Boeing 747-132

Service difficulty reports · 1,451

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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 = '747132'
  ORDER BY difficulty_date DESC"

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SDR 200200216Fitting · crackedMED NR 3 RIGHT FWD CORNER FITTING CRACKED AT LOWER AFT END. INSTALLED NEW CORNER FITTING AT NR 3 RIGHT FWD AFT END STA 1265 PER B747 SRM 51-30-02 & 51-10-01.Apr 4, 2002 · N479EV · Boeing 747132 · Fuselage Miscellaneous StructureSDR 200200125Fitting · crackedMED NR 3 LEFT FWD CORNER FITTING STA 1265 CRACKED AT LOWER END. INSTALLED MED NR 3 LT WD CORNER FITTING AT STA 1265 PER B747 SRM. REMOVED AND REPLACED LOCATED AND DRILLED FITTING PER B747 SRM.Apr 4, 2002 · N479EV · Boeing 747132 · Fuselage Main, Attach FittingsSDR 200200214Fitting · crackedMED 3 LEFT DOOR STOP FITTING CRACKED (FLANGE ONE SIDE BROKEN OFF) INSTALLED NR 3 LT DOOR STOP FITTING AT STR 20 PER B747 SRM 51-30-02 & 51-10-01. REMOVED AND REPLACED LOCATED AND DRILLED FITTING PER B747 SRM 51-30-02, 51-10-01 & 51-30-05.Apr 4, 2002 · N479EV · Boeing 747132 · Fuselage Main, StructureSDR 200200213Floor Support · crackedBULK PIT FLOOR SUPPORT AT BS 2160, ABOVE S-42 LEFT HAS A CRACK. REMOVED DAMAGED SECTION OF INTERCOSTAL AND PERFORMED SPLICE REPAIR PER B747 SRM 51-10-07 FIG 20 AND 747 SRM 51-30-02.Apr 4, 2002 · N479EV · Boeing 747132 · Fuselage Miscellaneous StructureSDR 200200212Stiffener · crackedLOWER FRAME STIFFENER AT BS 2160 BETWEEN S-49 AND S-50 LEFT IS CRACKED. FABRICATED AND INSTALLED SHEAR TIE, STRINGER CLIPS AND T CLIP SHEAR TIES PER B747 SRM.Apr 4, 2002 · N479EV · Boeing 747132 · Fuselage Main, StructureSDR 200200211Seat Track · corrodedMAIN DECK IN BETWEEN STA 440-460 RBL 66 HAS A CORRODED SEAT TRACK FLANGE. REMOVED AND REPLACED CORRODED SEAT TRACK FROM STA 332 RBL 45 TO STA 460 RBL 67 PER B747 SRM 53-10-05 FIG 1A.Apr 3, 2002 · N479EV · Boeing 747132 · Fuselage, Seat/Cargo Attach FittingsSDR 200200210Shear Tie · crackedLOWER FRAME STIFFENER AT BS 2140 BETWEEN S-46 AND S-47 RIGHT IS CRACKED. REMOVED DAMAGED SHEAR TIE SECTION BS 2140 AND 46R - AND 44L PER B747 SRM 53-10-4 FIG 3A. FABRICATED AND INSTALLED SECTIONS AND REPAIR PARTS PER B747 SRM 51-30-02 AND 53-10-04 FIG 41.Apr 3, 2002 · N479EV · Boeing 747132 · Fuselage Main, StructureSDR 200200209Seat Track · corrodedSEAT TRACK STA 400 RT SIDE 70" SIDE FROM BUTTLINE 0 CORROSION. REMOVED AND REPLACED DAMAGED SEAT TRACK FRAME FS 370-410 RBL 70 APPROX PER B747 SRM 53-10-5 FIG 1A.Apr 3, 2002 · N479EV · Boeing 747132 · Fuselage, Seat/Cargo Attach FittingsSDR 200200208Support · corrodedUPPER DECK LAV THRESHOLD SUPPORT BEAM STA 440 - 460 HAS CORROSION. REMOVED THRESHOLD PER SRM 51-30-2, FABBED NEW U-CHANNEL AND INSTALLED PER B747 SRM 51-30-2.Apr 3, 2002 · N479EV · Boeing 747132 · Fuselage Miscellaneous StructureSDR 200200207Frame · corrodedEXFOLIATION CORROSION ON TOPSIDE OF WHALE BONE STRUCTURE FS 987 LBL 45-47 WHERE AIR CONDITIONING BAY SERVICE LIGHT BRACKET MOUNTS TO WHALE BONE. REMOVED DAMAGED AREA PER SRM 51-40-04 FIG 2, FABRICATED AND INSTALLED REPAIR PER SRM 51-30-2.Apr 3, 2002 · N479EV · Boeing 747132 · Fuselage Main, FrameSDR 200200206Seat Track · corrodedMAIN DECK AT STATION 1914-1940 AT LBL 11 HAS CORRODED SEAT TRACK. REMOVED AND REPLACED CORRODED SEAT TRACK IAW B747 SRM.Apr 3, 2002 · N479EV · Boeing 747132 · Fuselage, Seat/Cargo Attach FittingsSDR 200200205Stiffener · crackedLEFT WING WS 1485 CRACKED STIFFENER ON REAR SPAR. REMOVED CRACKED STIFFENER AND INSTALLED NEW STIFFENER PER B747 SRM.Apr 3, 2002 · N479EV · Boeing 747132 · Wing Miscellaneous StructureSDR 200200203Structure · deterioratedNR 3 PYLON LOWER SURFACE, JUST AHEAD OF THE AFT ENGINE MOUNT ON THE LEFT SIDE FIRESHIELD DETERIORATED. FABRICATED, ALODINED, PRIMED AND INSTALLED PER B747 SRM.Apr 3, 2002 · N479EV · Boeing 747132 · Nacelle/Pylon, Main FrameSDR 200200202Seal · crackedREPAIR CRACKS IN LEFT AND RIGHT LOWER SLOT SEALS. THE LOWER SLOT SEALS ARE MADE FROM THE SAME MATERIAL AS THE UPPER SLOT SEALS BUT ARE NOT COVERED BY THE 747 SRM. THIS DOCUMENT ALLOWS WELDING OF THE LOWER SLOT SEAL ASSEMBLIES PROVIDED THE REPAIR IS NOT IN THEApr 3, 2002 · N479EV · Boeing 747132 · Nacelle/Pylon, Main FrameSDR 200200201Panel · delaminatedNR 3 ENGINE INTAKE NOSE COWL ACOUSTIC PANEL 5-6 OCLOCK FWD POSITION DELAMINATED. LOCATED AND DRILLED NEW ACOUSTIC PANEL, INSTALLED NEW ACOUSTIC PANEL.Apr 3, 2002 · N479EV · Boeing 747132 · Nacelle/Pylon, Main FrameSDR 200200200Frame · crackedFRAME AT BS 1940 STR WL125 IS CRACKED. (BETWEEN STR 37L AND 36L) INSTALLED NEW FRAME STA 1940 STR 34- 43L PER SRM 51-30-2 SEALED PER 51-10-6.Apr 3, 2002 · N479EV · Boeing 747132 · Fuselage Main, FrameSDR 200200199Skin · corrodedREPAIR FOR CORROSION ON LOWER IN SPAR SKIN PANEL AT FSS 1057. THE CORROSION WAS BLENDED AWAY WITH A 20:1 BLEND RATIO PER B747 SRM GUIDELINES AND HFEC INSPECTED TO ENSURE A CRACK FREE CONDITION.Apr 3, 2002 · N479EV · Boeing 747132 · Wing, Plate/SkinSDR 200200198Web · crackedREPAIR OF CRACK IN SECTION 41 FLOOR WED AT BS 140, LBL 38. THE CRACKED SECTION IS REPAIRED BY TRIMMING AWAY THE DAMAGED PORTION OF WEB, AND SPLICING IN A NEW SECTION OF WEB WITH A REPAIR DOUBLER PER B747 SRM.Apr 3, 2002 · N479EV · Boeing 747132 · Fuselage Miscellaneous StructureSDR 200200197Fitting · gougedGOUGE, NR 5 FLAP TRACK FWD FITTING, FAIL-SAFE BORE HOLE. THE GOUGE IS COMMON TO THE UPPER SURFACE OF THE BORE AT NEAR MIDPOINT. REPAIR IS ACCOMPLISHED BY LOCAL BLENDING.Apr 3, 2002 · N479EV · Boeing 747132 · Trailing Edge FlapsSDR 200200204Stiffener · crackedLEFT WING WS 1425 CRACKED STIFFENER ON REAR SPAR. REMOVED AND REPLACED STIFFENER ON REAR SPAR PER B747 SRM.Apr 2, 2002 · N479EV · Boeing 747132 · Wing Miscellaneous StructureSDR 200200196Floorbeam · corrodedCORROSION ON BS 400 FLOORBEAM AT RBL 70. SECTION OF FLOORBEAM UPPER AFT CHORD IS SPLICED IN FROM RBL 30 TO THE RT SIDE OF BODY PER ECRA 479-53-161-2.Apr 2, 2002 · N479EV · Boeing 747132 · Fuselage Main, Floor BeamSDR 200200195Spar · corrodedCORROSION ON BS 1241 WCS REAR SPAR WEB AT LBL 80. THE CORROSION WAS BLENDED PER SRM.Apr 2, 2002 · N479EV · Boeing 747132 · Wing SparSDR 200200194Support · damagedDAMAGED LOWER CHORD AND WEB OF TRAILING EDGE SUPPORT BEAM. TRIMMED OUT THE DAMAGE AREAS AND INSTALLED STRAPS, FILLERS AND DOUBLERS PER ECRA 479-57-160-2.Apr 2, 2002 · N479EV · Boeing 747132 · Wing Miscellaneous StructureSDR 200200193Frame · corrodedCORROSION AND SHORT EDGE MARGINS IN BS 340, 360 & 380 FRAME. CORROSION WAS FOUND IN THE HOLES COMMON TO THE FRAMES AND THE UPPER DECK FLOORBEAM UPPER CHORDS AT BS 340 & 360, LT & RT AND BS 360 RIGHT. THE HOLES WERE OVERSIZED TO REMOVE CORROSION CAUSING A SHOApr 2, 2002 · N479EV · Boeing 747132 · Fuselage Main, FrameSDR 200200192Skin · crackedSKIN CUTOUT AND CRACK DAMAGE AT BS 2210-2220, S35L-S37L. THE SUBJECT DAMAGE IS LOCATED COMMON TO BSB 747-53-2063 OUTFLOW VALVE CUTOUT REINFORCEMENT DOUBLER. REPAIR INSTALLED PER B747 SRM REPAIR PRACTICES.Apr 2, 2002 · N479EV · Boeing 747132 · Fuselage Main, Plate/SkinSDR EIA2002026Bulkhead · crackedFOUND RIGHT WING TRAILING EDGE CAVITY, LOWER BULKHEAD CHORD CRACKED AT APPROXIMATELY WBL 245, BELOW INTERSECTION OF NR 7 AND NR 8 SPOILERS. REMOVED DAMAGE AND REPAIRED PER ECRA 479-57-160-2. (M)Mar 30, 2002 · N479EV · Boeing 747132 · Wing, Rib/BulkheadSDR EIA2002031Failsafe · gougedMZJ - NR 5 FLAP TRACK FORWARD ATTACH FITTING FAIL/SAFE BORE HAS DEEP GOUGE. REPAIRED PER ECRA 479-57-159-2. (M)Mar 30, 2002 · N479EV · Boeing 747132 · Trailing Edge FlapsSDR EIA2002024Pressure Panel · corrodedMZJ - FOUND STATION 1241, LEFT WING GEAR WHEEL WELL, FORWARD SIDE SKIN WAS FOUND CORRODED. REPAIRED PER ECRA 479-57-157-2. (M)Mar 30, 2002 · N479EV · Boeing 747132 · Fuselage Main, BulkheadSDR EIA2002027Skin · crackedMZJ - FOUND 1.5 INCH CRACK AND SKIN BULGED AT STATION 2229, STRINGER 34L TO 36L, NEXT TO OUTFLOW VALVE. REMOVED DAMAGE AND REPAIRED PER ECRA 479-53-155-2. (M)Mar 30, 2002 · N479EV · Boeing 747132 · Fuselage Main, Plate/SkinSDR EIA2002021Frame · crackedMZJ - FOUND FRAME AT STATION 1940, WL 125, BETWEEN STRINGERS 36L AND 37L WAS FOUND CRACKED. INSTALLED NEW FRAME PER SRM 51-30-2. (M)Mar 30, 2002 · N479EV · Boeing 747132 · Fuselage Main, FrameSDR EIA2002020Web · crackedMZJ - DURING C-CHECK, FOUND SUBFLOOR WEB AT STATION 140, STRINGER 31A LEFT SIDE, IN LOWER NOSE COMPARTMENT, WAS FOUND TO HAVE A CRACK APPROXIMATELY 6 INCHES LONG. REMOVED DAMAGED AREA AND REPAIRED PER ECRA 479-53-154-2. (M)Mar 30, 2002 · N479EV · Boeing 747132 · Fuselage Miscellaneous StructureSDR EIA2002028Rib · damagedMZJ - FOUND C-CHECK SEVERLY DAMAGED HORIZONTAL STAB CLOSURE RIB AND TOTAL STRUCTURAL FAILURE OF WEB ALL AT HORIZONTAL STABILIZER APPROXIMATELY STATION 2598. REMOVED DAMAGED RIB AND WEB AND FABRICATED NEW AND INSTALLED PER SRM 51-32-02, 51-20-01, 51-10-02. (MMar 30, 2002 · N479EV · Boeing 747132 · Horizontal Stabilizer, Spar/RibSDR EIAA2002029Fitting · crackedMZJ - FOUND IN C-CHECK, LT WING WBL 235, UPPER TRAILING EDGE PANEL SUPPORT T-FITING CRACKED AT THE NR 4 FLAP TRACK. INSTALLED NEW T-FITTING PER SRM 51-30-05. (M)Mar 30, 2002 · N479EV · Boeing 747132 · Wing, Attach FittingsSDR EIAA2002023Frame · crackedMZJ - FOUND STATION 2140, RBL 19 LOWER WEB FRAME WAS FOUND CRACKED. REPAIRED PER SRM 53-10-23 AND 53-10-04. (M)Mar 30, 2002 · N479EV · Boeing 747132 · Fuselage Main, FrameSDR EIAA2002025Floorbeam · corrodedMZJ - NUMEROUS HOLES IN UPPER FLOORBEAMS AT STATIONS 340, 360, AND 380 WERE FOUND TO HAVE CORROSION. REPAIRED PER ECRA 53-162-2. (M)Mar 30, 2002 · N479EV · Boeing 747132 · Fuselage Main, Floor BeamSDR EIA2002022Skin · corrodedMZJ - FOUND BULGE IN SKIN BETWEEN STATION 2638 AND 2658 AT STRINGER 11 LT. REMOVED AND REPLACED DAMAGED SKIN PER ECRA 479-53-156-2. (M)Mar 30, 2002 · N479EV · Boeing 747132 · Fuselage Main, Plate/SkinSDR EIAA2002030Floorbeam · corrodedMZJ - FOUND DURING C-CHECK, STATION 400 FLOORBEAM AT RIGHT SIDE, 70 INCHES FROM BUTT LINE 0 WAS FOUND CORRODED. REPAIRED PER ECRA 479-53-262-2. (M)Mar 30, 2002 · N479EV · Boeing 747132 · Fuselage Main, Floor BeamSDR 2003F00056Engine · flamed outNR 4 ENGINE FLAMED OUT AT FL 38 ALL PARAMETERS NORMAL, RESTARTED ENGINE WITH NO FURTHER MALFUNCTIONS. INSPECTED NR 4 ENGINE IAW B747 MM CH 71-00, NO DEFECTS NOTED. RAN NR 4 ENGINE AND LEAK CHECK IAW B747 MM CH 71-00. NO LEAKS NOTED. (M)Mar 26, 2002 · N709CK · Boeing 747132 · Engine (Turbine/Turboprop)SDR 200200184Flange · crackedCRACK FROM THE "R" FLANGE LIGHTNING HOLE TO THE FLANGE OUTER DIAMETER AT THE 12 O'CLOCK POSITION. RADIAL CRACK ( 1/2 INCH LONG) FROM THE "R" FLANGE LIGHTNING HOLE TO THE CASE WALL BUT NOT TO THE FILLET RADIUS AT THE 12:30 O'CLOCK POSITION. CRACK FROM THE "R" Mar 21, 2002 · N479EV · Boeing 747132 · Turbine SectionSDR 200200186Fitting · crackedBS 2484, LEFT LOWER BULKHEAD SPLICE FITTING AT STRINGER 23, CRACKED FROM LOWER INBOARD FASTENER. REMOVED AND REPLACED FITTING PER SERVICE BULLETIN 53-2162, FIGURE 2.Mar 21, 2002 · N479EV · Boeing 747132 · Fuselage Miscellaneous StructureSDR 200200185Flange · crackedCRACK FROM -R- FLANGE LIGHTENING HOLE TO THE OUTER FLANGE AT THE 6 O'CLOCK POSITION. WELDED PER EIA ECRA 685755-72-010-1 AND 747 MM 72-53-02.Mar 21, 2002 · N479EV · Boeing 747132 · Turbine SectionSDR 2002F00270Battery Pack · dischargedFOUND A-CHECK, L5 AND R5 EMERGENCY LIGHT INOPERATIVE STATION 2280. BATTERY PACK REPLACED AND OPS CHECK PER MM. REF EIAA2002003. (M)Jan 29, 2002 · N481EV · Boeing 747132 · Emergency LightingSDR EIA2002003Light · inoperativeFOUND A-CHECK, L5 AND R5 EMERGENCY LIGHT INOPERATIVE STATION 2280. BATTERY PACK REPLACED AND OPS CHECK PER MM. (M)Jan 29, 2002 · N481EV · Boeing 747132 · Emergency LightingSDR EIA2001240Line · failedSUU - WHEN CLIMBING THROUGH FL300 TO FL380 NR 1 ENGINE HAD AN UNRECOVERABLE COMPRESSOR STALL, EPR WAS APPROX 1.49, WHEN STALL OCCURRED N1 AND N2 DECREASED EGT INCREASED THEN DECREASED PEAKING AT 850 DEGREE SHUTDOWN, RESTARTED ENGINE. PARAMETERS NORMAL AFTER RAug 21, 2001 · N479EV · Boeing 747132 · Fuel Controlling SystemSDR UPS01436141Stringer · crackedINSPECTION TYPE:C M/D - BS 1990 RT STR 13 STRINGER CRACKED. HFEC INSPECTION C/OUT AS PER NTM PART 6 51-00-00 FIG 4 NIL CRACK FOUND.Jun 4, 2001 · N674UP · Boeing 747132 · Fuselage Main, Longeron/StringerSDR EIA2001116Engine · failedCGK - NR 1 ENGINE SHUTDOWN IN FLIGHT AT 39,000 FEET, ON DESCENT TRIED TO START. N2 56 PERCENT EGT CLIMBED TO 948 RAPIDLY. ENGINE SHUTDOWN AFTER GOING THROUGH TURBULENCE. WINDMILLING CHECK PERFORMED, CHIP DETECTORS CHECKED GOOD. REPLACED OIL FILTER AND FUELMar 20, 2001 · N481EV · Boeing 747132 · Engine (Turbine/Turboprop)SDR EIA2001014Module · malfunctionedKJFK - EMERGENCY LIGHTS WOULD NOT SHUTOFF. REPLACED EMERGENCY LIGHT MODULE. (M)Feb 21, 2001 · N481EV · Boeing 747132 · Emergency LightingSDR EIA2001009Fitting · malfunctionedKJFK - FLT RCF7 - GEAR WOULD NOT RETRACT. LANDING GEAR LEVER LATCH DID NOT RELEASE. RT BODY GEAR WAS NOT TILTED PRIMARY AND ALT. REPLACED COBRA FITTING, PRIM TILT SWITCH, AND ALT TILT SWITCH ADJUSTED RIGHT BODY GEAR PRI AND ALT TILT SWITCHES PER MM 32-61-04Feb 3, 2001 · N481EV · Boeing 747132 · Landing Gear Retraction/Extension SystemSDR EIA2001019Floor Support · crackedHKG-HAECO - FOUND M/D BS 360 LBL 96 FLOOR SUPPORT WEB CRACKED. FLOOR SUPPORT WEB REPAIRED PER SRM 51-40-02. (M)Jan 26, 2001 · N481EV · Boeing 747132 · Fuselage Miscellaneous StructureSDR EIA2001020Floor Support · crackedHKG-HAECO - FOUND M/D BS 140 LBL 45 FLOOR SUPPORT WEB CRACKED. STOP HOLE DRILLED, NDT INSPECTED, REPAIRED FLOOR SUPPORT WEB PER SRM 51-40-02. (M)Jan 26, 2001 · N481EV · Boeing 747132 · Fuselage Miscellaneous Structure
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