Boeing 747-200

Service difficulty reports · 651

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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 = '747200'
  ORDER BY difficulty_date DESC"

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SDR UPS06446368Skin · corrodedBS 1240 LBL 90-94 WING CENTER SECTION SKIN UPPER SURFACE FOUND CORROSION. CORROSION BLEND OUT 0.078 X 3 X 3" EXCEED SRM 57-30-01 LIMIT. BS 1240 LBL 88.5-94 WING CENTER SECTION UPPER SKIN CORRODED AREA REPAIRED AS PER RS R57-14-35432 AND UPS EO B747-5710-2380Feb 2, 2006 · N522UP · Boeing 747200 · Fuselage Main, Plate/SkinSDR UPS06446324Stiffener · corrodedINSPECTION TYPE:C RIGHT BLG W/W TOP PANEL SUPPORT STIFFENER SURFACE CORROSION REVEALED AT STA 1403 RBL 96-98. CORROSION BLEND OUT 0.033 X 2 X 4 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT. SUPPORT STIFFENER REPAIRED AS PER SRM 51-40-04 FIG 1.Feb 2, 2006 · N522UP · Boeing 747200 · Fuselage Miscellaneous StructureSDR UPS06446219Skin · crackedINSPECTION TYPE:C NR 4 PYLON - SKIN / DOUBLER CRACKED FOUND 3EA FASTENER HOLES ON LEFT LWR EDGE BESIDE AFT UPPER ENG MOUNT FITTING NAC STA 220, (CRACK LENGTH .5 INCH). NR 4 PYLON LEFT LOWER EDGE SKIN REPAIRED AS PER SRM 54-34-03 FIG 24. AFTER STOP HOLES DRILFeb 2, 2006 · N522UP · Boeing 747200 · Nacelle/Pylon, Plate/SkinSDR UPS06446348Skin · corrodedAFT CARGO COMPT CARGO DOOR EXTERNAL SKIN SURFACE FOUND BILGE UP AT FWD MIDDLE ACCESS PNL FWD LOWER CUTOUT, CORROSION BLEND OUT 0.065" BY 2" BY 2". DOUBLER REPLACED AS PER SRM 51-10-01 PG 9 & INSTALLED AS PER SRM 51-30-02 AFTER CORROSION CLEANED AT THE MATING Feb 1, 2006 · N522UP · Boeing 747200 · Cargo/Baggage DoorsSDR UPS06446223Stiffener · crackedINSPECTION TYPE:C FX- AIR CONDITIONING BAY KEEL BEAM BOX RT EXTERNAL VERTICAL SURFACE ATT STIFFENER FOUND CRACKED AT STA 1000 RBL 9, CRACK LENGTH .5 INCH. FX- AIR CONDITIONING BAY KEEL BEAM BOX RT EXTERNAL VERTICAL SURFACE ATT STIFFENER REPLACED PER SRM 51-10Feb 1, 2006 · N522UP · Boeing 747200 · Fuselage Miscellaneous StructureSDR UPS06446222Stiffener · crackedINSPECTION TYPE:C FX AIR CONDITIONING BAY KEEL BEAM BOX LT EXTERNAL VERTICAL SURFACE ATT STIFFENER FOUND CRACKED AT BS 1000 LBL 9, CRACK LENGTH .375 INCH. STIFFENER REPLACED AS PER SRM 51-10-01 PG 9 & INSTALLED AS PER SRM 51-30-02.Feb 1, 2006 · N522UP · Boeing 747200 · Fuselage Miscellaneous StructureSDR UPS06446321Doubler · crackedINSPECTION TYPE:C FX LWR FX LEFT EXTERNAL SKIN ATT DOUBLER FOUND CRACKED AT STA 250 STR 32L TO S33L NOSE L/G FWD CORNER, CRACK LENGTH 3 INCHES. FX BS 250 S41L NWW FWD CORNER CUTOUT SKIN & EXTERNAL DOUBLER REPAIRED AS PER HX RS R53-18-35439 AND REFER UPS ENGINJan 31, 2006 · N522UP · Boeing 747200 · Fuselage Main, Plate/SkinSDR UPS06446226Cargo Track · corrodedFWD CARGO COMPT, BS 830-970 RT I/B FLOOR TRACK FOUND CORRODED. CORROSION BLEND OUT 0.035" BY 0.5" BY 10"). FLOOR TRACK REPAIRED AS PER SRM 53-10-05 FIG 5, JUST AT RBL 25" BETWEEN BS 930 AND 970.Jan 31, 2006 · N522UP · Boeing 747200 · Fuselage, Seat/Cargo Attach FittingsSDR UPS06446039Web · crackedINSPECTION TYPE:C NR 3 PYLON REAR MOUNT B/H FWD AND AFT OB FRAME WEB FOUND CRACKS. ( FWD FRAME .3125 INCH AND 1.375 INCHES ) ( AFT FRAME .1875 INCH AND 1INCH ) NR 3 PYLON REAR MOUNT B/H REPAIRED IAW HX RS NR R54-53-35416 AND UPS ENGINEERING FILE NR 747-54-20Jan 4, 2006 · N520UP · Boeing 747200 · Nacelle/Pylon, Main FrameSDR UPS06445940Stiffener · crackedINSPECTION TYPE:C NWW RT SIDE WALL PANEL BS 320-340 5TH (COUNT FROM TOP) STIFFENER FOUND CRACK AS RADIUS APPROX 5/8" LONG. NWW RT SIDEWALL PANEL BS 320-340 5TH STIFFENER REPLACED IAW SRM 51-10-01 PG 9.Jan 4, 2006 · N520UP · Boeing 747200 · Fuselage Miscellaneous StructureSDR UPS06446040Panel · blisteredINSPECTION TYPE:C RHW - IB MID FLAP LWR FLAP FOUND BULGED UP AT 95 INCHES - 135 INCHES FROM IB SIDE AS MARKED. TIME LIMITED REPAIR ACCOMPLISHED IAW HX RS NR R-57-55-35418 AND UPS EO NR B747-5750-23648-A.Dec 31, 2005 · N520UP · Boeing 747200 · Wing, Control SurfacesSDR UPS06446041Skin · corrodedINSPECTION TYPE:C FWD CARGO DOOR EXTERNAL SURFACE NR 821FR ACCESS PANEL CUTOUT AREA BILGE UP AT UPPER HALF TOP AREA. CORROSION BLEND OUT 0.070 INCH X 1INCH X 4 INCHES FWD CARGO DOOR NR 821FR ACCESS PANEL CUTOUT INTEGRAL FLANGE TRIMMED OUT AND REPAIRED IAW HX RDec 30, 2005 · N520UP · Boeing 747200 · Cargo/Baggage DoorsSDR WRNA20050028Fuse · blownTAKEOFF WARNING WENT OFF AT 140 KTS. ABORTED TAKEOFF. NR1,3,5,6, AND 7 MLG WHEEL ASSY'S THERMAL FUSE PLUG DISCHARGED AFTER RETURNING TO GATE. FREIGHT REMOVED FROM AIRCRAFT. PERFORMED TAKEOFF WARNING SYSTEM CHECK IAW 31-26-00 PGS 101 AND 501. SYSTEM OPS NORMALDec 1, 2005 · N524UP · Boeing 747200 · Wheel/Ski/FloatSDR UPS05445810Thrust Link · crackedINSPECTION TYPE:AD NR 2 ENG REF TAR FORM S/N: 115643 - UPS REQUEST REPLACEMENT OF THRUST LINK. NR 2 ENG THRUST LINK REPLACED AND BOTH ATTACH BOLTS REPLACED AS PER AMM 71-21-03.Nov 19, 2005 · N521UP · Boeing 747200 · Nacelle/Pylon, Main FrameSDR UPS05445809Thrust Link · crackedINSPECTION TYPE:AD NR 4 PYLON REAR ENGINE MOUNT THRUST LINK AFT LUG FOUND CRACK INDICATION AT UPPER AND LOWER SURFACE APPROX 100 PERCENT FSH. NR 4 ENG MOUNT THRUST LINK REPLACED AS PER AMM 71-21-03.Nov 19, 2005 · N521UP · Boeing 747200 · Nacelle/Pylon, Main FrameSDR UPS05445808Thrust Link · crackedINSPECTION TYPE:AD CRACK INDICATION REVEALED ON NR 3 PYLON THRUST LINK AFT LUG LOWER SURFACE BY APPROX 90 PERCENT FSH. NR 3 ENG PYLON THRUST LINK REPLACED AND AFT MOUNTING BOLT REPLACED AS PER AMM 71-21-03.Nov 18, 2005 · N521UP · Boeing 747200 · Nacelle/Pylon, Main FrameSDR UPS05445807Thrust Link · crackedINSPECTION TYPE:AD CRACK INDICATION REVEALED ON NR 3 PYLON THRUST LINK FWD LUG LOWER SURFACE BY APPROX 60 PERCENT FSH. NR 3 ENG THRUST LINK REPLACED AND AFT MOUNT BOLT REPLACED AS PER AMM 71-21-03.Nov 18, 2005 · N521UP · Boeing 747200 · Nacelle/Pylon, Main FrameSDR UPS05445806Thrust Link · crackedINSPECTION TYPE:AD CRACK INDICATION REVEALED NR 1 PYLON THRUST LINK AFT LUG LOWER SURFACE BY APPROX 90 PERCENT FSH. NR 1 PYLON THRUST LINK REPLACED AND FWD AND AFT MOUNT BOLTS REPLACED AS PER AMM 71-21-03.Nov 18, 2005 · N521UP · Boeing 747200 · Nacelle/Pylon, Main FrameSDR UPS05445805Thrust Link · crackedINSPECTION TYPE:AD CRACK INDICATION REVEALED ON NR 1 PYLON THRUST LINK FWD LUG LOWER SURFACE BY APPROX 80 PERCENT FSH. NR 1 PYLON THRUST LINK REPLACED AND FWD AND AFT MOUNT BOLTS REPLACED AS PER AMM 71-21-03.Nov 18, 2005 · N521UP · Boeing 747200 · Nacelle/Pylon, Main FrameSDR WRNA200050026Cowling · missingUPON LANDING AT SKBO, POST FLIGHT REVEALED THAT NR 1 ENGINE REVERSER COWLING MISSING.Nov 5, 2005 · N524UP · Boeing 747200 · Engine Thrust ReverserSDR UPS05445406Windshield · delaminatedINSPECTION TYPE:N/A F/O R1 WINDOW HAS CHIPPING AND CRACKING IN MAIN GLASS PLIES. COMPLETED R1 REMOVAL & INSTALLED NEW R1 REF TO MM 56-11-01 UP TO STEP 6.D. FIRST TORQUE COMPLETED. ITEM STEPS 6D THRU J NEED TO BE C/W. STEPS ARE FOR INSTALLATION OF SEALANT. Sep 12, 2005 · N523UP · Boeing 747200 · Flight Compartment WindowsSDR L0FR200500006Wheel · crackedCRACKED KEY BOSS IDENTIFIED WITH EDDY CURRENT PER HONEYWELL COMPONENT MAINTENANCE MANUAL 32-45-12 APPENDIX A, KEY BOSS NDT INSPECTION AREA.May 24, 2005 · Boeing 747200 · Wheel/Ski/FloatSDR L0FR200500005Wheel · crackedCRACKED KEY BOSS IDENTIFIED PER HONEYWELL CMM 32-45-12, APPENDIX A, KEY BOSS INSPECTION AREA. CRACKED IDENTIFIED USING EDDY CURRENT.Apr 28, 2005 · Boeing 747200 · Wheel/Ski/FloatSDR L0FR200500003Wheel · crackedINBOARD WHEEL HALF CRACKED AT TORQUE LUG KEY BOSS.Apr 22, 2005 · Boeing 747200 · Wheel/Ski/FloatSDR L0FR200500004Wheel · crackedINBOARD WHEEL HALF CRACKED AT TORQUE LUG KEY BOSS.Apr 22, 2005 · Boeing 747200 · Wheel/Ski/FloatSDR UPS05444353Fitting · crackedINSPECTION TYPE:C RIGHT BS 1480 B/H NR 16 HOLE FOUND CRACK AT OUTER CHORD SPLICE FITTING RUNNING OUTBOARD APPROX 0.030 INCH LONG (CRACK LENGTH 0.030 INCH). RIGHT BS 1480 B/H NR 16 HOLE OVERSIZED TO 0.406 INCH & CRACK FREE AS PER EO B747-5310-10732.Apr 14, 2005 · N523UP · Boeing 747200 · Fuselage Main, BulkheadSDR UPS05444352Frame · crackedINSPECTION TYPE: C, RT BS 1480 BULKHEAD NR 11 HOLE FOUND CRACK AT BULKHEAD FRAME RUNNING AFT APPROX 0.040 INCH LONG (CRACK LENGTH .0625 INCH). RIGHT BS 1480 B/H NR 11 HOLE OVERSIZED TO 0.562 INCH & CRACK FREE AS PER EO B747-5310-10732.Apr 14, 2005 · N523UP · Boeing 747200 · Fuselage Main, FrameSDR UPS05444346Skin · crackedINSPECTION TYPE:C LT BS 1480 BHD NR 11 HOLE FOUND CRACK AT FUSELAGE SKIN THROUGH THICKNESS RUNNING FWD ( CRACK LENGTH 0.325 INCH ). BS 1480 LT STR 32 TO STR 34 AREA SKIN REPAIRED AS PER SB 747-53A2390 FIG 28Apr 14, 2005 · N523UP · Boeing 747200 · Fuselage Main, Plate/SkinSDR UPS05444372Stringer Clip · corrodedINSPECTION TYPE: C, BS 1600 LT STR 3L TIE CLIP FOUND CORRODED. CORROSION BLEND OUT 0.021 X 1 X 3 INCH EXCEED SRM LIMITS. TIE CLIP REPLACED AT BS 1600 STR 3L AS PER SRM 51-10-01 PG 9.Apr 11, 2005 · N523UP · Boeing 747200 · Fuselage Main, Attach FittingsSDR UPS05444359Stringer Clip · corrodedINSPECTION TYPE: C - BS 1500, STR 3R, FRAME TIE CLIP FOUND CORROSION. CORROSION BLEND OUT 0.029 X 0.5 X 0.5 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS, TIE CLIP REPLACED AS PER SRM 51-10-01 PG 9.Apr 11, 2005 · N523UP · Boeing 747200 · Fuselage Main, Attach FittingsSDR UPS05444358Stringer Clip · corrodedINSPECTION TYPE: C- BS 1460 STR 6R FRAME TIE CLIP FOUND CORROSION. CORROSION BLEND OUT 0.010 X 0.5 X 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. TIE CLIP REPLACED AS PER SRM 51-10-01 PG 9.Apr 11, 2005 · N523UP · Boeing 747200 · Fuselage Main, Attach FittingsSDR UPS05444357Stringer Clip · corrodedINSPECTION TYPE:C M/D- BS 1416 STR -1R FRAME TIE CLIP FOUND CORROSION. CORROSION BLEND OUT 0.020 X 0.5 X 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. TIE CLIP REPLACED AS PER SRM 50-10-01 PG 9.Apr 11, 2005 · N523UP · Boeing 747200 · Fuselage Main, Attach FittingsSDR UPS05444354Seat Track · corrodedINSPECTION TYPE: C, BS 740 RBL 9 SEAT TRACK CORRODED. CORROSION BLEND OUT 0.020 X 2 X 2 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT, SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 4.Apr 11, 2005 · N523UP · Boeing 747200 · Fuselage, Seat/Cargo Attach FittingsSDR UPS05444347Strap · crackedINSPECTION TYPE:C M/D BS 1680 BETWEEN STR 11-12R FRAME O/B CHORD ATT STRAP FOUND CRACK ( CRACK LENGTH .3125 INCH). M/D BS 1680 BETWEEN STR 5R TO STR 12R FRAME ATTACH STRAP REPLACED AS PER SRM 51-10-01 PG 9Apr 11, 2005 · N523UP · Boeing 747200 · Fuselage Miscellaneous StructureSDR UPS05444429Retainer · corrodedINSPECTION TYPE:C FX - KEEL BEAM BOX LWR SUPPORT T-RETAINER FWD UPPER SURFACE FOUND CORROSION AT STA 1297 LBL 6 - RBL 6, CORROSION BLEND OUT 0.032 X .5 X 1.25 INCH, T-RETAINER REPLACED AS PER SRM 51-10-01 PG 9.Apr 10, 2005 · N523UP · Boeing 747200 · Fuselage Miscellaneous StructureSDR UPS05444360Stringer Clip · corrodedINSPECTION TYPE: C, STA 2100 STR 5R TIE CLIP CORROSION FOUND. CORROSION BLEND OUT 0.012 X 0.5 X 0.5 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. TIE CLIP REPLACED AS PER SRM 51-10-01 PG 9.Apr 10, 2005 · N523UP · Boeing 747200 · Fuselage Main, Attach FittingsSDR UPS05444356Stringer Clip · corrodedINSPECTION TYPE:C M/D - STA 1980 STR 4R TIE CLIP CORROSION FOUND. CORROSION BLEND OUT 0.016 X 2 X 2 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT. TIE CLIP REPLACED AS PER SRM 51-10-01 PG 9.Apr 10, 2005 · N523UP · Boeing 747200 · Fuselage Main, Attach FittingsSDR UPS05444349Clip · crackedINSPECTION TYPE:C M/D BS 400 S14L INTERCOSTAL AFT SUPPORT CLIP FOUND CRACKED ( CRACK LENGTH .125 INCH). M/D BS 400 STR 14L INTERCOSTAL AFT SUPT CLIP REPLACED AS PER SRM 51-10-01 PG 9Apr 9, 2005 · N523UP · Boeing 747200 · Fuselage Miscellaneous StructureSDR UPS05444348Strap · crackedINSPECTION TYPE:C LT BS 2231 FRAME INNER CHORD AREA FOUND 1EA FASTENER HOLE AT STR 25L CRACKED AT STRAP. ( CRACK LENGTH 0.040 INCH). STRAP REPLACED AS PER SRM 51-10-01 PG 9Apr 8, 2005 · N523UP · Boeing 747200 · Fuselage Miscellaneous StructureSDR LOFR200500002Wheel · crackedCRACKED SPOKES IDENTIFIED DURING VISUAL INSPECTION.Apr 7, 2005 · Boeing 747200 · Wheel/Ski/FloatSDR LOFR200500001Wheel · crackedCRACKED KEY BOSS IDENTIFIED PER HONEYWELL CMM 32-45-12, APPENDIX A, KEY BOSS NDT INSPECTION AREA. CRACK IDENTIFIED USING EDDY CURRENT METHOD.Apr 7, 2005 · Boeing 747200 · Wheel/Ski/FloatSDR WRNA200500008Fitting · out of adjustUPPER DECK ESCAPE HATCH MADE A LOUD BANG AT 23,000 FT. UNABLE TO HEAR DUE TO ESCAPING AIR. AIRCRAFT RETURNED TO AIRFIELD. LANDING NORMAL. ADJUSTED BAYONET FITTING ON THE HATCH. INSPECTED HATCH INTERIOR AND EXTERIOR IAW 52-21-00. ALL CHECKS SATISFACTORY. Apr 3, 2005 · N524UP · Boeing 747200 · Emergency ExitsSDR WRNA200500001Cap · looseON CLIMB-OUT FROM MIA, NR 1 OIL QTY STARTED TO DECREASE RAPIDLY. DID A PRECAUTIONARY ENG SHUTDOWN OF NR 1 ENGINE FOR OIL QTY LOSS. RETURNED TO AIRFIELD, LANDING NORMAL. MAINTENANCE INSPECTED NR 1 ENG AND FOUND OIL TANK CAP NOT IN CLOSE POSITION. SERVICED EFeb 20, 2005 · N524UP · Boeing 747200 · Turbine Engine Oil SystemSDR UPS05443734Unknown · fumesAFTER TAKEOFF THERE WERE STRONG FUMES IN COCKPIT. CREW DECLARED AN EMERGENCY AND LANDED SAFELY IN SDF. RAN ALL 3 PACKS, NO DEFECTS NOTED. OK FOR CONTINUED SERVICEJan 26, 2005 · N522UP · Boeing 747200 · Air Distribution SystemSDR UPS05443758Battery Pack · inoperativeEMERGENCY LIGHTS INOP OVER R-1 DOOR. REPLACED BATTERY PACK PER MM 33-51-02.Jan 25, 2005 · N522UP · Boeing 747200 · Emergency LightingSDR UPS05443623Battery Pack · inoperativeINSPECTION TYPE:N/A EMERGENCY EXIT LIGHT OVER R1 DOOR INOP. REMOVED AND REPLACED BATTERY PACK ASSY AS PER AMM 33-51-04. OPS CHECK GOOD.Dec 31, 2004 · N522UP · Boeing 747200 · Emergency LightingSDR UPS04443605Battery Pack · dischargedINSPECTION TYPE:N/A EXIT SIGN AT UPPER DECK EMERGENCY EXIT IS INOP AND MARKED AS DEACTIVATED. REMOVED DEACTIVATED LABEL, NO POWER AT EXIT SIGN REQUIRES FURTHER T/S. REPLACED BATTERY PACK IAW B747 MM 33-51-04, OPS CHECK GOOD.Dec 12, 2004 · N522UP · Boeing 747200 · Emergency LightingSDR L0FR200400005Wheel · crackedCRACKED KEY BOSS IDENTIFIED PER HONEYWELL COMPONENT MAINTENANCE MANUAL 32-45-12 APPENDIX A, KEY BOSS NDT INSPECTION AREA.Nov 18, 2004 · Boeing 747200 · Wheel/Ski/FloatSDR L0FR200400012Wheel · crackedFAILED BOLT HOLES ON OUTER RIM IDENTIFIED PER HONEYWELL COMPONENT MM 32-45-12 EDDY CURRENT PROCEDURES.Nov 18, 2004 · Boeing 747200 · Wheel/Ski/FloatSDR L0FR200400006Wheel · crackedCRACKED KEY BOSS IDENTIFIED PER HONEYWELL COMPONENT MAINTENANCE MANUAL 32-45-12 APPENDIX A, KEY BOSS NDT INSPECTION AREA.Nov 18, 2004 · Boeing 747200 · Wheel/Ski/Float
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