# Service difficulty reports: British Aerospace BAE 146 SERIES 200A

A list on [British Aerospace BAE 146 SERIES 200A](https://openairdocs.org/model/british-aerospace-bae-146-series-200a.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 20 · 954 reports

- [SDR NI6R202508200065](https://openairdocs.org/sdr/NI6R202508200065.md): Seal · leaking · Aug 20, 2025 · N470NA · Bag BAE146200A · Nacelle/Pylon, Main Frame
  > ENROUTE TO THE BEULAH INCIDENT, APPROXIMATELY 30 MILES EAST OF HIF, THE PYLON 3 OVHT LIGHT ILLUMINATED ON THE MWP. THE ENGINES WERE SET TO CLIMB THRUST OF 800 TGT WHEN THE LIGHT CAME ON. WE COMPLETED THE QRH PROCEDURE FOR PYLON OVERHEAT AND TURNED TOWARD THE N
- [SDR NI6R202505150060](https://openairdocs.org/sdr/NI6R202505150060.md): Wheel · cracked · May 15, 2025 · N477NA · Bag BAE146200A · Wheel/Ski/Float
  > AFTER AIRCRAFT DEPARTURE FROM GATEWAY AIRTANKER BASE, MESA, AZ, GROUND PERSONNEL FOUND A PIECE OF AIRCRAFT WHEEL LIP ON THE GROUND. THE SUSPECT AIRCRAFT WAS ENROUTE TO ALBUQUERQUE AIR TANKER BASE. THE BASE AND FLIGHT CREW WERE NOTIFIED THAT THERE COULD POTENTI
- [SDR CA071108007](https://openairdocs.org/sdr/CA071108007.md): Link · unserviceable · Nov 7, 2007 · Bag BAE146200A · Main Landing Gear
  > (CAN) IT HAS BEEN DISCOVERED DURING INSPECTION OF THE ABOVE MENTIONED PART THAT IT IS IN AN UNSERVICEABLE CONDITION. WHILE ON JACKS THE COMPONENT WAS INSPECTED AND MOVEMENT COULD BE FELT BETWEEN THE ROD ASSY AND EYE END. THE EYE END IS THREADED INTO THE ROD FO
- [SDR A6WA200560021](https://openairdocs.org/sdr/A6WA200560021.md): Flap System · malfunctioned · Mar 6, 2006 · N607AW · Bag BAE146200A · Trailing Flap Position Indicating System
  > WHEN DEPARTING, FLAPS FAIL AT 18 DEGREES. BOTH FLAP INOP LIGHT AND FLAP FAULT LIGHT ILLUMINATED, FOLLOW ALL QRH CHECKLIST LANDING. ECU FAULT LED NR 4 SHOWING C/W AMM, FLAPS RESET. FAULT LED 1 AND 2 AND 8 SHOWING, ACCOMPLISHED SL2 RESET. RAN FLAPS 0-33 DEGR
- [SDR AU510002070](https://openairdocs.org/sdr/AU510002070.md): Anti-Skid Sys · faulty · Dec 12, 2005 · Bag BAE146200A · Brake Anti-Skid Section
  > FOLLOWING TWO BURST TIRES ON NR 1 MAIN WHEEL, MAINTENANCE CHANGED THE GREEN SYSTEM ANTI-SKID VALVE FOR NR 1 WHEEL POSITION. INVESTIGATION CONTINUING.
- [SDR A6WA200560020](https://openairdocs.org/sdr/A6WA200560020.md): Seal · leaking · Dec 3, 2005 · N290UE · Bag BAE146200A · Pneumatic Distribution System
  > RT ZONE HI TEMP CAPTAIN ILLUMINATED ENROUTE IN ICING CONDITIONS. REPLACED SEALS AT NR 4 PYLON LEADING EDGE AND LEAK CHECKED WING ANTI-ICE. OPS CHECKED GOOD. (K)
- [SDR A6WA200560017](https://openairdocs.org/sdr/A6WA200560017.md): Apu · bird ingestion · Jul 30, 2005 · N610AW · Bag BAE146200A · APU Core Engine
  > SMOKE IN CABIN WHEN TURNING ON PACKS. MAINTNANCE C/W EO, BOTH AC PACKS. FOUND BIRD AND OIL IN APU INTAKE. REMOVED AND REPLACED APU, BOTH AC PACKS, JET PUMPS AND WATER INJECTOS IAW EO, SYSTEM OPS CHECK GOOD. (K)
- [SDR A6WA200560016](https://openairdocs.org/sdr/A6WA200560016.md): Fuel Control · unserviceable · Jul 14, 2005 · N179US · Bag BAE146200A · Fuel Control/Turbine Engines
  > CLIMBING THRU 9000 FT NR 1 ENGINE STARTED TO WIND DOWN. BOTH N1 AND N2 WERE DROPPING, TGT APPEARED TO BE RISING. SECURED ENGINE, PERFORMED IMMEDIATE ACTION CHECKLIST C/W QRH. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE. (K)
- [SDR A6WA200460055](https://openairdocs.org/sdr/A6WA200460055.md): Acm · malfunctioned · Nov 11, 2004 · N606AW · Bag BAE146200A · Cabin Cooling System
  > NR PACK TEMP IS UNCONTROLLABLE IN EITHER MANUAL OR AUTO WHEN USING APU AIR. WILL RUN FULL HOT AND SMOKES CABIN. NOTE: CONTROLLABLE IN (MAN) MODE WITH ENGINE AIR, OTHERWISE SMOKES CABIN. PACK NR 2 HIGH TEMP LIGHT COMES ON. MAINTENANCE REMOVED AND REPLACED N
- [SDR A6WA200460040](https://openairdocs.org/sdr/A6WA200460040.md): Structure · cracked · Sep 21, 2004 · N181US · Bag BAE146200A · Spoilers
  > AIRBRAKE STRUCTURE AFT OF FRAME 50 VERTICAL STIFFENER HAS A CRACK RADIATING FROM RIVET. REPAIR IN PROGRESS. (M)
- [SDR A6WA200460036](https://openairdocs.org/sdr/A6WA200460036.md): Frame · cracked · Sep 3, 2004 · N156TR · Bag BAE146200A · Fuselage Main, Frame
  > FOUND CRACK JUST AFT OF FRAME 29 RIGHT EMANATING FROM A RIVET. MAINTENANCE REQUESTED A REPAIR FROM BAE SYSTEMS REF AVMAX 656-2015002. (M)
- [SDR A6WA200460035](https://openairdocs.org/sdr/A6WA200460035.md): Skin · cracked · Sep 3, 2004 · N156TR · Bag BAE146200A · Fuselage Main, Plate/Skin
  > FOUND CRACK JUST AFT OF FRAME 39 LEFT EMANATING FROM A RIVET. MAINTENANCE REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX FAX 656-2015001. (M)
- [SDR A6WA20046002](https://openairdocs.org/sdr/A6WA20046002.md): Ecu · malfunctioned · Jun 13, 2004 · N610AW · Bag BAE146200A · Trailing Edge Flap Control System
  > WHEN FLAPS SELECTED FOR 24-33 DEGREES ON TO ASE, FLAP FAULTS AND INOPERATIVE LIGHTS ILLUMINATED FLAPS STUCK AT 24 DEGREES AIRCRAFT RETURNED TO DEN. MAINTENANCE FOUND CODE 4 ON FLAP ECU, RESET ECU, NO FAULTS. NOTED. (M)
- [SDR AUS20040414](https://openairdocs.org/sdr/AUS20040414.md): Seal · leaking · May 15, 2004 · Bag BAE146200A · Landing Gear Actuator
  > (AUS) RT MAIN LANDING GEAR ACTUATOR RESTRICTOR SEAL LEAKING.
- [SDR A6WA200460015](https://openairdocs.org/sdr/A6WA200460015.md): Flap Track · worn · May 12, 2004 · N607AW · Bag BAE146200A · Trailing Edge Flaps
  > NR 2 FLAP TRACK, WEAR FOUND ON NR 2 LT LOWER ROLLER THAT MEASURES.033 INCHES DEEP. REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX FAX 607-1907002. MAINTENANCE REMOVED LOWER CARRIAGE NR 2 LEFT. ROLLERS REPLACED IAW CMM 57-50-22. CARRIAGE REINSTALLED IAW AMM 2
- [SDR A6WA200460010](https://openairdocs.org/sdr/A6WA200460010.md): Shaft Seal · leaking · Mar 22, 2004 · N156TR · Bag BAE146200A · APU Oil System
  > STRONG ODOR IN COCKPIT, EYES BURNING WITH AC PACKS ON. MAINTENANCE PERFORMED PACK BURN OUT PROCEDURE. REMOVED AND REPLACED APU ASSEMBLY. (M)
- [SDR A6WA200460006](https://openairdocs.org/sdr/A6WA200460006.md): Turbine Wheel · damaged · Mar 10, 2004 · N181US · Bag BAE146200A · Turbine Section
  > NR 4 ENGINE, 4TH TURBINE WHEEL LOST HEAD OF RIVET WHICH HOLDS BLADE IN PLACE, CAUSING IMPACT DAMAGE TO 4TH NOZZLE CONTAINMENT RIGHT. MAINTENANCE REMOVED AND REPLACED 4TH T-WHEEL ASSEMBLY. (M)
- [SDR A6WA200360069](https://openairdocs.org/sdr/A6WA200360069.md): Skin · damaged · Dec 9, 2003 · N607AW · Bag BAE146200A · Fuselage Main, Plate/Skin
  > FOUND CRACKS ON THE LEFT AND RIGHT FUSELAGE ABOVE STRINGER 13 JUST AFT OF FRAME 29 EMANATING FROM THE RIVIT LOCATIONS. MAINTENANCE CUT OUT DAMAGE TO SKIN IAW BAE FAX BARA/AVR/6603/03-DC. NDT HFEC CARRIED OT IAW BAE FAX BARA/AVR/6603/03-DC, NO CRACKS NOTED.
- [SDR A6WA200360067](https://openairdocs.org/sdr/A6WA200360067.md): Structure · damaged · Dec 9, 2003 · N607AW · Bag BAE146200A · Trailing Edge Flaps
  > RIGHT FLAP AT THE NR 4 POSITION BETWEEN RIBS 33 AND 34 OVERSIZE BUSHING REQUIRED. BUSHING LOCALLY MANUFACTURED AT AAO AND CAD PLATED IAW BAE FAX BARA/AVR/6605/03-DC. BUSHING INSTALLED IAW FLAP EO EO2/021/657. (M)
- [SDR A6WA200360066](https://openairdocs.org/sdr/A6WA200360066.md): Structure · damaged · Nov 6, 2003 · N292UE · Bag BAE146200A · Trailing Edge Flaps
  > OVERSIZED BUSHING REQUIRED IN TWO PLACES ON RIGHT FLAP P/N HC579L1400-001, S/N 838H52-86. REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX FAX 1701-692001. (M)
- [SDR A6WA200360063](https://openairdocs.org/sdr/A6WA200360063.md): Flap Track · damaged · Oct 28, 2003 · N291UE · Bag BAE146200A · Trailing Edge Flaps
  > INSTALL OF FLAP TRACK NR 1 LANDING PLATE FASTENERS. MAINTENANCE REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX FAX 1698-6910005. (M)
- [SDR A6WA200360061](https://openairdocs.org/sdr/A6WA200360061.md): Skin · dented · Oct 28, 2003 · N291UE · Bag BAE146200A · Elevator, Tab Structure
  > FOUND DENTS LEFT AND RIGHT ELEVATOR SERVO AND TRIM TABS, LEFT AND RIGHT TRAILING EDGE PANELS RIB 14A TO 15, LEFT WING INBOARD CENTER, OUTBOARD SPOILERS, RT WING INBOARD, CENTER, SPOILERS. MAINTENANCE REQUESTED REPAIRS FROM BAE SYSTEMS REF AVMAX FAX 1698-69100
- [SDR A6WA200360059](https://openairdocs.org/sdr/A6WA200360059.md): Tab · damaged · Oct 22, 2003 · N291UE · Bag BAE146200A · Trailing Edge Flaps
  > RIGHT OUTBOARD FLAP TAB TRAILING EDGE DAMAGED. MAINTENANCE REQUESTED REPAIR FROM BAE SYSTEMS RED AVMAX FAX 1698-6910001. (M)
- [SDR A6WA200360057](https://openairdocs.org/sdr/A6WA200360057.md): Skin · dented · Oct 20, 2003 · N183US · Bag BAE146200A · Wing, Plate/Skin
  > LEFT AND RIGHT WING DENTED, SPOILERS AND T/E PANEL'S, MAINTENANCE REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX FAX 1693-6830005. (M)
- [SDR A6WA200360058](https://openairdocs.org/sdr/A6WA200360058.md): Wire · loose · Oct 18, 2003 · N610AW · Bag BAE146200A · Equipment/Furnishings Wiring
  > DURING SLIDE DEPLOYMENT FOR FUNCTION TEST LIGHTS CAME ON AND THEN OFF AFTER FULL DEPLOYMENT, INSPECTION FOUND WIRES PULLED OUT OF BATTERY CONNECTORS. MAINTENANCE REMOVED AND REPLACED EVACUATION SLIDE AND DISCREPANCY FORWARDED TO SLIDE SHOP. (M)
- [SDR A6WA200360055](https://openairdocs.org/sdr/A6WA200360055.md): Rivet · damaged · Oct 15, 2003 · N183US · Bag BAE146200A · Landing Gear Doors
  > RT MLG DOOR RIVETS, MAINTENANCE REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX FAX 1693-6830003. (M)
- [SDR A6WA200360053](https://openairdocs.org/sdr/A6WA200360053.md): Pan · damaged · Oct 7, 2003 · N181US · Bag BAE146200A · Fuselage Miscellaneous Structure
  > AFT BAGGAGE DOOR INTERFACE DAMAGE TO THE FORWAD EDGE OF THE AFT BAGGAGE DOOR PAN, LOCATED NEXT TO THE LOWE SHOOT BOLT GUIDE. MAINTENANCE REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX FAX 1683-6810009. (M)
- [SDR A6WA200360046](https://openairdocs.org/sdr/A6WA200360046.md): Skin · dented · Oct 6, 2003 · N181US · Bag BAE146200A · Horizontal Stabilizer, Plate/Skin
  > DENTS ON THE LEFT AND RIGHT HORIZONTAL STAB MAINTENANCE HAS REQUESTED REPAIR FROM BAE SYSTEMS RED AMAX FAX 1683-6810002. (M)
- [SDR A6WA200360045](https://openairdocs.org/sdr/A6WA200360045.md): Skin · delaminated · Oct 6, 2003 · N181US · Bag BAE146200A · Wing, Plate/Skin
  > DENTS ON THE LEFT AND RIGHT WING NOW SHOWING SIGNS OF DELAMINATION. MAINTENANCE HAS REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX FAX 1683-6810001. (M)
- [SDR A6WA200360051](https://openairdocs.org/sdr/A6WA200360051.md): Skin · dented · Oct 4, 2003 · N181US · Bag BAE146200A · Fuselage Main, Plate/Skin
  > FOUND DENTS FORWARD OF CARGO DOOR. MAINTENANCE HAS REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX CAX 1683-6810007. (M)
- [SDR A6WA200360048](https://openairdocs.org/sdr/A6WA200360048.md): Skin · delaminated · Oct 4, 2003 · N181US · Bag BAE146200A · Elevator, Plate/Skin
  > DENTS LEFT AND RIGHT ELEVATORS MAINTENANCE HAS REQUESTED REPAIR FROM BAE SYSTEMS REF AVMAX FAX 1683-6810004. (M)
- [SDR A6WA200360033](https://openairdocs.org/sdr/A6WA200360033.md): Spring · broken · Aug 31, 2003 · N292UE · Bag BAE146200A · Nose/Tail Landing Gear Strut/Axle
  > NLG RIGHT WHEEL BRAKE, SPRING BROKEN. MAINTENANCE REMOVED AND REPLACED BROKENS SPRING GUIDE TUBE, SPRING AND REPAIRED DAMAGE TO THE CEILING OVER NLG BAY. (M)
- [SDR AUS20010916](https://openairdocs.org/sdr/AUS20010916.md): Bearing · failed · Aug 21, 2001 · Bag BAE146200A · Wheel/Ski/Float
  > (AUS) NR 2 MAIN WHEEL INNER BEARING DISINTEGRATED CAUSING THE INNER RACE TO FUSE TO THE AXLE.
- [SDR AUS20010763](https://openairdocs.org/sdr/AUS20010763.md): Engine · leaking · Jul 15, 2001 · Bag BAE146200A · Engine (Turbine/Turboprop)
  > (AUS) NR 3 ENGINE HP COMPRESSOR CONTAMINATED WITH OIL. FUMES IN CABIN.
- [SDR CA010830017](https://openairdocs.org/sdr/CA010830017.md): Wheel · cracked · Jul 13, 2001 · Bag BAE146200A · Wheel/Ski/Float
  > (CAN) THE WHEEL HAD BEEN REMOVED DUE TO THE TIRE BEING WORN TO LIMITS. DURING THE CLEANING PROCESS, TWO CRACKS WERE DISCOVERED VISUALLY. THEY RAN FROM THE LIGHTENING HOLES TO UNDER THE WHEEL BEARING OUTTER RACE. PICTURES ARE AVAILABLE. THE WHEEL HALF HAD BEEN
- [SDR AUS20010793](https://openairdocs.org/sdr/AUS20010793.md): Pump · worn · Jul 10, 2001 · Bag BAE146200A · Hydraulic Pump (Electric/Engine), Main
  > (AUS) ENGINE DRIVEN HYDRAULIC PUMP INTERNAL AND EXTERNAL DRIVE SPLINES WORN EXCESSIVELY.
- [SDR AUS20010727](https://openairdocs.org/sdr/AUS20010727.md): Engine · failed · Jul 10, 2001 · Bag BAE146200A · Engine (Turbine/Turboprop)
  > (AUS) NR 3 ENGINE OIL PRESSURE LOSS.
- [SDR AUS20010691](https://openairdocs.org/sdr/AUS20010691.md): Engine · malfunctioned · Jul 7, 2001 · Bag BAE146200A · Engine (Turbine/Turboprop)
  > (AUS) NR 2 ENGINE HAD NO OIL PRESSURE. LIMITED INFORMATION PROVIDED.
- [SDR CA010703022](https://openairdocs.org/sdr/CA010703022.md): Bearing · making metal · Jun 27, 2001 · Bag BAE146200A · Engine (Turbine/Turboprop)
  > (CAN) DURING ROUTINE INSPECTION NR 4 ENGINE FULL FLOW CHIP DETECTOR WAS FOUND TO HAVE "CONDITION 2" CONTAMINATION. THE ENGINE WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. TEARDOWN REVEALED THAT THE PRE MOD NR 2 BEARING PACK LOCATING PIN HAD SHEARED A
- [SDR CA010723001](https://openairdocs.org/sdr/CA010723001.md): Computer · malfunctioned · Jun 21, 2001 · Bag BAE146200A · Air Intake Anti/De-Ice System
  > (CAN) DURING A MAINTENANCE ENGINE RUN, THE NR 1 ANTI-ICE VALVE CIRCUIT BREAKER POPPED AND WOULD NOT RESET. MAINTENANCE REPLACED THE JUST INSTALLED THRUST MODULATION SYSTEM (TMS) COMPUTER, AND THE PROBLEM WENT AWAY. APPARENTLY, A FAULT IN THE TMS COMPUTER BLEW
- [SDR AUS20010622](https://openairdocs.org/sdr/AUS20010622.md): Skin · cracked · Jun 16, 2001 · Bag BAE146200A · Fuselage Main, Plate/Skin
  > (AUS) FUSELAGE SKIN CRACKED IN AREA LOCATED IMMEDIATELY AFT OF FRAME 29 BENEATH THE WING ROOT DOUBLER. FOUND DURING INSPECTION IAWISB53-144 AND AD/BAE146/70.
- [SDR CA010625001](https://openairdocs.org/sdr/CA010625001.md): Pin · damaged · Jun 13, 2001 · Bag BAE146200A · Main Landing Gear
  > (CAN) LARGE SECTION OF CHROME MISSING FROM DIAMETER "A" PIN (PARENT METAL CORRODED UNDER AREA OF MISSING CHROME) DEFECT FOUND REMOVAL OF PIN WHEN RETRACTION ACTUATOR REPLACEMENT WAS REQUIRED. PIN REPLACED. ADDITIONAL INFORMATION & PICTURES E-MAILED TO STEVE DU
- [SDR AUS20010539](https://openairdocs.org/sdr/AUS20010539.md): Skin · cracked · May 28, 2001 · Bag BAE146200A · Fuselage Main, Plate/Skin
  > (AUS) FUSELAGE SKIN CRACKED IN THE AREA BETWEEN FR 35 AND FR 36 ATSTRINGER LOCATIONS 2L AND 3L. CRACK LENGTH 558.8MM (22IN).
- [SDR AUS20010538](https://openairdocs.org/sdr/AUS20010538.md): Recorder · unserviceable · May 28, 2001 · Bag BAE146200A · Data Recorders (Flight/Maintenance)
  > (AUS) OPERATIONAL CHECK AND CALIBRATION CHECK OF FLIGHT DATA RECORDER (FDR) NOT CARRIED OUT. PERSONNEL/MAINTENANCE ERROR.
- [SDR AUS20010506](https://openairdocs.org/sdr/AUS20010506.md): Fire Loop · worn · May 20, 2001 · Bag BAE146200A · Fire Detection
  > (AUS) NR 1 ENGINE FIRE DETECTOR WIRING LOOM CHAFED.
- [SDR A6WA200100035](https://openairdocs.org/sdr/A6WA200100035.md): Actuator · failed · May 20, 2001 · N156TR · Bag BAE146200A · Compressor Bleed Control
  > NR 4 ENGINE AUTO SHUTDOWN GROUND PERSONNEL NOTICED FLAMES COMING OUT OF TAIL PIPE PILOT FIRED BOTH FIRE BOTTLES. MAINTENANCE REMOVED AND REPLACED BLEED BAND ACTUATOR.
- [SDR CA010621041](https://openairdocs.org/sdr/CA010621041.md): Control Unit · leaking · May 11, 2001 · Bag BAE146200A · Trailing Edge Flap Control System
  > (CAN) INVESTIGATION INTO A HYDRAULIC LEAK RESULTED IN REPLACEMENT OF THE FLAP POWER UNIT WHICH WAS FOUND TO BE LEAKING FROM AN OUTPUT SHAFT CAVITY DRAIN. THIS POWER UNIT WAS AN EXCHANGE UNIT AND HAD BEEN INSTALLED FOR 498 HOURS. 17719
- [SDR CA010522011](https://openairdocs.org/sdr/CA010522011.md): Proximity Sensor · failed · Apr 29, 2001 · Bag BAE146200A · Landing Gear System
  > (CAN) THE FLIGHT CREW REPORTED THE L/H RED "GEAR UNSAFE" LIGHT ILLUMINATED ACCOMPANIED BY GEAR HORN, STICK SHAKER, AND MANUAL SPOILER FAULT WHILE AT THE GATE AFTER SWITCHING FROM GROUND POWER TO APU. MAINTENANCE INVESTIGATION REVEALED AN OPEN CIRCUIT IN THE L/
- [SDR A6WA200100033](https://openairdocs.org/sdr/A6WA200100033.md): Frame · cracked · Apr 26, 2001 · N181US · Bag BAE146200A · Fuselage Main, Frame
  > FUSELAGE FRAME 18 CRACKED. MAINTENANCE REPARED FRAME 18 LT SIDE IAW BAE SYSTEMS FAX REF BARA/AVR/5362/01, BARA/AVR/5360/01, AND RIL HC537H9453.
- [SDR A6WA200100030](https://openairdocs.org/sdr/A6WA200100030.md): Elevator · contaminated · Apr 22, 2001 · N183US · Bag BAE146200A · Elevator Structure
  > PITCH OSCILLATION OCCURRED ON CLIMBOUT. MAINTENANCE DRAINED WATER FROM ELEVATORS.

Next page: https://openairdocs.org/model/british-aerospace-bae-146-series-200a/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 = 'BAE146200A'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/british-aerospace-bae-146-series-200a/reports

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