# British Aerospace HS-748-2A - Type: Aircraft model (FAA registry) - Registry code: 1500249 - Manufacturer (registry): BRITISH AEROSPACE - Model: HS-748-2A - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 2 · Turbo-prop - Seats: 52 - Weight class: 20,000 lb and over - Certification: Type certificated - Data sheet: [TCDS A24EU](https://openairdocs.org/tcds/A24EU) (OpenAirDocs) - Holder: BAE Systems (Operations) Limited - Registered aircraft: 2 - Page: https://openairdocs.org/model/british-aerospace-hs-748-2a 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. - [AD 2026-13-02](https://openairdocs.org/ad/2026-13-02): Navigation · Airbus Canada Limited Partnership 18, 49-46, 80-A and 555 more. Effective Jul 1, 2026 - [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023 - [AD 2018-23-12](https://openairdocs.org/ad/2018-23-12): Equipment/furnishings · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 180 more. Effective Dec 28, 2018 - [AD 2011-05-10](https://openairdocs.org/ad/2011-05-10): Flight Controls · BAE Systems ATP, HS 748 Series 2A and HS 748 Series 2B. Effective Mar 25, 2011 - [AD 2009-11-07](https://openairdocs.org/ad/2009-11-07): Fuel · BAE Systems HS 748 Series 2A and HS 748 Series 2B. Effective Jun 12, 2009 - [AD 2006-03-11](https://openairdocs.org/ad/2006-03-11): Elevator gust lock · BAE Systems HS 748 Series 2A and HS 748 Series 2B. Effective Feb 24, 2006 - [AD 2005-23-22](https://openairdocs.org/ad/2005-23-22): Rear pressure bulkhead · BAE Systems HS 748 Series 2A and HS 748 Series 2B. Effective Dec 6, 2005 - [AD 2005-20-34](https://openairdocs.org/ad/2005-20-34): Battery earth posts. · BAE Systems HS 748 Series 2A and HS 748 Series 2B. Effective Oct 27, 2005 - [AD 2005-19-26](https://openairdocs.org/ad/2005-19-26): Fuel cross feed system · BAE Systems ATP, HS 748 Series 2A and HS 748 Series 2B. Effective Oct 12, 2005 - [AD 2005-19-13](https://openairdocs.org/ad/2005-19-13): Nose landing gear (NLG) · BAE Systems HS 748 Series 2A and HS 748 Series 2B. Effective Oct 6, 2005 - [AD 99-19-13](https://openairdocs.org/ad/99-19-13): AFM - Limitations Section - Ice Protection System · BAE Systems HS 748 Series 2A and HS 748 Series 2B. Effective Dec 27, 1999 - [AD 98-07-22](https://openairdocs.org/ad/98-07-22): AFM - Limitations Section - Stop Lever · BAE Systems HS 748 Series 2A and HS 748 Series 2B. Effective Apr 16, 1998 - [AD 98-06-09](https://openairdocs.org/ad/98-06-09): Inspect Aileron Operating Arm Bracket · BAE Systems HS 748 Series 2A and HS 748 Series 2B. Effective Mar 30, 1998 - [AD 98-03-17](https://openairdocs.org/ad/98-03-17): Inspect Aileron, Rudder and Elevator Gust Locks · BAE Systems HS 748 Series 2A and HS 748 Series 2B. Effective Feb 23, 1998 - [AD 98-01-05](https://openairdocs.org/ad/98-01-05): Aileron Cable Support Block · BAE Systems HS 748 Series 2A and HS 748 Series 2B. Effective Jan 15, 1998 - [AD 97-25-13](https://openairdocs.org/ad/97-25-13): Inspect Main Hydraulic Accumulator for Corrosion · BAE Systems ATP, HS 748 Series 2A and HS 748 Series 2B. Effective Jan 14, 1998 - [AD 97-26-05](https://openairdocs.org/ad/97-26-05): Inspect Inspection Locations · BAE Systems HS 748 Series 2A and HS 748 Series 2B. Effective Jan 2, 1998 - [AD 97-23-03](https://openairdocs.org/ad/97-23-03): Bearing Cap Attachment Bolts · BAE Systems HS 748 Series 2A and HS 748 Series 2B. Effective Nov 19, 1997 - [AD 97-20-05](https://openairdocs.org/ad/97-20-05): Aileron Cable Pulley Guard & Rubbing Strips · BAE Systems HS 748 Series 2A and HS 748 Series 2B. Effective Oct 15, 1997 - [AD 96-25-12](https://openairdocs.org/ad/96-25-12): Auxiliary Power Units · BAE Systems HS 748 Series 2A, HS 748 Series 2B, 707-100 Long Body and 74 more. Effective Jan 13, 1997 - [AD 96-20-09](https://openairdocs.org/ad/96-20-09): Flight Control Cable Tension Regulators · BAE Systems HS 748 Series 2A and HS 748 Series 2B. Effective Oct 25, 1996 - [AD 96-09-20](https://openairdocs.org/ad/96-09-20): AFM - Icing · BAE Systems HS 748 Series 2A and HS 748 Series 2B. Effective Jun 11, 1996 - [AD 94-23-08](https://openairdocs.org/ad/94-23-08): Nose Landing Gear and Main Landing Gear · BAE Systems HS 748 Series 2A and HS 748 Series 2B. Effective Dec 6, 1994 - [AD 88-06-01](https://openairdocs.org/ad/88-06-01): Main Landing Gear · BAE Systems HS 748 Series 2A and HS 748 Series 2B. Effective Apr 18, 1988 - [AD 88-05-03](https://openairdocs.org/ad/88-05-03): Rudder Lock Control · BAE Systems HS 748 Series 2A and HS 748 Series 2B. Effective Apr 6, 1988 - [AD 88-03-02](https://openairdocs.org/ad/88-03-02): Lower Wing Skins · BAE Systems HS 748 Series 2A and HS 748 Series 2B. Effective Mar 1, 1988 - [AD 87-26-07](https://openairdocs.org/ad/87-26-07): Escape Hatch Locking Mechanism · BAE Systems HS 748 Series 2A and HS 748 Series 2B. Effective Feb 1, 1988 - [AD 87-26-06](https://openairdocs.org/ad/87-26-06): Hydraulic Brake Accumulators · BAE Systems HS 748 Series 2A and HS 748 Series 2B. Effective Feb 1, 1988 - [AD 87-25-13](https://openairdocs.org/ad/87-25-13): Nose Landing Gear · BAE Systems HS 748 Series 2A and HS 748 Series 2B. Effective Jan 25, 1988 - [AD 87-25-11](https://openairdocs.org/ad/87-25-11): Bearing Installations · BAE Systems HS 748 Series 2A and HS 748 Series 2B. Effective Jan 25, 1988 - [AD 87-25-07](https://openairdocs.org/ad/87-25-07): Engine Support Structure · BAE Systems HS 748 Series 2A and HS 748 Series 2B. Effective Jan 19, 1988 - [AD 87-25-06](https://openairdocs.org/ad/87-25-06): Jet Pipe Manifold · BAE Systems HS 748 Series 2A and HS 748 Series 2B. Effective Jan 19, 1988 - [AD 87-22-05](https://openairdocs.org/ad/87-22-05): Freight Door Lever · BAE Systems HS 748 Series 2A and HS 748 Series 2B. Effective Nov 13, 1987 - [AD 86-14-09](https://openairdocs.org/ad/86-14-09): Microswitch Rocker Arm Assemblies · BAE Systems HS 748 Series 2A and HS 748 Series 2B. Effective Aug 4, 1986 - [AD 86-10-06](https://openairdocs.org/ad/86-10-06): Overwing Escape Hatches · BAE Systems HS 748 Series 2A and HS 748 Series 2B. Effective Jun 16, 1986 - [AD 86-09-04](https://openairdocs.org/ad/86-09-04): Emergency Lighting System · BAE Systems HS 748 Series 2A and HS 748 Series 2B. Effective May 26, 1986 - [AD 86-07-05](https://openairdocs.org/ad/86-07-05): Wing Structure · BAE Systems HS 748 Series 2A and HS 748 Series 2B. Effective May 8, 1986 - [AD 86-06-05](https://openairdocs.org/ad/86-06-05): Windshield Actuating Arm · BAE Systems HS 748 Series 2A and HS 748 Series 2B. Effective May 2, 1986 - [AD 85-03-05](https://openairdocs.org/ad/85-03-05): Baggage Door · BAE Systems HS 748 Series 2A and HS 748 Series 2B. Effective Mar 11, 1985 - [AD 83-26-01](https://openairdocs.org/ad/83-26-01): Unsafe Condition Prevention · BAE Systems HS 748 Series 2A and HS 748 Series 2B. Effective Jan 30, 1984 - [AD 83-24-08](https://openairdocs.org/ad/83-24-08): Wing Structure · BAE Systems HS 748 Series 2A. Effective Jan 15, 1984 - [AD 83-26-04](https://openairdocs.org/ad/83-26-04): Lock Levers Replacement · BAE Systems HS 748 Series 2A and HS 748 Series 2B. Effective Jan 11, 1984 - [AD 83-24-01](https://openairdocs.org/ad/83-24-01): Wing Structure · BAE Systems HS 748 Series 2A. Effective Dec 23, 1983 - [AD 83-23-06](https://openairdocs.org/ad/83-23-06): Engine Subframe Struts · BAE Systems HS 748 Series 2A and HS 748 Series 2B. Effective Dec 15, 1983 - [AD 83-17-03](https://openairdocs.org/ad/83-17-03): Rib/Stringer Bracket Fasteners · BAE Systems HS 748 Series 2A. Effective Sep 19, 1983 - [AD 83-15-01](https://openairdocs.org/ad/83-15-01): Relay Replacement Check · BAE Systems HS 748 Series 2A. Effective Aug 1, 1983 - [AD 82-25-06](https://openairdocs.org/ad/82-25-06): Cabin Wiring · BAE Systems HS 748 Series 2A and HS 748 Series 2B. Effective Dec 6, 1982 - [AD 82-19-04](https://openairdocs.org/ad/82-19-04): Overwing Exit Panel · BAE Systems HS 748 Series 2A. Effective Sep 28, 1982 - [AD 81-15-52 R1](https://openairdocs.org/ad/81-15-52-R1): Securing Of Entry/Cargo Doors · BAE Systems HS 748 Series 2A and HS 748 Series 2B. Effective Sep 9, 1981 - [AD 77-23-02](https://openairdocs.org/ad/77-23-02): Propeller Feathering System · BAE Systems HS 748 Series 2A. Effective Dec 7, 1977 Historical (superseded or no longer in force): - [AD 74-08-09 R2](https://openairdocs.org/ad/74-08-09-R2) (historical): Waste Receptacles · Aero Spacelines 377, 377MG, 377SGT and 268 more. Effective Jul 29, 1996 All 54: https://openairdocs.org/model/british-aerospace-hs-748-2a/ads.md ## Registered aircraft (2) - [N748FM](https://openairdocs.org/aircraft/N748FM): [Starling Aviation Services LLC](https://openairdocs.org/faa-owner/STARLING%20AVIATION%20SERVICES%20LLC), [Lewes, DE](https://openairdocs.org/faa-place/DE/Lewes), S/N 1561 - [N748YK](https://openairdocs.org/aircraft/N748YK): [Starling Aviation Services LLC](https://openairdocs.org/faa-owner/STARLING%20AVIATION%20SERVICES%20LLC), [Lewes, DE](https://openairdocs.org/faa-place/DE/Lewes), S/N 1701 ## NTSB investigations None matched to aircraft with this model. ## FAA accident and incident reports None matched to aircraft with this model. ## Service difficulty reports (190, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR CA190801002](https://openairdocs.org/sdr/CA190801002), Jul 30, 2019: CABLE. BROKEN. (CAN) DURING CLIMB THE GEAR WOULD NOT FULLY RETRACT. WHEN THE NORMAL GEAR DOWN SELECTION WAS DONE ONLY THE NOSE GEAR WENT TO LOCKED POSITION. AN EMERGENCY LOWER - [SDR CA160304004](https://openairdocs.org/sdr/CA160304004), Feb 12, 2016: BLADE. DAMAGED. (CAN) DURING START THE ENGINE STOPPED ACCELERATING AND A LOUD THUMP WAS HEARD AND UPON FURTHER INVESTIGATION SMOKE WAS OBSERVED COMING FROM THE ENGINE AND THE E - [SDR CA151005001](https://openairdocs.org/sdr/CA151005001), Oct 2, 2015: WIRE. CHAFED. (CAN) AIRCRAFT DECLARED AN EMERGENCY AFTER SHUTTING DOWN NR 1 ENGINE IN FLIGHT AFTER ENGINE FIRE WARNING LIGHT. CREW BLEW THE 2 FIRE EXTINGUISHER BOTTLES, BUT L - [SDR CA150528003](https://openairdocs.org/sdr/CA150528003), May 26, 2015: CONNECTOR. SHORTED. (CAN) DURING THE TAKEOFF ROLL THE FLIGHT CREW NOTICED THE FFP STOP REMOVED LIGHTS FOR BOTH ENGS REMAINED ILLUMINATED. THE FLIGHT CREW ABORTED THE TAKEOFF & TAXI - [SDR CA141120026](https://openairdocs.org/sdr/CA141120026), Nov 15, 2014: WIRE. FAULTED. (CAN) LT ENGINE FIRE BELL WENT OFF IN CRUISE. VISUALLY CONFIRMED FALSE INDICATION. LANDED, MAINTENANCE CONFIRMED FAULTY FIRE WIRE, SYS TESTED AND SERVICEABLE. - [SDR CA141003001](https://openairdocs.org/sdr/CA141003001), Sep 30, 2014: PUMP. FAILED. (CAN) ON TAKEOFF ROLL AT 75 KTS, NR 2 ENGINE LOST POWER AND SHUTDOWN. CREW ABORT TAKEOFF WITH NO INCIDENT. FOUND NR 2 ENGINE FUEL PUMP FAULTY, PUMP REPLACED AND - [SDR CA140414008](https://openairdocs.org/sdr/CA140414008), Apr 14, 2014: SKIN. CORRODED. (CAN) RIGHT MLG PIVOT BRACKET REMOVED DUE TO CRACK FOUND DURING PERIOD 19 INSPECTION. AFTER REMOVAL OF THE PIVOT BRACKET AND CLEANING OF THE LOWER WING SKIN HID - [SDR CA131107008](https://openairdocs.org/sdr/CA131107008), Nov 4, 2013: LINE. LEAKING. (CAN) HYDRAULIC PUMP AND LOW BRAKE PRESSURE LIGHT ILLUMINATED. COMPLETED EMERGENCY LANDING AND FOUND HYDRAULIC LINE LEAKING ON RT MAIN GEAR JACK UPLINE. ONCE TA - [SDR CA130507002](https://openairdocs.org/sdr/CA130507002), May 6, 2013: PROBE. UNKNOWN. (CAN) OVERHEAT AND FIRE WARNING LIGHTS WOULD NOT COME ON WITH HEAT TEST OF JANITROL HEATER SYS. FOUND THERE ARE 2 TYPES OF THERMOSTATS THAT CAN BE USED. 1 HAS A - [SDR CA130430017](https://openairdocs.org/sdr/CA130430017), Apr 29, 2013: BRAKE. FAILED. (CAN) UPON LANDING FLIGHT CREW NOTICED THE AIRCRAFT WOULD NOT TAXI UNDER NORMAL TAXI POWER SETTINGS. THE AIRCAFT WAS SHUT DOWN ON THE RUNWAY AND TOWED BY MAINTE - [SDR CA130422007](https://openairdocs.org/sdr/CA130422007), Apr 22, 2013: SPAR. CORRODED. (CAN) LOCALIZED CORROSION FOUND DURING INSPECTION, EXFOLIATION OF FWD FACE UPPER REAR SPAR, BOOM, ANGLE. - [SDR CA130304009](https://openairdocs.org/sdr/CA130304009), Mar 3, 2013: BLADE. MISSING. (CAN) ENGINE SN 13370, FOUND HP TURBINE BLADE MISSING DURING VISUAL INSPECTION. THERE SEEMS TO BE A TREND AS THIS IS THE 4TH HP TURBINE BLADE FOUND MISSING OVER - [SDR CA130210001](https://openairdocs.org/sdr/CA130210001), Jan 31, 2013: CASE. DAMAGED. (CAN) DURING CRUISE FLIGHT, 16,000 FT, THE PILOTS OBSERVED THE PORT HYD SYS LOW FLOW LIGHT ILLUMINATED, FOLLOWED BY THE STARBOARD HYD SYS LOW FLOW LIGHT ILLUMIN - [SDR CA130125008](https://openairdocs.org/sdr/CA130125008), Jan 21, 2013: LINE. LEAKING. (CAN) DURING CRUSE AT 14,000 FT, THE PORT LOW FLOW HYDRAULIC LIGHT ILLUMINATED, FOLLOWED WITHIN 60 SECONDS BY THE STARBOARD LOW FLOW HYDRAULIC LIGHT. APPROXIMAT - [SDR CA121109015](https://openairdocs.org/sdr/CA121109015), Nov 8, 2012: GENERATOR. SEIZED. (CAN) DURING THE TAKEOFF ROLL, ENGINE NR 1 DC GENERATOR TRIPPED DROPPED OFF LINE. THE PILOTS ABORTED THE TAKEOFF AND RETURNED TO THE TERMINAL. ATTEMPTS TO PUT T - [SDR CA121109014](https://openairdocs.org/sdr/CA121109014), Nov 7, 2012: OIL COOLER. LEAKING. (CAN) ACFT DEPARTED AIRPORT, APPROXIMATELY 15 MINUTES AFTER TAKEOFF, ENGINE NR 2 OIL PRESSURE GAUGE STARTED TO FLUTTER AND THE LOW OIL PRESURE LIGHT ILLUMINATED - [SDR CA120525008](https://openairdocs.org/sdr/CA120525008), May 18, 2012: SWITCH. MALFUNCTIONED. (CAN) DURING TAKEOFF ROLL, THE RT ENGINE AUTOFEATHERED AT LOW SPEEED. MAINTENANCE FOUND THE LOW TORQUE SWITCH HAD FAILED, CAUSING THE PROPELLER TO AUTOFEATHER. - [SDR CA120301003](https://openairdocs.org/sdr/CA120301003), Feb 28, 2012: VALVE. LEAKING. (CAN) FLIGHT CREW EXPERIENCED TOTAL LOSS OF HYD PRESSURE DURING FLIGHT. THE ACFT LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL FOUND THE HYDRAULIC CUT OUT VALV - [SDR CA110803022](https://openairdocs.org/sdr/CA110803022), Jul 25, 2011: VALVE. CRACKED. UPON LANDING GEAR EXTENSION IN PREPERATION FOR LANDING, CREW NOTICED A PRESSURE DROP IN THE HYD SYS. AFTER NORMAL LANDING, WHEN ACFT WAS PARKED ON RAMP, HYD FLU - [SDR CA110405003](https://openairdocs.org/sdr/CA110405003), Apr 1, 2011: IMPELLER. CRACKED. (CAN) HIGH PRESSURE IMPELLER FAILURE, SECTION APPROX 40 X 40 MM RELEASED FROM QTY 1 VANE. DOWNSTREAM IMPACT DAMAGE TO ADDITIONAL VANES. ITEM HAS BEEN REMOVED FR - [SDR CA110208006](https://openairdocs.org/sdr/CA110208006), Feb 2, 2011: LANDING GEAR. FAILED. (CAN) UPON LANDING THE MAIN GEAR HAD TO BE LOWERED BY EMERGENCY SELECTION. ON LANDING THE CREW HAD 3 GREEN INDICATION. - [SDR CA100603004](https://openairdocs.org/sdr/CA100603004), May 27, 2010: FLEX HOSE. RUPTURED. (CAN) AFTER TAKEOFF, THE CREW OF ANT 207 SELECTED THE LANDING GEAR TO RETRACT. THE LANDING GEAR RETRACTED PART WAY AND THE HYDRAULIC PUMP LOW PRESSURE LIGHTS IL - [SDR CA090615010](https://openairdocs.org/sdr/CA090615010), Jun 14, 2009: ENGINE. MAKING METAL. (CAN) DURING CLIMB, RT OIL PRESSURE LIGHT ILLUMINATED AND OIL PRESSURE WAS CONFIRMED TO BE LOW. ENG WAS SHUTDOWN AS A PRECAUTIONARY MEASURE. ACFT WAS LANDED WIT - [SDR CA090605009](https://openairdocs.org/sdr/CA090605009), Jun 1, 2009: BOLT. BROKEN. (CAN) BOLT THAT ACTUATED THE SWITCH FOR GEAR DOWN AND LOCKED, BROKE. THE BOLT BREAKING CAUSED THE MLG INDICATION TO SHOW IN TRANSIT AND THE MECHANICAL LANDING G - [SDR CA090519009](https://openairdocs.org/sdr/CA090519009), May 17, 2009: OIL COOLER. LEAKING. (CAN) DURING THE CLIMB, RT ENGINE LOST OIL PRESSURE WITH ILLUMINATION OF THE WARNING LIGHT. THE CREW SHUTDOWN THE RT ENGINE AND RETURNED TO BASE. UPON INVESTIGA - [SDR CA090213004](https://openairdocs.org/sdr/CA090213004), Feb 3, 2009: INDICATOR. LEAKING. (CAN) SHORTLY AFTER DEPARTURE, THE CREW OBSERVED A PORT HYD PUMP INDICATION LIGHT WHICH REMAINED ILLUMINATED WITH THE MAIN SYS CYCLING EVERY 5 SECONDS. THE ACFT - [SDR CA090211001](https://openairdocs.org/sdr/CA090211001), Jan 30, 2009: CONE. CRACKED. VISUAL INSPECTION DURING "A-CHECK" (WITH FLASHLIGHT) REVEALED LARGE CRACK IN CIRCUMFERENCE OF EXHAUST UNIT INNER CONE. CLOSER INSPECTION (CRAWLED UP JET-PIPE) I - [SDR CA081215001](https://openairdocs.org/sdr/CA081215001), Dec 11, 2008: DOOR. OBSTRUCTED. (CAN) AFTER DEPARTURE, THE CREW OBSERVED A PRESSURE LOCK NOT ENGAGED INDICATION FOR THE MAIN PAX DOOR. THE ACFT RETURNED TO POINT OF DEPARTURE AND LANDED WITHOU - [SDR CA090604004](https://openairdocs.org/sdr/CA090604004), Nov 3, 2008: BLADES. FAILED. (CAN) DURING NORMAL COMPANY OPERATIONS A VIBRATION WAS DETECTED COMING FROM RT ENG. UPON INVESTIGATION IT WAS FOUND THAT 1ST STAGE TURBINE ASSY HAD EXPERIENCED - [SDR CA080919007](https://openairdocs.org/sdr/CA080919007), Sep 17, 2008: SUPERCHARGER. INOPERATIVE. (CAN) WHILE IN CRUISE FLIGHT, ENROUTE, CREW NOTICED A STRANGE ODOR COMING FROM THE CABIN. CREWMAN ONBOARD WENT TO LOOK IN THE CABIN AND NOTICED TEMPERATURE IN T - [SDR CA080729006](https://openairdocs.org/sdr/CA080729006), Jul 27, 2008: COVER. LEAKING. (CAN) WHILE ENROUTE FROM YBK TO YTH FAMO EXPERIENCED LOSS OF HYDRAULIC PRESSURE. AN EMERGENCY WAS DECLARED AND THE ACFT DIVERTED TO YTH WHERE AN UNEVENTFUL LAND - [SDR CA080801001](https://openairdocs.org/sdr/CA080801001), Jul 26, 2008: FLEX LINE. CHAFED. (CAN) ON APPROACH, THE CREW OBSERVED A LOSS OF HYDRAULIC PRESS AFTER GEAR WAS SELECTED DOWN. THE ACFT LANDED WITHOUT FURTHER INCIDENT. MAINT IDENTIFIED THE HYDR - [SDR CA080313004](https://openairdocs.org/sdr/CA080313004), Mar 11, 2008: ENGINE. MALFUNCTIONED. DURING APPROACH IN ICING CONDITIONS AND HEAVY PRECIPITATION, WHEN THE PILOT THROTTLED BACK, ENGINE NR 2 FLAMED OUT AND AUTO FEATHERED. THE PILOT DID NOT ATTEMPT - [SDR CA071112003](https://openairdocs.org/sdr/CA071112003), Nov 9, 2007: FIRE LOOP. FAULTY. (CAN) AFTER TAKEOFF, ENGINE NR 1 FIRE-WARNING ALARM WENT OFF. THE FLIGHT CREW INFORMED TOWER AND RETURNED TO AIRPORT. A HOLE WAS FOUND IN THE FLEXIBLE DUCT AT T - [SDR CA071001005](https://openairdocs.org/sdr/CA071001005), Sep 28, 2007: IMPELLER. DAMAGED. (CAN) WHILE ON CLIMB AFTER DEPARTING, THE WAS A BANG FROM THE RT ENGINE, TOTAL LOSS OF POWER AND FIRE WARNING. THE FWD PART OF THE ENGINE WAS SEEN TO BE ON FIRE - [SDR CA070910003](https://openairdocs.org/sdr/CA070910003), Sep 6, 2007: LINE. RUPTURED. (CAN) 10 MINUTES PRIOR TO LANDING, THE PORT AND STARBOARD HYDRAULIC PUMP LIGHTS ILLUMINATED WITH MAIN PRESSURE DEPLETING AND STOPPING AT ACCUMULATOR PRESSURE. T - [SDR CA070905005](https://openairdocs.org/sdr/CA070905005), Aug 30, 2007: LEVER. FAILED. (CAN) AFTER ARRIVING AT AIRPORT, THE AIRCRAFT ROLLED FORWARD AFTER THE PARK BRAKE WAS APPLIED WITH ENGINES STILL RUNNING AND THEN CONTACTED GROUND EQUIPMENT. MA - [SDR CA070905002](https://openairdocs.org/sdr/CA070905002), Aug 28, 2007: ALTERNATOR. INOPERATIVE. (CAN) AFTER DEPARTING AND ENROUTE, THE CREW OBSERVED NR 2 ALTERNATOR HAD TRIPPED OFFLINE AND DID NOT RESET. THE AIRCRAFT RETURNED TO POINT OF DEPARTURE AND LAND - [SDR CA070824005](https://openairdocs.org/sdr/CA070824005), Jul 30, 2007: LINE. LEAKING. (CAN) WHILE FLYING BOTH HYDRAULIC PUMP LIGHTS CAME ON. THE AIRCRAFT LANDED USING ITS BACKUP SYSTEM. IT WAS FOUND THAT THE HYDRAULIC LINE THAT RUNS BETWEEN THE P - [SDR CA070712002](https://openairdocs.org/sdr/CA070712002), Jul 10, 2007: LINE. PERFORATED. (CAN) AFTER DEPARTING, THE CREW OBSERVED BOTH THE LT AND RT HYDRAULIC PRESSURE LOSS INDICATION LIGHTS WERE ILLUMINATED. THE AIRCRAFT DIVERTED AND LANDED WITHOUT - [SDR CA070507011](https://openairdocs.org/sdr/CA070507011), May 4, 2007: WIRE HARNESS. DAMAGED. (CAN) DEPARTING THE LANDING GEAR SELECT LEVER WOULD NOT MOVE TO THE GEAR UP POSITION. THE AIRCRAFT RETURNED TO POINT OF DEPARTURE AND LANDED WITHOUT FURTHER PRO - [SDR CA070319001](https://openairdocs.org/sdr/CA070319001), Mar 12, 2007: PRESSURE SWITCH. MALFUNCTIONED. (CAN) DURING DEPARTURE THE AIRCRAFT`S HEATER FAILED AND THE CREW WAS UNABLE TO RESTART THE HEATER. THE AIRCRAFT RETURNED TO POINT OF DEPARTURE AND LANDED WITHOU - [SDR CA070309001](https://openairdocs.org/sdr/CA070309001), Mar 3, 2007: VALVE. MALFUNCTIONED. (CAN) AC WAS IN CRUISE FLIGHT, WHEN THE FLIGHT CREW OPENED THE FUEL CROSSFEED VALVE TO BALANCE THE FUEL LOAD. WHEN THE FLIGHT CREW SELECTED THE LT BOOST PUMPS T - [SDR CA070131008](https://openairdocs.org/sdr/CA070131008), Jan 31, 2007: LINE. LEAKING. (CAN) IN CRUISE FLIGHT (30 MINUTES AFTER DEPARTURE THE FLIGHT CREW OBSERVED NR 1 AND NR 2 LOW HYDRAULIC PRESSURE LIGHTS ILLUMINATED. THE FLIGHT CREW RETURNED TO - [SDR CA070130002](https://openairdocs.org/sdr/CA070130002), Jan 23, 2007: INDICATOR. INOPERATIVE. (CAN) ON TAKEOFF ROLL THE CREW REJECTED THE TAKEOFF AT 85 KTS WITH NO INDICATION ON FIRST OFFICERS SIDE. MAINTENANCE CONDUCTED A PURGE OF THE SYSTEM AND CARRIED - [SDR CA070111012](https://openairdocs.org/sdr/CA070111012), Jan 11, 2007: WINDOW. CRACKED. (CAN) DURING CLIMB THE FIRST OFFICERS MAIN WINDOW CRACKED. THE AIRCRAFT RETURNED TO POINT OF DEPARATURE WITHOUT FURTHER PROBLEM. MAINTENANCE REPLACED THE WINDOW - [SDR CA070119003](https://openairdocs.org/sdr/CA070119003), Jan 9, 2007: INDICATOR. LEAKING. (CAN) ENROUTE, THE CREW OBSERVED BOTH HYD SYSTEMS INDICATING APPROXIMATELY 1200 PSI WITH LOW FLOW LIGHTS ON. THE CREW CONTINUED WHERE ON APPROACH THE HYDRAULIC - [SDR CA061219029](https://openairdocs.org/sdr/CA061219029), Dec 10, 2006: FUEL. CONTAMINATED. (CAN) PILOT OBSERVED ENGINE NR 1 FUEL FILTER DE-ICING WARNING LIGHT ILLUMINATED IN CRUISE FLIGHT. SHORTLY AFTER APPLYING FUEL HEAT, ENGINE NR 1 QUIT. PILOT FEAT - [SDR CA061128002](https://openairdocs.org/sdr/CA061128002), Nov 23, 2006: INDICATOR. FAILED. (CAN) DURING DEPARTURE THE CAPTAINS HORIZON FAILED ON CLIMB OUT. THE AIRCRAFT RETURNED TO POINT OF DEPARTURE WITHOUT FURTHER PROBLEM. MAINTENANACE REPLACED THE - [SDR CA061122007](https://openairdocs.org/sdr/CA061122007), Nov 11, 2006: INDICATOR. FAILED. (CAN) DEPARTING THE CAPT`S HORIZON FAILED DURING TAKE-OFF. THE AIRCRAFT RETURNED TO POINT OF DEPARTURE WITHOUT INCIDENT. MAINTENANCE REPLACED THE GYRO AND THE A All 190: https://openairdocs.org/model/british-aerospace-hs-748-2a/reports.md ## STCs that may be installed (OpenAirDocs) (11) Approved for this model: the STC's model list names it on its data sheet, or a series that includes it. In force first, then newest. The registry doesn't record which STCs an aircraft has. - [STC ST12461IB](https://openairdocs.org/stc/ST12461IB): Installation of Cockpit Voice Recorder with optional RIPS Upgrade. Mid- Canada Mod Center - [STC SA2622NM](https://openairdocs.org/stc/SA2622NM): Installation of Precise Flight Pulselite Control Unit in landing/taxi system. (767-200 B17) (DHC-8 101). Precise Flight Inc - [STC SA3956NM](https://openairdocs.org/stc/SA3956NM): Installation of Floor Proximity Emergency Escape Path Marking System. Bruce Aerospace Inc - [STC ST00098IB](https://openairdocs.org/stc/ST00098IB): Introduction of ADS-B Out. STC Twenty One Limited - [STC ST02632LA](https://openairdocs.org/stc/ST02632LA): Modification to replace the existing Mode S Transponder system with ACSS NXT-700 Mode S Transponder with ADS-B Out and optionally install ACSS NXG-900 GPS as a position source for ADS-B Out. Aviation Communications and Surveillance Systems - [STC SA302WE](https://openairdocs.org/stc/SA302WE): Incorporate a de-icing system (as manufactured by applicant) externally on Rotol propeller spinner as an alternate to Dowty Rotol internal elements. If applied to original spinner, Montgomery Systems Tech., Inc. P/N 72196-2 will apply. If applied to a new aluminum nose spinner P/N 72196-1 will apply. Dowty Rotol Service Bulletin Section 61-170 pages 1 and 2 outlines a revised spinner de-icing system. This is a Napier external system. Approval of the A.R.B. is indicated. (Continued on page 3). ROBERT W. MURRAY - [STC SA4574NM](https://openairdocs.org/stc/SA4574NM): Installation of a de-icing system on the Rolls Royce P/N RK29954A or P/N RK48279A (MO) 1800 engine inlet cowl. ROBERT W. MURRAY - [STC SA2944WE](https://openairdocs.org/stc/SA2944WE): Installation of DeVore emblem lights on horizontal stabilizer tips. DeVore Aviation Corporation of America, a New Mexico Corporation - [STC ST00291NY](https://openairdocs.org/stc/ST00291NY): Installation of windscreen heat relay replacement. Northern Aero Industries - [STC SA45GL](https://openairdocs.org/stc/SA45GL): Install AMF inverter MGH 549-1. Leland Electrosystems, Inc - [STC SA125GL](https://openairdocs.org/stc/SA125GL): Installation of Plessey Company P/N 612-1-39863 ground proximity warning system. Air Illinois, Inc ## PMA parts (OpenAirDocs) (30) Current parts manufacturer approvals (PMA): parts the FAA has approved companies to make as replacements or modifications. Each record lists its models as free text; OpenAirDocs matched them to this model on its data sheet, so check the FAA record before relying on it. Newest first. - [LM114848](https://drs.faa.gov/browse/excelExternalWindow/20BCFA269751D88186257FC5006D9F32.0001): CUP. Timken Corporation · PMA PQ4105CE · Replaces LM114848 · May 24, 2016 - [LM114848](https://drs.faa.gov/browse/excelExternalWindow/BAC3B32C705C21FF86257D2A0057462C.0001): CUP. Timken Corporation · PMA PQ4105CE · Replaces LM114848 · Jun 29, 2014 - [GMD65BE2966](https://drs.faa.gov/browse/excelExternalWindow/A9C34C05AB12C60686257A360072463F.0001): Hinge. General Machine - Diecron Inc · PMA PQ1586CE · Replaces Hawker Siddeley P/N 65BE2966 · May 24, 2012 - [AD-MISC066](https://drs.faa.gov/browse/excelExternalWindow/4ED7BED5020A0E8D8625760B0069B117.0001): Battery. Aero Design Inc · PMA PQ1465CE · Replaces Grimes Aerospace MISC066, S140… · Jul 8, 2009 - [All parts listed on the Master Drawing List (MDL) No. MDL-748](https://drs.faa.gov/browse/excelExternalWindow/48AE2F72847D7EB586257546006451E3.0001): Floor Proximity Emergency Escape Path Marking Systems. Bruce Aerospace Incorporated · PMA PQ1287NM · Modification part · Dec 8, 2008 - [2013-BR](https://drs.faa.gov/browse/excelExternalWindow/25FEB4C02EF5E7B3862575460064AFB2.0001): Battery Assembly. Bruce Aerospace Incorporated · PMA PQ1287NM · Replaces 2013-1A · Dec 8, 2008 - [7017238-1WD](https://drs.faa.gov/browse/excelExternalWindow/3C4EBE27B98B28E0862572910067A48B.0001): Bearing, Ball, Annular. Wencor LLC (formerly Dixie Aerospace LLC) · PMA PQ1630CE · Replaces Honeywell (Sperry) 7017238-1… · Jan 17, 2007 - [N131858M](https://drs.faa.gov/browse/excelExternalWindow/46352A7933935A6D852570490054D7C9.0001): Brush Electrical Contact. Miraj Corporation · Replaces Lucas N131858 · Mar 17, 2003 - [AD-4063P](https://drs.faa.gov/browse/excelExternalWindow/330D32BA16BC0B4685257038006B8DCE.0001): Battery. Aero Design Inc · Replaces Boeing, 2017 Installed in Boeing… · Feb 2, 2003 - [AD-2013-1A](https://drs.faa.gov/browse/excelExternalWindow/0662D6457AD79F4585257038006B8DD0.0001): Battery Pack. Aero Design Inc · Replaces Boeing 2013-1A Installed in Radiant… · Feb 2, 2003 - [2013-BR](https://drs.faa.gov/browse/excelExternalWindow/F385B8109DC085978525703E00672E5C.0001): Battery Assembly. Bruce Industries Inc · Replaces 2013-1A · Jul 31, 2002 - [24-7D5258-01](https://drs.faa.gov/browse/excelExternalWindow/FE9B2D843746DFBB85257042005A0F65.0001): Inbd. Wing De-Icer, LH. Goodrich Corporation · Replaces British Aerospace & BFG 24-7D5258-01 · Feb 1, 2001 - [24-7D5258-16](https://drs.faa.gov/browse/excelExternalWindow/C5EF8744B036FBAC85257042005A0F6E.0001): Inbd. Ctr. Wing De-Icer, RH. Goodrich Corporation · Replaces British Aerospace & BFG 24-7D5258-16 · Feb 1, 2001 - [24-7D5258-06](https://drs.faa.gov/browse/excelExternalWindow/C55DC6F65A432CE385257042005A0F6A.0001): Outbd. Center wing De-Icer, RH. Goodrich Corporation · Replaces British Aerospace & BFG 24-7D5258-06 · Feb 1, 2001 - [24-7D5258-15](https://drs.faa.gov/browse/excelExternalWindow/A1F2A7C7CF95718B85257042005A0F6D.0001): Inbd. Ctr. Wing De-Icer, LH. Goodrich Corporation · Replaces British Aerospace & BFG 24-7D5258-15 · Feb 1, 2001 - [24-7D5258-09](https://drs.faa.gov/browse/excelExternalWindow/A188EEDD871802CE85257042005A0F6B.0001): Inbd. Horiz. Stab. De-Icer. Goodrich Corporation · Replaces British Aerospace & BFG 24-7D5258-09 · Feb 1, 2001 - [23-7D5258-07](https://drs.faa.gov/browse/excelExternalWindow/9C203114B28D44E185257042005A0F5F.0001): Outbd. Wing De-Icer, LH. Goodrich Corporation · Replaces British Aerospace & BFG 23-7D5258-07 · Feb 1, 2001 - [24-7D5258-02](https://drs.faa.gov/browse/excelExternalWindow/79A5DBE54FEEC1F385257042005A0F66.0001): Inbd. Wing De-Icer, RH. Goodrich Corporation · Replaces British Aerospace & BFG 24-7D5258-02 · Feb 1, 2001 - [23-7D5258-13](https://drs.faa.gov/browse/excelExternalWindow/77744B38F948BE1485257042005A0F61.0001): Lower Vert. Stab. De-Icer. Goodrich Corporation · Replaces British Aeriospace & BFG 23-7D5258-13 · Feb 1, 2001 - [24-7D5258-11](https://drs.faa.gov/browse/excelExternalWindow/2222F11F8730067D85257042005A0F6C.0001): Outbd. Horiz. Stab. De-Icer. Goodrich Corporation · Replaces British Aerospace & BFG 24-7D5258-11 · Feb 1, 2001 - [23-7D5258-14](https://drs.faa.gov/browse/excelExternalWindow/0EF57B37BBBDE90685257042005A0F62.0001): Upepr Vert. Stab. De-Icer. Goodrich Corporation · Replaces British Aerospace & BFG 23-7D5258-14 · Feb 1, 2001 - [23-7D5258-08](https://drs.faa.gov/browse/excelExternalWindow/09ED01616B5CE75085257042005A0F60.0001): Outbd. Wing De-Icer, RH. Goodrich Corporation · Replaces British Aerospace & BFG 23-7D5258-08 · Feb 1, 2001 - [1532-10A](https://drs.faa.gov/browse/excelExternalWindow/C69E661988B22B6A85257042005A0F20.0001): Valve, distributor. Goodrich Corporation · Replaces IAI/BFG 1532-10A · Jan 24, 2001 - [RPS1-B](https://drs.faa.gov/browse/excelExternalWindow/FCE1049D227F21128525704B004F411E.0001): Battery Power Supply. Radiant Power Corp · Replaces 100865 · Dec 22, 1999 - [2017SMI](https://drs.faa.gov/browse/excelExternalWindow/CB415298EB2BAA0A8525704B0054D463.0001): Battery, NiCad (7.2v). Source Manufacturing Inc · Replaces 2017PK (Radiant Illumination Inc.)… · Nov 18, 1999 - [2042SMI](https://drs.faa.gov/browse/excelExternalWindow/7F8E0C0CB1552CB38525704B0054D464.0001): Case Assembly Battery. Source Manufacturing Inc · Replaces 2042 (Radiant Illumination Inc.) Note… · Nov 18, 1999 - [RPS1-B](https://drs.faa.gov/browse/excelExternalWindow/C47303814A5663268525703F004DCFAD.0001): Battery Power Supply. Derlan Inc · Replaces Bruce Industries, Inc. 100865 · Apr 6, 1995 - [BR9279-( )](https://drs.faa.gov/browse/excelExternalWindow/D4086741C4189C2C8525703E006B94A1.0001): Exit Identifier. Bruce Industries Inc · Modification part · Apr 1, 1993 - [BR9660-( )](https://drs.faa.gov/browse/excelExternalWindow/2059F17B788CF0ED8525703E006B94AC.0001): Exit Identifier. Bruce Industries Inc · Modification part · Apr 1, 1993 - [74800001](https://drs.faa.gov/browse/excelExternalWindow/0365F0E3BBC63D50862573FD005899AB.0001): Emblem Lights. Devore Aviation Corp of America · PMA PQ0626SW · May 4, 1982 ## The same model under other registry codes Amateur-built copies and renamed makers get their own codes. - [Hawker Siddeley HS.748 SERIES 2A](https://openairdocs.org/model/hawker-siddeley-hs-748-series-2a): 0 registered aircraft, registry code 4231008 --- 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.