Boeing 727-2M7

Service difficulty reports · 459

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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 = '7272M7'
  ORDER BY difficulty_date DESC"

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SDR EISA20010114Angle · crackedLT. WING SPOILER #4 ACTUATOR MOUNT O/B LWR. MOUNT LOBE IS BROKENFOUND DURING 'B' CHECK.CORRECTIVE ACTION:R/R #4 SPOILER ACTUATOR MOUNT BRACKET IAW B727 SRM 51-30-2.Aug 20, 2001 · N721RW · Boeing 7272M7 · Drag Control ActuatorSDR EISA20010112Transmitter · failedDURING NR 1 ENG START OIL PRESS STABILIZED AT 25 PSI, BELOW RED RADIAL. ENGINE SHUT DOWN ACCOMPLISHED. REMOVED AND REPLACED OIL PRESSURE TRANSMITTER, OPS CK OK PER MM REF 79-32.Aug 19, 2001 · N725RW · Boeing 7272M7 · Engine Oil PressureSDR SCNA01703Control Unit · malfunctionedAT SLOW SPEEDS, LESS THAN 20 KIAS THERE IS VIRTUALLY NO BRAKING ACTION WITH THE ANTI SKID ON, BUT OK WITH IT OFF. REMOVED AND REPLACED ANTI-SKID CONTROL UNIT.Jul 24, 2001 · N294SC · Boeing 7272M7 · Brake Anti-Skid SectionSDR EISA20010107Ground Wire · looseA/C WOULD NOT PRESSURIZE (ALL MODES). RESECURED GROUND TO FLOW CONTROL VALVES (SHARD GRND FOR BOTH). A/C PRESSURIZATION AND PNEUMATIC SYSTEMS, OPS OK.Jul 19, 2001 · N721RW · Boeing 7272M7 · Cabin Pressure Control SystemSDR 0102222762Switch · faultyAFTER TAKEOFF, CREW RETRACTED GEAR AND RECEIVED A RIGHT GEAR DOOR WARNING INDICATION. CREW PERFORMED COM PROCEDURE AND RECYCLED GEAR WITH NO HELP, WARNING LIGHT STILL ILLUMINATED. CREW FOLLOWED COM PROCEDURE AND RETURNED TO MSP AND MADE AN UNEVENTFUL LANDINGJun 20, 2001 · N722RW · Boeing 7272M7 · Landing Gear Position and WarningSDR SCNA01041Battery Pack · dischargedDURING A MAINTENANCE LINE CHECK THE MID CABIN EMERGENCY FLOOR TRACK LIGHTING WAS FOUND INOPERATIVE. REMOVED AND REPLACED THE POWER SUPPLY AND THE BATTERY PACK.May 19, 2001 · N294SC · Boeing 7272M7 · Emergency LightingSDR EISA20010091Skin · crackedL-1 LOWER DOOR HINGE AT FUSELAGE SKIN CRACKED. REPAIRED CRACK, ROUTING OUT AND FABRICATING AND INSTALLING REPAIR FILLER AND DOUBLER IAW 727 SB 727-53-0198 REV 1 FIGURE 4 DATED 07-25-1991.May 4, 2001 · N742RW · Boeing 7272M7 · Passenger/Crew DoorsSDR SCNA01025Light · inoperativeDURING A MAINTENANCE LINE CHECK THE RIGHT FORWARD GALLEY DOOR EMERGENCY EXIT LIGHT WILL NOT ILLUMINATE. REMOVED AND REPLACED LAMP AT R1 DOOR OVERHEAD EMERGENCY EXIT.Apr 6, 2001 · N294SC · Boeing 7272M7 · Emergency LightingSDR EISA20010072Switch · faultyAUTO PACK SYSTEM TRIPPED AT TAKEOFF POWER. REMOVED AND REPLACED AUTO PACK TRIP SWITCHES PER M/M 21-11-11, 21-30, OPS CHECK NORMAL.Mar 20, 2001 · N725RW · Boeing 7272M7 · Cabin Pressure Control SystemSDR EISA20010069Outflow Valve · stuckAIRCRAFT WOULD NOT PRESSURIZE IN ANY MODE, DURING CLIMB. AIR TURNBACK. REMOVED AND REPLACED OUTFLOW VALVE AND PRESSURE CONTROLLER. OPS CHECK NORMAL.Mar 16, 2001 · N721RW · Boeing 7272M7 · Pressure Regulator/Outflow ValveSDR SCNA01028Apu · fireAPU FIRE INDICATION, DISCHARGED THE APU FIRE BOTTLE. REMOVED AND REPLACED APU AND APU FIRE BOTTLE.Mar 7, 2001 · N294SC · Boeing 7272M7 · APU Core EngineSDR EISA20010003Clamp · wornNR 3 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED DURING FLIGHT. INSTALLED NEW CLAMPS ON DUCTS IN NR 3 STRUT. RAN UP TO POWER, NO LIGHT.Jan 27, 2001 · N725RW · Boeing 7272M7 · Pneumatic Distribution SystemSDR EISA20000227Fire Loop · brokenNR 1 ENGINE FIRE INDICATION SHUT-DOWN ENGINE. UNSCHEDULED LANDING ELP. REPLACED NR 1 ENGINE FIRE LOOP.Dec 22, 2000 · N725RW · Boeing 7272M7 · Fire DetectionSDR EISA20000219Control Unit · inoperativeAT FL 290 AT 270 KNOTS AIRCRAFT INITIATED A RUDDER HARD OVER TO THE RIGHT. CORRECTIVE ACTION: REMOVED AND REPLACED LOWER RUDDER POWER CONTROL UNIT OPS CHECK GOOD PER M/M 27-20-00.Dec 14, 2000 · N725RW · Boeing 7272M7 · Rudder Control SystemSDR EISA20000213Flow Valve · inoperativeAUTO PRESSURIZATION FAIL LIGHT CAME ON IN CLIMB UNABLE TO PRESSURIZE IN STANDBY OR MANUAL. REMOVED AND REPLACED FLOW CONTROL VALVE PER M/M 21-00, OPS CHECK NORMAL.Dec 2, 2000 · N721RW · Boeing 7272M7 · Cabin Pressure Control SystemSDR SCNA00124Switch · intermittentDURING TAKEOFF ROLL, TAKEOFF WARNING OCCURRED, ABORTED TAKEOFF. RESET FLAPS, TRIM, SPEED BRAKE AND COULD NOT DUPLICATE. FOUND INTERMITTANT SPEED BRAKE SWITCH AT SPEED BRAKE HANDLE. REMOVED AND REPLACED SWITCH, CHECKS NORMAL.Nov 24, 2000 · N294SC · Boeing 7272M7 · High Speed WarningSDR EISA20000200Battery · dischargedCOCKPIT AND FORWARD ENTRY EXIT LIGHTS WILL NOT ILLUMINATE. RECHARGED BATTERIES PER M/M 33-50-00, OPS CHECK GOOD.Nov 7, 2000 · N725RW · Boeing 7272M7 · Emergency LightingSDR EISA20000206Skin · cracked10 INCH CRACK, 1 INCH HOLE, AND 8 INCH CREASE FORWARD OF C1 DOOR. CORRECTIVE ACTION: FABRICATED DOUBLER, FILLERS, AND SHIMS, ALODINED, PRIMED, AND INSTALLED IAW 53-30-3 FIG 6, 51-10-2, 53-10-3 FIG 1 AND FIG 2, 53-10-4 FIG 13, 51-30-2, M/M 34-11-0052-35-21 ANNov 6, 2000 · N742RW · Boeing 7272M7 · Fuselage Main, Plate/SkinSDR EISA20000194Clamp · looseNR 3 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED IN FLIGHT. SECURED TWO CLAMPS AT 13TH STAGE MOD VALVE.Oct 26, 2000 · N725RW · Boeing 7272M7 · Pneumatic Distribution SystemSDR EISA20000193Clamp · looseNR 3 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED AFTER TAKE OFF ACCOMPLISHED CHECKLIST LIGHT WENT OUT AFTER NR 3 BLEED VALVE CLOSED. BEFORE CLOSING NR 3 BLEED VALVE RT. MAN PRESSURE 100PSI. CORRECTIVE ACTION: TIGHTENED CLAMPS ON 13TH STAGE MOD VALVE, OPS CHECK NOct 25, 2000 · N725RW · Boeing 7272M7 · Overheat DetectionSDR SCNA00378Frame · corrodedDURING HEAVY MAINTENANCE INSPECTION CORROSION WAS FOUND OUT OF LIMITS AT MAIN CABIN WINDOW FRAME ON AFT SIDE AT STA 720A THROUGH 720B WINDOW R15. REMOVED CORROSION IAW B727 SRM 511006. FABRICATED DOUBLER FROM 2024 T3 .160 IAW B727 SRM 562003 FIG 3. TREATED Oct 24, 2000 · N294SC · Boeing 7272M7 · Passenger Compartment WindowsSDR EISA20000151Catcher · stalledCOMPRESSOR STALL NR 2 ENGINE AIR TURNBACK TO (AUS). DRAINED MOISTURE TRAP IAW 73-33. RAN ENGINE, OPS CHECK GOOD PER M/M 71-00.Sep 22, 2000 · N721RW · Boeing 7272M7 · Turbine Engine Compressor SectionSDR SCNA00101Charger · inoperativeDURING A MAINTENANCE LINE CHECK, THE LEFT FORWARD OVERWING EMERGENCY TREAD LIGHT WAS FOUND INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK AND CHARGER FOR THE LEFT OVERWING TREAD EMERGENCY LIGHTING. OPERATIONAL CHECKS GOOD.Sep 10, 2000 · N294SC · Boeing 7272M7 · Emergency LightingSDR 0003302769Engine · stalledDURING APPROACH TO DEN, THE FLIGHT CREW RECEIVED A WINDSHEAR ALERT. THE ENGINE THROTTLES WERE ADVANCED PER PROCEDURES AND THE NR 2 ENGINE EXPERIENCED A COMPRESSOR STALL. AFTER THE WINDSHEAR ALERT, THE NR 2 ENGINE WAS RETARDED TO IDLE AND AN EMERGENCY WAS DECSep 9, 2000 · N729RW · Boeing 7272M7 · Engine (Turbine/Turboprop)SDR 0003082769Actuator · failedDURING CLIMB THE HORIZONTAL STABILIZER JAMMED. FLIGHT CREW PERFORMED COM PROCEDURE AND WAS ABLE TO RELEASE STAB BRAKE. FLIGHT RETURNED TO MSP AND MADE AN UNEVENTFUL LANDING. MAINTENANCE REPLACED THE PRIMARY STABILIZER TRIM ACTUATOR, AUTOPILOT TRIM SERVO, ANSep 4, 2000 · N729RW · Boeing 7272M7 · Stabilizer ActuatorSDR EISA20000128Clamp · looseNR 3 ENGINE STRUT OVERHEAT LIGHT CAME ON AFTER 10 MINUTES OF FLIGHT ON CLIMBOUT. PULLED NR 3 THROTTLE BACK AND LIGHT WENT OUT. WENT THROUGH PROCEDURES AND LIGHT DID NOT COME ON. CHECKED STRUT AREA FOR LEAKS, REPLACED 1 CLAMP ON 13TH STAGE DUCT PER M/M 36-00Aug 16, 2000 · N721RW · Boeing 7272M7 · Pneumatic Distribution SystemSDR SCNA00088Accessory Unit · inoperativeDURING CLIMBOUT FROM MSP, THE LANDING GEAR WOULD NOT RETRACT, THE CREW COMPLETED COM PROCEDURES. THE GEAR RETRACTED NORMALLY AND THE CREW RETURNED TO MSP. REMOVED AND REPLACED THE LANDING GEAR ACCESSORY UNIT, OPERATIONAL CHECKS GOOD.Aug 9, 2000 · N294SC · Boeing 7272M7 · Landing Gear Retraction/Extension SystemSDR SCNA00078Plug · leakingDURING CRUISE THE FLIGHT CREW NOTICED A SLOW LOSS OF B SYSTEM FLUID, DUE TO A DECREASE IN PRESSURE. SECURED REMAINNG B PUMP. SYSTEM FLUID REMAINED, NO SYSTEM OVERHEAT. HYDRAULIC PLUG AT NR 4 SLAT ACTUATOR WAS FOUND TO HAVE A BLOWN OUT SEAL. REMOVED AND REPJul 20, 2000 · N294SC · Boeing 7272M7 · Leading Edge Slat Position Indicating SystemSDR SCNA00071Power Supply · failedDURING A MAINTENANCE LINE CHECK THE EMERGENCY PATH LIGHTING FROM ROW 9 TO 13 WAS FOUND INOPERATIVE. REMOVED AND REPLACED BATTERY POWER SUPPLY OPERATIONAL CHECKS GOOD FROM ROW 9 TO 15.Jul 7, 2000 · N294SC · Boeing 7272M7 · Emergency LightingSDR EISA2000044Switch · out of adjLEFT LEADING EDGE NUMBER THREE FLAP LIGHT ILLUMINATED IN TURBULENT CONDITIONS. ADJUSTED POSTION INDICATOR MICROSWITCH ON NR 3 LEADING EDGE FLAP. OPERATIONAL CHECK GOOD. (M)Apr 8, 2000 · N742RW · Boeing 7272M7 · Leading Edge Slat Control SystemSDR SCNA00022Circuit Breaker · poppedON APPROACH LANDING GEAR UNSAFE INDICATION, EXECUTED A MISSED APPROACH. FOUND AND RESET CIRCUIT BREAKER GEAR INDICATION CIRCUIT BREAKER AND MADE A NORMAL LANDING. OPERATED ALL SYSTEMS AFFECTED BY THE CIRCUIT BREAKER THAT WAS RESET AND ALL SYSTEMS CHECK NORMAMar 23, 2000 · N294SC · Boeing 7272M7 · Landing Gear Position and WarningSDR SCNA00021Valve · failedON CLIMBOUT, THE RIGHT PACK WOULD NOT MOVE FROM FULL COLD POSITION. FURTHER INVESTIGATION REVEALED THAT IT HAD CEASED TO FUNCTION. AT FL 250 AIRCRAFT WOULD NOT MAINTAIN PRESSURIZATION. REPLACED RIGTH PACK VALVE PER M 215571. GROUND CHECKS NORMAL.Mar 5, 2000 · N294SC · Boeing 7272M7 · Cabin Cooling SystemSDR SCNA00020Actuator · malfunctionedCREW OBSERVED TAKEOFF WARNING HORN AT THE BEGINNING OF THE TAKEOFF ROLL. REJECTED TAKEOFF, FOUND ACTUATOR FOR S867 (SPEED BRAKE WARNING SWITCH) OUT OF ADJUSTMENT. READJUSTED ACTUATOR AND PERFORMED TAKEOFF WARNING. CHECKED GOOD PER MM 31260. NO FURTHER PROBFeb 28, 2000 · N294SC · Boeing 7272M7 · Drag Control ActuatorSDR EISA2000027Seat Track · crackedDURING ACCOMPLISHMENT OF A ROUTINE C-CHECK WORK CARD, FOUND MAIN CABIN SEAT TRACK CRACKED AT FS 1090 RBL 45.5. REMOVED DAMAGED SEAT TRACK FROM FS 1070 TO FS 1100. FABRICATED NEW SECTION PER SAMPLE FROM BAC 1520-792 EXTRUSION. INSTALLED NEW SECTION PER SRM 5Feb 27, 2000 · N721RW · Boeing 7272M7 · Fuselage, Seat/Cargo Attach FittingsSDR 20000329SH015Skin · corrodedDURING A C-CHECK, CORROSION WAS NOTED ON LOWER FORWARD CORNER AFT LAVATORY DUMP. (X)Feb 15, 2000 · N725RW · Boeing 7272M7 · Fuselage Main, Plate/SkinSDR 20000329SH014Threshold · corrodedDURING A C-CHECK, CORROSION WAS NOTED ON MOP SILL R-2 DOOR THRESHOLD. (X)Feb 15, 2000 · N725RW · Boeing 7272M7 · Fuselage Miscellaneous StructureSDR 20000329SH013Floorbeam · corrodedDURING A C-CHECK, CORROSION WAS NOTED ON TOP OF FLOORBEAM (CENTER SECTION) BS 360. (X)Feb 15, 2000 · N725RW · Boeing 7272M7 · Fuselage Main, Floor BeamSDR 20000329SH012Floorbeam · corrodedDURING A C-CHECK, CORROSION WAS NOTED ON LOWER CHORD, UPPER/LOWER SURFACES OF BS 1130 FLOORBEAM. (X)Feb 15, 2000 · N725RW · Boeing 7272M7 · Fuselage Main, Floor BeamSDR 20000329SH011Floorbeam · corrodedDURING A C-CHECK, CORROSION WAS NOTED ON LOWER CHORD, UPPER/LOWER SURFACES OF BS 1070 FLOORBEAM (RBL 44-LBL 44). (X)Feb 15, 2000 · N725RW · Boeing 7272M7 · Fuselage Main, Floor BeamSDR 20000329SH010Seat Track · corrodedDURING C-CHECK, CORROSION WAS NOTED ON SEAT TRACK AT FS 1130 AT RBL 44. (X)Feb 15, 2000 · N725RW · Boeing 7272M7 · Fuselage, Seat/Cargo Attach FittingsSDR 0000372769Power Unit · leakingON APPROACH TO LGA, AIRCRAFT LOST BOTH PRESSURE AND QUANTITY IN THE 'A' HYDRAULIC SYSTEM. CREW DECIDED TO DIVERT TO JFK DUE TO LONGER RUNWAYS. FLIGHT 522 MADE AN UNEVENTFUL LANDING IN JFK. NWA MAINTENANCE REPLACED THE RIGHT OUTBOARD FLAP HYDRAULIC POWER UNIFeb 10, 2000 · N729RW · Boeing 7272M7 · Trailing Edge Flap Control SystemSDR SCNA00016Line · rupturedON APPROACH, A LOSS OF THE 'A' SYSTEM HYDRAULICS WAS NOTED. MANUALLY EXTENDED THE GEAR AND A TOW TO THE GATE WAS REQUIRED. REPLACED SPOLIER 1 AND 2 RETURN RUPTURED HYDRAULIC LINE WITH A TEMPORARY LINE AND THEN PUT ON DMI.Feb 6, 2000 · N294SC · Boeing 7272M7 · Hydraulic System, MainSDR SCNA00011Warning Horn · soundedON TAKEOFF ROLL, THE TAKEOFF WARNING HORN SOUNDED. ABORTED TAKEOFF. EXERCISED AND CLEANED THE UPPER AND LOWER TRIM WARNING SWITCHES SYSTEM. TAKEOFF WARNING SYSTEM OPERATIONALLY CHECKS GOOD PER WORK CARD 3996.Jan 23, 2000 · N294SC · Boeing 7272M7 · Central WarningSDR EISA2000020Skin · crackedDURING ACCOMPLISHMENT OF A ROUTINE C-CHECK, WORKCARD FOUND CRACK IN RIGHT WING OUTBOARD AFT FLAP AT NR 2 ROLLER. FABRICATED AND INSTALLED DOUBLER PER SRM 57-50-4 FIG 5 MATERIAL IO 2024-53 .050. (M)Jan 18, 2000 · N721RW · Boeing 7272M7 · Trailing Edge FlapsSDR EISA2000021Skin · crackedDURING ACCOMPLISHMENT OF A ROUTINE C-CHECK, WORKCARD FOUND CRACK IN RIGHT WING OUTBOARD AFT FLAP AT NR 1 ROLLER. FABRICATED AND INSTALLED DOUBLER PE SRM 57-50-4 FIG 5 MATERIAL IO 2024-T3 .050. (M)Jan 18, 2000 · N721RW · Boeing 7272M7 · Trailing Edge FlapsSDR EISA2000023Floorbeam · corrodedDURING ACCOMPLISHMENT OF A ROUTINE C-CHECK, WORKCARD OF FLOORBEAM T-CAP DAMAGED AT FS 344 LBL 53 TO RBL 46. REMOVED DAMAGED FLOORBEAM UPPER T-CAP. FABRICATED REPAIR ANGLE PER SRM 53-10-8. INSTALLED PER SRM 53-10-8 MATERIAL ID BAC 1505-2922 7075-T6.(M)Jan 18, 2000 · N721RW · Boeing 7272M7 · Fuselage Main, Floor BeamSDR EISA2000024Skin · gougedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND GOUGE IN SKIN OF LOWER RUDDER RIGHT SIDE TRAILING EDGE. BURNISHED GOUGE. MATERIAL LOSS OUT OF LIMITS. FABRICATED EXTERNAL DOUBLER AND INSTALLED PER SRM 55-40-2 FIG 1. (M)Jan 18, 2000 · N721RW · Boeing 7272M7 · Rudder, Plate/SkinSDR EISA2000025Tie Clip · crackedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND TIE CLIP CRACKED AT FS 680 STRINGER 27L. REMOVED TIE CLIP. FABRICATED NEW CLIP PER SAMPLER AND INSTALLED PER SRM 51-30-2. (M)Jan 18, 2000 · N721RW · Boeing 7272M7 · Fuselage Miscellaneous StructureSDR EISA2000026Frame · crackedDURING ACCOMPLISHMENT OF A NON-ROUTINE WORK CARD, FOUND NR 3 ENGINE PYLON UPPER FORWARD MOUNT AFT T-CAP CRACKED FROM FASTENER HOLE. REMOVED AND REPLACED T-CAP ANGLE ON NR 3 PYLON PER SRM 51-10-1 AND 51-30-2. (M)Jan 18, 2000 · N721RW · Boeing 7272M7 · Nacelle/Pylon, Frame/Spar/RibSDR SCNA99159Circuit Breaker · failedAIR RETURN DUE TO ALL CIRCUIT BREAKERS FOR TANK NUMBER TWO FUEL BOOST PUMPS POPPED. FOUND NUMBER TWO FWD RT CIRCUIT BREAKER PHASE B AFT RT CIRCUIT BREAKER PHASE A AND AFT LEFT CIRCUIT BREAKERS PHASE A INTERMITTENTLY OPENING. REMOVED AND REPLACED CIRCUIT BREADec 29, 1999 · N294SC · Boeing 7272M7 · Fuel Boost Pump
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