# Service difficulty reports: British Aerospace HS748 SERIES 2B

A list on [British Aerospace HS748 SERIES 2B](https://openairdocs.org/model/british-aerospace-hs748-series-2b.md).

Newest first. General aviation reporting is voluntary.

- [SDR CA141021012](https://openairdocs.org/sdr/CA141021012.md): Elt · false activation · Oct 19, 2014 · Braero HS7482B · Emergency Locator Beacon
  > (CAN) ELT ACTIVATED WHILE AIRCRAFT WAS ON THE APRON, REASON UNKNOWN.
- [SDR CA140806005](https://openairdocs.org/sdr/CA140806005.md): Elt · malfunctioned · Jul 26, 2014 · Braero HS7482B · Emergency Locator Beacon
  > (CAN) ELT ACTIVATED WHILE ACFT WAS ON THE GROUND, REASON UNKNOWN.
- [SDR CA140715001](https://openairdocs.org/sdr/CA140715001.md): Elt · false activation · Jul 13, 2014 · Braero HS7482B · Emergency Locator Beacon
  > (CAN) ELT ACTIVATED WHILE ON GROUND. REASON UNKNOWN.
- [SDR CA140523007](https://openairdocs.org/sdr/CA140523007.md): Elt · false activation · May 2, 2014 · Braero HS7482B · Emergency Locator Beacon
  > (CAN) ELT ACTIVATED FOR UNKNOWN REASON WHILE ON GROUND.
- [SDR CA140307006](https://openairdocs.org/sdr/CA140307006.md): Elt · false activation · Mar 7, 2014 · Braero HS7482B · Emergency Locator Beacon
  > (CAN) ELT ACTIVATED WHILE ON THE GROUND. REASON UNKNOWN.
- [SDR CA050119009](https://openairdocs.org/sdr/CA050119009.md): Heater · failed · Jan 12, 2005 · Braero HS7482B · Heating System
  > (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 RETURNED TO SERVICE.
- [SDR CA050119007](https://openairdocs.org/sdr/CA050119007.md): Landing Gear · unknown · Jan 5, 2005 · Braero HS7482B · Main Landing Gear Attach Section
  > (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 HANGARED AND A GEAR SWING CARRIED OUT, THE FAULT COULD NOT BE DUPLICATED. THE AIRCRAFT WAS RETURNED TO
- [SDR CA040531002](https://openairdocs.org/sdr/CA040531002.md): Wire Harness · chafed · May 29, 2004 · Braero HS7482B · Engine EGT/TIT Indicating System
  > 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 TGT JUNCTION BOX, THE EXTERNAL CALIBRATION TEST CONNECTOR ASSY WAS REMOVED AND THE AIRCRAFT RETURN
- [SDR CA021125001](https://openairdocs.org/sdr/CA021125001.md): Oil Cooler · leaking · Nov 9, 2002 · Braero HS7482B · Engine Oil Cooler
  > (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 TO YVP, INSPECTION WAS CARRIED OUT, AND RT OIL COOLER HONEYCOMB WAS LEAKING. RT OIL COOLER WAS REP
- [SDR CA021030003](https://openairdocs.org/sdr/CA021030003.md): Actuator · failed · Oct 17, 2002 · Braero HS7482B · Steering Unit
  > (CAN) NOSEWHEEL STEERING INTERMITTENTLY STIFF. NOSE WHEEL STEERING ACTUATOR WAS DISASSEMBLED. O-RING ON PISTON ROD WAS FOUND CUT, ALLOWING PRESSURE TO EQUALIZE ON EITHER SIDE OF THE RAM. BACKUP RINGS WHICH ARE INSTALLED ON EITHER SIDE OF THE O-RING WERE MISSIN
- [SDR CA020531009](https://openairdocs.org/sdr/CA020531009.md): Supercharger · failed · May 28, 2002 · Braero HS7482B · Cabin Compressor System
  > (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 AND CONTINUED THE FLIGHT TO DESTINATION. MAINTENANCE FOUND THAT THE NR 1 SUPERCHARGER HAD FAILED. B
- [SDR CA011121006](https://openairdocs.org/sdr/CA011121006.md): Rotor · damaged · Nov 13, 2001 · Braero HS7482B · Air Distribution System
  > (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 & EMERG DESCENT MADE, FOLLOWED BY UNSCHED LDG IN LA RONGE, SK. AIR-COND SYS OPERATED NORMALLY ON SUBS
- [SDR CA010507011](https://openairdocs.org/sdr/CA010507011.md): Hose · ruptured · Apr 27, 2001 · Braero HS7482B · Landing Gear Brake System
  > (CAN) DURING ENGINE START, A/C LOST OUTBOARD BRAKE PRESSURE: MARSHALER NOTICED HYDRAULIC FLUID COMING FROM RIGHT NACELLE, & APPROPRIATELY SIGNALLED A/C CREW. ENG SHUTDOWN, & HYDRAULIC LEAK INVESTIGATED. RUPTURED HOSE FOUND AT TOP OF RT MAIN GEAR SHOCK STRUT.
- [SDR CA010511024](https://openairdocs.org/sdr/CA010511024.md): Pin · dislodged · Apr 24, 2001 · Braero HS7482B · Rudder Tab Control System
  > (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. TAPER PIN THAT HOLD RUDDER WHEEL WAS FOUND DISLODGED. PIN WAS RE INSTALLED AN SECURED. OVERWEIGHT LAN
- [SDR CA010425005](https://openairdocs.org/sdr/CA010425005.md): Contactor · intermittent · Apr 5, 2001 · Braero HS7482B · Trailing Edge Flap Control System
  > (CAN) ON APPROACH, CREW SELECTED FLAPS TO APPRAOCH FROM 15 DEGREES. FLAPS FAILED TO MOVE. HANDLE SELECTED & DE-SELECTED SEVERAL TIMES, FLAPS OPERATED NORMALLY. FOUND UP SIDE OF REVERSING CONTACTOR FAILING INTERMITTENTLY. REPLACED CONTACTOR, NO FURTHER PROBLEMS
- [SDR AU010022](https://openairdocs.org/sdr/AU010022.md): Hose · cracked · Jan 12, 2001 · Braero HS7482B · Hydraulic System, Main
  > (AUS) RT GEARBOX MOUNTED HYDRAULIC PUMP OUTLET HOSE END FITTING CRACKED ON FLARED OLIVE.
- [SDR CA010205023](https://openairdocs.org/sdr/CA010205023.md): Bolt · broken · Dec 30, 2000 · Braero HS7482B · Landing Gear Retraction/Extension System
  > (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 DOWNLOCK WAS BROKEN P/N 100021303 LEADING TO FALSE INDICATION. TRIP BOLT P/N 100021303 WAS REPLACED AND R
- [SDR CA010118004](https://openairdocs.org/sdr/CA010118004.md): Block · misinstalled · Dec 14, 2000 · Braero HS7482B · Trailing Edge Flap Control System
  > (CAN) PRECAUTIONAERY INSPECTION OF FLAP LEVER ASSEMBLY SLIPPER BLOCK FOR INCORRECT PRESENCE OF A SHIM UNDER, THE HEAD OF THE SLIPPER BLOCK, RETAINING BOLTS, SHIMS WERE FOUND LT SIDE STATION 0 IB BLOCK, STAION 91 IN AND OB BLOCK, STATION 296 OB AN IB BLOCK, RT
- [SDR CA001030009](https://openairdocs.org/sdr/CA001030009.md): Radar · failed · Oct 12, 2000 · Braero HS7482B · Central Display
  > (CAN) ON DEPARTURE, DURING CLIMB RADAR INDICATOR EMITTED SMOKE AFTER SELECTED ON. ELECTRICAL FIRE CHECK LIST CARRIED OUT AIRCRAFT RETURNED TO POINT OF DEPARTURE. THE INDICATOR WAS VERIFIED AS THE SOURCE OF THE PROBLEM AND NO WIRING ANOMOLIES WERE OBSERVED. THE
- [SDR CA000804022](https://openairdocs.org/sdr/CA000804022.md): Case · cracked · Jul 24, 2000 · Braero HS7482B · Turbine Engine Compressor Section
  > (CAN) DURING HOT SECTION INSPECTION, COMPRESSOR OUTLET CASING FOUND TO BE CRACKED BEYOND MAINTENANCE MANUAL LIMITS. CIRCUMFERENTIAL CRACK 7 IN, MAX ALLOWABLE IS 6 IN. AS VIEWED FROM REAR OF ENGINE THROUGH COMPRESSOR NR 1 OUTLET, WITH COMBUSTION CHAMBER REMOVE
- [SDR CA000606022](https://openairdocs.org/sdr/CA000606022.md): Window · separated · May 26, 2000 · Braero HS7482B · Passenger Compartment Windows
  > (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 PANE WAS OBSERVED TO HAVE DEPARTED THE AIRCRAFT. DAMAGE TO THE RT HORIZONTAL STABILIZER LEADING EDG
- [SDR CA000427019](https://openairdocs.org/sdr/CA000427019.md): Brush Block · failed · Apr 16, 2000 · Braero HS7482B · Propeller Hub Section
  > (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 ACTIVATED. INSPECTION SCHEDULE REQUESTED FROM OPERATOR. MAINTENANCE INSPECTIONS OF BRUSH BLOCK AR
- [SDR CA991209063](https://openairdocs.org/sdr/CA991209063.md): Fire Detector · failed · Nov 24, 1999 · Braero HS7482B · Detection System
  > (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.md): Bearings · wrong part · Apr 23, 1999 · Braero HS7482B · Air Distribution Fan
  > (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.md): Gearbox · making metal · Feb 19, 1999 · Braero HS7482B · Turbine Engine Accessory Drive
  > (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.md): Seal · leaking · Jan 24, 1999 · Braero HS7482B · Fuel Boost Pump
  > (AU) UPON INSTALLATION IN AIRCRAFT SEAL DRAIN BEGAN LEAKING. UPON INVESTIGATION BY R&O SHOP LEAK HAD DISSAPPEARED. THREE SIMILAR INSTANCES HAVE LED TO CONCLUSION THAT EVEN IN A SHORT PERIOD OF TIME THIS SEAL WILL DRY OUT. SUBMITTER SUGGESTS THAT THESE PUMP
- [SDR CA981230020](https://openairdocs.org/sdr/CA981230020.md): Line · leaking · Dec 18, 1998 · Braero HS7482B · Hydraulic System, Main
  > (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 OK. STANDBY HYD PUMP BLEED NIPPLE LEAKING, RESEALED, PUMPS BLED AND FLUID REPLENISHED. ON APPROA
- [SDR CA980916055](https://openairdocs.org/sdr/CA980916055.md): Tire · ruptured · Aug 7, 1998 · Braero HS7482B · Tire
  > (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 WHEELS REPLACED. DIAMOND SHAPE SECTION OF RUBBER 18 BY 11 MISSING FROM TIRE.
- [SDR CA980529006](https://openairdocs.org/sdr/CA980529006.md): Shaft · damaged · May 14, 1998 · Braero HS7482B · Turbine Engine Accessory Drive
  > (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.md): Selector · sticking · May 4, 1998 · Braero HS7482B · Landing Gear Selector
  > (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. PROBLEM OCCURRED AGAIN. TELEFLEX CABLE REPLACED, TESTED OK, OCCURRED AGAIN AND SELECTOR REPLACED SB
- [SDR CA980415018](https://openairdocs.org/sdr/CA980415018.md): Seal · leaking · Apr 8, 1998 · Braero HS7482B · Water Injection System
  > (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 LEAKING AT FIREWALL DISCONNECT SUPPLY LINE. SEAL REPLACED.
- [SDR CA980325041](https://openairdocs.org/sdr/CA980325041.md): Resevoir · cracked · Feb 24, 1998 · Braero HS7482B · Hydraulic Reservoir, Main
  > (CAN) HYDRAULIC RESERVOIR CRACKED AT FOOT WELD AREA. REPLACED. PART TC: 11,438.
- [SDR CA970822004](https://openairdocs.org/sdr/CA970822004.md): Contactor · burnt · Aug 13, 1997 · Braero HS7482B · Air Intake Anti/De-Ice System
  > (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 OF LOCAL FIRE IN THE AREA OF THE NACELLE WHERE THE UNIT IS LOCATED. REPLACED.
- [SDR CA970715027](https://openairdocs.org/sdr/CA970715027.md): Supercharger · failed · Jul 6, 1997 · Braero HS7482B · Cabin Cooling System
  > (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 ENGINE HARD TO ROTATE PRODUCING A GRINDING SOUND. THE #1 SUPERCHARGER WAS REPLACED AND THE AIRCRAFT
- [SDR CA970624002](https://openairdocs.org/sdr/CA970624002.md): Supercharger · shaft sheared · Jun 13, 1997 · Braero HS7482B · Cabin Cooling System
  > (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 SHAFT WAS FOUND SHEARED AND THE SCROLLS BINDING. THE SUPERCHARGER DRIVE BEARINGS LOCATED ON THE GEARBOX
- [SDR CA970609015](https://openairdocs.org/sdr/CA970609015.md): Stringer · cracked · May 13, 1997 · Braero HS7482B · Horizontal Stabilizer, Plate/Skin
  > (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; EXTENDING AFT 1" AT STRINGERS 4 AND 6. SLIGHT DOWNWARD BUCKLING AT DAMAGED AREAS. REPAIRED IN ACCORDANCE
- [SDR CA970326010](https://openairdocs.org/sdr/CA970326010.md): Bolts · loose · Mar 12, 1997 · Braero HS7482B · Turbine Engine Compressor Section
  > (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 BOLTS WHICH RETAIN THE FORWARD BEARING HOUSING FOR THE COUPLING SHAFT (OUTPUT SHAFT) WERE LOOSE. THE BOL
- [SDR CA970305004](https://openairdocs.org/sdr/CA970305004.md): Starter · failed · Feb 24, 1997 · Braero HS7482B · Starter-Generator
  > (CAN) #2 ENGINE FAILED TO START AFTER DE-ICING. STARTER REPLACED.
- [SDR CA970210001](https://openairdocs.org/sdr/CA970210001.md): Hose · leaking · Jan 27, 1997 · Braero HS7482B · Hydraulic System, Main
  > (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.md): Comb Chamber · broken · Jan 24, 1997 · Braero HS7482B · Turbine Engine Combustion Section
  > (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.md): Accumulator · leaking · Jan 7, 1997 · Braero HS7482B · Hydraulic Power Accumulator, Main
  > (CAN) AFTER DEPARTURE AIRCRAFT HYDRAULIC PRESSURE DROPPED TO 400 PSI. PRESSURE DROP DUE TO ACCUMULATOR FAILURE. REPLACED.
- [SDR CA970115004](https://openairdocs.org/sdr/CA970115004.md): Engine · making metal · Dec 23, 1996 · Braero HS7482B · Engine (Turbine/Turboprop)
  > (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 REMOVED.
- [SDR CA961223005](https://openairdocs.org/sdr/CA961223005.md): Connector · dirty · Dec 12, 1996 · Braero HS7482B · Fire Detection
  > (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.md): Bearing · failed · Nov 25, 1996 · Braero HS7482B · Turbine Engine Accessory Drive
  > (CAN) FORWARD TUNNEL SHAFT BEARING FAILED CAUSING FORWARD END CAP OF SHAFT TO DISCONNECT FROM INPUT SHAFT. SUSPECT BEARING FAILURE ATTRIBUTED T OIL STARVATION; PLUGGED JET AND/OR PUMP FAILURE. GEARBOX SHIPPED FOR TEARDOWN.
- [SDR CA960916013](https://openairdocs.org/sdr/CA960916013.md): Fire Wire · shorted · Sep 7, 1996 · Braero HS7482B · Fire Detection
  > (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.md): Bearing · failed · Sep 5, 1996 · Braero HS7482B · Wheel/Ski/Float
  > (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 AXLE. REPLACED.
- [SDR CA960812019](https://openairdocs.org/sdr/CA960812019.md): Fuel Trimmer · failure · Aug 6, 1996 · Braero HS7482B · Fuel Control/Turbine Engines
  > (CAN) IN CRUISE #2 ENGINE FUEL TRIM FAILED. AIRCRAFT RETURNED TO BLOCKS. FUEL TRIM REPLACED.
- [SDR CA970609032](https://openairdocs.org/sdr/CA970609032.md): Cover · damaged · Jun 1, 1996 · Braero HS7482B · Landing Gear Retraction/Extension System
  > (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 NORMAL SYSTEM PRESSURE. AIRCRAFT LANDED WITH 3 GREEN. THE UPPER SEAR COVER WAS FOUND BENT UPWARDS IN

## 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 = 'HS7482B'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/british-aerospace-hs748-series-2b/reports

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