdocs.org/stc/SE21WE): Installation of Turbosupercharger 406610-3. GE Engine Services-Corporate Aviation Inc. DBA Garrett Aviation Services
- [STC SE22WE](https://openairdocs.org/stc/SE22WE): Installation of AiResearch Turbosupercharger 406610-3. Approved for IO-540-J4A5 model. GE Engine Services-Corporate Aviation Inc. DBA Garrett Aviation Services. Lists IO-540 Series
- [STC SE5743NM](https://openairdocs.org/stc/SE5743NM): Intallation of adapter for externally mounted oil filter. Aviation Development Corporation
- [STC SE00890LA](https://openairdocs.org/stc/SE00890LA): Installation of Nickson's cylinder barrels on Lycoming reciprocating engine models. Nickson's Machine Shop Inc. Lists IO-540 Series
- [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. Lists IO-540 Series
- [STC SE00350SE](https://openairdocs.org/stc/SE00350SE): Installation of sump mounted chip detector. Aviation Development Corporation
- [STC SE835NE](https://openairdocs.org/stc/SE835NE): Installation of a Flowscan Model201B9 transducer. GEBE Instruments Corp
- [STC SE8023SW](https://openairdocs.org/stc/SE8023SW): Installation and usage of AEROSHELL. Shell Development Co. Lists IO-540 Series
- [STC SE452NE](https://openairdocs.org/stc/SE452NE): Installation and usage of 'Mobil AV 1' aviation oil. Mobil Research & Development Corp. Lists IO-540 Series
- [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. Lists IO-540 Series
- [STC SE5924SW](https://openairdocs.org/stc/SE5924SW): Installation of stainless steel replacement exhaust studs on AVCO engines. Perrigo & Steele Aircraft Engr Company. Lists IO-540 Series
- [STC SE244NE](https://openairdocs.org/stc/SE244NE): Installation of Mattituck plasma flame sprayed cylinder barrels in Teledyne reciprocating engines. Mattituck Airbase, Inc. Lists IO-540 Series
- [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. Lists IO-540 Series
- [STC SE1445SO](https://openairdocs.org/stc/SE1445SO): Use of Aero-blend oil additive in Teledyne (non turbocharged) aircraft engines. ProTec. Lists IO-540 Series
- [STC SE128NE](https://openairdocs.org/stc/SE128NE): Use of AMS/OIL 15W 50 synthetic piston aircraft oil in Avco engines. AMS/OIL. Lists IO-540 Series
- [STC SE44WE](https://openairdocs.org/stc/SE44WE): Use of Kling Aviation Oil, Specifications KL-100, KL-200 and KL-300 in Continental and Lycoming engines. Kling Oil Company. Lists IO-540 Series
- [STC SA01436DE](https://openairdocs.org/stc/SA01436DE) (historical): Installation of Firewall Forward Technologies, LLC modified camshaft. Centri-Lube Technologies LLC

## Related

- Other John T Stearman VANS ACFT RV-10 aircraft: https://openairdocs.org/model/john-t-stearman-vans-acft-rv-10/aircraft.md
- The Lycoming IO-540-C4B5 engine: https://openairdocs.org/engine/lycoming-io-540-c4b5.md

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