# Service difficulty reports: Cessna 150G

A list on [Cessna 150G](https://openairdocs.org/model/cessna-150g.md).

Newest first. General aviation reporting is voluntary.

- [SDR 2016FA0000404](https://openairdocs.org/sdr/2016FA0000404.md): Bolt · loose · Aug 13, 2016 · N3666J · Cessna 150G · Elevator Structure
  > LEFT ELEVATOR SEPARATED IN FLIGHT. BOLT CONNECTING ELEVATOR LOOSENED UP AND FELL OUT. ELEVATOR WAS DAMAGED AND APPEARED TO BE BENT FROM AERODYNAMIC FORCES. AIRCRAFT WAS DIFFICULT TO CONTROL. ANY CONTROL MOVEMENT CAUSED UNCONTROLLABLE PITCHING IN THE LATERAL
- [SDR CA150604020](https://openairdocs.org/sdr/CA150604020.md): Coupling · sheared · May 17, 2015 · Cessna 150G · Vacuum Distribution System
  > (CAN) VACUUM COUPLING FAILED. PROBLEM FOUND ON START UP AND FLIGHT ABORTED. REPLACED VACUUM PUMP WITH NEW UNIT. ALL WORK PERFORMED BY MAINTENANCE AND SIGNED OUT IN LOGS.
- [SDR CA150319006](https://openairdocs.org/sdr/CA150319006.md): Muffler · cracked · Oct 5, 2014 · Cessna 150G · Engine Noise Suppressor
  > (CAN) CRACK IN THE INTERIOR OF THE RT MUFFLER FOUND DURING ANNUAL ENGINE INSPECTION. NEW MUFFLER TO BE INSTALLED.
- [SDR CA130501003](https://openairdocs.org/sdr/CA130501003.md): Wire · burned · Apr 30, 2013 · Cessna 150G · Heating System
  > (CAN) AIRCRAFT IN CRUISE FLIGHT. PILOT SAW SMOKE AND SHUT DOWN ELECTRICAL POWER TO AIRCRAFT. AIRCRAFT LANDED WITHOUT INCIDENT. INVESTIGATION FOUND RING TERMINAL LAYING ON CABIN HEAT CONTROL. WIRE TRACED BACK AND FOUND CONNECTED TO AMMETER. THIS WIRE MUST B
- [SDR 2013FA0000019](https://openairdocs.org/sdr/2013FA0000019.md): Boss · cracked · Dec 6, 2012 · N2252J · Cessna 150G · Reciprocating Engine Cylinder Section
  > ROCKER SHAFT BOSSES FOUND CRACKED WHEN CYLINDER REMOVED DUE TO FAILURE. LAST DYE CHECK WAS DONE IN 5/6/2007 (O/H DATE 1998). CYLINDER ONLY HAD 50 HRS SINCE LAST INSPECTION, BUT 5 YEARS CALENDAR TIME. POSSIBLE MORE FREQUENT DYE CHECK ON ROCKER BOSSES FOR AD
- [SDR 2012FA0000247](https://openairdocs.org/sdr/2012FA0000247.md): Spark Plug · failed · Mar 6, 2012 · N3038S · Cessna 150G · Spark Plug/Igniter
  > TESTED EIGHT REM38S SPARK PLUGS WITH 200 HRS TT AND FOUND THE RESISTORS HAD FAILED, NO RESISTANCE FOUND THROUGH THE SPARK PLUG.
- [SDR LC1R201202011501](https://openairdocs.org/sdr/LC1R201202011501.md): Skin · corroded · Feb 1, 2012 · N2217J · Cessna 150G · Horizontal Stabilizer, Plate/Skin
  > DURING A PRE-PURCHASE INSPECTION, HEAVY CORROSION WAS FOUND AT THE JOINT BETWEEN THE LT STABILIZER SKIN, PN 0432001-55 AND THE RT STABILIZER SKIN, PN 0432001-54 AT THE LOWER CENTER RIVET LINE WHICH HAD EATEN AWAY NUMEROUS RIVETS, LOOSENED THE SKIN JOINT AND BE
- [SDR 2008FA0000087](https://openairdocs.org/sdr/2008FA0000087.md): Spar · corroded · Feb 15, 2008 · N3816J · Cessna 150G · Fuselage Main, Frame
  > WINGS WERE PREVIOUSLY REMOVED TO FACILITATE TRANSPORTATION. INSPECTION OF THE LT AND RT FWD SPAR BEARING BLOCKS IN THE FUSELAGE (P/N 0411129) FOUND SEVERE CORROSION DAMAGE. IT APPEARS TO BE DISSIMILAR METAL CORROSION BETWEEN THE SPAR BLOCKS AND THE AN3-21A ATT
- [SDR 2008FA0000086](https://openairdocs.org/sdr/2008FA0000086.md): Spar · corroded · Feb 15, 2008 · Cessna 150G · Wing Spar
  > WINGS WERE PREVIOUSLY REMOVED TO FACILITATE TRANSPORTATION. INSP OF THE LT AND RT FWD SPAR BEARING BLOCKS IN THE FUSELAGE (P/N 0411129) FOUND SEVERE CORROSION DAMAGE. IT APPEARS TO BE DISSIMILAR METAL CORROSION BETWEEN THE SPAR BLOCKS AND THE AN3-21A ATTACHMEN
- [SDR 2005FA0001283](https://openairdocs.org/sdr/2005FA0001283.md): Carburetor · mismanufactured · Sep 7, 2005 · Cessna 150G · Fuel Control/Reciprocating Engines
  > ENGINE HAD BAD HESITATION ON TAKEOFF ACCELERATION. SURGING OCCURRED DURING CLIMB WITH RPM FLUCTUATIONS OF +/- 50-75 RPM. AIRCRAFT AND ENGINE FUEL SCREENS WERE REMOVED AND INSPECTED 3 TIMES IN THE LAST 50 HOURS WITH NO EVIDENCE OF CONTAMINATION. FUEL LINE TO
- [SDR 2004FA0000751](https://openairdocs.org/sdr/2004FA0000751.md): Windshield · departed · Aug 3, 2004 · N4760X · Cessna 150G · Flight Compartment Windows
  > SECTION OF WINDSHIELD DEPARTED AIRCRAFT IN FLIGHT. WINDSHIELD HAD BEEN REPAIRED 7/15/00 IAW AC43.131B CHAPTER 3 SECTION 4, BUT NO REINFORCEMENT WAS EVIDENT ON PART REMAINING IN AIRCRAFT. HOW WINDSHIELD INSTALLED. THIS COULD HAVE BEEN PREVENTED IF NEW WINDSH
- [SDR 2003FA0000977](https://openairdocs.org/sdr/2003FA0000977.md): Bushing · worn · Aug 23, 2003 · N2698J · Cessna 150G · Reciprocating Engine Cylinder Section
  > EIGHT ROCKER ARM BUSHINGS SHOWED INDICATIONS OF EXCESSIVE WEAR. THE PROBLEM WAS INDICATED AT THE FIRST OIL CHANGE (10 HOURS) AFTER ENGINE OVERHAUL AS BRONZE PARTICLES IN THE OIL FILTER. THE OVERHAULED ROCKER ARMS WERE INSTALLED IN NEW MFG CYLINDERS P/N 65381
- [SDR CA030517002](https://openairdocs.org/sdr/CA030517002.md): Rudder · binding · May 17, 2003 · Cessna 150G · Rudder Control System
  > (CAN) INCORPORATION OF AD 2000-20R1 (CESSNA S/B SEB01-1) RESULTS IN BINDING BETWEEN NEW STOP BOLTS AND RUDDER STRUCTURE DUE TO THE INCREASED SIZE OF THE STOP BOLTS. BINDING WAS NOT APPARENT UNLESS PRESSURE WAS APPLIED TO BOTH RUDDER PEDALS.
- [SDR AUS20030261](https://openairdocs.org/sdr/AUS20030261.md): Indicator · mismarked · Feb 7, 2003 · Cessna 150G · Airspeed/Mach Indicator
  > (AUS) AIR SPEED INDICATOR (ASI) LIMITS INCORRECTLY MARKED.
- [SDR AUS20021059](https://openairdocs.org/sdr/AUS20021059.md): Piston · broken · Sep 18, 2002 · Cessna 150G · Reciprocating Engine Cylinder Section
  > (AUS) PISTON SIDE BROKEN AWAY. METAL CONTAMINATION OF OIL FILTER.
- [SDR 2001FA0000286](https://openairdocs.org/sdr/2001FA0000286.md): Magneto · inoperative · Aug 25, 2001 · N2750S · Cessna 150G · Magneto/Distributor
  > INSTALLED NEW LEFT AND RIGHT SIDE SLICK (UNISON) MAGNETOS AND IGNITION HARNESS. TEST RUN OK. ON FIRST FLIGHT AFTER 15 MIN. ENGINE POWER LOSS OCCURED. AFTER LANDING FOUND LEFT MAG INOP. REMOVED MAG AND FOUND THAT COIL INSULATION HAD BURNED THROUGH AND HIGH VO
- [SDR 2001FA0000100](https://openairdocs.org/sdr/2001FA0000100.md): Bellcrank · elongated · Jun 18, 2001 · N3343J · Cessna 150G · Elevator Control System
  > FOUND ELEVATOR BELLCRANKS CABLE ATTACH POINTS ELONGATED. RIGHT ATTACH WAS ELONGATED BY.215, LEFT ATTACH WAS ELONGATED BY.248, THE AN23-11 ATTACH BOLT IS.184. DRILLED OVERSIZE AND PUT NAS 75-3-004 STEEL BUSHING PRESSED IN, TO BRING BACK CORRECT TOLERANCE.
- [SDR 20010403CW019](https://openairdocs.org/sdr/20010403CW019.md): Bulkhead · damaged · Feb 26, 2001 · N3232X · Cessna 150G · Fuselage Main, Bulkhead
  > CORROSION FOUND EXFOLIATING (1) SPAR CAP ON RIGHT WING HEAVY CORROSION ON (2) UPPER CABIN CARRY THRU STRUCTURE. (3) VERTICAL STABILIZER SKIN PILLOWED AND RIVETS POPPED. FOUND 15 RIVET HEADS PULLED THRU SKIN ON (4)CANTED BULKHEAD AT FUSELAGE STATION 20.5 BOT
- [SDR 20010403CW018](https://openairdocs.org/sdr/20010403CW018.md): Skin · damaged · Feb 26, 2001 · N3232X · Cessna 150G · Vertical Stabilizer, Plate/Skin
  > CORROSION FOUND EXFOLIATING (1) SPAR CAP ON RIGHT WING HEAVY CORROSION ON (2) UPPER CABIN CARRY THRU STRUCTURE. (3) VERTICAL STABILIZER SKIN PILLOWED AND RIVETS POPPED. FOUND 15 RIVET HEADS PULLED THRU SKIN ON (4)CANTED BULKHEAD AT FUSELAGE STATION 20.5 BOTT
- [SDR 20010403CW017](https://openairdocs.org/sdr/20010403CW017.md): Spar · corroded · Feb 26, 2001 · N3232X · Cessna 150G · Wing Spar
  > CORROSION FOUND EXFOLIATING (1) SPAR CUP ON RIGHT WING HEAVY CORROSION ON UPPER CABIN (2) CARRY THRU STRUCTURE. (3) VERTICAL STABILIZER SKIN PILLOWED AND RIVETS POPPED. FOUND 15 RIVET HEADS PULLED THRU SKIN ON (4)CANTED BULKHEAD AT FUSELAGE STATION 20.5 BOTT
- [SDR 20010403CW016](https://openairdocs.org/sdr/20010403CW016.md): Spar Cap · corroded · Feb 26, 2001 · N3232X · Cessna 150G · Wing Spar
  > CORROSION FOUND EXFOLIATING SPAR CAP OR RIGHT WING HEAVY CORROSION ON UPPER CABIN CARRY THRU STRUCTURE. VERTICAL STABILIZER SKIN PILLOWED AND RIVETS POPPED. FOUND 15 RIVET HEADS PULLED THRU SKIN ON CANTED BULKHEAD AT FUSLAGE STATION 20.5 BOTTOM FUSELAGE. AIR
- [SDR 20010403CW009](https://openairdocs.org/sdr/20010403CW009.md): Rudder Pedal · worn · Feb 19, 2001 · N3057S · Cessna 150G · Rudder Control System
  > DURING ANNUAL INSPECTION PILOTS SIDE RUDDER PEDALS AND SHAFTS WERE FOUND TO BE BADLY WORN WHERE SHAFT PINS PASS THROUGH THE HOLES. IT IS EVIDENT THAT THIS ITEM IS OVERLOOKED.
- [SDR CA001207030](https://openairdocs.org/sdr/CA001207030.md): Horn · bent · Nov 3, 2000 · Cessna 150G · Rudder Control System
  > (CAN) DURING ANNUAL INSP AND PER AD CF-2000-20, RUDDER CNTL SYS CLOSELY INSP. RT SIDE OF RUDDER HORN HAD NICKS ON LOWER OTBD EDGE AND CANTED UP SEVERAL DEGS. AT ROOT OF RT HORN WERE TEETH MARKS INDICATING PLIERS HAD BEEN USED TO ATTEMPT TO STRAIGHTEN HORN.
- [SDR CA001018005](https://openairdocs.org/sdr/CA001018005.md): Battery · wrong part · Sep 28, 2000 · Cessna 150G · Emergency Locator Beacon
  > (CAN) ELT WAS EQUIPPED WITH A NON-APPROVED BATTERY FOR THE ELT TYPE. REF: ANO B014 EDITION 4, NOVEMBER 20, 1998. (X)
- [SDR AU000989](https://openairdocs.org/sdr/AU000989.md): Piston Pin · faulty · Sep 27, 2000 · Cessna 150G · Engine System Wiring
  > (AUS) PISTON PIN FAULTY. LIMITED INFORMATION PROVIDED. (X)
- [SDR AU991100](https://openairdocs.org/sdr/AU991100.md): Torque Link · cracked · Oct 13, 1999 · Cessna 150G · Nose/Tail Landing Gear Strut/Axle
  > (AUS) NOSE LANDING GEAR UPPER TORQUE LINK CRACKED IN THREE PLACES IN THE LOWER WEB AREA. CRACK LENGTHS APPROXIMATELY 6.35MM (0.25 INCH).
- [SDR 99ZZZX2639](https://openairdocs.org/sdr/99ZZZX2639.md): Encoder · malfunctioned · May 15, 1999 · N2977J · Cessna 150G · Altimeter, Barometric/Encoder
  > MODE C REPORTED AS INVALID. RETURNED DEFECTIVE ENCODER TO MANUFACTURER FOR REPAIR. PERFORMED BI-ANNUAL TESTS AND INSPECTIONS.
- [SDR CA981230034](https://openairdocs.org/sdr/CA981230034.md): Valve · leaking · Dec 8, 1998 · Cessna 150G · Fuel Storage
  > (CAN) ONE FUEL DRAIN LEAKING AND THE OTHER STUCK. FOUND THE STUCK DRAIN HEAVILY CORRODED WITH CORROSION ON THE PLUNGER ON THE INSIDE OF THE TANK.
- [SDR AU981527](https://openairdocs.org/sdr/AU981527.md): Pedestal · broken · Nov 18, 1998 · Cessna 150G · Reciprocating Engine Cylinder Section
  > (AUS) NR 1 CYLINDER ROCKER PEDESTAL BROKEN.
- [SDR 98ZZZX4591](https://openairdocs.org/sdr/98ZZZX4591.md): Stiffener · cracked · Nov 1, 1998 · N3877J · Cessna 150G · Fuselage Miscellaneous Structure
  > STIFFENER, P/N 0412521-3, WAS FOUND CRACKED IN 4 PLACES,.25 INCH TO.3750 INCH LONG. THIS CONDITION WAS CAUSED BY LOOSE BOLTS IN PLATE, P/N 0412010-1, FITTINGS, P/N 0432005-1, AND P/N 0432005-2. BOLTS AND BOLT HOLES WERE WORN EXCESSVIELY. THIS CONDITION CA
- [SDR 98ZZZX1605](https://openairdocs.org/sdr/98ZZZX1605.md): Angle · failed · Mar 27, 1998 · N8311J · Cessna 150G · Nacelle/Pylon, Bulkhead/Firewall
  > DURING ANNUAL INSPECTION, FOUND ANGLE WHICH MOUNTS FIREWALL TO FUSELAGE BUCKLED AND POORLY REPAIRED. DAMAGE EXTENDED FROM 7 O'CLOCK TO 10 O'CLOCK POSITIONS. THE REPAIR CONSISTED OF AN ANGLE DOUBLER WITH RIVETS PASSING THROUGH BEND RADIUS AND ZERO EDGE DISTAN
- [SDR 98ZZZX1604](https://openairdocs.org/sdr/98ZZZX1604.md): Strap · failed · Mar 27, 1998 · N8311J · Cessna 150G · Fuel Storage
  > DURING ANNUAL INSPECTION, FOUND LEFT FUEL TANK AFT MOUNTING STRAP BROKEN. NOTIFIED OWNER.
- [SDR 98ZZZX1603](https://openairdocs.org/sdr/98ZZZX1603.md): Firewall · buckled · Mar 27, 1998 · N8311J · Cessna 150G · Nacelle/Pylon, Bulkhead/Firewall
  > FOUND FIREWALL BUCKLED HEAVILY ALL THE WAY ACROSS APPROXIMATELY 8 INCHES FROM BOTTOM. ALSO, BUCKLED AT ALL ENGINE MOUNT LOCATIONS. NOTIFIED OWNER.
- [SDR 98ZZZX1602](https://openairdocs.org/sdr/98ZZZX1602.md): Screw · missing · Mar 27, 1998 · N8311J · Cessna 150G · Flight Compartment Equipment
  > DURING ANNUAL INSPECTION, A SMALL HOLE WAS FOUND IN RIGHT SIDE OF FORWARD FUSELAGE BELOW WINDSHIELD. PER CESSNA SB SB 68-16, THIS BOLT IS FOR SCREW THAT SUPPORTS FORWARD END OF GLOVE BOX. THIS HOLE WAS PAINTED OVER SHOWING SCREEN HAD BEEN MISSING SINCE LAST
- [SDR 98ZZZX1484](https://openairdocs.org/sdr/98ZZZX1484.md): Bracket · displaced · Mar 27, 1998 · N8311J · Cessna 150G · Engine Mount Section
  > FOUND LEFT LOWER ENGINE MOUNT BRACKET DISPLACED FROM NORMAL POSITION. THIS MAY HAVE OCCURRED DURING UNDOCUMENTED REPAIR IN AREA BY PERSONS UNKNOWN.
- [SDR AU980325](https://openairdocs.org/sdr/AU980325.md): Cylinder · worn · Mar 24, 1998 · Cessna 150G · Reciprocating Engine Cylinder Section
  > (AUS) ENGINE CYLINDERS HAD LOW COMPRESSION. INVESTIGATION FOUND WORN EXHAUST VALVE GUIDES AND GLAZED AND OUT OF ROUND CYLINDER BORES.
- [SDR AU980484](https://openairdocs.org/sdr/AU980484.md): Guide · worn · Mar 13, 1998 · Cessna 150G · Reciprocating Engine Cylinder Section
  > (AUS) NR 3 CYLINDER WAS REMOVED FOR LOW COMPRESSION. THE EXHAUST VALVE GUIDE WAS FOUND TO BE WORN 0.483 MM (0.019 INCH). THE REMAINING CYLINDERS WERE THEN REMOVED AND ALL WERE FOUND TO BE IN A SIMILAR CONDITION. TIME IN SERVICE FOR THE CYLINDERS WAS 55 HRS.
- [SDR AU980651](https://openairdocs.org/sdr/AU980651.md): Cylinder · worn · Feb 4, 1998 · Cessna 150G · Reciprocating Engine Cylinder Section
  > (AUS) NR 2 CYLINDER WORN BEYOND LIMITS.
- [SDR 98ZZZX978](https://openairdocs.org/sdr/98ZZZX978.md): Attach Fitting · worn · Jan 28, 1998 · N8623J · Cessna 150G · Horizontal Stabilizer, Attach Fittings
  > DURING AN ANNUAL INSPECTION, FOUND THE HORIZONTAL STABILZIER LOOSE AT THE REAR ATTACHMENTS. THE STABILIZER COULD BE MOVED UP AND DOWN ABOUT.25 INCH. THE REAR ATTACH FITTINGS WERE FOUND TO BE EXCESSIVELY WORN.
- [SDR AU971518](https://openairdocs.org/sdr/AU971518.md): Valve · sticking · Nov 22, 1997 · Cessna 150G · Reciprocating Engine Cylinder Section
  > (AUS) NO4 CYLINDER EXHAUST VALVE STUCK OPEN. LOSS OF POWER AND ROUGH RUNNING RESULTED IN A FORCED LANDING IN THE BUSH.
- [SDR 99ZZZX969](https://openairdocs.org/sdr/99ZZZX969.md): Clutch · damaged · Nov 17, 1997 · N3856J · Cessna 150G · Engine Starter
  > TEETH ON PINION GEAR WERE GROUND OFF; METAL WAS FOUND IN THE OIL SUMP AND SCREEN. THIS PART WAS NEW. STC SE00262NY CANADIAN AERO MANUFACTURING.
- [SDR 97ZZZX1707](https://openairdocs.org/sdr/97ZZZX1707.md): Bulkhead · cracked · Apr 1, 1997 · N4044J · Cessna 150G · Propeller Spinner Section
  > SPINNER BULKHEAD CRACKED. SUSPECT FROM PUSHING ON SPINNER WHEN MOVING A/C AND OR PUTTING TOO MANY SHIMS ON FORWARD BULKHEAD; THUS, HAVING TO PUSH TOO HARD TO GET SCREW IN. SECOND TIME THIS BULKHEAD WAS REPLACED.
- [SDR CA970310005](https://openairdocs.org/sdr/CA970310005.md): Blade · corroded · Mar 6, 1997 · Cessna 150G · Propeller Blade Section
  > (CAN) PROPELLER WAS SENT FOR 5 YEAR INSPECTION. CORROSION WAS FOUND PAINTED OVER. PROP HAD NOT BEEN INSPECTED SINCE 1970.
- [SDR 96ZZZX5892](https://openairdocs.org/sdr/96ZZZX5892.md): Dampener · failed · Oct 31, 1996 · N2951J · Cessna 150G · Shimmy Damper
  > AIRCRAFT LANDED, RAN OFF RUNWAY PUSHING NOSE GEAR UNDER FUSELAGE. OWNER SAID PLANE DEVELOPED SHIMMY AND HE COULDN'T KEEP ON RUNWAY. CHECKED SHIMMY DAMPENER AND FOUND ONE-HALF AIR IN IT. SUBMITTER STATED SHOULD MAYBE CHECK SHIMMY DAMPENER MORE OFTEN FOR FLUI
- [SDR 96ZZZX3433](https://openairdocs.org/sdr/96ZZZX3433.md): Control Cable · chafed · Jun 6, 1996 · Cessna 150G · Aileron Control System
  > DURING A 100-HOUR INSPECTION, THE FOLLOWING DEFECTS WERE FOUND: THE AILERON CONTROL CABLE WAS SCRAPING THE PRIMER LINE(S) LOCATED IN THE FIREWALL AND A CRACK IN THE CONTROL CABLE SUPPORT BETWEEN THE INSTRUMENT PANEL AND THE FIREWALL ON THE PILOT'S SIDE.
- [SDR AU960972](https://openairdocs.org/sdr/AU960972.md): Seat Belt · wrong part · May 1, 1996 · Cessna 150G · Flight Compartment Equipment
  > (AUS) SEAT BELTS CONTAINED NON APPROVED HARDWARE AND WEBBING - UNAPPROVED PART - PERSONNEL/MAINTENANCE ERROR
- [SDR AU960443](https://openairdocs.org/sdr/AU960443.md): Crankshaft · worn · Mar 8, 1996 · Cessna 150G · Reciprocating Engine Power Section
  > (AUS) ENGINE SUFFERED TWO CRANKSHAFT MAIN BEARING EXCESSIVE WEAR INCIDENTS IN APPROXIMATELY 50 HOURS OPERATION: 1. FIRST OCCURRENCE WAS AT 8.5 HOURS AFTER INSTALLATION FOLLOWING OVERHAUL - ENGINE WAS INSPECTED/CHECKED, NEW BEARINGS AND A USED SERVICEABLE CRAN
- [SDR 96ZZZX1084](https://openairdocs.org/sdr/96ZZZX1084.md): Cylinder · cracked · Jan 1, 1996 · N3824J · Cessna 150G · Reciprocating Engine Cylinder Section
  > PILOT REPORTED A ROUGH ENGINE AND A PARTIAL LOSS OF POWER. A PRECAUTIONARY LANDING MADE ON A COUNTY ROAD. NO DAMAGE TO AIRCRAFT, PERSONNEL, OR PROPERTY. FOUND NR 4 CYLINDER CRACKED AFTER CYLINDER REMOVED. CRACK WENT THROUGH VALVE GUIDE BOSS ALLOWING GUIDE
- [SDR 96ZZZX5905](https://openairdocs.org/sdr/96ZZZX5905.md): Strap · broken · Nov 17, 1995 · N2974S · Cessna 150G · Fuel Storage
  > WHILE REPLACING RUSTY LEFT FUEL TANK COVER SCREWS, FOUND REAR INBOARD TANK STRAP BROKEN AT BEND-WEAR MARKS ON TOPS OF TANK AND TANK COVER-INDICATIONS ARE TANK COVERS HAD NEVER BEEN REMOVED SINCE MANUFACTURE-FOUND SAME PROBLEM WITH RIGHT TANK STRAP 2-9-94 AT 27

## 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 = '150G'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/cessna-150g/reports

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