# Service difficulty reports: British Aerospace BAE 125-1000

A list on [British Aerospace BAE 125-1000](https://openairdocs.org/model/british-aerospace-bae-125-1000.md).

Newest first. General aviation reporting is voluntary.

- [SDR 2016120500007](https://openairdocs.org/sdr/2016120500007.md): Actuator · malfunctioned · Dec 1, 2015 · N730CJ · Braero BAE1251000 · Landing Gear Retraction/Extension System
  > DURING APPROACH, LT MLG, WHEN SELECTED DOWN, DID NOT SHOW DOWN AND SAFE INDICATION ON EITHER, NORMAL OR AUXILIARY, INDICATION SYSTEM. RT AND NLG BOTH SHOWED DOWN AND LOCKED. PILOT ATTEMPTED EMERGENCY EXTENSION UTILIZING AUXILIARY HYDRAULIC SYSTEM, IAW EMERGE
- [SDR E0X2008F00007](https://openairdocs.org/sdr/E0X2008F00007.md): Rudder · locked · Oct 25, 2008 · N505LR · Braero BAE1251000 · Rudder Control System
  > AFTER DEPARTED, GOING THROUGH APPROX 800 FT AGL THE F/O NOTED THAT THE RUDDER HAD LOCKED UP IN THE NEUTRAL POSITION. THE OAT AT THE TIME WAS +9C. ACFT CONTINUED TO CLIMB AND CAPTAIN INFORMED ATC THAT WOULD BE RETURNING TO DEPARTURE. ACFT WAS ABOVE MAX LANDIN
- [SDR E0X2008F00004](https://openairdocs.org/sdr/E0X2008F00004.md): Engine · damaged · Jun 6, 2008 · N513LR · Braero BAE1251000 · Engine (Turbine/Turboprop)
  > AC DEPARTED AND SHORTLY AFTER DEPARTURE, SMOKE WAS NOTED IN CABIN WITH BAGGAGE SMOKE DETECTOR INDICATING SMOKE IN BAGGAGE COMPARTMENT. FLIGHT CREW DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE, APPROACH AND LANDING WERE UNEVENTFUL WITH NO OTHER INDICATION O
- [SDR E0X2008F00005](https://openairdocs.org/sdr/E0X2008F00005.md): Starter Gen · failed · Jun 3, 2008 · N542LR · Braero BAE1251000 · Starter-Generator
  > IN CRUISE FLIGHT AT FL380, CREW FELT A VIBRATION, IT CONTINUED TO GET STRONGER. CREW REQUESTED ATC TO LAND AT NEAREST SUITABLE AIRPORT BUT DID NOT DECLARE AN EMERGENCY. FLIGHT CREW DETERMINED THAT NR 1 GENERATOR WAS GONG BAD AND DIVERTED THE AC. APPROACH WA
- [SDR E0X2007F00000](https://openairdocs.org/sdr/E0X2007F00000.md): Scavenge Port · worn · Nov 19, 2007 · N515LR · Braero BAE1251000 · Turbine Engine Oil System
  > DEPARTED, ENROUTE, AT 22,000FT THE FLIGHT CREW DECLARED AN EMERGENCY WHEN THE NR 1 (LT) ENGINE OIL PRESSURE STARTED FLUCTUATING AND ALL LOW PRESSURE LIGHT CAME ON. FLIGHT CREW SHUTDOWN NR 1 ENGINE AND MADE AN EMERGENCY LANDING. THE LANDING WAS UNEVENTFUL WIT
- [SDR 2006FA0001159](https://openairdocs.org/sdr/2006FA0001159.md): Pump · failed · Nov 17, 2006 · N46WC · Braero BAE1251000 · Fuel Boost Pump
  > THREE FUEL BOOST PUMPS IN OVERHAULED CONDITION, SAME PN, ORDERED FROM THE SAME VENDOR HAVE FAILED AFTER SHORT TIME ON SAME AIRCRAFT USED ON LT AND RT SIDES. 1) FUEL BOOST PUMP OVERHAULED CONDITION SN 11A557 FAILED 5/24/06 AFTER 247 HOURS. 2) FUEL BOOST PUMP
- [SDR 2006FA0001157](https://openairdocs.org/sdr/2006FA0001157.md): Pump · failed · May 24, 2006 · N46WC · Braero BAE1251000 · Fuel Boost Pump
  > THREE FUEL BOOST PUMPS IN OVERHAULED CONDITION, SAME PART NUMBER, ORDERED FROM THE SAME VENDER HAVE FAILED AFTER SHORT TIME ON SAME AIRCRAFT USED ON LT AND RT SIDES. 1) FUEL BOOST PUMP OVERHAULED CONDITION SN 11A557 FAILED 5/24/06 AFTER 247 HOURS. 2) FUEL BOO
- [SDR 2006FA0001158](https://openairdocs.org/sdr/2006FA0001158.md): Pump · failed · May 11, 2006 · N46WC · Braero BAE1251000 · Fuel Boost Pump
  > THREE FUEL BOOST PUMPS IN OVERHAULED CONDITION, SAME PN, ORDERED FROM SAME VENDOR HAVE FAILED AFTER SHORT TIME ON SAME AIRCRAFT USED ON LT AND RT SIDES. 1) FUEL BOOST PUMP OVERHAULED CONDITION SN 11A557 FAILED 5/24/06 AFTER 247 HOURS. 2) FUEL BOOST PUMP OVER
- [SDR CA060425010](https://openairdocs.org/sdr/CA060425010.md): Engine · malfunctioned · Apr 8, 2006 · Braero BAE1251000 · Engine (Turbine/Turboprop)
  > DURING CRUISE, THE ENGINE SURGED FOLLOWED BY AN UNCOMMANDED POWER REDUCTION TO IDLE. THE WAS NO SUBSEQUENT RESPONSE TO THROTTLE INPUT. P&WC WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED.
- [SDR CA060129015](https://openairdocs.org/sdr/CA060129015.md): Line · fractured · Jan 3, 2006 · Braero BAE1251000 · Pneumatic Distribution System
  > (CAN) FOLLOWING TAKEOFF, THE ENGINE FIRE WARNING ANNUNCIATED AND THE ENGINE WAS REPORTED TO BE (TRAILING SMOKE). THE ENGINE WAS SHUTDOWN IN FLIGHT, AN EMERGENCY DECLARED AND THE FLIGHT DIVERTED TO POINT OF DEPARTURE. SUBSEQUENT INSPECTION REVEALED NO EVIDENS
- [SDR CA051104011](https://openairdocs.org/sdr/CA051104011.md): Engine · power loss · Oct 22, 2005 · Braero BAE1251000 · Engine (Turbine/Turboprop)
  > (CAN) DURING A TRAINING TOUCH-AND-GO MANEUVER, THE ENGINE ROLLED BACK IN POWER AND THE LOW OIL PRESSURE WARNING ANNUNCIATED. THE ENGINE WAS SHUT DOWN IN FLIGHT AND AN UNSCHEDULED LANDING CARRIED OUT. MFG WILL INVESTIGATE THE INCIDENT AND ADVISE OF ROOT CAUSE
- [SDR DXTA200500718](https://openairdocs.org/sdr/DXTA200500718.md): Proximity Switch · malfunctioned · May 9, 2005 · N514QS · Braero BAE1251000 · Landing Gear Retraction/Extension System
  > NOSE GEAR GREEN LIGHT WILL NOT ILLUMINATE WITH GEAR DOWN. REPLACED NOSE LANDING GEAR CHANGE OVER SWITCH. OPS CHECK GOOD IAW THE HAWKER 1000 MM 32-60-05. REPLACED NOSE LANDING GEAR CHANGE OVER MICRO SWITCH P/N WITH NEW P/N 1EN1-14N119. PERFORMED SATISFACTOR
- [SDR CA050323005](https://openairdocs.org/sdr/CA050323005.md): Line · cracked · Mar 7, 2005 · Braero BAE1251000 · Engine Fuel Distribution
  > (CAN) DURING INSPECTION FUEL WAS FOUND LEAKING FROM A CRACKED HMU-TO-FUEL FLOW TRANSMITTER LINE. THE ENGINE HAD PREVIOUSLY EXPERIENCED AN AIRFRAME STARTER-GENERATOR FAILURE.
- [SDR DXTA200500535](https://openairdocs.org/sdr/DXTA200500535.md): Blanket · loose · Jan 15, 2005 · N505QS · Braero BAE1251000 · Fuselage Miscellaneous Structure
  > FIVE SECONDS AFTER ADDING TAKEOFF POWER REAR BAY OVERHEAT LOOKUP LIGHT ILLUMINATED. LIGHT WENT OUT TWO SECONDS AFTER THROTTLE REDUCED TO IDLE. RAN ENGINES. CHECKED FOR LEAKS, NO LEAKS FOUND AT THIS TIME. FOUND HEAT BLANKET NOT SECURE ON EXPANSION PIPE OUTB
- [SDR DXTA200400472](https://openairdocs.org/sdr/DXTA200400472.md): Odor · detected · Dec 8, 2004 · N505QS · Braero BAE1251000 · Air Distribution System
  > AT FL370 A BURNING ODOR WAS DETECTED, LASTING ABOUT 3-5 MINUTES. ANOTHER DIFFERENT BURNING ODOR WAS DETECTED PASSING 15,000 FEET IN THE DESCENT, IT LASTED UNTIL THE BLEED AIR WAS TURNED OFF PASSING 10,000 FEET. RAN ENGINES AND CHECKED OIL LEVEL. NR 2 ENGINE
- [SDR DXTA200400391](https://openairdocs.org/sdr/DXTA200400391.md): Coalescer Bag · dirty · Sep 14, 2004 · N505QS · Braero BAE1251000 · Humidity Control System
  > ON DESCENT WITH POWER LEVERS AT IDLE NOTICED EXHAUST FUME ODOR IN CABIN. REMOVED COALESOR SOCK AND INSTALLED NEW IAW MFG M/M CHAPTER 21-50-13. RAN AIRCRAFT AND LEAK CHECKED, NO LEAKS NOTED, COULD NOT DUPLICATE SMELL AT IDLE ON GROUND.
- [SDR DXTA200400389](https://openairdocs.org/sdr/DXTA200400389.md): Smoke · detected · Sep 11, 2004 · N520QS · Braero BAE1251000 · Air Distribution System
  > DURING TAXI OUT FOR A REPOSITION FLIGHT, THE AUX AND PAC WARNING LIGHT CAME ON, FOLLOWED BY THE REAR BAGGAGE SMOKE WARNING LIGHT. SMOKE BEGAN TO FILL THE CABIN AREA, PERFORMED EMERGENCY EVACUATION FOR FLIGHT CREW. ITEM IS UNDER INVESTIGATION.
- [SDR DXTA200400319](https://openairdocs.org/sdr/DXTA200400319.md): A/C Pack · malfunctioned · Jun 5, 2004 · N514QS · Braero BAE1251000 · Cabin Cooling System
  > NOTICED FUMES AND SLIGHT SMOKE COMING FROM THE CO-PILOTS AIR CONDITIONING VENT DURING DEPARTURE, ODOR WAS STRONGEST WHEN MAIN AIR VALVES WERE FIRST OPENED AND WENT AWAY AFTER THE VALVES WERE PLACED TO LOW PRESSURE. RAN BOTH ENGINES AND APU WITH BLEED AIR ON F
- [SDR DXTA200300090](https://openairdocs.org/sdr/DXTA200300090.md): Wire · broken · Aug 15, 2003 · N514QS · Braero BAE1251000 · Landing Gear System Wiring
  > AFTER TAKE-OFF COULD NOT RETRACT LANDING GEAR, ACCOMPLISHED AIR TURN BACK TO TPA AND LANDED OVERWEIGHT. - REPAIRED BROKEN WIRE AT KAPIS BY INSTALLING SPLICE P/N D436-36, OPS CHECKED GOOD I/A/W HAWKER 1000 MM CHAPTER 32-30-00. C/W PRESSURIZE CHECK ON GROUND O
- [SDR DXTA200300056](https://openairdocs.org/sdr/DXTA200300056.md): Engine · malfunctioned · Jul 3, 2003 · N514QS · Braero BAE1251000 · Fuel Flow Indicating
  > DURING TAKEOFF ROLL AT APPROX 100KTS A/C STARTED YAWING TO THE RIGHT ENGINE GUAGES REVEALED LEFT N1 98.4 PERCENT RIGHT N1 94 PERCENT LEFT ENGINE FUEL FLEW 2300 LBS/HR AND RIGHT 1900 LB/HR APR ARMED.
- [SDR UXF2002F00000](https://openairdocs.org/sdr/UXF2002F00000.md): Lamp · inoperative · Nov 16, 2001 · N119U · Braero BAE1251000 · Passenger Compartment Lighting
  > FLUORESCENT LAMP 22 INCHES LONG, MODEL F00100 HAS EVIDENCE OF SEVERE OVERHEATING (CHARRING) AT ONE END OF LAMP. LAMP USED IN GALLEY/CABIN LIGHTING SYSTEM.
- [SDR 98ZZZX4206](https://openairdocs.org/sdr/98ZZZX4206.md): P3 Line · broke · Oct 6, 1998 · N530QS · Braero BAE1251000 · Fuel Controlling System
  > PILOTS DISCREPANCY WAS NR 1 ENGINE TEMPORARILY LIMITED ABOVE CRUISE DETENT. REMOVED THE OUTBOARD 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 C
- [SDR 98ZZZX3222](https://openairdocs.org/sdr/98ZZZX3222.md): Tube · broken · Aug 1, 1998 · N513QS · Braero BAE1251000 · Compressor Bleed Control
  > RIGHT HAND ENGINE OUTBOARD BLEED AIR VALVE P3 LINE FOUND BROKEN AT WELDED 'L' FITTING. BY VISUAL INSPECTION, SUSPECTED CAUSE IS VIBRATION AND FATIGUE AND POSSIBILITY OF FLAW IN WELD.
- [SDR AU971506](https://openairdocs.org/sdr/AU971506.md): O-Ring · failed · Nov 25, 1997 · Braero BAE1251000 · Hydraulic Pump (Electric/Engine), Main
  > (AUS) NO1 ENGINE HYDRAULIC PUMP HIGH PRESSURE FITTING `O' RING SEAL FAILED. LOSS OF HYDRAULIC FLUID.
- [SDR 97ZZZX2089](https://openairdocs.org/sdr/97ZZZX2089.md): Line · chafed through · Apr 1, 1997 · N514QS · Braero BAE1251000 · Pitot/Static System
  > FOUND LEFT PITOT HEAD (P1) LINE 'SAWED THROUGH' BY LEFT ELEVATOR CONTROL CABLE DURING INVESTIGATION OF AN AIRSPEED DISCREPANCY. REMOVED AND REPLACED LINE. LINE IS PART OF A 4-GANG CLUSTER RUNNING UNDER THE CENTER COCKPIT FLOOR. SUBMITTER STATED THE LINES AR
- [SDR 97ZZZX1757](https://openairdocs.org/sdr/97ZZZX1757.md): Switch · faulty · Mar 25, 1997 · N81HH · Braero BAE1251000 · Landing Gear Position and Warning
  > KISP - ON APPROACH (PART 91 - NO PASSENGERS) WHEN GEAR HANDLE LOWERED, DID NOT GET A GREEN LIGHT FOR THE NLG. WITH GEAR HANDLE DOWN AND NO GREEN LIGHT FOR THE NLG, THE ALTERNATE INDICATOR (PIN POSITION ON CENTER CONSOLE) WAS CHECKED. IT INDICATED NLG DOWN.
- [SDR 97ZZZX1321](https://openairdocs.org/sdr/97ZZZX1321.md): Lever Arm · gouged · Mar 5, 1997 · N514QS · Braero BAE1251000 · Elevator Control System
  > DURING A ROUTINE INSPECTION, FOUND ELEVATOR LEVER ARM (IPC 55-20-05-01, ITEM 370) GOUGED ON THE OUTBOARD SIDE APPROXIMATELY.5 INCH ABOVE ELEVATOR ROD ATTACHEMENT BOLT. DURING REMOVAL AND INSTALLATION OF THE TAIL ASSEMBLY BULLET FAIRING, (IPC 55-30-10-01, PAG
- [SDR 97ZZZX597](https://openairdocs.org/sdr/97ZZZX597.md): Line · cracked · Jan 10, 1997 · N525QS · Braero BAE1251000 · Waste Disposal System
  > 80 INCH LONG GALLEY DRAIN LINE WAS FOUND CRACKED FROM WATER EXPANSION. THIS LINE RUNS FROM GALLEY ALONG LOWER SIDE PLATES INSIDE CABIN AREA. ATTACH POINTS FOR LINE ONLY ALLOW A LEVEL INSTALLATION UNTIL JUST BEFORE IT ANGLES BELOW THE CABIN. THE CRACK WAS IN
- [SDR 97ZZZX35](https://openairdocs.org/sdr/97ZZZX35.md): Aux Valve · malfunction · Nov 11, 1996 · N520QS · Braero BAE1251000 · Cabin Pressure Control System
  > AUX VALVE WILL NOT STAY OPEN. FOUND MALFUNCTIONING AUX VALVE.
- [SDR 97DXTA088](https://openairdocs.org/sdr/97DXTA088.md): Duct · leaking · Nov 5, 1996 · N525QS · Braero BAE1251000 · Air Distribution System
  > FLT 68798 - AIRCRAFT WILL NOT PRESSURIZE IN FLIGHT WITH MAIN AIR VALVE, BUT WILL WITH AUX VALVE. FOUND CABIN AIR FLOW DUCT LEAKING. REMOVED AND REPLACED DUCT. (X)
- [SDR 97DXTA087](https://openairdocs.org/sdr/97DXTA087.md): Control Valve · wrong position · Nov 1, 1996 · N540QS · Braero BAE1251000 · Cabin Pressure Controller
  > AIRCRAFT WILL NOT PRESSURIZE IN FLIGHT. FOUND MANUAL CONTROL VALVE 'OPEN' DURING GROUND CHECK. REPOSITIONED VALVE TO 'CLOSED'. (X)
- [SDR 96ZZZX4387](https://openairdocs.org/sdr/96ZZZX4387.md): Longeron · cracked · Aug 15, 1996 · N514QS · Braero BAE1251000 · Engine Thrust Reverser
  > FOUND CRACK ON LEFT ENGINE THRUST REVERSER UPPER DOOR INBOARD LONGERON ASSEMBLY ABOUT TWO INCHES FROM BUMPER. LONGERON ASSY IS WEAK IN MACHINED AREA WHICH IS WHERE THE CRACK IS LOCATED. SUBMITTER STATED IF THE BUMPER IS MODIFIED TO EXTEND PAST THE WEAK AREA,
- [SDR 96ZZZX3724](https://openairdocs.org/sdr/96ZZZX3724.md): Longeron Assy · cracked · Jul 3, 1996 · N513QS · Braero BAE1251000 · Engine Thrust Reverser
  > FOUND CRACK ON LEFT ENGINE THRUST REVERSER UPPER DOOR INBOARD LONGERON ASSEMBLY, ABOUT 2 INCHES FROM BUMPER. LONGERON ASSEMBLY IS WEAK IN MACHINED AREA WHICH IS WHERE THE CRACK IS LOCATED.
- [SDR 98ZZZX118](https://openairdocs.org/sdr/98ZZZX118.md): Wire · damaged · Jun 28, 1996 · N548QS · Braero BAE1251000 · Auto Flight System Wiring
  > HOSE CLAMP HOLDING CUSTOM MADE AIRBOX TO PILOTS SIDE PANEL WAS POSITIONED SO THAT WORM SCREW OF CLAMP FOR SCREWDRIVER SLOT END WAS CUTTING INTO WIRES ON TERMINAL BLOCK MOUNTED BELOW BOX CAUSING FAILURE OF AUTOPILOT TRIM SYSTEM. THIS CONDITION EXISTED ON PILOT
- [SDR 96ZZZX3420](https://openairdocs.org/sdr/96ZZZX3420.md): Mask · torn · Jun 20, 1996 · N81AB · Braero BAE1251000 · Passenger Oxygen System
  > RUBBER FACE CUP TORN. FOUR EACH PASSENGER FACE MASKS. ALL TORN IN THE SAME LOCATION. FOUND DURING 12-MONTH INSPECTION.
- [SDR 96ZZZX1154](https://openairdocs.org/sdr/96ZZZX1154.md): Bolt · wrong length · Feb 26, 1996 · N100U · Braero BAE1251000 · Elevator Structure
  > DURING A RECENT 2,400 HOUR-INSPECTION, THE LT ELEVATOR UPPER MID-ATTACH HINGE SEAL BOLTS WERE REPLACED WITH 5 EACH, DHS 1465-2DD, PER MOD 253410A DRAWING. AT 84 HRS FROM INSP DURING A PILOT PREFLT CHECK, A BINDING, AND SUBSEQUENT INSP REVEALED AT EXTREME AFT
- [SDR 96ZZZX968](https://openairdocs.org/sdr/96ZZZX968.md): Relief Valve · leaking · Jan 26, 1996 · N533QS · Braero BAE1251000 · Fuel Storage
  > THE AIRCRAFT WAS DETERMINED TO HAVE LEAKING THERMAL RELIEF VALVE. ORDERED REPLACEMENT PART. RECEIVED 4 EACH NEW RELIEF VALVES. ALL 4 EACH LEAKED. SUBMITTER SUSPECTS SPRING IS WEAK OR POOR FIT OF PISTON.
- [SDR 96ZZZX19](https://openairdocs.org/sdr/96ZZZX19.md): Mask · torn · Dec 13, 1995 · N544QS · Braero BAE1251000 · Passenger Oxygen System
  > MASK RUBBER FACE CUP IS TORN. ON THIS ACFT, 6 MASKS WERE FOUND UNSERVICABLE. ALL MASKS HAD THE SAME DISCREPANCY. ONE NEW MASK WAS FOUND TORN PRIOR TO INSTALLATION, ITS MFG DATE WAS 6-95. P/N WAS SAME, BUT AT REV. U.
- [SDR 95ZZZX756](https://openairdocs.org/sdr/95ZZZX756.md): Hose · burned · Jan 9, 1995 · N535QS · Braero BAE1251000 · APU Engine Fuel and Control
  > FUEL FEED LINE FOR APU FOUND DURING INSPECTION. OUTSIDE FUEL SLEEVEING HAD 2 HOLES BURNED THROUGH. FIRE RETARDANT SLEEVE HAD ONE HOLE BURNED IN RED RUBBER COVERING. WAS NOT BURNED TO HOSE AT THIS TIME.
- [SDR 95ZZZX755](https://openairdocs.org/sdr/95ZZZX755.md): Line · burned · Jan 9, 1995 · N539QS · Braero BAE1251000 · APU Engine Fuel and Control
  > APU FUEL FEED LINE FOUND BURNED ON INSPECTION. OUTSIDE FUEL SLEEVEING HAD A HOLE BURNED THROUGH. FIRE RETARDANT SLEEVE HAD A HOLE BURNED INTO THE RED RUBBER COVERING. WAS NOT BURNED TO FUEL HOSE AT THIS TIME.
- [SDR 95ZZZX754](https://openairdocs.org/sdr/95ZZZX754.md): Line · burned · Jan 4, 1995 · N541QS · Braero BAE1251000 · APU Engine Fuel and Control
  > FOUND DURING PRE-FLIGHT - APU HOSE (FUEL FEED) WAS BURNED THROUGH THE PLASTIC SHIELD, AND THROUGH THE RUBBER INSULATION HALF WAY. CAUSE: LEFT ENGINE BLEED AIR AT MIXER VALVE IS BURNING THROUGH THE APU FUEL FEED LINE. NEED LINE ROUTED TO A DIFFERENT PATH.
- [SDR 95ZZZX753](https://openairdocs.org/sdr/95ZZZX753.md): Hose · burned · Jan 4, 1995 · N533QS · Braero BAE1251000 · APU Engine Fuel and Control
  > FOUND DURING PRE-FLIGHT. APU HOSE (FUEL FEED) WAS BURNED THROUGH THE PLASTIC SHIELD. THE FIRE RETARDANT COATING HAD NOT BEEN DAMAGED. CAUSE: HOSE LOCATED TOO CLOSE TO HOT AIR LINE. FIX: ROUTE LINE IN NEW POSITION.
- [SDR 95ZZZX518](https://openairdocs.org/sdr/95ZZZX518.md): Feed Line · burned · Jan 4, 1995 · N520QS · Braero BAE1251000 · APU Engine Fuel and Control
  > FOUND DURING PRE-FLIGHT. APU FUEL FEED HOSE WAS BURNED THROUGH THE PLASTIC SHIELD AND INTO THE HOSE INSULATION. BLEEDAIR FROM LEFT MIXER VALVE IS BURNING THE APU FUEL FEED LINE. NEED LINE ROUTED AWAY FROM BLEED AIR.

## 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 = 'BAE1251000'
ORDER BY difficulty_date DESC
```

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

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