Boeing 747-121

Service difficulty reports · 3,030

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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 = '747121'
  ORDER BY difficulty_date DESC"

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SDR UPS06447907Hinge · crackedINSPECTION TYPE-C FWD CARGO DOOR CUTOUT AFT DOOR HINGE FOUND ONE EA FASTENER HOLE CRACKED A TEE APPROX 0.040 INCH LONG AT 4 O/C POSITION. TEE REPLACED IAW SRM 51-10-01 PG9.Aug 15, 2006 · N682UP · Boeing 747121 · Fuselage, Door HingeSDR UPS06447889Seat Track · corrodedINSPECTION TYPE-C M/D BS 532 RBL11 SEAT TRACK RT FLANGE CORROSION. CORROSION BLEND OUT 0.025 INCH X .5 INCH X 2 INCH EXCEED SRM LIMIT. M/D BS510-630 RBL11 TRACK REPLACED AND INSTALLED IAW SRM 51-10-01 P PG9 AND 51-30-02 REFER NRC 6163 FOR DETAIL.Aug 15, 2006 · N682UP · Boeing 747121 · Fuselage, Seat/Cargo Attach FittingsSDR UPS06447887Seat Track · corrodedINSPECTION TYPE-C M/D BS556-560 RBL11 SEAT TRACK LT FLANGE CORROSION. CORROSION BLEND OUT 0.028 INCH X .5 INCH X 5 INCH EXCEED SRM LIMIT. M/D BS510-630 RBL11 TRACK REPLACED AND INSTALLED IAW SRM 51-10-01 PG 9 AND 51-30-02 REFER NRC 613 FOR DETAIL.Aug 15, 2006 · N682UP · Boeing 747121 · Fuselage, Seat/Cargo Attach FittingsSDR UPS06447886Seat Track · corrodedINSPECTION TYPE-C M/D BS583-620 RBL11 SEAT TRACK RT FLANGE CORROSION. CORROSION BLEND OUT 0.021 INCH X .5 INCH X 10 INCH EXCEED SRM LIMIT. M/D BS510-630 RBL11 TRACK REPLACED AND INSTALLED IAW SRM 51-10-01 PG 9 AND 51-30-02 REFER NRC 6163 FOR WORKING DETAIL.Aug 15, 2006 · N682UP · Boeing 747121 · Fuselage, Seat/Cargo Attach FittingsSDR UPS06447885Seat Track · corrodedINSPECTION TYPE-C M/D BS520-528 RBL11 SEAT TRACK RT FLANGE CORROSION. CORROSION BLEND OUT 0.022 INCH X .5 INCH X 3 INCH EXCEED SRM LIMT. M/D BS510-630 RBL11 TRACK REPLACED AND INSTALLED INCH SRM 51-10-01 PG 9 AND 51-30-02.Aug 15, 2006 · N682UP · Boeing 747121 · Fuselage, Seat/Cargo Attach FittingsSDR UPS06447882Seat Track · corrodedINSPECTION TYPE-C M/D BS678 RBL11 SEAT TRACK LT FLANGE CORROSION. CORROSION BLEND OUT 0.017 INCH X .5 INCH X 3 INCH EXCEED SRM LIMIT. M/D BS630-690 RBL11 TRACK REPLACED AND INSTALLED IAW SRM 51-10-01 PG 9 AND 51-30-02.Aug 15, 2006 · N682UP · Boeing 747121 · Fuselage, Seat/Cargo Attach FittingsSDR UPS06447881Seat Track · corrodedINSPECTION TYPE-C M/D BS636-639 RBL11 SEAT TRACK CROWN CORROSION. CORROSION BLEND OUT 0.035 INCH X .7500 INCH X 3 INCH EXCEED SRM LIMIT. M/D BS630-690 RBL11 TRACK REPLACED AND INSTALLED IAW SRM 51-10-01 PG 9 AND 51-30-02.Aug 15, 2006 · N682UP · Boeing 747121 · Fuselage, Seat/Cargo Attach FittingsSDR UPS06447868Floorbeam · crackedINSPECTION TYPE-C U/D RT BS340 UPR DECK FLOORBEAM UPR CHORD AND FRAME ATTACHMENT AREA 2EA FASTENER HOLES FOUND CRACK AT UPR CHORD VERTICAL FLANGE. CRACK LENGTH 0.060. U/D BS340 LBL11 TO RT MOST OB FLOORBEAM UPPER CHORD REPAIRED IAW SRM 53-10-07 FIG2.Aug 15, 2006 · N682UP · Boeing 747121 · Fuselage Main, Floor BeamSDR UPS06447856Floorbeam · corrodedBS 680 RBL12 FLOORBEAM UPPER CHORD LWR SURFACE CORROSION. CORROSION BLEND OUT 0.062" BY 2" BY 2" EXCEED SRM LIMIT. M/D BS 680 RBL13 FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 51-40-04 FIG 3 REFER NRC 6712 FOR WORKING DETAIL.Aug 15, 2006 · N682UP · Boeing 747121 · Fuselage Main, Floor BeamSDR UPS06447855Floorbeam · corrodedBS 680 LBL4 FLOORBEAM UPPER SURFACE CORROSION. CORROSON BLEND OUT 0.055" BY 2" BY 4" EXCEED SRM LIMIT. M/D BS680 LBL4 FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 51-40-04 FIG 3.Aug 15, 2006 · N682UP · Boeing 747121 · Fuselage Main, Floor BeamSDR UPS06447854Floorbeam · corrodedBS 680 RBL13 FLOORBEAM UPPER SURFACE FOUND CORRODED. CORROSION BLEND OUT 0.062" BY 1.5" BY 2" EXCEED SRM LIMIT. M/D BS 680 RBL13 FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 51-40-04 FIG 3.Aug 15, 2006 · N682UP · Boeing 747121 · Fuselage Main, Floor BeamSDR UPS06447853Seat Track · corrodedFOUND BS 760 RBL 98 SEAT TRACK CROWN DAMAGED. CORROSION BLEND OUT EXCEED SRM LIMIT. M/D RBL98 BETWEEN BS 640 AND BS 770 SEAT TRACK REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.Aug 15, 2006 · N682UP · Boeing 747121 · Fuselage, Seat/Cargo Attach FittingsSDR UPS06447851Floorbeam · corrodedBS 640 RBL75 FLOORBEAM UPPER CHORD CORROSION. CORROSION BLEND OUT 0.062" BY 2" BY 2" EXCEED SRM LIMIT. M/D BS640 RBL40 TO 98 FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 51-40-04 FIG 3.Aug 15, 2006 · N682UP · Boeing 747121 · Fuselage Main, Floor BeamSDR UPS06447847Channel · corrodedBS 552 RBL11-33 HAT SECTION CORROSION. CORROSION BLEND OUT 0.020" BY 1" BY 10" EXCEED SRM LIMIT. HAT SECTION REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.Aug 15, 2006 · N682UP · Boeing 747121 · Fuselage Miscellaneous StructureSDR UPS06447843Stringer Splice · damagedINSPECTION TYPE:C FX, RT LOWER FUSELAGE INTERIOR STRUCTURE STRINGER SPLICE RETAINER ATT HOLE FOUND ELONGATED AT STA 2180 STRINGER 44R. FX BS 2180 STR 44R STRINGER SPLICE REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.Aug 15, 2006 · N682UP · Boeing 747121 · Fuselage Main, Longeron/StringerSDR UPS06447814Channel · crackedBS787 LBL11-33 HAT SECTION CRACKED, CRACK LENGTH 1/2". HAT SECTION REPLACED AS PER SRM 51-10-01 PG 9, PART NUMBER : BAC1510-335-7075T6511.Aug 15, 2006 · N682UP · Boeing 747121 · Fuselage Miscellaneous StructureSDR UPS06448125Skin · crackedINSPECTION TYPE:C NR 4 PYLON CAP SKIN SUSPECT CRACK AT SHEARED RIVET AREA, CRACK LENGTH 1/4". NR 4 PYLON CAP SKIN REPAIRED AS PER HX TOWS NO T-747-54-0224 AND RS R54-51-35569 AND UPS ENGINEERING FILE NUMBER 747-54-20055.Aug 14, 2006 · N682UP · Boeing 747121 · Nacelle/Pylon, Plate/SkinSDR UPS06448124Skin · crackedINSPECTION TYPE:C FWD CARGO DOOR CUTOUT FWD HINGE FAIRING AREA 1 HOLE CRACK AT FX SKIN APPROX 1/16" LONG. SKIN REPAIRED AS PER RS R53-21-35571 AND REFER NRC 6304 FOR WORKING DETAIL AND UPS EO B747-5320-25077-A.Aug 14, 2006 · N682UP · Boeing 747121 · Fuselage Main, Plate/SkinSDR UPS06447964Door Frame · crackedLT BS 488 FRAME FOUND CRACK AT DOOR STOP NR 9 AREA AND TOOLING HOLE, CRACK LENGTH 1/16" AND 5/16" AND 3/16". LT BS 488 FRAME REPAIRED BETWEEN STR 16L TO STR 19L AREA AS PER SRM 53-10-04 FIG 121.Aug 14, 2006 · N682UP · Boeing 747121 · Fuselage Main, StructureSDR UPS06447671Spoiler · inoperativeDIVERSION, NR 5 SPOILER WOULD NOT RETRACT. LEFT WING NR 5 SPOILER ROD AND TRAILING EDGE SUPPORT. A/C FERRIED TO SDF FOR REPAIR. STARTED ECA FORM 011205 COMPLETED. THIS CLEARS D331371.Aug 14, 2006 · N681UP · Boeing 747121 · Drag Control SystemSDR UPS06448115Skin · corrodedINSPECTION TYPE:C RT WING L/E CAVITY LWR PANEL FOUND BULGED UP AFT OF NR 25 VC FLAP. CORROSION BLEND OUT 0.080" BY 2" BY 2" EXCEED SRM LIMIT. RT WING LOWER SKIN AT FS 1445 TO 1468 REPAIRED AS PER RS R57-26-35582 AND UPS ENGINEERING FILE NUMBER 747-57-20109.Aug 13, 2006 · N682UP · Boeing 747121 · Wing, Plate/SkinSDR UPS06447974Stringer Clip · crackedLT NLG W/W INTERNAL SIDE STA340 WL140 CLIP FOUND CRACK, CRACK LENGTH 1/4". BRACKET REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.Aug 13, 2006 · N682UP · Boeing 747121 · Fuselage Main, Attach FittingsSDR UPS06447950Skin · bulgedINSPECTION TYPE:C FX RT LWR FUSELAGE EXTERNAL SKIN SURFACE FOUND BULGED UP AT STA 1610-1613 STR 43R. SKIN REPAIRED AS PER SRM 53-30-03 FIG1 SUBSEQUENT INSPECTION ARE NECESSARY FOR CAT B REPAIR REFER SRM 53-30-03 FIG 1 TABLE 4 FOR REFERENCE.Aug 13, 2006 · N682UP · Boeing 747121 · Fuselage Main, Plate/SkinSDR UPS06447844Stringer Splice · corrodedRT LOWER FUSELAGE EXTERNAL SKIN SURFACE FOUND BILGE UP AT STA 2180 TO STA 2183 STR 44R. FASTENER AND STRINGER 44R SPLICE AT BS 2180 AREA REMOVED AND REINSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02 AFTER INSPECTION CARRIED OUT AS PER SRM 51-10-01. SKIN SURFAug 13, 2006 · N682UP · Boeing 747121 · Fuselage Main, Longeron/StringerSDR UPS06448153Rib · crackedINSPECTION TYPE:C RT WING, NR 21 VC FLAP I/B ARM I/B SUPPORT RIB FWD VERTICAL FLANGE FASTENER HOLES CRACKED, CRACK LENGTH 5/8". REPAIRED AS PER RS R57-41-35563 AND UPS EO B747-5710-25082-A.Aug 12, 2006 · N682UP · Boeing 747121 · Wing, Rib/BulkheadSDR UPS06448145Spar · corrodedINSPECTION TYPE:C FX, RT WING CENTER SECTION REAR SPAR WEB FOUND CORROSION AT BS 1241 RBL 105-106 B/H FTG BTN NR 15 AND NR 16 FASTENER HEAD (RT WING LT W/W) REMAIN THICKNESS 0.345" TO 0.389'. FX , RT WING CENTER SECTION REAR SPAR WEB CORROSION REMOVED AS PER Aug 12, 2006 · N682UP · Boeing 747121 · Wing SparSDR UPS06448083Frame · crackedINSPECTION TYPE:C M/D BS 800 RT TENSION TIE TO FRAME CONNECTION ATTACHMENT FASTENER HOLE FOUND CRACK AT FRAME, CRACK LENGTH 0.040". M/D BS 800 RT FRAME CRACKED HOLE OVERSIZED TO 0.309" AND BOLT INSTALLED AS PER RS R53-25-35568 AFTER HFEC INSPECTION PER NTM PAAug 11, 2006 · N682UP · Boeing 747121 · Fuselage Main, FrameSDR UPS06448082Plate · damagedINSPECTION TYPE:C M/D BS 800 RT TENSION TIE FWD CHANNEL ATTACHED S/STEEL PLATE SHORT EDGE MARGIN (SEM) I/B UPPER 4EA FASTENER HOLE LOWER ROW NO.1,3,4,6 COUNT FROM I/B AND O/B LOWER FASTENER HOLE. M/D BS 800 RT TENSION TIE FWD CHANNEL ATTACHED S/STEEL PLATE REAug 11, 2006 · N682UP · Boeing 747121 · Fuselage Main, StructureSDR UPS06448081Tension Tie · crackedINSPECTION TYPE:C M/D BS800 RT TENSION TIE TO FRAME CONNECTION ATTACHMENT FASTENER HOLE FOUND CRACK AT TENSION TIE FWD CHANNEL, CRACK LENGTH 0.040". M/D RT BS 800 FRAME TO TENSION TIE FWD CHANNEL REPAIRED AS PER RS R53-25-35568. CONTINUE INSPECTION ARE REQUIAug 11, 2006 · N682UP · Boeing 747121 · Fuselage Main, StructureSDR UPS06448080Plate · damagedINSPECTION TYPE:C M/D BS 800 LT TENSION TIE FWD CHANNEL ATTACHED S/STEEL PLATE SHORT EDGE MARGIN (SEM) AT I/B UPPER NR 1, 3 AND I/B LOWER FASTENER HOLE AREA. M/D BS 800 LT TENSION TIE FWD CHANNEL ATTACHED S/STEEL PLATE REPAIRED AND ALUMINUM STRAP REPLACED AS Aug 11, 2006 · N682UP · Boeing 747121 · Fuselage Main, StructureSDR UPS06448079Tension Tie · crackedINSPECTION TYPE:C M/D LT BS 800 FRAME TO TENSION TIE CONNECTION FOUND TENSION TIE AFT CHANNEL 1 HOLE CRACK, CRACK LENGTH 1/16". M/D LT BS 800 TENSION TIE AFT CHANNEL REPAIRED AS PER RS R53-25-35568 CONTINUE INSPECTION IS REQUIRED AS PER RS R53-25-35568 AND UPAug 11, 2006 · N682UP · Boeing 747121 · Fuselage Main, StructureSDR UPS06448078Plate · damagedINSPECTION TYPE:C M/D BS 920 RT TENSION TIE FWD CHANNEL ATTACHED S/STEEL PLATE SHORT EDGE MARGIN (SEM) AT I/B UPPER I/B LOWER AND O/B LWER NR 2 (COUNT FROM O/B) FASTENER HOLE. M/D BS 920 RT TENSION TIE FWD CHANNEL ATTACHED S/STEEL PLATE REPAIRED AND ALUMINUM Aug 11, 2006 · N682UP · Boeing 747121 · Fuselage Main, StructureSDR UPS06448077Plate · damagedINSPECTION TYPE:C M/D BS920 LT TENSION TIE FWD CHANNEL ATTACHED S/STEEL PLATE SHORT EDGE MARGIN (SEM) AT I/B UPPER AND LOWER FASTENER HOLE. M/D BS 920 LT TENSION TIE FWD CHANNEL ATTACHED S/STEEL PLATE REPAIRED AND ALUMINUM STRAP REPLACED AS PER RS R53-25-3556Aug 11, 2006 · N682UP · Boeing 747121 · Fuselage Main, StructureSDR UPS06448076Plate · damagedINSPECTION TYPE:C M/D BS 880 RT TENSION TIE FWD CHANNEL ATTACHED S/STEEL PLATE SHORT EDGE MARGIN (SEM) AT I/B UPPER FASTENER HOLE. M/D BS 880 RT TENSION TIE FWD CHANNEL ATTACHED S/STEEL PLATE AND ALUMINUM STRAP REPLACED AS PER RS R53-25-35565. CONTINUE INSP Aug 11, 2006 · N682UP · Boeing 747121 · Fuselage Main, StructureSDR UPS06448075Plate · damagedINSPECTION TYPE:C M/D BS 880 LT TENSION TIE FWD CHANNEL ATTACHED S/STEEL PLATE SHORT EDGE MARGIN (SEM)AT I/B UPPER I/B LOWER AND UPPER NR 2, NR 5 COUNT FROM O/B FASTENER HOLE. M/D BS 880 LT TENSION TIE FWD CHANNEL ATTACHED S/STEEL PLATE REPAIRED AND ALUMINUM Aug 11, 2006 · N682UP · Boeing 747121 · Fuselage Main, StructureSDR UPS06448074Plate · damagedINSPECTION TYPE:C M/D BS 840 RT TENSION TIE FWD CHANNEL ATTACHED S/STEEL PLATE SHORT EDGE MARGIN (SEM) AT I/B LOWER FASTENER HOLE. M/D BS 840 RT TENSION TIE FWD CHANNEL ATTACHED S/STEEL PLATE REPAIRED AS PER RS R53-25-35564. CONTINUE INSPECTION ARE REQUIRED Aug 11, 2006 · N682UP · Boeing 747121 · Fuselage Main, StructureSDR UPS06448073Frame · crackedINSPECTION TYPE:C M/D LT BS 840 FRAME TO TENSION TIE CONNECTION FOUND FRAME 1 HOLE CRACK, CRACK LENGTH 0.040". M/D LT BS 840 BETWEEN STR 8L TO STR 12L FRAME REPAIRED AS PER RS R53-25-35564 AND UPS EO B747-5310-25079-A.Aug 11, 2006 · N682UP · Boeing 747121 · Fuselage Main, StructureSDR UPS06448072Plate · damagedINSPECTION TYPE:C M/D BS 840 LT TENSION TIE FWD CHANNEL ATTACHED S/STEEL PLATE SHORT EDGE MARGIN (SEM) AT I/B UPPER AND LWR FASTENER HOLE. M/D BS840 LT TENSION TIE FWD CHANNEL ATTACHED S/STEEL PLATE REPAIRED AS PER RS R53-25-35564. CONTINUE INSPECTION ARE REAug 11, 2006 · N682UP · Boeing 747121 · Fuselage Main, StructureSDR UPS06447967Beam · crackedRT NWW VERTICAL BEAM WEB AT BS 300 FOUND CRACK AT WL 171 INSULATION BLANKET STAND OFF, CRACK LENGTH 1/8". WEB REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED PER SRM 51-30-02.Aug 11, 2006 · N682UP · Boeing 747121 · Fuselage Main, StructureSDR UPS06447898Doubler · crackedINSPECTION TYPE-C M/D BS840 RT TENSION TIE TO FRAME CONNECTION FASTENER HOLE FOUND CRACK AT WEB DOUBLER. CRACK LENGTH .0625 INCH. M/D BS840 BETWEEN S9R TO S12R FRAME ATTACHED DOUBLER REPLACED AND INSTALLED IAW SRM 51-10-01 PG9 AND 51-30-02.Aug 11, 2006 · N682UP · Boeing 747121 · Fuselage Miscellaneous StructureSDR UPS06447841Stiffener · crackedINSPECTION TYPE:C NWW TOP PANEL RBL20 STIFFENER FOUND CRACKED AT BS 290, CRACK LENGTH 3/4". NWW BS290 RBL20 TOP PANEL ATTACH STIFFENER REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.Aug 11, 2006 · N682UP · Boeing 747121 · Fuselage Miscellaneous StructureSDR UPS06447839Stiffener · crackedTOP PANEL LBL20 STIFFENER FOUND CRACKED AT BS 290, CRACK LENGTH 1/2". NWW BS 290 LBL20 TOP PANEL ATTACH STIFFENER REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.Aug 11, 2006 · N682UP · Boeing 747121 · Fuselage Miscellaneous StructureSDR UPS06448122Plate · damagedINSPECTION TYPE:C M/D LT BS 940 TENSION TIE FWD CHANNEL ATTACHED S/STEEL PLATE SHORT EDGE MARGIN AT I/B UPPER AND LOWER FASTENER HOLE. M/D LT BS 940 TENSION TIE FWD CHANNEL ATTACHED S/STEEL PLATE REPAIRED AS PER RS R53-25-35491. CONTINUE INSPECTION ARE REQUIAug 10, 2006 · N682UP · Boeing 747121 · Fuselage Main, StructureSDR UPS06448121Tension Tie · damagedINSPECTION TYPE:C M/D LT BS 940 FRAME TO TENSION TIE CONNECTION FOUND FASTENER HOLE OVAL AT TENSION TIE FWD CHANNEL. M/D LT BS 940 FRAME TO TENSION TIE FWD CHANNEL REPAIRED AS PER RS R53-25-35491. CONTINUE INSPECTION IS REQUIRED AS PER RS R53-25-35491 AND UPAug 10, 2006 · N682UP · Boeing 747121 · Fuselage Main, StructureSDR UPS06448119Plate · damagedINSPECTION TYPE:C M/D LT BS 860 TENSION TIE FWD CHANNEL ATTACHED S/STEEL PLATE SHORT EDGE MARGIN AT I/B LOWER FASTENER HOLE. BS 860 LT TENSION TIE FWD CHANNEL ATTACHED S/STEEL PLATE AND ALUMINUM STRAP REPLACED AS PER RS R53-28-35574. CONTINUE INSP ARE REQUIRAug 10, 2006 · N682UP · Boeing 747121 · Fuselage Main, StructureSDR UPS06448116Structure · corrodedINSPECTION TYPE:C FX WING CTR SECTION RT LOWER CHORD FOUND HEAVY CORROSION AT STA983 RBL 78 TO RBL 86 EXTERNAL SURFACE. CORROSION BLEND OUT 0.151" BY 1.5" BY 5" EXCEED SRM LIMIT. FX WING CTR SECTION RT LOWER CHORD REPAIRED AT RBL75 TO RBL87 AREA AS PER RS R5Aug 10, 2006 · N682UP · Boeing 747121 · Wing, Center BoxSDR UPS06448087Frame · crackedINSPECTION TYPE:C M/D RT BS780 FRAME AT TENSION TIE CONNECTION FOUND 2 HOLE CRACK AT FRAME, CRACK LENGTH 0.040". M/D RT BS 780 FRAME CRACKED HOLE OVERSIZED AS PER UPS EO B747-5310-23715. NO CRACK FOUND AFTER HFEC INSPECTED PER NTM PART 6 51-00-00 FIG 16. S/Aug 10, 2006 · N682UP · Boeing 747121 · Fuselage Main, FrameSDR UPS06448086Tension Tie · crackedINSPECTION TYPE:C M/D RT BS780 FRAME AT TENSION TIE CONNECTION FOUND 1 HOLE CRACK AT TENSION TIE AFT CHANNEL. CRACK LENGTH 1.25". M/D RT BS 780 TENSION TIE AFT CHANNEL REPAIRED AT O/B OF RT VERT POST TO RT MOST O/B AREA AS PER RS R53-25-35540. CONTINUE INSPEAug 10, 2006 · N682UP · Boeing 747121 · Fuselage Main, StructureSDR UPS06448069Doubler · crackedINSPECTION TYPE:C M/D RT BS920 FRAME AT TENSION TIE CONNECTION FOUND 1 HOLE CRACK AT WEB DOUBLER, CRACK LENGTH 0.040". M/D BS 820 RHS FRAME ATTACHED DOUBLER BETWEEN STR 9R TO STR 12R AREA REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02 AND RS R53Aug 10, 2006 · N682UP · Boeing 747121 · Fuselage Main, StructureSDR UPS06448068Tension Tie · crackedINSPECTION TYPE:C M/D LT BS900 FRAME TO TENSION TIE CONNECTION FOUND CRACK AT TENSION TIE FWD CHANNEL 1 HOLE, CRACK LENGTH 0.030". M/D LT BS 900 TENSION TIE FWD CHANNEL REPAIRED AS PER RS R53-25-35559 CONTINUE INSPECTION IS REQUIRED AS PER RS R53-25-35559 ANDAug 10, 2006 · N682UP · Boeing 747121 · Fuselage Main, Structure
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