Boeing 727-2A7

Service difficulty reports · 60

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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 = '7272A7'
  ORDER BY difficulty_date DESC"

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SDR EISA20010090Splice · corrodedSTRINGER AT BS 680 27 RIGHT SPLICE IS CORRODED. REMOVED AND REPLACED STRINGER SPLICE, INSTALLED NEW SPLICE IAW SRM 53-10-3, 51-10-2, M/M 51-21-31.May 5, 2001 · N310NE · Boeing 7272A7 · Fuselage Miscellaneous StructureSDR EISA20000205Skin · dentedRT FUSELAGE SKIN DENTED BS 1260 TO 1280, STRINGER 21R TO 23R. CORRECTIVE ACTION: REMOVED DENTED AREA, FABRICATED DOUBLER, FILLER, AND STRINGER SPLICE REPAIRS, ALODINED, PRIMED AND INSTALLED, REPAIR DOUBLER, IAW 53-30-3 FIG 3, 53-10-3FIG 1, AND FIG 3, 51-10-2Nov 14, 2000 · N310NE · Boeing 7272A7 · Fuselage Main, Plate/SkinSDR EISA20000204Skin · dentedAFT AIRSTAIR SKIN HAS 12 INCH LONG DENT. CORRECTIVE ACTION: REMOVED DENTED AREA, FABRICATED, ALODINED, PRIMED, AND INSTALLED SKIN DOUBLER AND CHANNEL IAW SRM 53-10-3, 52-10-2 FIG. 5, 52-10-1, 51-10-2 AND 51-30-2.Nov 14, 2000 · N310NE · Boeing 7272A7 · Entrance StairsSDR EISA20000146Switch · out of adjON ASCENT TAIL SKID LIGHT ILLUMINATED (AIR TURNBACK). ADJUSTED TAIL SKID SWITCH PER M/M 32-71, OPS CHECK NORMAL.Sep 7, 2000 · N310NE · Boeing 7272A7 · Auxiliary Gear (Tail Skid)SDR EISA2000014Engine · leakingNR 2 ENGINE LOSING 1 QUART OF OIL EVERY 5-7 MINUTES. IN FLIGHT SHUTDOWN NR 2 ENGINE. UNSCHEDULED LANDING . (M)Feb 11, 2000 · N310NE · Boeing 7272A7 · Turbine Engine Oil SystemSDR EISA2000006Valve · damagedAIRCRAFT WOULD NOT PRESSURIZE ABOVE 10,000 FT, WENT TO MANUAL AND STANDBY POSITIONS. CABIN KEPT CLIMBING. AIR TURN BACK TO IND. REMOVED AND REPLACED RIGHT PACK VALVE PER MM 21-55. REPLACED CABIN PRESSURE CONTROLLER AND PACK SWITCHES. OPS CHECK OK PER MM 2Jan 13, 2000 · N310NE · Boeing 7272A7 · Cabin Pressure Control SystemSDR EISA2000017Valve · damagedAIRCRAFT WOULD NOT PRESSURIZE ABOVE 10,000 FT WENT TO MANUAL AND STANDBY POSITIONS. CABIN KEPT CLIMBING. AIR TURN BACK TO IND. REMOVED AND REPLACED RIGHT PACK VALVE PER MM 21-55. REPLACED CABIN PRESSURE CONTROLLER ADN PACK SWITCHES. OPS CHECK OK PER MM 21Jan 13, 2000 · N310NE · Boeing 7272A7 · Cabin Pressure Control SystemSDR EISA2000005Controller · failedPRESSURIZATION INOP, CABIN WAS UNCONTROLLABLE UNABLE TO MAKE CABIN DESCEND A/C ALTITUDE 10,000 CABIN WAS AT 8000 OUTFLOW VALVE CARGO HEAT CLOSED. CABIN STILL UNCONTROLLABLE IN ALL MODES. GROUND OPS TESTED PRESSURIZATION SYSTEM PER MM 21-30. PRESSURIZED TO 5Jan 12, 2000 · N310NE · Boeing 7272A7 · Cabin Pressure Control SystemSDR EISA99252Engine · lack of lubeNR 3 ENGINE SHUT DOWN DUE TO LOW OIL QUANTITY, AND LOW OIL PRESSURE. ENGINE WINDMILLED BELOW TEN PSI OIL PRESSURE FOR ONE HOUR AND TEN MINUTES. (M)Dec 7, 1999 · N310NE · Boeing 7272A7 · Turbine Engine Oil SystemSDR EISA99163Light · inoperativeON POST FLIGHT, L-1 DOOR EMERGENCY EXIT LIGHT INOPERABLE. REMOVED AND REPLACED L-1 EMERGENCY LIGHT PER MM 33-50-0. OPS CHECK GOOD. (M)Aug 23, 1999 · N310NE · Boeing 7272A7 · Emergency LightingSDR EISA99158Engine · failedNR 3 ENGINE EGT REACHED RED LINE ON TAKEOFF. REPLACED NR 3 ENGINE. (M)Aug 21, 1999 · N310NE · Boeing 7272A7 · Engine (Turbine/Turboprop)SDR EISA99155Light · defectedREMOVED AND REPLACED COCKPIT EMERGENCY EXIT LIGHT IAW MM 33-50. OPS CHECK GOOD. (M)Aug 20, 1999 · N310NE · Boeing 7272A7 · Emergency LightingSDR EISA99137Switch · dirtyLEADING EDGE FLAPS LIGHT WENT FROM GREEN TO AMBER, F/E PANEL LIGHT NORMAL. CLEANED AND RESET L/E SLAT SWITCH. (M)Jun 15, 1999 · N310NE · Boeing 7272A7 · Leading Edge Slat Position Indicating SystemSDR EISA99130Indicator · unserviceableCREW HAD SPLIT FLAP INDICATION, DECLARED EMERGENCY AND MADE 'GO AROUND'. CHECKED FLAP OPERATION, REPLACED OUTBOARD FLAP INDICATOR AND OPS CHECKED OK. (M)May 22, 1999 · N310NE · Boeing 7272A7 · Trailing Flap Position Indicating SystemSDR EISA99121Indicator · failedCREW HAD SPLIT INDICATOR DECLARED EMERGENCY AND MADE GO AROUND. CHECKED FLAP OPERATION. REPLACED OUTBOARD FLAP INDICATOR AND OPS CHECKED OK. (M)May 22, 1999 · N310NE · Boeing 7272A7 · Trailing Flap Position Indicating SystemSDR EISA98249Light · inoperativeEMERGENCY EXIT LIGHT ABOVE COCKPIT DOOR INOPERATIVE. GENERATED FROM MAINTENANCE REPORT. REMOVED AND REPLACED EMERGENCY LIGHT, OPS CHECK GOOD PER MM 33-50. (M)Oct 15, 1998 · N310NE · Boeing 7272A7 · Emergency LightingSDR EISA98223Door · leakingUNABLE TO PRESSURIZE DUE TO LEAK IN CREW FORWARD ENTRY DOOR. NO WARNING LIGHTS. AIR TURN BACK TO IND. FOUND L-1 DOOR NOT PROPERLY CLOSED. OPENED AND CLOSED DOOR. PRESSURIZED ON GROUND, OK FOR SERVICE. TT: 69,782:12 HOURS. TC: 46,771. (X)Sep 23, 1998 · N310NE · Boeing 7272A7 · Passenger/Crew DoorsSDR EISA98239Frame · crackedDURING ACCOMPLISHMENT OF C-ROUTINE INSPECTION CARD, FOUND FUSELAGE FRAME CRACKED AT STATION 570. REPAIRED FRAME PER SRM 53-20-2 DOUBLER INSTALLED. (M)Aug 10, 1998 · N310NE · Boeing 7272A7 · Fuselage Main, FrameSDR EISA98238Flange · corrodedDURING ACCOMPLISHMENT OF C-ROUTINE CPCP INSPECTION CARD, FOUND CORROSION IN NOSE WHEEL WELL PANEL 3120. CORROSION WAS FOUND ON OUTBOARD FLANGE. REPLACED FLANGE PER SRM 53-10-2 DOUBLER INSTALLED. (M)Aug 10, 1998 · N310NE · Boeing 7272A7 · Fuselage Miscellaneous StructureSDR EISA98237Seat Track · corrodedDURING ACCOMPLISHMENT OF C-ROUTINE INSPECTION, FOUND CORROSION ON SEAT TRACK STATION 344 TO 480 RBL 44. REMOVED AND REPLACED SEAT TRACK PER SRM 53-10-1. (M)Aug 10, 1998 · N310NE · Boeing 7272A7 · Fuselage, Seat/Cargo Attach FittingsSDR EISA98236Fitting · corrodedDURING ACCOMPLISHMENT OF C-CHECK, WHILE DOING SCHEDULED GEAR CHANGE LEFT FORWARD TRUNNION FITTING CORRODED. REMOVED AND REPLACED FWD TRUNNION FITTING PER SRM 51-10-1 AND 51-30-2 AND MM 20-80-1. (M)Aug 10, 1998 · N310NE · Boeing 7272A7 · Main Landing Gear Attach SectionSDR EISA98235Seat Track · corrodedDURING ACCOMPLISHMENT OF C-CHECK ROUTINE INSPECTION CARD, FOUND CORROSION ON SEAT TRACK STATION 560 RBL 44. REMOVED AND REPLACED DAMAGED AREA OF SEAT RACK PER SRM 53-10-5. (M)Aug 10, 1998 · N310NE · Boeing 7272A7 · Fuselage, Seat/Cargo Attach FittingsSDR EISA98234Seat Track · corrodedDURING ACCOMPLISHMENT OF C-CHECK ROUTINE INSPECTION, FOUND CORROSION ON SEAT TRACK STATION 837 RBL 24. REMOVED AND REPLACED DAMAGED AREA OF SEAT TRACK PER SRM 53-10-5. (M)Aug 10, 1998 · N310NE · Boeing 7272A7 · Fuselage, Seat/Cargo Attach FittingsSDR EISA98233Seat Track · corrodedDURING ACCOMPLISHMENT OF C-CHECK ROUTINE INSPECTION, FOUND CORROSION ON SEAT TRACK STATION 400 RBL 23. REMOVED SEAT TRACK FABRICATED NEW ONE PER SRM 53-10-5. (M)Aug 10, 1998 · N310NE · Boeing 7272A7 · Fuselage, Seat/Cargo Attach FittingsSDR EISA98232Web · crackedDURING ACCOMPLISHMENT OF C-CHECK ROUTINE CPCP INSPECTION, FOUND RIGHT WEB AT STATION 870 IN KEELBEAM CRACKED. REMOVED DAMAGED AREA FABRICATED DOUBLER AND INSTALLED PER SRM 53-10-2 FIGURE 4. (M)Aug 10, 1998 · N310NE · Boeing 7272A7 · Fuselage Miscellaneous StructureSDR EISA98231Angle · crackedDURING ACCOMPLISHMENT OF C-CHECK ROUTINE CPCP INSPECTION CARD, FOUND VERTICAL ATTACH ANGLE AT STATION 870 IN KEELBEAM CRACKED. REMOVED AND REPLACED WITH NEW PART PER SRM 51-10-1. (M)Aug 10, 1998 · N310NE · Boeing 7272A7 · Fuselage Miscellaneous StructureSDR EISA98230Seat Track · corrodedDURING ACCOMPLISHMENT OF C-CHECK ROUTINE INSPECTION CARD, FOUND CORROSION SEAT TRACK STATION 640 AND RBL 44. REMOVED AND REPLACED SEAT TRACK PER SRM 53-10-5. (M)Aug 10, 1998 · N310NE · Boeing 7272A7 · Fuselage, Seat/Cargo Attach FittingsSDR EISA98229Web · crackedDURING ACCOMPLISHMENT OF C-CHECK CPCP CARD INSPECTION, A 4 INCH CRACK WAS FOUND AT STATION 870 BULKHEAD AT APPROX BL 10. REPAIRED AREA WITH DOUBLER PER EO 53-98-143-1 AND SRM 51-30-2. (M)Aug 10, 1998 · N310NE · Boeing 7272A7 · Fuselage Miscellaneous StructureSDR EISA98228Stringer · missingDURING ACCOMPLISHMENT OF C-CHECK CPCP CARD 53-113-01, A 5 INCH SECTION OF STRINGER 30 WAS MISSING FROM FLOOR AFT CARGO PIT BS 1175. REMOVED DAMAGED STRINGER AND FABRICATED NEW STRINGER PER SRM 53-10-3. (M)Aug 10, 1998 · N310NE · Boeing 7272A7 · Fuselage Main, Longeron/StringerSDR EISA98227Frame · crackedDURING ACCOMPLISHMENT OF C-CHECK ROUTINE INSPECTION, FOUND FUSELAGE FRAME CRACKS AT STATION 540 WL 214. REMOVED DAMAGE AREA, FABRICATED DOUBLER AND INSTALLED PER SRM 51-30-2. (M)Aug 10, 1998 · N310NE · Boeing 7272A7 · Fuselage Main, FrameSDR EISA98226Frame · crackedDURING ACCOMPLISHMENT OF C-CHECK ROUTINE INSPECTION, FOUND FUSELAGE FRAME CRACKS AT STATION 560 WL 214. REMOVED DAMAGE AREA, FABRICATED DOUBLER AND INSTALLED PER SRM 51-30-2. (M)Aug 10, 1998 · N310NE · Boeing 7272A7 · Fuselage Main, FrameSDR EISA98225Seat Track · corrodedDURING ACCOMPLISHMENT OF C-CHECK ROUTINE INSPECTION, FOUND CORROSION ON SEAT TRACK AT STATION 1050 LBL 25. REMOVED AND REPLACED SEAT TRACK PER SRM 53-10-5. (M)Aug 10, 1998 · N310NE · Boeing 7272A7 · Fuselage, Seat/Cargo Attach FittingsSDR EISA98176Gearbox · contaminatedAFTER TAKEOFF FROM IND WHILE RETRACTING FLAPS, OUTBOARD FLAPS DID NOT RETRACT FROM 2 DEGREES TO UP. PERFORMED PROCEDURE AND PROBLEM REMAINED. RETURNED TO IND. GENERATED FROM PILOT REPORT. CYCLED FLAPS, FLUSHING ANY POSSIBILITY OF AIR, INSPECTED FLAPS, FLAPJul 11, 1998 · N310NE · Boeing 7272A7 · Trailing Edge Flap Control SystemSDR EISA98148Compressor · stalledON TAKEOFF OUT OF ICT NR 3 ENGINE COMPRESSOR STALLED TRIPPING BOTH PACKS ON CLIMB NR 3 REACHED MAX CONT EGT, .10 EPR, BELOW MAX CLIMB EPR, IN CRUISE ALL ENGINE PARAMETERS NORMAL. ICT TEMP 23 DEGREES CELSIUS WIND 100 AT 7 RUNWAY 19R. GENERATED FROM PILOT REPOJun 10, 1998 · N310NE · Boeing 7272A7 · Turbine Engine Compressor SectionSDR EISA98146Tire · failedRIGHT MAIN TIRES BLEW POSSIBLY ON TAKEOFF FROM ICT. ICT TOWER REPORTED RUBBER ON RUNWAY. REPAIRED AND REPLACED NR 3 AND NR 4 MAIN WHEEL ASSEMBLIES IAW 32-45-1. NR 4 TIRE IS THE TIRE THAT BLEW OUT. (M)Jun 10, 1998 · N310NE · Boeing 7272A7 · TireSDR EISA98123Hose · chafedAFTER TAKEOFF, INDIANAPOLIS (IND) WHILE CLIMBING THROUGH APPROXIMATELY 3,000 FEET, NR 1 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED. AOM ABNORMAL. C/W ENGINE NR 1, THRUST REDUCED, LIGHT EXTINGUISHED AFTER ABOUT 1 MINUTE COOLING. RETURNED TO (IND). GENERATED FRJun 9, 1998 · N310NE · Boeing 7272A7 · Engine Thrust ReverserSDR EISA98127Clamp · looseCLIMGING THROUGH 16,000 FEET AT 91 PERCENT N1, GOT A NR 1 STRUT OVERHEAT LIGHT OUT WITH THROTTLE RETARDED. SWAPPED NR 1 AND NR 3 BLEEDS PER AOM WITH NO RECURRENCE IN-FLIGHT. GENERATED FROM PILOT REPORT. TROUBLESHOT SYSTEM TO LOOSE CLAMP. TIGHTENED CLAMP. May 31, 1998 · N310NE · Boeing 7272A7 · Pneumatic Distribution SystemSDR EISA98118Clamp · looseDURING CLIMB-OUT, ENGINE NR 1 STRUT OVERHEAT LIGHT ILLUMINATED. REDUCING THRUST EXTINGUISHED LIGHT. GENERATED FROM PILOT REPORT. TROUBLESHOT FOUND 8TH STAGE DUCT CLAMP LOOSE, DUCT MISALIGNED, TIGHTENED AND ALIGNED CAMP, RAN ENGINE. NO LEAKS NOTED. (M)May 24, 1998 · N310NE · Boeing 7272A7 · Pneumatic Distribution SystemSDR EISA98117Clamp · looseDURING CLIMB-OUT, NR 1 STRUT OVERHEAT LIGHT ILLUMINATED. REDUCING THRUST PER ABNORMAL CHECK LIST EXTINGUISHED LIGHT. GENERATED FROM PILOT REPORT. REPOSITIONED AND TIGHTENED CLAMP ON PNEUMATIC DUCT NR 1 ENGINE. RAN ENGINE, LEAK CHECK GOOD. (M)May 24, 1998 · N310NE · Boeing 7272A7 · Pneumatic Distribution SystemSDR EISA98067Fuel Pump · failedAFTER TAKEOFF FROM BDL, NR 2 ENGINE COMPRESSOR STALLED AND FAILED. ACCOMPLISHED APPROPRIATE TWO ENGINE OPERATING CHECKLIST. FLIGHT CONTINUED TO DESTINATION BOS. REMOVED AND REPLACED ENGINE FUEL PUMP IAW PRATT AND WHITNEY MM 73-11-1. OPS LEAK CHECK GOOD IAWMar 24, 1998 · N310NE · Boeing 7272A7 · Engine Fuel PumpSDR EISA97224Switch · failedDURING CRUISE AT FLT 370, THE L/E FLAPS LGHT ON THE PILOT PANEL ILLUMINATED. POSITION TEST INDICATED AMBER IN TRANSIT LIGHT OR, NR 3 L/E FLAP. PERFORMED EMERGENCY CHECK LIST. L/E FLAP NR 3 REMAINED IN TRANSIT. REMOVED AND REPLACED NR 3 FLAP POSITION SWITCHNov 15, 1997 · N310NE · Boeing 7272A7 · Leading Edge Slat Position Indicating SystemSDR EISA97205Oil Cooler · failedNR 2 ENGINE OIL TEMPERATURE IN YELLOW ARC. PRECAUTIONARY SHUT DOWN PER MANUAL. REMOVED AND REPLACED OIL COOLER. (X)Oct 9, 1997 · N310NE · Boeing 7272A7 · Engine Oil CoolerSDR EISA97114Connector · dirtyWHEEL WELL FIRE WARNING LIGHT AND BELL CAME ON. CLEANED LOOP CONNECTOR, OPS CHECK GOOD. (M)Jun 10, 1997 · N310NE · Boeing 7272A7 · Fire DetectionSDR EISA97111Connector · dirtyWHEEL WELL FIRE WARNING LIGHT AND BELL CAME ON DURING PUSHBACK EMERGENCY SHUT DOWN PROCEDURES. CLEANED CONNECTORS WITH CONTACT CLEANER AT RT W/W AREA, OPS CHECK C/W PER 26-10-0 OK. (M)Jun 7, 1997 · N310NE · Boeing 7272A7 · Fire DetectionSDR EISA96119Support Web · crackedFOUR EACH FLOOR SUPPORT WEBS CRACKED AT AFT BULKHEAD LBL 40 TO RBL 35. FABRICATED AND INSTALLED NEW WEBS PER SRM 51-10-02 AND SRM 51-40-03. TT: 66,991:57 HOURS. TC: 45,084. (X)Jul 16, 1996 · N310NE · Boeing 7272A7 · Fuselage Miscellaneous StructureSDR EISA96118Floor Beam · corrodedFLOOR BEAM UNDER LAVATORY FLOOR IS CORRODED. REMOVED DAMAGED FLOOR STRINGER, FABRICATED AND INSTALLED NEW STRINGER PER SRM'S 51-40-04, 51-10-02, AND 51-20-01. TT: 66,991:57 HOURS. TC: 45,084. (X)Jul 16, 1996 · N310NE · Boeing 7272A7 · Fuselage Main, Floor BeamSDR EISA96117Frame · crackedFUSELAGE FORGING AT STA 740 RT, BETWEEN STR 18R AND STR 19R, HAS CRACK EMANATING FROM PREVIOUS STOP DRILL HOLES. INSTALLED REPAIR PER SRM'S 51-30-2, 51-10-04, SB 53-0062 AND BOEING DRAWING 65C 15314.Jul 16, 1996 · N310NE · Boeing 7272A7 · Fuselage Main, FrameSDR EISA96116Actuator Bracket · crackedRIGHT WING NR 5 SLAT ACTUATOR ATTACH RIB BRACKET CRACKED. FABRICATED AND INSTALLED REPAIR PER SRM 57-20-03. TT: 66,991:57 HOURS. TC: 45,084. (X)Jul 16, 1996 · N310NE · Boeing 7272A7 · Leading Edge Slat ActuatorSDR EISA96115Angle · crackedLEFT WING NR 1 SLAT OUTBOARD TRACK ATTACH FORWARD ANGLE BRACKET CRACKED. INSTALLED NEW ANGLE BRACKET PER SRM 51-10-1. TT: 66,991:57 HOURS. TC: 45,084. (X)Jul 16, 1996 · N310NE · Boeing 7272A7 · Leading Edge DevicesSDR EISA96114Angle · crackedLEFT WING, NR 1 SLAT, INBOARD TRACK ATTACH FORWARD ANGLE BRACKET CRACKED. FABRICATED AND INSTALLED REPAIR PER SRM 51-40-03. TT: 66,991:57 HOURS. TC: 45,084. (X)Jul 16, 1996 · N310NE · Boeing 7272A7 · Leading Edge Devices
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