Boeing 727-232

Service difficulty reports · 6,539

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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 = '727232'
  ORDER BY difficulty_date DESC"

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SDR DL72S952845Control Modular · crackedON TAXIOUT, HAD SMOKE IN CABIN. AIRCRAFT WAS EVACUATED. FOUND AILERON CONTROL MODULE WITH BLOWN SEAL AND CRACKED HOUSING, CAUSING HYDRAULIC LEAK AND CONTAMINATING APU INLET, WHICH CAUSED SMOKE IN CABIN. REPLACED MODULE, OPERATION NORMAL.Jun 12, 1995 · N526DA · Boeing 727232 · Aileron Control SystemSDR DL72S952572Stringer · corrodedCORROSION ON OB SIDE OF STGR 29L STA 1010 TO 1017, OB SIDE OF STGR 29L IS CRACKED AT STA 1012. REPAIRED PER SRM 53-10-3.Jun 11, 1995 · N416DA · Boeing 727232 · Fuselage Main, Longeron/StringerSDR DL72S952619Skin · crackedON WALK-AROUND FOUND CRACKS IN NR 5 KRUGER FLAP. CRACKS WERE REPAIRED PER SRM 57-50-3.Jun 10, 1995 · N495DA · Boeing 727232 · Leading Edge DevicesSDR CAL950471Accessory Unit · inoperativeFLT NR 0551 - IAH - THE RT MLG RED LIGHT REMAINED ILLUMINATED AFTER GEAR WAS EXTENDED ON FINAL APPROACH TO IAH. CYCLING THE GEAR DID NOT HELP. THE GEAR WAS CYCLED AGAIN DURING A 'GO AROUND' AND THE RED LIGHT EXTINGUISHED. IN ADDITION, A VISUAL CHECK CONFIRMJun 10, 1995 · N16784 · Boeing 727232 · Landing Gear Position and WarningSDR DL72S952648Bear Strap · corrodedDURING OVERHAUL, THE C-3 DOOR INTERNAL BEAR STRAP (.125 THICK 2024-T42 BARE) WAS FOUND CORRODED AT STA 1137 AND STA 1094, STR 27R. IN ACCORDANCE WITH FAA/DER FORM 8110, DATED 09 JUNE 1995, AN INTERNAL TITANIUM REPAIR DOUBLER WAS INSTALLED AT EACH LOCATION.Jun 9, 1995 · N497DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72K952550Eel Battery · dischargedDURING LAY OVER, R2 OVERWING EMERGENCY EXIT LIGHT FAILED TO TEST. REPLACED BATTERY PACK, OPERATION NORMAL.Jun 9, 1995 · N410DA · Boeing 727232 · Emergency LightingSDR DL72K952535Skin · crackedFOUND DURING A-2 LETTER CHECK - 3 EACH, .25 INCH CRACKS JUST FORWARD OF LOWER CORNER OF PNL 9501 LT SIDE, 3 EA .25 INCH CRACKS JUST FORWARD OF LOWER CORNER OF PNL 9501 RT SIDE. BOTH ITEMS REPAIRED PER MM 54-30-0, PG 801.Jun 9, 1995 · N412DA · Boeing 727232 · Vertical Stabilizer, Plate/SkinSDR DL72K952534Skin · crackedFOUND DURING A-2 LETTER CHECK - NR 2 L/E SLAT LOWER FORWARD SKIN ATTACH ANGLE CRACKED UNDER ANTI-ICE DUCT. REPAIRED PER MM 57-54-0, PG 807A.Jun 9, 1995 · N412DA · Boeing 727232 · Leading Edge DevicesSDR DL72K952533Skin · crackedFOUND DURING A-2 LETTER CHECK- .50 INCH CRACK COVESKIN ATTACH ANGLE BELOW I/B STOP PAD NR 8 SLAT, 1 INCH CRACK COVESKIN ATTACH ANGLE BELOW O/B STOP PAD NR 8 SLAT. REPAIRED BOTH CRACKS PER MM 57-54-0, PG 807.Jun 9, 1995 · N412DA · Boeing 727232 · Leading Edge DevicesSDR DL72K952532Skin · crackedFOUND DURING A-2 LETTER CHECK - .50 INCH CRACK COVESKIN ATTACH ANGLE UNDER I/B STOP PAD NR 7 SLAT. REPAIRED PER MM 57-54-0 OG 807.ER M/M 57-54-0 P807.Jun 9, 1995 · N412DA · Boeing 727232 · Leading Edge DevicesSDR DL72K952531Skin · crackedFOUND DURING A-2 LETTER CHECK - .25 INCH CRACK COVESKIN ATTACH ANGLE NR 6 SLAT BELOW TAI DUCT. REPAIRED PER MM 57-54-0, PG 807.Jun 9, 1995 · N412DA · Boeing 727232 · Leading Edge DevicesSDR CAL950467Hyd Pump · leakingFLT NR 525 - IAH - THE 'B' SYSTEM HYDRAULIC QUANTITY GAUGE INDICATED ZERO AND WAS ACCOMPANIED BY ILLUMINATION OF THE NR 2 'B' SYSTEM PUMP LIGHT WHILE IN FLIGHT. ABNORMAL PROCEDURES WERE COMPLIED WITH AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOJun 8, 1995 · N16784 · Boeing 727232 · Hydraulic Pump (Electric/Engine), MainSDR DL72S952524Air Distr · odorON APPROACH, SEVEN MINUTES PRIOR TO LANDING HAD SULFUR TYPE ODOR IN CABIN. SHUTDOWN GALLEY POWER AND GASPER, FAN ODOR QUICKLY DISSIPATED. LANDED TUL, INSPECTED CABIN LIGHTS GALLEYS, RAN AND INSPECTED PACKS, COULD NOT DUPLICATE. REPLACED WATER SEPARATOR BAGSJun 7, 1995 · N527DA · Boeing 727232 · Air Distribution SystemSDR DL72L952500Skin · crackedMAIN ENTRY DOOR OUTER SKIN IS CRACKED .125 AT RIVET, AFT UPPER CORNER. FOUND AT E-1 LTR CK. REPAIRED PER MM 52-11-01 PG 806.Jun 7, 1995 · N504DA · Boeing 727232 · Passenger/Crew DoorsSDR CALA950507Stringer · corrodedGSO - INSPECTION FOUND CORROSION ON STRINGER LOWER SURFACE AFT SIDE OF STA 720 FRAME IN FORWARD LOWER CARGO AREA. THE CORRODED SECTION WAS REMOVED AND A STRINGER AND STRINGER SPLICE WERE INSTALLED IAW SRM 53-10-3 AND SRM 51-30-2. (X)Jun 7, 1995 · N27783 · Boeing 727232 · Fuselage Main, Longeron/StringerSDR DL72S952493Angle · cracked1.25 INCH CRACK IN NR 7 SLAT ACT I/B ATTACH FITTING, AFT OF UPPER MOUNT BOLT ON WING FRONT SPAR. FOUND AT C-1 LTR CK. REPAIRED PER MM 57-42-0.Jun 6, 1995 · N529DA · Boeing 727232 · Leading Edge DevicesSDR DL72S952491Angle · crackedANGLE CRACKED .50 INCH BELOW TAI DUCT ON NR 3 SLAT. FOUND AT C-1 LTR CK. REPAIRED PER MM 57-54-0 PG 807.Jun 6, 1995 · N529DA · Boeing 727232 · Leading Edge DevicesSDR DL72S952490Fairing · crackedNR 5 SLAT I/B TRACK FAIRING CRACKED. FOUND AT C-1 LTR CK. REPAIRED PER MM 57-54-0 PG 820.Jun 6, 1995 · N529DA · Boeing 727232 · Leading Edge DevicesSDR DL72S952489Rib · cracked1) NR 7 SLAT ACT ROD END WEB CRACKED I/B AFT SIDE. 2) NR 7 SLAT ACT ROD END WEB CRACKED O/B AFT SIDE. FOUND DURING C-1 LTR CK. REPAIRED BOTH ITEMS PER MM 57-54-0 PAR 3B.Jun 6, 1995 · N529DA · Boeing 727232 · Leading Edge DevicesSDR DL72S952483Flap · crackedPREVIOUS REPAIR CRACKED AT CENTER ATTACH POINT FOR BULLNOSE, 36 INCHES FROM INBD END, OF NR 5 L/E KRUGER FLAP. REPAIRED PER SRM 57-50-3, FIG. 11 REFERENCE ERA NR 270969-14.Jun 6, 1995 · N532DA · Boeing 727232 · Leading Edge DevicesSDR DL72L952481Skin · crackedFOUND ON A1 LTR CK, 1.125 INCH CRACK AT MAIN ENT DOOR UPPER HINGE CUTOUT. REPAIR PER M/M 53-30-0 AND ERA 301886-14.Jun 5, 1995 · N512DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72L952471Rib · crackedTHE NR 7 SLAT ACTUATOR ATTACH NOSE RIB LWR SIDE AFT CRACKED .5 INCH. FOUND DURING A-1 LTR CK TPAMM. REPAIRED PER MM 57-54-0 PAR 3B.Jun 5, 1995 · N512DA · Boeing 727232 · Leading Edge DevicesSDR DL72L952470Angle · crackedA .5 INCH CRACK NR 3 SLAT COVE SKIN ATTACH ANGLE BELOW TAI DUCT. FOUND DURING A-1 LTR CK TPAMM. REPAIRED PER M/M 57-54-0 PG 807A.Jun 5, 1995 · N512DA · Boeing 727232 · Leading Edge DevicesSDR DL72L952469Angle · crackedNR 7 SLAT COVE SKIN ATTACH ANGLE UNDER TAI DUCT CRACKED 1 INCH. FOUND DURING A-1 LTR CK TPAMM. REPAIRED PER MM 57-54-0 PG 807A.Jun 5, 1995 · N512DA · Boeing 727232 · Leading Edge DevicesSDR DL72L952504Turb Shear Pin · failedTHIS ENGINE WAS EXHIBITING HIGH EGT INDICATIONS AND SENT TO ATL FOR ENGINE TEST RUN ON WING. A NORMAL START WAS PERFORMED WITH START VALVE LIGHT EXTINGUISHING. THEN, 15 MINUTES AFTER START AND IDLE THE ENGINE FIRE WARNING LIGHT ILLUMINATED, JUST PRIOR TO REAJun 4, 1995 · N503DA · Boeing 727232 · Turbine SectionSDR DL72S952660Skin · damagedNR 2 AFT FLAP REPLACED TEMP. REPAIR 50 FROM INBD END LOWER SKIN PER SRM 57-50-4, FIG. 10 AND ERA 27109-14. FOUND DURING SHOP INSPECTION.Jun 2, 1995 · N533DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S952464Fan · shortedDURING CRUISE, HAD ELECTRICAL BURNING ODOR IN CABIN AND FLIGHT DECK. ODOR STOPPED AFTER SECURING GASPER FAN. GASPER FAN WAS FOUND SHORTED. REPLACED FAN, OPERATION NORMAL.Jun 2, 1995 · N496DA · Boeing 727232 · Air Distribution FanSDR DL72S952462Fuel Control · malfunctionedDURING CRUISE, NR 3 ENGINE HAD FLUCTUATING FUEL FLOW AND N1, AND EPR. RETARDED THROTTLE, THEN ENGINE FLAMED-OUT. LANDED PHL WITHOUT INCIDENT. ENGINE WAS CHECKED PER MM, ALL PARAMETERS NORMAL. AS A PRECAUTION, THE FUEL CONTROL AND FUEL PUMP WERE REPLACED.Jun 2, 1995 · N482DA · Boeing 727232 · Fuel Control/Turbine EnginesSDR CALA950513Stringer · corrodedGSO - INSPECTION FOUND CORROSION ON STR 28R IN FORWARD BAG PIT AT STA 720. A REPAIR SPLICE WAS FABRICATED AND INSTALLED IAW SRM 51-10-6, SRM 51-30-2, AND SRM 51-20-4. (X)Jun 2, 1995 · N27783 · Boeing 727232 · Fuselage Main, Longeron/StringerSDR CALA950512Stringer · corrodedGSO - INSPECTION FOUND CORROSION ON LOWER SURFACE OF STRINGER 28L IN FORWARD BAG PIT AT STA 675. THE DAMAGED SECTION OF STRINGER WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 53-10-3 AND SRM 51-30-2. (X)Jun 2, 1995 · N27783 · Boeing 727232 · Fuselage Main, Longeron/StringerSDR CALA950506Floor · corrodedGSO - INSPECTION FOUND THE FORWARD BAG PIT CENTER FLOOR CORRODED AT STA 620. THE DAMAGED AREA WAS TRIMMED OUT AND REPAIR DOUBLER AND FILLER WERE INSTALLED IAW SRM 51-40-3 AND SRM 51-30-2. (X)Jun 2, 1995 · N27783 · Boeing 727232 · Fuselage Floor PanelSDR CALA950505Stringer · corrodedGSO - INSPECTION FOUND STRINGER 27R CORRODED IN FORWARD BAG PIT AT STA 740. THE STRINGER WAS REPAIRED IAW SRM 51-10-6, SRM 51-10-3, AND SRM 51-20-4. (X)Jun 2, 1995 · N27783 · Boeing 727232 · Fuselage Main, Longeron/StringerSDR CAL950511Skin · crackedGSO - INSPECTION FOUND FUSELAGE SKIN CRACKED THROUGH RIVET HOLES BETWEEN STA 720 AND STA 720A AT CENTERLINE ON LOWER FUSELAGE. THE CRACK WAS 2.5 INCHES LONG. THE DAMAGED AREA WAS REMOVED AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-30-3. (X)Jun 2, 1995 · N27783 · Boeing 727232 · Fuselage Main, Plate/SkinSDR CAL950510Skin · crackedGSO - INSPECTION FOUND A .25 INCH CRACK IN SKIN AT FASTENER HOLE, BS 580, LAP SEAM 26L. THE DAMAGED AREA WAS REMOVED AND REPAIRED. DOUBLER, FILLER, AND SHIM WERE INSTALLED IAW SRM 53-30-3 AND SRM 51-30-2. (X)Jun 2, 1995 · N27783 · Boeing 727232 · Fuselage Main, Plate/SkinSDR CAL950509Skin · crackedGSO - INSPECTION FOUND 3 CRACKS RUNNING FROM FASTENER HOLES IN SECTION 41 SKIN PANEL ON RT SIDE OF FUSELAGE. THE CRACKS WERE APPROXIMATELY .25 INCH LONG. THE EXISTING DOUBLER WAS REMOVED AND THE DAMAGED SKIN WAS CUT OUT. FILLERS AND DOUBLERS WERE INSTALLED Jun 2, 1995 · N27783 · Boeing 727232 · Fuselage Main, Plate/SkinSDR CAL950508Ribs · crackedGSO - INSPECTION FOUND 2 LOWER LEADING EDGE INBOARD SLAT RIBS CRACKED AT ACTUATOR. THE CRACKS WERE APPROXIMATELY .75 INCH LONG. THE CRACKS WERE STOP DRILLED AND DOUBLERS WERE INSTALLED IAW SRM 57-30-3 AND SRM 51-30-2. (X)Jun 2, 1995 · N27783 · Boeing 727232 · Leading Edge DevicesSDR CAL950504Support · corrodedGSO - THE FORWARD BAG PIT FLOOR SUPPORT JUST FORWARD OF STA 540 AND ABOVE STR 29L HAD CORROSION ON UPPER AND LOWER SURFACE. A REPAIR DOUBLER WAS INSTALLED IAW SRM 51-10-6, SRM 51-40-3, AND SRM 51-30-2. (X)Jun 2, 1995 · N27783 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CAL950503Skin · crackedGSO - INSPECTION FOUND 13 CRACKS RUNNING FROM FASTENER HOLES IN LEFT SECTION 41 SKIN PANEL. THE CRACKS RANGED IN LENGTH FROM 0.25 INCH TO 0.009 INCH. THE EXISTING DOUBLER WAS REMOVED AND THE DAMAGED AREAS WERE CUT OUT. FILLERS AND DOUBLERS WERE INSTALLED IAJun 2, 1995 · N27783 · Boeing 727232 · Fuselage Main, Plate/SkinSDR CAL950502Rib · crackedGSO - INSPECTION FOUND A 1 INCH CRACK IN RADIUS OF THE NR 3 SLAT OUTBOARD TRACK OUTBOARD RIB. THE CRACK WAS STOP DRILLED AND A REPAIR WAS INSTALLED IAW SRM 57-50-3, SRM 51-40-3, AND SRM 51-30-2. (X)Jun 2, 1995 · N27783 · Boeing 727232 · Leading Edge DevicesSDR CAL950501Rib · crackedGSO - INSPECTION FOUND A 2.25 INCH CRACK IN RADIUS OF NR 3 SLAT INBOARD TRACK INBOARD RIB. THE CRACK WAS STOP DRILLED AND A REPAIR WAS INSTALLED IAW SRM 57-30-2 AND SRM 51-30-2. (X)Jun 2, 1995 · N27783 · Boeing 727232 · Leading Edge DevicesSDR DL72S960277Skin · dentedDURING SHOP INSPECTION OF THE RT O/B AILERON, FOUND NR 0244, LOWER I/B SKIN BENT AND OVERSIZED HOLES. REPAIRED PER SRM 57-51-0. NR 9588, TOP SKIN HAS NUMEROUS OVERSIZED HOLES AND DENT. REPAIRED BY REPLACING SKIN. NR 9587, LOWER SKIN O/B 24 HAS MANY OVERSIZJun 1, 1995 · N477DA · Boeing 727232 · AileronsSDR DL72S952391Trunnion · pittedRIGHT MLG FWD TRUNNION ATTACH FITTING BUSHING IS PITTED. REPAIRED PER M/M 57-43-0.Jun 1, 1995 · N517DA · Boeing 727232 · Wing, Landing Gear Attach FittingsSDR DL72S952389Fitting · pittedRIGHT MLG SIDE BRACE AFT BEARING FITTING IS PITTED. REF MM REPAIR 57-43-00, PG 803.Jun 1, 1995 · N517DA · Boeing 727232 · Wing, Landing Gear Attach FittingsSDR DL72S952387Trunnion · pittedLEFT MLG FWD TRUNNION BEARING FITTING IS PITTED AROUND THE UPPER HOLE ON THE I/B AND O/B SURFACE OF THE O/B LUG. REF MM 57-43-00, PG 803.Jun 1, 1995 · N517DA · Boeing 727232 · Wing, Landing Gear Attach FittingsSDR DL72S952386Trunnion · corrosionLEFT MLG FWD TRUNNION BEARING FITTING HAS CORROSION ON THE O/B SURFACE OF THE I/B LUG. REF MM57-43-00, PG 803.Jun 1, 1995 · N517DA · Boeing 727232 · Wing, Landing Gear Attach FittingsSDR DL72S952385Trunnion · pittedLEFT MLG FWD TRUNNION FITTING ALL FOUR ATTACH BORES CORRODED. REF REPAIR 57-43-00, PG 803.Jun 1, 1995 · N517DA · Boeing 727232 · Wing, Landing Gear Attach FittingsSDR DL72S952384Trunnion · pittedLEFT MLG FWD TRUNNION BEARING FITTING IS PITTED AROUND THE LWR HOLE ON THE I/B AND O/B SURFACE ON THE I/B LUG. REF MM REPAIR 57-43-00, PG 803.Jun 1, 1995 · N517DA · Boeing 727232 · Wing, Landing Gear Attach FittingsSDR DL72S952383Trunnion · pittedLEFT MLG FWD TRUNNION BEARING FITTING IS PITTED AROUND UPPER HOLE ON THE I/B AND O/B SURFACE OF THE I/B LUG. REPAIRED PER MM 57-43-00 PG 803.Jun 1, 1995 · N517DA · Boeing 727232 · Wing, Landing Gear Attach FittingsSDR DL72S952382Trunnion · corrodedLEFT MLG FWD TRUNNION BEARING FITTING IS PITTED AROUND THE LWR HOLE ON THE I/B SURFACE OF THE O/B LUG. REPAIRED PER MM 57-43-00 PG 803.Jun 1, 1995 · N517DA · Boeing 727232 · Wing, Landing Gear Attach FittingsSDR DL72S952591Doubler · crackedDURING HMV, A CRACK WAS FOUND IN THE DOORWAY SURROUND DOUBLER AT THE UPPER FORWARD CORNER OF THE UPPER HINGE CUTOUT AT THE R1 DOOR. IN ACCORDANCE WITH BAC TWX DAL-ATL-95-0573RR DATED 30 MAY 1995, THE CRACK WAS STOP DRILLED AND A EXTENRNAL DOUBLER WILL BE USEDMay 31, 1995 · N497DA · Boeing 727232 · Fuselage Main, Plate/Skin
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