Boeing 747 212B

Service difficulty reports · 2,202

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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 = '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 UPS02439070Fitting · crackedINSPECTION TYPE:C BS 1480 RH B/H #3 HOLE FOUND CRACK AT OUTER CHORD SPLICE FTG, RUNNING FWD APPROX 1/16" & AFT APPROX 0.040" LONG. (STR R33 TO R34) RH BS 1480 B/H #3 HOLE AT OUTER CHORD SPLICE FTG REAMED TO 0.625" AND BUSHING INSTALLED AS PER SB 747-53A239Aug 4, 2002 · N526UP · Boeing 747212B · Fuselage Main, StructureSDR UPS02439069Fitting · crackedINSPECTION TYPE:C BS 1480 RH B/H #5 HOLE FOUND CRACK AT OUTER CHORD SPLICE FTG, RUNNING FWD APPROX 1/8" AND AFT APPROX 1/16" LONG. (STR R33 TO R34). RH BS 1480 B/H #5 HOLE AT OUTER CHORD SPLICE FTG REAMED TO 0.660" AND BUSHING INSTALLED AS PER SB747-53A239Aug 4, 2002 · N526UP · Boeing 747212B · Fuselage Main, StructureSDR UPS02439068Fitting · crackedINSPECTION TYPE:C BS 1480 RH B/H #6 HOLE FOUND CRACK AT OUTER CHORD SPLICE FTG RUNNING AFT APPROX 1/16" LONG.(STR R33 TO R34). RH BS 1480 B/H #6 HOLE AT OUTER CHORD SPLICE FTG REAMED TO 0.660" AND BUSHING INSTALLED AS PER SB 747-53A2390 REWORKED HOLE INSPAug 4, 2002 · N526UP · Boeing 747212B · Fuselage Main, StructureSDR UPS02439067Fitting · crackedINSPECTION TYPE:C BS 1480 RH B/H #9 HOLE FOUND CRACK AT OUTER CHORD SPLICE FTG. RUNNING AFT APPROX 1/16" LONG. (STR R33 TO R34) RH BS 1480 B/H #9 HOLE AT OUTER CHORD SPLICE FTG REAMED TO 0.660" AND BUSHING INSTALLED AS PER SB747-53A2390. REWORKED HOLE INSPAug 4, 2002 · N526UP · Boeing 747212B · Fuselage Main, StructureSDR UPS02439066Fitting · crackedINSPECTION TYPE:C BS 1480 RH B/H #7 HOLE FOUND CORROSION AROUND AND INSIDE HOLE BORE OF OUTER CHORD SPLICE FTG. (STR R33 TO R34). RH BS 1480 B/H #7 HOLE AT OUTER CHORD SPLICE FTG REAMED TO 0.660 AND BUSHING INSTALLED AS PER B747-53A2390 REWORKED HOLE INSPAug 4, 2002 · N526UP · Boeing 747212B · Fuselage Main, StructureSDR UPS02439065Fitting · crackedINSPECTION TYPE:C BS 1480 RH B/H #14 HOLE FOUND CRACK AT OUTER CHORD SPLICE FTG, RUNNING O/B APPROX 1/16" LONG. (STR R33 TO R34) RH BS 1480 B/H #14 HOLE AT OUTER CHORD SPLICE FTG REAMED TO 0.500" AND BUSHING INSTALLED AS PER SB 747-53A2390 REWORKED HOLE INAug 4, 2002 · N526UP · Boeing 747212B · Fuselage Main, StructureSDR UPS02439064Fitting · crackedINSPECTION TYPE:C BS 1480 RH B/H #16 HOLE FOUND CRACK AT OUTER CHORD SPLICE FTG, RUNNING I/B APPROX 1/16" & O/B APPROX 1/8" LONG.(STR R33 TO R34). RH BS 1480 B/H #16 HOLE AT OUTER CHORD SPLICE FTG REAMED TO 0.562" AND BUSHING INSTALLED AS PER SB 747-53A239Aug 4, 2002 · N526UP · Boeing 747212B · Fuselage Main, StructureSDR UPS02439063Fitting · crackedINSPECTION TYPE:C BS 1480 RH B/H #18 HOLE FOUND CRACK AT OUTER CHORD SPLICE FTG, RUNNING O/B APPROX 0.030" LONG. (STR R33 TO R34) RH BS 1480 B/H #10 HOLE AT OUTER CHORD SPLICE FTG REAMED TO 0.625" AND BUSHING INSTALLED AS PER SB 747-53A2390 REWORKED HOLE IAug 4, 2002 · N526UP · Boeing 747212B · Fuselage Main, StructureSDR UPS02439062Fitting · crackedINSPECTION TYPE:C RH BS 1480 B/H #14 HOLE CRACK AT B/H WEB AFT SURFACE RUNNING UP APPROX 3/16" LONG. REFER ATTACHED SKETCH. ( STR R33 TO R34) RH BS 1480 B/H #14 HOLE AT B/HEAD WEB REAMED TO 0.500" AND BUSHING INSTALLED AS PER SB747-53A2390 REWORKED HOLE CRAug 4, 2002 · N526UP · Boeing 747212B · Fuselage Main, StructureSDR UPS02439061Fitting · crackedINSPECTION TYPE:C RH BS 1480 #16 HOLE CRACK FOUND AT SPLICE PLATE AFT SURFACE RUNNING UP 1/8" AND RUNNING DOWN 3/16" LONG. REFER ATTACH SKETCH. (STR R33 TO R34) RH BS 1480 B/H SPLICE PLATE REPLACED DUE HOLE CRACK EXCCEED 'D' MAX LIMIT AS PER SB 747-53A2390Aug 4, 2002 · N526UP · Boeing 747212B · Fuselage Main, StructureSDR UPS02439060Skin · crackedINSPECTION TYPE:C RH BS 1480 BULKHEAD CHROD AREA #11 HOLE CRACK FOUND AT SKIN, APPROX 1/16" RUNNING FWD. REFER ATTACHED SKETCH. (STR R34 ) RH BS 1480 B/H #11 HOLE AT SKIN REAMED TO 0.625" AND BUSHING INSTALLED AS PER SB 747-53A2390 REWORKED HOLE INSPECTED Aug 4, 2002 · N526UP · Boeing 747212B · Fuselage Main, Plate/SkinSDR UPS02439058Skin · crackedINSPECTION TYPE:C RH BS 1480 B/H 33 HOLE CRACK FOUND AT SKIN THROUGH THICKNESS RUNNING FWD. REFER ATTACHED SKETCH. (STR R33 TO R34 ) RH BS 1480 B/H #3 HOLE AT SKIN REAMED TO 0.625" AND BUSHING INSTALLED AS PER SB 747-53A2390 REWORKED HOLE INSPECTED NIL CRAug 4, 2002 · N526UP · Boeing 747212B · Fuselage Main, Plate/SkinSDR UPS02439057Fitting · corrodedINSPECTION TYPE:C, RIGHT BS 1480 BULKHEAD NR 6 HOLE CORROSION FOUND AT EXTENSION FITTING AROUND BORE STR 33R TO 34R. RIGHT BS 1480 BULKHEAD NR 6 HOLE AT EXTENSION FITTING REAMED AND BUSHING INSTALLED AS PER SB 747-53A2390.Aug 4, 2002 · N526UP · Boeing 747212B · Fuselage Miscellaneous StructureSDR UPS02439056Fitting · crackedINSPECTION TYPE:C RH BS 1480 B/H #3 HOLE CRACK FOUND AT EXTENSION FITTING APPROX 1/16" LONG RUNNING FWD & 0.040" LONG RUNNING AFT. REFER ATTACHED SKETCH. (STR R33 TO R34). RH BS 1480 B/H #3 HOLE AT EXTENSION FITTING REAMED TO 0.625" AND BUSHING INSTALLED Aug 4, 2002 · N526UP · Boeing 747212B · Fuselage Main, StructureSDR UPS02439055Frame · crackedINSPECTION TYPE:C RIGHT BS 1480 BULKHEAD NR 3 HOLE CRACK FOUND AT BULKHEAD CHORD, APPROX .0625 INCH LONG, RUNNING FWD STR 33R TO 34R. RIGHT BS 1480 BULKHEAD NR 3 HOLE AT BULKHEAD CHORD REAMED AND BUSHING INSTALLED AS PER SB 747-53A2390.Aug 4, 2002 · N526UP · Boeing 747212B · Fuselage Main, FrameSDR UPS02439054Fitting · crackedINSPECTION TYPE:C RH BS 1480 B/H HOLE #5 CRACK FOUND 2EA AT EXTENSION FITTING 1/16" IN LENGTH APPROX AND 1EA AT HOLE #5 SKIN 1/16" IN LENGTH APPROX. REFER ATTACHED DWG FOR LOCATION. (STR R33 TO R34). RH BS1480 B/H HOLE #5 AT EXTENSION FITTING AND SKIN REAug 4, 2002 · N526UP · Boeing 747212B · Fuselage Main, StructureSDR UPS02439053Fitting · crackedINSPECTION TYPE:C LH BS 1480 B/H HOLE #5 CRACK FOUND 1EA AT FASTENER FITTING 1/16" IN LENGTH APPROX. REFER TO ATTACHED DWG FOR LOCATION. (STR L33 TO L34). LH BS 1480 B/H EXTENSION FITTING BOLT HOLE #5 REAMED TO 0.625" AND BUSHING INSTALLED AS PER SB 747-53Aug 4, 2002 · N526UP · Boeing 747212B · Fuselage Main, StructureSDR UPS02439052Fitting · crackedINSPECTION TYPE:C BS 1480 B/H LH #4 HOLE CRACK FOUND AT OUTER CHORD SPLICE FTG, RUNNING FWD APPROX 0.030" LONG. (CRACK AT O/B FACE). STR L33 TO L34 LH BS 1480 B/H LH #4 HOLE AT OUTER CHORD SPLICE FTG REAMED TO 0.625 AND BUSHING INSTALLED AS PER SB 747-53A2Aug 4, 2002 · N526UP · Boeing 747212B · Fuselage Main, StructureSDR UPS02439051Fitting · crackedINSPECTION TYPE:C LH BS 1480 B/H #7 HOLE 3EA CRACK FOUND AT OUTER CHORD SPLICE FTG RUNNING AFT 0.020" , 0.030" & 0.040" LONG (COUNT FROM UPPER TO LOWER ) (CRACK AT O/B FACE). STR L33 TO L34 LH BS 1480 B/H OUTER CHORD SPLICE FTG BOLT HOLE #7 REAMED TO 0.625Aug 4, 2002 · N526UP · Boeing 747212B · Fuselage Main, StructureSDR UPS02439050Fitting · crackedINSPECTION TYPE:C LH BS 1480 B/H #11 HOLE 2EA CRACK FOUND AT OUTER CHORD SPLICE FTG RUNNING FWD AT 8 O/C POSN & 7 O/C POSN (LOOKING I/B),CRACK AT 8 O/C POSN 3/16" LONG, CRACK AT 7 O/C POSN 0.040" LONG (CRACK AT O/B FACE) (STR L33 TO L34) LH BS 1480 B/H OUTAug 4, 2002 · N526UP · Boeing 747212B · Fuselage Main, StructureSDR UPS02439049Fitting · crackedINSPECTION TYPE:C LH BS 1480 B/H HOLE #23 CRACK FOUND AT SPLICE PLATE RUNNING CRACK FOUND AT SPLICE PLATE RUNNING UP APPROX 0.040" REFER ATTACHED SKETCH. (STR L33 TO L34) LH BS 1480 B/H HOLE #23 AT SPLICE PLATE REAMED TO 0.500" AND BUSHING INSTALLED AS PEAug 4, 2002 · N526UP · Boeing 747212B · Fuselage Main, StructureSDR UPS02439048Fitting · crackedINSPECTION TYPE:C LH BS 1480 B/H MOD HOLE #14 CRACK FOUND AT SPLICE PLATE AFT SURFACE RUNNING UP APPROX 1/16" LONG. REFER ATTACH SKETCH. (STR L33 TO L34) LH BS 1480 B/H SPLICE PLATE BOLT HOLE #14 REAMED TO 0.500" AND BUSHING INSTALLED AS PER SB 747-53A2390Aug 4, 2002 · N526UP · Boeing 747212B · Fuselage Main, StructureSDR UPS02439047Fitting · crackedINSPECTION TYPE:C LH BS 1480 B/H HOLE #15 CRACK FOUND AT SPLICE PLATE RUNNING UP & DOWN, BOTH CRACKS APPROX 0.020", REFER ATTACH SKETCH. LH B/H BOLT HOLE #15 REAMED TO 0.500" AS PER SB 747-53A2390 FIG.11 CRACK TEST DONE NO CRACK FOUND AS PER NTM PT6 51-00-Aug 4, 2002 · N526UP · Boeing 747212B · Fuselage Main, StructureSDR UPS02439046Stiffener · crackedINSPECTION TYPE:C M/D- BS 2300 RBL 10 WL 190 FLR BEAM ATT VERTICAL STIFFENER CRK. STIFFENER REPLACED AS PER SRM 51-10-01.Aug 4, 2002 · N526UP · Boeing 747212B · Fuselage Main, StructureSDR UPS02439213Floorbeam · corrodedINSPECTION TYPE:C, M/D BS 460 RBL 58 - RBL 70 FLOORBEAM WEB FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-01, CORROSION BLEND OUT EXCEEDS SRM 53-10-01 FIG 1 LIMITS, REPAIRED BS 460 RBL 70 FLOORBEAM WEB IAW SRM FIG 53-10-07 FIG 11.Aug 3, 2002 · N526UP · Boeing 747212B · Fuselage Main, Floor BeamSDR UPS02439174Web · crackedINSPECTION TYPE:C #4 PYLON REAR MOUNT B/H AFT WEB FOUND CRACKS. #4 PYLON REAR ENG MOUNT BULKHEAD REPAIR CARRIED OUT AS PER HX RS # R-54-53-3487.Aug 3, 2002 · N526UP · Boeing 747212B · Nacelle/Pylon, Main FrameSDR UPS02439173Web · crackedINSPECTION TYPE:C #1 PYLON REAR MOUNT B/H FWD & AFT WEB FOUND CRACKS. #1 PYLON REAR ENG MOUNT BULKHEAD REPAIR CARRIED OUT AS PER HX RS # R-54-53-34873.Aug 3, 2002 · N526UP · Boeing 747212B · Nacelle/Pylon, Main FrameSDR UPS02439172Web · crackedINSPECTION TYPE:C #2 PYLON REAR MOUNT B/H. FWD. AND AFT. WEB FOUND CRACKS. #2 PYLON REAR ENG MOUNT BULKHEAD REPAIR CARRIED OUT AS PER HX RS# R-54-53-34872Aug 3, 2002 · N526UP · Boeing 747212B · Nacelle/Pylon, Main FrameSDR UPS02439077Web · crackedINSPECTION TYPE:C FX- LOWER FUSELAGE PRESSURE BULKHEAD ATT WEB FOUND CRACKED AT STA 1480 RH SIDE O/B RBL 95. CLOSE OF SPLICE FITTING STRG 33R. WEB PANEL REPAIRED AS PER SRM 51-40-02 FIG 1Aug 3, 2002 · N526UP · Boeing 747212B · Fuselage Main, StructureSDR UPS02439214Skin · crackedINSPECTION TYPE:C AFT CARGO DOOR CUTOUT UPPER FWD CORNER 1EA FASTENER HOLE CRACK FOUND AT SKIN, APPROX 1/2" RUNNING DOWNWARD AND 5/16" RUNNING UPWARD PLS REFER ATT FTG. (BS1810 TO 1810, STR R28 TO R28) WASHER AND DOUBLER INSTALLED AT UPPER FWD CUTOUT AS PAug 2, 2002 · N526UP · Boeing 747212B · Fuselage Main, Plate/SkinSDR UPS02439112Web · corrodedINSPECTION TYPE:C FX- AIR CONDITIONING BAY REAR FIXED FAIRING INTERIOR REAR SURFACE FOUND SURFACE CORROSION AT STA 1255 RBL 9 TO RBL 30. REAR FIXED FAIRING REAR WEB AND SUPPORT CHORD REPAIRED AS PER SRM 51-40-02 FIG 1, 51-40-03 FIG 2 AND FIXED PNL REPLACED PEAug 2, 2002 · N526UP · Boeing 747212B · Aerodynamic FairingsSDR 0202516642Odor · detectedDURING FLIGHT, AN ELECTRICAL FUME EMITTED IN THE UPPER DECK. PULLED UPPER DECK GALLEY CIRCUIT BREAKERS AND AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. VISUALLY INSPECTED AND OPERATIONALLY CHECKED UPPER DECK WITH NO FAULTS FOUND.Jul 28, 2002 · N642NW · Boeing 747212B · Air Distribution SystemSDR EIA2002087Battery · smoke3 HOURS INTO FLIGHT, AIRCRAFT BATTERY BEGAN TO VENT SMOKE AND HAD AN ELECTRICAL ODOR. A FLIGHT TURN BACK WAS DONE.Jul 22, 2002 · N482EV · Boeing 747212B · Battery/Charger SystemSDR UPS02438694Light · inoperativeINSPECTION TYPE:N/A EXTERIOR ESCAPE SLIDE LIGHT INOP.Jun 24, 2002 · N520UP · Boeing 747212B · Emergency LightingSDR 0201776641Light · defectiveEN ROUTE TO AMS, SEAT 35A READING LIGHT WAS SMOKING AND SMELLED HOT. COVER AND BULB WERE REMOVED AND THE FLIGHT CONTINUED TO AMS AND LANDED WITHOUT INCIDENT. REPLACED THE SEB. OPERATIONAL CHECK OK.Jun 1, 2002 · N641NW · Boeing 747212B · Passenger Compartment LightingSDR UPS02438377Engine · malfunctionedINSPECTION TYPE:N/A ATB NR 2 ENG OVERTEMP, VIBRATION (IFSD) CREW DECLARED EMERGENCY. REMOVED AND REPLACED NR 2 ENGINE IAW TC NO 5000 LEAK AND OPS CHECK NORMAL.May 22, 2002 · N526UP · Boeing 747212B · Engine (Turbine/Turboprop)SDR EIA2002060Switch · faultySMOKE SEEN COMING FROM THE NR HF RADIO PANEL, SMOKE STOPPED IMMEDIATELY WHEN RADIO WAS SWITCHED OFF. FOUND RIGHT INBOARD LANDING LIGHT SWITCH BAD, REPLACED SWITCH AND HF CONTROL PANEL PER MM.May 5, 2002 · N486EV · Boeing 747212B · Exterior LightingSDR UPS02438067Fire Warning · false activationINSPECTION TYPE:N/A DURING CRUISE AT FL270, ALL FIRE WARNING/DET LIGHTS ILLUMINATED MOMENTARILY AND FIRE BELL ALSO RANG MOMENTARILY. THE FIELD OFF AND GEN OPEN LIGHT ON NUMBER 1 GEN WERE ILLUMINATED. REFER TO ITEM 2 AND T/S FOUND THAT FIRE WARNING/DET LIGHT Apr 19, 2002 · N525UP · Boeing 747212B · Fire DetectionSDR UPS02438066Power Supply · dischargedINSPECTION TYPE:PFLT EMERGENCY EXIT SIGN ABOVE UPPER DECK ESCAPE SLIDE DOOR INOP. LIGHT COMES ON AND THEN GOES OUT QUICKLY. REMOVED AND REPLACED POWER PACK PER AMM 33-51-04, OPS CHECK GOOD.Apr 18, 2002 · N525UP · Boeing 747212B · Emergency LightingSDR UPS02438065Skin · crackedINSPECTION TYPE: FOUND NUMEROUS BURNT AND PITTED FASTENERS ON RT SIDE OF FUSELAGE AT STA 140 AT ABOUT 4 O'CLOCK TO 6 O'CLOCK POSITION COUNTING AFT TO STA 2240. REMOVED DAMAGED FASTENERS PER 53-30-03, EDDIE CURRENT INSPECTION FOUND 3 SMALL CRACKS AT 3 SEPARATEApr 17, 2002 · N526UP · Boeing 747212B · Fuselage Main, Plate/SkinSDR EIA2002035Actuator · failedCBBI - AFTER NR 4 THRUST LEVER WAS RETARDED TO IDLE ON DESCENT THE NR 4 ENGINE HAD AN UNRECOVERABLE COMPRESSOR STALL. ENGINE SHUTDOWN ACCOMPLISHED. RESTART UNSUCCESSFUL. INSPECTED ENGINE. REPLACED NR 4 ENGINE EVC UNIT (P/N 7479555) AND STATOR VANE CONTROL Apr 12, 2002 · N482EV · Boeing 747212B · Turbine Engine Compressor SectionSDR UPS02438011Power Supply · dischargedINSPECTION TYPE:IN UPPER DECK AFT EMERGENCY LIGHT INOP. REMOVED SIDEWALL AND BOTH LIGHTS. REMOVED POWER SUPPLY, NO HELP. FOUND POWER SUPPLY TO BE BAD FROM STOCK. REMOVED AND REPLACED POWER SUPPLY IN STA 650 AND INSTALLED SIDEWALL & LIGHT ASSY, SYS CHECKS NApr 9, 2002 · N526UP · Boeing 747212B · Emergency LightingSDR UPS02437987Shear Tie · crackedINSPECTION TYPE:C NOSE WHEEL WELL VERTICAL BEAM WEB RT BS 280 NR 3 AND NR 4 SHEAR TIE CLIP (COUNT FROM TOP) CRACK FOUND AT FASTENER. NWW VERTICAL BEAM WEB RT BS 280 NR 3 AND 4 SHEAR TIE CLIP (COUNT FROM TOP) REPLACED AS PER SRM 51-10-01 & INSTALLED AS PER BOEMar 28, 2002 · N525UP · Boeing 747212B · Fuselage Main, StructureSDR UPS02437986Shear Tie · crackedINSPECTION TYPE:C NOSE WHEEL WELL VERTICAL BEAM WEB BS 280 LT NR 4 SHEAR TIE CLIP (COUNT FROM TOP) FOUND CRACK AT FASTENER. NWW VERTICAL BEAM WEB LT BS 280 NR 4 SHEAR TIE CLIP (COUNT FROM TOP) REPLACED AS PER SRM 51-10-01 & BOEING DWG 624U0005.Mar 28, 2002 · N525UP · Boeing 747212B · Fuselage Main, StructureSDR UPS02437984Shear Tie · crackedINSPECTION TYPE:C NOSE WHEEL WELL VERTICAL BEAM WEB BS 320 LT NR 3 SHEAR TIE CLIP (COUNT FROM TOP) FOUND CRACK AT FASTENER. NWW VERTICAL BEAM WEB LT BS 320 NR 3 SHEAR TIE CLIP (COUNT FROM TOP) REPLACED AS PER SRM 51-10-01 AND INSTALLED AS PER BOEING DWG 624U0Mar 28, 2002 · N525UP · Boeing 747212B · Fuselage Main, StructureSDR UPS02437983Shear Tie · crackedINSPECTION TYPE:C NOSE WHEEL WELL VERTICAL BEAM WEB RT BS 300 NR 2 AND 4 SHEAR TIE CLIP (COUNT FROM TOP) CRACK FOUND AT FASTENER. NWW VERTICAL BEAM WEB RT BS 300 NR 2 AND 4 SHEAR TIE CLIP REPLACED (COUNT FROM TOP) REPLACED AS PER SRM 51-10-01 AND INSTALLED ASMar 28, 2002 · N525UP · Boeing 747212B · Fuselage Main, StructureSDR UPS02437982Shear Tie · crackedINSPECTION TYPE:C NOSE WHEEL WELL VERTICAL BEAM WEB BS 300 LT NR 3 & 4 SHEAR TIE CLIP (COUNT FROM TOP) FOUND CRACK AT FASTENER. NWW VERTICAL BEAM WEB LT BS 300 NR 3 & 4 SHEAR TIE CLIP (COUNT FROM TOP) REPLACED AS PER SRM 51-10-01 AND INSTALLED AS PER BOEING DMar 28, 2002 · N525UP · Boeing 747212B · Fuselage Main, StructureSDR UPS02437981Clip · crackedINSPECTION TYPE:C NOSE WHEEL WELL VERTICAL BEAM WEB WEB R/H BS 320 #2 SHEAR TIE CLIP (COUNT FROM TOP) CRACK FOUND AT FASTENER AS MARKED. NWW VERTICAL BEAM WEB RH BS 320 #2 SHEAR TIE CLIP (COUNT FROM TOP) REPLACED AS PER SRM 51-10-01 & INSTALLED AS PER BOEIMar 28, 2002 · N525UP · Boeing 747212B · Fuselage Main, StructureSDR UPS02438018Fitting · corrodedINSPECTION TYPE:C LT MLG W/W STA 1480 LBL 65 STR 42L WL 122 LONGERON FITTING AND ATT PLATE FOUND CORROSION (AFT OF O/B TRUNNION SUPPORT FITTING).Mar 27, 2002 · N525UP · Boeing 747212B · Fuselage Miscellaneous StructureSDR UPS02437985Angle · crackedINSPECTION TYPE:C NLG W/W PRESSURE DECK LH CORNER LONG. ANGLE FOUND CRACKED AT BS 321 LBL 32 AS MARKED. NLG W/W PRESSURE DECK LH ANGLE REPLACE AS PER EO B747-5310-0574 DWG 624U0005 ST 3.Mar 27, 2002 · N525UP · Boeing 747212B · Fuselage Main, Structure
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