Boeing 727-227

Service difficulty reports · 5,082

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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 = '727227'
  ORDER BY difficulty_date DESC"

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SDR TAOA039611Brake Assy · out of adjustUPON LANDING, LGA TOWER REPORTED BRAKE SMOKING. FOUND NR 4 BRAKE HAD BEEN CHANGED ON THE OVERNIGHT SERVICE. CHECKED BRAKES PER MM 32-40 - CHECKED GOOD. (X)Mar 13, 1996 · N925TS · Boeing 727227 · Landing Gear Brake SystemSDR CAL960533Angle · corrosionDURING INSPECTION, FOUND CORROSION AT BS 1130 WEB BETWEEN STRINGER 30 AND STRINGER 29R. REMOVED CORROSION AND CORRODED REINFORCEMENT ANGLE FABRICATED REPAIR ANGLE FOR WEB AND REINFORCEMENT ANGLE SRM 51-10-6 AND B727 MM 51-20-11 AND INSTALLED PER SRM 51-30-2. Mar 12, 1996 · N15774 · Boeing 727227 · Fuselage Miscellaneous StructureSDR AALA960390Connector · brokenMIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS IN AFT CABIN BETWEEN AFT GALLEY AND AFT ENTRY DOOR INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT STRIP CONNECTOR AT AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)Mar 12, 1996 · N729AA · Boeing 727227 · Emergency LightingSDR 96ZZZM888Light · inoperativeIND - EMERGENCY LIGHT ABOVE R1 DOOR INOP. REPLACED LIGHT ASSEMBLY, OPS CHECK GOOD. (M)Mar 8, 1996 · N778AT · Boeing 727227 · Emergency LightingSDR 96FDEA00642Spar Chord · crackedWS 304 RT WING 3RD STRINGER AFT OF FWD UPPER STAR CHORD CRACKED. REPAIRED STRINGER AT WS 304, 3RD FROM TOP FRONT SPAR CHORD. REPAIRED PER SRM 57-10-4.Mar 8, 1996 · N119FE · Boeing 727227 · Wing SparSDR CAL960285Brake · inoperativeTPA - FLT 0437 - THE NR 4 MLG TIRE BLEW OUT ON LANDING AT TPA. THE LANDING WAS OTHERWISE ROUTINE WITH NO OTHER PROBLEMS. MAINTENANCE FOUND THE NR 4 BRAKE LOCKED. THE NR 4 BRAKE, TIRE AND WHEEL ASSMBLY WERE REMOVED AND REPLACED. IN ADDITION, THE NR 3 TIRE AMar 7, 1996 · N76752 · Boeing 727227 · BrakeSDR AALA960367Skin · corrodedTUL - BULGES IN SKIN ALONG STR 27L, BETWEEN STA 660 - STA 680. REPAIRED CORRODED SKIN AND STRINGER PER SRM 53-10-3, FIGURE 1, AND SRM 53-30-3, FIGURE 3. TST: 63,275 HRS. CYCLES: 44,950. (X)Mar 7, 1996 · N729AA · Boeing 727227 · Fuselage Main, Plate/SkinSDR AALA960366Skin · corrodedTUL - CORROSION THROUGH SKIN AT STA 490 BETWEEN STR 27L - STR 28L. REPAIRED AREA PER SRM 53-30-3. TST: 63,275. CYCLES: 44,950. (X)Mar 7, 1996 · N729AA · Boeing 727227 · Fuselage Main, Plate/SkinSDR AALA960365Skin · corrodedTUL - BULGE IN SKIN BETWEEN STA 680 TO STA 700 OR STR 27R. CORRODED PORTION OF SKIN REMOVED AND CORRODED PORTION. REPAIRED STRINGER PER SRM 53-10-3. REPAIRED FUSELAGE PER 53-30-3. TST: 63,275 HRS. CYCLES: 44,950. (X)Mar 7, 1996 · N729AA · Boeing 727227 · Fuselage Main, Plate/SkinSDR AALA960364Skin · crackedTUL - CRACK IN FUSELAGE SKIN AT STA 243 AND STR 222. CUT OUT CRACKED AREA AND INSTALLED DOUBLER PER SRM 53-30-3, PAGES 5-8. TST: 62,953 HRS. CYCLES 41,211. (X)Mar 7, 1996 · N727AA · Boeing 727227 · Fuselage Main, Plate/SkinSDR AALA960363Frame · crackedTUL - CRACK IN FRAME WEB, STA 825.95, LT STR 16 CUT-OUT. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 51-40-2, PAGES 1-8, AND SRM 51-40, PAGE 1. TST: 62,953 HRS. CYCLES: 41,811. (X)Mar 7, 1996 · N727AA · Boeing 727227 · Fuselage Main, FrameSDR 96FDEA00641Rib Chord · crackedLEFT 760 RIB CHORD AT BL 70.5, TOP FWD HOLE IND CRACK. ENLARGED TOP FWD HOLE. INSTALLED REPAIR PER DRAWING 65-68492-17, ESO 11782, DATED 2-24-96 AND EA.Mar 5, 1996 · N491FE · Boeing 727227 · Wing, Rib/BulkheadSDR 96ZZZM887Battery · dischargedIND - AFT AIRSTAIR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY, OPS CHECK NORMAL. (M)Mar 4, 1996 · N778AT · Boeing 727227 · Emergency LightingSDR 96FDEA00392Skin · corrodedLOWER FWD CARGO COMPT FUSE SKIN CORRODED STA 723 BETWEEN STR 28 LT AND RT. REMOVED CORROSION, SKIN THICKNESS BEYOND LIMITS. CUT OUT DAMAGE AND INSTALLED DOUBLER PER SRM 53-30-3.Feb 29, 1996 · N491FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR 96FDEA00391Rib Chord · crackedRT 760 RIB CHORD AT BL 70.5 TOP FWD HOLE IS CRACKED. ENLARGED TOP FWD HOLE TO REMOVE CRACK, HOLE ENLARGED TO .5 INCH DIA. CRACK REMOVED, INSTALLED 7075-T6 FREEZE PLUG PER SRM 51-10-7. INSTALLED SECOND OVERSIZED HI-LOK AT PLUG LOCATIONS PER ESO 11782.Feb 29, 1996 · N491FE · Boeing 727227 · Fuselage Miscellaneous StructureSDR 96FDEA00390Angle · corrodedFLOOR PLATE BULGING 36 FWD OF FLIGHT DECK ENTRY DOOR AT BL 0. REPLACED CORRODED CHORD ANGLE FROM LBL 6 TO RBL 18 PER SRM 51-40-4.Feb 29, 1996 · N491FE · Boeing 727227 · Fuselage Miscellaneous StructureSDR SCNA96028Batteries · dischargedTHE AFT AIRSTAIR EMERGENCY LIGHT WAS FOUND TO BE DIM. REPLACED BATTERIES IN LIGHT AND UNIT TESTED GOOD.Feb 28, 1996 · N275AF · Boeing 727227 · Emergency LightingSDR 96FDEA00389Stringer · corrosionCORROSION LT SIDE OF STR 28L STA 1040 TO 1050 IN AFT CARGO. CORROSION REMOVED, DAMAGE BEYOND MM LIMITS. REMOVED DAMAGED MATERIAL, INSTALLED DOUBLER AND STR REPAIR PER SRM 53-10-3.Feb 27, 1996 · N491FE · Boeing 727227 · Fuselage Main, Longeron/StringerSDR CAL960202Bus Protect Pnl · inoperativeFLT NR 1957 - IAH - ALL THREE BUS TIE BREAKERS TRIPPED AND THE SECOND OFFICERS FAULT ANNUNCIATOR INDICATED A PHASE UNBALANCE WHILE EN ROUTE TO IAH. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE BUS PROTECTION PANEL AT FAULT. THE BUS PROTECTIONFeb 26, 1996 · N73751 · Boeing 727227 · AC Power Distribution SystemSDR 96FDEA00388Skin · corrodedLOWER FWD CARGO COMPT FUSE BELLY SKIN CORRODED AT STA 683 O/B OF STR 28L. CUT OUT DAMAGED SECTION OF SKIN. INSTALLED REPAIR DOUBLER PER SRM 53-30-3 FIG 3A SHEET 3A.Feb 26, 1996 · N491FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR 96FDEA00387Flange · corrodedCORROSION ON O/B FLANGE OF STR 29R AFT SIDE STA 950E. CUT OUT DAMAGED AREA AND INSTALLED STR SPLICE AND SKIN DOUBLER PER ESO 11782 DATED 2-21-96, AUTHORIZED BY FEDEX EA 7-5310-27736 DATED 2-29-96.Feb 23, 1996 · N491FE · Boeing 727227 · Fuselage Miscellaneous StructureSDR AALA960279Stringer · corrodedTUL - LIGHT CORROSION ON STR 26L, STA 684. CUT OUT DAMAGED (CORRODED) SECTION OF STRINGER. INSTALLED NEW JOGGLED SECTION UNDER BELT FRAME AND INSTALLED SPLICES ON BOTH ENDS PER STRINGER SPLICE REPAIR SRM 53-10-3, PAGES 3-4B. TST: 62,862 HRS. CYCLES, 43,0Feb 21, 1996 · N721AA · Boeing 727227 · Fuselage Main, Longeron/StringerSDR 96FDEA00386Frame · bentFWD LOWER CARGO COMPT STA 720 FRAME BENT BETWEEN STR 23 TO 24L. INSTALLED DOUBLER PER SRM 53-10-4.Feb 21, 1996 · N491FE · Boeing 727227 · Fuselage Main, FrameSDR AALA960270Skin · corrodedTUL - SMALL HOLE IN BELLY SKIN BELOW FORWARD CARGO AREA CAUSED BY CORROSION. CUT OUT CORROSION, REPLACED CUT OUT PER SRM 53-30-3, PAGES 14B, 14C, AND 14D. INSTALLED 2024-T3 0.071 DOUBLER. TST: 62,772 HRS. CYCLES, 41,734. (X)Feb 16, 1996 · N727AA · Boeing 727227 · Fuselage Main, Plate/SkinSDR 96FDEA00385Floor Beam · corrosionUPPER LOBE CORROSION ON FLOOR BEAM STA 360 TOP CHORD, AFT FLANGE, BOTTOM SIDE LBL 8. INSTALLED REPAIR PER SRM 53-10-2 FIG 3.Feb 16, 1996 · N491FE · Boeing 727227 · Fuselage Main, Floor BeamSDR TAOA029611Pulley · frozen brgON APPROACH TO LANDING, OUTBOARD FLAPS STOPPED AT 15 DEGREES. COMPLIED WITH AOM ABONORMAL PROCEDURES, ON SECOND APPROACH ALL FLAPS WENT TO 30 DEGREE. PROCEEDED TO MAKE NORMAL APPROACH AND LANDING. UNABLE TO DUPLICATE CONDITION. FOUND ONE RIGHT OUTBOARD FLAFeb 15, 1996 · N925TS · Boeing 727227 · Trailing Edge Flap Control SystemSDR 96FDEA00640Floor Beam · corrodedFLOOR BEAM UPPER CHORD LOWER SURFACE CORRODED STA 344, LBL 50 - RBL 10, WL 200. INSTALLED FLOOR BEAM REPAIR PER STANDARD REPAIR DRAWING MANUAL SR 27-53-007.Feb 15, 1996 · N491FE · Boeing 727227 · Fuselage Main, Floor BeamSDR 96FDEA00395Floor Beam · corrodedFLOOR BEAM UPPER CHORD LWR SURFACE CORRODED STA 344 LBL 50 TO RBL 10 WL 200. *S/D* INSTALLED FLOOR BEAM REPAIR PER STANDARD REPAIR DRAWING MANUAL SRM 27-53-007, NR0346.Feb 15, 1996 · N491FE · Boeing 727227 · Fuselage Main, Floor BeamSDR TAOA029608Pos Ind · malfunctionedDURING APPROACH, OUTBOARD TRAILING EDGE FLAPS LOCKED AT 15 DEGREE PERFORMED ABNORMAL PROCEDURES AND LANDED. AT TOUCHDOWN OUTBOARD TRAILING EDGE FLAPS INDICATED 30 DEGREE. VISUALLY INSPECTED OUTBOARD AND INBOARD FLAPS, FOUND NORMAL. REPLACED FLAP POSITION INFeb 14, 1996 · N925TS · Boeing 727227 · Trailing Flap Position Indicating SystemSDR CAL960237Stringer · crackedSTATION 31J - INSPECTION FOUND A .25 INCH CRACK IN FLANGE WHERE NUT PLATE MOUNTS, ON STRINGER 26L IN AFT PIT. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1, PAGE 6A. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-4 AND 51-30-2. (M)Feb 14, 1996 · N79754 · Boeing 727227 · Fuselage Main, Longeron/StringerSDR 96FDEA00254Hyd Tube · failedHYD SYS 'A' LOSS ON DESCENT INTO TYS. ** (S/D) ** REMOVED AND REPLACED NR 1 ENG TO 'A' SYS MODULE PRESSURE TUBE ASSY. SERVICED HYD - AND RAN NR 1 ENG. OPS AND LEAK CHECKS GOOD.Feb 14, 1996 · N485FE · Boeing 727227 · Hydraulic System, MainSDR CAL960238Skin · corrodedSTATION 31J - INSPECTION FOUND CORROSION IN SKIN UNDER STRINGER 28L AT STATION 950F TO 1010. THE CORRODED AREA OF SKIN WAS CUT OUT. FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 53-30-3, 51-20-4, AND 51-30-2. (M)Feb 12, 1996 · N79754 · Boeing 727227 · Fuselage Main, Plate/SkinSDR CAL960235Stringer · corrodedSTATION 31J - INSPECTION FOUND STRINGER 28L CORRODED IN AFT CARGO COMPARTMENT BETWEEN STATION 950F AND 970. THE CORRODED SECTION OF STRINGER WAS REMOVED. A NEW SECTION OF STRINGER AND STRINGER SPLICES WERE FABRICATED AND INSTALLED IAW SRM 53-10-3, 51-20-4, AFeb 11, 1996 · N79754 · Boeing 727227 · Fuselage Main, Longeron/StringerSDR CAL960234Stringer · corrodedSTATION 31J - INSPECTION FOUND AFT CARGO FLOOR STRINGER WEB CORRODED AT BS 950F TO 970, STRINGER 28L. THE WEB WAS REMOVED AND A NEW WEB WAS FABRICATED AND INSTALLED IAW SRM 51-20-1, 51-40-3, AND 51-30-2. (M)Feb 11, 1996 · N79754 · Boeing 727227 · Fuselage Main, Longeron/StringerSDR TAOA029607Battery Pack · dischargedCEILING EMERGENCY LIGHT AT ROW 3 INOP. REPLACED BATTERY PACK. OPERATIONAL CHECK OK. (M)Feb 10, 1996 · N925TS · Boeing 727227 · Emergency LightingSDR CAL960239L-Angle · corrodedSTATION 31J - INSPECTION FOUND L-ANGLE NEXT TO SKIN ON VERTICAL IN FT CARGO COMPARTMENT CORRODED AT BS 980, LBL 14. THE L-ANGLE WAS REMOVED AND A NEW L-ANGLE WAS FABRICATED AND INSTALLED IAW SRM 53-10-4, 51-10-2, 53-10-4, AND MM 51-20-15. (M)Feb 9, 1996 · N79754 · Boeing 727227 · Fuselage Miscellaneous StructureSDR CAL960236Nose Cowl · crackedSTATION 31J - INSPECTION FOUND A 1.75 INCH CRACK AT RIVET OF NR 3 ENGINE NOSE COWL SKIN. THE CRACKED AREA OF SKIN WAS CUT OUT. FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 54-30-3, FIGURE 8 AND ECRA 5430-01377. (M)Feb 9, 1996 · N79754 · Boeing 727227 · Engine Cowling SystemSDR CAL960231Angle · crackedSTATION 31J - INSPECTION FOUND A 1 INCH CRACK IN ANGLE AT BS 950C, LBL 18. AN L-ANGLE AND Z-ANGLE WERE FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-30-2, AND 51-40-4. (M)Feb 9, 1996 · N79754 · Boeing 727227 · Fuselage Miscellaneous StructureSDR CAL960230Stiffener · crackedSTATION 31J - INSPECTION FOUND A 1.5 INCH CRACK IN STRINGER STIFFENER AT BS 970 TO 980, RBL 2. THE CRACKED STIFFENER WAS REMOVED. A NEW STIFFENER WAS FABRICATED AND INSTALLED IAW SRM 51-40-2 AND 51-30-2. (M)Feb 9, 1996 · N79754 · Boeing 727227 · Fuselage Miscellaneous StructureSDR CAL960232Angle · crackedSTATION 31J - INSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT ANGLE AT BS 950B, RBL 48. A NEW Z-ANGLE AND TWO PLATES WERE FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-40-4, AND MM 51-20-15. (M)Feb 7, 1996 · N79754 · Boeing 727227 · Fuselage Miscellaneous StructureSDR AALA960241Accessory Unit · defectiveDFW - FLT NR 1025 - DURING APPROACH TO DFW WHEN LANDING GEAR EXTENDED, ALL GREEN LANDING GEAR LIGHTS ILLUMINATED ALONG WITH THE RIGHT GEAR RED LIGHT. RECYCLED LANDING GEAR WITH SAME RESULTS. VISUALLY CONFIRMED ALL LANDING GEAR DOWN AND LOCKED AND AIRCRAFT LAFeb 7, 1996 · N720AA · Boeing 727227 · Landing Gear Position and WarningSDR MZZA96005Actuator · failedTPE - FLT CS921 - DURING CLIMB-OUT, NR 3 KRUEGER FLAP FAILED TO RETRACT. FLIGHT CREW RAN CHECK LIST AND AIR RETURNED TO TPE. MAINTENANCE REMOVED AND REPLACED NR 3 LEADING EDGE FLAP ACTUATOR PER MM 27-87-22 AND SYSTEM OPERATION CHECK GOOD. AIRCRAFT RELEASED Feb 6, 1996 · N89427 · Boeing 727227 · Leading Edge Slat ActuatorSDR CAL960233Support Angle · corrodedSTATION 31J - INSPECTION FOUND FLOOR STRINGER SUPPORT ANGLE CRUSHED IN AFT CARGO COMPARTMENT, BS 1010, BETWEEN STRINGER 29R AND 30R. A NEW SUPPORT ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-4, 51-30-2, AND 51-10-2. (M)Feb 1, 1996 · N79754 · Boeing 727227 · Fuselage Miscellaneous StructureSDR 96FDEA00243Shear Tie · corrodedAFT LEG OF SHEAR TIE ON BELL FRAME STA 590 IS DEEPLY CORRORED BETWEEN STR 26 TO 27L. CORROSION WAS FOUND BEYOND LIMITS. REMOVED SHEAR TIE AND REPLACES WITH SERVICEABLE SHEAR TIE PER SRM 51-10-1.Feb 1, 1996 · N494FE · Boeing 727227 · Fuselage Miscellaneous StructureSDR AALA960163Retract Mech · lack of lubeORD - FLT NR 517 - DURING APPROACH TO ORD WHEN LANDING GEAR EXTENDED, LEFT MAIN LANDING GEAR REQUIRED FOUR ATTEMPTS PLUS POSITIVE G-FORCE TO LOCK IN THE DOWN POSITION. AIRCRAFT LANDED ORD WITHOUT INCIDENT. CLEANED AND LUBRICATED LEFT MAIN LANDING GEAR DUE TOJan 30, 1996 · N723AA · Boeing 727227 · Landing Gear Retraction/Extension SystemSDR CAL960149Floor Skin · corrodedSTATION 31J - INSPECTION FOUND G2 GALLEY FLOOR AND MOUNT BRACKET CORRODED. THE MOUNT BRACKET AND FLOOR SKIN WERE REMOVED. A NEW FLOOR SKIN WAS FABRICATED AND INSTALLED. THE CORROSION WAS CLEANED FROM BLOCK TIE DOWN AND REBONDED AND A NEW UPPER SHELF WAS INSJan 27, 1996 · N73751 · Boeing 727227 · Fuselage Floor PanelSDR 96FDEA00154Stringer · corrosionFORWARD CARGO STA 720, STR 28R, HAS CORROSION ON STRINGER. REPLACED CORRODED STRINGER PER SRM 53-10-3 WITH NEW STRINGER, 3 FEET, AND SPLICE.Jan 25, 1996 · N494FE · Boeing 727227 · Fuselage Main, Longeron/StringerSDR 96FDEA00124Actuator · failedAFTER T/O, THE LANDING GEAR HAD TO BE RECYCLED TO EXTINGUISH THE TAIL SKID LIGHT. DURING THE SECOND ATTEMPT IT TOOK 10 SECONDS FOR THE LIGHT TO GO OUT. REPLACED TAIL SKID ACTUATOR PER MM 32-71-12 AND ADJ PER MM 32-71-01, GROUND CHECKS OK.Jan 25, 1996 · N485FE · Boeing 727227 · Auxiliary Gear (Tail Skid)SDR MZZA96004Cdi · failedGUM - FLT 977 - NR 2 OMEGA WARNING LIGHT ON AND DISPLAY BLANK. RESET CIRCUIT BREAKER, WORKED FOR 15 MINUTES, THEN SAME. AIR RETURN BACK TO GUAM AFTER DUMPING 9,000 POUNDS OF FUEL. MAINTENANCE REPLACED NR 2 OMEGA CDU AND RPU, WITH NO HELP. FURTHER TROUBLESHJan 24, 1996 · N86426 · Boeing 727227 · Integrated Flight SystemSDR 96FDEA00121Engine · oil lossAT APPROXIMATELY FLIGHT LEVEL 220, NR 3 LOW OIL PRESSURE/FILTER BYPASS LIGHT FLASHED ON AND OFF. CONFIRMING LOW PRESSURE ZERO QUANTITY AND RED LINE OIL TEMPERATURE. ENGINE WAS SHUT DOWN, LANDING ACCOMPLISHED DFW. REPLACED NR 3 ENGINE PER WORK CARDS 70T0001,Jan 24, 1996 · N482FE · Boeing 727227 · Engine (Turbine/Turboprop)
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