Boeing 727-247

Service difficulty reports · 2,669

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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 = '727247'
  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 DL72W991261Skin · crackedA 1.125 INCH VISABLE CRACK ON AFT SKIN OF NR 6 SLAT AT O/B TRAILING EDGE. SPLICED SKIN PER M/M 57-54-0, NR 1.Jun 4, 1999 · N294WA · Boeing 727247 · Leading Edge DevicesSDR 99FDEA00204Egt Indication · highNR 2 EGT HIGH INTO THE YELLOW BAND (640 DEG C) FOR MORE THAN 5 SEC. PULLED BACK TO 90 PERCENT N1. RETURN TO RDU. NR 2 FUEL FLOW WAS AT 3000 LBS PER HR AND EGT WAS STILL 100 DEG HOTTER THAN 1 AND 3. *S/D* INSTALLED BORESCOPE PLUGS AND IGNITER PLUGS. REMOVJun 3, 1999 · N233FE · Boeing 727247 · Engine EGT/TIT Indicating SystemSDR 99FDEA00202Floorbeam · corrodedCORROSION (C53-224-01,3) ON UPPER SURFACE OF UPPER CHORD BS 1130, RBL 47-49, WL 208. *S/D* REMOVED AND REPLACED CORROSION, FLAP PEENED AREA AND INSTALLED REPAIR STRAP PER FEDEX EA 7-5310-45275.Jun 1, 1999 · N234FE · Boeing 727247 · Fuselage Main, Floor BeamSDR UPS99229785Seat Track · corrodedINSPECTION TYPE:SI, CORROSION ON SEAT TRACK FLANGE BS 444 TO BS 457 LBL 45. SEAT TRACK FLANGE FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. REMOVED DAMAGED SECTION OF SEAT TRACK, FABRICATED NEW SEAT TRACK PER SRM 53-10-5. INSTALLED NEW SEAT TRACK PER MM SRM 53May 29, 1999 · N208UP · Boeing 727247 · Fuselage, Seat/Cargo Attach FittingsSDR UPS99229783Frame · crackedINSPECTION TYPE:SI, POSSIBLE CRACK AT FASTENER HOLE IN FRAME BS 540 WL 215 RBL 64. REMOVED DAMAGED AREA IN FRAME, FABRICATED REPAIR PARTS AND INSTALLED PER SRM 51-40-3, 51-30-2, 51-10-2.May 29, 1999 · N208UP · Boeing 727247 · Fuselage Main, FrameSDR UPS99229774Frame · corrodedINSPECTION TYPE:SI, CORROSION (C53-224-01.00-01) ON FRAME BS 560 WL 215 RBL 64. CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. COMPLETE STANDARD FORMED SECTION REPAIR PER SRM 51-40-03, SRM 51-10-2 AND SRM 51-40-3.May 29, 1999 · N208UP · Boeing 727247 · Fuselage Main, FrameSDR DL72W991199Engine · failedNR 3 ENG POPPED AND SHUDDERED DURING APPLICATION OF T/O PWR, APPROX 1.6 EPR PRIOR TO INDICATION OF AIRSPEED. REPLACED ENGINE.May 29, 1999 · N2820W · Boeing 727247 · Engine (Turbine/Turboprop)SDR 99FDEA00197Frame · corrodedCORROSION (C53-111-01,3) ON FRAME AT BS 1148, LBL 24 AND LBL 29, WL 161. *S/D* REMOVED AND REPLACED DAMAGE FROM FRAME, ACCOMPLISH SSI INSP AND FAB AND INSTALLED PARTS IAW FEDEX EA 7-5310-45290.May 28, 1999 · N234FE · Boeing 727247 · Fuselage Main, FrameSDR 99FDEA00196Frame · corrodedCORROSION (C53-111-01,3) ON I/B FRAME FLANGE AT BS 1166, STR 17R. *S/D* REMOVED AND REPLACED FRAME PER FEDEX EA 7-5310-45249.May 28, 1999 · N234FE · Boeing 727247 · Fuselage Main, FrameSDR 99FDEA00195Bulkhead Web · crackedWHILE WORKING W/C 7-5430-7-2303L1 PT 6 DISCOVERED CRACK IN THE BS 1342 BULKHEAD WEB AT WL 252, LBL 17. *S/D* REMOVED AND REPLACED BULKHEAD WEB PER IAW FEDEX EA 7-5310-45235.May 28, 1999 · N234FE · Boeing 727247 · Fuselage Main, BulkheadSDR UPS99229700Floorbeam · corrodedINSPECTION TYPE:SI, CORROSION ON FRAME BS 950, WL 207.5, LBL 55. REMOVED CORROSION AND TREATED AREA PER SRM 51-20-00.May 27, 1999 · N208UP · Boeing 727247 · Fuselage Main, Floor BeamSDR UPS99229699Frame · corrodedINSPECTION TYPE:SI, CORROSION ON FRAME BS 930, WL 207.5, LBL 66. REMOVED CORROSION AND TREATED AREA PER SRM 51-20-00.May 27, 1999 · N208UP · Boeing 727247 · Fuselage Main, FrameSDR UPS99229696Frame · corrodedINSPECTION TYPE:SI, CORROSION ON 940 FRAME WL 207.5 LBL 67 AT BS 939. REMOVED CORROSION AND TREATED AREA PER SRM 51-20-00.May 27, 1999 · N208UP · Boeing 727247 · Fuselage Main, FrameSDR UPS99229684Light · inoperativeCOCKPIT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY. OPS CHECK GOOD PER MM 33-50-01, P/N ON AND OFF 10-0067-9 S/N OFF 28158 S/N ON 28163.May 27, 1999 · N210UP · Boeing 727247 · Emergency LightingSDR UPS99229683Light · inoperativeMAIN ENTRY EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY, P/N ON AND OFF 10-00 67-9 S/N OFF 5200 S/N ON 27025. OPS CHECK GOOD PER MM 33-50-01.May 27, 1999 · N210UP · Boeing 727247 · Emergency LightingSDR DL72W991196Line · chafedCLIMBING THROUGH 13,000 FEET B-HYD SYSTEM FLUID QTY DECREASE TO ZERO AND BOTH B-SYSTEM PUMP LIGHTS ILLUMINATED. CHECKLIST PERFORMED SAFETY WIRE CUT ON GPWS AND THE PNEUMATIC BRAKE HANDLE. REPLACED CHAFED HYDRAULIC LINE IN HYD BAY.May 27, 1999 · N2807W · Boeing 727247 · Hydraulic System, MainSDR UPS99229799Shear Tie · corrodedINSPECTION TYPE:SI CORROSION ON FWD FACE OF FRAME AND SHEAR TIE BS 720F BETWEEN STR 27 AND 28 RT. BLENDED CORROSION ON FRAME, FOUND TO BE IN LIMITS PER SRM 53-10-1. SHEAR TIE FOUND TO BE OUT OF LIMITS PER 53-10-1 SRM. REPAIRED SHEAR TIE PER SRM 53-10-4.May 26, 1999 · N208UP · Boeing 727247 · Fuselage Miscellaneous StructureSDR UPS99229798Shear Tie · corrodedINSPECTION TYPE:SI CORROSION ON SHEAR TIE FWD SIDE BS 720E FRAME BETWEEN STR 26 AND 27 LEFT CORROSION ON SHEAR TIE FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED SHEAR TIE PER 53-10-4 SRM REPAIRED SHEAR TIE PER SRM 53-10-4.May 26, 1999 · N208UP · Boeing 727247 · Fuselage Miscellaneous StructureSDR UPS99229782Shear Tie · corrodedINSPECTION TYPE:SI, CORROSION (C53-111-01.00-03) ON SHEAR TIES FWD AND AFT SIDE BS 720A FRAME BETWEEN STR 25 AND 26 RT CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. INSTALLED NEW PART PER SRM 51-30-2 PG 2 AND 3.May 26, 1999 · N208UP · Boeing 727247 · Fuselage Miscellaneous StructureSDR UPS99229701Seat Track · corrodedINSPECTION TYPE:SI, CORROSION ON SEAT TRACK FLANGE BS 806, LBL 26, WL 208. REMOVED CORROSION AND TREATED AREA PER MM 51-20-00.May 26, 1999 · N208UP · Boeing 727247 · Fuselage, Seat/Cargo Attach FittingsSDR UPS99229698Seat Track · corrodedINSPECTION TYPE:SI, CORROSION ON SEAT TRACK FLANGE BS 826, LBL 26, WL 208. REMOVED CORROSION 2 X 4 X 0.001 WITHIN LIMITS PER SRM 53-10-1, ALODINED AND PRIMED.May 26, 1999 · N208UP · Boeing 727247 · Fuselage, Seat/Cargo Attach FittingsSDR UPS99229697Seat Track · corrodedINSPECTION TYPE:SI, CORROSION ON SEAT TRACK FLANGE BS 848, WL 208, LBL 26. REMOVED CORROSION TREATED AND PAINTED AREA PER MM 51-20-00.May 26, 1999 · N208UP · Boeing 727247 · Fuselage, Seat/Cargo Attach FittingsSDR UPS99229797Flap Track · corrodedINSPECTION TYPE:SI CORROSION (C57-581-06.00-03) ON NR 3 FLAP TRACK AT SPOILER BEAM MOUNT PAD AND HOLES AND AT REAR SPAR MOUNT HOLES. REMOVED NR 3 FLAP TRACK, REMOVED HARDWARE, SENT FLAP TRACK OUT TO OVERHAUL FACILITY. RECEIVED OVERHAULED FLAP TRACK AND INSTAMay 25, 1999 · N208UP · Boeing 727247 · Trailing Edge FlapsSDR UPS99229796Flap Track · corrodedINSPECTION TYPE:SI CORROSION (C57-581-06.00-04) ON NR 6 FLAP TRACK AT SPOILER BEAM PAD AND HOLES AND AT FORWARD LUG AND REAR SPAR MOUNT HOLES. REMOVED NR 6 FLAP TRACK, REMOVED HARDWARE, SENT TO OVERHAUL FACILITY. RECEIVED OVERHAULED FLAP TRACK, INSTALLED HARMay 25, 1999 · N208UP · Boeing 727247 · Trailing Edge FlapsSDR UPS99229664Valve · malfunctionedINSPECTION TYPE:N/A ON TAKEOFF ABOVE 80 KTS T6 NR 1 ENGINE OIL PRESSURE WENT ABOVE THE RED LINE TO 65 PSI. WHEN THRUST WAS REDUCED TO CLIMB POWER, T6 OIL PRESS REMAINED ABOVE THE RED LINE UNTIL POWER WAS REDUCED BELOW 1.5 EPR. OIL PRESS REMAINED BELOW THE THMay 21, 1999 · N208UP · Boeing 727247 · Engine Oil PressureSDR DL72E991153Frame · misdrilledWHILE PERFORMING REPETITIVE INSP PER OPN 5865 REQD BY AD 94-02-04 (REF 4-61904-3AD/-12AD) AN OVERSIZED FASTENER HOLE WAS FOUND IN THE RT BS 784 FRAME, I/B CHORD. THE SUBJECT HOLE IS THE 2ND BELOW THE FLOOR LINE. NO CRACKS WERE FOUND. REWORKED PER ERA 333135May 21, 1999 · N830WA · Boeing 727247 · Fuselage Main, FrameSDR DL72E991152Skin · damagedDURING HMV, A T/L REPAIR WAS REMOVED AND ADDITIONAL DAMAGE WAS NOTED (BELOW AND AFT OF ORIGINAL DAMAGE). BOTH DAMAGES WILL BE REPAIRED VIA ONE REPAIR SCHEME. REPAIRED PER ERA 300413-14, REV D.May 21, 1999 · N830WA · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72E991151Skin · wornLOWER SKIN BELOW THE WING TO BODY FAIRING AT BS 950D BETWEEN S26R AND S27R WAS FOUND DAMAGED DUE TO A LOOSE FASTENER. REPAIRED PER ERA 333123-14, REV A.May 21, 1999 · N830WA · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72E991150Skin · corrodedFUSELAGE SKIN FOUND WITH CORROSION AT BS 720E AND S26R. ONLY THE LOWER (OVERLAPPED) SKIN WAS DAMAGED. REPAIRED PER ERA 333122-14, REV B.May 21, 1999 · N830WA · Boeing 727247 · Fuselage Main, Plate/SkinSDR 99FDEA00182Frame · crackedFOUND BS 1010 FRAME TO BE CRACKED AT RBL 18, WL 149. *S/D* REMOVED AND REPLACED FRAME PER IAW FEDEX EA 7-5310-45281.May 19, 1999 · N234FE · Boeing 727247 · Fuselage Main, FrameSDR UPS99229640Compressor · stalledINSPECTION TYPE:N/A, JUST AFTER T/O PASSING 4,800 FT, NR 1 ENG HAD SEVERE VIBRATION AND EGT CLIMBED IMMEDIATELY TO 800 C WITH THRUST LEVER RETARDED TO FLT IDLE AND EGT CONTINUED TO CLIMB. LOUD BANG (COMPRESSOR STALL) ACCOMPANIED LOSS OF THRUST. REMOVED AND RMay 17, 1999 · N208UP · Boeing 727247 · Turbine Engine Compressor SectionSDR UPS99229634Door · crackedINSPECTION TYPE:N/A, RIGHT WING GEAR FLYING DOOR, FWD AND AFT OF HINGE PANEL AREA, SKIN CRACKED UNDER AND BEYOND DOUBLER. REMOVED EXISTING DOUBLER, STOP DRILLED CRACKS, INSTALLED DOUBLER PER SRM 52-80-2 FIG 2.May 17, 1999 · N212UP · Boeing 727247 · Landing Gear DoorsSDR UPS99229611Clamp · looseINSPECTION TYPE:N/A, NR 3 STRUT OVERHEAT LIGHT LIGHT WENT OUT AFTER 15-20 SECONDS. UNABLE TO COMPLETE CHECK LIST DUE TO NR 1 ENGINE SHUTDOWN AND CLOSE PROX TO LANDING. NR 3 PRECOOLER CLAMP LEAKING. TIGHTENED CLAMP, RAN ENGINE NO DEFECTS PER M/M 36-10-10 & 7May 17, 1999 · N208UP · Boeing 727247 · Pneumatic Distribution SystemSDR DL72E991079Keel Beam · crackedDURING INSPECTION OF THE LWR KEEL BEAM PER EO 4-64433-3, A CRACK WAS FOUND IN THE WEB (ONLY) JUST ABOVE THE VERT FLANGE OF THE LT SIDE BEAM. REPAIRED PER ERA 333113-14, REV B.May 17, 1999 · N830WA · Boeing 727247 · Fuselage Main, KeelSDR DL72E991078Skin · gougedGOUGES WERE FOUND IN THE SKIN AT THE AFT EDGE OF THE C2 DOOR CUTOUT AT BS 990. THE DAMAGE WAS LOCATED BETWEEN S24 AND S24+5 INCHES. REPAIRED PER ERA 333109-14, REV A.May 17, 1999 · N830WA · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W991088Skin · dentedTHE FUSELAGE SKIN WAS DENTED BETWEEN FS 1130 AND 1166 BETWEEN STRINGERS 23R AND 24R. THE SKIN DENT WAS CUT OUT WITH A 22.5 INCH X 6.5 INCH CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL DOUBLER PER ER/A 367383-14, REV A.May 15, 1999 · N2810W · Boeing 727247 · Fuselage Main, Plate/SkinSDR UPS99229605Duct · brokenINSPECTION TYPE:N/A, FIRE WARNING ON NR 1 ENGINE AFTER TAKEOFF ON CLIMBOUT. SECURED ENGINE IAW PROCEDURE. FIRE WARNING LIGHT/BELL WENT OUT WHEN POWER REDUCED. FOUND FUEL DEICING HEATER DUCT BROKEN. REMOVED AND REPLACED MANIFOLD AND RAN ENGINES. OPS CK ANDMay 14, 1999 · N208UP · Boeing 727247 · Fuel HeaterSDR DL72W991066Skin · gougedGOUGE ON THE OUTER SKIN FS 1148 STRINGER 24R. REPAIRED PER ERA 367383-14.May 13, 1999 · N2810W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72E991198Spar · misinstalledNR 2 MIDFLAP / UPPER SPAR CHORD / WBL 124 / ALT FAST INSTL. DURING ACCOMPLISHMENT OF EO 4-58705-3AD, MTC WAS UNABLE TO INSTALL THE REQUIRED COLLAR AT ONE OF THE MOD FASTENER HOLES DUE TO PROXIMITY OF HOLE TO SPAR FILLET RADIUS. AUTHORIZED USE OF MINI-NUT ANDMay 13, 1999 · N830WA · Boeing 727247 · Trailing Edge FlapsSDR DL72W991047Line · crackedB-SYS QTY FELL TO ZERO. FOUND HYD LINE CRACKED AT B-SYS HYD FILTER MODULE. REPLACED SAME, SERVICED QTY TO FULL. LEAK CHECK NORMAL.May 12, 1999 · N293WA · Boeing 727247 · Hydraulic System, MainSDR DL72W991046Angle · crackedTPA - LTR CHK D-1, NR 3 SPOILER I/B ACTUATOR ATTACH ANGLE CRACKED AT LWR BOLT. REPLACED ANGLE PER MM 57-42-0.May 12, 1999 · N2813W · Boeing 727247 · SpoilersSDR DL72W991045Bracket · crackedNR 1 L/E FLAP ACT O/B AND I/B MOUNT BRACKETS CRACKED AT UPPER AND LOWER MOUNT BOLTS. REPAIRED PER MM 57-20-21.May 12, 1999 · N2813W · Boeing 727247 · Leading Edge DevicesSDR DL72W991044Angle · crackedNR 2 SLAT LWR COVE SKIN ATTACH ANGLE CRACKED AT I/B STOP PAD. REPAIRED PER MM 57-54-0.May 12, 1999 · N2813W · Boeing 727247 · Leading Edge DevicesSDR DL72W991030Angle · crackedCOVE SKIN ATTACH ANGLE CRACKED BELOW I/B STOP PAD NR 8 SLAT. REPAIRED PER MM 57-54-0 FIG 812.May 10, 1999 · N2816W · Boeing 727247 · Leading Edge DevicesSDR DL72W991029Angle · crackedA 1.5 INCH CRACK IN SUPPORT ANGLE FWD OF NR 8 SPOILER. REPAIRED PER MM 57-20-22 FIG 806.May 10, 1999 · N2816W · Boeing 727247 · SpoilersSDR DL72E991004Skin · damagedINNER SKIN CUT TO GAIN ACCESS TO RIBS. REPAIRED SKIN PER M/M 57-54-0 FIG 80.May 7, 1999 · N830WA · Boeing 727247 · Leading Edge DevicesSDR DL72W991001Compressor · stalledDEPARTING DFW AFT CARGO DOOR CAME OPEN DURING ROTATION AT T/O. NUMBER 3 ENGINE PRECAUTIONARY SHUT DOWN IN FLIGHT DUE TO MULTIPLE COMPRESSOR STALLS. ONE FAN BLADE NICKED AND MINOR DAMAGE TO ACCOUSTICAL PANEL.May 6, 1999 · N2819W · Boeing 727247 · Turbine Engine Compressor SectionSDR DL72E990981Fairing · corrodedFUSELAGE FAIRING RT AC BAY FRAME, CORROSION AROUND HINGES FOR ACCESS PANEL 3448 RBL 9 STA 740 TO 774. REMOVED PANEL 3448 DAMAGED T/E. BEGAN FABRICATING REPAIR PER M/M 53-30-1. OK TO PAINT AND INSTALL. COMPLETED FABRICATION PRIOR TO TREAT AND PAINT. INSTALMay 5, 1999 · N830WA · Boeing 727247 · Aerodynamic FairingsSDR DL72E990969Fan · failedSMELL OF SMOKE NOTED IN CABIN PRIOR TO TAKEOFF. RETURNED TO GATE, GASPER FAN C/B POPPED. REPLACED GASPER FAN, OPS CKS OK. FAN HAD CAUSED SMOKE IN CABIN.May 3, 1999 · N282WA · Boeing 727247 · Air Distribution FanSDR DL72E992067Angle · mis instalkledDURING SHOP INSPECTION, THE AFT LOWER CLOSEOUT ANGLE WAS FOUND WITH FASTENERS MISSING. THE ANGLE WAS REPAIRED PER MM 57-52-0, FIG 802 BY INSTALLING A SPLICE DOUBLER AND NEW SECTION OF ANGLE.Apr 28, 1999 · N830WA · Boeing 727247 · Trailing Edge Flaps
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