# British Aerospace BAE 125-1000 - Type: Aircraft model (FAA registry) - Registry code: 1500288 - Manufacturer (registry): BRITISH AEROSPACE - Model: BAE 125-1000 - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 2 ยท Turbo-jet - Seats: 13 - Weight class: 12,500 to 19,999 lb - Certification: Not type certificated - Registered aircraft: 1 - Page: https://openairdocs.org/model/british-aerospace-bae-125-1000 Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker. ## ADs that may apply (OpenAirDocs) Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment. None matched. ## Registered aircraft (1) - [N518CJ](https://openairdocs.org/aircraft/N518CJ): [Skyview LLC](https://openairdocs.org/faa-owner/SKYVIEW%20LLC), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), S/N 259018 ## NTSB investigations None matched to aircraft with this model. ## FAA accident and incident reports None matched to aircraft with this model. ## Service difficulty reports (43) As reported by operators and repair stations, by the model named in the report. - [SDR 2016120500007](https://openairdocs.org/sdr/2016120500007), Dec 1, 2015: ACTUATOR. MALFUNCTIONED. 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 DOW - [SDR E0X2008F00007](https://openairdocs.org/sdr/E0X2008F00007), Oct 25, 2008: RUDDER. LOCKED. 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 - [SDR E0X2008F00004](https://openairdocs.org/sdr/E0X2008F00004), Jun 6, 2008: ENGINE. DAMAGED. AC DEPARTED AND SHORTLY AFTER DEPARTURE, SMOKE WAS NOTED IN CABIN WITH BAGGAGE SMOKE DETECTOR INDICATING SMOKE IN BAGGAGE COMPARTMENT. FLIGHT CREW DECLARED AN E - [SDR E0X2008F00005](https://openairdocs.org/sdr/E0X2008F00005), Jun 3, 2008: STARTER GEN. FAILED. 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 EM - [SDR E0X2007F00000](https://openairdocs.org/sdr/E0X2007F00000), Nov 19, 2007: SCAVENGE PORT. WORN. 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 - [SDR 2006FA0001159](https://openairdocs.org/sdr/2006FA0001159), Nov 17, 2006: PUMP. FAILED. 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) - [SDR 2006FA0001157](https://openairdocs.org/sdr/2006FA0001157), May 24, 2006: PUMP. FAILED. 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 S - [SDR 2006FA0001158](https://openairdocs.org/sdr/2006FA0001158), May 11, 2006: PUMP. FAILED. 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 - [SDR CA060425010](https://openairdocs.org/sdr/CA060425010), Apr 8, 2006: ENGINE. MALFUNCTIONED. 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 - [SDR CA060129015](https://openairdocs.org/sdr/CA060129015), Jan 3, 2006: LINE. FRACTURED. (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 - [SDR CA051104011](https://openairdocs.org/sdr/CA051104011), Oct 22, 2005: ENGINE. POWER LOSS. (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 - [SDR DXTA200500718](https://openairdocs.org/sdr/DXTA200500718), May 9, 2005: PROXIMITY SWITCH. MALFUNCTIONED. 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. REPLACE - [SDR CA050323005](https://openairdocs.org/sdr/CA050323005), Mar 7, 2005: LINE. CRACKED. (CAN) DURING INSPECTION FUEL WAS FOUND LEAKING FROM A CRACKED HMU-TO-FUEL FLOW TRANSMITTER LINE. THE ENGINE HAD PREVIOUSLY EXPERIENCED AN AIRFRAME STARTER-GENER - [SDR DXTA200500535](https://openairdocs.org/sdr/DXTA200500535), Jan 15, 2005: BLANKET. LOOSE. FIVE SECONDS AFTER ADDING TAKEOFF POWER REAR BAY OVERHEAT LOOKUP LIGHT ILLUMINATED. LIGHT WENT OUT TWO SECONDS AFTER THROTTLE REDUCED TO IDLE. RAN ENGINES. CHEC - [SDR DXTA200400472](https://openairdocs.org/sdr/DXTA200400472), Dec 8, 2004: ODOR. DETECTED. 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 - [SDR DXTA200400391](https://openairdocs.org/sdr/DXTA200400391), Sep 14, 2004: COALESCER BAG. DIRTY. 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 - [SDR DXTA200400389](https://openairdocs.org/sdr/DXTA200400389), Sep 11, 2004: SMOKE. DETECTED. 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 - [SDR DXTA200400319](https://openairdocs.org/sdr/DXTA200400319), Jun 5, 2004: A/C PACK. MALFUNCTIONED. 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 W - [SDR DXTA200300090](https://openairdocs.org/sdr/DXTA200300090), Aug 15, 2003: WIRE. BROKEN. 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 - [SDR DXTA200300056](https://openairdocs.org/sdr/DXTA200300056), Jul 3, 2003: ENGINE. MALFUNCTIONED. 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 - [SDR UXF2002F00000](https://openairdocs.org/sdr/UXF2002F00000), Nov 16, 2001: LAMP. INOPERATIVE. 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), Oct 6, 1998: P3 LINE. BROKE. PILOTS DISCREPANCY WAS NR 1 ENGINE TEMPORARILY LIMITED ABOVE CRUISE DETENT. REMOVED THE OUTBOARD INNER BYPASS ACCESS TO CHECK BLEED VALVES. UPON INVESTIGATION, - [SDR 98ZZZX3222](https://openairdocs.org/sdr/98ZZZX3222), Aug 1, 1998: TUBE. BROKEN. 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 POSSIB - [SDR AU971506](https://openairdocs.org/sdr/AU971506), Nov 25, 1997: O-RING. FAILED. (AUS) NO1 ENGINE HYDRAULIC PUMP HIGH PRESSURE FITTING `O' RING SEAL FAILED. LOSS OF HYDRAULIC FLUID. - [SDR 97ZZZX2089](https://openairdocs.org/sdr/97ZZZX2089), Apr 1, 1997: LINE. CHAFED THROUGH. FOUND LEFT PITOT HEAD (P1) LINE 'SAWED THROUGH' BY LEFT ELEVATOR CONTROL CABLE DURING INVESTIGATION OF AN AIRSPEED DISCREPANCY. REMOVED AND REPLACED LINE. LINE - [SDR 97ZZZX1757](https://openairdocs.org/sdr/97ZZZX1757), Mar 25, 1997: SWITCH. FAULTY. 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 N - [SDR 97ZZZX1321](https://openairdocs.org/sdr/97ZZZX1321), Mar 5, 1997: LEVER ARM. GOUGED. 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 ATTACHEME - [SDR 97ZZZX597](https://openairdocs.org/sdr/97ZZZX597), Jan 10, 1997: LINE. CRACKED. 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 L - [SDR 97ZZZX35](https://openairdocs.org/sdr/97ZZZX35), Nov 11, 1996: AUX VALVE. MALFUNCTION. AUX VALVE WILL NOT STAY OPEN. FOUND MALFUNCTIONING AUX VALVE. - [SDR 97DXTA088](https://openairdocs.org/sdr/97DXTA088), Nov 5, 1996: DUCT. LEAKING. 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. ( - [SDR 97DXTA087](https://openairdocs.org/sdr/97DXTA087), Nov 1, 1996: CONTROL VALVE. WRONG POSITION. 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), Aug 15, 1996: LONGERON. CRACKED. 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 WH - [SDR 96ZZZX3724](https://openairdocs.org/sdr/96ZZZX3724), Jul 3, 1996: LONGERON ASSY. CRACKED. 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 - [SDR 98ZZZX118](https://openairdocs.org/sdr/98ZZZX118), Jun 28, 1996: WIRE. DAMAGED. 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 TERMINA - [SDR 96ZZZX3420](https://openairdocs.org/sdr/96ZZZX3420), Jun 20, 1996: MASK. TORN. 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), Feb 26, 1996: BOLT. WRONG LENGTH. 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 - [SDR 96ZZZX968](https://openairdocs.org/sdr/96ZZZX968), Jan 26, 1996: RELIEF VALVE. LEAKING. THE AIRCRAFT WAS DETERMINED TO HAVE LEAKING THERMAL RELIEF VALVE. ORDERED REPLACEMENT PART. RECEIVED 4 EACH NEW RELIEF VALVES. ALL 4 EACH LEAKED. SUBMITTER SUSP - [SDR 96ZZZX19](https://openairdocs.org/sdr/96ZZZX19), Dec 13, 1995: MASK. TORN. 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 INSTALLATI - [SDR 95ZZZX756](https://openairdocs.org/sdr/95ZZZX756), Jan 9, 1995: HOSE. BURNED. 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 COVER - [SDR 95ZZZX755](https://openairdocs.org/sdr/95ZZZX755), Jan 9, 1995: LINE. BURNED. 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 COV - [SDR 95ZZZX754](https://openairdocs.org/sdr/95ZZZX754), Jan 4, 1995: LINE. BURNED. 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 A - [SDR 95ZZZX753](https://openairdocs.org/sdr/95ZZZX753), Jan 4, 1995: HOSE. BURNED. 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 CL - [SDR 95ZZZX518](https://openairdocs.org/sdr/95ZZZX518), Jan 4, 1995: FEED LINE. BURNED. 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 AP --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.