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 CALA9801502Support · corrodedINSPECTION FOUND LT AFT LAV AISLE SIDEWALL FLOOR SUPPORT CORRODED. THE FLOOR SUPPORT WAS REMOVED IAW SRM 51-10-1. A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-10-1, PAGE 4.Aug 25, 1998 · N32725 · Boeing 727224 · Fuselage Miscellaneous StructureSDR CALA9801446Angle · crackedINSPECTION FOUND A .5 INCH CRACK IN RT WING TRAILING EDGE UPPER ATTACH ANGLE ABOVE NR 6 GEARBOX FOR FLAP. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-1, 51-10-2, AND 51-10-6.Aug 11, 1998 · N66734 · Boeing 727224 · Wing Miscellaneous StructureSDR CALA9801445Panel · crackedINSPECTION FOUND THREE CRACKS IN LT HORIZONTAL STABILIZER BALANCE PANEL NR 9116. THE CRACKS WERE STOP DRILLED IAW SRM 51-10-1. TWO EACH DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 55-20-3.Aug 11, 1998 · N66734 · Boeing 727224 · Horizontal Stabilizer, Plate/SkinSDR CALA9801439Stiffener · crackedINSPECTION FOUND A 0.3 INCH CRACK IN AFT CARGO COMPARTMENT STIFFENER AT STA 950A, LONGERON 30R. THE STIFFENER WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-40-4.Aug 11, 1998 · N32725 · Boeing 727224 · Fuselage Miscellaneous StructureSDR CALA9801438Fitting · crackedINSPECTION FOUND A 0.6 CRACK IN FITTING AT RT INBOARD MIDFLAP RIB LEADING EDGE JUST OUTBOARD OF NR 5 CARRIAGE. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-10-1, PAGE 4. FASTENERS WERE INSTALLED IAW SRM 51-30-2.Aug 11, 1998 · N32725 · Boeing 727224 · Trailing Edge FlapsSDR CALA9801437Circumferential · corrodedINSPECTION FOUND CORROSION ON FORWARD AND AFT FACE OF CIRCUMFERENTIAL AT LOWER FORWARD NOSE COMPARTMENT, BS 219 BETWEEN STRINGER 24R AND 26R. THE CORRODED AREA WAS CUT OUT IAW SRM 51-40-2. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2, 51-10-Aug 10, 1998 · N32725 · Boeing 727224 · Fuselage Main, FrameSDR CALA9801436Web · crackedINSPECTION FOUND A .5 INCH CRACK IN WEB PANEL NEXT TO BOOST PUMP INSIDE NR 2 FUEL TANK AT LT WS 171.50. THE WEB PANEL WAS REPAIRED IAW SRM 51-40-2, FIGURE 1.Aug 10, 1998 · N32725 · Boeing 727224 · Wing Miscellaneous StructureSDR CALA9801435Seat Track · corrodedINSPECTION FOUND SEAT TRACK CORRODED AT BS 380-420, RBL 24. THE SEAT TRACK WAS REMOVED AND A NEW TRACK WAS FABRICATED AND INSTALLED IAW SRM 53-10-5 AND 51-10-5.Aug 10, 1998 · N32725 · Boeing 727224 · Fuselage, Seat/Cargo Attach FittingsSDR CALA9801434Bracket · crackedINSPECTION FOUND A 1 INCH CRACK AT LOWER AFT END OF AFT CARGO C-2 DOOR FRAME SIDE BRACKET. THE DOOR FRAME BRACKET WAS REMOVED AND REPLACED IAW SRM 51-30-2.Aug 10, 1998 · N32725 · Boeing 727224 · Cargo/Baggage DoorsSDR CALA9801433Stringer · crackedINSPECTION FOUND A .5 INCH CRACK AT ATTACH BOLT IN NR 7 STRINGER OF RT VERTICAL STABILIZER INNER COMPARTMENT AT NR 4 RIB. THE CRACKED SECTION WAS REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 55-30-4.Aug 10, 1998 · N32725 · Boeing 727224 · Vertical StabilizerSDR CALA9801429Spar Web · crackedINSPECTION FOUND A .25 INCH CRACK IN SECOND FROM AFT VERTICAL WEB AT RT WING FRONT SPAR CHORD INBOARD AREA JUST FORWARD OF BOTTLE PIN. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-3 AND 51-10-2.Aug 7, 1998 · N32725 · Boeing 727224 · Wing SparSDR CALA9801428Angle · crackedINSPECTION FOUND A .5 INCH CRACK IN FORWARD ANGLE AT RT WING LEADING EDGE FLAP WELL LOWER STIFFENER, FS 150. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-2.Aug 7, 1998 · N32725 · Boeing 727224 · Wing Miscellaneous StructureSDR CALA9801427Skin · crackedINSPECTION FOUND A .5 INCH CRACK IN LT INBOARD FLAP AFT SEGMENT LEADING EDGE SKIN, 64 INCHES FROM OUTBOARD END. THE CRACKED AREA WAS REMOVED. A REPAIR ANGLE AND STRAP WERE FABRICATED AND INSTALLED IAW SRM 51-40-2 AND 51-10-6.Aug 7, 1998 · N32725 · Boeing 727224 · Trailing Edge FlapsSDR CALA9801426Skin · crackedINSPECTION FOUND A .5 INCH CRACK IN LT INBOARD MIDFLAP LOWER TRAILING EDGE SKIN, 32 INCHES FROM INBOARD END. THE CRACK WAS STOP DRILLED. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-10-6 AND 51-10-1.Aug 7, 1998 · N32725 · Boeing 727224 · Trailing Edge FlapsSDR CALA9801425Angle · crackedINSPECTION FOUND A .15625 CRACK IN SUPPORT ANGLE FOR LT WING TRAILING EDGE PANEL FORWARD OF OUTBOARD AILERON, OUTBOARD OF AILERON LOCKOUT. THE CRACKED AREA WAS ROUTED OUT. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-40-1 AND 51-10-2.Aug 7, 1998 · N32725 · Boeing 727224 · Wing Miscellaneous StructureSDR CALA9801424Skin · crackedINSPECTION FOUND A .75 INCH CRACK IN RT WING INBOARD MIDFLAP LOWER CUTOUT FOR INBOARD ACTUATING ROD. THE CRACK WAS STOP DRILLED. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-2.Aug 7, 1998 · N32725 · Boeing 727224 · Trailing Edge FlapsSDR CALA9801417Anti-Ice Duct · blownTHE FIRE WARNING BELL SOUNDED FOLLOWED BY ILLUMINATION OF THE NR 3 ENGINE FIRE WARNING LIGHT ON CLIMB-OUT OF IAH AT ABOUT 900 FEET. THE NR 3 ENGINE POWER WAS REDUCED AND THE FIRE WARNINGS CEASED. A VALID FIRE TEST WAS RUN. THE LIGHT AND BELL CAME ON AGAIN WAug 7, 1998 · N69735 · Boeing 727224 · Engine Anti-Icing SystemSDR CALA9801414Skin · crackedINSPECTION FOUND A .15625 AND .09375 CRACK IN LT WING NR 4 SLAT LOWER TRAILING EDGE SKIN AT RADIUS OUTBOARD OF INBOARD TRACK, 36.5 INCHES FROM INBOARD END. THE CRACK WAS STOP DRILLED. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-50-3, 51-10-2, AND 51-40Aug 7, 1998 · N66734 · Boeing 727224 · Leading Edge DevicesSDR CALA9801413Bracket · crackedINSPECTION FOUND A .5 INCH CRACK IN INBOARD BRACKET WHERE LT WING NR 1 LEADING EDGE FLAP ACTUATOR MOUNTS. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-40-3.Aug 7, 1998 · N66734 · Boeing 727224 · Wing, Control Surface Attach FittingsSDR CALA9801412Bracket · crackedINSPECTION FOUND A .75 INCH CRACK IN INBOARD BRACKET WHERE LT WING NR 2 LEADING EDGE FLAP ACTUATOR MOUNTS. THE BRACKET WAS REMOVED IAW SRM 51-30-2. A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-10-1 AND 51-10-2.Aug 7, 1998 · N66734 · Boeing 727224 · Wing, Control Surface Attach FittingsSDR CALA9801406Angle · corrodedINSPECTION FOUND RT AFT LAV FLOOR ANGLE CORRODED OUTBOARD OF DUMP CHUTE AREA. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-6, 51-10-1, 51-30-2, AND 51-10-2.Aug 7, 1998 · N32725 · Boeing 727224 · Fuselage Miscellaneous StructureSDR CALA9801405Floor · corrodedINSPECTION FOUND RT AFT LAV FIXED FLOOR CORRODED INCLUDING AROUND DUMP CHUTE AT BS 1129-1176, RBL 25-63. THE CORROSION WAS REMOVED. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-10-2, 51-40-5, AND 51-10-6.Aug 7, 1998 · N32725 · Boeing 727224 · Fuselage Floor PanelSDR CALA9801411Bracket · crackedINSPECTION FOUND A 1 CRACK IN RT NR 5 LEADING EDGE FLAP ACTUATOR MOUNT BRACKET AT UPPER OUTBOARD LEADING EDGE. THE MOUNT BRACKET WAS REMOVED IAW SRM 51-30-2. A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-10-1.Aug 6, 1998 · N66734 · Boeing 727224 · Wing, Control Surface Attach FittingsSDR CALA9801404Web · corrodedINSPECTION FOUND FLOOR WEB CORRODED AT BS 1175, RBL 65, OUTBOARD OF RT AFT LAV DUMP CHUTE FLANGE. THE CORRODED AREA WAS CUT OUT. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-10-6 AND 51-30-2.Aug 6, 1998 · N32725 · Boeing 727224 · Fuselage Miscellaneous StructureSDR CALA9801403Floorbeam · corrodedINSPECTION FOUND CORROSION ON TOP OF FLOORBEAM AT BS 344, LBL 41-53. THE CORRODED AREA WAS CUT OUT. NEW PARTS WERE FABRICATED AND INSTALLED IAW SRM 53-10-8 AND 51-10-2.Aug 6, 1998 · N32725 · Boeing 727224 · Fuselage Main, Floor BeamSDR CALA9801402Angle · corrodedINSPECTION FOUND FLOOR PANEL SUPPORT ANGLE CORRODED AT BS 1130-1148, RBL 12. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-4, 51-10-2, AND 51-40-5.Aug 6, 1998 · N32725 · Boeing 727224 · Fuselage Miscellaneous StructureSDR CALA9801401Seat Track · corrodedINSPECTION FOUND CORROSION AT INBOARD AND OUTBOARD LEGS OF SEAT TRACK AT BS 1030-1120, LBL 45. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-2.Aug 6, 1998 · N32725 · Boeing 727224 · Fuselage, Seat/Cargo Attach FittingsSDR CALA9801400Angle · crackedINSPECTION FOUND A .5 INCH CRACK IN INTERCOSTAL WEB TOP ANGLE AT FORWARD SCREW HOLE BETWEEN FLOORBEAMS AT BS 970-990, BL 0. THE TOP ANGLE WAS REMOVED. A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-6 AND 51-40-3.Aug 6, 1998 · N32725 · Boeing 727224 · Fuselage Miscellaneous StructureSDR CALA9801399Clip · crackedINSPECTION FOUND A 1 INCH CRACK IN TIE CLIP IN AFT CARGO COMPARTMENT AT STA 1183, 36 INCHES BELOW LBL 9 BULKHEAD FITTING. THE TIE CLIP WAS REMOVED, A NEW TIE CLIP WAS FABRICATED AND INSTALLED IAW SRM 51-10-1.Aug 6, 1998 · N32725 · Boeing 727224 · Fuselage Miscellaneous StructureSDR CALA9801398Panel · crackedINSPECTION FOUND THREE .5 INCH CRACKS IN TOP CENTER PANEL OF NLG WHEEL WELL. THE AREA WAS REPAIRED IAW SRM 51-40-2.Aug 6, 1998 · N32725 · Boeing 727224 · Fuselage Miscellaneous StructureSDR CALA9801397Angle · corrodedINSPECTION FOUND ANGLE AT LT AFT LAV FIXED FLOOR CORRODED AT BS 1129 TO 1176, RBL 25 TO 63. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-30-2.Aug 6, 1998 · N32725 · Boeing 727224 · Fuselage Miscellaneous StructureSDR CALA9801396Hat Channel · corrodedINSPECTION FOUND FLOOR SUPPORT HAT CHANNEL CORRODED AT FORWARD LAV AREA, BS 320, RBL 15. THE HAT CHANNEL WAS REMOVED AND A NEW SECTION WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 51-40-4.Aug 6, 1998 · N32725 · Boeing 727224 · Fuselage Miscellaneous StructureSDR CALA9801395Sidewall · crackedINSPECTION FOUND A 0.3 CRACK IN TOP LT PANEL OF NLG WHEEL WELL. THE AREA WAS REPAIRED IAW SRM 51-40-2.Aug 6, 1998 · N32725 · Boeing 727224 · Fuselage Miscellaneous StructureSDR CALA9801394Sidewall · crackedINSPECTION FOUND A .5 INCH CRACK IN RT SIDEWALL OF NLG WHEEL WELL. THE CRACKED AREA WAS CUT OUT, A DOUBLER AND FITTING WERE FABRICATED AND INSTALLED IAW SRM 53-10-1.Aug 6, 1998 · N32725 · Boeing 727224 · Fuselage Miscellaneous StructureSDR CALA9801393Seat Track · corrodedINSPECTION FOUND SEAT TRACK CORRODED AT INBOARD AND OUTBOARD LEGS AND ALONG TOP AT BS 380 TO 420, RBL 45. THE SEAT TRACK WAS REMOVED AND A NEW ONE WAS FABRICATED AND INSTALLED IAW SRM 53-10-5.Aug 5, 1998 · N32725 · Boeing 727224 · Fuselage, Seat/Cargo Attach FittingsSDR CALA9801392Angle · crackedINSPECTION FOUND 2.5 INCH CRACK AT CURVED ANGLE AT OUTBOARD SIDE OF LT WING FIXED LEADING EDGE RIB SLAT STA 0. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-6 AND 51-40-3.Aug 5, 1998 · N66734 · Boeing 727224 · Wing Miscellaneous StructureSDR 98ZZZX3499Skin · corrodedDURING C-CHECK, CORROSION WAS NOTED ON EXTERIOR FUSELAGE ON PASSENGER WINDOW FRAME NR 35 BOTTOM AND FORWARD EDGES.Aug 2, 1998 · N32719 · Boeing 727224 · Fuselage Main, Plate/SkinSDR 98ZZZX3486Floorbeam · corrodedDURING C-CHECK, CORROSION WAS NOTED AFT RT LAVATORY AREA FLOORBEAM BOTTOM T-CHORD FS 1130 RBL 56.Aug 2, 1998 · N32719 · Boeing 727224 · Fuselage Main, Floor BeamSDR CALA9801377Skin · crackedINSPECTION FOUND A .5 INCH CRACK AT LEFT SIDE OF FUSELAGE AT CUTOUT FOR L-1 DOOR UPPER HINGE ARM. THE CRACKED AREA WAS CUT OUT. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW ECRA 5330-02675, SRM 51-10-2 AND SRM 51-30-2, AND SERVICE BULLETIN 727-53-0198.Jul 30, 1998 · N69735 · Boeing 727224 · Fuselage Main, Plate/SkinSDR CALA9801281Skin · crackedINSPECTION FOUND A 2.75 INCH CRACK IN FUSELAGE SKIN AT L-1 DOOR LOWER HINGE CUTOUT. THE CRACKED AREA WAS CUT OUT, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 51-20-4.Jul 20, 1998 · N69735 · Boeing 727224 · Fuselage Main, Plate/SkinSDR CALA9801280Angle · crackedINSPECTION FOUND A .5 INCH CRACK IN FRAME ATTACH ANGLE INSIDE LT SIDE OF VERTICAL STABILIZER AT STRINGER 5L. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-4.Jul 20, 1998 · N69735 · Boeing 727224 · Vertical StabilizerSDR CALA9801302Skin · crackedINSPECTION FOUND A 2.75 INCH CRACK IN LOWER AFT FUSELAGE SKIN CUTOUT AT R-1 DOOR. THE CRACK WAS STOP DRILLED, A DOUBLER AND TRIPLER WERE FABRICATED AND INSTALLED IAW ECRA 5307-01141.Jul 17, 1998 · N69735 · Boeing 727224 · Fuselage Main, Plate/SkinSDR CALA9801300Panel · crackedINSPECTION FOUND CRACKS IN THE NLG WHEEL WELL TOP LEFT AND TOP RIGHT SKIN PANELS. THE CRACKS WERE .75 TO 1 INCH LONG. THE SKIN WAS REMOVED IAW SRM 51-10-1. WEB SKIN WAS FABRICATED AND INSTALLED IAW SRM 53-10-2, 51-10-2, AND 51-30-2.Jul 17, 1998 · N69735 · Boeing 727224 · Fuselage Miscellaneous StructureSDR CALA9801299Skin · crackedINSPECTION FOUND A .75 INCH CRACK THROUGH FASTENER HOLE OF SKIN AT LT SIDE OF VERTICAL STABILIZER AROUND ACCESS PANEL 9523 ABOVE BS 1215. THE CRACK WAS STOP DRILLED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-10-0, 55-30-3, 51-10-2, 51-30-2, AND 51-00-Jul 17, 1998 · N69735 · Boeing 727224 · Vertical Stabilizer, Plate/SkinSDR CALA9801298Stringer · crackedINSPECTION FOUND A 1.375 INCH CRACK IN RT WING VENT BOX STRINGER 19 AT WS 171.5, NR 2 TANK. THE CRACKED AREA WAS CUT OUT, A REPAIR DOUBLER, FILLER, AND ANGLE WERE FABRICATED AND INSTALLED IAW SRM 57-10-4, 51-10-2, 51-30-2, 51-10-6, AND 51-20-4.Jul 17, 1998 · N69735 · Boeing 727224 · Wing, Longeron/StringerSDR CALA9801260Sequence Valve · leakingTHE A HYDRAULIC SYSTEM PRESSURE AND FLUID WAS LOST AFTER GEAR WAS RETRACTED DEPARTING IAH. FUEL WAS DUMPED AND THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RT MLG LOCK SEQUENCE VALVE LEAKING. THE VALVE WAS REMOVEDJul 16, 1998 · N32725 · Boeing 727224 · Landing Gear Retraction/Extension SystemSDR CALA9801317Support · crackedINSPECTION FOUND A 1 CRACK IN FLOORBEAM SUPPORT AT STA 400-420, BL 0. A 2 CRACK WAS FOUND IN FLOORBEAM SUPPORT AT STA 760, BL 0. THE FLOOR SUPPORT AT STA 400-420 WAS REMOVED IAW SRM 51-30-2. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, Jul 2, 1998 · N69735 · Boeing 727224 · Fuselage Miscellaneous StructureSDR CALA9801315Support · corrodedINSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 380 TO 400, RBL 16 AND STA 1150, RBL 18. THE FLOOR SUPPORTS WERE REMOVED, NEW FLOOR SUPPORTS WERE FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-30-2, AND 51-10-1.Jul 2, 1998 · N69735 · Boeing 727224 · Fuselage Miscellaneous StructureSDR CALA9801314Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 303 TO 344, LBL 28. THE CORROSION WAS REMOVED IAW SRM 51-10-8. ANGLES WERE FABRICATED AND INSTALLED IAW SRM 51-40-8.Jul 2, 1998 · N69735 · Boeing 727224 · Fuselage Main, Floor BeamSDR CALA9801313Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 380 BETWEEN RBL 32 AND RBL 42. THE CORRODED AREA OF FLOORBEAM WAS CUT OUT IAW SRM 53-10-8. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-8, 51-10-2, AND 51-40-4.Jul 2, 1998 · N69735 · Boeing 727224 · Fuselage Main, Floor Beam
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