Boeing 727-243

Service difficulty reports · 534

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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 97ZZZX1447Stringer · crackedDURING C-10 INSPECTION, A CRACK WAS NOTED ON VERTICAL STABILIZER, STR 8L AT RIB NR 7.Oct 4, 1996 · N14416 · Boeing 727243 · Vertical StabilizerSDR 97ZZZX1416Spar Cap · corrodedDURING C-10 INSPECTION, CORROSION WAS NOTED ON RT WING LOWER CAP OF FRONT SPAR, WS 519, AFT OF NR 6 L/E SLAT ACTUATOR.Oct 4, 1996 · N12411 · Boeing 727243 · Wing SparSDR CALA9601505Rib · corrodedINSPECTION FOUND RIB CORRODED AT STA 1130, STRINGER 29R. THE CORRODED SECTION OF RIB WAS REMOVED. NEW SPLICE REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 53-10-4.Oct 3, 1996 · N579PE · Boeing 727243 · Fuselage Miscellaneous StructureSDR CALA9601502Stringer · crackedINSPECTION FOUND A 1.125 INCH CRACK IN STRINGER 18A OUTBOARD FLANGE AT LT SIDE AFT OF BS 940 FRAME. THE CRACK WAS STOP DRILLED, REPAIR PARTS WERE FABRICATED AND INSTALLED IAW ECRA 5310-03340, SRM 51-10-00 AND BOEING DRAWING 65C27166.Oct 3, 1996 · N579PE · Boeing 727243 · Fuselage Main, Longeron/StringerSDR CALA9601501Frame · corrodedINSPECTION FOUND STRINGER 29R AND FRAME CORRODED AT STA 970. THE CORROSION WAS REMOVED FROM STRINGER AND FRAME IAW SRM 51-10-6. THE AREA WAS REPAIRED IAW SRM 53-10-4.Oct 3, 1996 · N579PE · Boeing 727243 · Fuselage Main, FrameSDR CALA9601500Door Frame · crackedINSPECTION FOUND A HOLE AND CRACKS IN AFT ENTRY DOOR FRAME ON LT SIDE, 31 INCHES UP FROM FLOOR. THE DAMAGED AREA WAS CUT OUT, AN ANGLE REPAIR WAS INSTALLED IAW SRM 51-40-3.Oct 3, 1996 · N579PE · Boeing 727243 · Passenger/Crew DoorsSDR CALA9601498Splice · corrodedINSPECTION FOUND STRINGER 27R SPLICES AT AFT CARGO DOOR CUTOUT LOWER CENTER SECTION CORRODED. A REPAIR WAS INSTALLED IAW ECRA 5310-02509.Oct 3, 1996 · N579PE · Boeing 727243 · Fuselage Miscellaneous StructureSDR CALA9601497Stiffener · crackedINSPECTION FOUND A 1.5 INCH CRACK IN FLOORBEAM LOWER CHORD STIFFENER AT STA 344, BL 0. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-3.Oct 3, 1996 · N579PE · Boeing 727243 · Fuselage Miscellaneous StructureSDR CALA9601496Stiffener · crackedINSPECTION FOUND A 1.5 INCH CRACK IN FLOORBEAM LOWER CHORD STIFFENER AT STA 328, LBL 24. THE STIFFENER WAS REMOVED, A NEW STIFFENER WAS FABRICATED AND INSTALLED IAW SRM 51-10-1.Oct 3, 1996 · N579PE · Boeing 727243 · Fuselage Miscellaneous StructureSDR CALA9601495Stiffener · crackedINSPECTION 'A', 2 INCH CRACK IN FLOORBEAM LOWER CHORD STIFFENER AT STA 328, RBL 48. THE CRACKED AREA WAS CUT OUT, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2.Oct 3, 1996 · N579PE · Boeing 727243 · Fuselage Miscellaneous StructureSDR 97ZZZX1495Support · crackedDURING C-10 INSPECTION, A CRACK WAS NOTED IN CABIN FLOOR SUPPORT AT STA 760.95 AT BL ZERO. REF: SI-158.1.Oct 3, 1996 · N14416 · Boeing 727243 · Fuselage Miscellaneous StructureSDR 97ZZZX1494Support · crackedDURING C-10 INSPECTION, A CABIN FLOOR SUPPORT WAS CRACKED AT STA 848.95 AT BL ZERO. REF: SI-158.1.Oct 3, 1996 · N14416 · Boeing 727243 · Fuselage Miscellaneous StructureSDR 97ZZZX1446Frame · corrodedDURING C-10 INSPECTION, CORROSION WAS NOTED ON FRAME AT STA 372 BETWEEN S16R AND S17R.Oct 3, 1996 · N14416 · Boeing 727243 · Fuselage Main, FrameSDR 97ZZZX1443Sill Web · corrodedDURING C-10 INSPECTION, CORROSION WAS NOTED ON THE R-1 DOOR BOTTOM SILL WEB BETWEEN STA 380 AND STA 420 AT S17R.Oct 3, 1996 · N14416 · Boeing 727243 · Fuselage Miscellaneous StructureSDR 97ZZZX1421Fitting · crackedDURING C-10 INSPECTION, THE LEFT MAIN LANDING GEAR REAR TRUNNION BEAM OUTBOARD ATTACH FITTING WAS FOUND CRACKED. REF: SI 106.Oct 3, 1996 · N12411 · Boeing 727243 · Wing, Landing Gear Attach FittingsSDR 97ZZZX1420Cap · corrodedDURING C-10 INSPECTION, CORROSION WAS NOTED ON LT WING LOWER CAP AT WS 437. REF: SI 104Oct 3, 1996 · N12411 · Boeing 727243 · Wing Miscellaneous StructureSDR 97ZZZX1419Floor Beam · corrodedDURING C-10 INSPECTION, CORROSION WAS NOTED ON FLOOR BEAM UPPER CORD, FS 400, WL 208.Oct 3, 1996 · N12411 · Boeing 727243 · Fuselage Main, Floor BeamSDR 97ZZZX1418Skin · corrodedDURING C-10 INSPECTION, CORROSION WAS NOTED ON BOTH LT AND RT SIDES OF AIR CONDITIONING FROM AIR INLET ACTUATOR ACCESS PANELS AT STA 720B, FROM RBL 10 TO LBL 10.Oct 3, 1996 · N12411 · Boeing 727243 · Fuselage Main, Plate/SkinSDR 97ZZZX1417Skin · corrodedDURING C-10 INSPECTION, CORROSION WAS NOTED ON EXTERNAL SKIN BETWEEN STA 1050 AND STA 1070 AT S28L.Oct 3, 1996 · N12411 · Boeing 727243 · Fuselage Main, Plate/SkinSDR CALA9601507Skin · crackedINSPECTION FOUND A .50 INCH CRACK IN LOWER SKIN OF NR 5 SLAT. THE CRACK WAS LOCATED AT CORNER OF SKIN BELOW INBOARD TRACK. THE CRACK WAS STOP DRILLED. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-50-3.Oct 2, 1996 · N579PE · Boeing 727243 · Leading Edge DevicesSDR CALA9601499Angle · crackedINSPECTION FOUND A 1 INCH CRACK IN ANGLE OF LT WING LEADING EDGE CAVITY AT STA 333. THE ANGLE WAS REMOVED, A REPLACEMENT ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-20-2.Oct 2, 1996 · N579PE · Boeing 727243 · Wing Miscellaneous StructureSDR CALA9601494Angle · crackedINSPECTION FOUND A 1.5 INCH CRACK AT AFT END OF UPPER RIB CAP INSIDE OF RT WING LEADING EDGE, FS 333. THE CRACKED ANGLE WAS REMOVED AND A REPLACEMENT ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-20-2.Oct 2, 1996 · N579PE · Boeing 727243 · Wing Miscellaneous StructureSDR 97ZZZX1424Hat Channel · corrodedDURING C-10 INSPECTION, CORROSION WAS NOTED ON HAT CHANNEL FROM STA 1136 - STA 1166, AT BL 20R.Oct 2, 1996 · N12411 · Boeing 727243 · Fuselage Miscellaneous StructureSDR 97ZZZX1423Hat Channel · corrodedDURING C-10 INSPECTION, CORROSION WAS NOTED ON HAT CHANNEL AT STA 1136, FROM BL 20R TO BL 45R.Oct 2, 1996 · N12411 · Boeing 727243 · Fuselage Miscellaneous StructureSDR 97ZZZX1422Web · corrodedDURING C-10 INSPECTION, CORROSION WAS NOTED ON WEB FROM FS 1136 TO FS 1166, FROM BL 20 RT TO BL 45 RT.Oct 2, 1996 · N12411 · Boeing 727243 · Fuselage Miscellaneous StructureSDR VSTA9609001Skin · damagedAEROSERVICES PORTABLE ENTRY STAND LOCATED AT FWD ENTRY DOOR ROLLED INTO NR 3 LEADING EDGE FLAP DURING HELICOPTER LAUNCHES CAUSING 4 CRACK INFLAP. REMOVED AND REPLACED NR 3 FLAP IAW MM 27-81-1.Sep 7, 1996 · N521DB · Boeing 727243 · Leading Edge DevicesSDR 96ZZZX4162Shear Web · corrodedRIGHT AFT LAVATORY SHEAR WEB CORRODED FROM STA 1136 TO STA 1166, BL 20R TO BL 45R. FOUND ON CPCP INSPECTION UNDER C10 CHECK.Aug 1, 1996 · N12411 · Boeing 727243 · Fuselage Miscellaneous StructureSDR CALA9600964Hyd Line · leakingTHE A-SYSTEM HYDRAULIC FLUID QUANTITY DECREASED FROM FOUR GALLONS TO .2 GALLONS DURING FLIGHT. THE GEAR AND FLAPS WERE LOWERED NORMALLY AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE HYDRAULIC A-SYSTEM RETURN LINE FROM WING TANK HEAT EXCHANGJul 4, 1996 · N17407 · Boeing 727243 · Hydraulic System, MainSDR 96ZZZX4136Hat Channel · corrodedRT AFT LAVATORY HAT CHANNEL CORRODED BL 20R, STA 1136 TO STA 1166. FOUND DURING C10 CHECK ON CPCP INSPECTION.Jul 1, 1996 · N12411 · Boeing 727243 · Fuselage Miscellaneous StructureSDR CALA9600860Floor Beam · corrodedINSPECTION FOUND CORROSION ON FLOOR BEAM AT STA 1130, RT SIDE OF AIRCRAFT. THE FLOOR BEAM WAS REPAIRED IAW ECRA 5310-03297.Jun 20, 1996 · N571PE · Boeing 727243 · Fuselage Main, Floor BeamSDR CALA9600828Frame · damagedINSPECTION FOUND IMPACT DAMAGE TO FRAMES AT STA 169.8 AND 211.5, WL 170. THE FRAMES WERE REPAIRED IAW SRM 51-40-4, FIGURE 3.Jun 12, 1996 · N578PE · Boeing 727243 · Fuselage Main, FrameSDR CALA9600772Skin · puncturedINSPECTION FOUND TWO SMALL HOLES IN FUSELAGE SKIN DUE TO GROUND DAMAGE AT STA 196 AND 211.5, RT SIDE. AN INTERIM REPAIR WAS INSTALLED IAW SRM 53-30-3, FIGURE 1, PAGE 5. A DIP WAS ISSUED TO INSPECT REPAIR EVERY 3,000 FLIGHTS AND TO PERFORM A PERMANENT REPAIR Jun 8, 1996 · N578PE · Boeing 727243 · Fuselage Main, Plate/SkinSDR 96ZZZX3524Chord · corrodedDURING C-10 CHECK, CORROSION WAS NOTED ON THE 950 BULKHEAD LOWER CHORD AT S29R.Jun 1, 1996 · N34415 · Boeing 727243 · Fuselage Main, BulkheadSDR 96ZZZX3525Floor Beam · corrodedEXFOLIATION CORROSION AT END OF SEAT TRACK FLOOR BEAM BL 24.75 RT WHERE IT ATTACHES TO STA 1130, FRAME RT.May 28, 1996 · N34415 · Boeing 727243 · Fuselage Main, Floor BeamSDR 96ZZZX2967Stringer · corrodedDURING A C-10 INSPECTION, STRINGER S28R, BETWEEN STA 480 AND STA 500, WAS NOTED TO HAVE HEAVY INTERGRANULAR CORROSION.May 1, 1996 · N34415 · Boeing 727243 · Fuselage Main, Longeron/StringerSDR 96ZZZX2966Keel Stringer · corrodedDURING C-10 CHECK, NOTED KEEL STRINGER S29R HAS INTERGRANULAR CORROSION EXTENDING FROM STA 950A TO STA 950D.May 1, 1996 · N34415 · Boeing 727243 · Fuselage Main, Longeron/StringerSDR CAL960425Dnlock Switches · inoperativeIAH - FLT 1902 - THE AIRCRAFT HAD A BRIEF HISTORY OF THE NLG RED UNSAFE LIGHT REMAINING ILLUMINATED AFTER GEAR RETRACTION. THE LIGHT EXTINGUISHED WHEN GEAR WAS CYCLED. MAINTENANCE REMOVED AND REPLACED THE NLG LOCK AND POSITION SWITCHES PER MM 32-61-71, PAGE Mar 29, 1996 · N571PE · Boeing 727243 · Landing Gear Position and WarningSDR CAL960374Hyd Pump · failedFLT NR 1929 - IAH - THE NR 1 ENGINE 'A' SYSTEM HYDRAULIC PUMP LOW PRESSURE LIGHT ILLUMINATED IN FLIGHT. THE HYDRAULIC PRESSURE ON BOTH PUMPS APPEARED NORMAL. 'ABNORMAL' CHECKLIST PROCEDURES WERE FOLLOWED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCEMar 20, 1996 · N17407 · Boeing 727243 · Hydraulic Pump (Electric/Engine), MainSDR CAL960373Flex Hose · leakingFLT NR 477 - TPA - A/C LOST THE 'B' SYS HYD FLUID IN FLT. THE LOSS WAS ACCOMPANIED BY FLICKERING 'B' SYS HYD LOW PRESS LIGHTS. CHECKLIST PROCEDURES WERE COMPLIED WITH AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MX FOUND THE HYD PRESS FLEX HOSE FROM THE NR 2 EMar 20, 1996 · N17402 · Boeing 727243 · Hydraulic System, MainSDR CAL960427Frame · crackedINSPECTION FOUND A 1.5 INCH CRACK IN AFT BAG PIT FLOOR LEVEL FRAME AT BS 1166, RBL 24. THE CRACKED AREA WAS CUT OUT. REPAIR DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 51-40-4, 51-10-2, AND 51-30-2. (M)Feb 27, 1996 · N17410 · Boeing 727243 · Fuselage Main, FrameSDR CAL960431Floorbeam · oversized holeINSPECTION FOUND OVERSIZED HOLE ON MAIN CABIN INTERIOR FLOORBEAM AT BS 350, RBL 40. THE EFFECTED SECTION WAS REMOVED. A REPAIR DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-10-1, 51-10-2, 51-30-8 AND MM 51-20-2. (M)Feb 25, 1996 · N17410 · Boeing 727243 · Fuselage Main, Floor BeamSDR CAL960433Stringer · corrodedINSPECTION FOUND STRINGER 28R CORRODED AT FORWARD CARGO COMPARTMENT BS 620. THE CORRODED SECTION OF STRINGER WAS CUT OUT. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-3, 51-10-2, AND 51-30-2. (M)Feb 22, 1996 · N17410 · Boeing 727243 · Fuselage Main, Longeron/StringerSDR CAL960432Floorbeam Web · crackedINSPECTION FOUND A .375 INCH CRACK IN LEFT FRAME OF FLOOR BEAM WEB OF RIGHT FORWARD LAV, BS 312, RBL 29. THE CRACKED AREA WAS REMOVED. A DOUBLER AND FILLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 51-30-2. (M)Feb 22, 1996 · N17410 · Boeing 727243 · Fuselage Main, Floor BeamSDR CAL960428Floor Support · crackedINSPECTION FOUND THE FORWARD FUSELAGE CARGO FLOOR SUPPORT CORRODED AND A CRACK ON UPPER FLANGE AT BS 643, RBL 20.5. THE CRACKED AREA OF FLOOR SUPPORT WAS CUT OUT. FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10-2, AND MM 51-40-5. (M)Feb 21, 1996 · N17410 · Boeing 727243 · Fuselage Miscellaneous StructureSDR CAL960435Channel · crackedINSPECTION FOUND A .5 INCH CRACK AT INBOARD SIDE OF OUTBOARD TRAILING EDGE LOWER SUPPORT CHANNEL, RIGHT WING STATION 447.9. THE CRACKED CHANNEL WAS REMOVED. A NEW CHANNEL WAS DRILLED AND INSTALLED IAW SRM 51-10-1, 51-10-2, AND 51-30-2. (M)Feb 19, 1996 · N17410 · Boeing 727243 · Wing Miscellaneous StructureSDR CAL960434Skin · separatedINSPECTION FOUND A 9 INCH SECTION OF SEPARATION ON AFT EDGE OF LEFT INBOARD MID FLAP TRAILING EDGE. THE INNER AND OUTER SKIN AND HONEYCOMB WERE REMOVED. INNER AND OUTER SKIN AND HONEYCOMB WERE FABRICATED AND COLD BONDED IAW SRM 51-40-6, 51-10-3, AND 57-50-2.Feb 19, 1996 · N17410 · Boeing 727243 · Trailing Edge FlapsSDR CAL960078Coalscer Bag · dirtyFLT NR 566 - EWR - THE RIGHT AIR CONDITIONING PACK BEGAN TO PRODUCE SMOKE IN THE CABIN WHILE ON DESCENT INTO EWR. THE COOLING DOOR WAS OPENED TO BRING TEMPERATURE DOWN AND THE SMOKE STOPPED. THE AIRCRAFT LANDED AT EWR WITHOUT INCIDENT. THE RIGHT PACK WATER Feb 4, 1996 · N17410 · Boeing 727243 · Humidity Control SystemSDR CAL960076Carbon Seal · leakingFLT NR 6834 - TPA - THE NR 2 ENGINE WAS SHUT DOWN WHILE EN ROUTE TO TPA DUE TO LOSS OF OIL QUANTITY. THE AIRCRAFT LANDED AT TPA WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 ENGINE STARTER DRIVE SPLINE ADAPTER CARBON SEAL LEAKING. THE SEAL WAS REPLACED IAW MFeb 3, 1996 · N17410 · Boeing 727243 · Turbine Engine Accessory DriveSDR CAL960251Angle · corrodedSTATION 31J - INSPECTION FOUND CORROSION AT BOTTOM OF FLOOR BEAM AT GILL SUPPORT FRAME ANGLE IN AFT CARGO PIT AT BS 1168, RBL 55. THE CORRODED AREA OF ANGLE WAS CUT OUT. A NEW ANGLE AND DOUBLER ANGLE WERE FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-20-2, ANFeb 2, 1996 · N17402 · Boeing 727243 · Fuselage Miscellaneous StructureSDR CAL960266Floor Pan · corrodedINSPECTION FOUND CENTER OF LT AFT LAV FLOOR PAN CORRODED AT BS 1140 TO BS 1176. THE CORROSION WAS REMOVED FROM THE FLOOR PAN. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND SRM 51-20-4. (X)Jan 27, 1996 · N17402 · Boeing 727243 · Fuselage Floor Panel
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