# British Aerospace HS748 SERIES 2B

- Type: Aircraft model (FAA registry)
- Registry code: 1500248
- Manufacturer (registry): BRITISH AEROSPACE
- Model: HS748 SERIES 2B
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 2 · Turbo-prop
- Seats: 60
- 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: 0
- Page: https://openairdocs.org/model/british-aerospace-hs748-series-2b

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 83-26-04](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 83-23-06](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 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 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 75-08-17](https://openairdocs.org/ad/75-08-17): Digital Flight Data Recorders · BAE Systems HS 748 Series 2A, HS 748 Series 2B, 727-100 Series and 90 more. Effective Dec 19, 1975

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

## Registered aircraft

None registered with this model now.

## NTSB investigations

None matched to aircraft with this model.

## FAA accident and incident reports (2)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 19830512031149I](https://openairdocs.org/incident/19830512031149I), May 12, 1983: Braero HS7482B (N117CA), Seattle, WA, Minor damage. Attendant struck her head on one of the open galley drawers. Light to moderate turbulence reported.
- [Incident 19821110065179I](https://openairdocs.org/incident/19821110065179I), Nov 10, 1982: Hwksly HS748* (N118CA), Seattle, WA, Minor damage. Pilot struck a parked aircraft while taxiing to ramp area. Wing walker was helping pilot.

## Service difficulty reports (48)

As reported by operators and repair stations, by the model named in the report.

- [SDR CA141021012](https://openairdocs.org/sdr/CA141021012), Oct 19, 2014: ELT. FALSE ACTIVATION. (CAN) ELT ACTIVATED WHILE AIRCRAFT WAS ON THE APRON, REASON UNKNOWN.
- [SDR CA140806005](https://openairdocs.org/sdr/CA140806005), Jul 26, 2014: ELT. MALFUNCTIONED. (CAN) ELT ACTIVATED WHILE ACFT WAS ON THE GROUND, REASON UNKNOWN.
- [SDR CA140715001](https://openairdocs.org/sdr/CA140715001), Jul 13, 2014: ELT. FALSE ACTIVATION. (CAN) ELT ACTIVATED WHILE ON GROUND. REASON UNKNOWN.
- [SDR CA140523007](https://openairdocs.org/sdr/CA140523007), May 2, 2014: ELT. FALSE ACTIVATION. (CAN) ELT ACTIVATED FOR UNKNOWN REASON WHILE ON GROUND.
- [SDR CA140307006](https://openairdocs.org/sdr/CA140307006), Mar 7, 2014: ELT. FALSE ACTIVATION. (CAN) ELT ACTIVATED WHILE ON THE GROUND. REASON UNKNOWN.
- [SDR CA050119009](https://openairdocs.org/sdr/CA050119009), Jan 12, 2005: HEATER. FAILED. (CAN) SHORTLY AFTER DEPARTING, THE CABIN HEATER FAILED. THE CREW RETURNED THE AIRCRAFT TO POINT OF DEPARTURE. THE HEATER UNIT WAS REPLACED AND THE AIRCRAFT RETU
- [SDR CA050119007](https://openairdocs.org/sdr/CA050119007), Jan 5, 2005: LANDING GEAR. UNKNOWN. (CAN) ON TAKEOFF, THE LANDING GEAR WOULD NOT RETRACT AFTER BEING SELECTED. THE AIRCRAFT RETURNED TO POINT OF DEPARTURE AND LANDED NORMALLY. THE AIRCRAFT WAS HAN
- [SDR CA040531002](https://openairdocs.org/sdr/CA040531002), May 29, 2004: WIRE HARNESS. CHAFED. AFTER DEPARTING, THE CREW OBSERVED ABNORMALLY LOW TGT VALUE ON NR 1 ENGINE. THE AIRCRAFT RETURNED TO POINT OF DEPARTURE. MAINTENANCE FOUND CHAFED WIRING AT THE 
- [SDR CA021125001](https://openairdocs.org/sdr/CA021125001), Nov 9, 2002: OIL COOLER. LEAKING. (CAN) AIRCRAFT TOOKOFF FROM YZG FOR YUZ, AFTER TAKEOFF IN FLIGHT THE RT ENGINE OIL PRESSURE LIGHT CAME ON, OIL PRESSURE ZERO, PILOT SHUTDOWN ENGINE. ON ARRIVING
- [SDR CA021030003](https://openairdocs.org/sdr/CA021030003), Oct 17, 2002: ACTUATOR. FAILED. (CAN) NOSEWHEEL STEERING INTERMITTENTLY STIFF. NOSE WHEEL STEERING ACTUATOR WAS DISASSEMBLED. O-RING ON PISTON ROD WAS FOUND CUT, ALLOWING PRESSURE TO EQUALIZE 
- [SDR CA020531009](https://openairdocs.org/sdr/CA020531009), May 28, 2002: SUPERCHARGER. FAILED. (CAN) DURING CRUISE FLIGHT, THE CREW NOTICED THAT THE CABIN PRESSURE WAS FLUXUATING ABNORMALLY. THE CREW SELECTED MANUAL OPERATION AND SELECTED THE NR 1 SOURCE 
- [SDR CA011121006](https://openairdocs.org/sdr/CA011121006), Nov 13, 2001: ROTOR. DAMAGED. (CAN) DURING CRUISE, PILOTS SMELLED SMOKE IN COCKPIT. AT SAME TIME FLT ATTENDANT NOTIFIED COCKPIT THAT LAVATORY SMOKE DETECTOR HAD GONE OFF. A/C DEPRESSURIZED &
- [SDR CA010507011](https://openairdocs.org/sdr/CA010507011), Apr 27, 2001: HOSE. RUPTURED. (CAN) DURING ENGINE START, A/C LOST OUTBOARD BRAKE PRESSURE: MARSHALER NOTICED HYDRAULIC FLUID COMING FROM RIGHT NACELLE, & APPROPRIATELY SIGNALLED A/C CREW. EN
- [SDR CA010511024](https://openairdocs.org/sdr/CA010511024), Apr 24, 2001: PIN. DISLODGED. (CAN) WHEN CLIMBING THROUGH 12,000 FEET, PILOT REALIZED THERE WAS NO RUDDER TRIM INPUT WHEN WHEEL WAS TURNED. AIRCRAFT RETURNED TO BASE AND LANDED OVERWEIGHT. T
- [SDR CA010425005](https://openairdocs.org/sdr/CA010425005), Apr 5, 2001: CONTACTOR. INTERMITTENT. (CAN) ON APPROACH, CREW SELECTED FLAPS TO APPRAOCH FROM 15 DEGREES. FLAPS FAILED TO MOVE. HANDLE SELECTED & DE-SELECTED SEVERAL TIMES, FLAPS OPERATED NORMALLY. 
- [SDR AU010022](https://openairdocs.org/sdr/AU010022), Jan 12, 2001: HOSE. CRACKED. (AUS) RT GEARBOX MOUNTED HYDRAULIC PUMP OUTLET HOSE END FITTING CRACKED ON FLARED OLIVE.
- [SDR CA010205023](https://openairdocs.org/sdr/CA010205023), Dec 30, 2000: BOLT. BROKEN. (CAN) CREW ON LANDING DECLARED AN EMERGENCY DUE TO RED LIGHT ON RT MAIN GEAR. INVESTIGATION AFTER LANDING REVEALED THAT TRIP BOLT OPERATING MICROSWITCH ON DOWNL
- [SDR CA010118004](https://openairdocs.org/sdr/CA010118004), Dec 14, 2000: BLOCK. MISINSTALLED. (CAN) PRECAUTIONAERY INSPECTION OF FLAP LEVER ASSEMBLY SLIPPER BLOCK FOR INCORRECT PRESENCE OF A SHIM UNDER, THE HEAD OF THE SLIPPER BLOCK, RETAINING BOLTS, SHI
- [SDR CA001030009](https://openairdocs.org/sdr/CA001030009), Oct 12, 2000: RADAR. FAILED. (CAN) ON DEPARTURE, DURING CLIMB RADAR INDICATOR EMITTED SMOKE AFTER SELECTED ON. ELECTRICAL FIRE CHECK LIST CARRIED OUT AIRCRAFT RETURNED TO POINT OF DEPARTURE
- [SDR CA000804022](https://openairdocs.org/sdr/CA000804022), Jul 24, 2000: CASE. CRACKED. (CAN) DURING HOT SECTION INSPECTION, COMPRESSOR OUTLET CASING FOUND TO BE CRACKED BEYOND MAINTENANCE MANUAL LIMITS. CIRCUMFERENTIAL CRACK 7 IN , MAX ALLOWABLE I
- [SDR CA000606022](https://openairdocs.org/sdr/CA000606022), May 26, 2000: WINDOW. SEPARATED. (CAN) THE CREW REPORTED HEARING AN UNUSUAL ONE TIME NOISE WHILE THEY WERE ENROUTE YYH TO YZF. AFTER ARRIVING YZF A PORTION OF THE RT EMERGENCY EXIT OUTER WINDOW
- [SDR CA000427019](https://openairdocs.org/sdr/CA000427019), Apr 16, 2000: BRUSH BLOCK. FAILED. (CAN) PROP BRUSH BLOCK FAILURE EXPERIENCED. SLIP RINGS WERE SEVERELY PITTED ALONG WITH SIGNS OF BURING AND MELTING OF BRUSH GEAR. NO CURCUIT PROTECTION WAS ACTI
- [SDR CA991209063](https://openairdocs.org/sdr/CA991209063), Nov 24, 1999: FIRE DETECTOR. FAILED. (CAN) ON TAXI, NR 1 ENGINE FIRE WARNING ILLUMINATED. INVESTIGATION REVEALED FAILED FIRE WIRE AND FERRULE. PARTS REPLACED.
- [SDR CA990521031](https://openairdocs.org/sdr/CA990521031), Apr 23, 1999: BEARINGS. WRONG PART. (CAN) SPILL VALVE IN FOR OVERHAUL. BEARINGS ON ARMATURE FOUND TO DIFFER FROM ONES LISTED IN IPL. BEARINGS WILL BE REPLACED.
- [SDR CA990308010](https://openairdocs.org/sdr/CA990308010), Feb 19, 1999: GEARBOX. MAKING METAL. (CAN) DURING REMOVAL OF THE ALTERNATOR, FERROUS METAL WAS FOUND IN THE ALTERNATOR AREA. THE GEARBOX WAS REPLACED.
- [SDR AU990416021](https://openairdocs.org/sdr/AU990416021), Jan 24, 1999: SEAL. LEAKING. (AU) UPON INSTALLATION IN AIRCRAFT SEAL DRAIN BEGAN LEAKING. UPON INVESTIGATION BY R&O SHOP LEAK HAD DISSAPPEARED. THREE SIMILAR INSTANCES HAVE LED TO CONCLUSIO
- [SDR CA981230020](https://openairdocs.org/sdr/CA981230020), Dec 18, 1998: LINE. LEAKING. (CAN) HYDRAULIC FLOW LIGHTS CAME ON IN-FLIGHT, EMERGENCY DECLARED. WHEN U/C LOWERED, THE STANDBY LIGHT WENT OUT, HYDRAULIC PRESSURE WAS NORMAL. AIRCRAFT LANDED 
- [SDR CA980916055](https://openairdocs.org/sdr/CA980916055), Aug 7, 1998: TIRE. RUPTURED. (CAN) ON DEPARTURE, GROUND PERSONNEL REPORTED DEBRIS ON RUNWAY, AIRCRAFT MADE LOW PASS AND NR 2 POSITION TIRE APPEARED FLAT. AIRCRAFT LANDED AND NR 1 AND NR 2 W
- [SDR CA980529006](https://openairdocs.org/sdr/CA980529006), May 14, 1998: SHAFT. DAMAGED. (CAN) GENERATOR WOULD NOT COME ON LINE. INSPECTION FOUND THE GENERATOR DRIVE (FEMALE) IN THE ACCESSORY GEARBOX NOT TURNING. GEARBOX REMOVED FOR REPAIR.
- [SDR CA980529005](https://openairdocs.org/sdr/CA980529005), May 4, 1998: SELECTOR. STICKING. (CAN) ON GEAR DOWN, SELECTION HANDLE DID NOT GO ALL THE WAY DOWN, SELECTOR RECYCLED AND OPERATED PROPERLY. SYSTEM CHECKED, LUBED, TESTED AND NO FAULT FOUND. PRO
- [SDR CA980415018](https://openairdocs.org/sdr/CA980415018), Apr 8, 1998: SEAL. LEAKING. (CAN) LEAK OCCURRED WHEN WATER METHANOL PUMPS TURNED ON PRIOR TO DEPARTURE. A/C INFORMED OF LEAK WHILE HOLDING SHORT. ENGINE SHUTDOWN AND A/C TOWED. SEAL LEAKIN
- [SDR CA980325041](https://openairdocs.org/sdr/CA980325041), Feb 24, 1998: RESEVOIR. CRACKED. (CAN) HYDRAULIC RESERVOIR CRACKED AT FOOT WELD AREA. REPLACED. PART TC: 11,438.
- [SDR CA970822004](https://openairdocs.org/sdr/CA970822004), Aug 13, 1997: CONTACTOR. BURNT. (CAN) AFTER LANDING CREW REPORTED NO ANTI-ICE ON NR1 ENGINE INTAKE. INSPECTION OF CONTINUOUS LIP HEAT RELAY FOUND THE UNIT SEVERELY OVERHEATED WITH INDICATIONS 
- [SDR CA970715027](https://openairdocs.org/sdr/CA970715027), Jul 6, 1997: SUPERCHARGER. FAILED. (CAN) WHILE IN CRUISE SMOKE ENTERED THE CABIN THROUGH THE HEATING DUCTS. THE AIRCRAFT MADE AN EMERGENCY DESCENT AND LANDING. POST FLIGHT INSPECTION FOUND THE #1
- [SDR CA970624002](https://openairdocs.org/sdr/CA970624002), Jun 13, 1997: SUPERCHARGER. SHAFT SHEARED. (CAN) LH ACCESSORY GEARBOX LOW ON OIL. THE OIL SUPPLY LINE TO THE CABIN SUPERCHARGER WAS BROKEN OFF AT THE FITTING. THE SUPERCHARGER WAS REMOVED, THE QUILL SHAF
- [SDR CA970609015](https://openairdocs.org/sdr/CA970609015), May 13, 1997: STRINGER. CRACKED. (CAN) APPROXIMATELY 6" OUTBOARD OF LH RIB 20.0 STRINGERS 4, 6, 8 CRACKED, SKIN CRACKED BENEATH STRINGERS, EXTENDING FORWARD O.5 INCH AT STRINGERS 4 AND 6; EXTEN
- [SDR CA970326010](https://openairdocs.org/sdr/CA970326010), Mar 12, 1997: BOLTS. LOOSE. (CAN) AFTER LANDING OIL WAS OBSERVED LEAKING FROM #1 ENIGNE COWLING. THE OIL QUANTITY WAS TOPPED UP AND A GROUND RUN WAS CARRIED OUT. MAINTENANCE FOUND THE BOLT
- [SDR CA970305004](https://openairdocs.org/sdr/CA970305004), Feb 24, 1997: STARTER. FAILED. (CAN) #2 ENGINE FAILED TO START AFTER DE-ICING. STARTER REPLACED.
- [SDR CA970210001](https://openairdocs.org/sdr/CA970210001), Jan 27, 1997: HOSE. LEAKING. (CAN) AIRCRAFT LOST HYDRAULIC SYSTEM PRESSURE ON DESTINATION. LANDED NORMALLY. TOWED OFF RUNWAY. HYDRAULIC LINE TO RH MAXARET LEAKING, REPLACED.
- [SDR CA970203011](https://openairdocs.org/sdr/CA970203011), Jan 24, 1997: COMB CHAMBER. BROKEN. (CAN) DURING INSPECTION THE NOSE CONE OF ONE OF THE COMBUSTION CHAMBERS WAS FOUND BROKEN AWAY FROM THE COMBUSTION CHAMBER BODY.
- [SDR CA970117003](https://openairdocs.org/sdr/CA970117003), Jan 7, 1997: ACCUMULATOR. LEAKING. (CAN) AFTER DEPARTURE AIRCRAFT HYDRAULIC PRESSURE DROPPED TO 400 PSI. PRESSURE DROP DUE TO ACCUMULATOR FAILURE. REPLACED.
- [SDR CA970115004](https://openairdocs.org/sdr/CA970115004), Dec 23, 1996: ENGINE. MAKING METAL. (CAN) ENGINE WAS SHUTDOWN DURING APPROACH DUE TO ILLUMINATED OIL PRESSURE WARNING LIGHT. POST FLIGHT INSPECTION FOUND METAL IN THE OIL FILTER. THE ENGINE WAS RE
- [SDR CA961223005](https://openairdocs.org/sdr/CA961223005), Dec 12, 1996: CONNECTOR. DIRTY. (CAN) PRIOR TO DEPARTURE, BOTH ENGINES RUNNING, FIRE INDICATION WAS OBSERVED ON NO.1. NO EVIDENCE OF FIRE. OIL CONTAMINATED CONNECTOR PLUG. CLEANED. SERVICEABLE
- [SDR CA961203012](https://openairdocs.org/sdr/CA961203012), Nov 25, 1996: BEARING. FAILED. (CAN) FORWARD TUNNEL SHAFT BEARING FAILED CAUSING FORWARD END CAP OF SHAFT TO DISCONNECT FROM INPUT SHAFT. SUSPECT BEARING FAILURE ATTRIBUTED T OIL STARVATION; 
- [SDR CA960916013](https://openairdocs.org/sdr/CA960916013), Sep 7, 1996: FIRE WIRE. SHORTED. (CAN) ON DESCENT FIRE INDICATION ON #1 ENGINE BOTTLES DISCHARGED AND ENGINE SHUT DOWN. INTERNALLY SHORTED FIRE WIRE. BOTTLES AND WIRE REPLACED.
- [SDR CA960916012](https://openairdocs.org/sdr/CA960916012), Sep 5, 1996: BEARING. FAILED. (CAN) ON ROLL OUT AIRCRAFT WAS PULLING TO THE LEFT AND DIFFICULT TO STEER. LH OUTER WHEEL BEARING HAD DISINTEGRATED CAUSING INNER RACE TO SEIZE TO SPACER AND AX
- [SDR CA960812019](https://openairdocs.org/sdr/CA960812019), Aug 6, 1996: FUEL TRIMMER. FAILURE. (CAN) IN CRUISE #2 ENGINE FUEL TRIM FAILED. AIRCRAFT RETURNED TO BLOCKS. FUEL TRIM REPLACED.
- [SDR CA970609032](https://openairdocs.org/sdr/CA970609032), Jun 1, 1996: COVER. DAMAGED. (CAN) DURING TRAINING FLIGHT THE GEAR WAS SELECTED DOWN IN THE EMERGENCY MODE. THE LH GEAR WOULD NOT LOCK DOWN WITH HAND PUMP PRESSURE BUT WOULD LOCK DOWN WITH 

## 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 SA1474NM](https://openairdocs.org/stc/SA1474NM): Installation of galley, P/N ATI75201. Gottlieb Corporation dba Air Transport Industries
- [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

## 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

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