# Search: 180

Service difficulty reports: 1,000+ matches in release 2026-11-04. Page 1.

- [SDR EY2R9600533](https://openairdocs.org/sdr/EY2R9600533.md): Bearing · Cessna 180 · Apr 1, 1996
  > BEARING CORRODED.
- [SDR EY2R9600308](https://openairdocs.org/sdr/EY2R9600308.md): Hub · Cessna 180 · Feb 1, 1996
  > HUB FOUND CORRODED.
- [SDR EY2R9600309](https://openairdocs.org/sdr/EY2R9600309.md): Hub · Cessna 180 · Feb 1, 1996
  > HUB FOUND CORRODED.
- [SDR EY2R9600383](https://openairdocs.org/sdr/EY2R9600383.md): Hub · Cessna 180 · Mar 1, 1996
  > CORROSION FOUND ON HUB.
- [SDR EY2R9600130](https://openairdocs.org/sdr/EY2R9600130.md): Hub · Cessna 180 · Oct 1, 1996
  > HUB CRACKED IN THREADS AREA
- [SDR EY2R9600002](https://openairdocs.org/sdr/EY2R9600002.md): Hub · Cessna 180 · Jan 1, 1996
  > HUB CRACKED IN NR2 BLADE SOCKET
- [SDR AU960969](https://openairdocs.org/sdr/AU960969.md): Spring · Cessna 180 · Jun 24, 1996
  > (AUS) LH MAGNETO IMPULSE COUPLING SPRING BROKEN
- [SDR CA050531004](https://openairdocs.org/sdr/CA050531004.md): Support Bracket · Cessna 180 · May 18, 2005
  > (CAN) INTERGRANULAR CORROSION FOUND ON INSPECTION.
- [SDR CA991028001](https://openairdocs.org/sdr/CA991028001.md): Mount · Cessna 180 · Aug 14, 1999
  > (CAN) ENGINE MOUNT FOUND CRACKED 75 PERCENT THROUGH.
- [SDR AU961065](https://openairdocs.org/sdr/AU961065.md): Bearing · Cessna 180 · Jul 20, 1996
  > (AUS) ENGINE NO3 MAIN BEARING SPALLED - BEARING HAD ROTATED
- [SDR 20000907SH040](https://openairdocs.org/sdr/20000907SH040.md): Drive Gear · Cessna 180 · Aug 10, 2000
  > RELEVANT MT INDICATION AROUND GEAR TEETH. (X)
- [SDR 20000517SH019](https://openairdocs.org/sdr/20000517SH019.md): Gear · Cessna 180 · Apr 24, 2000
  > RELEVANT INDICATION IN TEETH AREA OF IDLER GEAR. (X)
- [SDR 20000517SH020](https://openairdocs.org/sdr/20000517SH020.md): Lever · Cessna 180 · Apr 24, 2000
  > RELEVANT INDICATION AT CLAMP RETENTION AREA OF CONTROL LEVER. (X)
- [SDR CA970421080](https://openairdocs.org/sdr/CA970421080.md): Blade · Cessna 180 · Apr 11, 1997
  > (CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. LEADING EDGE HAD SPRAY CUT DAMAGE.
- [SDR CA040615004](https://openairdocs.org/sdr/CA040615004.md): Rocker Boss · Cessna 180 · Jun 10, 2004
  > (CAN) ROCKER BOSSES BROKE OFF, FOR ROCKER SHAFT ON EXHAUST VALVE.
- [SDR AU980509](https://openairdocs.org/sdr/AU980509.md): Block · Cessna 180 · May 5, 1998
  > (AUS) CARRY-THROUGH SPAR REAR WING ATTACHMENT BLOCKS (2OFF) CONTAINED SEVERE EXFOLIATION CORROSION.
- [SDR 20000602SH005](https://openairdocs.org/sdr/20000602SH005.md): Crankshaft · Cessna 180 · May 8, 2000 · N9028C
  > PER TCM MSB 00-5, CRANKSHAFT WAS REJECTED BY TELEDYNE CONTINENTAL MOTORS. (X)
- [SDR CA981125058](https://openairdocs.org/sdr/CA981125058.md): Support · Cessna 180 · Oct 21, 1998
  > (CAN) HORIZONTAL STABILIZER RIGHT REAR HINGE REINFORCEMENT BOX FOUND CRACKED FROM EDGE TO BOLT HOLE.
- [SDR 2020FA0000303](https://openairdocs.org/sdr/2020FA0000303.md): Connector · Cessna 180 · Jun 13, 2020 · N7620A
  > LOSS OF ELECTRICAL POWER IN FLIGHT. REWIRED ELECTRICAL CONNECTIONS ON GENERATOR AND TEST RAN ENGINE.
- [SDR 99ZZZX115](https://openairdocs.org/sdr/99ZZZX115.md): Clamp · Cessna 180 · Dec 7, 1998 · N6560A
  > ENGINE HAS HIGH BURN RATE DURING CRUISE. FOUND MIXTURE CONTROL CABLE HOUSING VERY LOOSE. INSTALLED TWO NEW CLAMPS.

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