# Service difficulty reports: Raytheon BAE 125-800A

A list on [Raytheon BAE 125-800A](https://openairdocs.org/model/raytheon-bae-125-800a.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 6 · 282 reports

- [SDR 2023FA0000353](https://openairdocs.org/sdr/2023FA0000353.md): Outflow Valve · jammed · Apr 27, 2023 · N800RG · Braero BAE125800A · Air Conditioning System
  > AIRCRAFT LOST PRESSURIZATION AT FL039, PERFORMED AN EMERGENCY DECENT AND LANDED BACK TO PBI WITHOUT INCIDENT.
- [SDR 2023FA0000352](https://openairdocs.org/sdr/2023FA0000352.md): Air Duct · detached · Apr 24, 2023 · N800RG · Braero BAE125800A · Air Conditioning System
  > AIRCRAFT LOST PRESSURIZATION AT FL015 AND RETURNED TO PBI. AFTER LANDING IT WAS DISCOVERED THAT AN AIR-CONDITIONING DUCT HAD SEPARATED FROM THE REAR PRESSURE BULKHEAD FITTING.
- [SDR 2022FA0000279](https://openairdocs.org/sdr/2022FA0000279.md): None · none · Jun 2, 2022 · N850SX · Braero BAE125800A · Cabin Pressure Indicator
  > DURING CLIMB PASSING FL 355 THE "CABIN ALTITUDE" LIGHT CAME ON WITH DIFFERENTIAL PRESSURE INDICATOR SHOWING ZERO. CABIN DID NOT LOSE PRESSURIZATION; HOWEVER THE CREW FOLLOWED THE CHECKLIST DECLARED EMERGENCY, DESCENDED TO LOWER ALTITUDE AND RETURNED TO THE DEP
- [SDR A8JA202103120035](https://openairdocs.org/sdr/A8JA202103120035.md): Circuit Breaker · faulted · Mar 12, 2021 · N777VW · Braero BAE125800A · Landing Gear Position and Warning
  > DURING APPROACH FROM KFXE TO KHOU AT APPROXIMATELY 1930 HRS LOCAL, FLIGHT CREW OBSERVED NO LANDING GEAR DOWN AND LOCKED INDICATION. CREW ELECTED TO ABORT LANDING AND CONTINUE FLIGHT TO COMPLETE ABNORMAL CHECKLIST, AND COMMUNICATED THIS TO KHOU TOWER. CREW CO
- [SDR JGVR20181102001](https://openairdocs.org/sdr/JGVR20181102001.md): Terminal · burned · Nov 2, 2018 · N549MF · Braero BAE125800A · Ice/Rain Protection System Wiring
  > INVESTIGATED SMOKE IN THE COCKPIT BEHIND THE CO-PILOT INSTRUMENT PANEL. FOUND THE -A- SCREEN ELECTROSTATIC FILTER WIRE TERMINALS BURNED ON SUPPLY SIDE. REMOVED AND REPLACED THE FILTER ASSEMBLY, REPLACED THE WIRING WITH NEW RING TERMINALS. RANG OUT WIRING T
- [SDR 4TDA2018091300001](https://openairdocs.org/sdr/4TDA2018091300001.md): Accumulator · low pressure · Sep 12, 2018 · N805JL · Braero BAE125800A · Landing Gear Brake System
  > AS AIRCRAFT WAS RELEASED FOR FLIGHT, THE PILOT RELEASED THE PARKING BRAKE, ACTIVATED THE REGULAR BRAKE SYSTEM AND NOTICED THE PRESSURES ROSE TO 1,000 PSI AND FELL OFF TO NEAR ZERO. AFTER SEVERAL ATTEMPTS TO CHECK THE SYSTEM THE PILOT CONTACTED MAINTENANCE CONT
- [SDR E0YA2018062900087](https://openairdocs.org/sdr/E0YA2018062900087.md): Starter Gen · failed · Jun 28, 2018 · N260H · Braero BAE125800A · Starter-Generator
  > DURING CRUISE THE NR 2 ENGINE STARTER/GENERATOR FAILED AND CAUSED VIBRATION.
- [SDR 4TDA201805293805](https://openairdocs.org/sdr/4TDA201805293805.md): Controller · malfunctioned · May 23, 2018 · N805JL · Braero BAE125800A · Cabin Pressure Controller
  > AT FL 400, THE CAPTAIN NOTICED AN INCREASE IN CABIN CLIMB RATE AND DECREASE IN CABIN PRESSURE. CREW DONNED OXYGEN MASKS AND MADE A DESCENT TO FL100. FLIGHT CONTINUED UNEVENTFUL, PRESSURIZATION WAS CONTROLLABLE AT THIS POINT.
- [SDR 2018FA0000149](https://openairdocs.org/sdr/2018FA0000149.md): Wire · pinched · Apr 22, 2018 · N976SC · Braero BAE125800A · Electrical Power System Wiring
  > WANDER LIGHT BEHIND CAPTAIN`S CHAIR, WIRING FOUND PINCHED AND ARCED. CREW REPORTED A SMALL FLAME FOR A MOMENT UNTIL THE CIRCUIT BREAKER. NOTHING FURTHER WAS REPORTED.
- [SDR 6EMY20171105856](https://openairdocs.org/sdr/6EMY20171105856.md): Not Reported · fire · Nov 2, 2017 · N180EG · Braero BAE125800A · Accessory Compartment
  > AN EMPLOYEE OBSERVED BLACK SMOKE EMERGING FROM THE UPPER FUSELAGE REAR EQUIPMENT BAY ACCESS PANELS OF THE SUBJECT AIRCRAFT. POWER WAS IMMEDIATELY TURNED OFF AND ALL PERSONNEL REMOVED FROM THE AIRCRAFT. ON INSPECTION OF THE REAR EQUIPMENT BAY SMALL NAKED FLAMES
- [SDR PAIR20160916S3570](https://openairdocs.org/sdr/PAIR20160916S3570.md): Air Duct · broken · Sep 14, 2016 · N326N · Braero BAE125800A · Cabin Cooling System
  > CLIMBING THROUGH 23,000 FT, AIRCRAFT EXPERIENCED REAR BAY OVERHEAT WARNING FOLLOWED BY CABIN ALTITUDE STARTING TO CLIMB. ACFT RETURNED TO POINT OF DEPARTURE. MAINTENANCE INSPECTOR FOUND ACM INLET DUCT BROKEN, ACM OUTLET CLAMP BROKEN, AND ACM TURBINE BLADES A
- [SDR ZP7A2016F00039](https://openairdocs.org/sdr/ZP7A2016F00039.md): Fuel Control · defective · Dec 1, 2015 · N798PA · Braero BAE125800A · Fuel Control/Turbine Engines
  > AT FL400, ENGINE NR 2 BEGAN LOOSING POWER, N1 REDUCED TO BELOW 60 PERCENT, DESCENDED TO 14,000 FT N1 REDUCED TO BELOW 40 PERCENT. AT BELOW 8000 FT MSL ENGINE POWER BECAME FULLY RESPONSIVE.
- [SDR 9PVA2015F00111](https://openairdocs.org/sdr/9PVA2015F00111.md): Seal · shifted · Sep 9, 2015 · N463DD · Braero BAE125800A · Doors
  > CABIN ALTITUDE TOD CABIN ALTITUDE INCREASED VIELENTY AT 200 FT + IAE MINUTE ALL THE WAY TO 20,000 FT. PAX O2 MASK PARTIALLY DEPLOYED. DOOR SEAL SHIFTED.
- [SDR 2015F00105](https://openairdocs.org/sdr/2015F00105.md): Bolt · corroded · Sep 2, 2015 · Braero BAE125800A · Elevator Miscellaneous Structure
  > REMOVED AND INSPECTED MASS BALANCE WEIGHTS, AND SPIGOTS. THE BOLT HAD EXCESSIVE CORROSION AND HAD TO BE REPLACED. WEIGHTS WERE CLEANED AND REUSED. BROKEN BOLT COULD LEAD TO JAMMING AND LOSS OF ELEVATOR CONTROL.
- [SDR 9PVA2015F00110](https://openairdocs.org/sdr/9PVA2015F00110.md): Irs · misaligned · Aug 28, 2015 · N463DD · Braero BAE125800A · Directional Gyro and Indicating System
  > HAD TO RETURN TO THE AIRPORT BECAUSE THERE WAS 30 TO 90 DEGREES HEADING DIFFERENCE DUE TO A MISS ALIGNMENT OF THE IRS SYSTEM.
- [SDR JLTA20150824001](https://openairdocs.org/sdr/JLTA20150824001.md): Engine · malfunctioned · Aug 21, 2015 · N118GA · Braero BAE125800A · Engine (Turbine/Turboprop)
  > ON FRIDAY, AUGUST 21ST AT APPROX 1900Z, ACFT DEPARTED EMPTY & ENTERED CRUISE, EVERYTHING WAS NORMAL. ON THE INITIAL DESCENT CREW HEARD A STRANGE NOISE & OBSERVED AN ENG COMPUTER LIGHT FOR THE NR 2 ENG. ALL OF THE INSTRUMENTS FOR THE NR 2 ENG THEN FLUCTUATED
- [SDR DIXA2015F00097](https://openairdocs.org/sdr/DIXA2015F00097.md): Overheat Sensor · intermittent · Aug 19, 2015 · N904JR · Braero BAE125800A · Overheat Detection
  > CREW REPORTED CLIMBING THROUGH FL 150, RED REAR BAY OVERHEAT LIGHT ILLUMINATED, CREW FOLLOWED CHECKLIST PROCEDURES. LIGHT EXTINGUISHED WHILE STILL CLIMBING THROUGH FL 180 RED REAR BAY OVER HEAT LIGHT ILLUMINATED FOLLOWED BY A BURNING ODOR AND LIGHT SMOKE IN C
- [SDR T6FA2015072903](https://openairdocs.org/sdr/T6FA2015072903.md): Intercostal · cracked · Jul 29, 2015 · N816BG · Braero BAE125800A · Fuselage Miscellaneous Structure
  > FOUND CRACKED DENT IN FUSELAGE RT SIDE INTERCOSTAL UNDER LAVATORY FLOOR BETWEEN FRAME 16 TO FRAME 17. REPAIRED IAW FIELD REPAIR.
- [SDR T6FA2015072902](https://openairdocs.org/sdr/T6FA2015072902.md): Skin · corroded · Jul 29, 2015 · N816BG · Braero BAE125800A · Fuselage Main, Plate/Skin
  > CORROSION FOUND ON FUSELAGE KEEL SKIN & DOUBLER BETWEEN FRAMES 12 & 12A. REPAIRED IAW FIELD REPAIR INSTRUCTIONS.
- [SDR T6FA2015072901](https://openairdocs.org/sdr/T6FA2015072901.md): Skin · corroded · Jul 29, 2015 · N816BG · Braero BAE125800A · Aerodynamic Fairings
  > CORROSION FOUND ON LT SIDE MLG LEG FAIRING OUTER SKIN. REPAIRED IAW FIELD REPAIR.
- [SDR CA150525014](https://openairdocs.org/sdr/CA150525014.md): B-Nut · cracked · May 24, 2015 · Braero BAE125800A · Oxygen System
  > (CAN) DURING THE REPLACEMENT OF THE OXYGEN SYS CHARGING VLV WHICH WAS SUSPECTED OF A LEAK, IT WAS NOTICED THAT THE B NUT WHICH CONNECTS TO THE FILTER & IS PART OF THE MANIFOLD WAS CRACKED.
- [SDR CA150113022](https://openairdocs.org/sdr/CA150113022.md): Tube · leaking · Jan 2, 2015 · Braero BAE125800A · Turbine Engine Oil System
  > (CAN) POST ARRIVAL, FLIGHT CREW CONDUCTED POST FLIGHT INSPECTION OF ACFT AND NOTED SIGNIFICANT OIL LEAKAGE ON LT ENGINE COWLINGS, NO INFLIGHT INDICATIONS WERE EVIDENT TO FLIGHT CREW DURING APPROXIMATE 4.5 HR FLIGHT. OIL LEVEL COULD NOT BE SEEN THROUGH OIL TANK
- [SDR 9JLA2014122607198](https://openairdocs.org/sdr/9JLA2014122607198.md): Position Switch · shorted · Dec 12, 2014 · N304HE · Braero BAE125800A · Trailing Flap Position Indicating System
  > DURING TAXI THE SSU STALL IDENT LIGHT ILLUMINATED & THE NR 1 STALL CHANNEL DOES NOT TEST. EXTENSIVE TROUBLESHOOTING FOUND THE LT INBD FLAP POSITION MICRO SWITCH GNDED OUT INTERNALLY. THE DEFECTIVE SWITCH WAS REMOVED & A NEW SWITCH INSTALLED PN 9002EN3.
- [SDR 9JLA2014122607197](https://openairdocs.org/sdr/9JLA2014122607197.md): Ahrs · intermittent · Dec 10, 2014 · N304HE · Braero BAE125800A · Integrated Flight System
  > NUMBER 2 AHRS UNIT INTERMITTENTLY ROLLS COPILOTS ATTITUDE INDICATOR CREATING A COMPARATOR MONITOR DISAGREE. THE DEFECTIVE UNIT WAS REMOVED PN7003360-943 SN 95083260 & AN OVERHAULED UNIT WAS INSTALLED.
- [SDR 2014FA0000506](https://openairdocs.org/sdr/2014FA0000506.md): Indication Sys · failed · Aug 26, 2014 · N82SR · Braero BAE125800A · Landing Gear Position and Warning
  > FAILURE OF RT MLG INDICATION WHEN GEAR SELECTED DOWN FOR LANDING.
- [SDR FVJA2014082600148](https://openairdocs.org/sdr/FVJA2014082600148.md): Cooling Turbine · failed · Aug 22, 2014 · N70NE · Braero BAE125800A · Cabin Cooling System
  > DURING THE CLIMB, CREW REPORTED LOUD SQUEAL FOLLOWED BY ODOR OF BURNED OIL AND REPORT OF SMOKE COMING FROM AIR VENTS. THE ACM, COOLING TURBINE FOUND TO HAVE FERROUS MATERIAL ON THE MAGNETIC DRAIN PLUG, COOLING TURBINE WAS DISCOVERED TO BE FAILED, INTERNAL BEA
- [SDR 9JLA201405217509](https://openairdocs.org/sdr/9JLA201405217509.md): Switch · stuck · May 9, 2014 · N800FL · Braero BAE125800A · Landing Gear Position and Warning
  > THE CREW REPORTED THAT AFTER TAKEOFF & GEAR RETRACTION AN UNSAFE GEAR INDICATION, 3 RED LIGHTS & 1 MAIN GEAR GREEN LIGHT. THE CREW CYCLED THE GEAR BACK DOWN & RETURNED BACK TO THE AIRPORT FOR MAINTENANCE. TROUBLESHOOTING FOUND THE RT NORMAL LG MICRO SWITCH C
- [SDR CA140407014](https://openairdocs.org/sdr/CA140407014.md): Wire Harness · chafed · Apr 2, 2014 · Braero BAE125800A · Landing Gear System Wiring
  > (CAN) FLIGHT CREW REPORTED LANDING GEAR SELECTOR WOULD NOT MOVE AFTER TAKEOFF. CHECKLIST CARRIED OUT AND FLIGHT CREW DECIDED TO RETURN TO AIRPORT AFTER CIRCLING SUFFICIENT TIME TO LOWER FUEL WEIGHT TO OBTAIN PROPER LANDING WEIGHT. ACFT LANDED WITHOUT INCIDENT
- [SDR CA140303002](https://openairdocs.org/sdr/CA140303002.md): Switch · failed · Feb 27, 2014 · Braero BAE125800A · Drag Control System
  > (CAN) FLIGHT CREW REPORTED AIRBRAKE SPOILER CIRCUIT BREAKER WAS FOUND TRIPPED AFTER SHUTDOWN. THE CIRCUIT BREAKER WAS RESET AND DID NOT OPEN AGAIN. DURING MAINTENANCE DAILY INSPECTION, THE CIRCUIT BREAKER WAS AGAIN FOUND TRIPPED. IT WAS RESET AND WITHIN A F
- [SDR BN5A20142190001](https://openairdocs.org/sdr/BN5A20142190001.md): Seal · weak · Feb 17, 2014 · N250MB · Braero BAE125800A · Pneumatic Distribution System
  > CREW REPORTED REAR BAY OVERHEAT AT FL 250. TROUBLESHOOTING FOUND BLEED AIR LEAK AT LT BLEED AIR VLV & LT NON-RETURN VLV. REMOVED LT BLEED AIR SOV & LT NON-RETURN VLV. REPLACE DEFECTIVE SEALS WITH NEW PN 20496-200A, 6-464-1PAR & HTE580-3060-112A & REINSTALLE
- [SDR BJYA 20130717001](https://openairdocs.org/sdr/BJYA%2020130717001.md): Warning Light · illuminated · Jul 15, 2013 · N337RE · Braero BAE125800A · Cabin Pressure Control System
  > CABIN HIGH ALTITUDE LIGHT ILLUMINATE AFTER REACHING FL 370. ON LEVEL OFF DURING ACCELERATION, CABIN HIGH ALTITUDE LIGHT ILLUMINATED. DONNED OXYGEN MASKS, DEPLOYED PAX MASKS AND COMPLETED CHECKLIST ITEMS. REFERRED TO CHECKLIST, ELECTED TO DECEND. PERFORME
- [SDR 2013FA0000351](https://openairdocs.org/sdr/2013FA0000351.md): Relay · blown · Jun 13, 2013 · N816BG · Braero BAE125800A · Windshield/Door Rain/Ice Removal
  > RIGHT WINDSHIELD HEAT WAS FOUND INOPERATIVE ALONG WITH TAXI LIGHTS. INVESTIGATION FOUND THAT RELAY FOR RT WINDHSHIELD DEICE HAD BLOWN THE GUTS OUT OF THE RELAY AND ACROSS TO THE CIRCUIT BREAKERS AND IT BUSTED THE POWER TAB OFF OF THE TAXI LIGHT CIRCUIT BREAKE
- [SDR WTXR2013060329204](https://openairdocs.org/sdr/WTXR2013060329204.md): Line · chafed · Jun 3, 2013 · N800FL · Braero BAE125800A · Cabin Pressure Control System
  > THE VENTURI VACUUM LINE, FROM THE PRESSURIZATION CONTROLLER TO THE CABIN AIR OPERATED VENTURI IS BEING RUBBED THROUGH BY THE AILERON CONTROL CABLE THAT SITS DIRECTLY ABOVE IT. THE LINE SHOULD HAVE A BEND THAT GIVES IT GREATER CLEARANCE FROM THE FLIGHT CONTRO
- [SDR VIBR20131202001](https://openairdocs.org/sdr/VIBR20131202001.md): Stud · unsecure · May 25, 2013 · N24JG · Braero BAE125800A · Electrical Power System Wiring
  > ENGINE STARTER GENERATOR "B" STUD NOT SECURE IN STARTER GENERATOR TERMINAL BLOCK.
- [SDR JLTA20130520001](https://openairdocs.org/sdr/JLTA20130520001.md): Bolt · corroded · May 15, 2013 · N855GA · Braero BAE125800A · Spoilers
  > DURING A POSTFLIGHT INSPECTION, DISCOVERED THE RT AIRBRAKE OTBD COVERS WERE NOT ALIGNED. FOUND BOLTS IN BRACKET WERE LOOSE. SAFETY WIRE WAS STILL INTACT. SAFETY WIRE REMOVED AND AN ATTEMPT WAS MADE TO TORQUE THE BOLTS, NO JOY. BOLTS REMOVED AND FOUND SEVER
- [SDR V0JA20130506001](https://openairdocs.org/sdr/V0JA20130506001.md): Filter · malfunctioned · Apr 30, 2013 · N1776H · Braero BAE125800A · Windshield/Door Rain/Ice Removal
  > PILOTS SIDE WINDSHIELD HEAT ELECTROSTATIC FILTER PRODUCED SMOKE DURING OPERATION AND OPENED CIRCUIT BREAKER.
- [SDR KKYA20121031001](https://openairdocs.org/sdr/KKYA20121031001.md): Filter · unknown · Oct 21, 2012 · N852A · Braero BAE125800A · Engine Fuel Distribution
  > AFTER DEPARTURE NR 1 ENGINE FUEL LIGHT CAME ON. REDUCED NR 1 THROTTLE TO IDLE - LIGHT REMAINED ON. REPLACED THE ENGINE FUEL FILTER WITH NEW PER HONEYWELL TFE731-5R LMM CH 73-21-02. PERFORMED SATISFACTORY GOUND OPERATIONAL CHECKS WITH NO DEFECTS NOTED.
- [SDR KKYA20120924001](https://openairdocs.org/sdr/KKYA20120924001.md): Pitot System · obstructed · Sep 21, 2012 · N852A · Braero BAE125800A · Pitot/Static System
  > COMPUTER MONITOR NR 1 AND NR 2 AIRSPEEDS PLUS ALTITUDE DISCREPANCIES. FOUND DEBRIS IN BOTH PITOT SYSTEMS AND ADC NR 1 SYSTEM WAS PLUGGED.
- [SDR 9JLA2012073106330](https://openairdocs.org/sdr/9JLA2012073106330.md): Computer · defective · Jul 25, 2012 · N800FL · Braero BAE125800A · Fuel Controlling System
  > CREW REPORTED THE LT ENGINE DEEC LIGHT COMES ON STEADY IN FLIGHT. THE ENGINE COMPUTER WAS REMOVED. A NEW COMPUTER WAS INSTALLED. FUNCTIONAL CHECKS WERE SATISFACTORY.
- [SDR 2012FA0000490](https://openairdocs.org/sdr/2012FA0000490.md): Autopilot Sys · malfunctioned · Jul 18, 2012 · N2033 · Braero BAE125800A · Auto Flight System
  > AT 24000 FT, INBOUND TO DESTINATION, AUTOPILOT WARNING HORN SOUNDED CONTINUOUSLY AND ALL AUTOPILOT WARNING LIGHTS WERE ON AND AUTOPILOT ENGAGE LIGHTS WERE ON WITH AUTOPILOT OFF. DETECTED A BURNED WIRE ODOR THAT PROGRESSIVELY INCREASED, DECIDED TO LAND. PULLE
- [SDR 2012F00067](https://openairdocs.org/sdr/2012F00067.md): Transducer · inoperative · Mar 29, 2012 · N801RM · Braero BAE125800A · Engine RPM Indicating System
  > ON THE LAST LEG OF THE TRIP, ON START UP, THE RT ENGINE COMPUTER INOPERATIVE LIGHT ILLUMINATED. FOUND BAD N2 TRANSDUCER. REPLACED THE TRANSDUCER, OPS CHECKED GOOD.
- [SDR L7OA201203270127](https://openairdocs.org/sdr/L7OA201203270127.md): Valve · malfunctioned · Mar 21, 2012 · N359CF · Braero BAE125800A · Fuel Storage
  > ON CLIMBOUT FROM SJU, IT WAS NOTICED THAT FUEL WAS COMING FROM THE LEFT WING VENT AREA. THE AIRCRAFT RETURNED TO SJU WITHOUT INCIDENT.
- [SDR L7OA2012F00066](https://openairdocs.org/sdr/L7OA2012F00066.md): Fuel Sys · leaking · Mar 21, 2012 · N359CF · Braero BAE125800A · Aircraft Fuel Distribution System
  > ON CLIMB OUT, NOTICED FUEL COMING FROM THE LT WING VENT AREA. ACFT RETURNED TO DEPARTURE WITHOUT INCIDENT.
- [SDR E81R2011122632222](https://openairdocs.org/sdr/E81R2011122632222.md): Pump · low pressure · Dec 26, 2011 · N800FL · Braero BAE125800A · Hydraulic Pump (Electric/Engine), Main
  > INVESTIGATED REPORTED "HYD 2 LO PRESS" ANNUNCIATOR LIGHT INDICATION. REPLACED FAILED NR 2 ENGINE HYD PUMP WITH AN O/H PUMP AND DRAINED HYD SYS RESERVOIR, REPLACED SYS SUCTION FILTER. HYDR SYS OPS NORMAL AFTER PUMP REPLACEMENT. HYD PUMP TSN/TSOH UNKNOWN, TRANS
- [SDR BLUA2012F00025](https://openairdocs.org/sdr/BLUA2012F00025.md): Monopole · failed · May 16, 2011 · N801RM · Braero BAE125800A · Engine Indicating System
  > NR 2 ENGINE COMPUTER LIGHT ILLUMINATED IN FLIGHT. FOUND MONOPOLE FAILED.
- [SDR UVCA20110418001](https://openairdocs.org/sdr/UVCA20110418001.md): Starter Gen · malfunctioned · Apr 18, 2011 · N705BB · Braero BAE125800A · Starter-Generator
  > RT STARTER GENEREATOR WOULD NOT START.
- [SDR CA110209027](https://openairdocs.org/sdr/CA110209027.md): B-Nut · cracked · Feb 9, 2011 · Braero BAE125800A · Hydraulic System, Main
  > (CAN) DURING INSPECTION A CRACK IN THE B-NUT ATTACHED TO THE SEQUENCE VALVE IN THE LT LANDING GEAR WELL AS NOTED. THE CRACK WAS RUNNING PERPENDICULAR TO THE THREADS OF THE NUT. THERE WERE NO PREVIOUS REPORTS OF HYDRAULIC FLUID LEAKAGE.
- [SDR CA110209031](https://openairdocs.org/sdr/CA110209031.md): Frame · cracked · Feb 9, 2011 · Braero BAE125800A · Fuselage Main, Frame
  > (CAN) DURING 24 YEAR INSP, A CRACK IN THE TOP CTR MEMBER OF THE LOWER PRESSING WAS FOUND.
- [SDR CA110209028](https://openairdocs.org/sdr/CA110209028.md): Nut · cracked · Feb 9, 2011 · Braero BAE125800A · Aircraft Fuel Distribution System
  > DURING REMOVAL OF THE VENTRAL FUEL TANK, THE ABOVE MENTIONED NUT WAS FOUND TO BE SEIZED IN PLACE. 2 CRACKS WERE NOTED ON THE OUTER SURFACE OF THE NUT: 1 PERPENDICULAR TO THE DIRECTION OF THE THREADS. AFTER DISASSEMBLY, SEVERE CORROSION OF THE THREADED PORTION
- [SDR CA110209026](https://openairdocs.org/sdr/CA110209026.md): B-Nut · cracked · Feb 9, 2011 · Braero BAE125800A · Hydraulic System, Main
  > DURING INSP, A CRACK IN THE B-NUT ATTACHED TO THE SEQUENCE VALVE IN THE LT LANDING GEAR WELL AS NOTED. THE CRACK WAS RUNNINQ PERPENDICULAR TO THE THREADS OF THE NUT. THERE WERE NO PREVIOUS REPORTS OF HYD FLUID LEAKAGE.

Next page: https://openairdocs.org/model/raytheon-bae-125-800a/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 = 'BAE125800A'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/raytheon-bae-125-800a/reports

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