# Service difficulty reports: N895US, cancelled Sep 27, 2007 A list on [N895US, cancelled Sep 27, 2007](https://openairdocs.org/deregistered/N895US-2007-09-27.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR USAAF01040](https://openairdocs.org/sdr/USAAF01040.md): Battery Pack · inoperative · Jun 30, 2001 · N895US · Fokker F28MK0100 · Emergency Lighting > IND- 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) - [SDR USAAF01035](https://openairdocs.org/sdr/USAAF01035.md): Battery Pack · discharged · Jun 25, 2001 · N895US · Fokker F28MK0100 · Emergency Lighting > IND - 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) - [SDR USAAF99036](https://openairdocs.org/sdr/USAAF99036.md): Modulating Valve · failed · Jul 20, 1999 · N895US · Fokker F28MK0100 · Cabin Cooling System > PHL - 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) - [SDR USAAF99020](https://openairdocs.org/sdr/USAAF99020.md): O-Ring · leaking · Apr 5, 1999 · N895US · Fokker F28MK0100 · Hydraulic System, Main > BOS - 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 44 - [SDR USAA980595](https://openairdocs.org/sdr/USAA980595.md): Skin · delaminated · Nov 13, 1998 · N895US · Fokker F28MK0100 · Fuselage Main, Plate/Skin > PIT - 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) - [SDR USAA980594](https://openairdocs.org/sdr/USAA980594.md): Beam · corroded · Nov 13, 1998 · N895US · Fokker F28MK0100 · Fuselage Miscellaneous Structure > PIT - 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) - [SDR USAA980593](https://openairdocs.org/sdr/USAA980593.md): Frame · cracked · Nov 13, 1998 · N895US · Fokker F28MK0100 · Fuselage Main, Frame > PIT - 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) - [SDR USAAF98085](https://openairdocs.org/sdr/USAAF98085.md): Valve · out of adjust · Oct 9, 1998 · N895US · Fokker F28MK0100 · Landing Gear Retraction/Extension System > BNA - 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 T - [SDR USAAF98084](https://openairdocs.org/sdr/USAAF98084.md): Sensor · out of adjust · Oct 8, 1998 · N895US · Fokker F28MK0100 · Drag Control System > CLT - 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 LIFTDUMP - [SDR USAAF98083](https://openairdocs.org/sdr/USAAF98083.md): Light · inoperative · Sep 23, 1998 · N895US · Fokker F28MK0100 · Emergency Lighting > GSO - FORWARD EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE FOUND PIN PUSHED BACK IN CONNECTOR P3858B. THE REPOSITIONED THE PIN IN THE CONNECTOR. (M) - [SDR USAAF97050](https://openairdocs.org/sdr/USAAF97050.md): Retract Mech · lack of lube · Jun 19, 1997 · N895US · Fokker F28MK0100 · Landing Gear Retraction/Extension System > DTW/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 UNSA - [SDR USAAF97012](https://openairdocs.org/sdr/USAAF97012.md): Connector · loose · Feb 3, 1997 · N895US · Fokker F28MK0100 · Landing Gear Position and Warning > FLT 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. TOWE - [SDR USAAF97005](https://openairdocs.org/sdr/USAAF97005.md): Cable · failed · Jan 17, 1997 · N895US · Fokker F28MK0100 · Landing Gear Retraction/Extension System > FLT 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 - [SDR 97ZZZM218](https://openairdocs.org/sdr/97ZZZM218.md): Skid · failed · Jan 17, 1997 · N895US · Fokker F28MK0100 · Landing Gear Retraction/Extension System > FLT 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 - [SDR 97ZZZM217](https://openairdocs.org/sdr/97ZZZM217.md): Skid · failed · Jan 17, 1997 · N895US · Fokker F28MK0100 · Landing Gear Retraction/Extension System > FLT 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 - [SDR USAAF97010](https://openairdocs.org/sdr/USAAF97010.md): Retract Mech · lack of lube · Jan 11, 1997 · N895US · Fokker F28MK0100 · Landing Gear Retraction/Extension System > FLT 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 WITHOUT - [SDR USAAF96087](https://openairdocs.org/sdr/USAAF96087.md): Battery Pack · discharged · Aug 7, 1996 · N895US · Fokker F28MK0100 · Emergency Lighting > CLT - EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REPLACED ALL EIGHT EMERGENCY LIGHT BATTERY PACKS. (X) - [SDR USAAF96012](https://openairdocs.org/sdr/USAAF96012.md): Test Valve · out of position · Jan 23, 1996 · N895US · Fokker F28MK0100 · Landing Gear Retraction/Extension System > PIT - 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 POSITION ## 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 = 'N895US' AND deregistration_id = 'N895US-2007-09-27' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N895US-2007-09-27/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.