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 DL72W992587Stiffener · crackedA 1 INCH CRACK WING L/E SPAR STIFFENER O/B SIDE OF I/B TRACK BOX NR 4 SLAT. REPLACED SPAR STIFFENER PER MM 57-20-21.Nov 23, 1999 · N2814W · Boeing 727247 · Wing Miscellaneous StructureSDR DL72E992573Skin · crackedA 1.5 CRACK WAS FOUND IN THE L1 DOOR SURROUND STRAP. THE DAMAGE WAS FOUND DURING HMV AND REPAIRED PER ERA 333818-14.Nov 22, 1999 · N831WA · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72E992572Skin · crackedA CRACK WAS FOUND IN THE VERTICAL STABILIZER SKIN, LEFT HAND SIDE, WHERE THE SKIN MEETS THE UPPER TORQUE BOX AT APPROX FS 1210. THE DAMAGE WAS FOUND DURING HMV AND REPAIRED PER ERA 333807-14.Nov 22, 1999 · N831WA · Boeing 727247 · Vertical Stabilizer, Plate/SkinSDR DL72E992570Skin · crackedTHE SKIN OF THE VERTICAL STABILIZER WAS FOUND CRACKED AT THE FUSELAGE CREASE LINE AND STRINGER 10L. THE DAMAGE WAS FOUND AT HMV AND REPAIRED PER ERA 333830-14AD.Nov 22, 1999 · N831WA · Boeing 727247 · Vertical Stabilizer, Plate/SkinSDR DL72W992561Battery · dischargedROW 28 OVERHEAD EMERGENCY LIGHT INOP. REPLACED BATTERIES.Nov 21, 1999 · N2821W · Boeing 727247 · Emergency LightingSDR DL72W992560Battery · dischargedR1 DOOR EMERGENCY EXIT LIGHT INOP. REPLACED BATTERIES.Nov 21, 1999 · N2821W · Boeing 727247 · Emergency LightingSDR DL72W992559Battery Pack · dischargedAFT CABIN DOOR EXIT EMERGENCY LIGHT INOP. REPLACED BATTERY PACK.Nov 21, 1999 · N2821W · Boeing 727247 · Emergency LightingSDR DL72W992575Shim · looseDURING INSPECTIONS OF THE I/B FLAP TRACK FOR THE RT I/B FLAP REQUIRED PER AD 90-07-05, THE EXISTING LAMINATED SHIM WAS FOUND TO HAVE MIGRATED .375 INCH. THE SHIM WAS REMOVED AND REPLACED PER THE REQUIREMENTS OF BAC S/B 727-57-0178 AND THEAD. THE WORK WAS ACCNov 20, 1999 · N290WA · Boeing 727247 · Trailing Edge FlapsSDR DL72W992523Engine · damagedFOUND PIECE OF METAL IN BOTTOM OF COWL. FOUND 4-6 INCH HOLE IN OUTER CASE APPROX 4 FT AFT OF NOSE COWL ATTACH FLANGE. REPLACED NR 1 ENG.Nov 15, 1999 · N295WA · Boeing 727247 · Turbine Engine Compressor SectionSDR DL72W992494Power Supply · failedFLIGHT ABORTED TAKEOFF DUE TO 115 VOLT AC. FUEL FLOW CIRCUIT BREAKER POPPED DURING TAKEOFF ROLL. REPLACED FUEL FLOW POWER SUPPLY, PRECAUTIONARY. CHECKED OK ON ENGINE RUN.Nov 11, 1999 · N295WA · Boeing 727247 · Fuel Flow IndicatingSDR DL72E992496Web · crackedFWD WEB CRACKED INSIDE NR 3 L/E SLAT AT ANTI-ICE DUCT. STOP DRILLED CRACK AND FABRICATED REPAIR PARTS PER M/M 57-40-0 FIG 802 A. OK TO INSTALL. INSTALLED DOUBLER PER M/M 57-40-0 FIG 802 A.Nov 11, 1999 · N831WA · Boeing 727247 · Leading Edge DevicesSDR DL72E992478Skin · crackedTHE FUSELAGE SKIN LAP WAS FOUND CRACKED AT STRINGER 4R BETWEEN FS 540 AND FS 560. THE DAMAGE WAS REPIARED PER ERA 333763-14 DURING HMV.Nov 10, 1999 · N831WA · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72E992465Rib · crackedACTUATOR RIB CRACKED. REPAIRED RIB PER M/M 57-54-0.Nov 8, 1999 · N831WA · Boeing 727247 · Wing, Rib/BulkheadSDR DL72E992461Skin · crackedTHE FUSELAGE SKIN WAS FOUND CRACKED AT THE STRINGER 4R LAP JOINT BETWEEN FS 620 AND 640. THE DISCREPANCY WAS REPAIRED BY ER/A 333765-14 AT HMV.Nov 8, 1999 · N831WA · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72E992459Skin · crackedA CRACK WAS FOUND IN THE STRINGER 4L LAP JOINT BETWEEN FS 1030 AND 1050 DURING INSPECTIONS PER AD 99-04-22. ERA 333766-14 REPAIRED THE DAMAGE AT HMV.Nov 8, 1999 · N831WA · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W992456Light · inopFC AISLE EMERGENCY LIGHTS AFT OF LIFE RAFT COMPARTMENT INOP. REPLACED CHARGING RACK.Nov 7, 1999 · N2810W · Boeing 727247 · Emergency LightingSDR DL72E992521Attach Bolt · cracksAT HMV2, FOUND NR 5 L/E SLAT 2 CRACKS AT FENCE ATTACH BOLT HOLES AT L/E. MFR REPAIR DOUBLER PER MM 57-54-0 FIG 813, REPAIRED PER SAME.Nov 5, 1999 · N831WA · Boeing 727247 · Leading Edge DevicesSDR DL72W992441Web · crackedREF SHIP 569 TPA LTR CHK B-2 11/04/99, .5 INCH CRACK AT LEFT TORQUE BOX VERT WEB LOWER LIGHTNING HOLE STA 1233. REPAIRED PER MM 53-11-0.Nov 4, 1999 · N2820W · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W992440Web · crackedREF SHIP 569 TPA LTR CHK B-2 11-04-99, .5 INCH CRACK AT UPPER ROW OF RIVETS LT TORQUE BOX, VERT WEB STA 1305. REPAIRED PER MM 53-11-0.Nov 4, 1999 · N2820W · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W992438Frame · crackedFOUND AT B-2 LETTER CK, AFT ENTRY DOOR LT CUTOUT FRAME CRACKED AT UPPER STOP FITTING STIFFENER. REPAIRED PER SRM 53-10-9.Nov 4, 1999 · N2820W · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W992432Bracket · crackedINBD ATTACH BRACKET CRACKED NR 1 SLAT ACTUATOR BRKT. INSTALLED DOUBLER PER M/M 57-20-21. TPA F-1 LETTER CHECK.Nov 3, 1999 · N2819W · Boeing 727247 · Leading Edge Slat ActuatorSDR DL72E992837Skin · wornDURING SHOP INSPECTION, THE LOWER L/E SKIN WAS FOUND WORN APPROX 1 INCH LENGTH AT THE O/B END OF THE FLAP. THE L/E WAS REPAIRED BY INSTALLING A DOUBLER PER MM 57-52-0 FIG 803.Nov 3, 1999 · N831WA · Boeing 727247 · Leading Edge DevicesSDR DL72E992460Blkhd Stiffener · crackedTHE LBL 36.83 VERTICAL STIFFENER OF THE 1183 BULKHEAD WAS FOUND CRACKED AT HMV. ERA 333764-14 REPAIRED THIS CONDITION.Nov 3, 1999 · N831WA · Boeing 727247 · Fuselage Main, BulkheadSDR DL72E992524Rib · crackedAT HMV2, FOUND DOUBLER CRACKED ON RIB LOC I/B SIDE OF ACTUATOR FITTING ON NR 3 L/E SLAT. STOP DRILLED CRACK PER MM 57-54-0. FABRICATED DOUBLER, FOUND SECOND RIB CRACK, DRILLED SECOND RIB, FABRICATED ANOTHER DOUBLER, CUT AND REMOVED RIBS. INSTALLED DOUBLERS Nov 2, 1999 · N831WA · Boeing 727247 · Leading Edge DevicesSDR DL72E992485Rib · crackedAT HMV2 FOUND NR 3 L/E SLAT, RIB CRACKED I/B SIDE OF I/B TRACK. REMOVED FASTENERS, STOPPED DRILLED CRACK. FABRICATED DOUBLER PER MM 54-57-0 FIG 811. INSTALLED DOUBLER PER SAME.Nov 2, 1999 · N831WA · Boeing 727247 · Leading Edge DevicesSDR DL72E992484Rib · crackedAT HMV2, FOUND RIB CRACKED INSIDE NR 3 L/E SLAT ON O/B SIDE OF I/B TRACK. TRIMMED OUT DAMAGE, AND REPAIR ANGLE PER MM 57-54-0 FIG 811. INSTALLED DOUBLER PER SAME.Nov 2, 1999 · N831WA · Boeing 727247 · Leading Edge DevicesSDR DL72E992483Rib · crackedAT HMV2, FOUND RIB CRACKED ON O/B SIDE OF ACT FITTING ON NR 2 L/E SLAT. STOP DRILLED CRACK PER MM 57-54-0 FIG 804. FABRICATED DOUBLER PER SAME, INSTALLED.Nov 2, 1999 · N831WA · Boeing 727247 · Leading Edge DevicesSDR DL72E992482Rib · crackedAT HMV2, FOUND NR 2 L/E SLAT, RIB TEMP REPAIR STOP DRILLED CRACK, I/B SIDE OF ACT FITTING. STOP DRILLED CRACK PER MM 57-54-0 FIG 804, FAB'D DOUBLER PER SAME, INSTALLED.Nov 2, 1999 · N831WA · Boeing 727247 · Leading Edge DevicesSDR DL72E992481Rib · crackedAT HMV2, FOUND NR 2 L/E SLAT, RIB CRACKED I/B SIDE OF ACT FITTING. STOPPED DRILLED CRACK PER MM 57-54-0 FIG 804. FAB'D DOUBLER PER SAME, AND INSTALLED.Nov 2, 1999 · N831WA · Boeing 727247 · Leading Edge DevicesSDR DL72W992400Skin · crackedFOUND ON D-2 LETTER CK, 1 INCH CRACK LT SIDE OF STRINGER 1 STA 1098. REPAIRED PER SRM 53-30-3 FIG 3.Oct 29, 1999 · N293WA · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W992399Web · crackedFOUND ON D-2 LETTER CK, .5 INCH CRACK ON LT LOWER TORQUE BOX LIGHTENING HOLE FWD END STA 1228. REPAIRED PER MM 53-11-0.Oct 29, 1999 · N293WA · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W992395Bulkhead Web · crackedTHE FS 1183 BULKHEAD WEB WAS FOUND WITH A 1 INCH TYPICAL CRACK AT WL 178 AND LBL 8. THE CRACK IS TYPICAL OF BAC S/B 727-53-0175. THE CRACK WAS CUT OUT OF THE WEB AND REPAIRED WITH AN ALUMINUM DOUBLER PER THE S/B AND ER/A 368608-14AD. THE WEB WILL BE MODIFIOct 28, 1999 · N297WA · Boeing 727247 · Fuselage Main, BulkheadSDR DL72W992389O-Ring · leakingNR 3 ENGINE FLAMED OUT ON APPROACH AT 6000 FEET. AT LEVEL OFF 6000 FEET DURING FINAL APPROACH SEGMENT NR 3 INSTRUMENTS INDICATED THE FOLLOWING FUEL FLOW 0 / 35 PERCENT N2 / EPR0 / N1 ZERO / NORMAL OIL PRESS, NORMAL OIL TEMP / THROTTLE MOVEMENT, NO EFFECT / NROct 28, 1999 · N292WA · Boeing 727247 · Engine Fuel DistributionSDR DL72W992382Angle · crackedTORQUE BOX Z ANGLE CRACKED LT SIDE STA 1253. REPAIRED PER SRM 51-40-3.Oct 27, 1999 · N297WA · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72E992493Skin · wornCOVE SKIN WORN 34 FROM INBD END, REPAIRED PER MM 57-52-0 FIG 809, ON SHOP ORDER 877885.Oct 26, 1999 · N282WA · Boeing 727247 · Trailing Edge FlapsSDR DL72W992340Light · inopAFT STAIR EMERGENCY OVERHEAD LIGHT INOP. REPLACED LIGHT PACK ASSY, OPS CHECK NORMAL.Oct 24, 1999 · N292WA · Boeing 727247 · Emergency LightingSDR 99FDEA00419Connector · contaminatedON GEAR RETRACTION ALL IND NORM WITH GEAR HANDLE UP POSITION. WHEN GEAR HANDLE OFF, DOOR IND UNSAFE WITH RED DOOR LIGHTS. ACCOMPLISHED RED TAB PROC, LIGHT EXTINGUISHED WHEN GEAR HANDLE WAS IN UP POS. *S/D* REMOVED CANNON PLUG TO SWITCH, REMOVED FOREIGN OBJOct 9, 1999 · N233FE · Boeing 727247 · Landing Gear Retraction/Extension SystemSDR DL72W992594Skin · dentedINBOARD L/E DENTED AND WORN. REPAIRED ON SHOP ORDER 927514 PER M/M 57-52-0 FIG 803 {FLAP SHOP}.Oct 8, 1999 · N2815W · Boeing 727247 · Trailing Edge FlapsSDR DL72W992359Insulation · damagedON HUSH KIT MOD FOUND NUMEROUS LONGITUDINAL SPLITS ON INSULATION OF ALL 3 GEN FEEDER CABLES IN MID PYLON AREA. REPLACED CABLES FROM SPLICES IN RT 48 SEC TO FIREWALL DISCONNECT WITH NEW TYPE CABLES BMS 13-58 DL (P/N 012210733) PER BOEING SERVICE LETTER 727-SLOct 7, 1999 · N2814W · Boeing 727247 · Electrical Power System WiringSDR DL72W992358Insulation · damagedON HUSH KIT MOD, FOUND NUMEROUS LONGITUDINAL SPLITS ON INSULATION OF ALL 3 GEN FEEDER CABLES IN MID PYLON AREA. REPLACED CABLES FROM SPLICES IN LT 48 SEC TO FIREWALL DISCONNECT WITH NEW TYPE CABLES BMS 13-58 DL (P/N 012210733) PER BOEING SERVICE LETTER 727-SLOct 7, 1999 · N2814W · Boeing 727247 · Electrical Power System WiringSDR DL72E992202Spar · misdrilledONE FASTENER HOLE WAS MISDRILLED AND ELONGATED IN THE WING CENTER SECTION REAR SPAR WEB AT APPROXIMATELY LBL 41 DURING THE ACCOMPLISHMENT OF A MODIFICATION TO THE WEB. THE DAMAGE WAS FOUND AT HMV AND REPAIRED PER ERA 333636-14AD.Oct 4, 1999 · N282WA · Boeing 727247 · Wing SparSDR DL72E992201Skin · corrodedTHE WING CENTER SECTION LOWER SKIN WAS FOUND CORRODED AT FS 820 AND RBL 13. THE DAMAGE WAS REPAIRED PER ERA 333611-14ADAT HMV.Oct 4, 1999 · N282WA · Boeing 727247 · Wing, Plate/SkinSDR DL72E992200Skin · crackedCRACK INDICATIONS WERE FOUND IN THE FUSELAGE SKIN LAP AT STRINGER 4L BETWEEN FS 360 AND FS 481. THE DAMAGE WAS REPAIRED PER ERA 333599-14AD AT HMV.Oct 4, 1999 · N282WA · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72E992199Doubler · tornTHE AFT LAV SERVICE PANEL DOUBLER WAS FOUND TORN DURING MODIFICATION PER EO 4-69078-3AD. THE DAMAGE WAS REPAIRED PER ERA 333642-14 AT HMV.Oct 4, 1999 · N282WA · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72E992198Frame · crackedTHE LT FS 783.95 OVERWING EXIT FRAME WAS FOUND CRACKED AT HMV. THE DAMAGE WAS REPAIRED PER ERA 333610-14AD.Oct 4, 1999 · N282WA · Boeing 727247 · Fuselage Main, FrameSDR DL72W992196Smoke Detector · defectiveLAV SMOKE LIGHT ILLUMINATED IN FLIGHT. TWICE AT AFT LAVS. WENT OUT ON OWN FIRST TIME. HAD TO PULL CB 2ND TIME. REPLACED AFT RT LAV SMOKE DETECTOR.Oct 3, 1999 · N293WA · Boeing 727247 · Smoke DetectionSDR UPS99230817Stringer · corrodedINSPECTION TYPE:C CORROSION STR 26R CORRODED BS 720F PLUS 16 740-4. REPAIRED STR 26R SRM 53-10-3, SPLICED IN NEW SECTION FROM BS 720F PLUS 5 TO BS 720F PLUS 16, AFTER BLENDING CORROSION OUT OF LIMITS.Sep 30, 1999 · N212UP · Boeing 727247 · Fuselage Main, Longeron/StringerSDR UPS99230816Stringer · corrodedINSPECTION TYPE:C CORROSION ON KEEL BEAM STRINGER 29L BS 950E PLUS 12 TO 950E PLUS 15 LBL 7 WL 138 (C53-113-01.06-02). REPAIRED PER ER NR 99-6148 AND 727 SRM.Sep 30, 1999 · N212UP · Boeing 727247 · Fuselage Main, Longeron/StringerSDR UPS99230819Seat Track · corrodedINSPECTION TYPE:C WHILE WORKING CARD 006467 UPON REMOVAL OF FLOOR PANEL BS 870-950, RBL 45-RBL 65, FOUND SEAT TRACK AT BS 900, RBL 47, WL 208 OUTBOARD FLANGE CORRODED. REMOVED AND REPLACED CORRODED SEAT TRACK IAW 51-30-02.Sep 29, 1999 · N212UP · Boeing 727247 · Fuselage, Seat/Cargo Attach FittingsSDR UPS99230818Clip · corrodedINSPECTION TYPE:C FWD CARGO COMPARTMENT STR CLIP BS 720F, STR 27R, RBL 15 IS CORRODED. REMOVED AND REPLACED CORRODED STR CLIP BS 720F STR 27R, RBL 15 IAW 51-30-02, 51-30-05.Sep 29, 1999 · N212UP · Boeing 727247 · Fuselage Miscellaneous Structure
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