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 DL72S000991Wire · brokenNUMBER 3 OIL TEMP WAS FLUCTUATING UP TO THE UPPER PEG. OIL QTY WAS SLOWLY DECREASING TO 1.4, OIL PRESS WAS NORMAL AT 50 PSI. ENG WAS SHUTDOWN IN FLT. ALL OTHER PARAMETERS WERE NORMAL. FOUND BROKEN WIRE AT CANNON PLUG TO OIL TEMP TRANSMITTER. REPAIRED BRMay 20, 2000 · N535DA · Boeing 727232 · Engine Oil TemperatureSDR DL72L000989Light · inoperativeLEFT AFT OVERWING EMERGENCY LIGHT INOP. REPLACED BATTERY PACK, CHECKS GOOD.May 20, 2000 · N509DA · Boeing 727232 · Emergency LightingSDR DL73K001000Frame · corrodedTHE FWD FRAME OF THE C2 DOOR OPENING (FS 794) WAS FOUND WITH AN AREA OF CORROSION IN THE FRAME WEB UNDER THE LOWER LATCH FITTING. THE CORROSION WAS REMOVED WITH 1.5 X .75 CUTOUT IN THE FRAME WEB AND REPAIRED WITH A FORMED ALUMINUM DOUBLER PER B737 SRM 51-40-May 19, 2000 · N239WA · Boeing 727232 · Fuselage Main, FrameSDR DL72S000998Frame · crackedA .5 INCH CRACK WAS FOUND IN THE WEB OF THE C1 DOOR OPENING AFT FRAME (FS 620) JUST BELOW THE NR 6 DOOR STOP. THE CRACK WAS COMMON TO A FASTENER HOLE ATTACHING THE WEB TO THE OUTER FRAME CHORD. THE WEB WAS LOCALLY TRIMMED AWAY TO REMOVE THE CRACK AND REPAIRMay 19, 2000 · N543DA · Boeing 727232 · Fuselage Main, FrameSDR DL72K000988Light · inoperativeRT OVERWING EMERGENCY LIGHT INOP (ON CARGO DOOR. REPLACED LIGHT RACK.May 19, 2000 · N415DA · Boeing 727232 · Emergency LightingSDR DL72S000982Light · inoperativeLEFT OVERWING EMERGENCY LIGHTS ARE OUT. REPLACED BATTERY PACK AND CHARGER.May 19, 2000 · N528DA · Boeing 727232 · Emergency LightingSDR DL72S000981Light · inoperativeON LAYOVER, FOUND EMERGENCY EXIT LIGHTS ROW 20 ABC AND 22 ABC, LEFT OVRWING EXITS, INOP. REPLACED EMERGENCY BATTERY PACK, SYSTEM CHECKS GOOD PER MM.May 19, 2000 · N542DA · Boeing 727232 · Emergency LightingSDR DL72S001019Flange · gougedAT HMV, THE NR 2 FIREWALL AFT FLANGE WAS FOUND TO BE WORN/GOUGED AT THE 6 O''CLOCK POS. IT WAS CHEMICALLY TREATED PER PS 900-2-4-1 NR 2 AND REPAIRED PER MM 53-11-0 PG 801.May 16, 2000 · N531DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S000971Battery · inoperativeFOUND RT AFT CARGO DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED M957 BATTERY PACK. EMERGENCY LIGHTS OPS GOOD.May 16, 2000 · N516DA · Boeing 727232 · Emergency LightingSDR DL72S000968Skin · crackedNR 3 KRUEGER FLAP CRACKED AT O/B LIP HINGE CUTOUT. TPA D-2 LTR CHK. INSTALLED DOUBLER PER M/M 57-53-0, NR 2A.May 16, 2000 · N544DA · Boeing 727232 · Leading Edge DevicesSDR DL72S001020Cowling · wornAT HMV, THE NR 2 FIREWALL COWL LANDING WAS FOUND TO BE WORN. IT WAS REPAIRED PER MM 53-11-0 PG 801.May 15, 2000 · N531DA · Boeing 727232 · Engine Cowling SystemSDR DL72S000966Skin · crackedLFEC INSPECTION OF THE STRINGER 26L SKIN LAP JOINT BETWEEN FS 481 & 681 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL MFEC CONFIRMED CRACKS IN TWO FRAME BAYS. BECAUSE OF THE CRACKS AND EXISTING PREVIOUS REPAIRS THE ENTIRE LAP JOINT May 15, 2000 · N536DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72K000956Skin · crackedA CRACK WAS FOUND IN THE VERTICAL STABILIZER SKIN AT FS 1210 AND STRINGER 3A ON THE LEFT HAND SIDE. THE CRACK WAS REMOVED WITH A 1.4 X 2.7 CUTOUT AND AN EXTERNAL DOUBLER WAS INSTALLED PER ERA 334389-14 AT HMV.May 15, 2000 · N529DA · Boeing 727232 · Vertical Stabilizer, Plate/SkinSDR GAIA00277Connector · dirtyMEM/IAH - FLT 1760 - AFTER FLAP RETRACTION, NR 4 LEADING EDGE DEVICE DID NOT INDICATE RETRACTED. PERFORMED ABNORMAL PROCEDURE WITH THE SAME RESULTS. THE CREW RETURNED TO MEM AND LANDED WITHOUT ANY FURTHER DIFFICULTIES. CLEANED CONNECTOR AT SWITCH AND OPERATMay 14, 2000 · N77780 · Boeing 727232 · Leading Edge Slat Position Indicating SystemSDR DL72S001061Frame · crackedAT HMV STRINGER 14RT STA 920 FRAME WAS FOUND TO BE CRACKED. REMOVED DAMAGED SECTION FORMED ANGLE PER SRM 53-10-4 FIG 806D. CHEM TREATED PER PS 900-2-4-1. INSTALLED REPAIR IAW SRM 53-10-4 FIG 806D.May 12, 2000 · N531DA · Boeing 727232 · Fuselage Main, FrameSDR DL72S001057Shear Tie · corrodedAT HMV2 FOUND AFT B/B SHEAR TIE CORRODED AT FS 1166 FROM STR 28L TO 28R. REMOVED FASTENERS TO GAIN ACCESS TO CORRODED AREA, CORROSION ON SHEAR TIE FROM STR 29-28 OUT OF LIMITS AND FRAME WEB BELOW FAIL-SAFE CHORD OUT OF LIMITS AS PER SRM 53-10-1 FIG 1. REMOVEMay 12, 2000 · N531DA · Boeing 727232 · Fuselage Main, StructureSDR DL72S000947Keelbeam · crackedFOUND ON C1 LETTER CK, LOWER I/B FWD VERTICAL KEEL BEAM ANGLE CRACKED RT WHEEL WELL STA 870. REPAIRED PER MM 53-10-9D.May 12, 2000 · N411DA · Boeing 727232 · Fuselage Main, KeelSDR DL72S000946Attach Angle · crackedFOUND ON C1 LETTER CK, 1 INCH CRACK NR 11 SPOILER ACTUATOR I/B ATTACH ANGLE. REPAIRED PER MM 57-42-0.May 12, 2000 · N411DA · Boeing 727232 · Wing Miscellaneous StructureSDR DL72K000945Light · inoperativeFOUND DURING L/O, EXT EMERGENCY EXIT SLIDE LIGHT ON MID CARGO DOOR RIGHT SIDE INOP. REPLACED BATTERY PACK RACK ASSY, CKS NORMAL PER M/M.May 12, 2000 · N495DA · Boeing 727232 · Emergency LightingSDR DL72L000941Valve · inoperativeCABIN PRESSURE WILL NOT HOLD MANUAL AC W/ OUTFLOW VALVE FULL CLOSED AND CARGO HEAT VALVE CLOSED WOULD NOT CONTROL PRESSURE. REPLACED AVIONICS COOLING AND OUTFLOW VALVE, NO HELP. (S/N 3147) OFF, (S/N 4400) ON, (P/N 254708948). REPLACED BOTH PNEU FLOW CONTROLMay 11, 2000 · N502DA · Boeing 727232 · Cabin Pressure Control SystemSDR DL72S000939Bracket · crackedFOUND ON F2 LETTER CK, INBOARD ATTACH BRACKET CRACKED NR 8 SLAT ACTUATOR. REPAIR PER MM 57-20-21.May 11, 2000 · N420DA · Boeing 727232 · Leading Edge DevicesSDR 20000731SH025Frame · corrodedDURING A C-CHECK, CORROSION WAS NOTED ON FRAME UPPER FLANGE AT STA 1010, RIGHT. (X)May 10, 2000 · N33785 · Boeing 727232 · Fuselage Main, FrameSDR DL72S001001Spar · crackedSPAR CRACKED. NR 8 L/E SLAT, FWD SPAR AT TAI DUCT. REPAIRED SLAT PER MM.May 10, 2000 · N531DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S000938Skin · corrodedTHE FUSELAGE SKIN WAS FOUND CORRODED AT FS 560 OVER STRINGER 28L. THE CORROSION WAS REMOVED WITH A 14 X 1.5 CUTOUT IN THE SKIN. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 377271-14.May 10, 2000 · N543DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S000931Angle · crackedFOUND AT F-1 LTR CHECK, AIRSTAIR ACTUATOR ATTACH FITTING LOWER FWD SUPPORT ANGLE CRACKED 2.5 INCH AT STA 1263. REPLACED ANGLE PER SRM 53-10-10D.May 10, 2000 · N534DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S000923Engine · leakingOIL QUANTITY DECREASED RAPIDLY ON NR 3 ENG. RATE WAS APPROX 1 GAL PER 5 MIN UNTIL REACHING ZERO. ENG CHANGE IN PROGRESS.May 9, 2000 · N544DA · Boeing 727232 · Engine (Turbine/Turboprop)SDR DL72K000936Hinge Fitting · corrodedTHE HORIZONTAL STABILIZER REAR SPAR HINGE FITTING LUGS WERE FOUND WORN ON THE LT AND RT I/B LUG FACES. THE LT I/B LUG FACE WAS SPOTFACED 0.010 AND THE RT I/B LUG FACE WAS SPOTFACED 0.015 TO REMOVE THE WEAR. THE LT I/B LUG BORE WAS REAMED TO 2.2345 DIA AND THMay 8, 2000 · N529DA · Boeing 727232 · Horizontal Stabilizer StructureSDR DL72K000920Pump · damagedAS ENG POWER WAS ADVANCED FOR TAKEOFF NR 1 ENG FLAMED OUT. EPR ON NR 1 ENG REACHED 1.3 BEFORE ENGINE INST. ROLLED BACK, NO TAKEOFF WAS INITIATED. FOUND ENG FUEL PUMP SHEARED. REPLACED SAME AND ENG FUEL CONTROL.May 8, 2000 · N410DA · Boeing 727232 · Engine Fuel PumpSDR DL72K000919Stiffener · crackedFOUND ON B1 LETTER CK, L/E SPAR STIFFENERS CRACKED L/E SPAR I/B AND O/B OF NR 7 SLAT ACTUATOR. REPAIRED PER MM 57-20-21.May 8, 2000 · N526DA · Boeing 727232 · Leading Edge DevicesSDR DL72S000916Fcu · malfunctionedON CLIMBOUT, NR 2 ENG ALL INDICATORS FLUX AND EGT AT 580 DEG. REPLACED FUEL CONTROL.May 7, 2000 · N404DA · Boeing 727232 · Fuel Control/Turbine EnginesSDR DL72S000913Warning Light · false indicationDURING CLIMBOUT EWR HAD A TAIL SKID LIGHT. AIRCRAFT WAS ON A MAINTENANCE FERRY TO ATL. NO OBVIOUS PROBLEM NOTICED ON INSPECTION. PROBLEM RELATED TO INDICATION ONLY. FLIGHT WAS AN AIR TURNBACK AFTER TAKEOFF. CLEANED PROX SWITCH.May 7, 2000 · N402DA · Boeing 727232 · Auxiliary Gear (Tail Skid)SDR DL72L000904Frame · crackedTHE FUSELAGE FRAME AT FS 825.92 WAS FOUND CRACKED AT STR 16L. THE CRACK WAS REMOVED AND REPAIRED PER ERA 334351-14 AT HMV.May 5, 2000 · N509DA · Boeing 727232 · Fuselage Main, FrameSDR DL72L000903Skin · corrodedCORROSION DAMAGE WAS FOUND ON THE FUSELAGE SKIN BETWEEN FS 700 AND 720 BETWEEN STRINGERS 28L AND 28R. ERA 334399-14AD AUTHORIZES THE CORROSION TO BE REMOVED AND REPAIRED PER SRM 53-30-3, FIGURE 1 AT HMV.May 5, 2000 · N509DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72L000902Skin · crackedCRACKS WERE FOUND AT THE UPPER AND LOWER HINGE CUTOUTS OF THE L1 DOOR. THE SKIN AND BONDED DOUBLER WERE CRACKED AT BOTH LOCATIONS AND THE BEAR STRAP WAS CRACKED AT THE UPPER HINGE LOCATION ONLY. THE CRACKS WERE REMOVED AND REPAIRED PER ERA 334353-14 AT HMV.May 5, 2000 · N509DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72K000901Skin · crackedTHE FUSELAGE SKIN WAS FOUND CRACKED AT THE STR 4L LAP JOINT BETWEEN FS 360 AND FS 481. THE LAP JOINT WAS REMOVED AND REPLACED PER ERA 334350-14AD AT HMV.May 5, 2000 · N529DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72K000900Skin · crackedTHE FUSELAGE SKIN WAS FOUND CRACKED AT THE STR 4R LAP JOINT BETWEEN FS 400 AND FS 420. ERA 334362-14AD AUTHORIZES THE REMOVAL OF THE DAMAGE AND REPAIRS THE DAMAGE PER SRM 53-30-3 FIGURE 5. THE DAMAGE WAS FOUND AT HMV.May 5, 2000 · N529DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72K000899Skin · crackedCRACKS WERE FOUND IN THE STR 4R LAP JOINT BETWEEN FS 480 AND FS 500. ERA 334363-14 AUTHORIZES THE DAMAGE TO BE CUT OUT AND REPAIRED PER SRM 53-30-3, FIGURE 5. THE DAMAGE WAS FOUND AT HMV.May 5, 2000 · N529DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72L000898Frame · crackedTHE WEB OF THE FS 761L FRAME WAS FOUND CRACKED RIGHT AT THE FLOOR LINE. ERA 334347-14 AUTHORIZES THE DAMAGE AT THIS ONE LOCATION TO BE REPAIRED PER EO 4-61904-3AD. THE DAMAGE WAS FOUND AT HMV.May 5, 2000 · N509DA · Boeing 727232 · Fuselage Main, FrameSDR DL72S000905Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 & 480 INDICATED A CRACK IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL MFEC INSPECTION ALONG THE LENGTH OF THE PANEL CONFIRMED A SINGLE CRACK LOCATION BETWEEN FS 360 & 380. THE CRACK WAMay 4, 2000 · N403DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72L000884Skin · wornUPPER SURFACE IS WORN ON NR 5 SLAT. BURNISHED WEAR AREA, MADE STAINLESS DOUBLER. INSTALLED DOUBLER PER MM 727 57-54-0 FIG 81.May 4, 2000 · N509DA · Boeing 727232 · Leading Edge DevicesSDR DL72S000883Engine · stalledNR 1 ENG STARTED COMPRESSOR STALLING 160 KTS DURING INITAL T/O AND CLIMBOUT. ENG FAIL LIGHTS CYCLED ON/OFF. AUTO PACK TRIP OCCURRED IMMEDIATELY. REPLACED ENGINE.May 4, 2000 · N400DA · Boeing 727232 · Engine (Turbine/Turboprop)SDR DL72S000881Switch · failedINFLIGHT SHUTDOWN DUE TO NR 2 ENG FILTER BYPASS LIGHT ON. REMOVED AND INSPECTED MAIN OIL FILTER. NO CONTAMINENTS FOUND. CHIP DET CHECKS CLEAN. REPLACED FILTER BYPASS SWITCH.May 4, 2000 · N519DA · Boeing 727232 · Engine Oil Indicating SystemSDR DL72S001060Door Frame · crackedONE INCH VISIBLE CRACK R-1 DOOR AFT FRAME AT LOWER STOP PAD. REPAIRED PER M/M 52-12-0.May 3, 2000 · N538DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72K000878Power Supply · intermittentFWD CTR AISLE EMERGENCY LIGHT WON''T TEST. REPLACED RACK, CHECKS OK.May 3, 2000 · N523DA · Boeing 727232 · Emergency LightingSDR DL72S000875Stringer · crackedFOUND AT D-2 LETTER CHECK, STR 18A CRACKED 15 INCHES FROM AFT END, RIGHT WING. REPAIRED PER M/M 53-12-0.May 2, 2000 · N515DA · Boeing 727232 · Fuselage Main, Longeron/StringerSDR DL72S000874Skin · crackedFOUND ON D2 LETTER CHECK, 2 INCH AND .25 INCH CRACK RT ELEVATOR LOWER SKIN 12 INCHES FWD OF I/B EDGE OF TAB. REPAIRED PER SRM 55-20-3.May 2, 2000 · N515DA · Boeing 727232 · Elevator, Plate/SkinSDR DL72K000872Bulkhead · crackedTHE FS 1183 BULKHEAD WAS FOUND WITH A 1.5 INCH LONG TYPICAL CRACK IN THE WEB JUST BELOW THE LBL & RBL 8 STIFFENERS AT WL 182. THE CRACKS ARE TYPICAL OF BAC S/B 727-53-0175. THE CRACKS WERE CUT OUT OF THE WEB AND REPAIRED WITH TITANIUM DOUBLERS PER ER/A 37720May 2, 2000 · N524DA · Boeing 727232 · Fuselage Main, BulkheadSDR 00FDEA00313Seat Track · corrodedCORROSION ON TOP OF EXPANSION JOINT FOUND AFT REMOVAL OF SEAT TRACK BS 758, LBL 25, WL 208. *S/D* REMOVED AND REPLACED PER FEDEX SRM 51-30-02.May 1, 2000 · N497FE · Boeing 727232 · Fuselage, Seat/Cargo Attach FittingsSDR 00FDEA00310Floorbeam · corrodedLONGITUDINAL FLOORBEAM BS 760 - 848, LBL 45, WL 208. CORRODED AROUND NUT PLATES. *S/D* REMOVED AND REPLACED PART PER FEDEX SRM 51-30-02.May 1, 2000 · N497FE · Boeing 727232 · Fuselage Main, Floor BeamSDR DL72K000870Battery · inoperativeAFT STAIR OVERHEAD E PATH LIGHT INOP. REPLACED BATTERIES, CHECKS NORMAL PER M/M.May 1, 2000 · N417DA · Boeing 727232 · Emergency Lighting
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