# Cub Crafters PA18-150

- Type: Aircraft model (FAA registry)
- Registry code: 2470000
- Manufacturer (registry): CUB CRAFTERS
- Model: PA18-150
- Aircraft type: Fixed wing single engine
- Category: Airplane
- Engines: 1 · Reciprocating
- Seats: 2
- Weight class: Up to 12,499 lb
- Certification: Type certificated
- Data sheet: [TCDS 1A2](https://openairdocs.org/tcds/1A2) (OpenAirDocs)
- Holder: Piper Aircraft Inc.
- Registered aircraft: 16
- Page: https://openairdocs.org/model/cub-crafters-pa18-150

Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker.

## ADs that may apply (OpenAirDocs)

Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment.

- [AD 2025-02-11](https://openairdocs.org/ad/2025-02-11): Rudder Structure · FS 2001 J5A (Army L-4F), J5A-80, J5B (Army L-4G) and 67 more. Effective Mar 20, 2025
- [AD 2022-03-15](https://openairdocs.org/ad/2022-03-15): Fuel Quantity Indicator · Garmin G3X Touch Electronic Flight Instrument System (STC SA01899WI or SA02658SE). Effective Mar 21, 2022
- [AD 2015-08-04](https://openairdocs.org/ad/2015-08-04): Wings · FS 2000 L-14, AE-1, HE-1 and 77 more. Effective Jun 3, 2015
- [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 2006-03-08](https://openairdocs.org/ad/2006-03-08): Vacuum pumps · Aero Advantage 14-19, 14-19-2, 14-19-3 and 299 more. Effective Mar 10, 2006
- [AD 2005-01-19](https://openairdocs.org/ad/2005-01-19): Mode S transponders · GARMIN International GTX 330D, GTX 330, GTX 33D and 830 more. Effective Feb 23, 2005
- [AD 2001-23-17](https://openairdocs.org/ad/2001-23-17): GNS 430 units · Cessna 172, 182, 206 and 209 more. Effective Dec 28, 2001
- [AD 96-09-06](https://openairdocs.org/ad/96-09-06): Air Filter Assemblies · Maule Aerospace Technology 7ACA, 7ECA, 7FC and 180 more. Effective Jun 7, 1996
- [AD 85-06-04](https://openairdocs.org/ad/85-06-04): Fuel Tank · FS 2001 AE-1, HE-1, J5A-80 and 60 more. Effective May 4, 1985
- [AD 81-06-08](https://openairdocs.org/ad/81-06-08): Lower Fuselage Attachment Tab · Piper PA-18-150. Effective Nov 19, 1981
- [AD 78-10-03](https://openairdocs.org/ad/78-10-03): Fuel Venting · FS 2001 AE-1, HE-1, J5A-80 and 66 more. Effective May 23, 1978
- [AD 69-23-03](https://openairdocs.org/ad/69-23-03): Lower Longeron Inspection · Piper PA-18-150. Effective Nov 15, 1969
- [AD 68-05-01](https://openairdocs.org/ad/68-05-01): Exhaust Mufflers · FS 2001 J5A-80, J5A (Army L-4F), J5B (Army L-4G) and 67 more. Effective Mar 31, 1968
- [AD 62-02-05](https://openairdocs.org/ad/62-02-05): Rudder Cable Attachment Lug · Piper PA-18, PA-18-105 (Special), PA-18-125 (Army L-21A) and 5 more
- [AD 61-16-05](https://openairdocs.org/ad/61-16-05): Control Cable Replacement · Piper PA-18-150, PA-18A-135, PA-18A-150 and 6 more. Effective Jul 26, 1961
- [AD 60-10-08](https://openairdocs.org/ad/60-10-08): Fuel Selector Valve · Piper PA-18, PA-18-105 (Special), PA-18-125 (Army L-21A) and 30 more. Effective Jul 15, 1960
- [AD 53-04-01](https://openairdocs.org/ad/53-04-01): Control Stick Attachment · Piper PA-18, PA-18-105 (Special), PA-18-125 (Army L-21A) and 16 more

Historical (superseded or no longer in force):

- [AD 99-01-05 R1](https://openairdocs.org/ad/99-01-05-R1) (historical): Wings · FS 2000 L-14, AE-1, HE-1 and 73 more. Effective Jan 14, 2014
- [AD 99-01-05](https://openairdocs.org/ad/99-01-05) (historical): Wing Lift Struts or Forks · FS 2000 L-14, AE-1, HE-1 and 73 more. Effective Feb 8, 1999

## Information bulletins (advisory) (3)

- [SAIB SW-18-31](https://openairdocs.org/saib/SW-18-31): NAVIGATION, ATTITUDE, AND DIRECTION DATA SYSTEM. Issued Nov 21, 2018
- [SAIB CE-03-02](https://openairdocs.org/saib/CE-03-02) (historical): . Issued Oct 8, 2002
- [SAIB ACE-96-04](https://openairdocs.org/saib/ACE-96-04): . Issued Aug 7, 1996

## Registered aircraft (16)

- [N113PJ](https://openairdocs.org/aircraft/N113PJ): [Lang Carl](https://openairdocs.org/faa-owner/LANG%20CARL), [Harper, TX](https://openairdocs.org/faa-place/TX/Harper), built 2003, S/N 9957CC
- [N143CC](https://openairdocs.org/aircraft/N143CC): [Aerial Messages Leasing Co](https://openairdocs.org/faa-owner/AERIAL%20MESSAGES%20LEASING%20CO), [Longwood, FL](https://openairdocs.org/faa-place/FL/Longwood), built 2003, S/N 9956CC
- [N146CC](https://openairdocs.org/aircraft/N146CC): built 2004, S/N 9970CC
- [N148CC](https://openairdocs.org/aircraft/N148CC): [Dream Aero Holdings LLC](https://openairdocs.org/faa-owner/DREAM%20AERO%20HOLDINGS%20LLC), [Clackamas, OR](https://openairdocs.org/faa-place/OR/Clackamas), built 2003, S/N 9955CC
- [N180EN](https://openairdocs.org/aircraft/N180EN): [Nealey Eric D](https://openairdocs.org/faa-owner/NEALEY%20ERIC%20D), [Barrington, IL](https://openairdocs.org/faa-place/IL/Barrington), built 2003, S/N 9966CC
- [N226JK](https://openairdocs.org/aircraft/N226JK): [Smith David C](https://openairdocs.org/faa-owner/SMITH%20DAVID%20C), [Brewster, WA](https://openairdocs.org/faa-place/WA/Brewster), built 2004, S/N 9965CC
- [N324A](https://openairdocs.org/aircraft/N324A): [Lauridsen Hans O](https://openairdocs.org/faa-owner/LAURIDSEN%20HANS%20O), [Scottsdale, AZ](https://openairdocs.org/faa-place/AZ/Scottsdale), S/N 9962CC
- [N365CC](https://openairdocs.org/aircraft/N365CC): [Ski Sawmill Family Resort Inc](https://openairdocs.org/faa-owner/SKI%20SAWMILL%20FAMILY%20RESORT%20INC), [Ulysses, PA](https://openairdocs.org/faa-place/PA/Ulysses), built 2004, S/N 9963CC
- [N392CC](https://openairdocs.org/aircraft/N392CC): [Cecil John P](https://openairdocs.org/faa-owner/CECIL%20JOHN%20P), [Willows, CA](https://openairdocs.org/faa-place/CA/Willows), built 2003, S/N 9960CC
- [N519WG](https://openairdocs.org/aircraft/N519WG): [Thunderbird Photography LLC](https://openairdocs.org/faa-owner/THUNDERBIRD%20PHOTOGRAPHY%20LLC), [Greenville, CA](https://openairdocs.org/faa-place/CA/Greenville), built 2003, S/N 9964CC
- [N55PZ](https://openairdocs.org/aircraft/N55PZ): [Vayda Douglas L](https://openairdocs.org/faa-owner/VAYDA%20DOUGLAS%20L), [Crescent City, FL](https://openairdocs.org/faa-place/FL/Crescent%20City), built 2004, S/N 9971CC
- [N5959K](https://openairdocs.org/aircraft/N5959K): [Kilo-Kilo LLC](https://openairdocs.org/faa-owner/KILO-KILO%20LLC), [Wausau, WI](https://openairdocs.org/faa-place/WI/Wausau), built 2004, S/N 9972CC
- [N65EJ](https://openairdocs.org/aircraft/N65EJ): [Robbins Lesley Linn](https://openairdocs.org/faa-owner/ROBBINS%20LESLEY%20LINN), [Bend, OR](https://openairdocs.org/faa-place/OR/Bend), built 2003, S/N 9959CC
- [N67XX](https://openairdocs.org/aircraft/N67XX): [Lane Aviation Inc](https://openairdocs.org/faa-owner/LANE%20AVIATION%20INC), [Rosenberg, TX](https://openairdocs.org/faa-place/TX/Rosenberg), built 2003, S/N 9958CC
- [N912S](https://openairdocs.org/aircraft/N912S): [Hamlin Edward D](https://openairdocs.org/faa-owner/HAMLIN%20EDWARD%20D), [Ward Cove, AK](https://openairdocs.org/faa-place/AK/Ward%20Cove), built 2004, S/N 9973CC
- [N955DW](https://openairdocs.org/aircraft/N955DW): [Witham David](https://openairdocs.org/faa-owner/WITHAM%20DAVID), [Sandpoint, ID](https://openairdocs.org/faa-place/ID/Sandpoint), built 2004, S/N 9969CC

## NTSB investigations (5)

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 ERA24LA128](https://openairdocs.org/ntsb/ERA24LA128), Mar 1, 2024: Cub Crafters PA18-150 (N143CC), Edgewater, FL, substantial damage. Probable cause: Maintenance personnel’s failure to detect the worn aileron cable during the most recent inspections, which resulted in the separation of the aileron control cable and a subsequent loss of airplane…
- [NTSB CEN18LA125](https://openairdocs.org/ntsb/CEN18LA125), Mar 21, 2018: Cub Crafters PA18 150 (N226JK), Beggs, OK, substantial damage. Probable cause: The pilot's failure to verify that the fuel selector was properly set before takeoff, which resulted in a total loss of engine power due to fuel starvation.
- [NTSB CEN17FA050](https://openairdocs.org/ntsb/CEN17FA050), Dec 7, 2016: Cub Crafters PA18 (N444GB), Basin, WY, substantial damage, 1 fatal. Probable cause: The pilot exceeded the airplane's critical angle of attack while maneuvering at low altitude, which resulted in an inadvertent aerodynamic stall and subsequent impact with terrain.
- [NTSB WPR09CA127](https://openairdocs.org/ntsb/WPR09CA127), Feb 23, 2009: Cub Crafters PA-18-150 (N324A), Buckeye, AZ, substantial damage. Probable cause: The pilot's failure to maintain directional control.
- [NTSB ANC05LA052](https://openairdocs.org/ntsb/ANC05LA052), Mar 27, 2005: Cub Crafters PA-18 (N955DW), Fairbanks, AK, substantial damage. Probable cause: The flight instructor's inadequate supervision of the flight, and the dual student's failure to maintain directional control.

## FAA accident and incident reports (8)

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.

- [Accident 20240301006319A](https://openairdocs.org/incident/20240301006319A), Mar 1, 2024: Cub Crafters PA18-150 (N143CC), New Smyrna Beac, FL, Destroyed. Pilot explained that he circled around the airport for landing after dropping off a banner. Whike on final approach and about 50 feet, an airleron cable…
- [Incident 20200214002539I](https://openairdocs.org/incident/20200214002539I), Feb 14, 2020: Cub Crafters PA18-150 (N65EJ), Salem, OR, Minor damage. Pilot was taxiing N65EJ to runway 34/16 for departure. As the aircraft approached the runway, the pilot applied the heel brakes and the aircraft tipped over on…
- [Accident 20180321009819A](https://openairdocs.org/incident/20180321009819A), Mar 21, 2018: Cub Crafters PA18-150 (N226JK), Beggs, OK, Substantial damage. The private pilot and private pilot rated passenger where flying a day VFR part 91 local flight. The pilot stated the aircraft had flown 4 days prior to the…
- [Accident 20161207021889A](https://openairdocs.org/incident/20161207021889A), Dec 7, 2016: Cub Crafters PA18-150 (N444GB), Basin, WY, Destroyed, 1 fatal. Investigation of accident appears to be the result of pilot's loss of control of aircraft. Stall spin.
- [Accident 20090223003899A](https://openairdocs.org/incident/20090223003899A), Feb 23, 2009: Piper PA18150 (N324A), Buckeye, AZ, Substantial damage. (-23) [privacy data omitted] was flying a cub crafters super cub. After landing roll out the aircraft veered left, the pilot corrected with right rudder pedal,…
- [Accident 20050327006549A](https://openairdocs.org/incident/20050327006549A), Mar 27, 2005: Piper PA18150 (N955DW), Fairbanks, AK, Substantial damage. (-23) [privacy data omitted] during rollout from the third, full stall, 3 point, stop and go landing, the aircraft ground looped to the left. No left aileron…
- [Incident 20050325004999I](https://openairdocs.org/incident/20050325004999I), Mar 25, 2005: Piper PA18150 (N143CC), Hemby Bridge, NC, Minor damage. (-23) Pilot was practicing a short field landing. He was almost stopped when he hit the heel brakes too hard and flipped the aircraft over.
- [Incident 20050208001799I](https://openairdocs.org/incident/20050208001799I), Feb 8, 2005: Piper PA18150 (N955DW), Fairbanks, AK, Minor damage. (-23) On 02/05/2005, the pilot stated, shortly after takeoff, he noticed the oil pressure light illuminated and oil streaks on the cowling. He returned to fai…

## Service difficulty reports (73, newest 50)

As reported by operators and repair stations, by the model named in the report.

- [SDR 2026F00198](https://openairdocs.org/sdr/2026F00198), Nov 9, 2025: CYLINDER. DAMAGED. ORIGINAL INSTALL DATE 8-28-2023. NEW CYLINDERS REMOVED AT 434HRS BY MECHANIC DUE TO RING FLUTTER, RING CHATTER, WASHBOARDING. INCONSISTENT METAL WEAR PATTERN ON
- [SDR 2022FA0000554](https://openairdocs.org/sdr/2022FA0000554), Sep 27, 2022: TORQUE TUBE. BROKEN. RH ELEVATOR TORQUE TUBE CRACKED/SEVERED/FAILED. MAIN SPAR TUBE FAILED JUST OUTBOARD OF OUTBOUND HINGE ATTACHMENT. FOUND DURING PRE-FLIGHT.
- [SDR 2022FA0000551](https://openairdocs.org/sdr/2022FA0000551), Sep 23, 2022: CARBURETOR. MISOVERHAULED. DURING DESCENT AND THROTTLE REDUCTION INTO KBZN, THIS AIRCRAFT EXPERIENCED A POWER LOSS DUE TO A HYDRAULIC LOCKING OF THE ACCELERATOR PUMP IN THE CARBURETOR. TH
- [SDR AQHR20150306001](https://openairdocs.org/sdr/AQHR20150306001), Mar 5, 2015: G SWITCH. FAULTY. "G" SWITCH WOULD NOT ACTIVATE ELT DURING REQUIRED INSPECTION.
- [SDR 2012FA0000821](https://openairdocs.org/sdr/2012FA0000821), Dec 1, 2012: DRAIN VALVE. FAILED. FUEL DRAIN VALVE CAME APART SHORTLY AFTER INSTALLATION CAUSING ALL OF THE FUEL IN THAT WING TO GUSH OUT. THE CENTER RETAINING RING FAILED ALLOWING THE INNER SEA
- [SDR 2011FA0000578](https://openairdocs.org/sdr/2011FA0000578), May 1, 2011: ENGINE. MAKING METAL. THE ENGINE NEVER DEVELOPED RATED HP. SINCE NEW. THEN FAILED TO MEET STATIC RPM. THE ENGINE ALWAYS GENERATED AN EXCESSIVE AMOUNT OF METAL. OIL SCREEN WAS CHECKED
- [SDR 2010FA0001123](https://openairdocs.org/sdr/2010FA0001123), Oct 19, 2010: DIPSTICK. BROKEN. OIL DIP STICK BROKE AND DROPPED INTO CRANKCASE. DIP STICK TUBE EXTENSION IS INSTALLED AND DIP STICK ANCHORED END FITS INTO CAP CASTING AND IS SECURED BY A ROLL 
- [SDR CA100813006](https://openairdocs.org/sdr/CA100813006), Aug 11, 2010: ENGINE. MAKING METAL. (CAN) DURING ROUTINE (50 HR) INSP OF THE ENGINE - METAL SHAVINGS WERE FOUND WHEN THE OIL SCREEN WAS CHECKED. METAL SHAVINGS WERE CONFIRMED BY A MAGNET TO BE STE
- [SDR CA091105002](https://openairdocs.org/sdr/CA091105002), Nov 2, 2009: CONTROL CABLE. FRAYED. (CAN) DURING AN INSP WHICH INCLUDED REMOVING THE FLOOR, THE AME NOTICED A SHINY SPOT ON THE RT AILERON CABLE WHERE IT PASSES A PULLY AND MEETS THE FUSELAGE. UPO
- [SDR 2007FA0001010](https://openairdocs.org/sdr/2007FA0001010), Nov 1, 2007: PIPE. FAILED. LEADING EDGE EXHAUST SYSTEM INSTALLED BY STC SA02200AK FAILED AT THE SAIL PIPE TO MUFFLER WELD. SYSTEM HAS 36 HOURS SINCE NEW. (K)
- [SDR 2007FA0000980](https://openairdocs.org/sdr/2007FA0000980), Oct 19, 2007: MUFFLER. BROKEN. THE TAILPIPE CRACKED AWAY FROM THE SHELL. THERE ARE NO STRAPS WELDED FROM THE PIPE TO THE SHELL LIKE SOME OTHER MUFFLERS. THE METAL FAILED, NOT THE WELD.
- [SDR 2007FA0000799](https://openairdocs.org/sdr/2007FA0000799), Sep 5, 2007: MUFFLER. BROKEN. ENGINE EXHAUST TAIL PIPE FAILED AT THE MUFFLER WELD. WITH 36 HOURS TOTAL TIME SINCE NEW. LEADING EDGE EXHAUST SYSTEM WAS INSTALLED BY STC SA02200AK.
- [SDR 2007FA0000693](https://openairdocs.org/sdr/2007FA0000693), Jun 21, 2007: BOLT. LOOSE. PILOT REPORTED SLIGHT VIBRATION DURING FLIGHT OF APPROX (1) HOUR. WHEN POWER WAS REDUCED FOR LANDING, VIBRATION BECAME MORE EVIDENT. INITIAL INSP FOUND (1) PROP
- [SDR CA060905002](https://openairdocs.org/sdr/CA060905002), Aug 30, 2006: BOLT. SHEARED. (CAN) DURING A ROUTINE INSPECTION OF THE AIRCRAFT, IT WAS DISCOVERED THAT THE FORWARD LT LANDING GEAR ATTACH BOLT WAS LOOSENED IN THE FUSELAGE ATTACH FITTING. C
- [SDR 2006FA0000885](https://openairdocs.org/sdr/2006FA0000885), Aug 12, 2006: MUFFLER. CRACKED. DURING ANNUAL INSP FOUND CRACK AT END OF ONE SUPPORT BRACE WITH EVIDENCE OF EXHAUST LEAK. ADVISED OWNER, HE SAID HE HAD EXPERIENCED EXHAUST LEAKAGE WITH MILD NO
- [SDR CA051221003](https://openairdocs.org/sdr/CA051221003), Dec 2, 2005: LONGERON. ROTTED. UPPER RT LONGERON AT TAIL WAS ROTTED. TUBING WAS REPLACED AS REQUIRED.
- [SDR 2005FA0001630](https://openairdocs.org/sdr/2005FA0001630), Nov 7, 2005: FUEL TANK. LEAKING. LT FUEL TANK WAS LEAKING. PILOT ADVISED US OF LEAK. WE DRAINED BOTH TANKS AND TURNED THEM INTO REP. THEY ADVISED US THERE WAS AS/L ON BOTH TANKS. WERE REMOVED A
- [SDR L7C2005F00000](https://openairdocs.org/sdr/L7C2005F00000), Jul 18, 2005: ELT. INOPERATIVE. ELT REMOTE WOULD NOT ACTIVATE. ELT LIGHT WOULD COME ON BUT DID NOT TRANSMIT. INSTALLED IN AC FOR LESS THAN 4 YEARS. (K)
- [SDR 2005FA0000838](https://openairdocs.org/sdr/2005FA0000838), Jun 3, 2005: CONVERTER. FAILED. CONVERTER WAS INSTALLED IAW MFG INSTRUCTIONS, DIAGRAMS AND INSTALLATION WAS APPROVED WITH A 337. CONVERTER FAILED IN LESS THAN 10 SECONDS. OUT OF FIVE CONVERTER
- [SDR 2005FA0000655](https://openairdocs.org/sdr/2005FA0000655), Apr 26, 2005: FITTING. CRACKED. DURING AN ANNUAL INSPECTION THE LT FRONT CABANE V ATTACH POINT ON THE FUSELAGE WAS FOUND TO BE CRACKED. THIS IS THE SECOND AIRCRAFT IN THE LAST MONTH THAT WAS F
- [SDR 2005FA0000173](https://openairdocs.org/sdr/2005FA0000173), Oct 12, 2004: LINK. FAILED. ON LANDING ROLLOUT, AIRCRAFT DRIFTED TO THE LT AND WENT INTO SOFT GROUND, COMING TO REST ON IT`S NOSE. FOUND LINK (PN 472681) PARTIALLY STRAIGHTENED, CAUSING TH
- [SDR 2004FA0000686](https://openairdocs.org/sdr/2004FA0000686), Jul 8, 2004: OIL COOLER. FAILED. INSTALLED OVERHAULED OIL COOLER, TO AIRCRAFT ON 4/30/04, TACH 2028.5. NO LEAKS AT RUN UP. AFTER INSTALL AND NO LEAKS NOTICED AFTER TAXI TO HANGER. AIRCRAFT WAS 
- [SDR AUS20040138](https://openairdocs.org/sdr/AUS20040138), Feb 22, 2004: LONGERON. CRACKED. (AUS) UPPER LT LONGERON TUBE CRACKED IN AREA BETWEEN FORWARD WELD OF LT REAR STABILIZER SUPPORT AND FORWARD WELD OF CROSS BRACE TUBE.
- [SDR 2004FA0000188](https://openairdocs.org/sdr/2004FA0000188), Feb 6, 2004: SELECTOR VALVE. BROKEN. PILOT TURNED FUEL VALVE TO CHECK FOR SMOOTH OPERATION AND DETENTS ON THE FUEL SELECTOR VALVE AS DIRECTED BY FLIGHT INSTRUCTOR. INSTRUCTOR HEARD (FUNNY SOUND) CO
- [SDR DHL200374248](https://openairdocs.org/sdr/DHL200374248), Dec 16, 2003: STEP. CORRODED. DURING C-CHECK, RIGHT AFT AIRSTAIR STEP SUPPORT AT STEP 10 FROM THE BOTTOM IS CORRODED. REMOVED DAMAGED ANGLE FROM RT AFT AIRSTAIR NR 10 STEP AND FABRICATED NEW
- [SDR DHL200374247](https://openairdocs.org/sdr/DHL200374247), Dec 4, 2003: SKIN. DELAMINATED. DURING C-CHECK, LEFT HAND INBOARD FORE FLAP UPPER SKIN DELAMINATED AT OUTBOARD END. CUT OUT UPPER SKIN DELAMINATION APPROX 1.7 INCH DIA & DOUBLER APPROX 4 X 4.7
- [SDR DHL200374246](https://openairdocs.org/sdr/DHL200374246), Dec 2, 2003: SKIN. SEPARATED. DURING A C-CHECK, LT WING OUTBOARD AILERON HAS THREE LOOSE RIVETS IN UPPER SKIN. REMOVED OLD SKIN FOR LT WING O/B AILERON IAW B727 SRM 51-30-2, FABRICATED NEW S
- [SDR 2003FA0001288](https://openairdocs.org/sdr/2003FA0001288), Sep 11, 2003: CONTROL CABLE. FRAYED. RUDDER CABLE WAS FRAYED WHERE IT PASSES THROUGH THE FAIRLEADS, 5 OUT OF 7 BUNDLES WERE CUT THROUGH THE STAINLESS STEEL CABLE.
- [SDR 2003FA0000783](https://openairdocs.org/sdr/2003FA0000783), Jul 1, 2003: BARREL. DAMAGED. UPON INSPECTION FOUND TURN BARREL THAT HAS GROOVE FOR CLIPS SPLIT LOCATION UPPER RT ALIRON TURNBUCKLE ONLY FOUND THESE STYLE TURN BARRELS THAT DONT REQUIRE SAFE
- [SDR CA030529003](https://openairdocs.org/sdr/CA030529003), May 23, 2003: STITCHING. BROKEN. (CAN) RIB STICHING BROKEN MOST RIBS RT WING RECORDS. ONLY GO BACK TO 1978 NO RECORD OF REPLACEMENT AT THAT TIME. FABRIC TESTED GOOD. (WING RESTITCHED.)
- [SDR CA030409006](https://openairdocs.org/sdr/CA030409006), Apr 7, 2003: BOLT. SHEARED. (CAN) GROUND CREW WAS MOVING THE AIRCRAFT ON RAMP AND RAN TAILWHEEL OF AIRCRAFT OVER SMALL ICE RIDGE IN ORDER TO GAIN ACCESS TO POSITION FOR PARKING. JOLT FROM 
- [SDR GJR2002F00000](https://openairdocs.org/sdr/GJR2002F00000), Aug 26, 2002: FUEL TANK. CRACKED. CRACK WAS FOUND ALONG THE LOWER SEAM ON THE INBOARD SIDE. APPLICATION 180HP FLOAT PLANE. INSUFFICIENT AMOUNT OF MATERIAL ALONG WELDED SEAMS.
- [SDR 2002FA0000957](https://openairdocs.org/sdr/2002FA0000957), Jul 26, 2002: EXHAUST VALVE. FRACTURED. AIRCRAFT EXPERIENCED PARTIAL LOSS OF POWER DUE TO FAILURE OF NR 3 CYLINDER EXHAUST VALVE. AIRCRAFT TERMINATED FLIGHT AND LANDED WITHOUT FURTHER INCIDENT.
- [SDR GJR2002F00001](https://openairdocs.org/sdr/GJR2002F00001), Jul 25, 2002: FUEL TANK. CRACKED. CRACK WAS FOUND ALONG THE LOWER SEAM ON THE OUTBOARD SIDE.
- [SDR 2001FA0000217](https://openairdocs.org/sdr/2001FA0000217), Jul 20, 2001: VALVE SEAT. LEAKING. DURING COMPRESSION CHECK, LOW CYLINDER PRESSURE WAS DISCOVERED. LEAKAGE WAS DETERMINED TO BE BETWEEN NUMBER FOUR CYLINDER INTAKE VALVE AND VALVE SEAT. AFTER REM
- [SDR 2001FA0000047](https://openairdocs.org/sdr/2001FA0000047), May 5, 2001: EXHAUST PIPE. CRACKED. FOUND WELD ON WYE PIPE CRACKED AT ANNUAL INSPECTION. (NO PARTS AVAILABLE AT THIS TIME) ALSO FOUND INNER BAFFLE ON SAME PIPE CRACKED.
- [SDR 2002FA0000221](https://openairdocs.org/sdr/2002FA0000221), Jan 25, 2001: CYLINDER. CRACKED. ENGINE INSTALLED IN FEBRUARY 1997. AT APPROXIMATELY 665 HOURS, TWO CYLINDERS WERE CRACKED THROUGH THE FINS OUTSIDE THE EXHAUST PORT, ADJACENT TOTHE EXHAUSE SEAT
- [SDR 20001120SH062](https://openairdocs.org/sdr/20001120SH062), Oct 25, 2000: ROCKER BOSS. OUT OF POSITION. CYLINDER HAD LOW COMPRESSION. WHEN ROCKER BOSS COVER WAS REMOVED, THE EXHAUST SIDE OF ROCKER SHAFT BOSS WAS FOUND IN BOTTOM OF COMPARTMENT. CHROME CYLINDER WAS 
- [SDR AU001137](https://openairdocs.org/sdr/AU001137), Aug 2, 2000: PROPELLER. UNAPPROVED PART. (AUS) INCORRECT PROPELLER FITTED TO AIRCRAFT. PERSONNEL/MAINTENANCE ERROR. UNAPPROVED PART.
- [SDR CA000724019](https://openairdocs.org/sdr/CA000724019), Jul 6, 2000: SCREW. MISSING. (CAN) THIS REPORT FOLLOWS LANDING INCIDENT. NO RIGHT BRAKE. AIRCRAFT LANDED AND PILOT CNTLLED A/C ONTO ECHO TAXIWAY. SHUT DOWN AND PUSHED A/C OFF TAXIWAY BY HAN
- [SDR CA000614023](https://openairdocs.org/sdr/CA000614023), Jun 2, 2000: CHANNEL. CRACKED. (CAN) DURING INSPECTION, CRACK WAS FOUND ON ONE VERTICAL MEMBER FROM CHANNEL. WHEN THE RIGHT HAND WING WAS REMOVED TO CARRY OUT REPAIR, THE WELDS ON THE ADJACEN
- [SDR AU000365](https://openairdocs.org/sdr/AU000365), May 5, 2000: CONTROL CABLE. WORN. (AUS) RIGHT AILERON CONTROL CABLES WORN BEYOND LIMITS IN THE AREA OF THE OUTER GUIDES.
- [SDR 20000413SH045](https://openairdocs.org/sdr/20000413SH045), Jan 2, 2000: SHAFT. DAMAGED. 1,590.6 HRS SINCE FACTORY NEW ENGINE INSTALLED. CRANKSHAFT APPEARED TO BE BINDING WITH SPARK PLUGS REMOVED. METAL (STEEL & ALUM) IN SCREENS. UPON REMOVAL OF MAG
- [SDR 99ZZZX4419](https://openairdocs.org/sdr/99ZZZX4419), Dec 9, 1999: GEAR. CRACKED. OIL PUMP CRACKED. KIT INSTALLED (LOG BOOK ENTRY) 12-19-86.
- [SDR CA990907022](https://openairdocs.org/sdr/CA990907022), Aug 26, 1999: FUEL TANK. DELAMINATED. (CAN) DURING A 100 HR INSPECTION, WHITE PARTICULATE WAS FOUND IN FUEL STRAINER AND RIGHT FUEL SIGHT GAUGE. WHEN SUMP DRAIN WAS REMOVED, A LARGE AMOUNT OF WHITE 
- [SDR 99ZZZX3405](https://openairdocs.org/sdr/99ZZZX3405), Aug 20, 1999: BLADE. FRACTURED. APPROXIMATELY 5 INCHES OF ONE PROPELLER BLADE TIP DEPARTED AIRCRAFT IN-FLIGHT. A SUCCESSFUL EMERGENCY LANDING WAS MADE. PROPELLER HAD BEEN RECONDITIONED AFTER P
- [SDR 99ZZZX631](https://openairdocs.org/sdr/99ZZZX631), Dec 7, 1998: BUSHING. WORN. ENGINE IS FACTORY REMANUFACTURED 2-11-98. MAGNETO DROP GOOD PREVIOUSLY. WOULD NOT START, NEXT FLIGHT. BRASS BUSHING IN DISTRIBUTOR BLOCK WORN BADLY.
- [SDR 99ZZZX630](https://openairdocs.org/sdr/99ZZZX630), Dec 7, 1998: BUSHING. WORN. ENGINE IS FACTORY REMANUFACTURED 2-11-98. MAGNETO GOOD, PREVIOUSLY WOULD NOT START, NEXT FLIGHT. BRASS BUSHING IS DISTRIBUTOR BLOCK WORN BADLY.
- [SDR 98ZZZX4512](https://openairdocs.org/sdr/98ZZZX4512), Oct 19, 1998: OIL COOLER. MALFUNCTIONED. PILOT STATES THAT OIL TEMPERATURE DOES NOT GO ABOVE 140 DEGREES FAHRENHEIT IN-FLIGHT OPS. LYCOMING REQUIRES 170 DEGREES PLUS PER OPERATOR'S MANUAL. SUBMITTER FO
- [SDR 98ZZZX4511](https://openairdocs.org/sdr/98ZZZX4511), Oct 19, 1998: MUFFLER. CORRODED. MUFFLER ASSY BAIL HAS CORRODED AWAY DUE TO 180 HP PER STC NR SA92NW AND LACK OF INSPECTION OF AD 68-05-01 AND OPERATOR COMPLIANCE. SUBMITTER RECOMMENDED EVERY 1

All 73: https://openairdocs.org/model/cub-crafters-pa18-150/reports.md

## STCs that may be installed (OpenAirDocs) (414, first 50)

Approved for this model: the STC's model list names it on its data sheet, or a series that includes it. In force first, then newest. The registry doesn't record which STCs an aircraft has.

- [STC SA01233SE](https://openairdocs.org/stc/SA01233SE): Fabrication and installation of Alaskan Bushwheel LLC tail wheel and fork assembly. ABI, LLC
- [STC SA02571SE](https://openairdocs.org/stc/SA02571SE): Installation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display). Garmin International Inc
- [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 SA12428CH](https://openairdocs.org/stc/SA12428CH): Installation of the Lycoming Engines Electronic Ignition System (EIS). Lycoming Engines, An Operating Division of AVCO Corporation
- [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 SA12406WI](https://openairdocs.org/stc/SA12406WI): Installation of a Garmin AXIS Flight Display System. Garmin International Inc
- [STC SA04652CH](https://openairdocs.org/stc/SA04652CH): To allow use of 100R grade aviation fuel meeting Swift Fuel, LLC specification. Swift Fuels LLC
- [STC SA02636SE](https://openairdocs.org/stc/SA02636SE): Installation of Garmin GPS 175 Navigation System and GNX 375 Navigation System with ADS-B In/Out Transponder. Garmin International 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 SA01147WI](https://openairdocs.org/stc/SA01147WI): Installation of Concorde FLA or VRSLA series batteries in Piper Light Airplanes. Concorde Battery Corporation
- [STC SA02511SE](https://openairdocs.org/stc/SA02511SE): Installation of replacement fuel quantity indicator sending unit(s). CiES Inc
- [STC SA02525LA](https://openairdocs.org/stc/SA02525LA): Installation of Wheel and Brake Assemblies. Game Aerospace LLC
- [STC SA01704LA](https://openairdocs.org/stc/SA01704LA): Installation of the Grove Disk Brake System. Grove Aircraft Landing Gear Systems Inc
- [STC SA02211AK](https://openairdocs.org/stc/SA02211AK): Installation of components to change thrust line orientation. Steve Pierce
- [STC SA00081NY](https://openairdocs.org/stc/SA00081NY): Installation of Iceman Aviation Supplies, Inc. Carburetor Ice Detector. Alcor LLC
- [STC SA02200AK](https://openairdocs.org/stc/SA02200AK): Fabrication of replacement engine exhaust system assembly (P/N PA18ESA). Power Flow Systems Inc
- [STC SA02738CH](https://openairdocs.org/stc/SA02738CH): Installation of L-3 Communications Avionics Systems. Acron Aviation Inc
- [STC SA04046CH PAGE 2](https://openairdocs.org/stc/SA04046CH%20PAGE%202): Installation of L-3 GENESIS (TM) Electronic Standby Instrument System (ESI-500/MAG-500). Acron Aviation Inc
- [STC SA575WE](https://openairdocs.org/stc/SA575WE): Belly master spray system. Texas Transland LLC
- [STC SA7965SW](https://openairdocs.org/stc/SA7965SW): Application of fabric and polyurethane finishing system. Shady Aviation LLC
- [STC SA11854CH](https://openairdocs.org/stc/SA11854CH): Installation of modified exhaust system in lieu of original components. Dakota Cub Aircraft Inc
- [STC SA04378CH](https://openairdocs.org/stc/SA04378CH): Installation of an engine modified per STC SE04349CH. SureFly Partners Ltd
- [STC SA11841BO](https://openairdocs.org/stc/SA11841BO): Installation of T3 Tailwheel Suspension System suspension. T3 Tailwheel Suspension System
- [STC SA02764SE](https://openairdocs.org/stc/SA02764SE): Installation of Acme Aero Shock landing gear shock absorbers. Acme Suspensions LLC
- [STC SA02765SE](https://openairdocs.org/stc/SA02765SE): Installation of Acme Stinger tailwheel landing gear shock absorber. Acme Suspensions LLC
- [STC SA02594SE](https://openairdocs.org/stc/SA02594SE): SkyView HDX Instrumentation and Autopilot System manufactured. Dynon Avionics
- [STC SA02386AK](https://openairdocs.org/stc/SA02386AK): Replacement of existing landing and/or taxi light reflector and bulbs with Light Emitting Diode (LED) lighting systems. AeroLED's Holding LLC
- [STC SA03898NY](https://openairdocs.org/stc/SA03898NY): Installation and maintenance of ORATEX covering and coating material. Aircraft Design & Certification Ltd
- [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 SA02580AK](https://openairdocs.org/stc/SA02580AK): Installation of Airframes Alaska Replacement Suspension. Airframes Alaska LLC
- [STC SA02191AK](https://openairdocs.org/stc/SA02191AK): Fabrication and installation of Dakota Cub extended wings and associated flaps and ailerons. Dakota Cub Aircraft Inc
- [STC SA02582AK](https://openairdocs.org/stc/SA02582AK): Installation of Airframes Alaska Brake Pedal and Master Cylinder Assembly. Airframes Alaska LLC
- [STC SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc
- [STC SA02579AK](https://openairdocs.org/stc/SA02579AK): Installation of Swing bar. Willow Mountain Ranch
- [STC SA02532AT](https://openairdocs.org/stc/SA02532AT): Installation of subject Michelin tires on appropriate aircraft. For Michelin 5, 6, 8, and 10-inch rim diameter tires on General Aviation Aircraft. Michelin North America Inc
- [STC SA00715AT](https://openairdocs.org/stc/SA00715AT): Installation of Aqua Floats Model 2200. Outpost X Aviation Inc
- [STC SA518CE](https://openairdocs.org/stc/SA518CE): Install Aqua Model 1900 floats. Outpost X Aviation Inc
- [STC SA01899WI](https://openairdocs.org/stc/SA01899WI): Installation of Garmin G3X Touch Electronic Flight Instrument System. Garmin International Inc
- [STC SA04563AT](https://openairdocs.org/stc/SA04563AT): Installation of Sensenich propeller model 2G0M6 C82BGF or 2G0M7 C82BGF. Sensenich Propeller Company
- [STC SP04490AT](https://openairdocs.org/stc/SP04490AT): Installation of Sensenich propeller model 2G0M8/C82BGF. Sensenich Propeller Company
- [STC SA02576AK](https://openairdocs.org/stc/SA02576AK): Installation of Cleveland and ABI, LLC Wheel and Brake Kits. ABI LLC
- [STC SA02233AK](https://openairdocs.org/stc/SA02233AK): Installation of high visibility fuel sight gauge. Dakota Cub Aircraft Inc
- [STC SA00417BO](https://openairdocs.org/stc/SA00417BO): Installation of T3 Tailwheel Suspension Systems Suspension. T3 Tailwheel Suspension Systems
- [STC SA02175AK](https://openairdocs.org/stc/SA02175AK): Fabrication of Airframes Alaska LLC Heavy Duty Standard Length or 3-inch Extended Main Landing Gear. Airframes Alaska LLC
- [STC SA01606CH](https://openairdocs.org/stc/SA01606CH): Installation of alternate electro-hydraulic power pack system for operation of main wheel skis. F.Atlee Dodge Aircraft Services
- [STC SA3-180](https://openairdocs.org/stc/SA3-180): Installation of Wipaire Skis, Inc. (Aircraft Skis) (FluiDyne) (Federal) Main Skis, Model C2200, Tail Ski, Model CTF2200 or CT3000, and Parts Kit No. W-PMA-001, issued February 26, 2001. F.Atlee Dodge Aircraft Services
- [STC SA3-328](https://openairdocs.org/stc/SA3-328): Installation of Model C-2200 main skis and Model AWT-2500 or AWT-2500A tail wheel skis. F.Atlee Dodge Aircraft Services
- [STC SA02987CH](https://openairdocs.org/stc/SA02987CH): Installation of the Electroair Electronic Ignition System. Electroair Acquisition Corporation
- [STC SA44AL](https://openairdocs.org/stc/SA44AL): Auxiliary wing fuel tanks. Wilbur Repair Service Marquerite Benson or Anne Wilbur

All 414: https://openairdocs.org/model/cub-crafters-pa18-150/stcs.md

## PMA parts (OpenAirDocs) (595, first 50)

Current parts manufacturer approvals (PMA): parts the FAA has approved companies to make as replacements or modifications. Each record lists its models as free text; OpenAirDocs matched them to this model on its data sheet, so check the FAA record before relying on it. Newest first.

- [73-CFG-R](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID139218545420260806152425.0001): Fuel Quantity Indication Placard. Swift Fuels, LLC · PMA PQ04423CE · Modification part · Jul 20, 2026
- [S1069](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID113256326820260806152332.0001): 100R Fuel Placard. Swift Fuels, LLC · PMA PQ04423CE · Modification part · Jul 20, 2026
- [210608](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID126781545220260701191843.0001): G35 Foam Insert. EarthX, Inc. · PMA PQ05466NM · Modification part · Jun 4, 2026
- [V674903-91](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID157004670620260423211206.0001): Leaded and Unleaded Automotive Gasoline. Air Plains Services Corp · PMA PQ3524CE · Modification part · Aug 29, 2025
- [300001-AS-AAD-AA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID189018217420260513140941.0001): Shock Assembly, Cub 3.0+ Length, Heavy. ACME Aero Suspensions LLC · PMA PQ00058EB · Replaces 300001-AS-AAD-AA · Jul 8, 2025
- [200000-AS-AAS-AA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID166566609020260513140945.0001): Stinger Dual Bolt Standard Shock. ACME Aero Suspensions LLC · PMA PQ00058EB · Replaces 200000-AS-AAS-AA · Jul 8, 2025
- [200002-AS-AAS-AA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID156408866720260513140948.0001): Stinger Dual Bolt Light Shock. ACME Aero Suspensions LLC · PMA PQ00058EB · Replaces 200002-AS-AAS-AA · Jul 8, 2025
- [200001-AS-AAS-AA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID155190170020260513140947.0001): Stinger Single Bolt Standard Shock. ACME Aero Suspensions LLC · PMA PQ00058EB · Replaces 200001-AS-AAS-AA · Jul 8, 2025
- [300000-AS-AAD-AA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID153279178820260513140940.0001): Shock Assembly, Cub Standard Length, Heavy. ACME Aero Suspensions LLC · PMA PQ00058EB · Replaces 300000-AS-AAD-AA · Jul 8, 2025
- [300003-AS-AAD-AA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID147563753420260513140944.0001): Shock Assembly, Cub 3.0+ Length, Light. ACME Aero Suspensions LLC · PMA PQ00058EB · Replaces 300003-AS-AAD-AA · Jul 8, 2025
- [300002-AS-AAD-AA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID133785033820260513140942.0001): Shock Assembly, Cub Standard Length, Light. ACME Aero Suspensions LLC · PMA PQ00058EB · Replaces 300002-AS-AAD-AA · Jul 8, 2025
- [200003-AS-AAS-AA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID124450920320260513140950.0001): Stinger Single Bolt Light Shock. ACME Aero Suspensions LLC · PMA PQ00058EB · Replaces 200003-AS-AAS-AA · Jul 8, 2025
- [LSM-200-700-11](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID187312814920250417183925.0001): Hub Cap Assy. Whelen Aerospace Technologies · PMA PQ1372CE · Modification part · Dec 10, 2024
- [110HS](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID193059656020240221142908.0001): Drain Valve Assembly. Saf-Air Products Inc · PMA PQ2036CE · Replaces CAV-110H-4 · Jan 30, 2024
- [110SS](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID184612663120240221142904.0001): Drain Valve Assembly. Saf-Air Products Inc · PMA PQ2036CE · Replaces CAV-110 · Jan 30, 2024
- [APS66-10600](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID143804207420221020170319.0001): Brake Lining. Aviation Products Systems Inc · PMA PQ3830CE · Replaces 066-10600 · Aug 10, 2022
- [APS105-00200](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID117355682120221020170415.0001): Rivet. Aviation Products Systems Inc · PMA PQ3830CE · Replaces 105-00200 · Aug 10, 2022
- [AF18-4](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID831508475420210727025117.0001): 4 Inch Wider Frame Assembly Fuselage. Airframes Alaska LLC · PMA PQ3848CE · Modification part · Jun 28, 2021
- [AF18](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID603508801520210727025115.0001): Frame Assembly Fuselage. Airframes Alaska LLC · PMA PQ3848CE · Modification part · Jun 28, 2021
- [409-00003-002](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID389167083420210702175234.0001): Internal Battery Pack, Refresh. Aspen Avionics · PMA PQ03868SW · Modification part · Jan 20, 2021
- [V674UL94](https://drs.faa.gov/browse/excelExternalWindow/E1C1EF6CEE5DC2EE862585990051C803.0001): UL94 Fuel Placard. Swift Fuels, LLC · PMA PQ04423CE · Modification part · Jun 7, 2020
- [CC15723-00](https://drs.faa.gov/browse/excelExternalWindow/CAC3C5DDB21989FE86258593004FF0A6.0001): Leading Edge Tip Cover, Left Hand. Carbon Concepts LLC · PMA PQ04422CE · Replaces 15723-00 15723-000 · Mar 1, 2020
- [CC15723-01](https://drs.faa.gov/browse/excelExternalWindow/609390B635512F5286258593004FF0DB.0001): Leading Edge Tip Cover, Right Hand. Carbon Concepts LLC · PMA PQ04422CE · Replaces 15723-01 15723-001 · Mar 1, 2020
- [2103](https://drs.faa.gov/browse/excelExternalWindow/B20F0FB3FB4275E386258439006DFBD4.0001): Extended Baggage Compartment. F Atlee Dodge Aircraft Services LLC · PMA PQ2509CE · Modification part · Dec 18, 2019
- [9100-001-C](https://drs.faa.gov/browse/excelExternalWindow/DD343890DCD8BFDB86258569004013FB.0001): MaxDim Lamp Intensity Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019
- [9100-001-D](https://drs.faa.gov/browse/excelExternalWindow/C7B6725B325949E98625856900401478.0001): MaxDim Lamp Intensity Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019
- [9200-000-B](https://drs.faa.gov/browse/excelExternalWindow/BD58B0712CA0C6AA86258569004016AD.0001): MaxPulse Landing Light Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019
- [9100-001-G](https://drs.faa.gov/browse/excelExternalWindow/ADE62C91D97E8B788625856900401557.0001): MaxDim Lamp Intensity Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019
- [9100-001-E](https://drs.faa.gov/browse/excelExternalWindow/A37F050253EE808A86258569004014BA.0001): MaxDim Lamp Intensity Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019
- [9200-000-A](https://drs.faa.gov/browse/excelExternalWindow/8E10EF4D973C1D6D8625856900401662.0001): MaxPulse Landing Light Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019
- [9100-001-A](https://drs.faa.gov/browse/excelExternalWindow/62DC748A2B9B1D9386258569004012FD.0001): MaxDim Lamp Intensity Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019
- [9100-001-F](https://drs.faa.gov/browse/excelExternalWindow/3746AAB4CC0D6883862585690040151B.0001): MaxDim Lamp Intensity Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019
- [9100-001-B](https://drs.faa.gov/browse/excelExternalWindow/32446D71EB78157686258569004013B2.0001): MaxDim Lamp Intensity Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019
- [9100-001-H](https://drs.faa.gov/browse/excelExternalWindow/1AEB415100FB45D8862585690040159F.0001): MaxDim Lamp Intensity Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019
- [3286-1](https://drs.faa.gov/browse/excelExternalWindow/B76C2E0C5EE6D037862584A5005D85D2.0001): Wing Tank Sight Gage. F Atlee Dodge Aircraft Services LLC · PMA PQ2509CE · Modification part · Apr 14, 2019
- [AF14457-00](https://drs.faa.gov/browse/excelExternalWindow/D3A943F4EC5D17308625849E005B5E88.0001): Baffle assembly. Airforms LLC · PMA PQ2644CE · Replaces 14457-00 · Apr 3, 2019
- [AF14456-00](https://drs.faa.gov/browse/excelExternalWindow/87BABE22F331EC758625849E005B5E75.0001): Baffle assembly. Airforms LLC · PMA PQ2644CE · Replaces 14456-00 · Apr 3, 2019
- [AF14452-00](https://drs.faa.gov/browse/excelExternalWindow/56419D3DB68177A98625849E005B5E4B.0001): Baffle assembly. Airforms LLC · PMA PQ2644CE · Replaces 14452-00 · Apr 3, 2019
- [AF14458-05](https://drs.faa.gov/browse/excelExternalWindow/33B63D0F7C7F4D088625849E005B5E9F.0001): Baffle assembly. Airforms LLC · PMA PQ2644CE · Replaces 14458-05 · Apr 3, 2019
- [AF14455-00](https://drs.faa.gov/browse/excelExternalWindow/2EC29135B68841708625849E005B5E61.0001): Baffle assembly. Airforms LLC · PMA PQ2644CE · Replaces 14455-00 · Apr 3, 2019
- [AF14467-07](https://drs.faa.gov/browse/excelExternalWindow/118864D5E94BF8DB8625849E005B5EB8.0001): Baffle assembly. Airforms LLC · PMA PQ2644CE · Replaces 14467-07 · Apr 3, 2019
- [3276](https://drs.faa.gov/browse/excelExternalWindow/40E5F35D6466C128862582BB0068A065.0001): Engine Cowling Top Channel Assembly. F Atlee Dodge Aircraft Services LLC · PMA PQ2509CE · Replaces Piper P/N 12362-03 · May 22, 2018
- [3277](https://drs.faa.gov/browse/excelExternalWindow/06F827E79D7F3430862582BB0068A067.0001): Engine Cowling Lower Channel Assembly. F Atlee Dodge Aircraft Services LLC · PMA PQ2509CE · Replaces Piper P/N 12364-03 and 12364-05 · May 22, 2018
- [3232W-2](https://drs.faa.gov/browse/excelExternalWindow/5DFCCCA00EC4A623862581F5005808DA.0001): Weld-on Shoulder harness attach Bracket (Rear). F Atlee Dodge Aircraft Services LLC · PMA PQ2509CE · Modification part · Nov 19, 2017
- [3232W-1](https://drs.faa.gov/browse/excelExternalWindow/3C50177848FDAC8F862581F5005808D8.0001): Weld-on Shoulder harness attach Bracket (Forward). F Atlee Dodge Aircraft Services LLC · PMA PQ2509CE · Modification part · Nov 19, 2017
- [MDL FWI660-90](https://drs.faa.gov/browse/excelExternalWindow/29970F80633E018B862581FB0062BFBF.0001): Tow Hook Install. Fliegen Works Inc · PMA PQ2380NM · Modification part · Nov 15, 2017
- [RR-1114.2](https://drs.faa.gov/browse/excelExternalWindow/FD7DE8E2D9349D178625816B0071DC1E.0001): Oil Cooler 10 Element. Rubbert Aircraft Services · PMA PQ4153CE · Modification part · Jul 24, 2017
- [R7/180-9](https://drs.faa.gov/browse/excelExternalWindow/E7B9FF8E9FCA865F8625816B0071D7E5.0001): Baffle Assembly- Left Rear (O-360 9 Ele.). Rubbert Aircraft Services · PMA PQ4153CE · Modification part · Jul 24, 2017
- [R7/150-10](https://drs.faa.gov/browse/excelExternalWindow/E2C94544C0918BAE8625816B0071D7A7.0001): Baffle Assembly- Left Rear (O-320 10 Ele.). Rubbert Aircraft Services · PMA PQ4153CE · Modification part · Jul 24, 2017
- [R11/180](https://drs.faa.gov/browse/excelExternalWindow/DA364CC62470C84B8625816B0071DADE.0001): Baffle Assembly- Right Front (O-320). Rubbert Aircraft Services · PMA PQ4153CE · Modification part · Jul 24, 2017

All of them: https://openairdocs.org/model/cub-crafters-pa18-150/pma.md

## The same model under other registry codes

Amateur-built copies and renamed makers get their own codes.

- [Piper PA-18-150](https://openairdocs.org/model/piper-pa-18-150): 2,054 registered aircraft, registry code 7101828
- [Piper/Cub Crafters PA-18-150](https://openairdocs.org/model/piper-cub-crafters-pa-18-150): 46 registered aircraft, registry code 7101843
- [Piper PA-18-150](https://openairdocs.org/model/piper-pa-18-150): 11 registered aircraft, registry code 7104221
- [Alaska Dept Of Public Safety PA-18 150](https://openairdocs.org/model/alaska-dept-of-public-safety-pa-18-150): 1 registered aircraft, registry code 056074T
- [Krupinski Floyd M PA-18-150](https://openairdocs.org/model/krupinski-floyd-m-pa-18-150): 1 registered aircraft, registry code 056156H
- [Cubs Unlimited/Piper PA 18-150](https://openairdocs.org/model/cubs-unlimited-piper-pa-18-150): 1 registered aircraft, registry code 05617YI
- [Ellis Wendell Kirk PA-18-150](https://openairdocs.org/model/ellis-wendell-kirk-pa-18-150): 1 registered aircraft, registry code 05620WD
- [Fryer Charles PA-18-150](https://openairdocs.org/model/fryer-charles-pa-18-150): 1 registered aircraft, registry code 05622QG
- [Johnson Justin T PA-18 150](https://openairdocs.org/model/johnson-justin-t-pa-18-150): 1 registered aircraft, registry code 05637DO
- [Weaver Neil PA-18-150](https://openairdocs.org/model/weaver-neil-pa-18-150): 1 registered aircraft, registry code 05643DW
- [Piper/Sorensen PA-18-150](https://openairdocs.org/model/piper-sorensen-pa-18-150): 1 registered aircraft, registry code 7101829
- [Piper/White Theordore F PA-18-150](https://openairdocs.org/model/piper-white-theordore-f-pa-18-150): 1 registered aircraft, registry code 7101833

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