# Service difficulty reports: N184SK, cancelled Sep 18, 2006

A list on [N184SK, cancelled Sep 18, 2006](https://openairdocs.org/deregistered/N184SK-2006-09-18.md).

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

- [SDR TC8A99015](https://openairdocs.org/sdr/TC8A99015.md): Fuel Control · malfunctioned · Apr 24, 1999 · N184SK · Doug DC861F · Fuel Control/Turbine Engines
  > TRIP NR 03295 LATI-EINN, NR 1 ENGINE FLAMEOUT AT 22:05 Z, ON DESCENT. ENGINE FLAMEOUT CHECKLIST COMPLETED, 35 PERCENT N2, OIL PRESSURE 20 PSI AND 25 PERCENT N1. PROCEEDED IN FLIGHT START JT3D CHECKLIST, NO RESPONSE. REMOVED AND REPLACED FUEL CONTROL IAW MM
- [SDR TC8A99013](https://openairdocs.org/sdr/TC8A99013.md): P & D Valve · failed · Apr 17, 1999 · N184SK · Doug DC861F · Fuel Controlling System
  > NR 1 ENGINE FLAME-OUT AFTER ENGINE START. FUEL FLOW INDICATOR SHOWING FLUCTUATION OF 1,000 +/- 500 PSI. FUEL PRESSURE ENGINE DRIVEN PUMP. NORMAL RANGE - FUEL PRESSURE INDICATION FUEL PUMP TANK PRESSURE/FEED. REMOVED AND REPLACED P & D VALVE AND FUEL FILTER
- [SDR TC8A98085](https://openairdocs.org/sdr/TC8A98085.md): Fuel Control · out of adjust · Dec 17, 1998 · N184SK · Doug DC861F · Fuel Control/Turbine Engines
  > NR 4 ENGINE WOULD NOT DEVELOPE TAKEOFF POWER, (1.87 EPR). REJECTED T/O AT 100 KTS. ADJUSTED NR 4 ENGINE FUEL CONTROL IAW DMM, CH 73-20-1. PERFORMED ENGINE RUN-UP TO T/O POWER, SYSTEM CHECKS GOOD DC8 ENGINE RUN UP MM IAW DMM 72-00.
- [SDR TC8A98080](https://openairdocs.org/sdr/TC8A98080.md): Fitting · loose · Nov 11, 1998 · N184SK · Doug DC861F · Hydraulic System, Main
  > SLOW HYDRAULIC FLUID DOWN TO STANDPIPE, MANUAL REVERSION LIGHT ON. ACCOMPLISHED ABNORMAL HYDRAULIC CHECKLIST. FOUND LOOSE FITTING PRESSURE SIDE OF NR 3 ENGINE HYDRAULIC PUMP. TIGHTENED FITTING, RAN ENGINE AND LEAK CHECK GOOD IAW 20-13-0.
- [SDR TC8A98079](https://openairdocs.org/sdr/TC8A98079.md): O-Ring · broken · Nov 11, 1998 · N184SK · Doug DC861F · Hydraulic System, Main
  > HYDRAULIC LOSS TO STANDPIPE IN FLIGHT. PERFORMED CHECKLIST, OPERATED IN MANUAL REVERSION. FOUND HYDRAULIC LEAD NR 3 ENGINE, HYDRAULIC PUMP INLET. REMOVED AND REPLACED BROKEN O-RING IAW 20-13-0, OPS CHECK GOOD.
- [SDR TC8A98067](https://openairdocs.org/sdr/TC8A98067.md): Engine · failed · Oct 7, 1998 · N184SK · Doug DC861F · Engine (Turbine/Turboprop)
  > DFW-DAY. TRIP# 02617 DISCREP: #1 ENGINE LOSS OF POWER ON CLIMBOUT 240-330. ENGINE SURGING FROM CLIMB EPR TO 1.6 THEN 1.3 SHUTDOWN, ALL PARAMETERS NORMAL. FERRIED AIRCRAFT TO KMIA. CORR. ACTION: 10/28/98 REMOVED AND REPLACED #1
- [SDR TC8A98065](https://openairdocs.org/sdr/TC8A98065.md): Fitting · failed · Oct 3, 1998 · N184SK · Doug DC861F · Hydraulic System, Main
  > DURING DESCENT, LOSS OF HYDRAULIC FLUID. QUANTITY DROPPED DOWN TO AUX MARK. PERFORMED IMMEDIATE ACTION ITEMS THEN ABNORMAL HYDRAULIC PROCEDURES. REPLACED NR 10 ELBOW FITTING ON NR 3 ENGINE HYDRAULIC BY-PASS PUMP. SYSTEM CHECKED ON ENGINE RUN. CHECKED IAW
- [SDR TC8A98051](https://openairdocs.org/sdr/TC8A98051.md): Cylinder · failed · Aug 25, 1998 · N184SK · Doug DC861F · Steering Unit
  > AFTER PUSHBACK, AIRCRAFT WOULD ONLY TURN SEVERAL DEGREES LEFT WITH NOSE WHEEL STEERING. FOUND RT STEERING CYLINDER FAILED DURING PUSHBACK. REPLACED RT STEERING CYLINDER AND FUNCTIONAL CHECK AND LEAK CHECK GOOD IAW 32-52-2.
- [SDR TC8A98038](https://openairdocs.org/sdr/TC8A98038.md): Engine · malfunctioned · Jul 2, 1998 · N184SK · Doug DC861F · Engine (Turbine/Turboprop)
  > ABORTED T/O AT IAH DUE TO HIGH EGT ON ENGINE NR 2, 1.85 EPR, EGT GOES 555 REDLINE AND CONTINUE TO CLIMB, SHUT DOWN ENGINE, TAXI BACK. ENGINE NR 2 EXCEEDS MAX EGT LIMITS. TO CLARIFY, NO LIMITS WERE EXCEEDED BUT APPEARED IT WOULD HAVE IF THROTTLE WAS NOT RETAR
- [SDR TC8A98030](https://openairdocs.org/sdr/TC8A98030.md): Line · failed · May 21, 1998 · N184SK · Doug DC861F · Hydraulic System, Main
  > DURING APPROACH, EXPERIENCED LOSS OF HYDRAULIC FLUID AND PRESSURE. COMPLIED WITH EMERGENCY CHECKLIST. FOUND AND REPLACED 2 PRESSURE HARD LINES FROM ENGINE HYDRAULIC PUMP THAT WERE SPLIT W/FLEX LINES. HYDRAULIC CASE DRAIN FILTERS FOUND OK. CHECKED ON RUN IA
- [SDR TC8A98020](https://openairdocs.org/sdr/TC8A98020.md): Cover Plate · loose · Apr 30, 1998 · N184SK · Doug DC861F · Turbine Engine Accessory Drive
  > PRECAUTIONARY SHUTDOWN NR 3 ENGINE ON SHORT FINAL. OIL PRESSURE STARTED FLUCTUATING BETWEEN 45 PSI AND YELLOW ARC. SHUT IT DOWN WHEN ITWENT BELOW THE RED LINE. REMOVED, INSPECTED AND REPLACED OIL FILTER PER MM 79-20-7, NO METAL FOUND IN FILTER, LEAK CHECKS
- [SDR TC8A98005](https://openairdocs.org/sdr/TC8A98005.md): Switch · failed · Jan 29, 1998 · N184SK · Doug DC861F · Leading Edge Slat Position Indicating System
  > TRIP NR 1259, SLOT DISAGREEMENT LIGHT STAYED ON ON TAXI-OUT, RETURNED TO RAMP. ENTERED ON DMI 8052 CAT C, REMOVED AND REPLACED INBOARD RT SWITCH, OPS CHECKED NORMAL IAW M/M 27-52-3, CLEARED DMI8052.
- [SDR TC8A98002](https://openairdocs.org/sdr/TC8A98002.md): Compressor · stalled · Jan 21, 1998 · N184SK · Doug DC861F · Turbine Engine Compressor Section
  > NR 2 ENGINE COMPRESSOR STALLED ON TAKEOFF, ABORTED TAKEOFF. INSPECTED ENGINE IAW 72-00, PERFORM GROUND RUN IAW TCA MIP VOL 2, OPS CHECK NORMAL, NO STALLS NOTED.
- [SDR TC8A97040](https://openairdocs.org/sdr/TC8A97040.md): Oil Line · loose · Aug 5, 1997 · N184SK · Doug DC861F · Turbine Engine Oil System
  > DUE TO LOW OIL QUANTITY AND PRESSURE FLUCTUATION SHUT DOWN NR 1 ENGINE IN FLIGHT AT 15:45PER ABNORMAL CHECKLIST PAGE 3-122 (HALF GALLON AND BELOW 40 PSI). DUE TO LOW OIL QUANTITY AND PRESSURE FOUND RETURN LINE TO OIL TANK LOOSE. RESECURED LINE, FILLED OIL TA
- [SDR TC8A97033](https://openairdocs.org/sdr/TC8A97033.md): Hyd Press Trans · failed · Jul 11, 1997 · N184SK · Doug DC861F · Hydraulic Pressure Sensor
  > DURING THE TAXI CHECKLIST UNABLE TO VERIFY SPOILER DROP / RISE, NO DEFLECTION ON GAUGE. REMOVED AND REPLACED SPOILER PRESSURE TRANSMITTER IAW MM 29-30-3, OPS AND LEAK CHECKS OK.
- [SDR TC8A97024](https://openairdocs.org/sdr/TC8A97024.md): Starter · failed · May 9, 1997 · N184SK · Doug DC861F · Engine Starter
  > NR 4 ENGINE STARTER FAILED ON STARTUP. REMOVED AND REPLACED PNEUMATIC STARTER, ENGINE OPS CHECKS OK IAW MM 80-10-1.
- [SDR TC8A97018](https://openairdocs.org/sdr/TC8A97018.md): Actuator · leaking · Mar 13, 1997 · N184SK · Doug DC861F · Landing Gear Door Actuator
  > TNCC-KMIA, FLT 00024. DISCREP: UNSATISFACTORY UPLATCH CHECK OUT OF TNCC. ABNORMAL CH 3, P.111, CONTINUE FLIGHT NORMALLY. REMOVED AND REPLACED LT MAIN GEAR DOOR LEAKING ACTUATOR IAW MM 32-32-7, LEAK AND OPS CHECKS OK. PERFORMED LANDING GEAR RETRACTION/EXTE
- [SDR TC8A97014](https://openairdocs.org/sdr/TC8A97014.md): Engine · out of trim · Feb 9, 1997 · N184SK · Doug DC861F · Fuel Controlling System
  > NR 2 ENGINE WOULD NOT GO TO TAKEOFF POWER. RETURNED TO RAMP. TRIMMED NR 2 ENGINE, SYSTEM OPS GOOD ON RUN-UP IAW MM 76-10.
- [SDR TC8A97013](https://openairdocs.org/sdr/TC8A97013.md): Engine · out of trim · Feb 9, 1997 · N184SK · Doug DC861F · Fuel Controlling System
  > NR 1 ENGINE WOULD NOT GO TO TAKEOFF POWER, RETURNED TO RAMP. TRIMMED NR 1 ENGINE, SYSTEM OPS GOOD ON RUN-UP IAW MM 76-10.
- [SDR TC8A97009](https://openairdocs.org/sdr/TC8A97009.md): Compressor · stalled · Jan 17, 1997 · N184SK · Doug DC861F · Turbine Engine Compressor Section
  > NR 4 ENGINE COMPRESSOR STALLED WITHIN 3 TO 4 SECONDS AFTER FULL TAKEOFF POWER APPLIED, 1.87 EPR / 22 DEGREES CELCIUS TEMP / ALTIMETER 30.17 AT SEA LEVEL.
- [SDR TC8A97008](https://openairdocs.org/sdr/TC8A97008.md): Bleed Valve · failed · Jan 17, 1997 · N184SK · Doug DC861F · Compressor Bleed Valve
  > NR 4 ENGINE COMPRESSOR STALLED WITHIN 3 TO 4 SECONDS AFTER FULL TAKEOFF POWER APPLIED, 1.87 EPR / 26 DEGREES CELSIUS TEMP / ALTIMETER 30.01 AT SEA LEVEL. REMOVED AND REPLACED NR 4 ENGINE SURGE BLEED VALVE AS PERMM 75-30-3, OPS CHECKS NORMAL ON ENGINE RUN-UP.
- [SDR TC8A97007](https://openairdocs.org/sdr/TC8A97007.md): Compressor · stalled · Jan 17, 1997 · N184SK · Doug DC861F · Turbine Engine Compressor Section
  > NR 4 ENGINE COMPRESSOR STALLED WITHIN 3 TO 4 SECONDS AFTER FULL TAKEOFF POWER APPLIED, 1.87 EPR / 21 DEGREES CELCIUS TEMP / ALTIMETER 30.1 AT SEA LEVEL. SECURED LOOSE SENSE LINE AT PRBC, PERFORMED GROUND RUN AT 1.87EPR, GROUND OPS CHECKS GOOD IAW DC8 M/M 71-0
- [SDR TC8A97003](https://openairdocs.org/sdr/TC8A97003.md): Circuit Breaker · tripped · Jan 15, 1997 · N184SK · Doug DC861F · Fuel Boost Pump
  > KMIA - FLT NR 01501. ON PUSHBACK, NR 4 MAIN FUEL PUMP BREAKERS (3) POPPED. CORRECTIVE ACTION: SUMPED TANK AND CLEANED BOOST AND FEED PUMP, SYSTEM CHECKS NORMAL PER MM, CH. 28.
- [SDR TC8A97002](https://openairdocs.org/sdr/TC8A97002.md): Smoke Detector · malfunctioned · Jan 15, 1997 · N184SK · Doug DC861F · Smoke Detection
  > ON PUSHBACK, CARGO SMOKE DETECTOR LIGHT ILLUMINATED. REPAIRED NR 2 SMOKE DETECTOR, SYSTEM OPS CHECKS NORMAL IAW MM 26.
- [SDR TC8A97001](https://openairdocs.org/sdr/TC8A97001.md): Crossfeed Valve · malfunctioned · Jan 15, 1997 · N184SK · Doug DC861F · Pneumatic Distribution System
  > PNEUMATIC CROSSFEED VALVE WON'T OPEN. REMOVED AND REPLACED CROSS FEED VALVE, SYSTEM OPS CHECKS GOOD IAW MM 36.

## 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 = 'N184SK' AND deregistration_id = 'N184SK-2006-09-18'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N184SK-2006-09-18/reports

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