# Service difficulty reports: N290UE, cancelled Feb 14, 2007

A list on [N290UE, cancelled Feb 14, 2007](https://openairdocs.org/deregistered/N290UE-2007-02-14.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [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 A6WA200460034](https://openairdocs.org/sdr/A6WA200460034.md): Bottle · discharged · Aug 31, 2004 · N290UE · Bac 146200A · Fire Bottle, Fixed
  > NR 1 INTAKE ASSEMBLY INBOARD FIRE BOTTLE EXCEEDS LOW WEIGHT LIMIT. REMOVED AND REPLACED FIRE BOTTLE. (M)
- [SDR A6WA200360032](https://openairdocs.org/sdr/A6WA200360032.md): Smoke · detected · Aug 19, 2003 · N290UE · Bac 146200A · Air Distribution System
  > ON TAXI, CABIN AND COCKPIT FILLED WITH SMOKE. MAINTENANCE PERFORMED DUCT CONTAMINATION CLEARING PROCEDURES PER SUP 96-31. CABIN TEMP CONTROL OPS NORMAL, OK FOR SERVICE. (M)
- [SDR A6WA200360023](https://openairdocs.org/sdr/A6WA200360023.md): Skin · dented · Apr 25, 2003 · N290UE · Bac 146200A · Spoilers
  > DENTS OUT OF LIMITS ON THE RT AIR BRAKE. REPAIR REQUESTED FOR BAE SYSTEM REF AVMAX FAX 1584-6900003.
- [SDR AW6A200360021](https://openairdocs.org/sdr/AW6A200360021.md): Panel · dented · Apr 25, 2003 · N290UE · Bac 146200A · Fuselage Main, Plate/Skin
  > DENTS OUT OF LIMITS ON THE LT WING PANEL BETWEEN RIB 14A AND 15. REPAIR REQUESTED FOR BAE SYSTEM REF.
- [SDR A6WA200360022](https://openairdocs.org/sdr/A6WA200360022.md): Structure · dented · Apr 25, 2003 · N290UE · Bac 146200A · Elevator, Tab Structure
  > DENTS OUT OF LIMITS ON THE RT ELEVATOR AND TABS. REPAIR REQUESTED FOR BAE SYSTEM REF AVMAX FAX 1584.
- [SDR A6WA200360012](https://openairdocs.org/sdr/A6WA200360012.md): Longeron · corroded · Apr 21, 2003 · N290UE · Bac 146200A · Fuselage Main, Longeron/Stringer
  > FORWARD CARGO DOOR CUTOUT LOWER LONGEORN CORROSION DAMAGE COMPLETELY THROUGH THE FACE LONGERON. REPAIR REQUESTED FOR BEE SYSTEM REF AVMAX-FAX 1584-60000. (M)
- [SDR A6WA200360010](https://openairdocs.org/sdr/A6WA200360010.md): Frame · cracked · Apr 9, 2003 · N290UE · Bac 146200A · Fuselage Main, Frame
  > FRAME 32 MLG WHEEL WELL RIGHT AFT BULKHEAD CRACKED IN TWO PLACES IN LOWER FALSE DIAPHRAGM FOR FAIRING ATTACHMENT. PATCH TWO ABOVE AREAS PER SRM 51-71-11. DOUBLE ROW RIVETS 2024 T3.050 ALUM. (M)
- [SDR A6WA200100058](https://openairdocs.org/sdr/A6WA200100058.md): Fcu · malfunctioned · Oct 7, 2001 · N290UE · Bac 146200A · Fuel Control/Turbine Engines
  > DURING CLIMB NR 3 ENGINE DID NOT RESPOND TO THRUST LEVER POWER CHANGES THEN NR 3 ENGINE TGT STARTED CLIMBING TO 870 DEGRESS PERFORMED SHUTDOWN. MAINTENANCE REMOVED AND REPLACED FUEL CONTROL UNIT.
- [SDR A6WA200100024](https://openairdocs.org/sdr/A6WA200100024.md): Cable · detached · Mar 27, 2001 · N290UE · Bag BAE146200A · Escape Slide
  > FWD PAX SLIDE DEPLOY CABLE NOT ATTACHED TO GIRT BAR. MAINTENANCE REMOVED AND REPLACED EVACUATION SLIDE ASSEMBLY.
- [SDR A6WA200100015](https://openairdocs.org/sdr/A6WA200100015.md): Unknown · odor · Feb 10, 2001 · N290UE · Bag BAE146200A · Air Distribution System
  > FLIGHT ATTENDANT REPORTED LIGHT SMOKE ODOR COMING FROM SEAT 18 D&F AREA INFLIGHT. MAINTENANCE INSPECTED SEAT AREA, NO ODOR NOTED. NO ODOR NOTED FROM AIR CONDITIONING PACKS AS WELL.
- [SDR A6WA0000020](https://openairdocs.org/sdr/A6WA0000020.md): Battery · discharged · Mar 2, 2000 · N290UE · Bag BAE146200A · Escape Slide
  > NR 2 EVAC SLIDE LIGHTING BATTERY FAILS VOLTAGE CHECK. REMOVED AND REPLACED NR 2 SLIDE ASSY. (M)
- [SDR A6WA0000019](https://openairdocs.org/sdr/A6WA0000019.md): Valve · out of adj · Feb 25, 2000 · N290UE · Bag BAE146200A · Fuel Control/Turbine Engines
  > NR 2 ENGINE PRODUCED 89.0 PERCENT N1 ON FULL POWER APPLICATION AT ASE N1 REF CALLED FOR 93.4 PERCENT ENGINE ANTI-ICE ON 904 TGT. REMOVED AND REPLACED NR 2 ENGINE FCU POPPET VALVE C/W BLEED BAND ADJUSTMENT AND TAKEOFF POWER CHECK. (M)
- [SDR A6WA9900032](https://openairdocs.org/sdr/A6WA9900032.md): Rib · cracked · Feb 15, 1999 · N290UE · Bag BAE146200A · Cargo/Baggage Doors
  > AFT CARGO DOOR UPPER MOST RIB IS CRACKING LOCATED UNDER UPPER AFT HINGE 'L' BRACKET ON UPPER MOST RIB IAW BAE REPAIR DRAWING REF HC523H9001 AND FOUND SERVICEABLE. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X)
- [SDR A6WA9900031](https://openairdocs.org/sdr/A6WA9900031.md): Bracket · cracked · Jan 29, 1999 · N290UE · Bag BAE146200A · Wing Miscellaneous Structure
  > LEFT WING TE SHROUD LOWER SKIN STIFFENER AFT (TAG) ANGLE BRACKET CRACKED BETWEEN RIB 8 AND RIB 9. REPLACED BRACKET. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X)
- [SDR A6WA9900030](https://openairdocs.org/sdr/A6WA9900030.md): Stiffener · broken · Jan 29, 1999 · N290UE · Bag BAE146200A · Wing, Plate/Skin
  > LEFT WING TE TOP SHROUD SKIN STIFFENER TO FALSE SPAR (AFT END) BROKEN BETWEEN RIBS 7 AND 8. REPLACED STIFFENER. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X)
- [SDR A6WA9900029](https://openairdocs.org/sdr/A6WA9900029.md): Bracket · cracked · Jan 27, 1999 · N290UE · Bag BAE146200A · Wing Miscellaneous Structure
  > LEFT WING TE SHROUD UPPER SKIN STIFFENER TO FALSE SPARE ANGLE BRACKET CRACKED BETWEEN RIBS 7 AND 8. REPLACED BRACKET. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X)
- [SDR A6WA9900028](https://openairdocs.org/sdr/A6WA9900028.md): Angle · corroded · Jan 20, 1999 · N290UE · Bag BAE146200A · Fuselage Miscellaneous Structure
  > RIGHT WEB CLOSING ANGLE AFT OF FRAME 50 HAS ONE INCH CRACK. REPAIRED IAW BAE SRM 51-71-11 FIG 2. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X)
- [SDR A6WA9900033](https://openairdocs.org/sdr/A6WA9900033.md): Stiffener · cracked · Jan 16, 1999 · N290UE · Bag BAE146200A · Wing Miscellaneous Structure
  > RIGHT WING STIFFENER BETWEEN RIBS 7 AND 8 CRACKED AT FORWARD END. REPLACED STIFFENER. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X)
- [SDR A6WA9900027](https://openairdocs.org/sdr/A6WA9900027.md): Stiffener · cracked · Jan 16, 1999 · N290UE · Bag BAE146200A · Wing Miscellaneous Structure
  > LEFT WING STIFFENER BETWEEN RIBS 7 AND 8 CRACKED AT FORWARD ENGINE. REPLACED STIFFENER. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X)
- [SDR A6WA9900038](https://openairdocs.org/sdr/A6WA9900038.md): Structure · cracked · Jan 14, 1999 · N290UE · Bag BAE146200A · Fuselage Main, Structure
  > FUSELAGE STRUCTURE AFT OF FRAME 50 ABOVE LT UPPER AIRBRAKE HINGE CORNER IS CRACKED. REPAIRED PER BAE FAX JM/RJ0491-96. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X)
- [SDR A6WA9900037](https://openairdocs.org/sdr/A6WA9900037.md): Structure · cracked · Jan 14, 1999 · N290UE · Bag BAE146200A · Fuselage Main, Structure
  > FUSELAGE STRUCTURE AFT OF FRAME 50 ABOVE RIGHT UPPER AIRBRAKE HINGE CORNER IS CRACKED. REPAIRED PER FAX JM/RJ049-96. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X)
- [SDR A6WA9900036](https://openairdocs.org/sdr/A6WA9900036.md): Rivet · sheared · Jan 14, 1999 · N290UE · Bag BAE146200A · Fuselage Miscellaneous Structure
  > FUSELAGE STRUCTURE AFT OF FRAME 50 ABOVE RT UPPER AIRBRAKE HINGE HAS RIVETS SHEARED OFF FOR CORNER ANGLE BRACKET. REPLACED RIVETS. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X)
- [SDR A6WA9900035](https://openairdocs.org/sdr/A6WA9900035.md): Rivet · sheared · Jan 14, 1999 · N290UE · Bag BAE146200A · Fuselage Miscellaneous Structure
  > FUSELAGE STRUCTURE AFT OF FRAME 50 ABOVE LT AIRBRAKE HINGE HAS RIVETS SHEARED OFF FOR CORNER ANGLE BRACKET. REPLACED RIVETS. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X)
- [SDR A6WA9900034](https://openairdocs.org/sdr/A6WA9900034.md): Gusset · cracked · Jan 14, 1999 · N290UE · Bag BAE146200A · Fuselage Miscellaneous Structure
  > FUSELAGE STRUCTURE AFT OF FRAME 50 ABOVE LT UPPER AIRBRAKE HINGE HAS A FILLER PANEL CRACKED AT THE LIGHTNING HOLE. REPLACED GUSSET PLATE. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X)
- [SDR A6WA9900022](https://openairdocs.org/sdr/A6WA9900022.md): Angle · cracked · Jan 10, 1999 · N290UE · Bag BAE146200A · Passenger/Crew Doors
  > FORWARD PASSENGER DOOR HAS 2 EACH CRACKED ANGLES IN THE HANDLE BOX AREA. MFG AND REPLACED PER BAE DRAWINGS HC521H0507 AND HC521H0508. INSTALLED ANGLES PER SRM AND BAE FAX DJR/RJ0049-97. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X)
- [SDR A6WA9900026](https://openairdocs.org/sdr/A6WA9900026.md): Gusset · corroded · Jan 9, 1999 · N290UE · Bag BAE146200A · Fuselage Miscellaneous Structure
  > SEVERAL GUSSET PLATES ON FLOOR ARE CORRODED (SURFACE CORROSION) AFT VESTIBULE. REPLACED CORRODED GUSSET PLATES, 2 EACH. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X)
- [SDR A6WA9900025](https://openairdocs.org/sdr/A6WA9900025.md): Seat · cracked · Jan 9, 1999 · N290UE · Bag BAE146200A · Passenger Compartment Equipment
  > FORWARD F/A SEAT PAN CRACKED. REPLACED PAN. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X)
- [SDR A6WA9900024](https://openairdocs.org/sdr/A6WA9900024.md): Longeron · cracked · Jan 6, 1999 · N290UE · Bag BAE146200A · Fuselage Main, Longeron/Stringer
  > FRAME 29 MLG BAY ROOF LONGERONS CRACKED, NR 3 AND NR 15, NEAR FORWARD ENG. REPAIRED PER BAE REPAIR DRAWING HC536H9211. ACFT TT: 19,327 HOURS. ACFT TC: 22,789. (X)
- [SDR A6WA9900023](https://openairdocs.org/sdr/A6WA9900023.md): Bolt · broken · Jan 6, 1999 · N290UE · Bag BAE146200A · Wing Miscellaneous Structure
  > FRAME 29 LEFT AND RIGHT BOTTOM BOLT OF WING ATTACHMENT BRACKET HEAD APPEARS TO BE BROKEN. REMOVED BOLT, CLEANED AND INSPECTED HOLE, PREP, ALODINE, PRIMED AND INSTALLED NEW BOLT AND NUT IAW FAX DJR/RJ0022/96 AND DJR/RJ0721-96. WITCO BOND WILL BE APPLIED ON WO
- [SDR 99ZZZM601](https://openairdocs.org/sdr/99ZZZM601.md): Structure · cracked · Sep 13, 1998 · N290UE · Bag BAE146200A · Nose/Tail Landing Gear Strut/Axle
  > DURING SCHEDULED NDT INSPECTION OF NGL RETRACTION JACK MOUNT STRUCTURE, FOUND CRAKS IN JACK PIN STRUCTURE BORE. (M)
- [SDR 98ZZZX3983](https://openairdocs.org/sdr/98ZZZX3983.md): Switch · contaminated · Apr 29, 1998 · N290UE · Bag BAE146200A · Landing Gear Position and Warning
  > MYR - FLT 690 - UPON GEAR RETRACTION, LANDING GEAR DID NOT RETRACT. CLEANED SQUAT SWITCHES.
- [SDR 98ZZZX3984](https://openairdocs.org/sdr/98ZZZX3984.md): Rod · broken · Mar 20, 1998 · N290UE · Bag BAE146200A · Passenger/Crew Doors
  > ATW - FORWARD PASSENGER DOOR DROPS BELOW DOOR FRAME WHEN OPENED AND DOES NOT DROP AND LATCH PROPERLY WHEN CLOSED. REPLACED BROKEN LOWER ROD END ON THE CONTROL SHAFT ASSY TO TORQUE SHAFT CONTROL ROD. REPLACED LOWER HINGE COVER. NOTE: REMOVED AND REPLACED EV

## 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 n_number = 'N290UE' AND deregistration_id = 'N290UE-2007-02-14'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N290UE-2007-02-14/reports

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