N683UP, cancelled Jan 26, 2012

Service difficulty reports · 468

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N683UP' AND deregistration_id = 'N683UP-2012-01-26'
  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 UPS08452094Skin · corrodedLOWER BELLY SKIN CORROSION. REPAIR DOUBLER INSTALLED AT STA 1780 SRT 50R PER SRM 53-30-03 FIG 1. CATEGORY B REPAIR REQUIRES REPEAT INSPECTION AT 15000 RIGHT CYCLES AND THEN EVERY 3000 FLIGHT CYCLES.Apr 29, 2008 · N683UP · Boeing 747121 · Fuselage Main, Plate/SkinSDR UPS08451553Light · inoperativeEMERGENCY LIGHT ABOVE SLIDE IN COCKPIT INOP. DEFERRED PER MEL 33-15 ON ITEM M367673. SLAVED IN NEW BATTERY PACK POWER SUPPLY, NO HELP. REMOVED AND REPLACED EMERG EXIT SIGN IAW AMM 33-1-51-04. EXIT LIGHT ASSY REPLACED PER MM 33-50-00. OPERATION NOW CHECKS Jan 24, 2008 · N683UP · Boeing 747121 · Emergency LightingSDR UPS07451218Electronic Unit · smokeFUEL FLOW ELECTRONICS UNIT SMOKING. REMOVED AND REPLACED FUEL FLOW ELECTRONICS UNIT PER MM 73-31-02. OPS CHECK NORMAL.Nov 26, 2007 · N683UP · Boeing 747121 · Fuel Flow IndicatingSDR UPS07451203Battery Pack · dischargedAF L1 DOOR ENTRY EMERGENCY LIGHT WOULD NOT TEST. REMOVED AND REPLACED EMERGENCY LIGHT/BATTERY PACK ASSY WITH REF TO MM 33-51-07. OPS CHECK GOOD PER SAME.Nov 26, 2007 · N683UP · Boeing 747121 · Emergency LightingSDR UPS07450948Web · crackedINSPECTION TYPE:C NWW RT SIDE PANEL STA 294 WL 170 SIDE PANEL WEB 1EA SUSPECT CRACK INDICATION FOUND ADJACENT LWR SIDE OF EXTERNAL STRAP APPROX. 0.5" LENGTH CRACK LENGTH 0.5" APPROX. NOSE WHEEL WELL SIDE PANEL REPAIRED AT BS 293 - BS 295 WL 170 AREA AS PER SROct 16, 2007 · N683UP · Boeing 747121 · Fuselage Miscellaneous StructureSDR UPS07449805Lamp · inoperativeEMERGENCY LIGHT CONTROL SWITCH INDICATOR 1/2 INOP. RELAMPED EMERGENCY, OPS CHECK GOOD.May 13, 2007 · N683UP · Boeing 747121 · Emergency LightingSDR UPS07449578Module · unknownHYD SYSTEM 3 FAILURE PRESSURE & QUANTITY ZERO DURING FLAP RETRACTION. HYD SYSTEM PR & QT LIGHTS ON. REMOVED AND REPLACED MODULAR ASSY & LEAK CHECK IAW 29-11-23.Mar 29, 2007 · N683UP · Boeing 747121 · Hydraulic System, MainSDR UPS07449433Bear Strap · crackedINSPECTION TYPE:C RIGHT NR 3 PAX DOOR CUTOUT FWD LOWER CORNER CRACK REVEALED AT THE EDGE OF BEAR STRAP. CRACK LENGTH 2.5 INCHES APPROX. RIGHT NR 3 PAX DOOR CUTOUT FWD LOWER CORNER SKIN AND BEAR STRAP REPAIRED AS PER RS R53-41-35782 AND UPS EO B747-5330-15047Mar 5, 2007 · N683UP · Boeing 747121 · Fuselage Main, Plate/SkinSDR UPS07449488Floor Support · crackedINSPECTION TYPE:C M/D BS 1220 LBL 98.8 FLOOR WEB SUPPORT FOUND CRACK AS MARKED. CRACK LENGTH .375 INCH. M/D BS 1220 LBL 98.8 FLOOR WEB SUPPORT REPAIRED AS PER RS R53-15-35777 AND UPS ENGINEERING FILE 747-53-20406.Mar 1, 2007 · N683UP · Boeing 747121 · Fuselage Miscellaneous StructureSDR UPS07449497Skin · crackedINSPECTION TYPE:C RIGHT NR 3 PAX DOOR CUTOUT FWD LOWER CORNER 1EA FASTENER HOLE (IDENT H) FOUND THROUGH THICKNESS CRACKED AT 7 O/C POSITION AND .0625 INCH CRACKED TO FWD AT BOTTOM OF HOLES BORE AT 5 O/C POSITION (LOOKING I/B). RIGHT NR 3 PAX DOOR CUTOUT FWD LFeb 28, 2007 · N683UP · Boeing 747121 · Fuselage Main, Plate/SkinSDR UPS07449496Skin · crackedINSPECTION TYPE:C RIGHT NR 3 PAX DOOR CUTOUT FWD LOWER CORNER 1EA FASTENER HOLE (IDENT G) FOUND CRACKED AT BEAR STRAP .125 INCH TO UPWARD AT 11 O/C POSITION (LOOKING I/B). RIGHT NR 3 PAX DOOR CUTOUT FWD LOWER CORNER SKIN AND BEAR STRAP REPAIRED AS PER RS R53-Feb 28, 2007 · N683UP · Boeing 747121 · Fuselage Main, Plate/SkinSDR UPS07449495Skin · crackedINSPECTION TYPE:C RIGHT NR 3 PAX DOOR CUTOUT FWD LOWER CORNER 1EA FASTENER HOLE (IDENT D) FOUND CRACKED AT SKIN .125 INCH APPROX RUNNING FWD AT 5 O/C POSITION (LOOKING I/B). RIGHT NR 3 PAX DOOR CUTOUT FWD LOWER CORNER SKIN AND BEAR STRAP REPAIRED AS PER RS R5Feb 28, 2007 · N683UP · Boeing 747121 · Fuselage Main, Plate/SkinSDR UPS07449494Skin · crackedINSPECTION TYPE:C RIGHT NR 3 PAX DOOR CUTOUT FWD LOWER CORNER 1E FASTENER HOLE (IDENT F) FOUND CRACKED AT BEAR STRAP .125 INCH APPROX RUNNING UPWARD AT 12 O/C POSITION (LOOKING I/B). CRACK LENGTH .125 INCH. RIGHT NR 3 PAX DOOR CUTOUT FWD LOWER CORNER SKIN ANFeb 28, 2007 · N683UP · Boeing 747121 · Fuselage Main, Plate/SkinSDR UPS07449493Skin · crackedINSPECTION TYPE:C RIGHT NR 3 PAX DOOR CUTOUT FWD LOWER CORNER 1EA FASTENER HOLE (IDENT E) FOUND CRACKED AT SKIN AND BEAR STRAP .125 INCH TO UPWARD AT 12 O/C POSITION (LOOKING I/B). RIGHT NR 3 PAX DOOR CUTOUT FWD LOWER CORNER SKIN AND BEAR STRAP REPAIRED AS PEFeb 28, 2007 · N683UP · Boeing 747121 · Fuselage Main, Plate/SkinSDR UPS07449492Skin · crackedINSPECTION TYPE:C RIGHT NR 3 PAX DOOR CUTOUT FWD COVER CORNER 1EA FASTENER HOLE (IDENT B) FOUND CRACKED AT BEAR STRAP .0625 INCH TO FWD AT 5 O/C POSITION (LOOKING I/B). CRACK LENGTH .0625 INCH. RIGHT NR 3 PAX DOOR CUTOUT FWD LOWER CORNER SKIN AND BEAR STRAP Feb 28, 2007 · N683UP · Boeing 747121 · Fuselage Main, Plate/SkinSDR UPS07449491Skin · crackedINSPECTION TYPE:C 1EA FASTENER HOLE (IDENT A) FOUND CRACKED AT RIGHT NR 3 PAX DOOR CUTOUT AREA FWD LOWER CORNER AT SKIN I/B FACE CRACK LENGTH 0.040 INCH APPROX WHICH RUNNING FWD AT 5 O/C POSITION (LOOKING I/B). RIGHT NR 3 PAX DOOR CUTOUT FWD LOWER CORNER SKINFeb 28, 2007 · N683UP · Boeing 747121 · Fuselage Main, Plate/SkinSDR UPS07449490Skin · crackedINSPECTION TYPE:C RIGHT NR 3 PAX DOOR CUTOUT FWD LOWER CORNER 1EA FASTENER HOLE (IDENT C) FOUND CRACKED AT BEAR STRAP .0625 INCH AT 11 O/C POSITION AND ANOTHER CRACK AT SKIN AND BEAR STRAP .0625 INCH AT 5 O/C POSITION (LOCKING I/B). RIGHT NR 3 PAX DOOR CUTOUTFeb 28, 2007 · N683UP · Boeing 747121 · Fuselage Main, Plate/SkinSDR UPS07449457Skin · crackedINSPECTION TYPE:C RIGHT NR 3 PAX DOOR CUTOUT FWD LOWER CORNER 1EA FASTENER HOLE (IDENT I) FOUND CRACK THRU THICKNESS AT 5:00 O/C POSITION (LOOKING I/B) CRACK LENGTH 2.5 INCH. RIGHT NR 3 PAX DOOR CUTOUT FWD LOWER CORNER SKIN AND BEAR STRAP REPAIRED AS PER RS RFeb 28, 2007 · N683UP · Boeing 747121 · Fuselage Main, Plate/SkinSDR UPS07449467Frame · crackedINSPECTION TYPE:C M/D BS 820 STR 11-12R FRAME FOUND CRACK. CRACK LENGTH .875 - 1 INCH. M/D BS 820 STR 11-12R FRAME REPAIRED AS PER RS R53-12-35770. CONTINUE INSPECTION IS REQUIRED AS PER RS R53-12-35770 AND UPS EO B747-5310-26322.Feb 27, 2007 · N683UP · Boeing 747121 · Fuselage Main, FrameSDR UPS07449425Stringer · crackedINSPECTION TYPE:C M/D BS 820-840 STR 10 LT STRINGER ATT WEB FOUND CRACKED. CRACK LENGTH .75 INCH. M/D BS 820-840 STR 10 LT ATTACH WEB REPAIRED AS PER SRM 51-40-03 FIG 1.Feb 27, 2007 · N683UP · Boeing 747121 · Fuselage Main, Longeron/StringerSDR UPS07449423Stringer · crackedINSPECTION TYPE:C M/D BS 820-840 S10 RIGHT STRINGER ATT WEB FOUND CRACK. CRACK LENGTH .625 INCH. M/D BS 820-840 STR 10R ATTACH WEB REPAIRED AS PER SRM 51-40-03 FIG 1.Feb 27, 2007 · N683UP · Boeing 747121 · Fuselage Main, Longeron/StringerSDR UPS07449313Web · crackedINSPECTION TYPE:C AFT CARGO COMPT LT VERTICAL WEB FOUND CRACKED AT STA 1500 TO STA 1520 STR 34L AFT EDGE AREA. CRACK LENGTH .75 INCH. VERTICAL WEB REPLACED PER SRM 51-10-01 PG 9.Feb 20, 2007 · N683UP · Boeing 747121 · Fuselage Miscellaneous StructureSDR UPS07449412Pressure Panel · corrodedINSPECTION TYPE:C LEFT BODY LANDING GEAR W/W PRESSURE DECK ATT WEB FOUND SURFACE CORROSION AT STA 1403 LBL 125. CORROSION BLEND OUT 0.034 X 1 X 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS. LEFT BODY LANDING GEAR W/W PRESSURE DECK ATT WEB REPAIRED AT STA 1403 LBLFeb 17, 2007 · N683UP · Boeing 747121 · Fuselage Main, BulkheadSDR UPS07449454Stringer · crackedINSPECTION TYPE:C BULK CARGO COMPT STRINGER FOUND CRACK AT STA 2185 STR 51R. CRACK LENTH .375 INCH. BULK CARGO COMPT BS 2185 STR 51R REPAIRED AS PER RS R53-11-35768 AND UPS ENGINEERING FILE NUMBER 747-53-20407.Feb 16, 2007 · N683UP · Boeing 747121 · Fuselage Main, Longeron/StringerSDR UPS07449443Skin · crackedINSPECTION TYPE:C M/D R3 DOOR SKIN FOUND CRACKED APPROX AT CTR LOWER PORTION. CRACK LENGTH .375 INCH. M/D R3 DOOR SKIN AT CTR LOWER PORTION AREA REPAIRED AS PER SRM 52-10-02 FIG 9.Feb 16, 2007 · N683UP · Boeing 747121 · Passenger/Crew DoorsSDR UPS07449436Door Frame · crackedINSPECTION TYPE:C RIGHT BS 2231 FRAME AT DOOR NR 5 BETWEEN S24R-25R FOUND 2EA HOLE CRACK. CRACK LENGTH .125 INCH, .25 INCH AND .1875 INCH. M/D RIGHT BS 2231 FRAME REVEAL, STRAP AND CHORD REPAIRED AS PER RS R53-62-35764. CONTINUE INSPECTION IS REQUIRED PER RFeb 16, 2007 · N683UP · Boeing 747121 · Fuselage Main, StructureSDR UPS07449419Shear Tie · crackedINSPECTION TYPE:C LEFT WING WS 469.8 FWD OF UPPER STR 29 SHEAR TIES FOUND CRACKED AS MARKED. CRACK LENGTH .5 INCH. LEFT WING WS 469.8 FWD OF UPPER STR 29 SHEAR TIE REPAIRED AS PER SRM 57-10-05 FIG 7.Feb 16, 2007 · N683UP · Boeing 747121 · Wing Main, Frame StructureSDR UPS07449416Door Frame · crackedINSPECTION TYPE:C M/D L5 DOOR UPPER FRAME FOUND CRACKED AT SEVERAL FASTENER HOLE AREA. CRACK LENGTH .375 INCH. M/D L5 DOOR UPPER FRAME REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 & 51-30-02.Feb 16, 2007 · N683UP · Boeing 747121 · Fuselage Main, StructureSDR UPS07449401Support · corrodedINSPECTION TYPE:C BULK CARGO COMPT - STA 2080 LT SIDEWALL SUPPORT ANCHOR NUT AREA FOUND CORRODED AS MARKED. CORROSION BLEND OUT 0.038" X 1" X 1" EXCEED SRM 53-10-01 FIG 1 LIMITS. BULK CARGO COMPT BS 2080 LEFT SIDEWALL SUPPORT REPAIRED AS PER SRM 51-40-04 FIGFeb 16, 2007 · N683UP · Boeing 747121 · Fuselage Miscellaneous StructureSDR UPS07449388Frame · crackedINSPECTION TYPE:C M/D R5 DOOR UPPER FRAME FOUND CRACKED AT SEVERAL FASTENER HOLE AREA. CRACK LENGTH .75 INCH. FRAME REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.Feb 16, 2007 · N683UP · Boeing 747121 · Passenger/Crew DoorsSDR UPS07449378Support · corrodedINSPECTION TYPE:C BULK CARGO COMPT - STA 1960 LEFT SIDEWALL SUPPORT ANCHOR NUT AREA FOUND CORRODED AS MARKED. CORROSION BLEND OUT 0.049" X .5" X 1" EXCEED SRM 53-10-01 FIG 1 LIMITS. BULK CARGO COMPT - STA 1960 LEFT SIDEWALL SUPPORT REPAIRED AS PER SRM 51-40-Feb 16, 2007 · N683UP · Boeing 747121 · Fuselage Miscellaneous StructureSDR UPS07449376Skin · crackedINSPECTION TYPE:C M/D L3 DOOR SKIN FOUND CRACKED APPROX AT CTR LOWER PORTION. CRACK LENGTH .75 INCH. L3 DOOR SKIN REPAIRED AS PER SRM 52-10-02 FIG 9.Feb 16, 2007 · N683UP · Boeing 747121 · Passenger/Crew DoorsSDR UPS07449347Sill · crackedINSPECTION TYPE:C U/D RIGHT DOOR SILL BS 400 RBL TO FLOOR SUPPORT CHORD FOUND CRACKED. CRACK LENGTH: .75 INCH. FLOOR SUPPORT CHORD REPAIRED AS PER SRM 51-40-04 FIG 1.Feb 16, 2007 · N683UP · Boeing 747121 · Fuselage Miscellaneous StructureSDR UPS07449319Support Fitting · crackedINSPECTION TYPE:C FWD CARGO COMPT AFT FIXED END STOP SUPPORT FITTING FOUND CRACK AT STA 980 RBL 45. CRACK LENGTH .75 INCH. FWD CARGO COMPT AFT FIXED END STOP SUPPORT FITTING REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02, JUST AT STA 980Feb 16, 2007 · N683UP · Boeing 747121 · Fuselage Miscellaneous StructureSDR UPS07449310Web · crackedINSPECTION TYPE:C U/D RIGHT CREW DOOR SILL AREA I/B VERTICAL WEB AND ANGLE FOUND CRACKED. CRACK LENGTH .5 INCH. VERTICAL WEB AND ANGLE REPLACED PER SRM 51-10-01 PG 9 & INSTALLED AS PER SRM 51-30-02.Feb 16, 2007 · N683UP · Boeing 747121 · Fuselage Miscellaneous StructureSDR UPS07449303Stringer · crackedINSPECTION TYPE:C M/D BS 380 S14EL FOUND CRACK. CRACK LENGTH .25 INCH. M/D BS 360-380 STRINGER S14EL REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.Feb 16, 2007 · N683UP · Boeing 747121 · Fuselage Main, Longeron/StringerSDR UPS07449297Floor Support · corrodedINSPECTION TYPE:C BULK CARGO COMPT LEFT STA 1940 LBL 55 FLOOR SUPPORT FOUND CORRODED CRACK AS MARKED. CORROSION BLEND OUT 0.025" X .5" X 1" EXCEED SRM 53-10-01 FIG 1 LIMITS. BULK CARGO COMPT FLOOR SUPPORT REPLACED WITH EXISTING SPLICE FROM BS 1920-1970 LBL 5Feb 16, 2007 · N683UP · Boeing 747121 · Fuselage Miscellaneous StructureSDR UPS07449295Floor Support · corrodedINSPECTION TYPE:C BULK CARGO COMPT LEFT STA 1920 TO STA 1940 LBL 55" FLOOR SUPPORT UNDER ANCHOR NUT FOUND CORRODED AS MARKED. CORROSION BLEND OUT 0.025" X .5" X 1" EXCEED SRM 53-10-01 FIG 1 LIMITS. BULK CARGO COMPT LEFT BS 1920 TO 1970 LBL 55" FLOOR SUPPORT Feb 16, 2007 · N683UP · Boeing 747121 · Fuselage Miscellaneous StructureSDR UPS07449294Support · corrodedINSPECTION TYPE:C BULK CARGO COMPT SLOPE PANEL SUPPORT SEVERAL LOCATION FOUND SURFACE CORROSION AT STA 1940 TO STA 2045 LBL 60 ANCHOR NUT AREA. CORROSION BLEND OUT 0.025" X .5" X 2" EXCEED SRM 53-10-01 FIG 1 LIMITS. SLOPE PNL SUPPORT BS 1940-2010 COR REMOVEDFeb 16, 2007 · N683UP · Boeing 747121 · Fuselage Miscellaneous StructureSDR UPS07449291Floorbeam · crackedINSPECTION TYPE:C BULK CARGO COMPT M/D FLOORBEAM LOWER WEB FOUND CRACK AT 1940 RBL 64". CRACK LENGTH .5 INCH. BULK CARGO COMPT M/D FLOORBEAM LOWER WEB REPAIRED AS PER SRM 51-40-02 FIG 1, JUST AT STA 1940 RBL 64 AREA.Feb 16, 2007 · N683UP · Boeing 747121 · Fuselage Main, Floor BeamSDR UPS07449489Skin · corrodedINSPECTION TYPE:C M/D BS 1210-1220 LBL 97 WING CTR SECTION TOP SURFACE FOUND CORROSION. CORROSION BLEND OUT 0.043 X .5 X 2 INCHES EXCEED SRM LIMIT. M/D BS 1210-1220 LBL 97 WING CTR SECTION TOP SKIN REPAIRED AS PER RS R57-14-35765 AND UPS EO B747-5730-15819.Feb 15, 2007 · N683UP · Boeing 747121 · Wing, Center BoxSDR UPS07449437Reveal · crackedINSPECTION TYPE:C RIGHT BS 2231 FRAME AREA 2EA FASTENER HOLE CRACK FOUND AT REVEAL BETWEEN S25R AND S26R. CRACK LENGTH .25 INCH, .125 INCH, AND .1875 INCH. M/D RIGHT BS 2231 FRAME REVEAL, STRAP AND CHORD REPAIRED AS PER RS R53-62-3764. CONTINUE INSPECTION IFeb 15, 2007 · N683UP · Boeing 747121 · Fuselage Miscellaneous StructureSDR UPS07449403Attach Fitting · crackedINSPECTION TYPE:C RIGHT WING L/E RIB TO FRONT SPAR UPPER CHORD ATT FITTING AT ILES 340 FOUND CRACKED. CRACK LENGTH .375 INCH. RIGHT WING L/E RIB TO FRONT SPAR UPPER CHORD ATTACH AT ILES 340 REPLACED & INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.Feb 15, 2007 · N683UP · Boeing 747121 · Wing, Attach FittingsSDR UPS07449369Frame · crackedINSPECTION TYPE:C M/D L4 DOOR LOWER AFT CORNER FRAME FOUND CRACKED. CRACK LENGTH 1.5 INCH. FRAME REPAIRED AS PER SRM 52-10-02 FIG 10 AT M/D L4 DOOR AFT VERTICAL FRAME CORNER AREA.Feb 15, 2007 · N683UP · Boeing 747121 · Cargo/Baggage DoorsSDR UPS07449357Frame · crackedINSPECTION TYPE:C M/D R4 DOOR UPPER FWD FRAME FOUND CRACKED. CRACK LENGTH 1.25 INCH. FWD FRAME REPAIRED AS PER SRM 52-10-02 FIG 10.Feb 15, 2007 · N683UP · Boeing 747121 · Passenger/Crew DoorsSDR UPS07449352Web · misrepairedINSPECTION TYPE:C NR 1 PYLON LWR WEB CRACK PREVIOUS REPAIR DOES NOT APPEAR TO COVER ENTIRE CONDITION. CRACK LENGTH .75 INCH. WEB REPAIRED PER SRM 54-10-03 FIG 2.Feb 15, 2007 · N683UP · Boeing 747121 · Nacelle/Pylon Miscellaneous StructureSDR UPS07449345Attach Fitting · crackedINSPECTION TYPE:C LEFT WING L/E RIB TO FRONT SPAR UPPER CHORD ATT FITTING AT ISLES 270 FOUND CRACKED. CRACK LENGTH: .25 INCH. UPPER CHORD ATT CLIP REPLACED PER SRM 51-10-01 PG 9 & INSTALLED PER SRM 51-30-02.Feb 15, 2007 · N683UP · Boeing 747121 · Wing, Attach FittingsSDR UPS07449316Support · corrodedINSPECTION TYPE:C BULK CARGO COMPT RIGHT SLOPE PANEL SUPPORT SEVERAL LOCATION CORROSION AT STA 2080 TO STA 2160 RBL 60 ANCHOR NUT AREA. CORROSION BLEND OUT 0.026" X 1" X 1" EXCEED SRM LIMIT. BULK CARGO COMPT BS 2040 - 2160 RBL 60 SLOPE PANEL SUPPORT REPLACEDFeb 15, 2007 · N683UP · Boeing 747121 · Fuselage Miscellaneous StructureSDR UPS07449456Skin · crackedINSPECTION TYPE:C M/D R3 DOOR CUTOUT FWD LOWER CORNER SKIN AND STRAP FOUND CRACKED. CRACK LENGTH 2.5 INCHES. RIGHT NR 3 PAX DOOR CUTOUT FWD LOWER CORNER SKIN AND BEAR STRAP REPAIRED AS PER RS R53-41-35782.Feb 14, 2007 · N683UP · Boeing 747121 · Fuselage Main, Plate/SkinSDR UPS07449455Frame · crackedINSPECTION TYPE:C RIGHT BS 800 FRAME FOUND 2EA FASTENER CRACKS AT STRAP LAYER. CRACK LENGTH 0.125 INCH AND 0.025 INCH. FRAME REPAIRED AS PER RS R53-12-35762 AT BS 800 STR 16R TO STA 18R STRAP AREA AND REFER UPS EO B747-5310-26131.Feb 14, 2007 · N683UP · Boeing 747121 · Fuselage Main, Frame
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