# Service difficulty reports: Beech C 23

A list on [Beech C 23](https://openairdocs.org/model/beech-c-23.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 3 · 104 reports

- [SDR 2023FA0000096](https://openairdocs.org/sdr/2023FA0000096.md): Magneto · destroyed · Feb 13, 2023 · N6632L · Beech C23 · Magneto/Distributor
  > BOTH MAGNETOS WERE REMOVED AS PART OF THE ANNUAL INSPECTION AND SENT TO NORVIC AERO ENGINES LTD (FAA APPROVAL 33NY343C) FOR THEIR 500 HOUR INSPECTION. THE MAGNETOS WERE RETURNED WITH 8130 PAPERWORK, RE-INSTALLED AND FOLLOWING COMPLETION OF THE ANNUAL INSPECTIO
- [SDR 2023FA0000095](https://openairdocs.org/sdr/2023FA0000095.md): Magneto · damaged · Feb 13, 2023 · N6632 · Beech C23 · Ignition System
  > FOLLOWING A CUSTOMER COMPLAINT ON MONDAY 13/2/23 OF A MAGNETO FAILURE AND EMERGENCY LANDING AT SLEAP AIRFIELD. STRIP AND INSPECT CARRIED OUT 16/2/23 ACCOMPANIED BY NAE QUALITY MANAGER, INITIAL EXTERNAL INSPECTION SHOWS ROTOR SHAFT TO BE BENT AND SEIZED, MARKS
- [SDR CA190522007](https://openairdocs.org/sdr/CA190522007.md): Slip Ring · out of position · May 17, 2019 · Beech C23 · Alternator-Generator Drive
  > (CAN) SLIPRING FOUND INCORRECTLY POSITIONED ON ROTOR SHAFT AND BRUSH BLOCK ASSY FOUND IN CONTACT WITH THE SLIPRING WIRES. (TC# 20190522007)
- [SDR CA180808017](https://openairdocs.org/sdr/CA180808017.md): Magneto · separated · Aug 8, 2018 · Beech C23 · Magneto/Distributor
  > (CAN) DURING A FLIGHT AIRCRAFT LOST THE USE OF A MAGNETO. AFTER OPENING THE ENGINE COVER, THE TECHNICIAN NOTICED THAT THE FLANGE OF THE MAGNETO WAS HANGING. A LARGE QUANTITY OF METAL FILINGS HAS BEEN FOUND IN THE OIL FILTER. (TC# 20180808017)
- [SDR 2017FA0000150](https://openairdocs.org/sdr/2017FA0000150.md): Cylinder · cracked · Mar 27, 2017 · N18889 · Beech C23 · Reciprocating Engine Cylinder Section
  > AFTER TAKE OFF, PILOT HEARD A LOUD BANG FROM THE ENGINE FOLLOWED BY VIBRATION AND LOSS OF POWER. SUCCESSFULLY RETURNED TO THE AIRPORT AND LANDED WITHOUT INCIDENT. INSPECTION OF THE ENGINE REVEALED THE NR 1 CYLINDER HAD CRACKED APPROXIMATLY 75% OF THE CIRCUMFE
- [SDR BQVR201603290001](https://openairdocs.org/sdr/BQVR201603290001.md): Engine · making metal · Mar 22, 2016 · N274CT · Beech C23 · Engine (Reciprocating)
  > WHILE ACCOMPLISHING AN ANNUAL INSPECTION OF THE ACFT, NOTED FERROUS METAL INSIDE OIL FILTER CAN, AND DRAINED OIL. ENGINE IS NOT APPROVED FOR RETURN TO SERVICE. CUSTOMER WAS ADVISED OF FINDINGS. THIS ENGINE HAS 805.6 HRS SINCE O/H.
- [SDR JJ8S2014FA0000693](https://openairdocs.org/sdr/JJ8S2014FA0000693.md): Valve · cracked · Dec 2, 2014 · N9298S · Beech C23 · Fuel Control/Reciprocating Engines
  > DURING TAKEOFF, PILOT NOTICED THE ENGINE HAD LOST POWER. PERFORMED AN EMERGENCY LANDING ON INTERSTATE. SUSPECT CARBURETOR HEAT BOX VALVE FAILURE. DURING VISUAL INSPECTION IT WAS DETERMINED THAT THE VALVE HAD FAILED AGAIN. THIS VALVE, HAD BEEN REPLACED 50 HR
- [SDR 2014FA0000551](https://openairdocs.org/sdr/2014FA0000551.md): Butterfly Valve · cracked · Sep 24, 2014 · N9298S · Beech C23 · Fuel Control/Reciprocating Engines
  > WHILE PERFORMING TOUCH AND GO, PILOT NOTICED THAT ENGINE LOST POWER. SAFELY LANDED ACFT AND INSPECTED ENGINE COMPARTMENT. VISUAL INSPECTION SHOWED THAT THE CARBURETOR HEAT BOX VALVE HAD SEPARATED AND JAMMED INSIDE INTAKE. REMOVED CARBURETOR HEAT BOX AND RE
- [SDR CA130128002](https://openairdocs.org/sdr/CA130128002.md): Engine · making metal · Jan 10, 2013 · Beech C23 · Engine (Turbine/Turboprop)
  > (CAN) PILOT GOT A CHIP DETECT ALARM ON ON THE NR 2 ENGINE. CREW APPLIED IMMEDIATELY AN ENGINE SHUT OFF PROCEDURE AND TERMINATED FLIGHT OEI AT CAEN WHICH IS LOCATED AT CHALAIR AVIATION MAINTENANCE SHOP WHERE THE PLANE IS MAINTAINED. AFTER LANDING ON GROUND INVE
- [SDR 2011FA0000264](https://openairdocs.org/sdr/2011FA0000264.md): Rib · corroded · Apr 27, 2011 · Beech C23 · Wing, Rib/Bulkhead
  > EXFOLIATION AND SEPARATION OF FWD RIBS ATTACHED TO FLAP ATTACH BRACKET. RT AND LT SIDE. CANNOT BE SEEN WITHOUT DOING SB27-3954. AFFECTS MODEL 19 SERIES, SERIALS MB-1 THROUGH MB-905, MODEL 23 SERIES, SERIALS M-1 THROUGH M-2392, MODEL 24 SERIES, SERIALS MA-1 THR
- [SDR 2011FA0000263](https://openairdocs.org/sdr/2011FA0000263.md): Rib · corroded · Apr 27, 2011 · Beech C23 · Wing, Rib/Bulkhead
  > EXFOLIATION AND SEPARATION OF FWD RIBS ATTACHED TO FLAP ATTACH BRACKET. RT AND LT SIDE. CANNOT BE SEEN WITHOUT DOING SB27-3954.
- [SDR 2011FA0000170](https://openairdocs.org/sdr/2011FA0000170.md): Attach Fitting · corroded · Feb 19, 2011 · N6664N · Beech C23 · Ailerons
  > RT FWD AILERON FAILED DUE TO CORROSION AT ATTACH POINT TO AILERON CONTROL ARM PN 169-5240201. CORROSION WAS ON LAST 6 INCHES OF CABLE AND WAS SMOOTH TO TOUCH. FAILED AFTER TAKEOFF APPROX 50 FT IN THE AIR, PLANE LANDED SAFELY. WOULD RECOMMEND SMALL INSPECTIO
- [SDR CA101117001](https://openairdocs.org/sdr/CA101117001.md): Valve Spring · broken · Nov 16, 2010 · Beech C23 · Reciprocating Engine Cylinder Section
  > (CAN) LORS D`UN INSPECTION DE 100 HRS, LE TECHNICIEN D`ENTRETIEN A DECOUVERT DU METAL (BRASSE) DANS LE FILTRE A L`HUILE. APRES INVESTIGATION, UNE "PUSH ROD TUBE" DE LA VALVE D`ADMISSION A ETE TROUVE DEFORME. APRES ANALYSE, LE RESSORT INTERIEUR DE LA VALVE A ET
- [SDR 2010FA0000384](https://openairdocs.org/sdr/2010FA0000384.md): Gasket · out of position · Apr 3, 2010 · N5289M · Beech C23 · Engine Air Intake System
  > GASKET IS OUT OF PLACE AND IS BEING NGESTED INTO INTAKE.
- [SDR 2010FA0000383](https://openairdocs.org/sdr/2010FA0000383.md): Gasket · out of position · Apr 3, 2010 · N5289M · Beech C23 · Engine Air Intake System
  > GASKET IS OUT OF PLACE AND IS BEING INGESTED INTO INTAKE.
- [SDR 2008FA0000280](https://openairdocs.org/sdr/2008FA0000280.md): Hose · leaking · Jan 12, 2008 · N2102W · Beech C23 · Reciprocating Engine Oil System
  > THE AC EXPERIENCED AN EMERGENCY LANDING AFTER THE PILOT REPORTED SMOKE IN THE COCKPIT. INSP AND INVESTIGATION REVEALED AN OIL COOLER LINE HAD BEEN MAKING CONTACT WITH THE NR4 EXHAUST STACK (RISER), EVENTUALLY CAUSED THE FIRE SHEATHING AND OIL LINE TO DETERIOR
- [SDR CA070423002](https://openairdocs.org/sdr/CA070423002.md): Cylinder · cracked · Apr 23, 2007 · Beech C23 · Reciprocating Engine Cylinder Section
  > (CAN) CRACK FOUND IN CYLINDER. (TC NR 20070423002)
- [SDR TZD2006F00000](https://openairdocs.org/sdr/TZD2006F00000.md): Duct · corroded · Nov 8, 2006 · N24580 · Beech C23 · Air Distribution System
  > FRESH AIR DUCT (PN 1695540113) ROUTED THROUGH CABIN FUSELAGE STRUCTURE SEEMS TO HAVE CAUSED GALVANIC CORROSION TO FUSELAGE STRUCTURE THAT HAD BEEN COVERED BY UPHOLSTRY PANELS. THE CONDITION FOUND IS TO SUCH OF AN EXTENT THAT IN SOME AREAS LOCATED AT OR ABOUT
- [SDR 2006FA0000964](https://openairdocs.org/sdr/2006FA0000964.md): Attach Bolt · worn · Sep 19, 2006 · N9239S · Beech C23 · Fuselage Main, Attach Fittings
  > DURING PRE-RUNUP INSPECTION FOR ANNUAL INSPECTION ALTERNATOR BELT NOTED TO BE LOOSE. UPON INSPECTION OF ALTERNATOR FOR BELT TENSION THE FOLLOWING WAS NOTED: THE CASTLE NUT WAS BACKED OUT TO THE POINT OF CHAFING ON THE A+ WIRE, THE WIRE WAS KEEPING THE NUT FR
- [SDR 2005FA0000306](https://openairdocs.org/sdr/2005FA0000306.md): Oil Cooler · cracked · Jan 17, 2005 · N9JY · Beech C23 · Engine Oil Cooler
  > IN-FLIGHT ENGINE FAILURE DUE TO OIL STARVATION RESULTING IN AN EMERGENCY LANDING IN TREES. POST ACCIDENT INVESTIGATION REVEALED A CRACKED OIL COOLER, WHICH ALLOWED ENGINE OIL SUPPLY TO BE PUMPED OVERBOARD. REFERENCE ACCIDENT (NR ATL05CA047).
- [SDR 2004FA0000296](https://openairdocs.org/sdr/2004FA0000296.md): Rod · corroded · Mar 25, 2004 · N24652 · Beech C23 · Elevator, Tab Structure
  > DURING ANNUAL INSPECTION THE TRIM TAB ROD WAS FOUND TO HAVE RUST ON IT. WHILE CLEANING THE PART, A HOLE WAS FOUND AT THE MID POINT OF THE ROD AND MOISTURE(WATER) WAS FOUND INSIDE. IT APPEARS THIS ROD IS RUSTING FORM THE INSIDE OUT. THIS UNIT SHOULD BE TAKEN
- [SDR 2004FA0000169](https://openairdocs.org/sdr/2004FA0000169.md): Pump · inoperative · Dec 15, 2003 · N6756B · Beech C23 · Engine Fuel Pump
  > AIRCRAFT EXPERIENCED ENGINE FAILURE DUE TO LOSS OF FUEL PRESSURE DURING TRAINING FLIGHT. STUDENT FAILED TO TURN ON ALTERNATOR SWITCH AND BATTERY POWER WAS INSUFFICIENT TO OPERATE ELECTRIC FUEL PUMP. FAILURE OCCURRED IN VICINITY OF AIRPORT AND SAFE LANDING WA
- [SDR AUS20030797](https://openairdocs.org/sdr/AUS20030797.md): Rotor · failed · Aug 8, 2003 · Beech C23 · Magneto/Distributor
  > (AUS) RT MAGNETO ROTATING MAGNETO DRIVE END SNAPPED IN AREA WHERE IT PASSES THROUGH THE REAR BEARING.
- [SDR 2002FA0001191](https://openairdocs.org/sdr/2002FA0001191.md): Lock · overtorqued · Oct 3, 2002 · N837KS · Beech C23 · Reciprocating Engine Power Section
  > LOCKPLATE FOR CRANKSHAFT GEAR RETAINING BOLT NOT SUFFICIENTLY BENT ALLOWING CRANKSHAFT GEAR BOLT TO LOOSEN. CRANKSHAFT GEAR DOWEL PIN SHEARED. RECOMMENDATION TO PREVENT RECURRENCE: CRANKSHAFT GEAR BOLT TORQUE SHOULD BE VERIFIED AT 204IN/LBS AND LOCKPLATE IN
- [SDR CA020503005](https://openairdocs.org/sdr/CA020503005.md): Crankcase · cracked · Apr 11, 2002 · Beech C23 · Reciprocating Engine Power Section
  > (CAN) DURING A 50 HOUR INSPECTION, AN OIL LEAK WAS NOTED ON THE CRANKCASE HOUSING. FURTHER INSPECTION REVEALED A CRACK ON THE FORWARD LEFT HAND PART OF THE CASE.
- [SDR AUS20020717](https://openairdocs.org/sdr/AUS20020717.md): Screw · missing · Mar 20, 2002 · Beech C23 · Engine Air Intake System
  > (AUS) CARBURETTOR HEAT INOPERATIVE DUE TO MISSING SCREWS (3OFF) AND NUTS ALLOWING THE BUTTERFLY VALVE TO ROTATE FREELY ON THE SHAFT PNO 169-910049-47.
- [SDR 2001FA0000245](https://openairdocs.org/sdr/2001FA0000245.md): Structure · broken · Sep 6, 2001 · N20087 · Beech C23 · Passenger/Crew Doors
  > PILOTS REPORTED SEVERE BUFFET DURING SLOW FLIGHT, APPROACH TO LANDING, ROUND-OUT, AND FLARE. BUFFET WAS AGGRAVATED BY LEFT SLIP. FOUND BOTTOM DOOR GASKET MISSING AND FIBERGLASS DOOR STRUCTURE BROKEN AT LAST RIVET ON DIAGONAL GUSSET. THIS ALLOWED AIR ESCAPIN
- [SDR 20010601CW010](https://openairdocs.org/sdr/20010601CW010.md): Selector Valve · damaged · May 11, 2001 · N9743L · Beech C23 · Fuel Selector/Shut-Off Valve
  > THIS FUEL VALVE DID NOT MEET THE CRITERIA OF MFG S.B.. THE RUNNING TORQUE OF THE VALVE WAS VERY HARD TO MOVE. WHEN TESTED WITH A TORQUE WRENCH IT EXCEEDED 25 INCH POUNDS. THE FUEL VALVE WAS DISASSEMBLED FOR LUBRICATION AND VALVE CONE WAS FOUND TO BE SEVERE
- [SDR 20010601CW009](https://openairdocs.org/sdr/20010601CW009.md): Line · leaking · May 11, 2001 · N9743L · Beech C23 · Landing Gear Brake System
  > MOST OF THE FLEXIBLE FLUID LINES IN THIS AIRCRAFT WERE FOUND TO BE STIFF. TWO OF THE BRAKE LINES WERE FOUND TO BE CHAFFING ON THE FORWARD FIREWALL AREA AND WERE WORN SMOOTH ON THE OUTSIDE. BOTH OF THESE WERE LEAKING THROUGH THE HOSE. ALL OF THE FLEXIBLE FLU
- [SDR CA001129010](https://openairdocs.org/sdr/CA001129010.md): Cylinder · cracked · Nov 1, 2000 · Beech C23 · Cylinder Head Temperature (CHT) Indicating System
  > (CAN) THE CYLINDER ASSEMBLY CRACKED AT THE CYLINDER HEAD FLANGE. THE CRACK EXTENDED HALF WAY THROUGH THE CIRCUMFERENCE OF THE CYLINDER. (X)
- [SDR CA001129004](https://openairdocs.org/sdr/CA001129004.md): Cylinder · cracked · Nov 1, 2000 · Beech C23 · Cylinder Head Temperature (CHT) Indicating System
  > (CAN) THE CYLINDER ASSEMBLY CRACKED AT THE CYLINDER HEAD FLANGE. THE CRACK EXTENDED HALF WAY THROUGH THE CIRCUMFERENCE OF THE CYLINDER. (X)
- [SDR 20001214SH006](https://openairdocs.org/sdr/20001214SH006.md): Spar Cap · cracked · Oct 30, 2000 · N6717K · Beech C23 · Vertical Stabilizer, Spar/Rib
  > DURING ANNUAL INSPECTION, ''CREAKING'' WAS HEARD WHEN FORCE WAS APPLIED TO STABILATOR TIP TO CHECK FOR BEARING PLAY. SOURCE OF SOUND WAS FOUND TO BE WORKING RIVETS AND CRACKED SPAR CAP INSIDE CENTER SPAR BOX ASSY IN THE LOOSE RIVETS OR CRACK COULD BE SEEN BY
- [SDR 20001127SH012](https://openairdocs.org/sdr/20001127SH012.md): Housing · broken · Oct 27, 2000 · N450BA · Beech C23 · Nose/Tail Landing Gear Attach Section
  > NOSE GEAR ASSEMBLY FELL OFF THE AIRCRAFT ON TAKEOFF. FOUND THE HOUSING HAD CRACKED OUT WHERE THE STEERING ASSY ATTACHES. THIS AREA SHOWED SIGNS OF BEING CRACKED FOR SOME TIME. (X)
- [SDR 20001103SH005](https://openairdocs.org/sdr/20001103SH005.md): Spar · corroded · Sep 25, 2000 · N7694R · Beech C23 · Wing Spar
  > INSPECTION OF LEFT AND RIGHT WINGS DUE TO ACCIDENT. EXFOLIATION CORROSION IN LOWER SPAR CAP WAS FOUND IN THE SAME AREA ON LEFT AND RIGHT WING SPARS. CORROSION IS LOCATED JUST OUTBOARD OF SPAR SPLICE CONTINUING ON TO WING TIP OR SPAR END. DAMAGE IS EXTREMELY
- [SDR CA000614041](https://openairdocs.org/sdr/CA000614041.md): Blade · inaccurate · Jun 2, 2000 · Beech C23 · Propeller Blade Section
  > (CAN) DIMENSIONAL CHECK, FOUND PROPELLER TO BE JUST UNDER MINIMUM ALLOWABLE THICKNESS AT THE 34.20 INCH STATION. PROPELLER RETIRED FROM SERVICE.
- [SDR 99ZZZX4435](https://openairdocs.org/sdr/99ZZZX4435.md): Spar · cracked · Nov 16, 1999 · N5167M · Beech C23 · Horizontal Stabilizer Structure
  > SPAR HAS CRACKS RADIATING OUT FROM CUT-OUTS FOR HINGE ATTACH POINT ON RIGHT SIDE. TIME IN SERVICE UNKNOWN.
- [SDR 99ZZZX4313](https://openairdocs.org/sdr/99ZZZX4313.md): Control Cable · frayed · Oct 24, 1999 · N66345 · Beech C23 · Trailing Edge Flap Control System
  > DURING ANNUAL INSPECTION, THE FLAP CABLE WAS FOUND FRAYED AROUND TORQUE TUBE. THIS COULD NOT BE EASILY SEEN UNTIL FLAPS WERE LOWERED AND CABLE CLEANED.
- [SDR 99ZZZX2655](https://openairdocs.org/sdr/99ZZZX2655.md): Bolt · misinstalled · Jul 7, 1999 · N180ED · Beech C23 · Nose/Tail Landing Gear Attach Section
  > FOUND AN 'AN' BOLT INSTALLED INSTEAD OF JO-BOLTS, NAS 699.667 IN LEFT LANDING GEAR STRUT.
- [SDR 20000508SH002](https://openairdocs.org/sdr/20000508SH002.md): Shimmy Dampener · failed · Jun 7, 1999 · N6639D · Beech C23 · Shimmy Damper
  > RETRIEVED SUBJECT SHIMMY DAMPENER FROM STOCK ROOM. ON FUNCTIONAL CHECK, DETERMINED MUCH WORSE THAN THE REMOVED UNIT.
- [SDR 20000508SH001](https://openairdocs.org/sdr/20000508SH001.md): Shimmy Dampener · leaking · Jun 7, 1999 · N6639D · Beech C23 · Shimmy Damper
  > SHIMMY DAMPENER HAS NUMEROUS DEAD SPOTS (AIR INSIDE) WHEN ACTUATED. CAUSES NOSE WHEEL TO SHIMMY READ BAD. (X)
- [SDR 99ZZZX283](https://openairdocs.org/sdr/99ZZZX283.md): Filter · contaminated · Dec 14, 1998 · N5289M · Beech C23 · Vacuum Distribution System
  > MAIN VACUUM FILTER WAS LOCATED UNDER WINDSHIELD FORWARD SEAM. DUE TO HEAVY RAINFALL AND A LEAKING SEAL BETWEEN WINDSHIELD AND BOOT COWL, THE MAIN FILTER BECAME SATURATED WITH WATER. ON START-UP THE GYROS FILLED WITH WATER. REPAIRED AND REPLACED GYROS. DRI
- [SDR 98ZZZX4508](https://openairdocs.org/sdr/98ZZZX4508.md): Shimmy Dampener · failed · Nov 6, 1998 · N6639D · Beech C23 · Shimmy Damper
  > AIRCRAFT EXPERIENCED NOSE WHEEL SHIMMY. A NEW SHIMMY DAMPENER INSTALLED. THE USUAL PRECAUTIONS AND TROUBLESHOOTING PROCEDURES WERE UTILIZED TO DETERMINE SHIMMY DAMPENER. WITHIN A FEW HOURS, ACFT REPORTED WITH SAME PROBLEM. INSTALLED NEW SHIMMY DAMPENER MF
- [SDR 99ZZZX1024](https://openairdocs.org/sdr/99ZZZX1024.md): Bracket · cracked · Oct 23, 1998 · N6704J · Beech C23 · Ailerons
  > DURING ANNUAL INSPECTION, FOUND BRACKET CRACKED AT AILERON CONTROL ARM ATTACH POINT.
- [SDR 99ZZZX95](https://openairdocs.org/sdr/99ZZZX95.md): Frame · cracked · Sep 2, 1998 · N831KS · Beech C23 · Fuselage Main, Frame
  > FOUND CRACKING IN FRAME ANGLE WHICH MOUNTS INSTRUMENT PANEL TO FUSELAGE AND CRACKS IN ADJACENT CHANNEL AND FUSELAGE SKIN. SUSPECT CRACKING BECAUSE OF LANDINGS MADE IN TRAINING AIRCRAFT. SUGGEST CLOSE INSPECTION OF STRUCTURE MOUNTING INSTRUMENT PANEL EVERY 10
- [SDR 99ZZZX94](https://openairdocs.org/sdr/99ZZZX94.md): Frame · cracked · Sep 2, 1998 · N831KS · Beech C23 · Fuselage Main, Frame
  > FOUND CRACKING IN FRAME ANGLE WHICH MOUNTS INSTRUMENT PANEL TO FUSELAGE AND CRACKS IN ADJACENT CHANNEL AND FUSELAGE SKIN. SUSPECT CRACKING BECAUSE OF LANDINGS MADE IN TRAINING AIRCRAFT. SUGGEST CLOSE INSPECTION OF STRUCTURE MOUNTING INSTRUMENT PANEL EVERY 10
- [SDR CA980908032](https://openairdocs.org/sdr/CA980908032.md): Rod · disconnected · Aug 20, 1998 · Beech C23 · Reciprocating Engine Power Section
  > (CAN) NR 1 AND NR 3 CONNECTING RODS WERE FOUND DISCONNECTED FROM THE CRANKSHAFT. ENGINE IS BEING SENT FOR INVESTIGATION.
- [SDR 98ZZZX3151](https://openairdocs.org/sdr/98ZZZX3151.md): Frame Angle · cracked · Jul 27, 1998 · N832KS · Beech C23 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CRACKING IN FRAME ANGLE WHICH MOUNTS INSTRUMENT PANEL TO FUSELAGE AND CRACKS IN ADJACENT CHANNEL AND FUSELAGE SKIN. SUSPECT CRACKING BECAUSE OF LANDINGS MADE IN TRAINING AIRCRAFT. SUGGEST CLOSE INSPECTION OF STRUCTURE MOUNTING INSTRUMENT PAN
- [SDR 98ZZZX3150](https://openairdocs.org/sdr/98ZZZX3150.md): Frame Angle · cracked · Jul 27, 1998 · N832KS · Beech C23 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CRACKING IN FRAME ANGLE WHICH MOUNTS INSTRUMENT PANEL TO FUSELAGE AND CRACKS IN ADJACENT CHANNEL AND FUSELAGE SKIN. SUSPECT CRACKING BECAUSE OF LANDINGS MADE IN TRAINING AIRCRAFT. SUGGEST CLOSE INSPECTION OF STRUCTURE MOUNTING INSTRUMENT PAN
- [SDR 98ZZZX3149](https://openairdocs.org/sdr/98ZZZX3149.md): Frame Angle · cracked · Jul 27, 1998 · N836KS · Beech C23 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CRACKING IN FRAME ANGLE WHICH MOUNTS INSTRUMENT PANEL TO FUSELAGE AND CRACKS IN ADJACENT CHANNEL AND FUSELAGE SKIN. SUSPECT CRACKING BECAUSE OF LANDINGS MADE IN TRAINING AIRCRAFT. SUGGEST CLOSE INSPECTION OF STRUCTURE MOUNTING INSTRUMENT PAN
- [SDR 98ZZZX3148](https://openairdocs.org/sdr/98ZZZX3148.md): Frame Angle · cracked · Jul 27, 1998 · N836KS · Beech C23 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CRACKING IN FRAME ANGLE WHICH MOUNTS INSTRUMENT PANEL TO FUSELAGE AND CRACKS IN ADJACENT CHANNEL AND FUSELAGE SKIN. SUSPECT CRACKING BECAUSE OF LANDINGS MADE IN TRAINING AIRCRAFT. SUGGEST CLOSE INSPECTION OF STRUCTURE MOUNTING INSTRUMENT PAN

Next page: https://openairdocs.org/model/beech-c-23/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 = 'C23'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/beech-c-23/reports

---
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