# Service difficulty reports: Champion 8KCAB

A list on [Champion 8KCAB](https://openairdocs.org/model/champion-8kcab.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 95 reports

- [SDR F35R20200518001](https://openairdocs.org/sdr/F35R20200518001.md): Bezel · cracked · May 18, 2020 · Bbavia 8KCAB · Airspeed/Mach Indicator
  > THE AIRSPEED INDICATOR WAS FOUND TO HAVE A CRACKED GLASS FACE WHEN CONDUCTING A PITOT STATIC LEAK TEST AFTER A TRANSPONDER INSTALLATION. IT APPEARS THAT THE PART IS MADE FROM A POLY-CARBONATE MATERIAL AND NOT GLASS. THE AIRSPEED IS LIGHTED AND IT APPEARS THA
- [SDR 2020FA0000037](https://openairdocs.org/sdr/2020FA0000037.md): Spar · cracked · Apr 19, 2019 · N50636 · Bbavia 8KCAB · Wing Spar
  > SPAR BUTT CRACKS, AFT SPARS, BOTH WINGS, NOTED AT ANNUAL INSPECTION, ALL SPARS, BOTH WINGS REPLACED REF FAA FORM 337 DATED APRIL 10, 2019.
- [SDR 2018FA0000459](https://openairdocs.org/sdr/2018FA0000459.md): Bolt · broken · May 14, 2018 · N5500W · Bbavia 8KCAB · Nose/Tail Landing Gear
  > THE PIVOT BOLT PART OF THE 3216-00 BRACKET ASSEMBLY SNAPPED IN TWO ALLOWING THE TAIL WHEEL AND FORK ASSEMBLY TO DEPART THE ACFT ON TAKEOFF. THE BOLT BROKE JUST ABOVE THE BEARING CONE PN 13286-00.
- [SDR XGKR2017122900003](https://openairdocs.org/sdr/XGKR2017122900003.md): Altimeter · damaged · Dec 29, 2017 · N675WM · Bbavia 8KCAB · Altimeter, Barometric/Encoder
  > ALTIMETER FAILED STATIC SYSTEM TEST DUE TO INDICATOR INTERNAL LIGHT MELTED FRONT OF PLASTIC CASE CAUSING LOSS OF CASE SEALING.
- [SDR XGKR2017122900002](https://openairdocs.org/sdr/XGKR2017122900002.md): Indicator · damaged · Dec 28, 2017 · N675WM · Bbavia 8KCAB · Airspeed/Mach Indicator
  > AIRSPEED INDICATOR FAILED DURING STATIC SYSTEM INSPECTION. FOUND THE INDICATOR LIGHT MELTED PLASTIC INDICATOR FRONT CAUSING LOSS OF INSTRUMENT CASE SEALING.
- [SDR F35R011220173](https://openairdocs.org/sdr/F35R011220173.md): Control Cable · frayed · Jan 12, 2017 · N126WB · Bbavia 8KCAB · Elevator Control System
  > UP ELEVATOR CABLE PART NUMBER 3-1072 HAD MULTIPLE BROKEN/FRAYED WIRE STRANDS AT AFT MOST PULLEY LOCATION (APPROX FUSELAGE STATION 167.50, JUST AFT OF THE FRONT STABILIZER ATTACH POINT) AND MID PULLEY (APPROX LOCATION UNDER REAR SEAT). DOWN ELEVATOR CABLE PART
- [SDR F35R201701122](https://openairdocs.org/sdr/F35R201701122.md): Control Cable · frayed · Jan 6, 2017 · N464SC · Bbavia 8KCAB · Elevator Control System
  > UP ELEVATOR CABLE PART NUMBER 3-1072 HAD MULTIPLE BROKEN/FRAYED WIRE STRANDS AT AFT MOST PULLEY LOCATION (APPROX FUSELAGE STATION 167.50, JUST AFT OF THE FRONT STABILIZER ATTACH POINT) AND MID PULLEY (APPROX LOCATION UNDER REAR SEAT). DOWN ELEVATOR CABLE PART
- [SDR F35R201701121](https://openairdocs.org/sdr/F35R201701121.md): Control Cable · frayed · Dec 5, 2016 · N696SP · Bbavia 8KCAB · Elevator Control System
  > UP ELEVATOR CABLE PART NUMBER 3-1072 HAD MULTIPLE BROKEN/FRAYED WIRE STRANDS AT AFT MOST PULLEY LOCATION (APPROX FUSELAGE STATION 167.50, JUST AFT OF THE FRONT STABILIZER ATTACH POINT) AND MID PULLEY (APPROX LOCATION UNDER REAR SEAT). DOWN ELEVATOR CABLE PART
- [SDR N3XR2016111700001](https://openairdocs.org/sdr/N3XR2016111700001.md): Gauge · contaminated · Nov 5, 2016 · N199SA · Bbavia 8KCAB · Manifold Pressure (MP) Indicating
  > THE PILOT REPORTED SLUGGISH MAP READINGS.INVESTIGATION REVEALED THAT THE MAP LINE HAD RESIDUAL FLUID IN IT AND THAT THIS FLUID ENTERED THE MAP GAUGE. THIS HAS PREVIOUSLY HAPPENED ON AT LEAST TWO OCCASIONS.
- [SDR N3XR20160609003](https://openairdocs.org/sdr/N3XR20160609003.md): Indicator · contaminated · Jun 9, 2016 · N199SA · Bbavia 8KCAB · Manifold Pressure (MP) Indicating
  > AFTER MANY HOURS OF AEROBATIC FLIGHT, SMALL TRACES OF OIL MIGRATED INTO THE MAP LINE BEHIND THE CYLINDER. EVENTUALLY THIS CAUSES ERRATIC OR COMPLETE LOSS OF THE MAP INDICATION. THERE IS NO SOLUTION FOR THIS OTHER THAN HAVING THE GAUGE REPAIRED AND BLOWING OUT
- [SDR XGKR20160428001](https://openairdocs.org/sdr/XGKR20160428001.md): Solenoid · faulty · Apr 26, 2016 · N675WM · Bbavia 8KCAB · Engine Starter
  > STARTER SOLENOID FAILURE.
- [SDR 2016FA0000186](https://openairdocs.org/sdr/2016FA0000186.md): G Switch · failed · Mar 26, 2016 · N86954 · Bbavia 8KCAB · Emergency Locator Beacon
  > THIS 406 MHZ WAS ORDERED NEW 2 YEARS AGO AND WAS SENT IN FOR REPAIR DUE TO A DEFECTIVE G-SWITCH THE VERY NEXT YEAR AFTER IT WAS INSTALLED. THIS YEAR SHOWED COMPLETE FAILURE DURING THE ANNUAL INSPECTION. THIS IS NOT AN ISOLATED INCIDENT AND OUR SHOP HAS SENT
- [SDR CA160218007](https://openairdocs.org/sdr/CA160218007.md): Servo · loose · Feb 18, 2016 · Bbavia 8KCAB · Engine Fuel Distribution
  > (CAN) AT REMOVAL OF COWL, FOUND FUEL INJECTION SERVO LOOSE, 3 OF 4 SECURING NUTS MISSING AND NOT FOUND.
- [SDR 2015FA0000116](https://openairdocs.org/sdr/2015FA0000116.md): Bolt · sheared · Dec 12, 2014 · N1091E · Bbavia 8KCAB · Fuselage, Landing Gear Attach Fittings
  > BOLT SHEARED DURING TAKEOFF ROLL, CAUSING RT LANDING GEAR STRUT TO COLLAPSE. REVIEW OF THE MAINTENANCE LOG BOOKS SHOW A RE-TORQUE AT 391 TT, FAILURE OCCURRED AT 1292 TT. NO RECORD OF RE-TORQUE OR REPLACEMENT BETWEEN THOSE 2 EVENTS. SERVICE MANUAL FOR MODEL,
- [SDR OG5S2014FA0000691](https://openairdocs.org/sdr/OG5S2014FA0000691.md): Longeron · cracked · Dec 8, 2014 · N316CA · Bbavia 8KCAB · Fuselage Main, Longeron/Stringer
  > DURING ANNUAL INSPECTION, A LONGERON WAS FOUND CRACKED AT THE AFT MLG ATTACHMENT HOLE ON BOTH SIDES.
- [SDR 2014FA0000194](https://openairdocs.org/sdr/2014FA0000194.md): Bearing · failed · Mar 6, 2014 · N291SA · Bbavia 8KCAB · Ailerons
  > FOUND THE AILERON CENTER SHAFT BEARINGS AND CENTER SHAFT EXTENSION TO BE OUT OF SPECIFICATION. THIS WAS THE CASE IN BOTH RT AND LT WINGS. THE BEARINGS, PN B65NS, HAD EXCESSIVE WEAR. THE TOP BEARING, DUE TO POOR QC IN THE BORE, HAD ALLOWED TO MOVE DOWN, OUT
- [SDR 2014FA0000193](https://openairdocs.org/sdr/2014FA0000193.md): Control Cable · out of tolerance · Mar 6, 2014 · N291SA · Bbavia 8KCAB · Power Lever
  > MIXTURE CONTROL CONTROL CABLE FAILED, DUE TO INSUFFICIENT WIRE SIZE. THE OUTER WOUND WIRE SHEATH EXTENDED UNDER LOAD, THIS CAUSED THE OUT OF RIG CONDITION, THAT WOULD NOT LET THE FUEL INJECTION MIXTURE CONTROL LEVER MOVE THROUGH ITS FULL RANGE. CHANGE THE TY
- [SDR CA120221011](https://openairdocs.org/sdr/CA120221011.md): Line · cracked · Feb 20, 2012 · Bbavia 8KCAB · Reciprocating Engine Power Section
  > (CAN) PILOT NOTICED NO MANIFOLD PRESSURE INDICATION, RETURNED TO BASE. INSPECTED AND FOUND LINE BROKEN AT ENGINE.
- [SDR 2011FA0000780](https://openairdocs.org/sdr/2011FA0000780.md): Bolt · broken · Nov 28, 2011 · N53757 · Bbavia 8KCAB · Main Landing Gear
  > BOLT BROKE ON ACFT ROLL OUT. SRM RECOMMENDS THE BOLT BE REPLACED EVERY 500 HRS, TIS.
- [SDR 2010FA0001185](https://openairdocs.org/sdr/2010FA0001185.md): Blade · delaminated · Nov 17, 2010 · N316CA · Bbavia 8KCAB · Propeller Blade Section
  > APPROX 8 INCHES OUT FROM BLADE CUFF IN CTR OF THE BACK OF THE PROP FOUND TO BE AN AREA OF DELAMINATION 1 INCH DIAMETER.
- [SDR CA100812004](https://openairdocs.org/sdr/CA100812004.md): Cylinder · cracked · Aug 11, 2010 · Bbavia 8KCAB · Reciprocating Engine Cylinder Section
  > APPROX 2 INCH CRACK VISUALLY FOUND BETWEEN FINS JUST ABOVE INTAKE PIPE.
- [SDR 2010FA0000210](https://openairdocs.org/sdr/2010FA0000210.md): Transmitter · leaking · Feb 22, 2010 · N829LT · Bbavia 8KCAB · Fuel Indicating System
  > FUEL LEAKING FROM SENDING UNIT, SCREW TOO LONG. WE ADDED NR 10 LOCK -O-SEAL TO EACH SCREW.
- [SDR 2010FA0000203](https://openairdocs.org/sdr/2010FA0000203.md): Spar · cracked · Feb 17, 2010 · N8693V · Bbavia 8KCAB · Wing Spar
  > FOUND CRACK IN LT MAIN WOOD SPAR APPROX 16 " INBD OF LIFT STRUT.
- [SDR 2010FA0000202](https://openairdocs.org/sdr/2010FA0000202.md): Spar · cracked · Feb 17, 2010 · N8693V · Bbavia 8KCAB · Ailerons
  > FOUND CRACK IN THE INBD AILRON BAY AREA.
- [SDR 2009FA0000988](https://openairdocs.org/sdr/2009FA0000988.md): Retainer · failed · Nov 24, 2009 · N571SA · Bbavia 8KCAB · Propeller Blade Section
  > DURING ANNUAL INSP FOUND COULD ROTATE ONE BLADE AN EXCESSIVE DISTANCE, SENT OUT FOR REPAIR AND IT WAS FOUND THAT THE INSIDE STAINLESS STEEL RETAINER HAD FAILED AND ALLOWED THE BALL BEARINGS TO FALL OUT OF THEIR SEAT, HUB WAS DAMAGED BEYOND REPAIR AND IT WAS CL
- [SDR 2009FA0001024](https://openairdocs.org/sdr/2009FA0001024.md): Baffle · mushroomed · Mar 3, 2009 · N725JM · Bbavia 8KCAB · Engine Noise Suppressor
  > ACFT WAS EXPERIENCING LARGE EGT DIFFERENCES BETWEEN THE RT AND LT CYL BANKS AT TAKEOFF AND CRUISE FLIGHT (BOTH FULL RICH AND LEAN OPERATIONS). ENG TREND MONITORING SHOWED THE DIFFERENCE GROWING SLOWLY OVER SEVERAL MONTHS TO MORE THAN 350F AT TAKEOFF FROM AN O
- [SDR 2008FA0000659](https://openairdocs.org/sdr/2008FA0000659.md): Seat · failed · Sep 16, 2008 · N7698S · Bbavia 8KCAB · Flight Compartment Equipment
  > REAR SEAT PN 7-1500 FAILED AT THE LT HINGE POINT. THE AN3 SERIES BOLT PULLED THRU THE HINGE LUGS WHICH ARE WELDED TO THE SEAT FRAME BOTTOM. THE RT HINGE HOLES SHOW ELONGATION, BUT REMAINED INTACT. THE AC WAS DOING SPIN TRAINING AT THE TIME OF THE INCIDENT. REC
- [SDR 2006FA0000591](https://openairdocs.org/sdr/2006FA0000591.md): Sleeve · broken · Jun 8, 2006 · N316CA · Bbavia 8KCAB · Fuel Storage
  > CREW REPORTED STRONG ODOR OF FUEL IN CABIN.MX INSPECTED FOUND FUEL LEAKING ONTO CARPET ON THE FWD LEFT SIDE OF CABIN. TRACED LEAK TO THE VENT LINE HEADER TANK ATTACH FITTING. FITTING FOUND TO BE TIGHT BUT LINE CRACKED AT COMPRESSION SLEEVE CONNECTOR. LINE AND
- [SDR 2006FA0000590](https://openairdocs.org/sdr/2006FA0000590.md): Vent Line · cracked · Jun 8, 2006 · N316CA · Bbavia 8KCAB · Fuel Storage
  > CREW REPORTED STRONG SMELL OF FUEL IN CABIN. MX INSPECTED FOUND FUEL LEAKING ONTO CARPET ON THE FWD LT SIDE OF CABIN. TRACED LEAK TO THE VENT LINE HEADER TANK ATTACH FITTING. FITTING FOUND TO BE TIGHT BUT LINE CRACKED AT COMPRESSION SLEEVE CONNECTOR. LINE AN
- [SDR 2005FA0001548](https://openairdocs.org/sdr/2005FA0001548.md): Harness · broken · Nov 9, 2005 · N912MA · Bbavia 8KCAB · Emergency Equipment
  > JUST PRIOR TO INITIATING AEROBATICS THE PILOT ATTEMPTED TO RATCHET DOWN HIS AEROBATIC HARNESS. THE HANDLE FOR THE RATCHET BROKE ALLOWING THE RATCHET LOCK TO FALL OUT OF THE ASSEMBLY. FLIGHT WAS TERMINATED. HARNESS REPLACED WITH NEW ASSEMBLY.
- [SDR 2005FA0001294](https://openairdocs.org/sdr/2005FA0001294.md): Bolt · misinstalled · Sep 15, 2005 · N912MA · Bbavia 8KCAB · Elevator Structure
  > DURING PREFLIGHT THE PILOT FOUND EXCESSIVE MOVEMENT IN THE LT OB ELEVATOR HINGE PIN. MAINTENANCE REMOVED BOTH ELEVATORS AND THE RUDDER AND FOUND LONGITUDINAL SCORING ON ALL THE HINGE BOLTS (AN23-40) APPARENTLY CAUSED DURING MFG OF THE AIRCRAFT. THE LONGITUDI
- [SDR 2004FA0000537](https://openairdocs.org/sdr/2004FA0000537.md): Spar · cracked · May 5, 2004 · N1182E · Bbavia 8KCAB · Wing Spar
  > SPAR INSPECTED IAW 00-25-02R1. FOUND 2 CRACKS IN BUTT END, DOUBLER PLATES APPEAR TO BE LOOSENING. CRACKS ARE HORIZONTAL ACROSS THE END GRAIN.
- [SDR MW82004F00000](https://openairdocs.org/sdr/MW82004F00000.md): Mount · chafed · Apr 7, 2004 · N912MA · Bbavia 8KCAB · Engine Mount Section
  > DURING A VISUAL INSPECTION OF THE NEW AC, ENGINE MOUNT WAS NOTED HAVING AN EXCESSIVE CHAFFING CAUSED BY A TINNERMAN NUT USED FOR WINTER BAFFLE ON IB SIDE OF OIL COOLER. SEVERAL OTHER AC HAVE BEEN NOTED WITH TINNERMAN NUTS ON THE OIL COOLERS BUT NO DAMAGE NOT
- [SDR 2004FA0000164](https://openairdocs.org/sdr/2004FA0000164.md): Fuel Cap · misinstalled · Feb 4, 2004 · N561ER · Bbavia 8KCAB · Fuel Storage
  > FUEL TANK CAPS ARE VERY DIFFICULT TO SECURE PROPERLY. IT IS EASY TO PUT THE CAP ON PARTIALLY. THE FACTORY RECOMMENDS THE CAP GASKETS BE LUBED WITH SILICONE SPRAY. WE ARE ALSO PUTTING ALIGNMENT MARKS ON THE CAP AND WING FOR POSITIVE ENGAGEMENT INDICATION.
- [SDR CA040106004](https://openairdocs.org/sdr/CA040106004.md): Window · broken · Dec 19, 2003 · Bbavia 8KCAB · Flight Compartment Windows
  > (CAN) TOP WINDOW (SKY LIGHT) SHATTERED AND BROKE AWAY AFTER LEVELLING OFF FROM DOING A CUBAN EIGHT.
- [SDR 2003FA0000884](https://openairdocs.org/sdr/2003FA0000884.md): Bushing · loose · Sep 3, 2003 · N330MS · Bbavia 8KCAB · Rudder Structure
  > RIGHT FORWARD RUDDER ATTACH BUSHING COTTER PIN HEAD WORN OFF BY CYCLIC CONTACT WITH FLOORBOARD. PIVOT BUSHING WAS FOUND MORE THAN HALF WAY OUT OF RUDDER ATTACH POINT.
- [SDR AUS20030799](https://openairdocs.org/sdr/AUS20030799.md): Spar · cracked · Jun 10, 2003 · Bbavia 8KCAB · Wing Spar
  > (AUS) LT WING REAR SPAR CONTAINED A NUMBER OF LENGTH WISE CRACKS. FOUND DURING INSPECTION IAW AD/CHA/23.
- [SDR AUS20030490](https://openairdocs.org/sdr/AUS20030490.md): Fuse · disconnected · May 8, 2003 · Bbavia 8KCAB · Engine Indicating System Wiring
  > (AUS) ENGINE HOURMETER INLINE FUSE HOLDER DISCONNECTED.
- [SDR 2003F00113](https://openairdocs.org/sdr/2003F00113.md): Attach Fitting · chafed · Feb 1, 2003 · N330MS · Bbavia 8KCAB · Wing, Attach Fittings
  > DURING A ROUTINE SERVICE INTERNAL CUSTOMER REQUESTED THE 1000 HOUR INSPECTION DETAILED IN AIRWORTHY LIMITATIONS OF MM. ON ALL FOUR STRUT ATTACH FITTINGS. BOTH FITTINGS WERE REJECTED ON LEFT WING DUE TO CHAFING ON EDGES WHERE FITTINGS PASS THROUGH LEADING EDG
- [SDR N3F2003F00000](https://openairdocs.org/sdr/N3F2003F00000.md): Line · leaking · Dec 9, 2002 · N28YH · Bbavia 8KCAB · Aircraft Fuel Distribution System
  > AIRCRAFT FORMED FUEL LEAKS WITHIN 28.8 HOURS OF SERVICE. THIS AIRCRAFT WAS BROUGHT IN FOR SERVICE WHEN THE PILOT REPORTED FUEL LEAKING FROM THE INVERTED FUEL SYSTEM HEADER TANK ONTO HIS LEGS AND FEET. PERFORMING A VISUAL INSPECTION OF THE SYSTEM SIX FUEL LEA
- [SDR 2002FA0001381](https://openairdocs.org/sdr/2002FA0001381.md): Blade · cracked · Nov 27, 2002 · N76KF · Bbavia 8KCAB · Propeller Blade Section
  > DURING INSPECTION, MAINTENANCE WAS UNABLE TO DETERMINE COMPLIANCE WITH AD. DUE TO INADEQUATE RECORDS, PROPELLER WAS SUBMITTED FOR OVERHAUL AND ALSO TO REPLACE THE HUB IAW AD. AT DISASSEMBLY, PROP WAS FOUND TO HAVE COLD COMPRESSION ROLLED SHANKS. HOWEVER, DU
- [SDR 2002FA0001090](https://openairdocs.org/sdr/2002FA0001090.md): Bracket · misinstalled · Sep 5, 2002 · N2523Z · Bbavia 8KCAB · Wing Miscellaneous Structure
  > DURING AN ANNUAL INSPECTION, FOUND WING ROOT FAIRING BRACKET AGAINST LOWER PART OF FORWARD SPAR (LEFT WING). THE BRACKET APPEARS TO HAVE BEEN INSTALLED TOO CLOSE TO THE SPAR AT MANUFACTURE, CAUSING LOCAL MINOR DAMAGE. REPAIRED LOCAL DAMAGE. INSPECTED ENTIRE
- [SDR OG5R092N](https://openairdocs.org/sdr/OG5R092N.md): Fuel Tank · cracked · May 8, 2002 · Bbavia 8KCAB · Fuel Storage
  > DURING ANNUAL INSPECTION A FUEL LEAK WAS NOTED ON THE BOTTOM OF THE LEFT WING BENEATH THE FUEL TANK. UPON MORE DETAILED INSPECTION THE INTERNAL BAFFLING OF THE FUEL TANK WAS FOUND TO BE SEPERATED AND THE TANK TO BE LEAKING FROM ONE OF THE BAFFLE ATTACH WELDS.
- [SDR OG52002F00000](https://openairdocs.org/sdr/OG52002F00000.md): Pitch Control · cracked · Dec 27, 2001 · N67ND · Bbavia 8KCAB · Propeller Controlling System
  > DURING SCHEDULED INSPECTION PITCH CYLINDER OF THE PROPELLER ASSEMBLY, WAS FOUND TO BE CRACKED ON THE FORWARD END. THE CRACK EXTENDED FROM BOTH SIDES OF THE LOW PITCH STOP NUT OUT BOARD.
- [SDR 2001FA0000259](https://openairdocs.org/sdr/2001FA0000259.md): Rib · damaged · Jul 3, 2001 · N80TA · Bbavia 8KCAB · Wing, Rib/Bulkhead
  > FOUND LOOSE AND/OR MISSING NAILS AT RIB/FRONT SPAR CONNECTION. 2 RIBS ON RT WING AND 2 RIBS ON LT WING FOUND DAMAGED WHILE INSPECTING PER REGMENTS OF AD.
- [SDR 2002FA0000244](https://openairdocs.org/sdr/2002FA0000244.md): Fastener · missing · May 17, 2001 · N2561Z · Bbavia 8KCAB · Miscellaneous Hardware
  > APPROXIMATELY 10 RIB NAILS WERE MISSING ON EACH WING. NAIL HOLES WERE NOT ELONGATED. NO OTHER DAMAGE WAS FOUND. THE GENERAL LOCATION OF MISSING NAILS WERE AT STRUT ATTACH AREAS.
- [SDR 20010205CW016](https://openairdocs.org/sdr/20010205CW016.md): Rib · cracked · Jan 4, 2001 · N68ND · Bbavia 8KCAB · Vertical Stabilizer, Spar/Rib
  > DURNING ANNUAL INSPECTION, TAIL FIN FABRIC WAS FOUND BUCKLING APPROX 1 INCH AFT OF TOP LEADING EDGE. UPON FABRIC REMOVAL FOR HIDDEN DAMAGE INSPECTION THE FIN RIB WAS FOUND TO BE CRACKED AND BUCKLED AT FWD ATTACHING WELD. FURTHER INSPECTION REVEALED AFT ATTA
- [SDR 20000621SH001](https://openairdocs.org/sdr/20000621SH001.md): Bellcrank · fod · May 31, 2000 · N53737 · Bbavia 8KCAB · Aileron Control System
  > PILOT WAS PERFORMING AEROBATICS WHEN, DURING A ROLL TO THE RIGHT, THE CONTROL STICK JAMMED DURING HIS ATTEMPT TO STOP THE ROLL. HE SLOWED/STOPPED THE ROLL USING ALL AVAILABLE AILERON INPUT USING FULL LEFT RUDDER. IN A HEAVY SLIP, HE WAS LOOKING AT AVAILABLE
- [SDR 20000505SH032](https://openairdocs.org/sdr/20000505SH032.md): Magneto · contaminated · May 5, 2000 · N50395 · Bbavia 8KCAB · Magneto/Distributor
  > OWNER COMPLAINED OF ROUGH RUNNING/MISSING WHEN ENGINE HOT WHILE AT LOW POWER SETTINGS. RT MAG (4150) REMOVED. EXCESS PLAY IN DIST END BEARING (APPROX PLAY,.030 INCH) SN 9010274. LT MAG REMOVED (4151) SN 9010270. FOUND ENTIRE INTERIOR OF MAG CONTAMINATED B
- [SDR 20000505SH031](https://openairdocs.org/sdr/20000505SH031.md): Magneto · contaminated · May 5, 2000 · N50395 · Bbavia 8KCAB · Magneto/Distributor
  > OWNER COMPLAINED OF ROUGH RUNNING/MISSING WHEN ENGINE HOT WHILE AT LOW POWER SETTINGS. RT MAG (4150) REMOVED. EXCESS PLAY IN DIST END BEARING (APPROX PLAY,.030 INCH) SN 9010274. LT MAG REMOVED (4151) SN 9010270. FOUND ENTIRE INTERIOR OF MAG CONTAMINATED B

Next page: https://openairdocs.org/model/champion-8kcab/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 = '8KCAB'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/champion-8kcab/reports

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