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SDR DL72K000268Battery · dischargedON LAYOVER NR 2 CHECK, FOUND AFT MEGAPHONE BATTERIES OUT OF DATE. INSTALLED NEW BATTERIES AND EXPIRATION PLACARD ON MEGAPHONE. OPS CHECK NML. SECURED MEGAPHONE.Feb 6, 2000 · N414DA · Boeing 727232 · Emergency EquipmentSDR DL72L000256Flap Track · corrodedDURING OVERHAUL OF THE I/B FLAP I/B TRACK ASSY, TYPICAL CORROSION WAS FOUND AT THE MLG AND SPOILER BEAM ATTACH PAD AREAS AND TYPICAL WEAR WAS FOUND AT THE FWD ATTACH LUGS, THE MLG DOOR HINGE FITTING ATTACH HOLES, AND THE TOGGLE DETENT HOLE. REPAIRED Feb 3, 2000 · N507DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S000249Door · failedRIGHT PACK TRIP FOLLOWED BY SMOKE IN CABIN. FOUND RT COOLING DOOR NOT OPENING WHEN PACK SELECTED. REPLACED RT COOLING DOOR ACTUATOR RELAY.Feb 2, 2000 · N543DA · Boeing 727232 · Cabin Cooling SystemSDR DL72S000224Engine · stalledCOMPRESSOR STALL NR 2 ENG ON T/O AT 300 FT. THREE LOUD POPS/BANGS, NO FUEL HEAT, NO NR 2 BLEED. IMMEDIATE RETURN FOR VISUAL LANDING. (INITIAL STALL WITH STEADY THROTTLE SETTING, LAST AT REDUCED THROTTLE SETTING). REPLACED C1 AND C2 FAN ASSYS.Jan 31, 2000 · N520DA · Boeing 727232 · Engine (Turbine/Turboprop)SDR DL72K000230Battery · dischargedAREA LIGHT ASSY AT AFT AIRSTAIR OVERHEAD POS WAS REPLACED AND ORIGINAL BATTERIES IN OLD ASSY HAD LOW CHARGE. REPLACED BATTERIES, CHECKS NORMAL.Jan 31, 2000 · N414DA · Boeing 727232 · Emergency LightingSDR DL72L000214Fcu · failedNR 3 THROTTLE BINDING IN FLT. NO THROTTLE/ENG RESPONSE IN UPPER ONE-THIRD OF TRAVEL. BINDING THEN RELOCATED TO LWR ONE-THIRD OF THROTTLE MOVEMENT. WHEN THROTTLE WAS ADVANCED THE LEVER WOULD TRAVEL AFT APPROX 1 TO 2 INCHES ON ITS OWN WITH NO ENG RESPONSE. RJan 29, 2000 · N510DA · Boeing 727232 · Fuel Control/Turbine EnginesSDR DL72S000216Door Frame · crackedFOUND DURING WALKAROUND CARGO STRAP STICKING OUT OF FWD LWR CORNER OF C-3 DOOR. UPON CLOSER INSPECTION A 10 INCH CRACK WAS FOUND ON INNER DOOR FRAME WHERE IT ATTACHES TO DOOR SKIN. REPLACED DOOR.Jan 28, 2000 · N538DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S000213Light · inoperativeRT AFT WING EMERGENCY LIGHT IS INOP. REPLACED LIGHT RACK.Jan 28, 2000 · N418DA · Boeing 727232 · Emergency LightingSDR DL72L000280Stringer · crackedSTRINGER 6 RT CRACKED VERT INTERIOR 4TH FRAME DOWN FROM 9504 RIB NR 2. BEGAN FABRICATED REPAIR PER M/M 55-30-0 PG 803. FINISHED FABRICATING REPAIR ANGLE PER M/M 55-30-0 FIG 803. OK TO TREAT AND PAINT. CHEM TREATED AS PER PS 900-2-4-1 NR 2. TREATED AND PAIJan 28, 2000 · N507DA · Boeing 727232 · Vertical Stabilizer, Spar/RibSDR DL72L000259Rib · crackedNR 5 SLAT NR 12 RIB CRACKED. REPAIRED PER MM 57-54-0.Jan 28, 2000 · N507DA · Boeing 727232 · Leading Edge DevicesSDR DL72L000252Skin · crackedSTOP DRILLED CRACK AND BEGAN FABRICATING REPAIR PER M/M 55-30-0 FIG 803. CHEM TREATED PER PS 900-2-4-1 NR 2. TREATED AND PAINTED PER PS 900-2 NR 5. OK TO INSTALL. INSTALLED REPAIR ANGLE PER M/M 55-30-0 PG 803. STRINGER WAS FOUND CRACKED ON VERTICAL STAB.Jan 28, 2000 · N507DA · Boeing 727232 · Vertical Stabilizer, Plate/SkinSDR DL72L000567Skin · crackedNR 2 MIDFLAP AFT SPAR DOUBLER CRACKED TWO PLACES AND COVE SKIN CRACKED. REPAIRED PER M/M 57-52-0 FIGURE 802 AND FIGURE 809.Jan 27, 2000 · N507DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S000205Sign · inoperativeEMERGENCY EXIT SIGN ON FRONT MAIN DOOR INOP. REPLACED LIGHT ASSY.Jan 27, 2000 · N539DA · Boeing 727232 · Emergency LightingSDR DL72S000200Skin · corrodedTWO CUTOUTS WERE MADE IN THE SKIN BETWEEN FS 950F AND 970 ALONG STR 28L DUE TO CORROSION. THE DAMAGE WAS FOUND AT MV AND REPAIRED PER ERA 334022-14.Jan 27, 2000 · N541DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72L000286Angle · wornSUPPORT ANGLE WORN VERT STAB LT SIDE JUST FWD OF SLIDING SEAL. REMOVED DAMAGED AREA AND DRILLED UP REPAIR PER SRM 55-30-6D. INSTALLED REPAIR PER SRM 55-30-6D.Jan 27, 2000 · N507DA · Boeing 727232 · Vertical StabilizerSDR DL72K000203Le Flap · separatedAFTER T/O FROM DCA, FLAPS DID NOT RETRACT PAST 2 DEGREE POSITION. A/C DIVERTED TO IAD. MTC IN IAD FOUND LT O/B FOREFLAP BROKEN FREE FROM I/B CARRIAGE. REPLACED FOREFLAP.Jan 27, 2000 · N521DA · Boeing 727232 · Leading Edge DevicesSDR DL72S000192Stringer · crackedTHERE WERE CRACKS FOUND IN STRINGER 18A AND THE FUSELAGE SKIN AT FS 946. THE DAMAGE WAS FOUND AT MV AND REPAIRED PER ERA 334023-14.Jan 26, 2000 · N541DA · Boeing 727232 · Fuselage Main, Longeron/StringerSDR DL72S000191Frame · corrodedTHE FUSELAGE FRAME 1166 HAD CORROSION AT THE SHEAR CLIP BETWEEN STR 29R AND STR 30. THE DAMAGE WAS FOUND AT MV AND REPAIRED PER ERA 334020-14.Jan 26, 2000 · N541DA · Boeing 727232 · Fuselage Main, FrameSDR DL72S000190Frame · dentedTHE FOLLOWING FRAMES WERE DENTED DUE TO SERVICE DAMAGE BETWEEN STR 23L AND 25L, FS 500, 520, 560, 620, 660 AND 720. THE DAMAGE WAS FOUND AT MV AND WERE REPAIRED PER ERA 334016-14.Jan 26, 2000 · N541DA · Boeing 727232 · Fuselage Main, FrameSDR DL72L000197Rib · crackedSLAT RIB NR 11 WAS CRACKED AT THE UPPER FWD END. INSTALLED A REPAIR DOUBLER PER 57-54-0 FIG 804.Jan 26, 2000 · N507DA · Boeing 727232 · Flight Control SystemSDR DL72L000196Rib · crackedSLAT RIB WAS CRACK AT THE O/B LWR AFT END. REPAIRED PER MM 57-54-0 FIG 814.Jan 26, 2000 · N507DA · Boeing 727232 · Leading Edge DevicesSDR DL72L000189Skin · gougedTHIS AIRCRAFT RECEIVED GROUND DAMAGE TO THE FUSELAGE SKIN AT FS 990 AND STR 24R. THE DAMAGE WAS FOUND AT HMV AND REPAIRED PER ERA 334013-14.Jan 26, 2000 · N503DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S000227Bolt · looseAT MV2 FOUND NR 11 SPOILER ACT MOUNT BOX LOOSE, LWR I/B BOLT. REMOVED BOLT AND REPAIRED HOLE PER MM 57-42-0.Jan 25, 2000 · N542DA · Boeing 727232 · Drag Control ActuatorSDR DL72S000226Mount · looseAT MV2 FOUND NR 12 SPOILER ACT MOUNT BOX LOOSE, LWR MOUNTS. REMOVED I/B AND O/B LWR FITTING BOLTS. O/B LWR HOLE WITHIN LIMITS PER MM 57-42-0. INSTALLED LWR BOLT PER SAME, REPAIRED I/B LWR BOLT PER MM 57-42-0.Jan 25, 2000 · N542DA · Boeing 727232 · Drag Control ActuatorSDR DL72S000187Skin · crackedLFEC INSPECTION OF THE STRINGER 26L SKIN LAP SPLICE BETWEEN FS 480 & 680 INDICATED A CRACK IN THE LOWER FASTENER ROW. INTERNAL MFEC INSPECTION CONFIRMED THREE CRACKS BETWEEN FS 520 & FS 540. THE CRACKS WERE ROUTED OUT OF THE SKIN LAP AND REPAIRED WITH AN EXJan 25, 2000 · N536DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72L000238Skin · crackedANTI-ICE SKIN CRACKED AT 4 LOCATIONS. INSTALLED DOUBLER PER MM 57-54-0.Jan 25, 2000 · N507DA · Boeing 727232 · Leading Edge DevicesSDR MZZA00002Battery · inoperativeGUM - FOUND 2L SERVICE DOOR EMERGNECY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERY PACK PER MM 33-50-01. OPS CHECK GOOD AND RELEASED AIRCRAFT FOR SERVICE. (M)Jan 24, 2000 · N15781 · Boeing 727232 · Emergency LightingSDR DL72L000195Rib · crackedSLAT RIB WAS CRACKED AT LWR AFT END NR 2 RIB. INSTALLED A REPAIR DOUBLER PER MM 57-54-0 FIG 814.Jan 24, 2000 · N507DA · Boeing 727232 · Leading Edge DevicesSDR DL72L000194Skin · crackedSLAT CRACKED. INSTALLED REPAIR DOUBLER PER MM 57-54-0 FIG 814.Jan 24, 2000 · N507DA · Boeing 727232 · Leading Edge DevicesSDR DL72L000212Gimbal Fitting · gougedLT AND RT GIMBAL ATTACH FITTINGS WERE FOUND GOUGED IN THE FILLET RADIUS OF THE UPPER LUGS. ER/A 333979-14 REV A.Jan 19, 2000 · N503DA · Boeing 727232 · Horizontal Stabilizer, Attach FittingsSDR CALA0000005Stringer · corrodedINSPECTION FOUND STRINGER 28R IN FORWARD CARGO AREA AT STA 510 CORRODED. THE CORRODED AREA WAS CUT OUT IAW SRM 53-10-3. A SPLICE AND FILLER REPAIR WAS INSTALLED SRM 53-10-3 AND 51-10-3.Jan 3, 2000 · N33785 · Boeing 727232 · Fuselage Main, Longeron/StringerSDR DL72L000240Spar · crackedLWR AFT SPAR CRACKED 19, 32 & 37 FROM I/B END. ALSO, CRACKED 37 & 43 FROM O/B END. THIS DAMAGE REPAIRED PER M/M 57-52-0 FIG 802.Jan 1, 2000 · N503DA · Boeing 727232 · Trailing Edge FlapsSDR DL72L000239Skin · crackedCOVE SKIN CRACKED 32 INCHES FROM I/B END. REPAIRED PER M/M 57-52-0.Jan 1, 2000 · N503DA · Boeing 727232 · Trailing Edge FlapsSDR DL72L000208Skin · crackedAPPROX .75 INCH LONG CRACK IN COVE SKIN, 32 FROM I/B END OF FLAP. REPAIRED PER MM 57-52-0 FIG 809.Jan 1, 2000 · N503DA · Boeing 727232 · Trailing Edge FlapsSDR DL72L000207Spar · crackedAFT SPAR DOUBLER CRACKED 21, 34 & 57S FROM I/B END DAMAGE LISTED ON N/R'S 016162, 016079 & 016080. REPAIRED PER CMM 57-52-0 FIG 802.Jan 1, 2000 · N503DA · Boeing 727232 · Trailing Edge FlapsSDR CALA9901759Angle · crackedINSPECTION FOUND A 3 INCH CRACK IN RT FLOOR SUPPORT ANGLE AT CUSP WEB, FS 1130, STRINGER 17R. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2, 51-10-2, AND MM 51-20-0.Dec 30, 1999 · N33785 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9901758Panel · corrodedINSPECTION FOUND LT WING NR 6 SPOILER PANEL UPPER SURFACE CORRODED. THE SPOILER PANEL WAS REMOVED, REPAIRED, AND REINSTALLED IAW SRM 57-50-6 AND MM 27-62-1.Dec 30, 1999 · N33785 · Boeing 727232 · SpoilersSDR CALA9901757Support · corrodedINSPECTION FOUND FORWARD CARGO FLOOR SUPPORT ANGLE CORRODED UNDER NUTPLATE AT FS 643, LBL 13. THE FLOOR SUPPORT ANGLE WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 51-30-2, 51-10-2, 51-40-4, AND MM 51-20-0.Dec 30, 1999 · N33785 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9901756Floorbeam · corrodedINSPECTION FOUND FLOORBEAM UPPER T-CHORD CORRODED AT STA 1166, BL O TO O/B RT SIDE. THE CORROSION WAS REMOVED IAW SRM 51-10-6. AN ANGLE REPAIR WAS INSTALLED IAW ECRA 5310-03961.Dec 30, 1999 · N33785 · Boeing 727232 · Fuselage Main, Floor BeamSDR CALA9901755Support · corrodedINSPECTION FOUND RT AFT LAV FORWARD WALL FLOOR SUPPORT CORRODED. A NEW SUPPORT WAS INSTALLED IAW SRM 51-10-2, 51-30-2, AND MM 51-20-0.Dec 30, 1999 · N33785 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9901753Frame · crackedINSPECTION FOUND A 2 INCH CRACK IN FRAME AT FS 880 BETWEEN STRINGER 18R AND 17R. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. A REPAIR ANGLE WAS INSTALLED IAW SRM 51-30-2 AND 51-40-3, FIGURE 1.Dec 30, 1999 · N33785 · Boeing 727232 · Fuselage Main, FrameSDR CALA9901752Web · crackedINSPECTION FOUND A 4 INCH CRACK IN CUSP WEB AT TOP OF BULKHEAD AT VERTICAL SUPPORT, FS 1188, RBL 20. THE CUSP WEB WAS REMOVED AND REPLACED IAW SRM 51-30-2.Dec 30, 1999 · N33785 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9901751Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED ON UPPER T-CHORD AT STA 1130, BL 0 TO O/B RT SIDE. THE FLOORBEAM WAS REPAIRED IAW ECRA 5310-03965 AND EA 27-5310-2-A0548.Dec 30, 1999 · N33785 · Boeing 727232 · Fuselage Main, Floor BeamSDR CALA9901750Frame · bentINSPECTION FOUND FRAME BENT AT FS 640 BETWEEN LONGERON 26 AND 27R. THE FRAME WAS REPAIRED IAW EA 27-5311-2-A0538 AND ECRA 5310-03968.Dec 30, 1999 · N33785 · Boeing 727232 · Fuselage Main, FrameSDR CALA9901749Door Pan · crackedINSPECTION FOUND A 1 INCH CRACK IN L-2 CABIN DOOR AT UPPER PAN AREA NEAR HINGE FITTING. THE AREA WAS REPAIRED IAW SRM 51-40-2.Dec 30, 1999 · N33785 · Boeing 727232 · Passenger/Crew DoorsSDR CALA9901748Seat Track · corrodedINSPECTION FOUND SEAT TRACK CORRODED AT FS 1110-1130, RBL 22. THE SEAT TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-10-2, 51-30-2, AND MM 51-20-0.Dec 30, 1999 · N33785 · Boeing 727232 · Fuselage, Seat/Cargo Attach FittingsSDR CALA9901747Support · bentINSPECTION FOUND FORWARD CARGO FLOOR SUPPORT BENT AT STA 650, LBL 3. THE BENT SECTION WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 51-40-4, FIGURE 1.Dec 30, 1999 · N33785 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9901746Angle · corrodedINSPECTION FOUND FORWARD CARGO FLOOR SUPPORT ANGLE CORRODED UNDER NUTPLATES AT STA 643, LBL 9. THE CORRODED SECTION OF FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT AND ANGLES WERE INSTALLED IAW SRM 51-40-4 AND 51-30-2.Dec 30, 1999 · N33785 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9901745Bulkhead · crackedINSPECTION FOUND A 4 CRACK IN WEB AT AFT PRESSURE BULKHEAD STA 1183, STRINGER 2L FITTING. THE CRACK WAS STOP DRILLED IAW ECRA 5310-03958 AND A DIP WAS ISSUED TO REINSPECT THE REPAIR EVERY 3000 CYCLES.Dec 29, 1999 · N33785 · Boeing 727232 · Fuselage Main, Floor BeamSDR CALA9901743Fairing Support · corrodedINSPECTION FOUND RT LOWER BODY FAIRING 3441 SUPPORT NR 7 CORRODED AT STA 720F, S26R. THE CORROSION WAS REMOVED IAW SRM 51-10-6. A NEW SUPPORT WAS INSTALLED IAW SRM 51-10-2 AND 51-30-2.Dec 29, 1999 · N33785 · Boeing 727232 · Aerodynamic Fairings
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