# Service difficulty reports: N869US, cancelled Jul 9, 2003 A list on [N869US, cancelled Jul 9, 2003](https://openairdocs.org/deregistered/N869US-2003-07-09.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR USAAF01006](https://openairdocs.org/sdr/USAAF01006.md): Inverter · inoperative · Feb 19, 2001 · N869US · Fokker F28MK0100 · Emergency Lighting > IND - MAIN ENTRANCE DOOR, SERVICE DOOR AND GALLEY AISLE FLOOR PROXIMITY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED INVERTER A AND THE OUTBOARD MARKER LIGHT ASSEMBLY. OPS CHECKED OK. (M) - [SDR USAAF00078](https://openairdocs.org/sdr/USAAF00078.md): Relay · failed · Oct 27, 2000 · N869US · Fokker F28MK0100 · Air Distribution System > CMH-PIT - FLT 2004 - DURING FLIGHT, AN ELECTRIC ODOR WAS NOTICED THROUGHOUT AIRCRAFT. THE ODOR THEN DISSIPATED AFTER TEN MINUTES. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED RELAY K0933A. AIRCRAFT AND EQUIPMENT COOLING FAN OPS CHECKED OK. (M) - [SDR USAAF00027](https://openairdocs.org/sdr/USAAF00027.md): Girt Bar · damaged · Mar 25, 2000 · N869US · Fokker F28MK0100 · Escape Slide > RIC - FOUND THE FORWARD SERVICE DOOR WILL NOT ARM PROPERLY. MAINTENANCE FOUND ARMING MECHANICAL LINKAGE BOUND AT DOOR OPEN/CLOSING HANDLE INTERFACE POINT. FREED LINKAGE AT INTERFACE/STICKING POINT. DOOR OPS CHECKED OK. (M) - [SDR USAAF00014](https://openairdocs.org/sdr/USAAF00014.md): Uplock Bracket · loose · Feb 14, 2000 · N869US · Fokker F28MK0100 · Landing Gear Retraction/Extension System > CLT-PIT - FLT 1422 - DURING APPROACH, LANDING GEAR WAS SELECTED TO EXTEND. ALL LANDING GEAR INDICATED DOWN AND LOCKED, HOWEVER, THE RT MAIN GEAR DOOR INDICATED NOT CLOSED. GEAR WAS RECYCLED WITH THE SAME RESULT. THE APPROPRIATE HYDRAULIC SYSTEM WAS SHUTDOWN - [SDR USAAF98061](https://openairdocs.org/sdr/USAAF98061.md): Slide · malfunctioned · Jul 19, 1998 · N869US · Fokker F28MK0100 · Escape Slide > PIT - DURING AN ANNUAL ESCAPE SLIDE OPERATIONAL CHECK SAMPLING PROGRAM, THE FORWARD ENTRY DOOR ESCAPE SLIDE DID NOT FULLY INFLATE. ACCORDING TO THE INSPECTOR THAT WITNESSED THE DEPLOYMENT, THE SLIDE INITIALLY WAS HUNG UP IN THE DOORWAY. WHEN THE MANUAL HANDL - [SDR USAAF98056](https://openairdocs.org/sdr/USAAF98056.md): Engine · failed · Jul 18, 1998 · N869US · Fokker F28MK0100 · Engine (Turbine/Turboprop) > PIT - FLT 8079 - EN ROUTE TO PHL AT FL33 AND ON DESCENT TO FL29, AS N1 CAME BACK THROUGH 50 PERCENT, NR 1 ENGINE VIBRATION INDICATION WENT TO TOP OF ORANGE BAND. THE VIBRATION WAS FELT IN THE COCKPIT FLOOR AND THROTTLE QUADRANT. ALSO, AN AUDIBLE RUMBLE WAS H - [SDR USAA970257](https://openairdocs.org/sdr/USAA970257.md): Angle · cracked · Aug 6, 1997 · N869US · Fokker F28MK0100 · Fuselage Miscellaneous Structure > PIT - DURING Q-1 CHECK, FOUND CRACK IN RADIUS AT FUSELAGE CTR PRESS BULKHEAD ANGLE, LT SIDE, STA 14911, STR 11. INSTALLED DOUBLER REPAIR PER US AIRWAYS EA NR 47506. (X) - [SDR USAA970256](https://openairdocs.org/sdr/USAA970256.md): Skin · delaminated · Aug 6, 1997 · N869US · Fokker F28MK0100 · Fuselage Main, Plate/Skin > PIT - DURING Q-1 CHECK, FOUND SKIN DELAMINATION 14.50 INCHES BY 3.50 INCHES IN SKIN AT STA 14011 TO STA 14611 STR 22 AND STR 23, RIGHT SIDE. INSTALLED EXTERNAL DOUBLER 20 INCHES BY 10.25 INCHES PER US AIRWAYS EA NR 29764A. (X) - [SDR USAAF96086](https://openairdocs.org/sdr/USAAF96086.md): Efis · failed · Aug 5, 1996 · N869US · Fokker F28MK0100 · Integrated Flight System > GSP-LGA - FLT 926 - DURING CLIMB-OUT OF GSP, NR 1 NAV DISPLAY LOCKED UP. CAPTAIN WAS UNABLE TO SWITCH TO ROSE OF SELECT HEADING. FLIGHT DIVERTED TO CLT. NO EMERGENCY DECLARED AND FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED LEFT EFIS CONTRO - [SDR USAAF96084](https://openairdocs.org/sdr/USAAF96084.md): Squat Sw · failed · Aug 1, 1996 · N869US · Fokker F28MK0100 · Landing Gear Position and Warning > FLT 1025 - PIT-ABE - AFTER TAKEOFF, PILOT TRIED TO RAISE GEAR. RECEIVED GRD/FTL CONTROLS, TCAS, AND LIFT DUMPER MESSAGES. RETURNED TO FIELD. MAINTENANCE REPLACED LEFT INBOARD GND/FLT SENSOR. CYCLED GEAR SEVERAL TIMES. ALL CHECKS NORMAL. (M) - [SDR USAAF96063](https://openairdocs.org/sdr/USAAF96063.md): Prsov · failed · Jun 21, 1996 · N869US · Fokker F28MK0100 · Cabin Pressure Control System > PIT - FLT 2049 - CLIMBING THROUGH 12,000 FEET, CREW NOTICED A NOISE FROM LEFT PACK, AFTER WHICH THE OUTPUT TEMPERATURE ROSE TO 150 DEGREES. RIGHT PACK TEMPERATURE WAS RUNNING HOT BUT COOLED WHEN ENGINE POWER WAS REDUCED ON DESCENT. CABIN BECAME VERY WARM. F - [SDR USAAF96051](https://openairdocs.org/sdr/USAAF96051.md): Door Seal · failed · May 22, 1996 · N869US · Fokker F28MK0100 · Cargo/Baggage Doors > PHL - FLT 328 - CREW LOST PRESSURIZATION AT 33,OOO FEET. CREW DESCENDED TO 10,000 FEET. FLIGHT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND THE FORWARD CARGO DOOR SEAL LEAKING. THE DOOR SEAL WAS REPLACED. AIRCRAFT WAS PRESSURIZED WITH LEAK RATE CHEC - [SDR USAAF96023A](https://openairdocs.org/sdr/USAAF96023A.md): Heat Shield · bent · Feb 22, 1996 · N869US · Fokker F28MK0100 · Landing Gear Brake System > FLT NR 1543 - CLT - ON TAKEOFF FROM RDU RWY 23R, CAPTAIN HAD GEAR FAULT MESSAGE, RDU TOWER TOLD HIM IT LOOKED LIKE SOMETHING FELL OFF THE AIRCRAFT. WHILE THE FLIGHT HELD IN THE AIR OVER RDU, THEY FOUND THE NR 2 MAIN WHEEL ASSEMBLY. FLIGHT PROCEEDED TO CLT. - [SDR USAAF96023](https://openairdocs.org/sdr/USAAF96023.md): Wheel · departed · Feb 22, 1996 · N869US · Fokker F28MK0100 · Wheel/Ski/Float > CLT - FLT 1543 - ON TAKEOFF FROM RDU RWY 23R, CAPT HAD GEAR FAULT MESSAGE, RDU TOWER TOLD HIM IT LOOKED LIKE SOMETHING FELL OFF THE AIRCRAFT. WHILE THE FLT HELD IN THE AIR OVER RDU, THEY FOUND THE NR 2 MAIN WHEEL ASSY. FLT PROCEEDED TO CLT. CORRECTIVE ACTIO - [SDR USAA950445](https://openairdocs.org/sdr/USAA950445.md): Windshield · cracked · May 4, 1995 · N869US · Fokker F28MK0100 · Flight Compartment Windows > PIT - FLIGHT NR 0403 - ON CLIMB-OUT, A CRACK DEVELOPED IN THE CAPTAINS WINDSHIELD. FLIGHT RETURNED TO PIT WITHOUT INCIDENT. (M) - [SDR USAA950224](https://openairdocs.org/sdr/USAA950224.md): Unsafe Light · illuminated · Feb 24, 1995 · N869US · Fokker F28MK0100 · Landing Gear Position and Warning > BUF - FLT 0873 - AFTER TAKEOFF, THE RIGHT MAIN LANDING GEAR UNSAFE LIGHT ILLUMINATED WHEN THE GEAR WAS RETRACTED. THE GEAR WAS RECYCLED TWICE WITH THE SAME RESULTS. CREW RETURNED TO BUF WITHOUT INCIDENT. MAINTENANCE INSPECTED THE GEAR AND FOUND HEAVY ICE. - [SDR USAA950039](https://openairdocs.org/sdr/USAA950039.md): Retract Mech · iced up · Jan 23, 1995 · N869US · Fokker F28MK0100 · Landing Gear Retraction/Extension System > PIT - FLT 977 - ON TAKEOFF, THE CREW GOT A RT MAIN LANDING GEAR WARNING ON THE MFDU. GEAR WAS RECYCLED BUT THE WARNING REMAINED. ACFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED A LARGE AMOUNT OF ICE AND SAND FROM THE MLG. OPERATION ## 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 = 'N869US' AND deregistration_id = 'N869US-2003-07-09' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N869US-2003-07-09/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.