# Service difficulty reports: Raytheon HS 125-700A

A list on [Raytheon HS 125-700A](https://openairdocs.org/model/raytheon-hs-125-700a.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 4 · 193 reports

- [SDR 2022F00301](https://openairdocs.org/sdr/2022F00301.md): Hydraulic System · failed · Jul 22, 2022 · N564BR · Braero HS125700A · Hydraulic System, Main
  > AFTER TAKEOFF, HAD #2 HYD LO PRESS ANNUNCIATOR. RETURNED TO AIRPORT. #2 HYD SYSTEM ONLY PRODUCING APPROX. 2000 PSI. PUMP TTIS AND TOTAL CYCLES ARE UNKNOWN.
- [SDR 2020F00033](https://openairdocs.org/sdr/2020F00033.md): Static Inverter · failed · Nov 4, 2019 · N564BR · Braero HS125700A · Pitot/Static System
  > ON THE FIRST LEG OF A FOUR LEG TRIP, THE INVERTER FAILED, AND FAILED TO RESET, AS WE WERE DESCENDING INTO DALLAS FOR A LANDING AT ADDISON (KADS) THE FAILURE OCCURED. WE ADVISED THE PASSENGERS, AND SINCE WE WERE PICKING UP AN ADDITIONAL PASSENGER FOR THEIR MEE
- [SDR 2020FA0000016](https://openairdocs.org/sdr/2020FA0000016.md): Inverter · failed · Nov 4, 2019 · N564BR · Braero HS125700A · AC Inverter
  > 10/29/2019 TRIP DATE, ON THE FIRST LEG OF A FOUR LET TRIP, THE INVERTER FAILED AND FAILED TO RESET. AS WE WERE DESCENDING INTO DALLAS FOR A LANDING AT ADDISON KADS, THE FAILURE OCCURRED. WE ADVISED THE PASSENGERS, AND SINCE WE WERE PICKING UP AN ADDITIONAL P
- [SDR J8GA2018100100000](https://openairdocs.org/sdr/J8GA2018100100000.md): Unknown · malfunctioned · Sep 18, 2018 · N109B · Braero HS125700A · Landing Gear Steering System
  > UPON LANDING THE AIRCRAFT STEERED TO THE RIGHT AS SOON AS THE NOSE WHEEL TOUCHED THE GROUND. CREW REPORTED THAT THEY WERE NOT ABLE TO USE THE TILLER TO CONTROL THE AIRCRAFT DIRECTION. CREW REPORTED THE TILLER WAS VERY STIFF. AT THIS TIME IT'S DIFFICULT TO DETE
- [SDR 2017FA0000297](https://openairdocs.org/sdr/2017FA0000297.md): Fire Warning · false activation · Jul 17, 2017 · N26ME · Braero HS125700A · Fire Detection
  > APU WARNING ANNUNCIATOR PANEL ILLUMINATED AFTER TAKE-OFF. (APU WAS OFF AT THIS TIME) CREW FOLLOWED EMERGENCY CHECK LIST AND DISCHARGED THE FIRE EXTINGUISHER AND RETURNED TO FIELD. UPON INSPECTION BY MECHANICS, FOUND NO SIGNS OF ACTUAL FIRE, IT APPEARED TO BE I
- [SDR CA150116011](https://openairdocs.org/sdr/CA150116011.md): Lever · binding · Jan 5, 2015 · Braero HS125700A · Landing Gear Retraction/Extension System
  > (CAN) REFER TO HS125-700A IPC 32-30-01-11 REVERSING VALVE MECHANISM LEVER COULD NOT TURN FREELY DUE TO CONTAMINATION, PART AND BRACKET ASSEMBLY WAS CLEANED, MANUFACTURER DOES NOT CALL FOR LUBRIFICATION. THIS LEVER ENABLES THE LOCKING OF THE SIDESTAY ASSEMBLY.
- [SDR 5MFA20140709001](https://openairdocs.org/sdr/5MFA20140709001.md): Pump · failed · Jul 2, 2014 · N700R · Braero HS125700A · Hydraulic Pump (Electric/Engine), Main
  > THE LT ENGINE DRIVEN HYDRAULIC PUMP FAILED AND BEGAN DUMPING HYDRAULIC FLUID OVERBOARD. THIS RESULTED IN THE CAVITATION OF BOTH ENGINE-DRIVEN HYDRAULIC PUMPS AND THE FAILURE OF THE MAIN HYD SYSTEM.
- [SDR 5MFA201407140001](https://openairdocs.org/sdr/5MFA201407140001.md): Bushing · failed · Jul 2, 2014 · N700RR · Braero HS125700A · Hydraulic Pump (Electric/Engine), Main
  > ENROUTE, LT ENGINE DRIVEN HYD PUMP FAILED AND BEGAN DUMPING HYD FLUID OVERBOARD. RESULTING IN CAVITATION OF BOTH HYD EDP`S AND FAILURE OF THE HYDRAULIC SYSTEM. MX FOUND BUSHINGS THAT THE DRIVE USES AS A BEARINGS, FAILED. BOTH PUMPS WERE REPLACED. OPS CHECKED
- [SDR 5MFA20140709002](https://openairdocs.org/sdr/5MFA20140709002.md): Pump · leaking · Jul 2, 2014 · N700RR · Braero HS125700A · Hydraulic Pump (Electric/Engine), Main
  > THE LT ENGINE-DRIVEN HYDRAULIC PUMP FAILED AND BEGAN DUMPING HYDRAULIC FLUID OVERBOARD. THIS RESULTED IN THE CAVITATION OF BOTH ENGINE-DRIVEN HYD PUMPS AND THE FAILURE OF THE MAIN HYD SYSTEM.
- [SDR A6YA2013F00161](https://openairdocs.org/sdr/A6YA2013F00161.md): Clamp · out of position · Aug 16, 2013 · N724B · Braero HS125700A · Pneumatic Distribution System
  > DURING CLIMB AT APPROXIMATELY 20,000 FT. REAR BAY OVERHEAT INDICATOR ILLUMINATED, EMERGENCY PROCEDURES FOLLOWED AND LANDED WITH OUT INCIDENT. A BLEED AIR LEAK WAS FOUND BETWEEN FLOW CONTROL VALVE AND BLEED AIR DISTRIBUTOR DUCT. V BAND CLAMP WAS REPOSITION
- [SDR CA130527008](https://openairdocs.org/sdr/CA130527008.md): Seal · deteriorated · May 7, 2013 · Braero HS125700A · Pneumatic Distribution System
  > (CAN) IT WAS DETERMINED THAT THE SEAL LOCATED AT THE HP/LP FLANGE HAD DETERIORATED AND WAS CAUSING A MINOR LEAK. BECAUSE OF IT`S CLOSE PROXIMITY TO A TEMPERATURE SENSOR: COMPARTMENT OVERTEMP WARNINGS WERE RECEIVED IN THE COCKPIT, CAUSING TO UTILIZE THE EMERGEN
- [SDR CA130326008](https://openairdocs.org/sdr/CA130326008.md): Indicator · burned · Mar 22, 2013 · Braero HS125700A · Rate of Climb Indicator
  > (CAN) DURING ENGINE GROUND RUNS, ABOUT 5 MIN AFTER THE MAIN BUSES WERE BROUGHT ON LINE A ELECTRICAL BURNING ODOR WAS NOTED IN THE COCKPIT. THE AVIONICS SYS WERE SYSTEMATICLY SHUTDOWN AND THE ODOR DISAPATED. THE ENGINE RUNS WERE COMPLETED AND THE ACFT BROUGHT
- [SDR CA130325005](https://openairdocs.org/sdr/CA130325005.md): Shaft · failed · Mar 22, 2013 · Braero HS125700A · Hydraulic Pump (Electric/Engine), Main
  > (CAN) IN CRUISE, ACFT EXPERIENCED HYD LOW NR 2 WARNING FOLLOWED BY HYDRAULIC LOW NR 1 WARNING. MAIN HYD PRESSURE DROPPED BELOW NOMINAL PRESSURE. GEAR EXTENSION WAS DONE WITH AUXILIARY HYD CIRCUIT. ACFT LANDED WITH NO FURTHER INCIDENT. INSPECTION BY MFG R
- [SDR CA130201005](https://openairdocs.org/sdr/CA130201005.md): Drive Shaft · broken · Jan 31, 2013 · Braero HS125700A · Hydraulic Pump (Electric/Engine), Main
  > (CAN) DURING PREFLIGHT GROUND RUN, RT HYDRAULIC LOW PRESSURE WARNING LIGHT DID NOT EXTINGUISH DURING ENGINE START. TROUBLESHOOTING DETERMINED THE RT HYDRAULIC PUMP FAILED. HYDRAULIC PUMP REPLACED IAW CH 29, FILTERS INSPECTED IAW CH 29. FUNCTION AND LEAK CHEC
- [SDR CA110514001](https://openairdocs.org/sdr/CA110514001.md): Coupling · failed · May 6, 2011 · Braero HS125700A · Pneumatic Distribution System
  > (CAN) ON CLIMB OUT HAD REAR BAY OVERHEAT COME ON INTERMITTENT THEN WENT OFF. THERE WERE NO INDICATIONS IN THE COCKPIT OTHER THAN THE NR2 ENGINE COMPUTER WENT TO MANUAL MODE. ON ARRIVAL, INSPECTION WAS CARRIED OUT AND FOUND THAT THE APU BLEED AIR DUCT FLEX COUP
- [SDR CA100927006](https://openairdocs.org/sdr/CA100927006.md): Transceiver · false indication · Jun 22, 2010 · Braero HS125700A · Weather Radar System
  > PILOTS REPORTS RADAR SHOWS FALSE RETURNS. C/O GND CHECKS/OPS CHECKS COULD NOT FAULT. JULY 09/10 PILOTS REPORTS RADAR SHOWS FALSE RETURNS LT OF CTR. REMOVE R/T AND SENT FOR BENCH CHECK/REPAIR. UNIT INSTALLED F/C OPS CHECKS SERVICEABLE. AUG 02/10 PILOTS REPO
- [SDR CA090811002](https://openairdocs.org/sdr/CA090811002.md): Structure · damaged · Aug 9, 2009 · Braero HS125700A · Fuselage Structure (General)
  > AUG 09-2009 HS-125 700A INCIDENT REPORT HAIL DAMAGE. ACFT WAS RETURNING TO MAIN BASE FROM A 704 TRIP AND ATC ADVISED CREW OF THUNDER STORM ACTIVITY IN AREA. ACFT WAS HELD IN A HOLDING PATTERN AND THEN CLEARED. BETWEEN 13000FT AND 10000FT ACFT ENTERED AN ARE
- [SDR EYDA12009](https://openairdocs.org/sdr/EYDA12009.md): Starter Gen · failed · Jul 24, 2009 · N411PA · Braero HS125700A · Starter-Generator
  > AT CRUISE ALTITUDE, NR 2 GEN FAIL LIGHT ILLUMINATED AND CREW FELT VIBRATION FROM ENG. CREW ELECTED TO LAND AT MID AIRPORT DUE TO IT'S CLOSE PROXIMITY. ENG WAS PRECAUTIONARILY SHUTDOWN AND THE ACFT LANDED. MX FINDINGS WERE THAT AFT BRG HAD FAILED AND SHAFT H
- [SDR 2009FA0000635](https://openairdocs.org/sdr/2009FA0000635.md): Shaft · failed · Jul 19, 2009 · N210RK · Braero HS125700A · Hydraulic Pump (Electric/Engine), Main
  > DURING CRUSE BOTH HYD LOW-PRESSURE LIGHTS ILLUMINATED. CREW COMPLETED ABNORMAL CHECKLIST FOR CONDITION. CREW DIVERTED FROM ORIGINAL DESTINATION (PWK) TO AIRPORT WITH LONGER RUNWAY (RFD) AS PRECAUTIONARY MEASURE. CREW DECLARED EMERGENCY AS A PRECAUTIONARY ME
- [SDR 2009F00031](https://openairdocs.org/sdr/2009F00031.md): Power Supply · inoperative · Apr 23, 2009 · N356SR · Braero HS125700A · Emergency Lighting
  > EMERGENCY LIGHTING SYS WOULD NOT OPERATE DURING FUNCTIONAL TESTS AS PART OF A SCHEDULED AIRFRAME INSP. FOUND FWD POWER SUPPLY UNIT TO HAVE FAILED INTERNALLY. REPLACED POWER SUPPLY, SYSTEM TESTS NORMAL.
- [SDR 2008F00027](https://openairdocs.org/sdr/2008F00027.md): Connector · defective · Dec 15, 2008 · N411P · Braero HS125700A · Engine Indicating System Wiring
  > ON NOVEMBER 23, 2008, THE NR 2 ENGINE N1 GAUGE DIGITAL PORTION FAILED. THE MALFUNCTION WAS TRACED TO A DEFECTIVE CONNECTOR AT THE GAUGE.
- [SDR 2009FA0000095](https://openairdocs.org/sdr/2009FA0000095.md): Axle · worn · Dec 12, 2008 · N483FG · Braero HS125700A · Nose/Tail Landing Gear Strut/Axle
  > CONTINUOUS NOSE GEAR VIBRATIONS UPON LANDING. TEARDOWN AND INSP OF NOSE GEAR AXLE BARREL ASSY REVEALED THE NOSE AXLE TO BE WORN BEYOND LIMITATIONS. TWO.005 INCH GROOVES WORN INTO AXLE. ONE ON EACH SIDE WHERE THE AXLE BARREL COVER PLATE SEALS ARE LOCATED.
- [SDR 2008FA0000923](https://openairdocs.org/sdr/2008FA0000923.md): Axle · worn · Dec 12, 2008 · N483FG · Braero HS125700A · Nose/Tail Landing Gear Strut/Axle
  > CONTINUOUS NOSE GEAR VIBRATIONS UPON LANDING. TEARDOWN AND INSPECTION OF NOSE GEAR AXLE BARREL ASSY REVEALED THE NOSE AXLE TO BE WORN BEYOND LIMITATIONS. (2).005" GROOVES WORN INTO AXLE. (1) ON EACH SIDE WHERE THE AXLE BARREL COVER PLATE SEALS ARE LOCATED.
- [SDR EYD2008F00001](https://openairdocs.org/sdr/EYD2008F00001.md): Controller · malfunctioned · Aug 6, 2008 · N411PA · Braero HS125700A · Cabin Pressure Controller
  > ON AUGUST 6TH, WHILE EN ROUTE AT AN ALTITUDE OF 35,000 FEET, THE CREW EXECUTED AN EMERGENCY DESCENT DUE TO A "CABIN ALTITUDE" LIGHT. THE CREW CONTINUED ON TO FXE UNEVENTFULLY. AFTER TROUBLESHOOTING THE PRESSURIZATION SYSTEM, IT WAS DETERMINED THAT THE PRESSU
- [SDR EYD2008F00000](https://openairdocs.org/sdr/EYD2008F00000.md): Check Valve · failed · Jul 27, 2008 · N411PA · Braero HS125700A · Data Recorders (Flight/Maintenance)
  > WHILE ENROUTE, THE FLIGHT CREW EXECUTED AN EMERGENCY DESCENT DUE TO A "CABIN ALTITUDE" WARNING LIGHT, MAINTENANCE HAS FOUND 2 DEFECTIVE CHECK VALVES, PN 130156-1 AND 2 PRESSURE REGULATORS, PN 1024665, THAT WERE SUSPECT. ARE ALSO REPLACING THE ENTRY DOOR SEAL
- [SDR S8A2008F00001](https://openairdocs.org/sdr/S8A2008F00001.md): Transducer · failed · Apr 18, 2008 · N110EJ · Braero HS125700A · Engine Oil Pressure
  > AT 15,000 ENROUTE, AIRCRAFT LOST INDICATION OF OIL PRESSURE ON THE NR ONE (LEFT) ENGINE AND THE FLIGHT CREW ACCOMPLISHED A PRECAUTIONARY SHUTDOWN OF THE NR ONE ENGINE. AFTER A REVIEW BY THE FLIGHT CREW OF ALL INDICATING ENGINE INSTRUMENTATION THE FLIGHT CREW D
- [SDR 080048](https://openairdocs.org/sdr/080048.md): Starter Gen · malfunctioned · Jan 18, 2008 · N9999V · Braero HS125700A · Starter-Generator
  > LEFT STARTER GENERATOR DROPPED OFF LINE.
- [SDR CA071224002](https://openairdocs.org/sdr/CA071224002.md): Aileron · iced · Dec 13, 2007 · Braero HS125700A · Aileron Control System
  > (CAN) PILOT’S REPORTED ON APPROACH INTO AIRPORT, COULD NOT GET ANY ROLL ON AC CONTROLS. IT APPEARED THAT AILERONS WERE FROZEN. SHORTLY BEFORE TOUCHDOWN THEY WERE ABLE TO GAIN CONTROL OF THE AILERON MOVEMENT. THE AC LANDED WITHOUT INCIDENT. MAINT WAS CALLED AND
- [SDR CA071214007](https://openairdocs.org/sdr/CA071214007.md): Pitot Tube · corroded · Dec 10, 2007 · Braero HS125700A · Pitot/Static System
  > (CAN) FOLLOWING A FAILED PITOT STATIC TEST, AN INSPECTION OF THE PITOT STATIC TUBING WAS CARRIED OUT AND MAINT FOUND THAT ONE OF THE TUBES (P/N 25-7SF209-9) HAD A PIN HOLE, WHICH APPEARS TO HAVE BEEN CAUSED BY INTERGRANULAR CORROSION. THE LINE WAS REPAIRED AND
- [SDR CA071106011](https://openairdocs.org/sdr/CA071106011.md): Tube · chafed · Oct 25, 2007 · Braero HS125700A · Aircraft Fuel Distribution System
  > (CAN) ON A PREFLIGHT INSPECTION, MAINTENANCE DISCOVERED THE FIRE DETECTOR (P/N 3001-31-900-400-17) AGAINST THE FUEL TUBE ASSEMBLY (P/N P-84417). UPON REPOSITIONING THE FIRE DETECTOR INTO POSITION, A CHAFED MARK ON THE NR 1 ENGINE FUEL TUBE ASSEMBLY WAS DISCOVE
- [SDR CA070911010](https://openairdocs.org/sdr/CA070911010.md): Fuel Control · faulty · Aug 29, 2007 · Braero HS125700A · Fuel Control/Turbine Engines
  > (CAN) - MANUAL MODE SELECTION PROVIDES IDLE ONLY FUEL. NO SPOOL UP WITH POWER LEVER INCREASE. ENGINE FUNCTIONS NORMALLY IN AUTO - COMPUTER (ON) MODE. (TC NR 20070911010)
- [SDR DTX2007F00000](https://openairdocs.org/sdr/DTX2007F00000.md): Manifold · leaking · Aug 6, 2007 · N943CE · Braero HS125700A · APU Engine Fuel and Control
  > THE FLIGHT CREW NOTED A STRONG FUEL ODOR IN THE AFT CABIN, UPON INVESTIGATION, FUEL WAS FOUND ON THE AFT EQUIPMENT ACCESS DOOR AND UNDER THE APU. THE APU SHROUD WAS OPENED AND THE FUEL MANIFOLD WAS REMOVED AND IT WAS DISCOVERED TO HAVE A SMALL PINHOLE IN ONE
- [SDR YNTA200728102](https://openairdocs.org/sdr/YNTA200728102.md): Rod End · corroded · May 14, 2007 · N281BT · Braero HS125700A · Trailing Edge Flap Control System
  > ON APPROACH THE FLAP SYSTEM FAILED TO EXTEND PAST 15 DEGREES AND THEN BECAME STUCK AT 15 DEGREES. TRIED TO SET FLAPS TO 25 DEGREES AND FLAPS DID NOT MOVE, RESET FOR 15 DEGREES AND THEN UP TO 0 DEGREES WITH NO MOVEMENT. RESELECTED FLAPS TO 15-DEGREE POSITION.
- [SDR YNTA200728101](https://openairdocs.org/sdr/YNTA200728101.md): Yoke · corroded · May 14, 2007 · N281BT · Braero HS125700A · Trailing Edge Flaps
  > ON APPROACH THE FLAP SYSTEM FAILED TO EXTEND PAST 15 DEGREES AND THEN BECAME STUCK AT 15 DEGREES. TRIED TO SET FLAPS TO 25 DEGREES AND FLAPS DID NOT MOVE, RESET FOR 15 DEGREES AND THEN UP TO 0 DEGREES WITH NO MOVEMENT. RESELECTED FLAPS TO 15-DEGREE POSITION. L
- [SDR 2007FA0000192](https://openairdocs.org/sdr/2007FA0000192.md): Skin · corroded · Feb 27, 2007 · N224EA · Braero HS125700A · Leading Edge Devices
  > RT WING LEADING EDGE(S) HAD SEVERE CORROSION WHERE THE TKS PANELS ATTACH. AFTER COMPLETE DISASSEMBLY, IT WAS DETERMNED TO BE BEYOND ECONOMICAL REPAIR. RT WING LEADING EDGE HAD BEEN INSPECTED AT MFG 2.5 YEARS PRIOR TO THIS DISCOVERY. (K)
- [SDR 2007FA0000191](https://openairdocs.org/sdr/2007FA0000191.md): Skin · corroded · Feb 27, 2007 · N224EA · Braero HS125700A · Wing, Plate/Skin
  > RT WING LEADING EDGE(S) HAD SEVERE CORROSION WHERE THE TKS PANELS ATTACH. AFTER COMPLETE DISASSEMBLY IT WAS DETERMINED TO BE BEYOND ECONOMICAL REPAIR. RT WING LEADING EDGE HAD BEEN INSPECTED AT MFG 2.5 YEAR PRIOR TO THIS DISCOVERY. (K)
- [SDR 2007FA0000194](https://openairdocs.org/sdr/2007FA0000194.md): Skin · corroded · Feb 21, 2007 · N224EA · Braero HS125700A · Horizontal Stabilizer, Plate/Skin
  > LT AND RT HORIXONTAL STABILIZER LEADING EDGES HAD SEVERE CORROSION WHERE THE TKS PANELS ATTACH. AFTER COMPLETE DISASSEMBLY, IT WAS DETERMINED TO BE BEYOND ECONOMICAL REPAIR. THIS AREA HAD BEEN INSPECTED AT MFG 2.5 YEARS PRIOR TO THIS DISCOVERY. (K)
- [SDR CA060906011](https://openairdocs.org/sdr/CA060906011.md): Skin · cracked · Sep 6, 2006 · Braero HS125700A · Landing Gear Doors
  > (CAN) DURING REMOVAL FOR ACCESS, A GENERAL VISUAL INSPECTION OF THE RT MAIN GEAR DOOR REVEALED A LARGE CRACK IN THE INNER SKIN PANEL AS WELL AS SEVERAL PULLED RIVETS ADJACENT TO THE GEAR DOOR JACK ATTACH BRACKET. SB 32-192-2845 (TO PREVENT CRACKING OF THE BRA
- [SDR CA051006008](https://openairdocs.org/sdr/CA051006008.md): Engine · leaking · Sep 13, 2005 · Braero HS125700A · Engine (Turbine/Turboprop)
  > (CAN) DURING CLIMB, THE CABIN AIR BECAME CONTAMINATED WITH SMOKE. ECS WAS SELECTED OFF AND AN EMERGENCY DECLARED. SUBSEQUENT INSPECTION FOUND EXTERNAL ENGINE OIL LEAKAGE. MFG WILL INVESTIGATE THE INCIDENT AND ADVISE OF ROOT CAUSE, ONCE DETERMINED.
- [SDR CA050919006](https://openairdocs.org/sdr/CA050919006.md): Gearshaft · broken · Aug 31, 2005 · Braero HS125700A · Turbine Engine Accessory Drive
  > (CAN) AS A/C WAS TAXIING FOR T/O, CREW LOST LT ENGINE OIL PRESSURE. ENGINE WAS SHUTDOWN AND A/C WENT BACK TO GATE. LT ENGINE OIL PUMP WAS FOUND DAMAGED. PUMP WAS REPLACED BUT ENGINE COULD NOT START AS N1 FAN WAS NOT TURNING. ENGINE WAS OPENED UP AND NR 1 B
- [SDR UG82005F00009](https://openairdocs.org/sdr/UG82005F00009.md): Gearshaft · worn · Aug 24, 2005 · N48FB · Braero HS125700A · Accessory Gearboxes
  > (REF CNTRL NR: PA05005) THE S.O.A.P. LAB REPORT INDICATED HIGH LEVEL OF IRON (STEEL) IN THE ENGINE. THE SAMPLE INDICATED A SPECIFIC (BELLEVILLE) WASHER IN THE LP COMPRESSOR GEARBOX WAS FAILING DUE TO A SHIFTING OF THE LP PLANETARY GEARSHAFT ASSY. AC WAS FER
- [SDR 2005FA0001355](https://openairdocs.org/sdr/2005FA0001355.md): Ballast · unserviceable · Aug 16, 2005 · N727TA · Braero HS125700A · Passenger Compartment Lighting
  > AC WAS DISASSEMBLED FOR INSP. GROUNDING STRAPS ON VALENCE LIGHTS BROKEN. REPAIRED GROUNDING STRAPS. AC WAS REASSEMBLED, PWR WAS APPLIED TO AC FOR CHECKOUT. PWR WAS ON AC FOR HOURS. INSPECTING OVERHEAD LIGHTING, NOTICED A SPARK. DROPPED VALENCE TO INVESTI
- [SDR UQR2005F00000](https://openairdocs.org/sdr/UQR2005F00000.md): Tire · cracked · Aug 1, 2005 · N700NW · Braero HS125700A · Tire
  > DURING PRELIMINARY INCOMING INSPECTION ON 7/11/05 IT WAS NOTED THAT NR3 MAIN WHEEL TIRE HAD CRACKS OR SPLITS RADIALLY IN BETWEEN TREAD. IT WAS DETERMINED THAT THIS TIRE WAS INSTALLED ON THE NR 3 WHEEL (PN AH52788, SN 675/8129 ON 6/8/05 ACTT 11,926.5, ACTL 12,
- [SDR CA050422003](https://openairdocs.org/sdr/CA050422003.md): Wire · broken · Apr 20, 2005 · Braero HS125700A · Fuel System Wiring
  > (CAN) SWITCH MONITORS FUEL TEMP AT ENGINE FUEL PUMP & IS FITTED TO TFE731-3 ENGINES INSTALLED ON HAWKER 700 ACFT. ON THIS INSTALL SWITCH WIRES CONNECT TO AIRFRAME SUPPLIED ENGINE HARNESS THROUGH IN-LINE CONNECTORS. THESE CONNECTORS ARE NORMALLY ONLY DISTURBED
- [SDR WCL2005F00000](https://openairdocs.org/sdr/WCL2005F00000.md): Pump · intermittent · Apr 16, 2005 · N188KA · Braero HS125700A · Engine Fuel Pump
  > LT FUEL PUMP PRESSURE LIGHT INTERMITTENT. TOOK PRECAUTIONARY ACTIONS AND STARTED TO FEED FUEL AND TURNED. THE INTERMITTENT FUEL PUMP OFF. (EA11200503945) (K)
- [SDR CA050414004](https://openairdocs.org/sdr/CA050414004.md): Fan Blade · separated · Apr 12, 2005 · Braero HS125700A · Turbine Engine Compressor Section
  > (CAN) AT ROTATION, A POPPING NOISE WAS HEARD BUT NO ABNORMAL INSTRUMENT INDICATIONS WERE OBSERVED. CLIMB AND CRUISE WERE NORMAL AS WERE ALL TREND MONITOR RESULTS. ABNORMAL VIBRATION WAS APPARENT ON DESCENT WITH LOWER POWER SETTINGS. POST FLIGHT INSPECTION F
- [SDR 2005FA0000491](https://openairdocs.org/sdr/2005FA0000491.md): Clamp · cracked · Apr 6, 2005 · N281BT · Braero HS125700A · Engine Collector/Tailpipe/Nozzle
  > FLUORESSCENT PENETRANT INSP OF THE TAIL PIPE CLAMP REVEALED ONE NUT TO BE CRACKED. (K)
- [SDR 2005FA0000010](https://openairdocs.org/sdr/2005FA0000010.md): Clamp · cracked · Dec 7, 2004 · N224EA · Braero HS125700A · Engine Collector/Tailpipe/Nozzle
  > THE DEFECT IS A FATIGUE CRACK, CAUSED BY BEING OVERSTRESSED DUE TO LOAD LIMITS, POSSIBLE OVERTORQUED. MAYBE THIS PART SHOULD BE MADE STRONGER, TO HANDLE THE STRESS. THIS DEFECT WAS FOUND BY A PENETRANT INSPECTION. THE LOCKING NUT NEEDS TO BE REMOVED, IN TH
- [SDR NA0207001](https://openairdocs.org/sdr/NA0207001.md): Fire Detector · false indication · Nov 9, 2004 · N70X · Braero HS125700A · Fire Detection
  > APU FIRE WARNING INDICATION AFTER APPROXIMATELY 15 MINUTES OF APU OPERATION ON GROUND. CREW DISCHARGED FIRE EXTINGUISHING SYSTEM AND SHUT DOWN APU. TROUBLESHOT PROBLEM TO A BAD BOTTOM APU HEAT DETECTOR. REPLACE HEAT DETECTOR WITH NEW UNIT. REPLACE FIRE BOT
- [SDR I262005F00000](https://openairdocs.org/sdr/I262005F00000.md): Pump · weak · Nov 5, 2004 · N125SJ · Braero HS125700A · Fuel Boost Pump
  > LT (FUEL LOW PRESSURE) LIGHT ILLUMINATED, CREW ELECTED TO LAND. FOUND LT FUEL BOOST PUMP WEAK. PUMP REPLACED WITH OVERHAULED PUMP. AWAITING TEARDOWN REPORT ON REMOVED PUMP. (NE05200503254) (K)

Next page: https://openairdocs.org/model/raytheon-hs-125-700a/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 = 'HS125700A'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/raytheon-hs-125-700a/reports

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