# Service difficulty reports: Corporate Jets BAE 125-1000A

A list on [Corporate Jets BAE 125-1000A](https://openairdocs.org/model/corporate-jets-bae-125-1000a.md).

Newest first. General aviation reporting is voluntary.

- [SDR 4USA20210709004](https://openairdocs.org/sdr/4USA20210709004.md): Display · smoke · Jul 5, 2021 · N524LR · Braero BAE1251000A · Indicating/Recording System
  > SMOKE DETECTED COMING FROM CAPTAIN A SCREEN AT CRUISE ALTITUDE. CORRECTIVE ACTION: INSPECTED A SCREEN AND SURROUNDING WIRING. INSPECTED INSTRUMENT PANEL AND AVIONICS FANS. NO EVIDENCE OF ELECTRICAL DISCREPANCIES FOUND. PERFROMED OPERATIONAL CHECKS OF AVIONICS
- [SDR 4USA04272021003](https://openairdocs.org/sdr/4USA04272021003.md): Engine · surges · Apr 23, 2021 · N524LR · Braero BAE1251000A · Engine (Turbine/Turboprop)
  > AFTER TAKEOFF FROM KOPF,WHILE CLIMBING THROUGH FLIGHT LEVEL 15000, RIGHT HAND ENGINE N2 BEGAN SURGING. THROTTLE WAS BROUGHT BACK TO IDLE AND ENGINE STABILIZED. AFTER APPROXIMATELY 20 MINUTES WHILE IN A HOLDING PATTERN, RH ENGINE N2 AGAIN BEGAN SURGING. LANDED
- [SDR CA190604008](https://openairdocs.org/sdr/CA190604008.md): Engine · malfunctioned · May 23, 2019 · Braero BAE1251000A · Engine (Turbine/Turboprop)
  > (CAN) CUSTOMER REPORTED THAT THEY COULD NOT SHUT DOWN THE ENGINE NORMALLY, THEY HAD TO PULL THE T-HANDLE TO SHUT DOWN. WHEN ATTEMPTING TO SHUT THE ENGINE DOWN, PUT POWER LEVER IN CUT OFF, AND ENGINE OSCILLATED AND HUNG AROUND 30% N2. ITT WAS NEAR UPPER LIMIT A
- [SDR CA140826003](https://openairdocs.org/sdr/CA140826003.md): Oil System · low pressure · Aug 4, 2014 · Braero BAE1251000A · Engine Oil Indicating System
  > (CAN) DURING FLIGHT, THE PILOT ELECTED TO SHUT DOWN THE LEFT ENGINE DUE TO LOW OIL PRESSURE. FLIGHT WAS DIVERTED TO VIE AIRPORT, VIENNA, AUSTRIA. UNEVENTFUL SINGLE ENGINE LANDING PERFORMED. AFTER LANDING THEY OIL FOUND LEAKED EXTERNALLY AND ENGINE LOST A LARGE
- [SDR CA131007001](https://openairdocs.org/sdr/CA131007001.md): Engine · surges · Sep 23, 2013 · Braero BAE1251000A · Engine (Turbine/Turboprop)
  > (CAN) DURING CRUISE FLIGHT, THE NR 2 ENGINE SURGED WHERE THE N2 AND FF IS FLUCTUATING AND N1 SPLIT OF 3 PERCENT.
- [SDR CA130819006](https://openairdocs.org/sdr/CA130819006.md): Engine · smoke · Aug 9, 2013 · Braero BAE1251000A · Engine (Turbine/Turboprop)
  > (CAN) DURING CLIMB AT 3000 FEET, THE PILOT REPORTED TO HAVE SMOKE IN CABIN. AFTER A FEW ACTIONS FROM THE CREW TRYING TO ISOLATE THE ENGINE FROM WHICH THIS SMOKE WAS COMING FROM, POWER WAS REDUCED AND SMOKE STOPPED. ACFT LANDED SAFELY WHERE ADDITIONAL GROUND
- [SDR CA130502002](https://openairdocs.org/sdr/CA130502002.md): Engine · shutdown · Apr 29, 2013 · Braero BAE1251000A · Engine (Turbine/Turboprop)
  > (CAN) THE CREW REPORTED THE LT ENGINE SPOOL BACK AND AN UNCOMMANDED SHUTDOWN AFTER 30 MINUTES OF FLIGHT DURING CRUISE AT FL 330. DURING THE SHUTDOWN, THE CREW PERFORMED THE EMERGENCY CHECK LIST AND DESCENDED TO FL210 WHERE THEY PERFORMED A START. THE DURATIO
- [SDR BLUA2012F00026](https://openairdocs.org/sdr/BLUA2012F00026.md): Computer · warning light · Jun 30, 2011 · N801RM · Braero BAE1251000A · Engine Indicating System
  > NR 2 ENGINE COMPUTER LIGHT ILLUMINATED IN FLIGHT.
- [SDR E0X2009F00002](https://openairdocs.org/sdr/E0X2009F00002.md): Unknown · unknown · Jun 27, 2009 · N539LR · Braero BAE1251000A · Central Warning
  > AT FL 410 ECS INLET OVERHEAT LIGHT ILLUMINATED, CREW PUT MAIN AIR VALVES BOTH ON LB AND STARTED A DESCENT TO FL 350. APPROX 1 MINUTE AFTER START OF DESCENT THE CABIN BEGAN A RAPID CLIMB IN EXCESS OF 10,000 FT. CREW BEGAN AN EMERGENCY DESCENT AND DECLARED AN
- [SDR E0X2008F00003](https://openairdocs.org/sdr/E0X2008F00003.md): Controller · defective · May 19, 2008 · N541LR · Braero BAE1251000A · Windshield/Door Rain/Ice Removal
  > ON CLIMBOUT, FLIGHT CREW ELECTED TO TURN ON WINDSHIELD HEAT, SOMETIME AFTER THAT AND BEFORE REACHING CRUISE ALT. THE FLIGHTCREW NOTED THE FO`S RT REAR WINDSHIELD DELAMINATING, LITERALLY COOKED, STATED BY CAPTAIN. FLIGHT CREW LEVELED AT 12,000 FT, DECLARED AN E
- [SDR E0X2008F00002](https://openairdocs.org/sdr/E0X2008F00002.md): Engine · failed · May 18, 2008 · N539LR · Braero BAE1251000A · Engine (Turbine/Turboprop)
  > NR 1 ENGINE QUIT AS AC WAS CLIMBING THROUGH FL370 WITH NO WARNING. FIRST INDICATION WAS LOSS OF OIL PRESSURE AS ENGINE SPOOLED DOWN. DIVERTED AND DECLARED AN EMERGENCY. THEIR WAS NOT AN ATTEMPT MADE TO AIRSTART THE FAILED ENGINE. SINGLE ENGINE LANDING WAS UNE
- [SDR E0X2008F00001](https://openairdocs.org/sdr/E0X2008F00001.md): Unknown · unknown · Feb 7, 2008 · N542LR · Braero BAE1251000A · Auto Flight System
  > ON APPROACH, AT 3000 FT, EXPERIENCED A PARTIAL PANEL FAILURE ON THE CAPT EADI, EHSI, MFG. TRANSFERRED CONTROL OF AC TO THE F/O. SELECTED THE NR 2 AFSC AND 30 SECONDS THE AC DEPARTED LEVEL FLIGHT AND STARTED AN UNCOMMANDED DESCENT. AT 2700 FT BOTH FLIGHT CRE
- [SDR CA071128009](https://openairdocs.org/sdr/CA071128009.md): O-Ring · leaking · Nov 16, 2007 · Braero BAE1251000A · Turbine Engine Oil System
  > (CAN) CREW REPORTED OIL PRESSURE FLUCTUATIONS AND ILLUMINATION OF THE LOW OIL PRESSURE WARNING INDICATOR. THE ENGINE WAS SHUTDOWN AND THE FLIGHT DIVERTED. INVESTIGATION REVEALED DEFECTIVE O-RINGS ON THE NR4 BEARING TRANSFER TUBES (TC NR 20071128009)
- [SDR 2005FA0001481](https://openairdocs.org/sdr/2005FA0001481.md): Drain · chafed · Oct 4, 2005 · N503QS · Braero BAE1251000A · Hydraulic Pump (Electric/Engine), Main
  > RT HYDRAULIC PUMP CASE DRAIN HYDRAULIC LINE RUPTURED IN FLIGHT, DRAINING HYDRAULIC FLUID FROM THE AIRCRAFT SYSTEM. FOUND RT HYDRAULIC PUMP CASE DRAIN LINE CRACKED WHERE LINE HAS BEEN CHAFING. INSPECTED AIRCRAFT AND FOUND SIMULAR CHAFE IN SAME LINE IN SAME LO
- [SDR DXTA200500519](https://openairdocs.org/sdr/DXTA200500519.md): Engine · overheated · Jan 7, 2005 · N533QS · Braero BAE1251000A · Engine (Turbine/Turboprop)
  > OVERTEMP NR 2 ENGINE ON TAKEOFF, TEMPERATURE WENT TO 797 DEGREES FOR 2 SECONDS. ABORTED TAKEOFF. ITEM IS UNDER INVESTIGATION.
- [SDR DXTA200400498](https://openairdocs.org/sdr/DXTA200400498.md): Cdu · faulty · Dec 26, 2004 · N523QS · Braero BAE1251000A · Central Display
  > BURING ELECTRICAL SMELL IN COCKPIT, NO OTHER INDICATIONS. GEN 1 AMPS 80/ GEN 2 AMPS 120. REMOVED NR 1 FMS CDU DUE TO NO DISPLAY AND FAINT BURNING ELECTRICAL SMELL. REPLACED WITH SERVICEABLE FMS CDU OPS CHECK GOOD IAW HAWKER 1000 MM CH 34-61-00 REV 27 10/04.
- [SDR DXTA200400478](https://openairdocs.org/sdr/DXTA200400478.md): Sequence Valve · malfunctioned · Dec 12, 2004 · N542QS · Braero BAE1251000A · Landing Gear Retraction/Extension System
  > IMMEDIATELY AFTER TAKEOFF AND GEAR RETRACTION, THE RT GEAR IN TRANSIT LIGHT (RED LIGHT) REMAINED ILLUMINATED. PRIOR TO LOWERING GEAR REQUESTED (2) LOW FLIGHT PASSES WITH LIT TOWER FOR VISUAL VERIFICATION, TOWER ADVISED THE RIGHT MAIN GEAR DOOR WAS SLIGHTLY OP
- [SDR 2005FA0000260](https://openairdocs.org/sdr/2005FA0000260.md): Alternator · failed · Dec 9, 2004 · N533QS · Braero BAE1251000A · AC Power Distribution System
  > AIRCRAFT WAS SQUAWKED WITH NR 1 ALTERNATOR DROPPING OFF IN FLIGHT. DURING TROUBLESHOOTING THE TECHNICIAN FOUND SMOKE TRAILS ON THE (GG PANEL), LOCATED ON THE AFT SIDE OF THE REAR FACE OF THE PRESSURE BULKHEAD. A MORE CLOSE INSPECTION REVEALED A DESTROYED FU
- [SDR 2005FA0000088](https://openairdocs.org/sdr/2005FA0000088.md): Holder · destroyed · Dec 9, 2004 · N533QS · Braero BAE1251000A · AC Power Distribution System
  > AIRCRAFT WAS SQUAWKED WITH NR 1 ALTERNATOR DROPPING OFF IN FLIGHT. DURING TROUBLESHOOTING THE TECHNICIAN FOUND SMOKE TRAILS ON THE GG PANEL. LOCATED ON THE AFT SIDE OF THE REAR FACE OF THE PRESSURE BULKHEAD. A MORE CLOSE INSPECTION REVEALED A DESTROYED FUSE
- [SDR DXTA200400419](https://openairdocs.org/sdr/DXTA200400419.md): Computer · failed · Oct 7, 2004 · N535QS · Braero BAE1251000A · Flight Management Computing Hardware System
  > NR 2 FMS WENT BLANK AND A ELECTRICAL BURNING ODOR WAS NOTICED SHORTLY AFTERWARDS IN COCKPIT. REPLACED NR 2 FMS IAW HAWKER 1000 AMM CHAPTER 34-61-00, OPS CHECK GOOD IAW HAWKER 1000 AMM CHAPTER 34-61-00.
- [SDR DXTA200300205](https://openairdocs.org/sdr/DXTA200300205.md): Controller · malfunctioned · Dec 18, 2003 · N540QS · Braero BAE1251000A · Trailing Edge Flap Control System
  > DURING FLIGHT FROM TEB TO ADS DURING DESCENT FLAPS WILL NOT LOWER WHEN SELECTED TO 15, 25, OR 45 DEGREES. DIVERTED TO DFW AND LANDED SAFELY. ITEM IS UNDER INVESTIGATION.
- [SDR DXTA200300121](https://openairdocs.org/sdr/DXTA200300121.md): Coalescer Bag · contaminated · Sep 19, 2003 · N503QS · Braero BAE1251000A · Humidity Control System
  > ON CLIMB OUT AT 15,000 FT BROUGHT THRUST LEVERS TO IDLE AND CABIN BEGAN FILLING WITH SMOKE. REPLACED WATER SEPARATOR SOCK, AND LOWERED NR 2 ENG OIL PRESS IAW HAWKER 1000 M/M, CHAPTER 71-00-00 AND CHAPTER 21-50-15. AIR CONDITIONING SYSTEM FUNCTIONAL CHECKED
- [SDR DXTA200300109](https://openairdocs.org/sdr/DXTA200300109.md): Indicator · erratic · Sep 2, 2003 · N540QS · Braero BAE1251000A · Trailing Flap Position Indicating System
  > ON TAKEOFF ROLL FLAP POSITION INDICATOR HAD ERRATIC MOVEMENT, FROM THE SET POSITION OF 15 DEGREES THEN MOVED TO 20 DEGREES THEN TO 25 DEGREES AND THEN BACK TO 15 DEGREES, FOLLOWED IMMEDIATELY BY IT MOVING BACK TO 25 DEGREES AND THEN CONTINUING DOWN TO 45 DEGRE
- [SDR DXTA200300093](https://openairdocs.org/sdr/DXTA200300093.md): Engine · failed · Aug 18, 2003 · N533QS · Braero BAE1251000A · Engine (Turbine/Turboprop)
  > ON SHORT FINAL WITH A REDUCTION IN POWER NR 2 ENG FAILED AND MASTER CAUTION ILLUMINATED. OIL PRESSURE CAUTION LIGHT CAME ON NOTICED OIL PRESSURE GAUGE READ 10 PSI, ENGINE SHUTDOWN UNCOMMANDED. - REMOVED RT THROTTLE RDVT AND INSTALLED A NEW RDVT AND RIGGED IAW
- [SDR DXTA200300035](https://openairdocs.org/sdr/DXTA200300035.md): Master Cylinder · overserviced · May 22, 2003 · N523QS · Braero BAE1251000A · Brake
  > NO BRAKING ACTION FROM CO-PILOT'S RIGHT BRAKE PEDAL (ONLY 300-400 PSI REGISTERED ON BRAKE PRESS. GAUGE). - BLED HYDRAULIC SYSTEM AND SERVICED MASTER CYLINDER TO PROPER FLUID LEVEL.
- [SDR 20001102SH031](https://openairdocs.org/sdr/20001102SH031.md): Bolt · failed · Oct 2, 2000 · N204R · Braero BAE1251000A · Wheel/Ski/Float
  > DUNLOP WHEEL CMM TIE BOLT RUNNING TORQUE CHECK DOES NOT CHECK FULL LENGTH OF THE THREADS. THE TIE BOLTS APPEAR TO BE STRETCHING FARTHER TOWARD THE SHANK OF THE BOLT. WHEN RUNNING TORQUE WAS CHECKED OVER, THE FULL LENGTH OF THE THREAD, 5 BOLTS FAILED. (X)
- [SDR VJ1R2000002](https://openairdocs.org/sdr/VJ1R2000002.md): Turbine Wheel · failed · Feb 10, 2000 · N119PW · Braero BAE1251000A · APU Core Engine
  > TURBINE WHEEL FAILURE. TURBINE WHEEL, P/N M167222-1, S/N V16-H329N. TSN: 661.9 HOURS. CSN: 2,311. SUBMITTER STATED THIS TURBINE WHEEL INSTALLED IN THIS APU 5-9-97. (X)
- [SDR 98ZZZX4648](https://openairdocs.org/sdr/98ZZZX4648.md): Line · broken · Oct 6, 1998 · N530QS · Braero BAE1251000A · Compressor Bleed Control
  > PILOT'S DISCREPANCY WAS NR 1 ENIGNE IS TEMP LIMITED ABOVE CRUISE DETENT. REMOVED THE OUTER AND INNER BYPASS ACCESS TO CHECK BLEED VALVES. UPON INVESTIGATION, FOUND THE BLEED AIR (P3 LINE) BROKEN AT B-NUT, P/N 3081695. IT APPEARED THE FIT OF THE LINE HAD CAU
- [SDR 99ZZZX889](https://openairdocs.org/sdr/99ZZZX889.md): Eec · failed · Apr 17, 1998 · N410US · Braero BAE1251000A · Fuel Controlling System
  > ENGINE UNRESPONSIVE TO THROTTLE MOVEMENT. TROUBLESHOT FADEC FAULT 'TE' (ENGINE SPEED LIMITED AT IDLE WHEN INTRANSIT DISCRETE). FADEC 'SEES' THRUST REVERSER INTRANSIT, HOLDS ENGINE AT IDLE. FOUND ELECTRONIC ENGINE CONTROL AT FAULT. REPLACED EEC. OPS CHECK

## 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 = 'BAE1251000A'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/corporate-jets-bae-125-1000a/reports

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