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 UPS98228167Battery · dischargedINSPECTION TYPE-N/A, PREFLIGHT COCKPIT EMER EXIT LIGHT CAME OUT OF ASSEMBLY ABOVE DOOR. INSTALLED NEW BATTS AND REPLACED ASSEMBLY, OPS CHECK OK.Nov 13, 1998 · N208UP · Boeing 727247 · Emergency LightingSDR DL72W982338Battery Pack · dischargedON S/C, FOUND RT OVERWING EMER LIGHT INOP. FOUND BATT PACK INOP. REPLACED SAME.Nov 13, 1998 · N2820W · Boeing 727247 · Emergency LightingSDR DL72E982337Angle · crackedNR 2 SLAT LWR COVE SKIN ATTACH ANGLE CRACKED AT I/B STOP PAD. REPAIRED PER M/M 57-54-0 PG 816.Nov 12, 1998 · N831WA · Boeing 727247 · Leading Edge DevicesSDR DL72E982336Chord · crackedFOUND ON F2 LETTER CK, 1 INCH CRACK IN STA 1342 CHORD ABOVE THE NUMBER 2 ENGINE S-DUCT. STOP DRILLED CRACK PER MM 53-11-0.Nov 12, 1998 · N831WA · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W982343Strap · crackedTHE R2 DOOR SURROUND BEAR STRAP WAS FOUND WITH A TYPICAL CRACK AT THE UPPER HINGE CUTOUT. THE CRACK WAS APPROX 2 INCHES LONG AND CONFINED TO THE BEAR STRAP ONLY. THE CRACK WAS REPAIRED WITH AN EXTERNAL DOUBLER PER BAC S/B 727-53-0136 & DOCUMENTED PER ER/ANov 11, 1998 · N2819W · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W982435Floorbeam · corrosionFOUND DURING MV2 CORROSION VISIT NRC 16, CORROSION ON FLOORBEAM STA 344 BETWEEN RBL 13 AND RBL 25. REPAIRED PER SRM 53-10-8 FIG 11.Nov 6, 1998 · N2819W · Boeing 727247 · Fuselage Main, Floor BeamSDR DL72W982335Floorbeam · corrodedFOUND DURING MV2 CORROSION VISIT NRC 81, CORROSION ON FLOORBEAM STA 1050 AT RBL 33. REPAIRED PER M/M 53-20-11 FIG 804A RBL 33 TO RBL 19.Nov 6, 1998 · N2819W · Boeing 727247 · Fuselage Main, Floor BeamSDR DL72W982334Frame · crackedA .5 INCH VISIBLE CRACK AT AFT ENTRY DOOR CUTOUT LT FRAME AT 2ND FROM UPPER DOOR STOP. REPAIRED PER SRM 53-10-09.Nov 6, 1998 · N2819W · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W982254Battery Pack · dischargedON L/O, FOUND EMERGENCY EXIT LIGHT OVER DOOR L2 INOP. REPLACED BATTERY PACK, OPS CKS NORMAL.Nov 1, 1998 · N292WA · Boeing 727247 · Emergency LightingSDR DL72W982250Battery · dischargedEMERGENCY LIGHT BATTERY PACK INOP. REPLACED BATTERY PACK.Nov 1, 1998 · N2812W · Boeing 727247 · Emergency LightingSDR DL72W982347Angle · crackedDURING SHOP INSP, THE LOWER AFT CHORD ANGLE WAS FOUND CRACKED 33 AND 36.5 INCHES FROM I/B END OF FLAP. THE ANGLE WAS REPAIRED PER MM 57-52-0, FIG 802 BY INSTALLING A DOUBLER.Oct 22, 1998 · N2815W · Boeing 727247 · Trailing Edge FlapsSDR DL72W982181Light · inopCOCKPIT OVERHEAD EMERGENCY LIGHT PACK INOP ON TEST. REPLACED BATTERIES, CKS OK.Oct 21, 1998 · N2809W · Boeing 727247 · Emergency LightingSDR DL72W982173Support · crackedNR 1 LE FLAP ACT SUPPORT BOX CRACKED AT UPPER IB CORNER. REPAIRED PER MM 57-21-21.Oct 21, 1998 · N294WA · Boeing 727247 · Leading Edge Slat ActuatorSDR DL72W982165Web · corrodedCORROSION WAS FOUND ON THE UPPER HORIZ PRESSURE WEB DOUBLER OF THE NLG W/W FWD OF BS 315. THE DAMAGE NECESSITATED A NEW SECTION BE SPLICED IN. REPAIRED PER ERA 332271-14.Oct 19, 1998 · N2816W · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W982138Frame · crackedCRACK WAS FOUND IN THE AFT ENTRY DOORWAY LT FRAME AT WL 276.6. THE CRACK WAS 4.5 INCH LENGTH AND TYPICAL OF THAT FOUND IN SB 727-53-0055 REV 9. REPAIRED PER ERA 332362-14AD.Oct 14, 1998 · N2816W · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W982119Skin · crackedA FAILED FASTENER WAS FOUND IN THE UPPER ROW OF THE S26R SKIN LAP JOINT AT BS 684. CRACKS WERE FOUND EMANATING FROM THIS FASTENER HOLE IN THE OUTER SKIN ONLY. THE CRACKS WERE .125 AND .0937 LONG. REPAIRED PER ERA 332342-14.Oct 12, 1998 · N2816W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W982118Stringer · corrodedCORROSION WAS FOUND ON THE I/B FLANGE OF S3R AT FS 371 REQUIRING A SECTION OF STRINGER TO BE CUT OUT. REPAIRED PER ERA 332244-14.Oct 12, 1998 · N2816W · Boeing 727247 · Fuselage Main, Longeron/StringerSDR DL72W982110Light · illuminatedAFTER GEAR EXTENSION THE NOSE GEAR UNSAFE LIGHT ILLUMINATED WITH NO GREEN NOSE GEAR LIGHT. POM PROCEDURES COMPLIED WITH AND A SAFE INDICATION OBTAINED AFTER MANUAL EXTENSION PROCEDURES ACCOMPLISHED.Oct 11, 1998 · N2809W · Boeing 727247 · Landing Gear Position and WarningSDR 98FDEA00646Adc · failed98-246 ON CLIMB-OUT, LOST CAPT AIRSPEED CAPT ALT, GPWS, ALT ALERTER, TRANSPONDER NR 1, & MODE C IN BOTH TRANSPONDER & AUTOPILOT. REMOVED AND REPLACED DADC PER BOEING 727 MM CHAPTER 34-12-11. OPER CKS NORM. AUTOPILOT DOWNGRADED TO CK CAT 2 STATUS. A/C DOWNGOct 9, 1998 · N235FE · Boeing 727247 · Air Data ComputerSDR DL72W982079Angle · corrodedWHILE PERFORMING HUSH-KIT MOD, FOUND RT CHORD ANGLE ON NR 2 ENG SLOPING WEB CORRODED BEYOND MFG SPECS. REPLACED RT CHORD WITH NEW SCV CHORD.Oct 7, 1998 · N296WA · Boeing 727247 · Nacelle/Pylon StructureSDR DL72W982073Skin · corrodedFUSELAGE SKIN FS 720 S-28L-28R, REPAIR FOR SKIN CORROSION. THE FUSELAGE SKIN WAS FOUND CORRODED AT FS 720 BETWEEN STRINGERS 28L AND 28R, DURING ROUTINE INSPECTIONS PER AD 91-09-09. THE CORRODED AREA OF SKIN WAS CUTOUT AN REPAIRED WITH AN EXTERNAL ALUMINUM Oct 7, 1998 · N2813W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W982105Angle · crackedDURING SHOP INSPECTION, THE AFT LOWER CLOSEOUT ANGLE WAS FOUND CRACKED 33 FROM THE IB END OF FLAP. THE ANGLE WAS REPAIRED PER 727 MM 57-52-0,FIG. 802 BY INSTALLING A DOUBLER AND STOP DRILLING THE CRACK.Oct 6, 1998 · N2816W · Boeing 727247 · Trailing Edge FlapsSDR DL72W982064Stringer · corrodedCORROSION DAMAGE FOUND THAT EXCEEDED ALLOWABLE LIMITS, ON THE S1L, AT BS 375. REPAIRED PER ERA 332246-14.Oct 6, 1998 · N2816W · Boeing 727247 · Fuselage Main, Longeron/StringerSDR DL72W982078Angle · corrodedFOUND LT CHORD ANGLE ON NR 2 ENG SLOPING WEB WITH CORROSION BEYOND MFG SPECS. REPLACED CHORD ANGLE WITH NEW CHORD ANGLE.Oct 5, 1998 · N296WA · Boeing 727247 · Nacelle/Pylon StructureSDR DL72W981996Heat Valve · failedNR 3 ENGINE OIL TEMPERATURE ROSE TO YELLOW BAND RANGE. FOLLOWED POM PROCEDURES FOR HIGH OIL TEMPERATURE. SHUTDOWN NR 3 ENGINE ACCORDING TO CHECKLIST PROCEDURES. REPLACED NR 3 ENGINE FUEL HEAT VALVE. LEAK AND FUNCTION CHECKS OK. INSPECTED ENGINE FOR OIL TESep 27, 1998 · N294WA · Boeing 727247 · Fuel HeaterSDR DL72W981971Spar · crackedSPAR CRACKED AT ANTI-ICE DUCT CUTOUT. REPAIRED PER MM 57-54-0.Sep 24, 1998 · N2816W · Boeing 727247 · Leading Edge DevicesSDR 98FDEA00588Light · intermittentNR 0648 - COCKPIT EMERGENCY EXIT LIGHT INTERMITTENT. REMOVED AND REPLACED COCKPIT EMERGENCY EXIT LIGHT PER FEDEX M/M 33-50-101. EMERGENCY LIGHT TESTED GOOD PER FEDEX MM 33-50-101.Sep 24, 1998 · N233FE · Boeing 727247 · Emergency LightingSDR DL72W981953Skin · crackedA .25 INCH CRACK WAS FOUND IN THE SKIN AT THE UPPER HINGE CUTOUT FOR THE L1 DOOR. THE CRACK WAS REPAIRED PER BAC S/B 53-0198 EXCEPT COUNTERSUNK HI-LOKS WERE INSTALLED INSTEAD OF PROTRUDING HEAD HI-LOKS. THE REPAIR WAS DOCUMENTED PER ER/A365693-14.Sep 19, 1998 · N290WA · Boeing 727247 · Fuselage Main, Plate/SkinSDR 98FDEA00580Switch · dirtyRIGHT GEAR DOOR LIGHT REMAINED ON AFTER GEAR RETRACTION. RAN RED TABS AND RECYCLE GEAR, DOOR LIGHT EXTINGUISHED. CLEANED RIGHT GEAR DOOR LIGHT SWITCH. OPERATED SEVERAL TIMES, OPER CHECKED NORMAL.Sep 17, 1998 · N236FE · Boeing 727247 · Landing Gear Position and WarningSDR DL72W981920Web · crackedREF SHIP 588 TPA LTR CHECK B-2, .25 INCH CRACK AT LIGHTENING HOLE 8AFT OF LT AIRSTAIR UPSTOP PAD. ROUT OUT AND TREAT PER MM 53-11-0.Sep 15, 1998 · N296WA · Boeing 727247 · Fuselage Miscellaneous StructureSDR 98FDEA00575Stringer · corrodedCORROSION (C53-113-01,11) ON STR 27 RT AT BS 720B+10 FWD CARGO BAY. *S/D* REPAIRED STR 27 RT, BS 720 AT 14 TO 720B+12 PER FED-EX SRM 53-10-3 FIG 1.Sep 15, 1998 · N233FE · Boeing 727247 · Fuselage Main, Longeron/StringerSDR DL72W982217S-Duct · crackedAT HMV FOUND SKIN - BENT/CRACKED INSIDE S-DUCT APPROX 4FT FROM L/E OF INLET AT 12 O-CLOCK POSITION. CORR: MANUFACTURED REPAIR DBLR AND FILLER PER SRM 54-10-3 P.63 INSTLD PER SAME.Sep 14, 1998 · N2816W · Boeing 727247 · Nacelle/Pylon StructureSDR DL72W981904Actuator · failedAFTER T/O, LOST 'A' SYS HYD QTY AND PRESS IND ZERO. PROCEDURES COMPLIED WITH ALT FLAP SW USED GPWS INHIBITED. GEAR PIN INSTALLED BY MTC. REMOVED AND REPLACED NR 1 SLAT ACT. OPS AND LEAK CKS GOOD.Sep 13, 1998 · N2814W · Boeing 727247 · Leading Edge Slat ActuatorSDR DL72W982216Stringer · crackedAT HMV, FOUND RT WING OUTER W/UPR STRINGER 2 RIB AT WS 656.5 STRINGER 13 IS CRACKED AT FASTENER HOLE. REPAIR INFO IS REF ON OPN 8602AD ITEM 5. CUT OUT VENT STRINGER, DRILLED UP REPAIR ANGLES RADIUS FILLER COVER ASSY PER M/M 57-13-00. INSTALLED PER SAME.Sep 11, 1998 · N2816W · Boeing 727247 · Wing, Longeron/StringerSDR DL72W982213Stringer · crackedON HMV, RT WING OUTER UPPER STRINGER 2 RIB AT WS 656.5 STR 12 IS CRACKD AT FASTENER HOLE. CUT OUT VENT STRINGER, DRILLED UP REPAIR ANGLES RADUIS FILLERS CVR ASSY PER MM 57-13-00. INSTALLED REPAIR ANGLES.Sep 11, 1998 · N2816W · Boeing 727247 · Wing, Longeron/StringerSDR DL72W982210Guide · wornAT HMV, FOUND GUIDE ON NR 5 SLAT TRAILING EDGE O/B OF ACTUATOR WORN. WEAR LIMITS OK, REPAIRED PER M/M 27-81-11.Sep 10, 1998 · N2816W · Boeing 727247 · Leading Edge DevicesSDR DL72W982209Angle · crackedAT HMV, FOUND NR 5 SLAT ANGLES - ACTUATOR ATTACH POINT BOTH I/B AND O/B ANGLES CRACKED. STOP DRILLED CRACK PER M/M, FABD REPAIR DOUBLERS, INSTALLED PER MM 57-54-00 FIG 809.Sep 10, 1998 · N2816W · Boeing 727247 · Leading Edge DevicesSDR DL72W982197Angle · crackedDURING SHOP INSPECTION, THE AFT LOWER SPAR ANGLE WAS FOUND CRACKED 32 INCHES FROM I/B END OF FLAP. THE ANGLE WAS REPAIRED PER MM 57-52-0 FIG 802, BY STOP DRILLING THE CRACK AND INSTALLING A DOUBLER.Sep 10, 1998 · N2816W · Boeing 727247 · Trailing Edge FlapsSDR 98FDEA00563Chord · corrodedCORROSION LUMINATING FROM UNDER SEAT TRACK AT BS 760 TO 850, LBL 25, WL 208. *S/D* REMOVED AND REPLACED LONGITUDINAL BEAM UPPER CHORD, BS 760 TO 850, LBL 25, WL 208 IAW DWG 65-16279 AND FEDEX SRM 51-30-2.Sep 10, 1998 · N233FE · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W981982Rib · crackedI/B AFT RIB IS CRACKED AT AFT LWR CORNER. REPAIRED PER MM 57-52-0 FIG 808.Sep 9, 1998 · N2816W · Boeing 727247 · Trailing Edge FlapsSDR DL72W981884Skin · damageDURING REPLACEMENT OF BELLY SKIN, A FASTENER HOLE SUSTAINED TOOLING DAMAGE NEAR THE C-1 DOOR CUTOUT. REPAIR PER ERA 332149-14.Sep 9, 1998 · N2817W · Boeing 727247 · Fuselage Main, Plate/SkinSDR 98FDEA00555Frame · corrodedWHILE WORKING NR 0164, FOUND CORROSION ON BS 420 FRAME LBL 15 - RBL 15, WL 135-133. *S/D* REPAIRED FRAME AT BS 420, LBL 15-RBL 15, WL 135-133 PER FED-EX SRM 51-40-3.Sep 9, 1998 · N233FE · Boeing 727247 · Fuselage Main, FrameSDR 98FDEA00554Skin · crackedNR 0480, CRACK IN SKIN AT 351, LBL 22, WL 140 CIRCLED IN RED. REPAIRED CRACK IN SKIN AT BSA 351, LBL 22, WL 140 CIRCLED IN RED PER FEDEX SRM 51-10-1 AND PER 53-30-2. POURED LEVEL COMPOUND OVER INTERVAL PORTION OF FASTENERS PER FEDEX M/M 20-60-1.Sep 9, 1998 · N233FE · Boeing 727247 · Fuselage Main, Plate/SkinSDR 98FDEA00553Stringer · corrodedCORROSION ON STRINGER NR 27 RT, BS 484 FWD CARGO BAY.Sep 9, 1998 · N233FE · Boeing 727247 · Fuselage Main, Longeron/StringerSDR 98FDEA00552Frame · gougedDAMAGE TO THE TOP FLANGE OF THE BS 1050 FRAME AT LBL 20, WL 151. *S/D* REPAIRED DAMAGE TO THE TOP FLANGE OF THE BS 1050 FRAME AT LBL 20, WL 151 IAW FED-EX SRM 53-10-1.Sep 9, 1998 · N233FE · Boeing 727247 · Fuselage Main, FrameSDR 98FDEA00551Frame · corrodedCORROSION (C53-224-03-1/2) ON E & E BAY DOOR CUTOUT FWD FRAME. *S/D* REMOVED AND REPLACED E & E BAY DOOR CUTOUT FWD FRAME PER FED-EX SRM 51-30-2 AND FED-EX DRAWING 65-16351.Sep 9, 1998 · N233FE · Boeing 727247 · Fuselage Main, FrameSDR 98FDEA00547Wheel · missingON WALKAROUND, FOUND NR 1 TIRE MISSING FROM AXLE. *S/D* PERFORM VISUAL INSPECT OF LEFT MAIN GEAR, NO DEFECT NOTED. REPLACED LEFT O/B AXLE SLEEVE ASSY PER BOEING OVERHAUL MAN 32-12-01. PER HARD LAND INSP PHASE 1 PER M/M 51-51-61. REMOVED AND REPLACED NR 1 Sep 9, 1998 · N234FE · Boeing 727247 · Wheel/Ski/FloatSDR UPS98227661Seat Track · crackedINSPECTION TYPE:C SEAT TRACK CRACKED BS 514 AND ELONGATED TEETH AT BS 526, RBL 25 WL 208. REPLACED SEAT TRACK BS 480 TO 530 PER SRM 53-10-5.Sep 8, 1998 · N208UP · Boeing 727247 · Fuselage, Seat/Cargo Attach FittingsSDR UPS98227662Web · corrodedINSPECTION TYPE:C WHILE WORKING TC NO CL2-224-03 DISCOVERED CORROSION AT BS 720E TO 725F LBL 65-70 WL 208. REMOVED, FABRICATED AND INSTALLED NEW SHEAR WEB IAW SRM 51-20-01, 51-30-05, 51-30-07, MM 51-20-151.Sep 7, 1998 · N208UP · Boeing 727247 · Fuselage Miscellaneous StructureSDR UPS98227617Skin · corrodedINSPECTION TYPE-N/A, CORROSION SKIN APPROX STA 1050 STR 27L, BULGE AND SEVERAL POPPED FASTENERS. TRANSFERRED TO NON-ROUTINE TALK SHEET AND NON ROUTINE NR 544152. REPAIRED PER SRM 53-10-3.Sep 4, 1998 · N209UP · Boeing 727247 · Fuselage Main, Plate/Skin
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