N895US, cancelled Sep 27, 2007

Service difficulty reports · 18

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 = 'N895US' AND deregistration_id = 'N895US-2007-09-27'
  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 USAAF01040Battery Pack · inoperativeIND- THE EMERGENCY LIGHTS WERE FOUND INOPERATIVE AT BOTH LAVATORIES, LAVATORY AREAS, AND THE AFT CABIN CEILING. MAINTENANCE REPLACED THE BATTERY PACK. OPERATIONALLY CHECKED OK. (M)Jun 30, 2001 · N895US · Fokker F28MK0100 · Emergency LightingSDR USAAF01035Battery Pack · dischargedIND - THE AFT CABIN CEILING EMERGENCY LIGHTS, LAVATORY EMERGENCY LIGHTS, AND THE LAVATORY AREA EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK IN THE AFT CABIN CEILING UNIT. OPERATIONALLY CHECKED OK. (M)Jun 25, 2001 · N895US · Fokker F28MK0100 · Emergency LightingSDR USAAF99036Modulating Valve · failedPHL - FLT 681 - FLIGHT RETURNED TO PHL DUE TO THE RIGHT PACK RUNNING FULL HOT AND CREATING A BURNING SMELL IN THE CABIN. THE LANDING WAS UNEVENTFUL. MAINTENANCE REPLACED THE RIGHT PACK MODULATING VALVE. (X)Jul 20, 1999 · N895US · Fokker F28MK0100 · Cabin Cooling SystemSDR USAAF99020O-Ring · leakingBOS - FLT 674 - DURING DESCENT A HYDRAULIC SYSTEM 1 LOW QUANTITY MESSAGE APPEARED. THE FLIGHT CREW DECLARED AN EMERGENCY AND DIVERTED TO BOS WHERE THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE NOTED THAT THE SYSTEM 1 HYDRAULICS QUANTITY WAS AT 44Apr 5, 1999 · N895US · Fokker F28MK0100 · Hydraulic System, MainSDR USAA980595Skin · delaminatedPIT - DURING Q1 CHECK, FOUND DELAMINATION 2 INCH BY 3 INCH CAUSED BY CORROSION AT C1 ANTENNA HOLD BETWEEN STATION 6305 AND 6805, STRINGERS 1 AND 74 ON SKIN. LOCALLY FABRICATED PARTS, CUT OUT DAMAGED AREA AND INSTALLED DOUBLER AND FILLER PER EA 50865. (M)Nov 13, 1998 · N895US · Fokker F28MK0100 · Fuselage Main, Plate/SkinSDR USAA980594Beam · corrodedPIT - DURING Q1 CHECK, FOUND .25 INCH TEE RAIL CORRODED AROUND RIVETS IN RIVET ATTACHMENT ON TOP ON BEAM 1127L FROM STATION 3870 TO 4610. INSTALLED REPLACEMENT 'T' ANGLE (RAIL) 37 INCH LONG PER SRM 51-20-02. (M)Nov 13, 1998 · N895US · Fokker F28MK0100 · Fuselage Miscellaneous StructureSDR USAA980593Frame · crackedPIT - DURING Q1 CHECK, FOUND 1 INCH CRACK AT FORWARD CARGO CEILING STATION NR 8305 BL '0' LINE FRAME. LOCALLY MANUFACTURED PART. REPLACED 15 INCH LONG SECTION WHICH HAD A 1 INCH CRACK IN IT PER SRM REF 53-21-10, 51-70-07, 51-30-01 AND 51-10-02. (M)Nov 13, 1998 · N895US · Fokker F28MK0100 · Fuselage Main, FrameSDR USAAF98085Valve · out of adjustBNA - FLT 1105 - ON APPROACH TO BNA WHEN LANDING GEAR HANDLE WAS SELECTED TO 'DOWN', GEAR HESITATED AND THEN SLOWLY EXTENDED. THE GREEN NOSE GEAR DOWN AND LOCKED INDICATOR DID NOT ILLUMINATE. CREW ABORTED APPROACH AND RECYCLED THE LANDING GEAR HANDLE. ALL TOct 9, 1998 · N895US · Fokker F28MK0100 · Landing Gear Retraction/Extension SystemSDR USAAF98084Sensor · out of adjustCLT - FLT 1856 - AFTER TAKEOFF FROM CLT, CREW RECEIVED SEVERAL LIFTDUMPER UNSAFE WARNINGS AND LIFTDUMPER FAULTS. NO EMERGENCY WAS DECLARED, HOWEVER, FLIGHT RETURNED TO CLT. FLIGHT LANDED CLT WITHOUT FURTHER INCIDENT. MAINTENANCE ADJUSTED RIGHT SIDE LIFTDUMPOct 8, 1998 · N895US · Fokker F28MK0100 · Drag Control SystemSDR USAAF98083Light · inoperativeGSO - FORWARD EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE FOUND PIN PUSHED BACK IN CONNECTOR P3858B. THE REPOSITIONED THE PIN IN THE CONNECTOR. (M)Sep 23, 1998 · N895US · Fokker F28MK0100 · Emergency LightingSDR USAAF97050Retract Mech · lack of lubeDTW/CLT - FLT 267 - DURING APPROACH TO CLT WHEN LANDING GEAR WAS SELECTED DOWN, THE NOSE GEAR DID NOT EXTEND FOR APPROXIMATELY 10-20 SECONDS AS INDICATED BY UNSAFE NOSE GEAR INDICATION. AS THE CREW PERFORMED A TOWER FLY-BY, THE NOSE GEAR EXTENDED AND THE UNSAJun 19, 1997 · N895US · Fokker F28MK0100 · Landing Gear Retraction/Extension SystemSDR USAAF97012Connector · looseFLT 1475 - BTV-PHL - ON APPROACH TO PHL OVER OUTER MARKER, LANDING GEAR WAS SELECTED DOWN. BLUE GEAR INTRANSIT LIGHTS ILLUMINATED BUT GREEN DOWN AND LOCKED LIGHTS NEVER ILLUMINATED. RECYCLED GEAR TWICE. HEARD GEAR FALL BUT NEVER RECEIVED GREEN LIGHTS. TOWEFeb 3, 1997 · N895US · Fokker F28MK0100 · Landing Gear Position and WarningSDR USAAF97005Cable · failedFLT 1150 - PHL-PWM - DURING APPROACH TO PWM, LANDING GEAR HANDLE WAS STUCK AND WOULD NOT MOVE. FLIGHT DIVERTED TO BOS WHERE MAINTENANCE COULD BE PERFORMED. BEFORE LANDING AT BOS, LANDING GEAR WAS EXTENDED USING ALTERNATE GEAR METHOD. AIRCRAFT LANDED WITHOUT Jan 17, 1997 · N895US · Fokker F28MK0100 · Landing Gear Retraction/Extension SystemSDR 97ZZZM218Skid · failedFLT 1150 - PHL-PWM - DURING APPROACH TO PWM, LANDING GEAR HANDLE WAS STUCK AND WOULD NOT MOVE. FLIGHT DIVERTED TO BOS WHERE MAINTENANCE COULD BE PERFORMED. BEFORE LANDING AT BOS, LANDING GEAR WAS EXTENDED USING ALTERNATE GEAR METHOD. FLIGHT LANDING WITHOUT Jan 17, 1997 · N895US · Fokker F28MK0100 · Landing Gear Retraction/Extension SystemSDR 97ZZZM217Skid · failedFLT 1150 - PHL-PWM - DURING APPROACH TO PWM, LANDING GEAR HANDLE WAS STUCK AND WOULD NOT MOVE. FLIGHT DIVERTED TO BOS WHERE MAINTENANCE COULD BE PERFORMED. BEFORE LANDING AT BOS, LANDING GEAR WAS EXTENDED USING ALTERNATE GEAR METHOD. FLIGHT LANDING WITHOUT Jan 17, 1997 · N895US · Fokker F28MK0100 · Landing Gear Retraction/Extension SystemSDR USAAF97010Retract Mech · lack of lubeFLT 1653 - PWM-PIT - ON APPROACH TO PIT, NOSE GEAR DID NOT COME DOWN ON FIRST ATTEMPT (NO INDICATION AND TOWER SAID NOSE GEAR WAS NOT DOWN). RECYCLED IAW CHECKLIST AND GEAR CAME DOWN NORMALLY THE SECOND TIME. CREW SUSPECTED ICE BUILDUP. FLIGHT LANDED WITHOUTJan 11, 1997 · N895US · Fokker F28MK0100 · Landing Gear Retraction/Extension SystemSDR USAAF96087Battery Pack · dischargedCLT - EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REPLACED ALL EIGHT EMERGENCY LIGHT BATTERY PACKS. (X)Aug 7, 1996 · N895US · Fokker F28MK0100 · Emergency LightingSDR USAAF96012Test Valve · out of positionPIT - AFTER TAKEOFF, CREW RECEIVED LEFT AND RIGHT MAIN LANDING GEAR WARNING ON THE MFDU. THE GEAR WAS CYCLED WITH THE SAME RESULT. FLIGHT RETURNED TO PIT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND THE LANDING GEAR TEST VALVE IN THE TEST POSITIONJan 23, 1996 · N895US · Fokker F28MK0100 · Landing Gear Retraction/Extension System
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