# Service difficulty reports: N881US, cancelled Jun 3, 2003 A list on [N881US, cancelled Jun 3, 2003](https://openairdocs.org/deregistered/N881US-2003-06-03.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR USAAF01076](https://openairdocs.org/sdr/USAAF01076.md): Actuator · failed · Oct 7, 2001 · N881US · Fokker F28MK0100 · Landing Gear Actuator > PIT-RDU - FLT 280 - AFTER TAKEOFF, THE LEFT MAIN LANDING GEAR WOULD NOT RETRACT. WHEN TRYING TO EXTEND THE LANDING GEAR, THE NOSE GEAR EXTENDED BUT NOT THE MAIN GEAR. THE ALTERNATE GEAR EXTENSION WAS USED TO EXTEND THE GEAR. THE AIRCRAFT RETURNED TO THE FIE - [SDR USAAF01034](https://openairdocs.org/sdr/USAAF01034.md): Windshield · cracked · Jun 23, 2001 · N881US · Fokker F28MK0100 · Window/Windshield System > CLT-MEM - FLT 865 - THE RIGHT FORWARD WINDSHIELD INNER PANE SHATTERED, AND HAD A LARGE BUBBLE ON THE OUTER PANE DURING FLIGHT. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE FIRST OFFICERS WINDSHIELD. OPERATIONALLY CHECKED OK. (M) - [SDR USAAF00084](https://openairdocs.org/sdr/USAAF00084.md): Battery Pack · discharged · Nov 27, 2000 · N881US · Fokker F28MK0100 · Emergency Lighting > RDU - THE CABIN EMERGENCY EXIT LIGHTING FLOOR STRIP WAS INOPERATIVE JUST FORWARD OF THE EMERGENCY EXIT ROW. MAINTENANCE REPLACED THE BATTERY PACK. OPERATIONALLY CHECKED OK. (M) - [SDR USAAF00023](https://openairdocs.org/sdr/USAAF00023.md): Sequence Valve · malfunctioned · Mar 9, 2000 · N881US · Fokker F28MK0100 · Landing Gear Retraction/Extension System > CLT-CMH - FLT 912 - AFTER TAKEOFF, THE NOSE GEAR RETRACTED BUT THE MAIN LANDING GEAR DID NOT. FLIGHT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE MLG SEQUENCE VALVES. OPS AND LEAK CHECK OK. (M) - [SDR USAAF00022](https://openairdocs.org/sdr/USAAF00022.md): Selector Valve · malfunctioned · Mar 7, 2000 · N881US · Fokker F28MK0100 · Landing Gear Selector > CLT-CHS - FLT 553 - ON FINAL APPROACH, SELECTED GEAR DOWN AND ONLY RECEIVED NOSE GEAR DOWN INDICATION. A FLYBY OF THE TOWER CONFIRMED THAT ONLY THE NOSE GEAR WAS DOWN AND MLG DOORS WERE OPEN. AFTER A MISSED APPROACH TO DOWNWIND, BOTH MAINS FINALLY EXTENDED. - [SDR USAAF00020](https://openairdocs.org/sdr/USAAF00020.md): Light · inoperative · Feb 28, 2000 · N881US · Fokker F28MK0100 · Emergency Lighting > CLE - THE GALLEY SERVICE DOOR EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE AT THE GALLEY SERVICE DOOR EMERGENCY EXIT LIGHT. (M) - [SDR USAAF99060](https://openairdocs.org/sdr/USAAF99060.md): Selector Valve · failed · Dec 31, 1999 · N881US · Fokker F28MK0100 · Landing Gear Selector > CLT/ROA - FLT 2122 - DURING CLIMB OUT FROM CLT, LANDING GEAR WOULD NOT RETRACT. ACCOMPLISHED CHECKLIST PROCEDURES. RETURNED TO FIELD FOR A NORMAL LANDING. MAINTENANCE REPLACED THE LANDING GEAR SELECTOR VALVE. LEAKS AND OPS CHECKED GOOD. ALL GEAR RETRACT. - [SDR USAAF00001](https://openairdocs.org/sdr/USAAF00001.md): Selector Valve · failed · Jan 2, 1999 · N881US · Fokker F28MK0100 · Landing Gear Selector > RDU/CLT - FLT 2327 - DURING CLIMB-OUT FROM CLT, LANDING GEAR WOULD NOT RETRACT. RECYCLED GEAR AFTER 2-3 MINUTES, GEAR RETRACTED. ON APPROACH, GEAR SELECTED DOWN, BUT MAINS DID NOT EXTEND. FOUR MINUTES LATER, RECEIVED THREE GREEN INDICATIONS. MADE SAFE LAND - [SDR USAA980576](https://openairdocs.org/sdr/USAA980576.md): Skin · chafed · Nov 11, 1998 · N881US · Fokker F28MK0100 · Fuselage Main, Plate/Skin > PIT - DURING C-1 CHECK, FOUND TWO 1 INCH HOLES CHAFFED IN SKIN BETWEEN STATION 27526 AND OBLIQUE FRAME NR 16-2. INSTALLED DOUBLER PER EA 50951. (M) - [SDR USAA980575](https://openairdocs.org/sdr/USAA980575.md): Longeron · chafed · Nov 11, 1998 · N881US · Fokker F28MK0100 · Fuselage Main, Longeron/Stringer > PIT - DURING C-1 CHECK, FOUND LONGERON CHAFED THROUGH.125 INCH BY.25 INCH AT LONGERON NR 50 CHAFED THROUGH AT STATION 27526. LONGERON DAMAGE CUT OUT, NEW PIECE SPLICED IN PER SRM 51-70-06 PAGE 206. (M) - [SDR USAAF98045](https://openairdocs.org/sdr/USAAF98045.md): Rt Unit · failed · May 24, 1998 · N881US · Fokker F28MK0100 · Ground Proximity System > PIT - FLT 0669 - AFTER TAKEOFF FROM PIT, RA FLAG ON PFD ILLUMINATED ALONG WITH THE FOLLOWING FAULT MESSAGES: GPWS, ALAND, STAB TRIM 1. THE NR 1 AUTOPILOT DISENGAGED. FLIGHT RETURNED TO PIT WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 1 RADIO ALTIME - [SDR USAAF98033](https://openairdocs.org/sdr/USAAF98033.md): Lights · inoperative · Mar 17, 1998 · N881US · Fokker F28MK0100 · Emergency Lighting > PIT - DURING OVERNIGHT MAINTENANCE VISIT, FOUND LOW LEVEL LIGHTING IN AFT CABIN INOPERATIVE. MAINTENANCE REPAIRED WIRING IN AFT LOW LEVEL LIGHTING CIRCUIT. (M) - [SDR USAAF97019](https://openairdocs.org/sdr/USAAF97019.md): Flow Contl Valve · failed · Feb 14, 1997 · N881US · Fokker F28MK0100 · Cabin Cooling System > ILM/GRR - FLT 1612 - EN ROUTE TO GRR, BOTH AUTOMATIC PRESSURIZATION SYSTEMS WENT OFF LINE. MANUAL SYSTEM WORKED OK. FLIGHT DIVERTED TO PIT TO ACCOMMODATE MAINTENANCE. FLIGHT LANDED IN PIT WITHOUT FURTHER INCIDENT. MAINTENANCE ADJUSTED LEFT AND RIGHT PRESSU - [SDR USAAF96111](https://openairdocs.org/sdr/USAAF96111.md): Battery Pack · discharged · Oct 26, 1996 · N881US · Fokker F28MK0100 · Emergency Lighting > DURING OVERNIGHT MAINTENANCE CHECK, MECHANIC FOUND FIRST CLASS FLOOR LEVEL EMERGENCY LIGHTING INOP. MAINTENANCE REPLACED BATTERY PACK. OPERATIONAL CHECK GOOD. (M) - [SDR USAAF96055](https://openairdocs.org/sdr/USAAF96055.md): Inverter · inoperative · Jun 7, 1996 · N881US · Fokker F28MK0100 · Emergency Lighting > FIRST CLASS FLOOR EMERGENCY LIGHTS INOPERATIVE. REPLACED INVERTER. (M) - [SDR USAAF96038](https://openairdocs.org/sdr/USAAF96038.md): Adc · malfunctioned · Apr 28, 1996 · N881US · Fokker F28MK0100 · Air Data Computer > STL - FL 2129 - AT FL 350, CREW NOTICED THE THRUST WAS BEING REDUCED BY THE AUTOPILOT, THE CAPT'S AIRSPEED WAS DEGRADING DOWNWARD WHILE THE F/O'S WAS GOING TO REDLINE. THE CAPT TOOK CONTROL OF THE A/C, FLYING MANUALLY, AND STARTED A DESCENT. AT FL 300 THE A/ - [SDR USAAF96031](https://openairdocs.org/sdr/USAAF96031.md): Tube · cracked · Mar 25, 1996 · N881US · Fokker F28MK0100 · Compressor Bleed Control > CLT - FLT 242 - AFTER TAKEOFF, CREW RECEIVED A NR 2 BLEED FAULT MESSAGE AND THEN A NR 2 DUCT LEAK MESSAGE. FLIGHT RETURNED TO CLT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND A CRACKED LINE IN THE NR 2 ENGINE SUB WING TEST BLOCK AREA. A TEMPORARY - [SDR USAA950008](https://openairdocs.org/sdr/USAA950008.md): Shut Off Valve · failed · Jan 6, 1995 · N881US · Fokker F28MK0100 · Airfoil Anti/De-ice System > PIT - FLT 508 - 'THE WING ANTI-ICE CAPACITY' MESSAGE CAME ON WITH THE WING AN TAIL ANTI-ICE TURNED ON. ACFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RT HPSOV NOT OPENING COMPLETELY WHEN AIR IS ON. REPLACED THE RT HPSOV. OPERATIO ## 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 = 'N881US' AND deregistration_id = 'N881US-2003-06-03' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N881US-2003-06-03/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.