Boeing 727-185C

Service difficulty reports · 425

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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 = '727185C'
  ORDER BY difficulty_date DESC"

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SDR UPS06246460Shim · looseRT WING O/B AILERON TAB DELAM DBLR LWR SURFACE. UPON INVESTIGATION FOUND DELAMINATION TO BE A SHIM THAT CAME LOOSE. STARTED REMOVAL OF AILERON BAL. TAB UP TO STEP D ON MM 27-10-19-4 REINSTALLED BOLTS IN TAB REDS AND INSTALLED COTTER PINS. RESECURED LOOSE SHMar 17, 2006 · N940UP · Boeing 727185C · Aileron TabsSDR UPS06246058Battery · inoperativeEMERGENCY EXIT LIGHTS OVER COCKPIT DOOR AND MAIN ENTRY DOOR ARE INOP. REPLACED EMERGENCY LIGHT BATTERY AS PER MM 33-50-90-2.Jan 27, 2006 · N940UP · Boeing 727185C · Emergency LightingSDR UPS05245641Battery · inoperativeEXIT LIGHT OVER COCKPIT DOOR INOP. REMOVED AND REPLACED LIGHT ASSY AND BATTERIES. OPS CK GOOD PER AMM 33-50-01-5.Oct 21, 2005 · N954UP · Boeing 727185C · Emergency LightingSDR UPS05243707Skin · crackedINSPECTION TYPE: C, LE SLAT ACCESS PANEL (NR 6 SLAT) HAS 1/2 INCH CRACK ON SKIN. REPAIR CARRIED OUT IAW SRM 51-10-01, 51-40-02 AND 51-30-02.Jan 13, 2005 · N940UP · Boeing 727185C · Leading Edge DevicesSDR UPS05243700Bracket · crackedINSPECTION TYPE: C, NR 5 FLAP TRACK, FWD O/B FAIRING ATTACH ANGLE BRACKET IS CRACKED. BRACKET REPLACED IAW SRM 51-20-1.Jan 13, 2005 · N940UP · Boeing 727185C · Trailing Edge FlapsSDR UPS05243684Fitting · crackedINSPECTION TYPE:C SUSPECT CRACK ON CLEAT AT STR 28L ON FWD SIDE OF BS 1070 AFT CARGO BAY. HFEC CARRIED OUT IAW NDTM 51-00-00 FIG 4. RESULT CRACK CONFIRMED. REMOVED CRACKED CLEAT, FABRICATED AND INSTALLED NEW CLEAT IAW SRM 51-20-1.Jan 13, 2005 · N940UP · Boeing 727185C · Fuselage Main, Attach FittingsSDR UPS05243683Fitting · crackedINSPECTION TYPE:C, SUSPECT CRACK ON CLEAT AT STR 29L ON FWD SIDE OF BS 1110 AFT CARGO BAY. HFEC CARRIED OUT IAW NDTM 51-00-00 FIG 4. CRACK CONFIRMED. REMOVED CRACKED CLEAT, FABRICATED AND INSTALLED NEW CLEAT IAW SRM 51-30-02.Jan 13, 2005 · N940UP · Boeing 727185C · Fuselage Main, Attach FittingsSDR UPS05243762Door · corrodedINSPECTION TYPE:C, CORROSION FOUND AT TAIL SKID DOOR UPPER ATTACH POINTS BS 1183 S 28L + 28R. ON REMOVAL OF PANEL IT WAS FOUND TO BE CORRODED BEYOND LIMITS IAW 53-30-1. NEW PANEL FABRICATED IAW SRM 51-20-1. TAIL SKID MOUNTING CASTING SHOW SIGNS OF WEAR. NEJan 12, 2005 · N940UP · Boeing 727185C · Landing Gear DoorsSDR UPS05243685Hinge · crackedINSPECTION TYPE:C, LEFT O/B AILERON O/B BALANCE PANEL FWD IDLER HINGE CRACKED. HINGE REPLACED IAW 51-30-2.Jan 12, 2005 · N940UP · Boeing 727185C · AileronsSDR UPS05243774Skin · corrodedINSPECTION TYPE:C, AREA OF LITE SURFACE CORROSION ON SKIN BELOW S4L AT BS 1183. CORROSION FOUND TO BE RUNNING UNDER LAP. FURTHER RECTIFICATION CARRIED OUT IAW UPS EO B727-5330-0509.Jan 11, 2005 · N940UP · Boeing 727185C · Fuselage Main, Plate/SkinSDR UPS05243763Structure · crackedINSPECTION TYPE:C, SUSPECT CRACK ON LT CHORD ABOVE NR 2 ENGINE HORIZONTAL FIREWALL AT UPPER END OF CHORD. HFEC CARRIED OUT IAW NDTM PART 6 51-00-00, FIG 4. CRACK FOUND TO BE 5.0 INCH IN LENGTH. CHORD REMOVED AND NEW CHORD DRILLED OFF AND INSTALLED IAW SRM 5Jan 11, 2005 · N940UP · Boeing 727185C · Fuselage Main, BulkheadSDR UPS05243702Support Angle · crackedINSPECTION TYPE: C, NR 3 FLAP TRACK FAIRING SUPPORT ANGLE CRACKED AT I/B AFT END. FAIRING SUPPORT ANGLE REPAIRED IAW SRM 51-20-01.Jan 11, 2005 · N940UP · Boeing 727185C · Trailing Edge FlapsSDR UPS05243701Support Angle · crackedINSPECTION TYPE: C, NR 4 FLAP TRACK FAIRING SUPPORT ANGLE CRACKED AT O/B SIDE AT MLG BEAM. FAIRING SUPPORT ANGLE REPAIRED IAW SRM 51-20-1.Jan 11, 2005 · N940UP · Boeing 727185C · Trailing Edge FlapsSDR UPS05243698Rib · crackedINSPECTION TYPE: C, NR 8 LE SLAT STRUCTURE HAS CRACKED RIB JUST O/B OF ACTUATOR ATTACH POINT. REPAIR CARRIED OUT IAW SRM 57-50-03.Jan 11, 2005 · N940UP · Boeing 727185C · Leading Edge DevicesSDR UPS05243697Rib · crackedINSPECTION TYPE:C NR 5 LE SLAT STRUCTURE HAS THREE RIBS CRACKED BETWEEN O/B TRACK AND O/B EDGE OF SLAT. REPAIRED CRACKED RIBS 3 PLACES AT NR 5 LE SLAT IAW SRM 57-50-03 FIG 9.Jan 11, 2005 · N940UP · Boeing 727185C · Leading Edge DevicesSDR UPS05243687Hook · crackedINSPECTION TYPE:C SUSPECT CRACK ON NR 2 SLAT O/B HOOK UPPER FASTENER. HFEC CARRIED OUT IAW NDTM 51-00-00 FIG 4. RESULT - CRACK CONFIRMED. REPAIR CARRIED OUT IAW SRM 57-50-3 FIG 10.Jan 11, 2005 · N940UP · Boeing 727185C · Leading Edge DevicesSDR UPS05243792Pressure Panel · crackedINSPECTION TYPE:C, NLG WHEEL WELL HAS 3 SUSPECT CRACKS AT RT AFT PRESSURE PANEL CUTOUT. TWO AT LWR FWD CORNER AND ONE NEAR UPPER AFT CORNER. REPAIR CARRIED OUT IAW AAAE EO 2005-001-004.Jan 10, 2005 · N940UP · Boeing 727185C · Fuselage Main, BulkheadSDR UPS05243783Web · crackedINSPECTION TYPE:C, RT VENTRAL STAIRWAY TORQUE BOX WEB SKIN CRACK EXTENDING BEYOND STOP DRILL HOLE ON FWD O/B END ADJACENT TO FUEL SHROUD HOLE & CRACK ON DOUBLER AT AFT SIDE BS 1263. REPAIR CARRIED OUT IAW EO B727-5310-1239-E.Jan 10, 2005 · N940UP · Boeing 727185C · Fuselage Miscellaneous StructureSDR UPS05243769Door · corrodedINSPECTION TYPE:C, NLG LT FWD DOOR HAS EVIDENCE OF CORROSION UNDER SEAL RETAINER. LT NLG DOOR REMOVED AND REPLACED IAW AMM 32-22-01.Jan 10, 2005 · N940UP · Boeing 727185C · Landing Gear DoorsSDR UPS05243768Bushing · corrodedINSPECTION TYPE:C, ENGINE NR 3 FWD MOUNT FITTING HAS PITTING CORROSION IN BOTH O/B (LARGE) HOLES. FWD O/B HOLE BUSHING REMOVED OHM 20-50-03. HFEC CARRIED OUT IAW NDTM 51-00-00 FIG 13, NO DEFECTS FOUND. REPAIRED IAW UPS EO B727-5440-11592-A.Jan 10, 2005 · N940UP · Boeing 727185C · Engine Mount SectionSDR UPS05243766Bushing · corrodedINSPECTION TYPE:C, ENGINE NR 1 FWD MOUNT FITTING HAS PITTING CORROSION IN ALL MOUNT HOLES. AFT O/B HOLE CORRODED BUSHING REMOVED IAW OHM 20-50-03. HFEC CARRIED OUT IAW NDTM 51-00-00 FIG 13, NO DEFECTS FOUND. REPAIRED IAW UPS EO B727-5440-11592-A.Jan 10, 2005 · N940UP · Boeing 727185C · Engine Mount SectionSDR UPS05243699Tab · delaminatedINSPECTION TYPE: C, LT O/B AILERON TAB DELAMINATED AT UPPER I/B END. AILERON TAB REPAIRED IAW SRM 51-40-20.Jan 10, 2005 · N940UP · Boeing 727185C · Aileron TabsSDR UPS05243686Bracket · crackedINSPECTION TYPE:C, NR 1 KRUEGER FLAP TRUNNION BRACKET IS CRACKED ON O/B SIDE. BRACKET REPLACED IAW DRG 65-16275.Jan 10, 2005 · N940UP · Boeing 727185C · Leading Edge DevicesSDR UPS05243791Skin · crackedINSPECTION TYPE:C SUSPECT CORROSION BETWEEN SKIN AND INTERNAL STRUCTURE BS 294 BETWEEN S18R + S19R ON CLOSER INSPECTION CORROSION FOUND TO BE WELL WITHIN LIMITS IAW SRM 53-30-01. A SMALL CRACK WAS FOUND COMING FROM A FASTENER HOLE. AREA CUT OUT IAW SRM 53-30Jan 8, 2005 · N940UP · Boeing 727185C · Fuselage Main, Plate/SkinSDR UPS05243710Casting · corrodedINSPECTION TYPE:C, NR 3 KRUEGER FLAP INBOARD HINGE, FIXED LEADING EDGE CASTING HAS EVIDENCE OF INTERGRANULAR CORROSION. REPLACED AND INSTALLED NEW CASTING IAW DRG 64-8343.Jan 7, 2005 · N940UP · Boeing 727185C · Leading Edge DevicesSDR UPS05243777Panel · delaminatedINSPECTION TYPE:C, ENGINE NR 1 PYLON PANEL 5408 IS DELAMINATED INNER SURFACE FWD END. PANEL REPAIRED IAW SRM 51-40-20.Jan 6, 2005 · N940UP · Boeing 727185C · Nacelle/Pylon, Plate/SkinSDR UPS05243776Panel · delaminatedINSPECTION TYPE:C, ENGINE NR 3 PYLON PANEL 5508 IS DELAMINATED INNER SURFACE FWD END. PANEL REPAIRED IAW MM 20-60-04.Jan 6, 2005 · N940UP · Boeing 727185C · Nacelle/Pylon, Plate/SkinSDR UPS04243588Battery Pack · inoperativeFORWARD ENTRY EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK. OPS CHECK GOOD.Dec 4, 2004 · N940UP · Boeing 727185C · Emergency LightingSDR UPS04243559Valve · stuckCAPT O2 MASK HAS STUCK VALVE. REPLACED MASK ASSY, OPS CK NORMAL.Nov 30, 2004 · N940UP · Boeing 727185C · Crew Oxygen SystemSDR UPS04243374Tab · corrodedINSPECTION TYPE:C, I/B RIGHT AILERON TAB HINGE CASTINGS ARE CORRODED AND SUSPECT CRACK ON AILERON REAR SPAR. REMOVED AILERON IAW AMM 27-10-00, REMOVED HINGES & SPAR IAW SRM 51-3 -30-02. SPAR REPAIRED IAW SRM 57-30-2 FIG 7 & SRM 51-40-02 FIG 1. NEW HINGES INOct 20, 2004 · N954UP · Boeing 727185C · Aileron Tab Control SystemSDR UPS04243352Control Unit · malfunctionedWHEN F/O TURNED OFF F/D ALTITUDE HOLD, RECEIVED AN INTERMITTENT FIRE WARNING. THE F/O TAPPED THE GLARE SHIELD AND THE FIRE WARNING LIGHT AND BELL CAME ON STEADY. ENGINE NR 3 WAS SHUTDOWN IAW PROCEDURES AND UNEVENTFUL. SIMULATED CREW ACTION BY TAPPING ONOct 17, 2004 · N940UP · Boeing 727185C · Fire DetectionSDR UPS04243410Intercostal · crackedINSPECTION TYPE: C, ON REMOVAL OF INTERCOSTAL TO FACILITATE RIGHT FITTING REPLACEMENT AT BS 740, A CRACK WAS FOUND. REPLACED INTERCOSTAL WEB IAW SRM 51-20-04.Oct 11, 2004 · N954UP · Boeing 727185C · Fuselage Miscellaneous StructureSDR UPS04243413Web · crackedINSPECTION TYPE:C, BS 740 LOWER WEB RBL 35, WL 160 SUSPECT CRACK IN THIS LOCATION. HFEC CARRIED OUT IAW NDTM 51-00-00, CRACK CONFIRMED WITHIN FASTENER HOLE. REPAIR CARRIED OUT IAW SRM 53-10-9 FIG 4.Oct 8, 2004 · N954UP · Boeing 727185C · Fuselage Miscellaneous StructureSDR UPS04243383Web · crackedINSPECTION TYPE-C BS 740 LOWER WEB RT BL 35 WL160 APPROX SUSPECT CRACK IN THIS LOCATION. HFEC CARRIED OUT ON ABOVE AREA IAW NDTM 51-00-00 PT 6 FIG 4 CRACKS CONTAINED WITHIN FASTENER HOLE. REPAIR PARTS FABRICATED IAW SRM 53-10-09. REPROTECTED REP PARTS AND DAOct 8, 2004 · N954UP · Boeing 727185C · Fuselage Miscellaneous StructureSDR UPS04243393Door · crackedINSPECTION TYPE:C, BRACKET CRACKED ON WING DOOR FWD OF HINGE CASTING. STOP DRILLED CRACK IAW SRM 51-10-01. HFEC CARRIED OUT AROUND STOP DRILLED AREA IAW B727 NDTM 51-00-00 PT 6 FIG 4. CRACK CONTAINED WITHIN STOP DRILLED AREA. REPAIRED IAW SRM 51-20-01.Oct 6, 2004 · N954UP · Boeing 727185C · Landing Gear DoorsSDR UPS04243392Skin · corrodedINSPECTION TYPE-C RT OB AILERON HAS PITTING CORROSION ON CONTROL ROD ATTACH CASTING. AILERON REPLACED IAW MM 27-10-14.Oct 6, 2004 · N954UP · Boeing 727185C · AileronsSDR UPS04243406Bracket · crackedINSPECTION TYPE: C, FWD CARGO DOOR BRACKETS CRACKED AT UPPER AFT HINGE ATTACH POINT. REMOVED BRACKETS IAW 51-30-02. NEW BRACKETS FABRICATED IAW BOEING DRAWING 69-18203. NEW BRACKETS INSTALLED IAW 51-30-02.Oct 5, 2004 · N954UP · Boeing 727185C · Cargo/Baggage DoorsSDR UPS04243405Fitting · corrodedINSPECTION TYPE:C, LEFT O/B AILERON TAB MAST FITTINGS HAVE PITTING CORROSION AROUND BUSHINGS. ON INVESTIGATION LEFT O/B AILERON TAB FITTINGS FOUND TO BE OUTSIDE LIMITS. LEFT O/B AILERON TAB REPLACED IAW 27-10-19.Oct 5, 2004 · N954UP · Boeing 727185C · Aileron Control SystemSDR UPS04243394Fitting · corrodedINSPECTION TYPE:C DURING REMOVAL OF RIGHT 740 FITTING CORROSION FOUND ON CENTER WING SECTION FRONT SPAR UPPER CHORD AT RBBL 65-70 APPROX CORROSION REMOVED IAW SRM 51-10-06. REPAIR ANGLES FABRICATED IAW SRM 53-30-03. HFEC CARRIED OUT ON ABOVE AREA IAW B727-NDOct 5, 2004 · N954UP · Boeing 727185C · Fuselage Main, Attach FittingsSDR UPS04243382Skin · crackedINSPECTION TYPE: C, SUSPECT CRACK AT FWD UPPER CORNER OF LEFT WING ICE LIGHT CUTOUT. HFEC CARRIED OUT ON ABOVE AREA IAW B727 NDTM 51-00-00 PT 6 FIG 4, CRACKS CONFIRMED, ENDS MARKED. DOUBLER AND FILLER INSTALLED IAW SRM 53-30-03. WEIGHT OF REPAIR 2.37 LBS.Oct 5, 2004 · N954UP · Boeing 727185C · Wing, Plate/SkinSDR UPS04243411Bulkhead · crackedINSPECTION TYPE:C, BS 178 BULKHEAD: EVIDENCE OF CRACK ON FWD FACE AT RBL 10 WL 235.1 EMANATING FROM FASTENER HOLE. HFEC CARRIED OUT IAW NDTM 51-00-00 FIG 4. CRACK CONFIRMED AND ENDS MARKED. CUT OUT DAMAGED AREA IAW SRM 53-10-9. HFEC CARRIED OUT, NO DEFECTSOct 4, 2004 · N954UP · Boeing 727185C · Fuselage Main, BulkheadSDR UPS04243409Stringer · corrodedINSPECTION TYPE: C, SKIN BULGING AT BS 1307-1315 STR 8L. FOUND BULGING WAS CAUSED BY CORROSION ON STRINGER EXTRUSION. CORROSION REMOVED AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. REPAIR DOUBLER INSTALLED IAW SRM 53-30-3.Oct 4, 2004 · N954UP · Boeing 727185C · Fuselage Main, Longeron/StringerSDR UPS04243403Terminal · crackedINSPECTION TYPE: C, TAIL SKID BAY STABILIZING LINKS UPPER AND LOWER LEFT AFT TERMINALS CRACKED AND LOWER AFT RIGHT TERMINAL CRACKED. INSTALLED NEW UPPER AND LOWER LEFT AFT TERMINALS ON TAILSKID BAY, FABRICATED LOWER AFT RIGHT TERMINAL AND FITTED IAW SRM 51-30Oct 4, 2004 · N954UP · Boeing 727185C · Fuselage Main, Attach FittingsSDR UPS04243397Hinge · corrodedINSPECTION TYPE-C RT IB AILERON TAB HINGE CASTINGS ARE CORRODED AND SUSPECT CRACK ON AILERON REAR SPAR. REPLACED REAR SPAR IAW SRM 51-30-02. NEW TAB HINGES INSTALLED IAW SRM 51-30-02Oct 4, 2004 · N954UP · Boeing 727185C · AileronsSDR UPS04243396Fitting · crackedINSPECTION TYPE:C, TO GAIN ACCESS FOR NDT PLEASE REMOVE FASTENERS BETWEEN STR 23 & 24 BS 740 FITTING RIGHT. REMOVED FASTENERS IAW SRM 51-30-02. HFEC CARRIED OUT ON ABOVE AREA IAW B727 NDTM 51-00-00 PT6 FIG 4, CRACK CONFIRMED, ENDS MARKED. REF UPS EO B727-53Oct 4, 2004 · N954UP · Boeing 727185C · Fuselage Main, StructureSDR UPS04243395Pressure Panel · crackedINSPECTION TYPE: C, CRACK FOUND ON NWW LEFT SIDEWALL JUST BELOW LEFT AFT SIDE PRESSURE PANEL. HFEC CARRIED OUT IAW B727 NDTM 51-00-00 PT 6 FIG 4, CRACK CONFIRMED, ENDS MARKED. STOP DRILLED CRACKS IAW SRM 51-10-01. HFEC CARRIED OUT AROUND STOP DRILLED AREAS Oct 4, 2004 · N954UP · Boeing 727185C · Fuselage Main, BulkheadSDR UPS04243134Light · inoperativeINSPECTION TYPE:N/A, CREW ENTRY EMERGENCY LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM 33-50-67, OPS CHECK GOOD.Sep 20, 2004 · N954UP · Boeing 727185C · Emergency LightingSDR UPS04243019Fan · inoperativeDURING CLIMB ACRID ODOR NOTED IN COCKPIT. CREW TURNED OFF GASPER FAN, ODOR WENT AWAY. GASPAR FAN DEACTIVATED AND PLACED ON MEL M286609 & MEL CLOSED ON LP 212332. REPLACED GASPER FAN PER B727 MM CH 21-23-22, GASPER FAN OPS CHECK NORMAL.Aug 25, 2004 · N954UP · Boeing 727185C · Air Distribution FanSDR UPS04242309A/C Pack · overtempJUST AFTER T/O COCKPIT FILLED WITH FUMES, RIGHT PACK TEMP WAS 170'. TURNED OFF PAC FUMES STOPPED. ALL C/B'S CHECKED & IN PAC FAN OPS NORMAL. R/R 35 FT CONTROL VALVE PER AMM 21-51-42, OPS CHECK GOOD.Apr 28, 2004 · N940UP · Boeing 727185C · Cabin Temperature Control SystemSDR UPS04242079Lamp · inoperativeINSPECTION TYPE:N/A COCKPIT EMERGENCY EXIT LIGHT HAS 1 LAMP INOP. RELAMPED AS REQUIRED, OPS CHECKS GOOD IAW M/M 33-50-01.Mar 31, 2004 · N954UP · Boeing 727185C · Emergency Lighting
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