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 UPS03440345Floor Support · corrodedINSPECTION TYPE: C U/D - FLOOR SUPPORT FOUND HEAVY CORROSION. FLOOR SUPPORT ANGLE REPLACED AS PER SRM 51-10-01 PG 8. (DEPTH 0.060 INCH, WIDTH 1 INCH, LENGTH 2 INCH).Mar 4, 2003 · N520UP · Boeing 747200 · Fuselage Miscellaneous StructureSDR UPS03440342Strap · crackedINSPECTION TYPE: C, CRACKS FOUND AT BS 2231 RT INBOARD ATTACHED STRAP, THE CRACKS RUNNING FWD AND AFT DIRECTION OF ONE EACH FASTENER HOLE AND CRACKED THROUGH THICKNESS. M/D - RIGHT BS 2231 STR 24-25 REVEAL PANEL STRAP REPAIRED AS PER SRM 53-10-04 FIG 115.Mar 4, 2003 · N520UP · Boeing 747200 · Fuselage Main, StructureSDR UPS03440333Bracket · crackedINSPECTION TYPE:C FWD CRACKS WITH THROUGH THICKNESS FOUND AT ONE EACH FASTENER HOLE AT TIE CLIP AT THE I/B CHORD AT STR 25L OF BS 2231. TIE CLIP REPLACED AT BS 2231 STR 25L AREA AS PER SRM 51-10-01 PG.8.Mar 4, 2003 · N520UP · Boeing 747200 · Fuselage Main, StructureSDR UPS03440326Seat Track · corrodedINSPECTION TYPE:C U/D SEAT TRACK FOUND HEACY CORR AS MARKED. CORROSION BLEND OUT 0.055"X1"X3" SEAT TRACK REPLACED AT U/D BS 480 - BS 530RBL 65 AS PER SRM 51-10-01 P.8.Mar 4, 2003 · N520UP · Boeing 747200 · Fuselage, Seat/Cargo Attach FittingsSDR UPS03440252Skin · crackedINSPECTION TYPE:ASV NR 4 ENGINE PYLON CRACKED ON I/B SIDE. CRACK IN NR 4 ENG PYLON INBD SIDE AFT OF SLOT SEAL COMING FROM TOP SIDE OF PREVIOUS DOUBLER. REMOVED EXISTING DOUBLER FROM A/C 75705 03/04/03, REPAIRED PER EO B747-5430-18401-A. NEW DOUBLER REPAIR IMar 4, 2003 · N528UP · Boeing 747200 · Nacelle/Pylon, Plate/SkinSDR P5CA0300772Compressor · stalledAT FLT LEVEL 19.0 WHEN THRUST LEVER WAS RETARDED NR 3 ENG COMPRESSOR STALLED. REMOVED AND REPLACED FLOW DIVIDER AND SECURE PT 2 LINE. OPERATIONAL CHECK OK ON ENGINE RUN UP. APPARENT FAILURE OF ENG BLEED SYSTEM ON DESCENT WHEN THROTTLE WAS RETARDED.Mar 4, 2003 · N524UP · Boeing 747200 · Compressor Bleed ValveSDR UPS03440398Bracket · corrodedINSPECTION TYPE: C, LT MLG WW - BS 1241 LBL 1 TO 8 HORIZONTAL BRACKET FOUND CORROSION CRACKED. CORROSION BLEND OUT 0.050 X 1 X 1 INCH EXCEED SRM LIMIT. BRACKET REPLACED AS PER SRM 51-10-01 PAGE 8 TOTALLY 2 EA (P/N: 65B82011-3 AND 69B11570-1).Mar 2, 2003 · N520UP · Boeing 747200 · Fuselage Main, Attach FittingsSDR UPS03440393Skin · crackedINSPECTION TYPE: C, AFT LOWER CARGO DOOR CUTOUT UPPER CORNERS TWO FASTENER HOLES FOUND CRACK REVEALED FWD CORNER CRACKED HOLE AT SKI AND BEAR STRAP LAYER. AFT CORNER CRACKED HOLE AT BEAR STRAP LAYER. FOR DETAIL PLS REFER ATTACHED SKETCH. FWD UPPER CORNER RMar 2, 2003 · N520UP · Boeing 747200 · Fuselage Main, Plate/SkinSDR UPS03440235Module · inoperativeEMERGENCY LIGHTS UNARMED ANNUNCIATOR INOPERATIVE. RELAMPED, NO HELP. REPLACED EMERGENCY LIGHT MODULE ASSY, OPS CHECK OK.Feb 24, 2003 · N523UP · Boeing 747200 · Emergency LightingSDR UPS03440187Skin · crackedINSPECTION TYPE:PFLT NR 3 ENG PYLON INBOARD SIDE AFT ENG MOUNT ACCESS CUT PANEL PREVIOUS DOUBLER HOLE CHAFED THROUGH, HOLE CHAFED APPROX 2 INCHES AFT OF CUTOUT. REMOVED PREVIOUS REPAIR TO INBOARD SIDE OF PYLON. REPAIRED ACCESS DOOR/TAB SPACER,REMOVED FASTENEFeb 14, 2003 · N528UP · Boeing 747200 · Nacelle/Pylon, Plate/SkinSDR UPS03440193Angle · crackedINSPECTION TYPE:C CRACK REVEALED AT PASSENGER DOOR #5R AT THE DOOR FRAMES FWD BOTTOM CORNER VERTICAL RADIUS, THE CRACK RUNNING UPWARD WITH LENGTH 2.5" LONG APPROX. DOOR FWD ANGLE INSTALLED AS PER SRM 52-10-02 FIG.10Feb 6, 2003 · N522UP · Boeing 747200 · Passenger/Crew DoorsSDR UPS03440177Frame · crackedINSPECTION TYPE:C CRACK REVEALED AT PASSENGER DOOR #1R AT THE DOOR FRAMES FWD BOTTOM CORNER VERTICAL RADIUS. THE CRACK RUNNING UPWARD WITH LENGTH 3" LONG APPROX. AND A STOP HOLE DRILLED AT UPPER CRACK END. #1R DOOR FWD VERTICAL FRAME CRACKED AT RADIUS PREFeb 6, 2003 · N522UP · Boeing 747200 · Passenger/Crew DoorsSDR UPS03440176Skin · crackedINSPECTION TYPE:C DURING PATCH N522UP-46-08 BTN BS 1935-1945 STR 43L-45L REMOVED SHORT EDGE MARGIN FOUND BTN FASTENER & CUT OUT ABOUT 0.280" REPAIR AGAIN REQUIRED. FX - BS 1935-1945 STR 43L-45L SKIN REPAIRED AS PER SRM 53-30-03 FIG.1.Feb 6, 2003 · N522UP · Boeing 747200 · Fuselage Main, Plate/SkinSDR UPS03440229Fitting · corrodedINSPECTION TYPE: C, LT WING REAR SPAR KICK FITTING AREA, CORROSION FOUND ON HOLE-D AT TERMINAL FITTING. D-HOLE REWORK AS PER EO B747-5710-18343A AND RS 57-12-34973.Feb 4, 2003 · N522UP · Boeing 747200 · Wing SparSDR UPS03440228Fitting · crackedINSPECTION TYPE: C, RIGHT BS 1241 WING REAR SPAR KICK FITTING, HOLE D-CORROSION CRACK FOUND APPROX 0.040 INCH RUNNING I/B FWD SURFACE. D-HOLE REWORKED AS PER EO B747-5710-12138 AND EO B747-5710-18343A RS 57-12-34973.Feb 4, 2003 · N522UP · Boeing 747200 · Wing SparSDR UPS03440227Stringer · corrodedINSPECTION TYPE:C FX - LOWER FUSELAGE INTERIOR STRUCTURE ATT STRINGER FOUND HEAVY CORROSION AT STA 2340 TO STA 2360 STR 50R. STRINGER CUT OFF AND REPROTECTED AS PER SRM 51-10-01 AND SRM 51-10-0 2. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1. TIE CLIP REPLACFeb 4, 2003 · N522UP · Boeing 747200 · Fuselage Main, Longeron/StringerSDR UPS03440241Flap Track · corrodedINSPECTION TYPE: C, LEFT WING - NR 3 FLAP TRACK AFTER END INNER SURFACE I/B WALL AREA FOUND CORROSION (FINDING AFTER PIVOT FITTING REMOVAL). LEFT WING NR 3 FLAP TRACK AFT END INNER SURFACE INBD WALL AREA CORROSION REMOVED AND REPROTECTED REFER CWS SERIAL NR Jan 31, 2003 · N522UP · Boeing 747200 · Trailing Edge FlapsSDR UPS03440181Angle · crackedINSPECTION TYPE: C M/D, R4 DOOR AFT UPPER CORNER FOUND CRACKED (AS MARKED). M/D - R4 DOOR AFT UPPER CORNER REPAIRED AS PER SRM 51-10-02 FIG 10.Jan 31, 2003 · N522UP · Boeing 747200 · Fuselage Miscellaneous StructureSDR UPS03440145Frame · crackedINSPECTION TYPE: C, M/D - BS 1840 BETWEEN STR 12R AND 14R ATT FRAME FOUND CRACKED. BS 1840 BETWEEN STR 12R AND 14R FRAME I/B CRACKED AREA REPAIRED PER SRM 53-10-04 FIGURE 87.Jan 31, 2003 · N520UP · Boeing 747200 · Fuselage Main, FrameSDR UPS03440180Skin · crackedINSPECTION TYPE: C M/D, L4 DOOR FUSELAGE CUTOUT REVEAL FOUND CRACKED AT BS 1664 BELOW STR 24. M/D- L4 DOOR FUSELAGE CUTOUT REVEAL PANEL REPLACED AS PER SRM 51-10-01, JUST AT BS 1664 BELOW STR-24.Jan 30, 2003 · N522UP · Boeing 747200 · Fuselage Main, Plate/SkinSDR UPS03440179Skin · crackedINSPECTION TYPE: C M/D, R4 DOOR FUSELAGE CUTOUT REVEAL FOUND CRACKED BELOW STR 24. M/D - R4 DOOR FUSELAGE CUTOUT REVEAL PANEL REPLACED AS PER SRM 51-10-01, JUST AT BS 1664 BELOW STR 24.Jan 30, 2003 · N522UP · Boeing 747200 · Fuselage Main, Plate/SkinSDR UPS03440178Skin · crackedINSPECTION TYPE: C M/D, R2 DOOR FUSELAGE CUTOUT REVEAL FOUND CRACKED AT BS 805 BELOW STR 24. M/D - R2 DOOR FUSELAGE CUTOUT REVEALED PANEL REPLACED AS PER SRM 51-10-01, JUST AT BS 805 BELOW STR 24.Jan 30, 2003 · N522UP · Boeing 747200 · Fuselage Main, Plate/SkinSDR UPS03440242Skin · bulgedINSPECTION TYPE: C M/D, BS 2360 BULKHEAD SKIN TO Y-RING FOUND BULGED UP AT STR 51L. BULKHEAD SKIN REPAIRED AS PER RS NR R53-83-34972 AND FX SKIN REPAIRED AT BS 2360 - 2370 BETWEEN S46L TO S46R AS PER SRM 53-10-04 FIG 5 DETAIL V, REF EO B747-5310-18355-A. TRJan 29, 2003 · N522UP · Boeing 747200 · Fuselage Main, Plate/SkinSDR UPS03440245Angle · corrodedINSPECTION TYPE: C FX, KEELBEAM BOX INTERIOR LONGER FRAME FOUND HEAVY CORROSION AT LT SIDE STA 1465 TO STA 1475 LBL 6 TO LBL 8. REPAIRED ANGLE FABRICATED AS PER HX RS R53-49-34970 AND EA 747-53-20123. BLEND OUT 0.079 X 2.4 X 4 INCH.Jan 28, 2003 · N522UP · Boeing 747200 · Fuselage Main, KeelSDR UPS03440244Angle · corrodedINSPECTION TYPE: C FX, KEEL BEAM BOX INTERIOR LOWER FRAME RT SIDE FOUND HEAVY CORROSION AT STA 1460 TO STA 1470 RBL 6 TO RBL 9. REPAIRED ANGLE FABRICATED AS PER HX RS R53-49-34970 AND EA 747-53-20123. BLEND OUT 0.146 X 2.4 X 3 INCH.Jan 28, 2003 · N522UP · Boeing 747200 · Fuselage Main, KeelSDR P5CA0300747Flap · crackedCRACK, 1" LONG, IN O/B AFT FLAP, INBD SIDE, 4" FROM AFT EDGE. REPAIR CARRIED OUT IAW SRM 51-40-14, FIG. 10.Jan 28, 2003 · N524UP · Boeing 747200 · Trailing Edge FlapsSDR P5CA0300746Cap · crackedNR 4 PYLON WING KNEE-PAD (NU-CAP) PANEL TRAILING EDGE FASTENER HOLE BROKEN OUT. REPAIRED AND FILLED AREA, RE-DRILLED HOLE AND PROTECTED IAW SRM 51-40-00.Jan 26, 2003 · N524UP · Boeing 747200 · Nacelle/Pylon, Plate/SkinSDR UPS03440146Skin · corrodedINSPECTION TYPE:C FX - LOWER FUSELAGE EXTERNAL SKIN EDGE FOUND CORRROSION CRACKED AT STA 983 STRG 42L. FX - LOWER FUSELAGE STA 975 TO STA 987 S42L EXTERNAL SKIN REPAIRED AS PER SRM 53-30-03 FIG.1.Jan 24, 2003 · N520UP · Boeing 747200 · Fuselage Main, Plate/SkinSDR UPS03440005Battery Pack · inoperativeINSPECTION TYPE: PFLT, EMERGENCY EXIT SIGN ABOVE ESCAPE SLIDE DOOR INOP. REMOVED AND REPLACED BATTERY PACK. OPS CHECK OK.Jan 8, 2003 · N522UP · Boeing 747200 · Emergency LightingSDR UPS02439990Light · inoperativeINSPECTION TYPE:PFLT EMERG LIGHTS UNARMED LIGHT INOP RELAMPED. OPS CK GOOD.Dec 19, 2002 · N520UP · Boeing 747200 · Emergency LightingSDR P5CA0200710Light · inoperativeUPPER DECK FWD EMERGENCY LIGHT WOULD NOT STAY ILLUMINATED. REPLACED EMERGENCY LIGHT ASSY & OPERATIONS RETURNED TO NORMAL.Dec 3, 2002 · N524UP · Boeing 747200 · Emergency LightingSDR S02234040Transponder · failedBOTH ATC TRANSPONDER FAILED LIGHT ILLUM. BEFORE T/O. ATC CONTROL PANEL REPLACED NR 2 ATC NML IAW 34-53-00 T/S BUT NR 1 ATC STILL NO GOOD IAW MEL 34-26 SAFE FOR FLIGHT,ITEM C/F TO D/D PAGE D0045481 CAT "C". THE ATC FRONT PANEL TEST SWITCH LOST THE BITE TEST Nov 17, 2002 · Boeing 747200 · ATC Transponder SystemSDR UPS02439915Battery Pack · inoperativeINSPECTION TYPE: PFLT, UPPER DECK CEILING EMERGENCY LIGHTS AT STA 590 AND STR 710 INOPERATIVE. R & R EMERGENCY LIGHT BATTERY PACK M335. OPS TEST NORMAL.Nov 16, 2002 · N520UP · Boeing 747200 · Emergency LightingSDR UPS02439914Wire · damagedINSPECTION TYPE: PFLT, UPPER DECK PASSENGER AREA 3 EA CEILING EMERGENCY LIGHTS INOP. REF L/P 914473, M249145. REPAIRED GROUND WIRE W894-L4734-20 PULLED FROM SOCKET CONTACT AT D5127P. TEST OK. THIS CLEARS M249145Nov 16, 2002 · N520UP · Boeing 747200 · Light System WiringSDR S02271039Oil System · lowNR 1 ENGINE OIL QUANTITY SHOW ZERO AND LOW OIL PRESS LIGHT ILLUMINATED DURING CLIMB. FLIGHT CREW DECIDED TO SHUT DOWN ENGINE IN FLIGHT. THEN DIVERT TO SINGAPORE. ENGINE REPLACED, WAITING SHOP INVESTIGATION.Nov 10, 2002 · Boeing 747200 · Turbine Engine Oil SystemSDR UPS02439902Skin · crackedINSPECTION TYPE: ASV NR 3 PYLON INBD SIDE AFT AND BELOW "TEXAS" DOUBLER PREVIUOS REPAIR SHO WS EVIDENCE OF CRACK EXTENDING UPWARD FROM REPAIR.(MARKED). VERIFIED END OF CRACK WITH HFEC G. BUCHERT QC 10445. REMOVED DOUBLER . HS 86801 11 10 02. STOPDRILLED CRACKNov 10, 2002 · N520UP · Boeing 747200 · Nacelle/Pylon, Plate/SkinSDR UPS02439846Wire · brokenINSPECTION TYPE:PFLT FOUND F/O EMERGENCY LIGHT INOP ON GLARESHIELD. R/R BULB NO HELP. FOUND WIRE W2032-WHT/BLU BROKEN. REPAIRED IAW WDM 33-13-11. OPS CHECK OKAY.Oct 31, 2002 · N521UP · Boeing 747200 · Light System WiringSDR P5CA0200706Rod · brokenDURING OFF LOADING OPERATIONS, LWR AFT CARGO DOOR EXPERIENCED AN OUT OF SEQUENCE CONDITION. UPON INSPECTION FOUND SEVEN ROD ASSYS HAD SHEARED & THE MOST FORWARD DOOR INSPECTION PANEL WAS DAMAGED. REMOVED & REPLACED ROD ASSYS & INSPECTION DOOR PANEL AS PER 52Oct 27, 2002 · N524UP · Boeing 747200 · Cargo/Baggage DoorsSDR S02252036Warning System · false activationB18771 SIDE CARGO DOOR DOOR WARNING LIGHT ILLUM. ON BOTH FORWARD AND F/E PANEL DURING TAKE-OFF PHASE. CHECKED OPEN/CLOSE MOVEMENT AND CLOSING/LOCKING DEVICES FOUND ALL OK. CLOSED AND LOCKED DOOR.Oct 26, 2002 · Boeing 747200 · Door Warning SystemSDR UPS02439805Battery Pack · dischargedINSPECTION TYPE: ASE UPPER DECK EMERGENCY EXIT DOOR SILL WOULD NOT ILLUMINATE DURING ASE CHECK REPLACED EMERGENCY LIGHT BATTERY PACK REF MM 33-51-04. LIGHT OPS CHECK GOOD.Oct 22, 2002 · N522UP · Boeing 747200 · Emergency LightingSDR UPS02439802Light · inoperativeINSPECTION TYPE:N/A MAIN CARGO DECK CEILING EMERGENCY LIGHT JUST OUTBD OF FWD ENTRY INOP ALSO FWD DOOR FRAME EMERG LIGHT INOP REMOVED AND REPLACED LT ASSY PER AMM33-51-04 AND RELAMPED LIGHT OPS CHECKS GOOD.Oct 17, 2002 · N520UP · Boeing 747200 · Emergency LightingSDR UPS02439795Light · inoperativeINSPECTION TYPE: ASV EMERGENCY LIGHT ON UPPER DECK ABOVE STAIRS INOP. RELAMPED OPS CHECKED GOOD.Oct 17, 2002 · N520UP · Boeing 747200 · Emergency LightingSDR P5CA0200703Fuel Cell · leakingDURING EXTENDED GROUND TIME, NOTICED FUEL SEEP/STAIN RT WING GEAR DOOR FWD EDGE. SEEP SEALED PER FSM 4-05-1 NR 3 MAIN KICK FITTING AREA. STAIN WIPED CLEAN. OK FOR SERVICE.Oct 11, 2002 · N524UP · Boeing 747200 · Fuel StorageSDR P5CA0200702Case · crackedEN ROUTE NR 2 ENG OIL DROPPED FROM 6.7 GALLONS TO 3.9 GALLONS BY TOC. OIL QTY CONTINUED TO DROP AT A RATE OF 1.4 GALLONS IN 1ST HOUR OF CRUISE. ALL OTHER PARAMETERS NORMAL. AN EMERGENCY WAS DECLARED, DIVERTED TO NRT. FUEL DUMP WAS PERFORMED TO LAND AT MAX Oct 7, 2002 · N524UP · Boeing 747200 · Turbine Engine Compressor SectionSDR UPS02439629Light · inoperativeESCAPE SLIDE EMERGENCY LIGHT INOP. TRANSFER TO MEL 25-11-1 CAT C PLACARD INSTALLED.Oct 7, 2002 · N521UP · Boeing 747200 · Emergency LightingSDR P5CA0200701Garlock Seal · leakingUSED 2 GALLONS OF ENG OIL ON NR 2 ENG IN 3.7 HOURS OF FLT. QTY LOSS TO 0.1 GALLONS INDICATED. NR 2 ENG OIL SYSTEM STATIC LEAK CHECKED IN HKG. TEST NR 6 CARRIED IAW AMM 71-00-00. FOUND GENERATOR DRIVE CARBON GARLOCK SEAL LEAKING. SEAL CHANGED IAW AMM 72-61Oct 6, 2002 · N524UP · Boeing 747200 · Turbine Engine Oil SystemSDR P5CA0200700Oil System · malfunctionedPRECAUTIONARY ENGINE SHUTDOWN OCCURRED AT 2250 DUE TO NR 2 OIL QTY DECREASED TO 0.1 GAL. INDICATED, FOLLOWED BY SLOW DECREASE IN OIL PRESSURE ALT PROCEDURES 6-15-9 & 6-15-11 C/W & ENGINE SECURED IAW 5-04-9. FL 390 FUEL APPROX 78.0. DISPATCH NOTIFIED, PROCEOct 5, 2002 · N524UP · Boeing 747200 · Turbine Engine Oil SystemSDR UPS02439771Wire Harness · burnedINSPECTION TYPE: C, FWD BOOST PUMP PRESS LIGHT ON , C/B CYCLES AND POPS PUMP C/B ON P14 PANEL; NR 1 & 3 BOOST PUMP PRESS LIGHT ON. FWD CGO CEILING AT STA 920 RBL 5 WIRING BUNDLES W220 & W842 ADJACENT T O NR 4 FWD BOOST PUMP FOUND BURNED WIRE AND POOR CONOct 4, 2002 · N528UP · Boeing 747200 · Fuel System WiringSDR UPS02439600Skin · puncturedHOLE PUNCTURED IN FUSELAGE SKIN FWD OF AFT LWR CARGO DOOR. BS 1790 - 1805 STR 37R TO STR 38 RT EXTERIOR SKIN REPAIRED AS PER SRM 53-30-03 FIG 1.Oct 1, 2002 · N528UP · Boeing 747200 · Fuselage Main, Plate/SkinSDR UPS02439539Light · inoperativeINSPECTION TYPE:AS EMERGENCY ENTRY LIGHT IN CEILING AT BOTTOM OF CREW STAIRS INOP. INSTALLED LIGHT BULBS OPS CHECK NORMAL.Sep 25, 2002 · N521UP · Boeing 747200 · Emergency Lighting
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