Boeing 727-243

Service difficulty reports · 534

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 = '727243'
  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 CALA9700518Skin · delaminatedINSPECTION FOUND OUTBOARD END OF LT OUTBOARD AILERON TAB DELAMINATED. THE TAB WAS REMOVED AND A HOT BOND REPAIR WAS ACCOMPLISHED IAW SRM 51-40-6. THE TAB WAS REINSTALLED.Mar 25, 1997 · N17410 · Boeing 727243 · Aileron TabsSDR CALA9700514Skin · disbondedINSPECTION FOUND LEFT OUTBOARD FOREFLAP DISBONDING AT INBOARD END. THE END CAP WAS REMOVED, THE DISBONDED AREA WAS CUT OUT, A HOT BOND REPAIR WAS ACCOMPLISHED IAW SRM 51-40-6 AND THE END CAP WAS REINSTALLED.Mar 25, 1997 · N17410 · Boeing 727243 · Trailing Edge FlapsSDR CALA9700513Rib · crackedINSPECTION FOUND A 1 INCH CRACK BETWEEN TWO AFT UPPER BOLTS OF LT WING LEADING EDGE RIB AT SLAT STA 0. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-3.Mar 25, 1997 · N17410 · Boeing 727243 · Wing, Rib/BulkheadSDR CALA9700311Actuator · failedTHE A-HYDRAULIC SYSTEM QUANTITY WAS LOST WHEN GEAR WAS EXTENDED FOR LANDING ON APPROACH. CHECKLIST PROCEDURES WERE COMPLIED WITH AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LT MLG DOOR RETRACT AND EXTEND ACTUATOR FAILED. THE ACTUATOR WASMar 5, 1997 · N578PE · Boeing 727243 · Landing Gear Door ActuatorSDR CALA9700293Angle · crackedINSPECTION FOUND A 1.5 INCH CRACK IN ANGLE UNDER CABIN FLOOR AT STA 297, RBL 12. THE CRACK WAS STOP DRILLED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-30-2.Feb 23, 1997 · N571PE · Boeing 727243 · Fuselage Miscellaneous StructureSDR CALA9700294Stringer · corrodedINSPECTION FOUND CORROSION IN BILGE AREA OF AFT PIT AT STA 950E, STRINGER 27R. THE CORRODED AREA WAS CUT OUT IAW SRM 53-30-3, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3.Feb 22, 1997 · N571PE · Boeing 727243 · Fuselage Main, Longeron/StringerSDR CALA9700283Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED BETWEEN TIE DOWN TRACKS AND OUTBOARD TO END AT BS 348.2, LT SIDE. THE CORRODED AREA WAS REMOVED, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-8.Feb 20, 1997 · N571PE · Boeing 727243 · Fuselage Main, Floor BeamSDR CALA9700290Skin · damagedINSPECTION FOUND DAMAGE IN THE FORM OF MATERIAL LOSS ON EDGE OF SKIN AT LT SIDE OF FUSELAGE, BS 360 BETWEEN STRINGER 17L AND 18L, AT PRODUCTION JOINT. THE AREA WAS BLENDED AND A DOUBLER WAS FABRICATED AND INSTALLED IAW ECRA 5330-02493 AND SRM 53-30-3.Feb 19, 1997 · N571PE · Boeing 727243 · Fuselage Main, Plate/SkinSDR CALA9700292Frame · crackedINSPECTION FOUND A CRACK IN RIGHT FRAME INBOARD FLANGE AT FIRST FASTENER HOLE BELOW FLOORBOARD ATTACH ANGLE AT BS 783.95. THE CRACK LENGTH WAS NOT IDENTIFIED, A REPAIR KIT WAS INSTALLED IAW BOEING DRAWING 65C36280-2.Feb 14, 1997 · N571PE · Boeing 727243 · Fuselage Main, FrameSDR CALA9700286Skin · bulgedINSPECTION FOUND RT WING OUTBOARD LOWER SKIN BULGED JUST AFT OF PANEL NR 7703. THE BULGED AREA WAS CUT OUT, A DOUBLER WAS FABRICATED AND INSTALLED IAW ECRA 5730-01484.Feb 12, 1997 · N571PE · Boeing 727243 · Wing, Plate/SkinSDR CALA9700282Skin · creasedINSPECTION FOUND A 6 INCH CREASE EXTENDING FORWARD OF DOUBLER IN RT AFT FUSELAGE AT BS 1152 TO 1121 BETWEEN STRINGER 22R AND 23R. A REPAIR DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 53-30-2, 51-30-2, 53-30-3 AND 53-30-4.Feb 12, 1997 · N571PE · Boeing 727243 · Fuselage Main, Plate/SkinSDR CALA9700285Ceiling Panel · crackedINSPECTION FOUND TWO .125 INCH CRACKS AT ONE FASTENER HEAD IN NLG CEILING PANEL AT BS 276, RBL 14. THE CRACKS WERE ROUTED OUT, A FILLER AND DOUBLER REPAIR WERE FABRICATED AND INSTALLED IAW SRM 51-40-2.Feb 11, 1997 · N571PE · Boeing 727243 · Fuselage Miscellaneous StructureSDR CALA9700284Ceiling Panel · crackedINSPECTION FOUND A .125 INCH CRACK AT TWO EACH FASTENER HEADS IN NLG CEILING PANEL AT BS 285, LBL 4. THE CRACKED AREA WAS CUT OUT, A FILLER AND DOUBLER REPAIR WERE FABRICATED AND INSTALLED IAW SRM 51-40-2.Feb 11, 1997 · N571PE · Boeing 727243 · Fuselage Miscellaneous StructureSDR CALA9700291Skin · delaminatedINSPECTION FOUND LT OUTBOARD AILERON OUTBOARD TRAILING EDGE WEDGE DELAMINATED AND ERODED. SKIN WAS FABRICATED AND INSTALLED IAW SRM 51-40-6.Feb 10, 1997 · N571PE · Boeing 727243 · AileronsSDR CALA9700177Skin · crackedINSPECTION FOUND A .5 INCH CRACK IN CUTOUT FOR NR 3 LEADING EDGE SLAT INBOARD TRACK, LT WING. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-30-4.Feb 2, 1997 · N578PE · Boeing 727243 · Wing, Plate/SkinSDR CALA9700126Pulley Assy · wornNOSE GEAR FAILED TO RETRACT AFTER TAKEOFF. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NLG DOOR FORWARD PULLEY ASSEMBLY WITH SIGNS OF CONTACTING THE PULLEY FOLLOWUP LINKAGES. THE FORWARD PULLEY ASSEMBLY WAS REMOVED AJan 31, 1997 · N571PE · Boeing 727243 · Landing Gear Door Retract SectionSDR CALA9601767Control Module · inoperativeTHE AIRCRAFT LOST A-SYSTEM HYDRAULIC PRESSURE AND QUANTITY APPROXIMATELY 10 MINUTES AFTER TAKEOFF. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE A-SYSTEM ELEVATOR CONTROL MODULE AT FAULT. THE ELEVATOR CONTROL MODULE WAS REPLACED. THE NR 1 ENGDec 9, 1996 · N578PE · Boeing 727243 · Elevator Control SystemSDR CALA9601700Angle · crackedINSPECTION FOUND RT WING NR 11 SPOILER ACTUATOR SUPPORT FITTING INBOARD ATTACH ANGLE CRACKED. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-1 AND 51-30-2.Nov 13, 1996 · N17407 · Boeing 727243 · SpoilersSDR CALA9601687Skin · corrodedINSPECTION FOUND SKIN CORRODED UNDER WEB IN AFT CARGO COMPARTMENT AT STA 970, STRINGER 28L. THE CORRODED AREA OF SKIN WAS CUT OUT, FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 53-30-3.Nov 6, 1996 · N17407 · Boeing 727243 · Fuselage Main, Plate/SkinSDR CALA9601689Stringer · corrodedINSPECTION FOUND STRINGER 28L CORRODED AT STA 965 IN AFT CARGO COMPARTMENT. THE CORRODED SECTION OF STRINGER WAS CUT OUT, A REPLACEMENT STRINGER AND SPLICE WERE FABRICATED AND INSTALLED IAW SRM 53-10-3.Nov 5, 1996 · N17407 · Boeing 727243 · Fuselage Main, Longeron/StringerSDR CALA9601697Rib · crackedINSPECTION FOUND A 1 INCH CRACK IN NR 3 SLAT ACTUATOR OUTBOARD ATTACH RIB. THE CRACK WAS STOP DRILLED, AN ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-1 AND 51-40-3.Nov 3, 1996 · N17407 · Boeing 727243 · Leading Edge DevicesSDR CALA9601696Rib · crackedINSPECTION FOUND A .75 INCH CRACK IN NR 3 SLAT ACTUATOR INBOARD ATTACH RIB. A REPAIR PART WAS FABRICATED, HEAT TREATED AND INSTALLED IAW SRM 51-40-3 AND 51-30-2.Nov 3, 1996 · N17407 · Boeing 727243 · Leading Edge DevicesSDR CALA9601699Skin · gougedINSPECTION FOUND RT WING OUTBOARD FOREFLAP INBOARD LOWER SURFACE GOUGED AND DELAMINATED. THE DAMAGED AREA WAS CUT OUT, FILLER AND DOUBLER WERE FABRICATED AND A HOT BOND REPAIR WAS ACCOMPLISHED IAW SRM 51-40-6.Nov 1, 1996 · N17407 · Boeing 727243 · Trailing Edge FlapsSDR CALA9601692Skin · crackedINSPECTION FOUND A .5 AND 1 INCH CRACK IN RT FUSELAGE SKIN JUST BELOW PANEL NR 9516, RT SIDE NR 2 ENGINE INLET. THE CRACKS WERE STOP DRILLED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 54-30-3.Nov 1, 1996 · N17407 · Boeing 727243 · Fuselage Main, Plate/SkinSDR CALA9601698Rib · crackedINSPECTION FOUND A 2 INCH CRACK AT UPPER EDGE OF RT WING LEADING EDGE RIB, SLAT STA 0. THE CRACK WAS STOP DRILLED, A WEB REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-20-1.Oct 31, 1996 · N17407 · Boeing 727243 · Wing, Rib/BulkheadSDR CALA9601695Skin · separatingINSPECTION FOUND LT OUTBOARD AILERON TAB SEPARATING AT OUTBOARD TRAILING EDGE. THE SEPARATING AREA WAS CUT OUT AND A HOT BOND REPAIR WAS ACCOMPLISHED IAW SRM 51-40-6.Oct 31, 1996 · N17407 · Boeing 727243 · Aileron TabsSDR CALA9601694Skin · delaminatedINSPECTION FOUND OUTBOARD TRAILING EDGE CORNER OF LEFT OUTBOARD AILERON DELAMINATED. THE DELAMINATED AREA WAS CUT OUT AND A HOT BOND REPAIR WAS INSTALLED IAW SRM 51-40-6.Oct 31, 1996 · N17407 · Boeing 727243 · AileronsSDR CALA9601693Skin · delaminatedINSPECTION FOUND TOP OF LT INBOARD FOREFLAP DELAMINATED AT MID SPAN. THE DELAMINATED AREA WAS CUT OUT, NEW CORE, FILLER AND DOUBLER WERE FABRICATED AND A HOT BOND REPAIR WAS ACCOMPLISHED IAW SRM 51-40-6.Oct 31, 1996 · N17407 · Boeing 727243 · Trailing Edge FlapsSDR CALA9601691Battery Pack · dischargedINSPECTION FOUND EMERGENCY PATH LIGHTS INOPERATIVE AT ROW 12 AND ROW 15 TO 23. A BROKEN WIRE WAS REPAIRED IN FORWARD SECTION AND THE FORWARD BATTERY PACK WAS REPLACED.Oct 31, 1996 · N17407 · Boeing 727243 · Emergency LightingSDR CALA9601688Skin · crackedINSPECTION FOUND A .5 INCH CRACK IN WING LEADING EDGE SKIN AT TOP OF CUTOUT FOR NR 3 SLAT OUTBOARD TRACK. THE CRACK WAS STOP DRILLED, A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-30-4.Oct 31, 1996 · N17407 · Boeing 727243 · Wing, Plate/SkinSDR CALA9601686Actuator Mount · crackedINSPECTION FOUND A .5 INCH CRACK IN NR 2 KREUGER FLAP ACTUATOR MOUNT. THE CRACK WAS LOCATED BELOW AND FORWARD OF INBOARD AND OUTBOARD LOWER MOUNT BOLTS. THE CRACK WAS STOP DRILLED, A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-10-1 AND 51-40-3.Oct 31, 1996 · N17407 · Boeing 727243 · Leading Edge Slat ActuatorSDR CALA9601524Gearbox · failedTHE NR 3 ENGINE OIL TEMPERATURE BEGAN TO RISE SHORTLY AFTER TAKEOFF. THE OIL TEMPERATURE RED LINED APPROXIMATELY 13 MINUTES AFTER TAKEOFF. THE NR 3 ENGINE WAS SHUT DOWN AND THE AIRCRAFT WAS DIVERTED TO BOS WHERE IT LANDED WITHOUT INCIDENT. THE ENGINE OIL PROct 28, 1996 · N17407 · Boeing 727243 · Turbine Engine Accessory DriveSDR CALA9601514O-Ring · leakingTHE NR 3 ENGINE BEGAN TO LOSE OIL QUANTITY AFTER TAKEOFF. THE NR 3 ENGINE WAS SHUT DOWN AND THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND PLUG ON FORWARD END OF OIL COOLER LEAKING. THE O-RING PLUG WAS REPLACED. THE NROct 27, 1996 · N17407 · Boeing 727243 · Engine Oil CoolerSDR CALA9601446Clamp · brokenON APPROACH, GEAR EXTENDED NORMAL THEN FLAPS SELECTED TO 30, A-SYTEM QUANTITY REDUCED TO 0. SYSTEM PUMPS WERE TURNED OFF. FOUND A-SYSTEM RETURN FILTER MOUNT CLAMP BROKEN. REPLACED RETURN FILTER ASSEMBLY PER MM 29-11-102 AND REPLACED ENGINE A-PUMP, EDP CASE Oct 13, 1996 · N579PE · Boeing 727243 · Hydraulic Filter, MainSDR CALA9601506Skin · corrodedINSPECTION FOUND SKIN CORRODED AT DRAIN LINE IN AFT CARGO COMPARTMENT, STA 1150, STRINGER 30. THE AREA WAS REPAIRED IAW SRM 51-10-1.Oct 11, 1996 · N579PE · Boeing 727243 · Fuselage Main, Plate/SkinSDR CALA9601503Skin · dentedINSPECTION FOUND INBOARD UPPER SKIN TRAILING EDGE OF RIGHT ELEVATOR DENTED. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 55-20-3, FIGURE 5.Oct 11, 1996 · N579PE · Boeing 727243 · Elevator, Plate/SkinSDR 97ZZZX1609Cap · corrodedDURING C-CHECK INSPECTION, CORROSION WAS NOTED ON UPPER CAP STA 328 AT LBL 20.Oct 9, 1996 · N58414 · Boeing 727243 · Fuselage Miscellaneous StructureSDR 97ZZZX1608Floor Beam · corrodedDURING C-CHECK INSPECTION, A CRACK WAS NOTED IN FLOOR BEAM UPPER CHORD AT FS 890, BL ZERO.Oct 9, 1996 · N58414 · Boeing 727243 · Fuselage Main, Floor BeamSDR 97ZZZX1445Fitting · crackedDURING C-10 INSPECTION, NOSE LANDING GEAR ACTUATOR FITTING FOUND CRACKED AT UPPER ACTUATOR ATTACH BOLT HOLE.Oct 9, 1996 · N14416 · Boeing 727243 · Landing Gear ActuatorSDR 97ZZZX1444Floor Beam · corrodedDURING C-10 INSPECTION, CORROSION WAS NOTED ON UPPER SURFACE OF FLOOR BEAM AT FS 1130 AT RBL 24.Oct 9, 1996 · N14416 · Boeing 727243 · Fuselage Main, Floor BeamSDR 97ZZZX1610Seat Track · corrodedDURING C-CHECK INSPECTION, CORROSION WAS NOTED ON 4 EACH CABIN SEAT TRACKS FROM FS 344 GTO FS 45.5 IN THE FOLLOWING BL LOCATIONS: LBL 45.5. RBL 45.5. LBL 24.75. RBL 24.75.Oct 8, 1996 · N58414 · Boeing 727243 · Fuselage, Seat/Cargo Attach FittingsSDR 97ZZZX1607Floor Beam · corrodedDURING C-CHECK INSPECTION, CORROSION WAS NOTED ON UPPER CHORD OF CABIN FLOOR BEAM FS 344.Oct 8, 1996 · N58414 · Boeing 727243 · Fuselage Main, Floor BeamSDR 97ZZZX1606Support Channel · corrodedDURING C-CHECK INSPECTION, CORROSION WAS NOTED ON SUPPORT CHANNEL AT FS 1030 FROM S30 TO S29R.Oct 8, 1996 · N58414 · Boeing 727243 · Fuselage Miscellaneous StructureSDR 97ZZZX1605Shear Tie · corrodedDURING C-CHECK INSPECTION, CORROSION WAS NOTED ON SHEAR TIE AT FRAME 950F AT S28R.Oct 8, 1996 · N58414 · Boeing 727243 · Fuselage Miscellaneous StructureSDR 97ZZZX1604Skin · damagedDURING C-CHECK INSPECTION, A LONG DENT AND CREASE WAS NOTED IN LT AFT AIRCRAFT SKIN AT FS 1130.Oct 8, 1996 · N58414 · Boeing 727243 · Fuselage Main, Plate/SkinSDR 97ZZZX1493Skin · corrodedDURING C-10 INSPECTION, CORROSION WAS NOTED ON EXTERNAL SKIN AT STA 950F AT S28L.Oct 4, 1996 · N14416 · Boeing 727243 · Fuselage Main, Plate/SkinSDR 97ZZZX1492Stringer · corrodedDURING C-10 INSPECTION, CORROSION WAS NOTED ON KEEL STRINGER S29L FROM STA 950F TO STA 1010.Oct 4, 1996 · N14416 · Boeing 727243 · Fuselage Main, Longeron/StringerSDR 97ZZZX1491Stringer · corrodedDURING C-10 INSPECTION, CORROSION WAS NOTED ON S28L FROM STA 950F TO STA 970.Oct 4, 1996 · N14416 · Boeing 727243 · Fuselage Main, Longeron/StringerSDR 97ZZZX1490I Beam · corrodedDURING C-10 INSPECTION, CORROSION WAS NOTED ON UPPER I-BEAM AT STA 1166, AT RBL 45.Oct 4, 1996 · N14416 · Boeing 727243 · Fuselage Miscellaneous StructureSDR 97ZZZX1448Web Supports · crackedDURING C-10 INSPECTION, THREE CRACKS WERE NOTED ON RT HAND LOWER TORQUE BOX HORIZONTAL WEB SUPPORTS BELOW AIRSTAIR TORQUE TUBE SUPPORT FITTING.Oct 4, 1996 · N14416 · Boeing 727243 · Fuselage Miscellaneous Structure
Back to Boeing 727-243