Boeing 727-227

Service difficulty reports · 5,082

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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 = '727227'
  ORDER BY difficulty_date DESC"

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SDR 96ZZZX5826Pulley · bearing failedDURING MID-D CHECK INSPECTION, RT INBD AILERON TAB CONTROL CABLE TURNAROUND PULLEY WAS FOUND TO HAVE A RUSTED AND FROZEN BEARING. SUSPECT CAUSES ARE WATER INTRUSION OR INSUFFICIENT LUBRICATION DURING MANUFACTURE. SUBMITTER STATED SPECIAL ATTENTION SHOULD BE Oct 25, 1996 · N76753 · Boeing 727227 · Aileron Tab Control SystemSDR 96ZZZX5825Pulley · bearing failedDURING MID-D CHECK INSPECTION, LT INBD AIL TAB CONTROL CABLE TURNAROUND PULLEY WAS FOUND TO HAVE A RUSTED AND FAILED BEARING. SUSPECT CAUSES ARE WATER INTRUSTION OR INSUFFICIENT LUBRICATION DURING BEARING MANUFACTURE. SUBMITTER STATED SPECIAL ATTENTION SHOULOct 25, 1996 · N76753 · Boeing 727227 · Aileron Tab Control SystemSDR TAOA109611Smoke Detector · failedSMOKE ALARM IN LEFT AFT LAVATORY ACTIVATED DURING LANDING, NO SIGNS OF SMOKE OR FIRE. REPLACED LEFT AFT LAVATORY SMOKE DETECTOR, OPERATIONAL CHECKS OK PER MM 26-10-00. (M)Oct 23, 1996 · N925TS · Boeing 727227 · Smoke DetectionSDR CALA9601595Stringer · corrodedINSPECTION FOUND STRINGER 24R CORRODED IN AFT CARGO COMPARTMENT AT STA 1166 UNDER CIRCUMFERENTIAL. THE CORRODED SECTION OF STRINGER WAS REMOVED AND A REPLACEMENT WAS FABRICATED AND INSTALLED IAW SRM 53-10-3.Oct 23, 1996 · N76753 · Boeing 727227 · Fuselage Main, Longeron/StringerSDR CA961114001Switch · faulty(CAN) ON DESCENT #2 ENGINE LOW OIL PRESSURE/FILTER BYPASS LIGHT ILLUMINATED. OIL TEMPERATURE, OIL QUANTITY AND OIL PRESSURE ALL INDICATED NORMAL. POWER WAS REDUCED, LIGHT WOULD NOT EXTINGUISH, #2 ENGINE WAS SHUTDOWN. POST FLIGHT INSPECTION AND ENGINE GROUND RUOct 23, 1996 · Boeing 727227 · Engine Oil PressureSDR CALA9601596Stringer · corrodedINSPECTION FOUND STRINGER 27L CORRODED FROM STA 1050-1070. THE CORRODED SECTION OF STRINGER WAS CUT OUT. A REPLACEMENT WAS FABRICATED AND INSTALLED IAW SRM 53-10-3.Oct 22, 1996 · N76753 · Boeing 727227 · Fuselage Main, Longeron/StringerSDR TAOA109609Switch · failedNR 3 ENGINE LOW OIL PRESSURE/FILTER BYPASS LIGHT CAME ON. FOLLOWED ABNORMAL CHECKLIST NO HELP. ENGINE SHUT DOWN AS A PRECAUTION. OIL PRESSURE STAYED AT 15 PLUS PSI AFTER SHUT DOWN. CHECKED MAIN ENGINE OIL FILTER-CHECKS OK. REPLACED OIL FILTER AND REPLACEDOct 18, 1996 · N926TS · Boeing 727227 · Engine Oil PressureSDR CALA9601625Stringer · corrodedINSPECTION FOUND STRINGER 30 AND SKIN CORRODED BETWEEN STA 1148 TO 1166. THE CORRODED AREA WAS CUT OUT, A STRINGER AND TWO SPLICES WERE FABRICATED AND INSTALLED IAW SRM 53-10-3.Oct 18, 1996 · N76753 · Boeing 727227 · Fuselage Main, Longeron/StringerSDR CALA9601599Skin · corrodedINSPECTION FOUND SKIN AND STRINGERS IN AFT CARGO COMPARTMENT CORRODED BETWEEN STA 1010 AND 1030, STRINGERS 30R - 29R. THE CORRODED AREAS WERE REMOVED. A REPLACEMENT CHANNEL WAS FABRICATED AND INSTALLED IAW SRM 51-10-1 AND 51-30-2.Oct 18, 1996 · N76753 · Boeing 727227 · Fuselage Main, Plate/SkinSDR CALA9601593Intercostal · crackedINSPECTION FOUND A 2 INCH CRACK AT SCREW HOLE IN FLOOR SUPPORT INTERCOSTAL BETWEEN FLOORBEAMS AT STA 990-1010, BL ZERO.Oct 18, 1996 · N76753 · Boeing 727227 · Fuselage Miscellaneous StructureSDR CALA9601590Hinge Housing · crackedINSPECTION FOUND A .50 INCH CRACK IN L-2 DOOR UPPER HINGE HOUSING. THE HINGE HOUSING WAS REMOVED AND REPLACED IAW SRM 51-10-2.Oct 18, 1996 · N76753 · Boeing 727227 · Service DoorsSDR 96FDEA01586Air Distr · odorFAINT SMELL IN CABIN BECAME A VERY HEAVY PAINT SMELL, SO MUCH SO THAT NORMAL BREATHING IN CARGO AREA WAS DIFFICULT. PAINT SMELL WAS VERY NOTICEABLE IN COCKPIT. DONNED OXYGEN AND DIVERTED TO TYS. SOURCE OF HEAVY SMELL SEEMED TO BE EMANATING FROM NORMAL CARGOOct 18, 1996 · N492FE · Boeing 727227 · Air Distribution SystemSDR CALA9601626Skin · corrodedINSPECTION FOUND FUSELAGE SKIN PANEL BULGED JUST AFT OF RT RAM AIR DOOR ACTUATOR STA 720, STRINGER 28R. THE CORROSION WAS REMOVED, A FILLER AND DOUBLER WAS FABRICATED AND INSTALLED IAW ECRA 5330-02459.Oct 17, 1996 · N76753 · Boeing 727227 · Fuselage Main, Plate/SkinSDR CALA9601532Angle · corrodedINSPECTION FOUND THE RIGHT AFT LAV FLOOR SUPPORT, JUST AFT OF FORWARD WALL U-CHANNEL CORRODED AT BS 1140. THE SUPPORT ANGLE WAS REMOVED AND A REPLACEMENT WAS FABRICATED AND INSTALLED IAW SRM 51-40-4.Oct 17, 1996 · N76753 · Boeing 727227 · Fuselage Miscellaneous StructureSDR CALA9601622Floorbeam · corrodedINSPECTION FOUND CORROSION ON TOP OF FLOORBEAM AT BS 380, RBL 48 TO RBL 67. THE CORRODED AREA WAS CUT OUT, A REPAIR WAS INSTALLED IAW SRM 53-10-8, FIGURE 1.Oct 16, 1996 · N76753 · Boeing 727227 · Fuselage Main, Floor BeamSDR CALA9601592Angle · corrodedINSPECTION FOUND FORWARD LAV FLOOR ANGLE CORRODED AT B.S. 392. THE FLOOR ANGLE WAS REMOVED AND A REPLACEMENT ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-1.Oct 16, 1996 · N76753 · Boeing 727227 · Fuselage Miscellaneous StructureSDR AALA961520Beam · corrodedTUL - FOUND CORROSION UPPER HORIZONTAL TE BEAM 2 PLACES BEYOND LIMITS. CUT OUT AND BLENDED AREAS. TREATED AND PRIMED, REPAIRED PER ESO 11697 AND SRM 55-10-6 FIG 1. (M)Oct 16, 1996 · N726AA · Boeing 727227 · Horizontal Stabilizer StructureSDR AALA961519Stringer · corrodedTUL - FOUND STRINGER 22L HEAVILY CORRODED STATION 1166 TO 1183. REPAIRED STRINGER 22L, STATION 1166 TO 1183 PER SRM 53-10-3 AND STATION 1183, STRINGER 22L AND FITTING REPLACED. (M)Oct 16, 1996 · N726AA · Boeing 727227 · Wing, Longeron/StringerSDR AALA961517Skin · corrodedTUL - FOUND SKIN BULGING AND FASTENER HEAD SHEAR BELOW AFT LAV SERVICE DOOR. REPAIRED AFFECTED AREA PER ESO 11697 DATED 2 OCT 1996. (M)Oct 16, 1996 · N726AA · Boeing 727227 · Fuselage Main, Plate/SkinSDR AALA961515Skin · corrodedTUL - FOUND LOWER WING SKIN CORRODED ABOVE AFT HEAT EXCHANGER INBOARD DUCT MOUNT ANGLE. CORROSION ON BOTH SIDES OF ANGLE APPROX 3 INCH DIAMETER. REMOVED CORROSION AND REPAIRED PER ESO 11697, DATED 10-8-96. (M)Oct 16, 1996 · N726AA · Boeing 727227 · Wing, Plate/SkinSDR AALA961511Skin · corrodedTUL - FOUND FUSELAGE SKIN LAP HAS 3 POPPED RIVETS AND BUBBLED SKIN STRINGER 26L. REMOVED DAMAGED SKIN AND INSTALLED DOUBLER REPAIR PER SRM 53-30-3 FIG 14 PAGE 80 A. (M)Oct 16, 1996 · N726AA · Boeing 727227 · Fuselage Main, Plate/SkinSDR CALA9601624Angle · corrodedINSPECTION FOUND LOWER BEACON LIGHT PANEL BULGED AT RT EDGE. CORRODED ANGLES WERE REMOVED AND REPLACEMENT ANGLES WERE FABRICATED AND INSTALLED IAW SRM 51-40-4.Oct 15, 1996 · N76753 · Boeing 727227 · Fuselage Miscellaneous StructureSDR CALA9601598Skin · crackedINSPECTION FOUND THREE 1 INCH CRACKS IN RT NR 4 LEADING EDGE FLAP AFT SURFACE. THE CRACKS WERE STOP DRILLED. DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 51-10-1, 51-10-2, AND ECRA 5720-01064.Oct 15, 1996 · N76753 · Boeing 727227 · Leading Edge DevicesSDR CALA9601597Skin · crackedINSPECTION FOUND A 1 INCH CRACK IN LOWER OUTBOARD AREA OF RT NR 4 LEADING EDGE FLAP AFT SURFACE. THE CRACK WAS STOP DRILLED. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-10-1, 51-10-2, AND ECRA 5720-01064.Oct 15, 1996 · N76753 · Boeing 727227 · Leading Edge DevicesSDR CALA9601594Skin · crackedINSPECTION FOUND A 3 INCH CRACK IN LOWER FUSELAGE SKIN AT STA 1050, STRINGER 27L. THE CRACKED AREA WAS CUT OUT. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3 AND 51-40-5.Oct 15, 1996 · N76753 · Boeing 727227 · Fuselage Main, Plate/SkinSDR CALA9601591Intercostal · brokenINSPECTION FOUND INTERCOSTAL BROKEN OUT ALONG TOP AT SCREW HOLES (BELOW FLOOR PANEL NR 49) AT BL ZERO BETWEEN FLOORBEAMS, B.S. 720-720A. THE INTERCOSTAL ANGLE WAS REMOVED AND A REPLACEMENT ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-1.Oct 15, 1996 · N76753 · Boeing 727227 · Fuselage Miscellaneous StructureSDR CALA9601589Skin · dentedINSPECTION FOUND THE RT FUSELAGE SKIN DENTED AT STA 416 JUST BELOW AND AFT OF OXYGEN SERVICE DOOR. THE DENTED AREA WAS CUT OUT. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-30-3, FIGURE 1.Oct 15, 1996 · N76753 · Boeing 727227 · Fuselage Main, Plate/SkinSDR CALA9601588Skin · crackedINSPECTION FOUND THE RT WING LEADING EDGE SKIN DENTED WITH A .25 INCH CRACK JUST OUTBOARD OF NR 5 SLAT INBOARD TRACK. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 57-30-4, FIGURE 1.Oct 15, 1996 · N76753 · Boeing 727227 · Wing, Plate/SkinSDR CALA9601531Skin · gougedINSPECTION FOUND THE RT ELEVATOR LOWER SKIN GOUGED JUST AFT OF NR 2 HINGE. THE GOUGED AREA WAS CUT AWAY. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 55-30-3.Oct 15, 1996 · N76753 · Boeing 727227 · Elevator, Plate/SkinSDR AALA961513Skin · corrodedTUL - FOUND LOWER WING SKIN CORRODED ABOVE THE AFT HEAT EXCHANGER INBOARD DUCT STATION 826. REMOVED AND BLENDED CORROSION PER SRM 51-10-6. PERFORMED THICKNESS CHECK RANGE FROM .209 TO .238, ORIGINAL THICKNESS .220-0226. (M)Oct 13, 1996 · N726AA · Boeing 727227 · Wing, Plate/SkinSDR TAOA109608Fitting · exceeded limitsDURING D-CHECK, THE VERTICAL STABILZIER TENSION TIES REQUIRED REWORK ACCORDING TO BOEING SB 55-0071. THE REWORK DIMENSIONS SET FORTH EXCEEDED THE SB LIMITS. REWORK DIMENSIONS WERE APPROVED BY BOEING. (X)Oct 11, 1996 · N926TS · Boeing 727227 · Vertical StabilizerSDR AALA961489Skin · crackedTUL - FOUND FORWARD ENTRY DOOR UPPER HINGE CUT OUT, SKIN CRACKED APPROX .1875 INCH LONG AT 10 O'CLOCK POSITION. INSTALLED DOUBLER AS PER SERVICE BULLETIN 727-53-0198. (M)Oct 9, 1996 · N726AA · Boeing 727227 · Fuselage Main, Plate/SkinSDR SCNA96268Battery · dischargedFOUND AFT AIRSTAIR EMERGENCY LIGHT INOP. REPLACED BATTERIES AND OPS CHECKED GOOD.Sep 29, 1996 · N275AF · Boeing 727227 · Emergency LightingSDR MZZA96078Skin · gougedDURING B-CHECK, LEFT AFT FUSELAGE SKIN HAS 2 DEEP GOUGES LOCATED AT BS 1151.5 AND RIGHT BELOW STRINGER 21L. CUT OUT DAMAGED AREA, FABRICATED FILLER FROM .080, 2024T3 ALUMINUM SHEET AND REPAIR DOUBLER FROM .090 2024T3. INSTALLED REPAIR WITH SOLID FASTENERS PESep 27, 1996 · N89427 · Boeing 727227 · Fuselage Main, Plate/SkinSDR AALA961424Angle · corrodedTUL - FOUND LEFT CREASE ANGLE CORRODED STATION 1060 TO 1170. CUT OUT CORRODED AREA AND INSTALLED ANGLE PER SRM 51-10-1 FIG 4. (M)Sep 25, 1996 · N717AA · Boeing 727227 · Fuselage Miscellaneous StructureSDR AALA961423Splice Plate · crackedTUL - SPLICE PLATE CRACKED ABOVE NR 5 LEFT FLAP ACT. STOP DRILLED CRACKS AND INSTALLED DOUBLER PER SRM 51-40-02 R8-12. (M)Sep 25, 1996 · N717AA · Boeing 727227 · Wing Miscellaneous StructureSDR AALA961421Floor · corrodedTUL - FOUND CORROSION ON LEFT AFT LAV FLOOR AT STATION 1170 TO STATION 1176. REMOVED CORROSION AND INSTALLED DOUBLER PER SRM 51-40-2 PAGES 1-6. (M)Sep 25, 1996 · N717AA · Boeing 727227 · Fuselage Floor PanelSDR AALA961420Skin · dentedTUL - FOUND DENT IN FUSELAGE SKIN STATION 640, STRINGER 25L. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER PER SRM 53-30-3 FIG 3. (M)Sep 25, 1996 · N717AA · Boeing 727227 · Fuselage Main, Plate/SkinSDR AALA961419Skin · damagedTUL - FOUND DAMAGED SKIN AT BS 683. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER PER SRM 53-30-3 FIG 1. (M)Sep 25, 1996 · N717AA · Boeing 727227 · Fuselage Main, Plate/SkinSDR AALA961359Skin · crackedTUL - FOUND CRACK IN SKIN RIGHT SIDE OF VERT. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 55-30-07-1 PG 3. (M)Sep 17, 1996 · N718AA · Boeing 727227 · Vertical Stabilizer, Plate/SkinSDR AALA961356Trunnion Fitting · corrodedTUL - FOUND CORROSION AT 2 FASTENERS, AFT OUTBOARD END OF LEFT TRUNNION FITTING. OBTAINED ESO 11697, DATED 9-9-96, AARD AND BLENDED AREA, REMOVED CORROSION. HFEC AREA TO CONFIRM DEPTH, TREATED AND PRIMED. (M)Sep 17, 1996 · N718AA · Boeing 727227 · Fuselage, Landing Gear Attach FittingsSDR TAOA099606Compressor · stalledDURING TAKEOFF, COMPRESSOR STALL REPORTED TO BE LEFT SIDE AT 800 FEET ALTITUDE. RAN ALL THREE ENGINES, CHECKED THE POWER, BLEED SCHEDULING AND ACCELERATION. ALL CHECKED OK WITH NO STALLS. ACCOMPLISHED COMPRESSOR WASH NR 1 ENGINE, RAN ENGINE, ALL NORMAL IAW Sep 10, 1996 · N925TS · Boeing 727227 · Turbine Engine Compressor SectionSDR CA960919002Line · leaks(CAN) "A" SYSTEM HYDRAULIC FLUID LOSS AIRCRAFT RETURNED, LEAK AT AFT STAIRWELL AREA RH SIDE, #2 HYDRAULIC PUMP PRESSURE LINE WAS TEMPORARY FIX, REPLACED.Sep 10, 1996 · Boeing 727227 · Hydraulic System, MainSDR SCNA96249Bulb · failedLEFT AFT OVERWING EXIT LOWER SIGN HAS A BULB INOP. RELAMPED EMERGENCY EXIT LIGHTING AND OPS CHECKED GOOD IN ACCORDANCE WITH MM 33-50-01.Sep 8, 1996 · N275AF · Boeing 727227 · Emergency LightingSDR SCNA96244Bulb · failedTHE AFT EXTERIOR OVERWING EMERGENCY LIGHT WAS FOUND INOP. REMOVED AND REPLACED THE AFT LAMP, AND OPS CHECKED NORMAL.Sep 3, 1996 · N275AF · Boeing 727227 · Emergency LightingSDR CALA9601265Floorbeam · corrodedINSPECTION FOUND LOWER SURFACE OF FLOOR BEAM CORRODED AT F.S. 1130. THE AREA WAS REPAIRED IAW ECRA 5310-03318.Sep 2, 1996 · N70755 · Boeing 727227 · Fuselage Main, Floor BeamSDR AALA961300Operating Rod · defectiveDFW - FLT 1503 - DURING APPROACH TO DFW WHEN LANDING GEAR EXTENDED, NOSE LANDING GEAR DID NOT EXTEND. RECYCLED LANDING GEAR AND NOSE LANDING GEAR EXTENDED NORMALLY. AIRCRAFT LANDED DFW WITHOUT INCIDENT. REPLACED AND RIGGED NOSE LANDING GEAR DOOR OPERATING RAug 30, 1996 · N717AA · Boeing 727227 · Landing Gear Door Retract SectionSDR TAOA089612Uplock Sensor · inoperativeRIGHT MAIN GEAR UNSAFE LIGHT CAME ON DURING GEAR EXTENSION, LIGHT WENT OUT UNDER 160 KTS. VISUAL INDICATION CONFIRMED GEAR DOWN AND LOCKED. REPLACED RIGHT UPLOCK SENSOR PER 32-61-01, OPERATIONAL CHECKED NORMAL PER MM CHAPTER 32-61-81. (M)Aug 28, 1996 · N925TS · Boeing 727227 · Landing Gear Retraction/Extension SystemSDR CA960919004Probe · broken wire(CAN) #2 ENGINE SHUT DOWN IN CLIMB DUE TO OIL TEMPERATURE AT ALLOWABLE MAXIMUM. BROKEN GROUND WIRE AT PROBE.Aug 28, 1996 · Boeing 727227 · Engine Oil TemperatureSDR TAOA089610Slide · deployedFLT ATTENDANT TRAINING, DEPLOYED SLIDE FROM FORWARD RIGHT GALLEY SERVICE DOOR. SLIDE INFLATION AND EMERGENCY LIGHTS CHECKED NORMAL. (M)Aug 27, 1996 · N925TS · Boeing 727227 · Escape Slide
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