Boeing 727-254

Service difficulty reports · 149

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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 aircraft_model_key = '727254'
  ORDER BY difficulty_date DESC"

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SDR USAA119907Socket · missingFLT 6359 - LGA-DCA - FOUND ON POST FLIGHT INSPECTION, ON WHITE EPL LIGHT MISSING AT ROW 5 DEF. REPLACED EPL LIGHT SOCKET ASSEMBLY AND LENS ASSEMBLY. (M)Nov 15, 1999 · N912TS · Boeing 727254 · Emergency LightingSDR 99ZZZM801Lens · missingFLT 6359 - LGA-DCA - FOUND ON POST FLIGHT INSPECTION, ON WHITE EPL LIGHT MISSING AT ROW 5 DEF. REPLACED EPL LIGHT SOCKET ASSEMBLY AND LENS ASSEMBLY. (M)Nov 15, 1999 · N912TS · Boeing 727254 · Emergency LightingSDR USAA119906Light · corrodedOVERNIGHT L/S DCA- EMERGENCY LIGHT INOPERATIVE RIGHT OVERWING EXIT. CLEANED CORROSION FROM LIGHT SOCKETS. OPERATIONAL CHECK NORMAL. (M)Nov 12, 1999 · N916TS · Boeing 727254 · Emergency LightingSDR USAA119905Light · inoperativeFLT 6364 - DCA-LGA - ESCAPE PATH LIGHTING AT SEAT 10D INOPERATIVE. INSTALLED EPL LIGHT ASSEMBLY, OPERATIONAL CHECK NORMAL. (M)Nov 12, 1999 · N912TS · Boeing 727254 · Emergency LightingSDR USAA119904Light · inoperativeOVERNIGHT L/S DCA - AFT AIRSTAIR EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED EMERGENCY EXIT LIGHTS ASSEMBLY. OPERATIONAL CHECK NORMAL. (M)Nov 12, 1999 · N916TS · Boeing 727254 · Emergency LightingSDR USAA119902Lens · missingFLT 6376 - DCA-LGA - EMERGENCY PATH LIGHTING HAS ONE LIGHT OUT ADJACENT TO ROW 10. REPLACED MISSING LENS. (M)Nov 12, 1999 · N912TS · Boeing 727254 · Emergency LightingSDR USAA119901Battery Pack · dischargedEMERGENCY EXIT LIGHTS AT L-1 DOOR AND COCKPIT DOOR WON'T TEST. REPLACED EMERGENCY EXIT LIGHTS (S/N 2019 AND 4459) AT L-1 DOOR AND COCKPIT DOOR. (M)Nov 6, 1999 · N913TS · Boeing 727254 · Emergency LightingSDR USAA109903Accessory Unit · inoperativeFLT 6050 - LGA-BOS - HAD TO USE GEAR TRIGGER TO RAISE GEAR. OIL COOLER CSD RETURNED TO NORMAL WHEN FLAPS RAISED FROM 5-2 DEGREES. AURAL WARNING SOUNDED. HAD TO PULL C/B TO SILENCE HORN. ALL OTHER INDICATIONS NORMAL. T/S TO LANDING GEAR ACCESSORY UNIT, REPOct 14, 1999 · N916TS · Boeing 727254 · Landing Gear Position and WarningSDR USAA109901Pump · failedFLT 6470 - DCA-LGA - ON TAKEOFF, DURING GEAR RETRACTION, NR 3 ENGINE FAILED. EMERGENCY DECLARED, RETURNED TO DCA. REPLACED NR 3 ENGINE DRIVEN FUEL PUMP. (M)Oct 2, 1999 · N913TS · Boeing 727254 · Engine Fuel PumpSDR USAA099903Smoke Detector · failedFLT 6511 - LGA-DCA - FORWARD LAVATORY SMOKE DETECTOR INOPERATIVE. REPLACED SMOKE DETECTOR. OPERATIONAL CHECK NORMAL. (M)Sep 17, 1999 · N913TS · Boeing 727254 · Smoke DetectionSDR USAA079901Battery Pack · dischargedRIGHT FORWARD OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK OPERATIONAL CHECK OK. (M)Jul 21, 1999 · N916TS · Boeing 727254 · Emergency LightingSDR USAA069943Accumulator · rupturedSYSTEM 'B FAILURE EN ROUTE TO LGA. AS PER ABNORMAL, SAFETY WIRE BROKEN ON GPWS AND PNEUMATIC BRAKE. FOUND BRAKE ACCUMULATOR RUPTURED. REPLACED SAME PER MM 29-32-40. RESAFTIED GPWS SWITCH AND PNEUMATIC BRAKE HANDLE. BLED PNEUMATIC BRAKE LINE PER MM 32-43-0Jun 13, 1999 · N912TS · Boeing 727254 · Hydraulic Power Accumulator, MainSDR USAA069942Fuel Control · malfunctionedFLT 6461 - LGA-DCA - AT 10,000 FT CRUISE, PULLED ALL POWER LEVERS TO IDLE. NR 3 WENT TO FULL POWER, NO CONTROL WITH POWER LEVER. ENGINE LIMITS NOT EXCEEDED. SHUT DOWN ENGINE. 10 MINUTES WINDMILL AT 15 PSI OIL PRESSURE. REPLACED NR 3 ENGINE FUEL CONTROL PEJun 9, 1999 · N914TS · Boeing 727254 · Fuel Control/Turbine EnginesSDR USAA049905Duct · damagedFLT 6520- DCA-LGA - AIR RETURN TO DCA - NR 1 ENGINE FIRE LIGHT ILLUMINATED ON TAKEOFF, REDUCED THROTTLE TO IDLE, LIGHT EXTINGUISHED MOMENTARILY. RANCID SMELL IN CABIN, NO SECONDARY ENGINE INDICATIONS. REPLACED 8TH STAGE DUCT. (M)Apr 15, 1999 · N916TS · Boeing 727254 · Pneumatic Distribution SystemSDR USAA049902Light · inoperativeCOCKPIT DOOR EMERGENCY EXIT LIGHT WOULD NOT WORK. REPLACED LIGHT ASSEMBLY, OPERATIONAL CHECK NORMAL. (M)Apr 3, 1999 · N913TS · Boeing 727254 · Emergency LightingSDR USAA039914Module · leakingFLT 6470 - DCA-LGA - EN ROUTE LOST ALL SYSTEM 'A' HYDRAULIC FLUID. EMERGENCY DECLARED. MANUAL LANDING GEAR EXTENSION PERFORMED. FOUND SYSTEM 'A' AILERON MODULAR PACKAGE SEPARATED. REPLACED AILERON PACKAGE PER MM 27-10-141. REPLACED NR 1 AND NR 2 ENGINE HYMar 19, 1999 · N916TS · Boeing 727254 · Hydraulic System, MainSDR USAA039902Coalescer · dirtyFLT 6161 - BOS-LGA - ON APPROACH, FLIGHT ATTENDANTS REPORT A BURNING SMELL IN FORWARD CABIN BY L1 DOOR. SMELL WAS BURNING PLASTIC OR WAX LIKE ORDER. TROUBLESHOT SMELL TO DEICING/ANTI-ICING FLUID IN RIGHT PACK SYSTEM. REPLACED RIGHT WATER SEPARATOR BAG PER MMar 9, 1999 · N913TS · Boeing 727254 · Humidity Control SystemSDR USAA069909Web · crackedNOSE WHEEL WELL PRESSURE WEB CRACKED ONE INCH ABOVE RIGHT AFT ACCESS PANEL. INSTALLED REPAIR AT NOSE WHEEL WELL PRESSURE WEB, ABOVE RIGHT AFT ACCESS PANEL. MATERIAL USED, 2024-T3, .050 INCH, 11 INCH BY 8 INCH. REPAIR ACCOMPLISHED IAW SB 727-53-0145. (M)Mar 6, 1999 · N913TS · Boeing 727254 · Fuselage Miscellaneous StructureSDR USAA069908Strap · crackedCRACKS ON CIRCUMFERENTIAL SPLICE STRAP BS 930, STRINGER 14R. INSTALLED FUSELAGE FRAME REPAIR AT BS 930, STRINGER 14R. MATERIAL USED, 7075-T6, .125 INCH, 14.5 INCH BY 1.25 INCH. REPAIR ACCOMPLISHED IAW SB 727-53-0162. (M)Mar 6, 1999 · N913TS · Boeing 727254 · Fuselage Miscellaneous StructureSDR USAA069907Circumferential · crackedCRACK ON CIRCUMFERENTIAL AT BS 930 STRINGER 13L. INSTALLED FUSELAGE FRAME REPAIR AT BS 930 BETWEEN STRINGER 11 AND STRINGER 12, AND BETWEEN STRINGER 13 AND STRINGER 14 LEFT. MATERIAL USED, 7075-T6, .125 INCH, 14.5 INCH BY 1.25 INCH. REPAIR INSTALLED IAW SB Mar 6, 1999 · N913TS · Boeing 727254 · Fuselage Main, FrameSDR USAA069906Skin · corrodedEXTERIOR SKIN HAS POPPED RIVET HEAD (MISSING) STATION 720D AT STRINGER 28L. INSTALLED FUSELAGE EXTERIOR SKIN REPAIR AT BSB 720D, STRINGER 28L. MATERIAL USED 7075-T6, .125 INCH, 17 INCH BY 13.5 INCH. REPAIR ACCOMPLISHED IAW SRM 53-30-3 FIG 1. (M)Mar 6, 1999 · N913TS · Boeing 727254 · Fuselage Main, Plate/SkinSDR USAA069905Skin · corrodedEVIDENCE OF CORROSION AT BS 351 STRINGER 26R EXTERIOR. INSTALLED FUSEALGE EXTERIOR SKIN REPAIR AT BS 351, STRINGER 26R. MATERIAL USED, 2024-T3, .063 INCH , 19 INCH BY 11 INCH. REPAIR ACCOMPLISHED IAW SRM 53-30-3 FIG 1. (M)Mar 6, 1999 · N913TS · Boeing 727254 · Fuselage Main, Plate/SkinSDR USAA029905Drive Motor · failed'A' SYSTEM HYDRAULICS WENT OT ZERO DURING CLIMB-OUT. PERFORMED ABNORMAL CHECK LIST, GEAR AND FLAPS WERE LOWERED USING ALTERNATE METHOD. REPLACED HYDRAULIC FLAP DRIVE MOTOR PER MM 27-51-62 DUE TO LEAK. REPLACED NR 1 ENGINE DRIVEN HYDRAULIC FLAP DRIVE MOTOR PFeb 8, 1999 · N912TS · Boeing 727254 · Trailing Edge Flap ActuatorSDR USAA129808Engine · vibratesNR 1 ENGINE VIBRATION ABNORMAL ON START BETWEEN 35-45 PERCENT N2. AT REDUCED TAKEOFF POWER 1.81 EPR, N1 INDICATION 96 PERCENT VS 91 PERCENT ON NR 2 AND NR 3 ENGINES. IN FLIGHT VIBRATION IN TAIL SECTION OF CABIN NOTED. EMERGENCY WAS NOT DECLARED, ENGINE WAS Dec 19, 1998 · N913TS · Boeing 727254 · Engine (Turbine/Turboprop)SDR USAA129810JFloorbeam · corrosionCABIN FLOOR STRUCTURE BEAM UPPER FLANGE, LOWER SECTION BS 1148, AT RBL 12 EVIDENCE OF CORROSION. INSTALLED REPAIR ON CABIN FLOORBEAM UPPER FLANGE BS 1148, RBL 12. ACCOMPLISHED IAW 727 SRM 53-10-8, FIG 8. MATERIAL USED 7075T-6, .090 INCH.Dec 17, 1998 · N916TS · Boeing 727254 · Fuselage Main, Floor BeamSDR USAA129810ISkin · damagedFUSELAGE EXTERIOR - TEMPORARY PLUG REPAIR INSTALLED IN FUSELAGE SKIN BETWEEN BS 950D AND BS 950E, BETWEEN STR 22R AND STR 23R. INSTALLED FLUSH REPAIR AT FUSELAGE EXTERIOR SKIN BETWEEN BS 950D AND BS 950E, STR 22R AND STR 23R. ACCOMPLISHED IAW B727 SRM 53-30-Dec 17, 1998 · N916TS · Boeing 727254 · Fuselage Main, Plate/SkinSDR USAA129810HSkin · corrodedBULGE ON FUSELAGE EXTERIOR SKIN LEFT HAND SIDE STA 1183, BETWEEN STR 20 AND STR 22 NEXT TO LAVATORY SERVICE PANEL. INSTALLED STRINGER AND EXTERNAL DOUBLER REPAIR AT LEFT HAND BS 1183 FROM STR 20L TO STR 22L. ACCOMPLISHED IAW AVITAS ENGINEERING ORDER NR 98PMSDec 17, 1998 · N916TS · Boeing 727254 · Fuselage Main, Plate/SkinSDR USAA129810GFrame · crackedRIGHT CABIN FRAME STA 930 CRACKED BETWEEN STR 14R - STR 15R BELOW CABIN WINDOW. ACCOMPLISHED RIGHT CABIN FRAME REPAIR BS 930 BETWEEN STR 14 - STR 15R. INSTALLED KIT NR 65C25313-2. ACCOMPLISHED IAW SB 727-53-130 AND SB 727-53-162. (X)Dec 17, 1998 · N916TS · Boeing 727254 · Fuselage Main, FrameSDR USAA129810FFrame · crackedLEFT CABIN FRAME STA 930 CRACKED BETWEEN STR 14L - STR 15L BELOW CABIN WINDOW. ACCOMPLISHED LEFT CABIN WINDOW FRAME REPAIR BS 930 BETWEEN STR 14L AND STR 15L. INSTALLED KIT NR 65C25313-1. ACCOMPLISHED IAW SB 727-53-130 AND SB 727-53-162. (X)Dec 17, 1998 · N916TS · Boeing 727254 · Fuselage Main, FrameSDR USAA129810ESeat Track · corrodedCABIN SEAT TRACK LIGHT CORROSION FROM BS 380 THROUGH BS 760.95 LBL 25.5. REPLACED CABIN SEAT TRACK LBL 25.5 FROM BS 380 TO BS 480. MATERIAL USED BAC 1570-797, 100 INCHES LONG. ACCOMPLISHED IAW SRM 51-30-2 FIG 1. (X)Dec 17, 1998 · N916TS · Boeing 727254 · Fuselage, Seat/Cargo Attach FittingsSDR USAA129810DTube · wornRIGHT WING FUEL VENT TUBE SURFACE AND CLAMPS WORN BETWEEN WS 491 - WS 686 INTERIOR. ACCOMPLISHED RIGHT WING FUEL VENT TUBE REPAIRS WS 491.5, 546.5, 574.0, 601.5, 629.0, 656.5, AND 686.5. MATERIAL USED 2024T-3, .040 INCH, 2.5 INCHES BY 3.0 INCHES. ACCOMPLISHDec 17, 1998 · N916TS · Boeing 727254 · Aircraft Fuel Distribution SystemSDR USAA129810CSkin · crackedFUSELAGE SKIN CRACKED ABOVE THE RBL 70.5 CHORD ANGLE, BS 848.95 WL 196. EMANATING FROM THE FLOOR BEAM ATTACH ANGLE, LOWER FASTENER. INSTALLED FUSELAGE SKIN REPAIR RIGHT BS 848.95. MATERIAL USED 15-5PH HT 180-200 KSI 12 INCHES BY 31 INCHES. ACCOMPLISHED IAWDec 17, 1998 · N916TS · Boeing 727254 · Fuselage Main, Plate/SkinSDR USAA129810BAngle · crackedVERTICAL FLANGE OF THE RBL 70.5 WING TO CENTER TANK CHORD ANGLE IS CRACKED IN TWO PLACES, LOWER FASTENER. BS 846, WL 193, 15 INCHES BELOW CABIN FLOOR. INSTALLED BS 870 PREVENTIVE MOD RT SIDE KIT NR 65-92431-2. ACCOMPLISHED IAW SB 727-53-116. INSTALLED RT SDec 17, 1998 · N916TS · Boeing 727254 · Fuselage Miscellaneous StructureSDR USAA129810AChord · corrosionLEFT HORIZONTAL STABILIZER AFT SPAR AT UPPER AND LOWER CHORDS HAS CORROSION AT ATTACH ANGLE TO AFT HINGE FITTING AT STABILIZER STA 32 INCH. ACCESS THROUGH LOWER INBOARD ACCESS PANELS 9112, 9121. INSTALLED DOUBLER REPAIR ON LEFT HORIZONTAL STABILIZER LOWER CHDec 17, 1998 · N916TS · Boeing 727254 · Horizontal Stabilizer StructureSDR USAA129806Pulley · jammedFLT 6531 - LGA-DCA - AFTER LANDING NOSE STEERING INOPERATIVE FOR RIGHT TURNS. CONTROL STEERING TILLER BINDING WHEN TURNED TO RIGHT, TOWED AIRCRAFT FROM RUNWAY. CHECKED AND LUBED RUDDER STEERING SYSTEM, CHECKED STEERING CABLES AND PULLEYS FOUND PULLEY ON LEFTDec 17, 1998 · N914TS · Boeing 727254 · Landing Gear Steering SystemSDR USAA129805Smoke Detector · malfunctionedFLT 6540 - DCA-LGA - FORWARD LAVATORY SMOKE DETECTOR INOPERATIVE. REPLACED FORWARD LAVATORY SMOKE DETECTOR, OPERATIONAL CHECK NORMAL. (M)Dec 11, 1998 · N914TS · Boeing 727254 · Smoke DetectionSDR USAA119804Battery · dischargedBOTH LEFT AND RIGHT FORWARD OVERWING EXTERIOR EMERGENCY EXIT LIGHTS INOP. BOTH LEFT AND RIGHT MID OVERWING EXTERIOR EMERGENCY EXIT LIGHTS INOP. REPLACED LEFT AND RIGHT FORWARD EXTERIOR EMERGENCY EXIT LIGHT BATTERIES PER MM 33-50-0. REPLACED MID LEFT OVERWINGNov 19, 1998 · N913TS · Boeing 727254 · Emergency LightingSDR TAOA109806Indicator · malfunctionedFLT 6500 - DCA-LGA - ON APPROACH, UPON FLAP EXTENSION, INBOARD FLAPS WOULD NOT EXTEND BEYOND 25 DEGREES. REPLACED INBOARD FLAP POSITION INDICATOR. (M)Oct 17, 1998 · N912TS · Boeing 727254 · Trailing Flap Position Indicating SystemSDR TAOA109802Light · inoperativeFLT 6540 - DCA-LGA - LEFT OVERWING EMERGENCY EXIT LIGHT OUT. REPLACED LIGHT ASSEMBLY OPERATIONAL CHECK NORMAL. (M)Oct 11, 1998 · N914TS · Boeing 727254 · Emergency LightingSDR TAOA099810Battery Pack · dischargedFLT 6030 - LGA-BOS - LEFT AFT OVERWING EMERGENCY EXIT LIGHT INOP. REPLACED BATTERIES, TEST OK. (M)Sep 11, 1998 · N914TS · Boeing 727254 · Emergency LightingSDR 98ZZZX3577Fasteners · looseLOOSE FASTENERS AT RT WING FRONT SPAR UPPER CHORD. WS 330.5.Sep 11, 1998 · N912TS · Boeing 727254 · Wing SparSDR TAOA099805Smoke Detector · failedFLIGHT 6520 - DCA-LGA - FORWARD LAVATORY SMOKE DETECTOR GOES OFF CONTINOUSLY. REPLACED FORWARD LAVATORY SMOKE DETECTOR OPERATIONAL CHECK NORMAL. (M)Sep 6, 1998 · N916TS · Boeing 727254 · Smoke DetectionSDR TAOA099804Flashlight · dischargedFLT 6050, FOUND ON L/S CHECK, EMERGENCY FLASH LIGHT AT L-1 DOOR INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT AT L-1 DOOR CHECKS OK. (M)Sep 5, 1998 · N913TS · Boeing 727254 · Emergency LightingSDR TAOA099803Modular Unit · leakingLGA-DCA - FLT 6451 - 'A' HYDRAULIC SYSTEM FAILURE IN FIGHT AFTER FLAP RETRACTION. FOUND 'A' SYSTEM MODULAR UNIT LEAKING DUE TO CRACKED FITTING REPLACED MODULE. REPLACED 1 AND 2 HYDRAULIC PUMPS, CASE DRAIN RETURN AND PRESSURE FILTERS. SERVICED HYDRAULIC SYSTSep 4, 1998 · N913TS · Boeing 727254 · Hydraulic System, MainSDR TAOA079809Fire Loop · malfunctionedFLT 6480 - DCA-LGA - WHEEL WELL FIRE WARNING LIGHT CAME ON IN FLIGHT FOLLOWED EMERGENCY PROCEDURES. REPLACED NOSE WHEEL WELL FIRE LOOP ALSO REPLACED MAIN LEFT AND RIGHT WHEEL WELL FIRE LOOP. REPLACED FIRE AND OVERHEAT CONTROL BOX. PERFORMED RESISTANCE CHECKJul 16, 1998 · N916TS · Boeing 727254 · Fire DetectionSDR TAOA079805Valve · malfunctionFLT 6420 - DCA-LGA - RIGHT PACK OVERHEATED ON TAXI OUT WITH RIGHT PACK SWITCH IN OFF POSITION. REPLACED RIGHT PACK SHUT OFF VALVE. OPERATIONAL CHECK NORMAL. (M)Jul 10, 1998 · N914TS · Boeing 727254 · Cabin Cooling SystemSDR TAOA059815Fan · shortedFLT 6480 - DCA-LGA - GASPER FAN CIRCUIT BREAKER POPPED FOLLOWED BY BURNING SMELL FROM GASPER FAN VENTS. GASPER FAN SWITCH WAS PLACED TO OFF. REPLACED GASPER FAN IAW MM CHAPTER 21-23-1. OPERATIONAL CHECK NORMAL. (M)Jun 1, 1998 · N914TS · Boeing 727254 · Air Distribution FanSDR TAOA059811Switch · failedNR 1 ENGINE FIRE WARNING AT 3000 FT FIRE WARNING LIGHT AND BELL REPEATEDLY CYCLED ON AND OFF AFTER ENGINE SHUTDOWN. FIRE BOTTLE EXPENDED BOTH SIDES. FOUND WIRE NR W150-028-28 CHAFED AND SHORTING TO GROUND IN NR 1 ENGINE PYLON, REPAIRED WIRE PER CHAPTER 20 STMay 21, 1998 · N913TS · Boeing 727254 · Fire DetectionSDR TAOA059809Fire Sensor · malfunctionedFLT 6160 - LGA-BOS - ENGINE NR 1 FIRE WARNING IN FLIGHT. UNABLE TO PUT OUT LIGHT. SHUTDOWN ENGINE AND DISCHARGED FIRE BOTTLE, AFTER COMPLETING PROCEDURE LIGHT REMAINED ILLUMINATED. REPLACED NR 1 ENGINE LOWER FIRE WARNING SENSOR AND FIRE WARNING CONTROL UNITMay 18, 1998 · N913TS · Boeing 727254 · Fire DetectionSDR TAOA059803Fire Loop · malfunctionedNR 1 ENGINE FIRE WARNING ILLUMINATED ON DESCENT AT IDLE POWER, DESCENDING THROUGH 15,000 FEET AT 300 KNOTS, WHILE ACCOMPLISHING AIRCRAFT OPERATIONS PROCEDURE, FIRE WARNING EXTINGUISHED. ENGINE AT IDLE POWER REMAINDER OF FLT NO FURTHER FIRE INDICATION. INSPECMay 4, 1998 · N913TS · Boeing 727254 · Fire Detection
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