# Service difficulty reports: Beechcraft B200

A list on [Beechcraft B200](https://openairdocs.org/model/beechcraft-b200.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 17 · 830 reports

- [SDR 55YR202610130001](https://openairdocs.org/sdr/55YR202610130001.md): Strut · damaged · Oct 5, 2026 · N326KW · Beech B200 · Main Landing Gear Strut/Axle/Truck
  > CAME IN FOR PHASE MAINTENANCE, AND THE OPERATOR REQUESTED AN EARLY LANDING GEAR REPLACEMENT. THE LANDING GEAR WAS DUE SOON FOR REPLACEMENT, AND REPRESENTATIVES FROM BERING AIR DECIDED TO HAVE IT CHANGED AHEAD OF SCHEDULE. AFTER INSTALLING NEW MLG ASSEMBLIES
- [SDR O9IA202609140206](https://openairdocs.org/sdr/O9IA202609140206.md): Unknown · smoke · Sep 14, 2026 · N531LM · Beech B200 · Air Distribution System
  > PILOTS NOTED SMOKE IN THE COCKPIT. MEDICAL CREW ONBOARD CONFIRMED SMOKE IN THE CABIN. SMOKE WAS EMITTING FROM THE COPILOTS INSTRUMENT PANEL NEAR THE SIDEWALL. THE CREW ACTIVATED THE O2 MASKS TO DROP AND TURNED OFF THE BLEED AIR AND SMOKE APPEARED TO CLEAR.
- [SDR G1IA20260821116](https://openairdocs.org/sdr/G1IA20260821116.md): Socket · backed out · Aug 21, 2026 · N411WA · Beech B200 · Landing Gear System Wiring
  > SELECTED GEAR DOWN ON FINAL IN PAYA AND GEAR FAILED TO EXTEND. DID NOT LAND, DIVERTED TO PANC. EXTENDED GEAR MANUALLY AT PANC, GOT THREE GREEN AND LANDED.
- [SDR 55YR2026080400919](https://openairdocs.org/sdr/55YR2026080400919.md): Actuator · cracked · Jul 31, 2026 · N949BW · Beech B200 · Landing Gear Actuator
  > ACFT IN FOR A PHASE 1 INSPECTION. GEAR SWINGS REQUIRED FOR PHASE AND MAINT PERFORMED. 10 SWINGS REQUIRED TO BLEED SYS AFTER OPENING LINES. 6 SWINGS WERE PERFORMED WITH MANUAL GEAR PUMP UNTIL THE RESERVOIR WAS SERVICED PROPERLY. TECHNICIANS BEGAN PERFORMING
- [SDR 2026FA0000611](https://openairdocs.org/sdr/2026FA0000611.md): Pin · broken · Jul 30, 2026 · N442P · Beech B200 · Trailing Edge Flap Actuator
  > FLAP DRIVE PIN IN FLAP GEAR BOX WAS BROKEN IN 1/2 WHEN REMOVED FOR 1200 HR LUBRICATION
- [SDR 2026F00162](https://openairdocs.org/sdr/2026F00162.md): Clevis Pin · sheared · Jul 24, 2026 · N239JV · Beech B200 · Passenger/Crew Doors
  > PIN ATTACHING FOWARD DOOR HOOK ON UPPER MAIN DOOR LOCKING MECHANISM SHEARED ALLOWING HOOK TO COME LOOSE ALLOWING ENOUGH MOVEMENT IN THE MAIN CABIN DOOR IN FLIGHT TO CAUSE A SIGNIFICANT PRESSURIZATION LOSS.
- [SDR GRTA20260715002](https://openairdocs.org/sdr/GRTA20260715002.md): Angle · cracked · Jul 1, 2026 · N503AW · Beech B200 · Nacelle/Pylon Miscellaneous Structure
  > LEFT MLG ACTUATOR INBOARD SUPPORT BRACKET CRACKED. REMOVED LEFT MLG ACTUATOR, ASSOCIATED PLUMBING/ELECTRICLA WIRING, AND LEFT MLG DRAG BRACE. REMOVED LH INBOARD AND OUTBOARD SUPPORT BRACKET ANGLES PN 101-120122-15 (INBOARD) AND 101-120122-13 (OUTBOARD) AND RE
- [SDR GRTA20260715001](https://openairdocs.org/sdr/GRTA20260715001.md): Angle · cracked · Jul 1, 2026 · N503AW · Beech B200 · Nacelle/Pylon Miscellaneous Structure
  > RIGHT INBD MLG ACTUATOR SUPPORT BRACKET CRACKED. REMOVED RT MLG ACTUATOR, ASSOCIATED PLUMBING, ELECTRICLA WIRING, AND RT MLG DRAG BRACE. REMOVED RT INBD AND OTBD SUPPORT BRACKET ANGLES (INBD) AND 101-120122-14 (OTBD), REPLACED WITH NEW IAW SRM 20-50-03. RE-I
- [SDR TIMA202604297003](https://openairdocs.org/sdr/TIMA202604297003.md): Indication Sys · faulted · Apr 28, 2026 · N125KS · Beech B200 · Landing Gear Position and Warning
  > RIGHT LANDING GEAR DOWN LIGHT DIDN’T ILLUMINATE, APPROPRIATE CHECKLIST WAS PREFORMED, EMERGENCY GEAR EXTENSION WAS INEFFECTIVE AND THE AIRCRAFT WAS LANDED AS PRESCRIBED IN THE CHECKLIST
- [SDR TIMA2026042900701](https://openairdocs.org/sdr/TIMA2026042900701.md): Landing Gear · faulted · Apr 27, 2026 · N125KS · Beech B200 · Landing Gear Retraction/Extension System
  > ON DECENT WHEN GEAR WAS SELECTED DOWN ONLY THE NOSE AND LEFT GEAR DOWN LIGHTS ILLUMINATED, THE PRESS TO TEST WAS CHECKED AND THE BULB WAS NOT BURNT OUT SO ATC WAS ADVISED AND THE APPROACH WAS BROKEN OFF TO RUN THE APPROPRIATE CHECKLIST. EMERGENCY EXTENSION AS
- [SDR 2026FA0000188](https://openairdocs.org/sdr/2026FA0000188.md): Windshield · cracked · Mar 13, 2026 · N667CC · Beech B200 · Flight Compartment Windows
  > DURING TAKEOFF FROM KBIL TO KHLN, THE CREW OBSERVED THE LEFT WINDSHIELD CRACK. THE CREW RETURNED TO KBIL WITHOUT INCIDENT.
- [SDR 2026F00026](https://openairdocs.org/sdr/2026F00026.md): Door · no discrepancy · Mar 10, 2026 · N680TW · Beech B200 · Wing, Plate/Skin
  > DURING A RETURN FLIGHT FROM KMLK TO KBIL, THE MED CREW NOTICED THAT THE LEFT WING LOCKER HAD OPENED. THE CREW CONTINUED TO KBIL AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND LEFT WING LOCKER DOOR AND FOUND NO DEFECTS.
- [SDR G1IA2026012219103](https://openairdocs.org/sdr/G1IA2026012219103.md): Downlock Switch · failed · Jan 19, 2026 · N68MN · Beech B200 · Landing Gear Retraction/Extension System
  > LANDING GEAR NOSE WHEEL DOWN LIGHT EXTINGUISHED ON SHORT FINAL IN KENAI. WENT MISSED, CYCLED THE GEAR TWICE, GOT THE LIGHT BACK, WHICH THEN EXTINGUISHED ON SHORT FINAL AGAIN. THEN DECLARED AN EMERGENCY, PERFORMED THE ALTERNATE GEAR EXTENSION CHECKLIST VIA QRH,
- [SDR G1IA20250928098](https://openairdocs.org/sdr/G1IA20250928098.md): Check Valve · faulted · Sep 28, 2025 · N6728H · Beech B200 · Fuel Controlling System
  > DURING CRUISE LT FUEL PRESSURE LIGHT ILLUMINATED. LT FUEL FLOW GAUGE ERRATIC. TURNING ON LT STNDBY PUMP HAD NO EFFECT ON FUEL FLOW. LT ENG BEGAN SPOOLING DOWN ON IT'S OWN. SECURED ENG IAW CHKLST. NO EXTERNAL ABNORMALITIES, LEAKS, SMOKE, FUMES, OR FLAMES N
- [SDR 2025FA0000639](https://openairdocs.org/sdr/2025FA0000639.md): Cross Tie · cracked · Sep 11, 2025 · N76PM · Beech B200 · Fuselage Main, Structure
  > DURING PHASE INSPECTION FOUND THE LEFT CROSS TIE AT FUSELAGE STATION 201.775 CRACKED IN HALF. CRACK RUNS HORIZONTAL AND GOES THROUGH A RIVET HOLE. CRACK IS LOCATED AT THE AFT LOWER CORNER OF THE EMERGENCY EXIT FRAME OPENING. DURING FURTHER INSPECTION, FOUND TH
- [SDR ENHA 20250721001](https://openairdocs.org/sdr/ENHA%2020250721001.md): Annunciator · activated · Jul 20, 2025 · N24GN · Beech B200 · Fire Detection
  > LEFT ENGINE FIRE ANNUNCIATOR CAME ON IN FLIGHT. MECHANICS INSPECTED AND TESTED THE SYSTEM IAW THE KING AIR 200 MM SECTIONS 26-10-00 AND 26-10-01. ALL CHECKS WERE SATISFACTORY. NO DEFECTS NOTED AT THIS TIME.
- [SDR JBZA20250714001](https://openairdocs.org/sdr/JBZA20250714001.md): Elec Connector · loose · Jul 9, 2025 · N911RX · Beech B200 · Fire Protection System Wiring
  > DURING FLIGHT LEFT ENGINE FIRE WARNING LIGHT ERRATICALLY FLASHES. ELECTED TO PRECAUTIONARY LAND BACK TO BASE. MAINTENACE DISCOVERED LOOSE FIRE DETECTION AMPLIFIER CONNECTOR BACKSHELL
- [SDR GRTA20250910001](https://openairdocs.org/sdr/GRTA20250910001.md): Stiffener · cracked · Jul 7, 2025 · N503AW · Beech B200 · Fuselage Main, Bulkhead
  > WHILE PERFORMING THE AFT PRESSURE BULKHEAD INSPECTION FOUND A CRACK AT THE # 5 ZEE STIFFENER FROM THE TOP OF THE BULHEAD ON THE FWD SIDE OF THE BULKHEAD THE CRACK STARTS 2.1 INCHES FROM THE OUTBD R/H SIDE AND RUNS HORIZONTALY 21 INCHES JUST UNDER THE RIVET LI
- [SDR O9IA202505270132](https://openairdocs.org/sdr/O9IA202505270132.md): Fire Warning · false activation · May 27, 2025 · N546LM · Beech B200 · Fire Detection
  > DEPARTING PANC. WHILE PASSING THRU FL310 THE LH ENG FIRE LIGHT ILLUMINATED. PILOT DECLARED AN EMERGENCY AND RETURNED TO THE AIRPORT. NO INDICATIONS OUTSIDE OF THE WARNING LIGHT WERE PRESENT REGARDING ANY FIRE. LANDING WAS UNEVENTFUL AND AIRCRAFT RETURNED TO
- [SDR G1IA20250127482](https://openairdocs.org/sdr/G1IA20250127482.md): Switch · failed · Jan 24, 2025 · N351SA · Beech B200 · Landing Gear Retraction/Extension System
  > ONCE WERE ON VISUAL APPROACH IN ANCHORAGE, I SELECTED THE GEAR LEVER DOWN. THE PLANE'S NOSEWHEEL FAILED TO ILLUMINATE GREEN. AFTER VERIFYING THAT IT WASN'T A BULB BURNT OUT, WE PERFORMED A FLYBY, AND TOWER STATED THAT THE GEAR APPEARED TO BE DOWN. WE CYCLED TH
- [SDR 2025FA0000053](https://openairdocs.org/sdr/2025FA0000053.md): Indicator · no indication · Jan 24, 2025 · N351SA · Beech B200 · Landing Gear Position and Warning
  > THE NOSEWHEEL GEAR DOWN INDICATOR LIGHT FAILED TO ILLUMINATE. THE ACTUAL NOSEWHEEL HAD COME DOWN AND LOCKED, BUT WITH NO INDICATION TO THE PILOT OF ITS STATUS, AND EMERGENCY WAS DECLARED. THE PLANE LANDED WITHOUT INCIDENT.
- [SDR ENHA2024F00292](https://openairdocs.org/sdr/ENHA2024F00292.md): Bulkhead · corroded · Nov 19, 2024 · N24GN · Beech B200 · Fuselage Main, Bulkhead
  > DURING INSPECTION, THE AFT PRESSURE BULKHEAD SHOWED CORROSION ON THE AFT SIDE. THE CORROSION WAS BEYOND THE STRUCTURAL REPAIR MANUAL SO ENGINEERING WAS NEED AIN ORDER TO RETURN THE AIRCRAFT TO SERVICE.
- [SDR 2024FA0000823](https://openairdocs.org/sdr/2024FA0000823.md): Windshield · fractured · Nov 5, 2024 · N793DC · Beech B200 · Flight Compartment Windows
  > AIRCRAFT WAS IN CRUISE FLIGHT AT 16,000 FT ENROUTE KBZN FROM KBIL WHEN THE RIGHT (COPILOT) WINDSHIELD SHATTERED. AT THAT TIME, THE FLIGHT CREW RETURNED TO KBIL AND LANDED WITHOUT INCIDENT.
- [SDR O9IA20241015530LM](https://openairdocs.org/sdr/O9IA20241015530LM.md): Pressure Switch · faulted · Oct 14, 2024 · N530LM · Beech B200 · Propeller Feathering/Reversing
  > FROM PILOTS REPORT THRU PRISM SMS: IN CRUISE AT 28,000 FT LEFT HAND ENGINE SEEMED TO WANT TO GO INTO FEATHER. HAPPENED TWO TIMES. DID A PRECAUTIONARY LANDING IN GALENA. SUSPECTED THE LOW PRESSURE SWITCH FOR AUTOFEATHER AFTER DEBREIF WITH THE PILOT. STATE
- [SDR J95A202410230001](https://openairdocs.org/sdr/J95A202410230001.md): Landing Gear · failed · Sep 24, 2024 · N924AC · Beech B200 · Nose/Tail Landing Gear
  > WHEN PILOT CAME IN FOR LANDING, THE LANDING GEAR FAILED TO EXTEND. AFTER PERFORMING THE LANDING GEAR EMERGENCY EXTENTION PROCEDURE, THE NOSE LANDING GEAR FAILED TO EXTEND COMPLETELY. THE PILOT THEN PERFORMED AN EMERGENCY LANDING WITH JUST THE TWO MAIN GEARS EX
- [SDR 2025F00078](https://openairdocs.org/sdr/2025F00078.md): Landing Gear · inoperative · Aug 31, 2024 · N411KC · Beech B200 · Landing Gear Retraction/Extension System
  > REPORTED THAT THE LANDING GEAR WOULD NOT EXTEND WHEN GEAR HANDLE WAS PLACED IN THE DOWN POSITION ON APPROACH TO KPHX ON 8-31-2024 WITH A PATIENT ON BOARD. HE WENT TO A HOLDING AREA, MANUALLY EXTENDED THE GEAR AND DID A LOW PASS SO THE TOWER COULD VERIFY GEAR W
- [SDR 2024F00167](https://openairdocs.org/sdr/2024F00167.md): Fan · shorted · Jul 10, 2024 · N132N · Beech B200 · Air Distribution Fan
  > CABIN ENECTRICAL SMELL WITH SOME SMOKE. UPON INVESTIGATION FOUND FORWARD CABIN DISTRUBTION FAN FAILURE.
- [SDR 2024FA0000463](https://openairdocs.org/sdr/2024FA0000463.md): Hydraulic System · low quantity · Jun 24, 2024 · N954MS · Beech B200 · Hydraulic System, Main
  > CREW RECCIVED A LOW HYDRALIC WARRNING LIGHT ON TAKE OFF AFTER PHASE INSPECTION. CREW ABORTED TAKEOFF TAXIED BACK TO MAINTENANCE. MAINTENANCE SERVICED HYDRALIC SYSTEM WITH LESS THAN 1/2 QT 5606. JACKED AIRCRAFT ACTUATED GEAR CHECKED SERVICING NOTED NO DEFECTS.
- [SDR 2024F00100](https://openairdocs.org/sdr/2024F00100.md): Motor · failed · Mar 21, 2024 · N205EJ · Beech B200 · Trailing Edge Flap Actuator
  > DEPARTED KBIL ENROUTE KMSO. AFTER TAKEOFF THE CREW REPORTED THAT THE FLAPS WOULD NOT RETRACT BEYOND THE APPROACH POSITION. THEY THEN RETURNED TO KBIL WITHOUT INCIDENT. MAINTENANCE REPLACED THE FLAP MOTOR AND THE FLAPS OPS CHECKED GOOD.
- [SDR GRTA20240315004](https://openairdocs.org/sdr/GRTA20240315004.md): Skin · cracked · Mar 14, 2024 · N503AW · Beech B200 · Fuselage Main, Plate/Skin
  > BELLY SKIN CRACKED 3/8"AT APPROX FS 181.0 AT STRINGER 16. REPAIRED IAW KING AIR SIRM 20-10-16.
- [SDR GAYA2024031300002](https://openairdocs.org/sdr/GAYA2024031300002.md): Landing Gear · malfunctioned · Mar 12, 2024 · N299AV · Beech B200 · Landing Gear System
  > PILOT REPORTED ON CLIMB JUST PRIOR TO LEVEL OFF HE SAW AN AMBER RA INOP ON THE PILOT PFD FOLLOWED BY PT TRIM AND AMBER INOP AP RED FAIL. THE RIGHT PFD WENT BLANK FOLLOWED BY THE MFD AND THE THE PILOT PFD. (AIRCRAFT IS EQUIPPED WITH A GARMIN G1000). TURNED ALL
- [SDR 2024F00053](https://openairdocs.org/sdr/2024F00053.md): Hose · deteriorated · Mar 7, 2024 · N667CC · Beech B200 · Navigation System
  > WHILE TAXIING OUT AT 0630 IN KBIL ENROUTE KMLS, PILOT REPORTED THAT LEFT AIRSPEED INDICATOR NEVER ROSE ABOVE 0. AVIONICS TROUBLESHOT AND FOUND A ROTTED HOSE TO LEFT PITOT PROBE. REPLACED HOSE AND PRESSURE LEAK CHECK OK.
- [SDR GRTA20240315003](https://openairdocs.org/sdr/GRTA20240315003.md): Frame · cracked · Mar 6, 2024 · Beech B200 · Fuselage Main, Frame
  > FRAME CRACKED CENTER LINE ABOVE BELLY SKIN @ APPROXIMATE F.S. 167.625. REPAIRED IAW SIRM 20-10-34.
- [SDR GRTA20240315002](https://openairdocs.org/sdr/GRTA20240315002.md): Frame · cracked · Mar 6, 2024 · Beech B200 · Fuselage Main, Frame
  > FRAME CRACKED AT FS 236.5 BETWEEN STRINGERS 12L AND 13L. REPAIRED IAW KING AIR SIRM 20-10-34.
- [SDR GRTA20240315001](https://openairdocs.org/sdr/GRTA20240315001.md): Skin · cracked · Mar 6, 2024 · N503AW · Beech B200 · Fuselage Main, Plate/Skin
  > BELLY SKIN CRACKED APPROX 3 1/2" ON FRAME AT FS 167.625 BETWEEN STRINGERS 15L AND 16. C/W SKIN DAMAGE REPAIR (PRESSURIZED AREA) COVER PATCH METHOD AND SHIM INSTALLATION IRW BEECHCRAFT SIRM 98-39006, REV D5, 20-10-16, 2. A-D & 20-10-10, 1-4, A.C. FABRICATED
- [SDR GRTA20240221001](https://openairdocs.org/sdr/GRTA20240221001.md): Door Seal · damaged · Feb 20, 2024 · N505AW · Beech B200 · Passenger/Crew Doors
  > AFTER TAKE OFF FROM LAS VEGAS, NM, WE HAD A RAPID DECOMPRESSION AT FL260 WITH AIRFLOW HEARD AT THE CABIN DOOR FOLLOWED BY CABIN ALT HI ANNUNCIATOR AND MASTER WARNING. WE DONNED OUR O2 MASKS AND DESCENDED TO 15K' AND DIVERTED TO ABQ. MAINTENANCE FOUND PASSEN
- [SDR G1IA20240215258](https://openairdocs.org/sdr/G1IA20240215258.md): Circuit Breaker · tripped · Feb 12, 2024 · N858GF · Beech B200 · Landing Gear System Wiring
  > LANDING GEAR CIRCUIT BREAKER ACTIVATED ON APPROACH, GEAR WAS PUMPED DOWN MANUALLY.
- [SDR G1IA202402095055](https://openairdocs.org/sdr/G1IA202402095055.md): Downlock Switch · inoperative · Feb 5, 2024 · N607FJ · Beech B200 · Landing Gear Position and Warning
  > NOSE GEAR DOWN AND LOCKED GREEN INDICATOR LIGHT DID NOT ILLUMINATE.
- [SDR 2024F00005](https://openairdocs.org/sdr/2024F00005.md): Pitot System · false indication · Jan 8, 2024 · N205EJ · Beech B200 · Pitot/Static System
  > AFTER DEPARTING KBIL FOR KGGW THE CREW OBSERVED LOSS OF PRIMARY AIRSPEED INDICATION SO THEY RETURNED TO KBIL WITHOUT INCIDENT.
- [SDR 2023FA0000851](https://openairdocs.org/sdr/2023FA0000851.md): Unknown · unknown · Dec 11, 2023 · N530LM · Beech B200 · Aircraft Fuel Distribution System
  > LH FUEL QUANTITY DROPPED DURING CLIMB FROM FAI. PILOT NOTICED A MIST COMING FROM THE COWLING AND RETURNED TO BASE. MAINTENANCE MET THE AIRCRAFT AND NOTICED FUEL LEAKING FROM THE FUEL BOWL STRAINER. UPON FURTHER INVESTIGATION, IT WAS NOTED THAT THE FUEL STRAI
- [SDR ENHA202311160001](https://openairdocs.org/sdr/ENHA202311160001.md): Unknown · unknown · Nov 16, 2023 · N24GN · Beech B200 · Fuselage Structure (General)
  > DURING SCHEDULED INSPECTION IT WAS NOTED THAT FORWARD DOOR FRAME AT STATION 273.520 BUCKLED, CROSS TIE AT STATION 246.750 ON LEFT SIDE BUCKLED, CROSS TIE AT STATION 227.00 ON LEFT SIDE BUCKLED, CROSS TIE AT STATION 246.750 ON RIGHT SIDE BUCKLED, CROSS
- [SDR 2023FA0000739](https://openairdocs.org/sdr/2023FA0000739.md): Wire · corroded · Nov 3, 2023 · N24 · Beech B200 · Electrical Power System Wiring
  > SHORTLY AFTER DEPARTURE THE CAPTAIN NOTICED THE COCKPIT LIGHTING OSCILLATING BETWEEN NORMAL AND SLIGHTLY DIMMER. THE CAPTAIN TURNED THE STROBES OFF AND THEN BACK ON TO SEE IF THIS WAS THE SOURCE. NOTHING CHANGED. HE THEN TURNED THE ROTATING BEACON OFF IN WHICH
- [SDR 2023F00320](https://openairdocs.org/sdr/2023F00320.md): Hydraulic Line · ruptured · Oct 31, 2023 · N793DC · Beech B200 · Hydraulic System, Main
  > WHILE ON APPROACH INTO BFI FROM BIL, THE LANDING GEAR EXTENDED UN-COMMANDED, THE LANDING GEAR HANDLE LIGHT (IN-TRANSIT LIGHT) ILLUMINATED, THE "HYD LOW" ANNUNCIATOR LIGHT ILLUMINATED AND THE LANDING GEAR CIRCUIT BREAKER POPPED. THE THREE GREEN "GEAR DOWN AND L
- [SDR 2023FA0000536](https://openairdocs.org/sdr/2023FA0000536.md): Unknown · unknown · Sep 12, 2023 · N898BR · Beech B200 · Auto Flight System
  > ON DEPARTURE IN CLIMB MASTER WARNING (ILLUMINATED) AND A/P DISENGAGED. RESET ELEVATOR TRIM AND WHEN ENGAGED YAW (DAMPENER) THE PLANE WENT INTO A DIVE TO THE LEFT. DISENGAGED AND CHANGED (AC) INVERTER, HIT YAW DAMPENER AND AGAIN DIVE TO THE LEFT. AIRCRAFT WAS H
- [SDR GRTA20230809001](https://openairdocs.org/sdr/GRTA20230809001.md): Aileron · cut · Aug 4, 2023 · N505AW · Beech B200 · Ailerons
  > LH AILERON TIP CAP DAMAGE DUE TO COLLISION WITH HANGAR DOOR FRAME. REPAIRED LEFT HAND AILERON, P/N 101-130001-325 S/N BB1755, TIP DAMAGE BY REPLACING TIP PN 101-130001-211 IAW KING AIR SERIES STRUCTURAL INSPECTION AND REPAIR MANUAL (SIRM) 20-50-03. PAINTED N
- [SDR E5WR202305180001](https://openairdocs.org/sdr/E5WR202305180001.md): Wheel · cracked · May 18, 2023 · N300AJ · Beech B200 · Wheel/Ski/Float
  > USING EDDY CURRENT TESTING, A FLAW WAS FOUND ON THE WHEEL HALF IN THE BEAD AREA. INSPECTION WAS PERFORMED IAW MM 32-45-23.
- [SDR G1IA20230420044](https://openairdocs.org/sdr/G1IA20230420044.md): Lug · broken · Apr 20, 2023 · N351SA · Beech B200 · Doors
  > AIRCRAFT DEPRESSURIZED AT 23,000 FEET. WOULD NOT PRESSURIZE AFTER THAT. MADE A "PAN PAN" CALL TO ATC AS I PERFORMED AN EMERGENCY DECENT AND DONNING MY OXYGEN MASK. AIRFRAME FWD UPPER LUG WELD ASSEMBLY BROKEN.
- [SDR GRTA20230506002](https://openairdocs.org/sdr/GRTA20230506002.md): Frame · cracked · Apr 18, 2023 · N503AW · Beech B200 · Fuselage Main, Frame
  > FRAME CRACKED AT FS 256.250 AND STRINGER 13L, PN 50-420068-31. REPAIRED CRACKED FRAME AT FS 256.250 AND STRINGER 13L USING 2024-T3, 0.063" ALCLAD IAW SIRM 20-10-34.
- [SDR GRTA20230506001](https://openairdocs.org/sdr/GRTA20230506001.md): Unknown · unknown · Apr 18, 2023 · N503AW · Beech B200 · Fuselage Main, Frame
  > FRAME CRACKED AT LIGHTNING HOLE AT FS 187.383 JUST ABOVE STRINGER 10R. REPAIRED CRACK FS 187.383 ABOVE STRINGER 10R USING 0.071", 2024-T3 ALCLAD IAW SIRM 20-10-31.
- [SDR GRTA20230420001](https://openairdocs.org/sdr/GRTA20230420001.md): Unknown · unknown · Apr 11, 2023 · N505AW · Beech B200 · Fuselage Main, Structure
  > IMPACT DAMAGE NOTED ON RH SIDE FUSELAGE, BELOW AND AFT RH AVIONICS DOOR (PROP ARC). REPAIRED IMPACT DAMAGE TO PRESSURE VESSEL AT FS 94.0, WL 84.0 RH SIDE, AFT OF AVIONICS DOOR IAW BEECHCRAFT SERIES SIRM 20-10-16.

Next page: https://openairdocs.org/model/beechcraft-b200/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 = 'B200'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/beechcraft-b200/reports

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