Boeing 747-200

Service difficulty reports · 651

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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 = '747200'
  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 UPS06446363Frame · crackedCOCKPIT BS 380 STR10L, 10AL AND 11L FRAME O/B AREA FOUND CRACK. COCKPIT BS 380 STR 0 TO STR 13AL FRAME REPLACED AND INSTALLED AS PER RS R53-12-35444 CONTINUED SB747-53A2265 INSPECTIONS REQUIRE AND WHEN SB 747-53-2272 MOD IS DONE AT THIS FRAME LOCATION, THE REFeb 7, 2006 · N522UP · Boeing 747200 · Fuselage Main, StructureSDR UPS06446362Frame · crackedINSPECTION TYPE:C U/D BS400 STR10L FRAME O/B AREA FOUND CRACK. CRACK LENGTH 1/2" U/D BS400 STR9L TO STR10AL FRAME REPAIRED AS PER RS R53-10-35442 CONTINUED INSPECTIONS REQUIRE WHILE PERFORMING SB 747-53A2265 INSPECTIONS & REPLACEMENT WITH SB747-53-2272 AT Feb 7, 2006 · N522UP · Boeing 747200 · Fuselage Main, FrameSDR UPS06446360Frame · crackedBS 420 STR 10L FRAME O/B AREA FOUND CRACK, CRACK LENGTH 1/2". BS420 STR9/10 TO STR 11 FRAME REPAIRED AS PER RS R53-10-35441 CONTINUED INSPECTION REQUIRE WHILE PERFORMING SB 747-53A2265 INSPECTIONS AND REPLACEMENT WITH SB747-53-2272 MOD AT OR BEFORE 20000 FLIGFeb 7, 2006 · N522UP · Boeing 747200 · Fuselage Main, FrameSDR UPS06446349Structure · crackedFWD CARGO COMPT BS 1000 B/H CHORD COMMON TO UPPER BATH TUB FTG AFT FASTENER HOLE FOUND CRACK AT CHORD RUNNING FWD APPROX 1/16" LONG. FWD CARGO COMPT BS 1000 BULKHEAD CHORD REPAIR AS PER EO# B747-5310-18579-F AT BETWEEN STR 36 / 37L TO STR 40 / 41L AREA.Feb 7, 2006 · N522UP · Boeing 747200 · Fuselage Miscellaneous StructureSDR UPS06446346Stiffener · crackedNOSE W/W TOP PANEL BS 265-280 LBL 20 STIFFENER RADIUS FOUND CRACK APPROX 3/4" LONG. NOSE W/W TOP PANEL BS 265-280 LBL 20" STIFFENER REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 & 51-30-02.Feb 7, 2006 · N522UP · Boeing 747200 · Fuselage Miscellaneous StructureSDR UPS06446342Structure · crackedFWD CARGO COMPT BS 1000 B/H CHORD FOUND CRACK ALONG RADIUS JUST EXTEND BEYOND LOWER BATH TUB FTG APPROX 1/4" (CRACK LENGTH 1/4") FWD CARGO COMPT BS 1000 BULKHEAD CHORD REPAIRED AS PER EO# B747-5310-18579-F AT BETWEEN STR 36/37R TO STR 40/41R AREA.Feb 7, 2006 · N522UP · Boeing 747200 · Fuselage Main, StructureSDR UPS06446320Tank · crackedINSPECTION TYPE:C LT WING SURGE TANK WS 1516 LWR AREA STR 5 & 6 FOUND CRACKED, CRACK LENGTH .4375 INCH AND PIECE BROKEN. LT WING SURGE TANK WS 1516 FULL LENGTH LOWER CHORD REPAIRED AS PER HX RS R57-22-35446 AND UPS ENGINEER FILE 747-57-20088.Feb 7, 2006 · N522UP · Boeing 747200 · Wing Main, Frame StructureSDR UPS06446267Stiffener · crackedINSPECTION TYPE:C NWW - RIGHT SIDEWALL PANEL BS 265-280 WL 180 STIFFENER RADIUS FOUND CRACK APPROX .25 INCH LONG. STIFFENER REPLACED & INSTALLED AS PER SRM 51-10-01 PG 9 & 51-30-02 AT BS 265-280 WL 180 AREA OF NWW RIGHT SIDEWALL PANEL.Feb 7, 2006 · N522UP · Boeing 747200 · Fuselage Miscellaneous StructureSDR UPS06446266Stiffener · crackedINSPECTION TYPE:C NWW - RIGHT SIDEWALL PANEL BS 280-300 WL 160 STIFFENER RADIUS FOUND 2EA CRACKS APPROX .375 INCH LONG. STIFFENER REPLACED & INSTALLED AS PER SRM 51-10-01 PG 9 & 51-30-02 AT NWW RIGHT SIDEWALL PANEL BS 280-300 WL 160 AREA.Feb 7, 2006 · N522UP · Boeing 747200 · Fuselage Miscellaneous StructureSDR UPS06446265Stiffener · crackedINSPECTION TYPE:C NWW - RIGHT SIDEWALL PANEL BS 320-340 WL 130 STIFFENER 1EA FASTENER ADJ AREA FOUND CRACK, CRACK LENGTH .25 INCH. STIFFENER REPLACED & INSTALLED AS PER SRM 51-10-01 PG 9 & 51-30-02 AT NWW RIGHT SIDEWALL PANEL BS 320-340 WL 130 AREA.Feb 7, 2006 · N522UP · Boeing 747200 · Fuselage Miscellaneous StructureSDR UPS06446264Stiffener · crackedINSPECTION TYPE:C NWW - RT SIDEWALL PANEL BS 280-300 WL 150 STIFFENER RADIUS FOUND CRACK APPROX .25 INCH LONG. STIFFENER REPLACED & INSTALLED AS PER SRM 51-10-01 PG 9 & 51-30-02 AT NWW RIGHT SIDEWALL PANEL BS 280-300 WL 150 AREA.Feb 7, 2006 · N522UP · Boeing 747200 · Fuselage Miscellaneous StructureSDR UPS06446262Stiffener · crackedINSPECTION TYPE:C NWW - RIGHT SIDEWALL PANEL BS 300-320 WL 160 STIFFENER RADIUS FOUND 2EA CRACKS APPROX .25 INCH LONG. STIFFENER REPLACED & INSTALLED AS PER SRM 51-10-01 PG 9 & 51-30-02 AT NWW RIGHT SIDEWALL PANEL BS 300-320 WL 160 AREA.Feb 7, 2006 · N522UP · Boeing 747200 · Fuselage Miscellaneous StructureSDR UPS06446261Stiffener · crackedINSPECTION TYPE:C NWW - RIGHT SIDEWALL PANEL BS 300-320 WL 170 STIFFENER RADIUS INTERMITTENT CRACK APPROX TOTAL : 6 INCHES LONG. STIFFENER REPLACED & INSTALLED AS PER SRM 51-10-01 PG 9 & 51-30-02 AT NWW RIGHT SIDEWALL PANEL BS 300-320 WL 170 AREA.Feb 7, 2006 · N522UP · Boeing 747200 · Fuselage Miscellaneous StructureSDR UPS06446260Stiffener · crackedINSPECTION TYPE:C NWW - RIGHT SIDEWALL PANEL BS 280-300 WL 180 STIFFENER RADIUS FOUND CRACK APPROX .375 INCH LONG. STIFFENER REPLACED & INSTALLED AS PER SRM 51-10-01 PG 9 & 51-30-02 AT NWW RIGHT SIDEWALL PANEL BS 280-300 WL 180 AREA.Feb 7, 2006 · N522UP · Boeing 747200 · Fuselage Miscellaneous StructureSDR UPS06446259Stiffener · crackedINSPECTION TYPE:C NWW TOP PANEL BS 260-280 LBL 10 STIFFENER RADIUS FOUND CRACK APPROX .25 INCH LONG. STIFFENER REPLACED & INSTALLED AS PER SRM 51-10-01 PG 9 & 51-30-02 AT BS 265-280 LBL 10" AREA OF NWW TOP PANEL.Feb 7, 2006 · N522UP · Boeing 747200 · Fuselage Miscellaneous StructureSDR UPS06446258Stiffener · crackedINSPECTION TYPE:C NWW - RIGHT SIDEWALL PANEL BS 280-300 WL 170 STIFFENER RADIUS FOUND CRACKS APPROX 2 INCHES LONG. STIFFENER REPLACED & INSTALLED AS PER SRM 51-10-01 PG 9 & 51-30-02 AT NWW RIGHT SIDEWALL PANEL BS 280-300 WL 170 AREA.Feb 7, 2006 · N522UP · Boeing 747200 · Fuselage Miscellaneous StructureSDR UPS06446257Stiffener · crackedINSPECTION TYPE:C NWW - RIGHT SIDEWALL PANEL BS 300-320 WL 180 STIFFENER RADIUS FOUND CRACK APPROX .25 INCH LONG. STIFFENER REPLACED & INSTALLED AS PER SRM 51-10-01 PG 9 & 51-30-02 AT NWW RT SIDEWALL PANEL BS 300-320 WL 180 AREA.Feb 7, 2006 · N522UP · Boeing 747200 · Fuselage Miscellaneous StructureSDR UPS06446256Stiffener · crackedINSPECTION TYPE:C NWW - RIGHT SIDEWALL PANEL BS 300-320 WL 150 STIFFENER RADIUS FOUND INTERMITTENT CRACK APPROX 7 INCHES. STIFFENER REPLACED & INSTALLED AS PER SRM 51-10-01 PG 9 & 51-30-02 AT NWW RIGHT SIDEWALL PANEL BS 300-320 WL 150 AREA.Feb 7, 2006 · N522UP · Boeing 747200 · Fuselage Miscellaneous StructureSDR UPS06446255Stiffener · crackedINSPECTION TYPE:C NWW - LEFT SIDEWALL PANEL BS 320-4 WL 150 STIFFENER RADIUS FOUND CRACK APPROX .125 INCH IN LENGTH. STIFFENER REPLACED & INSTALLED AS PER SRM 51-10-01 PG 9 & 51-30-02 AT NWW LEFT SIDEWALL PANEL BS 320-340 WL 150 AREA.Feb 7, 2006 · N522UP · Boeing 747200 · Fuselage Miscellaneous StructureSDR UPS06446254Stiffener · crackedINSPECTION TYPE:C NWW - LT SIDEWALL PANEL BS 300-320 WL 180 STIFFENER RADIUS FOUND CRACK APPROX .5 INCH IN LENGTH. STIFFENER REPLACED & INSTALLED AS PER SRM 51-10-01 PG 9 & 51-30-02 AT NWW LT SIDEWALL PANEL BS 300-320 WL 180 AREA.Feb 7, 2006 · N522UP · Boeing 747200 · Fuselage Miscellaneous StructureSDR UPS06446253Stiffener · crackedINSPECTION TYPE:C NWW - LT SIDEWALL PANEL BS 320-340 WL 130 STIFFENER RADIUS FOUND CRACK APPROX .375 INCH IN LENGTH. STIFFENER REPLACED & INSTALLED AS PER SRM 51-10-01 PG 9 & 51-30-02 AT NWW LEFT SIDEWALL PANEL BS 320-340 WL 130 AREA.Feb 7, 2006 · N522UP · Boeing 747200 · Fuselage Miscellaneous StructureSDR UPS06446252Stiffener · crackedINSPECTION TYPE:C NWW - LEFT SIDEWALL PANEL BS 265-280 WL 180 STIFFENER RADIUS FOUND CRACK APPROX .3125 INCH IN LENGTH. STIFFENER REPLACED & INSTALLED AS PER SRM 51-10-01 PG 9 & 51-30-02 AT NWW LEFT SIDEWALL PANEL BS 265-280 WL 180 AREA.Feb 7, 2006 · N522UP · Boeing 747200 · Fuselage Miscellaneous StructureSDR UPS06446247Clip · crackedINSPECTION TYPE:C U/D BS 440 STR 10R FRAME FWD & AFT ATT -L- CLIPS FOUND CRACK (TOTAL 2EA), CRACK LENGTH .375 INCH. TIE CLIPS TOTAL 2EA REPLACED AS PER SRM 51-10-01 PG 9 & INSTALLED AS PER SRM 51-30-02.Feb 7, 2006 · N522UP · Boeing 747200 · Fuselage Miscellaneous StructureSDR UPS06446227Splice · crackedINSPECTION TYPE:C FX- BS 420 STR 27AR FX STRINGER SPLICE FOUND CRACKED, CRACK LENGTH 3/4". FX- BS 420 STR 27AR FX STRINGER SPLICE REPLACED AS PER SRM 51-10-01 PG 9.Feb 7, 2006 · N522UP · Boeing 747200 · Fuselage Miscellaneous StructureSDR UPS06446218Panel · debondedINSPECTION TYPE:C RIGHT WING - I/B AFT FLAP I/B LWR FIXED PANEL FOUND DEBOND AT PANEL I/B PORTION (AFTER PANEL REMOVAL). DEBONDED AREA ACCOMPLISHED METAL HOT BOND REPAIR AS PER SRM 51-40-24 FIG 2.Feb 7, 2006 · N522UP · Boeing 747200 · Trailing Edge FlapsSDR UPS06446385Gate · corrodedINSPECTION TYPE:C M/D - RIGHT NR 5 DOOR LWR GATE FACE AND PUSH ROD ATT BRACKET FOUND CORROSION. CORROSION BLEND OUT 0.095 X 2 X 2 INCH. LWR GATE REPLACED & DOOR RIGGING CHECK PERFORMED AS PER MM 52-11-09.Feb 6, 2006 · N522UP · Boeing 747200 · Service DoorsSDR UPS06446374Stringer · crackedBS 420 STR 34R STRINGER FOUND CRACKED, CRACK LENGTH 3/4". BS 400-426 STR -34R, REPAIRED AS PER SRM 53-10-03 FIG 3.Feb 6, 2006 · N522UP · Boeing 747200 · Fuselage Main, Longeron/StringerSDR UPS06446373Support Tube · corrodedRHW I/B FORE FLAP I/B LEVER SUPPORT TUBE FOUND CORRODED AT FWD FACE INSIDE THE FORE FLAP, EXFOLIATION CORROSION. SUPPORT TUBE REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.Feb 6, 2006 · N522UP · Boeing 747200 · Trailing Edge FlapsSDR UPS06446371Frame · crackedNR 3 PYLON REAR MOUNT BULKHEAD FOUND CRACK AT FWD AND AFT FRAME MOST O/B CRACK LENGTH 3/8" AND 1/4". NR 3 PYLON REAR MOUNT BULKHEAD BOTH SIDES FWD AND AFT FRAMES REPLACED AND REPAIRED AS PER RS R54-53-35431 DETAIL VISUAL AND HFEC INSPECTION OF THE BULKHEAD LWFeb 6, 2006 · N522UP · Boeing 747200 · Nacelle/Pylon, Frame/Spar/RibSDR UPS06446366Frame · crackedBS 440 STR9-10R FRAME O/B FLANGE FOUND CRACK. CRACK LENGTH 1.5". BS440 STR9-10R FRAME O/B FLANGE. REPAIRED AS PER RS R53-12-35438 AND UPS RO B747-5310-23800-A.Feb 6, 2006 · N522UP · Boeing 747200 · Fuselage Main, FrameSDR UPS06446365Frame · crackedCOCKPIT BS 287 S10-10A RHS FRAME O/B AREA FOUND CRACK. CRACK LENGTH 0.25" AND 1". COCKPIT BS 287 S10-10A FRAME REPAIRED AS PER RS R53-12-35435 AND UPS EO B747-5310-23811-A.Feb 6, 2006 · N522UP · Boeing 747200 · Fuselage Main, FrameSDR UPS06446361Frame · crackedCOCKPIT BS 360 STR8-9R FRAME O/B FLANGE FOUND CRACK, CRACK LENGTH 0.19" TO 1 1/4". COCKPIT BS 360 STR8-9R FRAME O/B FLANGE REPAIRED AS PER RS R53-12-35433 CONTINUED INSPECTIONS REQUIRE WHILE PERFORMED SB 747-53A2265 INSPECTIONS AND REPLACEMENT WITH SB747-2272Feb 6, 2006 · N522UP · Boeing 747200 · Fuselage Main, FrameSDR UPS06446325Structure · corrodedINSPECTION TYPE:C M/D RIGHT NR 5 DOOR LWR HINGE AREA UPPER BEARING ATT AREA FOUND CORROSION. EXFOLIATION CORROSION 2 X 3 INCH. M/D RIGHT NR 5 DOOR LWR HINGE UPPER WEB REPLACED AS PER SRM 51-10-01 PG 9 & INSTALLED AS PER SRM 51-30-02.Feb 6, 2006 · N522UP · Boeing 747200 · Fuselage Main, StructureSDR UPS06446316Support · crackedINSPECTION TYPE:C M/D RIGHT NR 5 DOOR LWR HINGE LWR SUPPORT WEB FOUND CORROSION CRACK, CRACK LENGTH .75 INCH. M/D RIGHT NR 5 DOOR LWR HINGE LWR SUPPORT WEB REPLACED AS PER SRM 51-10-01 PG 9.Feb 6, 2006 · N522UP · Boeing 747200 · Fuselage Main, StructureSDR UPS06446290Stringer Clip · crackedBS 440 STR 36R STRINGER FOUND CRACKED AT STR TIE CLIP, CRACK LENGTH 5/8". BS 434 TO BS 453 STR 36R REPAIRED AS PER SRM 53-10-03 FIG 3.Feb 6, 2006 · N522UP · Boeing 747200 · Fuselage Main, Attach FittingsSDR UPS06446289Web · crackedRT NR 5 DOOR LWR WEB FOUND CRACK. CRACK LENGTH 2". LWR WEB REPLACED AS PER SRM 51-10-01 P9.Feb 6, 2006 · N522UP · Boeing 747200 · Cargo/Baggage DoorsSDR UPS06446225Rib · crackedINSPECTION TYPE:C NR 2 PYLON, RT INTERIOR RIB CRACKED AT NAC STA 210 BELOW MID SPAR, CRACK LENGTH 2.5". NR 2 PYLON RT INTERIOR RIB AT NAC STA 210 BELOW MID SPAR AREA REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.Feb 5, 2006 · N522UP · Boeing 747200 · Nacelle/Pylon, Frame/Spar/RibSDR UPS06446224Bulkhead · crackedINSPECTION TYPE:C EMP - BS 2658 FIREWALL BULKHEAD FORWARD SIDE WL 350 RBL 10 FOUND CRACKED, CRACK LENGTH .875 INCH. BS 2658 BULKHEAD WL 350 RBL 10" FWD SIDE AREA REPAIRED AS PER SRM 53-10-04 FIG 30.Feb 5, 2006 · N522UP · Boeing 747200 · Fuselage Main, BulkheadSDR UPS06446381Skin · corrodedINSPECTION TYPE:C RT WING T/E CAVITY REAR SPAR LOWER SKIN FOUND CORRODED BETWEEN WS 510 & WS 515 (ACCESS FROM T/E PNL 671AB). CORROSION BLEND OUT 0.074 X 2 X 5 INCH EXCEED SRM LIMIT. RT WING T/E CAVITY REAR SPAR LOWER SKIN UPPER SURFACE AT WS 516.5 REPAIRED Feb 4, 2006 · N522UP · Boeing 747200 · Wing, Plate/SkinSDR UPS06446287Web · corrodedBS 2240-2260 WL206 R NR 5 DOOR INTERIOR LWR WEB FOUND CORROSION. CORROSION BLEND OUT 0.060" BY 2" BY 2". LWR WEB REPLACED AS PER SRM 51-10-01 P9 (REFER NRC 6509 FOR WORKING D DETAIL).Feb 4, 2006 · N522UP · Boeing 747200 · Passenger/Crew DoorsSDR UPS06446250Reveal · crackedINSPECTION TYPE:C M/D LEFT NR 2 DOOR FWD CUTOUT LWR REVEAL FOUND CRACKED, CRACK LENGTH .5 INCH. LEFT NR 2 DOOR FWD CUTOUT LOWER REVEAL REPLACED AS PER SRM 51-10-01 PG 9 & INSTALLED AS PER SRM 51-30-02.Feb 4, 2006 · N522UP · Boeing 747200 · Fuselage Main, StructureSDR UPS06446220Skin · dentedINSPECTION TYPE:C EMP - BS 2680 TO BS 2690 SKIN ABOVE LT APU COOLING EXHAUST FOUND 1EA DENT MARK AS MARKED. DAMAGED SKIN TRIMMED OFF AT BS 2680 - BS 2690 ABOVE LT APU COOLING EXHAUST AS PER SRM 53-30-03 FIG 1A & REPAIRED AS PER SRM 53-30-03 FIG 1A AFTER NDT IFeb 4, 2006 · N522UP · Boeing 747200 · Fuselage Main, Plate/SkinSDR UPS06446214Panel · chafedINSPECTION TYPE:C LHW, O/B AFT FLAP UPPER CENTER FLAP PANEL NR 588JT FOUND CHAFE MARKS. CHAFED AREA ACCOMPLISHED METAL HOT BOND REPAIR AS PER SRM 51-40-24 FIG 2.Feb 4, 2006 · N522UP · Boeing 747200 · Trailing Edge FlapsSDR UPS06446367Frame · crackedBS240 FRAME CRACKED AT S11L CUTOUT. CRACK LENGTH 0.75". M/D BS240 S11L FRAME REPAIRED AS PER RS R53-12-35440 AND UPS EO B747-5310-23825-A AFTER CRACK FREE CONFIRMED BY NDT INSPECTION PER NTM PT6 51-00-00 FIG4.Feb 3, 2006 · N522UP · Boeing 747200 · Fuselage Main, FrameSDR UPS06446345Frame · crackedFOUND LT STA 500 FRAME CRACKED AT BETWEEN STR 13L & 14L U/D FLOORBEAM LOWER CHORD ATTACHMENT AREA, CRACK LENGTH 7/8". BS 500 BETWEEN STR 13L TO STR 16/17L AREA FRAME REPAIRED AS PER SRM 51-40-03 FIG 2.Feb 3, 2006 · N522UP · Boeing 747200 · Fuselage Main, FrameSDR UPS06446323Splice · crackedINSPECTION TYPE:C M/D LEFT STA 500 FRAME ATT SPLICE CRACKED BETWEEN STR 13L & STR 14L, CRACK LENGTH .375 INCH. M/D BS 500 BTN S11L - 16L FRAME ATT SPLICE ANGLE REPLACED & INSTALLED AS PER SRM 51-10-01 PG 9 & 51-30-02.Feb 3, 2006 · N522UP · Boeing 747200 · Fuselage Miscellaneous StructureSDR UPS06446228Angle · crackedINSPECTION TYPE:C M/D, LT STA 400 FRAME SPLICE ANGLE FOUND CRACKED AT STR 24L (CRACK LENGTH 7"). M/D LT BS 400 FRAME SPLICE ANGLE REPLACED AT STA 24L AREA AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.Feb 3, 2006 · N522UP · Boeing 747200 · Fuselage Miscellaneous StructureSDR UPS06446221Splice · crackedINSPECTION TYPE:C M/D BS 400 STR 23-25R FRAME I/B CHORD ATT SPLICE FOUND CRACK,CRACK LENGTH .375 INCH. BS 400 STR 23-25R FRAME I/B CHORD ATT SPLICE ANGLE REPLACED AS PER SRM 51-10-01 PG 9.Feb 3, 2006 · N522UP · Boeing 747200 · Fuselage Main, FrameSDR UPS06446215Panel · delaminatedINSPECTION TYPE:C RIGHT WING: O/B AFT FLAP PANEL 688IT UPPER SURFACE FOUND DELAMINATED. DELAMINATED AREA ACCOMPLISHED METAL HOT BOND REPAIR AS PER SRM 51-40-24 FIG 1.Feb 3, 2006 · N522UP · Boeing 747200 · Trailing Edge FlapsSDR UPS06446379Skin · crackedINSPECTION TYPE:C FX - SKIN AT BS 980 STR 38L 1EA FASTENER HOLE COMMON TO FWD LWR DRAG SPLICE FTG FOUND CRACK AT SKIN RUNNING DOWN, CRACK LENGTH .125 INCH. SKIN REPAIRED AS PER SRM 53-30-03 FIG 60 AND MPI P18440 ISSUED TO CONTROL THE REPEAT INSEPCTION INTERVAFeb 2, 2006 · N522UP · Boeing 747200 · Fuselage Main, Plate/Skin
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