# Service difficulty reports: N49543, cancelled Jul 8, 2014

A list on [N49543, cancelled Jul 8, 2014](https://openairdocs.org/deregistered/N49543-2014-07-08.md).

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

Page 1 of 2 · 72 reports

- [SDR 29GA94357052812A](https://openairdocs.org/sdr/29GA94357052812A.md): Skin · corroded · May 28, 2012 · N49543 · Beech 1900D · Wing, Plate/Skin
  > DURING SCHEDULED ROUTINE INSPECTION DISCOVERED LEFT WING ON TOP TRAILING EDGE SURFACE CORROSION. REMOVED DAMAGED AREA AND INSTALLED DOUBLER REPAIR.
- [SDR 29GA94332033112A](https://openairdocs.org/sdr/29GA94332033112A.md): Wire · shorted · Mar 31, 2012 · N49543 · Beech 1900D · Landing Gear System Wiring
  > FLIGHT 4026, LANDING GEAR HAS TO BE MANUALLY PUMPED, THREE GREEN AFTER MANUAL EXTENSION. RECONNECTED HYDRAULIC POWER PACK SELECT VALVE WIRING AT LEFT STUB WING INBOARD OF FUSELAGE, LANDING GEAR EXTENSION AND RETRACTION. OPS CHECKED GOOD.
- [SDR 29GA20120331943](https://openairdocs.org/sdr/29GA20120331943.md): Wire · shorted · Mar 31, 2012 · N49543 · Beech 1900D · Landing Gear System Wiring
  > FLIGHT4026, LANDING GEAR HAS TO BE MANUALLY PUMPED, THREE GREEN AFTER MANUAL EXTENSION. RECONNECTED HYDRAULIC POWER PACK SELECT VALVE WIRING AT LEFT STUB WING INBOARD OF FUSELAGE, LANDING GEAR EXTENSION AND RETRACTION, OPS CHECKED GOOD.
- [SDR 29GA94352012412B](https://openairdocs.org/sdr/29GA94352012412B.md): Handle · lack of lube · Jan 24, 2012 · N49543 · Beech 1900D · Emergency Exits
  > DURING SCHEDULED ROUTINE C-3 INSPECTION DISCOVERED RIGHT FORWARD EMERGENCY EXIT OUTER HANDLE WILL NOT SPRING OPEN. LUBRICATED RIGHT FORWARD EMERGENCY EXIT DOOR OUTER HANDLE.
- [SDR 29GA94352012412A](https://openairdocs.org/sdr/29GA94352012412A.md): Handle · lack of lube · Jan 24, 2012 · N49543 · Beech 1900D · Emergency Exits
  > DURING SCHEDULED ROUTINE C-3 INSPECTION DISCOVERED RIGHT AFT EMERGENCY EXIT INNER HANDLE STIFF. LUBRICATED RIGHT AFT EMERGENCY EXIT HANDLE.
- [SDR 29GA94353102211A](https://openairdocs.org/sdr/29GA94353102211A.md): Skin · corroded · Oct 22, 2011 · N49543 · Beech 1900D · Fuselage Main, Plate/Skin
  > REPORT: DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED BELLY SKIN CORROSION AFT OF LOWER BEACON AT FS 378.25. REMOVED CORROSION AND INSTALLED FILLER AND DOUBLER REPAIR.
- [SDR 29GA94355101211B](https://openairdocs.org/sdr/29GA94355101211B.md): Torque Tube · corroded · Oct 12, 2011 · N49543 · Beech 1900D · Elevator Control System
  > DURING SCHEDULED ROUTINE INSPECTION DISCOVERED RIGHT ELEVATOR TORQUE TUBE CORROSION. REPLACED RIGHT ELEVATOR TORQUE TUBE.
- [SDR 29GA94355101211A](https://openairdocs.org/sdr/29GA94355101211A.md): Torque Tube · corroded · Oct 12, 2011 · N49543 · Beech 1900D · Elevator Control System
  > DURING SCHEDULED ROUTINE INSPECTION DISCOVERED LEFT ELEVATOR TORQUE TUBE CORROSION. REPLACED LEFT ELEVATOR TORQUE TUBE.
- [SDR 29GA94353091611A](https://openairdocs.org/sdr/29GA94353091611A.md): Door Frame · cracked · Sep 16, 2011 · N49543 · Beech 1900D · Fuselage Main, Structure
  > DURING SCHEDULED ROUTINE INSPECTION DISCOVERED AVIONICS DOOR FUSELAGE FRAME RIGHT CHANNEL HAS.6 INCH CRACK AT AFT LOWER CORNER RADIUS. CUT OUT CRACK AND INSTALLED REPAIR STRAP.
- [SDR 29GA94361071611A](https://openairdocs.org/sdr/29GA94361071611A.md): Switch · out of adjust · Jul 16, 2011 · N49543 · Beech 1900D · Propeller Feathering/Reversing
  > FLIGHT 9205 TCB/FLL DURING DESCENT AND APPROACH TO LANDING WITH AUTOFEATHER ARMED THE AFX DISABLE ANNUNCIATOR ILLUMINATES WITH VERY MOVEMENT OF THE POWER LEVER. RE-ADJUSTED AUTOFEATHER ARMING SWITCH OPERATIONAL CHECK SATISFACTORY.
- [SDR GUUA94353011911A](https://openairdocs.org/sdr/GUUA94353011911A.md): Stringer · debonded · Jan 19, 2011 · N49543 · Beech 1900D · Fuselage Main, Longeron/Stringer
  > DURING SCHEDULED ROUTINE INSP DISCOVERED BONDED STRINGER DEBONDED FROM FUSELAGE SKIN FROM FS 363 TO FS 423. OPEN
- [SDR GUUA94353011811A](https://openairdocs.org/sdr/GUUA94353011811A.md): Bulkhead · cracked · Jan 18, 2011 · N49543 · Beech 1900D · Fuselage Main, Bulkhead
  > DURING SCHEDULED ROUTINE INSP DISCOVERED CRACK BETWEEN FS 456 TO 468.25 BETWEEN STRINGERS 11R AND 12R ON CARGO FLOOR BULKHEAD. 288. REPAIRED CRACK, INSTALLED DOUBLER 2.1 INCHES X 8.3 INCHES BETWEEN FS 456.00 TO 468.25.
- [SDR GUUA94353011711A](https://openairdocs.org/sdr/GUUA94353011711A.md): Angle · cracked · Jan 17, 2011 · N49543 · Beech 1900D · Fuselage Miscellaneous Structure
  > DURING SCHEDULED ROUTINE INSP DISCOVERED LT WING FUSELAGE CLOSING ANGLE CRACKED APPROX 1.75 INCHES AT FS 288. REPAIRED LT WING FUSELAGE CLOSING ANGLE.
- [SDR GUUA94352010611A](https://openairdocs.org/sdr/GUUA94352010611A.md): Handle · stiff · Jan 6, 2011 · N49543 · Beech 1900D · Emergency Exits
  > DURING SCHEDULED ROUTINE INSP, DISCOVERED RT AFT EMERGENCY EXIT DOOR INNER HANDLE STIFF TO OPERATE. LUBRICATED RT EMERGENCY EXIT DOOR INNER HANDLE. OPS CHECK NORMAL.
- [SDR GUUA94371010111A](https://openairdocs.org/sdr/GUUA94371010111A.md): Isolator · cracked · Jan 1, 2011 · N49543 · Beech 1900D · Engine Mount Section
  > DURING MAGNETIC PARTICLE INSP DISCOVERED ISOLATOR MOUNT WELD AREA CRACKS. PERFORMED WELD REPAIR TO ENGINE TRUSS TUBE WELD AREAS.
- [SDR GUUA94352091310A](https://openairdocs.org/sdr/GUUA94352091310A.md): Handle · binding · Sep 13, 2010 · N49543 · Beech 1900D · Emergency Exits
  > DURING SCHEDULED ROUTINE INSP DISCOVERED RT AFT EMERGENCY EXIT DOOR HARD TO OPEN. LUBRICATED RT AFT EMERGENCY EXIT DOOR HANDLE. OPS CHECK OK.
- [SDR GUUA94353061610A](https://openairdocs.org/sdr/GUUA94353061610A.md): Skin · corroded · Jun 16, 2010 · N49543 · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING SCHEDULED ROUTINE MX, DISCOVERED FUSEALGE BELLY SKIN EXFOLIATION AT FS 423.25 STRINGER 16. REMOVED DAMAGED SKIN AND INSTALLED EXTERNAL DOUBLER REPAIR.
- [SDR GUUA94352061210A](https://openairdocs.org/sdr/GUUA94352061210A.md): Cable · frayed · Jun 12, 2010 · N49543 · Beech 1900D · Entrance Stairs
  > DURING SCHEDULED ROUTINE MX DISCOVERED AIRSTAIR DOOR LOWER AFT CABLE FRAYED AND LOWER BELLCRANK LOOSE. REPLACED AIRSTAIR DOOR LOWER AFT CABLE AND ADJUSTED LOWER BELLCRANK SCREWS.
- [SDR GUUA94327041610A](https://openairdocs.org/sdr/GUUA94327041610A.md): Trimmer · binding · Apr 16, 2010 · N49543 · Beech 1900D · Elevator Tab Control System
  > DURING FLIGHT ELEVATOR TRIM WHEEL BINDS UP UNABLE TO SEE TRIM TABS ON WHEEL FOR ALL STAGES OF FLIGHT. REPLACED ELEVATOR TRIM TAB INDICATOR OPS CHECK OK. TEST FLIGHT SATISFACTORY.
- [SDR GUUA94627041610A](https://openairdocs.org/sdr/GUUA94627041610A.md): Trimmer · binding · Apr 16, 2010 · N49543 · Beech 1900D · Elevator Tab Control System
  > DURING FLIGHT, ELEVATOR TRIM WHEEL BINDS UP UNABLE TO SEE TRIM TABS ON WHEEL FOR ALL STAGES OF FLIGHT. REPLACED ELEVATOR TRIM TAB INDICATOR OPS CHECK OK. TEST FLIGHT SATISFACTORY.
- [SDR GUUA94332041110A](https://openairdocs.org/sdr/GUUA94332041110A.md): Uplock Switch · out of adjust · Apr 11, 2010 · N49543 · Beech 1900D · Landing Gear Position and Warning
  > DURING FLIGHT LANDING GEAR CONTROL HANDLE RED LIGHTS FLICKER ON AND OFF WHEN IN TURBULENT FLIGHT CONDITIONS. C/A: ADJUSTED RT MLG UP POSITION INDICATOR SWITCH. LANDING GEAR OPS CHECK GOOD.
- [SDR GUUA94353011910A](https://openairdocs.org/sdr/GUUA94353011910A.md): Frame · cracked · Jan 19, 2010 · N49543 · Beech 1900D · Fuselage Main, Frame
  > DURING SCHEDULED ROUTINE MX DISCOVERED AIRSTAIR DOOR FUSELAGE FRAME ANGLE CRACKED AT FS 150.60 AT GAS STRUT LOWER ATTACH POINT. REMOVED DAMAGED SECTION OF ANGLE AND INSTALLED FRAME ANGLE REPAIR.
- [SDR GUUA94357112409A](https://openairdocs.org/sdr/GUUA94357112409A.md): Spar · corroded · Nov 24, 2009 · N49543 · Beech 1900D · Wing Spar
  > DURING SCHEDULED X-RAY INSP, DISCOVERED RT WING LWR AFT SPAR ON COLLECTOR TANK HAS SMALL SPOT OF SURFACE CORROSION BETWEEN WS 114.25 TO 124.25. BLENDED OUT CORROSION AND INSTALLED REPAIR STRAP. NOTE: PREVIOUSLY SUBMITTED, OPEN.
- [SDR GUUA9432071909B](https://openairdocs.org/sdr/GUUA9432071909B.md): Torque Tube · corroded · Jul 19, 2009 · N49543 · Beech 1900D · Elevator Structure
  > DURING SCHEDULED ROUTINE INSP DISCOVERED RT ELEVATOR TORQUE TUBE SHOW SIGNS OF EXFOLIATION. REPLACED RT ELEVATOR TORQUE TUBE.
- [SDR GUUA94327071909A](https://openairdocs.org/sdr/GUUA94327071909A.md): Torque Tube · corroded · Jul 19, 2009 · N49543 · Beech 1900D · Elevator Structure
  > DURING SCHEDULED ROUTINE INSP DISCOVERED LT ELEVATOR TORQUE TUBE SHOW SIGNS OF EXFOLIATION. REPLACED LT ELEVATOR TORQUE TUBE ASSY.
- [SDR GUUA94327071709A](https://openairdocs.org/sdr/GUUA94327071709A.md): Horn · corroded · Jul 17, 2009 · N49543 · Beech 1900D · Elevator, Tab Structure
  > DURING SCHEDULED ROUTINE INSP, DISCOVERED RT ELEVATOR INBD TRIM TAB HORN EXFOLIATED. REPLACED RT ELEVATOR TRIM TAB.
- [SDR GUUA94355071709C](https://openairdocs.org/sdr/GUUA94355071709C.md): Hinge Bracket · corroded · Jul 17, 2009 · N49543 · Beech 1900D · Horizontal Stabilizer, Attach Fittings
  > DURING ROUTINE INSP DISCOVERED RT ELEVATOR CTR HINGE BRACKET EXFOLIATED. REPLACED RT ELEVATOR CTR HINGE BRACKET.
- [SDR GUUA94355071709B](https://openairdocs.org/sdr/GUUA94355071709B.md): Hinge Bracket · corroded · Jul 17, 2009 · N49543 · Beech 1900D · Horizontal Stabilizer, Attach Fittings
  > DURING SCHEDULED ROUTINE INSP DISCOVERED LT ELEVATOR OTBD HINGE BRACKET EXFOLIATED. REPLACED LT ELEVATOR OTBD HINGE BRACKET.
- [SDR GUUA94355071709A](https://openairdocs.org/sdr/GUUA94355071709A.md): Hinge Bracket · corroded · Jul 17, 2009 · N49543 · Beech 1900D · Horizontal Stabilizer, Attach Fittings
  > DURING SCHEDULED ROUTINE INSP DISCOVERED LT ELEVATOR CTR HINGE BRACKET EXFOLIATED. REPLACED LT ELEVATOR CTR HINGE BRACKET.
- [SDR GUUA94355021009C](https://openairdocs.org/sdr/GUUA94355021009C.md): Hinge Bracket · corroded · Feb 10, 2009 · N49543 · Beech 1900D · Wing, Control Surface Attach Fittings
  > DURING SCHEDULED ROUTINE MX DISCOVERED RT ELEVATOR OTBD HINGE BRACKET HAS EXFOLIATION. REPLACED RT ELEVATOR OTBD HINGE BRACKET.
- [SDR GUUA94355021009B](https://openairdocs.org/sdr/GUUA94355021009B.md): Hinge Bracket · corroded · Feb 10, 2009 · N49543 · Beech 1900D · Rudder/Tab, Attach Fittings
  > DURING SCHEDULED ROUTINE MX DISCOVERED RUDDER UPPER HINGE BRACKET HAS EXFOLIATION. REPLACED RUDDER UPPER HINGE BRACKET
- [SDR GUUA94355021009A](https://openairdocs.org/sdr/GUUA94355021009A.md): Hinge Bracket · corroded · Feb 10, 2009 · N49543 · Beech 1900D · Rudder/Tab, Attach Fittings
  > DURING SCHEDULED ROUTINE MX DISCOVERED LOWER RUDDER HINGE BRACKET HAS EXFOLIATION. REPLACED LOWER RUDDER HINGE BRACKET.
- [SDR GUUA94352011209A](https://openairdocs.org/sdr/GUUA94352011209A.md): Door · stuck · Jan 12, 2009 · N49543 · Beech 1900D · Emergency Exits
  > DURING SCHEDULED ROUTINE MAINT, DISCOVERED LT EMERGENCY EXIT DOOR DIFFICULT TO OPEN. LUBRICATED LT EMERGENCY EXIT DOOR. OPS CHECK GOOD.
- [SDR GUUA11100801](https://openairdocs.org/sdr/GUUA11100801.md): Skin · corroded · Nov 10, 2008 · N49543 · Beech 1900D · Fuselage Main, Plate/Skin
  > AT SCHEDULED INSPECTION DISCOVERED EXFOLIATION AT LOWER FUSELAGE SKIN AT FS 250.750 STRINGER 15L. REMOVED DAMAGED SKIN AND INSTALLED REPAIR DOUBLER PER BEECH STRUCTURAL REPAIR MANUAL 51-70-06.
- [SDR GUU2008F00056](https://openairdocs.org/sdr/GUU2008F00056.md): Cable Assy · broken · Oct 4, 2008 · N49543 · Beech 1900D · Passenger/Crew Doors
  > FLIGHT 9146 - TPA/MIA - PILOT REPORTED FORWARD DOOR CAMLOCKS STUCK. DOOR WOULD NOT OPEN FROM INSIDE OR OUTSIDE. REPLACED FORWARD AIRSTAIR DOOR UPPER FORWARD CABLE ASSEMBLY.
- [SDR GUUA94357061208A](https://openairdocs.org/sdr/GUUA94357061208A.md): Skin · corroded · Jun 12, 2008 · N49543 · Beech 1900D · Wing, Plate/Skin
  > DURING SCHEDULED ROUTINE MX DISCOVERED RT OTBD WING, UPPER SKIN, T/E HAD CORROSION AND DEBOND BETWEEN WS 121 THROUGH 194.85. REMOVED DAMAGED SKIN FABRICATED AND INSTALLED AND EXTERNAL REPAIR DOUBLER
- [SDR GUUA04100801](https://openairdocs.org/sdr/GUUA04100801.md): Wire · loose · Apr 10, 2008 · N49543 · Beech 1900D · Fire Protection System Wiring
  > FLIGHT:9263, DURING FLIGHT, RT DISCHARGE LIGHT ILLUMINATED INTERMITTENTLY. RESECURED WIRE AT RT FIRE BOTTLE.
- [SDR GUUA09240702](https://openairdocs.org/sdr/GUUA09240702.md): Skin · cracked · Sep 24, 2007 · N49543 · Beech 1900D · Fuselage Main, Plate/Skin
  > AT SCHEDULED INSPECTION DISCOVERED AIRCRAFT BELLY RT SIDE HAS A FUSELAGE CRACK AT FS 288.0. STOP DRILLED CRACK AND INSTALLED EXTERNAL REINFORCEMENT DOUBLER IAW STRUCTURAL REPAIR MANUAL 53-90-18.
- [SDR GUUA05080702](https://openairdocs.org/sdr/GUUA05080702.md): Handle · out of alignment · May 8, 2007 · N49543 · Beech 1900D · Emergency Exits
  > AT SCHEDULED FLEET CAMPAIGN INSPECTION: SEAT 6F HATCH COVER NEEDS ADJUSTMENT CATCHING ON SIDEWALL. ADJUSTED SEAT 6F EMERGENCY HATCH COVER.
- [SDR GUUA12150603](https://openairdocs.org/sdr/GUUA12150603.md): Skin · ground damage · Dec 15, 2006 · N49543 · Beech 1900D · Fuselage Main, Structure
  > FLIGHT: 9214, DURING GROUND HANDLING BAGGAGE CART DAMAGE BELOW CARGO DOOR LOCATED AT F.S 482.75 TO F.S 500. CUT OUT DAMAGE SECTION OF SKIN 17.0 IN X 7.0 IN FABRICATED AND INSTALLED EXTERNAL REPAIR DOUBLER 20.0 IN X 10.0 IN IAW STRUCTURAL REPAIR MANUAL 51-70-
- [SDR GUUA07220601](https://openairdocs.org/sdr/GUUA07220601.md): Smoke · detected · Jul 22, 2006 · N49543 · Beech 1900D · Air Distribution System
  > MCO/MIA DURING FLIGHT SMELL OF SMOKE, NO SMOKE WAS VISUALLY OBSERVED AND ODOR WAS DISSIPATING. CONTINUED TO MIA LANDED WITHOUT INCIDENT. INSPECTED BOTH VENT BLOWERS UNDER CABIN FLOOR, NO DEFECTS NOTED. COULD NOT DUPLICATE SMELL OF SMOKE.
- [SDR GUUA02170601](https://openairdocs.org/sdr/GUUA02170601.md): Warning Light · false activation · Feb 17, 2006 · N49543 · Beech 1900D · Smoke Detection
  > DURING FLIGHT RIGHT FIRE DISCHARGE ANNUNCIATOR ILLUMINATED INTERMITTENTLY. INSPECTED THE RIGHT FIRE PROTECTION SYSTEM, NO DEFECTS NOTED.
- [SDR GUUA02160602](https://openairdocs.org/sdr/GUUA02160602.md): Warning Light · false activation · Feb 16, 2006 · N49543 · Beech 1900D · Detection System
  > DURING FLIGHT RIGHT FIRE EXTINGUISHER DISCHARGE LIGHT ILLUMINATES INTERMITTENTLY. CLEANED CONTACTS AT THE RIGHT FIRE EXTINGUISHER.
- [SDR GUUA02060603](https://openairdocs.org/sdr/GUUA02060603.md): Wire · out of position · Feb 6, 2006 · N49543 · Beech 1900D · Fire Protection System Wiring
  > DURING FLIGHT RIGHT ENGINE FIRE EXTINGUISHER DISCHARGE LIGHT ILLUMINATED INTERMITTENTLY. REPOSITION WIRES AT THE RIGHT FIRE EXTINGUISHER ANNUNCIATOR.
- [SDR GUUA02060602](https://openairdocs.org/sdr/GUUA02060602.md): Wire Harness · loose · Feb 6, 2006 · N49543 · Beech 1900D · Fire Protection System Wiring
  > DURING FLIGHT RIGHT ENGINE DISCHARGE LIGHT ILLUMINATED ON AND OFF. SECURED WIRE BUNDLE AT THE RIGHT WHEEL WELL FIRE EXTINGUISHER BOTTLE.
- [SDR GUU2006F00007](https://openairdocs.org/sdr/GUU2006F00007.md): Connector · loose · Dec 28, 2005 · N49543 · Beech 1900D · Fire Protection System Wiring
  > DURING FLIGHT, RT FIRE EXTINGUISHER DISCHARGE ANNUNCIATOR ILLUMINATED INTERMITTENTLY. RESECURED WIRE CONNECTORS AT RT FIRE EXTINGUISHER ANNUNCIATOR SWITCH. (K)
- [SDR GUU2005F00058](https://openairdocs.org/sdr/GUU2005F00058.md): O-Ring · worn · Oct 11, 2005 · N49543 · Beech 1900D · Landing Gear Brake System
  > NO BRAKES AFTER PRESSING THE RT BRAKE PEDAL. REPLACED NR 3 AND 4 BRAKE ASSEMBLIES. UPON BRAKE REMOVAL, DETERMINED NR 3 BRAKE SWIVEL FITTING O-RING TO BE LEAKING. (K)
- [SDR GUU2005F00017](https://openairdocs.org/sdr/GUU2005F00017.md): Blade · failed · Aug 27, 2004 · N49543 · Beech 1900D · Turbine Section
  > DURING APPROACH, ON SHORT FINAL TO RUNWAY 9 LEFT AT 500 FEET, THE NR2 ENGINE FAILED. LANDED WITHOUT FURTHER INCIDENT. PILOT SHUTDOWN ENGINE ON TAXI IN. REMOVED AND REPLACED NR2 ENGINE ASSY (GG AND PS). OPERATIONAL CHECK NORMAL. NOTE: VERIFIED TO BE 2ND S
- [SDR GUU2004F00028](https://openairdocs.org/sdr/GUU2004F00028.md): Engine · failed · Aug 27, 2004 · N49543 · Beech 1900D · Engine (Turbine/Turboprop)
  > DURING APPROACH, ON SHORT FINAL TO RUNWAY 9 LT AT 500 FT, THE NR 2 ENGINE FAILED. LANDED WITHOUT FURTHER INCIDENT. PILOT SHUT DOWN ENGINE ON TAXI IN. REMOVED AND REPLACED NR 2 ENGINE ASSEMBLY (GG AND PS). OPERATIONAL CHECK NORMAL. NOTE: SUSPECT NR 2 PT BL
- [SDR 2004F00406](https://openairdocs.org/sdr/2004F00406.md): Engine · failed · Aug 27, 2004 · N49543 · Beech 1900D · Engine (Turbine/Turboprop)
  > FLT 9187 - MHH/FLL - DUIRNG APPROACH, ON SHORT FINAL TO RUNWAY 9 LEFT AT 500 FEET, THE NR 2 ENGINE FAILED. LANDED WITHOUT FURTHER INCIDENT. PILOT SHUTDOWN ENGINE ON TAXI IN. REMOVED AND REPLACED NR 2 ENGINE ASSY. OPERATIONAL CHECK NORMAL. (M)

Next page: https://openairdocs.org/deregistered/N49543-2014-07-08/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 n_number = 'N49543' AND deregistration_id = 'N49543-2014-07-08'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N49543-2014-07-08/reports

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