# Service difficulty reports: Cessna 182B

A list on [Cessna 182B](https://openairdocs.org/model/cessna-182b.md).

Newest first. General aviation reporting is voluntary.

- [SDR 2021FA0000304](https://openairdocs.org/sdr/2021FA0000304.md): Gasket · failed · Jul 30, 2021 · N2605G · Cessna 182B · Reciprocating Engine Oil System
  > ON SHUT DOWN NOTICED POOL OF OIL ON RAMP AND THICK ALONG ENTIRE BELLY. MEASURED 5 QTS OIL REMAINING. INSPECTION REVEALED FIBER GASKET SHOWED NICK AND DEFORMATION OF OIL FILTER ADAPTER GASKET SWIFT PN FM-07. ON REMOVAL IT WAS CONFIRMED THAT GASKET ON OIL FILT
- [SDR GEN202108060001](https://openairdocs.org/sdr/GEN202108060001.md): Gasket · deformed · Jul 30, 2021 · N2605G · Cessna 182B · Reciprocating Engine Oil System
  > ON SHUTDOWN, NOTICED A POOL OF OIL ON THE RAMP, AND THICK ALONG THE ENTIRE BELLY. MEASURED 5 QTS OF OIL REMAINING. INSPETION REVEALED THE FIBER GASKET SHOWED A NICK AND DEFROMATION OF THE OIL FILTER ADAPTER. ON REMOVAL, CONFIRMED THE GASKET ON THE OIL FILTER
- [SDR CA140717012](https://openairdocs.org/sdr/CA140717012.md): Muffler · cracked · Jul 8, 2014 · Cessna 182B · Engine Noise Suppressor
  > (CAN) AD CF-90-03 R2 EXHAUST TYPE CABIN HEATER INSPECTION CARRIED OUT. FOUND EXHAUST CRACKED AT RIGHT HAND INLET FLANGE RADIUS. EXHAUST MUFFLER, LEFT HAND & RIGHT HAND EXHAUST HEADER PIPES REMOVED. SENT TO MANUFACTURER FOR REPAIR & FIT INSPECTION.
- [SDR 2013FA0000557](https://openairdocs.org/sdr/2013FA0000557.md): Nut · backed out · Sep 25, 2013 · N2653G · Cessna 182B · Fuselage, Landing Gear Attach Fittings
  > DURING AN INVESTIGATION CONCERNING A NLG COLLAPSE, DISCOVERED THE LOWER STRUT SUPPORT BRACKET ONLY HAD 1 OF 2 BOLTS SECURING IT. AFTER THE ACFT LANDED, THE BRACKET BROKE AWAY FROM THE NOSE GEAR. AS THE ACFT TURNED ONTO THE TAXIWAY, LATERAL LOADS CAUSED THE U
- [SDR CA121126014](https://openairdocs.org/sdr/CA121126014.md): Pivot · cracked · Nov 12, 2012 · Cessna 182B · Wheel/Ski/Float
  > (CAN) CRACK DISCOVERED ON THE TUBE OF THE BOW WHEEL PIVOT ASSY. CRACK FORMED CLOSE TO WHERE THE ARM ASSY MOUNTS TO THE BOW OF THE FLOAT.
- [SDR 2010FA0001191](https://openairdocs.org/sdr/2010FA0001191.md): Gps · failed · Oct 2, 2010 · N2267G · Cessna 182B · Global Positioning System
  > ALTITUDE 11,000 (VFR ON TOP - IFR FLIGHT PLAN) DURING CRUISE FLIGHT THE GARMIN GPS 430W FAILED TO THE DR MODE. SATELLITE ACQUISITION WAS LOST. AFTER ABOUT 30 MINUTES IT RE-ACQUIRED THE SATELLITES AND CONTINUED TO FUNCTION TO DESTINATION. TRANSITIONED TO A GARM
- [SDR CA100706011](https://openairdocs.org/sdr/CA100706011.md): Support · cracked · Jul 2, 2010 · Cessna 182B · Fuselage, Landing Gear Attach Fittings
  > LT MLG OTBD SUPPORT ASSY (PRIMARY STRUCTURE) FOUND CRACKED DURING ANNUAL INSP. CRACK PROPOGATED THROUGH SUPPORT FITTING AND U-BOLT HOLE. CRACK VISUAL TO NAKED EYE. LOCATED AT AFT END OF CUTOUT FOR L/G SPRING.
- [SDR 2009FA0000299](https://openairdocs.org/sdr/2009FA0000299.md): Elt · broken · Apr 8, 2009 · N2642G · Cessna 182B · Emergency Locator Beacon
  > WHILE UNDER INITIAL TEST, JUST PRIOR TO INSTALLING THIS NEW UNIT IN THE ACFT, THE CONTROL TOGGLE SWITCH ON THE FRONT OF THE UNIT BROKE, THE TOGGLE ARM CAME OFF. IT WAS NOT ABUSED IN ANY WAY, IT WAS JUS A NORMAL TEST. UNIT IS BEING REPAIRED, BUT WHEN CALLED
- [SDR CA090319012](https://openairdocs.org/sdr/CA090319012.md): Engine · making metal · Dec 10, 2008 · Cessna 182B · Engine (Reciprocating)
  > FERRIOUS METAL WAS FOUND IN FILTER, THE TEARDOWN FOUND.
- [SDR AUS20040392](https://openairdocs.org/sdr/AUS20040392.md): Bulkhead · cracked · Jan 13, 2004 · Cessna 182B · Fuselage Main, Bulkhead
  > (AUS) FUSELAGE BULKHEAD CRACKED IN AREA DESCRIBED IN AD/CESSNA180/75AMDT2. CRACK LENGTH APPROXIMATELY 38.1MM (1.5IN). AD IS NOT APPLICABLE TO THIS MODEL AIRCRAFT.
- [SDR 2003FA0001216](https://openairdocs.org/sdr/2003FA0001216.md): Gear · worn · Sep 23, 2003 · N7150E · Cessna 182B · Reciprocating Engine Rear Section
  > TEETH TOO SHALLOW, TOOTH DEPTH WAS 0.152, NORMAL.0.180 TO 0.185.
- [SDR AUS20031098](https://openairdocs.org/sdr/AUS20031098.md): Hub · wrong part · Sep 23, 2003 · Cessna 182B · Propeller Hub Section
  > (AUS) PROPELLER HUB FAULTY. DURING COMPLIANCE WITH AD/PMC/47 IT WAS FOUND THAT THE MOUNTING STUDS HAD BEEN INCORRECTLY SEALED. SILASTIC MATERIAL WAS USED FOR SEALING RATHER THAN THE CORRECT PROCEDURE AS INDICATED IN MFG SL 1993-17. THE HUB WAS ALSO INCORRECTL
- [SDR CA030703010](https://openairdocs.org/sdr/CA030703010.md): Skin · cracked · Jun 27, 2003 · Cessna 182B · Fuselage Main, Plate/Skin
  > (CAN) AIRCRAFT IS USED FOR PARACHUTE OPERATIONS AND DOES MANY CYCLES. ON INSPECTION FOUND VISIBLE CRACK ABOUT 1 INCH LONG AT REAR OF GEAR CUT OUT.
- [SDR AUS20020087](https://openairdocs.org/sdr/AUS20020087.md): Blade · misrepaired · Jan 21, 2002 · Cessna 182B · Propeller Blade Section
  > (AUS) INSPECTION OF PROPELLER WHEN RECEIVED FOR REPAIR FOUND THAT THE BLADE THREADS HAD BEEN TRUNCATED TO COMPLY WITH AD/PMC/24/3 BUT HAD NOT BEEN SHOT PEENED. THE RETENTION NUTS DID NOT HAVE THE O-RING GROOVE WIDENED AS LISTED IN SL 1990-2. AD/PMC/41HAD NOT B
- [SDR 2001FA0000551](https://openairdocs.org/sdr/2001FA0000551.md): Adapter · defective · Nov 14, 2001 · N7179E · Cessna 182B · Reciprocating Engine Oil System
  > NO OIL PRESSURE UPON ENGINE START UP. OIL PUMP, SUCTION TUBE, AND CONNECTIONS CHECKED OK. REMOVED FILTER ADAPTER, INSTALLED FILTER SCREEN ENGINE HAD PROPER OIL PRESSURE. NO APPARENT DAMAGE TO FILTER ADAPTER.
- [SDR 20001227SH012](https://openairdocs.org/sdr/20001227SH012.md): Vent Line · corroded · Dec 7, 2000 · N2711G · Cessna 182B · Fuel Storage
  > DURING AN ANNUAL INSPECTION, THE FUEL TANK VENT CARRY-THROUGH WAS FOUND CORRODED THROUGH AT SEVERAL POINTS ALONG THE TUBINGS LENGTH. FUEL STAINS WERE ALSO VISIBLE. THE VENT LINE WAS HIDDEN BEHIND A LAYER OF FIBERGLASS INSULATION. THIS PART CAN ONLY BE INSPE
- [SDR CA990907070](https://openairdocs.org/sdr/CA990907070.md): Support · cracked · Aug 27, 1999 · Cessna 182B · Fuselage, Landing Gear Attach Fittings
  > (CAN) LEFT MLG OUTBOARD SUPPORT FITTING CRACKED AT REAR U-BOLT HOLE.
- [SDR 99ZZZX2777](https://openairdocs.org/sdr/99ZZZX2777.md): Control Cable · misinstalled · Jul 9, 1999 · N2356G · Cessna 182B · Elevator Control System
  > DURING RAMP INSPECTION BY THE FAA, IT WAS DISCOVERED THE ELEVATOR WOULD NOT MOVE TO THE DOWN POSITION. IT WAS FOUND THAT AN AVIONICS (COAX) CABLE WAS ROUTED IN FRONT OF THE FLIGHT CONTROLS TEE BEHIND THE INSTRUMENT PANEL AND WAS BLOCKING ANY FORWARD MOVEMENT
- [SDR CA970902015](https://openairdocs.org/sdr/CA970902015.md): Cylinder · cracked · Jul 24, 1997 · Cessna 182B · Reciprocating Engine Cylinder Section
  > (CAN) PILOT REPORTED POWER LOSS AND TEMPORARY ENGINE FAILURE. POST FLIGHT INSPECTION FOUND NR1 CYLINDER CRACKED.
- [SDR 97ZZZX24](https://openairdocs.org/sdr/97ZZZX24.md): U-Bolt · cracked · Dec 13, 1996 · N2340G · Cessna 182B · Main Landing Gear Attach Section
  > DURING ANNUAL INSPECTION, THE MLG U-BOLT NUTS WERE CHECKED FOR SECURITY. THE REAR RIGHT U-BOLT NUT WAS FOUND TO BE LOOSE. SUBSEQUENT INSPECTION REVEALED A PRE-EXISTING CRACK HAD ALLOWED THE U-BOLT TO STRETCH. THE U-BOLT WAS FOUND TO BE CRACKED APPROXIMATELY
- [SDR 97ZZZX4](https://openairdocs.org/sdr/97ZZZX4.md): Bolt · corroded · Dec 3, 1996 · N2405G · Cessna 182B · Wing, Fuselage Attach Fittings
  > FOUND THE RT WING SPAR BOLT HEAD CORRODED DURING INSPECTION. AFTER REMOVAL SHANK ALSO CORRODED. SUBMITTER RECOMMENDS LIBERAL POLICY OF REPLACING HARDWARE ON OLD AIRCAFT WHEN CORROSION IS SHOWING.
- [SDR 96ZZZX2293](https://openairdocs.org/sdr/96ZZZX2293.md): Impulse Cam · worn · Apr 11, 1996 · N7244E · Cessna 182B · Magneto/Distributor
  > UPON INSPECTION OF CAMS IN IMPULSE COUPLINGS FOR WEAR PER AD 78-09-07, FOUND ONE FLYWEIGHT AND RIVET WORN WELL BEYOND LIMITS. THIS IS NEW STYLE CAM WITH SNAP RING ASSEMBLY. FOR A TOTAL TIME OF ONLY 595 HOURS, FEEL THIS TO BE SIGNIFICANT WEAR AND WOULD ALSO Q
- [SDR EY2R9600307](https://openairdocs.org/sdr/EY2R9600307.md): Hub · corroded · Feb 1, 1996 · Cessna 182B · Propeller Hub Section
  > HUB FOUND CORRODED.
- [SDR 95ZZZX3326](https://openairdocs.org/sdr/95ZZZX3326.md): Cell · leaking · May 21, 1995 · N2496G · Cessna 182B · Fuel Storage
  > AT LEVEL OFF AS POWER WAS REDUCED, CABIN FILLED WITH FUEL VAPORS. FLIGHT ABORTED. AFTER LANDING, FUEL WAS FOUND DRIPPING FROM RIGHT WING. CAUSE AND SPECIFIC INFORMATION PENDING INVESTIGATION BY MECHANIC.
- [SDR 95ZZZX3012](https://openairdocs.org/sdr/95ZZZX3012.md): Bulkhead · cracked · May 9, 1995 · N2496G · Cessna 182B · Fuselage Main, Bulkhead
  > FORWARD OF BULKHEAD CRACK FOUND - UNKNOWN ORIGIN. CRACK FOUND DURING ANNUAL INSPECTION OF LT MLG OUTB THROUGH-BOLT.
- [SDR 95ZZZX3011](https://openairdocs.org/sdr/95ZZZX3011.md): Cell · leaking · Jan 6, 1995 · N2496G · Cessna 182B · Fuel Storage
  > SECOND REPORT - FOLLOW-UP TO 21 MAY REPORT. RT FUEL CELL FOUND TO HAVE A SMALL LEAK IN AND AROUND MAIN FUEL SUPPLY NIPPLE. FUEL CELL REPLACED AND CORE SENT IN FOR INSPECTION. LEAK COMING FROM NIPPLE BONDING PATCH SEALING COMPOUND.

## 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 = '182B'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/cessna-182b/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.