N894US, cancelled Aug 10, 2007

Service difficulty reports · 27

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 = 'N894US' AND deregistration_id = 'N894US-2007-08-10'
  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 USAAF01079Light · inoperativePIT - A FIRST CLASS SECTION OF THE FLOOR PROXIMITY EMERGENCY LIGHTS WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT SECTION. (M)Oct 16, 2001 · N894US · Fokker F28MK0100 · Emergency LightingSDR USAAF00047Warning Light · false indicationCLT-SAV - FLT 2395 - THE APU FIRE WARNING ILLUMINATED, WITH SUBSEQUENT FIRE BOTTLE DISCHARGE, AFTER THE SPEEDBRAKE WAS DEPLOYED DURING DESCENT. THE FLIGHT LANDED WITHOUT INCIDENT. (M)Jun 17, 2000 · N894US · Fokker F28MK0100 · Fire DetectionSDR USAAF99015Roller · out of positionPIT - FLT 864 - AFTER DEPARTURE FROM PIT, THERE WAS AN EXCESSIVE AMOUNT OF AIR NOISE FROM THE LEFT SLIDING WINDOW EVEN THOUGH THE WINDOW WAS CLOSED AND LOCKED. FLIGHT RETURNED AND LANDED AT PIT WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE AFT ROLLER WAS OMar 17, 1999 · N894US · Fokker F28MK0100 · Flight Compartment WindowsSDR USAA980493Mount · corrodedPIT - DURING Q1 CHECK, FOUND CORROSION AT GIRT BAR MOUNT BEYOND LIMITS, 1 INCH BY .50 INCH AT STA 4850 AFT SIDE MED. REPAIRED PER SRM CHAPTER 51. (X)Sep 29, 1998 · N894US · Fokker F28MK0100 · Emergency EquipmentSDR USAA980492Floor Beam · corrodedPIT - DURING Q1 CHECK, FOUND .50 INCH BY 2 INCH FLOOR BEAM CORRODED AT STA 3870 - STA 4610, AT BL 600R. FABRICATED NEW PARTS FROM 2024-T-3, .032 INCH ANGLES AND STRIPS 204-T-3, .040 INCH DWG II A23622, A22271, D23695 AND D23699, FIG 09, FLOOR BEAM 600R. REPASep 29, 1998 · N894US · Fokker F28MK0100 · Fuselage Main, Floor BeamSDR USAA980491Mount · corrodedPIT - DURING Q1 CHECK, FOUND GALLEY 2 INBOARD MOUNT EXCESSIVLEY CORRODED, .50 INCH BY .25 INCH AREA AT STA 4850 - STA 5305. REPAIRED PER SRM 51-70-00. (X)Sep 29, 1998 · N894US · Fokker F28MK0100 · Fuselage Miscellaneous StructureSDR USAA980490Rail · corrodedPIT - DURING Q1 CHECK, FOUND LIGHT CORROSION (.50 INCH BY 12 INCH AREA) FORWARD SECTION OF CARGO RT TIE DOWN RAIL AFT. SECTION NEEDS REPLACED AT STA 18921 TO STA 22236. CORROSION TREATED FROM STA 18921 TO STA 22236 AND REPLACED FRAMES 22236 TO 22706. REPLACESep 29, 1998 · N894US · Fokker F28MK0100 · Fuselage, Seat/Cargo Attach FittingsSDR USAA980489Beam · corrodedPIT - DURING Q1 CHECK, FOUND BL ZERO CORRODED THROUGH AT STA 3870, 1 INCH BY .50 INCH AREA, T-CAP (BEAM). REPAIRED PER SRMS 51-70-06. (X)Sep 29, 1998 · N894US · Fokker F28MK0100 · Fuselage Miscellaneous StructureSDR USAA980488Beam · corrodedPIT - DURING Q1 CHECK, FOUND BEAM CORRODED THROUGH AT STA 3820 (1 INCH BY 1 INCH AREA) AT BL 1127R. REPAIRED PER SRM CHAPTER 51. (X)Sep 29, 1998 · N894US · Fokker F28MK0100 · Fuselage Miscellaneous StructureSDR USAA980487Beam · corrodedPIT - DURING Q1 CHECK, FOUND CORROSION BEYOND LIMITS AFTER REMOVAL ON BEAM (3 INCHES BY .50 INCH AREA), AT BL 600R AT STA 3870 - STA 4610. REPAIRED PER SRM 53-12-10, FIG 09. (X)Sep 29, 1998 · N894US · Fokker F28MK0100 · Fuselage Miscellaneous StructureSDR USAA980479Door Pan · crackedPIT - DURING Q1 CHECK, FOUND .5 INCH CRACK AFT CARGO DOOR PAN AT PAN AFT EDGE BELOW LATCH CAM ARM. INSTALLED DOUBLER PER SRM 52-05 FIG 35A. (M)Sep 29, 1998 · N894US · Fokker F28MK0100 · Fuselage Miscellaneous StructureSDR USAA980478Beam · corrodedPIT - DURING Q-1 CHECK, FOUND 29.125 INCH LONG 740MM CORRODED T-CAP BEYOND LIMITS AT T-CAP AT BL 1127R STATION 3870-4610. REPLACED T-CAP PER SRM CHAPTER 51. (M)Sep 29, 1998 · N894US · Fokker F28MK0100 · Fuselage Miscellaneous StructureSDR USAA980477Beam · corrodedPIT - DURING Q-1 CHECK, FOUND 38.625 INCH 980 MM CORRODED BEAM CORRODED BEYOND LIMITS MED FLOOR THRESHOLD SUPPORT AT STATION 3870-4850. REPLACED SUPPORT PER SRM CHAPTER 51. (M)Sep 29, 1998 · N894US · Fokker F28MK0100 · Fuselage Miscellaneous StructureSDR USAA980476Beam · corrodedPIT - DURING Q-1 CHECK, FOUND HEAVY CORROSION ON BEAM 24 INCHES LONG AT VALET AREA BL 475 AT STATION 5600-6600. REMOVED AND REPLACED PER SRM 51-70-06. (M)Sep 29, 1998 · N894US · Fokker F28MK0100 · Fuselage Miscellaneous StructureSDR USAA980475Beam · corrodedPIT - DURING Q-1 CHECK, FOUND CORRODED MATERIAL 29.125 INCH 740MM AT BL 1127L STATION 3870-4610 T-CAP CORRODED BEYOND LIMIT. REPLACED T-CAP PER SRM CHAPTER 51. (M)Sep 29, 1998 · N894US · Fokker F28MK0100 · Fuselage Miscellaneous StructureSDR USAA980474Skin · disbondedPIT - DURING Q-1 CHECK, FOUND DISBONDING 1.5 INCH BY 1.5 INCH AT SEAT AND 16 INCH BY 4.5 INCH STRINGER AT STATION 24011 AND 24611 WITHIN STRINGERS 21A AND 23 ON SKIN. FILLED CAVITY WITH SEALANT AND APPLIED RIVETS TO DISBOND AREA, PER EA NR 29417E. (M)Sep 29, 1998 · N894US · Fokker F28MK0100 · Fuselage Main, Plate/SkinSDR USAA980428Beam · crackedPIT - DURING Q1 CHECK, FOUND CORROSION FROM STA 4610 - STA 6030 BEAM BL 1127R, 1 INCH BY 3 INCH AREA. CORROSION ENTIRE LENGTH, DEEP AREA AT END OF SPLICE HAS .008 INCH METAL LEFT. (X)Sep 29, 1998 · N894US · Fokker F28MK0100 · Fuselage Miscellaneous StructureSDR USAAF98040Battery Pack · dischargedGSO - CENTER SECTION OF FLOOR LEVEL EMERGENCY LIGHTING INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK. (X)May 9, 1998 · N894US · Fokker F28MK0100 · Emergency LightingSDR USAAF98014Upstop · failedPIT - FLT 0864 - AFTER TAKEOFF FROM PIT, THE RT MLG WOULD NOT RETRACT. FLIGHT RETURNED TO PIT WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND MLG UPSTOP DAMPER (RS) MALFUNCTIONING. SERVICED UPSTOP DAMPER PER F100 MM 32-11-05. PERFORMED OPERATFeb 9, 1998 · N894US · Fokker F28MK0100 · Landing Gear Retraction/Extension SystemSDR USAAF97087Sensor · looseFLT 1546 AND FLT 527 - ORF - BOTH FLIGHTS RETURNED TO ORF DUE TO LANDING GEAR PROBLEMS. ON BOTH OCCASIONS AFTER TAKEOFF FROM ORF, WHEN THE LANDING GEAR WAS RETRACTED, THE INTRANSIT LIGHT REMAINED LIT AND A 'RT MLG' WARNING ANNUNCIATED ON THE MULTIFUNCTION DISNov 6, 1997 · N894US · Fokker F28MK0100 · Landing Gear Position and WarningSDR USAAF97083Valve · failedPIT/BOS - FLT 1696 - AT FL 330, RECEIVED 3 CHIME ALARM INDICATING THE CABIN ALTITUDE WAS CLIMBING. CAPTAIN PERFORMED EMERGENCY DESCENT TO 10,000 FEET. THE MAXIMUM CABIN ALTITUDE WAS 13,000 FEET. THE OXYGEN MASKS DID NOT DEPLOY. AT 10,000 FEET, CABIN DIFFEROct 19, 1997 · N894US · Fokker F28MK0100 · Cabin Pressure Control SystemSDR USAAF97081Switch · failedFLT 8077 - IND-MSP - ON CLIMB-OUT FROM IND, RUD2 FAULT ANNUNCIATED ON MFDU. FLIGHT RETURNED TO IND WITHOUT INCIDENT. MAINTENANCE REPLACED NR 2 ACTUATOR STICKING SWITCH. (M)Oct 14, 1997 · N894US · Fokker F28MK0100 · Rudder Control SystemSDR USAAF97082Manifold · failedFLT 8078 - IND-PHL - EN ROUTE TO PHL, RUD2 FAULT ANNUNCIATED ON MFDU. FLIGHT DIVERTED TO RIC FOR MAINTEANCE CONVENIENCE. FLIGHT LANDED RIC WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 2 RUDDER MANIFOLD. (M)Oct 13, 1997 · N894US · Fokker F28MK0100 · Rudder Control SystemSDR USAAF96069Battery Pack · dischargedPIT - FOUND EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE RESET THE EMERGENCY LIGHT CIRCUIT BREAKERS AND REPLACED THE MAIN ENTRANCE DOOR EXIT SIGN BATTERY PACK. (M)Jun 29, 1996 · N894US · Fokker F28MK0100 · Emergency LightingSDR USAA951040Prox Sensor · misalignedGSO - FLIGHT NR 1794 - AFTER TAKEOFF, LANDING GEAR WOULD NOT RETRACT. GROUND FLIGHT FAULT ON MULTI FUNCTION DISPLAY UNIT. RETURNED TO GSO FOR LANDING. FOUND PROXIMITY SENSORS ON LEFT GEAR FOR FLT GROUND OUT OF ADJUSTMENT. ADJUSTED BOTH FLT GROUND PROXIMITYSep 29, 1995 · N894US · Fokker F28MK0100 · Landing Gear Position and WarningSDR USAA950651Fire Wire · chafedPIT - FLT 348 - AFTER TAKEOFF, THE APU FIRE LIGHT ILLUMINATED. THE CAPTAIN DISCHARGED THE BOTTLES AND THE LIGHT EXTINGUISHED. FLIGHT RETURNED TO PIT. MAINTENANCE FOUND THE APU FIRE DETECTION WIRE CHAFED THROUGH. THE DETECTION ELEMENT, FIRE BOTTLE AND FIRE Jun 27, 1995 · N894US · Fokker F28MK0100 · Fire DetectionSDR USAA950088Eel Batt Pack · dischargedPIT - FLT 883 - DURING PREFLIGHT, FOUND FLT DECK EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED BATTERY PACK, OPERATION CHECKS NORMAL. (W)Feb 5, 1995 · N894US · Fokker F28MK0100 · Emergency Lighting
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