N887US, cancelled Aug 2, 2004

Service difficulty reports · 20

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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 = 'N887US' AND deregistration_id = 'N887US-2004-08-02'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR USAAF01033Coalescer Bag · contaminatedTRI-CLT - FLT 242 - THE AIRCONDITIONING PACKS PRODUCED AN ODOR DURING CRUISE AND WOULD NOT COOL THE CABIN. THE FLIGHT CONTINUED AND LANDED IN CLT WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT WATER SEPARATOR BAG AND REPAIRED A LEAK AT THE DUCT ON Jun 15, 2001 · N887US · Fokker F28MK0100 · Humidity Control SystemSDR USAA010588Frame · crackedPIT - FOUND FRAME CRACKED 1.25 INCH, LEFT SIDE TOP OF OBLIQUE FRAME 67.2. TEMPORARY REPAIR WITH STOP DRILL PER EA 71082 AND SRM 51-22-01. (M)May 19, 2001 · N887US · Fokker F28MK0100 · Fuselage Structure (General)SDR USAAF01016Wire · damagedIND- A SECTION OF FLOOR ESCAPE LIGHTING WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED WIRING TO LIGHT STRIP. OPS CHECKED OK. (M)Apr 25, 2001 · N887US · Fokker F28MK0100 · Light System WiringSDR USAAF01005Actuator · brokenPHL-SYR - FLT 768 - AFTER GEAR UP WAS SELECTED, A LOUD FLUTTERING NOISE WAS PRESENT WITH A NOSE LANDING GEAR INDICATION LIGHT. THE FLIGHT RETURNED TO PHL AND MADE A NORMAL LANDING. MAINTENANCE REPLACED THE NOSE LANDING GEAR DOOR ACTUATOR. OPERATIONALLY CHECJan 31, 2001 · N887US · Fokker F28MK0100 · Landing Gear Door ActuatorSDR USAAF99059Switch · out of positionCLT-IAH - FLT 463 - DURNG CLIMB-OUT FROM CLT, CAPTAIN RECEIVED AUTO FUEL CROSSFEED FAIL ALERT. ALSO, CLT TOWER ADVISED THAT THERE WAS SUBSTANTIAL FUEL ESCAPING FROM WINGS. SEVERAL TURNS WERE MADE TO BURN FUEL TO REACH LESS THAN MAXIMUM LANDING WEIGHT. FLIGHDec 31, 1999 · N887US · Fokker F28MK0100 · Aircraft Fuel Distribution SystemSDR USAAF99039Battery Pack · dischargedIND - FOUND FORWARD EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. (M)Aug 3, 1999 · N887US · Fokker F28MK0100 · Emergency LightingSDR USAAF98097Trim System · malfunctionedCLT - FLT 2208 - ON CLIMB-OUT FROM CLT, CREW RECEIVED A DOUBLER STAB TRIM FAULT INDICATION. FLIGHT RETURNED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE RESET THE STAB TRIM SYSTEM. ALL MAINTENANCE BITE TESTS PASSED. AIRCRAFT WAS RETURNED TO SERVDec 18, 1998 · N887US · Fokker F28MK0100 · Stabilizer Control SystemSDR USAAF98062Control Box · failedCLT - FLT 476 - AFTER TAKEOFF FROM CLT, WHEN LANDING GEAR WAS RETRACTED, 'ANTI-SKID' FAULT MESSAGE APPEARED. FLIGHT RETUREND TO CLT. MESSAGE REMAINED ON UNTIL LANDING GEAR WAS EXTENDED THEN MESSAGE EXTINGUISHED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINJul 26, 1998 · N887US · Fokker F28MK0100 · Brake Anti-Skid SectionSDR USAAF98032Downlock Pin · not engagedPWM - FLT 1824 - ON APPROACH, NOSE GEAR WAS SHOWING AN UNSAFE NOSE LIGHT. AIRCRAFT DID A GO-AROUND. CAPTAIN DECIDED TO FREE FALL THE NOSE GEAR AND GOT A GREEN LIGHT. AN EMERGENCY WAS DECLARED AND CABIN WAS PREPARED FOR AN EMERGENCY LANDING. FLIGHT HAD NO PMar 25, 1998 · N887US · Fokker F28MK0100 · Landing Gear Retraction/Extension SystemSDR USAAF98025Switch · failedCLT - FLT 1210 - ON CLIMB-OUT OF CLT AIRCRAFT HAD A WING ANTI-ICE FAULT TWICE BETWEEN 9000 FEET - 11,000 FEET. FLIGHT RETURNED TO CLT WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED WING ANTI-ICE SWITCH IN OVERHEAD PANEL. PERFORMED OPERATIOMar 4, 1998 · N887US · Fokker F28MK0100 · Airfoil Anti/De-ice SystemSDR USAA980051Skin · delaminatedPIT - DURING Q-1 CHECK, FOUND RT SKIN DELAMINATION AND SIGNS OF DISCOLORATION BETWEEN FRAMES 23011 AND 24611 AT STRINGER 53. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER REPAIR 12 INCH BY 8 INCH PER US AIRWAYS EA 29352A. (M)Mar 1, 1998 · N887US · Fokker F28MK0100 · Fuselage Main, Plate/SkinSDR USAAF97097Engine · vibrationIND - FLT 1057 - EN ROUTE, CREW EXPERIENCED HIGH VIBRATION ON THE LEFT ENGINE. CREW WAS ABLE TO CONTROL THE VIBRATION BY REDUCING THE ENGINE EPR. VIBRATION RETURNED DURING DESCENT. FLIGHT DIVERTED TO IND AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE CHENov 25, 1997 · N887US · Fokker F28MK0100 · Engine (Turbine/Turboprop)SDR USAAF97066Thrust Plate · dirtyPHL/ROC - FLT 504 - ON APPROACH TO ROC WHEN THE LANDING GEAR WAS EXTENDED, A 'NOSE GEAR UNSAFE' WARNING ILLUMINATED ALONG WITH NO ILLUMINATION OF GREEN 'NOSE GEAR' DOWN AND LOCKED INDICATOR. CREW PERFORMED A GO-AROUND PROCEDURE AND CYCLED THE LANDING GEAR. WJul 27, 1997 · N887US · Fokker F28MK0100 · Landing Gear Retraction/Extension SystemSDR USAAF97046Bulb · failedFLT 2228 - DCA-CLT - ON APPROACH TO CLT, DID NOT RECEIVE A GREEN DOWN AND LOCKED INDICATION FOR THE RIGHT MAIN GEAR. CAPTAIN ELECTED TO PERFORM A GO AROUND PROCEDURE. CREW DETERMINED THAT THE LAMP WAS BURNED OUT IN THE INDICATOR. FLT LANDED AT CLT WITHOUT IMay 13, 1997 · N887US · Fokker F28MK0100 · Landing Gear Position and WarningSDR USAAF97031Fire Warning · activatedERI - FL 1202 - ON APPROACH, WITH APU RUNNING, CREW RECEIVED APU FIRE WARNING. APU PERFORMED AUTO SHUT DOWN, AND THE FIRE BOTTLE DISCHARGED. FLIGHT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND NO EVIDENCE OF A FIRE. THE EXHAUST DUCTING, BLEED/LOAD COMar 15, 1997 · N887US · Fokker F28MK0100 · Fire DetectionSDR USAAF97015Sequence Valve · failedFLT 1239 - PIT-DAY - ON APPROACH TO DAY THE NOSE GEAR DID NOT EXTEND ON THE FIRST TRY. PILOT RECYCLED TEH GEAR AND ALL INDICATIONS WERE NORMAL ON THE SECOND TRY. FLIGHT LANDED AT DAY WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NOSE GEAR SEQUENCE VALVJan 13, 1997 · N887US · Fokker F28MK0100 · Landing Gear Retraction/Extension SystemSDR USAAF97014Retract Mech · lack of lubeFLT 466 - GSP-PHL - ON APPROACH TO PHL, THE NOSE GEAR DID NOT EXTEND ON THE FIRST TRY. PILOT ACCOMPLISHED ABNORMAL CHECKLIST ITEMS AND RECYCLED GEAR. THE SECOND EXTENSION WAS NORMAL. FLIGHT LANDED IN PHL WITHOUT FURTHER INCIDENT. MAINTENANCE BITE CHECKED SJan 10, 1997 · N887US · Fokker F28MK0100 · Landing Gear Retraction/Extension SystemSDR USAAF96130Retract Mech · lack of lubeFLT 1475 - PHL-DTW - ON DESCENT INTO DTW RECEIVED AN UNSAFE GEAR INDICATION WARNING AT FL 010. NOSE GEAR DID NOT COME DOWN. CREW DID A GO AROUND AND RECYCLED THE GEAR. LANDING GEAR OPERATED NORMALLY AFTER RECYCLE. NO EMERGENCY DECLARED AND FLIGHT LANDED WIDec 21, 1996 · N887US · Fokker F28MK0100 · Landing Gear Retraction/Extension SystemSDR USAAF96107Diode · overheatedFLT 1206 - RDU-PIT, AT 50S OF PIT, CRWE GOT 'EMERGENCY DC BUS FAILED' ON MFDU. COMMUNICATINOS WERE LOST WITH ZOB AND PIT APPROACH. AIRCRAFT SHED SOME ELECTRICAL LOAD AND COMMUNICATION WAS RE-ESTABLISHED. AN EMERGENCY WAS DECLARED AND FLIGHT LANDED WITHOUT ISep 21, 1996 · N887US · Fokker F28MK0100 · DC Power Distribution SystemSDR USAAF96082Flex Duct · leakingGRR - FL 862 - UPON DESCENT INTO GRR, CREW RECEIVED APU FIRE WARNING. APU WAS AUTOMATICALLY SHUT DOWN AND THE FIRE BOTTLE DISCHARGED. FLIGHT CONTINUED TO GRR AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND NO EVIDENCE OF A FIRE. A BLEED AIR LEAK WAS Aug 1, 1996 · N887US · Fokker F28MK0100 · APU Bleed Air System
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