Please drop me a line if you have further details or if there are any errors.
NOTE : The information given below is intended to make UK owners / builders aware that this information is available. They should confirm for themselves if the information is correct and valid for their aircraft. If in doubt consult your inspector or LAA engineering.
The list below excludes mods for prop and engine changes and repairs specific to certain aircraft.
| Mod Number | Aircraft Reg | Aircraft Type | Title | Detail | Applies to |
| 10242 | NPKJ | VANS RV-6 | HIGH SPEED WARNING DEVICE | Pressure switch connected to secondary pitot source to actuate light in cockpit if Vne is approached. | ALL AIRCRAFT OF TYPE |
| 10215 | NPKJ | VANS RV-6 | ALTERNATE AIR SOURCE FOR IO-360 | CONVENTIONAL SPRUNG-CLOSED AIR DOOR ADDED IN AIR BOX | ALL AIRCRAFT OF TYPE |
| 10305 | OJVA | VANS RV-6 | REPLACE FUEL TAP | THIS AIRCRAFT ONLY | |
| 10431 | RVIB | VANS RV-6 | REPLACE MAGNETO | THIS AIRCRAFT ONLY | |
| 10432 | RVIB | VANS RV-6 | FIT NAVAID DEVICES | THIS AIRCRAFT ONLY | |
| 10480 | GRIN | VANS RV-6 | ANDAIR FUEL VALVE | THIS AIRCRAFT ONLY | |
| 10544 | ONUN | VANS RV-6A | FLAP OPERATING SYSTEM | THIS AIRCRAFT ONLY | |
| 10545 | ONUN | VANS RV-6A | ENHANCED FUEL SUPPLY SAFETY | THIS AIRCRAFT ONLY | |
| 10546 | ONUN | VANS RV-6A | PREVENTION OF ELEVATOR LEVER & TAIL POST TOUCHING | THIS AIRCRAFT ONLY | |
| 10547 | ONUN | VANS RV-6A | AVOIDANCE OF DRILLING HOLES IN LONGERONS | THIS AIRCRAFT ONLY | |
| 10548 | ONUN | VANS RV-6A | FUEL FILTRATION | THIS AIRCRAFT ONLY | |
| 10549 | ONUN | VANS RV-6A | FUEL COCK BRACKET | THIS AIRCRAFT ONLY | |
| 10550 | ONUN | VANS RV-6A | GAP SEAL BETWEEN RUDDER & REAR BULKHEAD | THIS AIRCRAFT ONLY | |
| 10576 | BXVM | VANS RV-6A | |||
| 10640 | RVNS | VANS RV-4 | STALL WARNING DEVICE | Standard stall warning vane fitted to leading edge. | THIS AIRCRAFT ONLY |
| 10641 | RVNS | VANS RV-4 | STROBE LIGHTS | Skyflash double dual magnum smart strobe mounted to port and stbd fibreglass section of wingtip underside. | THIS AIRCRAFT ONLY |
| 10642 | RVNS | VANS RV-4 | CIRCUIT PROTECTION | Solid State overvoltage protection device (crowbar) fitted. | THIS AIRCRAFT ONLY |
| 10714 | VANS RV8 | INSTALLATION OF ADDITIONAL PORTS IN FUEL TANKS |
AN AN832-6D FITTING IS ADDED IN THE ACCESS PLATE OF EACH FUEL TANK. THIS MODIFICATION IS PART OF THOSE REQUIRED FOR INSTALLATION OF A WILKSCH AIRMOTIVE WAM 160 ENGINE. IF THE INVERTED FUEL SYSTEM FLOP-TUBE OPTION IS CHOSEN, THE ADDITIONAL FUEL FITTING M |
THIS AIRCRAFT ONLY | |
| 10896 | GPAG | VANS RV-6 | DUAL THROTTLE CONTROLS | THIS AIRCRAFT ONLY | |
| 10897 | VANS RV-6 | ALTERNATIVE CONSTRUCTION OF AILERON NOSE RIBS | AILERON RIB FRONT FLANGE ATTACHED AS RIVETTED LOOSE ANGLE FOR EASE OF MANUFACTURE | THIS AIRCRAFT ONLY | |
| 10923 | GDRV | VANS RV-6 | FUEL TIP-TANK INSTALLATION |
FUEL TIP-TANKS MANUFACTURED BY FLYMORE PTY, AUSTRALIA, INSTALLED IN
ACCORDANCE WITH COMPONENT MANUFACTURER'S INSTRUCTIONS. FLOAT-TYPE GAUGES INSTALLED IN FILLER CAPS TO ESTABLISH FUEL CONTENTS AND TO CONFIRM SATISFACTORY FLOW OF FUEL TO MAIN FUEL TANKS. |
THIS AIRCRAFT ONLY |
| 10971 | TOGO | VANS RV-6 | TO IMPROVE COCKPIT ACCESS | THIS AIRCRAFT ONLY | |
| 10979 | CCGU | VANS RV-9A | PEDESTAL TYPE THROTTLE SUBSTITUTED | THROTTLE PEDESTAL SUBSTUTUTED FOR STANDARD VANS PUSH-PULL CONTROL. | THIS AIRCRAFT ONLY |
| 11011 | CCZT | VANS RV-9A | INSTALLATION OF TRIO WING LEVELLER | TRIO WING LEVELLER INSTALLED IN ACCORDANCE WITH APPLICANT's SUBMISSION | THIS AIRCRAFT ONLY |
| 11065 | JFRV | VANS RV-7A | AOA SPORT STALL WARNER | AOA STALL WARNER INSTALLED IN ACCORDANCE WITH MANUFACTURERS INSTRUCTIONS AND APPLICANT'S SUBMISSION | THIS AIRCRAFT ONLY |
| 11076 | ODEE | VANS RV-6 | ENGINE MOUNT REINFORCEMENT | TO ADD FOUR 0.125 INCH THICK 4130N GUSSETTS TO RV6 ENGINE FRAME BY WELDING. | THIS AIRCRAFT ONLY |
| 11085 | RVAL | VANS RV 8 | TO PROVIDE FULL WIDTH BAGGAGE HOLD | THIS AIRCRAFT ONLY | |
| 11089 | RVAL | VANS RV 8 | PROVIDE ACCESS TO A REAR BATTERY | THIS AIRCRAFT ONLY | |
| 11090 | RVAL | VANS RV 8 | LATCH TO PREVENT OBJECTS FALLING INTO CONTROL WELL | THIS AIRCRAFT ONLY | |
| 11091 | RVAL | VANS RV 8 | SAFETY IN EVENT OF FORCED LANDING | THIS AIRCRAFT ONLY | |
| 11095 | RVAL | VANS RV 8 | PROVIDE AIRCRAFT WITH HEATED PITOT | THIS AIRCRAFT ONLY | |
| 11102 | CCJI | VANS RV6 | RELOCATION OF BATTERY | ||
| 11103 | CCJI | VANS RV6 | INC LOCATION OF ENGINE & ELEVATOR CONTROLS | ||
| 11104 | CCJI | VANS RV6 | BRAKE FLUID PIPES & RESERVOIR | THIS AIRCRAFT ONLY | |
| 11105 | CCJI | VANS RV6 | FUEL CENTRE | ||
| 11106 | CCJI | VANS RV6 | FLOOR & SKIN | ||
| 11107 | CCJI | VANS RV6 | STICK & HANDLE SHORTENED | ||
| 11108 | CCJI | VANS RV6 | STALL WARNER | ||
| 11109 | CCJI | VANS RV6 | TRUTRAK DIGITRAK WING LEVELLER | INSTALLATION OF TRUTRAK DIGITRAK WING LEVELLING AUTO-PILOT WITH SERVO MOUNTED IN PORT WING | THIS AIRCRAFT ONLY |
| 11110 | RVAL | VANS RV 8 | STROBE LIGHTS FOR SAFETY | THIS AIRCRAFT ONLY | |
| 11111 | RVAL | VANS RV 8 | FIT DIGITRACK AUTOPILOT | THIS AIRCRAFT ONLY | |
| 11130 | RVAL | VANS RV 8 | TO ADD A PARKING BRAKE | THIS AIRCRAFT ONLY | |
| 11133 | JFRV | VANS RV-7A | DIGITRAK AUTOPILOT | DIGITRAK WING LEVELLER FITTED, SERVO INSTALLED IN WING, CONNECTED BY PUSHROD TO EXISTING AILERON BELLCRANK PER TRUTRAK INSTRUCTIONS | THIS AIRCRAFT ONLY |
| 11138 | RVSX | VANS RV-6 | THROTTLE QUADRANT | THIS AIRCRAFT ONLY | |
| 11145 | RVIX | VANS RV9A | MODULER INSTUMENT PANEL | THIS AIRCRAFT ONLY | |
| 11148 | RVIX | VANS RV9A | CHANGE RIVETS IN RUDDER STOPS | THE RUDDER STOP ANGLE HAS BEEN REPROFILED AND THE FOUR FASTENERS ATTACHING IT HAVE BEEN INCREASED FROM 3/32" TO 1/8". | THIS AIRCRAFT ONLY |
| 11153 | RVIX | VANS RV9A | REPLACEMENT FIXINGS IN F787 | THE ATTACHMENT OF AN UPPER REAR FUSELAGE INTERCOSTAL HAS BEEN MADE WITH FOUR SCREWS IN LIEU OF RIVETS. | ALL AIRCRAFT OF TYPE |
| 11156 | RVIX | VANS RV9A | LUGGAGE TIE DOWNS | THIS AIRCRAFT ONLY | |
| 11158 | RVIX | VANS RV9A | REPLACEMENT FUEL TANK CONTROL | FITTMENT OF THE ALTERNATIVE ANDAIR FUEL GAUGE | THIS AIRCRAFT ONLY |
| 11160 | RVIX | VANS RV9A | MODULA INSTRUMENT PANEL | THIS AIRCRAFT ONLY | |
| 11161 | RVIX | VANS RV9A | MODIFICATION OF F - 7105 PANELS | THIS AIRCRAFT ONLY | |
| 11165 | RVIX | VANS RV9A | LASAR ELECTRONIC IGNITION | THIS AIRCRAFT ONLY | |
| 11170 | RVIX | VANS RV9A | COCKPIT SIDEWALL LIGHTS | A PLASTIC EYEBALL LED LIGHT INSTALLED IN EACH COCKPIT SIDEWALL | ALL AIRCRAFT OF TYPE |
| 11172 | RVIX | VANS RV9A | WINDSCREEN/ROLLBAR STRENGHTHEN | THIS AIRCRAFT ONLY | |
| 11173 | RVIX | VANS RV9A | REPLACEMENT STATIC VENTS | THIS AIRCRAFT ONLY | |
| 11174 | RVIX | VANS RV9A | CHANGES TO F/WALL PENETRATIONS | SHORT FLARED STAINLESS STEEL TUBES HAVE BEEN INTRODUCED WHERE CABLES AND CONTROLS PENETRATE THE FIREWALL TO REDUCE THE CHAFFING RISK. | ALL AIRCRAFT OF TYPE |
| 11175 | RVIX | VANS RV9A | INCREASED FIXINGS IN W/TIP LENSES | ADDITIONAL FIXINGS HAVE BEEN ADDED TO THE PERSPEX WINGTIP LENSES TO REDUCE GAPS AND PREVENT MOISTURE INGRESS. | ALL AIRCRAFT OF TYPE |
| 11182 | RVSA | VANS RV-6A | BAFFLES CLOSED WITH PLENUM | THIS AIRCRAFT ONLY | |
| 11195 | RVIX | VANS RV9A | F - 7107 - L RIB CUT OUT | A SMALL SECTION OF THE INTERCOSTAL ATTACHING BEHIND THE LH SIDE OF THE INSTRUMENT PANEL HAS BEEN CUT AWAY AND A DOUBLER ADDED. | THIS AIRCRAFT ONLY |
| 11197 | RVIX | VANS RV9A | HEATED PITOT HEATER | THIS AIRCRAFT ONLY | |
| 11198 | RVIX | VANS RV9A | CABIN HEAT CABLE BRACKET | CABIN HEAT CONTROL ADDED TO COCKPIT ON LHS | THIS AIRCRAFT ONLY |
| 11199 | RVIX | VANS RV9A | PARK BRAKE CABLE BRACKET | THIS AIRCRAFT ONLY | |
| 11200 | RVIX | VANS RV9A | FLAP POSITION SWITCHES | A BRACKET IS MANUFACTURED AND INSTALLED AGAINST THE FLAP TORQUE TUBE TO MOUNT A MICROSWITCH WHICH DETECTS THE FLAP POSITION. | THIS AIRCRAFT ONLY |
| 11201 | RVIX | VANS RV9A | ENGINE COWL FRONT FIXING | A STAINLESS STEEL COVER IS WRAPPED AROUND THE LEADING EDGE OF THE COWLING TO RETAIN THE COWLING JOINING PINS LH AND RH. THE PIN IS SECURED WITH FOUR SCREWS. | ALL AIRCRAFT OF TYPE |
| 11202 | RVIX | VANS RV9A | RUDDER CABLE FAIRINGS | A SMALL ALUMINUIM FAIRING IS MANUFACTURED AND INSTALLED OVER THE CABLE EXIT TUBE IN THE REAR FUSELAGE. | ALL AIRCRAFT OF TYPE |
| 11203 | RVIX | VANS RV9A | FIRE EXTINGUISHER | THIS AIRCRAFT ONLY | |
| 11206 | RVIX | VANS RV9A | SHORTENED CONTROL STICKS | TOP OF CONTROL COLUMNS CUT DOWN BY 2" TO SUIT PILOT PREFERENCE | THIS AIRCRAFT ONLY |
| 11207 | RVIX | VANS RV9A | STRENGTHEN TUNNEL COVER | THE TOP PLATE OF THE CENTRAL TUNNEL INCREASED IN THICKNESS TO PROVIDE INCREASED ROBUSTNESS | ALL AIRCRAFT OF TYPE |
| 11208 | RVIX | VANS RV9A | CUT OUT IN FLOOR (F982-C LDRWG34) | CUTOUT IN FLOOR PROVIDED TO PROVIDE ROUTE FOR WIRING FROM UNDER FLOOR COVER TO FIREWALL CONDUIT AND PROVIDE CLEARANCE AROUND FLOOR MOUNTED PARK BRAKE VALVE. | THIS AIRCRAFT ONLY |
| 11213 | XVOM | VANS RV-6 | WINGTIP STROBES | FITMENT OF SKYFLASH WINGTIP STROBE KIT | THIS AIRCRAFT ONLY |
| 11216 | RVSA | VANS RV-6A | VERTICAL STAB TO HORIZONTAL STAB | THIS AIRCRAFT ONLY | |
| 11217 | CCZD | VANS RV-7 | BONDING OF FLEXIGLASS CANOPY | Sikaflex - 295 UV adhesive compound used to attach canopy bubble in lieu of multiple AN507-6R8 screws | ALL AIRCRAFT OF TYPE |
| 11238 | RVIX | VANS RV9A | PROVIDE FITTING SPACE FOR RADIO/NAV. EQPT. | VARIOUS RE-INFORCED CUTOUTS HAVE BEEN MADE IN THE BULKHEAD IN FRONT OF THE INSTRUMENT PANEL TO ALLOW LONG ITEMS OF RADIO EQUIPMENT TO BE FITTED. | THIS AIRCRAFT ONLY |
| 11269 | CBUK | VANS RV-6A | ENGINE CONTROL PANEL | SUB-PANEL ADDED UNDER INSTRUMENT PANEL TO MOUNT THROTTLE AND MIXTURE PUSH-PULL CONTROLS PER APPLICANT'S SUBMISSION | THIS AIRCRAFT ONLY |
| 11274 | CBUK | VANS RV-6A | NAV/STROBE LIGHT SYSTEM | WHELEN STROBES FITTED AT WINGTIPS AND TAIL PER SUBMISSION FROM APPLICANT | THIS AIRCRAFT ONLY |
| 11275 | RVIX | VANS RV9A | CANOPY LOCK | THIS AIRCRAFT ONLY | |
| 11290 | RVVI | VANS RV-6 | ELECTRIC SERVO OPERATED SPRING BIAS | THIS AIRCRAFT ONLY | |
| 11299 | IINI | VANS RV-9A | LANDING LIGHT | THIS AIRCRAFT ONLY | |
| 11302 | VANS RV-6 | MODULAR INSTRUMENT PANEL | The existing Vans supplied panel is replaced with a modular panel and sub-panel which are available as a kit from "Affordable Panels Inc". The specific product installed to this aircraft is the "standard " panel applicable to the RV-6. | THIS AIRCRAFT ONLY | |
| 11317 | CCZT | VANS RV-9A | FITMENT OF EXTRA PITOT TUBE FOR AOA INDICATION | ADDITIONAL PITOT TUBE ADDED SOLELY TO OPERATE AOA INDICATOR, IN ADDITION TO STANDARD PITOT STATIC SYSTEM AND STALL WARNER SWITCH | THIS AIRCRAFT ONLY |
| 11318 | CCZT | VANS RV-9A | FITMENT OF STROBE POWER SUPPLY | Three sheet metal parts are installed under the baggage bay to support the Whelen LN.A415-HDA-CF Strobe Power Supply unit. | THIS AIRCRAFT ONLY |
| 11319 | CCZT | VANS RV-9A | FITMENT OF REMOTE COMPASS HEAD | A compass sender unit weighing less than 4 oz is mounted on a fabricated aluminuim bracket mounted to a fuselage frame in the tailcone. | THIS AIRCRAFT ONLY |
| 11326 | IINI | VANS RV-9A | LOCKING OF CANOPY RELEASE MECHANISM | canopy hinge release wire locked closed | THIS AIRCRAFT ONLY |
| 11376 | CDMF | VANS RV-9A | COWL FASTENING (CAM LOCKS) | The existing "piano hinge" arrngement to fasten the upper and lower cowlings is replaced by standard aircraft camlocs. | ALL AIRCRAFT OF TYPE |
| 11438 | BVDI | VANS RV-4 | SMOKE SYSTEM INSTALLATION |
SMOKING AIRPLANES INC. SMOKE SYSTEM KIT INSTALLED IN ACCORDANCE WITH
MANUFACTURER'S INSTRUCTIONS. SMOKE TANK INSTALLED IN BAGGAGE BAY AREA BY RIVETS TO FLOOR AND UNDER-FLOOR RIB SECTIONS. |
THIS AIRCRAFT ONLY |
| 11480 | RVAL | VANS RV 8 | FUEL FILLER CAP RETRO-FIT | NEWTON EQUIPMENT LTD. AERO FILLER CAP, PART NUMBER A20L-VNS 05-01006 INSTALLED IN ACCORDANCE WITH COMPONENT MANUFACTURER'S INSTRUCTIONS. | THIS AIRCRAFT ONLY |
| 11481 | RVAL | VANS RV 8 | E.I. INC. FP 5 FUEL MONITORING INSTRUMENT |
ELECTRONICS INTERNATIONAL FUEL MONITORING SYSTEM INSTALLED IN
ACCORDANCE WITH COMPONENT MANUFACTURER'S INSTRUCTIONS. MAJOR COMPONENTS ARE FT-60 FUEL TRANSDUCER AND FP-5 INSTRUMENT. COMPONENT MANUFACTURER'S DETAILS ARE: ELECTRONICS INTERNATIONAL, INC., 6 |
THIS AIRCRAFT ONLY |
| 11482 | RVAL | VANS RV 8 | TAIL WHEEL STEERING LINK |
RV/Rocket Steering Link fitted between steering arms on rudder and
tailwheel. Installation carried out in accordance with instruction sheets provided by component manufacturer. Component manufacturer details are: Terry Jantzi, P.O. Box 20052, Pioneer Pa |
THIS AIRCRAFT ONLY |
| 11488 | RVIX | VANS RV9A | TRIO WING LEVELLER | TRIO WING LEVELLER INSTALLATION WITH SERVO MOUNTED AT WING BELLCRANK. BRACKET STIFFENED TO AVOID FLEXING UNDER SERVO LOAD. | THIS AIRCRAFT ONLY |
| 11490 | GDRV | VANS RV-6 | AUTOPILOT INSTALLATION | TRU-TRAK 200 WING-LEVER AND ALTITUDE-HOLD AUTOPILOT INSTALLED AND TESTED IN ACCORDANCE WITH COMPONENT MANUFACTURER'S INSTRUCTIONS. | THIS AIRCRAFT ONLY |
| 11491 | GDRV | VANS RV-6 | LONG RANGE FUEL SYSTEM | TWO COCKPIT FUEL TANKS DESIGNED BY FRAZER NASH CONSULTANCY LIMITED INSTALLED IN PASSENGER SEAT AREA FOR LONG-DISTANCE FLYING. | THIS AIRCRAFT ONLY |
| 11563 | BZUY | VANS RV-6 | FUSELAGE UPPER LONGERON REPAIR |
NEW FORWARD FUSELAGE UPPER LONGERON INSTALLED, WITH SPLICE. SCHEME BASED ON VANS AIRCRAFT RECOMMENDATION, THE FASTENER PITCH AND SIZE BASED ON THE REQUIREMENTS OF AC43.13-1B. |
THIS AIRCRAFT ONLY |
| 11575 | PWUL | VANS RV-6 | TAILWHEEL STEERING LINK |
RV/Rocket Steering Link fitted between steering arms on rudder and
tailwheel. Installation carried out in accordance with instruction sheets provided by component manufacturer. Component manufacturer details are: Terry Jantzi, P.O. Box 20052, Pioneer Pa |
THIS AIRCRAFT ONLY |
| 11576 | PWUL | VANS RV-6 | RUDDER CABLE EXIT FAIRINGS | Covers added to rudder cable exits in fuselage to reduce drag and FOD risk. | THIS AIRCRAFT ONLY |
| 11577 | PWUL | VANS RV-6 | ADDITIONAL REAR FUSELAGE ACCESS PANEL | An additional rear-fuselage access hole has been added to better gain access to the elevator horn bolt for installation and inspection purposes. | THIS AIRCRAFT ONLY |
| 11581 | PWUL | VANS RV-6 | REPLACEMENT OF RIVETS WITH SCREWS ON COCKPIT FLOOR |
STANDARD COCKPIT FLOOR IS ATTACHED TO UNDERLYING STRUCTURE WITH
POP-RIVETS, APART FROM AREAS REQUIRING REMOVAL FOR INSPECTION
PURPOSES. BUILDER HAS MADE ALL FLOOR PANELS REMOVABLE BY REPLACEMENT OF POP RIVETS BY #8 STAINLESS-STEEL MACHINE SCREWS AND ANCH |
THIS AIRCRAFT ONLY |
| 11588 | PWUL | VANS RV-6 | COVER-PLATE INSTALLED FOLLOWING STEP REMOVAL |
AIRCRAFT CONVERTED FROM RV-6A TO RV-6 DURING BUILD. BLANKING PLATES RIVETTED TO FUSELAGE SKIN TO FILL HOLE IN EACH FUSELAGE SIDE FOLLOWING REMOVAL OF STEPS. |
THIS AIRCRAFT ONLY |
| 11591 | PWUL | VANS RV-6 | STROBE AND NAVIGATION LIGHT INSTALLATION |
STROBE LIGHT INSTALLED AT TOP OF FIN. STROBE/NAVIGATION LIGHTS INSTALLED IN WING-TIPS. INSTALLATIONS CARRIED OUT IN ACCORDANCE WITH EQUIPMENT MANUFACTURER'S INSTRUCTIONS. |
THIS AIRCRAFT ONLY |
| 11596 | PWUL | VANS RV-6 | ADDITIONAL HARNESS ATTACHMENT | CROTCH-STRAP HARNESS ATTACHMENT ADDED FOR EACH OCCUPANT. | THIS AIRCRAFT ONLY |
| 11599 | PWUL | VANS RV-6 | MODIFIED BATTERY BOX INSTALLATION | INSTALLATION OF RV-7 BATTERY BOX ON FIREWALL IN ACCORDANCE WITH VANS AIRCRAFT INSTALLATION INSTRUCTIONS. | THIS AIRCRAFT ONLY |
| 11600 | PWUL | VANS RV-6 | RELOCATED CANOPY RELEASE |
CANOPY RELEASE HANDLE IS RELOCATED TO PROVIDE INCREASE SPACE ON
INSTRUMENT PANEL. MODIFICATION ACHIEVED BY INVERTING CANOPY RELEASE MECHANISM AND SHORTENING RELEASE HANDLE. |
THIS AIRCRAFT ONLY |
| 11601 | PWUL | VANS RV-6 | FITMENT OF THROTTLE QUADRANT | THREE LEVEL THROTTLE QUADRANT PART NUMBER DJM1/3 SOURCED FROM AIRCRAFT SPRUCE AND SPECIALITY CO. AND INSTALLED IN AIRCRAFT WITH PURPOSE DESIGN MOUNTINGS. | THIS AIRCRAFT ONLY |
| 11642 | RVCH | VANS RV- 8A | CHANGE OF BOLT DIAMETER FROM 3/16" TO 1/4" |
Two inboard tailplane forward-spar to fuselage attachment bolts
changed from AN3 to AN4. Two lower fin-spar to fuselage attachment bolts changed from AN3 to AN4. PFA Inspector must inspect the opened out holes for quality, and must check that the bolt h |
THIS AIRCRAFT ONLY |
| 11645 | RVIX | VANS RV9A | ALTITUDE HOLD SYSTEM | TRIO ALTITUDE HOLD SYSTEM FITTED PER APPLICANT'S DRAWING, INCLUDING ALTITUDE HOLD ACTIVE WARNING LIGHT AND DUPLICATED DISENGAGE SWITCHES. | THIS AIRCRAFT ONLY |
| 11649 | SEVN | VANS RV-7 | ENGINE MOUNT MODIFICATION |
1.625 in OD undercarriage leg sockets on engine mount replaced by
1.875 inch OD undercarriage leg sockets. Welding to be carried out by CAA Approved welder, with due regard to precautions when welding thin wall tubing to thick-wall tubing. All other det |
THIS AIRCRAFT ONLY |
| 11650 | RIVT | VANS RV-6 | ENGINE MOUNT MODIFICATION |
1.625 in OD undercarriage leg sockets on engine mount replaced by
1.875 inch OD undercarriage leg sockets. Welding to be carried out by CAA Approved welder, with due regard to precautions when welding thin wall tubing to thick-wall tubing. All other det |
THIS AIRCRAFT ONLY |
| 11651 | RVJP | VANS RV-9A | NAVAID AUTOPILOT | NAVAID WING LEVELLER FITTED PER APPLICANT'S SUBMISSION USING HENDERSON MODIFICATION 11011 | THIS AIRCRAFT ONLY |
| 11654 | CCZT | VANS RV-9A | A102 MACHINE SCREWS FOR FWD RIB ATTACH TO SPAR |
A102-1/2B BOLTS USED INSTEAD OF 1/8" AD RIVETS TO ATTACH FORWARD
RIBS TO SPAR DURING LEADING-EDGE REPLACEMENT ON STARBOARD WING. BOLT SIZE IS 6-32 UNC, REQUIRING AN INCREASE IN HOLE SIZE FROM 1/8" NOMINAL TO 0.138" NOMINAL (BOLT DIA TO BE MEASURED PRIOR |
THIS AIRCRAFT ONLY |
| 11681 | RVIV | VANS RV-4 | STRENGTHEN ENGINE MOUNT WITH GUSSETS | Three 0.060" thick 4130N gussets welded to both sides of engine frame in the area of the firewall attachments. | THIS AIRCRAFT ONLY |
| 11687 | BZXB | VANS RV-6 | MAIN UNDERCARRIAGE SOCKET BRACING | ADDITIONAL BRACING TUBES ADDED TO ENGINE MOUNT TO STIFFEN ATTACHMENT OF MAIN GEAR LEG SOCKETS TO PREVENT CRACKING IN THIS VICINITY CAUSED BY REPEATED LANDING LOADS | THIS AIRCRAFT ONLY |
| 11733 | CDAE | VANS RV-6A | TRUTRAK DIGITRAK WING LEVELLER | INSTALLATION OF TRUTRAK DIGITRAK WING LEVELLING AUTO-PILOT ACCORDING TO TRUTRAK'S INSTALLATION INSTRUCTIONS | THIS AIRCRAFT ONLY |
| 11781 | GNRV | VANS RV-9A | SHORTEN CONTROL STICKS | CONTROL STICKS SHORTENED AT TOP BY 3 INCHES IN SIMILAR MANNER AS ACCEPTED ON G-RVIX | THIS AIRCRAFT ONLY |
| 11813 | JSRV | VANS RV-6 | PORT WING SKIN REPAIR | WING SKIN CUT BACK AND REPAIR PATCH SPLICED IN, IN VICINITY OF FLAP SHROUD, TO CORRECT ERROR MADE IN MANUFACTURE. | THIS AIRCRAFT ONLY |
| 11804 | TUCK | VANS RV-8 | GROUND POWER SOCKET | Installation of ‘Piper’ style ground power socket under rear battery bay | THIS AIRCRAFT ONLY |
| 11805 | TUCK | VANS RV-8 | CUSTOM STICK GRIPS | Installation of Infinity Stick Grips front and rear. | THIS AIRCRAFT ONLY |
| 11806 | TUCK | VANS RV-8 | PITOT STATIC TUBE | Installation of pitot static tube on port wing. | THIS AIRCRAFT ONLY |
| 11807 | TUCK | VANS RV-8 | VOR AERIAL LOCATION AND MOUNTIN | Installation of VOR/ILS/GS antenna on top of tail fin. (see 21 years of RVator) | THIS AIRCRAFT ONLY |
| 11808 | TUCK | VANS RV-8 | VHF AERIAL LOCATION AND MOUNTING | Installation of VHF antenna on underside of wings. | THIS AIRCRAFT ONLY |
| 11841 | CDMF | VANS RV-9A | ENGINE BAFFLE PLENUM | INSTALLATION OF BAFFLE PLENUM OVER ENGINE | THIS AIRCRAFT ONLY |
| 11861 | TUCK | VANS RV-8 | LASAR IGNITION | Installation of LASAR ignition. | THIS AIRCRAFT ONLY |
| 11865 | TUCK | VANS RV-8 | WINGTIP FUEL TANKS AND STROBE LIGHTS | Instillation of Vans wingtip fuel tanks with strobe/nav lights and tail strobe/nav light. | THIS AIRCRAFT ONLY |
| 11899 | CCND | VANS RV-9A | FLEXIBLE FUEL PIPE SUBSTITUTED | STANINLESS STEEL SHEATHED RUBBER AIRCRAFT FLEXIBLE FUEL TUBING SUBSTITUTED BETWEEN WING TANK AND FUEL SELECTOR, IN PLACE OF STANDARD ALUMINIMUM TUBING, FOR EASE OF ROUTING PAST OBSTRUCTIONS. | THIS AIRCRAFT ONLY |
| 11900 | CCND | VANS RV-9A | ADDITIONAL CANOPY TRIM AND CENTRAL HANDLE ADDED | ADDITIONAL ALUMINIUM ALLOY TRIM ADDED TO PROVIDE NEAT CANOPY SEAL AND ALSO CENTRAL EXTERNAL HANDLE ADDED TO ALLOW CANOPY TO BE OPENED WITHOUT TWISTING CANOPY. | THIS AIRCRAFT ONLY |
| 11901 | CCND | VANS RV-9A | SPATS DELETED, ALTERNATIVE WHEEL NUT LOCKING | DUE TO ABSENCE OF WHEEL SPATS ON THIS AIRCRAFT, ALTERNATIVE DESIGN OF WHEEL NUT RETENTION INCORPORATED. SPACERS ALSO INCLUDED BETWEEN WHEEL BEARINGS TO ALLOW WHEEL NUTS TO BE PINCHED UP. | THIS AIRCRAFT ONLY |
| 11902 | CCND | VANS RV-9A | QUADRANT THROTTLE | QUADRANT THROTTLE/MIXTURE UNIT OF CONVENTIONAL DESIGN SUPPLIED BY AIRCRAFT SPRUCE AND SPECIALTY FITTED AT AIRCRAFT CENTRELINE USING CUSTOM BRACKETS | THIS AIRCRAFT ONLY |
| 11903 | RVAW | VANS RV-6 | SEAT ALTERATION | REPLACEMENT OF SEAT PAN RIB SECTIONS TO ORIGINAL PROFILE FOLLOWING ATTEMPT TO LOWER SEAT PAN FOR EXTRA HEADROOM. | THIS AIRCRAFT ONLY |
| 11909 | BXPI | VANS RV-4 | SMOKE SYSTEM | INSTALLATION OF SMOKE SYSTEM INCORPORATING OIL TANK AND PUMP ASSEMBLY FASTENED ONTO BAGGAGE BAY FLOOR VIA REMOVABLE ANGLE BRACKETS | THIS AIRCRAFT ONLY |
| 11910 | GNRV | VANS RV-9A | TWIN HAND OPERATED BRAKES FITTED | TWIN HAND OPERATED BRAKES FITTED INACCORDANCE WITH BUILDER'S SUBMISSION DETAILS. PROVEN SATISFACTORY BY FLIGHT TEST. | THIS AIRCRAFT ONLY |
| 11941 | ONUN | VANS RV-6A | NAVAID WING LEVELLER INSTALLATION | NAVAID WING LEVELLER SERVO INSTALLED UNDER STARBOARD SEAT PER STANDARD NAVAID SCHEME | THIS AIRCRAFT ONLY |
| 12000 | RVCE | RV-6A | WINDSCREEN DE-MISTER | INSTALLATION OF PILOT OPERATED DE-MISTER USING HOT AIR FROM CABIN HEATER | THIS AIRCRAFT ONLY |
| 12001 | RVCE | RV-6A | NAVAID AUTO-PILOT | INSTALLATION OF NAVAID DEVICES WING LEVELLING AUTO-PILOT WITH SERVO FITTED UNDER P2 SEAT | THIS AIRCRAFT ONLY |
| 12002 | RVCE | RV-6A | 5TH POINT SEAT BELT | ADDITION OF CROTCH STRAP WITH ASSOCIATED MOUNTING UNDER SEAT PAN INCLUDING ANTI-CHAFING TUBES WHERE STRAP PASSES THROUGH SEAT PAN. | THIS AIRCRAFT ONLY |
| 12003 | RVCE | RV-6A | ENGINE AND TRIM CONTROLS MOUNTING | MOUNTING OF ENGINE CONTROLS ON BRACKET MOUNTED HORIZONTALLY UNDER CENTRAL PORTION OF INSTRUMENT PANEL AND PITCH TRIM KNOB ON SEPARATE PANEL WITH FUEL SELECTOR VALVE. | THIS AIRCRAFT ONLY |
| 12004 | RVCE | RV-6A | CENTRE ARM REST AND MAP BOX | INSTALLATION OF CENTRALLY LOCATED MAP BOX WITH HINGED LID ACTING AS ARM REST. | THIS AIRCRAFT ONLY |
| 12005 | RVCE | RV-6A | WINGTIP STROBE POWER SUPPLY | INSTALLATION OF STROBE POWER SUPPLIES ONTO TIP RIB OF WINGS | THIS AIRCRAFT ONLY |
| 12006 | RVCE | RV-6A | MATRONICS FUELCHEC LT FUEL COMPUTER | INSTALLATION OF MATRONICS FUELCHEC LT FUEL FLOW MONITORING SYSTEM USING FLOSCAN 201B TRANSDUCER | THIS AIRCRAFT ONLY |
| 12007 | RVCE | RV-6A | HEATED PITOT | INSTALLATION OF HEATED PITOT HEAD IN PLACE OF STANDARD 'BENT TUBE' PITOT HEAD | THIS AIRCRAFT ONLY |
| 12020 | CCVM | VANS RV-7A | TRUTRAK DIGIFLIGHT IIVS ALTITUDE HOLD | INSTALLATION OF TRUTRAK DIGITRAK IIVS AUTOPILOT HEAD AND ALTITUDE HOLD SERVO | THIS AIRCRAFT ONLY |
| 12045 | CECV | VANS RV-7 | DIGIFLIGHT II AUTOPILOT | INSTALLATION OF TRUTRAK DIGIFLIGHT II DUAL AXIS AUTO PILOT ACCORDING TO VANS APPROVED INSTRUCTIONS PROVIDED BY TRUTRAK | THIS AIRCRAFT ONLY |
| 12049 | RVMZ | VANS RV-8 | REAR BATTERY AND THROTTLE |
BATTERY RELOCATED TO REAR POSITION AS VANS OPTION DRAWING REAR THROTTLE CONTROL ADDED AS VANS OPTION DRAWING |
THIS AIRCRAFT ONLY |
| 12080 | OPVM | VANS RV-9A | INSTALLATION OF STROBE SYSTEM | INSTALLATION OF STARBURST/AVI-PAK STROBE SYSTEM USING TWO WING MOUNTED AIRWORLD SKYFLASH STROBE HEADS AND ONE RUDDER MOUNTED WHELAN A500-14 STROBE HEAD | THIS AIRCRAFT ONLY |
| 12082 | OPVM | VANS RV-9A | MODULAR INSTRUMENT PANEL | INSTALLATION OF AFFORDABLE PANELS' MODULAR INSTRUMENT PANEL | THIS AIRCRAFT ONLY |
| 12092 | CDVT | VANS RV-6 | FUEL FLOW MONITORING SYSTEM | INSTALLATION OF MATRONICS FUELCHEC DX FUEL FLOW MONITORING SYSTEM INCORPORATING FLOSCAN 201B TRANSDUCER | THIS AIRCRAFT ONLY |
| 12150 | CEEP | VANS RV-9/9A | REPLACEMENT OF INSTRUMENT PANEL | INSTALLATION OF MODULAR INSTRUMENT PANELS IN PLACE OF SINGLE PIECE PANEL ENABLING OWNER CHOICE OF INSTRUMENT LAYOUT. | THIS AIRCRAFT ONLY |
| 12159 | ORVE | VANS RV-6 | VAPOUR RETURN PIPE ADDED | VAPOUR RETURN LINE ADDED PER APPLICANT'S DRAWING SUPPLIED. THIS HAS BEEN FITTED IN THE HOPE THAT AT SOME TIME IN THE FUTURE THE AIRCRAFT WILL BE ABLE TO BE CLEARED FOR USE WITH MOGAS FUEL. APPROVAL OF THIS MOD DOES NOT CONFER APPROVAL TO USE MOGAS. | THIS AIRCRAFT ONLY |
| 12185 | RVSA | VANS RV-6A | LARGER NOSEWHEEL AND MODIFIED NOSEWHEEL FORK | LARGER DIAMETER NOSEWHEEL TYRE FITTED USING REDESIGNED NOSEWHEEL FORK | THIS AIRCRAFT ONLY |
| 12223 | XSAM | VANS RV-9A | BATTERY BOX RELOCATED | BATTERY BOX RELOCATED TO FIREWALL PER APPLICANT'S DRAWING | THIS AIRCRAFT ONLY |
| 12224 | XSAM | VANS RV-9A | CANOPY HANDLE ADDED | EXTERNAL CANOPY HANDLE ADDED PER APPLICANT'S DRAWING | THIS AIRCRAFT ONLY |
| 12225 | XSAM | VANS RV-9A | RUDDER TRIM TAB ADDED | SMALL GROUND-ADJUSTABE RUDDER TRIM TAB ADDED PER APPLICANT'S DRAWING | THIS AIRCRAFT ONLY |
| 12244 | CDXT | VANS RV9 | EZ1- ALTITUDE HOLD | WITH SERVO BEHIND BAGGAGE COMP. | THIS AIRCRAFT ONLY |
| 12245 | CDXT | VANS RV9 | EZ AUTOPILOT | WITH SAFEAIR WING TIP INSTALLATION | THIS AIRCRAFT ONLY |
| 12276 | DUDE | VANS RV8 | DOUG BELL TAIL WHEEL | REFIT VANS UNIT WITH A DOUG BELLS | THIS AIRCRAFT ONLY |