Boeing 727-247

Service difficulty reports · 2,669

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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 = '727247'
  ORDER BY difficulty_date DESC"

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SDR DL72W960927Swivel Fitting · out of adjustMLG SPAR BEING CHAFED BY STRUT DOOR SIDE BRACE SWIVEL FITTING. REWORK PER M/M 57-43-0.Apr 18, 1996 · N2819W · Boeing 727247 · Wing, Landing Gear Attach FittingsSDR DL72W960926Web · cracked.3750 INCH CRACK IN LIGHTNING HOLE OF LT LOWER TORQUE BOX WEB, STA 1263, TOP HOLE. REPAIR PER M/M 53-11-0.Apr 18, 1996 · N2819W · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W961020Blkhd Web · crackedTHE STA 1183 BULKHEAD WEB WAS FOUND CRACKED IN TWO LOCATIONS. THE DAMAGE WAS TRIMMED OUT WITH DIMENSIONS OF 2.6250 INCH AT LBL 8, WL 190 AND 8 INCH BY 3.1250 INCH AT LBL 14, WL 173. THE BULKHEAD WEB IS MANUFACTURED FROM 0.050 INCH CLAD 2024-T3. THIS ER/A AUApr 15, 1996 · N2811W · Boeing 727247 · Fuselage Main, BulkheadSDR DL72E960868Wire · brokenEMERGENCY TRACK LIGHTS INOP FROM 20ABC TO 27ABC. FOUND WIRES BROKEN AT 20ABC AND 27ABC. REPAIRED SAME, EMERGENCY TRACK LIGHTING SYSTEM OPS CHECKS GOOD.Apr 15, 1996 · N831WA · Boeing 727247 · Light System WiringSDR DL72W960938Floor Beam · corrodedFOUND ON MV1 CHECK - CORROSION ON FLOOR BEAM TOP SURFACE STA 1050 FROM RBL 10 TO 14. REPAIR - REPAIRED PER M/M 53-20-11.Apr 12, 1996 · N2811W · Boeing 727247 · Fuselage Main, Floor BeamSDR UPS96205954Battery · dischargedMAINTENANCE REPORTED, EMERGENCY EXIT LIGHT OVER FWD ENTRY DOOR DOES NOT ILLUMINATE. REPLACED BATTERY IN EMERGENCY LIGHT PANEL, OP CHECK GOOD.Apr 10, 1996 · N209UP · Boeing 727247 · Emergency LightingSDR DL72W960835Skin · punctureA .25 INCH LONG PUNCTURE HOLE IN LOWER SKIN OF LT ELEVATOR, 14 INCHES AFT OF NR 2 BALANCE BOARD. INSTALLED DOUBLER PER SRM 55-20-3 FIG 4, RECALCULATE BALANCE PER SRM 51-80-7.Apr 10, 1996 · N295WA · Boeing 727247 · Elevator, Plate/SkinSDR DL72W960808S-Duct Skin · crackedFOUND ON MV1 CHECK, TIME LIMITED REPAIR INSTALLED, 1 INCH CRACK IN S-DUCT HOUSING RT SIDE JUST FWD OF SADDLE PANEL, VERT STAB FRONT SPAR. INSTALLED PERMANENT REPAIR PER M/M 54-30-0 PG 801 FIG 802.Apr 8, 1996 · N2810W · Boeing 727247 · Nacelle/Pylon StructureSDR DL72E960784Light · inoperativeON LAYOVER, FOUND EMERGENCY LIGHT ABOVE AFT AIRSTAIR INOP. RESEATED BATTERY PACK, FOUND CONTACT BROKEN ON LIGHT ASSY. REPLACED SAME.Apr 6, 1996 · N830WA · Boeing 727247 · Emergency LightingSDR DL72W960978Skin · corrosionFUSELAGE SKIN WAS FOUND CORRODED JUST AFT OF THE BUTT SPLICE AT STA 480 FROM STRINGER 28R-28L. CORROSION WAS ALSO FOUND ON THE SPLICE STRAP AT ONE FASTENER LOCATION BETWEEN BL ZERO AND 28L. THE SKIN DAMAGE RESULTED IN CUTOUT THAT EXTENDS AFT APPROX. 1.75 INCApr 5, 1996 · N2810W · Boeing 727247 · Fuselage Main, Plate/SkinSDR UPS96205862Light · inoperativeMAINTENANCE REPORTED ON PRE-DEPARTURE CHECK, EXIT LIGHTS IN COCKPIT FOUND INOPERATIVE. LIGHT ABOVE DOOR. REMOVED AND REPLACED LIGHT ASSY. OPS NORMAL.Apr 4, 1996 · N902UP · Boeing 727247 · Emergency LightingSDR DL72W960739Skin · crackedFOUND ON A-2 LETTER CHECK, .25 INCH CRACK IN MAIN ENTRY DOOR OUTER DOOR SKIN AT UPPER HINGE CUTOUT LOWER AFT CORNER. REPAIRED PER M/M 52-11-01.Apr 1, 1996 · N293WA · Boeing 727247 · Passenger/Crew DoorsSDR DL72W960737Skin · crackedFOUND ON A-2 LETTER CHECK, LOWER SKIN CRACKED .375 INCH AFT INBD CORNER OF PNEUMATIC GROUND AIR CONNECT DOOR CUTOUT. REPAIRED PER MM 53-30-0.Apr 1, 1996 · N293WA · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W960763Frame · crackedFOUND ON MV1 CHECK, L-2 DOOR FWD FRAME HAS .375 INCH CRACK AT UPPER HINGE CUTOUT. REPAIRED PER SRM 52-40-2 FIG 4.Mar 29, 1996 · N2810W · Boeing 727247 · Passenger/Crew DoorsSDR DL72W960697Skin · crackedINNER SKIN CRACKED AT NUTPLATES, RIBS 10, 11, 12 AND 13. REPAIRED PER M/M 57-54-0, FOR NR 6 L/E SLAT.Mar 29, 1996 · N2809W · Boeing 727247 · Leading Edge DevicesSDR DL72W960696Rib · crackedDURING INSPECTION, FOUND NR 6 L/E SLAT WITH INTERNAL SUPPORT RIB NR 10 CRACKED. REPAIRED PER MM 57-54-0.Mar 29, 1996 · N2809W · Boeing 727247 · Leading Edge DevicesSDR DL72W960695Rib · crackedDURING INSPECTION, NR 6 L/E SLAT WAS FOUND WITH INTERNAL SUPPORT RIB NR 11 CRACKED. REPAIRED PER MM 57-54-0.Mar 29, 1996 · N2809W · Boeing 727247 · Leading Edge DevicesSDR DL72E960700Door Pan · crackedFOUND ON D-2 LETTER CHECK, 3 INCH CRACK IN FWD SERVICE DOOR PAN EXTENDING FROM LOWER FWD STOP CASTING. REPAIRED PER ERA 303377-14 AND M/M 52-12-0.Mar 28, 1996 · N830WA · Boeing 727247 · Service DoorsSDR DL72E960699Angle · crackedFOUND ON D-2 LETTER CHECK, WEB TO STRINGER ATTACH ANGLE CRACKED. VERTICAL CRAWL WAY 3RD BAY FROM TOP LT SIDE CRACK LOCATED IN STA 133.8 AT STR 9. REPAIRED PER M/M 55-30-0.Mar 28, 1996 · N830WA · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72E960694Tq Box Web · crackedFOUND ON D-2 LETTER CHECK, TORQUE BOX WEB LIGHTENING HOLE CRACKED .25 INCH, STA 1223 RT. REPAIRED PER M/M 53-11-0.Mar 28, 1996 · N830WA · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W960869Battery Pack · dischargedON SERVICE CHECK, FOUND OVERWING EXIT SIGNS RIGHT SIDE INOP. REPLACED BATTERY PACK M1086, CHECKS OK.Mar 27, 1996 · N290WA · Boeing 727247 · Emergency LightingSDR DL72W960764Skin · crackedFOUND ON MV1 CHECK, .375 INCH VISIBLE CRACK IN R-2 SERVICE DOOR AT UPPER FWD HINGE CUTOUT. REPAIRED PER SRM 52-40-2 FIG 4.Mar 27, 1996 · N2810W · Boeing 727247 · Service DoorsSDR DL72W960747Skin · crackedFUSELAGE SKIN AND UNDERLYING DOUBLER HAVE .25 INCH CRACK IN UPPER FWD CORNER OF L-1 DOOR CUTOUT. ACCOMPLISHED REPAIRS PER DL ERS 303365-14AD.Mar 27, 1996 · N2810W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W960762S-Duct · crackedFOUND ON MV1 CHECK, TIME LIMITED REPAIR INSTALLED, 1 INCH CRACK IN S-DUCT HOUSING LT SIDE JUST ABOVE AND AFT OF ACCESS PLATE 9523. REPAIRED PER M/M 54-30-0 PG 801 FIG 802, INSTALLED PERMANENT REPAIR.Mar 25, 1996 · N2810W · Boeing 727247 · Nacelle/Pylon StructureSDR DL72W960647Track Light · inoperativeTHREE EMERGENCY EXIT TRACK LIGHTS INOP AT AFT GALLEY DOOR. REPAIRED TRACK LIGHTS, OPS NORMAL.Mar 24, 1996 · N291WA · Boeing 727247 · Emergency LightingSDR DL72W960611Skin · crackedFOUND DURING E-2 LETTER CHECK - 2 EA, .25 INCH CRACKS EXTENDING FROM RIVET HOLES, RT VERTICAL STAB SKIN, JUST BELOW SADDLE PLATE 9501. REPAIRED PER M/M 54-30-0.Mar 19, 1996 · N2816W · Boeing 727247 · Vertical Stabilizer, Plate/SkinSDR DL72W960610Web · crackedFOUND DURING E-2 LETTER CHECK - .50 INCH CRACK, LT FWD TORQUE BOX LIGHTENING HOLE. REPAIRED PER M/M 53-11-0.Mar 19, 1996 · N2816W · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W960609Angle · corrodedFOUND DURING E-2 LETTER CHECK - CORROSION AT HINGE ON LOWER FUSELAGE FAIRING PANEL FWD OF LOWER BEACON. REPAIRED PER M/M 53-30-1.Mar 19, 1996 · N2816W · Boeing 727247 · Aerodynamic FairingsSDR DL72W960592Attach Fitting · brokenLT MAIN LANDING GEAR DOOR OPENED IN FLIGHT. FOUND LANDING GEAR DOOR ACTUATOR ATTACH FITTING BROKEN, IPC 32-10-4 FIG 2 ITEM 250.Mar 16, 1996 · N2809W · Boeing 727247 · Landing Gear Door ActuatorSDR DL72E960730Rib · crackedDURING INITIAL INSPECTION OF THE NR 7 LEADING EDGE SLAT, THE NR 11 RIB WAS FOUND TO BE CRACKED. THE RIB WAS REPAIRED PER M/M 57-54-0 FIG 804.Mar 15, 1996 · N830WA · Boeing 727247 · Leading Edge DevicesSDR DL72E960728Rib · crackedDURING INITIAL INSPECTION OF THE NR 7 LEADING EDGE SLAT, THE NR 8 RIB WAS FOUND TO BE CRACKED. THE RIB WAS REPAIRED PER M/M 57-54-0.Mar 15, 1996 · N830WA · Boeing 727247 · Leading Edge DevicesSDR DL72E960726Rib · crackedDURING INITIAL INSPECTION OF THE NR 7 LEADING EDGE SLAT, THE NR 10 RIB WAS FOUND TO BE CRACKED. THE RIB WAS REPAIRED PER M/M 57-54-0 FIG 814.Mar 15, 1996 · N830WA · Boeing 727247 · Leading Edge DevicesSDR DL72E960725Heat Shield · dentedDURING INITIAL INSPECTION OF THE NR 7 LEADING EDGE SLAT, A DENT WAS FOUND IN THE HEAT SHIELD BETWEEN THE NR 11 AND NR 12 RIB. THE DENT WAS REPAIRED PER M/M 57-50-3 FIG 4.Mar 15, 1996 · N830WA · Boeing 727247 · Leading Edge DevicesSDR DL72E960677Rib · crackedDURING SHOP INSPECTION, THE NINTH AND SIXTEENTH RIBS FROM THE OUTBOARD END OF NR 7 SLAT WERE FOUND TO BE CRACKED. THE DAMAGE WAS REPAIRED PER 727 M/M 57-54-0.Mar 15, 1996 · N830WA · Boeing 727247 · Leading Edge DevicesSDR DL72E960662Rib · crackedDURING SHOP INSPECTION, THE SECOND AND SIXTH RIBS FROM THE OUTBOARD END OF NR 7 SLAT WERE FOUND TO BE CRACKED. THE DAMAGE WAS REPAIRED PER 727 M/M 57-54-0.Mar 15, 1996 · N830WA · Boeing 727247 · Leading Edge DevicesSDR DL72E960583Fuel Contl Unit · failedNR 1 ENGINE FLAMED-OUT AS TAKEOFF POWER WAS BEING APPLIED. C/A: REPLACED FCU AND FUEL PUMP. LEAK CHECKED AND RIGGED PER PFHB. OPS CKS OK.Mar 14, 1996 · N2829W · Boeing 727247 · Fuel Control/Turbine EnginesSDR DL72W960535Light · inoperativeCOCKPIT EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT ASSY. OPS CHECKS GOOD.Mar 9, 1996 · N2811W · Boeing 727247 · Emergency LightingSDR DL72W960576Skin · crackedDURING LETTER CHECK AT TAMPA, A .5 INCH CRACK IN THE FUSELAGE SKIN AT STA 1098 ALONG S-1. CRACK WAS REPAIRED PER B727 SRM 53-30-3, FIGURE 3.Mar 8, 1996 · N2821W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W960519Angle · crackedFOUND DURING B-2 LETTER CHECK - NR 8 L/E SLAT COVE SKIN ATTACH ANGLE CRACKED AT OUTBOARD UPSTOP PAD. REPAIRED PER M/M 57-54-0, PAR 5A.Mar 7, 1996 · N2821W · Boeing 727247 · Leading Edge DevicesSDR DL72W960518Angle · crackedFOUND DURING B-2 LETTER CHECK - 1 INCH CRACK NR 1 L/E SLAT COVE SKIN ATTACH ANGLE BELOW TAI DUCT. REPAIRED PER M/M 57-54-0 PAR 12.Mar 7, 1996 · N2821W · Boeing 727247 · Leading Edge DevicesSDR DL72W960511Battery Pack · dischargedLEFT OVER WING EXTERIOR FWD EMERG ESCAPE PATH ILLUMINATION LIGHT INOPERATIVE. REPLACED BOTH BULBS - NO HELP. REPLACED BATTERY PACK - OPERATION NOW NORMAL.Mar 6, 1996 · N293WA · Boeing 727247 · Emergency LightingSDR DL72W960469Angle · crackedNR 2 SLAT COVE SKIN ANGLE AT TAI DUCT CRACKED .5 INCH. FOUND DURING A-2 LTR CK, REPAIRED PER MM 57-54-0.Feb 29, 1996 · N291WA · Boeing 727247 · Leading Edge DevicesSDR DL72E960490Brakes · reqd serviceAFTER INITIAL BREAK APPLICATION ON RUNWAY, BRAKES WERE NORMAL. BUT ON SUBSEQUENT APPLICATION TO TURN OFF RUNWAY LEFT BRAKES WERE SOFT AND INEFFECTIVE. BLED NR 3 AND NR 4 BRAKES, ANTI-SKID TEST WAS NORMAL, RESET DEBOOST ON LEFT GEAR AND OPERATION NORMAL.Feb 29, 1996 · N2826W · Boeing 727247 · Landing Gear Brake SystemSDR DL72W960698Eng Mount Ftg · crackedDURING ROUTING MAINTENANCE, NR 3 ENGINE WAS NOTICE TO BE LOOSE ON THE PYLON AND THE PYLON SEPARATED FROM THE FUSELAGE SKIN AT THE FORWARD ENGINE MOUNT AREA. THE ENGINE WAS REMOVED AND AREA INSPECTED. FOUND THE FORWARD ENGINE MOUNT FITTING AT FS 1183 COMPLETFeb 27, 1996 · N290WA · Boeing 727247 · Engine Mount SectionSDR DL72E960549Fitting · pittedLT MLG NR 4 FLAP TRACK PORKCHOP FITTING HAS PITTED BUSHING. FORWARD HOLE BORED TO 1.7068 INCH PER MM 57-42-0, PAGE 814.MPI PER PS 900-6-2, NR 01. OK. TURNED O/D OF BUSHING BRUSH CAD FITTING IN STRIKE CAD PLATE BUSHING, PAINTED FITTING PER MM 57-42-0. INSTAFeb 27, 1996 · N831WA · Boeing 727247 · Wing, Control Surface Attach FittingsSDR UPS205568Support · crackedCREW REPORTED, AFTER TAKEOFF LOUD AIR LEAK COMING FROM FWD ENT DOOR. FOUND CRACK AROUND A LIGHTENING HOLE SUPPORT AREA FOR TORQUE TUBE LATCH ARM FWD UPPER CORNER OF DOOR. NO TYPICAL SRM REPAIR ADDRESSING EITHER REPLACING THE DOOR OR AN EO FOR REPAIR.Feb 24, 1996 · N210UP · Boeing 727247 · Passenger/Crew DoorsSDR DL72E960412Batteries · dischargedEMERGENCY EXIT LIGHT OVER THE BOTTOM STEP OF THE AIR STAIRS IS INOP. REPLACED BATTERIES, OPS NORMAL.Feb 21, 1996 · N2826W · Boeing 727247 · Emergency LightingSDR UPS2005546Line · failedCREW REPORTED, AFTER GEAR EXT, LOSS OF B-SYSTEM PRESSURE AND LOW PRESSURE LIGHTS CAME ON. B-SYS PRESS ZERO AND QUANTITY DECREASED FROM 3 TO 1.9, RAN APPROVED CHECKLIST, LOST B-SYS. REPLACED NR 2 PUMP PRESSURE LINE WITH TEMPORARY FLEX LINE BETWEEN B-PUMP AND Feb 20, 1996 · N207UP · Boeing 727247 · Hydraulic System, MainSDR DL72W960363Stringer · crackedFROM MV-2 ATL, LT WING INSIDE WS 656.5 FWD STRINGER NR 14 FWD ATTACH TAB CRACKED. VIEWED WITH MIRROR TOP SURFACE OF TAB AT ATTACH HOLE. REPAIRED PER MM 57-13-0 PG 811.Feb 16, 1996 · N295WA · Boeing 727247 · Wing, Longeron/StringerSDR DL72W960349Angle · crackedFOUND DURING F-1 LETTER CHECK, .375 INCH CRACK NR 2 L/E SLAT COVE SKIN ATTACH ANGLE BELOW TAI DUCT. REPAIRED PER MM 57-54-0.Feb 15, 1996 · N296WA · Boeing 727247 · Leading Edge Devices
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