Boeing 727-232

Service difficulty reports · 6,539

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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 = '727232'
  ORDER BY difficulty_date DESC"

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SDR DL72L972042Wire · cutON L/O 2 CK, FOUND EMERGENCY TRACK LIGHTING INOP NEAR L1 DOOR. REPAIR SPLICED WIRES, OPN CKS GOOD PER M/M.Oct 11, 1997 · N511DA · Boeing 727232 · Light System WiringSDR DL72S972119Bracket · crackedTHE NR 2 L/E FLAP ACTUATOR SUPPORT BRACKETS I/B AND O/B ARE CRACKED. REMOVED SUPPORT BRACKETS AND BEGAN REPAIRS PER M/M 57-20-21 FIG 807, FINISHED REPAIR PER MM 57-20-21 FIG 807.Oct 10, 1997 · N519DA · Boeing 727232 · Leading Edge Slat ActuatorSDR DL72S972097Skin · damagedELEVATOR BONDED BEADED SKIN DAMAGED LT ELEVATOR STA 15 LWR SKIN 3RD AND 4TH BEAD. MFG AND SEALED REPAIR DOUBLERS, INSTALLED DOUBLERS REPAIRED PER SRM 55-20-3 PG 4 FIG 3.Oct 10, 1997 · N546DA · Boeing 727232 · Elevator, Plate/SkinSDR DL72S972041Light · inoperativeEMERGENCY LIGHT ABOVE ROW 26 INOP. REPLACED LIGHT ASSY.Oct 10, 1997 · N484DA · Boeing 727232 · Emergency LightingSDR CALA9701542Angle · crackedINSPECTION FOUND A 2 INCH CRACK IN REPAIR ANGLE ON FORWARD SIDE OF RT BS 1263 TORQUE BOX WEB BELOW HORIZONTAL DECK. THE CRACKED AREA WAS REMOVED AND A REPAIR KIT WAS INSTALLED IAW BOEING DRAWING 65C27136.Oct 10, 1997 · N33785 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9701536Plate · crackedINSPECTION FOUND VERTICAL STABILIZER UPPER LT REINFORCEMENT PLATE JUST FOWARD OF TENSION TIE FORWARD ATTACH BOLT AREA CRACKED. THE CRACK WAS 1.5 INCH LONG. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 55-30-3.Oct 10, 1997 · N33785 · Boeing 727232 · Vertical StabilizerSDR CALA9701535Bulkhead · crackedINSPECTION FOUND VERTICAL STABILIZER LEADING EDGE LOWER PANEL UPPER ATTACH BULKHEAD CRACKED AT ATTACH HOLES. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 55-30-3.Oct 10, 1997 · N33785 · Boeing 727232 · Vertical StabilizerSDR DL72S972078Angle · crackedAFT LOWER CHORD ANGLE IS CRACKED AT I/B AFT FLAP TRACK CUTOUT I/B AND O/B CORNERS. INSTALLED DOUBLER PER M/M 57-52-0 FIG 802.Oct 9, 1997 · N519DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S972024Light · inoperativeEMERGENCY LIGHT ABOVE L-1 DOOR INOP. REPLACED LIGHT ASSY AND BATTERIES, CKS GOOD.Oct 9, 1997 · N518DA · Boeing 727232 · Emergency LightingSDR DL72L972025Power Supply · inoperativeFOUND REAR CEILING EMER EXIT LIGHT OUT DURING L/O CHECK. REPLACED POWER SUPPLY, OPS CKS GOOD.Oct 9, 1997 · N513DA · Boeing 727232 · Emergency LightingSDR DL72L972021Airstair · not latchedAFT AIRSTAIR FELL OPEN ON T/O ROLL. CHECKED AIRSTAIR OPERATION PER MM. NO TROUBLE FOUND.Oct 9, 1997 · N507DA · Boeing 727232 · Entrance StairsSDR CALA9701532Sidewall · crackedINSPECTION FOUND A CRACK BETWEEN TWO FASTENERS IN RIGHT SIDEWALL PANEL OF NLG WHEEL WELL, FS 290. THE CRACKED AREA WAS CUT OUT, A REPAIR WAS FABRICATED AND INSTALLED IAW EA 5362-01016.Oct 9, 1997 · N33785 · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72K972036Bulkhead Web · crackedSEVERAL CRACKS FOUND IN THE FS 178 BLKHD RBL 6, LBL 5 AND BL 0. REPAIRED PER ERA 330815-14.Oct 8, 1997 · N466DA · Boeing 727232 · Fuselage Main, BulkheadSDR CALA9701550Stringer · crackedINSPECTION FOUND LT WING UPPER AFT VENT BOX STRINGER FORWARD MOUNT EAR CRACKED OUT AT WS 66.50. A REPAIR WAS FABRICATED AND INSTALLED IAW EA 5762-01050.Oct 7, 1997 · N33785 · Boeing 727232 · Wing, Longeron/StringerSDR CALA9701549Stringer · crackedINSPECTION FOUND A CRACK AT LT WING FORWARD VENT BOX STRINGER FORWARD AND AFT MOUNT EARS AT WS 686.50. REPAIRS WERE FABRICATED AND INSTALLED IAW EA 5762-01050.Oct 7, 1997 · N33785 · Boeing 727232 · Wing, Longeron/StringerSDR CALA9701543Tab · crackedINSPECTION FOUND STIFFENER TAB CRACKED INSIDE OF NR 3 TANK TOP OF RIB AT STA 601.50 AT OUTBOARD SIDE. THE TAB WAS CUT OFF AND A REPAIR WAS INSTALLED IAW EA 5762-01050.Oct 7, 1997 · N33785 · Boeing 727232 · Wing Miscellaneous StructureSDR CALA9701533Circumferential · corrodedINSPECTION FOUND CORROSION ON CIRCUMFERENTIAL IN AIR CONDITIONING DISTRIBUTION BAY AT STA 740 FROM STRINGER 26L TO S26R. THE CIRCUMFERENTIAL WAS REMOVED AND REPLACED IAW SRM 51-40-3.Oct 7, 1997 · N33785 · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S971984Flap · crackedA .75 INCH CRACK IN NR 4 L/E FLAP AT OUTBOARD LIP HINGE CUTOUT. REPAIRED PER ERA NR 362925-14 AND M/M 57-53-0.Oct 6, 1997 · N408DA · Boeing 727232 · Leading Edge DevicesSDR DL72S971982Fitting · crackedFOUND DURING A1 LETTER CHECK, 1 INCH CRACK NR 8 SLAT ACT INBD ATTACH FITTING OUTBD SIDE. REPAIRED PER M/M 57-20-21.Oct 6, 1997 · N408DA · Boeing 727232 · Leading Edge DevicesSDR DL72S971981Frame · crackedFOUND ON A1 LETTER CK, .5 IN CRACK FWD FRAME AT LOWER STOP CASTING R-1 DOOR. REPAIRED PER MM 52-12-0 AND ERA.Oct 6, 1997 · N408DA · Boeing 727232 · Passenger/Crew DoorsSDR DL72S971980Rib · crackedFOUND ON A1 LETTER CK, 2 IN VISIBLE CRACK NR 1 SLAT ACTUATOR INBD ATTACH RIB. REPAIRED PER MM 57-20-21.Oct 6, 1997 · N408DA · Boeing 727232 · Leading Edge DevicesSDR DL72S971979Actuator · leakingAFTER T/O AT 5,000 FT, A-SYS HYD QTY WENT TO ZERO. REPLACED NR 3 L/E FLAP ACTUATOR.Oct 6, 1997 · N524DA · Boeing 727232 · Leading Edge Slat ActuatorSDR DL72L971978Heat Manifold · blownNR 2 ENG DETECTOR ILLUM AFTER POSITIONING TO A AND TESTING LIGHT STAYED ON AND FOLLOWED BY NR 2 FIRE WARNING LIGHT. THROTTLE TO IDLE ALL INDICATIONS NORMAL AND ALL TESTS NORMAL, THROTTLE IN IDLE FOR DURATION. REPLACED NR 2 ENG FUEL HEAT MANIFOLD.Oct 6, 1997 · N511DA · Boeing 727232 · Fuel HeaterSDR CALA9701548Fitting · corrodedINSPECTION FOUND NR 13 SPOILER ACTUATOR SUPPORT FITTING CORRODED. THE SUPPORT FITTING WAS REMOVED AND REPLACED IAW MM 27-61-81.Oct 6, 1997 · N33785 · Boeing 727232 · Drag Control ActuatorSDR CALA9701541Frame · corrodedINSPECTION FOUND FRAME AT FS 1030 BETWEEN STRINGER 18L AND 19L CORRODED. A DOUBLER AND SHEAR TIE WERE FABRICATED AND INSTALLED IAW SRM 53-10-4.Oct 6, 1997 · N33785 · Boeing 727232 · Fuselage Main, FrameSDR DL72S971975Battery · dischargedEMERGENCY TRACK LIGHTING REMAINED ILLUMINATED WITH SWITCH IN OFF POSITION. REPLACED BATTERY.Oct 5, 1997 · N520DA · Boeing 727232 · Emergency LightingSDR CALA9701546Sidewall · crackedINSPECTION FOUND A CRACK BETWEEN TWO FASTENER HEADS IN RIGHT SIDEWALL PANEL OF NLG WHEEL WELL FS 259. THE CRACKED AREA WAS CUT OUT, A REPAIR WAS FABRICATED AND INSTALLED IAW ECRA 5310-03600.Oct 4, 1997 · N33785 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9701545Sidewall · crackedINSPECTION FOUND A CRACK AT FASTENER HEAD IN LT SIDEWALL PANEL OF NLG WHEEL WELL FS 272. THE CRACKED AREA WAS CUT OUT, A REPAIR WAS INSTALLED IAW ECRA 5310-03599.Oct 4, 1997 · N33785 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9701538Sidewall · crackedINSPECTION FOUND A CRACK AT FASTENER HEAD IN LT CEILING PANEL OF NLG WHEEL WELL AT FS 286. THE CRACKED AREA WAS CUT OUT, FILLER, DOUBLER AND STRAP WERE FABRICATED AND INSTALLED IAW EA 5362-01016.Oct 4, 1997 · N33785 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9701537Sidewall · crackedINSPECTION FOUND A CRACK AT FASTENER HEAD IN RT SIDEWALL PANEL OF NLG WHEEL WELL AT FS 286. THE CRACKED AREA WAS CUT OUT, A REPAIR WAS FABRICATED AND INSTALLED IAW EA 5362-01016.Oct 4, 1997 · N33785 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9701531Sidewall · crackedINSPECTION FOUND A CRACK AT FASTENER HEAD IN LEFT SIDEWALL PANEL OF NLG WHEEL WELL, FS 272. THE CRACKED AREA WAS CUT OUT, A REPAIR WAS FABRICATED AND INSTALLED IAW EA 5362-01016.Oct 4, 1997 · N33785 · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S972238Web · crackedA 1.5 INCH CRACK UPPER RT CUTOUT 1303 WEB ABOVE S-DUCT. A 1 INCH CRACK LOWER RT CUTOUT 1303 WEB ABOVE S-DUCT. A 1 INCH CRACK LOWER LT CUTOUT 1303 WEB. A 1 INCH CRACK UPPER LT CUTOUT 1303 WEB. FOUND DURING B2 LETTER CHECK, INSTALLED PERM REPAIR PER SRM 53-1Oct 3, 1997 · N493DA · Boeing 727232 · Vertical StabilizerSDR DL72S972237Web · crackedA .25 INCH CRACK AT LIGHTNING HOLE, TORQUE BOX VERTICAL WEB, LT SIDE STA 1243 LOWER HOLE. ROUTED CRACK PER M/M 53-11-0, NR 15.Oct 3, 1997 · N493DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S972105Skin · corrosionTHE FUSELAGE SKIN BETWEEN FS 1050 TO 1060 AND STR 28L WAS FOUND CORRODED. THE REPAIR CUTOUT IS APPROXIMATELY 11.375 IB/OB. THE CUTOUT EXTENDS FROM FS 1050 TO 1060 ALONG STRINGER 28L. REPAIRED PER ERA 362905-14.Oct 3, 1997 · N418DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR CALA9701547Skin · disbondedINSPECTION FOUND AN 8 AREA OF LEFT AFT INBOARD FLAP DISBONDED BETWEEN SPAR AND LOWER SKIN AT INBOARD END. THE AFT FLAP SEGMENT WAS REMOVED AND REPLACED IAW MM 27-51-1.Oct 3, 1997 · N33785 · Boeing 727232 · Trailing Edge FlapsSDR DL72S972337Doubler · crackedDOUBLER ON AFT SPAR RAIL CRACKED FROM I/B END OF FLAP. REPLACED FLAP.Oct 2, 1997 · N546DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S972336Skin · crackedCOVE SKIN CRACKED 32 INCHES FROM I/B END OF FLAP. REPAIRED PER MM 57-52-0 PAGE 819.Oct 2, 1997 · N546DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S972094Rib · crackedRIB CRACKED, THE NR 4 L/E SLAT ACTUATOR SUPPORT RIB IS CRACKED AND MARKED WITH TEMPORARY REPAIR. REMOVED TEMP REPAIR AND BEGAN FABRICATION OF PERMANENT REPAIR PER M/M 57-54-0 FIG 804. INSTALLED REPAIR.Oct 2, 1997 · N546DA · Boeing 727232 · Leading Edge DevicesSDR DL72S972071Rib · crackedNR 4 L/E SLAT ATTACH RIBS ARE CRACKED I/B AND O/B SIDE OF ACTUATOR ATTACH POINT. REMOVED TEMP REPAIR ON OTBD RIB OF ACTUATOR ATTACH POINT AND BEGAN FABRICATION OF RIB DOUBLERS PER M/M 57-54-0 FIG 804. OK TO INSTALL INBD REPAIR. OK TO INSTALL OUTBD REPAIR. Oct 2, 1997 · N546DA · Boeing 727232 · Leading Edge DevicesSDR DL72S972067Rib · crackedRIB CRACKED NR 6 SLAT, RIB NR 18 IS CRACKED. FABRICATED REPAIR DOUBLER PER M/M 57-54-0 FIG 814. OK TO INSTALL. REPAIRED PER M/M 57-54-0 FIG 814.Oct 2, 1997 · N546DA · Boeing 727232 · Leading Edge DevicesSDR DL72S972066Rib · crackedRIB CRACKED NR 6 SLAT, RIB NR 12 IS CRACKED. FABRICATED REPAIR DOUBLER PER M/M 57-54-0 FIG 814. OK TO INSTALL. REPAIRED PER M/M 57-54-0 FIG 814.Oct 2, 1997 · N546DA · Boeing 727232 · Leading Edge DevicesSDR DL72S972055Rib · crackedTHE OB MIDFLAP IB AFT CLOSEOUT RIB WAS FOUND CRACKED AT THE AFT LOWER CORNER DURING SHOP INSPECTION. THE RIB WAS REPAIRED BY STOP DRILLING THE CRACK AND INSTALLING A DOUBLER PER MM 57-52-0.Oct 2, 1997 · N546DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S972026Rib · crackedNUMBER 3 AND 7 RIB CRACKED. REPAIRED PER SRM 57-54-0.Oct 2, 1997 · N546DA · Boeing 727232 · Leading Edge DevicesSDR DL72S972015Rib · crackedRIB CRACKED NR 17 ON L/E NR 3 SLAT. REPAIRED PER MM 57-54-0.Oct 2, 1997 · N546DA · Boeing 727232 · Leading Edge DevicesSDR DL72S972000Rib · crackedNUMBERS 5, 8 AND 12 RIB CRACKED ON NR 3 SLAT. REPAIRED PER MM57-54-0.Oct 2, 1997 · N546DA · Boeing 727232 · Leading Edge DevicesSDR DL72S971963Beam · crackedFOUND DURING LETTER CHECK, A1-AFT BEAM RUNNING INBD AND OUTBD CRACKED AT STA 1273 VENTRAL STAIR TORQUE BOX. REPAIRED PER OPN 5967AD.Oct 2, 1997 · N521DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S971962Chord · crackedFOUND DURING LETTER CHECK, A1 INBD CHORD BELOW VENTRAL STAIRS ACTUATOR CRACKED. REPAIRED PER OPN 5967AD.Oct 2, 1997 · N521DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S971961Stiffener · crackedFOUND ON A1 LETTER CK, LEADING EDGE SPAR STIFFENER CRACKED 1.25 INCH AT NR 7 SLAT INBD TRACK INBD SIDE. REPAIRED PER MM 57-20-21.Oct 2, 1997 · N521DA · Boeing 727232 · Wing Miscellaneous StructureSDR CALA9701544Beam · corrodedINSPECTION FOUND RT HORIZONTAL STABILIZER UPPER SKIN TRAILING EDGE BEAM CORRODED. THE TRAILING EDGE BEAM WAS REMOVED AND REPLACED IAW SRM 51-30-2.Oct 2, 1997 · N33785 · Boeing 727232 · Horizontal Stabilizer StructureSDR CALA9701540Skin · dentedINSPECTION FOUND LEADING EDGE OF NR 6 SLAT DENTED. THE DENTED AREA WAS CUT OUT, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-50-3, FIGURE 1.Oct 2, 1997 · N33785 · Boeing 727232 · Leading Edge Devices
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