Boeing 747-259B

Service difficulty reports · 139

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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 = '747259B'
  ORDER BY difficulty_date DESC"

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SDR KCSA081619Light · inoperativeUPPER DECK EXIT DOOR EMERGENCY SILL LIGHTS ARE INOP.Dec 24, 2008 · N701CK · Boeing 747259B · Emergency LightingSDR KCSA081499Skin · damagedNR PYLON OTBD SKIN LOWER FASTERNER HOLES DAMAGED AT NAC 221.9. (K)Sep 30, 2008 · N701CK · Boeing 747259B · Nacelle/Pylon, Plate/SkinSDR KCSA081367Skin · damagedNR 4 PYLON INBOARD LOWER SKIN DAMAGED AT NAC STA 215. (S)Aug 3, 2008 · N701CK · Boeing 747259B · Nacelle/Pylon, Plate/SkinSDR KCSA081365Skin · crackedNR 3 PYLON SKIN OUTBOARD SIDE EXTENDING FROM DOUBLER CRACKED 3 INCHES. (A)Jul 31, 2008 · N701CK · Boeing 747259B · Nacelle/Pylon, Plate/SkinSDR KCSA081364Linkage · brokenESCAPE SLIDE RELEASE LINKAGE BROKEN ON LATCH SIDE (FWD). (A)Jul 31, 2008 · N701CK · Boeing 747259B · Escape SlideSDR KCSA081269Bulkhead · chafedNR 2 PYLON HYDRAULIC PRESSURE LINE BULKHEAD FITTING CHAFING AFT SIDE OF NAC STA 221.9 BULKHEAD.May 31, 2008 · N701CK · Boeing 747259B · Nacelle/Pylon, Bulkhead/FirewallSDR KCSA081029Skin · crackedNR 3 PYLON I/B SKIN HAS A CRACK AT AFT UPPER CORNER OF ACCESS PANEL OPENING AT NAC STA 208.Jan 20, 2008 · N701CK · Boeing 747259B · Nacelle/Pylon, Plate/SkinSDR KCSA071529Frame · damagedDAMAGED STRUCTURE BEHIND LT COUNTER BALANCE WHEEL FOR FLIGHT DECK STAIRS AT STA 460 TO 480, WL 305, LBL 35.Dec 5, 2007 · N701CK · Boeing 747259B · Fuselage Main, FrameSDR 061028Lamp · burned outRIGHT UPPER DECK SLIDE EMERGENCY LIGHT LAMP BURNED OUT.Mar 25, 2006 · N701CK · Boeing 747259B · Emergency LightingSDR P5CA0401025Actuator · failedMAIN SIDE CARGO DOOR WILL NOT LOCK. MOTOR RUNS BUT ACTUATOR DOES NOT TURN. CORRECTIVE ACTION TAKEN: REMOVED AND REPLACED LATCH ACTUATOR IAW AMM 52-32-09 OPERATION, INDICATION CK OK.Jan 10, 2004 · N924FT · Boeing 747259B · Cargo/Baggage DoorsSDR UPS03440023Bolt · brokenINSPECTION TYPE: C, CENTER TANK RIGHT FS 1241 AFT BULKHEAD FITTING ATT BOLT FOUND LEAKAGE AS MK. A 1.125 INCH DIAMETER BROKEN BOLT REPLACED AS PER MM 20-51-01 AND REFER CWS FOR WORK DETAIL.Jan 16, 2003 · N527UP · Boeing 747259B · FastenersSDR UPS03440040Clip · crackedINSPECTION TYPE:C M/D - BS 2200 STRINGER S25R TIE CLIP FOUND CRACK. BS 2200 STRINGER 25R TIE CLIP REPLACED AS PER SRM 51-10-01 P.8.Jan 7, 2003 · N527UP · Boeing 747259B · Fuselage Main, StructureSDR UPS03440016Beam · crackedINSPECTION TYPE:C NO.1R DOOR FWD VERTICAL BEAM LOWER CORNER FOUND CRACK AS MARKED. ANGLE REPLACED AND INSTALLED AS PER SRM 52-10-02 FIG.10.Jan 6, 2003 · N527UP · Boeing 747259B · Passenger/Crew DoorsSDR UPS03440015Beam · crackedINSPECTION TYPE:C NO.2R DOOR FWD VERTICAL BEAM LOWER CORNER FOUND CRACK AS MARKED. ANGLE REPLACED & INSTALLED AS PER SRM 52-10-02 FIG.10.Jan 6, 2003 · N527UP · Boeing 747259B · Passenger/Crew DoorsSDR UPS03440014Beam · crackedINSPECTION TYPE: C, NR 2L DOOR FWD VERTICAL BEAM LOWER CORNER FOUND CRACK AS MARKED. ANGLE REPLACED AS PER SRM 52-10-02 FIG 10.Jan 6, 2003 · N527UP · Boeing 747259B · Passenger/Crew DoorsSDR UPS03440012Panel · corrodedINSPECTION TYPE:C LH WLG BAY AREA MOST I/B SKIN PNL (TRIANGLE SHAPE) EDGE SHOCK STRUT DOOR CUTOUT EDGE SEAL RETAINER EDGE CORROSION FOUND AT 3 LOCATIONS. SEAL RETAINER SUPPORT REPAIRED AS PER SRM 51-40-03 FIG.2.Jan 5, 2003 · N527UP · Boeing 747259B · Wing, Plate/SkinSDR UPS03440010Floor Support · corrodedINSPECTION TYPE: C M/D - AFTER FLOOR PANEL REMOVED, FLOOR SUPPORT FOUND CORROSION AT BS 2280-2300 LBL 60. FLOOR SUPPORT REPLACED AS PER SRM 51-10-01 PG 8. DEPTH 0.035 INCH, WIDTH 1 INCH, LENGTH 3 INCHES.Jan 4, 2003 · N527UP · Boeing 747259B · Fuselage Miscellaneous StructureSDR UPS03440060Fitting · crackedINSPECTION TYPE:C LH BS 1480 B/H NO.24 HOLE CRACK AT OUTER CHORD SPLICE FITTING RUNNING O/B APPROX 5/32". REFER ATTACH SKETCH FOR DETAILS. DEFECTIVE HOLE REWORKED AS PER RS-53-43-34957 ISSUE 'B' AND EO B747-5310-18127-AJan 3, 2003 · N527UP · Boeing 747259B · Fuselage Main, StructureSDR UPS03440059Fitting · crackedINSPECTION TYPE:C RH BS 1480 B/H NO.17 HOLE CRACK AT OUTER CHORD SPLICE FITTING RUNNING O/B AND I/B APPROX 3/16" AND 0.040" RESPECTIVELY. REFER G ATTACH SKETCH FOR DETAILS. DEFECTIVE HOLE REWORKED AS PER RS 53-43-34957 ISSUE B AND EO B747-5310-18127-A.Jan 3, 2003 · N527UP · Boeing 747259B · Fuselage Main, StructureSDR UPS03440047Skin · crackedINSPECTION TYPE:C RH BS 1480 FX SKIN AT EXTENSION FTG AREA HOLE #12 TWO CRACKS FOUND THROUGH FOR DETAIL, PLS REF ATTACHED SKETCH. HOLE REWORKED AS PER RS R-53-43-34957 DUE EXCEEDED SB B747-53A2390 LIMIT. (REF EO B747-5310-18127-A FOR DETAIL INSTRUCTIONS).Jan 3, 2003 · N527UP · Boeing 747259B · Fuselage Main, Plate/SkinSDR UPS03440046Skin · crackedINSPECTION TYPE:C LH BS 1480 B/H NO.11 HOLE CRACK AT FX SKIN RUNNING FWD AD AFT AND THRU THICKNESS. REER ATTACH SKETCH FOR DETAILS. CRACKED FASTENER HOLE REWORK AS PER RS NO.R53-43-34957 DUE TO HOLE DIMENSION EXCEEDED SB REPAIR LIMIT. (REF EO B747-5310-181Jan 3, 2003 · N527UP · Boeing 747259B · Fuselage Main, Plate/SkinSDR UPS03440045Frame · crackedINSPECTION TYPE:C, RIGHT BS 1480 BULKHEAD NR 11 HOLE FOUND CRACK AT BULKHEAD FRAME RUNNING FWD AND AFT APPROX .0625 INCH AND THROUGH THICKNESS RESPECTIVELY. CRACKED FASTENER HOLE REWORKED AS PER RS NR R534334957 DUE TO DIMENSION OF HOLE EXCEEDED S/B REPAIR LIJan 3, 2003 · N527UP · Boeing 747259B · Fuselage Main, FrameSDR UPS03440044Fitting · crackedINSPECTION TYPE:N/A LH BS 1480 B/H NO.7 HOLE CRACK AT EXTENSION FTG RUNNING AFT UPWARD DIRECTION APPROX 1/16" LONG. REFER ATT SKETCH FOR DETAILS. HOLE REWORKED AS PER RS-53-43-34957 DUE EXCEEDED SB 747-53A2390 REPAIR LIMIT. (REF EO B747-5310-18127-A FOR DEJan 3, 2003 · N527UP · Boeing 747259B · Fuselage Main, StructureSDR UPS03440043Skin · crackedINSPECTION TYPE:C B/H BS 1480 BULKHEAD NO.11 HOLE CRACK AT FX SKIN RUNNING FWD AND AFT THROUGH THICKNESS. REFER ATTACH SKETCH FOR DETAILS. HOLE REWORKED AS PER RS-53-43-43957 DUE EXCEEDED SB 747-53A2390 REPAIR LIMIT. (REF EO B747-5310-18127-A FOR DETAIL INJan 3, 2003 · N527UP · Boeing 747259B · Fuselage Main, StructureSDR UPS03440042Fitting · crackedINSPECTION TYPE:C LH BS 1480 B/H NO.24 HOLE AT OUTER CHORD SPLICE FITTING RUNNING O/B APPROX 5/32" REFER ATTACH SKETCH FOR DETAILS. CRACKED FASTENER HOLE REAMED TO 0.530" AND BUSHING INSTALLED AS PER SB 747-53A2390 AND EO 747-5310-10732-H WITHIH PLAN 'A' LJan 3, 2003 · N527UP · Boeing 747259B · Fuselage Main, StructureSDR UPS03440070Bulkhead · corrodedINSPECTION TYPE:C LH WLG W/W FWD BULKHEAD WEB UPPER AREA BS 1241 LBL 60-100 CORROSION REVEALED. CORROSION REMOVED AND C/OUT REPAIR AS PER RS R57-12-34959. DEPTH 0.038, WIDTH 1", LENGTH 2".Jan 2, 2003 · N527UP · Boeing 747259B · Fuselage Main, StructureSDR UPS03440041Web · corrodedINSPECTION TYPE:C L/H WLG W/W FWD BULKHEAD WEB UPPER AREA BS 1241 LBL 60-100 CORROSION REVEALED. CORROSION REMOVED IAW SRM51-10-01, CORROSION DEPTH 0.038", WIDTH 1", LENGTH 2".Jan 2, 2003 · N527UP · Boeing 747259B · Fuselage Main, StructureSDR UPS03440011Skin · corrodedINSPECTION TYPE:C FX LOWER FUSELAGE, EXTERNAL SKIN EDGE FOUND HEAVY CORROSION AT STA 983 LH SIDE STG 41L TO STG 42L(2 LOCATIONS). SKIN REPAIRED AS PER SRM 53-30-03 FIG.1. (DEPTH 0.063", WIDTH 2", LENGTH 4")Dec 31, 2002 · N527UP · Boeing 747259B · Fuselage Main, Plate/SkinSDR UPS02439916Light · inoperativeINSPECTION TYPE:PFLT 1 EMERGENCY LT INOP UPPER DECK JUST FWD OF JUMPSEATS ON CEILING. RELAMPED. OPS CK OK.Nov 16, 2002 · N527UP · Boeing 747259B · Emergency LightingSDR UPS02439008Terminal · looseINSPECTION TYPE:N/A OUTBOARD FLAPS WOULD NOT EXTEND. SECURED TERMINALS 6 & 7 OF TB 258 AND TERMINAL 11 OF TB 259 IN J42, REPLACED S1404 GL 51752, S329, S339, PER MM 27-51-07. CYCLED FLAPS, NO MALFUNCTIONS FOUND.Aug 6, 2002 · N527UP · Boeing 747259B · Trailing Edge Flap Control SystemSDR UPS02438644Brake · malfunctionedINSPECTION TYPE:N/A AUTOBRAKES DISENGAGED IMMEDIATELY AFTER TOUCHDOWN. PERFORMED AUTO BRAKES ADJUSTMENT TEST AS PER MM 34-43-00 NO DEFECTS NOTED.Jun 18, 2002 · N527UP · Boeing 747259B · Landing Gear Brake SystemSDR UPS02438575Lens · crackedINSPECTION TYPE:N/A LENS CRACKED ON DOME LIGHT AT UPPER DECK EMERGENCY EXIT. REMOVED AND REPLACED LIGHT ASSY.Jun 10, 2002 · N527UP · Boeing 747259B · Emergency LightingSDR UPS02438509Seat Track · shearedINSPECTION TYPE:N/A CAPT SEAT TRACK STOP SHEARED OFF REF D238709 AND M238705 AND REQ A238705. CAPTS SEAT ELECTRICAL CHORD ISNTALLED AND ELECTRIC OPERATION NORMAL AT THIS TIME, THIS CLEARS M238705 R&R LT SEAT TRACK ASSY. (CAPT'S) (AFT OTBD) OPS NORMAL AT THIS Jun 1, 2002 · N527UP · Boeing 747259B · Fuselage, Seat/Cargo Attach FittingsSDR UPS02438280Fuse · not seatedINSPECTION TYPE:N/A EMERGENCY LIGHT INOP ON UPPER DECK. RESEATED FUSES IN PS, OPS NORMAL.May 16, 2002 · N527UP · Boeing 747259B · Emergency LightingSDR UPS02438229Fuse · not seatedINSPECTION TYPE:N/A EMERGENCY EXIT LIGHT AT FWD PART OF UPPER DECK IS INOP. RESEATED FUSES IN POWER SUPPLY. OPS NORMAL PER MM 33-51-00.May 11, 2002 · N527UP · Boeing 747259B · Emergency LightingSDR UPS01437353Light · inoperativeINSPECTION TYPE:N/A TWO EMERGENCY LIGHTS INOP. (CAPTS/CENTER) RELAMPED LIGHTS IAW MM 33-10-00 CK OK.Dec 5, 2001 · N527UP · Boeing 747259B · Emergency LightingSDR UPS01436854Fuel Line · chafedINSPECTION TYPE:N/A NR 4 ENGINE HAS FUEL LEAK - TUBES TAGGED - CHAFED WITH ANOTHER TUBE. REMOVED TWO CHAFED LINES KLS 82050 INSTALLED SERVICEABLE FUEL SIGNAL TUBE ASSY AND INSTALLED SERVICEABLE DRAIN TUBE ASSY PER AMM 30-10-10 LEAK CHECK GOOD.Sep 25, 2001 · N527UP · Boeing 747259B · Engine Fuel DistributionSDR UPS01436030Battery Pack · dischargedINSPECTION TYPE:N/A, EMERGENCY LIGHT INOP IN UPPER DECK MOST AFT LIGHT. RELAMPED, NO HELP. REPLACED EMERGENCY EXIT LIGHT BATTERY PACK AND CKS GOOD.Jun 8, 2001 · N527UP · Boeing 747259B · Emergency LightingSDR UPS01435450Skin · crackedINSPECTION TYPE:C, LEFT HORIZONTAL STAB L/E. IS CRACKED AT L/E. STA. 360 REPAIRED SKIN I.A.W. SRM. 55-10-03 FIG. 1Mar 26, 2001 · N527UP · Boeing 747259B · Horizontal Stabilizer, Plate/SkinSDR UPS01435351Structure · corrodedINSPECTION TYPE:C, RIGHT WING I/B FOREFLAP IS CORRODED BEYOND LIMITS WBL 128.4675 TO WBL 445. REMOVED AND REPLACED RIGHT I/B FOREFLAP.Feb 12, 2001 · N527UP · Boeing 747259B · Leading Edge DevicesSDR UPS01435153Web · crackedINSPECTION TYPE:C2,3, HFEC INSP REVEALED TWO CRACKS EXTENDING FROM 3RD INSULATION BLANKET STANDOFF HOLE FROM TOP AT LT SIDE STA 320 ON VERTICAL WEB OF NOSE WHEEL WELL IN CABIN. REMOVED AND REPLACED WEB IAW DWG 65B07942, AND SRM 51-30-02.Feb 12, 2001 · N527UP · Boeing 747259B · Fuselage Miscellaneous StructureSDR UPS01435152Web · crackedINSPECTION TYPE:C HFEC INSP REVEALED TWO CRACKS AT 3RD INSULATION BLANKET STANDOFF HOLE FROM TOP AT STA 300 ON VERTICAL WEB OF NOSE WHEEL WELL INSIDE CABIN RT SIDE. REMOVED AND REPLACED WEB IAW DWG 65B07942 AND SRM 51-30-02.Feb 12, 2001 · N527UP · Boeing 747259B · Fuselage Miscellaneous StructureSDR UPS01435350Spar Cap · corrodedINSPECTION TYPE:C, RIGHT WING FRONT SPAR LOWER CAP LOWER LEG IS CORRODED BEYOND LIMITS, 15 INCHES I/B OF STA FSSO, WS 1322. REPAIRED LOWER SPAR CAP IAW SRM 57-30-03 FIG 4.Feb 11, 2001 · N527UP · Boeing 747259B · Wing SparSDR UPS01435342Support · corrodedINSPECTION TYPE:C2, 3, STA 1306 LOWER SUPPORT FRAME BETWEEN BODY DOORS IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED SUPPORT FRAME IAW DWG 65B14056, AND SRM 51-30-02.Feb 11, 2001 · N527UP · Boeing 747259B · Fuselage Miscellaneous StructureSDR UPS01435341Support · corrodedINSPECTION TYPE:C STA 1329 LOWER FUSELAGE SUPPORT BETWEEN BODY GEAR DOORS IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED SUPPORT IAW DWG 65B14056, AND SRM 51-10-02.Feb 11, 2001 · N527UP · Boeing 747259B · Fuselage Miscellaneous StructureSDR UPS01435164Clip · corrodedINSPECTION TYPE:C, LEFT LOWER BODY FAIRING SUPPORT HANGER CLIPS ARE CORRODED BEYOND LIMITS AT STA 860 LBL 31 FWD AND AFT CLIP. REMOVED, FABRICATED, AND REPLACED CLIPS IAW DWG 65B01834, AND SRM 51-30-02.Feb 11, 2001 · N527UP · Boeing 747259B · Fuselage Miscellaneous StructureSDR UPS01435163Support Fitting · corrodedINSPECTION TYPE:C, LEFT LOWER BODY FAIRING SUPPORT AT STA 940 LBL 14 TO LBL 20 IS CORRODED BEYOND LIMITS. REPAIRED SUPPORT IAW SRM 53-50-04 FIG 1.Feb 11, 2001 · N527UP · Boeing 747259B · Fuselage Miscellaneous StructureSDR UPS01435162Support Fitting · corrodedINSPECTION TYPE:C, LEFT LOWER BODY FAIRING SUPPORT IS CORRODED BEYOND LIMITS AT STA 1000 LBL 43. REPAIRED SUPPORT IAW SRM 53-50-04.Feb 11, 2001 · N527UP · Boeing 747259B · Fuselage Miscellaneous StructureSDR UPS01435161Support Fitting · corrodedINSPECTION TYPE:C, LEFT BODY FAIRING SUPPORT IS CORRODED BEYOND LIMITS AT STA 1064 LBL 23 TO LBL 50. REPAIRED SUPPORT IAW SRM 53-50-04 FIG 2.Feb 11, 2001 · N527UP · Boeing 747259B · Fuselage Miscellaneous StructureSDR UPS01435160Support Fitting · corrodedINSPECTION TYPE:C, LEFT BODY FAIRING SUPPORT IS CORRODED BEYOND LIMITS AT STA 1112 BETWEEN LBL 25 TO LBL 40. REPAIRED SUPPORT IAW SRM 53-50-04.Feb 11, 2001 · N527UP · Boeing 747259B · Fuselage Miscellaneous Structure
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