# Service difficulty reports: N187SW, cancelled Sep 12, 2005

A list on [N187SW, cancelled Sep 12, 2005](https://openairdocs.org/deregistered/N187SW-2005-09-12.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 · 90 reports

- [SDR SWIA200514909](https://openairdocs.org/sdr/SWIA200514909.md): Selector · malfunctioned · Apr 15, 2005 · N187SW · Emb EMB120ER · Trailing Edge Flap Control System
  > CREW REPORTED FLAP CONTROL FAULT AND ADVANCED SWS WHEN FLAPS SELECTED. REMOVED AND REPLACED FLAP LEVER IAW MM 27-50-01, OPERATIONAL CHECK GOOD.
- [SDR SWIA200514858](https://openairdocs.org/sdr/SWIA200514858.md): Selector · binding · Apr 9, 2005 · N187SW · Emb EMB120ER · Trailing Edge Flap Control System
  > FLAP SELECTOR BINDS IN 45 DEG NOTCH. REPLACED FLAP SELECTOR LEVER ASSY IAW EMB MM 27-50-01, OPERATIONAL CHECK GOOD.
- [SDR SWIA200514857](https://openairdocs.org/sdr/SWIA200514857.md): Actuator · malfunctioned · Apr 9, 2005 · N187SW · Emb EMB120ER · Rudder Control System
  > ONCE AIRBORNE, RIGHT RUDDER WOULD ONLY MOVE HALF WAY. REPLACED BLUE SYSTEM RUDDER ACTUATOR IAW EMB MM 27-22-02, OPERATIONAL CHECK IAW EMB MM 27-24-00 GOOD.
- [SDR SWIA200514415](https://openairdocs.org/sdr/SWIA200514415.md): Fcu · malfunctioned · Jan 17, 2005 · N187SW · Emb EMB120ER · Trailing Edge Flap Control System
  > AFTER LANDING FLAPS STAYED AT 45 DEGREES. INSTALLED A SERVICEABLE FCU. OPERATIONAL CHECK GOOD.
- [SDR SWIA200514339](https://openairdocs.org/sdr/SWIA200514339.md): Actuator · malfunctioned · Jan 6, 2005 · N187SW · Emb EMB120ER · Rudder Actuator
  > ON TAKEOFF, THE RIGHT RUDDER HAD VERY LIMITED TRAVEL. REPLACED GREEN HYDRAULIC RUDDER ACTUATOR IAW 27-22-02. OPS AND LEAK CHECK GOOD.
- [SDR SWIA200413590](https://openairdocs.org/sdr/SWIA200413590.md): Control Panel · malfunctioned · Jul 15, 2004 · N187SW · Emb EMB120ER · Stall Warning System
  > STALL WARNING ON MAP WILL NOT CLEAR. REMOVED AND REPLACED STALL WARNING PANEL. OPERATIONAL CHECK GOOD. P/N: 120-84428-505, S/N OFF: 1200034R.
- [SDR SWIA200413524](https://openairdocs.org/sdr/SWIA200413524.md): Bracket · cracked · May 6, 2004 · N187SW · Emb EMB120ER · Wing Miscellaneous Structure
  > LEFT WING UPPER 2ND FROM LAST SKIN SUPPORT BRACKET CRACKED. DISCOVERED DURING C-CHECK INSPECTION. SKIN SUPPORT REMOVED AND REPLACED IAW SRM 57-20-07, 51-25-00, 51-40-05, AND 51-40-02.
- [SDR SWIA200413523](https://openairdocs.org/sdr/SWIA200413523.md): Bracket · cracked · May 6, 2004 · N187SW · Emb EMB120ER · Wing Miscellaneous Structure
  > LEFT WING UPPER 3RD FROM FRONT SKIN SUPPORT BRACKET IS CRACKED AT RIB 22. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW CLIP IAW SRM 57-20-07, 51-40-05, 51-25-00, 51-40-02.
- [SDR SWIA200413495](https://openairdocs.org/sdr/SWIA200413495.md): Rib · worn · May 6, 2004 · N187SW · Emb EMB120ER · Wing, Rib/Bulkhead
  > RIGHT WING LEADING EDGE INBOARD OF NACELLE, OUTBOARD ATTACH POINT RIB WORN THROUGH. DISCOVERED DURING C-CHECK INSPECTION. RIB REPAIRED IAW EMB 120 SRM 51-70-05 FIG 1.
- [SDR SWIA200413494](https://openairdocs.org/sdr/SWIA200413494.md): Support Bracket · cracked · May 6, 2004 · N187SW · Emb EMB120ER · Wing Miscellaneous Structure
  > RIGHT WING UPPER 4TH FROM FRONT SKIN SUPPORT BRACKET CRACKED AT RIB 8. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED SKIN SUPPORT CLIP IAW SRM 57-20-07, 51-25-40, 51-40-05, AND 51-40-02.
- [SDR SWIA200413493](https://openairdocs.org/sdr/SWIA200413493.md): Rib · cracked · May 6, 2004 · N187SW · Emb EMB120ER · Wing, Rib/Bulkhead
  > RIGHT WING FORWARD RIB 19 CRACKED AT TWO SPOTS. DISCOVERED DURING C-CHECK INSPECTION. RIGHT WING FORWARD RIB 19 REPLACED IAW EMB 120 SRM 51-40-07, 51-40-04, 51-40-05, 51-22-00, AND 51-40-07, AND CONTINUATION SHEET 1 AND 2.
- [SDR SWIA200413492](https://openairdocs.org/sdr/SWIA200413492.md): Rib · cracked · May 6, 2004 · N187SW · Emb EMB120ER · Wing, Rib/Bulkhead
  > RIGHT WING FORWARD RIB 20 CRACKED AT TOP TWO SPOTS. DISCOVERED DURING C-CHECK INSPECTION. RIGHT WING FORWARD RIB 20 REPLACED IAW 51-25-00, 51-40-05, 51-40-02, 51-22-00.
- [SDR SWIA200413491](https://openairdocs.org/sdr/SWIA200413491.md): Support Bracket · corroded · May 6, 2004 · N187SW · Emb EMB120ER · Wing Miscellaneous Structure
  > RIGHT WING UPPER 2ND FROM FRONT SKIN SUPPORT BRACKET AT RIB 20 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED SKIN SUPPORT CLIP IAW SRM 57-20-07, 51-25-00, 51-40-05, 51-40-02.
- [SDR SWIA200413490](https://openairdocs.org/sdr/SWIA200413490.md): Support Bracket · cracked · May 6, 2004 · N187SW · Emb EMB120ER · Wing Miscellaneous Structure
  > RIGHT WING UPPER 2ND FROM FRONT SKIN SUPPORT BRACKET CRACKED AT RIB 21. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED SKIN SUPPORT CLIP IAW SRM 57-20-07, 51-25-00, 51-40-05, AND 51-40-02.
- [SDR SWIA200413489](https://openairdocs.org/sdr/SWIA200413489.md): Support Bracket · cracked · May 6, 2004 · N187SW · Emb EMB120ER · Wing Miscellaneous Structure
  > RIGHT WING UPPER FORWARD SKIN SUPPORT BRACKET CRACKED AT RIB 21. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED SKIN SUPPORT IAW SRM 57-20-07, 51-25-00, 51-40-05, AND 51-40-02.
- [SDR SWIA200413488](https://openairdocs.org/sdr/SWIA200413488.md): Support Bracket · cracked · May 6, 2004 · N187SW · Emb EMB120ER · Wing Miscellaneous Structure
  > RIGHT WING UPPER AFT SKIN SUPPORT BRACKET CRACKED AT RIB 23. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED SKIN SUPPORT CLIP IAW SRM 57-20-07, 51-25-00, 51-40-05, AND 51-40-02.
- [SDR SWIA200413487](https://openairdocs.org/sdr/SWIA200413487.md): Support Bracket · cracked · May 6, 2004 · N187SW · Emb EMB120ER · Wing Miscellaneous Structure
  > RIGHT WING UPPER 3RD FROM FRONT SKIN SUPPORT BRACKET AT RIB 23 IS CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED SKIN SUPPORT CLIP IAW SRM 57-20-07, 51-25-00, 52-40-05, 51-40-02.
- [SDR SWIA200413486](https://openairdocs.org/sdr/SWIA200413486.md): Support Bracket · cracked · May 6, 2004 · N187SW · Emb EMB120ER · Wing Miscellaneous Structure
  > RIGHT WING RIB 24 LOWER 2ND FROM FRONT SKIN SUPPORT BRACKET CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED CRACKED BRACKET IAW SRM 57-20-07, 51-25-00, 51-40-05, AND 51-40-02.
- [SDR SWIA200413485](https://openairdocs.org/sdr/SWIA200413485.md): Structure · cracked · May 6, 2004 · N187SW · Emb EMB120ER · Wing, Fuselage Attach Fittings
  > LEFT ZONE 193 LOWER FLANGE WING TO FUSELAGE IS CRACKED IN THREE LOCATIONS. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED ANGLE IAW EMB 120 SRM 53-20-13 PG 205-206 FIG 202.
- [SDR SWIA200413484](https://openairdocs.org/sdr/SWIA200413484.md): Support Bracket · cracked · May 6, 2004 · N187SW · Emb EMB120ER · Wing Miscellaneous Structure
  > LEFT WING UPPER AFT SKIN SUPPORT BRACKET CRACKED AT RIB 8. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED CLIPS IAW SRM 57-20-07, 51-40-05, 52-25-00, 51-40-02.
- [SDR SWIA200413483](https://openairdocs.org/sdr/SWIA200413483.md): Support Bracket · cracked · May 6, 2004 · N187SW · Emb EMB120ER · Wing Miscellaneous Structure
  > LEFT WING UPPER 3RD FROM FRONT SKIN SUPPORT BRACKET CRACKED AT RIB 8. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED SKIN SUPPORT IAW SRM 57-20-07, 51-40-05, 51-25-00, AND 51-40-02.
- [SDR SWIA200413482](https://openairdocs.org/sdr/SWIA200413482.md): Support Bracket · cracked · May 6, 2004 · N187SW · Emb EMB120ER · Wing Miscellaneous Structure
  > LEFT WING UPPER 2ND FROM FRONT SKIN SUPPORT BRACKET CRACKED AT RIB 8. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED SKIN SUPPORT IAW SRM 57-20-07, 51-40-05, 51-25-00, AND 51-40-02.
- [SDR SWIA200413481](https://openairdocs.org/sdr/SWIA200413481.md): Support Bracket · cracked · May 6, 2004 · N187SW · Emb EMB120ER · Wing Miscellaneous Structure
  > LEFT WING UPPER AFT SKIN SUPPORT BRACKET CRACKED AT RIB 23. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED SKIN SUPPORT CLAMP IAW SRM 57-20-07, 51-25-00, 51-40-05, AND 51-40-02.
- [SDR SWIA200413480](https://openairdocs.org/sdr/SWIA200413480.md): Frame · cracked · May 6, 2004 · N187SW · Emb EMB120ER · Fuselage Main, Frame
  > FRAME 15 IN BELLY CRACKED FRAME AT AFT AIR STAIR ACTUATOR. DISCOVERED DURING C-CHECK INSPECTION. FRAME REPAIRED IAW EMB 120 SRM 53-00-04 PG 201-204.
- [SDR SWIA200412932](https://openairdocs.org/sdr/SWIA200412932.md): Proximity Switch · faulty · Feb 20, 2004 · N187SW · Emb EMB120ER · Elevator Control System
  > FIRST FLIGHT AURAL WARNING TRIM CHECK FAILS. REMOVED LEFT AND RIGHT ELEVATOR TRIM PROX SWITCHES HAND SHAKE CONNECTORS AND REPLACED WITH ENVIRONMENTAL SPLICE CONNECTORS IAW EMB 120 WMM 20-21-00 AND 31-52-00, OPS CHECKED GOOD.
- [SDR SWIA200412861](https://openairdocs.org/sdr/SWIA200412861.md): Shutoff Valve · malfunctioned · Feb 5, 2004 · N187SW · Emb EMB120ER · Pneumatic Distribution System
  > SMOKE IN COCKPIT AND CABIN WITH BOTH PACKS OFF. REMOVED AND REPLACED LT ENGINE PRESSURE REGULATOR SHUT OFF VALVE WITH SERVICEABLE UNIT IAW MM 36-10-04. OPS CHECKS GOOD AT THIS TIME.
- [SDR SWIA200412853](https://openairdocs.org/sdr/SWIA200412853.md): Annunciator · malfunctioned · Jan 27, 2004 · N187SW · Emb EMB120ER · Trailing Flap Position Indicating System
  > FLAP CONTROL FAULT, DISAGREE, AND ASYM MESSAGE OVERHEAD FLAP AND ADVANCED SWS ON MAP STAY ON. INSTALLED A SERVICEABLE FLAP ANNUNCIATOR IAW 27-50-05. OPS CHECK GOOD. REMOVED AND REPLACED FLAP CONTROL UNIT. P/N OFF: 347200-1001, SN OFF: 0194.
- [SDR SWIA200312609](https://openairdocs.org/sdr/SWIA200312609.md): Light · shorted · Nov 13, 2003 · N187SW · Emb EMB120ER · Emergency Lighting
  > EMERGENCY EXIT LIGHTS AT 6A AND 6C OVERWING EXIT AND THE MIDDLE CEILING LIGHT AS WELL AS FOUR OR FIVE FLOOR LEVEL LIGHTS DO NOT ILLUMINATE OR JUST BARELY LIGHT UP. FOUND SHORT AT LEFT OVERWING EMERGENCY EXIT FLOOD LIGHT. RECONNECTED, REPOSITIONED TERMINALS A
- [SDR SWIA200312408](https://openairdocs.org/sdr/SWIA200312408.md): Control Unit · malfunctioned · Sep 14, 2003 · N187SW · Emb EMB120ER · Trailing Edge Flap Control System
  > CONTROL FAULT WITH FLAP AND ADVANCED SWS IN FLIGHT INBOARD FLAPS FLASHING. CLEARED WITH RESET IAW QRH. REMOVED AND REPLACED RIGHT INBOARD FLAP ACTUATOR AND REPLACED FCU IAW 27-80-08. OPS AND LEAK CHECKS GOOD. PN: 320300-1005 SN OFF: 0885
- [SDR SWIA200312381](https://openairdocs.org/sdr/SWIA200312381.md): Control Unit · malfunctioned · Sep 6, 2003 · N187SW · Emb EMB120ER · Trailing Edge Flap Control System
  > ON APPROACH INTO SLC WE SELECTED FLAPS 15 AND GOT THE ''CONTROL FAULT'' WITH THE ''FLAP'' AND ''ADVANCED SWS'' ON THE MAP. QRH PROCEDURE CORRECTED PROBLEM.REMOVED AND REPLACED FLAP CONTROL UNIT IAW MM 27-50-06. OPS CHECK GOOD.
- [SDR SWIA200312382](https://openairdocs.org/sdr/SWIA200312382.md): Bracket · cracked · Sep 2, 2003 · N187SW · Emb EMB120ER · Trailing Edge Flaps
  > RT INBOARD FLAP ROLLER BRACKET IS CRACKED. REPLACED RT INBOARD FLAP OUTBOARD GAP PANEL ROLLER BRACKET. CHECKS GOOD.
- [SDR SWIA200312076](https://openairdocs.org/sdr/SWIA200312076.md): Wire Harness · unserviceable · Jun 7, 2003 · N187SW · Emb EMB120ER · Landing Gear Position and Warning
  > WHEN LANDING GEAR LEVER WAS MOVED DOWN, RIGHT RED TRANSITION -A- LIGHT STAYED ON, RIGHT GREEN -A- LIGHT DID NOT COME ON. REMOVED AND INSTALLED SERVICEABLE WIRE HARNESS. OPS CHECK GOOD ON GEAR SWING IAW EMB MM 32-61-01. P/N OFF/ON 120-22623-501.
- [SDR SWIA200312070](https://openairdocs.org/sdr/SWIA200312070.md): Actuator · malfunctioned · Jun 4, 2003 · N187SW · Emb EMB120ER · Trailing Edge Flap Control System
  > INFLIGHT FLAP CONTROL FAULT INDICATION WOULD NOT CLEAR. RETURNED TO FIELD. REMOVED AND REPLACED RIGHT OUTBOARD FLAP ACTUATOR. OPS AND LEAK CHECKS GOOD IAW MM 27-50-09.
- [SDR SWIA200311896](https://openairdocs.org/sdr/SWIA200311896.md): Relay · malfunctioned · Apr 21, 2003 · N187SW · Emb EMB120ER · Landing Gear Retraction/Extension System
  > DURING FLIGHT, RIGHT MAIN ''A'' GREEN LIGHT ILLUMINATED. GEAR WOULD NOT EXTEND - ALL THREE GEAR RED LIGHTS ILLUMINATED EXCEPT RIGHT ''A'' RED WITH HANDLE DOWN. AFTER 5 MINUTES THE PROBLEM FIXED ITSELF AND THE GEAR LOWERED NORMALLY. REPLACED LANDING GEAR REL
- [SDR SWIA200311687](https://openairdocs.org/sdr/SWIA200311687.md): Connector · contaminated · Jan 7, 2003 · N187SW · Emb EMB120ER · Trailing Edge Flap Control System
  > CONTROL FAULT ON INBOARD FLAPS DURING FLAP RETRACTION. CLEANED CONNECTOR ON FLAP INBOARD ACTUATORS ON BOTH SIDES. RAN SEVERAL TIMES. NO FAULTS AT THIS TIME.
- [SDR SWIA200211584](https://openairdocs.org/sdr/SWIA200211584.md): Wire Harness · malfunctioned · Dec 16, 2002 · N187SW · Emb EMB120ER · Landing Gear System Wiring
  > ON TAKEOFF FROM PSP, THE RT GEAR GREEN SYS A LIGHT REMAINED ON. UPON PUTTING GEAR DOWN AT LAX, THE GEAR DID NOT COME DOWN. PERFORMED ELECTRIC OVERRIDE QRH PROCEDURE AND THE GEAR CAME DOWN OK. REMOVED RIGHT A-HARNESS, REPAIRED AND REINSTALLED IAW 32-60-00.
- [SDR SWIA200211579](https://openairdocs.org/sdr/SWIA200211579.md): Annunciator · malfunctioned · Dec 15, 2002 · N187SW · Emb EMB120ER · Trailing Flap Position Indicating System
  > AFTER LANDING AT PSP THE INBOARD FLAPS WOULD NOT RETRACT. REPLACED FLAP ANNUNCIATOR WITH A SERVICEABLE UNIT. OPS CHECK GOOD.
- [SDR SWIA200211561](https://openairdocs.org/sdr/SWIA200211561.md): Switch · lack of lube · Dec 1, 2002 · N187SW · Emb EMB120ER · Door Warning System
  > FORWARD DOOR LIGHT ILLUMINATED INFLIGHT. LUBED FORWARD DOOR MICROSWITCHES. OPS CHECK GOOD.
- [SDR SWIA200211185](https://openairdocs.org/sdr/SWIA200211185.md): Wire · broken · Aug 30, 2002 · N187SW · Emb EMB120ER · Light System Wiring
  > FLOOR LIGHTING IN FRONT OF GALLEY NOT WORKING. REPAIRED BROKEN WIRE. OPS CHECK GOOD.
- [SDR SWIA200210925](https://openairdocs.org/sdr/SWIA200210925.md): Link · corroded · May 9, 2002 · N187SW · Emb EMB120ER · Passenger/Crew Doors
  > PASSENGER DOOR PUSH-PULL LINKS CORRODED (FORWARD AND AFT). REMOVED AND REPLACED PASSENGER DOOR FORWARD AND AFT PUSH-PULL LINKS IAW EMB MM 52-11-03.
- [SDR SWIA200210924](https://openairdocs.org/sdr/SWIA200210924.md): Wire · burned · May 9, 2002 · N187SW · Emb EMB120ER · Electrical Power System Wiring
  > WIRE AT CANNON PLUG J0958 PIN F ON RIGHT SIDE DC RELAY BOX IS BURNED AND NEEDS TO BE REPLACED. REMOVED AND REPLACED WIRE W208-0064 AT CANNON PLUG J0958 PIN F WITH A NEW WIRE 1 GAUGE LARGER AND PERFORMED OPERATIONAL CHECK AS PER MM 30-40-00. OPS CHECK GOOD.
- [SDR SWIA200210923](https://openairdocs.org/sdr/SWIA200210923.md): Torque Tube · corroded · May 9, 2002 · N187SW · Emb EMB120ER · Entrance Stairs
  > NR 2 AND NR 3 PASSENGER DOOR STEP RODS FOUND CORRODED DURING INSPECTION. REMOVED AND REPLACED NR 2 AND NR 3 PASSENGER DOOR STEP TORQUE TUBES IAW EMB MM 52-10-03.
- [SDR SWIA200210922](https://openairdocs.org/sdr/SWIA200210922.md): Actuator · corroded · May 9, 2002 · N187SW · Emb EMB120ER · Entrance Stairs
  > PASSENGER DOOR STEP ACTUATOR ARM FOUND CORRODED. REMOVED AND REPLACED PASSENGER DOOR STEP ACTUATOR ARM WITH NEW. OPS CHECK GOOD.
- [SDR SWIA200210830](https://openairdocs.org/sdr/SWIA200210830.md): Pcu · malfunctioned · Apr 28, 2002 · N187SW · Emb EMB120ER · Rudder Control System
  > ON TAKEOFF, COULD NOT MOVE RUDDER PAST HALF TRAVEL TO THE RIGHT. TURNING BLUE SYSTEM OFF MADE NO DIFFERENCE. UPON LANDING FULL TRAVEL WAS RESTORED. REPLACED RUDDER PCU. INFLIGHT FUNCTIONAL TEST OF RUDDER SYSTEM NORMAL. FLIGHT TEST OK.
- [SDR SWIA200210704](https://openairdocs.org/sdr/SWIA200210704.md): Support · worn · Mar 2, 2002 · N187SW · Emb EMB120ER · Elevator Tab Control System
  > THE ELEVATOR TRIM FORWARD QUADRANT IDLER SPROCKET SUPPORT HAS CHAIN TRACKS WORN IN IT. REMOVED DAMAGED SUPPORT AND INSTALLED NEW IAW EMB SRM 51-40-02.
- [SDR SWIA200210618](https://openairdocs.org/sdr/SWIA200210618.md): Trim Tab · out of adjust · Feb 1, 2002 · N187SW · Emb EMB120ER · Elevator Tab Control System
  > ON DESCENT INTO EKO, TRIM FAIL WARNING WENT OFF. AFTER A/P DISCONNECT, AIRCRAFT PITCHED UP AT 230 KTS WITH ELEVATOR TRIM AT FULL NOSE DOWN STOP. AIRCRAFT NOT UNDER NORMAL CONTROL UNTIL SLOWED BELOW 200 KTS. ADJUSTED RT ELEVATOR TRIM TAB AS REQUIRED TO RECEI
- [SDR SWIA200210588](https://openairdocs.org/sdr/SWIA200210588.md): Controller · failed · Jan 25, 2002 · N187SW · Emb EMB120ER · Cabin Pressure Controller
  > ON DEPARTURE, AIRCRAFT WOULD NOT PRESSURIZE AT ALL. MANUAL CONTROLLER WOULD NOT FUNCTION. RETURNED TO ELKO. REMOVED AND REPLACED AUTO PRESSURIZATION CONTROLLER IAW EMB MM 21-30-01. AUTO PRESSURIZATION OPS CHECKS GOOD IAW EMB MM 21-30-00.
- [SDR SWIA200110514](https://openairdocs.org/sdr/SWIA200110514.md): Stringer · cracked · Dec 28, 2001 · N187SW · Emb EMB120ER · Wing, Longeron/Stringer
  > STRINGER NR 8 CRACKED AT LEFT WING NR 2 FUEL PANEL. REPAIRED STRINGER CRACK IAW EMB SRM 57-20-03.
- [SDR SWIA200110031](https://openairdocs.org/sdr/SWIA200110031.md): Warning System · activated · Jul 11, 2001 · N187SW · Emb EMB120ER · Propeller Feathering/Reversing
  > AUTO FEATHER WARNING ON TAKE OFF ROLL.RAN BOTH ENGINES W/AUTO FEATHER ARMED. APPLIED 60% TORQUE. NO AUTO FEATHER WARNINGS. OPS CHECK GOOD.
- [SDR SWIA972561](https://openairdocs.org/sdr/SWIA972561.md): Valve · failed · May 9, 2001 · N187SW · Emb EMB120ER · Cabin Cooling System
  > RIGHT PACK FAILED DURING CLIMB. APPROXIMATELY 1 MINUTE LATER, THE LAV SMOKE DETECTOR STARTED BEEPING AND THE FLIGHT ATTENDANT REPORTED SMOKE IN THE CABIN. WITH RECIRCS AND GASPERS OFF, THE CABIN SLOWLY CLEARED. REMOVED LEFT AND RIGHT RAM AIR VENTILATION VAL

Next page: https://openairdocs.org/deregistered/N187SW-2005-09-12/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 = 'N187SW' AND deregistration_id = 'N187SW-2005-09-12'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N187SW-2005-09-12/reports

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