Boeing 727-232

Service difficulty reports · 6,539

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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 = '727232'
  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 DL72S002297Bulb · burned outR-2 EMERGENCY DOOR LIGHT INOP. CA- RELAMPED SAME.Nov 24, 2000 · N539DA · Boeing 727232 · Emergency LightingSDR DL72S002291Light · inoperativeRT EXTRERIOR EMERGENCY LIGHT BETWEEN OVER WING DOORS INOP CA- RPLD BATTERY RACKNov 23, 2000 · N539DA · Boeing 727232 · Emergency LightingSDR GAIA00718Actuator · inoperativeFLT 3736 - BNA-FWA - NR 5 LEADING EDGE FLAP DID NOT FULLY EXTEND ON FLAP EXTENSION. HOWEVER, AT SLOW SPEED, FLAP FULLY EXTENDED. AIRCRAFT MADE AN UNEVENTFUL LANDING AT FWA. REMOVED AND REPLACED NR 5 KRUEGER FLAP ACTUATOR IAW 272 MM 27-81-22. OPS CHECK GOODNov 22, 2000 · N77780 · Boeing 727232 · Leading Edge Slat ActuatorSDR DL72S002288Frame · corrodedFUSELAGE / C3 DOOR CUTOUT SURROUND STRUCTURE / AFT FRAME : CORROSION REPAIR. THE AFT FRAME OF THE C3 DOOR CUTOUT (FS 1142) WAS FOUND WITH CORROSION IN THE SKIN FLANGE BETWEEN STRINGER 28R AND 29R. THE CORRODED FLANGE WAS TRIMMED AWAY. THE DAMAGE WAS REPAIRNov 22, 2000 · N522DA · Boeing 727232 · Fuselage Main, FrameSDR DL72S002285Skin · crackedFUSELAGE / SKIN / FS 360-380 / STRG. 4R / SKIN LAP SPLICE : CRACK REPAIR. LFEC INSPECTIONS OF THE STRINGER 4R SKIN LAP SPLICE INDICATED A CRACK. INTERNAL MFEC INSPECTION OF THE SKIN LAP CONFIRMED A SINGLE CRACKED FASTENER HOLE IN THE LOWER FASTENER ROWNov 22, 2000 · N517DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S002284Frame · crackedFUSELAGE / C1 DOOR OPENING SURROUND STRUCTURE / AFT FRAME / FS 620 : WEB CRACK AND CHORD GOUGE REPAIR NSPECTIONS OF THE AFT DOOR FRAME OF THE C1 DOOR OPENING AT FS 620 REVEALED A .5 INCH CRACK IN THE FRAME WEB JUST BELOW THE #6 DOOR STOP. THE INNER FRAME CHONov 22, 2000 · N522DA · Boeing 727232 · Fuselage Main, FrameSDR DL72S002281Skin · crackedFUSELAGE / SKIN / FS 269-276 / STRG. 19R-21R : CRACK REPAIR AN EXISTING FLUSH SKIN REPAIR INSTALLED BETWEEN FS 269 & 276AND BETWEEN STRINGERS 19R & 21R WAS FOUND WITH A .4 INCH CRACK EMANATING FROM THE CORNER OF THE 7INCH X 9.5INCH REPAIR CUTOUT. THE EXISTNov 21, 2000 · N539DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S002280Window · leakingLOUD SQUUEAL FROM R2 WINDOW AT 1000 FEET AGL. REPLACED R2 WINDOW AND CHECKED TORQUE ON R3 WINDOW, PRESSURIZIED A/C CHECKS NORMALNov 21, 2000 · N538DA · Boeing 727232 · Flight Compartment WindowsSDR DL72S002277Skin · wornTHE HORIZONTAL STABILIZER ELEVATOR SKINS WERE FOUND WITH WORN, WITH ELONGATED FASTENER HOLES. THE FASTENER HOLES ARE COMMON TO THE UPPER AND LOWER SKINS AND THE REAR SPAR. REPAIR PER ER/A 396929-14ADNov 21, 2000 · N522DA · Boeing 727232 · Elevator, Spar/RibSDR DL72S002282Frame · crackedFUSELAGE / C1 CARGO DOOR CUTOUT SURROUND STRUCTURE / FWD FRAME / FS 560 : WEB CRACK REPAIR THE FWD FRAME OF THE C1 CARGO DOOR CUTOUT (FS 560) WAS FOUNDWITH A CRACK IN THE FRAME WEB. THE CRACK WA REMOVED WITH A .75" DIA HOLE THROUGHT THE WEB. THE FRAME WASNov 20, 2000 · N522DA · Boeing 727232 · Fuselage Main, FrameSDR DL72L002272Transponder · inoperativeNR 2 ATC TRANSPONDER IS INOP. REPLACED TRANSPONDER PERFORMED TEST PER M/M CHECKS NORMAL.Nov 20, 2000 · N506DA · Boeing 727232 · ATC Transponder SystemSDR DL72S002252Compressor · stalledCOMPRESSOR STALL ON T/O ROLL NR 2 ENG. ABORT AT 30 KTS RETURN TO GATE. INSP INLET AND EXAUST. RAN ENG PER PFHB. ALL CK NORMAL, 13 KNT CROSS WIND GUSTING TO 19 KNTS.Nov 19, 2000 · N518DA · Boeing 727232 · Turbine Engine Compressor SectionSDR DL72L002251Connector · shortedWORKING MCO - REFUEL PANEL QTY INDICATORS INOP. FOUND CANNON PLUG TIED BACK AND CAPPED D1756 SHORTED AND BURNED. REMOVED CONNECTOR AND TERMINATED WIRES AND TIED BACK HARNESS.Nov 19, 2000 · N513DA · Boeing 727232 · Fuel Indicating SystemSDR DL72S002237Door Frame · crackedA .625 INCH CRACK AT L-2 DOOR CUTOUT FWD FRAME AT UPPER STOP PAD. REPAIRED PER MM 53-13-0 PG 808.Nov 16, 2000 · N539DA · Boeing 727232 · Fuselage Main, StructureSDR DL72S002236Skin · crackedFOUND AT F-1 LTR CK, .75 INCH CRACK IN NR 4 L/E FLAP OUTER SKIN AT O/B LIP HINGE CUTOUT. REPAIRED PER M/M 57-53-00.Nov 16, 2000 · N539DA · Boeing 727232 · Leading Edge DevicesSDR DL72S002229Battery Pack · dischargedAFT CABIN O/H EMERGENCY LIGHT BETWEEN LAVS INOP. REPLACED BATTERY PACK.Nov 14, 2000 · N490DA · Boeing 727232 · Emergency LightingSDR DL72S002220Spring · failedF/O QUICK DON O2 MASK HAS SPRUNG SPRING. REPLACED O2 MASK ASSY, OPS CHECK AND LEAK CHECK OK.Nov 13, 2000 · N405DA · Boeing 727232 · Crew Oxygen SystemSDR GAIA00690Actuator · inoperativeBNA/FWA - FLT 3735 - DURING LANDING, THE NR 5 LE KRUGER FLAP DID NOT FULLY EXTEND ON FLAP EXTENSION. THE CREW DECLARED AN EMERGENCY. AIRCRAFT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE NR 5 LE KRUGER FLAP ACTUATOR. OPS CHECK PERFORMED, AIRCRAFT RENov 10, 2000 · N77780 · Boeing 727232 · Leading Edge Slat ActuatorSDR DL72S002208Light · inoperativeEMERGENCY LIGHT OVER L2 DOOR INOP. REPLACED LIGHT ASSY AND BATTERIES, OPS NML.Nov 10, 2000 · N411DA · Boeing 727232 · Emergency LightingSDR 00FDEA00768Warning Light · illuminatedAPU FIRE WARN LIGHT CAME ON IN FLT. AC RELEASE PER SERVICE PER MEL/CDL. RAN APU IAW JET RUN HANDBOOK AND NO DISCREPANCIES NOTED.Nov 10, 2000 · N499FE · Boeing 727232 · Fire DetectionSDR DL72L002209Light · brokenEMERGENCY SEAT LIGHT ROW 10D LENS MISSING. REPLACED ASSY, CKS GOOD.Nov 8, 2000 · N507DA · Boeing 727232 · Emergency LightingSDR DL72S002196Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 1009 AND 1183 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL MFEC INSPECTION CONFIRMED 8 CRACKS. THE ENTIRE SKIN LAP JOINT WAS CUTOUT BETWEEN FS 1009 AND 1120. THE JOINT WNov 8, 2000 · N408DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S002173Battery Pack · inoperativeR1 EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY/ BATTERY PACK P/N 334701743, S/N OFF 4833, S/N ON 8676.Nov 5, 2000 · N520DA · Boeing 727232 · Emergency LightingSDR DL72L002166Battery Pack · dischargedDURING EMERGENCY LIGHT CHECK OUT FOUND RT OUTSIDE OVERWING EXIT LIGHT OUT. REPLACED BATTERY PACK.Nov 4, 2000 · N507DA · Boeing 727232 · Emergency LightingSDR DL72L002152Fitting · corrodedTHE VERTICAL STABILIZER TENSION TIE FITTING FORWARD AND AFT ATTACH BOLT HOLES WERE FOUND WITH CORROSION IN THE BORES. THE BORES WERE OVERSIZED AND BUSHED PER ERA 396341-14 AT HMV.Nov 2, 2000 · N508DA · Boeing 727232 · Vertical Stabilizer, Attach FittingsSDR DL72S002149Actuator · leakingON SLAT EXTENSION NR 6 SLAT NO INTRANSIT OR EXTEND LIGHT. CYCLED SLATS AND LOST A SYS HYD QTY. REPLACED NR 6 SLAT ACTUATOR FOR LEAKING.Nov 2, 2000 · N411DA · Boeing 727232 · Leading Edge Slat ActuatorSDR DL72S002140Light · damagedFOUND SEAT MOUNTED EMERGENCY LIGHT DAMAGED AND INOP AT 11D. REPLACED LIGHT ASSY.Oct 31, 2000 · N520DA · Boeing 727232 · Emergency LightingSDR DL72S002129Battery Pack · dischargedON SERVICE CK, EMERGENCY LIGHT INOP. REPLACED BATTERY PACK.Oct 28, 2000 · N411DA · Boeing 727232 · Emergency LightingSDR DL72L002118Angle · crackedA 1.25 INCH VISIBLE CRACK ON NR 3 SLAT AT O/B STOP PAD. REPAIRED PER MM 57-54-0 PG 816.Oct 26, 2000 · N511DA · Boeing 727232 · Leading Edge DevicesSDR DL72L002117Rib · crackedA .75 INCH CRACK IN L/E NOSE RIB OF NR 7 SLAT AT O/B SIDE OF ACTUATOR ATTACH FITTING. REPAIR PER M/M 57-54-0.Oct 26, 2000 · N511DA · Boeing 727232 · Leading Edge DevicesSDR DL72L002116Spar · crackedROUTINE INSPECTIONS OF THE LT ELEVATOR REAR SPAR REVEALED A .25 INCH LONG TYPICAL CRACK EMANATING FROM A TAB HINGE BRACKET. THE CRACK IS TYPICAL OF AD 96-06-05 AND BAC S/B 727-55-0089. THE CRACK WAS STOP DRILLED ON A TEMPORARY BASIS PER THE REQUIREMEOct 26, 2000 · N514DA · Boeing 727232 · Elevator, Spar/RibSDR DL72L002114Beam · corrodedLT MLG BEAM LOWER FACE CORRODED AT LWR T/E PANEL BORES 2, 5, 6, 7, 8, 9, 11, 12, 14, 15, 28. ALL WORK ACCOMPLISHED PER ERA NR 396313-14, NO REVISION.Oct 26, 2000 · N508DA · Boeing 727232 · Wing, Landing Gear Attach FittingsSDR DL72S002115Light · inoperativeON L/O CHECK, FOUND RT EXTERIOR FWD EMERGENCY OVERWING EXIT LIGHT OUT. REPLACED BASE AND BATTERY PACK, OPERATIONAL CHECKS OK.Oct 25, 2000 · N539DA · Boeing 727232 · Emergency LightingSDR DL72S002112Battery Pack · dischargedR-2 DOOR OVERHEAD EMERGENCY LIGHT INOP. REPLACED OVERHEAD LIGHT BATTERY PACK ON R-2 DOOR.Oct 25, 2000 · N408DA · Boeing 727232 · Emergency LightingSDR DL72L002111Frame · crackedAFT DEACTIVATED CARGO DOOR HAD 7 INCH CRACK IN FWD LOWER CORNER FORMER. REPLACED AFT CARGO DOOR, PRESS CKS GOOD.Oct 25, 2000 · N513DA · Boeing 727232 · Cargo/Baggage DoorsSDR DL72L002109Structure · damagedAFT END OF DOGHOUSE 6 O''CLOCK POSITION DOUBLER PEELED BACK ON BOTH SIDES OF INLET SKIN BUTT JOINT. REMOVED DAMAGE PER SRM 54-10-3D FIG 801D. DYE PENETRANT INSP AREA, NO CRACKS FOUND SRM 54-10-10-3D. CHEMICAL TREATED PER 900-2-4 NR 02. APPLIED EPOXY PRIMEOct 25, 2000 · N508DA · Boeing 727232 · Nacelle/Pylon, Main FrameSDR DL72L002108Beam · corrodedLT MLG BEAM LWR T/E PNL BORES CORRODED. REAMED HOLES 34, 35, 36, 37 AND 18 TO .312 PER SRM 57-40D. REAMED HOLES 28 AND 39 TO .359 PER SRM 57-40D. REAMED HOLE 32 TO .312 PER SRM 57-40-D. BHEC INSP OF FASTENER FOR CRACKS AND CORROSION. NO ITEM. TURNED O/B Oct 25, 2000 · N508DA · Boeing 727232 · Wing, Landing Gear Attach FittingsSDR DL72L002107Beam · corrodedLT MLG BEAM HOLES BORES NR 2, 5, 6, 7, 8, 9, 11, 12, 14, 15 AND 28 SHOW CORROSION. REAMED HOLES 2, 5 6, 7, 8, 9, 11, 12, 14, 15 TO .312. HOLE 28 TO .359 PER SRM 57-40-D. BHEC INSP OF FASTENERS FOR CRACKS AND COROSION. NO ITEMS. TURNED O/B ON IN PROCESS Oct 25, 2000 · N508DA · Boeing 727232 · Wing, Landing Gear Attach FittingsSDR DL72K002100Light · inoperativeEMERGENCY LIGHT AT R1 DOOR WON''T TEST. SWITCH BAD. REPLACED LIGHT ASSY.Oct 24, 2000 · N417DA · Boeing 727232 · Emergency LightingSDR DL72L002094Fitting · crackedDURING INSPECTIONS REQUIRED BY AD 97-05-08 6 CRACKS WERE FOUND IN THE NR 1 FORWARD ENGINE PYLON AND ONE CRACK WAS FOUND IN THE NR 3 PYLON. ERA 396334-14AD OVERSIZES THE FASTENER HOLES TO REMOVE THE CRACK PER FEDEX AVIATION SERVICES S/B 2000-5410A01 AT HMV.Oct 24, 2000 · N508DA · Boeing 727232 · Nacelle/Pylon, Main FrameSDR DL72S002085Battery Pack · inoperativeFOUND THE BATTERY PACK INOP AT THE AFT CARGO DOOR EMERGENCY LIGHTS. CHANGED BATTERY PACK, EMERGENCY LIGHTS ARE OK.Oct 22, 2000 · N406DA · Boeing 727232 · Emergency LightingSDR DL72L011138Angle · crackedDURING SHOP VISIT THE LOWER AFT CHORD ANGLE WAS FOUND CRACKED AT I/B AFT FLAP DRIVE ROD CUTOUT.Oct 20, 2000 · N508DA · Boeing 727232 · Wing Miscellaneous StructureSDR DL72L002061Skin · crackedCRACKS WERE FOUND ALONG THE STR 4R LAP JOINT BETWEEN FS 1070 AND FS 1090. THE CRACKS WERE REMOVED AND REPAIRED SIMILIAR TO THAT OF B727 SRM 53-30-3, FIGURE 5 PER ERA 396320-14AD AT HMV.Oct 19, 2000 · N508DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72L002060Skin · crackedSKIN CRACKS WERE FOUND IN THE STR 4L LAP JOINT BETWEEN FS 1050 AND 1070. THE CRACKS WERE REMOVED AND REPAIRED SIMILIAR TO B727 SRM 53-30-3, FIGURE 5 PER ERA 396304-14AD.Oct 19, 2000 · N508DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72L002059Skin · crackedCRACKS WERE FOUND ALONG THE STR 4R LAP JOINT BETWEEN FS 1030 AND FS 1050. THE CRACKS WERE REMOVED AND REPAIRED SIMILIAR TO B727 SRM 53-30-3, FIGURE 5 PER ERA 396305-14AD.Oct 19, 2000 · N508DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72L002058Skin · crackedCRACKS WERE FOUND IN THE STR 26L LAP JOINT BETWEEN FS 600 AND FS 620. THE DAMAGE WAS REMOVED AND REPAIRED PER ERA 396310-14AD SIMILIAR TO THAT OF B727 SRM 53-30-3, FIGURE 5.Oct 19, 2000 · N508DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72L002054Skin · crackedMULTIPLE CRACKS WERE FOUND BETWEEN FS 481 AND FS 681 IN THE STR 4R LAP JOINT. THE CRACKS WERE REMOVED AND REPAIRED PER ERA 396303-14 AT HMV.Oct 19, 2000 · N508DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S002044Bolt · brokenFOUND ON CREW WALKAROUND, NR 3 ENGINE AFT MOUNT BOLT BROKEN. REMOVED ENGINE, REPAIRED DAMAGE, REPLACED CONE BOLT, REINSTALLED ENGINE.Oct 18, 2000 · N534DA · Boeing 727232 · Engine Mount SectionSDR DL72L002042Rib · crackedFOUND ON C2 LETTER CK, NR 5 SLAT O/B ROD END ATTACH RIB AFT LEG CRACKED. REPAIRED PER MM 57-54-0.Oct 17, 2000 · N504DA · Boeing 727232 · Leading Edge DevicesSDR DL72L002041Rib · crackedFOUND ON C2 LETTER CK, NR 5 SLAT INBOARD ROD END ATTACH RIB AFT LEG CRACKED. REPAIRED PER MM 57-54-0.Oct 17, 2000 · N504DA · Boeing 727232 · Leading Edge Devices
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