# Service difficulty reports: N119AA, cancelled Jun 12, 2002

A list on [N119AA, cancelled Jun 12, 2002](https://openairdocs.org/deregistered/N119AA-2002-06-12.md).

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

- [SDR HALA0000007](https://openairdocs.org/sdr/HALA0000007.md): Warning Light · illuminated · Jan 3, 2000 · N119AA · Doug DC1010 · Leading Edge Slat Position Indicating System
  > HNL - FLT 931 - SLAT DISAGREE LIGHT ILLUMINATED INTERMITTENTLY DURING CRUISE AT FL 350 MACH.82 MINUS 57 DEGREES CELSIUS. CONTINUITY CHECK SLATS SENSOR, NO DEFECTS NOTED, CHECK SLAT HANDLE SWITCH, NO DEFECTS NOTED, CHECKED SLAT PROXIMITY SWITCHES, NO DEFECTS
- [SDR HALA9900235](https://openairdocs.org/sdr/HALA9900235.md): Engine · vibration · Nov 19, 1999 · N119AA · Doug DC1010 · Engine (Turbine/Turboprop)
  > NR 1 ENGINE IN CRUISE FL360, 1 HOUR OUT OF LAX HAD NOTICEABLE VIBRATION ABOVE 88.9 PCT, N2 94.0 PCT, NR 1 CSD TEMP 30 DEGREES CELSIUS RISE 60 DEGREES CELSIUS BELOW 89 PCT N2 VIBRATION WAS LESS FELT IN AIRFRAME AND N1 FUEL LEVER. REPLACED ENGINE PER MCM SECT 1
- [SDR HALA9900202](https://openairdocs.org/sdr/HALA9900202.md): Coalescer Bags · dirty · Oct 19, 1999 · N119AA · Doug DC1010 · Humidity Control System
  > FLT 2 - HNL - STRONG ODOR IN CABIN SERVICE AREA MOSTLY BURNING OIL SMELL, BUT ALSO LIGHT PLASTIC SMELL. REMOVED AND REPLACED ALL 3 WATER SEPARATOR SOCKS. PURGED AIR CONDITION SYSTEM PER TAFI 21-50-00 PAGE 120. OPS CHECK OK. (M)
- [SDR HALA9900108](https://openairdocs.org/sdr/HALA9900108.md): Splice · failed · May 3, 1999 · N119AA · Doug DC1010 · Emergency Lighting
  > IN FLIGHT, DOOR 1L, 2L, 3L, EMERGENCY LIGHTS DIMLY AND INTERMITTENTLY ILLUMINATED. OCCASSIONALLY BRIGHT. SEAT LIGHT ON LEFT AND RIGHT SIDE OF LEFT AISLE IN 'A' AND 'B' CABINS ALSO. REPAIRED EMERGENCY LIGHT WIRE AT SEAT 1B. OPERATIONAL CHECK OK. (M)
- [SDR HALA9800410](https://openairdocs.org/sdr/HALA9800410.md): Engine · failed · Dec 16, 1998 · N119AA · Doug DC1010 · Engine (Turbine/Turboprop)
  > FLT 21 - SEA - NR 2 ENGINE FAILURE ON TAKEOFF ROLL. N1 STARTED DECREASING AND EGT STARTED INCREASING IMMEDIATELY AFTER POWER SET FOR TAKEOFF. EGT INCREASED TO 925 AND ANOTHER AIRCRAFT REPORTED FLAMES EXITING TAILCONE. REPLACED NR 2 ENGINE PER MCM DR719401.
- [SDR HALA9800375](https://openairdocs.org/sdr/HALA9800375.md): Light · inoperative · Nov 3, 1998 · N119AA · Doug DC1010 · Flight Compartment Lighting
  > LAS - FLT 935 - NR 3 FUEL LEVER LIGHT WON'T TEST. NR 2 FUEL LEVER AND FIRE T-HANDLE LIGHT DON'T ILLUMINATE DURING FIRE WARNING TEST. REPLACED NR 3 ENGINE FUEL SHUT OFF LIGHT ASSY. OPS CHECK OK. REPLACED NR 2 FUEL SHUT OFF HANDLE, LIGHT ASSY AND CONTROLLER,
- [SDR HALA9800099](https://openairdocs.org/sdr/HALA9800099.md): Control Valve · malfunctioned · Apr 22, 1998 · N119AA · Doug DC1010 · Trailing Edge Flap Control System
  > LAS - FLT 03 - LOG PAGE 4091834 - WHILE TURNING ONTO RUNWAY FOR DEPARTURE, SELECTED FLAPS AT 10 DEGREES. SHORTLY AFTER FLAPS AND INDICATOR REACHED 10 DEGREES, THE FLAP INDICATORS INDICATED THAT FLAPS WERE STILL CREEPING DOWN. RAN FLAP FULL DOWN THEN UP AND T
- [SDR HALA9800080](https://openairdocs.org/sdr/HALA9800080.md): Control Box · failed · Apr 1, 1998 · N119AA · Doug DC1010 · Emergency Lighting
  > HNL - FLT 10 - EMERGENCY LIGHT TEST INOP (GREEN LT) AND 2L AND 4L FAULT LIGHT CAME ON DURING TEST. REPLACED EMERGENCY LIGHT CONTROL BOX ON 2L AND 4L DOOR, OPS CHECK GOOD. (M)
- [SDR HALA9800018](https://openairdocs.org/sdr/HALA9800018.md): Npu · failed · Jan 19, 1998 · N119AA · Doug DC1010 · Visual Omnirange (VOR) System
  > FLT 26 - HNL - NAV UNREADABLE, BOTH HSI AND RMI HEADINGS WERE DIFFERENT IN NAV POSITION UP TO 50 DEGREES AT ONE POINT. HSI COURSE INDICATORS DID NOT AGREE WITH LEGS PAGE COURSE. NR 1 WENT TO VERIFY POSITION, NR 2 WENT TO DR. POSITION CHECKED OK FOR BOTH. A/
- [SDR HALA9800006](https://openairdocs.org/sdr/HALA9800006.md): Fitting · loose · Jan 8, 1998 · N119AA · Doug DC1010 · Pitot/Static System
  > PDX - FLT 25 - ON TAKEOFF ROLL, CAPTAIN HAD NO AIRSPEED IND, F/O AIRSPEED READ 115 KTS, DID HIGH SPEED ABORT. LEAK TESTED CAPT PITOT/STATIC SYSTEM. FOUND LEAK AT NR 1 ADC QUICK DISCONNECT FITTING. RE-SEATED FITTING. SYSTEM LEAK CHECKS OK. BITE CHECK NR 1
- [SDR HALA9700316](https://openairdocs.org/sdr/HALA9700316.md): Rccb · failed · Dec 19, 1997 · N119AA · Doug DC1010 · DC Generating System
  > HNL - FLT NR 4 - IN CRUISE FLIGHT, NR 1 GEN OFF LIGHT CAME ON. VOLT/FREQENCY ZERO. FOLLOWED ABNORMAL PROCEDURES AND RESET NR 1 GEN. VOLT/FREQS OK. 4 MINUTES LATER NR 1 GEN DROPPED OFF LINE AGAIN. FOUND NR 1 DC BUS TIE RCCB CLOSED, REPLACED RCCB AND NR 1
- [SDR HALA9700315](https://openairdocs.org/sdr/HALA9700315.md): Csd · failed · Dec 19, 1997 · N119AA · Doug DC1010 · Alternator-Generator Drive
  > FLT 4 - HNL - ON CLIMB-OUT, AC BUS TIE NR 3 ISOL LIGHT CAME ON. CHECKED FREQ AT 392. NR 3 WOULD NOT PARALLEL. AIRCRAFT RETURNED TO HNL, WHERE A UNEVENTFUL LANDING WAS MADE. ADJUSTED CSD, FREQS TO 400HZ. GROUND RUN CHECKED NORMAL. (M)
- [SDR 98ZZZM145](https://openairdocs.org/sdr/98ZZZM145.md): Ecu · failed · Dec 19, 1997 · N119AA · Doug DC1010 · DC Generator-Alternator
  > HNL - FLT NR 4 - IN CRUISE FLIGHT, NR 1 GEN OFF LIGHT CAME ON. VOLT/FREQENCY ZERO. FOLLOWED ABNORMAL PROCEDURES AND RESET NR 1 GEN. VOLT/FREQS OK. 4 MINUTES LATER NR 1 GEN DROPPED OFF LINE AGAIN. FOUND NR 1 DC BUS TIE RCCB CLOSED, REPLACED RCCB AND NR 1
- [SDR HALA9700231](https://openairdocs.org/sdr/HALA9700231.md): Fitting · cracked · Nov 19, 1997 · N119AA · Doug DC1010 · Horizontal Stabilizer, Attach Fittings
  > DURING B-CHECK IN LAX, A CRACK WAS FOUND ON THE HORIZONTAL STAB UPPER RIGHT AFT FITTING, APPROX 2 INCHES INBOARD OF ATTACH BOLTS. HORIZONTAL STABILIZER UPPER LEFT AFT ATTACH FITTING CRACKED 4.75 INCH INBOARD OF ATTACH BOLTS. (M)
- [SDR HALA96163](https://openairdocs.org/sdr/HALA96163.md): Cadc · malfunctioned · Nov 21, 1996 · N119AA · Doug DC1010 · Air Data Computer
  > SEA - FLT 2025 - OVERSPEED WARNING ON TAKEOFF AT 90 KNOTS. ABORTED TAKEOFF. NO STICK SHAKER. PERFORMED AURAL WARNING CHECKS PER TAFI 31-51-00 PAGE 105. PERFORMED PITOT STATIC CHECKS. ALL SYSTEM CHECK NORMAL. REPLACED NR 1 CADC AS A PRECAUTIONARY. (M)
- [SDR HALA96129](https://openairdocs.org/sdr/HALA96129.md): Control Module · malfunctioned · Sep 3, 1996 · N119AA · Doug DC1010 · Emergency Lighting
  > HNL - FLT 21 - FOUND EMERGENCY FLOOR LIGHTS, CABIN C, RIGHT SIDE CAME ON DURING FLIGHT. REPLACED THR NR 1 CONTROL MODULE AND THE OPERATIONAL CEHCK WAS OK. (M)
- [SDR HAL9639](https://openairdocs.org/sdr/HAL9639.md): Battery Pack · discharged · Apr 11, 1996 · N119AA · Doug DC1010 · Emergency Lighting
  > HNL - FLT 10 - ON PRE-FLIGHT IN HNL, FOUND AFT POWER PACK OF EMERGENCY LIGHTING SYSTEM INOPERATIVE. REPLACED POWER PACK. OPS CHECK OK. (X)
- [SDR HALA95161](https://openairdocs.org/sdr/HALA95161.md): Connectors · dirty · Nov 23, 1995 · N119AA · Doug DC1010 · Fire Detection
  > HNL - FLT NR 25 - NR 1 FUEL LEVER, FIRE HANDLE AND A-LOOP LIGHT FLICKERED INTERMITTENTLY ON DESCENT WITH ENGINES AT IDLE. NO AURAL WARNING. MOVED NR 1 THROTTLE SLIGHTLY FORWARD AND INDICATION WENT AWAY. OTHERWISE, FOLLOWED H.A. S.O.P. AFTER LANDING ON TAXI
- [SDR HAL95092](https://openairdocs.org/sdr/HAL95092.md): Fire Loop · chafed · Jul 6, 1995 · N119AA · Doug DC1010 · Fire Detection
  > LAX - INFORMATION FROM LOG PAGE 142093. DURING ENGINE NR 1 LOOP, 'B' FLICKERED ON OVER A ONE MINUTE PERIOD. ACCOMPLISHED ABNORMAL PROCEDURE 1 IN FIRE PROTECTION SECTION OF FCOM. WITH ENGINE 1 LOOPS SWITCH SELECTED TO 'A' LOOP, A SATISFACTORY LOOPS 'A' TEST

## 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 = 'N119AA' AND deregistration_id = 'N119AA-2002-06-12'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N119AA-2002-06-12/reports

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