# Service difficulty reports: Beech 95-B55

A list on [Beech 95-B55](https://openairdocs.org/model/beech-95-b55.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 5 · 218 reports

- [SDR 2025FA0000751](https://openairdocs.org/sdr/2025FA0000751.md): Wire · shorted · Nov 6, 2025 · N1116T · Beech 95B55 · Electrical Power System Wiring
  > WE TURNED THE BATTERY MASTER ON TO TEST A LANDING LIGHT THAT WAS REPORTED TO BE OUT. AFTER ABOUT ONE MINUTE OF THE BATTERY MASTER BEING ON, LARGE AMOUNTS OF SMOKE CAME FROM THE LEFT ENGINE. TROUBLESHOOTING FOUND THAT THE ALTERNATOR OUTPUT WIRE WAS SHIELDED AND
- [SDR 2022FA0000276](https://openairdocs.org/sdr/2022FA0000276.md): Vacuum Sys · failed · May 20, 2022 · N955RH · Beech 95B55 · Fuselage Structure (General)
  > TWO VACUUM PUMPS WERE INSTALLED AT ENGINE CHANGE. THEY BOTH FAILED IN UNDER 25 HOURS. BOTH INTERNAL FAILURES. SHEARING THE DRIVE COUPLING. BOTH PURCHASED FROM MAFARLANE AVIATION ON 2/8/22. INVOICE 0453567IN.
- [SDR 2022FA0000275](https://openairdocs.org/sdr/2022FA0000275.md): Vacuum Sys · failed · May 20, 2022 · N955RH · Beech 95B55 · Fuselage Structure (General)
  > TWO VACUUM PUMPS WERE INSTALLED AT ENGINE CHANGE THEY BOTH FAILED AT 25 HOURS PUMPS WERE PURCHASED FROM MCFARLAND AVIATION ON 2/8/22 MCFARLAND INVOICE 0453567-IN
- [SDR 2022FA0000244](https://openairdocs.org/sdr/2022FA0000244.md): Filter Adapter · failed · May 4, 2022 · N2772 · Beech 95B55 · Oxygen System
  > OIL FILTER ADAPTER IS AN F&M ENTERPRISES ADAPTER INSTALLED UNDER AN STC. IT IS AFFECTED BY A STRATUS MANDATORY SERVICE BULLETIN NO. SB-001, REV B AND AN AIRWORTHINESS DIRECTIVE AD22-04-04. A FIBER GASKET WAS INSTALLED BETWEEN THE ADAPTER NUT AND OIL PUMP BODY.
- [SDR 2021FA0000115](https://openairdocs.org/sdr/2021FA0000115.md): Line · leaking · Apr 27, 2021 · N95SL · Beech 95B55 · Aircraft Fuel Distribution System
  > CUSTOMER REPORTED SMELLING PAINT THINNER WHILE TAXYING BY AN AIRCRAFT PAINTING CENTER. THOUGHT NOTHING OF IT AND MADE 2 HR FLIGHT. AFTER LANDING AND DURING TAXI THE ODOR WAS ONCE AGAIN NOTED RAISING SUSPICION. AIRCRAFT USES A FUEL PRESSURE GAGE CALIBRATED IN G
- [SDR CA190731020](https://openairdocs.org/sdr/CA190731020.md): Fuel Control · malfunctioned · Jul 23, 2019 · Beech 95B55 · Fuel Control/Reciprocating Engines
  > (CAN) RH ENGINE WAS SURGING ON TAKE OFF. PILOT ABORTED TAKE OFF AND MAINTENANCE TROUBLESHOT THE PROBLEM AND FOUND THAT THE MIXTURE SETTING ON THE RH ENGINE WAS EXCESSIVELY RICH. MAINTENANCE SET THE MIXTURE AS PER MAINTENANCE MANUAL AND AIRCRAFT WAS GROUND RUN
- [SDR CA190731022](https://openairdocs.org/sdr/CA190731022.md): Door · malfunctioned · Jul 23, 2019 · Beech 95B55 · Fixed Inner Doors
  > (CAN) DURING TAKEOFF CABIN ENTRANCE DOOR OPENED AND PILOT RETURNED TO AIRPORT. THE PILOT PROPERLY CLOSED THE DOOR AND ENSURED IT WAS LATCHED. HE THEN RETURNED TO THE RUNWAY TO CONTINUE THE INTENDED FLIGHT. (TC# 20190731022)
- [SDR 2019FA0000192](https://openairdocs.org/sdr/2019FA0000192.md): Bearing · failed · Jun 25, 2019 · N76CB · Beech 95B55 · Landing Gear Actuator
  > UPON INITIAL TAKEOFF, A LOUD NOISE WAS HEARD WHEN LANDING GEAR CAME UP. WHEN PLANNING FOR LANDING, GEAR WAS SELECTED DOWN, IT MOVED DOWN FOR A SPLIT SECOND AND THEN THE CIRCUIT BREAKER FOR THE LANDING GEAR MOTOR POPPED AND THERE WAS A SMELL OF SMOKE OR BURNING
- [SDR 2019FA0000089](https://openairdocs.org/sdr/2019FA0000089.md): Actuator Cable · unsecure · Mar 24, 2019 · N95BA · Beech 95B55 · Power Lever
  > DURING ANNUAL INSPECTION HEIM JOINT USED TO CONNECT THROTTLE CABLE TO THROTTLE BODY WAS FOUND TO BE PARTIALLY UNSCREWED FROM THROTTLE CABLE. THE WITNESS HOLE ALLOWED A WIRE TO PASS THROUGH, INDICATING INSUFFICIENT ATTACHMENT.
- [SDR 2019FA0000043](https://openairdocs.org/sdr/2019FA0000043.md): Connecting Rod · broken · Dec 6, 2018 · N955D · Beech 95B55 · Reciprocating Engine Power Section
  > PILOT FELT A SHUDDER OF THE LEFT ENGINE AND IT SHUT DOWN ON ITS OWN. THE AIRCRAFT LANDED WITHOUT INCIDENT. UPON INSPECTION WE FOUND THAT THE PROP DID NOT FEATHER, THE ENGINE SEIZED, THERE ARE THREE HOLES IN THE TOP ON THE LEFT ENGINE CASE HALF, OBSERVED THROUG
- [SDR E5ZR20180613001](https://openairdocs.org/sdr/E5ZR20180613001.md): Connecting Rod · failed · May 21, 2018 · N206S · Beech 95B55 · Reciprocating Engine Power Section
  > AFTER TEARING DOWN THE ENGINE IN QUESTION IT IS OUR OPINION THAT THE FAILURE WAS DO TO OIL STARVATION OF THE NR 5 CYLINDER CONNECTING ROD CAP FOR UNKNOWN REASONS. THIS CAUSED FAILURE OF THE ROD CAP BOLTS. THE CAP BOLTS STRETCHED, SNAPPED AND THEY SHOW SIGNS
- [SDR E5ZR2018061300178](https://openairdocs.org/sdr/E5ZR2018061300178.md): Connecting Rod · failed · May 21, 2018 · N206S · Beech 95B55 · Reciprocating Engine Power Section
  > AFTER TEARING DOWN OF THE ENGINE IN QUESTION IT IS OUR OPINION THAT THE FAILURE WAS DO TO OIL STARVATION OF THE #5 CYLINDER CONNECTING ROD CAP FOR UNKNOWN REASONS. THIS CAUSED FAILURE OF THE ROD CAP BOLTS. THE CAP BOLTS STRETCHED, SNAPPED AND THEY SHOW SIGNS
- [SDR E5ZR2018061300177](https://openairdocs.org/sdr/E5ZR2018061300177.md): Connecting Rod · oil starvation · May 21, 2018 · N206S · Beech 95B55 · Reciprocating Engine Cylinder Section
  > AFTER TEARING DOWN OF THE ENGINE, THE NR 5 CYLINDER FAILED DUE TO OIL STARVATION OF THE CONNECTING ROD CAP FOR UNKNOWN REASONS. THIS CAUSED FAILURE OF THE ROD CAP BOLTS. THE CAP BOLTS STRETCHED, SNAPPED AND THEY SHOW SIGNS OF BURN MARKS.
- [SDR JZRR2015011200004](https://openairdocs.org/sdr/JZRR2015011200004.md): Adapter · corroded · Mar 29, 2017 · N7734R · Beech 95B55 · Fuel Storage
  > WHILE COMPLETING AN ANNUAL INSPECTION, REMOVED FUEL CAPS TO INSPECT THE CAPS, SEALS AND ADAPTERS. FOUND THE LEFT WING MAIN TANK FUEL CAP ADAPTER HEAVILY CORRODED AND PITTED. WITH THE EXTENT OF CORROSION ON THE ADAPTER, THE CAP WOULD NOT SEAL ALLOWING WATER TO
- [SDR PAIR201510131457](https://openairdocs.org/sdr/PAIR201510131457.md): Mount · chafed · Oct 12, 2015 · N9054S · Beech 95B55 · Engine Mount Section
  > DURING SCHEDULED ENGINE CHANGE FOUND LT ENGINE MOUNT CHAFED BY EXHAUST PIPE AT LOWER INBD ATTACH FITTING. FOUND RT ENGINE MOUNT CHAFED BY EXHAUST PIPE AT LOWER OTBD ATTACH FITTING. AIRCRAFT HAS BEEN MODIFIED BY STC SA432SO, REPLACEMENT OF ENGINES WITH DIFFER
- [SDR 2015FA0000456](https://openairdocs.org/sdr/2015FA0000456.md): Attach Fitting · cracked · Sep 18, 2015 · N8911U · Beech 95B55 · Wing, Attach Fittings
  > DURING ANNUAL INSPECTION, LT AFT LOWER WING ATTACH FITTING WAS FOUND TO BE CRACKED ALONG LOWER SURFACE, AND VERIFIED BY DYE PENETRANT INSPECTION. CRACK MEASURES APPROXIMATELY 0.85" IN LENGTH AND 0.35" DEEP, AS MEASURED ON INBD SURFACE OF FITTING. REPLACEMENT
- [SDR CA150831012](https://openairdocs.org/sdr/CA150831012.md): Gear · worn · Aug 26, 2015 · Beech 95B55 · Engine Fuel Pump
  > (CAN) LEFT ENGINE LOST POWER IN FLIGHT. APPROXIMATELY 25 MINUTES AFTER DEPARTING, WHILE IN CRUISE AT 8000 FT, THE LT ENGINE QUIT. FUEL PUMP REMOVED AND FOUND THE COUPLING SHAFT, PN: 631683 ROUNDED INTERNALLY AND DRIVE GEAR, PN: 631684 WORN. DRIVE GEAR AND C
- [SDR CA150831011](https://openairdocs.org/sdr/CA150831011.md): Drive Coupling · worn · Aug 26, 2015 · Beech 95B55 · Engine Fuel Pump
  > (CAN) LEFT ENGINE LOST POWER IN FLIGHT, APPROXIMATELY 25 MINUTES AFTER DEPARTING, WHILE IN CRUISE AT 8000`, THE LT ENGINE QUIT. FUEL PUMP REMOVED AND FOUND THE COUPLING SHAFT PN: 631683 ROUNDED INTERNALLY AND DRIVE GEAR, PN: 631684 WORN. DRIVE GEAR AND COUPLIN
- [SDR 2015FA0000063](https://openairdocs.org/sdr/2015FA0000063.md): Bearing · failed · Feb 17, 2015 · N9404Q · Beech 95B55 · Landing Gear Door Retract Section
  > PILOT REPORTED THAT HE HAD GREEN GEAR DOWN AND LOCKED LIGHTS PRIOR TO LANDING AND WHEN THE NOSE TOUCHED DOWN IT FOLDED. FOUND THAT THE AFT RETRACT ROD,ROD-END AT THE EXTENSION IDLER FAILED CAUSING THE COLLAPSE. ONLY MINOR AIRFRAME DAMAGE TO THE NOSE AND NOSE
- [SDR CA141231002](https://openairdocs.org/sdr/CA141231002.md): Relay · failed · Dec 24, 2014 · Beech 95B55 · Landing Gear System Wiring
  > (CAN) WHILE GEAR OPERATION SWITCH WAS IN THE UP POSITION, GEAR LOWERED VIA THE MOTOR ON ITS OWN. PIC NOTED THAT SWITCH WAS UP AND LOCKED AND NO BREAKERS HAS "POPPED", HOWEVER BOTH PIC AND PASSENGER ALSO NOTICED THAT THE 3 GREEN WERE INDICATING. UPON TROUBLESH
- [SDR CA141203006](https://openairdocs.org/sdr/CA141203006.md): Indicator · leaking · Dec 3, 2014 · Beech 95B55 · Fuel Pressure Indicator
  > (CAN) DURING FLIGHT, PILOT NOTICED THE FACE OF THE FUEL PRESSURE INDICATOR HAD FLUID POOLING IN THE BOTTOM OF IT. IT WAS REPORTED TO MAINTENANCE AND THE INDICATOR WAS REPLACED.
- [SDR 2013FA0000503](https://openairdocs.org/sdr/2013FA0000503.md): Cylinder · failed · Aug 23, 2013 · N892P · Beech 95B55 · Reciprocating Engine Cylinder Section
  > ENGINE RAN INTERMITTENTLY ROUGH. NR 1 CYLINDER SHOWED VERY LOW EGT AND CHT. PERFORMED COMPRESSION TEST ON NR 1 CYLINDER. COMPRESSION WAS LOW AND AIR WAS ESCAPING PAST EXHAUST VALVE INTO EXHAUST STACK. R & R CYLINDER WITH REPAIRED AND INSPECTED UNIT. REPO
- [SDR CA130807012](https://openairdocs.org/sdr/CA130807012.md): Line · cracked · Jul 31, 2013 · Beech 95B55 · Engine Fuel Distribution
  > (CAN) DURING A DAILY INSPECTION ON THE RT ENGINE, THE FUEL INJECTOR LINE AT THE NR 3 CYLINDER FUEL INJECTOR WAS FOUND FUEL/SOOT STAINED. A QUICK LEAK CHECK WITH THE FUEL BOOST PUMP RUNNING REVEALED A LEAK NEAR THE FITTING ATTACHING THE LINE TO THE FUEL INJECT
- [SDR 2013FA0000372](https://openairdocs.org/sdr/2013FA0000372.md): Tube · defective · May 9, 2013 · N364GL · Beech 95B55 · Tire Tube
  > NOSE TIRE WENT FLAT ON LANDING. TUBE HAD PIN HOLE.
- [SDR CA120809014](https://openairdocs.org/sdr/CA120809014.md): Control Cable · crossed · Jul 27, 2012 · Beech 95B55 · Rudder Tab Control System
  > (CAN) IN CRUISE, PILOT ATTEMPTED TO CENTER THE BALL IN THE TURN AND BANK INDICATOR BY APPLYING RUDDER TRIM. WHEN APPLIED, AFFECT WAS OPPOSITE TO NORMAL, TURNED TRIM WHEEL LT AND RT RUDDER TRIM WAS NOTED. PILOT LANDED AND ADVISED MAINTENANCE. MAINTENANCE DISC
- [SDR 2012FA0000540](https://openairdocs.org/sdr/2012FA0000540.md): Motor · failed · Jun 30, 2012 · N308RB · Beech 95B55 · Landing Gear Retraction/Extension System
  > LANDING GEAR MOTOR WOULD TRIP CIRCUIT BREAKER DURING ALL ATTEMPTS AT LOWERING LANDING GEAR. EMERGENCY PROCEDURES FOR LANDING GEAR EXTENSION FAILURE AND MANUAL GEAR EXTENSION UNSUCCESSFUL RESULTING IN A GEAR-UP LANDING. ON INSPECTION OF LANDING GEAR COMPONENT
- [SDR CA110503006](https://openairdocs.org/sdr/CA110503006.md): Aileron · misinstalled · Apr 27, 2011 · Beech 95B55 · Ailerons
  > (CAN) RT AILERON OUTBOARD ATTACH DISCONNECTED IN FLIGHT DUE TO IMPROPER INSTALLATION. ON INSPECTION PICK UP POINTS FOR AILERON ATTACH HAD BEEN MISSED INTERNALLY DUE TO DIFFICULTY IN VISUAL ALIGNMENT IN BETWEEN SKINS WHERE ATTACH HARDWARE PURCHASE AILERON ATTAC
- [SDR 2010FA0001234](https://openairdocs.org/sdr/2010FA0001234.md): Line · corroded · Dec 7, 2010 · N464V · Beech 95B55 · Aircraft Fuel Distribution System
  > ACCESSED & CLOSELY INSPECTED RT FUEL FLOW/PRESSURE GAGE LINE WHERE IT CROSSED DEFROST DUCT BECAUSE IT LOOKED LIKE THEY MAY BE CONTACTING. FOUND EXTENSIVE CORROSION AT POINT OF CONTACT. AFTER LINE WAS REMOVED, SLIGHT BENDING PRESSURE CRACKED AREA WIDE OPEN AN
- [SDR 2010FA0001103](https://openairdocs.org/sdr/2010FA0001103.md): Control Cable · detached · Sep 20, 2010 · N9420Y · Beech 95B55 · Mixture Control
  > DURING FLIGHT, THE RT ENGINE MIXTURE CONTROL FAILED AND THE ENGINE QUIT. AFTER LANDING, FOUND THE SWAGGED END OF THE MIXTURE CONTROL CABLE (PN 50-389010-21) HAD SEPARATED AT THE FUEL CONTROL UNIT.
- [SDR 2010FA0000249](https://openairdocs.org/sdr/2010FA0000249.md): Lifter · spalled · Mar 9, 2010 · N519BG · Beech 95B55 · Reciprocating Engine Cylinder Section
  > ENGINE CYLINDERS HAD LOW COMPRESSION. REMOVED CYLINDERS AND FUND LIFTERS HAD SPALLING AND CAM SHAFT WAS WORN. LIFTER PN 653888 AND PN 653877 INSTALLED. THESE PN ARE DESIGNATED AS NOT AFFECTED BY MSB 09-8 OR AD 2009-24-52.
- [SDR 2008FA0000847](https://openairdocs.org/sdr/2008FA0000847.md): Spring · broken · Nov 25, 2008 · N5716V · Beech 95B55 · Engine Starter
  > STARTER ADAPTER P/N 635050-A4, STARTER SPRING FAILED. STARTER ADAPTER OVERHAULED, RETURNED TO SERVICE AFTER OVERHAUL. PART SOLD, STARTER ADAPTER INSPECTED AND RETAGGED AND SOLD TO MFG. MAINT INSTALLED STARTER ADAPTER AND SPRING FAILED 14 HOURS LATER.
- [SDR 2008FA0000710](https://openairdocs.org/sdr/2008FA0000710.md): Tube · chafed · Oct 27, 2008 · N527T · Beech 95B55 · Propeller Controlling System
  > ALUMINUM TUBING TO PROP GOVERNOR FOUND CHAFED DUE TO TIE RAP RUBBING TUBE. FABRICATED NEW TUBE, INSTALLED AND LEAK CHECKED.
- [SDR 2007FA0001088](https://openairdocs.org/sdr/2007FA0001088.md): Rib · cracked · Nov 9, 2007 · N127RW · Beech 95B55 · Trailing Edge Flaps
  > AT ANNUAL INSPECTION FOUND CRACK ON FLAP RIB. (FLAP ROD ATTACH POINT) BOTH LT AND RT FLAPS. (K)
- [SDR CA071002005](https://openairdocs.org/sdr/CA071002005.md): Piston · damaged · Sep 28, 2007 · Beech 95B55 · Reciprocating Engine Cylinder Section
  > (CAN) DURING CRUISE FLT, RT ENGINE BEGAN TO LOOSE OIL PRESSURE. OIL TEMP & CHT INCREASED. PILOT ELECTED TO SHUTDOWN ENGINE AS A VIBRATION BECAME APPARENT & OIL PRESSURE DECREASED TO NEAR ZERO. AN EMERGENCY DECLARED & AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. U
- [SDR CA071212002](https://openairdocs.org/sdr/CA071212002.md): Spar · cracked · Sep 21, 2007 · Beech 95B55 · Wing Spar
  > (CAN) DURING ANNUAL INSPECTION, VISUAL INSPECTION OF AREA REVEALED A SUSPECTED CRACK. NOT OF DYE PENETRANT AND EDDY CURRENT CONFIRMED. MFG SERVICE KIT TO INSTALLED. PART LAST NDT INSPECTED 22.1 HRS PREVIOUS AND NO INDICATIONS. (TC NR 20071212002)
- [SDR CA070801001](https://openairdocs.org/sdr/CA070801001.md): Fuel Cell · deteriorated · Jul 27, 2007 · Beech 95B55 · Fuel Storage
  > (CAN) THE RT WING LEADING EDGE FUEL CELL WAS REMOVED BECAUSE OF A FUEL LEAK. A REPLACEMENT FUEL CELL WAS ORDERED. PRIOR TO INSTALLATION OF THE NEW (OVERHAULED) CELL, IT WAS INSPECTED AND FOUND TO CONTAIN A LARGE QUANTITY OF SAWDUST-LIKE PARTICLES. ON FURTHER I
- [SDR ATL07LA057](https://openairdocs.org/sdr/ATL07LA057.md): Fuel Cell · leaking · Mar 19, 2007 · N500JP · Beech 95B55 · Fuel Storage
  > DURING START OF RT ENGINE, PILOT REPORTED HEARING A LOUD THUMP, NOTED FIRE COMING FROM THE BOTTOM OF THE RT COWLING. SHUTDOWN ENGINES, EVACUATED AIRCRAFT, AND NOTED APPARENT EXPLOSION HAD OCCURRED IN RT WING. VISUAL INSPECTION DID NOT REVEAL CAUSE OF EVENT
- [SDR 2007FA0000030](https://openairdocs.org/sdr/2007FA0000030.md): Valve · failed · Dec 15, 2006 · N3845L · Beech 95B55 · Heating System
  > FOUND THERMOSTAT WORKING, BUT FUEL SOLENOID NOT STOPPING FUEL DELIVERY EVEN WITH POWER TO VALVE DISTUPTED. CABIN HEATER ONLY SHUTDOWN WHEN OVERHEAT SWITCH OPENED. VALVE INFO: MODEL NR 4400B.
- [SDR CA060624001](https://openairdocs.org/sdr/CA060624001.md): Bolt · loose · Jun 15, 2006 · Beech 95B55 · Aileron Tab Control System
  > (CAN) AILERON TRIM BOLT FOUND MIGRATING OUT OF LINKAGE ARM ON LT AILERON TRIM TAB ASSEMBLY. BOLT WAS NOTED TO BE FINGER-TIGHT ONLY AND NOT SET INTO LOCKING DEVICE. NOTE: BOLT WAS FOUND IN THIS CONDITION AFTER FLIGHT CONTROLS WERE INSTALLED AFTER AIRCRAFT WAS P
- [SDR PAI5200604049](https://openairdocs.org/sdr/PAI5200604049.md): Plate · cracked · Apr 17, 2006 · N6747V · Beech 95B55 · Brake
  > DURING ANNUAL INSPECTION FOUND RT BRAKE TORQUE PLATE CRACKED.7500 OF THE LENGTH OF THE CALIPER PIN BORE.
- [SDR 2006FA0000327](https://openairdocs.org/sdr/2006FA0000327.md): Impulse Coupling · rusted · Mar 13, 2006 · N2278S · Beech 95B55 · Magneto/Distributor
  > DURING A ROUTINE INSP, ALL MAGNETOS WERE REMOVED FOR POINTS AND CONDENSER REPLACEMENT. RUST WAS FOUND ON THE FLYWEIGHT/AXLE AREA OF THE IMPULSE COUPLING. A WEAR CHECK WAS MADE AND IT WAS DETERMINED THAT ALL COUPLINGS FAILED IAW MSB. NOTE: THE FLYWEIGHT/ AX
- [SDR 2006FA0000265](https://openairdocs.org/sdr/2006FA0000265.md): Baffle · deteriorated · Mar 1, 2006 · N56JK · Beech 95B55 · Fuel Storage
  > FOUND FUEL SYSTEM CONTAMINATED WITH AN UNKNOWN SUBSTANCE. AFTER HAVE THE ENTIRE SYSTEM DRAINED, FLUSHED AND THE ENGINE FUEL INJECTION SYSTEM OVERHAULED, THE AIRCRAFT WAS REFUELED AND FLOWN. AFTER A SHORT FLIGHT, THE SUMPS WERE CHECKED AGAIN AND THE SUBSTANCE
- [SDR 2006FA0000262](https://openairdocs.org/sdr/2006FA0000262.md): Fuel Cell · deteriorated · Mar 1, 2006 · N56JK · Beech 95B55 · Fuel Storage
  > FOUND FUEL SYTEM CONTAMINATED WITH AN UNKNOWN SUBSTANCE. AFTER HAVING THE ENTIRE SYSTEM DRAINED, FLUSHED AND THE ENGINE FUEL INJECTION SYSTEM OVERHAULED, THE AIRCRAFT WAS REFUELED AND FLOWN. AFTER A SHORT FLIGHT, THE SUMPS WERE CHECKED AGAIN AND THE SUBSTANC
- [SDR 2005FA0001364](https://openairdocs.org/sdr/2005FA0001364.md): Spar Cap · corroded · Sep 28, 2005 · N1071T · Beech 95B55 · Wing Spar
  > DURING AN ANNUAL INSPECTION, SOME CORROSION WAS FOUND IN THE AREA OF THE RT WING TIE DOWN ASSY, UPON FURTHER INVESTIGATION AN AREA OF APPROXIMATELY 8 INCHES IN LENGTH WITH SEVERE INTERGRANULAR CORROSION WAS DISCOVERED ON THE LOWER SPAR CAP POSSIBLY CAUSED BY D
- [SDR CA050617007](https://openairdocs.org/sdr/CA050617007.md): Doubler · cracked · Jun 15, 2005 · Beech 95B55 · Wing Spar
  > (CAN) DURING ROUTINE LPI INSPECTION OF THE FRONT WING SPAR CARRY THRU STRUCTURE AND REPAIR DOUBLERS IN ACCORDANCE WITH AD90-08-14, THE LT FWD REPAIR DOUBLER WAS FOUNDCRACKED IN THE LOWER BEND RADIUS IN THE SAME SPOT AS THE ACTUAL WING SPAR WHICH THE DOUBLER WA
- [SDR 2005FA0000794](https://openairdocs.org/sdr/2005FA0000794.md): Door · delaminated · May 23, 2005 · N4455B · Beech 95B55 · Landing Gear Doors
  > IB LANDING GEAR DOORS HAD CORROSION DUE TO DELAMINATION OF FORWARD EDGE OF GEAR DOORS.
- [SDR IS4R200500003](https://openairdocs.org/sdr/IS4R200500003.md): Combustion Head · worn · May 13, 2005 · N560X · Beech 95B55 · Heating System
  > HEATER CORE RECEIVED FROM CUSTOMER. UPON TEARDOWN, FOUND INTERIOR OF THE COMBUSTION HEAD SEVERELY WORN FROM FLAME EROSION. PREVIOUS INSPECTIONS BY THIS REPAIR STATION HAVE FOUND SMALL HOLES APPEARING IN THE WALL OF THE COMBUSTION HEAD. FROM THE OUTSIDE, THE
- [SDR IS4R200500002](https://openairdocs.org/sdr/IS4R200500002.md): Tube · cracked · May 13, 2005 · N560X · Beech 95B55 · Heating System
  > HEATER COR RECEIVED FROM CUSTOMER. COMBUSTION TUBE FOUND CRACKED AT CROSSOVER PART WHICH CONNECTS THE INNER COMBUSTION TUBE TO THE OUTER COMBUSTION TUBE. MALFUNCTION FOUND USING A PRESSURE DECAY TEST, EVEN THOUGH THIS TEST IS NOT REQUIRED ON THE D83A28 HEATE
- [SDR CA050512009](https://openairdocs.org/sdr/CA050512009.md): Coupling · worn · May 12, 2005 · Beech 95B55 · Engine Fuel Pump
  > AIRCRAFT IN CRUISE, ENGINE SPUTTERED AND DIED. BOOST PUMP ACTIVATED AND ENGINE RESTARTED. PART IS AN ON-CONDITION ITEM. THE SQUARE DRIVE ROUNDED OFF UNTIL IT WOULD NO LONGER ENGAGE THE DRIVE GEAR P/N 631684. THIS CAUSED THE FUEL PUMP TO STOP ROTATING RESUL
- [SDR CA041215003](https://openairdocs.org/sdr/CA041215003.md): Relay · malfunctioned · Dec 13, 2004 · Beech 95B55 · Landing Gear Retraction/Extension System
  > (CAN) DURING A MISSED APPROACH PILOT INITIATED A TURN TO RETURN FOR A 2ND APPROACH WHEN MLG EXTENDED UNCOMMANDED WITH NO DOWN OR UP INDICATION LIGHTS. PILOT SLOWED ACRFT & CONTINUED TO DESTINATION WITH MLG SELECTED DOWN & CONFIRMED MLG DOWN WITH EMERGENCY GEAR

Next page: https://openairdocs.org/model/beech-95-b55/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 = '95B55'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/beech-95-b55/reports

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