N255US, cancelled Feb 10, 2006

Service difficulty reports · 53

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 = 'N255US' AND deregistration_id = 'N255US-2006-02-10'
  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 GAIA02134OPLight · inoperativeDURING ROUTINE MAINTENANCE AT FWA, IT WAS DISCOVERED THAT THE COCKPIT EMERGENCY EXIT LIGHT WAS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY. OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Sep 25, 2002 · N255US · Boeing 727251 · Emergency LightingSDR GAIA02079OPLight · dischargedDURING ROUTINE MAINTENANCE, IT WAS DISCOVERED THAT THE COCKPIT EMERGENCY EXIT LIGHT WAS INOPERATIVE. C/A: RECHARGED EMERGENCY LIGHT ASSEMBLY FROM THE GROUND POWER UNIT. OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.Aug 9, 2002 · N255US · Boeing 727251 · Emergency LightingSDR GAIA02076OPSmoke Detector · malfunctionedFLT 3706 - FWA-ELP - AFTER TAKEOFF, THE NR 1 SMOKE DETECTOR LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO FWA AND AN UNEVENTFUL LANDING WAS MADE. REMOVED AND REPLACED NR 1 SMOKE DETECTOR. OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETUREND TO SERVICE. (M)Jul 24, 2002 · N255US · Boeing 727251 · Smoke DetectionSDR GAI2002F00002Light · inoperativeDURING ROUTINE MAINTENANCE, IT WAS DISCOVERED THAT THE COCKPIT EMERGENCY EXIT LIGHT WOULD NOT TEST. REMOVED AND REPLACED EMERGENCY EXIT LIGHT. OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.Oct 2, 2001 · N255US · Boeing 727251 · Emergency LightingSDR GAIA01301OPLight · inoperativeDURING MAINTENANCE AT PHL, IT WAS DISCOVERED THAT THE COCKPIT EMERGENCY EXIT LIGHT WAS INOPERATIVE. REMOVED AND REPLACED THE COCKPIT EMERGENCY EXIT LIGHT. OPERATIONALLY CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Aug 24, 2001 · N255US · Boeing 727251 · Emergency LightingSDR GAIA01300OPLight · inoperativeFLT 1705 - IAH-FWA - DURING CRUISE, THE COCKPIT EMERGENCY EXIT LIGHT ILLUMINATED AND THEN DISCHARGED. THE AIRCRAFT CONTINUED TO FWA AND LANDED WITHOUT ANY FURTHER DIFFICULTIES. REMOVED AND REPLACED THE COCKPIT EMERGENCY EXIT LIGHT. OPERATIONALLY CHECKS GOODAug 20, 2001 · N255US · Boeing 727251 · Emergency LightingSDR GAIA00788Wire · brokenFLT 2014 - SLC-BOI - ON LANDING, THE FLIGHT CREW OBSERVED THAT THE LEADING EDGE AMBER LIGHT STAYED ON. NR 4 KRUGER FLAP INDICATED NOT EXTENDED. AN EMERGENCY WAS DECLARED AND AN UNEVENTFUL LANDING WAS MADE AT BOI. UPON INVESTIGATION A BROKEN GROUND WIRE WAS Dec 14, 2000 · N255US · Boeing 727251 · Leading Edge Slat Position Indicating SystemSDR GAIA0064Skin · gougedDURING C-CHECK AT TIMCO/OSC THE FOLLOWING DISCREPANCY WAS FOUND AT STATION 312, THE SKIN WAS FOUND GOUGED AND DENTED BETWEEN STRINGER 20L AND 21L. REPAIRED DAMAGE IAW SRM 51-30-3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Feb 9, 2000 · N255US · Boeing 727251 · Fuselage Main, Plate/SkinSDR GAIA0065Stringer · corrodedDURING C-CHECK AT TIMCO/OSC, THE FOLLOWING DISCREPANCY WAS FOUND AT STATION 360 TO 3790, STRINGER S-18 HAS CORROSION. REPAIRED STRINGER S18 IAW SRM 53-10-3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Feb 9, 2000 · N255US · Boeing 727251 · Fuselage Main, Longeron/StringerSDR GAIA0066Frame · gougedDURING C-CHECK AT TIMC/OSC THE FOLLOWING DISCREPANCY WAS FOUND AT STATION 640, THE FUSELAGE FRAME INBOARD FLANGE WAS FOUND TO BE GOUGED AT STRINGER S-5R. REPAIRED DAMAGED AREA IAW SRM 51-40-3, FIGURE 1. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Feb 9, 2000 · N255US · Boeing 727251 · Fuselage Main, FrameSDR GAIA0067Frame · gougedDURING C-CHECK AT TIMCO/OSC THE FOLLOWING DISCREPANCY WAS FOUND AT STATION 660, THE FUSELAGE FRAME INBOARD FLANGE WAS FOUND TO BE GOUGED AT STRINGER S-5R. REPAIRED DAMAGED AREA IAW SRM 51-40-3, FIGURE 1. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Feb 9, 2000 · N255US · Boeing 727251 · Fuselage Main, FrameSDR GAIA0068Floorbeam · crackedDURING C-CHECK AT TIMCO/OSC THE FOLLOWING DISCREPANCY WAS FOUND AT STATION 294.5, THE FLOORBEAM WEB WAS FOUND TO BE CRACKED AT LBL 54.5. CUT OUT DAMAGED PART OF WEB AND FABRICATED WEB AND DOUBLER. INSTALLED IAW SRM 51-40-2. THE AIRCRAFT WAS RETURNED TO SERVFeb 9, 2000 · N255US · Boeing 727251 · Fuselage Main, Floor BeamSDR GAIA0069Floorbeam · crackedDURING C-CHECK AT TIMCO/OSC THE FOLLOWING DISCREPANCY WAS FOUND AT STATION 948, THE CREASE BEAM WEB WAS FOUND TO BE CRACKED AT LBL 66. REMOVED AND REPLACED WEB IAW SRM 51-20-1 AND 51-30-2. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Feb 9, 2000 · N255US · Boeing 727251 · Fuselage Main, Floor BeamSDR GAIA0070Frame · gougedDURING C-CHECK AT TIMCO/OSC THE FOLLOWING DISCREPANCY WAS FOUND AT STATION 720E, THE FUSELAGE FRAME INBOARD FLANGE WAS FOUND GOUGED AT STRINGER S-5R. REPAIRED IAW SRM 51-40-3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Feb 9, 2000 · N255US · Boeing 727251 · Fuselage Main, FrameSDR GAIA0071Floorbeam · crackedDURING C-CHECK AT TIMCO/OSC THE FOLLOWING DISCREPANCY WAS FOUND AT STATION 848, IT WAS FOUND THAT THE ANGLED STIFFENER AND FLOORBEAM WEB WAS CRACKED THROUGH AT RBL 45. REPAIRED WEB AND REPLACED ANGLE IAW SRM 51-40-2 AND 51-30-2. THE AIRCRAFT WAS RETURNED TO Feb 9, 2000 · N255US · Boeing 727251 · Fuselage Main, Floor BeamSDR GAIA0072Plate · crackedDURING C-CHECK AT TIMCO/OSC THE FOLLOWING DISCREPANCY WAS FOUND AT STATION 940, THE LEFT GEAR WELL PRESSURE DECK HAD CRACK INDICATION AT LBL 30. REPAIRED CRACK IAW SB 727-53-0149 AND BOEING DRAWING 65-89360. THE AIRCRAFT WAS RETURNED TO SERVICE (M)Feb 9, 2000 · N255US · Boeing 727251 · Fuselage Main, Plate/SkinSDR GAIA0073Frame · crackedDURING C-CHECK AT TIMCO/OSC THE FOLLOWING DISCREPANCY WAS FOUND AT STATION 1166, FUSELAGE FRAME WAS FOUND CRACKED AT FLOOR LEVEL ON THE RIGHT SIDE OF AIRCRAFT. REPAIRED CRACKED FRAME IAW SRM 51-40-3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Feb 9, 2000 · N255US · Boeing 727251 · Fuselage Main, FrameSDR GAIA0074Skin · damagedDURING C-CHECK AT TIMCO/OSC THE FOLLOWING DISCREPANCY WAS FOUND AT STATION 370 TO 380, THE SKIN WAS FOUND TO BE CREASED BETWEEN STRINGERS S-17L TO S-18L. REPAIRED SKIN IAW SRM 53-30-3, FIGURE 3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Feb 9, 2000 · N255US · Boeing 727251 · Fuselage Main, Plate/SkinSDR GAIA0075Plate · crackedDURING C-CHECK AT TIMCO/OSC THE FOLLOWING DISCREPANCY WAS FOUND AT STATION 940, IN THE RIGHT WHEEL WELL PRESSURE DECK CRACK WAS FOUND AT RBL 30. REPAIRED CRACK IAW SB 727-53-0149 AND BOEING DRAWING PL65-89360. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Feb 9, 2000 · N255US · Boeing 727251 · Fuselage Main, Plate/SkinSDR GAIA0076Floorbeam · corrodedDURING C-CHECK AT TIMCO/OSC THE FOLLOWING DISCREPANCY WAS FOUND AT STATION 1070, CORROSION WAS FOUND ON THE FLOORBEAM UPPER CHORD REPAIR AT LBL 6. REPAIRED FLOORBEAM UPPER CAP IAW SRM 53-10-8. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Feb 9, 2000 · N255US · Boeing 727251 · Fuselage Main, Floor BeamSDR GAIA0077Fitting · crackedDURING C-CHECK AT TIMCO/OSC THE FOLLOWING DISCREPANCY WAS FOUND AT STATION 870, THE BULKHEAD FITTING BELOW STRINGER S-18R, OUTBOARD FLANGE HAS CRACK INDICATION. REPAIRED CRACK IAW S/B 727-53-0116. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Feb 9, 2000 · N255US · Boeing 727251 · Fuselage Miscellaneous StructureSDR GAIA0078Skin · crackedDURING C-CHECK AT TIMCO/OSC THE FOLLOWING DISCREPANCY WAS FOUND AT STATION 235.8, THE FUSELAGE SKIN HAD A CRACK INDICATION AT WL 215. REPAIRED CRACK IAW SRM 53-30-3, FIGURE 3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Feb 9, 2000 · N255US · Boeing 727251 · Fuselage Main, Plate/SkinSDR GAIA0079Plate · crackedDURING C-CHECK AT TIMCO/OSC, THE FOLLOWING DISCREPANCY WAS FOUND AT STATION 260, THE NOSE WHEEL WELL SIDE WALL HAS CRACK UNDER DOUBLER EXTENDING PAST FASTENER HOLES. INSTALLED DOUBLER IAW SB 727-53-0065. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Feb 9, 2000 · N255US · Boeing 727251 · Fuselage Main, Plate/SkinSDR GAIA0080Frame · gougedDURING C-CHECK AT TIMCO/OSC THE FOLLOWING DISCREPANCY WAS FOUND AT STATION 720D, THE FUSELAGE FRAME INBOARD FLANGE WAS FOUND GOUGED AT STRINGER S-5R. REPAIRED IAW SRM 51-40-3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Feb 9, 2000 · N255US · Boeing 727251 · Fuselage Main, FrameSDR GAIA0081Skin · crackedDURING C-CHECK AT TIMCO/OSC THE FOLLOWING DISCREPANCY WAS FOUND AT STATION 203, A CRACK INDICATION WAS FOUND AT A FASTENER HOLE AT WL 210. REPAIRED IAW SRM 51-30-3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Feb 9, 2000 · N255US · Boeing 727251 · Fuselage Main, Plate/SkinSDR GAIA0082Skin · crackedDURING C-CHECK AT TIMCO/OSC, THE FOLLOWING DISCREPANCY WAS FOUND AT STATION 251.6, A CRACK INDICATION WAS FOUND AT A FASTENER HOLE AT WL 210. REPAIRED IAW SRM 51-30-3. THE AIRCRAFT WS RETURNED TO SERVICE. (M)Feb 9, 2000 · N255US · Boeing 727251 · Fuselage Main, Plate/SkinSDR GAIA0083Frame · gougedDURING C-CHECK AT TIMCO/OSC THE FOLLOWING DISCREPANCY WAS FOUND AT STATION 620, THE FUSELAGE FRAME INBOARD FLANGE WAS FOUND GOUGED AT STRINGER S5R. REPAIRED FRAME IAW SRM 51-40-3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Feb 9, 2000 · N255US · Boeing 727251 · Fuselage Main, FrameSDR GAIA0084Skin · corrodedDURING C-CHECK AT TIMCO/OSC, THE FOLLOWING DISCREPANCY WAS FOUND AT AFT CARGO AFT DOOR INNER SKIN CORROSION WAS FOUND. REPAIRED IAW SRM 51-40-2. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Feb 9, 2000 · N255US · Boeing 727251 · Cargo/Baggage DoorsSDR GAIA0085Skin · crackedDURING C-CHECK AT TIMCO/OSC, THE FOLLOWING DISCREPANCY WAS FOUND AT STATION 235.8, FIVE EACH CRACK INDICATIONS WERE FOUND SKIN AT WL 210 TO 220 RIGHT SIDE. REPAIRED IAW SRM 53-30-3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Feb 9, 2000 · N255US · Boeing 727251 · Fuselage Main, Plate/SkinSDR GAIA0055Floorbeam · crackedDURNG C-CHECK AT TIMCO/OSC, THE FOLLOWING DISCREPANCY WAS FOUND AT STATION 826, THE WEB IN A FLOORBEAM HAS A CRACK AT THE THROUGH HOLE FOR THE ELECTRICAL CONDUIT, RIGHT SIDE. REPAIRED PART IAW TIMCO REO 500041. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Feb 9, 2000 · N255US · Boeing 727251 · Fuselage Main, Floor BeamSDR GAIA0056Seat Track · corrodedDURING C-CHECK AT TIMCO/OSC, THE FOLLOWING DISCREPANCY WAS FOUND AT STATION 710, THE SEAT TRACK AT RBL 24 HAS A SPLICE ANGLE CORRODED. REMOVED AND REPLACED SPLICE ANGLE IAW SRM 53-10-5. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Feb 9, 2000 · N255US · Boeing 727251 · Fuselage, Seat/Cargo Attach FittingsSDR GAIA0057Floorbeam · corrodedDURING C-CHECK AT TIMCO/OSC, THE FOLLOWING DISCREPANCY WAS FOUND AT STATION 1110, THE FLOORBEAM HAS AREAS OF CORROSION AT SCREW HOLES AT LBL 11, LBL 17 AND LBL 20. REPAIRED FLOORBEAM IAW SRM 53-10-0, FIGURE 3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Feb 9, 2000 · N255US · Boeing 727251 · Fuselage Main, Floor BeamSDR GAIA0058Floorbeam · corrodedDURING C-CHECK AT TIMCO/OSC, THE FOLLOWING DISCREPANCY AS FOUND AT STATION 1050, THE FLOORBEAM LOWER CHORD WAS FOUND TO BE CORRODED AT RBL 20 TO RBL 45. REPAIRED LOWER CHORD IAW SRM 53-10-8. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Feb 9, 2000 · N255US · Boeing 727251 · Fuselage Main, Floor BeamSDR GAIA0059Frame · gougedDURING C-CHECK AT TIMCO/OSC, THE FOLLWING DISCREPANCY WAS FOUND. AT STATION 720F, THE FUSELAGE FRAME INBOARD FLANGE WAS FOUND TO GOUGED AT STRINGER S-5R. REPAIRED IAW SRM 51-40-3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Feb 9, 2000 · N255US · Boeing 727251 · Fuselage Main, FrameSDR GAIA0060Floorbeam · corrodedDURNG C-CHECK AT TIMCO/OSC, THE FOLLOWING DISCREPANCY WAS FOUND. AT STATION 1050, THE FLOORBEAM LOWER CHORD AND STABILIZATION STRAP WAS FOUND CORRODED AT RBL 26. CLEANED CORROSION ON LOWER CHORD AND WAS FOUND TO BE WITHIN LIMITS. FABRICATED A NEW STABILIZATFeb 9, 2000 · N255US · Boeing 727251 · Fuselage Main, Floor BeamSDR GAIA0061Seat Track · corrodedDURING C-CHECK AT TIMCO/OSC, THE FOLLOWING DISCREPANCY WAS FOUND. AT STATION 760 TO 848, THE SEAT TRACK WAS FOUND TO HAVE CORROSION AROUND FASTENERS AT LBL 45. REMOVED AND REPLACED SEAT IAW SRM 53-10-5. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Feb 9, 2000 · N255US · Boeing 727251 · Fuselage, Seat/Cargo Attach FittingsSDR GAIA0062Stringer · corrodedDURING C-CHECK AT TIMCO/OSC, THE FOLLOWING DISCREPANCY WAS FOUND. AT THE AFT CARGO FORWARD DOOR SILL, CORROSION WAS FOUND BETWEEN DOOR LATCH FITTINGS. REPAIRED DAMAGED STRINGER IAW TIMCO DRAWING TIO-B727-006, DATED 1-22-00. THE AIRCRAFT WAS RETURNED TO SERVFeb 9, 2000 · N255US · Boeing 727251 · Fuselage Main, Longeron/StringerSDR GAIA0063Floorbeam · corrodedDURING C-CHECK AT TIMCO/OSC, THE FOLLOWING DISCREPANCY WAS FOUND. AT STATION 1130, THE FLOORBEAM CAP AT LBL 30 HAS CORROSION AT SCREW HOLES. INSTALLED REPAIR IAW TIMCO DRAWING TIO-B727-00005, DATED 1-17-2000. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Feb 9, 2000 · N255US · Boeing 727251 · Fuselage Main, Floor BeamSDR GAIA0086Skin · gougedDURING C-CHECK AT TIMCO/OSC, THE FOLLOWING DISCREPANCY WAS FOUND. AT STATION 1090, A GOUGE WAS FOUND IN THE SKIN AT STRINGER S3L. REPAIRED IAW SRM 53-30-3, FIGURE 1. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Feb 9, 2000 · N255US · Boeing 727251 · Fuselage Main, Plate/SkinSDR GAIA0087Skin · damagedDURING C-CHECK AT TIMCO/OSC, THE FOLLOWING DISCREPANCY WAS FOUND. AT AFT CARGO AFT DOOR A HOLE WAS FOUND. REPAIRED IAW SRM 51-40-2. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Feb 9, 2000 · N255US · Boeing 727251 · Cargo/Baggage DoorsSDR GAIA99229Lamp · inoperativeDURNIG ROUTINE MAINTENANCE IN DEN, IT WAS DISCOVERED THAT THE EMERGENCY EXIT LIGHTS AT THE MAIN ENTRANCE DOOR WERE INOPERATIVE. RELAMPED THE EMERGENCY EXIT LIGHTS AT THE MAIN ENTRANCE DOOR. OPERATIONALLY CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (Dec 3, 1999 · N255US · Boeing 727251 · Emergency LightingSDR GAIA9933Light · inoperativeFOUND DURING POSTFLIGHT INSPECTION, THE EMERGENCY EXIT LIGHT IN COCKPIT DIM AND INTERMITTENT. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. OPERATIONAL CHECKS GOOD. RETURNED THE AIRCRAFT TO SERVICE. (M)Feb 9, 1999 · N255US · Boeing 727251 · Emergency LightingSDR CKSA97317Accessory Unit · malfunctionRIGHT MAIN GEAR EXTENDED BY EMERGENCY GEAR EXTENSION SYSTEM. RIGHT GEAR UNSAFE INDICATION AFTER NORMAL EXTENSION. TROUBLESHOT MAIN LANDING GEAR SYSTEM, REMOVED AND REPLACED LANDING GEAR ACCESSORY UNIT AND OPS CHECKED IN IAW MM 32-09-121. SWUNG GEAR SYSTEM, Jul 3, 1997 · N255US · Boeing 727251 · Landing Gear Position and WarningSDR CKSA96405Bolt · wornON TAKEOFF, LEFT MAIN GEAR SHOWED LEFT GEAR RED LIGHT AND LEFT GEAR GREEN LIGHT. CYCLED GEAR, NO HELP. ON LANDING 3 GREEN, NO RED LIGHTS FORWARD PANEL SECONDARY GEAR INDICATION, NO GREEN ON LEFT MAIN GEAR OPERATED NORMALLY THROUGH FLIGHT. FOUND LEFT HAND MADec 20, 1996 · N255US · Boeing 727251 · Landing Gear Door ActuatorSDR 9612082255Start Valve · failedDURING CRUISE FLIGHT, THE NR 1 ENGINE START VALVE LIGHT CAME ON. NR 1 ENGINE SHUT DOWN. AIRCRAFT COMPLETED SCHEDULED FLIGHT TO DTW AND LANDED WITHOUT FURTHER EVENT. ENGINE WINDMILL INSPECTION C/W, MAIN OIL STRAINER AND MAG PLUGS CHECKED OK. STARTER, START Jun 2, 1996 · N255US · Boeing 727251 · Engine Start Valves/ControlsSDR 9612752255Frame · crackedDURING L-CHECK, FOUND A CRACK IN THE BS 870 FRAME BELOW STR 13R. REPAIRED FRAME PER EA B727-53-002.May 25, 1996 · N255US · Boeing 727251 · Fuselage Main, FrameSDR 9519932255Ind Switch · malfunctionedDURING APPROACH ON LANDING GEAR EXTENSION, NO GREEN LIGHTS ILLUMINATED, JUST ONE RED GEAR LIGHT. RECYCLED GEAR, TWO GREEN MAIN ON AND THIRTY SECONDS LATER NOSE GREEN LIGHT ILLUMINATED. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED SWITCHES AT S93 AND S96 AND LDec 8, 1995 · N255US · Boeing 727251 · Landing Gear Position and WarningSDR 9514392255Oil Filter · dirtyNR 1 ENGINE OIL FILTER CLOG WARNING LIGHT ILLUMINATED ON TAKEOFF. THE TAKEOFF WAS ABORTED AND AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE OIL FILTER, AIRCRAFT WAS RUNUP AND SYSTEM CHECKED OK.Sep 20, 1995 · N255US · Boeing 727251 · Turbine Engine Oil SystemSDR 9510842255Epr Transmitter · malfunctionedNR 1 EPR INDICATION DID NOT REACH TARGET EPR ON TAKEOFF ROLL. THE TAKEOFF WAS ABORTED, THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE EPR TRANSMITTER AND INDICATOR. SYSTEM CHECKED OK ON RUNUP. AIRCRAFT RETURNED TO SERVICE.Jul 17, 1995 · N255US · Boeing 727251 · Engine Pressure Ratio (EPR)SDR 9511822252Prbc · malfunctionedNR 1 ENGINE HAD LOW FREQUENCY VIBRATION AT POWER SETTINGS ABOVE 70 PERCENT N2. FLIGHT RETURNED TO DTW WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE PRBC AND TESTED THE ENGINE. ENGINE PERFORMANCE WAS SATISFACTORY. AIRCRAFT RETURNED TO SERVICE.Jul 4, 1995 · N255US · Boeing 727251 · Compressor Bleed Valve
Back to N255US, cancelled Feb 10, 2006