# Service difficulty reports: N882US, cancelled Oct 7, 2003 A list on [N882US, cancelled Oct 7, 2003](https://openairdocs.org/deregistered/N882US-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 USAAF01090](https://openairdocs.org/sdr/USAAF01090.md): Light · inoperative · Dec 28, 2001 · N882US · Fokker F28MK0100 · Emergency Lighting > PIT - THE RIGHT FAIRING EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT ASSEMBLY. (M) - [SDR USAAF01075](https://openairdocs.org/sdr/USAAF01075.md): Actuator · failed · Oct 6, 2001 · N882US · Fokker F28MK0100 · Landing Gear Door Actuator > RIC-CLT - FLT 1008 - AFTER TAKEOFF, THE NOSE LANDING GEAR FAILED TO RETRACT. THE GEAR WAS CYCLED WITH NO CHANGE. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE GEAR AND FOUND SAFE TO FERRY TO PIT WITH THE GEAR DOWN - [SDR USAAF01024](https://openairdocs.org/sdr/USAAF01024.md): Light · inoperative · May 15, 2001 · N882US · Fokker F28MK0100 · Emergency Lighting > IND - THE EMERGENCY EXIT LIGHT ON THE MAIN ENTRY DOOR HINGE WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. FUNCTIONALLY CHECKED OK. (M) - [SDR USAAF99055](https://openairdocs.org/sdr/USAAF99055.md): Unknown · odor · Dec 1, 1999 · N882US · Fokker F28MK0100 · Air Distribution System > ORD - FLT 1999 - STRONG OIL BURNING ODOR DETECTED DURING TAKEOFF AND CLIMB-OUT. ODOR WENT AWAY ONCE THE NR 2 PACK WAS TURNED OFF. MAINTENANCE OPS CHECKED NR 2 PACK FOR OIL ODOR, BUT DID NOT DETECT ANY ODOR. PACK OK FOR SERVICE. (X) - [SDR USAAF99027](https://openairdocs.org/sdr/USAAF99027.md): Pump · failed · May 21, 1999 · N882US · Fokker F28MK0100 · Hydraulic Pump (Electric/Engine), Main > SBN - FLT 1240 EN ROUTE PIT-SBN, CREW EXPERIENCED TOTAL HYDRAULIC FAILURE. FLIGHT PROCEEDED TO SBN. UPON LANDING, THE NR 3 TIRE BLEW, CAUSING LOSS OF DIRECTIONAL CONTROL OF THE AIRCRAFT. THE AIRCRAFT CAME TO A STOP APPROXIMATELY 6000 FEET DOWN THE RUNWAY AN - [SDR USAAF98063](https://openairdocs.org/sdr/USAAF98063.md): Hydraulic System · failed · Jul 30, 1998 · N882US · Fokker F28MK0100 · Hydraulic Power System > CLT - FLT 281 - ON CLIMB-OUT FROM CLT, SYSTEM 1 HORIZONTAL STABILIZER HYDRAULICS FAILED. SEVERAL MINUTES LATER, SYSTEM 2 HORIZONTAL STABILIZER HYDRAULICS FAILED. FLIGHT RETURNED TO CLT WITHOUT DECLARING AN EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. MAIN - [SDR USAAF98057](https://openairdocs.org/sdr/USAAF98057.md): Mlg · failed · Jul 18, 1998 · N882US · Fokker F28MK0100 · Landing Gear Retraction/Extension System > PIT - FLT 671 - ON APPROACH TO CRW WHEN THE LANDING GEAR WAS SELECTED DOWN, THE MAIN LANDING GEAR DID NOT EXTEND. CREW RECYCLED THE GEAR HANDLE WITH THE SAME RESULT. FLIGHT RETURNED TO PIT. ON APPROACH TO PIT, CREW USED THE ALTERNATE GEAR EXTENSION PROCEDUR - [SDR 98ZZZX2863](https://openairdocs.org/sdr/98ZZZX2863.md): Door · damaged · Jul 18, 1998 · N882US · Fokker F28MK0100 · Landing Gear Doors > PIT - FLT 671 - ON APPROACH TO CRW WHEN THE LANDING GEAR WAS SELECTED DOWN, THE MAIN LANDING GEAR DID NOT EXTEND. CREW RECYCLED THE GEAR HANDLE WITH THE SAME RESULT. FLIGHT RETURNED TO PIT. ON APPROACH TO PIT, CREW USED THE ALTERNATE GEAR EXTENSION PROCEDUR - [SDR USAAF98053](https://openairdocs.org/sdr/USAAF98053.md): Pseu · failed · Jun 17, 1998 · N882US · Fokker F28MK0100 · Landing Gear Position and Warning > CLT - FLT 1458 - AFTER TAKEOFF, 'GND/FLT CONTROL' MESSAGE ALONG WITH MASTER CAUTION LIGHT WOULD INTERMITTENTLY APPEAR EVERY 2-3 MINUTES. FLIGHT RETURNED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE PROXIMITY SWITCHING ELECTRONIC UNIT, - [SDR 98ZZZX2831](https://openairdocs.org/sdr/98ZZZX2831.md): Sensor · failed · Jun 17, 1998 · N882US · Fokker F28MK0100 · Landing Gear Position and Warning > CLT - FLT 1458 - AFTER TAKEOFF, 'GND/FLT CONTROL' MESSAGE ALONG WITH MASTER CAUTION LIGHT WOULD INTERMITTENTLY APPEAR EVERY 2-3 MINUTES. FLIGHT RETURNED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE PROXIMITY SWITCHING ELECTRONIC UNIT, - [SDR 98ZZZX2830](https://openairdocs.org/sdr/98ZZZX2830.md): Sensor · failed · Jun 17, 1998 · N882US · Fokker F28MK0100 · Landing Gear Position and Warning > CLT - FLT 1458 - AFTER TAKEOFF, 'GND/FLT CONTROL' MESSAGE ALONG WITH MASTER CAUTION LIGHT WOULD INTERMITTENTLY APPEAR EVERY 2-3 MINUTES. FLIGHT RETURNED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE PROXIMITY SWITCHING ELECTRONIC UNIT, - [SDR 98ZZZX2829](https://openairdocs.org/sdr/98ZZZX2829.md): Harness · failed · Jun 17, 1998 · N882US · Fokker F28MK0100 · Landing Gear Position and Warning > CLT - FLT 1458 - AFTER TAKEOFF, 'GND/FLT CONTROL' MESSAGE ALONG WITH MASTER CAUTION LIGHT WOULD INTERMITTENTLY APPEAR EVERY 2-3 MINUTES. FLIGHT RETURNED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE PROXIMITY SWITCHING ELECTRONIC UNIT, - [SDR USAAF97075](https://openairdocs.org/sdr/USAAF97075.md): Battery Pack · discharged · Sep 22, 1997 · N882US · Fokker F28MK0100 · Emergency Lighting > DURING ROUTINE OVERNIGHT MAINTENANCE INSPECTION, MAIN ENTRY DOOR EXIT SIGN WOULD NOT ILLUMINATE. MAINTENANCE REPLACED THE BATTERY PACK. (X) - [SDR USAAF97057](https://openairdocs.org/sdr/USAAF97057.md): Aux Power Unit · failed · Jul 9, 1997 · N882US · Fokker F28MK0100 · APU Core Engine > PIT/ERI - FLT 502 - ON DESCENT INTO ERI, THE APU SHUT DOWN AUTOMATICALLY WHEN THE SPEED BRAKE WAS DEPLOYED. A 'LOW AGENT' FOR THE APU FIRE SYSTEM ALSO ILLUMINATED. THE FLIGHT LANDED ERI WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE APU ASSY. US AIRWAY - [SDR USAAF97052](https://openairdocs.org/sdr/USAAF97052.md): Swivel Joint · leaking · Jun 26, 1997 · N882US · Fokker F28MK0100 · APU Bleed Air System > RDU/CLT - FLT 1614 - ON APPROACH TO CLT, APPROXIMATELY 15 MILES FROM AIRPORT, APU FIRE WARNING ILLUMINATED, ALONG WITH AUTOMATIC APU SHUT DOWN AND FIRE BOTTLE DISCHARGE. CAPTAIN DECLARED AN EMERGENCY. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUN - [SDR 97ZZZX3180](https://openairdocs.org/sdr/97ZZZX3180.md): Fire Contl Unit · malfunctioned · Jun 26, 1997 · N882US · Fokker F28MK0100 · Fire Detection > RDU/CLT - FLT 1614 - ON APPROACH TO CLT, APPROXIMATELY 15 MILES FROM AIRPORT, APU FIRE WARNING ILLUMINATED, ALONG WITH AUTOMATIC APU SHUT DOWN AND FIRE BOTTLE DISCHARGE. CAPTAIN DECLARED AN EMERGENCY. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUN - [SDR USAAF97033](https://openairdocs.org/sdr/USAAF97033.md): Battery Pack · discharged · Mar 22, 1997 · N882US · Fokker F28MK0100 · Emergency Lighting > IND - FORWARD OVERHEAD EXIT SIGN AND AREA EMERGENCY LIGHT INOP. MAINTENANCE REPLACED THE BATTERY PACK. (M) - [SDR USAAF97026](https://openairdocs.org/sdr/USAAF97026.md): Windshield · failed · Mar 8, 1997 · N882US · Fokker F28MK0100 · Flight Compartment Windows > PIT - FL 8565 - EN ROUTE MCO-PIT - CREW NOTED STRONG ELECTRICAL SMELL IN COCKPIT. CREW DONNED OXYGEN MASKS. FLIGHT LANDED AT PIT WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT WINDSHIELD. (M) - [SDR USAAF96115](https://openairdocs.org/sdr/USAAF96115.md): Bulb · failed · Nov 5, 1996 · N882US · Fokker F28MK0100 · Emergency Lighting > EMERGENCY EXIT LIGHT AT 12A IS OUT OF SERVICE. MAINTENANCE RELAMPED EXIT LIGHT. (M) - [SDR USAAF96097](https://openairdocs.org/sdr/USAAF96097.md): Bypass Vlv · failed · Sep 8, 1996 · N882US · Fokker F28MK0100 · Cabin Cooling System > RDU-PIT - FLT 1423 - ON CLIMB GOING THROUGH FL 100, PACK CABIN SUPPLY TEMP WENT TO 100F EVEN WITH TEMP SELECT FULL COLD. ONE PACK WAS ON MEL AS WELL AS APU BLEED AIR. AIRCRAFT DIVERTED TO GSO. NO FURTHER INCIDENTS. MAINTENANCE REPLACED LEFT BYPASS VALVE. - [SDR USAAF96025](https://openairdocs.org/sdr/USAAF96025.md): Windshield · cracked · Feb 24, 1996 · N882US · Fokker F28MK0100 · Flight Compartment Windows > FLT NR 275 - RDU - OUTER PANE OF CAPTIANS WINDSHIELD SHATTERED IN FLIGHT AT 29,000 FEET PRECAUTIONARY LANDING MADE AT RDU. REPLACED L1 WINDOW. (M) - [SDR USAAF96008](https://openairdocs.org/sdr/USAAF96008.md): Shutoff Valve · inoperative · Jan 12, 1996 · N882US · Fokker F28MK0100 · Airfoil Anti/De-ice System > CLT - FL 1295 - EN ROUTE PIT - LGA, CREW RECEIVED TAIL ANTI-ICING FAULT SHORTLY AFTER SELECTING TAIL ANTI-ICE. FLIGHT DIVERTED TO CLT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE TAIL ANTI-ICE SHUTOFF VALVE. (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 = 'N882US' AND deregistration_id = 'N882US-2003-10-07' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N882US-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.