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 95FDEA00086Switch · failedAFTER T/O, DURING FLAP RETRACTION, GOT STEADY AMBER LEADING EDGE FLAP LIGHT AT 2 DEG. CHECKED S/O PANEL, IT SHOWED NR 1 FLAP STILL EXTENDED CYCLED FLAPS, NO HELP. RETURNED TO AIRPORT AND LANDED UNEVENTFULLY. REPLACED NR 1 L/E FLAP SWITCH. CHECKS OK PER MM Jan 26, 1995 · N499FE · Boeing 727232 · Trailing Flap Position Indicating SystemSDR DL72S950350Skin · crackedFOUND DURING B-2 LETTER CHECK TPA, OUTER SKIN BROKEN OUT FWD RT SVC DOOR LOWER HINGE. INSTALLED DOUBLER REPAIR PER SRM 52-40-2.Jan 25, 1995 · N470DA · Boeing 727232 · Service DoorsSDR DL72S950476Horiz Walkway · corrodedFOUND ON CV2 CHECK TPAMM, OUTBOARD LEG OF LEFT NLG HORIZONTAL WALKWAY CORRODED STA 303.9. REPAIRED PER SRM 53-10-4 AND ERA 303065-14.Jan 23, 1995 · N411DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S950475Floor Beam · corrodedFOUND ON CV2 CHECK TPAMM, CORROSION ON FLOOR BEAM STA 1030. REPAIRED PER SRM 53-10-8 FIG 3.Jan 23, 1995 · N411DA · Boeing 727232 · Fuselage Main, Floor BeamSDR DL72L950326Switch · faultyDURING CLIMB THROUGH 12,000 FEET ELEVATOR FEEL DIFF, PRESSURE LIGHT ILLUMINATED. PERFORMED PROCEDURES IAW POM, FOUND NO OTHER DISCREPANCIES. AFTER ONE HOUR AT CRUISE, LIGHT EXTINGUISHED FOR 5 MINUTES THEN ILLUMINATED, THEN LIGHT EXTINGUISHED IN DESCENT. LANJan 22, 1995 · N514DA · Boeing 727232 · Elevator Control SystemSDR DL72S950313Duct · brokenDURING CLIMB-OUT, AIRCRAFT WOULD NOT HOLD PRESSURE, SELECTED ALTERNATE BLEED WITH NO HELP. DIVERTED TO MCO. FOUND LEFT PACK WATER SEPARATOR ASSEMBLY LEAKING AIR. ALSO, FOUND DUCT FROM MIX VALVE TO SEPARATOR ASSEMBLY BROKEN IN SEVERAL PLACES. REPLACED DUCT Jan 21, 1995 · N490DA · Boeing 727232 · Cabin Pressure Control SystemSDR DL72S950682Rib · crackedDURING INITIAL INSPECTION OF THE NR 7 LEADING EDGE SLAT, RIB MARKED NR 11 WAS FOUND TO HAVE A CRACK. THE RIB WAS REPAIRED PER MM 57-54-0.Jan 20, 1995 · N421DA · Boeing 727232 · Leading Edge DevicesSDR DL72S950680Slat · crackedDURING THE INITIAL INSPECTION OF THE NR 7 LEADING EDGE SLAT, THERE WAS A CRACK FOUND THE UPPER I/B CORNER OF THE 'T' DUCT OPENING. THE CRACK WAS REPAIRED PER MM 57-54-0 PG 802A.Jan 20, 1995 · N421DA · Boeing 727232 · Leading Edge DevicesSDR DL72S950679Skin · damagedUPON INITIAL INSPECTION OF THE NR 7 LEADING EDGE SLAT, THERE WAS A TEMPORARY REPAIR FOUND ON THE OUTER SKIN 45 INCHES FROM THE OUTBOARD END. THE DAMAGE WAS REPAIRED PER SRM 57-50-3.Jan 20, 1995 · N421DA · Boeing 727232 · Leading Edge DevicesSDR DL72S950474Seat Track · crackedFOUND ON CV2 CHECK TPAMM, LEFT INBD SEAT TRACK CRACKED STA 1033. REPAIRED PER SRM 53-10-5 FIG 7.Jan 20, 1995 · N411DA · Boeing 727232 · Fuselage, Seat/Cargo Attach FittingsSDR DL72S950473Seat Track · corrodedFOUND ON CV2 CHECK TPAMM, CORROSION ON SEATTRACK BS 380 RBL48. REPAIRED PER SRM 53-10-5 FIG 7.Jan 20, 1995 · N411DA · Boeing 727232 · Fuselage, Seat/Cargo Attach FittingsSDR DL72S950446Torque Box · crackedDURING LETTER CHECK INSPECTION, THE UPPER CHORD AT RBL 20 RUNNING FORE/AFT IN THE AFT VENTRAL STAIRWAY TORQUE BOX WAS FOUND CRACKED AT STA. 1273. IN ORDER TO GAIN ACCESS FOR REPAIR OF THE CHORD, THE I/B WEB WAS CUT BETWEEN STA 1253 AND STA 1273. BOTH THE WEBJan 20, 1995 · N531DA · Boeing 727232 · Fuselage Main, StructureSDR DL72S950292Skin · crackedDURING E-2 LETTER CHECK, FOUND MAIN ENTRY DOOR OUTER SKIN CRACKED .5 INCH AT LOWER HINGE CUTOUT LOWER AFT CORNER. REPAIRED PER B727MM 52-11-01 PG808.Jan 20, 1995 · N546DA · Boeing 727232 · Passenger/Crew DoorsSDR DL72S950290Skin · crackedDURING E-2 L/C, FOUND ONE .25 INCH CRACK IN LWR SKIN OF LEFT ELEVATOR, 7 INCHES FROM I/B EDGE. REPAIRED PER SRM 55-20-3 FIG 4.Jan 20, 1995 · N546DA · Boeing 727232 · Elevator, Plate/SkinSDR DL72S950746Midflap · corrosionDURING SHOP VISIT THE OB CARRIAGE SUPPORT FITTING WAS FOUND TO HAVE THE TWO IB THRUST BEARING RETAINER BOLT HOLES CORRODED, IN NR 2 MID FLAP. REPAIRED PER SRM 57-50-4.Jan 19, 1995 · N542DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S950745Midflap · crackedDURING SHOP VISIT AFT LOWER CHORD WAS FOUND CRACKED 15 INCHES AND 29 INCHES FROM IB END, OF NR 2 MID FLAP. REPAIRED PER MM 57-52-0.Jan 19, 1995 · N542DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S950744Midflap · crackedDURING SHOP INSPECTION A CRACK WAS FOUND AT THE 2ND FROM IB AFT FLAP TRACK CUT-OUT IN AFT LOWER CHORD OF NR 2 MID FLAP. REPAIRED PER MM 57-52-0.Jan 19, 1995 · N542DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S950743Midflap · crackedDURING SHOP INSP. CRACK AT IB ACTUATOR CUT-OUT WAS REPAIRED PER MM 57-52-0, DAMAGE FOUND IN NR 2 MID FLAP.Jan 19, 1995 · N542DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S950742Midflap · crackedDURING SHOP INSPECTION A CRACK WAS FOUND IN AFT LOWER CHORD 12 INCHES AFT OF IB CARRIAGE SUPPORT. THE CHORD WAS REPAIRED PER MM 57-52-0. THIS DAMAGE WAS IN NR 2 MID FLAP.Jan 19, 1995 · N542DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S950526Foreflap · damagedDURING SHOP INSP NR 1 FORE FLAP WAS FOUND WITH WEAR DAMAGE AT 108 INCHES FROM THE INBOARD END OF FLAP. REPAIRED PER SRM 57-50-4.Jan 19, 1995 · N496DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S950471Former · crackedFOUND ON CV2 CHECK TPAMM, 1 INCH CRACK FORMER UP RADIUS STA 600, REPAIRED PER SRM 53-10-4 FIG 21.Jan 19, 1995 · N411DA · Boeing 727232 · Fuselage Main, FrameSDR DL72S950277Skin Doubler · corrodedDURING B-1 LETTER CHECK, FOUND TWO RIVETS SHEARED IN FUSELAGE SKIN DOUBLER AND DOUBLER IS BULGED AFT OF FS 1010 AT STRINGER 29R. REPAIRED PER SRM 53-10-3.Jan 19, 1995 · N531DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72L950479Track · corrodedDURING INSPECTION AT HMV, THE LEFT SIDE INBD TRACK FOR THE INBD FLAP WAS FOUND WITH CORROSION IN THE RADIUS BLOCK FASTENER HOLE FWD OF THE AFT TRACK TO MAIN LANDING GEAR BEAM ATTACH HOLE, ON BOTH THE INBD AND OUTBD SIDES OF THE TRACK. THE HOLES WERE REPAIRED Jan 19, 1995 · N514DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S950470Seat Track · corrodedFOUND ON CV2 CHECK, CORROSION ON SEAT TRACK STA 344. REPAIRED PER SRM 53-10-5 FIG 7.Jan 18, 1995 · N411DA · Boeing 727232 · Fuselage, Seat/Cargo Attach FittingsSDR DL72S950469Seat Track · corrodedFOUND ON CV2 CHECK, CORROSION ON SEAT TRACK O/B RT STA 420-445, REPAIRED PER SRM 53-10-5 FIG 7.Jan 18, 1995 · N411DA · Boeing 727232 · Fuselage, Seat/Cargo Attach FittingsSDR DL72S950463Seat Track · corrodedFOUND ON CV2 CHECK, CORROSION SEVERAL PLACES ON RT I/B SEAT TRACK RBL 23 FROM STA 380 - 480, REPAIR. REPLACED SEAT TRACK SECTION FROM STA 380 TO 440 PER SRM 53-10-5 FIG 7.Jan 18, 1995 · N411DA · Boeing 727232 · Fuselage, Seat/Cargo Attach FittingsSDR DL72S950462Seat Track · corrodedFOUND ON CV2 CHECK, CORRROSION FOUND SEAT TRACK RBL 45 BETWEEN 1090 AND 1136 TOP AND BOTTOM SIDES, REPAIR. REPLACED SEAT TRACK FROM 1110 TO 1136 PER SRM 53-10-3 FIG 7.Jan 18, 1995 · N411DA · Boeing 727232 · Fuselage, Seat/Cargo Attach FittingsSDR DL72S950461Seat Track · corrodedFOUND ON CV2 CHECK, CORROSION FOUND SEAT TRACK LOCATED AT LBL 25 BETWEEN 1130 AND 1110, REPAIR. REPLACED SEAT TRACK SECTION PER SRM 53-10-5 FIG 3.Jan 18, 1995 · N411DA · Boeing 727232 · Fuselage, Seat/Cargo Attach FittingsSDR DL72S950460Floor Beam · corrodedFOUND ON CV2 CHECK, CORROSION TOP OF FLOOR BEAM STA 1030 AT CENTER LINE, REPAIR. FABRICATED AND INSTALLED SEC OF T CAP PER SRM 53-10-8 FIG 3.Jan 18, 1995 · N411DA · Boeing 727232 · Fuselage Main, Floor BeamSDR DL72S950459Seat Track · corrodedFOUND ON CV2 CHECK, CORROSION ON LEFT O/B SEAT TRACK BETWEEN STA 1030 AND 1050 BOTH SIDES OF TRACK, REPAIR. REPLACED SEAT TRACK SECTION PER CVSRM 53-10-5.Jan 18, 1995 · N411DA · Boeing 727232 · Fuselage, Seat/Cargo Attach FittingsSDR DL72S950450Floor Beam · corrosionFOUND ON CV2 CHECK, CORROSION ON BEAM TOP/BOTTOM AT STA 1050 BETWEEN LEFT INBOARD AND LEFT O/B SEAT TRACK REPAIRED PER M/M 53-20-11 PG 802.Jan 18, 1995 · N411DA · Boeing 727232 · Fuselage Main, Floor BeamSDR DL72S950261Attach Angle · crackedDURING LETTER CHECK, THE LEFT WING NR 4 LEADING EDGE SLAT LOWER FORWARD SKIN ATTACH ANGLE WAS FOUND WITH A .5 INCH CRACK IN ITS RADIUS BEHIND THE INBOARD SLAT UPSTOP. REPAIRED PER MM 57-54-0 FIG 812.Jan 18, 1995 · N421DA · Boeing 727232 · Leading Edge DevicesSDR DL72K950908Nose Cowl · wornDURING SHOP VISIT, FOUND WORN AREAS ON AFT LANDING EDGE BETWEEN 6 AND 9 O'CLOCK POSITION ON NOSE COWL. REPAIRED AS PER 727 SRM 54-10-3.Jan 18, 1995 · N481DA · Boeing 727232 · Engine Cowling SystemSDR CAL950049Circuit Breaker · trippedFLT NR 1911 - IAH - THE AIRCRAFT WAS RETURNED TO IAH AFTER TAKEOFF DUE TO UNEVEN FUEL BURN FROM FUEL TANKS. THE NR 1 TANK WAS BURNING FASTER THAN OTHERS. FUEL WAS DUMPED TO CONTROL BALANCE. MAINTENANCE FOUND THAT THE NR 1 FUEL TRANSFER VALVE WAS NOT WORKINGJan 18, 1995 · N17789 · Boeing 727232 · Aircraft Fuel Distribution SystemSDR DL72S950305Fuel Pump · sheared shaftDURING DESCENT, NR 3 ENGINE FLAMED OUT. UNABLE TO RESTART, LANDED ORD WITHOUT INCIDENT. REPLACED FUEL PUMP AND FUEL CONTROL, OPERATION NORMAL. SHOP INSPECTION FOUND FUEL PUMP SHAFT WAS SHEARED.Jan 17, 1995 · N532DA · Boeing 727232 · Engine Fuel PumpSDR DL72S950180Cowl · crackedDURING SHOP INSPECTION, NR 1 ENGINE NOSE COWL WAS FOUND WITH LEADING EDGE LIP CRACKED. REPAIRED PER SRM 54-30-3.Jan 16, 1995 · N518DA · Boeing 727232 · Engine Cowling SystemSDR DL72S951146Rib · crackedDURING SHOP INSPECTION, RIB AT ACTUATOR FITTING WAS FOUND CRACKED ON L/WING NR 3 L/E SLAT. REPAIRED PER SRM 57-54-0.Jan 14, 1995 · N517DA · Boeing 727232 · Leading Edge DevicesSDR DL72L950167Le Rib · crackedDURING HMV, FOUND RIB INSIDE NR 3 L/E SLAT CRACKED. REPAIRED PER SRM 57-50-3 FIG 9.Jan 13, 1995 · N514DA · Boeing 727232 · Leading Edge DevicesSDR DL72S951003Slat · crackedDURING INSPECTION OF NR 5 L/E SLAT, N/R CARD WAS WRITTEN TO COMPLY WITH EO NR 4-55122-3AD. THIS EO WAS COMPLIED WITH AND N/R CARD SIGNED OFF.Jan 12, 1995 · N526DA · Boeing 727232 · Leading Edge DevicesSDR DL72L950369Skin · corrosionBELLY SKIN AT STR 28R, STA 990 FOUND CORRODED. A 2.5 INCH BY 2.5 INCH SECTION WAS CUT OUT TO REMOVE CORROSION. A 0.040 INCH TI-6AL-4V DOUBLER, AND A 0.063 INCH TI-6AL-4V TRIPLER WILL BE INSTALLED OVER CUTOUT.Jan 12, 1995 · N514DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S950533Skin · wornDURING INSPECTION ON A B727 NR 5 L/E SLAT, A HOLE WAS FOUND TO BE ELONGATED UNDER WHERE THE FENCE IS MOUNTED. IN ADDITION, THE OUTER SKIN WAS FOUND TO BE WORN AT THE SAME LOCATION. AN EXTERNAL DOUBLER WAS INSTALLED PER THE M/M 57-54-00 PG 817.Jan 11, 1995 · N526DA · Boeing 727232 · Leading Edge DevicesSDR DL72S950532Rib · crackedON NR 5 L/E SLAT DURING INSPECTION A CRACK WAS FOUND ON A RIB. A REPAIR DOUBLER WAS INSTALLED PER M/M 57-54-00 FIG 809.Jan 11, 1995 · N526DA · Boeing 727232 · Leading Edge DevicesSDR DL72S950194Kruger Flap · crackedDURING SHOP INSPECTION, A CRACK WAS FOUND ON THE NR 3 KRUGER FLAP NEAR THE I/B HINGE. REPAIRED CRACK PER SRM 57-50-3.Jan 11, 1995 · N493DA · Boeing 727232 · Leading Edge DevicesSDR DL72S950370Skin · dentedDURING SHOP INSPECTION, RIGHT WING NR 8 SLAT WAS FOUND WITH THE LEADING EDGE SKIN DENTED AT 51 INCHES TO 57 INCHES FROM THE I/B END OF SLAT. REPAIRED PER SRM 57-50-3 FIG 1.Jan 10, 1995 · N419DA · Boeing 727232 · Leading Edge DevicesSDR DL72S950216Ribs · crackedDURING SHOP INSPECTION, LEFT WING NR 3 LEADING EDGE SLAT WAS FOUND WITH INTERNAL SUPPORT RIBS NR 7 AND NR 9 CRACKED. REPAIRED PER SRM 57-54-0.Jan 10, 1995 · N484DA · Boeing 727232 · Leading Edge DevicesSDR MZZA9501Bearing · seizedFLT 821 - GUM - AIRCRAFT AIR RETURNED AFTER TAKEOFF CREW ADVISED THAT DURING FLAP RETRACTION, INBOARD FLAPS STUCK BETWEEN 2 AND 5 DEGREES. FOUND LEFT FLAP THRUST BEARING FROZEN. REPLACED THRUST BEARING AND SYSTEM OPERATIONAL CHECKED SATISFACTORY. (Z)Jan 9, 1995 · N15781 · Boeing 727232 · Trailing Edge Flap Control SystemSDR DL72S950143Web · crackedDURING LETTER CHECK, FOUND AFT FUSELAGE STAIRWELL RIGHT SIDE VERTICAL WEB CRACKED AT FS 1243 AT LIGHTENING HOLE. REPAIRED PER MM 53-11-0 PG 828.Jan 9, 1995 · N517DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72L950206Le Skin · wornAT HMV SHOP INSPECTION, THE RIGHT WING NR 4 FORE FLAP WAS FOUND WITH WEAR DAMAGE TO THE LEADING EDGE SKIN AT 86 INCHES FROM THE INBOARD END OF FLAP. REPAIRED PER SRM 5750-4.Jan 8, 1995 · N514DA · Boeing 727232 · Trailing Edge FlapsSDR DL72L950205Le Skin · wornAT HMV, SHOP INSPECTION THE RIGHT WING NR 4 FORE FLAP HAS FOUND WITH WEAR DAMAGE ON THE LEADING EDGE SKIN AT 29 INCHES FROM THE OUTBOARD END OF FLAP. REPAIRED DAMAGE PER SRM 57-50-4.Jan 8, 1995 · N514DA · Boeing 727232 · Trailing Edge FlapsSDR DL72L950125Frame · crackedDURING HMV, FOUND FRAME 804.5 BETWEEN L/A O/W EXIT OPENINGS STR 14 FRAME CHORD CRACKED. REPAIRED PER SRM 53-10-4 FIG 17.Jan 7, 1995 · N514DA · Boeing 727232 · Fuselage Main, Frame
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