# Service difficulty reports: Cessna 175

A list on [Cessna 175](https://openairdocs.org/model/cessna-175.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 51 reports

- [SDR 2016FA0000034](https://openairdocs.org/sdr/2016FA0000034.md): Angle · cracked · Jan 28, 2016 · Cessna 175 · Fuselage Miscellaneous Structure
  > BELIEVE OVER TIGHTING OF BOLT CAUSED STRAIN ON PART MOUNTED IN HIGH VIBRATION AREA.
- [SDR 2013FA0000396](https://openairdocs.org/sdr/2013FA0000396.md): Contact · corroded · Jul 8, 2013 · N9456B · Cessna 175 · Emergency Locator Beacon
  > DURING INSPECTION OF ELT, FOUND TWO OF THE FOUR BATTERY CONTACTS CORRODED, THERE WAS NO EVIDENCE OF A LEAKING BATTERY. ELT WAS STILL FUNCTIONAL.
- [SDR 2013FA0000395](https://openairdocs.org/sdr/2013FA0000395.md): Cylinder Head · cracked · Jul 8, 2013 · N9456B · Cessna 175 · Reciprocating Engine Cylinder Section
  > WHILE PERFORMING A COMPRESSION TEST NR 5 CYLINDER HAD AN AIR LEAK, SPRAYED SOAPY SOLUTION ON CYLINDER AND OBSERVED BUBBLES COMING FROM A CRACK BETWEEN COOLING FINS BETWEEN THE VALVES, UNDER THE UPPER SPARK PLUG AND ANOTHER AREA AFT OF THE SPARK PLUG HOLE.
- [SDR 2013FA0000394](https://openairdocs.org/sdr/2013FA0000394.md): Cylinder Head · cracked · Jul 5, 2013 · N9456B · Cessna 175 · Reciprocating Engine Cylinder Section
  > NR 3 CYLINDER FAILED COMPRESSION TEST DURING ANNUAL INSPECTION. BORESCOPED CYLINDER AND COULD NOT FIND OBVIOUS PROBLEM. SQUIRTED SOAPY WATER SOLUTION ON CYLINDER AND DISCOVERED SMALL LEAK COMING FROM ARE BETWEEN UPPER SPARK PLUG HELI-COIL AND COOLING FINS.
- [SDR 2009FA0000392](https://openairdocs.org/sdr/2009FA0000392.md): Flange · warped · May 11, 2009 · N9456B · Cessna 175 · Reciprocating Engine Rear Section
  > WHILE LOOKING FOR THE SOURCE OF AN OIL LEAK FOUND THE TACHOMETER DRIVE ADAPTER HOUSING FLANGE WARPED AND CRACKED.
- [SDR 2008FA0000756](https://openairdocs.org/sdr/2008FA0000756.md): Mount · cracked · Nov 12, 2008 · N175UK · Cessna 175 · Engine Mount Section
  > DURING INSP, MECHANIC FOUND THE LT UPPER ENGINE MOUNT BRACKET, PN 0513132-11, CRACKED ALL THE WAY THROUGH. CRACK WAS AT THE OUTER RADIUS OF THE WASHER.
- [SDR 2008FA0000281](https://openairdocs.org/sdr/2008FA0000281.md): Mount · cracked · Apr 16, 2008 · N6620E · Cessna 175 · Engine Mount Section
  > INSP FOUND UPPER LT BRACKET (0513132-11) WITH A SMALL CRACK ORIGINATING FROM THE LOWER EDGE OF THE ENGINE MOUNT BOLT WASHER. ONLY A SMALL BEND LINE WAS VISIBLE FROM THE COCKPIT SIDE OF THE BRACKET VIA BOROSCOPE. AFTER REMOVAL OF THIS BRACKET A CRACK WAS CLEA
- [SDR RDA092407](https://openairdocs.org/sdr/RDA092407.md): Transmitter · cracked · Sep 24, 2007 · N9456B · Cessna 175 · Fuel Quantity Sensor
  > WHILE CALIBRATING THE FUEL QUANTITY SYSTEM THE LT FUEL GAUGE WOULD SHOW AN INCREASE IN QUANTITY THEN START DECREASING. WHILE TROUBLESHOOTING THE LT TANK FUEL QUANTITY SENDER, FOUND 2 CRACKS APPROXIMATELY 1 INCH LONG IN THE BRASS FLOAT.
- [SDR RDA113006](https://openairdocs.org/sdr/RDA113006.md): Ammeter · failed · Nov 30, 2006 · N9456B · Cessna 175 · DC Indicating System
  > AEROSPACE LOGIC VA-100 DIGITAL VOLT/AMMETER AMP FUNCTION FAILED. AMP READING VARIES FROM -12 TO -18.5 AMPS, THIS INDICATION IS PRESENT WITH NO LOAD ON SYSTEM OR WITH ENGINE OPERATING AND GENERATOR OPERATING NORMALLY. VOLT FUNCTION OPERATES NORMALLY AND VOLTA
- [SDR 2006FA0000599](https://openairdocs.org/sdr/2006FA0000599.md): Gusset · cracked · Jun 13, 2006 · N6540E · Cessna 175 · Engine Mount Section
  > FOUND 2 OF 4 ENGINE MOUNT TO FIREWALL BRACKETS CRACKED. BRACKETS ARE LOCATED IN CABIN, ATTACHING AC SKIN TO FIREWALL. POSSIBLE CAUSE OF CRACKEING MAY BE OVERTORQUING OF ENGINE MOUNT TO FIREWALL BOLTS. (K)
- [SDR 2006FA0000598](https://openairdocs.org/sdr/2006FA0000598.md): Gusset · cracked · Jun 13, 2006 · N6540E · Cessna 175 · Engine Mount Section
  > FOUND 2 OF 4 ENGINE MOUNT TO FIREWALL BRACKETS CRACKED, BRACKETS ARE LOCATED IN CABIN, ATTACHING AC SKIN TO FIREWALL. POSSIBLE CAUSE OF CRACKING MAY BE OVERTORQUING OF ENGINE MOUNT TO FIREWALL BOLTS. (K)
- [SDR 2006FA0000597](https://openairdocs.org/sdr/2006FA0000597.md): Gusset · cracked · Jun 13, 2006 · N6540E · Cessna 175 · Engine Mount Section
  > FOUND 2 OF 4 ENGINE MOUNT TO FIREWALL BRACKETS CRACKED, BRACELETS ARE LOCATED IN CABIN, ATTACHING AC SKIN TO FIREWALL. POSSIBLE CAUSE OF CRACKING MAY BE OVERTORQUING OF ENGINE MOUNT TO FIREWALL BOLTS. (K)
- [SDR 2006FA0000561](https://openairdocs.org/sdr/2006FA0000561.md): Attach Bracket · cracked · May 31, 2006 · N6622E · Cessna 175 · Fuselage, Powerplant Attach Fittings
  > ENGINE MOUNT ATTACHMENT BRACKET WITH CRACKS AT THE 12 AND 6 O`CLOCK POSITION. CRACKS ON IB AND OB SIDES OF THE AN960-616 WASHER. NORMAL FLIGHT CONDITIONS UNDER WHICH IT OCCURRED. POSSIBLE CAUSE AN960-616 WASHER TOO SMALL. LARGER AREA AND THICKER WASHER NEE
- [SDR 2006FA0000560](https://openairdocs.org/sdr/2006FA0000560.md): Attach Bracket · broken · Apr 30, 2006 · N175FW · Cessna 175 · Fuselage, Powerplant Attach Fittings
  > ENGINE MOUNT ATTACHMENT BRACKET BROKEN AND WITH CRACKS AT THE 12 AND 6 O`CLOCK POSITION. CRACKS ON IB AND OB SIDES OF THE AN960-616 WASHER. NORMAL FLIGHT CONDITIONS UNDER WHICH IT OCCURRED. POSSIBLE CAUSE AN960-616 WASHER TOO SMALL. LARGER AREA AND THICKER
- [SDR 2006FA0000559](https://openairdocs.org/sdr/2006FA0000559.md): Attach Bracket · cracked · Apr 30, 2006 · N9366B · Cessna 175 · Fuselage, Powerplant Attach Fittings
  > ENGINE MOUNT ATTACHMENT BRACKET BROKEN AND WITH CRACKS AT THE 12 AND 6 O`CLOCK POSITION. CRACKS ON IB AND OB SIDES OF THE AN960-616 WASHER. NORMAL FLIGHT CONDITIONS UNDER WHICH IT OCCURRED. POSSIBLE CAUSE AN960-616 WASHER TOO SMALL. LARGER AREA AND THICKER
- [SDR 2006FA0000399](https://openairdocs.org/sdr/2006FA0000399.md): Bracket · cracked · Mar 27, 2006 · N7259M · Cessna 175 · Engine Mount Section
  > FOUND THE UPPER RIGHT ENGINE MOUNT BRACKET, P/N 0513132-11 IN THE 0513132-4 UPPER ENGINE MOUNT STRINGER, CRACKED. INSPECTION WAS ACCOMPLISHED DUE TO NUMEROUS REPORTS OF THE SAME CONDITION FOUND ON LIKE MODELS OF AIRCRAFT.
- [SDR 2006FA0000398](https://openairdocs.org/sdr/2006FA0000398.md): Bracket · cracked · Mar 27, 2006 · N7259M · Cessna 175 · Fuselage, Powerplant Attach Fittings
  > FOUND THE UPPER LEFT ENGINE MOUNT BRACKET, P/N 0513132-11 IN THE 0513132-3 UPPER ENGINE MOUNT STRINGER CRACKED THROUGH THE BRACKET AROUND THE RADIUS OF THE WASHER. INSPECTION WAS ACCOMPLISHED DUE TO NUMEROUS REPORTS OF THE SAME CONDITION FOUND ON LIKE MODELS
- [SDR 2006FA0000318](https://openairdocs.org/sdr/2006FA0000318.md): Bracket · cracked · Feb 27, 2006 · N141JA · Cessna 175 · Fuselage, Powerplant Attach Fittings
  > FOUND THE LEFT UPPER ENGINE MOUNT BRACKET P/N 0513132-11 CRACKED THROUGH AROUND THE WASHER. BRACKET IS LOCATED AT THE FRONT OF THE 0513132-3 ENGINE MOUNT STRINGER AND IS DIFFICULT TO SEE DURING ROUTINE INSPECTIONS. INSPECTION WAS PERFORMED DUE TO SEVERAL OTHER
- [SDR 2006FA0000313](https://openairdocs.org/sdr/2006FA0000313.md): Bracket · cracked · Feb 26, 2006 · N7536M · Cessna 175 · Fuselage, Powerplant Attach Fittings
  > DURING VISUAL INSPECTION OF UPPER ENGINE MOUNT BRACKETS IN THE UPPER ENGINE MOUNT STRINGER ASSEMBLIES, FOUND THE L/H 0513132-11 BRACKET CRACKED. INSPECTION WAS PERFORMED DUE TO RECENT REPORTS OF FINDING BRACKETS CRACKED ON LIKE MODELS OF AIRCRAFT.
- [SDR 2006FA0000157](https://openairdocs.org/sdr/2006FA0000157.md): Bracket · bent · Feb 22, 2006 · N9456B · Cessna 175 · Fuselage, Powerplant Attach Fittings
  > A REPLACEMENT 0513132-11 ENGINE MOUNT BRACKET WAS ORDERED TO REPLACE ONE FOUND CRACKED. THE JOGGLED FLANGE WAS INCORRECTLY FORMED. THE FLANGE WAS BENT OUTWARD TO THE POINT THAT IT WOULD NOT FIT IN THE AIRCRAFT.
- [SDR 2006FA0000250](https://openairdocs.org/sdr/2006FA0000250.md): Bracket · cracked · Feb 22, 2006 · N7362M · Cessna 175 · Fuselage, Powerplant Attach Fittings
  > INSP 0513132-11, MOUNT BRACKET WAS FOUND TO BE CRACKED. CRACK RAN VERT THROUGH BRACKET AROUND OUTER RADIUS OF AN960-616 WASHER ON UPPER ENG MOUNT BOLT. INSP WAS DONE DUE TO 2 OTHER KNOWN REPORTS OF CRACKS IN THIS BRACKET ON SAME MODEL OF AC, ONE RESULTED IN A
- [SDR 2006FA0000156](https://openairdocs.org/sdr/2006FA0000156.md): Attach Bracket · cracked · Feb 13, 2006 · N9456B · Cessna 175 · Fuselage, Powerplant Attach Fittings
  > FOUND THE LT UPPER ENGINE MOUNT ATTACHMENT BRACKET CRACKED THROUGH ON THE IB SIDE. CRACK APPEARS TO HAVE ORIGINATED AT OUTER RADIUS OF WASHER THEN PROGRESSED UP AND DOWN THROUGH BRACKET. THIS INSPECTION WAS PROMPTED AFTER REPORTED FAILURE OF SAME BRACKET, SAME
- [SDR 2006FA0000134](https://openairdocs.org/sdr/2006FA0000134.md): Attach Bracket · broken · Jan 31, 2006 · N6612E · Cessna 175 · Engine Mount Section
  > THE AC EXPERIENCED A HARD LANDING. DURING THE LANDING THE 2 TOP ENGINE MOUNT ATTACH BRACKETS FAILED BEHIND THE FIREWALL, ALLOWING THE TOP HALF OF THE FIREWALL TO FAIL, PULLING FORWARD AND DOWN ABOUT 18 INCHES. PN 051313211 ENGINE MOUNT ATTACH BRACKET FITS ON
- [SDR IGL1520050080](https://openairdocs.org/sdr/IGL1520050080.md): Muffler · deteriorated · Sep 15, 2005 · N7219M · Cessna 175 · Engine Noise Suppressor
  > EXHAUST MUFFLER CRACKED AND DETERIORATED AND WAS NOT DETECTED DUE TO LOCATION UNDER HEAT SHROUD. MUFFLER IS PART OF ENGINE CONVERSION STC NR SA777CE, KIT NR 740.
- [SDR 2005FA0001237](https://openairdocs.org/sdr/2005FA0001237.md): Connecting Rod · broken · Aug 30, 2005 · N7600M · Cessna 175 · Reciprocating Engine Power Section
  > NR 3 CONNECTING ROD PENETRATED CASE. ENGINE TSO 848 HRS. LAST ENGINE O/H 06/10/1964 OR 41 YEARS AGO. MANUFACTURER RECOMMENDS 12 YEARS IAW SIL 98-9.
- [SDR 2005FA0001395](https://openairdocs.org/sdr/2005FA0001395.md): Cylinder · failed · Aug 22, 2005 · N7218M · Cessna 175 · Reciprocating Engine Cylinder Section
  > CYLINDER WAS REBUILT 5/12/05 USING CURRENT PRODUCTION MFG EXHAUST VALVE AND GUIDE. THE EXHAUST VALVE STRUCK (17 HOURS IN SERVICE) RESULTING IN A BROKEN EXHAUST ROCKER ARM, AS A RESULT AN EMERGENCY LANDING WAS SUCCESSFULLY MADE. (K)
- [SDR 2004FA0000752](https://openairdocs.org/sdr/2004FA0000752.md): Bracket · cracked · Sep 3, 2004 · N7487M · Cessna 175 · Engine Mount Section
  > THE FUSELAGE UPPER ENGINE MOUNT BRACKETS WERE DISCOVERED TO BE CRACKED AT MOUNTING HOLES. PN 0513132-11 FOR UPPER LT AND UPPER RT. NEW REPLACEMENT PARTS WERE NOTED TO BE SLIGHTLY THICKER AND MADE FROM SAME MATERIAL. SUGGEST ENGINE MOUNT REMOVAL FOR INSPECTI
- [SDR CA031021005](https://openairdocs.org/sdr/CA031021005.md): Spar · broken · May 16, 2003 · Cessna 175 · Horizontal Stabilizer, Spar/Rib
  > (CAN) DISCOVERED A BREAK IN THE STABILIZER SPAR DURING AN ANNUAL INSPECTION.
- [SDR 2002FA0001258](https://openairdocs.org/sdr/2002FA0001258.md): Fork · cracked · Oct 10, 2002 · N9391B · Cessna 175 · Propeller Hub Section
  > OVERHAUL WAS BEING ACCOMPLISHED DUE TO HIGH CALENDER TIME, LOW HOURS SINCE NEW. DURING MAGNETIC PARTICAL INSPECTION, MULTIPLE LARGE CRACKS WERE DISCOVERED IN PITCH CHANGE FORK. FORK APPEARS TO BE MANUFACTURING DEFECTS, POSSIBLY HEAT TREAT CRACKS.
- [SDR 2002FA0000667](https://openairdocs.org/sdr/2002FA0000667.md): Master Switch · failed · May 23, 2002 · N7535M · Cessna 175 · Electrical Power System
  > WHILE TAXING FOR DEPARTURE AT TAOS AIRPORT. THE PILOT EXPERIENCED AN AVIONICS MASTER SWITCH FAILURE. UPON SEEING A SMALL AMOUNT OF SMOKE AT THE UPPER AREA OF THE INSTRUMENT PANEL THE PILOT IMMEDIATELY SHUT DOWN THE AIRCRAFT AND TAXIED BACK TO THE FBO
- [SDR 2001FA0000121](https://openairdocs.org/sdr/2001FA0000121.md): Wire · defective · Jul 11, 2001 · N6651E · Cessna 175 · Electrical Power System Wiring
  > AIRCRAFT BROUGHT TO BE CLEAN-UP WIRING BEHIND INSTRUMENT PANEL. UPON FURTHER INSPECTION I IMMEDIATELY DISCONNECTED THE SHIPS BATTERY DUE TO THE FACT THE WIRING WAS IN SUCH A DISARRAY I COULD NOT BELIEVE IT WORKED AND IF SO WHY IT HAD NOT CAUSED A FIRE. IE: E
- [SDR 20001018SH001](https://openairdocs.org/sdr/20001018SH001.md): Float · cracked · Aug 31, 2000 · N9366B · Cessna 175 · Wheel/Ski/Float
  > RIGHT FRONT STRUT FLOATS CRACKED. (X)
- [SDR 99ZZZX2720](https://openairdocs.org/sdr/99ZZZX2720.md): Bracket · cracked · Jun 30, 1999 · N6672E · Cessna 175 · Engine Mount Section
  > ALL FOUR ENGINE MOUNT ATTACH BRACKETS WERE DESTROYED AND 3 WERE CRACKED WHERE THE ENGINE MOUNT BOLTS PASS THROUGH THE FIREWALL. THIS IS AN ALUMINUM ANGLE THAT THE FIREWALL ATTACHES TO THAT IS.060 INCH THICK THAT COVERS PART OF THE FACE OF THE BRACKET. THIS
- [SDR 99ZZZX2719](https://openairdocs.org/sdr/99ZZZX2719.md): Bracket · cracked · Jun 30, 1999 · N6672E · Cessna 175 · Engine Mount Section
  > ALL FOUR ENGINE MOUNT ATTACH BRACKETS WERE DESTROYED AND 3 WERE CRACKED WHERE THE ENGINE MOUNT BOLTS PASS THROUGH THE FIREWALL. THIS IS AN ALUMINUM ANGLE THAT THE FIREWALL ATTACHES TO THAT IS.060 INCH THICK THAT COVERS PART OF THE FACE OF THE BRACKET. THIS
- [SDR 99ZZZX2718](https://openairdocs.org/sdr/99ZZZX2718.md): Bracket · cracked · Jun 30, 1999 · N6672E · Cessna 175 · Engine Mount Section
  > ALL FOUR ENGINE MOUNT ATTACH BRACKETS WERE DESTROYED AND 3 WERE CRACKED WHERE THE ENGINE MOUNT BOLTS PASS THROUGH THE FIREWALL. THIS IS AN ALUMINUM ANGLE THAT THE FIRWALL ATTACHES TO THAT IS.060 INCH THICK THAT COVERS PART OF THE FACE OF THE BRACKET. THIS L
- [SDR 98ZZZX1861](https://openairdocs.org/sdr/98ZZZX1861.md): Connecting Rod · failed · Apr 11, 1998 · N7111M · Cessna 175 · Reciprocating Engine Power Section
  > CONNECTING ROD BROKE AT PISTON PIN AREA. REMAINING POSTION OF ROD PUNCHED HOLE IN CRANKCASE, DAMAGED PISTON, AND RESULTED IN ENGINE SHUT DOWN.
- [SDR 98ZZZX1462](https://openairdocs.org/sdr/98ZZZX1462.md): Bracket · cracked · Mar 19, 1998 · N7288M · Cessna 175 · Engine Mount Section
  > LOWER RIGHT FIREWALL ENGINE MOUNT BRACKET FOUND CRACKED INTO TWO PIECES. UPPER LEFT AND RIGHT BRACKETS FOUND TO HAVE SIMILAR CRACKS, BUT NOT AS EXTENSIVE. AREA IS DIFFICULT TO INSPECT AS ENGINE MOUNT BOLTS NEED TO BE REMOVED AND BRACKETS ARE OFTEN COVERED UP
- [SDR 98ZZZX1461](https://openairdocs.org/sdr/98ZZZX1461.md): Bracket · cracked · Mar 19, 1998 · N7288M · Cessna 175 · Engine Mount Section
  > LOWER RIGHT FIREWALL ENGINE MOUNT BRACKET FOUND CRACKED INTO TWO PIECES. UPPER LEFT AND RIGHT BRACKETS FOUND TO HAVE SIMILAR CRACKS, BUT NOT AS EXTENSIVE. AREA IS DIFFICULT TO INSPECT AS ENGINE MOUNT BOLTS NEED TO BE REMOVED AND BRACKETS ARE OFTEN COVERED UP
- [SDR 97ZZZX5125](https://openairdocs.org/sdr/97ZZZX5125.md): Bracket · cracked · Oct 17, 1997 · N7518M · Cessna 175 · Engine Mount Section
  > ALL FOUR ENGINE MOUNT BRACKETS ON THE FORWARD END OF THE ENGINE MOUNT STRINGERS WERE CRACKED AND HOLE AREA BENT OUT. THIS AREA BULGED OUT AROUND BOLT HOLE. AIRCRAFT HAS LYCOMING 180 HP MOD.
- [SDR 97ZZZX5124](https://openairdocs.org/sdr/97ZZZX5124.md): Bracket · cracked · Oct 17, 1997 · N7518M · Cessna 175 · Engine Mount Section
  > ALL FOUR ENGINE MOUNT BRACKETS ON THE FORWARD END OF THE ENGINE MOUNT STRINGERS WERE CRACKED AND HOLE AREA BENT OUT. THIS AREA BULGED OUT AROUND BOLT HOLE. AIRCRAFT HAS LYCOMING 180 HP MOD.
- [SDR 97ZZZX5123](https://openairdocs.org/sdr/97ZZZX5123.md): Bracket · cracked · Oct 17, 1997 · N7518M · Cessna 175 · Engine Mount Section
  > ALL FOUR ENGINE MOUNT BRACKETS ON THE FORWARD END OF THE ENGINE MOUNT STRINGERS WERE CRACKED AND HOLE AREA BENT OUT. THIS AREA BULGED OUT AROUND BOLT HOLE. AIRCRAFT HAS LYCOMING 180 HP MOD.
- [SDR 98ZZZX224](https://openairdocs.org/sdr/98ZZZX224.md): Rocker Boss · failed · Oct 3, 1997 · N7115M · Cessna 175 · Reciprocating Engine Cylinder Section
  > DURING ANNUAL INSPECTION, NR 4 CYLINDER COMP AT 50/80 WITH AIR NOISE IN EXHAUST STACK. ON REMOVAL OF ROCKER BOX COVER, THE TOP HALF OF THE LEFT BOSS CAME OUT WITH THE COVER. TEN HOURS PREVIOUSLY, THE COVER HAD BEEN REMOVED AND PUSH ROD TUBES HAD BEEN RESEALE
- [SDR 97ZZZX3410](https://openairdocs.org/sdr/97ZZZX3410.md): Mount · cracked · Jul 9, 1997 · N7151M · Cessna 175 · Engine Mount Section
  > ACFT OWNER REPORTED THE COWL DID NOT FIT RIGHT. UPON EXAMINATION, DETERMINED THE RT STRINGER ASSY, ENGINE MOUNT UPPER, HAD FAILED AT THE POINT WHERE THE UPPER RT ENGINE MOUNT BOLT PASSES THROUGH THE MOUNTING BRACKET. THE FIREWALL ATTACH RIVETS HAD RIPPED OUT
- [SDR 97ZZZX3409](https://openairdocs.org/sdr/97ZZZX3409.md): Mount · failed · Jul 9, 1997 · N7151M · Cessna 175 · Engine Mount Section
  > ACFT OWNER REPORTED THE COWL DID NOT FIT RIGHT. UPON EXAMINATION, DETERMINED THE RT STRINGER ASSY, ENGINE MOUNT UPPER, HAD FAILED AT THE POINT WHERE THE UPPER RT ENGINE MOUNT BOLT PASSES THROUGH THE MOUNTING BRACKET. THE FIREWALL ATTACH RIVETS HAD RIPPED OUT
- [SDR 97ZZZX625](https://openairdocs.org/sdr/97ZZZX625.md): Spar Cap · corroded · Jan 14, 1997 · N7464M · Cessna 175 · Wing Spar
  > AFTER REMOVING FUEL TANK COVER PANELS TO REPLACE SOME GASKETS DURING AN ANNUAL INSP, INTERGRANULAR CORROSION WAS FOUND ON SPAR CAP FWD OF THE RT TANK. WING LEADING EDGE WAS REMOVED FOR FURTHER INSP AND THE SAME TYPE OF CORROSION WAS FOUND ALONG THE FULL LENGT
- [SDR 96ZZZX5493](https://openairdocs.org/sdr/96ZZZX5493.md): Bracket · failed · Oct 2, 1996 · N6624E · Cessna 175 · Engine Mount Section
  > ENG MOUNT BRACKET LOCATED AT UPPER RT SIDE FUSELAGE IMMEDIATELY AFT OF FIREWALL. NUT AND WASHER OF ENGINE MOUNT BOLT PULLED THROUGH BRACKET, BOWED FIREWALL, AND PRODUCED CRACKS IN FIREWALL DOUBLER PN 0513109-29. NOTED LACK OF TACHOMETER MARKINGS REQUIRED BY
- [SDR 96ZZZX1790](https://openairdocs.org/sdr/96ZZZX1790.md): Spring · broken · Mar 6, 1996 · N9462B · Cessna 175 · Reciprocating Engine Cylinder Section
  > ROUGH ENGINE OPERATION ABOVE 2,500 RPM'S. FOUND NR 4 CYLINDER OUTER EXHAUST VALVE SPRING BROKEN.
- [SDR CA951123103](https://openairdocs.org/sdr/CA951123103.md): Bracket · broken · Oct 20, 1995 · Cessna 175 · Trailing Edge Flap Control System
  > (CAN)BRACKET AT THE RIGHT INBOARD FLAP TRACK CRACKED AT BOTH RIVETS. BRACKET DROPPED DOWN AND PREVENTED THE FLAPS FROM RETRACTING.
- [SDR 95ZZZX4271](https://openairdocs.org/sdr/95ZZZX4271.md): Gasket · wrong part · Jul 27, 1995 · N6618E · Cessna 175 · Fuel Control/Reciprocating Engines
  > FOLLOWING ENGINE OVERHAUL, CARBURETOR WAS RE-INSTALLED TO OIL SUMP USING O-RING SUPPLIED IN KIT NR 627372-A1, PAGE 25 OF GO-300 PARTS MANUAL, FORM X30020. CARBURETOR INSTALLED PER G0-300 PARTS MANUAL, FIGURE 5, WHICH CALLS FOR AN O-RING. NO O-RING GROOVE EXIS
- [SDR 96ZZZX5210](https://openairdocs.org/sdr/96ZZZX5210.md): Cylinder · failed · Jun 8, 1995 · N7227M · Cessna 175 · Reciprocating Engine Cylinder Section
  > INTAKE SIDE ROCKER SHAFT BOSS BROKE. SHAFT BUSHINGS HAD BEEN INSTALLED.

Next page: https://openairdocs.org/model/cessna-175/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE aircraft_model_key = '175'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/cessna-175/reports

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