Boeing 747-200

Service difficulty reports · 651

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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 = '747200'
  ORDER BY difficulty_date DESC"

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SDR UPS07449429Skin · damagedHOLE IN FUSELAGE TAIL SECTION LEFT SIDE ABOVE HORIZONTAL STABILIZIER/ ELEVATOR APPROX 5 X 7 INCHES. FABRICATED AND INSTALLED SHEET METAL DOUBLER PER 747 SRM 53-30-03.Mar 13, 2007 · N522UP · Boeing 747200 · Horizontal Stabilizer, Plate/SkinSDR UPS07449325Light · inoperativeINSPECTION TYPE:N/A EMERGENCY LIGHTS INOP AT ESCAPE SLIDE DOOR FRAME AND EXIT SIGN ABOVE SLIDE. REMOVED AND REPLACED POWER SUPPLY MODULE FOR EXIT SIGN PER MM 33-51-04. EXIT SIGN OPS CHECKS NORMAL. LIGHTS IN ESCAPE DOOR FRAME STILL INOP. NEEDS MODULE X327, Mar 5, 2007 · N523UP · Boeing 747200 · Emergency LightingSDR 758001Trim System · failedASTU WAS ON DEFERRAL. REMOVED AND REPLACED ASTU PRIOR TO DEPARTURE OUT OF PANC IAW AMM 22-14-01. AFFECTED BOTH AUTOPILOT A AND B SYSTEMS AND COULD NOT ENGAGE BOTH AUTOPILOT IN FLIGHT. RETURNED TO PANC. ASTU OPERATIONAL CHECK ACCOMPLISHED ON GROUND AND FAILEFeb 14, 2007 · N758SA · Boeing 747200 · Auto Flight SystemSDR UPS06448778Lock · damagedATB - NR 1 THRUST REVERSER UNLOCK LIGHT FLASHING DURING FLIGHT. NR 1 THRUST REVERSER DEFERRED AND LOCKED OUT M340031 ASSIGNED. NR 1 ENGINE SHUT DOWN AS A PRECAUTION. R & R NR 1 ENGINE THRUST REVERSER SYCN LOCK PER MM 78-34-12. #1 T/R AND OPS CHECKS GOOD PER Dec 17, 2006 · N523UP · Boeing 747200 · Engine Thrust ReverserSDR UPS06448707Battery Pack · inoperativeUPPER DECK DOOR AISLE EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED AISLE LIGHT AND BATTERY PACK ASSY MM 33-51-02.Nov 20, 2006 · N522UP · Boeing 747200 · Emergency LightingSDR UPS06448701Light · illuminatedINSPECTION TYPE:N/A ATB - FWD L1 DOOR LIGHT ILLUMINATED. DOOR VERY NOISY AND APPEARED TO BE OFF LOCKS. PRESSURE 3.0 ALT 10,000 FT DEPRESSURIZED. RETURNED TO ANC. FOUND AFT SIDE LATCH ROLLER AND CAM UNSECURED. PERFORMED GVI, NO DEFECTS NOTED. PERFORMED OPNov 17, 2006 · N522UP · Boeing 747200 · Passenger/Crew DoorsSDR UPS06448292A/C Pack · odorINSPECTION TYPE:N/A NR 3 PACK OVERHEATS, ALSO BURNING SMELL. TRIPS RESET, TRIPPED AGAIN. NR 3 PACK AUTO FEATURE DEFERRED PER MEL 21-6-1, BYPASS VALVE GOES TO FULL HOT IN AUTO. R/R PACK TEMP CONTROLLER PER 21-62-06. OPS CK NORMAL. THIS CLEARS M336046.Oct 20, 2006 · N523UP · Boeing 747200 · Cabin Cooling SystemSDR UIEA200600226Control Unit · malfunctioned(DIV) AFTER T/O GROUND SAFETY RELAY LIGHT REMAINED ON ALONG WITH G/S 1 ANT LIGHT, PROBE HEAT LIGHT AND ALL 4 ALTERNATE NOT TILTED LIGHTS WERE ILLUMINATED. NR 1 ENG OVER SPEED ON N2 110.2 FOR 15 SEC AT CRUISE ALL OTHER ENG INDICATIONS NORMAL. NR 3 ENG N1 OVERSep 3, 2006 · N505MC · Boeing 747200 · Brake Anti-Skid SectionSDR UPS06447890Oxygen Bottle · leakingAIR TURN BACK. IN CRUISE O2 DROPPED TO 150 PSI. REPLACED CREW O2 BOTTLES, USED SONICAIR AND SOAP LEAK CHECK FOR ALL FLEX LINES, ON DEMAND REGULATORS, O2 BOTTLES, ALL ACCESSIBLE (B) NUT CONNECTIONS AND LINES, REG AND SHUT OFF VALVES. BLOW OUT DISC STILL INTASep 2, 2006 · N521UP · Boeing 747200 · Crew Oxygen SystemSDR UPS06447866Connector · looseFIRE DETECTION LIGHT ON FWD ANNUNCIATOR PANEL FLICKERED FOR A FEW SECONDS AFTER TAKEOFF. DEFERRED PER MEL 26-15; PERFORMED T/S IAW WDM 26-11-61 AND RESECURED LOOSE CONNECTION ON REAR OF PILOT'S PANEL. FIRE DET LIGHT OPS TEST NOW NORMAL. M332692 CLOSED AND PLSep 1, 2006 · N522UP · Boeing 747200 · Fire Protection System WiringSDR UPS06447825Controller · smokeZONE TEMP CONTROLLER NR 1 SMELLS OF SMOKE. REMOVED AND REPLACED CONTROLLER IAW MM 21 61 01.Aug 28, 2006 · N522UP · Boeing 747200 · Cabin Temperature Control SystemSDR UPS06447744Chip Detector · damagedATB - OIL QTY ON NR 2 ENGINE DROPPED TO ZERO OIL PRESSURE DECREASING SHUT DOWN NR 2 ENGINE. LANDING WT 629.0. REPLACED NR 4 BEARING MAG PLUG PER MM 72-61-00.Aug 22, 2006 · N523UP · Boeing 747200 · Turbine Engine Oil SystemSDR UPS06447496Pump · leakingNR 4 HYD SYS LOST ALL FLUID, SYS INOP. FOUND HYD LEAK FROM NR 4 EDP BODY. REPLACED NR 4 HYD PUMP PER MM 29-11-05 & REPLACED CASE DRAIN & PRESS FILTERS PER MM 29-11-00. LEAK CHECK & OPS OK. HYD PWR INSP PER MM 29-00-00 OK.Jul 31, 2006 · N523UP · Boeing 747200 · Hydraulic Pump (Electric/Engine), MainSDR UPS06447304Indicator · activatedPBE PRESS IND IS EXTENDED. INSTALLED NEW PBE.Jul 9, 2006 · N523UP · Boeing 747200 · Emergency EquipmentSDR UPS06447091Crank Assy · brokenCLIMBING THRU 20,000 FT HEARD & FELT THUMP L ENTRY DOOR 1 LIGHT CAME ON. DUMPED FUEL. FOUND L1 DOOR UPPER & LOWER CRANKS BROKEN ON AT SIDE OF DOOR. R/R'D CRANK ASSY, RE-RIGGED PER MM 52-11-01. DOOR OPS NORMAL.Jun 10, 2006 · N522UP · Boeing 747200 · Passenger/Crew DoorsSDR UPS06447083Light · inoperativeINSPECTION TYPE:N/A EMERGENCY LIGHTS OVER STEPS INOP. RELAMPED BATTERY PACK PER MM 33-51-04Jun 8, 2006 · N521UP · Boeing 747200 · Emergency LightingSDR KCSA061171Light · inoperativeUPPER DECK RIGHT EMERGENCY LIGHT IS INOP.May 27, 2006 · N704CK · Boeing 747200 · Emergency LightingSDR UPS06447023Frame · damagedINSPECTION TYPE:C M/D LT BS 488 FRAME EXISTING REPAIR BETWEEN S16 AND S22 REPLACE FRAME WEB REPAIR PER SRM 53-10-04 FIG 121. FRAME WEB REPAIRED AS PER SRM 53-10-04 FIG 121 AT BS 488 BETWEEN STR 15L - 19L AREA NEW SEGMENT WEB REPLACED AND INSTALLED AT BETWEEN May 22, 2006 · N521UP · Boeing 747200 · Fuselage Main, FrameSDR UPS06447024Spar · crackedINSPECTION TYPE:C LT WING FRONT SPAR WEB AT WS 642 AREA 1EA HOLE (9TH HOLE COUNT FROM TOP) COMMON TO RIB POST FOUND CRACK AT WEB. CRACK LENGTH .0625 INCH. LT WING FRONT SPAR WEB AT WS 642 (9TH HOLE COUNT FROM TOP) COMMON TO RIB POST IN ZONE A AS PER SB 747-5May 19, 2006 · N521UP · Boeing 747200 · Wing SparSDR UPS06446970Attach Angle · crackedINSPECTION TYPE:C NR 4 PYLON NAC STA 221.9 REAR ENG MOUNT B/H UPPER OF MID SPAR WEB ATT T-ANGLE FOUND CRACKED JUST AT O/B SIDE. CRACK LENGTH 1.75 INCH. NR 4 PYLON NAC STA 221.9 REAR ENG MOUNT B/H UPPER OF MID SPAR WEB ATT T-ANGLE REPAIRED AS PER SRM 51-40-04May 14, 2006 · N521UP · Boeing 747200 · Nacelle/Pylon, Frame/Spar/RibSDR UPS06446891Channel · crackedINSPECTION TYPE:C M/D BS 2350 LBL 10 TO 40 HAT SECTION FLANGE FOUND CORRODED. CORRORION BLEND OUT 0.032" X 1" X 10" EXCEED SRM LIMIT. HAT SECTION REPLACED AS PER SRM 51-10-01 PG 9 AND 51-30-02.May 13, 2006 · N521UP · Boeing 747200 · Fuselage Miscellaneous StructureSDR UPS06446890Channel · crackedINSPECTION TYPE:C M/D BS 2350 LBL 30 HAT SECTION FOUND CRACK. CRACK LENGTH .5 INCH. HAT SECTION REPLACED AS PER SRM 51-10-01 AND 51-30-02.May 13, 2006 · N521UP · Boeing 747200 · Fuselage Miscellaneous StructureSDR UPS06446903Cargo Track · crackedINSPECTION TYPE:C M/D BS 520-530 RBL 91 TIE DOWN TRACK I/B FLANGE FOUND CRACK. CRACK LENGTH .4375 INCH. M/D BS 480 TO BS 530 RBL 91 AREA SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 4.May 12, 2006 · N521UP · Boeing 747200 · Fuselage, Seat/Cargo Attach FittingsSDR UPS06446967Cargo Track · corrodedINSPECTION TYPE:C M/D TIE DOWN TRACK BS 480-510 LBL 33 CORRODED. CORROSION BLEND OUT 0.042 X .75 X 3 INCH EXCEED SRM LIMIT. CABIN BS 460 TO BS 510 LBL 33 TRACK REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.May 11, 2006 · N521UP · Boeing 747200 · Fuselage, Seat/Cargo Attach FittingsSDR UPS06446973Reveal · crackedINSPECTION TYPE:C M/D R1 DOOR CUTOUT FWD UPPER CORNER REVEAL FOUND CRACK. CRACK LENGTH .75 INCH. CORNER REVEAL REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.May 10, 2006 · N521UP · Boeing 747200 · Passenger/Crew DoorsSDR UPS06446965Stiffener · crackedINSPECTION TYPE:C NR 3 PYLON REAR MOUNT B/H UPPER T-CHORD RT END 2EA HOLE FOUND CRACKED. CRACK LENGTH .5 INCH. NR 3 PYLON REAR MOUNT B/H UPPER T-CHORD REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.May 10, 2006 · N521UP · Boeing 747200 · Nacelle/Pylon Miscellaneous StructureSDR UPS06447031Floorbeam · crackedINSPECTION TYPE:C U/D BS 340 FLOORBEAM UPPER CHORD FWD AND AFT FLANGE FOUND 8EA FLOOR PANEL ATT HOLE CRACKED. CRACK LENGTH 0.063 INCH. U/D BS 340 RBL 36 TO LHS MOST O/B FLOORBEAM UPPER CHORD REPAIRED AS PER RS R53-15-35489 AND UPS EO B747-5310-24401-A.May 9, 2006 · N521UP · Boeing 747200 · Fuselage Main, Floor BeamSDR UPS06447018Floorbeam · corrodedINSPECTION TYPE:C U/D BS 520 LBL 56-74 FLOORBEAM UPPER CHORD FOUND CORRODED. CORROSION BLEND OUT 0.070" X 1.5" X 2" EXCEED SRM LIMIT. U/D BS 520 LEFT O/B MOST TO RBL 56 FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 53-10-07 FIG 13.May 9, 2006 · N521UP · Boeing 747200 · Fuselage Main, Floor BeamSDR UPS06447016Panel · damagedINSPECTION TYPE:C RIGHT WING I/B LANDING LIGHT I/B PANEL FOUND PUNCH HOLE. CRACK LENGTH .375 INCH DIA. PANEL REPAIRED AS PER RS R57-41-35483 AND ENGINEERING FILE NUMBER 747-57-20091.May 9, 2006 · N521UP · Boeing 747200 · Wing, Plate/SkinSDR UPS06447014Web · crackedINSPECTION TYPE:C RIGHT WING - L/E D-FAIRING SUPPORT WEB FOUND CRACK AT R2 PDU I/B AREA. CRACK LENGTH 3.5 INCHES. RIGHT WING L/E D-FAIRING SUPPORT WEB REPAIRED AT ILES943 TO ILES955.5 AREA APPROX AS PER SRM 57-20-03 FIG 7.May 9, 2006 · N521UP · Boeing 747200 · Wing Miscellaneous StructureSDR UPS06446979Stiffener · crackedINSPECTION TYPE:C U/D BS 400 AND BS 410 RBL 78-80 RIGHT CREW DOOR CUTOUT LWR SILL AREA 2EA VERTICAL STIFFENER FOUND CRACK. CRACK LENGTH .25 INCH. STIFFENER REPLACED AS PER SRM 51-10-01 PG 9, 51-30-05 AND INSTALLED AS PER SRM 51-30-02.May 9, 2006 · N521UP · Boeing 747200 · Fuselage Miscellaneous StructureSDR UPS06446902Floor Support · corrodedINSPECTION TYPE:C COCKPIT BS 380-390 LBL 58-63 FLOOR SUPPORT -T- ANGLE LWR FACE FOUND CORROSION. CORROSION BLEND OUT 0.035" X 1" X 1" EXCEED SRM LIMIT. COCKPIT BS 340 TO BS 400 LBL 58-63 SUPPORT -T- REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-0May 9, 2006 · N521UP · Boeing 747200 · Fuselage Miscellaneous StructureSDR UPS06446901Structure · misrepairedINSPECTION TYPE:C SHORT EDGE MARGIN FOUND AT U/D BS 380 AFT FLANGE LBL 44, 50, 55.5, 61, 66.5 AND 72 AREA (LESS THAN 1.3). U/D BS 380 AFT FLANGE UPPER CHORD AT LBL 44, 50, 55.5, 61, 66.5 AND 72 AREA REPAIRED AS PER EO B747-5320-12407-F APP D PLAN C FIG 3.May 9, 2006 · N521UP · Boeing 747200 · Fuselage Miscellaneous StructureSDR UPS06446900Structure · misrepairedINSPECTION TYPE:C SHORT EDGE MARGIN FOUND AT U/D BS 380 AFT FLANGE RBL 40, 45, 50, 55.5, 61 AND 66.5 (LESS THAN 1.3). U/D BS 380 AFT FLANGE UPPER CHORD RBL 40, 45, 50, 55.5, 61 AND 66.5 AREA REPAIRED AS PER EO B747-5320-12407 APP D PLAN C FIG 3.May 9, 2006 · N521UP · Boeing 747200 · Fuselage Miscellaneous StructureSDR UPS06446899Floorbeam · crackedINSPECTION TYPE:C U/D BS 360 FLOORBEAM UPPER CHORD AFT FLANGE AT RBL 43 FOUND 1EA FLOOR PANEL ATT HOLE CRACK RUNNING FWD .0626 INCH LONG. CRACK LENGTH .0625 INCH. U/D BS 360 FLOORBEAM UPPER CHORD AFT FLANGE AT RBL43 REPAIRED AS PER EO B747-5320-12407 APP D PMay 9, 2006 · N521UP · Boeing 747200 · Fuselage Main, Floor BeamSDR UPS06446898Floorbeam · crackedINSPECTION TYPE:C U/D BS 360 FLOORBEAM UPPER CHORD AFT FLANGE AT LBL 47 FOUND 1EA PANEL ATT HOLE CRACK RUNNING AFT .0625 INCH LONG. CRACK LENGTH .0625 INCH. U/D BS 360 FLOORBEAM UPPER CHORD AFT FLANGE AT LBL 47 AREA REPAIRED AS PER RO B747-5320-12407 APP D PMay 9, 2006 · N521UP · Boeing 747200 · Fuselage Main, Floor BeamSDR UPS06446864Floorbeam · crackedINSPECTION TYPE:C U/D BS 360 FLOORBEAM AFT FLANGE AT LBL 26 FOUND 1EA FLOOR PANEL ATT HOLE CRACK RUNNING AFT 0.040 INCH. U/D BS 360 LBL 26 FLOORBEAM AFT FLANGE REPAIRED AS PER EO B747-5320-12407 APP D PLAN C FIG 3.May 9, 2006 · N521UP · Boeing 747200 · Fuselage Main, Floor BeamSDR UPS06447025Spar · crackedINSPECTION TYPE:C LT WING FRONT SPAR UPPER CHORD WS 642 AREA FOUND 1EA HOLE CRACK AT WEB RUNNING O/B APPROX .0625 INCH LONG. LT WING FRONT SPAR UPPER CHORD WS 642 WEB REPAIRED AS PER RS R57-21-35488. INSPECT THE FRONT SPAR IN ZONE-A AS PER SB 747-57A2311 R2 May 8, 2006 · N521UP · Boeing 747200 · Wing SparSDR UPS06447020Shear Tie · crackedINSPECTION TYPE:C CTR TANK LT LBL 83 LWR SHEAR TIE SUSPECT CRACK. CRACK LENGTH .625 INCH. CTR TANK LT LBL 83 LWR SHEAR TIE REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.May 8, 2006 · N521UP · Boeing 747200 · Fuselage Internal Mounting StructureSDR UPS06447019Shear Tie · crackedINSPECTION TYPE:C CTR TANK RT RBL 83 LWR SHEAR TIE SUPPORT CRACK. CRACK LENGTH .875 INCH. CTR TANK RT RBL 83 LWR SHEAR TIE REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.May 8, 2006 · N521UP · Boeing 747200 · Fuselage Internal Mounting StructureSDR UPS06446997Plate · crackedINSPECTION TYPE:C LEFT WING SURGE TANK WS 1516 UPPER STR 10 VENT CHANNEL ATTACH PLATE CRACK. CRACK LENGTH .375 INCH. LEFT WING SURGE TANK WS 1516 UPPER STR 10 VENT CHANNEL ATTACH PLATE REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 & 51-30-02.May 8, 2006 · N521UP · Boeing 747200 · Wing Miscellaneous StructureSDR UPS06446974Support Fitting · crackedINSPECTION TYPE:C FWD CARGO COMPT RT AFT STOP FITTING LOWER SUPPORT I/B SIDE FOUND CRACKED AT STA 970 TO STA 975 RBL 24 BELOW FLOOR AREA AS MARKED. CRACK LENGTH 6.5 INCH. FWD CARGO COMPT RT AFT STOP FITTING LWR SUPPORT REPLACED AS PER SRM 51-10-01 PG 9 & INSMay 8, 2006 · N521UP · Boeing 747200 · Fuselage Miscellaneous StructureSDR UPS06446906Stringer Splice · crackedINSPECTION TYPE:C AFT CARGO STR SPLICE CRACKED ON BS 1740 S49L. CRACK LENGTH .25 INCH. AFT CARGO COMPT BS 1740 STR 49L SPLICE REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.May 8, 2006 · N521UP · Boeing 747200 · Fuselage Main, Longeron/StringerSDR UPS06446998Floor Support · corrodedINSPECTION TYPE:C M/D BS 240-260 RBL 72 FLOOR SUPPORT CORROSION. CORROSION BLEND OUT 0.028" X .5" X 1" EXCEED SRM 53-10-01 FIG 1 LIMITS. M/D BS 220 TO BS 300 RT FLOOR SUPPORT REPLACED & INSTALLED AS PER SRM 51-10-01 PG 9 & 51-30-02.May 7, 2006 · N521UP · Boeing 747200 · Fuselage Miscellaneous StructureSDR UPS06446907Stringer Clip · crackedINSPECTION TYPE:C AFT CARGO STR CLIP BROKEN ON BS 1720 S40L. CRACK LENGTH .25 INCH AFT CARGO COMPT BS 1720 STR 40L ATT CLIP REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.May 7, 2006 · N521UP · Boeing 747200 · Fuselage Main, Attach FittingsSDR UPS06446895Cargo Track · corrodedINSPECTION TYPE:C M/D BS 440-460 RBL 88 TIE DOWN TRACK O/B FLANGE FOUND CORROSION. CORROSION BLEND OUT 0.055" X 1" X 1" EXCEED SRM LIMIT. M/D BS 410-460 RBL 88 TRACK REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.May 7, 2006 · N521UP · Boeing 747200 · Fuselage, Seat/Cargo Attach FittingsSDR UPS06446893Cargo Track · corrodedINSPECTION TYPE:C M/D - BS 440-460 LBL 11 TIE DOWN TRACK I/B FLANGE FOUND CORROSION. CORROSION BLEND OUT 0.057" X .5" X 1.5" EXCEED SRM LIMIT. M/D BS 440-460 LBL 11 TIE DOWN TRACK REPAIRED AS PER SRM 53-10-05 FIG 17.May 7, 2006 · N521UP · Boeing 747200 · Fuselage, Seat/Cargo Attach FittingsSDR UPS06447026Frame · crackedINSPECTION TYPE:C NR 3 PYLON REAR MOUNT BULKHEAD FOUND CRACKS AT BOTH SIDES FWD AND AFT FRAME WEB. CRACK LENGTH 1 INCH TO 3.5 INCH. NR 3 PYLON REAR MOUNT BULKHEAD FWD AND AFT BOTH SIDES FRAME WEB REPLACED AND REPAIRED AS PER RS R54-53-35482 AND ENGINEERING FMay 6, 2006 · N521UP · Boeing 747200 · Nacelle/Pylon, Frame/Spar/RibSDR UPS06446966Attach Angle · crackedINSPECTION TYPE:C NR 4 PYLON NAC STA 221.9 REAR ENG MOUNT B/H LOWER OF MID SPAR WEB LHS I/B AREA T-ANGLE CRACKED. CRACK LENGTH .5 INCH. NR 4 PYLON NAC STA 221.9 REAR ENG MOUNT B/H LOWER OF MID SPAR WEB ATTACH T-ANGLE REPLACED AND INSTALLED AS PER SRM 51-10-0May 6, 2006 · N521UP · Boeing 747200 · Nacelle/Pylon, Frame/Spar/RibSDR UPS06446894Stringer · crackedINSPECTION TYPE:C FWD CARGO LT SIDEWALL BS 500 STR 38 FOUND CRACKED AT RIVET AREA. CRACK LENGTH .5 INCH. FWD CARGO LT BS 473 TO BS 500 STR 38 REPAIRED AS PER SRM 53-10-03 FIG 3.May 6, 2006 · N521UP · Boeing 747200 · Fuselage Main, Longeron/Stringer
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