# Service difficulty reports: N886US, cancelled Jun 19, 2013 A list on [N886US, cancelled Jun 19, 2013](https://openairdocs.org/deregistered/N886US-2013-06-19.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR USAAF01031](https://openairdocs.org/sdr/USAAF01031.md): Battery Pack · discharged · May 31, 2001 · N886US · Fokker F28MK0100 · Emergency Lighting > RDU - THE AFT CABIN AND LAVATORY EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY IN THE AFT EMERGENCY LIGHTS BATTERY PACK. OPS CHECKED OK. (M) - [SDR USAAF01025](https://openairdocs.org/sdr/USAAF01025.md): Battery Pack · corroded · May 15, 2001 · N886US · Fokker F28MK0100 · Emergency Lighting > RDU - THE AFT LAVATORY AREA EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE CLEANED CORROSION FROM BATTERY PACK CONTACTS IN NR 8 EMERGENCY POWER SUPPLY. OPERATIONALLY CHECKED OK. (M) - [SDR USAAF01012](https://openairdocs.org/sdr/USAAF01012.md): Wire · broken · Mar 26, 2001 · N886US · Fokker F28MK0100 · Light System Wiring > RDU - THE RIGHT SERVICE DOOR EXIT LIGHT WAS INOPERATIVE IN STANDBY AND EMEGENCY LIGHTING. MAINTENANCE REPAIRED TWO BROKEN WIRES ON THE BACK OF THE EXIT LIGHT ASSEMBLY. OPERATIONALLY CHECKED OK. (M) - [SDR USAAF00036](https://openairdocs.org/sdr/USAAF00036.md): Unknown · odor · May 8, 2000 · N886US · Fokker F28MK0100 · Air Distribution System > TYS-CLT - FLT 1731 - BURNING SMELL NOTED BY F/O, FLIGHT ATTENDANTS AND CAPTAIN DURING CLIMB-OUT. SMELL DIMINISHED CLIMBIN THROUGH 10,000, BUT STILL NOTICEABLE IN CRUISE FLIGHT. MAINTENANCE GROUND RAN ENGINES AT HIGH AND COULD NOT SMELL BURNING SMELL. GROUND - [SDR USAAF99041](https://openairdocs.org/sdr/USAAF99041.md): Battery Pack · discharged · Aug 23, 1999 · N886US · Fokker F28MK0100 · Emergency Lighting > CLT - FOUND THE NR 8 EMERGENCY BATTERY PACK INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. (M) - [SDR USAAF98071](https://openairdocs.org/sdr/USAAF98071.md): Warning System · activated · Aug 20, 1998 · N886US · Fokker F28MK0100 · Central Warning > PIT - FLT 274 - EN ROUTE LGA-SDF, CREW RECEIVED THREE CHIME WARNING FROM THE MFDU AND NOTED THAT THE CABIN ALTITUDE WAS CLIMBING THROUGH 10,000 FT. CREW PERFORMED AN EMERGENCY DESCENT. THE FLIGHT DIVERTED TO PIT AND LANDED WITH NO FURTHER INCIDENT. (M) - [SDR USAAF98065](https://openairdocs.org/sdr/USAAF98065.md): Detector · malfunctioned · Aug 4, 1998 · N886US · Fokker F28MK0100 · Fire Detection > TYS - FLT 1633 - ON APPROACH TO TYS DESCENDING THROUGH 4000 FEET, WHEN SPEEDBRAKES WERE DEPLOYED THE APU FIRE WARNING ANNUNCIATED. THE APU AUTOMATICALLY SHUT DOWN AND THE FIRE BOTTLE DISCHARGED. THE APU WAS BEING RUN BECAUSE THE NR 1 GENERATOR WAS ON MEL. F - [SDR 98ZZZM607](https://openairdocs.org/sdr/98ZZZM607.md): Gcu · failed · Aug 4, 1998 · N886US · Fokker F28MK0100 · AC Generation System > TYS - FLT 1633 - ON APPROACH TO TYS DESCENDING THROUGH 4000 FEET, WHEN SPEEDBRAKES WERE DEPLOYED THE APU FIRE WARNING ANNUNCIATED. THE APU AUTOMATICALLY SHUT DOWN AND THE FIRE BOTTLE DISCHARGED. THE APU WAS BEING RUN BECAUSE THE NR 1 GENERATOR WAS ON MEL. F - [SDR 98ZZZM606](https://openairdocs.org/sdr/98ZZZM606.md): Idg · failed · Aug 4, 1998 · N886US · Fokker F28MK0100 · AC Generator-Alternator > TYS - FLT 1633 - ON APPROACH TO TYS DESCENDING THROUGH 4000 FEET, WHEN SPEEDBRAKES WERE DEPLOYED THE APU FIRE WARNING ANNUNCIATED. THE APU AUTOMATICALLY SHUT DOWN AND THE FIRE BOTTLE DISCHARGED. THE APU WAS BEING RUN BECAUSE THE NR 1 GENERATOR WAS ON MEL. F - [SDR USAAF98034](https://openairdocs.org/sdr/USAAF98034.md): Controller · malfunctioned · Apr 1, 1998 · N886US · Fokker F28MK0100 · Cabin Pressure Controller > CLT - FLT 1079 - EN ROUTE FROM MDT TO CLT WHILE DESCENDING FROM 350 TO 310, AIRCRAFT EXPERIENCED A LOSS OF CABIN PRESSURE. A RAPID DESCENT TO 10,000 FEET WAS MADE. MASKS DID NOT DROP. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 1 AU - [SDR USAAF96043](https://openairdocs.org/sdr/USAAF96043.md): Flap Synchro · failed · May 13, 1996 · N886US · Fokker F28MK0100 · Trailing Edge Flap Control System > PIT - FL 8075 - DURING DESCENT INTO AVP, THE CREW COULD NOT GET THE FLAPS TO EXTEND. A DECISION WAS MADE TO DIVERT TO PIT WHERE MAINTENANCE IS AVAILABLE TO MAKE REPAIRS. THE CAPTAIN DECLARED AN EMERGENCY FOR PRECAUTIONARY MEASURES. THE FLIGHT LANDED WITHOUT - [SDR USAAF96004A](https://openairdocs.org/sdr/USAAF96004A.md): Harness · faulty · Jan 5, 1996 · N886US · Fokker F28MK0100 · Landing Gear Position and Warning > CLT - AFTER TAKEOFF, CREW RECEIVED GND/FLT FAULT, LIFT DUMPER FAULT, TCAS FAULT AND PROX SW SYS INOP. FLIGHT RETURNED TO CLT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT MAIN LANDING GEAR HARNESS AND THE SENSOR. (M) - [SDR USAAF96004](https://openairdocs.org/sdr/USAAF96004.md): Ground Sense · malfunctioned · Jan 5, 1996 · N886US · Fokker F28MK0100 · Landing Gear Position and Warning > FLT NR 1007 - CLT - THE FLIGHT RETURNED TO FIELD DUE TO A GROUND SENSE PROBLEM. (M) - [SDR USAAF96003A](https://openairdocs.org/sdr/USAAF96003A.md): Prox Sensor · out of adjust · Jan 5, 1996 · N886US · Fokker F28MK0100 · Landing Gear Position and Warning > FLT NR 1488 - RIC - SHORTLY AFTER GEAR RETRACTION THE FOLLOWING ALERTS, 'LD FAULT', 'STAB TRIM CONFIG' AND 'TCAS'. WHEN GEAR EXTENDED, LOUD RELAY CLICKING FOLLOWED BY ALL MESSAGES CLEARING. MAINTENANCE ADJUSTED THE LEFT MAIN GEAR NR 3 PROXIMITY SENSOR AND SW - [SDR USAAF95008](https://openairdocs.org/sdr/USAAF95008.md): Pack · failed · Dec 28, 1995 · N886US · Fokker F28MK0100 · Cabin Cooling System > FLT NR 689 - PIT - WHILE AT FL 350 THE AIRCRAFT PRESSURIZATION STARTED TO CLIMB TO 10K FEET. THE CAPTAIN REQUESTED DESCENT TO FL 100 AND RECEIVED SAME FROM ATC. THE FLT WAS DIVERTED TO PIT. NO EMERGENCY WAS DECLARED. THE FLT LANDED IN AT PIT WITH NO FURTHE - [SDR USAA950024](https://openairdocs.org/sdr/USAA950024.md): Nut · loose · Jan 19, 1995 · N886US · Fokker F28MK0100 · Hydraulic System, Main > PIT - FLT 1025 - AFTER TAKEOFF, THE CREW GOT A 'HYD SYS 2 LO QTY' ALERT. ACFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND PRESSURE LINE 'B' NUT ON UPPER PUMP LOOSE AT QUICK DISCONNECT. MAINTENANCE TIGHTENED FITTING. SERVICED, RAN ENGIN ## 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 = 'N886US' AND deregistration_id = 'N886US-2013-06-19' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N886US-2013-06-19/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.