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 DL72E961709Rib · crackedLOWER AFT FLANGE CRACKED, UPPER FLANGE CRACKED AND STOP DRILLED BUT NO DOUBLER AND FWD FLANGE HAS TEMPORARY REPAIR. REPLACED RIB.Jun 25, 1996 · N282WA · Boeing 727247 · Leading Edge DevicesSDR DL72E961708Rib · crackedLOWER AFT FLANGE DOUBLER CRACKED, UPPER FWD FLANGE CRACKED PAST STOP DRILL AND LOWER FWD FLANGE DOUBLER CRACKED. REPLACED RIB.Jun 25, 1996 · N282WA · Boeing 727247 · Leading Edge DevicesSDR DL72W961520Door · crackedTHE R-1 DOOR WAS FOUND CRACKED AT THE UPPER FWD CORNER. REPAIRED PER 52-12-0, FIG 805.Jun 24, 1996 · N2807W · Boeing 727247 · Passenger/Crew DoorsSDR DL72W961518Bulb · failedON LAYOVER, FOUND RIGHT AFT SLIDE LIGHT INOP. RELAMPED SAME, CHECKS GOOD.Jun 24, 1996 · N2819W · Boeing 727247 · Emergency LightingSDR DL72W961509Light · inoperativeR2 ABOVE DOOR EXIT EMERGENCY LIGHT INOP. REPLACED EXIT LIGHT AND BATTERIES, CKS NORMAL.Jun 22, 1996 · N2807W · Boeing 727247 · Emergency LightingSDR DL72W961452Channel · crackedDURING INSPECTION, FOUND CHANNEL AT FS 1263 TORQUE BOX CRACKED. CRACK LENGTH WAS APPROXIMATELY 1.5 INCH. REPLACED CHANNEL PER AD 94-07-08 AND B727 S/B 53-0129, R 4.Jun 15, 1996 · N294WA · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W961435Angle · crackedNR 6 SLAT LOWER COVE SKIN ANGLE CRACKED 1.5 INCH INBD OF ACTUATOR. REPAIRED PER M/M 57-54-0.Jun 14, 1996 · N294WA · Boeing 727247 · Leading Edge DevicesSDR DL72W961427Heat Exchangers · leakingAT 25,000 FT ENG'S AT IDLE, ENG ANTI-ICE ON, LOST CONTROL OF CABIN PRESSURIZATION. DURING EMERGENCY DECENT CABIN CLIMBED TO 12,000 FT. FOUND BOTH LEFT AND RIGHT HEAT EXCHANGERS LEAKING THROUGH CORE. REPLACED BOTH EXCHANGERS, LEAK AND PRESSURIZATION CHECKS GJun 14, 1996 · N297WA · Boeing 727247 · Cabin Cooling SystemSDR DL72W961369Light · inopAIRSTAIRS AREA EMERGENCY LIGHT INOP. REPLACED LIGHT.Jun 6, 1996 · N293WA · Boeing 727247 · Emergency LightingSDR 96FDEA01071Closing Mech · out of adjustALL MODES OF CABIN PRESSURIZATION SYS FAILED, NO DOOR LIGHT. WHEN A/C BLOCKED IN, FOUND FWD CABIN DOOR IMPROPERLY CLOSED, AFT PART ADJAR. OPS CHECKED DOOR, DOOR CLOSED PROPERLY. FOUND UPPER AFT PORTION OF DOOR REQ MODERATE PRESSURE WHILE CLOSING TO INSURE UJun 4, 1996 · N233FE · Boeing 727247 · Passenger/Crew DoorsSDR DL72W961459Skin · crackedTHE SKIN JUST BELOW FWD LAV SERVICE PANEL WAS FOUND CRACKED. THE SKIN IS MADE FROM 0.040 2024-T3 AND THE_FINAL CUTOUT DIMENSIONS WERE 1.375 FWD/AFT AND 2.5 ABOVE/BELOW. THIS ERA GIVES INSTRUCTIONS TO REPAIR THE DAMAGE WITH A 0.050 2024-T3 DOUBLER.Jun 2, 1996 · N2811W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W961352Skin · corrosionMTC REPORTS CORROSION ON THE FUSELAGE SKIN AT STA 540 AT STR 27R. CUT-OUT RESULTED IN 5.5 INCHES FWD/AFT BY 3.3 INCHES CIRCUM. AN EXISTING REPAIR INBD OF NEW DAMAGE REPAIRS A CUTOUT MEASURING .15 INCH FWD/AFT BY 2.5 INCHES CIRCUM. SKIN IS MACHINED FROM .125 May 29, 1996 · N2815W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W961316Rib · crackedRIB NR 21 CRACKED. REPAIRED PER MM 57-54-0.May 29, 1996 · N2820W · Boeing 727247 · Leading Edge DevicesSDR DL72W961315Skin · crackedSKIN CRACKED AT UPPER FWD BOLT HOLE, FENCE ATTACH POINT. REPAIRED PER MM 57-54-0 FIG 813.May 29, 1996 · N2820W · Boeing 727247 · Leading Edge DevicesSDR DL72W961314Relay · failedEMERGENCY EXIT LIGHTS WILL NOT GO OUT AFTER TEST. REPLACED R-70 RELAY AND SYSTEM TEST CHECKED NORMAL (P/N 244201154) (MFG 10-60450-3). EVENT OCCURED ON THE GROUND AFTER FLT 1739 ARRIVED FROM TUS\AND THE CREW NOTICED THAT THE EXIT LIGHTS WERE ON AFTER TESTINGMay 29, 1996 · N2811W · Boeing 727247 · Emergency LightingSDR DL72W961310Frame · crackedL-2 DOOR FRAME UPPER HINGE CUTOUT CRACKED. REPAIRED PER SRM 52-40-2.May 28, 1996 · N2815W · Boeing 727247 · Passenger/Crew DoorsSDR DL72W961309Skin · crackedTWO, .75 INCH CRACKS IN VERTICAL STAB SKIN FWD OF SADDLE PANEL RT SIDE ABOVE PANEL 9516. REPAIRED PER M/M 54-30-0.May 28, 1996 · N2815W · Boeing 727247 · Vertical Stabilizer, Plate/SkinSDR DL72W961308Doubler · crackedREPAIR DOUBLER CRACKED RT ELEV 3RD FROM O/B HINGE RIB. REPAIRED PER M/M 55-10-31.May 28, 1996 · N2815W · Boeing 727247 · Elevator StructureSDR DL72W961468Skin · crackedTHE SKIN JUST FWD OF STA 700 BETWEEN STR 28L AND 28R NEAR BL 0 WAS FOUND CRACKED AND CORRODED. REPAIRED WITH A DOUBLER AND TRIPLER PER FAA/DER FORM 8110-3, DER DESIGNATION SO-9-57.May 24, 1996 · N2809W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W961283Skin · crackedSKIN CORROSION AND CRACK JUST FWD OF STA 700 BETWEEN STRINGERS 28L AND 28R NEAR BL 0. CUTOUT MEASURED 7.5 BY 3.75 INCH. REPAIRED PER DAL ER/A 303637-14, REV A.May 24, 1996 · N2809W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W961488Bulkhead · crackedA .5 INCH CRACK WAS FOUND IN THE 1183 BULKHEAD AT RBL 8 AND WL 172. REPAIRED PER DELTA ER/A 303629-14AD.May 23, 1996 · N2813W · Boeing 727247 · Fuselage Main, BulkheadSDR DL72W961289Bulkhead · crackedA .5 CRACK FOUND IN 1183 BULKHEAD AT RBL 8 AND WL 172. THIS ERA WILL GIVE INSTRUCTIONS TO ACCOMPLISH A REPAIR UNTIL THE FULL MODIFICATION REQUIRED BY AD 90-06-09 IS ACCOMPLISHED. THE REPAIR WILL BE INSTALLED ON THE FORWARD SIDE OF THE 1183 BULKHEAD.May 23, 1996 · N2813W · Boeing 727247 · Fuselage Main, BulkheadSDR DL72W961270Light · inoperativeON T/S INSP, FOUND COCKPIT OVER DOOR EMERGENCY EXIT/FLASHLIGHT DID NOT OPERATE IN THE ON POSITION DURING TEST. REPLACED ASSEMBLY 334701743.May 23, 1996 · N2815W · Boeing 727247 · Emergency LightingSDR DL72W961489Channel · crackedFOUND A CRACK IN THE ANGLE OF THE FWD TRANSVERSE BEAM AND AFT CHANNEL OF THE RT TORQUE BOX AT FS 1263. REPAIRED PER DELTA ER/A 303628-14AD.May 22, 1996 · N2813W · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W961294Traverse Beam · crackedCRACK IN ANGLE OF THE FWD TRANSVERSE BEAM AND AFT CHANNEL OF THE RT TORQUE BOX AT FS 1263. THIS AREA OF THE TORQUE BOX IS THE SUBJECT OF AD 94-07-08 WHICH REQUIRES INSPECTION PER S/B 53-0129. THIS ER/A WILL REPLACE THE DAMAGED PART IN ACCORDANCE WITH THE S/BMay 22, 1996 · N2813W · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W961258Hinge Cutout · crackedFOUND DURING A-2 LETTER CHECK, L-2 DOOR UPPER HINGE CUTOUT CRACKED. REPAIRED PER SRM 52-40-2.May 22, 1996 · N2813W · Boeing 727247 · Service DoorsSDR DL72W961257Skin · crackedFOUND DURING A-2 LETTER CHECK, TWO .25 INCH CRACKS AT CONSECUTIVE RIVET HOLES LT SIDE OF VERT STAB 10 FT AFT OF NR 2 ENG INLET. REPAIRED PER M/M 54-30-0 FIG 801.May 22, 1996 · N2813W · Boeing 727247 · Vertical Stabilizer, Plate/SkinSDR DL72W961256Stringer · crackedFOUND DURING A-2 LETTER CHECK, 1 INCH CRACK AT STRINGER TO BULKHEAD ATTACH BOLT AT FIN STA 180.6 STR 8 LT SIDE. REPAIRED PER M/M 55-30-0 FIG 803.May 22, 1996 · N2813W · Boeing 727247 · Vertical StabilizerSDR DL72W961250Fuel Pump · failedNUMBER 1 ENGINE SHUTDOWN 30 SECONDS AFTER LIFT OFF. FOUND SHAFT SHEARED ON FUEL PUMP. REPLACED PUMP AND CONTROL.May 21, 1996 · N2817W · Boeing 727247 · Engine Fuel PumpSDR DL72W961411Skin · crackedDURING INSPECTION, FOUND 1 INCH CRACK IN THE UPPER FWD CORNER OF THE L-1 DOOR CUTOUT. REPAIRED PER ER/A 303614-14AD.May 19, 1996 · N2807W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W961290Skin · fatigueTHE FUSELAGE SKIN AND UNDERLYING DOUBLER WAS FOUND TO HAVE A ONE INCH CRACK IN THE UPPER FWD CORNER OF THE L-1 DOOR CUTOUT. REPAIRED PER DAL ER/A 303614-14AD.May 19, 1996 · N2807W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W961462Skin · corrosionSKIN CORROSION AT FS 720F AT STR 27R. REMOVED A 1.75 INCH BY 5 INCH CUTOUT JUST FWD OF AN EXISTING REPAIR AT STA 730. ERA WILL INCORPORATE BOTH REPAIRS INTO ONE REPAIR.May 18, 1996 · N2809W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W961282Skin · corrodedSKIN CORROSION AT STA 720F AT STRINGER 27R. DAMAGE REMOVAL RESULTED IN A 1.75 BY 5 INCH CUTOUT JUST FWD OF AN EXISTING REPAIR AT STA 730, ERA 213172. EXISTING REPAIR REQUIRED THE REMOVAL OF THE CORNER OF THE LWR SKIN AT STA 740 AND STRINGER 26R. REPAIRED PEMay 18, 1996 · N2809W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W961200Stiffener · crackedFOUND ON A-1 LETTER CHECK, FWD SPAR STIFFENER CRACKED I/B SIDE NR 3 SLAT I/B TRACK. REPLACED STIFFENER PER MM 57-20-21.May 17, 1996 · N2814W · Boeing 727247 · Leading Edge DevicesSDR DL72W961199Doubler · damagedDOUBLER DAMAGED LOWER RUDDER LOWER RT HINGE AREA. REPLACED RUDDER PER SRM 55-2-3.May 17, 1996 · N2814W · Boeing 727247 · Rudder StructureSDR DL72W961234Floor Beam · corrodedFOUND ON MV1 CK, CORROSION/RIVETS SHEARD AT CABIN FLOOR BEAM STA 1070 AT RT O/B GALLEY FLOOR TRACK. REPAIRED PER M/M 53-20-11 FIG 804.May 15, 1996 · N2809W · Boeing 727247 · Fuselage Main, Floor BeamSDR DL72W961171Floor Beam · corrodedFOUND CORROSION ON FLOOR BEAM UPPER ANGLE STA 400 RBL 55. REPAIRED PER M/M 53-20-11 PG 811 B.May 14, 1996 · N2809W · Boeing 727247 · Fuselage Main, Floor BeamSDR DL72E961269Angle · corrodedAT MID VISIT FASTENER HOLES WERE FOUND CORRODDED AT STA 400 RBL 33. CAP AND ANGLES REPLACED PER SRM 53-10-8.May 13, 1996 · N2829W · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72E961226Skin · corrosionTHE FUSELAGE SKIN HAS A 2 BY 2 CUTOUT AT FS 1050, NEAR S-28R. THE SKIN IS 2024-T3 CLAD CHEM-MILLED SKIN WITH A LOCAL THICKNESS OF 0.050 AND 0.070. UPON REMOVAL OF TIME-LIMITED REPAIR AT HMV, ADDITIONAL DAMAGE HAS BEEN DICOVERED. S-28R AT STATION 1050 HAS EXMay 13, 1996 · N2829W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72E961143Stringer · corrosionUPON REMOVAL OF TIME-LIMITED REPAIR AT HMV, ADDITIONAL DAMAGE HAS BEEN DICOVERED. STRINGER 28R AT STATION 1050 HAS EXTENSIVE CORROSION AND WILL REQUIRE INSTALLATION OF A SPLICE SECTION. ADDITIONAL CORROSION DAMAGE IS LOCATED APPROXIMATELY 2 INCHES INBOARD ANMay 13, 1996 · N2829W · Boeing 727247 · Fuselage Main, Longeron/StringerSDR DL72E961142Stringer · crackedSTRINGER CRACKED INSIDE TAIL CRAWLWAY 3RD BAY FROM TOP LT SIDE. REPAIRED PER MM 55-30-0 FIG 803.May 13, 1996 · N283WA · Boeing 727247 · Vertical StabilizerSDR DL72E961141Frame · crackedA .375 INCH VISUAL CRACK R-2 DOOR UPPER HINGE CUTOUT AT FWD FRAME. REPAIRED PER SRM 52-40-2.May 13, 1996 · N283WA · Boeing 727247 · Service DoorsSDR DL72W961106Battery Pack · dischargedRIGHT AFT OVERWING SLIDE LIGHT INOP. REPLACED BATTERY PACK AND RACK, LIGHT CHECKS NORMAL.May 7, 1996 · N293WA · Boeing 727247 · Emergency LightingSDR DL72W961044Hyd Pump · inoperativeFLT 893 - AIR TURN BACK DUE TO B-SYSTEM HYDRAULIC WENT TO ZERO WITH LOW PRESSURE LIGHT ON. A-SYSTEM AT 2.5 GALLONS. REPLACED INBOARD B-SYSTEM HYDRAULIC PUMP AND FILTERS. REPLACED NR 5 SPOILER FILTER HOUSING PACKING. RESERVICED HYDRAULIC SYSTEM. OPS AND LEMay 1, 1996 · N292WA · Boeing 727247 · Hydraulic Pump (Electric/Engine), MainSDR DL72W961035Light · inoperativeAFT AIRSTAIRS EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT ASSY AND BATTERIES. CHECKS NORMAL.Apr 30, 1996 · N295WA · Boeing 727247 · Emergency LightingSDR DL72W961047Light · inoperativeEMERGENCY EXIT LIGHT AT L1 DOOR INOPERATIVE. REPLACED LIGHT ASSY AND BATTERIES.Apr 28, 1996 · N2809W · Boeing 727247 · Emergency LightingSDR DL72W961626Mount Fitting · crackedTHE NR 3 ENGINE FORWARD MOUNT FITTING WAS FOUND CRACKED AND REQUIRED REPLACEMENT. THE CRACK EXTENDED FROM THE TOP OF THE FITTING TO THE BOTTOM OF THE FITTING APPROXIMATELY 2 INCHES OUTBOARD OF THE FUSELAGE SKIN. THE CRACK FOLLOWED THE BLEND LINE BETWEEN PLANApr 22, 1996 · N290WA · Boeing 727247 · Engine Mount SectionSDR DL72W961019Bulkhead Fitting · misdrilledWHILE ACCOMPLISHING A PRELIMINARY ATTEMPT TO FIT THE 65-18722-8 FORWARD MOUNT FITTING INTO POSITION, NOTED THAT SEVEN OF THE HOLES COMMON TO THE B.S. 1183 FRAME DO NOT LINE UP. THESE HOLES AND THE AMOUNT OF OFFSET ARE INDICATED ON FIGURE 1. DL ERA 3033483-14Apr 22, 1996 · N290WA · Boeing 727247 · Fuselage Main, BulkheadSDR DL72W960930Act Angle · crackedNR 8 SLAT ACTUATOR INBOARD ATTACH ANGLE CRACKED. REPAIR PER M/M 57-20-21.Apr 18, 1996 · N2819W · Boeing 727247 · Leading Edge Slat ActuatorSDR DL72W960929Act Support · crackedFOUND TWO-INCH CRACK IN NR 8 SLAT OUTBOARD ACTUATOR SUPPORT WHILE SHOWING MAINTENANCE LOCATION OF CRACK AT INBOARD SUPPORT. REPAIR PER M/M 57-20-21.Apr 18, 1996 · N2819W · Boeing 727247 · Leading Edge Slat Actuator
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