# Service difficulty reports: Beech E-90

A list on [Beech E-90](https://openairdocs.org/model/beech-e-90.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 3 · 139 reports

- [SDR 2024FA0000739](https://openairdocs.org/sdr/2024FA0000739.md): Gps · defective · Sep 26, 2024 · N98PM · Beech E90 · Global Positioning System
  > WHILE ENROUTE TO KLVS FROM KGUY, THE GARMIN GNS530W SCREEN SHUT OFF. WHILE TROUBLESHOOTING, A STRONG ELECTRICAL SMELL FILLED THE CABIN. THE AIRCRAFT DIVERTED TO KTDW FOR FURTHER EVALUATION BY THE MAINTENANCE TEAM. UPON FURTHER EVALUATION, IT HAS BEEN DETERMINE
- [SDR T4OR2022071400002](https://openairdocs.org/sdr/T4OR2022071400002.md): Brake Assy · broken · Jul 14, 2022 · N29M · Beech E90 · Landing Gear Brake System
  > DURING LANDING ROLL-OUT BRAKING, THE LEFT BRAKE PEDAL WENT MOST OF ITS TRAVEL WITH LITTLE BRAKING EFFECT. IT WAS DISCOVERED THE LEFT BRAKE TORQUE PLATE WAS CRACKED AND OPENED UP SO CALIPER THE GUIDE PIN WAS NOT RETAINED IN THE TORQUE PLATE. TORQUE PLATE P/N
- [SDR 9LMR032222N600AC](https://openairdocs.org/sdr/9LMR032222N600AC.md): Test Switch · crew error · Mar 22, 2022 · N600AC · Beech E90 · Landing Gear Position and Warning
  > LANDING GEAR INDICATOR GREEN LIGHT PRESS-TO-TEST, REMOVED, INSPECTED AND RE-INSTALLED. NO DISCREPANCIES NOTED AT THIS TIME. LANDING GEAR RETRACTION SYSTEM INSPECTION COMPLIED WITH, FOR PROPER OPERATION, WARNING HORN AND LIGHT, BY TWO COMPLETE CYCLES, OPER
- [SDR HAEA20190614001](https://openairdocs.org/sdr/HAEA20190614001.md): Axle · missing · Jun 12, 2019 · N176TW · Beech E90 · Main Landing Gear Strut/Axle/Truck
  > ON DEPARTURE FROM KGVT THE CREW HEARD A NOISE FROM THE RH WING AREA, NOT SURE WHAT IT WAS THEY LEFT THE GEAR DOWN AND LOCKED AND PERFORMED A FLY BY THE TOWER AND DETERMINUED THE RH M/L/G PISTON/AXLE ASSEMBLY WAS MISSING. THE AIRCRAFT WAS FLOWN TO KAFW WHERE TH
- [SDR 2019F00061](https://openairdocs.org/sdr/2019F00061.md): Boot · detached · Aug 13, 2018 · N9029R · Beech E90 · Propeller Deice Boot Section
  > 08-11-2018 THE AIRCRAFT HAD A PROPELLER DE-ICE BOOT REPLACED THAT HAD FALLEN OFF. 08-12-2018 ON A FLIGHT, THE BOOT DETACHED FROM THE PROPELLER AND WAS REPAIRED. 08/15/2018 AT APPROXIMATELY 17:10, AT ABOUT 1000' AGL, THE PILOT HEARD A POP IN THE COCKPIT, C
- [SDR 2018FA0000290](https://openairdocs.org/sdr/2018FA0000290.md): Bolt · loose · Mar 29, 2018 · N77CE · Beech E90 · Fuel Storage
  > DURING FLIGHT FROM KVNY TO KJAC THE CAPTAIN NOTICED FUEL LEAKING FROM THE FILL CAP AREA OF THE LEFT HAND NACELLE FUEL TANK. THE AIRCRAFT WAS DIVERTED TO KLAS FOR INSPECTION. UPON INSPECTION BY A MAINTENANCE TECHNICIAN IT WAS DETERMINED THAT THE LEAK WAS DUE
- [SDR 2018FA0000081](https://openairdocs.org/sdr/2018FA0000081.md): Skin · chafed · Mar 7, 2018 · N500MS · Beech E90 · Fuselage Main, Plate/Skin
  > ON REMOVAL OF THE HORIZONTAL STABILIZERS FROM THE FUSELAGE, SIGNIFICANT FUSELAGE SKIN CHAFFING WAS FOUND ON BOTH SIDES OF THE AIRCRAFT FROM THE RUBBER SEAL THAT FITS BETWEEN THE FUSELAGE AND HORIZONTAL STABILIZERS. IT WOULD BE ASSUMED TIME, VIBRATION, AND ATM
- [SDR 2018FA0000057](https://openairdocs.org/sdr/2018FA0000057.md): Clamp · broken · Feb 14, 2018 · N500MS · Beech E90 · Fuselage Main, Attach Fittings
  > FOUND BOTH OXYGEN BOTTLE HOLD-DOWN CLAMP BASES BROKEN IN TWO.
- [SDR CA180117004](https://openairdocs.org/sdr/CA180117004.md): Bracket · cracked · Jan 16, 2018 · Beech E90 · Trailing Edge Flaps
  > (CAN) DURING ROUTINE MAINTENANCE DISCOVERED FLAP TRACK BRACKET CRACKED AT REAR OF SLOT. (TC NR 20180117004).
- [SDR 2016F00123](https://openairdocs.org/sdr/2016F00123.md): Wire · chafed · May 7, 2016 · N181CG · Beech E90 · Fire Protection System Wiring
  > EXPERIENCED A MASTER WARNING & FIRE INDICATION ON THE NR 2 ENG, SHORTLY AFTER GETTING INTO SOME HEAVY PRECIPITATION. THE PILOT RESET THE MASTER WARNING, BOTH THE MASTER WARNING & ENG FIRE INDICATION WENT OUT. ALL OTHER ENG PARAMETERS WERE NORMAL. HE ASKED T
- [SDR NBFA201508030001](https://openairdocs.org/sdr/NBFA201508030001.md): Unknown · smoke · Aug 1, 2015 · N22N · Beech E90 · Air Distribution System
  > DURING CRUISE, THE CREW SMELLED AND SAW LIGHT SMOKE COMING FROM BEHIND THE GLARE SHIELD. USING CREW PROCEDURES, UNNECESSARY ELECTRICAL SYSTEM WERE SHUTDOWN. SOURCE OF SMELL AND SMOKE STOPPED. THE ACFT LANDED SAFELY.
- [SDR HAEA2015040500231](https://openairdocs.org/sdr/HAEA2015040500231.md): Rudder Mast · damaged · Jun 2, 2015 · N176TW · Beech E90 · Rudder Control System
  > DURING PHASE 1 ACFT INSPECTION, DISCOVERED THE RUDDER TO BELL CRANK RT ATTACH BOLT MISSING. FURTHER INVESTIGATION REVEALED THE BOLT HAD FAILED. AN INSPECTION OF THE RUDDER TORQUE TUBE WAS CONDUCT & IT WAS NOTED THAT THE ATTACH HOLES OF THE BELL CRANK & RUDDE
- [SDR CA130524003](https://openairdocs.org/sdr/CA130524003.md): Gyro · failed · May 23, 2013 · Beech E90 · Attitude Gyro and Indicating System
  > (CAN) AFTER REPLACEMENT OF DISPLACEMENT GYRO, FLIGHT CREW NOTIFIED MAINTENANCE THAT THE ATTITUDE INDICATOR INFORMATION WAS BACKWARDS. MAINTENANCE FOUND THE FORWARD POINTING ARROW ON THE COVER OF THE UNIT WAS INSTALLED BACKWARDS. THIS ARROW IS TO GUIDE THE IN
- [SDR GNL2013F00000](https://openairdocs.org/sdr/GNL2013F00000.md): Attach Fitting · cracked · Apr 2, 2013 · N21NM · Beech E90 · Wing, Attach Fittings
  > LEFT LOWER FORWARD WING ATTACH FITTING CRACKED. CRACK WAS FOUND DURING SIRM WING ATTACH FITTING INSPECTION. EDDY CURRENT WAS THE INSPECTION METHOD. MFG SUPPORT WAS CONTACTED IAW SIRM INSTRUCTIONS. THE FITTING WAS REPLACED BY MFG SERVICES TECH USING WING FI
- [SDR 2013FA0000150](https://openairdocs.org/sdr/2013FA0000150.md): G Switch · misinstalled · Mar 6, 2013 · N92DV · Beech E90 · Emergency Locator Beacon
  > WHILE PERFORMING THE ANNUAL ELT INSPECTION, THE ELT WOULD NOT SIGNAL DURING THE "SHAKE" TEST. THE COVER WAS REMOVED FOR A VISUAL INSPECTION. THE G-SWITCH WAS INSTALLED BACKWARD. ALL INDICATIONS WITH A MAGNIFYING GLASS APPEAR THIS TO BE A FACTORY INSTALL, NO
- [SDR CA121004006](https://openairdocs.org/sdr/CA121004006.md): Support Bracket · cracked · Oct 4, 2012 · Beech E90 · Main Landing Gear
  > (CAN) DURING SCHEDULED INSPECTION, THE BEARING INSIDE THE LANDING GEAR TORQUE TUBE SUPPORT BRACKET HAD MOVED OUT OF PLACE. FURTHER INVESTIGATION REVEALED A CRACK THROUGH THE GREASE FITTING HOLE ON THE SUPPORT BRACKET.
- [SDR CA120719002](https://openairdocs.org/sdr/CA120719002.md): Gasket · split · Jul 17, 2012 · Beech E90 · Nacelle/Pylon, Main Frame
  > (CAN) NACELLE GASKETS SPLIT AT BOLT HOLES AND CAUSED FUEL LEAK. GASKETS REPLACED IAW SB 28-4059.
- [SDR CA110802009](https://openairdocs.org/sdr/CA110802009.md): Rib · cracked · Aug 2, 2011 · Beech E90 · Elevator, Spar/Rib
  > DURING INSP, FRETTING (SMOKING) WAS FOUND TO BE COMING FROM BETWEEN THE ELEVATOR TORQUE TUBE AND THE INBD RIB THAT THE TUBE ATTACHES TO. AFTER DISASSEMBLY, CRACKS WERE FOUND IN THE RIB AND DOUBLER. BOTH ELEVATORS HAVE SIMILAR DAMAGE.
- [SDR GNL2011F00001](https://openairdocs.org/sdr/GNL2011F00001.md): Resistor · shorted · Jul 26, 2011 · N21NM · Beech E90 · Instrument System Wiring
  > ACFT IN CRUISE FLIGHT. ELECTRIC SMOKE FILLED THE CABIN AND COCKPIT. NON-ESSENTIAL EQUIPMENT WAS TURNED OFF AND THE SMOKE CLEARED. THERE WERE NO TRIPPED CIRCUIT BREAKERS AND THE PILOT NOTICED THE "PILOT INSTRUMENT LIGHTS" RHEOSTAT WAS ONLY PARTIALLY FUNCTION
- [SDR GNL2011F00000](https://openairdocs.org/sdr/GNL2011F00000.md): Controller · intermittent · Dec 27, 2010 · N304LG · Beech E90 · Cabin Temperature Controller
  > ACFT CLIMBING THROUGH 12,000 FT, CREW NOTICED A HAZE IN THE CABIN FOLLOWING INCREASE IN CABIN TEMP. A DESCENT TO 11,000 FT WAS MADE. ATTEMPTS WERE MADE TO STOP BOTH THE HEAT AND SMOKE. CABIN PRESSURIZATION "DUMP" SWITCH WAS SELECTED AND THE ACFT WAS LANDED
- [SDR YUUR101220105690](https://openairdocs.org/sdr/YUUR101220105690.md): Connector · separated · Dec 7, 2010 · N2192L · Beech E90 · Ice/Rain Protection System Wiring
  > (YUUR) DURING PRE-INSP GROUND RUNS THE PROPELLER DE-ICE AMPERAGE WAS NOTED LOW. INSP REVEALED THE BLADE DE-ICE BOOT LEAD IS A 2 PIECE ASSY WITH A MOLEX TYPE CONNECTOR SECURED TO THE BLADE. INSIDE THE CONNECTOR THERE IS AN ORANGE PIECE OF FOAM FOR SEALING THE
- [SDR DGCA10851](https://openairdocs.org/sdr/DGCA10851.md): Windshield · cracked · Dec 3, 2010 · N824AC · Beech E90 · Flight Compartment Windows
  > CO-PILOTS WINDSHIELD CRACKED.
- [SDR 2010FA0001089](https://openairdocs.org/sdr/2010FA0001089.md): Fire Warning · false activation · Oct 6, 2010 · N181CG · Beech E90 · Fire Detection
  > FIRE WARNING ON RT ENGINE WITH NO SUPPORTING EVEDENCE OF ACTUAL FIRE. CHECK LIST COMPLIED WITH AND PRECAUTIONARY LANDING ACCOMPLISHED. INSPECTED AND TROUBLESHOT FIRE DETECTION SYS IAW MM 26-10-00 CHART 101, PROBLEM NR4. NO DEFECT NOTED CLEANED AND DRIED ELECT
- [SDR 2010FA0001085](https://openairdocs.org/sdr/2010FA0001085.md): Fire Warning · false activation · Oct 6, 2010 · N181CG · Beech E90 · Fire Detection
  > FIRE WARNING ON RT ENGINE WITH NO SUPPORTING EVIDENCE OF ACTUAL FIRE. CHECKLIST COMPLIED WITH AND PRECAUTIONARY LANDING ACCOMPLISHED.
- [SDR CA100922002](https://openairdocs.org/sdr/CA100922002.md): Control Cable · damaged · Sep 17, 2010 · Beech E90 · Elevator Tab Control System
  > ELEVATOR TRIM CABLE WAS FOUND UNSPOOLED OFF BOTH FWD AND AFT TRIM DRUMS.
- [SDR CA100531006](https://openairdocs.org/sdr/CA100531006.md): Blower Motor · overheated · May 21, 2010 · Beech E90 · Air Distribution Fan
  > CABIN VENTILATION BLOWER MOTOR OVERHEATED AND CREATED SMOKE IN THE COCKPIT. PILOT WAS FORCED TO DO AN EMERGENCY LANDING. UPON INVESTIGATION THE BLOWER MOTOR CIRCUIT BREAKER WAS FOUND TRIPPED. THE BLOWER MOTOR WAS REPLACED WITH A O/H UNIT AND THE CIRCUIT BRE
- [SDR VIB4 1536](https://openairdocs.org/sdr/VIB4%201536.md): Circuit Breaker · intermittent · Apr 22, 2010 · N93A · Beech E90 · Landing Gear Retraction/Extension System
  > (VIB4) DURING TAKEOFF THE ACFT ATTEMPTED A NORMAL GEAR RETRACTION. THE LANDING GEAR STARTED A NORMAL RETRACTION WHEN IT STOPPED EARLY IN THE RETRACTION CYCLE. WHEN IT STOPPED THE ACFT DID NOT HAVE ANY DOWN AND LOCK LIGHTS NOR DID IT HAVE AN UNSAFE LIGHT IN THE
- [SDR CA100218013](https://openairdocs.org/sdr/CA100218013.md): Skin · cracked · Feb 10, 2010 · Beech E90 · Fuselage Main, Plate/Skin
  > (CAN) FUSELAGE PRESSURE SKINS P/N 50-420011-1051 AND 1052 CRACKED AND WORN BY CHAFING ACTION BETWEEN THEM AND FILLETS PN 50-420023-31 AND 32 DUE TO NORMAL WING MOVEMENT. (TC 20100218013)
- [SDR CA100218012](https://openairdocs.org/sdr/CA100218012.md): Skin · cracked · Feb 10, 2010 · Beech E90 · Fuselage Main, Plate/Skin
  > (CAN) FUSELAGE PRESSURE SKINS PN 50-120156-81 AND 82 CRACKED AT LOWER SPAR CAP PENETRATIONS. (TC 20100218012)
- [SDR DGCA09331](https://openairdocs.org/sdr/DGCA09331.md): Fuel Control · hung up · Nov 2, 2009 · N824AC · Beech E90 · Fuel Controlling System
  > ON LANDING THE ENG POWER HUNG AT APP 800 LBS OF TORQUE. FOUND FUEL CONTROL UNIT FAULTY.
- [SDR CA091020001](https://openairdocs.org/sdr/CA091020001.md): Splice · missing · Oct 20, 2009 · Beech E90 · Fuselage Main, Plate/Skin
  > (CAN) DURING INSP OF FUSELAGE BELLY SKINS JUST AFT OF FWD WING SPAR, AN UNUSUAL SKIN BUTT SPLICE WAS FOUND. SPLICE HAS ONLY A SINGLE ROW OF RIVETS IN A PRESSURIZED VESSEL, WHERE THERE IS NORMALLY A DOUBLE ROW. FURTHER INVESTIGATION OF THE INSTALLATIOIN DWG FOR
- [SDR CA090617003](https://openairdocs.org/sdr/CA090617003.md): Hinge · cracked · Jun 16, 2009 · Beech E90 · Elevator Structure
  > (CAN) LT HORIZ STAB CTR HINGE LWR OTBD CORNER CRACKED. INITIALLY APPEARED TO BE CRACK IN THE PAINT UNTIL CLOSER EXAMINATION.
- [SDR 2009F00036](https://openairdocs.org/sdr/2009F00036.md): Bolt · cracked · May 27, 2009 · N48W · Beech E90 · Wing Main, Frame Structure
  > POSSIBLE CRACK IN AFT WING BOLTS UPPER (POSSIBLY WAS CAD PLATING ON BOLTS) SHOWING IN THREADS OF BOLTS.
- [SDR T4OR 4995 70](https://openairdocs.org/sdr/T4OR%204995%2070.md): Roller · worn · Apr 23, 2009 · N965LG · Beech E90 · Trailing Edge Flaps
  > RT OTBD FLAP ATTACH POINT BRACKETS (RIBS) ARE WORN WHERE AFT FLAP TRACK ROLLERS ARE ATTACHED. BRACKETS ARE WORN APPROXIMATELY.015 INCH TO.020 INCH DEEP IN THE BRACKET SIDES FROM THE ROLLER IN THE SHAPE OF THE ROTATING ROLLER ENDS. SUSPECT CAUSE TO BE WORN
- [SDR VQMAF010510](https://openairdocs.org/sdr/VQMAF010510.md): Circuit Board · burned out · Mar 13, 2009 · N379VM · Beech E90 · Central Warning
  > A CABIN ALTITUDE WARNING PRESSURE SWITCH TEST WAS PERFORMED BY METHOD 2, AS REFERENCED IN MM 21-30-00, PAGE 214, ITEMS A-F. DETERMINED THAT THE TEST FAILED ITEM C OF THE TEST, BECAUSE THERE WAS NO VISUAL AMBER "CABIN ALTITUDE HIGH" WARNING ANNUNCIATION AVAILAB
- [SDR CIEA200800009](https://openairdocs.org/sdr/CIEA200800009.md): Windshield · cracked · Dec 16, 2008 · N63BV · Beech E90 · Flight Compartment Windows
  > DURING CRUISE AT FL240 APPROX 80 TO 90 MILES FROM KCPR, THE RT SIDE FRONT WINDSHIELD CRACKED. AT THE TIME, THE TEMPERATURE OUTSIDE WAS -38 DEGREES CELSIUS AND THE WINDSHIELD HEAT WAS OFF WITH CLEAR SKIES OBSERVED. THE PILOT CONTACTED ATC AND LET THEM KNOW TH
- [SDR 2008FA0000670](https://openairdocs.org/sdr/2008FA0000670.md): Fuel Line · cracked · Oct 10, 2008 · N379VM · Beech E90 · Engine Fuel Distribution
  > WHILE PERFORMING ENGINE RUNS FOR RIGHT ENGINE FLOW PACK CHANGE FOUND FUEL LEAK FROM FUEL LINE FROM FCU TO TOP OF START CONTROL UNIT. FITTING CRACKED ABOVE SCU. REMOVED CRACKED FUEL LINE FROM FCU TO TOP OF START CONTROL UNIT. INSTALLED OVERHAULED LINE P/N 30
- [SDR 2008FA0000321](https://openairdocs.org/sdr/2008FA0000321.md): Spar Cap · cracked · Apr 25, 2008 · N692M · Beech E90 · Wing Spar
  > THE CRACK EMANATES FROM THE 5TH RIVET OUTBOARD OF THE LOWER FORWARD WING BOLT FITTING, (4TH RIVET FROM END OF SPAR CAP)IN THE REAR ROW OF RIVETS, & EXTENDS TO THE TRAILING EDGE OF CAP. THE A/C PASSED 2-400 HR WING SIRM INSPECTIONS. THE CRACK WAS DETECTED AT TH
- [SDR 2008FA0000326](https://openairdocs.org/sdr/2008FA0000326.md): Spar Cap · cracked · Apr 25, 2008 · N776DC · Beech E90 · Wing Spar
  > THE CRACK EMANATES FROM THE 5TH RIVET OUTBOARD OF THE LOWER FORWARD WING BOLT FITTING, 4TH RIVET FROM END OF SPAR CAP, IN THE FRONT ROW OF RIVETS, AND EXTENDS TO THE LEADING EDGE OF CAP. THE A/C PASSED 2-400 HOUR WING SIRM INSPECTIONS. 181 HRS INTO NEXT INTE
- [SDR R025878](https://openairdocs.org/sdr/R025878.md): Clamp · cracked · Apr 9, 2008 · Beech E90 · Propeller Assembly
  > 838-67 CLAMP ASSY SN EF3099. CRACK FOUND INTERSECTING THE THREADED LINK SCREW HOLE.
- [SDR CA080423013](https://openairdocs.org/sdr/CA080423013.md): Fuel Control · malfunctioned · Mar 28, 2008 · Beech E90 · Fuel Control/Turbine Engines
  > (CAN) DURING APPROACH, UPON RETARDING THE POWER LEVER TO IDLE, THE ENGINE ACCELERATED TO 90 PERCENT NG WITH AN ASSOCIATED TEMPERATURE OF 800 DEGREES. THE PILOT ELECTED TO SHUTDOWN THE ENGINE AND FEATHER THE PROP. THE FUEL CONTROL WAS SUBSEQUENTLY REPLACED AND
- [SDR 2008FA0000082](https://openairdocs.org/sdr/2008FA0000082.md): Capacitor · burned · Feb 18, 2008 · N662JS · Beech E90 · Light System Wiring
  > AT CRUISE FL 150, CREW NOTICED SMOKE AND ELECTRICAL ODOR COMING FROM SIDEWALL UNDERNEATH EMERGENCY EXIT. PIC DECLARED EMERGENCY AND LANDED AC WITHOUT FURTHER INCIDENT. UPON INSP OF SIDEWALL UNDER EMERGENCY EXIT, IT WAS NOTICED THAT A SMALL HOLE WHICH APPEAR
- [SDR O7Z2008F00000](https://openairdocs.org/sdr/O7Z2008F00000.md): Spar Cap · cracked · Jan 28, 2008 · N152D · Beech E90 · Wing Spar
  > FWD OB LOWER WING SPAR CAPS ARE CRACKED. LT AND RT ASSY CRACKS RADIATE FROM THE (4) HUCK RIVET FWD THROUGH WING ATTACH HINGE. THE AIRCRAFT WAS INSPECTED 15 MONTHS AND 404.2 HOURS AGO BY EDDY CURRENT AND NO CRACKS WERE FOUND AT THAT TIME. (K)
- [SDR LW29212112007](https://openairdocs.org/sdr/LW29212112007.md): Unknown · odor · Dec 11, 2007 · N92DV · Beech E90 · Air Distribution System
  > DEPARTED, UPON REACHING 7500 FEET SMELLED BURNING OIL FUMES IN CABIN. CLOSED BLEED AIR'S, TURNED OFF ENVIRONMENTAL SYSTEMS AND DUMPED CABIN. SAFELY RETURNED TO DEPARTURE. MAINTENANCE CHECKED AIRCRAFT AND ENGINE PNEUMATIC LINES, INSPECTED THE PRESSURIZATION SY
- [SDR 2007FA0000853](https://openairdocs.org/sdr/2007FA0000853.md): Flange · cracked · Sep 20, 2007 · N90XS · Beech E90 · Engine Collector/Tailpipe/Nozzle
  > (2) NEW ENGINES WERE INSTALLED IAW MFG MODIFICATIONS, WITH 938.0 HRS SINCE NEW. AIRCRAFT WAS IN FOR A PHASE INSPECTION AND FOUND 3 OUT OF L1 EXHAUST FLANGES ON THE ENGINE CRACKED. ACCORDING TO THE MFG PARTS MANUAL, EXHAUST STIFFENERS ARE NOT USED ON THIS SN
- [SDR 2007FA0000752](https://openairdocs.org/sdr/2007FA0000752.md): Engine · failed · Jul 25, 2007 · N71WB · Beech E90 · Engine (Turbine/Turboprop)
  > AIRCRAFT IN CRUISE AT 22,000 WITH ALL ENGINE INDICATIONS NORMAL. A LOUD NOISE FOLLOWED BY POWER LOSS AND REDLINE ITT ON THE LT ENGINE. THE CT BLADES, ITT PROBES, PT VANE AND PT BLADES ALL MELTED AND WENT THROUGH THE EXHAUST STACKS. COMPRESSOR STATOR AND SPA
- [SDR CIEA200700003](https://openairdocs.org/sdr/CIEA200700003.md): Cowling · bent · Apr 6, 2007 · N63BV · Beech E90 · Magneto/Distributor
  > DURING TAKEOFF ROLL OF THE AC, AT THE POINT OF LIFTOFF, THE PILOT NOTICED THE LT ENGINE UPPER AFT COWLING HAD COME OPEN. THE TAKEOFF WAS ABORTED AND THE AC CAME TO A SAFE STOP ON THE RUNWAY. THE PILOT SHUTDOWN THE LT ENGINE AND TAXIED BACK TO THE HANGAR ON T
- [SDR LE72008F00000](https://openairdocs.org/sdr/LE72008F00000.md): Relay · failed · Jan 16, 2007 · N10WG · Beech E90 · Landing Gear Retraction/Extension System
  > LANDING GEAR FAILED TO EXTEND, GEAR LOWERED MANUALLY. (K)
- [SDR CA060822006](https://openairdocs.org/sdr/CA060822006.md): Frame · cracked · Aug 22, 2006 · Beech E90 · Fuselage Main, Frame
  > (CAN) LT SIDE OF FUSELAGE, DISCOVERED 4 LOOSE RIVETS AT FS 176.5. MAINTENANCE DEPT REMOVED INTERIOR TO INVESTIGATE DEFECT. IT WAS DISCOVERED THAT FRAME MEMBER P/N 50-420028-57 WAS CRACKED IN SEVEN SPOTS. MAINTENANCE DECIDED TO INVESTIGATE THE RIGHT HAND OF
- [SDR 2006FA0000090](https://openairdocs.org/sdr/2006FA0000090.md): Plate · cracked · Jan 6, 2006 · N200RE · Beech E90 · Landing Gear Brake System
  > DURING A PHASE I AND II INSPECTION A CRACK WAS FOUND IN THIS PART ATTACHED TO THE RT GEAR ASSY. THE CRACK IS ON THE TORQUE PLATE UPPER FORWARD BRAKE CYLINDER PIN ATTACH HOLE. A BUSHING INSTALLED IN THIS HOLE HAS NO SIGN OF DAMAGE. PROBABLE CAUSE OF CRACKING

Next page: https://openairdocs.org/model/beech-e-90/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 = 'E90'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/beech-e-90/reports

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