# Service difficulty reports: N865US, cancelled Oct 7, 2003 A list on [N865US, cancelled Oct 7, 2003](https://openairdocs.org/deregistered/N865US-2003-10-07.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR USAAF01081](https://openairdocs.org/sdr/USAAF01081.md): Battery · discharged · Nov 4, 2001 · N865US · Fokker F28MK0100 · Emergency Lighting > CLT - THE EMERGENCY FLOOR LIGHTS AT SEAT ROWS 4 TO 8 WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. (M) - [SDR USAAF01043](https://openairdocs.org/sdr/USAAF01043.md): Battery Pack · faulty · Jul 8, 2001 · N865US · Fokker F28MK0100 · Emergency Lighting > GSO - SEVERAL EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED A BATTERY PACK. OPERATIONALLY CHECKED OK. (M) - [SDR USAAF01022](https://openairdocs.org/sdr/USAAF01022.md): Landing Gear · lack of lube · May 10, 2001 · N865US · Fokker F28MK0100 · Landing Gear Retraction/Extension System > PIT-SBN - FLT 1152 - ON APPROACH INTO SBN, THE NOSE LANDING GEAR DID NOT INDICATE DOWN. A GO AROUND WAS MADE WITH THE GEAR BEING CYCLED. THE GEAR WAS LOWERED AGAIN, AND THIS TIME RECEIVED AN ALL GREEN INDICATION. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAI - [SDR USAAF00056](https://openairdocs.org/sdr/USAAF00056.md): Coalescer Bag · contaminated · Aug 4, 2000 · N865US · Fokker F28MK0100 · Humidity Control System > ORF-LGA - FLT 739 - AT TAKEOFF PLUS 30 MINUTES, HAD A STRONG, BURNING WIRES ODOR IN COCKPIT. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED COALESCER BAGS. OPS CHECKED OK. (M) - [SDR USAAF99031](https://openairdocs.org/sdr/USAAF99031.md): Valve · failed · Jun 4, 1999 · N865US · Fokker F28MK0100 · Landing Gear Retraction/Extension System > BOS - FLT 1010 - ON APPROACH TO MHT, CREW SELECTED GEAR DOWN. AN UNUSUAL NOISE WAS HEARD, THEN THE MAIN GEAR GREEN LGIHTS ILLUMINATED. AFTER APPROXIMATELY 3-5 MINUTES, THE NOSE GEAR GREEN LIGHT ILLUMINATED. FLIGHT DIVERTED TO BOS AND, AFTER TOWER FLY-BY, LA - [SDR USAAF98088](https://openairdocs.org/sdr/USAAF98088.md): Switch · failed · Oct 30, 1998 · N865US · Fokker F28MK0100 · Stabilizer Control System > PIT - FLT 667 - AFTER TAKEOFF FROM PIT, STAB TRIM 1 AND 2 FAULT MESSAGE ILLUMINATED. FLIGHT RETURNED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 1 TRIM SWITCH. (M) - [SDR USAAF98080](https://openairdocs.org/sdr/USAAF98080.md): Warning Unit · malfunctioned · Sep 23, 1998 · N865US · Fokker F28MK0100 · Central Warning > PHL - FLT 1620 - TEN MINUTES AFTER DEPARTURE FROM PHL, FLIGHT WARNING COMPUTER INOP MESSAGE APPEARED ON THE MULTI FUNCTION DISPLAY. CREW RECYCLED BREAKERS BUT FAULT MESSAGE REMAINED. FLIGHT RETURNED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE TE - [SDR USAAF98029](https://openairdocs.org/sdr/USAAF98029.md): Fault Light · illuminated · Mar 16, 1998 · N865US · Fokker F28MK0100 · Pneumatic Indicating System > PIT - FLT 540 - AIRCRAFT WAS CLIMBING TO FL250 OUT OF PIT WHEN A BLEED FAULT 1 LIGHT ILLUMINATED. CAPTAIN DESCENDED TO FL240 AND TRIED TO RESET WITHOUT SUCCESS. FLIGHT RETURNED TO PIT WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED BLEED S - [SDR USAAF98007](https://openairdocs.org/sdr/USAAF98007.md): Battery Pack · discharged · Jan 14, 1998 · N865US · Fokker F28MK0100 · Emergency Lighting > IND - MAINTENANCE FOUND EMERGENCY LIGHTS INOPERATIVE AT FORWARD CABIN FLOOR, GALLEY AND COCKPIT. REPLACED THE BATTERY PACK. (M) - [SDR USAAF97088](https://openairdocs.org/sdr/USAAF97088.md): Landing Gear · collapsed · Nov 7, 1997 · N865US · Fokker F28MK0100 · Main Landing Gear > FLT 479 - MKE-CLT - UPON LANDING IN CLT, LANDING GEAR SHIMMIED VIOLENTLY. AIRCRAFT PULLED HARD RIGHT AND RIGHT MAIN LANDING GEAR COLLAPSED. THE RIGHT WING TIP TOUCHED THE RUNWAY AFTER GEAR COLLAPSED. PASSENGERS WERE EVACUATED. MAINTENANCE REPAIRED THE AIRC - [SDR USAAF97086](https://openairdocs.org/sdr/USAAF97086.md): Sensor · failed · Nov 2, 1997 · N865US · Fokker F28MK0100 · Landing Gear Position and Warning > FLT 627 - PIT - AVP - AFTER TAKEOFF FROM PIT WHEN LANDING GEAR WAS RETRACTED, A GROUND/FLT FAULT, LIFT DUMPER FAULT, AND TCAS FAULT ILLUMINATED ON THE MULTIFUNCTION DISPLAY. THE AIRCRAFT RETURNED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLAC - [SDR USAA970064](https://openairdocs.org/sdr/USAA970064.md): Skin · disbonded · Feb 20, 1997 · N865US · Fokker F28MK0100 · Fuselage Main, Plate/Skin > PIT - DURING Q1 CHECK, FOUND 20 INCH BY 24 INCH AREA OF DISBONDED/HEAT DAMAGE SKIN AT LEFT STUBWING FUSELAGE SKIN BETWEEN FRAMES 24011 AND 24611. CUT OUT AREA OF DISBONDED/HEAT DAMAGED SKIN AND INSTALLED EXTERNAL DOUGLAS PER EA 80083A. (M) - [SDR USAA970062](https://openairdocs.org/sdr/USAA970062.md): Skin · corroded · Feb 20, 1997 · N865US · Fokker F28MK0100 · Fuselage Main, Plate/Skin > PIT - DURING Q1 CHECK, FOUND SKIN CORROSION AT FUSELAGE FORWARD DRAIN MAST SKIN AREA. INSTALLED DOUBLER REPAIR PER USAIR EA NR 46267. (M) - [SDR USAAF96116](https://openairdocs.org/sdr/USAAF96116.md): Bypass Switch · failed · Nov 10, 1996 · N865US · Fokker F28MK0100 · Elevator Control System > FLT 2341 - PIT-RSW - UPON CLIMB-OUT AT 7500 FEET, AIRCRAFT ENCOUNTERED LIGHTNING AND HEARD LOUD THUNDER IN AIRCRAFT. CAPTAIN HAD A DOUBLE FAULT ON ELEVATOR. RETURNED TO PIT WITH MANUAL REVERSION LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED LIGHTNI - [SDR USAA960063](https://openairdocs.org/sdr/USAA960063.md): Bulkhead Angle · cracked · Feb 26, 1996 · N865US · Fokker F28MK0100 · Fuselage Main, Bulkhead > PIT - DURING Q- CHECK, FOUND 1 INCH CRACK IN ANGLE AT CTR PRESSURE BULKHEAD ANGLE CRACK, STRINGER 64 RHS, STATION 14911. VISUALLY DETECTED AND VERIFIED BY NDT. INSTALLED REPAIR ANGLES PER USAIR EA NR 46216. (M) - [SDR USAA951096](https://openairdocs.org/sdr/USAA951096.md): Eel Strip · failed · Oct 12, 1995 · N865US · Fokker F28MK0100 · Emergency Lighting > IND - FLT NR 301 - EMERGENCY FLOOR LIGHTING IN FIRST CLASS WAS REPORTED AS INOP. REPLACED EMERGENCY FLOOR LIGHTING LAMP STRIP. (M) - [SDR USAA950575](https://openairdocs.org/sdr/USAA950575.md): Gcu · failed · Jun 8, 1995 · N865US · Fokker F28MK0100 · Airborne Auxiliary Power Unit (APU) System > CLT - FLT 1170 - CAPTAIN ADVISED THAT THE APU GENERATOR WAS LOST AT APPROXIMATELY 40 MILES OUT OF CLT. FLIGHT RETURNED TO CLT. FLIGHT RETURNED TO CLT AND LANDED WITHOUT INCIDENT. REPLACED GCU. (M) - [SDR USAA950456](https://openairdocs.org/sdr/USAA950456.md): Idg · req'd service · May 11, 1995 · N865US · Fokker F28MK0100 · Alternator-Generator Drive > PIT - FLT 0214 - EN ROUTE FROM CLT TO MKE, AIRCRAFT LOST APU AND ITS GENERATOR. AIRCRAFT DIVERTED TO PIT. MAINTENANCE SERVICED THE RIGHT IDG WITH OIL. OPERATIONS CHECKED GOOD. (M) ## 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 = 'N865US' AND deregistration_id = 'N865US-2003-10-07' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N865US-2003-10-07/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.