# Service difficulty reports: N8974U, cancelled Jul 11, 2005

A list on [N8974U, cancelled Jul 11, 2005](https://openairdocs.org/deregistered/N8974U-2005-07-11.md).

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

- [SDR ARWA20040105](https://openairdocs.org/sdr/ARWA20040105.md): Attach Fitting · loose · Jan 30, 2004 · N8974U · Doug DC862 · Elevator Miscellaneous Structure
  > DURING PREFLIGHT FOUND ELEVATOR STARBOARD SIDE UP SLIGHTLY AND PORT SIDE SLIGHTLY DOWN, SLIGHT DIFFERENCE IN TRAVEL BETWEEN PORT AND STARBOARD SIDE ELEVATORS. FOUND LOOSE ATTACHMENT AT PORT SIDE ELEVATOR ATTACHMENT TO TORQUE TUBE. PERFORMED ELEVATOR INSPECTI
- [SDR ARWA20030702](https://openairdocs.org/sdr/ARWA20030702.md): Skin · cracked · Jul 7, 2003 · N8974U · Doug DC862 · Fuselage Main, Plate/Skin
  > NR 34M. DURING "A" CHECK NON-ROUTINE INSPECTION, THE FOLLOWING WAS FOUND- NLG WW LT SIDE, STA. 208 L-33L CORNER WITH.2500 INCH CRACK. TRIMMED OUT CRACK ON EDGE OF NOSE SKIN AT NOSE LANDING GEAR DOOR LEFT AFT CORNER AND FABRICATED FILLER FROM 707STG.O50 AND
- [SDR ARWA20030206](https://openairdocs.org/sdr/ARWA20030206.md): Line · leaking · Feb 16, 2003 · N8974U · Doug DC862 · Hydraulic System, Main
  > IN FLIGHT ABOUT ONE HOUR OUT OF VTBU AFTER TAKE-OFF AIRCRAFT WAS LOSING HYDRAULIC FLUID. DID IN-FLIGHT TURNBACK, DUMPED FUEL AND LANDED BACK AT VTBU. RAN ALL APPROPIATE CHECK LISTS. FOUND NR 3 ENGINE HYDRAULIC PUMP SUPPLY LINE LEAKING. REMOVED AND REPLACE
- [SDR ARWA20021205](https://openairdocs.org/sdr/ARWA20021205.md): O-Ring · leaking · Dec 14, 2002 · N8974U · Doug DC862 · Hydraulic System, Main
  > ON FINAL APPROACH LOSS OF HYDRAULIC FLUID TO THE STAND PIPE. FOUND EMPENNAGE FILTER BOWL LEAKING AT MAGNETIC PLUG. REMOVED AND REPLACED O-RING LEAK CHECK NORMAL IAW MM.
- [SDR IXXA0000021](https://openairdocs.org/sdr/IXXA0000021.md): Seal · leaking · Jun 8, 2000 · N8974U · Doug DC862 · Cabin Compressor System
  > EN ROUTE FROM QPG TO OKO, WHEN THE FLIGHT CREW TURNED ON THE NUMBER ONE TURBO COMPRESSOR A SQUEAL WAS HEARD AND AN ODOR WAS SENSED IN THE COCKPIT. THE FLIGHT CREW SECURED THE TURBO COMPRESSOR, THE ODOR SUBSIDED. THE FLIGHT CONTINUED TO OKO FOR AN UNEVENTFUL
- [SDR IXXA0000018](https://openairdocs.org/sdr/IXXA0000018.md): Line · defective · May 3, 2000 · N8974U · Doug DC862F · Hydraulic System, Main
  > EN ROUTE FROM KWI TO HIK, THE FLIGHT CREW NOTICED THE MAIN HYDRAULIC SYSTEM FLUID QUANTITY DECLINING. THE FLIGHT CREW FOLLOWED COMPANY EMERGENCY PROCEDURES, DECLAIRED AN EMERGENCY, AND CONTINUED TO HIK FOR AN UNEVENFUL LANDING. MAINTENANCE INSPECTED THE AIRC
- [SDR IXXA0000013](https://openairdocs.org/sdr/IXXA0000013.md): Uplock · malfunctioned · Mar 29, 2000 · N8974U · Doug DC862 · Landing Gear Position and Warning
  > HIK - FLT JZ43 - EN ROUTE TO KWA, THE LANDING GEAR FAILED THE GEAR UPLATCH CHECK, ACCOMPANIED BY GEAR AND DOOR WARNING LIGHTS ILLUMINATING. THE FLIGHT CREW CYCLED THE GEAR BUT THE WARNING INDICATION REMAINED THE SAME. THE FLIGHT RETURNED TO HIK FOR AN UNEVEN
- [SDR IXXA9800058](https://openairdocs.org/sdr/IXXA9800058.md): Pumps · defective · Jun 21, 1998 · N8974U · Doug DC862 · Hydraulic Pump (Electric/Engine), Main
  > EN ROUTE, THE MAIN HYDRAULIC SYSTEM FAILED AND HYDRAULIC PRESSURE DROPPED TO ZERO. THE FLIGHT CONTROL MANUAL REVERSION LIGHTS ILLUMINATED CONFIRMING THE FAILURE. THE FLIGHT WAS DIVERTED TO DNA FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT AN
- [SDR IXXA9700119](https://openairdocs.org/sdr/IXXA9700119.md): Actuator · failed · Aug 13, 1997 · N8974U · Doug DC862 · Landing Gear Actuator
  > AFTER TAKEOFF UPON GEAR RETRACTION, THE DOORS LIGHT REMAINED ILLUMININATED AFTER THE UPLATCH CHECK. THE GEAR WAS RECYCLED SEVERAL TIMES WITH NO CHANGE IN WARNING STATUS. THE FLIGHT RETURNED TO HIK. MAINTENANCE REPLACED THE MAIN GEAR CONTROL VALVE, THE HYDRA
- [SDR 96ZZZM272](https://openairdocs.org/sdr/96ZZZM272.md): Unsafe Light · illuminated · Feb 11, 1996 · N8974U · Doug DC862 · Landing Gear Position and Warning
  > RIA FLT NR 7700 MIA - DOVER AIRCRAFT RETURNED TO MIA AFTER TAKEOFF WHEN MLG DOOR UNSAFE LIGHT ILLUMINATED. IN MIA, AIRCRAFT JACKED AND RIGGED LEFT DOOR ACTUATOR. OPS CHECK OK, AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR 96ZZZX905](https://openairdocs.org/sdr/96ZZZX905.md): Skin · corroded · Feb 5, 1996 · N8974U · Doug DC862 · Fuselage Main, Plate/Skin
  > LEVEL 2 CORROSION/AFT CARGO COMPARTMENT LOWER AREA, STR 34R BETWEEN STA 1220 AND STA 1240, FUSELAGE SKIN HAS CORROSION. REMOVED DAMAGED AREA, FABRICATED, AND INSTALLED REPAIR PER SRM 51-1-0. (X)
- [SDR 96ZZZX904](https://openairdocs.org/sdr/96ZZZX904.md): Doubler · corroded · Feb 5, 1996 · N8974U · Doug DC862 · Fuselage Miscellaneous Structure
  > LEVEL 2 CORROSION/AFT CARGO COMPARTMENT, STR 21R BETWEEN STA 1160 AND STA 1180, FLOOR SUPPORT HAS CORROSION. REMOVED DAMAGED AREA, FABRICATED, AND INSTALLED REPAIR PER RICH E.O. NR RCH D85310-6124. (X)
- [SDR 96ZZZX903](https://openairdocs.org/sdr/96ZZZX903.md): Doubler · corroded · Feb 5, 1996 · N8974U · Doug DC862 · Fuselage Miscellaneous Structure
  > LEVEL 2 CORROSION/AFT CARGO COMPARTMENT STR 21R BETWEEN STA 1160 AND STA 1180, FLOOR SUPPORT HAS CORROSION. REMOVED DAMAGED AREA, FABRICATED, AND INSTALLED REPAIR PER SRM 53-2-5. (X)
- [SDR 96ZZZX902](https://openairdocs.org/sdr/96ZZZX902.md): Doubler · corroded · Feb 5, 1996 · N8974U · Doug DC862 · Fuselage Miscellaneous Structure
  > LEVEL 2 CORROSION/AFT CARGO COMPARTMENT, LT SIDE STR 21L BETWEEN STA 1240 AND STA 1260, FUSELAGE SKIN HAS CORROSION. REMOVED DAMAGED AREA, FABRICATED, AND INSTALLED REPAIR PER RICH E.O. D85310-6124, REV 1.
- [SDR 96ZZZX901](https://openairdocs.org/sdr/96ZZZX901.md): Doubler · corroded · Feb 5, 1996 · N8974U · Doug DC862 · Fuselage Miscellaneous Structure
  > LEVEL 2 CORROSION/AFT CARGO COMPARTMENT, LT SIDE STR 21L, BETWEEN STA 1240 AND STA 1260, FLOOR SUPPORT CORRODED. REMOVED DAMAGED AREA, FABRICATED, AND INSTALLED REPAIR PER RICH DRAWING D85310-6124. (X)
- [SDR 96ZZZX900](https://openairdocs.org/sdr/96ZZZX900.md): Skin · corroded · Feb 5, 1996 · N8974U · Doug DC862 · Fuselage Main, Plate/Skin
  > LEVEL 2 CORROSION/LOWER FUSELAGE IS BULGED WITH CORROSION AT FS 540R BETWEEN LONGERONS 35R AND 34R BELOW FORWARD CARGO DOOR SILL PLATE. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 52-2-1.
- [SDR 96ZZZX899](https://openairdocs.org/sdr/96ZZZX899.md): Skin · corroded · Feb 5, 1996 · N8974U · Doug DC862 · Fuselage Main, Plate/Skin
  > LEVEL 2 CORROSION/2 SMALL SKIN BULGES JUST AFT OF NR 4 PIT DOOR FS 1290, STR 28R. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 53-2-1.
- [SDR 96ZZZW49](https://openairdocs.org/sdr/96ZZZW49.md): Skin · corroded · Feb 5, 1996 · N8974U · Doug DC862 · Fuselage Main, Plate/Skin
  > LEVEL 2 CORROSION, AFT CARGO COMPARTMENT LOWER AREA STRINGER 34R BETWEEN STA 1220 AND 1240 FUSELAGE SKIN HAS CORROSION. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 51-1-0.
- [SDR 96ZZZW48](https://openairdocs.org/sdr/96ZZZW48.md): Stringer · corroded · Feb 5, 1996 · N8974U · Doug DC862 · Fuselage Main, Longeron/Stringer
  > LEVEL 2 CORROSION, AFT CARGO COMPARTMENT STRINGER 21R BETWEEN STA 1160 AND 1180 FLOOR SUPPORT HAS CORROSION. REMOVED DAMAGED AREA FABRICATED AND INSTALLED REPAIR PER SMR 53-2-5.
- [SDR 96ZZZW47](https://openairdocs.org/sdr/96ZZZW47.md): Stringer · corroded · Feb 5, 1996 · N8974U · Doug DC862 · Fuselage Main, Longeron/Stringer
  > LEVEL 2 CORROSION, AFT CARGO COMPARTMENT LEFT SIDE STRINGER 21L BETWEEN STA 1240 AND 1260 FUSELAGE SKIN HAS CORROSION. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER RICH EO D85310-6124 REV 1.
- [SDR 96ZZZW46](https://openairdocs.org/sdr/96ZZZW46.md): Skin · corroded · Feb 5, 1996 · N8974U · Doug DC862 · Fuselage Main, Plate/Skin
  > LEVEL 2 CORROSION, LOWER FUSELAGE IS BULGED WITH CORROSION AT FS 540R BETWEEN LONGERONS 35R AND 34R BELOW FORWARD CARGO DOOR SILL PLATE. REMOVED DAMAGED AREA FABRICATED AND INSTALLED REPAIR PER SRM 52-2-1.
- [SDR 96ZZZW45](https://openairdocs.org/sdr/96ZZZW45.md): Skin · corroded · Feb 5, 1996 · N8974U · Doug DC862 · Fuselage Main, Plate/Skin
  > LEVEL 2 CORROSION, TWO SMALL SKIN BULGES JUST AFT OF NR 4 PIT DOOR FS 1290 STRINGER 28R. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 53-2-1.
- [SDR 95ZZZX6787](https://openairdocs.org/sdr/95ZZZX6787.md): Fire Loop · broken · Oct 31, 1995 · N8974U · Doug DC862 · Fire Detection
  > LICZ/ETAR - FLT BEHF800 - FIRE INDICATION DURING FLIGHT AT CRUISE ON NR 2 ENGINE. SHUT DOWN ENGINE, AND FIRED BOTH FIRE BOTTLES. AIRCRAFT LANDED WITHOUT INCIDENT. FOUND FIRE LOOP BROKEN AND SHORTED. REPLACED LOOP AND BOTH FIRE BOTTLES. SYSTEM OPERATED GOO

## 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 = 'N8974U' AND deregistration_id = 'N8974U-2005-07-11'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N8974U-2005-07-11/reports

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