# Service difficulty reports: British Aerospace BAE 146 SERIES 300A

A list on [British Aerospace BAE 146 SERIES 300A](https://openairdocs.org/model/british-aerospace-bae-146-series-300a.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 10 · 481 reports

- [SDR AU510002205](https://openairdocs.org/sdr/AU510002205.md): Hose · failed · Dec 12, 2005 · Bag BAE146300A · Landing Gear Retraction/Extension System
  > NOSE LANDING GEAR RETRACTION ACTUATOR FLEXIBLE HYDRAULIC HOSE RUPTURED. LOSS OF GREEN SYSTEM HYDRAULIC FLUID.
- [SDR AU510001941](https://openairdocs.org/sdr/AU510001941.md): Frame · cracked · Dec 12, 2005 · Bag BAE146300A · Fuselage Main, Frame
  > (AUS) FUSELAGE FRAME 41 AND FRAME 43 CRACKED. FOUND DURING INSPECTION IAW AD/BAE146/116. (OTHER CAUSE: MATERIAL) (CASA NR 510001941)
- [SDR AU510001940](https://openairdocs.org/sdr/AU510001940.md): Frame · cracked · Dec 12, 2005 · Bag BAE146300A · Fuselage Main, Frame
  > (AUS) FUSELAGE FRAME 43 CRACKED. FOUND DURING INSPECTION IAW AD/BAE146/116. (OTHER CAUSE: MATERIAL) (CASA NR 510001940)
- [SDR AU510001797](https://openairdocs.org/sdr/AU510001797.md): Jackshaft · corroded · Dec 12, 2005 · Bag BAE146300A · Drag Control Actuator
  > (AUS) LT CENTER AND RT OB LIFT SPOILER JACKS CORRODED BEYOND LIMITS IN PISTON THREADS FOR EYE ENDS. FOUND DURING INSPECTION IAW AAES ER BA6-27-60-23B AND BAE SYSTEMS SB 27-176. (CASA NR 510001797)
- [SDR AU510001750](https://openairdocs.org/sdr/AU510001750.md): Indicator · damaged · Dec 12, 2005 · Bag BAE146300A · Auxiliary Gear (Tail Skid)
  > (AUS) AIRCRAFT EXPERIENCED A HIGH SINK RATE DURING LANDING. INVESTIGATION FOUND THAT THE MAIN LANDING GEAR AND TAILSKID CONTACTED THE GROUND CAUSING DAMAGE TO THE TAIL STRIKE INDICATOR. (CASA NR 510001750)
- [SDR AU510001495](https://openairdocs.org/sdr/AU510001495.md): Selector · failed · Dec 12, 2005 · Bag BAE146300A · Landing Gear Selector
  > LANDING GEAR SELECTOR LEVER WOULD NOT MOVE TO THE `UP` POSITION.
- [SDR AU510001709](https://openairdocs.org/sdr/AU510001709.md): Wire · shorted · Oct 8, 2005 · Bag BAE146300A · Fuel System Wiring
  > RT INNER FUEL BOOST PUMP PRESSURE SWITCH TO PRINTED CIRCUIT BOARD WIRE SHORT CIRCUITED.
- [SDR AU510001967](https://openairdocs.org/sdr/AU510001967.md): Bolt · sheared · Jun 10, 2005 · Bag BAE146300A · Wing Spar
  > CENTER FUEL TANK WING SPAR ATTACHMENT BOLTS (4OFF) HAD SHEAR BOLT HEADS. FUEL LEAKING FROM CENTER TANK AT RT FRONT CORNER ABOVE THE WING TO FUSELAGE ATTACHMENT LINK AT FRAME 26 RIB 2.
- [SDR AU510001664](https://openairdocs.org/sdr/AU510001664.md): Hinge · corroded · Feb 8, 2005 · Bag BAE146300A · Landing Gear Doors
  > RT MAIN LANDING GEAR DOOR HINGE FITTINGS CORRODED IN BORES. BEARING HOUSINGS ALSO CONTAINED PITTING AND RUST DEPOSITS ON THE OUTER SURFACES. FOUND DURING INSPECTION IAW BAE SYSTEMS ISB 52-113 REV 1 AND AAES AD ER BA6-32-10-43B AND UK CAA AD G-2005-0017.
- [SDR A6WA200460066](https://openairdocs.org/sdr/A6WA200460066.md): Acm · odor · Dec 30, 2004 · N616AW · Bag BAE146300A · Cabin Cooling System
  > NR 2 PACK WAS INADVERTENTLY SWITCHED ON FOR APPROX 10 MINUTES ENROUTE. PILOTS NOTICED ODOR IN COCKPIT, PACK SWITCHED OFF AND A PUFF OF WHITE SMOKE CAME OUT OF VENT IN COCKPIT THEN SMOKE ODOR DISSIPATED. MAINTENANCE REMOVED AND REPLACED RIGHT HAND AIR CYCLE M
- [SDR A6WA200460054](https://openairdocs.org/sdr/A6WA200460054.md): Oxygen Mask · missing · Nov 10, 2004 · N612AW · Bag BAE146300A · Passenger Oxygen System
  > ROWS 14 AND 16 DEF HAVE NR O2 MASKS INSTALLED IN PSU BOXES. MAINTENANCE INSTALLED PASSENGER ALL O2 MASKS AS REQUIRED IAW 35-20-45.
- [SDR AUS20040512](https://openairdocs.org/sdr/AUS20040512.md): Rib · cracked · Jun 15, 2004 · Bag BAE146300A · Nacelle/Pylon, Frame/Spar/Rib
  > (AUS) NR 1, NR 3 AND NR 4 PYLONS HAD NR 4 RIB CRACKED IN THE LOWER FLANGE RADIUS. PYLON NR 1, CRACK LENGTH 22.86MM (0.9IN) PYLON NR 3, CRACK LENGTH 12.7MM (0.5IN) PYLON NR 4, CRACK LENGTH 20.32 (0.8IN).
- [SDR AUS20040501](https://openairdocs.org/sdr/AUS20040501.md): Firewall · cracked · Jun 10, 2004 · Bag BAE146300A · Fuselage Main, Bulkhead
  > (AUS) APU FIREWALL CRACKED AT 7 O'CLOCK POSITION. FOUND DURING INSPECTION IAW AD/BAE146/053.
- [SDR A6WA200460019](https://openairdocs.org/sdr/A6WA200460019.md): Skin · scratched · Jun 2, 2004 · N611AW · Bag BAE146300A · Cargo/Baggage Doors
  > AFT CARGO DOOR SCRATCHES BEYOND THE ALLOWABLE SRM LIMITS. MAINTENANCE REQUESTED REPAIR FROM MFG SYSTEMS. MAINTENANCE CUT DAMAGED AREA OUT IAW BAE SRM 52-32-11 FIG 201 PARA 3B PER BAE FAX BARA/AVR/6767/04-DC. HFEC INSPECTION C/O ON CUT OUT REPAIR, NO CRACKS N
- [SDR A6WA200460016](https://openairdocs.org/sdr/A6WA200460016.md): Floorbeam · cracked · May 26, 2004 · N611AW · Bag BAE146300A · Fuselage Main, Floor Beam
  > CRACK LOCATED IN THE LOWER RADIUS OF FLOORBEAM 33B AT LBL 62.0 INCHES. MAINTENANCE REQUESTED REPAIRS FROM MFG SYSTEMS REF AVMAX FAX 611-1908002. REPAIRED IAW BAE FAX BARA/AVR/6759/04-DC AND BARA/AVR/6752/04-02. PRIMED IAW BAE 146 AMM 20-10-11. (M)
- [SDR AUS20040444](https://openairdocs.org/sdr/AUS20040444.md): Computer · faulty · May 20, 2004 · Bag BAE146300A · Trailing Edge Flap Control System
  > (AUS) FLAP COMPUTER FAULTY.
- [SDR AUS20040429](https://openairdocs.org/sdr/AUS20040429.md): Link · fractured · May 17, 2004 · Bag BAE146300A · Landing Gear Retraction/Extension System
  > (AUS) MAIN LANDING GEAR ASSISTOR JACK TRIANGULAR LINK FAILED AT JACK ATTACHMENT POINT.
- [SDR AUS20040410](https://openairdocs.org/sdr/AUS20040410.md): Intercostal · corroded · May 17, 2004 · Bag BAE146300A · Fuselage Miscellaneous Structure
  > (AUS) AFT CABIN FLOOR INTERCOSTAL CONTAINED LEVEL 2 CORROSION ON THESIDE AND UPPER SURFACES. THE INTERCOSTAL DAMAGE WAS LOCATED INZONE 251 BETWEEN FRAMES 41 AND 53 AT BL9 LH. AREA OF CORROSION MEASURED 38.1MM (1.5 IN) IN LENGTH BY 3.175MM (0.125 IN) IN WIDTH A
- [SDR AUS20040405](https://openairdocs.org/sdr/AUS20040405.md): Frame · corroded · May 17, 2004 · Bag BAE146300A · Fuselage Main, Frame
  > (AUS) LT FUSELAGE FRAME 43 CONTAINED LEVEL 2 CORROSION ON THE FORWARD FACE AT FLOOR LEVEL. DAMAGE WAS LOCATED AT ZONE 20 FRAME 43 STA 726.9 AND WAS 38.1MM (1.5IN) LONG BY 38.1MM (1.5IN) WIDE AND 4.546MM (0.179IN) DEEP. CAUSE OF DAMAGE WAS ASSESSED AS ENVIRONME
- [SDR AUS20040401](https://openairdocs.org/sdr/AUS20040401.md): Actuator · seized · May 17, 2004 · Bag BAE146300A · Drag Control Actuator
  > (AUS) RT NR 2 LIFT SPOILER ACTUATOR SPINDLE SEIZED IN LOCKED POSITION WITH THE ACTUATOR EXTENDED. FOUND DURING INSPECTION IAW AD/BA6-27-60-16D BAE MANDATORY ISB 27-137.
- [SDR A6WA200460014](https://openairdocs.org/sdr/A6WA200460014.md): Fuel Control · fluctuates · May 9, 2004 · N611AW · Bag BAE146300A · Fuel Control/Turbine Engines
  > WHILE IN VMC CLIMBING THROUGH 16000 FEET THE NR 3 ENGINE N1 FLUCTUATION FOLLOWED BY FUEL FLOW DROPPING TO ZERO. ENGINE WAS SHUTDOWN, REMAINDER OF FLT MIN N2 OF 8 PERCENT, N1 26, 10 PSI, OIL QUANT 3/4 FULL. MAINTENANCE REMOVED AND REPLACED NR 3 FUEL CONTROL U
- [SDR AUS20040372](https://openairdocs.org/sdr/AUS20040372.md): Angle · corroded · May 7, 2004 · Bag BAE146300A · Fuselage Miscellaneous Structure
  > (AUS) RT REAR ENTRY SILL PLATE ATTACHMENT ANGLE CONTAINED LEVEL 2 CORROSION ON THE UPPER SURFACE. AREA OF CORROSION 48.26MM (1.9IN) LONG BY 20.8MM (0.82IN) WIDE AND 0.584MM (0.023IN) DEEP. LOCATION OF CORROSION, ZONE 252 STRINGER 19, BETWEEN FRAMES 41AND 43
- [SDR AUS20040351](https://openairdocs.org/sdr/AUS20040351.md): Seat Track · corroded · May 6, 2004 · Bag BAE146300A · Fuselage, Seat/Cargo Attach Fittings
  > (AUS) SEAT TRACKS CORRODED. PN HC538J0343-001 RT IB SEAT TRACK FOUND CORRODED ON UPPER SURFACE. CORROSION MEASURES 106.68MM (4.2IN) LENGTH, 24.13MM (0.95IN) WIDTH WITH DEPTH OUT OF LIMITS. LOCATION, ZONE 251, FRAME 40, RBL 21 RT. REPORTED CAUSE OF DEFECT,
- [SDR AUS20040345](https://openairdocs.org/sdr/AUS20040345.md): Bolt · corroded · May 6, 2004 · Bag BAE146300A · Fasteners
  > (AUS) FORWARD OUTER ATTACHMENT SPECIAL BOLT SHAFT CORRODED AND PLATING MISSING. CORROSION WAS LOCATED APPROXIMATELY 12.7MM (0.5IN) DOWN FROM THE BOLT HEAD. AREA OF CORROSION 25.4MM (1IN) IN LENGTH BY 9.39MM (0.370IN) IN WIDTH BY0.127MM (0.005IN) DEPTH.BOLTS A
- [SDR AUS20040379](https://openairdocs.org/sdr/AUS20040379.md): Seat Track · corroded · May 5, 2004 · Bag BAE146300A · Fuselage, Seat/Cargo Attach Fittings
  > (AUS) CABIN FLOOR STRUCTURE CONTAINED LEVEL 2 CORROSION IN THE FOLLOWING AREAS: PN HC536H1063-001 RT OB SEAT TRACK END ON UPPER SURFACE. AREA OF CORROSION MEASURED 38.1MM (1.5IN) IN LENGTH BY 12.7MM (0.5IN) IN WIDTH WITH A DEPTH OF 2.54MM (0.10IN). CORROSI
- [SDR AUS20040357](https://openairdocs.org/sdr/AUS20040357.md): Frame · cracked · May 5, 2004 · Bag BAE146300A · Fuselage Main, Frame
  > (AUS) CABIN CROWN FRAME TO SKIN STRUCTURE ANGLE CLEATS (8OFF) CRACKED FROM BEND RADIUS EDGE. THE ANGLE CLEATS ARE LOCATED IN FOLLOWING AREAS: FRAME 19A BETWEEN STRINGERS 1 AND 2 LT. FRAME 19A BETWEEN STRINGERS 2 AND 3 LT 3. FRAME 19B BETWEEN STRINGERS 1 AND
- [SDR AUS20040339](https://openairdocs.org/sdr/AUS20040339.md): Plate · corroded · May 5, 2004 · Bag BAE146300A · Fuselage Main, Structure
  > (AUS) INSP OF REAR CABIN WET AREA AT FLOOR LEVEL FOUND CORROSION IN FOLLOWING PLATES: SHEAR PLATE PN HC538H1183-000 LOCATED ON TOP OF LONGITUDINAL BEAM FRAME 43 RBL 34. CORROSION WAS LOCATED ON UPPER SURFACE MEASURING 17.018MM (0.67IN) LENGTH, 16.002MM (0.63
- [SDR A6WA200460012](https://openairdocs.org/sdr/A6WA200460012.md): Angle · cracked · Apr 12, 2004 · N615AW · Bag BAE146300A · Nacelle/Pylon Miscellaneous Structure
  > FOUND CRACK IN THE NR 4 PYLON AT THE FORWARD END OF THE CENTER ANGLE JUST AFT OF RIB NR 3. REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX FAX 615-18830001. (M)
- [SDR AUS20040237](https://openairdocs.org/sdr/AUS20040237.md): Pin · cracked · Mar 31, 2004 · Bag BAE146300A · Trailing Edge Flap Control System
  > (AUS) FAIL SAFE PIN ASSEMBLY OF THE RT FLAP TAB NR 2 HINGE BOLT CRACKED. FOUND DURING NDT INSPECTION.
- [SDR AUS20040148](https://openairdocs.org/sdr/AUS20040148.md): Plate · corroded · Mar 3, 2004 · Bag BAE146300A · Elevator, Tab Structure
  > (AUS) RT ELEVATOR TAB NR 1 HINGE UPPER REINFORCEMENT PLATE CONTAINED LEVEL 2 CORROSION. CORROSION DIMENSIONS WERE 25.4MM (1IN) BY50.8MM (2IN) AND PENETRATING TO FULL DEPTH.
- [SDR AUS20040129](https://openairdocs.org/sdr/AUS20040129.md): Bolt · cracked · Feb 26, 2004 · Bag BAE146300A · Fasteners
  > (AUS) RUDDER FIXED HINGE BOLT CRACKED UNDER BOLT HEAD. BOLT IS LOCATED AT VERTICAL STABILISER RIB 5. CRACK LENGTH 2.286MM (0.090IN). FOUND DURING NDT INSPECTION.
- [SDR AUS20040065](https://openairdocs.org/sdr/AUS20040065.md): Harness · faulty · Feb 5, 2004 · Bag BAE146300A · Fire Detection
  > (AUS) NR 4 ENGINE FIRE WARNING SYSTEM WIRING HARNESS FAULTY.
- [SDR AUS20031342](https://openairdocs.org/sdr/AUS20031342.md): Display · wrong part · Dec 12, 2003 · Bag BAE146300A · Flight Environment Data
  > (AUS) ELECTRONIC DISPLAY UNIT (EDU) WAS INCORRECT PART. MANUFACTURERS AME PLATE WAS IN RED WHICH INDICATED THAT IT WAS AN ENGINEERING EVALUATION UNIT. THE AIRWORTHY UNITS HAVE A BLACK NAMEPLATE. AND CARRY THE PN 4066192-901. PERSONNEL/MAINTENANCE ERROR. U
- [SDR A6WA200360044](https://openairdocs.org/sdr/A6WA200360044.md): Skin · lightning strike · Oct 2, 2003 · N611AW · Bag BAE146300A · Fuselage Main, Plate/Skin
  > DAMAGE NOTED ON LEFT SIDE OF FUSELAGE DURING LIGHTNING STRIKE INSPECTION. EXIT BURN MARK LOCATED 8 INCHES AFT OF FRAME 19C BETWEEN STRINGER 21 AND 22 AT CENTER AND APPROX.375 INCH IN DIAMETER BY.010 INCHES DEPTH. MAINTENANCE BLENDED DAMAGE TO A SMOOTH MIRRO
- [SDR AUS20030929](https://openairdocs.org/sdr/AUS20030929.md): Gcu · failed · Sep 12, 2003 · Bag BAE146300A · AC Regulator
  > (AUS) NR 1 GENERATOR CONTROL UNIT (GCU) FAILED.
- [SDR AUS20030922](https://openairdocs.org/sdr/AUS20030922.md): Hose · ruptured · Sep 10, 2003 · Bag BAE146300A · Landing Gear Retraction/Extension System
  > (AUS) LT MLG RETRACTION JACK FLEXIBLE HYDRAULIC HOSE RUPTURED. LOSS OF GREEN SYSTEM HYD FLUID.
- [SDR AUS20030830](https://openairdocs.org/sdr/AUS20030830.md): Seal · failed · Aug 17, 2003 · Bag BAE146300A · Drag Control System
  > (AUS) LT GROUND SPOILER FLOW VALVE RETURN LINE CONNECTOR O-RING SEAL LEAKING. GRADUAL LOSS OF APPROXIMATELY TEN LITRES OF HYDRAULIC FLUID.
- [SDR AUS20030555](https://openairdocs.org/sdr/AUS20030555.md): Skin · corroded · Jun 4, 2003 · Bag BAE146300A · Wing, Plate/Skin
  > (AUS) LT AND RT LOWER WING SKINS CORRODED IN AREA OF FUEL PUMP WATER SCAVENGE GUARDS AT RIB 15. FOUND DURING INSPECTION IAW ER BA6-28-10-7 AND ISB 28-028.
- [SDR AUS20030410](https://openairdocs.org/sdr/AUS20030410.md): Speed Brake · faulty · Apr 9, 2003 · Bag BAE146300A · Drag Control System
  > (AUS) UNCOMMANDED AIRBRAKE OPERATION. EXTENSIVE INVESTIGATION AND TESTING COULD FIND NO CAUSE FOR THE PROBLEM.
- [SDR AUS20030363](https://openairdocs.org/sdr/AUS20030363.md): Pin · damaged · Mar 23, 2003 · Bag BAE146300A · Main Landing Gear Strut/Axle/Truck
  > (AUS) LT MAIN LANDING GEAR DIRECTIONAL LINK UPPER ATTACHMENT PIN FOUND TO BE MIGRATING FROM THE LUG LOCATED AT FRAME 29. LOCKING PLATE AND PIN INCORRECTLY FITTED. MAIN LANDING GEAR IS A NEWLYOVERHAULED UNIT AND HAD ONLY JUST BEEN FITTED TO THE AIRCRAFT 48CYCLE
- [SDR AUS20030121](https://openairdocs.org/sdr/AUS20030121.md): Skin · corroded · Feb 6, 2003 · Bag BAE146300A · Wing, Plate/Skin
  > (AUS) RT LOWER WING SKIN CHAFED ON WATER SCAVENGE PIPE DEBRIS GUARDS. CORROSION WAS ALSO FOUND IN THE SAME AREA BETWEEN FRAME 14 AND FRAME 15.
- [SDR AUS20030120](https://openairdocs.org/sdr/AUS20030120.md): Skin · corroded · Feb 6, 2003 · Bag BAE146300A · Wing, Plate/Skin
  > (AUS) LT WING LOWER SKIN CORRODED BEYOND LIMITS. FOUND DURING X-RAY INSPECTION.
- [SDR AUS20021456](https://openairdocs.org/sdr/AUS20021456.md): Wire · worn · Dec 28, 2002 · Bag BAE146300A · Electrical Power System Wiring
  > (AUS) NR 4 GENERATOR DIFFERENTIAL PROTECTION CIRCUIT WIRE XB108 CHAFED IN AREA ADJACENT TO IDG.
- [SDR AUS20021452](https://openairdocs.org/sdr/AUS20021452.md): Circuit Board · faulty · Dec 10, 2002 · Bag BAE146300A · Landing Gear Position and Warning
  > (AUS) RT MAIN LANDING GEAR UPLOCK SENSOR PRINTED CIRCUIT BOARD (GJ21) FAULTY.
- [SDR AUS20021338](https://openairdocs.org/sdr/AUS20021338.md): Cable · chafed · Nov 15, 2002 · Bag BAE146300A · Power Lever
  > (AUS) NR 4 THROTTLE LEVER CABLE FOULING ON CENTER ROOF PANEL. PREVIOUS MAINTENANCE HAD BEEN CARRIED OUT FOR BATTERY PACK REPLACEMENT. PERSONNEL/MAINTENANCE ERROR.
- [SDR AUS20021184](https://openairdocs.org/sdr/AUS20021184.md): Manifold · leaking · Oct 18, 2002 · Bag BAE146300A · Engine Fuel Distribution
  > (AUS) NR 3 ENGINE RT FUEL MANIFOLD LEAKING AT MANIFOLD TO COMBUSTOR CASE JOIN. EVIDENCE OF FIRE AROUND LEAK.
- [SDR A6WA200260044](https://openairdocs.org/sdr/A6WA200260044.md): Floor Support · corroded · Oct 10, 2002 · Bag BAE146300A · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON FLOOR SUPPORT STRUCTURE FRAME 15 - 2.5 INCH PORT OF AIRCRAFT CENTERLINE RIL.
- [SDR AUS20021106](https://openairdocs.org/sdr/AUS20021106.md): Cooling Fan · failed · Oct 7, 2002 · Bag BAE146300A · Air Distribution Fan
  > (AUS) LT ELECTRONIC FLIGHT INDICATION SYSTEM (EFIS) FAN FAILED. INVESTIGATION FOUND FAN BLADE CRACKED AND RUBBING ON GRILL.
- [SDR AUS20020714](https://openairdocs.org/sdr/AUS20020714.md): Brake · overheated · Jul 6, 2002 · Bag BAE146300A · Brake
  > (AUS) BOTH LT MAIN LANDING GEAR BRAKES OVERHEATED TO 800 DEGREES C.
- [SDR AUS20020591](https://openairdocs.org/sdr/AUS20020591.md): Buss · failed · Jun 13, 2002 · Bag BAE146300A · AC Generation System
  > (AUS) NR 2 AC BUS FAILED. THE FOLLOWING COMPONENTS WERE REPLACED:- 1. NR 4 GENERATOR CONTROL UNIT 2. GENERATOR LINE CONTACTOR 4XB33. NR 4 ENGINE GENERATOR AND CSD

Next page: https://openairdocs.org/model/british-aerospace-bae-146-series-300a/reports.md?page=2

## 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 = 'BAE146300A'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/british-aerospace-bae-146-series-300a/reports

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