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 CALA9601399Support · corrodedINSPECTION FOUND FLOORBOARD SUPPORT CORRODED IF FORWARD CARGO COMPARTMENT AT STA 720D, STRINGER 26L. THE CORRODED AREA WAS CUT OUT, A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2.Sep 9, 1996 · N69736 · Boeing 727224 · Fuselage Miscellaneous StructureSDR CALA9601404Angle · crackedINSPECTION FOUND LOWER ANGLE OF FORWARD CARGO FORWARD BULKHEAD PANEL CRACKED AT STA 480 ABOVE STRINGER 27. THE ANGLE WAS REMOVED AND THE CRACK WAS STOP DRILLED, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-3 AND THE ANGLE WAS REINSTALLED.Sep 8, 1996 · N69736 · Boeing 727224 · Fuselage Miscellaneous StructureSDR CALA9601403Support · crackedINSPECTION FOUND FORWARD CARGO COMPARTMENT FLOORBOARD SUPPORT CRACKED AT STA 480. THE CRACKED AREA WAS CUT OUT, A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-3.Sep 8, 1996 · N69736 · Boeing 727224 · Fuselage Miscellaneous StructureSDR CALA9601402Stringer · corrodedINSPECTION FOUND STRINGER 28L CORRODED IN FORWARD CARGO COMPARTMENT BETWEEN BS 480 AND 500. THE CORRODED AREA WAS CUT OUT, A STRINGER AND SPLICE WERE FABRICATED AND INSTALLED IAW 51-20-2.Sep 8, 1996 · N69736 · Boeing 727224 · Fuselage Main, Longeron/StringerSDR CALA9601398Bracket · crackedINSPECTION FOUND BRACKET CRACKED IN RT MLG WHEEL WELL AT STA 940, STRINGER 18A. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-10-2, 51-40-5 AND 51-10-6.Sep 8, 1996 · N69736 · Boeing 727224 · Fuselage Miscellaneous StructureSDR CALA9601397Bracket · crackedINSPECTION FOUND A CRACK ON ANGLE BRACKET IN LT MLG WHEEL WELL AT STA 940, STRINGER 18A. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-10-1 AND 51-30-2.Sep 8, 1996 · N69736 · Boeing 727224 · Fuselage Miscellaneous StructureSDR CALA9601418Angle · crackedINSPECTION FOUND A 1.5 INCH CRACK IN UPPER ANGLE JUST FORWARD OF FRONT SPAR AT LT WING LEADING EDGE RIB, STA 338. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-3.Sep 7, 1996 · N69736 · Boeing 727224 · Wing Miscellaneous StructureSDR CALA9601396Stop Plate · corrodedINSPECTION FOUND RIVETS PULLING THROUGH AND BULGING UNDER STOP PLATE INSIDE C-2 DOOR AT AFT PRESSURE RELIEF DOOR. THE STOP PLATE WAS REMOVED AND REPLACED IAW SRM 51-30-2, 51-10-1 AND 51-10-6.Sep 7, 1996 · N69736 · Boeing 727224 · Cargo/Baggage DoorsSDR CALA9601395Stop Plate · corrodedINSPECTION FOUND RIVET PULLING THROUGH AND SLIGHT BULGING UNDER STOP PLATE INSIDE C-2 DOOR AT FORWARD PRESSURE RELIEF DOOR. THE STOP PLATE WAS REMOVED AND REPLACED IAW SRM 51-40-1.Sep 6, 1996 · N69736 · Boeing 727224 · Cargo/Baggage DoorsSDR CALA9601394Flying Door · crackedINSPECTION FOUND RT MLG FLYING DOOR CRACKED AT AFT SECTION LOWER CORNER NEXT TO SEAL RETAINER. THE CRACK WAS STOP DRILLED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-4.Sep 6, 1996 · N69736 · Boeing 727224 · Landing Gear DoorsSDR CALA9601432Rib · crackedINSPECTION FOUND A .50 INCH CRACK IN BOTTOM OF RIB INSIDE OF RIGHT NAV LIGHT COMPARTMENT (RT WING TIP). THE RIB WAS REMOVED . A NEW RIB WAS FABRICATED AND INSTALLED IAW SRM'S 51-10-1 AND 51-40-2. A DOUBLER WAS ALSO INSTALLED TO REPAIR CRACKED WEB IN SAME ARESep 5, 1996 · N69736 · Boeing 727224 · Wing, Rib/BulkheadSDR CALA9601431Skin · dentedINSPECTION FOUND TWO DENTS ON LOWER SURFACE OF RT OUTBOARD FLAP AFT SEGMENT. THE DENTED AREAS WERE CUT OUT. FILLERS AND CORE WERE FABRICATED AND A HOT BOND REPAIR WAS ACCOMPLISHED IAW SRM 51-40-6.Sep 5, 1996 · N69736 · Boeing 727224 · Trailing Edge FlapsSDR CALA9601433Bracket · crackedINSPECTION FOUND LOWER OUTBOARD RADIUS OF NR 6 KRUGER FLAP ACTUATOR MOUNT BRACKET CRACKED.Sep 4, 1996 · N69736 · Boeing 727224 · Leading Edge DevicesSDR CALA9601393Skin · dentedINSPECTION FOUND RT FUSELAGE SKIN DENTED JUST ABOVE ANTI- HIJACK VANE AT STA 1313. THE DENTED AREA WAS CUT OUT AND A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3.Sep 4, 1996 · N69736 · Boeing 727224 · Fuselage Main, Plate/SkinSDR CALA9601392Skin · crackedINSPECTION FOUND CONNECTING CRACKS COVERING AN AREA OF APPROXIMATELY 4 BY 8 IN LOWER INBOARD SKIN OF RT ELEVATOR. THE SKIN PANEL WAS REMOVED, A REPAIR DOUBLER WAS INSTALLED IAW SRM 55-20-3, FIGURE 5 AND THE PANEL WAS REINSTALLED.Sep 4, 1996 · N69736 · Boeing 727224 · Elevator, Plate/SkinSDR CALA9601391Skin · separatingINSPECTION FOUND RT ELEVATOR SEPARATING JUST OUTBOARD OF TAB TRAILING EDGE. THE AREA WAS SMOOTHED AND A BONDING REPAIR WAS INSTALLED IAW SRM 51-20-3.Sep 4, 1996 · N69736 · Boeing 727224 · Elevator, Plate/SkinSDR CALA9601390Skin · crackedINSPECTION FOUND INBOARD LEADING EDGE OF RT HORIZONTAL STABILIZER DENTED. A HFEC INSPECTION FOUND A .5 INCH CRACK. THE CRACKED AND DENTED AREA WAS CUT OUT, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 55-10-3.Sep 4, 1996 · N69736 · Boeing 727224 · Horizontal Stabilizer, Plate/SkinSDR CALA9601388Skin · bentINSPECTION FOUND RT SERVICE DOOR SKIN BENT AT BOTH HINGES. THE SKIN AT UPPER HINGE CUTOUT WAS STRAIGHTENED AND NO CRACKS WERE FOUND. THE LOWER HINGE CUTOUT WAS CRACKED AND THE CRACK WAS ROUTED OUT. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IASep 4, 1996 · N69736 · Boeing 727224 · Service DoorsSDR CALA9601387Skin · dentedINSPECTION FOUND LT FUSELAGE SKIN DENTED AT STA 1000, BETWEEN STRINGER 17 AND 18. THE DENTED AREA WAS CUT OUT, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3.Sep 4, 1996 · N69736 · Boeing 727224 · Fuselage Main, Plate/SkinSDR CALA9601255Fuses · blownINSPECTION FOUND THE EMERGENCY AISLE PATH LIGHTING INOPERATIVE IN FIRST CLASS CABIN. THE FORWARD BATTERY PACK FUSES WERE REPLACED AND OPERATION OF THE LIGHTS WAS RESTORED.Sep 2, 1996 · N93738 · Boeing 727224 · Emergency LightingSDR 96ZZZX5047Frame · corrodedDURING C-CHECK INSPECTION, LEVEL 2 CORROSION WAS FOUND ON FRAME 219.8, LT SIDE OF LOWER NOSE COMPARTMENT DOOR CUT-OUT.Sep 1, 1996 · N32719 · Boeing 727224 · Fuselage Main, FrameSDR CALA9601294Skin · delaminatedINSPECTION FOUND RT ELEVATOR TRIM TAB TRAILING EDGE DELAMINATED. A COLD BOND REPAIR WAS ACCOMPLISHED IAW SRM 51-40-6. WEIGHT AND BALANCE CHECKED WITHIN LIMITS IAW SRM 51-80-9.Aug 31, 1996 · N79748 · Boeing 727224 · Elevator, Tab StructureSDR MZZA96069Actuator · crackedFLT NR 916 - SPN - MAINTENANCE FOUND NR 3 LEADING EDGE SLAT LEAKING HYDRAULIC FLUID ON GROUND. MAINTENANCE REMOVED AND REPLACED NR 3 SLAT ACTUATOR DUE TO CRACK IN THE ACTUATOR HOUSING SYSTEM LEAK CHECK AND OPERATION CHECK GOOD, MM REFERENCE 27-81-22. (M)Aug 29, 1996 · N69742 · Boeing 727224 · Leading Edge Slat ActuatorSDR CALA9601289Stringer · corrodedINSPECTION FOUND STRINGER 30 CORRODED BETWEEN STA 1166 AND 1148. A STRINGER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-3-10, FIGURE 1, SHEET 1 TO 4.Aug 24, 1996 · N79748 · Boeing 727224 · Fuselage Main, Longeron/StringerSDR CALA9601288Frame · corrodedINSPECTION FOUND FRAME CORRODED BETWEEN STRINGER 27L AND 28L AT STA 1130. A SHEAR TIE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-4.Aug 24, 1996 · N79748 · Boeing 727224 · Fuselage Main, FrameSDR CALA9601299Flange · crackedINSPECTION FOUND COLLAR CRACKED THROUGH LOCKING BOLT HOLE AT PIN BETWEEN INBOARD END OF GEAR BEAM AND H-LINK IN LT WHEELWELL AREA. THE PIN RETAINER FLANGE WAS REMOVED AND REPLACED IAW SRM 57-40-0.Aug 23, 1996 · N79748 · Boeing 727224 · Wing, Landing Gear Attach FittingsSDR CALA9601296Battery · inoperativeTHE RT OVERWING EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE DURING EMERGENCY LIGHT OPERATIONAL CHECK. THE BATTERY CARTRIDGE WAS REMOVED AND REPLACED AND OPERATION OF THE EXIT LIGHT CHECKED GOOD IAW MM 33-50-0.Aug 23, 1996 · N79748 · Boeing 727224 · Emergency LightingSDR CALA9601295Skin · dentedINSPECTION FOUND RT FUSELAGE SKIN DENTED AT STA 720C. THE DENT WAS REWORKED IAW SRM 53-30-1. AN HFEC INSPECTION WAS ACCOMPLISHED WITH NO CRACKS NOTED.Aug 23, 1996 · N79748 · Boeing 727224 · Fuselage Main, Plate/SkinSDR CALA9601290Skin · crackedINSPECTION FOUND THE LT WING LEADING EDGE SKIN BENT AND WITH SEVERAL 1 INCH CRACKS AT NR 3 SLAT ACTUATOR CUTOUT. REPAIR DOUBLERS AND FILLER WERE FABRICATED AND INSTALLED IAW ECRA 5720-01540.Aug 23, 1996 · N79748 · Boeing 727224 · Wing, Plate/SkinSDR CALA9601293Skin · delaminatedINSPECTION FOUND A DENT WITH DELAMINATION 33 INCHES FROM INBOARD END LOWER SURFACE OF LT OUTBOARD AFT FLAP. THE DAMAGED AREA WAS CUT OUT AND A HOT BOND REPAIR WAS ACCOMPLISHED IAW SRM 51-40-6.Aug 22, 1996 · N79748 · Boeing 727224 · Trailing Edge FlapsSDR CALA9601292Skin · delaminatedINSPECTION FOUND LT INBOARD FORE FLAP LOWER SURFACE DELAMINATED BOTH SIDES OF NR 4 FLAP TRACK. A FIBERGLASS OVERLAY REPAIR WAS ACCOMPLISHED IAW SRM 51-40-6.Aug 22, 1996 · N79748 · Boeing 727224 · Trailing Edge FlapsSDR CALA9601291Skin · chafedINSPECTION FOUND THE RT INBOARD TRAILING EDGE AFT FLAP CHAFED AT TOP SURFACE, INBOARD END. THE CHAFED AREA WAS CUT OUT AND A HOT BOND REPAIR WAS ACCOMPLISHED IAW SRM 51-40-6.Aug 22, 1996 · N79748 · Boeing 727224 · Trailing Edge FlapsSDR MZZA96066Connector · failedGUM - FLT 958 - SITTING AT GATE WITH APU RUNING, APU ELECTRICAL POWER KICKED OFF WITH A PHASE UNBALANCED LIGHT ON, ON ELECTRICAL FAULT PANEL. SHORTLY THEREAFTER, ELECTRICAL SMOKE IN COCKPIT. FOUND T3 TERMINAL ON 'A' PHASE FEEDER CABLE BURNED AT APU GENERATORAug 18, 1996 · N69742 · Boeing 727224 · AC Power Distribution SystemSDR IXKA9600070Controller · failedTPA/ATL - FLT 12 - ON CLIMB-OUT, NR 2 A/C PACK TRIPPED. RESET, TRIPPED AGAIN. UNABLE TO MAINTAIN PRESSURIZATION ON LEFT A/C PACK. FOLLOWED ABNORMAL PROCEDURES AND RETURNED TO TPA. REMOVED AND REPLACED FAILED AUTO CONTROLLER AND OPS CHECK OK PER MM 21-31-0.Aug 16, 1996 · N32719 · Boeing 727224 · Cabin Pressure ControllerSDR CALA9601159Skin · crackedINSPECTION FOUND A 3 INCH CRACK IN FUSELAGE SKIN AFT OF RADOME AT 12 O'CLOCK POSITION. THE SKIN PANEL WAS REMOVED AND A NEW SKIN PANEL WAS FABRICATED AND INSTALLED IAW SRM 51-30-2.Aug 10, 1996 · N93738 · Boeing 727224 · Fuselage Main, Plate/SkinSDR CALA9601158Intercostal · crackedINSPECTION FOUND A .75 INCH CRACK IN THE UPPER AFT RADIUS OF CABIN FLOOR INTERCOSTAL AT B.S. 1128, BL ZERO. A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-3 AND SRM 51-30-2.Aug 10, 1996 · N93738 · Boeing 727224 · Fuselage Miscellaneous StructureSDR CALA9601161Floorbeam · corrodedINSPECTION FOUND FLOOR BEAM LOWER CHORD CORRODED AT STA 1130, RBL 1 TO RBL 40. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-04, FIGURE 1 AND SRM 51-30-2.Aug 8, 1996 · N93738 · Boeing 727224 · Fuselage Main, Floor BeamSDR CALA9601160Stringer · crackedINSPECTION FOUND NR 1 FUEL TANK STRINGER CRACKED ON HORIZONTAL FLANGE AT WS 656.50. THE CRACK WAS STOP DRILLED IAW SB 727-57A159. A REPAIR WAS FABRICATED AND INSTALLED IAW SB 727-57A159 AND EA 5762-01050, REV J.Aug 8, 1996 · N93738 · Boeing 727224 · Wing, Longeron/StringerSDR CALA9601163Rudder · chafedINSPECTION FOUND LOWER LEFT LEADING EDGE OF UPPER RUDDER CHAFED. THE ACCESS PANELS WERE REMOVED, THE AREA WAS CLEANED AND THE FASTENERS WERE REMOVED IAW SRM 51-30-2. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 55-40-3, FIGURE 1. THE ACCESS PANELS WERE REAug 6, 1996 · N93738 · Boeing 727224 · Rudder StructureSDR CALA9601165Tab · delaminatedINSPECTION FOUND LT ELEVATOR TAB DELAMINATED ALONG TRAILING EDGE. THE ELEVATOR TAB WAS REPAIRED IAW SRM 51-40-6 AND 51-40-10. THE ELEVATOR TAB WAS REBALANCED IAW SRM 51-80-9.Aug 5, 1996 · N93738 · Boeing 727224 · Elevator, Tab StructureSDR CALA9601164Fitting · corrodedINSPECTION FOUND STRINGER 22L ATTACH FITTING CORRODED AT STA 1183. THE FITTING WAS REMOVED AND REPLACED IAW SRM 53-10-3, 51-10-1, AND 51-30-2.Aug 5, 1996 · N93738 · Boeing 727224 · Fuselage Miscellaneous StructureSDR CALA9601162Skin · corrodedINSPECTION FOUND FUSELAGE SKIN CORRODED AROUND AFT LAV SERVICE PANEL AT STA 1183, STRINGER 20L TO 23L. THE CORRODED AREA OF SKIN AND STRINGER WERE REMOVED, SKIN AND STRINGER WERE FABRICATED AND INSTALLED IAW SRM 53-30-3, FIGURE 12 AND SRM 53-10-3, FIGURE 1.Aug 5, 1996 · N93738 · Boeing 727224 · Fuselage Main, Plate/SkinSDR CALA9601166Skin · wornINSPECTION FOUND NR 3 ENGINE PYLON TOP PORTION OF APRON INBOARD CENTER SECTION WORN THROUGH. THE WORN SKIN AND LONGERON WERE REMOVED. REPLACEMENT SKIN AND LONGERON WERE FABRICATED AND INSTALLED IAW SRM 54-30-2, FIGURE 1 AND 51-30-2.Aug 4, 1996 · N93738 · Boeing 727224 · Nacelle/Pylon, Plate/SkinSDR CALA9601155Skin · crackedINSPECTION FOUND A 2 INCH CRACK IN RT SIDE VERTICAL STABILIZER EXTERNAL SKIN AT FIN STA 180, STRINGER 7. THE CRACKED SECTION OF SKIN WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 55-30-3, FIGURE 1.Aug 4, 1996 · N93738 · Boeing 727224 · Vertical Stabilizer, Plate/SkinSDR CALA9601154Cover Plate · crackedINSPECTION FOUND A .25 INCH CRACK IN C-3 DOOR FORWARD FRAME COVER PLATE AT B.S. 1090, STRINGER 27. THE FRAME COVER PLATE WAS REPAIRED IAW SRM 51-40-2 AND 51-30-0.Aug 4, 1996 · N93738 · Boeing 727224 · Fuselage Miscellaneous StructureSDR CALA9601157Skin · crackedINSPECTION FOUND A .25 INCH CRACK AT FASTENER HOLE OF LEFT SIDE VERTICAL STABILIZER EXTERNAL SKIN AT FIN STA 157 BETWEEN STRINGER S 4 AND 5. THE CRACKED SECTION OF SKIN WAS REMOVED IAW SRM 55-30-3. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 55-30-3 AND SRAug 3, 1996 · N93738 · Boeing 727224 · Vertical Stabilizer, Plate/SkinSDR CALA9601156Skin · crackedINSPECTION FOUND TWO .25 INCH CRACKS AT FASTENER HOLES IN RIGHT SIDE VERTICAL STABILIZER EXTERNAL SKIN JUST BELOW PANEL 9516. THE PANEL WAS REMOVED FOR ACCESS. THE CRACKED SKIN WAS CUT OUT IAW SRM 54-30-3. REPAIR DOUBLER AND FILLER WERE FABRICATED AND INSTAug 2, 1996 · N93738 · Boeing 727224 · Vertical Stabilizer, Plate/SkinSDR CALA9601109Hyd Line · leakingTHE A-SYSTEM HYDRAULIC FLUID QUANTITY DROPPED TO ZERO ON FINAL APPROACH TO EWR. THE FLUID LOSS WAS ACCOMPANIED BY ILLUMINATION OF HYDRAULIC SYSTEM LOW PRESSURE LIGHTS. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A LEAK IN THE LEADING EDGE SLAT HYJul 31, 1996 · N69736 · Boeing 727224 · Hydraulic System, MainSDR MZZA96060Turbine · failureAT GEAR RETRACTION, PASSING ABOUT 300 FEET, NR 3 ENGINE FAILED (TURBINE SECTION) CLIMBED TO 1000 FEET, CLEANED UP, DID ENGINE FAIL CHECK LIST AND RETURNED TO PONAPE FOR NORMAL TWO ENGINE LANDING. REMOVED AND REPLACED NR 3 ENGINE PER JOB CARD 07-7100-1-8001 ANJul 26, 1996 · N69741 · Boeing 727224 · Turbine SectionSDR CALA9601045Pack · smokingWHILE OPERATING RT PACK IN MANUAL WITH MIX VALVE AT HALF POSITION, THE RIGHT PACK TEMP WENT TO 150 DEGREES AND WAS ACCOMPANIED BY CABIN SMOKE DURING DESCENT INTO EWR. THE SMOKE CLEARED WHEN COOLING DOOR WAS OPENED AND MIX VALVE WAS ADJUSTED. THE AIRCRAFT LAJul 20, 1996 · N69735 · Boeing 727224 · Cabin Cooling System
Back to Boeing 727-224