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 DL72W990617Coupling · failedDURING APPROACH TO ATL, UPON SEL 5 DEG FLAPS THE OUTBOARD NEEDLES SPLIT AND REMAINED AT 2 DEG. FOUND LT OUTBOARD T/E FLAP DRIVE (TORQUE) TUBE COUPLING, FAILED JUST INBOARD OF LT MLG SPAR.Mar 23, 1999 · N296WA · Boeing 727247 · Trailing Edge Flap Control SystemSDR DL72W990612Web · crackedA .5 INCH CRACK TORQUE BOX VERT WEB FS 1213 RT SIDE. SEVERAL SMALL CRACKS LIGHTENING HOLE ON TORQUE BOX VERT WEB AT FS 1231 RT SIDE. REPAIRED PER MM 53-11-0 PG 833. ROUTED CRACKS PER MM 53-11-0 PG 828.Mar 22, 1999 · N293WA · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W990919Spar · crackedAFT SPAR CRACKED 22 FROM I/B END OF FLAP, THIS DAMAGED WAS REPAIRED PER MM 57-52-0 FIG 802 ON SHOP N/R 011630 LOCATED SHOP ORDER 709228.Mar 19, 1999 · N2820W · Boeing 727247 · Trailing Edge FlapsSDR DL72W990918Spar · damagedTEMP SPLICE AFT SPAR AT 57 AND 46 FROM I/B END OF FLAP. THIS DAMAGE WAS REPAIRED PER MM 57-52-0 FIG 802 ON SHOP N/R 011626, LISTED ON SHOP ORDER 709228.Mar 19, 1999 · N2820W · Boeing 727247 · Trailing Edge FlapsSDR DL72W990814Angle · crackedDURING SHOP INSPECTION, THE AFT LOWER CLOSEOUT SPAR ANGLE WAS FOUND CRACKED 2 PLACES 35 FROM IB END OF FLAP. A NEW SECTION OF SPAR ANGLE WAS DRILLED UP AND INSTALLED PER MM 57-52-01, FIG. 802.Mar 19, 1999 · N2820W · Boeing 727247 · Trailing Edge FlapsSDR DL72W990677Doubler · corrodedBONDED DOUBLER - CORRODED FS 72OB AND JUST BELOW STR 4R. REPAIRED PER SRM 53-30-4, METHOD 2, (H). WITHIN LIMITS PER SRM 53-30-4, METHOD 2 (H). OK TO T & P. TREATED PER SRM 53-30-4 METHOD 2 (J). PAINTED PER SRM 53-30-4 METHOD 2 STEP (K).Mar 19, 1999 · N2820W · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W990607Skin · corrodedTHE FUSELAGE SKIN WAS FOUND CORRODED AT THE FS 680 BUTT SPLICE BETWEEN STRINGER 28L AND 28R. AN EXISTING LOCAL REPAIR WAS REMOVED AT THIS LOCATION AND ALL CORROSION AREAS WERE CUT OUT OF THE SKIN WITH A 1 X 3 CUTOUT AND A 10 X 5 CUTOUT. BOTH CUTOUTS WERE REPMar 19, 1999 · N2821W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W990769Stringer · crackedSTR RT CRACKED INSIDE VERT STA AT B/H STA 133.8 LOC INSIDE VERT STAB. BEGAN FABRICATING REPAIR ANGLE. FABRICATED REPAIR ANGLES PER M/M 55-30-0 PG 803. OK TO INSTALL REPAIR. INSTALLED REPAIR PER M/M 55-30-0 PG 803.Mar 18, 1999 · N2820W · Boeing 727247 · Vertical StabilizerSDR DL72W990684Doubler · corrodedBONDED DOUBLER, CORRODED FS 500 STR 3R TO 3L. REPAIRED PER SRM 53-30-4, METHOD 2 (H). WITHIN LIMITS PER SRM 53-30-4, METHOD 2 (H). OK TO T & P. TREATED PER SRM 53-30-4 METHOD 2 (J). PAINTED PER SRM 53-30-4 METHOD 2 STEP (K).Mar 18, 1999 · N2820W · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W990683Doubler · corrodedBONDED DOUBLER, CORRODED FS 520 TO 540 FROM STR 4R TO 3L. REPAIRED PER SRM 53-30-4, METHOD 2 (H). WITHIN LIMITS PER SRM 53-30-4 METHOD 2, (H). OK TO T & P. TREATED PER SRM 53-30-4 METHOD 2 (J). PAINTED PER SRM 53-30-4 METHOD 2 STEP (K).Mar 18, 1999 · N2820W · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W990682Doubler · corrodedDOUBLER CORRODED FS 560 TO 580 STR 1-2R. REPAIRED PER SRM 53-30-4, METHOD 2, H. WITHIN LIMITS PER SRM 53-30-4, METHOD 2 (H). OK TO T & P. TREATED PER SRM 53-30-4 METHOD 2 (J). PAINTED PER SRM 53-30-4 METHOD 2 STEP (K).Mar 18, 1999 · N2820W · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W990681Doubler · corrodedBONDED DOUBLER, CORRODED FS 560 STR 4L TO 3L. REPAIRED PER SRM 53-30-4, METHOD 2 (H). WITHIN LIMITS PER SRM 53-30-4 METHOD 2, (H). OK TO T & P. TREATED PER SRM 53-30-4 METHOD 2 (J). PAINTED PER SRM 53-30-4 METHOD 2 STEP (K).Mar 18, 1999 · N2820W · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W990680Doubler · corrodedBONDED DOUBLER, CORRODED FS 580 FROM STR 4L TO 4R. REPAIRED PER SRM 53-30-4, METHOD 2 (H). WITHIN LIMITS PER SRM 53-30-4 METHOD 2 (H). OK TO T & P. TREATED PER SRM 53-30-4 METHOD 2 (J). PAINTED PER SRM 53-30-4 METHOD 2 STEP (K).Mar 18, 1999 · N2820W · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W990679Doubler · corrodedBONDED DOUBLERS, CORRODED FS 600 TO 620 AT STR 4R O/B SIDE OF STR AND SPLICE CORRODED ON I/B SIDE OF STR 22. REPAIRED PER SRM 53-30-4, METHOD 2, (H). WITHIN LIMITS PER SRM 53-30-4 METHOD 2, H. OK TO T & P. TREATED PER SRM 53-30-4 METHOD 2 (J). PAINTED PER Mar 18, 1999 · N2820W · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W990678Doubler · corrodedBONDED DOUBLER, CORRODED FS 620 FROM STR 1R TO 4L. REPAIRED PER SRM 53-30-4, METHOD 2, (4). WITHIN LIMITS PER SRM 53-30-4, METHOD 2 (H). OK TO T & P. TREATED PER SRM 53-30-4 METHOD 2 (J). PAINTED PER SRM 53-30-4 METHOD 2 STEP (K).Mar 18, 1999 · N2820W · Boeing 727247 · Fuselage Miscellaneous StructureSDR 99ZZZM345Wire · shortedTHE NR 3 AND NR 4 MAIN TIRES BLEW ON LANDING. REMOVED AND REPLACED TIRES AND BRAKES. FOUND PROBLEM IN THE WIRING TO THE ANTI-SKID CONTROL BOX. WIRES 034 AND 025 AT CONNECTOR 4656P WERE FOUND EXPOSED AND SHORTED TO GROUND. WIRES WERE RE-SPLICE AND TESTED GOMar 18, 1999 · N784AT · Boeing 727247 · Brake Anti-Skid SectionSDR DL72W990543Skin · crackedLFEC INSPECTION OF THE STRINGER 26R SKIN LAP SPLICE BETWEEN FS 360 AND 681 REVEALED A CRACK IN THE LOWER FASTENER ROW OF THE LOWER SKIN. HFEC INSPECTION CONFIRMED TWO CRACKS/CORROSION AT FS 505. THE SKIN WAS CUTOUT WITH A 2 X 1 CUTOUT IN THE LAPMar 12, 1999 · N2811W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W990530Coalescer · dirtySTRONG BURNING SMELL IN CABIN NEAR OVERWING EXITS WHEN MAIN SUPPLY TEMP EXCEEDS 80 DEGREES F. ISOLATED PACKS WITH APU AND ALL ENG BLEED SOURCES. RAN SUPPLY TEMP TO 130 DEGREES F WITH EVERY COMBINATION POSSIBLE. NO SMELLS OF ANY KIND. REPLACED BOTH WATER SEMar 12, 1999 · N2817W · Boeing 727247 · Humidity Control SystemSDR DL72W990517Air Distribution · odorSTRONG BURNING SMELL IN MID CABIN NEAR OVERWING EXITS. CKD APU FOR SIGNS OF OIL LEAKS, NONE FOUND. CHECKED OPR OF PACKS AND PACK FANS, NORMAL. RAN PACKS NO ABNORMAL ODORS NOTED IN CABIN.Mar 12, 1999 · N2817W · Boeing 727247 · Air Distribution SystemSDR DL72E990536Battery · shortedEMERGENCY EXIT LIGHTS ILLUMINATE WHEN ARMED SEAT 1 TO 26. FOUND LIGHTS ILLUM INTERMITTENTLY. ISOLATED PROBLEM TO RT CONTROL SYSTEM, FOUND POWER AT PIN 4 AT FWD BATTERY PACK. INSPECTED WIRE BUNDLE IN CEILING, AT ALL BATTERY PACKS. FOUND AFT AIRSTAIR LIGHT AMar 12, 1999 · N2829W · Boeing 727247 · Emergency LightingSDR DL72E990513Power Supply · inoperativeEMERGENCY EXIT LIGHTS ILLUMINATED IN FLIGHT, CHECKED COCKPIT SWITCH. REPLACED AFT EMERGENCY LIGHTS POWER SUPPLY.Mar 11, 1999 · N2829W · Boeing 727247 · Emergency LightingSDR DL72W990511Bulb · failed2L EMERGENCY EXIT SIGN INOP. RELAMPED EXIT SIGN, OPS CK NORMAL.Mar 10, 1999 · N2814W · Boeing 727247 · Emergency LightingSDR DL72W990498Angle · corrodedON HUSH-KIT MOD FOUND RT NR 2 ENG AFT MOUNT CHORD ANGLE CORRODED BEYOND MFG LIMITS. REPLACED CHORD ANGLE WITH PART OF NEW MFG.Mar 10, 1999 · N2815W · Boeing 727247 · Engine Mount SectionSDR DL72E990502Power Supply · inopALL EMER LIGHTS TURN ON AND OFF WITHOUT CONTROL SWITCH TURNED ON. REPLACED EMERGENCY LIGHT POWER SUPPLY.Mar 10, 1999 · N2829W · Boeing 727247 · Emergency LightingSDR DL72E990499Power Supply · inopEMERGENCY EXIT LIGHTING FLICKERED ON AND OFF DURING FLIGHT. REPLACED F/C EMER LIGHT POWER SUPPLY AND BATTERY TEST OK.Mar 10, 1999 · N2829W · Boeing 727247 · Emergency LightingSDR DL72W990583Stringer · crackedA .25 INCH VISIBLE CRACK AT UPPER STRINGER 10 AT WS 629 AT ATTACH BOLT. REPAIRED PER MM 57-13-0.Mar 9, 1999 · N2821W · Boeing 727247 · Wing, Longeron/StringerSDR DL72W990582Stringer · crackedA .25 INCH VISIBLE CRACK AT UPPER STRINGER 10 AT WS 656.5 AT ATTACH BOLT. REPAIRED PER MM 57-13-0.Mar 9, 1999 · N2821W · Boeing 727247 · Wing, Longeron/StringerSDR DL72W990581Stringer · crackedA .25 INCH VISIBLE CRACK AT UPPER STRINGER 10 AT WS 686.5 AT ATTACH BOLT. REPAIRED PER MM 57-13-0.Mar 9, 1999 · N2821W · Boeing 727247 · Wing, Longeron/StringerSDR DL72W990496Angle · corrodedON HUSH-KIT MOD FOUND LT NR 2 ENGINE AFT MOUNT CHORD ANGLE CORRODED BEYOND MFG LIMITS. REMOVED CHORD ANGLE AND REPLACED WITH NEW MFG PART.Mar 9, 1999 · N2815W · Boeing 727247 · Engine Mount SectionSDR DL72W990585Insulation · crackedDURING HUSH-KIT MOD FOUND INSULATION CRACKED ON GEN FEEDER CABLES IN PYLON ON NR 3 ENGINE. SPLICED IN NEW CABLE (P/N 0122107330) FROM SPLICES IN 48 SECTION TO FIREWALL DISCONNECT.Mar 4, 1999 · N2815W · Boeing 727247 · Electrical Power System WiringSDR DL72W990476Angle · crackedCRACK ORIGINATING UNDER I/B UPSTOP PAD ON NR 7 SLAT ANGLE RUNNING I/B .25 INCH. REPAIRED PER MM 57-40-0 PAGE 816.Mar 1, 1999 · N2821W · Boeing 727247 · Wing Miscellaneous StructureSDR DL72W990421Web · damagedWHILE ACCOMPLISHING THE CENTER WING REAR SPAR WEB MOD PER BAC S/B 57A0182, SEVERAL FASTENER HOLE LOCATIONS WERE DAMAGED. THE MODIFICATION DOUBLERS AND FILLERS WERE EXTENDED TO REPAIR THE EXTRA DAMAGE PER ER/A 366706-14AD.Feb 27, 1999 · N294WA · Boeing 727247 · Wing SparSDR DL72W990395Actuator · leakingLOST MAJORITY OF A SYS HYD FLUID WITH SYS A HYD PUMPS OFF. LEAK/LOSS STOPPED AT 1/2 GAL ON INDICATOR. FOUND NR 2 L/E FLAP ACTUATOR LEAKING. REPLACED ACTUATOR, LEAK CHKS NORMAL.Feb 25, 1999 · N2820W · Boeing 727247 · Leading Edge Slat ActuatorSDR DL72W990390Actuator · failedNR 4 SLAT DID NOT RETRACT. C/W POM. VISUALLY CONFIRMED. REPLACED NR 4 SLAT ACTUATOR.Feb 25, 1999 · N296WA · Boeing 727247 · Leading Edge Slat ActuatorSDR DL72W990321Light · inopF/O MAP LIGHT SMOKED AND FUMED. REPLACED LIGHT ASSY.Feb 17, 1999 · N2815W · Boeing 727247 · Flight Compartment LightingSDR DL72W990320Skin · crackedFUSELAGE SKIN FS 681-740 STRINGER 4R, SKIN LAP SPLICE, REPAIR FOR CRACKS. LFEC INSPECTION OF THE STRINGER 4R LAP SPLICE BETWEEN FS 681 AND 740. INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL. INTERNAL HFEC INSPECTION CONFIRMED 15 CRACKS Feb 17, 1999 · N2819W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W990319Skin · crackedFUSELAGE SKIN FS 481-680 STRINGER 4R SKIN LAP SPLICE, REPAIR FOR CRACKS. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 481 AND 680 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL. INTERNAL HFEC INSPECTION CONFIRMED 23 CRACKFeb 17, 1999 · N2819W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W990315Actuator · leakingINFLIGHT 'A' SYS HYD QTY DECREASED TO NEAR ZERO, ACCOMPLISHED PROD IAW POM. REPLACED INBOARD KRUEGER FLAP ACTUATOR.Feb 17, 1999 · N292WA · Boeing 727247 · Leading Edge Slat ActuatorSDR DL72W990307Clacker · failedATB - ELECT SMELL FROM RT SIDE OF COCKPIT. REPLACED OVERSPEED CLACKER.Feb 16, 1999 · N2815W · Boeing 727247 · Central WarningSDR DL72E990306Skin · puncturedFUSELAGE SKIN FS 520-540, STRINGER 25L-26L, REPAIR FOR PUNCTURE. THE FUSELAGE SKIN BETWEEN FS 520 AND 540 AND BETWEEN STRINGERS 25L AND 26L WAS PUNCTURED. THE DAMAGED SKIN WAS CLEANED UP WITH A 9 BY 5 CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMIFeb 14, 1999 · N282WA · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W990285Battery Pack · dischargedREAR AISLE EMERGENCY EXIT SIGN BATTERY WEAK. REPLACED BATTERY PACK.Feb 12, 1999 · N2819W · Boeing 727247 · Emergency LightingSDR UPS99228684Compressor · stalledCOMPRESSOR STALL PASSING FL270. MAX TEMP 620 DEGREES. ALL OTHER LIMITS NORMAL. DID SHUT DOWN OF NR 3 ENGINE. REMOVED AND REPLACED THE NR 3 ENGINE.Feb 10, 1999 · N208UP · Boeing 727247 · Turbine Engine Compressor SectionSDR DL72W990276Skin · crackedFUSELAGE SKIN FS 548, STRG 4R SKIN LAP SPLICE, CRACK REPAIR. EXTERNAL LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SHOWED A CRACK INDICATION AT FS 548. INTERNAL HFEC INSPECTION OF THE ENTIRE PANEL LENGTH CONFIRMED ONLY ONE CRACK AT FS 548 ALONG THE LOWER FASFeb 10, 1999 · N2807W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W990246Sill · corrodedTHE OUTER CHORD OF THE C-2 DOOR SURROUND LOWER SILL WAS FOUND WITH CORROSION ON THE OUTER FLANGE BETWEEN THE DOOR FRAME JAMBS. THE CORRODED AREAS WERE TRIMMED OUT AND TWO STEEL REPAIR ANGLES WERE INSTALLED TO REPAIR THE CUTOUTS. THE REPAIR WAS ACCOMPLISHEDFeb 4, 1999 · N2814W · Boeing 727247 · Fuselage Miscellaneous StructureSDR UPS99228620Fire Light · malfunctionedINSPECTION TYPE-N/A, BLOCK TURN BACK DUE TO APU FIRE LIGHT ON INDICATION. PULLED THE SWITCH AND PRESS THE DISCHARGE BUTTON. DEFERRED APU PER MEL 49-1 AND DEFERRED FIRE WARNING SYSTEM PER MEL 26-11-0-2.Feb 3, 1999 · N211UP · Boeing 727247 · Fire DetectionSDR DL72W990218Skin · crackedFOUND DURING MV1 CORROSION VISIT NRC 126 ON OK TO INSTALL L-4 WINDOW, FOUND .375 INCH CRACK IN FUSELAGE SKIN AT BOTTOM I/B BOLT HOLE. REPAIRED PER SRM 53-30-3 FIG 8.Feb 2, 1999 · N2814W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W990822Spar · crackedREAR SPAR CRACKED 19 AND 37 FROM I/B END. REPAIRED PER M/M 57-52-0.Jan 22, 1999 · N2820W · Boeing 727247 · Trailing Edge FlapsSDR DL72W990156Sign · missingRT FWD OVERWING EXIT SIGN MISSING. REPLACED RT FWD OVERWING EXIT SIGN, OP CKS OK.Jan 22, 1999 · N2816W · Boeing 727247 · Emergency LightingSDR DL72W990139Engine · failedNR 2 ENGINE OIL PRESSURE INDICATION WENT TO 100 PSI. ON ENGINE SHUTDOWN, INDICATION WENT TO 60 PSI. ALL OTHER ENGINE INDICATIONS NORMAL WHEN ENGINE RUNNING. SHUTDOWN ENGINE PER POM, REPLACED ENGINE.Jan 22, 1999 · N2811W · Boeing 727247 · Engine (Turbine/Turboprop)SDR DL72W990134Bearing · rustedDURING TAXI CONTROL CK WAS NORMAL, AFTER T/O AILERONS WERE VERY HEAVY AND ABRUPT MOVEMENT CAUSED WHAT FELT LIKE MANUAL REVERSION. GROUND CHECKS AFTER LANDING SHOWS HEAVIER THAN NORMAL. FAST INPUT STILL SHOWS TENDENCY TO LOCK UP. REPLACED AILERON CENTERING SJan 21, 1999 · N291WA · Boeing 727247 · Aileron Control System
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