Boeing 747 212B

Service difficulty reports · 2,202

Newest first. General aviation reporting is voluntary.

Query with SQL
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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR UPS07450306Skin · crackedINSPECTION TYPE:C NR 3L MED CUTOUT FWD LOWER CORNER FOUND SKIN AND BEARSTRAP EDGE CRACKED, CRACK LENGTH 1/16" TO 5/8" RESP. NR 3L MED CUTOUT FWD LOWER CORNER SKIN AND BEARSTRAP REPAIRED AS PER UPS EO B747-5330-24674 APP M.Jul 6, 2007 · N522UP · Boeing 747212B · Fuselage Main, Plate/SkinSDR UPS07450280Bear Strap · crackedINSPECTION TYPE:C NR 3R MED CUTOUT AFT UPPER CORNER FOUND SKIN AND BEARSTRAP EDGE CRACKED, CRACK LENGTH 1/8" TO 2". NR 3R MED CUTOUT AFT UPPER CORNER SKIN AND BEARSTRAP REPAIRED AS PER UPS EO B747-5330-24674 APPENDIX P & L.Jul 6, 2007 · N522UP · Boeing 747212B · Fuselage Main, Plate/SkinSDR UPS07450273Frame · crackedINSPECTION TYPE:C M/D RT BS 2231 FRAME INNER CHORD S23R-25R FOUND 2 HOLES CRACK AT FRAME STRAP, CRACK LENGTH 1/16" AND 0.040". M/D BS 2231 FRAME ATTACH INNER CHORD AND STRAP AT BEN STR 22R TO STR26R AREA REPAIRED AS PER SRM 53-10-04 FIG 115. CONTINUE INSP REJul 6, 2007 · N522UP · Boeing 747212B · Fuselage Main, FrameSDR UPS07450264Skin · crackedINSPECTION TYPE:C NR 3L MED CUTOUT AFT UPPER CORNER FOUND SKIN AND BEARSTRAP EDGE FOUND CRACKED, CRACK LENGTH 1/8" APPROX. NR 3L MED CUTOUT AFT UPPER CORNER AND BEARSTRAP REPAIRED AS PER UPS EO B747-5330-24674 APP I AND O.Jul 6, 2007 · N522UP · Boeing 747212B · Fuselage Main, Plate/SkinSDR UPS07450254Stringer Clip · crackedINSPECTION TYPE:C AFT CARGO COMPT S33L STRINGER CLIP FOUND CRACKED AT STA 1760, CRACK LENGTH 5/16". AFT CARGO COMPT BS 1760 STR 33L STRINGER CLIP REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.Jul 6, 2007 · N522UP · Boeing 747212B · Fuselage Main, Attach FittingsSDR UPS07450253Intercostal · crackedINSPECTION TYPE:C LT FUSELAGE SKIN AREA AT BS 340-350 STR 5A 1 FASTENER HOLE FOUND CRACKED AT INTERCOSTAL. (1ST LAYER FROM I/B) RUNNING DOWNWARD APP 0.030" IN LENGTH (REFER SKETCH FOR DETAIL). LT FUSELAGE SKIN BS 340-360 STR 5A ATTACHED INTERCOSTAL REPLACED AJul 6, 2007 · N522UP · Boeing 747212B · Fuselage Miscellaneous StructureSDR UPS07450250Frame · crackedINSPECTION TYPE:C M/D LT BS2231 FRAME INNER CHORD S24L-25L FOUND 1 HOLE CRACK AT FRAME STRAP RUNNING FWD APPROX 1/8". M/D BS2231 FRAME ATTACH INNER CHORD AND STRAP REPAIRED BTN STR22L TO 26L AREA AS PER SRM 53-10-04 FIG 115. CONTINUE INSPECTION ARE REQ AS PEJul 6, 2007 · N522UP · Boeing 747212B · Fuselage Main, FrameSDR UPS07450248Intercostal · crackedINSPECTION TYPE:C NWW TOP PANEL LBL20 INTERCOSTAL FOUND CRACK AT 1 FASTENER LOCATION AT BS290 AS MARKED, CRACK LENGTH 1/2". NWW TOP PANEL AT BS 290 LBL20 INTERCOSTAL REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.Jul 6, 2007 · N522UP · Boeing 747212B · Fuselage Miscellaneous StructureSDR WRNA200700044Unknown · sparksON TAXI OUT, DURING FLIGHT CONTROL CHECK, CREW IN AIRCRAFT FOLLOWING BEHIND REPORTED SPARKS COMING FROM RT AILERONS, RETURNED TO BLOCKS. RAN NR 3 AND NR 4 ENGINES IAW 71-00-00, ACCOMPLISHED OPERATION CHECK OF GENERATORS IAW 24-21-01 PG 601. OPENING AND CLOSIJul 5, 2007 · N526UP · Boeing 747212B · Aileron Control SystemSDR UPS07450318Stringer Splice · crackedINSPECTION TYPE:C FWD CARGO COMPT S31R STRINGER SPLICE FOUND CRACKED AT STA738. CRACK LENGTH 1/4". FWD CARGO COMPT BS 738 STR 31R STRINGER SPLICE REPLACED AND INSTALLED AS PER SRM 51-10-01 PG9 AND 51-30-02.Jul 5, 2007 · N522UP · Boeing 747212B · Fuselage Main, Longeron/StringerSDR UPS07450317Stiffener · corrodedINSPECTION TYPE:C RT W/G W/W STIFFENER APPEAR CORRODED AT STA1241 RBL 63. RT W/G W/W AT BS 1241 RBL63 VERTICAL STIFFENER REPLACED AND INSTALLED AS PER SRM 51-10-10 PG 9 AN 51-30-02.Jul 5, 2007 · N522UP · Boeing 747212B · Wing Miscellaneous StructureSDR UPS07450308Stringer Clip · crackedINSPECTION TYPE:C FWD CARGO COMPT S33L STRINGER CLIP FOUND CRACKED AT STA780, CRACK LENGTH 1/4". FWD CARGO COMPT BS 780 STR 33L STRINGER CLIP REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 3 AND 51-30-02.Jul 5, 2007 · N522UP · Boeing 747212B · Fuselage Main, Attach FittingsSDR UPS07450301Floorbeam · corrodedINSPECTION TYPE:C M/D BS2340 LBL40-59 FLOORBEAM UPPER CHORD FOUND SEVERAL AREAS OF CORROSION. CORROSION BLEND OUT 0.040" BY 1" BY 3" EXCEED SRM LIMIT. M/D BS 2340 LBL 25 TO LT MOST O/B FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 51-40-04 FIG 1.Jul 5, 2007 · N522UP · Boeing 747212B · Fuselage Main, Floor BeamSDR UPS07450293Support · corrodedINSPECTION TYPE:C RT WING WS500 L/E MOST FWD INTERIOR LOWER SUPPORT CHORD BULGED AS MARK. CORROSION BLEND OUT EXFOLIATION THROUGH WHOLE THICKNESS EXCEED SRM LIMIT. RHW WS 492 TO WS 508 L/E MOST FWD INTERIOR LOWER SUPPORT REPAIRED AS PER SRM 51-40-03 FIG 1.Jul 5, 2007 · N522UP · Boeing 747212B · Wing Main, Frame StructureSDR UPS07450290Skin · crackedINSPECTION TYPE:C AFT CARGO DOOR CUTOUT FWD UPPER CORNER SKIN REPAIRED AS PER HX RS NR R53-61-35822, CRACK LENGTH 0.030" AND 0.090"). AFT CARGO DOOR CUTOUT FWD UPPER CORNER SKIN REPAIRED AS PER HX RS NR R53-61-35822. CONTINUE INSPECTION ARE REQUIRED AS PER HJul 5, 2007 · N522UP · Boeing 747212B · Fuselage Main, Plate/SkinSDR UPS07450281Support Angle · crackedINSPECTION TYPE:C FWD CARGO COMPT STA 1000 BULKHEAD 1 SUPPORT ANGLE FOUND CRACKED AT LBL 100 WL 155, CRACK LENGTH 1/2". FWD CARGO COMPT BS 1000 BULKHEAD AT LBL 100 WL 155 SUPPORT ANGLE REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.Jul 5, 2007 · N522UP · Boeing 747212B · Fuselage Miscellaneous StructureSDR UPS07450279Stiffener · corrodedINSPECTION TYPE:C RT W/G W/W STIFFENER CORROSION AT STA 1241 RBL 85, CORROSION BLEND OUT 0.105" BY 2" BY 4" EXCEED SRM 57-10-01 FIG 1 LIMITS. RT W/G W/W AT BS 1241 RBL 85" VERT STIFFENER REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.Jul 5, 2007 · N522UP · Boeing 747212B · Fuselage Miscellaneous StructureSDR UPS07450278Shear Tie · corrodedINSPECTION TYPE:C RT W/G REAR SPAR WS 375 UPPER FIXED PANEL SUPPORT APPEARED CORRODED. CORROSION BLEND OUT EXFOLIATION THROUGH WHOLE THICKNESS 2" BY 3/4" EXCEED SRM LIMIT. RT W/G REAR SPAR WS375 UPPER FIXED PANEL SUPPORT REPAIRED AS PER SRM 51-40-04 FIG 2.Jul 5, 2007 · N522UP · Boeing 747212B · Wing Main, Frame StructureSDR UPS07450276Floor Support · corrodedINSPECTION TYPE:C M/D STA2300-2320 LBL34 FLOOR SUPPORT FOUND SEVERAL CORROSION. CORROSION BLEND OUT 0.023" BY 1" BY 4" EXCEED SRM LIMIT. M/D BS 2300-2320 LBL34 FLOOR SUPPORT REPLACED AND INSTALED AS PER SRM 51-10-01 PG 9 AND 51-30-02.Jul 5, 2007 · N522UP · Boeing 747212B · Fuselage Miscellaneous StructureSDR UPS07450275Floorbeam · corrodedINSPECTION TYPE:C M/D BS 2360 LBL 55 FLOORBEAM UPPER CHORD FOUND CORROSION. CORROSION BLEND OUT 0.047" BY 1" BY 2" EXCEED SRM LIMIT. M/D BS 2360 LBL25 TO LT MOST O/B AREA FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 51-40-04 FIG 1.Jul 5, 2007 · N522UP · Boeing 747212B · Fuselage Main, Floor BeamSDR UPS07450274Crease Beam · crackedINSPECTION TYPE:C RT FX CROWN BS980-1000 UPPER CREASE BEAM FWD RADIUS FOUND CRACK APPROX 1" LONG. FX CROWN BS 980-1000 RT UPPER CREASE BEAM REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.Jul 5, 2007 · N522UP · Boeing 747212B · Fuselage Main, StructureSDR UPS07450272Floorbeam · crackedINSPECTION TYPE:C M/D BS 2300 LBL50 FLOORBEAMS WEB REAR SIDE STIFFENER FOUND CRACKED AS MARKED, CRACK LENGTH 3/8". M/D BS 2300 LBL50 FLOORBEAM WEB REAR SIDE STIFFENER REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.Jul 5, 2007 · N522UP · Boeing 747212B · Fuselage Main, Floor BeamSDR UPS07450261Crease Beam · crackedINSPECTION TYPE:C RT FX CROWN BS960-980 LOWER CREASE BEAM FWD FLANGE FOUND CRACK APPROX 1/2" LONG. FX CROWN BS 960-980 RT LOWER CREASE BEAM REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.Jul 5, 2007 · N522UP · Boeing 747212B · Fuselage Main, StructureSDR UPS07450260Crease Beam · crackedINSPECTION TYPE:C FX CROWN BS 940-960 LOWER CREASE BEAM FWD FLANGE RADIUS FOUND CRACK APPROX 3/8" LONG. FX CROWN BS 940-960 LOWER CREASE BEAM REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.Jul 5, 2007 · N522UP · Boeing 747212B · Fuselage Main, StructureSDR UPS07450259Crease Beam · crackedINSPECTION TYPE:C LT FX CROWN BS 960-980 UPPER CREASE BEAM FWD FRAME ATTACH ANGLE RADIUS FOUND CRACK APPROX 1/2" LONG. FX CROWN BS960-980 LT UPPER CREASE BEAM FWD FRAME ATTACH ANGLE REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.Jul 5, 2007 · N522UP · Boeing 747212B · Fuselage Main, StructureSDR UPS07450258Crease Beam · crackedINSPECTION TYPE:C RT FX CROWN BS 960-980 UPPER CREASE BEAM FWD FRAME ATTACH ANGLE RADIUS FOUND CRACK APPROX 1/2" LONG. FX CROWN BS 960-980 RT UPPER CREASE BEAM FWD FRAME ATTACH ANGLE REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.Jul 5, 2007 · N522UP · Boeing 747212B · Fuselage Main, StructureSDR UPS07450257Stringer Clip · crackedINSPECTION TYPE:C AFT CARGO COMPT S33L STRINGER CLIP FOUND CRACKED AT STA1680, CRACK LENGTH 3/8". AFT CARGO COMPT BS 1680 STR33L STRINGER CLIP REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.Jul 5, 2007 · N522UP · Boeing 747212B · Fuselage Main, Attach FittingsSDR UPS07450255Panel Support · crackedINSPECTION TYPE:C AFT CARGO COMPT SLOPE PANEL LT SIDE UPPER SUPPORT FOUND CRACKED AT STA 1540, CRACK LENGTH 1/2". AFT CARGO COMPT BS 1530 TO BS 1550 LT SIDE SLOPE PANEL UPPER SUPPORT REPAIRED AS PER SRM 51-40-03 FIG 2.Jul 5, 2007 · N522UP · Boeing 747212B · Fuselage Miscellaneous StructureSDR UPS07450252Stringer · crackedINSPECTION TYPE:C FWD CARGO COMPT S30L STRINGER FOUND DAMAGED AT STA 550, CRACK LENGTH 7/16". FWD CARGO COMPT BS 550 STR 30L STRINGER REPAIRED AS PER SRM 53-10-03 FIG 2. REPEAT INSPECTION IS REQUIRED AS PER SRM 53-10-03 FIG 2 SHEET 4 TABLE 3. UPS MPI NR P109Jul 5, 2007 · N522UP · Boeing 747212B · Fuselage Main, Longeron/StringerSDR UPS07450251Door Frame · chafedINSPECTION TYPE:C APU COMPT AFT DOOR CUTOUT SUPPORT FRAME LWR FLANGE LWR SURFACE FOUND CHAFED MARKED. APU COMPT AFT DOOR CUTOUT SUPPORT FRAME LWR FRAME REPAIRED AS PER SRM 51-40-03 FIG 2.Jul 5, 2007 · N522UP · Boeing 747212B · Fuselage Main, StructureSDR UPS07450245Stringer · deformedINSPECTION TYPE:C FWD CARGO COMPT S38L STRINGER FOUND DEFORM AT STA 485, FWD CARGO COMPT BS 484 TO BS 496 STR38L STRINGER REPAIRED AS PER SRM 53-10-03 FIG 3.Jul 5, 2007 · N522UP · Boeing 747212B · Fuselage Main, Longeron/StringerSDR UPS07450320Skin · crackedINSPECTION TYPE:C U/D FX SKIN AT BS340-350 S5-5A FOUND CRACKS AT 3 FASTENER HOLES, CRACK LENGTH 1/16, 1/2 AND 9/16". FX BS 340 TO 350 STR5L SKIN REPAIRED WITHOUT ZERO TIMING AT CRITICAL ROW FASTENERS AS PER SRM 53-30-03 FIG 1 AND TAR S/N 127807 REV A REPEAT IJul 4, 2007 · N522UP · Boeing 747212B · Fuselage Main, Plate/SkinSDR UPS07450315Skin · crackedINSPECTION TYPE:C U/D FX SKIN AT BS 340 S5-5A FOUND CRACK AT 1 FASTENER HOLE CRACK LENGTH 1/16". FX BS 340 BETWEEN STR 5R TO 5 AR SKIN REPAIRED WITHOUT ZERO TIMING AT CRITICAL ROW FASTENERS AS PER SRM 53-30-03 FIG 1 AND TAR S/N 127808 REV A REPEAT INSP IS REQJul 4, 2007 · N522UP · Boeing 747212B · Fuselage Main, Plate/SkinSDR UPS07450270Panel · bulgedINSPECTION TYPE:C LWS 888 L/E LOWER FIXED PANEL FWD BULGED AS MARKED. CORROSION BLEND OUT 0.040" BY 1" BY 2". LHW L/E WS888 LOWER FIXED PANEL FWD SUPPORT REPAIRED AS PER SRM 51-40-04 FIG 1.Jul 4, 2007 · N522UP · Boeing 747212B · Wing, Plate/SkinSDR UPS07450269Floorbeam · crackedINSPECTION TYPE:C M/D STA2280 LBL39 FLOORBEAMS WEB REAR SIDE FOUND SEVERAL CRACKS, CRACK LENGTH 1/4". M/D BS 2280 LBL 39 FLOORBEAM WEB REPAIRED AS PER SRM 51-40-02 FIG 1.Jul 4, 2007 · N522UP · Boeing 747212B · Fuselage Main, Floor BeamSDR UPS07450256Support · crackedINSPECTION TYPE:C AFT CARGO COMPT DIVIDER SUPPORT HOOK AREA FOUND CRACKED AT STA 1920 LBL 4 TO RBL 4 FLOOR AREA, CRACK LENGTH 2". AFT CARGO COMPT DIVIDER SUPPORT AT BS 1920 LBL 42 TO RBL 42 REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.Jul 4, 2007 · N522UP · Boeing 747212B · Fuselage Miscellaneous StructureSDR UPS07450246Skin · dentedINSPECTION TYPE:C EMP LT TAIL CONE SKIN FOUND DENT MARK AT STA 2725 BTN S0L AND S1L. EMP LT TAIL CONE SKIN AT BS2725 BTN STR 0 AND STR 1L SKIN REPAIRED AS PER SRM 53-30-03 FIG 1A.Jul 4, 2007 · N522UP · Boeing 747212B · Fuselage Main, Plate/SkinSDR UPS07450322Channel · crackedINSPECTION TYPE:C LT BS 880 TENSION TIE NR 6 HOLE FOUND CRACK AT AFT CHANNEL APPROX 0.040" RUNNING UP. M/D BS 880 TENSION TIE AFT CHANNEL REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER UPS EO B747-5310-23715-C AND SRM 51-30-02 REFER NRC 50076 FOR WORKJul 3, 2007 · N522UP · Boeing 747212B · Fuselage Miscellaneous StructureSDR UPS07450321Channel · crackedINSPECTION TYPE:C RT BS940 TENSION TIE TO FRAME CONNECTION AREA FOUND 2 FASTENER HOLES CRACKED AND 3 FASTENER HOLES OVAL AT AFT CHANNEL. M/D BS 940 RT TENSION TIE AFT CHANNEL LT TO RT REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02 AND EO B747-53Jul 3, 2007 · N522UP · Boeing 747212B · Fuselage Miscellaneous StructureSDR UPS07450316Plate · misinstalledINSPECTION TYPE:C M/ BS940 LT TENSION TIE FWD ATT STEEL PLATE UPPER ROW MOST I/B FASTENER HOLE FOUND SHORT EDGE MARGIN. M/D BS 940 LT TENSION TIE FWD ATTACH STEEL PLATE REPLACED AND INSTALLED AS PER RS R53-25-35824 AND EO B747-5310-23715-C. CONTINUED INSPECTJul 3, 2007 · N522UP · Boeing 747212B · Fuselage Miscellaneous StructureSDR UPS07450313Channel · crackedINSPECTION TYPE:C RT BS 940 TENSION TIE TO FRAME CONNECTION AREA FOUND 1 FASTENER HOLE CRACKED AND 3 FASTENER HOLES OVAL AT FWD CHANNEL, CRACK LENGTH 0.090" APPROX. M/D BS 940 RT TENSION TIE FWD CHANNEL LT TO RT REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9Jul 3, 2007 · N522UP · Boeing 747212B · Fuselage Miscellaneous StructureSDR UPS07450309Keelbeam · corrodedINSPECTION TYPE:C FX KEEL BEAM BOX LOWER EXTERNAL PANEL SUPPORT ATT SHIM FOUND CORROSION AT STA 1460 LBL4 TO LBL5 AND RBL4 TO RBL5 UPPER SURFACE TO STIFFENER AREA AS MARKED. CORROSION BLEND OUT 0.065" BY 3/4" BY 1 1/4" EXCEED SRM LIMIT. FX KEEL BEAM BOX LOWEJul 3, 2007 · N522UP · Boeing 747212B · Fuselage Main, KeelSDR UPS07450307Keelbeam · corrodedINSPECTION TYPE:C FX KEEL BEAM RT LOWER CHORD UPPER SURFACE FOUND CORROSION AT STA 1445-1448 RBL8. CORROSION BLEND OUT 0.091" BY 2" BY 3" EXCEED SRM LIMIT. FX KEEL BEAM RT LOWER CHORD BS 1445-1448 RBL8 LWR FLANGE UPPER SURFACE CORROSION REMOVED AND REPROTECTJul 3, 2007 · N522UP · Boeing 747212B · Fuselage Main, KeelSDR UPS07450303Channel · crackedINSPECTION TYPE:C LT BS 820 TENSION TIE NR 4 FASTENER HOLE FOUND CRACK AT FWD CHANNEL APPROX 1/16" IN LENGTH RUNNING UP. M/D BS 820 TENSION TIE FWD CHANNEL REPAIRED AS PER RS R53-25-35817 AND UPS EO B747-5310-27264-A. CONTINUE INSPECTION IS REQUIRED AS PER RJul 3, 2007 · N522UP · Boeing 747212B · Fuselage Miscellaneous StructureSDR UPS07450300Frame · crackedINSPECTION TYPE:C LT BS 940 TENSION TIE NR 1 FASTENER HOLE FOUND CRACK AT WEB DOUBLER RUNNING 5 O/C POSITION APPROX 1/16" IN LENGTH. M/D BS 940 LT SIDE FRAME DOUBLER THROUGH FRAME TENSION TIE, STEEL PLATE AND FAIL/SAFE CHORD HOLE OVERSIZED AND FASTENER INSTALJul 3, 2007 · N522UP · Boeing 747212B · Fuselage Main, FrameSDR UPS07450299Frame · crackedINSPECTION TYPE:C LT BS 940 TENSION TIE NR 1 FASTENER HOLE FOUND CRACK AT FRAME RUNNING 7 O/C POSITION APPROX 0.040" IN LENGTH (LOOKING AFT). M/D BS 940 LT SIDE FRAME THROUGH FRAME DOUBLER, TENSION TIE, STEEL PLATE AND FAIL/SAFE CHORD HOLE OVERSIZED AND FASTEJul 3, 2007 · N522UP · Boeing 747212B · Fuselage Main, FrameSDR UPS07450297Channel · crackedINSPECTION TYPE:C RT BS 860 TENSION TIE TO FRAME CONNECTION AREA FOUND HOLE NR 5 CRACK AT FWD CHANNEL APPROX 0.030". M/D BS 860 RT TENSION TIE FWD CHANNEL REPAIRED AS PER RS R53-25-35820 AND UPS EO B747-5310-27253. CONTINUED INSPECTIONS ARE REQUIRED AS PER RJul 3, 2007 · N522UP · Boeing 747212B · Fuselage Miscellaneous StructureSDR UPS07450295Frame · crackedINSPECTION TYPE:C RT BS 820 TENSION TIE TO FRAME CONNECTION AREA FOUND HOLE NR 4 CRACK AT FRAME WEB DOUBLER APPROX 0.040". M/ BS 820 RT TENSION TIE TO FRAME WEB ATTACH DOUBLER REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND EO B747-5310-23715-C AND SRM 51Jul 3, 2007 · N522UP · Boeing 747212B · Fuselage Main, FrameSDR UPS07450294Plate · misinstalledINSPECTION TYPE:C M/D BS 820 RT TENSION TIE FWD ATT STEEL PLATE LOWER ROW MOST O/B FASTENER HOLE FOUND SHORT EDGE MARGIN. M/D BS820 RT TENSION TIE FWD ATTACH STEEL PLATE REPAIRED AS PER RS R53-25-35817 AND UPS EO B747-5310-27264. CONTINUED INSPECTION IS REQUJul 3, 2007 · N522UP · Boeing 747212B · Fuselage Miscellaneous StructureSDR UPS07450283Plate · misinstalledINSPECTION TYPE:C M/D BS 900 RT TENSION TIE FWD ATT STEEL PLATE UPPER ROW NR 5 FASTENER HOLE (COUNT FROM I/B) FOUND SHORT EDGE MARGIN. M/DECK BS 900 RT TENSION TIE FWD ATTACH STEEL PLATE REPAIRED AS PER HX RS NR R53-25-35819 CONTINUE INSPECTION IS REQUIRED ASJul 3, 2007 · N522UP · Boeing 747212B · Fuselage Miscellaneous Structure
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