Boeing 727-180C

Service difficulty reports · 279

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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 = '727180C'
  ORDER BY difficulty_date DESC"

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SDR UPS06248626Indicator · inoperativeN/A ATB - FUEL IMBALANCE BETWEEN TANK NR 1 AND NR 3 STARTED AT NR 1, 11.9, NR 3, 11.2 AFTER TA/O TANK NR 1, 11.5, TANK NR 3, 9.5 DEFERRED NR 3 COCKPIT GAUGE NR M337674 ISSUED. DEFERRED NR 3 COCKPIT GAUGE IAW MEL 28-11-1-1. VERIFIED FUELING STATION GAUGES ARE ONov 14, 2006 · N920UP · Boeing 727180C · Fuel Quantity IndicatorSDR UPS06248464Light · weakFOUND COCKPIT EMERGENCY EXIT LIGHT WEAK. REPLACED C/P EMERGENCY LIGHT ASSY CKS OK.Nov 2, 2006 · N920UP · Boeing 727180C · Emergency LightingSDR UPS06247335Smoke Goggles · dirtyF/O SMOKE GOGGLES DIRTY AND NOT BAGGED. INSTALLED NEW MASK.Jul 15, 2006 · N920UP · Boeing 727180C · Emergency EquipmentSDR UPS06246958Skin · corrodedINSPECTION TYPE:SV RIVET HEAD POPPED OFF AT STA 680 LONG 6L JUST FWD OF DOUBLER. FOUND CORROSION IN LAP FROM STA 620-720 AT S-6L. REPAIRED LAP PER EO B727-5330-0509-T APPX C, SAA EA 727-5330-01-A0201, AND EO B727- 5330-24413-A.May 12, 2006 · N920UP · Boeing 727180C · Fuselage Main, Plate/SkinSDR UPS06246273Panel · delaminatedINSPECTION TYPE:N/A RT INBOARD SPOILER PANEL DELAMINATED. REPAIRED SPOILER PANEL PER SRM 51-40-21.Feb 24, 2006 · N920UP · Boeing 727180C · SpoilersSDR UPS05245867Light · looseCOCKPIT EMERGENCY EXIT LIGHT LOOSE OUT OF FITTING ABOVE DOOR. SECURED EMERGENCY EXIT LIGHT ON CASE AND INSTALLED LENS REF MM 33-50-67-2.Dec 9, 2005 · N920UP · Boeing 727180C · Emergency LightingSDR UPS05245632Fitting · crackedINSPECTION TYPE: C, SEVERAL CRACKS ON LT MLG TRUNNION FITTING. REPLACED MLG TRUNNION FITTING IAW AAAE EO = 2005-091-001 AND UPS FILE APPROVAL B727-5740-23096.Oct 4, 2005 · N920UP · Boeing 727180C · Wing, Landing Gear Attach FittingsSDR UPS03240426Longeron · crackedINSPECTION TYPE: C2, WHILE WORKING EO B727-5330-17160-A, STA 366.65 LONGERON S1 IS CRACKED. REMOVED FASTENERS, CUTOUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED REPAIR CHANNEL AND FILLER IAW SRM 53-10-2 FIG 9 AND 53-10-3 FIG 2.Apr 10, 2003 · N920UP · Boeing 727180C · Fuselage Main, Longeron/StringerSDR UPS03240405Light · inoperativeAT CRUISE NR 1 START VALVE LIGHT FLICKERED THEN CAME ON FOR A FEW SECONDS. ENG BLEED WAS CLOSED AND ENGINE SHUTDOWN IN ACCORDANCE WITH AOM PROCEDURES. REMOVED AND REPLACED NR 1 ENGINE START VALVE IAW TAY ENGINE MM 80-11-01. OPS CHECK NORMAL.Apr 2, 2003 · N920UP · Boeing 727180C · Engine Starting SystemSDR UPS03240223Light · inoperativeEMERGENCY EXIT LIGHT AT CREW ENTRANCE DOOR INOP. RESET LIGHT PACK, CHECKS GOOD.Feb 22, 2003 · N920UP · Boeing 727180C · Emergency LightingSDR UPS03240209Battery · inoperativeINSPECTION TYPE: C, COCKPIT EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERIES AND OPS CHECKS GOOD IAW M/M 33-50-01.Feb 19, 2003 · N920UP · Boeing 727180C · Emergency LightingSDR UPS02239825Light · not seatedINSPECTION TYPE:PFLT EMERGENCY EXIT LIGHTS ABOVE CABIN ENTRY DOOR ARE VERY DIM. CHARGED BATTERY FOR 3 HRS, RESEATED LIGHT ASSY, GROUND CHECK GOOD.Oct 25, 2002 · N921UP · Boeing 727180C · Emergency LightingSDR UPS02239750Light · inoperativeEMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED CREW ENTRY DOOR EMERGENCY EXIT LIGHT ASSY. OPS CHECK GOOD MM 33-50-01.Oct 15, 2002 · N921UP · Boeing 727180C · Emergency LightingSDR UPS02238111Skin · corrodedINSPECTION TYPE:C CORROSION FOUND AT LAP SKINS BS 479 STRINGER 26R FASTENERS REMOVED IAW SRM51-30-02, UPUPER SKIN CUT OUT BETWEEN BS 47 2-485, NDT NDF, REPAIR PARTS FABRICATED IAW AND INSATLLED IAW EO B72 7-5330-16775.Apr 22, 2002 · N921UP · Boeing 727180C · Fuselage Main, Plate/SkinSDR UPS02238094Skin · crackedINSPECTION TYPE:C NR 3 KRUEGER FLAP ANTI ICE SKIN CRACKED 14 INCHES FROM I/B END. INSPECTED IAW NDTM PT 6 51-00-00 FIG 4, REPAIR CARRIED OUT IAW UPS EO B727-5750-3082-D.Apr 22, 2002 · N921UP · Boeing 727180C · Leading Edge DevicesSDR UPS02238102Seat Track · corrodedINSPECTION TYPE:C CORROSION FOUND ON SEAT TRACK O/B FLANGE AT BS 500 AT R/H O/B SEAT T RACK SEAT TRACK REPAIRED IAW SRM 53-10-5Apr 20, 2002 · N921UP · Boeing 727180C · Fuselage Main, StructureSDR UPS02238068Doubler · corrodedINSPECTION TYPE:C DOUBLER ON LEFT FWD WHEEL WELL PANEL IS PULLING LOOSE, AND IS CORRODED AT LOWER FASTENER. REMOVED AND REPLACED DOUBLER PER B727 SRM 51-30-2 ON LEFT FWD WHEEL WELL BELOW APU EXTINGUISHER BLOW OUT DISC.Apr 18, 2002 · N920UP · Boeing 727180C · Fuselage Main, Plate/SkinSDR UPS02238112Doubler · corrodedINSPECTION TYPE:C SUSPECT CORROSION BETWEEN FUSELAGE SKIN AND TOILET SERVICE PAN UPPER FLANGE, AFT SERVICE PAN. AREA PAINT STRIPPED, SERVICE PAN DE-RIVETED AND REMOVED, SKIN PANEL DE-RIVETED BETWEEN STR 17L-23L BS 1183 - 1150. INTERNAL DOUBLER AROUND PAN FOApr 18, 2002 · N921UP · Boeing 727180C · Fuselage Main, Plate/SkinSDR UPS02238103Skin · crackedINSPECTION TYPE:C SUSPECT CRACK IN FUSELAGE SKIN BS 310 S8 L/H AT FWD ENTRY DOOR FWD D OOR CUT OUT REPAIR CARRIED OUT IAW UPS EO B727-5340-1460Apr 18, 2002 · N921UP · Boeing 727180C · Fuselage Main, Plate/SkinSDR UPS01237092Hydraulic Line · crackedINSPECTION TYPE:N/A SYSTEM A-HYDRAULIC FAILURE, QTY ZERO. FOUND NR 13 SPOILER ACTUATOR RETURN LINE CRACKED. PER GMM INSTALLED A FLEX HOSE. CHECKED CASE DRAIN FILTERS, REPLACED NR 2 HYD EDP. SERVICED SYSTEM AND OPS CHK'D GOOD. PUMPED CHANGED DUE TO BYPASS SOct 18, 2001 · N920UP · Boeing 727180C · Hydraulic System, MainSDR UPS01235994Light · inoperativeINSPECTION TYPE:N/A REF ITEM 1 THIS PAGE. SUSPECT EMER LIGHT FWD SOCKET TO BE BAD. REMOVED AND REPLACED EMERGENCY EXIT LIGHT, OPS CK GOOD.May 24, 2001 · N920UP · Boeing 727180C · Emergency LightingSDR UPS01235993Light · malfunctionedINSPECTION TYPE:N/A EMERGENCY EXIT LIGHT CAME ON IN FLIGHT, NOW WILL NOT TEST ON THE GROUND. PERFORMED OPS CHECK OF EMERGENCY EXIT LIGHTS, OPS CHECK OK. NO DEFECTS NOTED.May 24, 2001 · N920UP · Boeing 727180C · Emergency LightingSDR UPS01235238Cover · looseINSPECTION TYPE:N/A, COCKPIT EMERGENCY EXIT LIGHT COVER FALLS OFF ON LANDING. REPLACED EXIT LIGHT COVER.Mar 7, 2001 · N920UP · Boeing 727180C · Emergency LightingSDR UPS01234998Fitting · brokenINSPECTION TYPE:IN OXYGEN BOTTLE ATTACHING HARDWARE BROKEN. *S/D* REMOVED AND REPLACED MS FITTING ON BLOWOUT LINE AND UPPER 02 BOTTLE CLAMP. REMOVED AND REPLACED 02 BOTTLE. LK CHECK GOOD.Feb 15, 2001 · N921UP · Boeing 727180C · Crew Oxygen SystemSDR UPS01234918Access Panel · corrodedINSPECTION TYPE:IN FUSELAGE - RT ACCESS PANEL 3420 - BS 630 AFT FRAME OF ACCESS PANEL CUTOUT HAS CORROSION BEYOND LIMITS PER B727 SRM 53-01-1. REMOVED CENTER SECTION OF AFT FRAME OF PANEL CUTOUT ON FUSELAGE BODY PANEL 3420 AT BS 630, FABRICATED A NEW SECTION Jan 26, 2001 · N920UP · Boeing 727180C · Fuselage Main, Plate/SkinSDR UPS01234919Angle · crackedINSPECTION TYPE:IN RT WING LEADING EDGE STA 349.6 WEB O/B UPPER SUPPORT ANGLE CRACKED. STOPPED DRILLED CRACK PER B727 SRM 51-10-1, NDT STOPPED DRILLED INSTALLED ANGLE REPAIR PER B727 SRM 51-40-3.Jan 25, 2001 · N920UP · Boeing 727180C · Wing Miscellaneous StructureSDR UPS00234545Switch · inoperativeINSPECTION TYPE:N/A CO PILOTS EMERG 0XYGEN SWITCH FAILS TO FULLY CLOSE ***SUPPLEMENTAL MRR*** REPLACED CO-PILOTS REGULATION W/SERVICABLE RUGULATION AND REPLACED W ITH SERVICABLE BOTTLE. LEAKED CHECK OK OPS CHECK PER 727 MM CHPT 35- 11-31 AND 12-15-11Dec 13, 2000 · N921UP · Boeing 727180C · Crew Oxygen SystemSDR UPS00234250Motor · failedINSPECTION TYPE:C, O/B ALT FLAP MOTOR NOT RETRACTING FLAPS. REPLACED MOTOR IAW MM 27-51-141.Oct 26, 2000 · N921UP · Boeing 727180C · Trailing Edge Flap Control SystemSDR UPS00234247Shear Tie · crackedINSPECTION TYPE:C, FLOORBEAM SHEAR TIE CRACKED AT BS 318 AND LBL 4. REPAIR CARRIED OUT IAW SRM 51-40-2.Oct 18, 2000 · N921UP · Boeing 727180C · Fuselage Main, StructureSDR UPS00234246Shear Tie · crackedINSPECTION TYPE:C, FLOORBEAM SHEAR TIE CRACKED AT BS 312 RBL 24. REPAIR CARRIED OUT IAW SRM 51-40-2.Oct 18, 2000 · N921UP · Boeing 727180C · Fuselage Main, StructureSDR UPS00234257Flange · crackedINSPECTION TYPE:C, SUSPECT CRACK ON AFT O/B AND FWD FLANGES OF BS 930 FUSELAGE FITTING BETWEEN S18A AND S19 LT. REPAIR CARRIED OUT IAW UPS EO B727-5310-2611 APPENDIX 8.1Oct 16, 2000 · N921UP · Boeing 727180C · Fuselage Miscellaneous StructureSDR UPS00234249Fitting · corrodedINSPECTION TYPE:C, DUE TO EXCESSIVE CORROSION IN BS 940 LT FITTING FASTENER HOLES, REPLACE FITTING BS 940 LT. REPLACED IAW UPS EO B727-5310-4501 APPENDIX C.Oct 16, 2000 · N921UP · Boeing 727180C · Fuselage Main, Attach FittingsSDR UPS00234256Stiffener · crackedINSPECTION TYPE:C, KEEL BEAM AREA, HORIZ STIFFENER AT BS 900 IS CRACKED STIFFENER IS LOCATED ON INTERNAL SIDE OF LT KEEL BEAM WALL. REPAIR CARRIED OUT IAW SRM 51-30-2 DRG NR 65-28900 AND SMRO EO 2000-38-006 UPS ENGINEERING FILE NR 727-53-2293.Oct 14, 2000 · N921UP · Boeing 727180C · Fuselage Miscellaneous StructureSDR UPS00234255Stiffener · crackedINSPECTION TYPE:C, KEEL BEAM AREA (INTERNAL) HORIZ STIFFENER AT BS 900 APPROX IS CRACK ED AT SITE OF PREVIOUS REPAIR RT KEEL BEAM WALL. REPAIR CARRIED OUT IAW DRG NR 65-28900 AND SMRO EO 2000-38-006 UPS ENGINEERING FILE NR 727-53-2293.Oct 14, 2000 · N921UP · Boeing 727180C · Fuselage Miscellaneous StructureSDR UPS00234252Stiffener · crackedINSPECTION TYPE:C, KEEL BEAM AREA, HORIZ STIFFENER AT BS 900 IS CRACKED. STIFFENER IS LOCATED ON INTERNAL SIDE OF LT KEEL BEAM WALL. STIFFENER INSTALLED IAW DRG NR 65-18636 AND SRM 51-30-2.Oct 14, 2000 · N921UP · Boeing 727180C · Fuselage Miscellaneous StructureSDR UPS00234251Stiffener · crackedINSPECTION TYPE:C, KEEL BEAM AREA (INTERNAL) HORZ STIFFENER AT BS 900 APPROX IS CRACKED AT SITE OF PREVIOUS REPAIR RT KEEL BEAM WALL. STIFFENER INSTALLED IAW DRG 65-18636 AND SRM 51-30-2.Oct 14, 2000 · N921UP · Boeing 727180C · Fuselage Miscellaneous StructureSDR UPS00234248Mount · corrodedINSPECTION TYPE:C, ENGINE NR 3 FWD MOUNT PITTING CORROSION FWD IN BOTH I/B MOUNT HOLES. REPAIR CARRIED OUT IAW EO B7274401592.Oct 13, 2000 · N921UP · Boeing 727180C · Engine Mount SectionSDR UPS00234244Mount · corrodedINSPECTION TYPE:C, ENG NR 1 FWD MOUNT, PITTING CORROSION FOUND IN FWD BOLT HOLES I/B, O/B. REPAIR CARRIED OUT IAW EOJ NR B727-5440-11592.Oct 13, 2000 · N921UP · Boeing 727180C · Engine Mount SectionSDR UPS00234241Beam · crackedINSPECTION TYPE:C, CRACK FOUND AT BS 1183 BULKHEAD VERTICAL BEAM RBL 26.83 AT WL 259.5. REPAIR CARRIED OUT IAW APPENDIX D OF EO B727-5311-0631.Oct 13, 2000 · N921UP · Boeing 727180C · Fuselage Miscellaneous StructureSDR UPS00234254Flange · corrodedINSPECTION TYPE:C, EVIDENCE OF CORROSION TO S18A FLANGE (HORIZ) AT BS 870 LT. REPAIR CARRIED OUT IAW SRM 53-10-1 AND 51-30-2 AND SMRO EO 2000-38-003 AND EO B727-5330-3815 UPS ENGINEERING FILE NR 727-53-2292.Oct 12, 2000 · N921UP · Boeing 727180C · Fuselage Miscellaneous StructureSDR UPS00234243Skin · crackedINSPECTION TYPE:C, SKIN CRACKS AT BS 203.8 RT AT WL 18 AND WL 20. DAMAGE REPAIRED IAW SRM 53-30-3 FIG 3.Oct 12, 2000 · N921UP · Boeing 727180C · Fuselage Main, Plate/SkinSDR UPS00234242Bracket · crackedINSPECTION TYPE:C, ENGINE NR 3 THRUST REV O/B FAIRING MID SUPPORT BRACKET CRACKED. BRACKET REPLACE IAW MM 20-80-01.Oct 12, 2000 · N921UP · Boeing 727180C · Engine Thrust ReverserSDR UPS00234240Beam · crackedINSPECTION TYPE:C, FOUR CRACKS FOUND AT BS 1183 BULKHEAD VERTICAL BEAM LBL 26.83 AT WL 257 AND WL 260. REPAIR CARRIED OUT IAW APPENDIX D OF EO B727-5311-0631AND BOEING DRG 65C34406.Oct 12, 2000 · N921UP · Boeing 727180C · Fuselage Miscellaneous StructureSDR UPS00234228Skin · crackedINSPECTION TYPE:C, SKIN CRACK AT BS 243.7 WL 19 LT. CRACKED AREA OF SKIN CUT OUT IAW SRM 53-30-3 FIG 3. HFEC C/O IN ALL ACCESSED HOLES AND AROUND PERIFERY OF CUTOUT. POST FASTENER REMOVAL AND SKIN CUTOUT IAW B727 NDTM. NO DEFECTS FOUND IN FASTENER HOLES ANOct 12, 2000 · N921UP · Boeing 727180C · Fuselage Main, Plate/SkinSDR UPS00234229Structure · corrodedINSPECTION TYPE:C, BILGE IN SKIN (SUSPECT CORROSION) AT BS 1030 ABOVE STR 18 LT. GILL LINER REMOVED IAW MM 25-52-02. CORROSION ON EXTRUSION FOUND TO BE CORRODED AND OUTSIDE LIMITS SRM 53-30-01. NEW EXTRUSION INSTALLED IAW SRM 51-30-02. GILL LINER INSTALLEDOct 11, 2000 · N921UP · Boeing 727180C · Fuselage Main, StructureSDR UPS00233068Floor Support · crackedINSPECTION TYPE: C CARGO BAY FLOOR SUPPORT LONGTITUDINAL BEAMS CRACKED TWO PLACES, BS 2020, BL 0, BS 1988, LBL 30 FLOOR SUPPORT BEAMS REPAIRED IAW SRM 53-10-07Jun 23, 2000 · N921UP · Boeing 727180C · Fuselage Miscellaneous StructureSDR UPS99231117Link · corrodedINSPECTION TYPE: AD, RT MLG TRUNNION LINK HAS PITTING CORROSION ON FORWARD BEARING SURFACE. REPLACED TRUNNION LINK ASSEMBLY. INSTALLED IAW MM 32-11-01.Nov 8, 1999 · N921UP · Boeing 727180C · Main Landing Gear Attach SectionSDR UPS99231116Support · corrodedINSPECTION TYPE: AD, RT SUPPORT ASSEMBLY INBOARD FLAP TRACK FORWARD CORRODED. SUPPORT ASSEMBLY REPLACED IAW BOEING DRAWING NR 65 19297, SHEET 3, REV E.Nov 8, 1999 · N921UP · Boeing 727180C · Trailing Edge FlapsSDR UPS99231120Fitting · leakingINSPECTION TYPE:AD, FUEL LEAK AT RT WING BEHIND LANDING GEAR TRUNNION FITTING, ONLY STAINS. THIS MRR RESUBMITTED TO INCLUDE TRUNNION FITTING, FUEL LEAK REPAIRED IAW SMRO EO 99-35-001. TRUNNION FITTING REMOVED AND REPLACED DUE TO MECHANICAL DAMAGE.Nov 5, 1999 · N921UP · Boeing 727180C · Fuel StorageSDR UPS99231119Fitting · leakingINSPECTION TYPE:AD FUEL LEAK AT LT WING BEHIND LANDING GEAR TRUNNION FITTING. THIS MRR RESUBMIT TO INCLUDE TRUNNION FUEL LEAK. REPAIRED IAW SMRO EO 99-35-01 TRUNNION FITTING REMOVED AND REPLACED DUE TO MECHANICAL DAMAGE.Nov 5, 1999 · N921UP · Boeing 727180C · Fuel Storage
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