# Service difficulty reports: Cessna 177B

A list on [Cessna 177B](https://openairdocs.org/model/cessna-177b.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 65 reports

- [SDR 2023FA0000027](https://openairdocs.org/sdr/2023FA0000027.md): Aileron · restricted · Jan 12, 2023 · N34739 · Cessna 177B · Aileron Control System
  > INSTALLATION OF TRUTRAK AUTOPILOT STC'D ROLL SERVO LIMITED AILERON TRAVEL. THE SERVO ARM IS CONNECTED TO THE RIGHT AILERON BELLCRANK VIA A ROD. THE SERVO ARM CONTACTED A SERVO BRACKET IN THE AFT DIRECTION AND THE BOLT ATTACHING THE ROD TO THE ARM CONTACTED TH
- [SDR CA190719009](https://openairdocs.org/sdr/CA190719009.md): Spar · corroded · Jul 19, 2019 · Cessna 177B · Wing Spar
  > (CAN) DURING INSPECTION OF LOWER SPAR CARRY THRU FOR CORROSION, SEVERAL (5) SMALL SPOTS OF CORROSION FOUND ON UPPER SURFACE OF THE LOWER FORWARD SPAR FLANGE. SIZE OF CORROSION VARRIED FROM 5 MM TO 10 MM.APPEARS TO BE SURFACE ONLY. TEXTRON CESSNA CONTACTED AND
- [SDR CA140909009](https://openairdocs.org/sdr/CA140909009.md): Bracket · cracked · Sep 8, 2014 · Cessna 177B · DC Generator-Alternator
  > (CAN) WITH THE ALTERNATOR REMOVED FROM ITS MOUNTING BRACKET FOR CLOSER INSPECTION, IT WAS NOTED THAT THE BRACKET HAD 2 CRACKS, 1 FROM EACH HOLE USED FOR THE SINGLE MOUNTING BOLT. EACH CRACK WENT FROM THE HOLE TO THE CLOSEST EDGE OF THE MATERIAL. ALSO, WHILE T
- [SDR 2012FA0000552](https://openairdocs.org/sdr/2012FA0000552.md): Gasket · not seated · Aug 9, 2012 · N110PF · Cessna 177B · Reciprocating Engine Oil System
  > DURING REPLACEMENT OF THE CANISTER-TYPE OIL FILTER AT THE TIME OF OIL CHANGE, IT IS DIFFICULT TO ACHIEVE A GOOD SEAL OF THE CANISTER AGAINST THE SEAT THROUGH THE FILTER GASKET THAT IS SUPPLIED WITH THE CFO100-1 FILTER KIT. THE GASKET VERY EASILY SLIPS INSIDE
- [SDR 2011FA0000283](https://openairdocs.org/sdr/2011FA0000283.md): Shock Mount · broken · May 2, 2011 · N11625 · Cessna 177B · Instrument Panel
  > THE DIRECT CONTACT OF THE DIRECTIONAL GYRO WITH THE CONTROL COLUMN AS A RESULT OF THE SHOCK MOUNTED BRACKET COMING FREE FROM THE INSTRUMENT PANEL; POSSIBLY THE REASON WHY THE CONTROL YOKE WAS NOT ABLE TO MOVE BACK MORE THEN 1 INCH. THERE WAS IMPROPER HARDWARE
- [SDR CA110314014](https://openairdocs.org/sdr/CA110314014.md): O-Ring · worn · Mar 11, 2011 · Cessna 177B · Aircraft Fuel Distribution System
  > (CAN) DURING A PRE-FLIGHT INSPECTION, THE OWNER/PILOT OF THE AIRCRAFT NOTICED A STRONG FUEL SMELL IN THE CABIN. UPON FURTHER INSPECTION, MAINTENANCE PERSONNEL DISCOVERED FUEL LEAKING FROM THE FUEL VALVE ASSEMBLY MOUNTED ON THE INSIDE OF THE FIREWALL. THE UNIT
- [SDR CA101116019](https://openairdocs.org/sdr/CA101116019.md): Alternator · malfunctioned · Oct 29, 2010 · Cessna 177B · DC Generator-Alternator
  > AMMETER SHOWING DISCHARGE IN FLIGHT. ALTERNATOR REPLACED.
- [SDR CA100924008](https://openairdocs.org/sdr/CA100924008.md): Starter · weak · Sep 23, 2010 · Cessna 177B · Engine Starter
  > STARTER IS WEAK AND HAS SLOW CRANKING SPEED.
- [SDR CA100915001](https://openairdocs.org/sdr/CA100915001.md): Control Cable · broken · Sep 14, 2010 · Cessna 177B · Air Intake Anti/De-Ice System
  > CARB HEAT CONTROL CABLE BROKE WHERE IT ENTERS THE SHEATH. CABLE WAS REPLACED AND NO FURTHER ISSUES.
- [SDR CA090923001](https://openairdocs.org/sdr/CA090923001.md): Carburetor · malfunctioned · Sep 15, 2009 · Cessna 177B · Fuel Control/Reciprocating Engines
  > (CAN) CAUSES RPM TO STUMBLE AND DROPOFF GOING THROUGH 1500 RPM, POOR IDLE CUTOFF (TC# 20090923001)
- [SDR CA090812001](https://openairdocs.org/sdr/CA090812001.md): Air Box · cracked · Aug 7, 2009 · Cessna 177B · Engine Air Intake System
  > FOUND CRACKED IN TWO PLACES.
- [SDR CA090731002](https://openairdocs.org/sdr/CA090731002.md): Carburetor · malfunctioned · Jul 30, 2009 · Cessna 177B · Fuel Control/Reciprocating Engines
  > (CAN) ENG RPM FLUCTUATES AT 1500 RPM-MID RANGE MIXTURE THICK.
- [SDR 2009FA0000305](https://openairdocs.org/sdr/2009FA0000305.md): Gasket · not seated · Apr 17, 2009 · N1351C · Cessna 177B · Reciprocating Engine Oil System
  > DURING REPLACEMENT OF THE CANISTER-TYPE OIL FILTER AT THE TIME OF OIL CHANGE, IT IS TRICKY TO ACHIEVE A GOOD SEAL OF THE CANISTER AGAINST THE SEAT THROUGH THE FILTER GASKET THAT IS SUPPLIED WITH THE CFO100-1 FILTER KIT. THE GASKET VERY EASILY SLIPS INSIDE THE
- [SDR 2009FA0000090](https://openairdocs.org/sdr/2009FA0000090.md): Line · cracked · Jan 20, 2009 · N30740 · Cessna 177B · Engine Oil Distribution (Airframe Furnished)
  > LINE CRACKED AT FWD FLARE AT STEEL NUT PN AN818-6, CAUSING LOSS OF ENGINE OIL. PREVIOUS MAINTENANCE FOR REPORTED OIL LEAK. REPLACED CRANKCASE SEAL. ENGINE RUN UP PERFORM, NO OIL LEAKS NOTED. ACFT RETURNED TO SERVICE. (K)
- [SDR MALA080223](https://openairdocs.org/sdr/MALA080223.md): Pdu · malfunctioned · Dec 14, 2008 · N410 · Cessna 177B · Hydraulic System, Main
  > "AFTER T/O SELECTED GEAR UP AND HYDRAULIC CAUTION LIGHT ILLUMINATED. COMPLETED MEMORY ITEMS THEN COMPLETED AFTER T/O CHECK. COMPLETED EMERGENCY/NON-NORMAL CHECKLIST HYDRAULIC PROC 2. RETURNED TO TRI. DECLARED EMERGENCY AND RETURNED TO GATE. FLAPS REMAINED
- [SDR 2008FA0000288](https://openairdocs.org/sdr/2008FA0000288.md): Bulkhead · cracked · Apr 1, 2008 · N99NA · Cessna 177B · Wing, Rib/Bulkhead
  > DURING ROUTINE INSPECTION, FOUND PART CRACKED. CHECKED (2) OTHER CARDINALS THAT HAPPENED TO BE IN OUR SHOP AND FOUND (1) OF THEM TO HAVE A SIMILAR CRACK. THIS SECTION OF THE BULKHEAD IS THE ATTACH STRUCTURE FOR THE LOWER ATTACH ANGLE FOR THE IB FLAP DRIVE BE
- [SDR 2008FA0000018](https://openairdocs.org/sdr/2008FA0000018.md): Yoke · misinstalled · Jan 8, 2008 · N30673 · Cessna 177B · Control Column Section
  > WHILE DOING AN ANNUAL, FOUND LOOSENESS IN THE YOKE FOR AND AFT MOVEMENT. AFTER MUCH CHECKING, FOUND THE LOOSENESS TO BE BETWEEN THE YOKE LEVER ASSY 1767033-7 AND 1767037-2 WHICH IS THE SHAFT. ALSO THERE WAS LOOSENESS BETWEEN THE SHAFT 1767037-2 AND THE QUADRA
- [SDR CA061108004](https://openairdocs.org/sdr/CA061108004.md): Hinge Bracket · cracked · Aug 28, 2006 · Cessna 177B · Elevator Structure
  > (CAN) RT STABILIZER HINGE BRACKET FOUND CRACKED AT FASTENER LOCATION. (TC NR 20061108004)
- [SDR 2006FA0000624](https://openairdocs.org/sdr/2006FA0000624.md): Shimmy Dampener · leaking · Jun 7, 2006 · N34597 · Cessna 177B · Landing Gear System
  > PART BECAME SUSPECT WHEN DAMPENER FLUID WAS NOTICED DRIPPING OFF END OF SHAFT. DURING THE CLEANING/INSP. COMPRESSED AIR WAS INTRODUCED TO SHAFT'S OPEN END. AIR BUBBLES WERE OBSERVED AT BASE OF PISTON. FOUND CRACK ON DAMPENER SHAFT AT BASE OF PISTON. CRACK IS
- [SDR MCC2006F00000](https://openairdocs.org/sdr/MCC2006F00000.md): Brake Assy · burned · Feb 28, 2006 · N1205C · Cessna 177B · Brake
  > BRAKE FIRE AFTER TAKEOFF. DISCOVERED AFTER ARRIVAL, BRAKE WAS SATURATED WITH BURNED HYDRAULIC FLUID, BOTH LOWER BRAKE LINES DAMAGED AND NR 4 TIRE IS BURNED TO CORD. (K)
- [SDR AU510001681](https://openairdocs.org/sdr/AU510001681.md): Rod End · separated · Feb 7, 2005 · Cessna 177B · Power Lever
  > CARBURETOR THROTTLE ARM DISCONNECTED FROM RODEND DUE TO USE OF INCORRECT HARDWARE. LIMITED INFORMATION PROVIDED. PERSONNEL/MAINTENANCE ERROR.
- [SDR 2004FA0000068](https://openairdocs.org/sdr/2004FA0000068.md): Air Filter · mismanufactured · Jan 5, 2004 · N30695 · Cessna 177B · Engine Air Intake System
  > FACTORY NEW PART- SCREEN ATTACH TABS ARE BENT 90, AND SPOT WELDED ON TO SCREEN FRAME. WELDS DO NOT PENETRATE BASE MATERIAL. ATTACH TABS WORK LOOSE. HAVE FOUND THIS CONDITION 3 TIMES. SOME HAVE BEEN REPAIRED WITH SHEET METAL SCREWS. TABS SHOULD BE RIVETED
- [SDR CA030723004](https://openairdocs.org/sdr/CA030723004.md): Rotor · worn · Jul 16, 2003 · Cessna 177B · AC Generator-Alternator
  > (CAN) ALTERNATOR WAS REMOVED AT 225.9 HRS BECAUSE OF DECREASING OUTPUT & VOLTAGE AS ELECTRICAL LOAD WAS APPLIED. ON DISASSEMBLY, TWO DEFECTS WERE FOUND. THE ROTOR SHAFT BEARING JOURNAL AT THE DRIVE END WAS FOUND LOOSE TO THE BEARING BY ABOUT.080 INCHES, ALLO
- [SDR DLD2003F00000](https://openairdocs.org/sdr/DLD2003F00000.md): Shroud · failed · Jun 16, 2003 · N34229 · Cessna 177B · Engine Collector/Tailpipe/Nozzle
  > THE SCREEN THAT KEEPS FOREIGN MATERIAL FROM ENTERING CARBURETOR WHEN CARB HEAT IS ON. SPOT WELDS THAT HOLD SCREEN IN PLACE ARE COMING LOOSE AND LETTING SCREEN VIBRATE AND COME APART. THIS WOULD LET PIECES OF THE SCREEN GO INTO ENGINE WHEN CARB HEAT IS ON.
- [SDR CA030424005](https://openairdocs.org/sdr/CA030424005.md): Magneto · misoverhauled · Apr 14, 2003 · Cessna 177B · Magneto/Distributor
  > (CAN) MAGNETO FAILED ON LT PORTION (DUAL MAG) ON RUN UP. MAGNETO WAS REMOVED AND EXAMINED, BUT NO OBVIOUS DAMAGE OR FAILURE WAS EVIDENT. AS THE PART ONLY HAD 72.5 HOURS SINCE ENGINE WAS OVERHAULED. REPAIRED THE MAGNETO. WHEN I RECEIVED THE MAGNETO BACK AFTER
- [SDR CA020730006](https://openairdocs.org/sdr/CA020730006.md): Rotor · out of tolerance · Jul 29, 2002 · Cessna 177B · DC Generator-Alternator
  > (CAN) NEW ROTOR WAS INSTALLED AT OVERHAUL. AFTER 374 HRS, UNIT FAILED TO PRODUCE OUTPUT. ON DISASSEMBLY AND INSPECTION, ONE BRUSH WAS FOUND COMPLETELY WORN OUT, AND THE BRUSH SHUNT BRAIDED LEAD WAS CHAFED IN TWO. FOUND THAT THE SLIP RINGS ON THE ROTOR WERE OU
- [SDR A852002F00000](https://openairdocs.org/sdr/A852002F00000.md): Valve · failed · Apr 15, 2002 · N20300 · Cessna 177B · Vacuum Distribution System
  > VALVE WAS REPLACED WAS WITH IN SERIAL NUMBERS TO BE RE-USED IN MOD TO SVS V SYSTEM TO COMPLY WITH ALTERNATE METHOD OF COMPLAIANCE TO AD. VALVE WAS FOUND TO HAVE FAILED INT HE OPEN POSITION ON BACK UP SIDE.
- [SDR 2001FA0000379](https://openairdocs.org/sdr/2001FA0000379.md): Panel · loose · Sep 9, 2001 · N13519 · Cessna 177B · Fuselage Miscellaneous Structure
  > OWNER/OPERATOR REPORTED THAT CONTROL YOKE WOULD NOT PULL BACK TO RAISE THE ELEVATOR. ON INSPECTION IT WAS FOUND THAT THE PANEL MOUNT TRAY FOR THE TRANSPONDER ON THE RIGHT SIDE OF THE PANEL HAD DROPPED.2500 OF INCH AND WAS CONTAINING AND RESTRICTING AFT MOVEM
- [SDR 20010222CW001](https://openairdocs.org/sdr/20010222CW001.md): Lever · broken · Jan 25, 2001 · N16021 · Cessna 177B · Mixture Control
  > MIXTURE CONTROL BROKE ON GROUND RUN UP. BREAK APPEARS TO BE DEFECT IN MATERIAL.
- [SDR 20001109SH016](https://openairdocs.org/sdr/20001109SH016.md): Cylinder · broken · Oct 30, 2000 · N13472 · Cessna 177B · Reciprocating Engine Cylinder Section
  > THE PUSH ROD TUBE RETAINER CLIPS, PN SL14995, IN NR 2, NR 3, AND NR 4 VALVE COVERS WERE BROKEN OFF AT THE BOLT HEADS. DETECTION WAS DUE TO A DENT IN THE VALVE COVER OF NR 2 CYLINDER. SUBMITTER STATED IT APPEARED TO BE A MATERIAL DEFECT. (X)
- [SDR 20001109SH015](https://openairdocs.org/sdr/20001109SH015.md): Cylinder · broken · Oct 30, 2000 · N13472 · Cessna 177B · Reciprocating Engine Cylinder Section
  > THE PUSH ROD TUBE RETAINER CLIPS, PN SL14995, IN NR 2, NR 3, AND NR 4 VALVE COVERS WERE BROKEN OFF AT THE BOLT HEADS. DETECTION WAS DUE TO A DENT IN THE VALVE COVER OF NR 2 CYLINDER. SUBMITTER STATED IT APPEARED TO BE A MATERIAL DEFECT. (X)
- [SDR 20001109SH014](https://openairdocs.org/sdr/20001109SH014.md): Cylinder · broken · Oct 30, 2000 · N13472 · Cessna 177B · Reciprocating Engine Cylinder Section
  > THE PUSH ROD TUBE RETAINER CLIPS, SL 14995, IN NR 2, NR 3, AND NR 4 VALVE COVERS WERE BROKEN OFF AT THE BOLT HEADS. DETECTION WAS DUE TO A DENT IN THE VALVE COVER OF NR 2 CYLINDER. SUBMITTER STATED IT APPEARED TO BE A MATERIAL DEFECT. (X)
- [SDR 20001019SH013](https://openairdocs.org/sdr/20001019SH013.md): Condenser · inoperative · Jul 11, 2000 · N34194 · Cessna 177B · Magneto/Distributor
  > THE AIRCRAFT MADE AN EMERGENCY LANDING IN A FIELD AFTER A LOSS OF ENGINE POWER. INSPECTION BY A MECHANIC REVEALED THE POINTS WERE BURNED AND THE CONDENSER WERE PART OF A NEWLY INSTALLED FACTORY REMANUFACTURED MAGNETO. THE POINTS AND CONDENSER WERE REPLACED,
- [SDR 2000ZZZX614](https://openairdocs.org/sdr/2000ZZZX614.md): Shimmy Dampener · broken · Feb 24, 2000 · N35033 · Cessna 177B · Shimmy Damper
  > AFTER REPLACING AN OLD SHIMMY DAMPENER WITH A NEW ONE AT APPROXIMATELY 100 HOURS IN SERVICE, THE NEW PART BROKE AT THE OUTER C-CLAMP RING SPLITTING THE OUTER CYLINDER CASE. THIS HAPPENED AS THE AIRCRAFT STOPPED SHIMMING. THE END PLUG, C-CLAMP AND ALL FLUID W
- [SDR CA000224020](https://openairdocs.org/sdr/CA000224020.md): Cable · damaged · Feb 9, 2000 · Cessna 177B · Power Lever
  > (CAN) DURING APPROACH ENGINE POWER INCREASED. PILOT COULD NOT CNTL ENGINE WITH THROTTLE CNTL AND CARRIED OUT A MISSED APPROACH. ON A SUBSEQUENT APPROACH AND LANDING, PILOT USED MIXTURE CNTL TO SHUT DOWN ENGINE PRIOR TO TOUCHDOWN. A/C HAD TO BE TOWED FROM RU
- [SDR CA991229057](https://openairdocs.org/sdr/CA991229057.md): Coupling · failed · Dec 13, 1999 · Cessna 177B · Vacuum Distribution System
  > (CAN) DURING CRUISE FLIGHT, THE VACUUM SYSTEM FAILED. MAINTENANCE FOUND THE VACUUM PUMP FAILED AT THE DRIVE COUPLING.
- [SDR CA990812005](https://openairdocs.org/sdr/CA990812005.md): Points · worn · Aug 2, 1999 · Cessna 177B · Magneto/Distributor
  > (CAN) ACCELERATED WEAR OF POINTS IN MAGNETO SUSPECTED BY OPERATOR.
- [SDR 99ZZZX2346](https://openairdocs.org/sdr/99ZZZX2346.md): Cylinder · cracked · Jun 11, 1999 · N67MM · Cessna 177B · Reciprocating Engine Cylinder Section
  > NR 2 CYLINDER DEVELOPED AN OIL LEAK DIAGNOSED AS A CRACK THROUGH THE CYLINDER CASTING IN THE AREA OF THE INTAKE VALVE SEAT. UPON REMOVING THE CYLINDER FOR EXCHANGE UNDER WARRANTY, THE EXHAUST AND INTAKE ROCKER ARMS WERE DISCOVERED SWAPPED AS DELIVERED FROM TH
- [SDR AU990416048](https://openairdocs.org/sdr/AU990416048.md): Blade · corroded · Apr 12, 1999 · Cessna 177B · Propeller Blade Section
  > (AU) PROPELLER RECEIVED FOR CORROSION INSPECTION. THE PROPELLER BLADES WERE FOUND CORRODED ON THE LEADING EDGES AND THE BUTTS. THIS PROPELLER WAS LAST INSPECTED ON 7 NOVEMBER 1990.
- [SDR CA990129008](https://openairdocs.org/sdr/CA990129008.md): Cylinder · worn · Jan 15, 1999 · Cessna 177B · Propeller Hub Section
  > (CAN) PROPELLER CYLINDER WORN BEYOND MANUFACTURER'S LIMITS.
- [SDR 99ZZZX397](https://openairdocs.org/sdr/99ZZZX397.md): Seal · torn · Dec 1, 1998 · N177A · Cessna 177B · Engine Air Intake System
  > THE RUBBER SEAL AROUND THE EDGE OF THE VALVE RIPPED AND LOOKED LIKE IT WOULD HAVE BEEN SUCKED INTO THE ENGINE IN A COUPLE OR MORE HOURS. SUBMITTER STATED THE RUBBER SEAL LOOKED LIKE IT WAS MADE FROM THE WRONG MATERIAL. TT ON PART, 8 HOURS.
- [SDR 98ZZZX3058](https://openairdocs.org/sdr/98ZZZX3058.md): Wheel Pant · cracked · Jul 21, 1998 · N28P · Cessna 177B · Landing Gear/Wheel Fairing
  > INSPECTION FOUND LEFT HAND FIBERGLASS WHEEL PANTS ATTACHING BOLT HOLE MOUNT HOLE HAS 2 INCH LONG CRACK.
- [SDR CA980602093](https://openairdocs.org/sdr/CA980602093.md): Blade · corroded · Jun 2, 1998 · Cessna 177B · Propeller Blade Section
  > (CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. PROPELLER BLADE FOUND DAMAGED. BLADE REPAIRED AND BLADE ANODIZED.
- [SDR CA980519010](https://openairdocs.org/sdr/CA980519010.md): Blade · damaged · May 4, 1998 · Cessna 177B · Propeller Blade Section
  > (CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. THE LEADING EDGES OF THE PROPELLER BLADES WERE FOUND NICKED. THE BLADES HAD NOT BEEN REPAIRED PER THE MCCAULEY MANUAL.
- [SDR 97ZZZX3380](https://openairdocs.org/sdr/97ZZZX3380.md): Hose · leak · Jul 3, 1997 · N19974 · Cessna 177B · Engine Fuel Distribution
  > DURING ANNUAL INSPECTION, FUEL WAS SHUT OFF FOR CLEANING CARBURETOR, DRAIN, AND GASCULATOR. UPON TURNING FUEL ON, FUEL LEAKED FROM HOSE IN A STEADY STREAM. HOSE WAS LOCATED ON LOW PRESSURE SIDE FEEDING ENGINE DRIVEN PUMP. HOSE WAS ALSO IN A LOCATION WHERE I
- [SDR 97ZZZX3379](https://openairdocs.org/sdr/97ZZZX3379.md): Cylinder · failed · Jul 3, 1997 · N19974 · Cessna 177B · Shimmy Damper
  > SHIMMY DAMPENER HOUSING FAILED DURING FLIGHT. UNIT FAILED AT THE OUTER PORTION OF OUTER RETAINING RING FLANGE. FAILURE WAS ON DOWN-WIND LEG AFTER A NORMAL TOUCH AND GO. SUBMITTER STATES OWNER MENTIONED SEVERAL YEARS AGO, TWO SEPARATE SEVERE SHIMMY INSTANCES
- [SDR 97ZZZX3405](https://openairdocs.org/sdr/97ZZZX3405.md): Spar · corroded · Jun 1, 1997 · N35090 · Cessna 177B · Wing Spar
  > FOUND ON ANNUAL INSPECTION, INTERGRANULAR CORROSION ON CARRY-THROUGH SPAR. SOME SPOTS 2 INCHES AND.0625 INCH DEEP, PLUS OTHER CORROSION. SUBMITTER STATED THIS IS HARD TO SEE WITHOUT REMOVING HEADLINER.
- [SDR 97ZZZX1915](https://openairdocs.org/sdr/97ZZZX1915.md): Casting · creep · Apr 11, 1997 · N17142 · Cessna 177B · Altimeter, Barometric/Encoder
  > INCOMING INSPECTION CHECKS ON ALTIMETER REVEALED JUMPS IN THE OPERATION OF 100 FEET TO 200 FEET. THE END-SHAKES ON THE MECHANISM SHAFTS WERE MEASURED. ONE END-SHAKE MEASURED ZERO. THE OH MANUAL CALLS OUT A MINIMUM END-SHAKE OF.0020 INCH ON ALL THREE CRITICA
- [SDR 97ZZZX531](https://openairdocs.org/sdr/97ZZZX531.md): Fitting · loose · Dec 3, 1996 · N13468 · Cessna 177B · Wing, Fuselage Attach Fittings
  > DURING ANNUAL INSPECTION, IT WAS DISCOVERED THAT THERE WAS MOVEMENT IN THE WING ATTACH FITTINGS WHERE ATTACH PIN ATTACHES WING TO FUSELAGE. THE AMOUNT OF MOVEMENT WAS.0035 INCH BY MEASUREMENT.
- [SDR 96ZZZX5807](https://openairdocs.org/sdr/96ZZZX5807.md): Hose · leaking · Oct 24, 1996 · N34933 · Cessna 177B · Engine Fuel Distribution
  > PILOT REPORTED A FUEL LEAK FROM THE ENGINE COMPARTMENT. FOUND THE FUEL PRESSURE HOSE LEAKING. THIS PROBLEM HAS BEEN ADDRESSED BY AEROQUIP SB AA135. THIS HOSE WAS DATED 2Q86. ALTERNATE P/N FROM CESSNA: S1236-3-0092.

Next page: https://openairdocs.org/model/cessna-177b/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 = '177B'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/cessna-177b/reports

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