# Service difficulty reports: British Aerospace BAE 146 SERIES 100A

A list on [British Aerospace BAE 146 SERIES 100A](https://openairdocs.org/model/british-aerospace-bae-146-series-100a.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 4 · 188 reports

- [SDR AU510001710](https://openairdocs.org/sdr/AU510001710.md): Frame · cracked · Oct 8, 2005 · Bag BAE146100A · Fuselage Main, Frame
  > FUSELAGE FRAME 15 AND FRAME 41 CRACKED. FOUND DURING INSPECTION IAW AD/BAE146/116.
- [SDR AU510001880](https://openairdocs.org/sdr/AU510001880.md): Frame · cracked · May 9, 2005 · Bag BAE146100A · Fuselage Main, Frame
  > FUSELAGE FRAMES 15 AND 18 CRACKED, FOUND DURING INSPECTION IAW AD/BAE146/116.
- [SDR AUS20010835](https://openairdocs.org/sdr/AUS20010835.md): Fastener · corroded · Aug 1, 2001 · Bag BAE146100A · Fuselage Main, Frame
  > (AUS) DURING INSPECTION FOR LOCATION OF CENTRE FUEL TANK LEAK THE FOLLOWING DEFECTS WERE FOUND: 1. FRAME 29 LT HAND UPPER SIDE (AFT WING ATTACHMENTS) FASTENER IN POSITION NR 11 FOUND WITH SHEARED HEAD 2. FRAME 29 RIGHT HAND UPPER SIDE (AFT WING ATTACHMENT) FAS
- [SDR AUS20010857](https://openairdocs.org/sdr/AUS20010857.md): Skin · corroded · Jul 16, 2001 · Bag BAE146100A · Wing, Plate/Skin
  > (AUS) LT WING LOWER SKIN CORRODED IN AREA BETWEEN RIB 13 AND RIB 15.CORROSION WAS BEYOND ALLOWIABLE LIMITS.
- [SDR AUS20010619](https://openairdocs.org/sdr/AUS20010619.md): Engine · leaking · Jun 16, 2001 · Bag BAE146100A · Engine (Turbine/Turboprop)
  > (AUS) NR 2 ENGINE LEAKING CONTAMINATED AIR INTO CABIN.
- [SDR AUS20010421](https://openairdocs.org/sdr/AUS20010421.md): Fire Bottle · misinstalled · May 14, 2001 · Bag BAE146100A · Fire Bottle, Fixed
  > (AUS) NR 3 ENGINE FIRE BOTTLE FIRING SWITCH WIRING CONTAINED TWO INLINESPLICES FITTED WITH SMALLER GAUGE WIRES. UNAPPROVED MODIFICATION. PERSONNEL/MAINTENANCE ERROR.
- [SDR AUS20010480](https://openairdocs.org/sdr/AUS20010480.md): Cooling Fan · failed · May 5, 2001 · Bag BAE146100A · Air Distribution Fan
  > (AUS) CABIN FAN FAILED. INVESTIGATION FOUND BOTH FORE AND AFT FAN MOTOR SHAFT BEARINGS FAILED. THE MOTOR ALSO FAILED ELECTRICALLY WITHSIGNS OF OVERHEATING. BEARING PNO S38SS6CXOG33 AND PNOS100SS6CXOG33.
- [SDR AUS20010424](https://openairdocs.org/sdr/AUS20010424.md): Transceiver · intermittent · May 3, 2001 · Bag BAE146100A · Altimeter, Barometric/Encoder
  > (AUS) RADIO ALTIMETER TRANSCEIVER INTERMITTENT OPERATION. INVESTIGATION FOUND THE FAULT WAS DUE TO A STRAY VOLTAGE ON A SPARE PIN IN THETRANSCEIVER DUE TO A WIRE FITTED BY A PREVIOUS OPERATOR. THEMODIFICATION WAS NOT NOTIFIED TO THE MANUFACTURER AND THE WIRING
- [SDR AUS20010535](https://openairdocs.org/sdr/AUS20010535.md): Spar · corroded · Apr 26, 2001 · Bag BAE146100A · Wing Spar
  > (AUS) LT AND RT WING FORWARD AND AFT SPAR LOWER FLANGES CORRODED IN AREA BETWEEN RIB 13 AND RIB 18.
- [SDR AU010321](https://openairdocs.org/sdr/AU010321.md): Pipe · loose · Apr 10, 2001 · Bag BAE146100A · Fuel Controlling System
  > (AUS) NO3 ENGINE P3 SENSE LINE TO FCU LOOSE. THE AIRCRAFT HAD A NO3 ENGINE AND FCU CHANGED THE PREVIOUS DAY. PERSONNEL/MAINTENANCEERROR.
- [SDR AU010192](https://openairdocs.org/sdr/AU010192.md): Wire · loose · Mar 12, 2001 · Bag BAE146100A · Navigation System Wiring
  > (AUS) NR 2 COMPASS SYSTEM FAULTY. INVESTIGATION FOUND A LOOSE WIRE TERMINAL AND NUT ON THE RT FLUX VALVE TERMINAL BLOCK LOCATED AT THE RH OUTER WING TRAILING EDGE.
- [SDR AU010257](https://openairdocs.org/sdr/AU010257.md): Spar · corroded · Feb 13, 2001 · Bag BAE146100A · Wing Spar
  > (AUS) LT AND RT WING FORWARD AND AFT SPAR LOWER FLANGES CORRODED.
- [SDR AU010259](https://openairdocs.org/sdr/AU010259.md): Skin · corroded · Feb 12, 2001 · Bag BAE146100A · Wing, Plate/Skin
  > (AUS) LT WING LOWER SKIN CORRODED AT RIB BAYS NR 14 TO NR 16. RT WING LOWER SKIN CORRODED AT RIB BAYS NR 14 AND NR 15.
- [SDR AU010258](https://openairdocs.org/sdr/AU010258.md): Spar · cracked · Feb 12, 2001 · Bag BAE146100A · Wing Spar
  > (AUS) LT AND RT WING FORWARD AND AFT LOWER SPAR CAPS CRACKED IN AREABETWEEN RIBS NR 13 AND NR 18. CORROSION ALSO FOUND ON LOWER SKINS AT RIB BAYS NR 13 TO NR 18.
- [SDR AU001029](https://openairdocs.org/sdr/AU001029.md): Generator · faulty · Oct 23, 2000 · Bag BAE146100A · AC Generation System
  > (AUS) NR 1 GENERATOR WENT OFF LINE. GENERATOR CONTROL UNIT AND LINE CONTACTOR CHANGED AND WIRING INSPECTED WITH NIL FAULTS FOUND. INVESTIGATION CONTINUING.
- [SDR AU000935](https://openairdocs.org/sdr/AU000935.md): Cdu · faulty · Sep 16, 2000 · Bag BAE146100A · Flight Management Computing Hardware System
  > (AUS) GPS CENTRAL DATA UNIT (CDU) LOCKED UP. GPS WOULD NOT TRACK.
- [SDR AU000829](https://openairdocs.org/sdr/AU000829.md): Wire · faulty · Sep 6, 2000 · Bag BAE146100A · Communications System Wiring
  > (AUS) GROUND CALL HORN WIRE FAULTY.
- [SDR AU000828](https://openairdocs.org/sdr/AU000828.md): Light · failed · Sep 5, 2000 · Bag BAE146100A · Passenger Compartment Lighting
  > (AUS) LAMP HOLDERS LOCATED AT ROW 14 AND ROW 10 ON THE RT SIDE WALLS BURNED OUT.
- [SDR AU000943](https://openairdocs.org/sdr/AU000943.md): Indicator · fluctuates · Sep 4, 2000 · Bag BAE146100A · Engine EGT/TIT Indicating System
  > (AUS) NR 2 ENGINE EGT INDICATOR FLUCTUATING.
- [SDR AU000690](https://openairdocs.org/sdr/AU000690.md): Spar · cracked · Sep 1, 2000 · Bag BAE146100A · Wing Spar
  > (AUS) LT AND RT WINGS FORWARD AND REAR SPARS CRACKED IN AREA LOCATED OUTBOARD OF RIB NR 13.
- [SDR AU000689](https://openairdocs.org/sdr/AU000689.md): Indicator · faulty · Sep 1, 2000 · Bag BAE146100A · Airspeed/Mach Indicator
  > (AUS) AIR SPEED INDICATOR FAULTY.
- [SDR AU000666](https://openairdocs.org/sdr/AU000666.md): Engine · failed · Sep 1, 2000 · Bag BAE146100A · Engine (Turbine/Turboprop)
  > (AUS) NR 2 ENGINE TGT EXCEEDED 900 DEGREES AND FLAMES CAME FROM THEENGINE. THE ENGINE WAS REMOVED AND SENT FOR INVESTIGATION AND REPAIR.
- [SDR AU000651](https://openairdocs.org/sdr/AU000651.md): Seal · leaking · Sep 1, 2000 · Bag BAE146100A · Turbine Engine Compressor Section
  > (AUS) ENGINE NR 1 BEARING SEAL LEAKING.
- [SDR AU000631](https://openairdocs.org/sdr/AU000631.md): Turbine Nozzle · failed · Sep 1, 2000 · Bag BAE146100A · Turbine Section
  > (AUS) NR 2 ENGINE FAILED ON TAKEOFF WITH THE TGT EXCEEDING 1000 DEGREESC. SUSPECT CAUSED BY FAILURE OF THE SECOND STAGE HP TURBINE NOZZLE.
- [SDR AU000630](https://openairdocs.org/sdr/AU000630.md): Engine · vibrates · Sep 1, 2000 · Bag BAE146100A · Engine (Turbine/Turboprop)
  > (AUS) NO1 ENGINE VIBRATION WITH INDICATION OF 1.5. GROUND CHECKS COULDFIND NO PROBLEMS AND AIRCRAFT RETURNED TO SERVICE. SUSPECT ICING.
- [SDR AU000936](https://openairdocs.org/sdr/AU000936.md): Trim Tab · damaged · Jul 16, 2000 · Bag BAE146100A · Aileron Tabs
  > (AUS) LT AILERON TRIM TAB DAMAGED DURING GROUND OPERATION.
- [SDR AU000219](https://openairdocs.org/sdr/AU000219.md): Pipe · failed · Apr 24, 2000 · Bag BAE146100A · Engine Fuel Distribution
  > (AUS) ENGINE FUEL PIPE FAILED. FUEL LEAK.
- [SDR AU000277](https://openairdocs.org/sdr/AU000277.md): Indicator · shorted · Apr 11, 2000 · Bag BAE146100A · Landing Gear Position and Warning
  > (AUS) RT MAIN LANDING GEAR STANDBY INDICATOR LAMP SHORT CIRCUIT.
- [SDR CA000320002](https://openairdocs.org/sdr/CA000320002.md): Wire · chafed · Mar 8, 2000 · Bag BAE146100A · DC Generating System
  > (CAN) NR 1 GENERATOR HARNESS WIRE FOUND CHAFED. WIRE REPAIRED.
- [SDR 2000ZZZX179](https://openairdocs.org/sdr/2000ZZZX179.md): Driveshaft · worn · Dec 22, 1999 · Bag BAE146100A · Engine Fuel Pump
  > ENGINE SHUTDOWN IN-FLIGHT. DRIVE SPLINES ON FUEL PUMP SEVERELY WORN. PUMP TO BE OVERHAULED. HIGH OPERATING TIME LED TO FAILIURE.
- [SDR AU990787](https://openairdocs.org/sdr/AU990787.md): Skin · cracked · Aug 9, 1999 · Bag BAE146100A · Fuselage Main, Plate/Skin
  > (AUS) FUSELAGE SKIN CRACKED IN THE AREA OF FRAME 29 LOCATED BETWEEN STRINGER NR 12 AND STRINGER NR 13. FOUND DURING INSPECTION IAW AD/BAE/146/70. LIMITED INFORMATION PROVIDED.
- [SDR AU990804](https://openairdocs.org/sdr/AU990804.md): Gcu · faulty · Jul 26, 1999 · Bag BAE146100A · AC Regulator
  > (AUS) NR 2 AC BUS FAILED. GENERATOR CONTROL UNIT REPLACED.
- [SDR A6WA9900049](https://openairdocs.org/sdr/A6WA9900049.md): Angle · cracked · May 29, 1999 · N463AP · Bag BAE146100A · Passenger/Crew Doors
  > FORWARD PASSENGER DOOR, INTERNAL ANGLE CRACKED. REPLACED ANGLE. (X)
- [SDR A6WA9900048](https://openairdocs.org/sdr/A6WA9900048.md): Skin · damaged · May 29, 1999 · N463AP · Bag BAE146100A · Fuselage Main, Plate/Skin
  > REPAIR TO RIGHT SIDE OF FUSELAGE AT FRAMES 11-13 AT LAP 'E' AREA. C/W REPAIR IAW BAE 146 SRM AND FAX CW/RJ/0754-99, CW/RJ/0761-99 AND DRAWING HC537H9411. (X)
- [SDR AU990524](https://openairdocs.org/sdr/AU990524.md): Spoiler · faulty · May 28, 1999 · Bag BAE146100A · Drag Control System
  > (AUS) MANUAL SPOILER CAUTION LIGHT ILLUMINATED AFTER TAKEOFF. THE FAULT WAS UNABLE TO BE REPRODUCED ON THE GROUND AND THE AIRCRAFT HAS SINCE FLOWN SERVICEABLE. DEFECT NOT CONFIRMED.
- [SDR AU990512](https://openairdocs.org/sdr/AU990512.md): Warning System · illuminated · May 28, 1999 · Bag BAE146100A · Drag Control System
  > (AUS) MANUAL SPOILER FAULT LIGHT ILLUMINATED. INVESTIGATION COULD FIND NO DEFECT. PCB CHX6 RE-RACKED.
- [SDR A6WA9900054](https://openairdocs.org/sdr/A6WA9900054.md): Stiffener · cracked · May 7, 1999 · N463AP · Bag BAE146100A · Wing Miscellaneous Structure
  > LEFT WING TRAILING EDGE UPPER SHROUD SKIN STIFFENER NR 176 BEWEEN RIBS 7 AND 8 CRACKED, FORWARD END. REPLACED LEFT WING TRAILING EDGE UPPER SHROUD SKIN STIFFENER BETWEEN RIBS 7 AND 8. (X)
- [SDR A6WA9900053](https://openairdocs.org/sdr/A6WA9900053.md): Stiffener · cracked · May 7, 1999 · N463AP · Bag BAE146100A · Wing Miscellaneous Structure
  > RIGHT WING TRAILING EDGE UPPER SHROUD SKIN STIFFENER, NR 176 BETWEEN RIBS 7 AND 8, CRACKED FORWARD END. REPAIRED RT WING TRAILING EDGE UPPER SHROUD SKIN STIFFENER BETWEEN RIBS 7 AND 8 IAW BAE FAX DJR/RJ0630-98. (X)
- [SDR A6WA9900052](https://openairdocs.org/sdr/A6WA9900052.md): Stiffener · cracked · May 7, 1999 · N463AP · Bag BAE146100A · Wing Miscellaneous Structure
  > RIGHT WING TRAILING EDGE UPPER SHROUD SKIN STIFFENER, NR 172 BETWEEN RIBS 3 AND 4, CRACKED FORWARD END. REPLACED RT WING TRAILING EDGE UPPER SHROUD SKIN STIFFENER BETWEEN RIBS 3 AND 4. (X)
- [SDR A6WA9900051](https://openairdocs.org/sdr/A6WA9900051.md): Stiffener · cracked · May 7, 1999 · N463AP · Bag BAE146100A · Wing Miscellaneous Structure
  > LEFT WING TRAILING EDGE UPPER SHROUD SKIN STIFFENER, NR 178 BETWEN RIBS 8 AND 9, CRACKED FORWARD END. REPLACED LT WING TRAILING EDGE UPPER SHROUD SKIN STIFFENER BETWEEN RIBS 8 AND 9. (X)
- [SDR 17WA9900050](https://openairdocs.org/sdr/17WA9900050.md): Stiffener · cracked · May 7, 1999 · N463AP · Bag BAE146100A · Wing Miscellaneous Structure
  > LEFT WING TRAILING EDGE UPPER SHROUD SKIN STIFFENER NR 177 BETWEEN RIBS 8 AND 9 CRACKED FORWARD END. REPAIRED LEFT WING SKIN TRAILING EDGE, UPPER WING SKIN TRAILING EDGE STIFFENER BETWEEN RIBS 8 AND 9 IAW BAE FAX DJR/RJ0630-98. (X)
- [SDR AU990442](https://openairdocs.org/sdr/AU990442.md): Transducer · malfunctioned · May 6, 1999 · Bag BAE146100A · Engine Oil Pressure
  > (AUS) NR 3 ENGINE OIL PRESSURE TRANSDUCER FAULTY.
- [SDR AU990423](https://openairdocs.org/sdr/AU990423.md): Switch · faulty · May 4, 1999 · Bag BAE146100A · Cabin Temperature Control System
  > (AUS) AIR CONDITIONING PACK FLOW SWITCH FAULTY.
- [SDR A6WA9900055](https://openairdocs.org/sdr/A6WA9900055.md): Stiffener · cracked · Apr 21, 1999 · N463AP · Bag BAE146100A · Wing Miscellaneous Structure
  > UPPER WING SKIN TRAILING EDGE STIFFENER IS CRACKED AT FORWARD END LOCATED BETWEEN RIBS 9 AND 10, LEFT WING. REPAIRED LT WING SKIN TRAILING EDGE UPPER WING SKIN STIFFENER BETWEEN RIBS 9 AND 10 IAW BAE FAX DJR/RJ0630-98. (X)
- [SDR AU990415](https://openairdocs.org/sdr/AU990415.md): Floorbeam · cracked · Apr 7, 1999 · Bag BAE146100A · Fuselage Main, Floor Beam
  > (AUS) CRACKS FOUND IN FLOOR BEAM AT FRAME 18 LOCATED ON THE RIGHT SIDE JUST BELOW THE FLOOR LINE.
- [SDR 99ZZZX2700](https://openairdocs.org/sdr/99ZZZX2700.md): Slide · deployed · Jan 1, 1999 · N463AP · Bag BAE146100A · Emergency Equipment
  > ORD - FLT 545 - WHILE INSPECTING GIVE BAR MECHANISM ON FORWARD PASSENGER DOOR, SLIDE PARTIALLY DEPLOYED. REMOVED AND REPLACED FORWARD PASSENGER DOOR SLIDE IAW MM.
- [SDR 99ZZZM548](https://openairdocs.org/sdr/99ZZZM548.md): Slide · out of position · Jan 1, 1999 · N463AP · Bag BAE146100A · Escape Slide
  > WHILE INSPECTIONG GIVE BAR MECHANISM ON FORWARD PASSENGER DOOR SLIDE PARTIALLY DEPLOYED. REMOVED AND REPLACED FORWARD PASSENGER DOOR SLIDE IAW MM. (M)
- [SDR AU981563](https://openairdocs.org/sdr/AU981563.md): Link · corroded · Nov 22, 1998 · Bag BAE146100A · Landing Gear Door Retract Section
  > (AUS) MAIN LANDING GEAR DOOR RT AND LT FORWARD HINGE LINKS CORRODED BEYOND LIMITS. LINKS P/N HC321H0026-002, P/N HC321B0045-002, AND P/N HC321B0043-001.
- [SDR AU981461](https://openairdocs.org/sdr/AU981461.md): Sensor · malfunctioned · Nov 7, 1998 · Bag BAE146100A · Landing Gear Position and Warning
  > (AUS) EFT MAIN LANDING GEAR UPLOCK PROXIMITY SENSOR FAULTY.
- [SDR AU981205](https://openairdocs.org/sdr/AU981205.md): Warning System · activated · Sep 21, 1998 · Bag BAE146100A · Drag Control System
  > (AUS) MANUAL SPOILER FAULT LIGHT ILLUMINATED. SYSTEM CHECKED, BUT NO REASON FOR THE FAULT COULD BE FOUND. DEFECT HAS NOT OCCURRED SINCE.

Next page: https://openairdocs.org/model/british-aerospace-bae-146-series-100a/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 = 'BAE146100A'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/british-aerospace-bae-146-series-100a/reports

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