# Service difficulty reports: N887US, cancelled Aug 2, 2004

A list on [N887US, cancelled Aug 2, 2004](https://openairdocs.org/deregistered/N887US-2004-08-02.md).

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

- [SDR USAAF01033](https://openairdocs.org/sdr/USAAF01033.md): Coalescer Bag · contaminated · Jun 15, 2001 · N887US · Fokker F28MK0100 · Humidity Control System
  > TRI-CLT - FLT 242 - THE AIRCONDITIONING PACKS PRODUCED AN ODOR DURING CRUISE AND WOULD NOT COOL THE CABIN. THE FLIGHT CONTINUED AND LANDED IN CLT WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT WATER SEPARATOR BAG AND REPAIRED A LEAK AT THE DUCT ON
- [SDR USAA010588](https://openairdocs.org/sdr/USAA010588.md): Frame · cracked · May 19, 2001 · N887US · Fokker F28MK0100 · Fuselage Structure (General)
  > PIT - FOUND FRAME CRACKED 1.25 INCH, LEFT SIDE TOP OF OBLIQUE FRAME 67.2. TEMPORARY REPAIR WITH STOP DRILL PER EA 71082 AND SRM 51-22-01. (M)
- [SDR USAAF01016](https://openairdocs.org/sdr/USAAF01016.md): Wire · damaged · Apr 25, 2001 · N887US · Fokker F28MK0100 · Light System Wiring
  > IND- A SECTION OF FLOOR ESCAPE LIGHTING WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED WIRING TO LIGHT STRIP. OPS CHECKED OK. (M)
- [SDR USAAF01005](https://openairdocs.org/sdr/USAAF01005.md): Actuator · broken · Jan 31, 2001 · N887US · Fokker F28MK0100 · Landing Gear Door Actuator
  > PHL-SYR - FLT 768 - AFTER GEAR UP WAS SELECTED, A LOUD FLUTTERING NOISE WAS PRESENT WITH A NOSE LANDING GEAR INDICATION LIGHT. THE FLIGHT RETURNED TO PHL AND MADE A NORMAL LANDING. MAINTENANCE REPLACED THE NOSE LANDING GEAR DOOR ACTUATOR. OPERATIONALLY CHEC
- [SDR USAAF99059](https://openairdocs.org/sdr/USAAF99059.md): Switch · out of position · Dec 31, 1999 · N887US · Fokker F28MK0100 · Aircraft Fuel Distribution System
  > CLT-IAH - FLT 463 - DURNG CLIMB-OUT FROM CLT, CAPTAIN RECEIVED AUTO FUEL CROSSFEED FAIL ALERT. ALSO, CLT TOWER ADVISED THAT THERE WAS SUBSTANTIAL FUEL ESCAPING FROM WINGS. SEVERAL TURNS WERE MADE TO BURN FUEL TO REACH LESS THAN MAXIMUM LANDING WEIGHT. FLIGH
- [SDR USAAF99039](https://openairdocs.org/sdr/USAAF99039.md): Battery Pack · discharged · Aug 3, 1999 · N887US · Fokker F28MK0100 · Emergency Lighting
  > IND - FOUND FORWARD EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. (M)
- [SDR USAAF98097](https://openairdocs.org/sdr/USAAF98097.md): Trim System · malfunctioned · Dec 18, 1998 · N887US · Fokker F28MK0100 · Stabilizer Control System
  > CLT - FLT 2208 - ON CLIMB-OUT FROM CLT, CREW RECEIVED A DOUBLER STAB TRIM FAULT INDICATION. FLIGHT RETURNED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE RESET THE STAB TRIM SYSTEM. ALL MAINTENANCE BITE TESTS PASSED. AIRCRAFT WAS RETURNED TO SERV
- [SDR USAAF98062](https://openairdocs.org/sdr/USAAF98062.md): Control Box · failed · Jul 26, 1998 · N887US · Fokker F28MK0100 · Brake Anti-Skid Section
  > CLT - FLT 476 - AFTER TAKEOFF FROM CLT, WHEN LANDING GEAR WAS RETRACTED, 'ANTI-SKID' FAULT MESSAGE APPEARED. FLIGHT RETUREND TO CLT. MESSAGE REMAINED ON UNTIL LANDING GEAR WAS EXTENDED THEN MESSAGE EXTINGUISHED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAIN
- [SDR USAAF98032](https://openairdocs.org/sdr/USAAF98032.md): Downlock Pin · not engaged · Mar 25, 1998 · N887US · Fokker F28MK0100 · Landing Gear Retraction/Extension System
  > PWM - FLT 1824 - ON APPROACH, NOSE GEAR WAS SHOWING AN UNSAFE NOSE LIGHT. AIRCRAFT DID A GO-AROUND. CAPTAIN DECIDED TO FREE FALL THE NOSE GEAR AND GOT A GREEN LIGHT. AN EMERGENCY WAS DECLARED AND CABIN WAS PREPARED FOR AN EMERGENCY LANDING. FLIGHT HAD NO P
- [SDR USAAF98025](https://openairdocs.org/sdr/USAAF98025.md): Switch · failed · Mar 4, 1998 · N887US · Fokker F28MK0100 · Airfoil Anti/De-ice System
  > CLT - FLT 1210 - ON CLIMB-OUT OF CLT AIRCRAFT HAD A WING ANTI-ICE FAULT TWICE BETWEEN 9000 FEET - 11,000 FEET. FLIGHT RETURNED TO CLT WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED WING ANTI-ICE SWITCH IN OVERHEAD PANEL. PERFORMED OPERATIO
- [SDR USAA980051](https://openairdocs.org/sdr/USAA980051.md): Skin · delaminated · Mar 1, 1998 · N887US · Fokker F28MK0100 · Fuselage Main, Plate/Skin
  > PIT - DURING Q-1 CHECK, FOUND RT SKIN DELAMINATION AND SIGNS OF DISCOLORATION BETWEEN FRAMES 23011 AND 24611 AT STRINGER 53. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER REPAIR 12 INCH BY 8 INCH PER US AIRWAYS EA 29352A. (M)
- [SDR USAAF97097](https://openairdocs.org/sdr/USAAF97097.md): Engine · vibration · Nov 25, 1997 · N887US · Fokker F28MK0100 · Engine (Turbine/Turboprop)
  > IND - FLT 1057 - EN ROUTE, CREW EXPERIENCED HIGH VIBRATION ON THE LEFT ENGINE. CREW WAS ABLE TO CONTROL THE VIBRATION BY REDUCING THE ENGINE EPR. VIBRATION RETURNED DURING DESCENT. FLIGHT DIVERTED TO IND AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE CHE
- [SDR USAAF97066](https://openairdocs.org/sdr/USAAF97066.md): Thrust Plate · dirty · Jul 27, 1997 · N887US · Fokker F28MK0100 · Landing Gear Retraction/Extension System
  > PHL/ROC - FLT 504 - ON APPROACH TO ROC WHEN THE LANDING GEAR WAS EXTENDED, A 'NOSE GEAR UNSAFE' WARNING ILLUMINATED ALONG WITH NO ILLUMINATION OF GREEN 'NOSE GEAR' DOWN AND LOCKED INDICATOR. CREW PERFORMED A GO-AROUND PROCEDURE AND CYCLED THE LANDING GEAR. W
- [SDR USAAF97046](https://openairdocs.org/sdr/USAAF97046.md): Bulb · failed · May 13, 1997 · N887US · Fokker F28MK0100 · Landing Gear Position and Warning
  > FLT 2228 - DCA-CLT - ON APPROACH TO CLT, DID NOT RECEIVE A GREEN DOWN AND LOCKED INDICATION FOR THE RIGHT MAIN GEAR. CAPTAIN ELECTED TO PERFORM A GO AROUND PROCEDURE. CREW DETERMINED THAT THE LAMP WAS BURNED OUT IN THE INDICATOR. FLT LANDED AT CLT WITHOUT I
- [SDR USAAF97031](https://openairdocs.org/sdr/USAAF97031.md): Fire Warning · activated · Mar 15, 1997 · N887US · Fokker F28MK0100 · Fire Detection
  > ERI - FL 1202 - ON APPROACH, WITH APU RUNNING, CREW RECEIVED APU FIRE WARNING. APU PERFORMED AUTO SHUT DOWN, AND THE FIRE BOTTLE DISCHARGED. FLIGHT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND NO EVIDENCE OF A FIRE. THE EXHAUST DUCTING, BLEED/LOAD CO
- [SDR USAAF97015](https://openairdocs.org/sdr/USAAF97015.md): Sequence Valve · failed · Jan 13, 1997 · N887US · Fokker F28MK0100 · Landing Gear Retraction/Extension System
  > FLT 1239 - PIT-DAY - ON APPROACH TO DAY THE NOSE GEAR DID NOT EXTEND ON THE FIRST TRY. PILOT RECYCLED TEH GEAR AND ALL INDICATIONS WERE NORMAL ON THE SECOND TRY. FLIGHT LANDED AT DAY WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NOSE GEAR SEQUENCE VALV
- [SDR USAAF97014](https://openairdocs.org/sdr/USAAF97014.md): Retract Mech · lack of lube · Jan 10, 1997 · N887US · Fokker F28MK0100 · Landing Gear Retraction/Extension System
  > FLT 466 - GSP-PHL - ON APPROACH TO PHL, THE NOSE GEAR DID NOT EXTEND ON THE FIRST TRY. PILOT ACCOMPLISHED ABNORMAL CHECKLIST ITEMS AND RECYCLED GEAR. THE SECOND EXTENSION WAS NORMAL. FLIGHT LANDED IN PHL WITHOUT FURTHER INCIDENT. MAINTENANCE BITE CHECKED S
- [SDR USAAF96130](https://openairdocs.org/sdr/USAAF96130.md): Retract Mech · lack of lube · Dec 21, 1996 · N887US · Fokker F28MK0100 · Landing Gear Retraction/Extension System
  > FLT 1475 - PHL-DTW - ON DESCENT INTO DTW RECEIVED AN UNSAFE GEAR INDICATION WARNING AT FL 010. NOSE GEAR DID NOT COME DOWN. CREW DID A GO AROUND AND RECYCLED THE GEAR. LANDING GEAR OPERATED NORMALLY AFTER RECYCLE. NO EMERGENCY DECLARED AND FLIGHT LANDED WI
- [SDR USAAF96107](https://openairdocs.org/sdr/USAAF96107.md): Diode · overheated · Sep 21, 1996 · N887US · Fokker F28MK0100 · DC Power Distribution System
  > FLT 1206 - RDU-PIT, AT 50S OF PIT, CRWE GOT 'EMERGENCY DC BUS FAILED' ON MFDU. COMMUNICATINOS WERE LOST WITH ZOB AND PIT APPROACH. AIRCRAFT SHED SOME ELECTRICAL LOAD AND COMMUNICATION WAS RE-ESTABLISHED. AN EMERGENCY WAS DECLARED AND FLIGHT LANDED WITHOUT I
- [SDR USAAF96082](https://openairdocs.org/sdr/USAAF96082.md): Flex Duct · leaking · Aug 1, 1996 · N887US · Fokker F28MK0100 · APU Bleed Air System
  > GRR - FL 862 - UPON DESCENT INTO GRR, CREW RECEIVED APU FIRE WARNING. APU WAS AUTOMATICALLY SHUT DOWN AND THE FIRE BOTTLE DISCHARGED. FLIGHT CONTINUED TO GRR AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND NO EVIDENCE OF A FIRE. A BLEED AIR LEAK WAS

## 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 = 'N887US' AND deregistration_id = 'N887US-2004-08-02'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N887US-2004-08-02/reports

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