# Service difficulty reports: N186SW, cancelled Feb 21, 2006

A list on [N186SW, cancelled Feb 21, 2006](https://openairdocs.org/deregistered/N186SW-2006-02-21.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 · 71 reports

- [SDR SWIA200515683](https://openairdocs.org/sdr/SWIA200515683.md): Light · broken · Oct 13, 2005 · N186SW · Emb EMB120ER · Emergency Lighting
  > RT OVERWING EMERGENCY LIGHT BROKEN. REPLACED RIGHT WING EMERGENCY EXIT LIGHT ASSY, OPERATIONAL CHECK GOOD.
- [SDR SWIA200515564](https://openairdocs.org/sdr/SWIA200515564.md): Lamp · burned out · Sep 15, 2005 · N186SW · Emb EMB120ER · Emergency Lighting
  > ROW 9A FLOOR EMERGENCY LIGHTING, ONE RED LIGHT INOP. RELAMPED BULB TO LIGHT SOCKET, OPERATIONAL CHECK GOOD.
- [SDR SWIA200514491](https://openairdocs.org/sdr/SWIA200514491.md): Line · leaking · Jan 15, 2005 · N186SW · Emb EMB120ER · Hydraulic System, Main
  > AFTER GEAR EXTENSION, GREEN HYDRAULIC LOW LEVEL LIGHT, THE GUAGE CONFIRMED ZERO QUANTITY. REPLACED GEAR DOWN HYDRAULIC FLEXIBLE LINE ON RIGHT MAIN GEAR. SERVICED HYDRAULICS TO PROPER LEVEL. OPERATIONAL CHECK GOOD.
- [SDR SWIA200414044](https://openairdocs.org/sdr/SWIA200414044.md): Door · binding · Nov 1, 2004 · N186SW · Emb EMB120ER · Passenger/Crew Doors
  > MAIN CABIN DOOR IS DIFFICULT TO OPEN AND CLOSE. REMOVED DOOR, CLEANED AND REPLACED HARDWARE IAW 52-10-00.
- [SDR SWIA200413896](https://openairdocs.org/sdr/SWIA200413896.md): Rib · cracked · Jul 16, 2004 · N186SW · Emb EMB120ER · Wing, Rib/Bulkhead
  > LEFT WING AT RIB 8 WING TO WEB CLIP IS CRACKED. ITEM FOUND AT C-CHECK. REPLACED SUPPORT BRACKET IAW SRM 51-25-00, 51-40-00.
- [SDR SWIA200413313](https://openairdocs.org/sdr/SWIA200413313.md): Power Supply · malfunctioned · May 10, 2004 · N186SW · Emb EMB120ER · Emergency Lighting
  > REAR HALF OF EMERGENCY FLOOR LIGHTING STRIPS ARE NOT WORKING. REMOVED AND REPLACED NR 4 POWER SUPPLY IAW 33-50-00. OPS CHECK GOOD. P/N: D366-04-001, S/N ON: 1204, S/N OFF: 1209.
- [SDR SWIA200413009](https://openairdocs.org/sdr/SWIA200413009.md): Control Unit · malfunctioned · Mar 8, 2004 · N186SW · Emb EMB120ER · Trailing Edge Flap Control System
  > DURING TAKEOFF RUN JUST AFTER POWER UP, A SINGLE CHIME WITH FLAP, CONTROL FAULT, ADVANCED SWS. PERFORMED THE ABORT AND RETURNED TO THE GATE. RERACKED FLAP CONTROL UNIT PER MAINT MM 22-50-06. CYCLED POWER, PERFORMED HIGH SPEED TAXI WITH CREW. OPS CHECK GOOD
- [SDR SWIA200412948](https://openairdocs.org/sdr/SWIA200412948.md): Annunciator · malfunctioned · Feb 20, 2004 · N186SW · Emb EMB120ER · Trailing Flap Position Indicating System
  > FLAP FAULTS INTERMITTENTLY IN AIR AND ON GROUND. REPLACED FLAP ANNUNCIATOR. OPS CHECKED GOOD.
- [SDR SWIA200412837](https://openairdocs.org/sdr/SWIA200412837.md): Panel · cracked · Jan 26, 2004 · N186SW · Emb EMB120ER · Wing, Plate/Skin
  > STRINGER ON LT WING FORWARD OF NR 2 FUEL PANEL CRACKED. DISCOVERED DURING LINE INSPECTION. REPAIRED LEFT WING FORWARD STRINGER AT NR 2 FUEL PANEL IAW SRM 120 57-20-03 PG 205 TO 211, FIG 202 & IAW RII CARD 28-301.
- [SDR SWIA200312108](https://openairdocs.org/sdr/SWIA200312108.md): Roller · binding · Jun 18, 2003 · N186SW · Emb EMB120ER · Trailing Edge Flaps
  > OUTBOARD FLAP DISAGREEMENT DURING FLAP RETRACTION. RESET BY SLOWING TO APPROX 140 AND RESETTING LEVER. FOUND RIGHT OUTBOARD FLAP LOWER MOVEABLE CHANNEL MISSING ROLLER AND FLAP WAS BINDING. INSTALLED NEW ROLLER AND SUPPORT BRACKET IAW MM 57-52-00. OPS CHEC
- [SDR SWIA200311938](https://openairdocs.org/sdr/SWIA200311938.md): Switch · out of position · Apr 29, 2003 · N186SW · Emb EMB120ER · Passenger/Crew Doors
  > HYDRAULIC LOCK ON MAIN CABIN DOOR WITH OCCASIONAL FORWARD ACTUATOR LIGHT ON OVERHEAD PANEL. PERFORMED QRH PROCEDURE AND THE DOOR OPENED. REPOSITIONED SWITCH IN HOUSING. TESTED AND DOOR WORKS OK. WORK PERFORMED IAW EMB MM 52-12-00.
- [SDR SWIA200311765](https://openairdocs.org/sdr/SWIA200311765.md): Indicator · malfunctioned · Jan 28, 2003 · N186SW · Emb EMB120ER · Engine BMEP/Torque Indicating
  > ON DEPARTURE FROM SLC, WHEN CLIMB POWER WAS SET 84 PERCENT TORQUE THE RIGHT TORQUE GUAGE FLUCTUATED, BOTH ANALOG AND DIGITAL. ALL OTHER ENGINE PARAMETER STAYED STABILIZED. FLUCTUATIONS WERE FROM 84 PERCENT TO APPROXIMATELY 50 PERCENT. REMOVED AND REPLACED R
- [SDR SWIA200211499](https://openairdocs.org/sdr/SWIA200211499.md): Battery · discharged · Nov 18, 2002 · N186SW · Emb EMB120ER · Emergency Lighting
  > EMERGENCY LIGHTS INOPERATIVE, INSTALLED SERVICEABLE EMERGENCY LIGHTS BATTERY PACK. OPS CHECK GOOD.
- [SDR SWIA200211184](https://openairdocs.org/sdr/SWIA200211184.md): Hydraulic Line · cracked · Aug 29, 2002 · N186SW · Emb EMB120ER · Hydraulic System, Main
  > DURING APPROACH, EXPERIENCED LOSS OF HYDRAULIC FLUID IN BLUE SYSTEM. FOLLOWED QRH, LANDED UNEVENTFULLY. FOUND CRACKED LINE IN RIGHT NACELLE. REMOVED AND REPLACED LINE. RAN ENGINES. LEAK CHECK GOOD.
- [SDR SWIA200211171](https://openairdocs.org/sdr/SWIA200211171.md): Frame · cracked · Jul 19, 2002 · N186SW · Emb EMB120ER · Nacelle/Pylon, Frame/Spar/Rib
  > FOUND DURING C-CHECK, RIGHT NACELLE FRAME -0- HAS SEVERAL CRACKS IN IT. REMOVED AND REPLACED FRAME -0- IAW SRM 51-40-02.
- [SDR SWIA200211170](https://openairdocs.org/sdr/SWIA200211170.md): Intercostal · cracked · Jul 19, 2002 · N186SW · Emb EMB120ER · Fuselage Miscellaneous Structure
  > FOUND DURING C-CHECK, INTERCOSTAL AFT OF PILOT'S SIDE WINDOW CRACKED. FABRICATED AND INSTALLED DOUBLER TO PART IAW EMB SRM 51-00-00 AND 51-40-02.
- [SDR SWIA200211169](https://openairdocs.org/sdr/SWIA200211169.md): Frame · cracked · Jul 19, 2002 · N186SW · Emb EMB120ER · Nacelle/Pylon, Frame/Spar/Rib
  > FOUND DURING C-CHECK, RIGHT NACELLE FRAME NR 1 CRACKED. ACCOMPLISHED EMB S/B 120-54-0036 REV 2. C/W PART 1-2.2.1, 2.2.2.1 THROUGH 2.2.3.8 & PART 2-2.3.
- [SDR SWIA200211168](https://openairdocs.org/sdr/SWIA200211168.md): Frame · cracked · Jul 19, 2002 · N186SW · Emb EMB120ER · Nacelle/Pylon, Frame/Spar/Rib
  > FOUND DURING C-CHECK, LEFT NACELLE FRAME ONE IS CRACKED AT THE I/B TORSION MOUNT. COMPLIED WITH S/B 120-54-0036 REV 2 NACELLES - INSPECTION/REPLACEMENT OF NACELLE FRAME ONE.
- [SDR SWIA200211167](https://openairdocs.org/sdr/SWIA200211167.md): Bracket · cracked · Jul 19, 2002 · N186SW · Emb EMB120ER · Nacelle/Pylon Miscellaneous Structure
  > FOUND DURING C-CHECK, AT FRAME 13, THE BRACKET THAT HOLDS THE POWER POSITION PULLEY QUADRANT, RT NACELLE, I/B SIDE IS CRACKED. REMOVED AND REPLACED THE CRACKED BRACKET AT FRAME 13, RT NACELLE IAW EMB SRM 51-00-00 AND 51-40-02.
- [SDR SWIA200211166](https://openairdocs.org/sdr/SWIA200211166.md): Frame · cracked · Jul 19, 2002 · N186SW · Emb EMB120ER · Nacelle/Pylon, Frame/Spar/Rib
  > FOUND DURING C-CHECK, RIGHT SIDE NACELLE O/B SIDE FRAME 15 CRACKED. FABRICATED AND INSTALLED DOUBLER AND FILLER IAW EMB SRM 51-00-00 AND 51-40-02.
- [SDR SWIA200211165](https://openairdocs.org/sdr/SWIA200211165.md): Frame · cracked · Jul 19, 2002 · N186SW · Emb EMB120ER · Nacelle/Pylon, Frame/Spar/Rib
  > FOUND DURING C-CHECK, RIGHT NACELLE I/B SIDE FRAME 16 CRACKED. STOP-DRILLED CRACK AND INSTALLED A REPAIR DOUBLER ON THE FRAME IAW EMB SRM 51-70-05.
- [SDR SWIA200211164](https://openairdocs.org/sdr/SWIA200211164.md): Frame · cracked · Jul 19, 2002 · N186SW · Emb EMB120ER · Nacelle/Pylon, Frame/Spar/Rib
  > FOUND DURING C-CHECK, LEFT NACELLE I/B SIDE FRAME 15 CRACKED. STOP-DRILLED CRACK. FABRICATED AND INSTALLED DOUBLER IAW EMB SRM 51-40-02 AND 51-70-05.
- [SDR SWIA200211163](https://openairdocs.org/sdr/SWIA200211163.md): Frame · cracked · Jul 19, 2002 · N186SW · Emb EMB120ER · Nacelle/Pylon, Frame/Spar/Rib
  > FOUND DURING C-CHECK, LEFT NACELLE O/B SIDE FRAME 17 CRACKED. STOP-DRILLED CRACK AND INSTALLED A REPAIR DOUBLER ON THE FRAME IAW EMB SRM 51-70-05 AND 51-40-02.
- [SDR SWIA200211162](https://openairdocs.org/sdr/SWIA200211162.md): Frame · cracked · Jul 19, 2002 · N186SW · Emb EMB120ER · Nacelle/Pylon, Frame/Spar/Rib
  > C-CHECK, LT NACELLE O/B SIDE FRAME 15 CRACKED. STOP-DRILLED CRACK AND INSTALLED A REPAIR DOUBLER ON THE FRAME IAW EMB SRM 51-70-05 AND 51-40-02.
- [SDR SWIA200211161](https://openairdocs.org/sdr/SWIA200211161.md): Bushing · corroded · Jul 19, 2002 · N186SW · Emb EMB120ER · Aileron Tabs
  > DURING C-CHECK, RIGHT AILERON TRIM TAB BUSHINGS AND HARDWARE ARE CORRODED. REMOVED AND REPLACED RIGHT AILERON TRIM TAB BUSHINGS AND HARDWARE IAW 57-60-00.
- [SDR SWIA200211160](https://openairdocs.org/sdr/SWIA200211160.md): Bushing · corroded · Jul 19, 2002 · N186SW · Emb EMB120ER · Aileron Tabs
  > DISCOVERED DURING C-CHECK, LEFT AILERON TRIM TAB BUSHINGS AND HARDWARE ARE CORRODED. REMOVED AND REPLACED LEFT AILERON TRIM TAB BUSHINGS AND HARDWARE IAW 57-60-00.
- [SDR SWIA200211159](https://openairdocs.org/sdr/SWIA200211159.md): Seat Track · corroded · Jul 19, 2002 · N186SW · Emb EMB120ER · Fuselage, Seat/Cargo Attach Fittings
  > DISCOVERED DURING C-CHECK, LEFT AND RIGHT FWD FLOOR SEAT TRACKS ARE CORRODED. REMOVED AND REPLACED LEFT AND RIGHT FWD FLOOR SEAT TRACKS IAW 53-01-05.
- [SDR SWIA200211158](https://openairdocs.org/sdr/SWIA200211158.md): Seat Track · corroded · Jul 19, 2002 · N186SW · Emb EMB120ER · Fuselage, Seat/Cargo Attach Fittings
  > DISCOVERED DURING C-CHECK, LEFT AND RIGHT FWD AND AFT WALL SEAT TRACKS ARE CORRODED. REMOVED AND REPLACED LEFT AND RIGHT FWD AND AFT WALL SEAT TRACKS IAW 53-01-05.
- [SDR SWIA200211157](https://openairdocs.org/sdr/SWIA200211157.md): Cable · corroded · Jul 19, 2002 · N186SW · Emb EMB120ER · Cargo/Baggage Doors
  > DURING C-CHECK, FOUND CABLES AND PULLEYS ON CARGO DOOR CORRODED. REMOVED AND REPLACED CABLES AND PULLEYS IAW 52-31-00.
- [SDR SWIA200211156](https://openairdocs.org/sdr/SWIA200211156.md): Antenna · corroded · Jul 19, 2002 · N186SW · Emb EMB120ER · DME/TACAN System
  > DURING C-CHECK FOUND SEVERAL LOWER FUSELAGE ANTENNAS WITH CORROSION: MKR 1/TDR 1/ DME 2/ RADAR ALT/ TDR 2. REPLACED DME AND MARKER BEACON ANTENNAS. FUNCTION CHECKED FOLLOWING SYSTEM: DME 1 & 2 IAW 34-51-00, ATC 1 & 2 IAW 34-52-00, MARKER BEACON 1 & 2 IAW 3
- [SDR SWIA200211033](https://openairdocs.org/sdr/SWIA200211033.md): Connector · faulty · Jul 4, 2002 · N186SW · Emb EMB120ER · Engine Oil Pressure
  > AFTER TAKEOFF AT 100 AGL, RECEIVED AN AURAL OIL WITH TRIPLE CHIME. NO ASSOCIATED MAP WARNINGS AND NO ENGINE PARAMETERS TO SUPPORT THE WARNING. ALARM WAS CONTINUOUS AND COULD NOT BE CANCELLED. RETURNED TO SLC. REMOVED AND REPLACED OIL PRESSURE TRANSDUCER CA
- [SDR SWIA200211012](https://openairdocs.org/sdr/SWIA200211012.md): Actuator · failed · Jul 3, 2002 · N186SW · Emb EMB120ER · Trailing Edge Flap Actuator
  > FLAP CONTROL FAULT INDICATION WITHOUT SELECTING ANY FLAP SETTINGS. LEFT OUTBOARD FLAP ACTUATOR FAILED THE OHM TEST. REMOVED AND REPLACED ACTUATOR ON LEFT OUTBOARD FLAP IAW 27-50-00.
- [SDR SWIA200210995](https://openairdocs.org/sdr/SWIA200210995.md): Cover · out of position · Jun 27, 2002 · N186SW · Emb EMB120ER · Propeller Feathering/Reversing
  > ABORTED TAKEOFF WHEN LEFT ENGINE FEATHERED ON TAKEOFF ROLL. INSPECTED AND FOUND SWITCH COVER FOR LEFT ENGINE ELECT FEATHER INTERFERING WITH THE SWITCH. REPOSITIONED SWITCH COVER AND ENSURED CLEARANCE ON SWITCH. PERFORMED EXTENSIVE GROUND RUNS WITH NO FURTHE
- [SDR SWIA200210981](https://openairdocs.org/sdr/SWIA200210981.md): Headset · shorted · Jun 24, 2002 · N186SW · Emb EMB120ER · Interphone/Passenger Announcement (PA) System
  > ELECTRICAL BURNING SMELL IN CABIN ASSOCIATED WITH TWO FLASHING CABIN PASSENGER LIGHTS ON CAPTAIN'S SIDE. REMOVED AND REPLACED FLIGHT ATTENDANT'S HANDSET IAW MM 23-41-01. OPS CHECKS GOOD.
- [SDR SWIA200210625](https://openairdocs.org/sdr/SWIA200210625.md): Switch · loose · Jan 24, 2002 · N186SW · Emb EMB120ER · Door Warning System
  > FORWARD CABIN DOOR LIGHT ON TAKEOFF. ABORTED TAKEOFF. INSPECTED/RECYCLED DOOR. LIGHT DID NOT ILLUMINATE AGAIN. FOUND UPPER MICRO SWITCH LOOSE. ADJUSTED SWITCH AND SECURED. OPS CHECKS GOOD.
- [SDR SWIA200210596](https://openairdocs.org/sdr/SWIA200210596.md): Switch · loose · Jan 22, 2002 · N186SW · Emb EMB120ER · Door Warning System
  > FORWARD DOOR WARNING LIGHT CAME ON DURING TAKEOFF ROLL. ABORTED TAKEOFF. CYCLED DOOR AS PER MX CONTROL. DOOR LIGHT EXTINGUISHED. FORWARD DOOR WARNING LIGHT ON TAKEOFF ROLL. ABORTED TAKEOFF. INSPECTED FORWARD DOOR INDICATION SYSTEM. WORKING NORMALLY, NO
- [SDR SWIA200110401](https://openairdocs.org/sdr/SWIA200110401.md): Boot · damaged · Nov 29, 2001 · N186SW · Emb EMB120ER · Airfoil Anti/De-ice System
  > LEFT AND RIGHT MIDDLE WING DEICE BOOTS LIGHTS CAME ON IN CLIMB.PATCHED HOLE IN LEFT MIDDLE WING DEICE BOOT IAW CMM.
- [SDR SWIA200110343](https://openairdocs.org/sdr/SWIA200110343.md): Battery Pack · discharged · Nov 2, 2001 · N186SW · Emb EMB120ER · Emergency Lighting
  > THREE CONSECUTIVE WHITE EMERGENCY LIGHTS (ROW 3-6), 1 RED FLOOR EMERGENCY LIGHT OUT AT ROW 6, 4 EXIT SIGNS AT ROW 6 OUT, 2 OVERHEAD WHITE EXIT LIGHTS OUT AT ROW 6. INSTALLED SERVICEABLE ELBP IN MID EMERGENCY LIGHT SECTION IAW MM 33-50-00. CHECKS GOOD.
- [SDR SWIA972456](https://openairdocs.org/sdr/SWIA972456.md): Actuator · failed · Mar 26, 2001 · N186SW · Emb EMB120ER · Trailing Edge Flap Actuator
  > FLAP CONTROL FAULT ON TAXI OUT. COULD NOT RESET. REMOVED AND REPLACED RIGHT OUTBOARD FLAP ACTUATOR IAW 27-50-09. OPS AND LEAK CHECK GOOD. P/N ON 320300-1007, S/N ON 1093, S/N OFF 1146.
- [SDR SWIA972455](https://openairdocs.org/sdr/SWIA972455.md): Actuator · faulty · Mar 25, 2001 · N186SW · Emb EMB120ER · Trailing Edge Flap Actuator
  > INTERMITTENT CONTROL FAULT FOR ALMOST THE ENTIRE FLIGHT, OUTBOARD FLAP INDICATING FLASHING. REMOVED AND REPLACED LEFT OUTBOARD FLAP ACTUATOR PER MM 27-50-09 AND RII 27-307. OPS CHECKS GOOD, NO LEAKS. P/N ON 320300-1007, S/N ON 0864, S/N OFF 0552.
- [SDR SWIA971939](https://openairdocs.org/sdr/SWIA971939.md): Flap · malfunctioned · Aug 19, 2000 · N186SW · Emb EMB120ER · Trailing Edge Flap Control System
  > FLAP CONTROL DID NOT RESET. DIVERTED TO SFO. FLAP 0 DEG LANDING. CHECKED THE RESISTANCE BETWEEN PIN G AND D AND E AS PER FAULT ISOLATION MANUAL 27-50-00 ON BOTH OUTBOARD FLAP ACTUATORS. FOUND THE RESISTANCE WITHIN LIMITS. PERFORMED FUNCTIONAL CHECK SEVERA
- [SDR SWIA971885](https://openairdocs.org/sdr/SWIA971885.md): Warning System · false activation · Jul 18, 2000 · N186SW · Emb EMB120ER · Propeller Feathering/Reversing
  > ON TAKEOFF ROLL, RECEIVED TAKEOFF AUTO FEATHER AURAL WARNING. ABORTED, VERIFIED SWITCH POSITION ON, NO CBS POPPED. REMOVED AND REPLACED AUTO FEATHER ON/OFF SWITCH MM 615320, RAN BOTH ENGINES, PERFORMED POWER RUNS AND AUTO FEATHER TEST CHECKS GOOD. P/N 8856K
- [SDR SWIA971748](https://openairdocs.org/sdr/SWIA971748.md): Switch · dirty · Mar 31, 2000 · N186SW · Emb EMB120ER · Landing Gear Position and Warning
  > AFTER DEPARTURE FROM SLC, RECEIVED LANDING GEAR AURAL WARNING AND RED LIGHT ON MAP ALARM, WOULD NOT CANCEL. RETURNED TO SLC. CLEANED POWER LEVER MICRO SWITCHES AS REQUIRED, OPS CHECKS GOOD.
- [SDR SWIA971713](https://openairdocs.org/sdr/SWIA971713.md): Harness · malfunctioned · Feb 26, 2000 · N186SW · Emb EMB120ER · Landing Gear Position and Warning
  > RIGHT A SYSTEM GEAR LIGHT WOULD NOT EXTINGUISH, ON RETRACTION THE GEAR WOULD NOT COME DOWN, HAD TO USE ELECTRIC OVERRIDE SWITCH. REMOVED AND REPLACED RIGHT MLG A SYSTEM WIRING HARNESS PER MM 326101, CYCLED GEAR.
- [SDR SWIA971159](https://openairdocs.org/sdr/SWIA971159.md): Prox Sensor · malfunctioned · Apr 4, 1998 · N186SW · Emb EMB120ER · Landing Gear Position and Warning
  > LEFT MAIN LANDING GEAR DOES NOT INDICATE GREEN WHEN SELECTED DOWN. REPAIRED LEFT A SYSTEM DOWN LOCK PROX SENSOR IAW MM 32-61-01. OPS CHECKS GOOD.
- [SDR SWIA971085](https://openairdocs.org/sdr/SWIA971085.md): Sensor · failed · Feb 23, 1998 · N186SW · Emb EMB120ER · Landing Gear Position and Warning
  > RIGHT MAIN GEAR IGNITION A GREEN LIGHT ON IN FLIGHT. GEAR WOULD NOT EXTEND NORMALLY SO USED EMERGENCY OVERRIDE TO EXTEND. REPLACED RIGHT MAIN A SYSTEM DOWN LOCK SENSOR PER MM 32-60-00. LANDING GEAR FUNCTIONAL CHECKS GOOD.
- [SDR SWIA971093](https://openairdocs.org/sdr/SWIA971093.md): Doors · iced up · Feb 4, 1998 · N186SW · Emb EMB120ER · Landing Gear Door Retract Section
  > RIGHT MAIN LANDING FAILED TO EXTEND UPON DOWN SELECTIONS. RIGHT MAIN WOULD ALSO NOT EXTEND DURING EMERGENCY EXTENSION PROCEDURE. INDICATIONS IN BOTH CASES, 2 RED TRANSIT LIGHTS ONLY ON RIGHT MAIN. RIGHT EVENTUALLY EXTENDED DURING A NORMAL SELECTION CYCLE.
- [SDR SWIA971075](https://openairdocs.org/sdr/SWIA971075.md): Oil Syst · reqd service · Jan 8, 1998 · N186SW · Emb EMB120ER · Turbine Engine Oil System
  > MOMENTARY LOW OIL PRESSURE INDICATION ON LEFT ENGINE ON CLIMB-OUT. RETURNED TO TWF. SERVICED OIL TO THE ADD 1 QUART MARK ON SIGHT GLASS. CHECKED ENGINE FOR OIL LEAKS BUT NONE WERE NOTED. GROUND RUN CHECKS GOOD WITH NO LEAKS.
- [SDR SWIA971069](https://openairdocs.org/sdr/SWIA971069.md): Oil Syst · reqd service · Jan 8, 1998 · N186SW · Emb EMB120ER · Turbine Engine Oil System
  > AFTER DEPARTURE FROM EKO, HAD A INTERMITTENT LOW OIL PRESSURE INDICATION ON LEFT ENGINE. RETURNED TO EKO. ADDED TWO QUARTS OF EXXON 2380 OIL TO LEFT ENGINE PER INSTRUCTIONS FROM MAINTENANCE CONTROL. AIRCRAFT WAS RUN UP TO 100 PERCENT ENGINE INSTRUMENTS SHOW
- [SDR SWIA971061](https://openairdocs.org/sdr/SWIA971061.md): Stringer · corroded · Dec 5, 1997 · N186SW · Emb EMB120ER · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND AT PASSENGER ENTRY AREA BELOW FORWARD AND AFT DOOR ACTUATORS, STRINGER 17. REMOVED AND REPLACED STRINGER 17 BELOW CABIN DOOR OPENING, IAW SRM 51-40-02.

Next page: https://openairdocs.org/deregistered/N186SW-2006-02-21/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 = 'N186SW' AND deregistration_id = 'N186SW-2006-02-21'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N186SW-2006-02-21/reports

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