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 WRNA200700063Sensor · no testDURING TAKEOFF, AT 80 KNOTS, CREW RECEIVED A STALL WARNING, TAKEOFF WAS ABORTED. AOA FAILED TEST IAW B747 MM 27-32-00 PG 507. REPLACED AOA SENSOR IAW 747 MM 27-32-01 PG 102. SYSTEM TEST GOOD IAW 747 MM 27-32-00 PG 507. AIRCRAFT RELEASED FOR SERVICE.Dec 20, 2007 · N526UP · Boeing 747212B · Stall Warning SystemSDR UPS07451134Battery Pack · dischargedINSPECTION TYPE:N/A EMERGENCY LIGHT ON MCD AT STA 420 LT DOES NOT TEST. REMOVED AND REPLACED EMERGENCY LIGHT/BATTERY ASSY WITH REF TO MM 33-51 51-07. OPS CHECK GOOD PER SAME.Nov 11, 2007 · N520UP · Boeing 747212B · Emergency LightingSDR EIA2007191Skin · damagedEXTERNAL SKIN AT BS 1320 HAS ELONGATED FASTENER HOLES JUST 4" AFT OF R3 DOOR CUT-OUT. REPAIRED EXTERNAL SKIN AT BS 1324 FASTENER HOLE AFT OF R3 DOOR CUT-OUT PER ECRA 482-53-220-2.Oct 29, 2007 · N482EV · Boeing 747212B · Fuselage Main, Plate/SkinSDR EIA2007192Battery Pack · inoperativeCREW SERVICE DOOR GROUND/SLIDE LIGHTS INOP MOUNTED ON DOOR JAMB. REMOVED AND REPLACED EMERGENCY BATTERY PACK PER B747 MM 33-51-04. OPS CHECKED NORMAL PER B747 MM 33-51-04 PAGE 204.Oct 26, 2007 · N482EV · Boeing 747212B · Emergency LightingSDR KCSA07073Unknown · odorSMOKE (ODOR) FROM AIR COND SYSTEM. SMOKE OBSERVED FROM FLT DECK FAN. SMOKE (ODOR) STOPPED WHEN FLT DECK FAN OFF. WHEN FLT DECK FAN ON, MADE UNUSUAL SOUND W/VIBRATION.Sep 23, 2007 · N703CK · Boeing 747212B · Air Distribution SystemSDR EIA2007159Skin · corrodedEXTERNAL FUSELAGE EMPENNAGE CUTOUT DOOR SKIN RETAINER, FRAME ARE CORRODED AND PAINT DETERIORATED. WORK ACCOMPLISHED PER ECRA NR 486-53-062-2.Sep 21, 2007 · N486EV · Boeing 747212B · Fuselage Main, Plate/SkinSDR KCSA071382Light · inoperativeUPPER DECK RT SLIDE LIGHT INOPERATIVE.Sep 19, 2007 · N703CK · Boeing 747212B · Emergency LightingSDR EIA2007164Frame · corrodedWHALE BONE (WING TO BODY FAIRING FRAME) CORRODED AT STA 880 STRINGER 46R TO 48R UPPER SURFACE OF LOWER BEAM. REPLACED WHALE BONE AT STA 880 BETWEEN STR 46R TO 48R PER ECRA NR 486-53-059-2.Sep 18, 2007 · N486EV · Boeing 747212B · Fuselage Main, FrameSDR EIA2007162Plate · misinstalledTENSION TIE STEEL PLATE STA 840 LT HAS ONE PREVIOUSELY DAMAGED FASTENER HOLE WITH SHORT ESGE MARGIN. FABRICATED REPAIR PARTS (STRAPS) PER ECRA 486-53-065-2 AND INSTALLED PER B747 SRM 51-30-02 PAGES 8-19 AND EO 53-747-1818-03 REV "A".Sep 18, 2007 · N486EV · Boeing 747212B · Fuselage Miscellaneous StructureSDR EIA2007166Pressure Panel · corrodedNOSE LANDING GEAR WHEEL WELL, RT UPPER AT APPROX STA 280 HAS CORROSION BELOW AND UNDER STANDOFF. REMOVED CORROSION UNDER LINES SUPPORT (WEB) STA 280 RT WL 190 FOUND TO BE OUT OF LIMITS PER B747 SRM 53-30-01 AND 51-10-01. CUT OUT CORRODED SECTION AND INSTALLESep 17, 2007 · N486EV · Boeing 747212B · Fuselage Main, BulkheadSDR EIA2007165Skin · crackedEXTERNAL FUSELAGE STA 390 STR 44R SKIN IS CRACKED AT FASTENER HOLE. REPAIRED EXTERNAL FUSELAGE AT STA 390 STR 44R PER ECRA NR 486-53-061-2 PART 1.Sep 17, 2007 · N486EV · Boeing 747212B · Fuselage Main, Plate/SkinSDR EIA2007161Skin · damagedRIGHT WING LANDING LIGHT SKIN PANEL OUTBOARD HAS NUMEROUS RIVETS PULLED/WORN THRU SKIN AND FASTENERS DISTRESSED. REPAIRED RT LEADING EDGE LANDING LIGHT SKIN PANEL PER ECRA NR 486-57-057-2.Sep 17, 2007 · N486EV · Boeing 747212B · Wing, Plate/SkinSDR KCSA071379Light · failedUPPER DECK AFT CEILING EMERGENCY LIGHT EXTINGUISHES AFTER 5 SECONDS.Sep 17, 2007 · N703CK · Boeing 747212B · Emergency LightingSDR EIA2007167Frame · damagedAFT PIT BOOR CUT OUT FWD LOWER SIDE FRAME WEB AND SKIN CUT. FOUND UPON REMOVAL OF SEAL DEPRESSOR FOR REPAIR. REPAIRED PER ECRA NR 486-53-064-2.Sep 14, 2007 · N486EV · Boeing 747212B · Fuselage Main, FrameSDR EIA2007160Frame · damagedFWD PIT DOOR CUT OUT, AFT LOWER SIDE, FRAME WEB HAS DRILL STARTS, NEXT TO ATTACH LOCATIONS, FOUND UPON REMOVAL OF SEAL DEPRESSOR FOR REPAIR. REPAIRED DAMAGED AREA ON WEB AT FWD PIT DOOR CUT OUT AFT LOWER SIDE PER ECRA 3 486-53-063-2.Sep 14, 2007 · N486EV · Boeing 747212B · Fuselage Main, FrameSDR EIA2007155Battery Pack · inoperativeAFT CABIN CEILING EMERGENCY LIGHT OUT. REMOVED AND REPLACED BATTERY PACK PER B747MM 33-51-04, TEST GOOD PER MM 33-51-04.Sep 9, 2007 · N485EV · Boeing 747212B · Emergency LightingSDR EIA2007157Stand Off · brokenNR 4 ENGINE NACELLE I/B INSIDE 3RD ACCESS DOOR UPPER ROW, HYD STAND OFF BRACKET IS BROKEN AT BOTTOM WITH FASTENERS PULLED THROUGH WEB FRAME. REMOVED AND REPLACED HYD STAND-OFF BRACKET AND REPLACED WEB WHERE FASTENERS PULLED THROUGH WEB FRAME ON NR 4 ENGINE NASep 5, 2007 · N486EV · Boeing 747212B · Nacelle/Pylon Miscellaneous StructureSDR EIA2007156Tension Tie · damagedSTA 800 RT TENSION TIE HAS ONE DEFECTIVE FASTENER HOLE AFTER MAX ALLOWABLE REAM TO .309" PER SB 747-53-2502 VERIFIED WITH OPEN HOLE HFEC INSPECTION. REMOVED TENTION TIE (DAMAGED). FABRICATED TENSION TIE BEAM AND SPLICE PER B747 SRM 53-10-11 FIG 2 AND INSTALLSep 4, 2007 · N486EV · Boeing 747212B · Fuselage Main, StructureSDR EIA2007158Skin · chafedNUMBER ONE ENGINE PYLON RIGHT SIDE NACELLE STA 180 TO NACELLE STA 236YLON SKIRT CHAFED AND FASTENERS SHEARED. REMOVED EXISTING DAMAGE NR 1 PYLON, RT SKIRT REPAIR DOUBLER AND SHEARED FASTENERS, FABRICATED AND INSTALLED NEW REPAIR DOUBLER AND NEW FASTENERS ON NAug 28, 2007 · N486EV · Boeing 747212B · Nacelle/Pylon, Plate/SkinSDR EIA2007151Light · no testEMERGENCY EXIT LIGHT AT ATATION 400 UPPER DECK BY CREW DOOR INOP. REPLACED SODERBERG EMERGENCY EXIT LIGHT AT STATION 400 PER B747MM 33-51-00. OPS CHECKED GOOD.Aug 25, 2007 · N485EV · Boeing 747212B · Emergency LightingSDR KCSA071313Attach Angle · wornATTACH ANGLE HAS WORN HOLES AT STA 1480 WL 100 LBL 113.Aug 17, 2007 · N703CK · Boeing 747212B · Fuselage Miscellaneous StructureSDR KCSA071312Longeron · damagedLONGERON BOX LOWER CHANNEL AT STA 1438 TO1480 IS DAMAGED AT AFT END WL 100 LBL 113.Aug 17, 2007 · N703CK · Boeing 747212B · Fuselage Main, Longeron/StringerSDR UPS07450565Rib · crackedINSPECTION TYPE:C NR 1 PYLON REAR ENG MOUNT BULKHEAD ATTACHMENT UPPER LINK BEAM O/B SIDE RIB ANGLE FOUND CRACKED FWD SIDE, CRACK LENGTH 1" BY 1/2". NR 1 PYLON REAR ENG MOUNT BULKHEAD ATTACHMENT UPPER LINK BEAM O/B SIDE RIB ANGLE REPAIRED AS PER HX RS NR R54-51Aug 13, 2007 · N521UP · Boeing 747212B · Nacelle/Pylon, Frame/Spar/RibSDR UPS07450563Rib · crackedINSPECTION TYPE:C NR 1 PYLON DRY BAY UPPER LINK STRUT BEAM O/B SIDE ATTACHMENT RIB ANGLE FOUND CRACKED AS MARKED NAC STA 223 (AFT SIDE) , CRACK LENGTH 5/8" APPROX NR 1 PYLON DRY BAY UPPER LINK STRUT BEAM O/B SIDE ATTACHMENT RIB ANGLE REPAIRED AS PER HX RS NR RAug 13, 2007 · N521UP · Boeing 747212B · Nacelle/Pylon, Frame/Spar/RibSDR UPS07450548Spar · crackedINSPECTION TYPE:C LHW O/B MID FLAP REAR SPAR O/B UPPER CHORD FOUND CRACKED, CRACK LENGTH 18" APPROX. LHW O/B MID FLAP REAR SPAR O/B UPPER CHORD BETWEEN WBL 801 TO MOST O/B AREA REPAIRED AS PER HX RS NR R57-58-35853 AND UPS ENGINEERING FILE NR 747-57-20148.Aug 12, 2007 · N521UP · Boeing 747212B · Trailing Edge FlapsSDR EIA2007163Frame · dentedIN FWD PIT BILGE AREA DENT IN BS 560 FRAME WEB LBL19. IN FWD PIT BS 560 LBL 19 MEASURED DENT IN FRAME WERE FOUND TO BE OUT OF LIMITS PER SRM 53-10-01 FIG 1. REMOVED DAMAGE PER B747 SRM 51-40-02 FIG 1, FABRICATED DOUBLER PER B747 SRM 51-20-01 PAGES 11, 14-20 Aug 11, 2007 · N486EV · Boeing 747212B · Fuselage Main, FrameSDR UPS07450546Frame · crackedINSPECTION TYPE:C E/E COMPT STA400 FRAME INNER CHORD FOUND CRACKED AT S44L, CRACK LENGTH 5/8". E/E COMPT BS 400 FRAME INNER CHORD AT ABOVE STR 44L AREA REPAIRED AS PER SRM 51-40-04 FIG 3.Aug 11, 2007 · N521UP · Boeing 747212B · Fuselage Main, FrameSDR UPS07450560Bear Strap · crackedINSPECTION TYPE:C M/D RT NR 3 MED CUTOUT FWD LOWER CORNER FOUND SKIN CRACK AND BEARSTRAP CORROSION, CRACK LENGTH 1/16 INCH APPROX. M/D RT NR 3 MED CUTOUT FWD LOWER CORNER SKIN AND BEAR STRAP REPAIRED AS PER UPS EO B747-5330-24674 APPENDIX 'N', BEAR STRAP CORRAug 10, 2007 · N521UP · Boeing 747212B · Fuselage Main, Plate/SkinSDR UPS07450559Skin · crackedINSPECTION TYPE:C M/D LT NR 3 MED CUTOUT FWD LOWER CORNER FOUND SKIN AND BEAR STRAP CRACK, CRACK LENGTH 0.040" TO 3/4". M/D LT NR 3 MED CUTOUT FWD LOWER CORNER SKIN AND BEARSTRAP REPAIRED AS PER UPS EO NR B747-5330-24674 APPX 'M'.Aug 10, 2007 · N521UP · Boeing 747212B · Fuselage Main, Plate/SkinSDR UPS07450564Support · corrodedINSPECTION TYPE:C FX AIR CONDITIONING BAY PANEL SUPPORT FRAME FOUND CORROSION AT STA 1018 TO STA 1045 LBL 58, CORROSION BLEND OUT 0.045" BY 1" BY 1" EXCEED SRM 53-10-01 FIG 1 LIMITS, FX BS 987 TO BS 1060 LBL 58" FAIRING SUPPORT REPAIRED AS PER SRM 51-40-04 FIAug 8, 2007 · N521UP · Boeing 747212B · Fuselage Miscellaneous StructureSDR UPS07450545Reveal · corrodedINSPECTION TYPE:C M/D L1 DOOR FWD CUTOUT REVEAL NR 9 STOP FTG DOUBLER BULGED UP. M/D L1 DOOR FWD CUTOUT REVEAL NR 9 STOP FTG AREA SPLICE DOUBLER REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.Aug 8, 2007 · N521UP · Boeing 747212B · Fuselage Miscellaneous StructureSDR UPS07450567Skin · crackedINSPECTION TYPE:C U/D LT BS 340-360 S5L LOCATION FOUND 1 HOLE CRACK AT FX SKIN RUNNING FWD AND AFT APPROX 1/8" BEYOND RIVET HEAD FX BS 340-360 STR 5L AREA SKIN REPAIRED WITH OUT ZERO TIMING AT CRITICAL ROW FASTENER AS PER SRM 53-30-03 FIG 1 AND UPS EO B747-533Aug 7, 2007 · N521UP · Boeing 747212B · Fuselage Main, Plate/SkinSDR UPS07450558Skin · crackedINSPECTION TYPE:C U/D RT BS 340-360 S5R LOCATION FOUND 1 HOLE CRACK AT FX SKIN RUNNING FWD AND AFT APPROX 1/8" BEYOND RIVET HEAD. FX BS340-360 STR5R AREA SKIN REPAIRED WITHOUT ZERO TIMING AT CRITICAL ROW FASTENER AS PER SRM 53-30-03 FIG 1 AND UPS EO B747-5330Aug 7, 2007 · N521UP · Boeing 747212B · Fuselage Main, Plate/SkinSDR UPS07450543Shear Tie · damagedINSPECTION TYPE:C M/D BS 940 LT TENSION TIE STEEL PLATE FOUND SEM. M/D BS 940 LT TENSION TIE ATTACH STEEL PLATE REPLACED AND INSTALLED AS PER HX RS NR R53-25-35850 CONTINUE INSPECTION ARE REQUIRED AS PER UPS EO B747-5310-27442.Aug 7, 2007 · N521UP · Boeing 747212B · Fuselage Internal Mounting StructureSDR UPS07450542Shear Tie · damagedINSPECTION TYPE:C M/D BS 900 LT TENSION TIE STEEL PLATE FOUND SEM. M/D LT BS 900 TENSION TIE STEEL PLATE REPAIRED AS PER HX RS NR R53-25-35847 AND REPEAT INSPECTION IS REQUIRED AS PER UPS EO NR B747-5310-27440.Aug 7, 2007 · N521UP · Boeing 747212B · Fuselage Internal Mounting StructureSDR UPS07450541Shear Tie · damagedINSPECTION TYPE:C M/D BS 900 RT TENSION TIE STEEL PLATE FOUND SEM. M/DECK BS 900 RT TENSION TIE ATTACH STEEL PLATE REPAIRED. AS PER HX RS NR R53-25-35847 REPEAT INSPECTION IS REQUIRED AS PER UPS EO NR B747-5310-27440.Aug 7, 2007 · N521UP · Boeing 747212B · Fuselage Internal Mounting StructureSDR UPS07450544Plate · damagedINSPECTION TYPE:C M/D BS 920 RHS TENSION TIE TO FRAME STEEL PLATE 2EA HOLE FOUND SEM AT MOST O/B AS MARKED. M/D BS 920 RT TENSION TIE ATTACH STEEL PLATE REPLACED AND INSTALLED AS PER HX RS NR R53-25-35848 AND REPEAT INSPECTION IS REQUIRED AS PER UPS EO NR B74Aug 6, 2007 · N521UP · Boeing 747212B · Fuselage Miscellaneous StructureSDR UPS07450540Channel · crackedINSPECTION TYPE:C M/D RT BS 840 TENSION TIE TO FRAME CONNECTION FOUND NR 8 HOLE CRACK AND NR 20 HOLE OVAL AT FWD CHANNEL.(CRACK LENGTH 0.040"). M/D RT BS 840 TENSION TIE FWD CHANNEL REPAIRED AS PER SRM 53-10-11 FIG 2 REPEAT INSPECTION IS REQUIRED AS PER SRM 5Aug 6, 2007 · N521UP · Boeing 747212B · Fuselage Miscellaneous StructureSDR WRNA200700045Transmitter · malfunctionedON APPROACH TO ANC, OUTBOARD TRAILING EDGE FLAP HAD AN ASYMMETRICAL TRIP AND NR 2 LT LEADING EDGE FLAP DID NOT EXTEND. CONTINUED APPROACH AND MADE A SAFE LANDING. REPLACED FLAP POSITION TRANSMITTER IAW MM 27-58-01 PAGE 401, SYSTEM CHECKED NORMAL AND LEADING Jul 20, 2007 · N526UP · Boeing 747212B · Trailing Flap Position Indicating SystemSDR UPS07450267Support · crackedINSPECTION TYPE:C M/D BS 930-940 LBL30 TENSION TIE SUPPORT FOUND CRACK, CRACK LENGTH 3/8". M/D BS 920-940 LBL30 TENSION TIE SUPPORT REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.Jul 14, 2007 · N522UP · Boeing 747212B · Fuselage Miscellaneous StructureSDR UPS07450266Support · crackedINSPECTION TYPE:C M/D BS920-940 RBL30 TENSION TIE SUPPORT FOUND CRACK, CRACK LENGTH 5/16". M/D BS 920-940 RBL30 TENSION TIE SUPPORT REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.Jul 14, 2007 · N522UP · Boeing 747212B · Fuselage Miscellaneous StructureSDR UPS07450277Floorbeam · corrodedINSPECTION TYPE:C AFT CARGO COMPT CARGO FLOORBEAM UPPER TEE FOUND CORROSION AT STA 1920 CARGO NET ATT HOOK RBL4 TO LBL4. CORROSION BLEND OUT 0.045" BY 1.5" BY 2". AFT CARGO COMPT BS 1920 LBL 42 TO RBL 42 FLOORBEAM UPPER CHORD REPLACED AND INSTALLED AS PER SRJul 10, 2007 · N522UP · Boeing 747212B · Fuselage Main, Floor BeamSDR UPS07450271Sill · crackedINSPECTION TYPE:C M/D L1 DOOR SILL FOUND CRACK, CRACK LENGTH 1" APPROX. M/D L1 DOOR SILL AT BS 434 TO BS 440 WEB REPAIRED AS PER SRM 51-40-02 FIG 1.Jul 9, 2007 · N522UP · Boeing 747212B · Fuselage Miscellaneous StructureSDR UPS07450289Door Frame · crackedINSPECTION TYPE:C M/D AFTER FURTHER FASTENER REMOVED INNER CHORD AREA S23L - 26L FOUND TOTAL HOLES CRACK AT DIFFERENT STACK UP STRUCTURES (FRAME,STRAP, INNER CHORD OR REVEAL) (CRACK LENGTH 0.050" & THROUGH THICKNESS) M/D BS2231 FRAME ATTACH REVEAL REPAIREDJul 8, 2007 · N522UP · Boeing 747212B · Fuselage Main, StructureSDR UPS07450288Frame · crackedINSPECTION TYPE:C M/D AFTER FURTHER FASTENER REMOVED, RT BS 2231 FRAME INNER CHORD AREA S23R-26R FOUND TOTAL 4 HOLES CRACK AT DIFFERENT STACK UP STRUCTURES (FRAME STRAP, INNER CHORD) (CRACK LENGTH 0.040",1/16", THROUGH THICKNESS). M/DECK BS 2231 FRAME ATTACHJul 8, 2007 · N522UP · Boeing 747212B · Fuselage Main, FrameSDR UPS07450263Shear Tie · corrodedINSPECTION TYPE:C AFT OF BULK CARGO COMPT SKIN ATT ANGLE FOUND BULGE AT STA 2200 BTN S42L AND S37L. CORROSION BLEND OUT EXFOLIATION THROUGH WHOLE THICKNESS. AFT OF BULK CARGO COMPT BS 2200 STR 37L TO STR 42L FRAME ATTACH SUPPORT ANGLE REPLACED AND INSTALLED Jul 8, 2007 · N522UP · Boeing 747212B · Fuselage Internal Mounting StructureSDR UPS07450249Sill · crackedINSPECTION TYPE:C M/D RT BS434 TO BS 440 FLOOR SILL WEB CORROSION CRACK REVEALED, CRACK LENGTH 1" APPROX. M/D BS 434 TO BS 440 DOOR 1R SILL WEB REPAIRED AS PER SRM 51-40-02 FIG 1.Jul 8, 2007 · N522UP · Boeing 747212B · Fuselage Miscellaneous StructureSDR UPS07450268Reveal · crackedINSPECTION TYPE:C M/D R3 DOOR FWD LOWER CUTOUT CORNER REVEAL FOUND CRACK AS MARKED, CRACK LENGTH 1/2" APPROX. M/D R3 DOOR FWD LOWER CUTOUT CORNER REVEAL FTG REPLACED AN INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.Jul 7, 2007 · N522UP · Boeing 747212B · Fuselage Miscellaneous StructureSDR UPS07450265Reveal · crackedINSPECTION TYPE:C M/D L3 DOOR FWD CUTOUT LWR CORNER REVEAL FTG FOUND CRACK, CRACK LENGTH 3/4" APPROX. M/D L3 DOOR FWD CUTOUT LWR CORNER REVEAL FTG REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.Jul 7, 2007 · N522UP · Boeing 747212B · Fuselage Miscellaneous StructureSDR UPS07450319Skin · crackedINSPECTION TYPE:C NR 3R MED CUTOUT FWD LOWER CORNER FOUND SKIN AND BEARSTRAP EDGE CRACKED. NR 3R MED CUTOUT FWD LOWER CORNER SKIN AND BEARSTRAP REPAIRED AS PER UPS EO B747-5310-24674 APP N.Jul 6, 2007 · N522UP · Boeing 747212B · Fuselage Main, Plate/Skin
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