# N625PL: 2007 Cessna T206H

- Status: Valid registration
- Airframe: [Cessna T206H](https://openairdocs.org/model/cessna-t206h) (registry code 2073303, 6 seats)
- Engine: [Lycoming TIO-540-AJ1A](https://openairdocs.org/engine/lycoming-tio-540-aj1a) (registry code 42004)
- Data sheets: [TCDS A4CE](https://openairdocs.org/tcds/A4CE) (Textron Aviation Inc.), [TCDS E14EA](https://openairdocs.org/tcds/E14EA) (Lycoming Engines) (OpenAirDocs)
- Serial number: T20608787
- Year built: 2007
- Type: Fixed wing single engine
- Engine type: Reciprocating
- Airworthiness: Standard, normal
- Airworthiness date: November 28, 2007
- Certificate issued: December 1, 2018
- Expires: December 31, 2028
- Mode S code: A82A20
- Registered owner: [Gv Air Inc](https://openairdocs.org/faa-owner/GV%20AIR%20INC)
- Location: [Medford, OR](https://openairdocs.org/faa-place/OR/Medford)
- Owner type: Corporation
- Owner's area on the map: 42.3276° N, 122.7958° W: Placed by OpenAirDocs at the center of ZIP code 97504, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=625PL
- Page: https://openairdocs.org/aircraft/N625PL

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): 34 in force

### Matched by airframe (Cessna T206H)

- [AD 2024-14-03](https://openairdocs.org/ad/2024-14-03): Autopilot System · Garmin GFC 500 Autopilot (STC SA01866WI). Effective Aug 20, 2024
- [AD 2023-09-09](https://openairdocs.org/ad/2023-09-09): Exhaust Turbine System (Recip) · Aerostar PA-60-600 (Aerostar 600), PA-60-601 (Aerostar 601), PA-60-601P (Aerostar 601P) and 292 more. Effective Jul 17, 2023
- [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023
- [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 2013-11-11](https://openairdocs.org/ad/2013-11-11): Engine Oil Pressure · Cessna 172R, 172S, 182S and 4 more. Effective Aug 1, 2013
- [AD 2012-10-52](https://openairdocs.org/ad/2012-10-52): Turbochargers · Cessna T206H, T207A, T210F and 21 more. Effective Jun 26, 2012
- [AD 2008-26-10](https://openairdocs.org/ad/2008-26-10): Alternate static air source selector valve · Cessna 172, 172A, 172B and 179 more. Effective Jan 5, 2009
- [AD 2008-10-02](https://openairdocs.org/ad/2008-10-02): Part number identification placard · Cessna 172, 172R, 172RG and 64 more. Effective May 12, 2008
- [AD 2008-05-09](https://openairdocs.org/ad/2008-05-09): Crew seats · Cessna 172R, 172S, 182T and 3 more. Effective Apr 8, 2008
- [AD 2008-02-06](https://openairdocs.org/ad/2008-02-06): GSM 85 servo gearbox units · Cessna 182T, 206H, LC40-550FG and 11 more. Effective Feb 26, 2008
- [AD 2007-08-03](https://openairdocs.org/ad/2007-08-03): Flexible fuel hoses · Cessna 172R, 172S, 182T and 3 more. Effective May 2, 2007
- [AD 2007-05-10](https://openairdocs.org/ad/2007-05-10): Steel lock rod/bar on both crew seat back cylinder lock assemblies · Cessna 172R, 172S, 182S and 4 more. Effective Apr 11, 2007
- [AD 2006-17-04](https://openairdocs.org/ad/2006-17-04): Flexible fuel hoses located in the engine compartment · Cessna 172R, 172S, 182T and 3 more. Effective Sep 1, 2006
- [AD 2005-13-10](https://openairdocs.org/ad/2005-13-10): Main electrical power junction box circuit breakers · Cessna 172R, 172S, 182T and 3 more. Effective Aug 9, 2005
- [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 2004-15-18](https://openairdocs.org/ad/2004-15-18): Honeywell KAP 140 Autopilot Computer System · Cessna 172R, 172S, 182S and 4 more. Effective Sep 12, 2004
- [AD 2001-09-06](https://openairdocs.org/ad/2001-09-06): Horizontal Stabilizer Attachment Reinforcement Brackets · Cessna 206H and T206H. Effective May 18, 2001
- [AD 99-13-04](https://openairdocs.org/ad/99-13-04): Aileron Control Bellcrank Stop Bolts & Lock Nuts · Cessna 206H and T206H. Effective Jul 13, 1999

### Matched by engine (Lycoming TIO-540-AJ1A)

- [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 2017-11-10](https://openairdocs.org/ad/2017-11-10): Engine Exhaust System · Lycoming Engines TIO-540-AJ1A. Effective Jun 28, 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 2015-10-06](https://openairdocs.org/ad/2015-10-06): Engine exhaust pipes · Lycoming Engines TIO-540-AJ1A. Effective Jul 2, 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 71-13-01 R1](https://openairdocs.org/ad/71-13-01-R1): Rescinding an airworthiness directive · Lycoming Engines TIO-540-A1A, TIO-540-A1B, TIO-540-A1C and 13 more. Effective Mar 8, 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 2009-02-03](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 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 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 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

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

- [AD 2003-24-13](https://openairdocs.org/ad/2003-24-13) (historical): Honeywell KAP 140 autopilot computer system · 172R, 172S, 182S and 4 more. Effective Jan 20, 2004
- [AD 2000-04-01](https://openairdocs.org/ad/2000-04-01) (historical): Oil Pressure Switch · Cessna 172R, 172S, 182S and 2 more. Effective Mar 11, 2000
- [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 2008-14-07](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 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

## Information bulletins (advisory) (12 in force)

- [SAIB SW-18-31](https://openairdocs.org/saib/SW-18-31): NAVIGATION, ATTITUDE, AND DIRECTION DATA SYSTEM. Issued Nov 21, 2018
- [SAIB CE-13-07R1](https://openairdocs.org/saib/CE-13-07R1): Engine Exhaust; Tailpipe V-band Couplings. Issued May 1, 2013
- [SAIB CE-12-41](https://openairdocs.org/saib/CE-12-41): Flight Controls  Loose Glide Screw. Issued Aug 9, 2012
- [SAIB CE-12-15](https://openairdocs.org/saib/CE-12-15): DC Power Distribution System - Avionics Master Switch. Issued Jan 30, 2012
- [SAIB CE-10-40R1](https://openairdocs.org/saib/CE-10-40R1): Aircraft Fuel System; water contamination of fuel tank systems on Cessna single engine airplanes. Issued Jul 30, 2010
- [SAIB CE-09-12](https://openairdocs.org/saib/CE-09-12): Navigation: CRS/BARO Knob Interference in some G1000/G900X/G950 Installations. Issued Feb 11, 2009
- [SAIB CE-09-11](https://openairdocs.org/saib/CE-09-11): Turbocharged Engines. Issued Feb 9, 2009
- [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-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 CE-19-01](https://openairdocs.org/saib/CE-19-01) (historical): Engine Oil and Airplane Hour Meter; Pressure Switch Failure. Issued Feb 12, 2019
- [SAIB CE-13-07](https://openairdocs.org/saib/CE-13-07) (historical): Engine Exhaust; Tailpipe V-band Couplings. Issued Dec 13, 2012
- [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 N625PL.

## FAA accident and incident reports

None matched to N625PL.

## Reports on N625PL not matched to an aircraft (3)

They name N625PL, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 19951220044779I](https://openairdocs.org/incident/19951220044779I), Dec 20, 1995: Boeing 747132 (N625PL), Honolulu, HI, Minor damage. Narrative: on December 19, 1995, connie kallitta (cksa-american international airways) B-747-132, N625PL flight 761 departed los angeles, CA to Honolulu, HI.…
- [Incident 19941112047079I](https://openairdocs.org/incident/19941112047079I), Nov 12, 1994: Boeing 747132 (N625PL), Pago Pago, American Samoa, Minor damage. On touchdown blew two tires, engine cowl hit runway. Heavy rain and windshift were factors.
- [Incident 19941011039399I](https://openairdocs.org/incident/19941011039399I), Oct 11, 1994: Boeing 747100 (N625PL), Detroit, MI, Minor damage. Wing tip damaged while taxiing on ramp. Crew unable see wings. Marshallers and wing walkers need more training.

## 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 N625PL not matched to an aircraft (69, newest 50)

They name N625PL, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR CKSA98384](https://openairdocs.org/sdr/CKSA98384), Jun 30, 1998: WEB. CORRODED. DURING ROUTINE CPCP INSPECTION FOUND LEVEL 2 CORROSION FUSELAGE LWR AREA, BS 1200, RBL 58, WEB CORRODED AT O/B FACE LWR AREA. REMOVED CORROSION IAW B747 SRM 51-
- [SDR CKSA98383](https://openairdocs.org/sdr/CKSA98383), Jun 30, 1998: FLOORBEAM. CRACKED. DURING ROUTINE CPCP INSPECTION, FOUND FS 440 RBL 50 UPPER DECK FLOORBEAM WEB CRACKED. REMOVED DAMAGED WEB IAW B747 SRM 51-30-02. FABRICATED REPAIR DOUBLERS IAW 
- [SDR CKSA98382](https://openairdocs.org/sdr/CKSA98382), Jun 30, 1998: INTERCOSTAL. CRACKED. DURING ROUTINE CPCP INSPECTION, FOUND FS 440 TO FS 460 RBL 50 INTERCOSTAL WEB CRACKED. REMOVED CRACKED WEB IAW B747 SRM 51-30-02. FABRICATED REPAIR DOUBLERS IAW
- [SDR CKSA98381](https://openairdocs.org/sdr/CKSA98381), Jun 30, 1998: ANGLE. CRACKED. DURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION, FS440 RBL50 UPPER DECK FLOORBEAM ATTACH ANGLE CRACKED ON AFT INBD SIDE. REMOVED AND REPLACED ATTACH ANG
- [SDR CKSA98380](https://openairdocs.org/sdr/CKSA98380), Jun 30, 1998: FRAME. CORRODED. DURING ROUTINE C CHECK INSPECTION, FOUND BS 2020 RBL 22 UPPER CHORD OF MAIN FRAME CORRODED AND A FLOOR SUPPORT. PERFORMED HFEC PER NDT MANUAL 51-00-00 PART 6. N
- [SDR CKSA98379](https://openairdocs.org/sdr/CKSA98379), Jun 30, 1998: FRAME. CORRODED. DURING ROUTINE C CHECK INSPECTION, FOUND BS 2000 RBL 22 UPPER CHORD OF MAIN FRAME CORRODED UNDER FLOOR SUPPORT. REPAIRED UPPER CHORD IAW AIA EDR NBR B4-05879. I
- [SDR CKSA98378](https://openairdocs.org/sdr/CKSA98378), Jun 30, 1998: FRAME. CORRODED. DURING ROUTINE C CHECK INSPECTION, FOUND BS 1980 RBL 22 UPPER CHORD OF MAIN FRAME CORRODED UNDER FLOOR SUPPORT. REPAIRED UPPER CHORD IAW AIA EDR NBR B4-05878. I
- [SDR CKSA98377](https://openairdocs.org/sdr/CKSA98377), Jun 30, 1998: LONGERON. CORRODED. DURING ROUTINE CPCP INSPECTION, FOUND CORROSION ON UPPER SURFACE OF LEFT OVERWING LONGERON APPROX STA 1320. REMOVED CORROSION FROM ACCESSABLE AREA IAW SRM 51-10
- [SDR CKSA98376](https://openairdocs.org/sdr/CKSA98376), Jun 30, 1998: KEEL BEAM. CORRODED. DURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION UPPER WEB OF KEEL BEAM BOX CORRODED AND CRACKED APPROX STA 1265 AT PREVIOUS REPAIR. REMOVED FASTENERS IA
- [SDR CKSA98375](https://openairdocs.org/sdr/CKSA98375), Jun 30, 1998: FLOORBEAM. CORRODED. DURING ROUTINE CPCP INSPECTION, FOUND FS2240 RBL75 FLOORBEAM T CHORD HAS CORROSION. REMOVED CORROSION IAW B747 SRM 51-10-01. FOUND TO BE OUT OF LIMITS IAW B747 
- [SDR CKSA98374](https://openairdocs.org/sdr/CKSA98374), Jun 30, 1998: SPAR. CORRODED. DURING ROUTINE C CHECK INSPECTION, FOUND LOWER FWD SPAR LWS1356 EXFOLIATED. REMOVED NR 2 PANEL RT SIDE. HFEC INSPECTED FASTENERS HOLES IN THE HORIZ FLANGE OF TH
- [SDR CKSA98373](https://openairdocs.org/sdr/CKSA98373), Jun 30, 1998: FLOORBEAM. CORRODED. DURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION, FS440 RBL50 UPPER DECK FLOORBEAM HAS CORROSION ON FWD SIDE. REMOVED CORROSION IAW B747 SRM 51-10-01. FO
- [SDR CKSA98372](https://openairdocs.org/sdr/CKSA98372), Jun 30, 1998: FLOORBEAM. CORRODED. DURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION, STA1940-1960 LBL11.33 LONGITUDINAL FLOORBEAM UPPER CHORD CORRODED. REMOVED CORROSION IAW B747 SRM 51-10
- [SDR CKSA98371](https://openairdocs.org/sdr/CKSA98371), Jun 30, 1998: SEAT TRACK. CORRODED. DURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION, FS1100 LBL70 SEAT TRACK UNDERSIDE HAS CORROSION. REMOVED CORROSION IAW B747 SRM 51-10-01. FOUND OUT OF 
- [SDR CKSA98370](https://openairdocs.org/sdr/CKSA98370), Jun 30, 1998: SEAT TRACK. CORRODED. DURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION, STA 340 FWD SIDE LBL33 SEAT TRACK FLANGE HAS CORROSION. REMOVED CORROSION IAW B747 SRM 51-10-01. FOUND 
- [SDR CKSA98369](https://openairdocs.org/sdr/CKSA98369), Jun 30, 1998: SEAT TRACK. CORRODED. DURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION. CORROSION AROUND 2 CLIP NUTS ON RBL 49 SEAT TRACK FWD OF BS 240. REMOVED CORROSION IAW 51-10-01. FOUND 
- [SDR CKSA98368](https://openairdocs.org/sdr/CKSA98368), Jun 30, 1998: FLOORBEAM. CORRODED. DURING ROUTINE CPCP INSPECTION FOUND LEVEL 2 CORROSION, CORROSION AROUND CLIP NUT ON UPPER CHORD OF BS680 FLOORBEAM LBL3. CUTOUT DAMAGE AREA IAW SRM 51-40-04 FI
- [SDR CKSA98367](https://openairdocs.org/sdr/CKSA98367), Jun 30, 1998: FLOORBEAM. CORRODED. DURING ROUTINE CPCP INSPECTION FOUND LEVEL 2 CORROSION STA760 FWD LBL44 FLOORBEAM HAS CORROSION. CORROSION FOUND TO BE OUT OF LIMITS IAW B747 SRM 53-10-1. CUTOU
- [SDR CKSA98366](https://openairdocs.org/sdr/CKSA98366), Jun 30, 1998: FLOORBEAM. CORRODED. DURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION STA760 FWD LBL72 FLOORBEAM HAS CORROSION. CORROSION FOUND TO BE OUT OF LIMITS IAW B747 SRM 53-10-1. CUTO
- [SDR CKSA98365](https://openairdocs.org/sdr/CKSA98365), Jun 30, 1998: FITTING. CORRODED. DURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION STA 760 AFT, LBL 79 FLOORBEAM ANGLE HAS CORROSION. REMOVED FITTING IAW B747 SRM 51-30-2. REPLACED FITTIN
- [SDR CKSA98364](https://openairdocs.org/sdr/CKSA98364), Jun 30, 1998: FLOOR. CORRODED. DURING ROUTINE CPCP INSPECTION, FOUND FLOOR HAS CORROSION BETWEEN STA 860 AND STA 880 RBL 98 BOTTOM SIDE. REMOVED FLOOR PANEL CORROSION FOUND TO BE OUT OF LIMIT
- [SDR CKSA98363](https://openairdocs.org/sdr/CKSA98363), Jun 30, 1998: SEAT TRACK. CORRODED. DURING ROUTINE CPCP INSPECTION, FOUND 1 AREA OF CORROSION ON BOTTOM OF RBL11.33 SEAT TRACK FWD OF BS 520. REMOVED CORROSION IAW B747 SRM 51-10-01. FOUND TO BE O
- [SDR CKSA98362](https://openairdocs.org/sdr/CKSA98362), Jun 30, 1998: FLOORBEAM. CORRODED. DURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION 2 AREA OF CORROSION ON BS480 FLOOR BEAM FWD, UPPER, SIDE AT RBL-76. REMOVED CORROSION IAW B747 SRM 51-10
- [SDR CKSA98361](https://openairdocs.org/sdr/CKSA98361), Jun 30, 1998: ANGLE. CRACKED. DURING ROUTINE CPCP INSPECTION, FOUND FS1000 LBL 30 FRONT SPAR FLOOR SUPPORT ATTACH ANGLE CRACKED. REMOVED FLOOR SUPPORT. REWORKED FITTINGS IAW EDR B4-05869 DTD
- [SDR CKSA98360](https://openairdocs.org/sdr/CKSA98360), Jun 30, 1998: ANGLE. CRACKED. DURING ROUTINE CPCP INSPECTION, FOUND FS1080 LBL90 OUTBD SIDE WEB ATTACH ANGLE CRACKED. FAB NEW ATTACH ANGLE 7075-T6. INSTALLED ATTACH ANGLE IAW B747 SRM 51-30-
- [SDR CKSA98359](https://openairdocs.org/sdr/CKSA98359), Jun 30, 1998: FRAME. CORRODED. DURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION BS980, RBL50, PANEL SUPPORT FRAME CORRODED. REMOVED CORROSION IAW B747 SRM 51-10-01. FOUND TO BE OUT OF 
- [SDR CKSA98358](https://openairdocs.org/sdr/CKSA98358), Jun 30, 1998: FRAME. CORRODED. DURING ROUTINE CPCP INSPECTION, FOUND BS920, FROM BOTTOM CENTERLINE TO BOTH RT AND LEFT BL50, PANEL SUPPORT FRAME CORRODED. REMOVED CORROSION IAW B747 SRM 51-10
- [SDR CKSA98357](https://openairdocs.org/sdr/CKSA98357), Jun 30, 1998: ANGLE. CORRODED. DURING ROUTINE CPCP INSPECTION, FOUND AT BS1060, FROM BOTTOM CENTERLINE TO LBL50, PANEL SUPPORT FRAME WITH CORROSION AROUND ANCHOR NUTS AND FASTENERS. REMOVED D
- [SDR CKSA98356](https://openairdocs.org/sdr/CKSA98356), Jun 30, 1998: SKIN. CORRODED. DURING ROUTINE CPCP INSPECTION FOUND LEVEL 2 CORROSION: FS1200 RBL95 CNTR WING SKIN HAS CORROSION. REMOVED CORROSION IAW B747 SRM 51-10-01. FOUND TO BE OUT OF L
- [SDR CKSA98355](https://openairdocs.org/sdr/CKSA98355), Jun 30, 1998: SKIN. CRACKED. DURING ROUTINE CPCP INSPECTION FOUND: C-2 DOOR OUTER SKIN IS DENTED AND HAS 2 EA 1 CRACKS AT BOTTOM EDGE BETWEEN BS 1840 AND BS 1860. DAMAGED FOUND TO BE OUT OF
- [SDR CKSA98354](https://openairdocs.org/sdr/CKSA98354), Jun 30, 1998: SKIN. GOUGED. DURING ROUTINE C CHECK INSPECTION FOUND: SEVERAL GOUGES IN FUSELAGE SKIN AT AFT LOWER CORNER OF C-2 DOOR CUT-OUT BS1920. REMOVED FASTENERS AND BLENDED AREA IAW 
- [SDR CKSA97458](https://openairdocs.org/sdr/CKSA97458), Aug 22, 1997: BLEED AIR DUCT. LEAKING. NUMBER 2 FIRE DETECTION FAULT LIGHT CAME ON IN FLIGHT BLEED VALVE WENT TO CLOSE POSITION AND A AND B INDICATORS SHOW 8.5 AND 7. TEMP WAS NORMAL ON ALL ENGINE PA
- [SDR CKSA97437](https://openairdocs.org/sdr/CKSA97437), Jul 30, 1997: DOOR LIGHT. ILLUMINATED. DURING DESCENT FL20.0, DOOR OPEN LIGHT ILLUMINATED ALONG WITH PRIMARY NOSE DOOR OPEN LIGHT. PRIMARY NOSE GEAR DOOR IND. TRANSFERRED TO DMI NR 612 IAW MEL 32-12,
- [SDR CKSA96195](https://openairdocs.org/sdr/CKSA96195), Nov 7, 1996: DRIVE UNIT. WORN. UHHH-FLT NR 80738: WHEN RETRACTING FLAPS, NR 1 LEADING EDGE FLAP, LEFT SIDE WOULD NOT RETRACT. NR 1 REMAINED INTRANSIT DURING EXTENSION ALSO. REPLACED NR 1 LEFT
- [SDR CKSA96187](https://openairdocs.org/sdr/CKSA96187), Oct 18, 1996: SEAT TRACK. CORRODED. KOSC - DURING C-2 CHECK INSPECTION FOUND: SEAT TRACK REPAIR BETWEEN STA 1210 AND 1265 LBL 75 CORRODED. REMOVED AND REPLACED IAW SRM 51-30-02 AND AIA/E/2359. C-C
- [SDR CKSA96186](https://openairdocs.org/sdr/CKSA96186), Oct 18, 1996: ANGLE. CORROSION. KOSC - DURING C-2 CHECK INSPECTION FOUND: FLOOR BEAM ANGLE AT FS 330 UPPER CABIN HAS CORROSION FROM LBL 6 TO FUSELAGE SKIN. REPAIRED IAW ENGINEERING DOC B405022
- [SDR CKSA96185](https://openairdocs.org/sdr/CKSA96185), Oct 18, 1996: STRINGER. CRACKED. KOSC - DURING C-2 CHECK INSPECTION FOUND: A PIT STA 743R CRACK IN STRINGER 44 AT RIVET. REPAIRED IAW SRM 53-10-3. CORROSION TASK CARD NR C53-110-01, TASK CARD N
- [SDR CKSA96184](https://openairdocs.org/sdr/CKSA96184), Oct 18, 1996: ANGLE. CRACKED. KOSC - DURING C-2 CHECK INSPECTION FOUND: A PIT STA 560 LEFT INNER CORD LOWER SUPPORT ANGLE CRACKED IN RADIUS ABOVE STR 39. REMOVED CRACKED ANGLE AND FABRICATED
- [SDR CKSA96183](https://openairdocs.org/sdr/CKSA96183), Oct 18, 1996: SHEAR TIE. CRACKED. KOSC - DURING C-2 CHECK INSPECTION FOUND: FORWARD NR 3 PYLON SUPPORT STRUT SHEAR TIE CRACKED AT WS 670 IN NR 3 MAIN FUEL TANK 11 INCHES AFT OF FRONT SPAR WEB. R
- [SDR CKSA96182](https://openairdocs.org/sdr/CKSA96182), Oct 18, 1996: ANGLE. CRACKED. KOSC - DURING C-2 CHECK INSPECTION FOUND: A PIT STA 680L ABOVE STRINGER 38 INNER CORD REINFORCEMENT ANGLE CRACKED. REMOVED CRACKED ANGLE. VERIFIED AND FABRICATE
- [SDR CKSA96181](https://openairdocs.org/sdr/CKSA96181), Oct 18, 1996: FRAME. CORROSION. KOSC - DURING C-2 CHECK INSPECTION FOUND: AFT PIT CARGO DOOR AFT FRAME BEHIND LOCK SWITCH SKIN HAS CORROSION. REPAIRED IAW SKETCH AIA/EI2357. CORROSION TASK CAR
- [SDR CKSA96180](https://openairdocs.org/sdr/CKSA96180), Oct 18, 1996: SKIN. CORRODED. KOSC - DURING C-2 CHECK INSPECTION FOUND: STA 2055 BETWEEN 37R AND 38R SKIN HAS CORROSION. CUT OUT DAMAGED AREA, FABRICATED REPAIR IAW SRM 53-30-03 FIGURE 1. CO
- [SDR CKSA96179](https://openairdocs.org/sdr/CKSA96179), Oct 18, 1996: FLOOR BEAM. CORRODED/SPLIT. KOSC - DURING C-2 CHECK INSPECTION FOUND: STA 1820 LBL 67 FLOOR BEAM UPPER CORD SPLIT AND CORRODED. REPAIRED FLOOR BEAM STA 1820 LBL 67 IAW REPORT NR 96AIA-152 
- [SDR CKSA96178](https://openairdocs.org/sdr/CKSA96178), Oct 18, 1996: SEAT TRACK. CORRODED. KOSC - DURING C-2 CHECK INSPECTION FOUND: STA 1230 RIGHT OUTBOARD SEAT TRACK HAS CORROSION ON INBOARD SIDE. REMOVED DAMAGED SEAT TRACK STA 1230 RIGHT OUTBOARD. 
- [SDR CKSA96177](https://openairdocs.org/sdr/CKSA96177), Oct 18, 1996: SPAR CAP. CORRODED. KOSC - DURING C-2 CHECK INSPECTION FOUND: RIGHT WING LEADING EDGE LOWER SPAR CAP CORRODED AT WS 1300. REMOVED CORRODED SPAR CAP AND REPAIRED IAW B747 SRM 57-30-
- [SDR CKSA96176](https://openairdocs.org/sdr/CKSA96176), Oct 18, 1996: SEAT TRACK. CORRODED. KOSC - DURING C-2 CHECK INSPECTION FOUND: CABIN: STATION 1242 MAIN CABIN RBL 82 SEAT TRACK FLANGE CORRODED. REMOVED CORRODED SEAT TRACK AND REPAIRED IAW AIA/EA 
- [SDR CKSA96175](https://openairdocs.org/sdr/CKSA96175), Oct 18, 1996: SKIN. CORRODED. KOSC - DURING C-2 CHECK INSPECTION FOUND: STATION 2220 STR 35R SKIN HAS CORROSION AT SHEAR TIE AND TEAR STRAP. REMOVED CORROSION. CORROSION OUT OF LIMITS IAW SR
- [SDR CKSA96174](https://openairdocs.org/sdr/CKSA96174), Oct 18, 1996: FRAME. CORRODED. KOSC - DURING C-2 CHECK INSPECTION FOUND: FS 1700 RBL 65 FLOOR FRAME CORRODED. REPAIRED PER AMERICAN INTERNATIONAL AIRWAYS ENGINEERING SKETCH AIA/E/2372. PART F
- [SDR CKSA96173](https://openairdocs.org/sdr/CKSA96173), Oct 18, 1996: SEAT TRACK. CORRODED. KOSC - DURING C-2 CHECK INSPECTION FOUND: STA 1905 MAIN CABIN RBL 34 SEAT TRACK CORRODED. REMOVED AND REPLACED SEAT TRACK STA 1905 PER SRM'S 51-10-01 AND 51-30-
- [SDR CKSA96172](https://openairdocs.org/sdr/CKSA96172), Oct 18, 1996: SEAT TRACK. CORRODED. KOSC - DURING C-2 CHECK INSPECTION FOUND: SEAT TRACK AT STA 1860 RBL 34 CORRODED. REMOVED AND REPLACED SEAT TRACK STA 1860 AS REQUIRED PER SRM'S 51-10-01 AND 51

All 69: https://openairdocs.org/aircraft/N625PL/unmatched-reports.md

## STCs that may be installed (OpenAirDocs) (315, first 50)

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

### Approved for the airframe (Cessna T206H)

- [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 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 SA02069AK](https://openairdocs.org/stc/SA02069AK): Fabrication and installation of the Airglas, Inc., Landes PA32-206LA Nose Fork equipped with up to a 8.50 x 6 tire. Airglas Inc
- [STC SA02279AT](https://openairdocs.org/stc/SA02279AT): Installation of a Boom Beam bulb, starter, and ballast. Whelen Aerospace Technologies
- [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 SA01134DE](https://openairdocs.org/stc/SA01134DE): Installation of EarthX ETX680-24-TSO Lithium Battery. EarthX Inc
- [STC SA12406WI](https://openairdocs.org/stc/SA12406WI): Installation of a Garmin AXIS Flight Display System. Garmin International Inc
- [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 SA02511SE](https://openairdocs.org/stc/SA02511SE): Installation of replacement fuel quantity indicator sending unit(s). CiES Inc
- [STC SA12276IB](https://openairdocs.org/stc/SA12276IB): Payload System Installation. Icarus Aero Inc
- [STC SA01005DE](https://openairdocs.org/stc/SA01005DE): Installation of a EarthX ETX900-TSO Lithium battery. EarthX Inc
- [STC SA02266AK](https://openairdocs.org/stc/SA02266AK): Replacement of Rudder and Elevator Hinge Bearings with P. Ponk Aviation Bearing p/n PPA-1401. McFarlane Aviation LLC
- [STC SA11158SC](https://openairdocs.org/stc/SA11158SC): Demonstration of aircraft tolerance to potential electromagnetic interference from certain Transmitting Potable Electronic Devices (T-PEDS). Liberty Partners Inc
- [STC SA5581SW](https://openairdocs.org/stc/SA5581SW): Installation of ALCOR true-flow/ totalizer system. Alcor LLC. Lists 206 Series
- [STC SA02738CH](https://openairdocs.org/stc/SA02738CH): Installation of L-3 Communications Avionics Systems. Acron Aviation Inc
- [STC SA04046CH PAGE 1](https://openairdocs.org/stc/SA04046CH%20PAGE%201): Installation of L-3 GENESIS (TM) Electronic Standby Instrument System (ESI-500/MAG-500). Acron Aviation Inc
- [STC SA01330LA](https://openairdocs.org/stc/SA01330LA): Installation of alternate avionics support assembly. Radiorax Aviation Systems LLC
- [STC SA01120SE](https://openairdocs.org/stc/SA01120SE): Installation of Door Steward. Mountain View Aviation LLC
- [STC SA39CH](https://openairdocs.org/stc/SA39CH): Installation of an Amphibian Landing Gear Position Advisory System/Laser Gear Advisory System. Wipaire Inc
- [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 SA04550NY](https://openairdocs.org/stc/SA04550NY): Installation of the Split Forward Cargo Door Window. Airworthiness Resources Corporation
- [STC SA00871SE](https://openairdocs.org/stc/SA00871SE): Installation of cockpit sunvisors. Rosen Sunvisor Systems LLC
- [STC SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc
- [STC SA01105DE](https://openairdocs.org/stc/SA01105DE): Installation of the Persistent Systems MPU5 Wave Radio System. Persistent Systems
- [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 SA01899WI](https://openairdocs.org/stc/SA01899WI): Installation of Garmin G3X Touch Electronic Flight Instrument System. Garmin International Inc
- [STC SA02575AK](https://openairdocs.org/stc/SA02575AK): Installation of the nose tire scraper P/N TSL-100. Aero Twin Inc
- [STC SA02576AK](https://openairdocs.org/stc/SA02576AK): Installation of Cleveland and ABI, LLC Wheel and Brake Kits. ABI LLC
- [STC SA02019WI](https://openairdocs.org/stc/SA02019WI): Installation of the Trig Avionics TX56, TX56A, TX57, or TX57A VHF Nav-Com Radio. Peregrine
- [STC SA03147AT-D](https://openairdocs.org/stc/SA03147AT-D): Installation of an Autopilot Aileron Disconnect System. Summit Aviation Inc
- [STC SA03150AT-D](https://openairdocs.org/stc/SA03150AT-D): Installation of a Wulfsberg P-2000 FM radio. Summit Aviation Inc
- [STC SA04400NY](https://openairdocs.org/stc/SA04400NY): Installation of the Integrated Back-up Battery System (IBBS). TCW Technologies LLC
- [STC SA02554AK](https://openairdocs.org/stc/SA02554AK): Installation of the Cargo Door Release System. Airframe Innovations Inc
- [STC SA11137SC](https://openairdocs.org/stc/SA11137SC): Installation of Plane-Power ALT-FLX alternator. Hartzell Engine Technologies, LLC
- [STC SA00858SE](https://openairdocs.org/stc/SA00858SE): Install observation window. DV Aviation Inc
- [STC SA01688SE](https://openairdocs.org/stc/SA01688SE): Installation of a revised shoulder harness restraint system and new rear cabin headliner. DV Aviation Inc
- [STC SA01878SE](https://openairdocs.org/stc/SA01878SE): Installation of Rolls-Royce 250-B17F/2 series engine with a Hartzell Model HC-B3TF-7A/T10173FN(K)-11R Propeller. DV Aviation Inc
- [STC SA01985SE](https://openairdocs.org/stc/SA01985SE): Installation of new rear observation seat. DV Aviation Inc
- [STC SA02271SE](https://openairdocs.org/stc/SA02271SE): Fabrication of Soloy wing mounted LED landing and taxi light kits. DV Aviation Inc
- [STC SA02748AT](https://openairdocs.org/stc/SA02748AT): Installation of Wescam Wing Mounted Forward Looking Infrared Camera System, Monitor Stand and Microwave Downlink Antenna System. DV Aviation Inc
- [STC SA2353NM](https://openairdocs.org/stc/SA2353NM): Installation of the Soloy Turbine Pac (Rolls-Royce 250-C20S engine modified per Soloy, LLC STC SE2352NM) and related changes. DV Aviation Inc
- [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 SA00673DE](https://openairdocs.org/stc/SA00673DE): Installation of B&C Specialty Standby Alternator System. Freedom Aviation Inc
- [STC SA01552WI](https://openairdocs.org/stc/SA01552WI): Installation of Supplemental Audio System, including #2 GMA 1347 Audio Panel. Yingling Aircraft Inc
- [STC SA04586CH](https://openairdocs.org/stc/SA04586CH): Installation of Electroair Back Up Battery Panel System Control. Electroair Aquisition Corp
- [STC SA990CE](https://openairdocs.org/stc/SA990CE): Install STOL kits (wing leading edge cuffs, drooped tips, and stall fences). Curry Aviation LLC
- [STC SA00076IB](https://openairdocs.org/stc/SA00076IB): Installation of Photo luminescent Safety Systems. STG AEROSPACE GERMANY GmbH

All 315: https://openairdocs.org/aircraft/N625PL/stcs.md

## Related

- Other Cessna T206H aircraft: https://openairdocs.org/model/cessna-t206h/aircraft.md
- The Lycoming TIO-540-AJ1A engine: https://openairdocs.org/engine/lycoming-tio-540-aj1a.md

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