Boeing 727-224

Service difficulty reports · 2,252

Newest first. General aviation reporting is voluntary.

Query with SQL
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 = '727224'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR IXKA9500018Valve · failedON APPROACH EWR, FLT NR 10, NR 1 ENG SHUT DOWN IN FLIGHT DUE TO HIGH OIL TEMPERATURE PER A 6-7. FOUND FUEL HEAT VALVE FAILED OPEN. REMOVED AND REPLACED VALVE PER 73-14-11. PERFORMED INSPECTION AND GROUND RUN OPS CHECK OK AS PER PW MM 72-00, PG 518D. (M)May 28, 1995 · N32719 · Boeing 727224 · Engine Fuel DistributionSDR CAL950422Carriage · brokenEWR - MAINTENANCE FOUND LT MID-FLAP INBOARD CARRIAGE BROKEN. THE LT MID-FLAP INBOARD CARRIAGE WAS REMOVED AND REPLACED IAW MM 27-51-3 AND OPERATION CHECKED GOOD. (X)May 25, 1995 · N93738 · Boeing 727224 · Trailing Edge FlapsSDR CAL950372Rib · crackedGSO - INSPECTION FOUND A .5 INCH CRACK IN NR 3 SLAT RIB INBOARD OF TRACK. THE CRACK WAS STOP DRILLED. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-6 AND 57-50-3. (M)May 2, 1995 · N66734 · Boeing 727224 · Leading Edge DevicesSDR CAL950371Rib · crackedGSO - INSPECTION FOUND A .5 INCH CRACK IN NR 7 SLAT RIB AT OUTBOARD SIDE ON OUTBOARD TRACK. THE CRACK WAS STOP DRILLED. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-30-3 AND 57-50-3. (M)May 2, 1995 · N66734 · Boeing 727224 · Leading Edge DevicesSDR CAL950370Rib · crackedGSO - INSPECTION FOUND A .5 INCH CRACK IN NR 4 SLAT OUTBOARD SECOND RIB. A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 57-50-3. (M)May 2, 1995 · N66734 · Boeing 727224 · Wing, Rib/BulkheadSDR CAL950369Skin · crackedGSO - INSPECTION FOUND A .125 INCH CRACK IN THE NR 2 LEADING EDGE FLAP INNER SKIN UNDER ACTUATOR. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW EC 5720-01064 AND SRM 51-30-2. (M)May 2, 1995 · N66734 · Boeing 727224 · Leading Edge DevicesSDR CAL950368Te Panel · crackedGSO - INSPECTION FOUND THE LEFT WING UPPER SURFACE TRAILING EDGE PANEL AT OUTBOARD END OF OUTBOARD FLAP WITH A 1 INCH CRACK IN DOUBLER ATTACHED TO INBOARD SIDE. THE CRACKED DOUBLER WAS REMOVED. A NEW DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-30-1 AND 5May 2, 1995 · N66734 · Boeing 727224 · Wing, Plate/SkinSDR CAL950367Support · corrodedGSO - INSPECTION FOUND CORROSION ON LOWER SIDE OF FLOOR SUPPORT IN FORWARD PIT AT STATION 620. THE CORRODED AREA WS REMOVED AND A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-4 AND 51-30-2. (M)May 2, 1995 · N66734 · Boeing 727224 · Fuselage Miscellaneous StructureSDR CAL950366Intercostal · crackedGSO - INSPECTION FOUND THE LT MAIN LANDING GEAR BAY INTERCOSTAL AT BS 890 CRACKED AND CORRODED. THE CRACK WAS .75 INCH LONG. THE DAMAGED AREA OF INTERCOSTAL WAS CUT OUT. REPAIR FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-40-3. (May 2, 1995 · N66734 · Boeing 727224 · Fuselage Miscellaneous StructureSDR CAL950365Stringer · crackedGSO - INSPECTION FOUND, CRACKS AND CORROSION IN STRINGER 20R AT STA 500 TO 520. THE CRACKS WERE .125 INCH TO .25 INCH IN LENGTH. THE DAMAGED SECTION OF STRINGER WAS REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-3 AND 51-30-2. (Z)May 2, 1995 · N66734 · Boeing 727224 · Fuselage Main, Longeron/StringerSDR CAL950363Angle · crackedGSO - INSPECTION FOUND A .5 INCH CRACK IN FLOOR PANEL SUPPORT ANGLE AT BS 760, BL 0 - BL 24R. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 51-40-4, 51-40-3, AND 51-30-2. (W)May 2, 1995 · N66734 · Boeing 727224 · Fuselage Miscellaneous StructureSDR CAL9503624Angle · crackedGSO - INSPECTION FOUND A .5 INCH CRACK IN FLOOR SUPPORT ANGLE AT BS 760, BL 0 - BL 24L. A NEW FLOOR SUPPORT ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-40-4, AND 51-30-2. (W)May 2, 1995 · N66734 · Boeing 727224 · Fuselage Miscellaneous StructureSDR CAL950362Pressure Web · corrodedGSO - INSPECTION FOUND CORROSION ON PRESSURE WEB IN RT LAVATORY. THE CORROSION WAS REMOVED. DOUBLERS AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-30-2, AND 51-40-2. (W)May 2, 1995 · N66734 · Boeing 727224 · Fuselage Miscellaneous StructureSDR CAL950361Web · crackedGSO - INSPECTION FOUND A .25 INCH CRACK IN WEB AT STRINGER 16L, STATION 308.9 INSIDE CONTROL CABIN AT MAIN ENTRY DOOR FRAME. THE CRACKED WEB WAS REPLACED IAW SRM 51-30-2 AND 51-10-1. (W)May 2, 1995 · N66734 · Boeing 727224 · Fuselage Miscellaneous StructureSDR CAL950360Support · crackedGSO - INSPECTION FOUND A .5 INCH CRACK IN FLOOR SUPPORT FLANGE AT BS 990. A NEW FLOOR SUPPORT ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-4 AND 53-10-2. (W)May 2, 1995 · N66734 · Boeing 727224 · Fuselage Miscellaneous StructureSDR CAL950359Support · crackedGSO - INSPECTION FOUND FLOOR SUPPORT IN FORWARD PIT AT STATION 720 ABOVE STRINGER 26L CRACKED IN TWO PLACES. THE CRACKS WERE .75 INCH LONG. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-30-2, AND 53-10-5. (W)May 2, 1995 · N66734 · Boeing 727224 · Fuselage Miscellaneous StructureSDR CAL950358Rib · crackedGSO - INSPECTION FOUND A .5 INCH CRACK ON LOWER SIDE OF LEFT WING INTERNAL RIB AT WS 738.5, ABOVE S-8. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 57-10-5. (W)May 2, 1995 · N66734 · Boeing 727224 · Wing, Rib/BulkheadSDR CAL950357Chord · corrodedGSO - INSPECTION FOUND REINFORCEMENT CHORD AT STATION 1183 CORRODED. THE CHORD WAS REMOVED AND A NEW CHORD WAS INSTALLED IAW SRM 51-30-2. (W)May 2, 1995 · N66734 · Boeing 727224 · Fuselage Miscellaneous StructureSDR CAL950356Support · corrodedGSO - INSPECTION FOUND FLOOR SUPPORT CORRODED ON BOTTOM SIDE AT FORWARD PIT STATION 720. THE CORROSION WAS REMOVED AND A REPAIR WEB WAS INSTALLED IAW SRM 51-30-2. (W)May 2, 1995 · N66734 · Boeing 727224 · Fuselage Miscellaneous StructureSDR CAL950355Skin · crackedGSO - INSPECTION FOUND A .125 INCH CRACK IN SKIN AT LAP SPLICE 26L, BS 513. THE CRACKED AREA WAS CUT OUT. REPAIRED DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 53-30-3. (W)May 2, 1995 · N66734 · Boeing 727224 · Fuselage Main, Plate/SkinSDR MZZA9528Apu · failedFLT NR 93827 - CTS - DURING BOARDING, MAIN CABIN FILLED WITH SMOKE, OFF LOADED PASSENGERS. TRACED SMOKE TO FAILED APU. PLACARDED APU INOPERATIVE PER MEL 49-01. RAN ENGINES AND CLEARED CABIN AND PACKS OF RESIDUE. (W)Apr 27, 1995 · N69741 · Boeing 727224 · Airborne Auxiliary Power Unit (APU) SystemSDR MZZA95027Lock Actuator · dirtyFLT NR 932 - GUM - ON FINAL, GEAR HANDLE DOWN, NOSE GEAR DID NOT EXTEND. NOSE GEAR DOORS DID NOT OPEN. UNSAFE GEAR LIGHT NOSE, DID NOT HAVE ANNUNCIATOR NOSE GEAR LIGHT. RECYCLE GEAR, OPERATED NORMALLY. MAINTENANCE FOUND LEFT AND RT NOSE GEAR DOOR FORWARD FApr 23, 1995 · N69741 · Boeing 727224 · Landing Gear Retraction/Extension SystemSDR CAL950305Eel Battery Pack · dischargedFLT NR 0279 - EWR - A FORWARD SECTION OF EMERGENCY TRACK LIGHTING ILLUMINATED WHEN TESTED, BUT WENT DIM SHORTLY AFTER. THE FORWARD BATTERY PACK WAS REMOVED AND REPLACED AND OPERATION OF THE EMERGENCY TRACK LIGHTING WAS RESTORED. (W)Apr 20, 1995 · N79746 · Boeing 727224 · Emergency LightingSDR MZZA95026Eel · inoperativeGUM - ON B-CHECK, MAINTENANCE FOUND R-1 SERVICE DOOR EMERGENCY EXIT LIGHT INOPERATIVE AND REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. (W)Apr 19, 1995 · N69742 · Boeing 727224 · Emergency LightingSDR CAL950307Eel · inoperativeGUM - THE R-1 SERVICE DOOR EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE DURING B-CHECK. THE EMERGENCY EXIT LIGHT ASSEMBLY WAS REPLACED. (W)Apr 18, 1995 · N69742 · Boeing 727224 · Emergency LightingSDR MZZA9522Power Supply · inoperativeGUM - FLT 919 - L/P 7912625 - AFTER DEPARTURE, ALL FUEL FLOW INDICATORS WENT TO ZERO. AIRCRAFT RETURNED TO GUAM. AFTER TROUBLESHOOTING, THE AIRCRAFT FUEL FLOW POWER SUPPLY UNIT WAS FOUND AT FAULT. FUEL POWER SUPPLY UNIT WAS REMOVED AND REPLACED WITH SERVICEApr 17, 1995 · N79744 · Boeing 727224 · Fuel Flow IndicatingSDR MZZA9521Valve · malfunctionedGUM - FLT 275 - L/P 7016123 - DUE TO NR 1 FUEL MANIFOLD VALVE PREVIOUSLY PLACARDED (MEL 28-07, L/P 791622) AND THE MANIFOLD VALVE SAFETIED IN THE OPEN POSITION, FLIGHT CREW REPORTED NR 1 TANK BURNED FUEL REGARDLESS IF THE BOOST PUMPS WERE TURNED OFF WHEN ATTEMApr 14, 1995 · N79745 · Boeing 727224 · Aircraft Fuel Distribution SystemSDR MZZA9519Oil Press Transm · malfunctionedKHH - FLT 994 - L/P 7916155 - AFTER TAKEOFF, NR 1 ENGINE OIL PRESSURE WAS ABOVE RED LINE. WHEN THROTTLE RETARDED, OIL PRESSURE DECREASED. FLIGHT CREW REDUCED POWER AND AIR RETURNED TO KHH. MAINTENANCE REMOVED AND REPLACED THE OIL PRESSURE RELIEF VALVE AND OApr 11, 1995 · N79745 · Boeing 727224 · Engine Oil PressureSDR CAL950283Skin · crackedGSO - INSPECTION FOUND A .375 INCH CRACK AND A DENT IN THE LEFT WING NR 4 SLAT ACTUATOR CUT OUT. A REPAIR DOUBLER WAS FORMED AND INSTALLED IAW EC5762-01020 AND SRM 51-30-2. (W)Apr 11, 1995 · N79749 · Boeing 727224 · Wing, Plate/SkinSDR CAL950282Door Sill · corrodedGSO - INSPECTION FOUND THE AFT AIRSTAIR DOOR SILL CORRODED. THE CORROSION WAS REMOVED IAW SRM 51-10-6. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-2 AND 51-30-2. (W)Apr 11, 1995 · N79749 · Boeing 727224 · Fuselage Miscellaneous StructureSDR CAL950281Stringer · corrodedGSO - INSPECTION FOUND STRINGER 27R CORRODED AT STA 446. REPAIR ANGLES WERE FABRICATED AND INSTALLED IAW SRM 53-10-3 AND 51-30-2. (W)Apr 11, 1995 · N79749 · Boeing 727224 · Fuselage Main, Longeron/StringerSDR CAL950280Floor Support · corrodedGSO - INSPECTION FOUND CORROSION UNDER FLOOR SUPPORT AT STA 312. THE CORRODED AREA WAS CUT OUT IAW SRM 51-40-4. A REPAIR ANGLE AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 51-40-4. (W)Apr 11, 1995 · N79749 · Boeing 727224 · Fuselage Miscellaneous StructureSDR CAL950279Stringer · corrodedGSO - INSPECTION FOUND STRINGER 23R IN AFT PIT AT STA 1130 CORRODED. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 53-10-2, 53-10-3, AND 51-30-2. (W)Apr 11, 1995 · N79749 · Boeing 727224 · Fuselage Main, Longeron/StringerSDR CAL950278Support · corrodedGSO - INSPECTION FOUND L-2 DOOR THRESHOLD SUPPORT CORRODED. THE CORROSION WAS REMOVED IAW SRM 51-10-6. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 51-40-3 AND 51-30-2. (W)Apr 11, 1995 · N79749 · Boeing 727224 · Fuselage Miscellaneous StructureSDR CAL950277Angle · corrodedGSO - INSPECTION FOUND DOOR SILL ANGLE AND NUT PLATES CORRODED INSIDE WEB AT STATION 440, STRINGER 25R. THE CORROSION AND ANGLE WERE REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-2 AND 51-1-21A. (W)Apr 11, 1995 · N79749 · Boeing 727224 · Fuselage Miscellaneous StructureSDR CAL950276Stringer · crackedGSO - INSPECTION FOUND A 1 INCH CRACK IN FORWARD PIT STRINGER 28R BETWEEN STATION 420 AND 440. THE CRACKED AREA WAS CUT OUT AND CHANNEL FILLER AND SHIMS WERE FABRICATED AND INSTALLED IAW SRM 53-10-3, 51-10-2, AND 51-30-2. (W)Apr 11, 1995 · N79749 · Boeing 727224 · Fuselage Main, Longeron/StringerSDR CAL950275Intercostal · crackedGSO - INSPECTION FOUND A 1 INCH CRACK IN INTERCOSTAL UPPER FLANGE AT BS 984, LBL 37. THE INTERCOSTAL WAS REMOVED AND REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 53-10-2 AND 51-3-0. (W)Apr 11, 1995 · N79749 · Boeing 727224 · Fuselage Miscellaneous StructureSDR MZZA9517Gasket · failedGUM - FLT 917 - APPROXIMATELY 25 MINUTES OUT OF SAIPAN, FLT 917, ACFT 741, CREW REPORTED STRUT OVERHEAT LIGHT CAME ON WHEN CLIMBING THROUGH APPROXIMATELY 10,000 FEET. THROTTLE WAS BROUGHT TO IDLE AND LIGHT WENT OUT. ABNORMAL CHECKLIST WAS RUN (ENGINE BLEEDS Mar 31, 1995 · N69741 · Boeing 727224 · Pneumatic Distribution SystemSDR IXKA9500014Walking Beam · defectiveFLT 9719 - AFTER TAKEOFF, LEFT GEAR AND DOOR LIGHT ON. RETURNED TO EWR. REMOVED AND REPLACED LEFT MLG WALKING BEAM ASSY IAW MM 32-32-2. PERFORMED MULTIPLE GEAR SWINGS IAW MM 32-10-0. ALL INDICATIONS SATISFACTORY. (X)Mar 24, 1995 · N32719 · Boeing 727224 · Landing Gear Retraction/Extension SystemSDR MZZA9514Engine · failedGUM - FLT 976 - NR 2 ENGINE LOST OIL PRESSURE APPROXIMATELY 33 MINUTES OUT OF GUAM. ENGINE SHUT-DOWN PROCEDURE PERFORMED. ENGINE WINDMILL TIME 33 MINUTES, N1 18 PERCENT, N2 24 PERCENT, OIL PRESSURE 2 PSI, OIL PRESSURE AT TIME OF SHUT DOWN 5 PSI, OIL QUANTITYMar 23, 1995 · N79743 · Boeing 727224 · Engine (Turbine/Turboprop)SDR MZZA9516Roller · damagedTNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, FROZEN WATER FOUND ON RT MLG DOOR GROUND RELEASE CRANK ROLLER. THE DAMAGED ROLLER WAS REMOVED AND REPLACED PER B727 MM 32-34-21 AND OPERATIONAL CHECK FOUND SATISFACTORY. HANGAR NON-ROUTINE REPAIR, ITEMMar 14, 1995 · N69741 · Boeing 727224 · Landing Gear Door Retract SectionSDR MZZA9515Skin · corrodedTNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CORROSION FOUND ON CENTER WING LOWER SKIN AT STIFFENER S-5, LBL 27. THE CORRODED SKIN WAS CLEANED UP AND REPAIRED PER EC/RA 5710-01663. HANGAR NON-ROUTINE REPAIR, ITEM CARD NR 0729690 (SEQ NR 01038). Mar 14, 1995 · N69741 · Boeing 727224 · Wing, Plate/SkinSDR MZZA9510Engine · failedGUM - FLT 956 - DURING CLIMB PASSING 5,000 FEET, NR 3 ENGINE OIL QUANTITY DECREASING THROUGH 2.5 GALLONS, OIL PRESSURE AT 57 PSI, OIL TEMP 120 DEGREES CENTIGRADE. AT 1.6 GALLONS, AIRCRAFT SHUDDERED MODERATELY. NR 3 THROTTLE RETARDED TO CLOSED POSITION WHICH Mar 8, 1995 · N79743 · Boeing 727224 · Engine (Turbine/Turboprop)SDR MZZA9511Cable · brokenTNN - DURING 1/2D CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, EXCESSIVE BROKEN WIRES WERE FOUND ON RT/LT AFT OVERWING EMERGENCY ESCAPE HATCH STEP FORWARD CABLES. THE DAMAGED CABLE ASSEMBLIES WERE REMOVED AND REPLACED PER B727 MM 52-21-0. REF: HANGAR NON-ROUTIFeb 21, 1995 · N79744 · Boeing 727224 · Emergency ExitsSDR CAL950139Hyd Pump · leakingEWR - FLT 0376 - AIRCRAFT LOST A-SYSTEM HYDRUALIC QUANTITY WHILE EN ROUTE TO EWR. AIRCRAFT LANDED AT EWR WITHOUT INCIDENT. MAINTENANCE FOUND A-SYSTEM NR 1 ENGINE DRIVEN HYDRAULIC PUMP LEAKING. THE PUMP WAS REMOVED AND REPLACED. LEAK AND OPERATIONAL CHECKS Feb 19, 1995 · N93738 · Boeing 727224 · Hydraulic Pump (Electric/Engine), MainSDR CAL950104Eel Wiring · cutEWR - FLT 0397 - EMERGENCY AISLE PATH LIGHTING WAS FOUND INOPERATIVE IN FIRST CLASS SECTION OF CABIN DURING A PRE-FLIGHT CHECK. MAINTENANCE FOUND WIRING TO BATTERY PACK CUT UNDER LT FIRST CLASS SEATS AND 3 BLOWN FUSES. THE WIRING WAS REPAIRED AND THE THREE FFeb 8, 1995 · N79749 · Boeing 727224 · Emergency LightingSDR CAL950029Transmission · inoperativeIAH - FLT 0414 - THE OUTBOARD FLAPS HAD A HISTORY OF NOT EXTENDING BOTH ON THE GROUND AND IN-FLIGHT. MAINTENANCE FOUND EXCESSIVE SHAFT PLAY IN THE NR 8 FLAP TRANSMISSION. THE NR 8 FLAP TRANSMISSION WAS REMOVED AND REPLACED. THE FLAPS WERE OPERATED ELECTRICAJan 8, 1995 · N69735 · Boeing 727224 · Trailing Edge Flap Control SystemSDR CAL950013Control Cable · corrodedEWR - FLT 0232 - NOSE GEAR DOOR OPEN LIGHT ON FORWARD PANEL AND SECOND OFFICER'S PANEL REMAINED ILLUMINATED AFTER RAISING THE LANDING GEAR ON TAKEOFF FROM EWR. CYCLING GEAR DID NOT HELP. CREW CONFIRMED DOOR WAS OPEN BY VISUAL INSPECTION THROUGH THE VIEW PORJan 5, 1995 · N79746 · Boeing 727224 · Landing Gear Door Retract SectionSDR 95ZZZX426Control Cable · corrodedEWR - FLT 0232 - NOSE GEAR DOOR OPEN LIGHT ON FORWARD PANEL AND SECOND OFFICER'S PANEL REMAINED ILLUMINATED AFTER RAISING THE LANDING GEAR ON TAKEOFF FROM EWR. CYCLING GEAR DID NOT HELP. CREW CONFIRMED DOOR WAS OPEN BY VISUAL INSPECTION THROUGH THE VIEW PORJan 5, 1995 · N79746 · Boeing 727224 · Landing Gear Door Retract SectionSDR CAL950011Oil Press Tube · brokenGSO - FLT 0383 - THE NR 1 ENGINE OIL QUANTITY DROPPED TO ZERO WHILE EN ROUTE FROM EWR TO RSW. THE OIL PRESSURE DECREASED TO THE YELLOW ARC. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT WAS DIVERTED TO GSO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NR Jan 4, 1995 · N66734 · Boeing 727224 · Turbine Engine Oil System
Back to Boeing 727-224