Boeing 747 212B

Service difficulty reports · 2,202

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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 = '747212B'
  ORDER BY difficulty_date DESC"

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SDR UPS04442362Light · inoperativeUPPER DECK SERVICE DOOR FRAME EMERGENCY LIGHTS 2EA INOP. PANEL OPENED FOR ACCESS TO BATTERY PACK. APPLIED POWER TO A/C & ALLOWED EMERGENCY LIGHTS TO CHARGE SEVERAL HOURS. UPPER DECK DOOR LTS OPERATED NORMAL PER B747 MM 33-51-04 INSTALLED & SECURED PANEL.May 7, 2004 · N526UP · Boeing 747212B · Emergency LightingSDR EIA2004033Connector · dirtyON CLIMBOUT WITH FLAPS UP, NOTICED IN LEFT TURN SLIGHT BUFFETING. UPON VISUAL FOUND LEFT OUTBOARD AILERON NOT LOCKED OUT. RETURNED TO PHIK. COULD NOT DUPLICATE. CLEANED AND FOUND OILY GRIME ON LEFT HAND OUTBOARD AILERON CANNON PLUG. CHECKED VOLTAGE WITH FApr 29, 2004 · N485EV · Boeing 747212B · Aileron Control SystemSDR EIA2004031Battery Pack · dischargedEMERGENCY EXIT LIGHT INOP ABOVE CREW EXIT DOOR. REPLACED EMERGENCY EXIT BATTERY PACK PER MM 33-51-04. REPLACED SIGN PER 33-51-02, OPS CHECKED GOOD. ALSO REPLACED SIGN BATTERY PACK.Apr 24, 2004 · N486EV · Boeing 747212B · Emergency LightingSDR EIA2004030Light · inoperativeEMERGENCY LIGHT LT SIDE STATE ROOM UPPER DECK WENT OUT IN 5 SECONDS. REMOVED & REPLACED LT SIDE STATE ROOM (UPPER DECK) EMERGENCY LIGHT PER B747 MM 33-51-00. OP'S CHECK GOOD PER MM 33-51-00.Apr 22, 2004 · N486EV · Boeing 747212B · Emergency LightingSDR EIA2004029Floorbeam · damagedSTA 360 LT UPPER DECK FLOORBEAM UPPER CHORD HAS NUMEROUS HOLES WITH SHORT EDGE MARGIN BETWEEN LBL 55 & LBL 82. REPAIRED STA 360 LH UPPER DECK FLOORBEAM UPPER CHORD SHORT EDGE MARGIN HOLES, LBL 55-LBL 82, PER ECRA #486-53-025-2, PART "C"Apr 21, 2004 · N486EV · Boeing 747212B · Fuselage Main, Floor BeamSDR EIA2004027Frame · crackedLEFT HAND AFT INNER CHORD CRACKED AT STA 2598 AT SHEAR DECK. FABRICATED AND INSTALLED SPLICE ANGLES LT AFT INNER CHORD STA 2598 AT SHEAR DECK, PER B747 SRM 53-10-04, FIG 72.Apr 21, 2004 · N486EV · Boeing 747212B · Fuselage Main, FrameSDR EIA2004026Web · gougedAFT PIT STA 1500 BETWEEN STR 41-42 LEFT FWD SIDE OF WEB HAS DEEP GOUGE. FABRICATED AND INSTALLED FRAME SECTION & DOUBLER PER B747 SRM 51-4-003, PAGES 7-12 AT STA 1500 STR 41-42 L DUE TO GOUGE EXCEEDING LIMIT PER B747 SRM 53-10-01, PAGE 1-4. MTL ID 7075T6,.06Apr 21, 2004 · N486EV · Boeing 747212B · Fuselage Miscellaneous StructureSDR EIA2004025Floorbeam · damagedSTA 340 LT UPPER DECT FLOORBEAM TO FRAME INTERFACE HAS ELONGATED HOLES. OVERSIZED ELONGATED HOLES AT BS 340 LT FLOORBEAM TO FRAME INTERFACE TO ROUND CONDITION PER ECRA 486-53-25-2, PART B, STEP 2. HFEC & 10X VISUAL INSP SHOWS HOLES ARE CRACK AND CORROSION FRApr 21, 2004 · N486EV · Boeing 747212B · Fuselage Main, Floor BeamSDR EIA2004024Floorbeam · damagedSTA 340 RT UPPER DECK FLOORBEAM TO FRAME INTERFACE HAS ELONGATED HOLES. OVERSIZED, ELONGATED HOLES TO ROUND CONDITION. HFEC & 1OX VISUAL INSPECTION SHOWS HOLES TO BE CRACK AND CORROSION FREE. (SEE ECRA 486-53-025-2) REMOVED EXISTING FREEZE PLUGS AT HOLES NApr 21, 2004 · N486EV · Boeing 747212B · Fuselage Main, Floor BeamSDR EIA2004023Floorbeam · damagedSTA 360 LT UPPER DECK FLOORBEAM, TO FRAME INTERFACE HAS (4) ELONGATED HOLES. OVERSIZED ELONGATED HOLES AT STA 360 LT UPPER DECK FLOORBEAMS TO FRAME INTERFACE TO ROUND CONDITION. HFEC & 1OX VISUAL INSP SHOWS HOLES TO BE CRACK AND CORROSION FREE. (SEE ECRA 486Apr 21, 2004 · N486EV · Boeing 747212B · Fuselage Main, Floor BeamSDR EIA2004022Floorbeam · damagedSTA 340, 360 RT UPPER DECK FLOORBEAM HAS NUMEROUS HOLES WITH SHORT EDGE MARGIN BETWEEN RBL 55-80. STA 340 AND 360 RT UPPER DECK FLOORBEAM WITH SHORT EDGE MARGIN HOLES REPAIRED PER ECRA 3486-53-025-2Apr 19, 2004 · N486EV · Boeing 747212B · Fuselage Main, Floor BeamSDR UPS04442208Light · malfunctionedEMERGENCY EXIT LIGHT AT POS 500 ON MCD HAS ONE LAMP INOP. REPLACED LAMP, OPS CHECKS OK.Apr 18, 2004 · N526UP · Boeing 747212B · Emergency LightingSDR UPS04442207Light · malfunctionedEMERGENCY EXIT LIGHT AT ESCAPE DOOR ON FLIGHT DECK GOES OUT 3-5 SECONDS AFTER BEING TURNED ON. REPLACED LIGHT PACK ASSY, OPS CHECKS OK.Apr 18, 2004 · N526UP · Boeing 747212B · Emergency LightingSDR UIEA200400046Slide · malfunctionedUPPER RT EMERGENCY DOOR SLIDE PARTIAL DEPLOYMENT; DURING UPPER RT EMERGENCY DOOR SLIDE RAFT ASSEMBLY DEPLOYMENT TEST, SLIDE/RAFT FAILED TO FULLY INFLATE. SEQUENCING MECHANISM RELEASED TO FACILITATE SLIDE RAFT REMOVAL AND DISPATCH TO STOP. NOTE: ACTUAL OR APApr 8, 2004 · N808MC · Boeing 747212B · Escape SlideSDR 0400536642Battery Pack · inoperativeDURING LINE CHECK, FOUND 'E' ZONE FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK GOOD.Apr 4, 2004 · N642NW · Boeing 747212B · Emergency LightingSDR EIA2004017Stringer · dentedSTRINGER 38R STA. 535 DENTED. REMOVED DAMAGED STR. FABBED AND INSTALLED NEW STRINGER PER B747 SRM 51-30-02,51-20-01, 51-20-01, & 51-10-02Apr 2, 2004 · N486EV · Boeing 747212B · Fuselage Main, Longeron/StringerSDR EIA2004016Bulkhead · corrodedRT WING LANDING GEAR BAY CANTED BULKHEAD STA. 1261 RBL 0 UPPER INBD CORNER (TEE CHORD) HAS CORROSION. REMOVED AND REPLACED TEE CHORD AT STA. 1261 RBL 0 PER 747 SRM 51-10-02 PG 1, 51-30-05 PAGES 6-9, 51-30-02 PAGES 8-9 AND 51-10-16 PAGES 1-30.Apr 1, 2004 · N486EV · Boeing 747212B · Fuselage Main, BulkheadSDR EIA2004014Engine · flamed outCLIMBING THROUGH 38500 FT NR 4 ENGINE FLAMED OUT. INFLIGHT RESTART NORMAL. INSPECTED INTAKE AND EXHAUST NO DEFECTS NOTED INSPECTED BLEED SCREENS NO FOREIGN OBJECTS NO DEFECTS. REPLACED MAIN FUEL FILTERS, SUMPED NR 4 FUEL DRAIN NO WATER FOUND. FUEL PUMP PRESSMar 28, 2004 · N482EV · Boeing 747212B · Engine (Turbine/Turboprop)SDR UPS04442068Battery Pack · dischargedINSPECTION TYPE:N/A EMERGENCY EXIT SIGN OVER UPPER DOCK ESCAPE SLIDE DOOR INOP. REMOVED AND REPLACED BATTERY PACK PER AMM 33-31-04. OPS CHECKED GOOD.Mar 25, 2004 · N526UP · Boeing 747212B · Emergency LightingSDR UPS04441984Fitting · corrodedINSPECTION TYPE: C, RIGHT WING REAR SPAR LOWER KICK FITTING HOLE -A- FOUND CORROSION INSIDE FASTENER HOLE. CORROSION REMOVED AND HOLE -A- FREEZE PLUG INSTALLED AS PER RS R-57-12-35115 AND UPS EO B747-5710-20028-A.Feb 19, 2004 · N526UP · Boeing 747212B · Wing, Attach FittingsSDR UPS04441959Frame · crackedINSPECTION TYPE: C, M/D - NR 5R MED CUTOUT BS 2231 FRAME AT S25R FOUND 1 FASTENER HOLE CRACK AT STRAP. M/D R5 DOOR FWD CUTOUT FRAME STRAP REPAIRED PER SRM 53-10-04 FIG 115.Feb 12, 2004 · N526UP · Boeing 747212B · Fuselage Main, FrameSDR UPS04441981Frame · crackedINSPECTION TYPE: C, NR 3 PYLON REAR MOUNT BULKHEAD FOUND CRACKS AT O/B FWD AND AFT FRAME WEB. FRAME WEB ATTACH PARTS REINSTALLED PER BS 54-53-34870 AND CONTINUE REPEAT INSPECTION PER RS OR UPS EO SINCE NO FURTHER CRACK PROPAGATION AFTER REPAIR PARTS REMOVED.Feb 11, 2004 · N526UP · Boeing 747212B · Nacelle/Pylon, Frame/Spar/RibSDR UPS04441983Reveal · crackedINSPECTION TYPE: C, M/D - LEFT NR 4 DOOR CUTOUT FWD LOWER BET S24-25L, CUTOUT REVEAL FOUND CRACK AS MARKED. CUTOUT REVEAL REPAIRED AS PER SRM 53-10-04 FIG 84 AND HX RS R-53-62-35110, CRACKS STOPPED AT FASTENER HOLE FROM EDGE CONFIRMED BY NDT INSPECTION, SURRFeb 10, 2004 · N526UP · Boeing 747212B · Fuselage Miscellaneous StructureSDR UPS04441982Door Frame · crackedINSPECTION TYPE: C, M/D - LEFT NR 4 DOOR FWD CUTOUT FWD FRAME APPROX S16L AREA, FRAME I/B FWD FACE FOUND CRACK AS MARKED. FWD FRAME CRACKED PORTION TRIMMED OFF, REPAIRED AS PER HX RS 53-62-35110. SURROUNDING STRUCTURE IS CORROSION AND DAMAGE FREE AFTER INSPFeb 10, 2004 · N526UP · Boeing 747212B · Fuselage Main, StructureSDR UPS04441990Skin · corrodedINSPECTION TYPE: C, RIGHT WING UPPER SURFACE T/E RABBET AREA STRAP PNL BULGED UP AT 20 INCHES O/B OF ROOT AREA. CORROSION BLEND OUT 11.5 X 1, DEPTH .115 TO .62, ORI .332 TO .328. FPI C/O SOPM 20-20-02 AT REWORK AREA CORROSION FREE NDT INSPECTED, NIL FINDINGFeb 9, 2004 · N526UP · Boeing 747212B · Wing, Plate/SkinSDR 0400136642Battery Pack · inoperativeDURING LINE CHECK, FOUND ZONE E-FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK GOOD.Jan 27, 2004 · N642NW · Boeing 747212B · Emergency LightingSDR EIA2004009Screw · looseDURING COCKPIT CHECK NOTICED ELECTRICAL ODOR. FOUND ONE SCREW HAD COME LOOSE ON LT OB LDG LIGHT SWITCH CAUSING ARCHING. UNABLE TO TIGHTEN SCREW REQUIRES NEW SWITCH. DEACTAVATED CIRCUIT AND ENTERED DMI 483. SWITCH ORDERED.Jan 25, 2004 · N486EV · Boeing 747212B · Exterior LightingSDR EIA2004006Transformer · overheatedSTRONG ELECTRICAL ODOR IN COCKPIT PANEL LIGHT. C/B PULLED FUMES DISSIPATED. TRANSFERRED TO DMI 475. REPLACED RIGHT EIDS DISPLAY DUE IT WAS REPORTED FLASHING ON T/O. REPLACED AVIONICS ADAPTER RACK AND REPLACED DIMMEN TRANSFORMER DUE TO SIGNS OF OVERHEAT. OJan 15, 2004 · N486EV · Boeing 747212B · Flight Compartment LightingSDR EIA2004004Wire · brokenSTRONG SMOKE /FUME ODOR, PULLED CTR PNL CB ODOR SEEMED TO GO AWAY. FOUND BROKEN WIRE L77-20 AT DIMMER BROKEN WITH SIGNS OF ARCHING AT TERMINAL. REPAIRED WIRE PER SWPM 20-10-13, OPS CHECKED PER B747 MM 33-11-00. NO ODOR NOTED.Jan 14, 2004 · N486EV · Boeing 747212B · Light System WiringSDR EIA2004003A/C Pack · odorWHILE AIRCRAFT WAS IN CLEAN CONFIGURATION AND LEVEL AT 6000 FEET HAD AN ELECTRICAL TYPE ODOR THAT APPEARS TO BE COMING FROM NR 1 A/C PACK, INTERMITTENT ODOR DURING APPROACH AND LANDING. DEFERRED NR 1 A/C PACK DMI 470.Jan 11, 2004 · N486EV · Boeing 747212B · Cabin Cooling SystemSDR EIA2004002Rheostat · overheatedON FINAL APPROACH NOTICED STRONG ELECTRIAL BURNING ODOR UPON SELECTING FLAPS DOWN. FOUND CENTER FWD BACKGROUND LIGHTING DIMMER/TRANSFORMER EXTREMELY HOT CB T137, PULLED AND COLLARED DMI PER 33-1 DMI 469. REMOVED AND REPLACED INSTRUMENT LIGHT DIMMER AND CTR IJan 9, 2004 · N486EV · Boeing 747212B · Flight Compartment LightingSDR EIA2003166Frame · crackedAIRCRAFT NOSE W/W TUNNEL RT SIDE BS 300 3 EA HOLES CRACKED IN THE FRAME SEGMENT ABOVE STR. 40, 41, AND 42 RT. REMOVED DAMAGE, NDT AREA, FABRICATED REPAIR AND INSTALLED IAW SRM 53-10-04 FIG 94 DETAIL III AND ECRA 485-53-168-2Dec 5, 2003 · N485EV · Boeing 747212B · Fuselage Main, FrameSDR EIA2003164Battery · inoperativeOVERHEAD EMERGENCY LIGHT AT STA 2130 IS INOPERATIVE. REMOVED AND REPLACED BATTERY ASSY IAW BMM 33-35-01 OPS CKD GOOD.Dec 1, 2003 · N482EV · Boeing 747212B · Emergency LightingSDR EIA2003165Battery · inoperativeUPPER DECK CREW SERVICE DOOR EMERGENCY SILL LIGHTS INOPERATIVE. REMOVED AND REPLACED UPPER DECK CREW SERVICE DOOR EMERGENCY LIGHT IAW B747MM 33-51-07. OPS CHECKED GOOD.Dec 1, 2003 · N482EV · Boeing 747212B · Emergency LightingSDR UPS03441577Skin · crackedINSPECTION TYPE: PFLT CRACK NR 3 ENGINE PYLON OUTBOARD SIDE AT PYLON EMERGENCY DRAIN TUBE. REPAIRED CRACK IAW 54-34-03 FIG 7.Nov 27, 2003 · N526UP · Boeing 747212B · Nacelle/Pylon, Plate/SkinSDR EIA2003147Hose · failedNR 1 ENGINE OIL QUANTITY DECREASED RAPIDLY ON CLIMB OUT FROM EROS. REDUCED NR 1 ENGINE TO IDLE AND DECREASED LESSEND , PERFORMED FUEL JETTISON AND RETURNED TO EROS. CORRECTIVE ACTION SECURED CLAMP MID POSITION NR 4 BEARING SCAVENGE LINE RETORQUED MID (B) NUT Oct 26, 2003 · N482EV · Boeing 747212B · Engine Oil QuantitySDR EIA2003146O-Ring · leakingNR 1 ENGINE OIL QUANTITY DECREASED TO 1 GALLON AND NR 1 ENGINE OIL PRESSURE LIGHT CAME ON, SHUT DOWN NR 1 ENGINE, NR 1 ENGINE OIL PRESSURE AT 34 PSI. REPLACED ANGLE GEARBOX CHIP DETECTOR O-RINGS, PERFORMED LEAK CHECK NO OIL LOSS ON ENGINE RUN, SERVICE ENGINE Oct 25, 2003 · N482EV · Boeing 747212B · Turbine Engine Oil SystemSDR EIA2003145Hose · chafedAFTER TAKE-OFF NR 3 HYD SYSTEM QUANITY DROPPED TO ZERO, EDP PRESSURE INDICATING ZERO, ADP PRESSURE NORMAL. ON CHECK FOUND NR 3 ENGINE EDP PRESSURE HOSE CHAFED, REPLACED PRESSURE HOSE IAW MM 29-00-00, LEAK CHECK GOOD ON ENGINE RUN.Oct 23, 2003 · N486EV · Boeing 747212B · Hydraulic System, MainSDR EIA2003132Skin · chafedVERTICAL STAB TO FUSELAGE. AREA LT SIDE BELOW RUDDER BETWEEN STA. 2521 AND 2598 HAS A GOUGE IN FUS. REMOVED DAMAGED, NDT AREA, FABBED AND INSTALLED REPAIR IAW ECRA 482-53-181-2.Oct 20, 2003 · N482EV · Boeing 747212B · Fuselage Main, Plate/SkinSDR EIA2003130Spar · corrodedRT WING UPPERCHORD OF FIX TRAILING EDGE PANEL SUPPORT BEAM SPAR APPROX WBL 235.2-445 CORRODED. REMOVED DAMAGE, NDT AREA, FABBED AND INSTALLED REPAIR IAW ECRA 482-57-184-2Oct 20, 2003 · N482EV · Boeing 747212B · Wing SparSDR EIA2003127Skin · corrodedRT FUSELAGE SEC 48 EXT SKIN HAS CORROSION LOCATED BETWEEN STA 2436-2460 STR 23R-25R. REMOVED DAMAGE, NDT AREA, FABBED AND INSTALLED REPAIR IAW ECRA 482-53-165-2.Oct 20, 2003 · N482EV · Boeing 747212B · Fuselage Main, Plate/SkinSDR EIA2003143Beam · damagedVERTICAL STAB RT TRAILING EDGE BEAM FWD AND AFT WEBS DAMAGED, DO TO POWER PACK LOWER RUDDER INSTALLATION. INSTALLED FORWARD WEB DOUBLER AND 2 EA. FILLERS IAW MFG 747 SRM 51-30-02 AND ECRA 482-55-183-2Oct 20, 2003 · N482EV · Boeing 747212B · Vertical StabilizerSDR EIA2003139Frame · brokenVERTICAL STAB RT SIDE ACCESS PANEL 324 DR AFT SECTION OF PANEL ATTACH FRAME HAS SECTION BROKEN OFF. REMOVED DAMAGED, NDT AREA, FABBED AND INSTALLED REPAIR IAW ECRA 482-55-196-2Oct 20, 2003 · N482EV · Boeing 747212B · Vertical StabilizerSDR EIA2003135Structure · damagedBS 1760 STR 49 RT HAS CORROSION ON STRUCTURE LOWER SURFACE. REPLACED DAMAGED STR FROM BS 1740-1770 IAW B747 SRM 53-10-03 FIG 8.Oct 20, 2003 · N482EV · Boeing 747212B · Fuselage Main, StructureSDR EIA2003134Skin · wornFUSELAGE SKIN WORN AT INTERFACE OF VERTICAL STAB SEAL RT SIDE BS 2280-2416 REMOVED DAMAGED, NDT AREA, FABBED AND INSTALLED REPAIR IAW ECRA 482-53-181-2Oct 20, 2003 · N482EV · Boeing 747212B · Fuselage Main, Plate/SkinSDR EIA2003137Skin · chafedVERTICAL STABILIZER TO FUSELAGE RIGHT BELOW RUDDER HAS CHAFE CONDITION FROM STA 2605-2608. REMOVED DAMAGED, NDT AREA, FABBED AND INSTALLED REPAIR IAW ECRA 482-53-181-2.Oct 20, 2003 · N482EV · Boeing 747212B · Fuselage Main, Plate/SkinSDR EIA2003136Structure · damagedAFT CARGO DOOR FWD, LOWER CORNER, REPAIR DOUBLER IS CRACKED. REMOVED DAMAGED EXTERNAL DOUBLER, FABRICATED, ALODINED AND INSTALLED NEW REPAIR DOUBLER IAW ECRA 482-52-031-2 AT AFT CARGO DOOR, FWD LOWER CORNER.Oct 20, 2003 · N482EV · Boeing 747212B · Cargo/Baggage DoorsSDR EIA2003141Skin · crackedFUSELAGE BELLY SKIN CRACKING AT THE AFT EDGE OF THE EQUIPMENT COOLING OUTLET BETWEEN STRINGER 44L AND 45L AT BS 580 ( APPROX) CRACK IS BOTH FORWARD AND AFT OF COUNTER SUNK RIVET FASTNER. REMOVED DAMAGED, FABRICATED AND INSTALLED REPAIR IAW ECRA 482-53-189-2 AOct 20, 2003 · N482EV · Boeing 747212B · Fuselage Main, Plate/SkinSDR EIA2003140Web · damagedVERTICAL STAB RT HANDSIDE ACCESS PANEL 324DR AFT WEB AND GUSSET DAMAGED. REMOVED 2 EA. GUSSETS, FABRICATED 2 EA. GUSSETS, SPLICE PLATE, FILLERS (2EA) AND WEB AND INSTALLED IAW ECRA 482-55-183-2Oct 20, 2003 · N482EV · Boeing 747212B · Vertical StabilizerSDR EIA2003138Skin · chafedINSIDE LOWER SURFACE OUTBOARD SIDE NR 2 PYLON APPROX. 15 INCHES AFT OF ENGINE REAR MOUNT HAS LARGE CHAFED AREA. OB SIDE OF NR 2 PYLON SKIN REPAIRED IAW ECRA 482-54-177-2.Oct 20, 2003 · N482EV · Boeing 747212B · Nacelle/Pylon, Plate/Skin
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