Boeing 767-300

Service difficulty reports · 2,161

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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 = '767300'
  ORDER BY difficulty_date DESC"

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SDR HALA0600701Floorbeam · crackedFOUND CRACKED FLOORBEAM AT BS 1439, LBL 22.20. REMOVED AND REPLACED FLOORBEAM AT BS 1439, LBL 22.20 IAW SRM 51-40-02.Jul 29, 2006 · N596HA · Boeing 767300 · Fuselage Main, Floor BeamSDR HALA0600530Switch · malfunctionedETOPS SIGNIFICANT SYSTEM, RIGHT PACK BITE MAINTENANCE MESSAGE FOUND ON ECS/MSG PAGE DURING OVERNIGHT CHECK. PERFORMED TROUBLESHOOTING PROCEDURES PER FIM 21-51-00/103 BITE TEST FAULTED ALTITUDE SWITCH. PREVIOUS TEST FAULTED ALTITUDE SWITCH. VERIFY TEST HAD NJul 29, 2006 · N587HA · Boeing 767300 · Cabin Cooling SystemSDR HALA0600523Lamp · inoperativeEXTERIOR EMERGENCY LIGHT AT L2 DOOR INOP. RELAMPED, OPS CHECK GOOD.Jul 28, 2006 · N592HA · Boeing 767300 · Emergency LightingSDR HALA0600522Outflow Valve · malfunctionedETOPS SIGNIFICANT SYSTEM, EICAS MSG CABIN ALT AUTO 2 ILLUMINATED. R AND R ALT 2 OUTFLOW VLV PER FIM 21-31-00 BIT CK AND VERIFY NML, OPS CK OK.Jul 27, 2006 · N588HA · Boeing 767300 · Pressure Regulator/Outflow ValveSDR NOCA10606Battery · dischargedDUE TO INOPERATIVE EMERGENCY LIGHT REPLACED BATTERY.Jul 27, 2006 · N765NA · Boeing 767300 · Emergency LightingSDR HALA0600576Seat Track · crackedWHILE WORKING STA 786-999 LBL 54 WL 200 LONGITUDIAL BEAM REPLACEMENT FOUND THE STA 999-1060 SEAT TRACK LOWER SADLE CRACKED LBL 54 WL 200. REPLACED SEAT TRACK AT BS 999-1060, LBL 54, WL 200, IAW SRM 51-40-02.Jul 26, 2006 · N596HA · Boeing 767300 · Fuselage, Seat/Cargo Attach FittingsSDR HALA0600517Power Supply · unknownBTB SPOILERS EICAS & ANNUNCIATOR ILLUMINATED. REMOVED AND REPLACED CSEU POWER SUPPLY PER 27-09-00 OPS CHECK GOOD PER AMM 27-09-00. ACCOMPLISHED LMP TEST 30 PER AMM 22-00-03 LMP STATUS REMAINS IN LAND 3.Jul 26, 2006 · N585HA · Boeing 767300 · Drag Control SystemSDR HALA0600513Starter · failedETOPS SIGNIFICANT SYSTEMS - MAINT ENTRY: APU WILL NOT START- APU FAULT LITE ILLUMINATED AND APU BITE MSG ON EICAS (STATUS LEVEL). T/S TO BAD APU STARTER (FIM 49-11-00) REMOVE AND INSTALL STARTER (49-41-01-004-001 AND 49-41-01-404-007). REPLACED STARTER. OPJul 25, 2006 · N590HA · Boeing 767300 · APU Start/Ignition SystemSDR HALA0600514Circuit Card · faultyAPU FIRE LP1 STATUS MESSAGE. APPROX 3 HRS INTO FLIGHT. NO STATUS MESSAGE ON ENGINE PAGE. (FIM 26150700) WIRING CHECK OK IAW FIM 26-15-00, FIG.103. REPLACED APU FIRE DET 1 CARD M685. OPS CHECK OK IAW FIM 26-15-00. MESSAGE CLEARED. SYSTEM TEST OKJul 25, 2006 · N585HA · Boeing 767300 · Fire DetectionSDR HALA0600574Frame · crackedAFT CARGO BAY, CRACKED VERTICAL SUPPORT ON FRAME AT BS 1439, LBL 22.20, WL 130. REMOVED AND REPLACED VERTICAL SUPPORT ON FRAME BS 1439 LBL 22.2, WL 130 PER SRM 51-40-02.Jul 23, 2006 · N596HA · Boeing 767300 · Fuselage Main, FrameSDR HALA0600547Attach Fitting · crackedAFT HINGE ATTACHMENT SUPPORT CRACKED AT BS 1461, LBL 25, WL 191, ON AFT CARGO BAY, BULK CARGO DOOR, INNER DOOR GUARD. REMOVED DAMAGED AFT HINGE SUPPORT BRACKET FROM INNER BULK CARGO DOOR BS 1461, LBL 25, WL 191, FABRICATED NEW BRACKET, ALODINE, PRIMED, PAINTEJul 23, 2006 · N596HA · Boeing 767300 · Fuselage, Door HingeSDR HALA0600546Floorbeam · crackedHOLES CRACKED, FASTENERS LOOSE, IN AFT CARGO BAY, FLOORBEAM AT BS 1439, LBL 15.40. REMOVED FASTENERS AND FLOORBEAM FROM BS 1439, LBL 15.40, AFT CARGO BAY IAW SRM 51-40-02-06-0. INSTALLED NEW FLOORBEAM IAW SRM 51-30-01.Jul 23, 2006 · N596HA · Boeing 767300 · Fuselage Main, Floor BeamSDR HALA0600661Support Channel · corrodedCORROSION L-1 DOOR CENTER AND FWD SCUFF PLATES ATTACHED SUPPORT CHANNEL CORRODED. REMOVED DAMAGED CHANNEL AND FABRICATED NEW CHANNEL FROM 0.045" 7075 T6 LOT 671963. ALODINED AND PRIMED IAW SRM 51-20-01. INSTALLED NEW CHANNEL FOR L-1 DOOR CENTER AND FWD SCUFJul 22, 2006 · N596HA · Boeing 767300 · Fuselage Miscellaneous StructureSDR HALA0600573Shear Tie · corrodedCORROSION FWD CARGO COMPT SHEAR TIE CORRODED AT BS 654+22, BETWEEN STL 39L AND 39R. FWD CARGO COMP SHEAR TIE BS 654+22 BETWEEN STR 39L AND 39R FOUND TO BE OUT OF LIMITES SRM 53-00-07. REMOVED SHEAR TIE IAW SRM 51-40-02. FABRICATED NEW SHEAR TIE FROM 7075-TO .Jul 22, 2006 · N596HA · Boeing 767300 · Fuselage Internal Mounting StructureSDR HALA0600564Shear Tie · corrodedCORROSION FWD CARGO COMPT SHEAR TIE CORRODED AT BS 742 BETWEEN STR 38R AND 39R. FOUND SHEAR TIE AT BS 742 BETWEEN STR 38R & 39R TO BE OUT OF LIMITS, 100 PERCENT EXFOLIATED IAW SRM 53-00-07-12-25 SHEET 1. REMOVED CLIP & SHEAR TIE FROM BS 742 STR 38R & 39R FWDJul 22, 2006 · N596HA · Boeing 767300 · Fuselage Internal Mounting StructureSDR HALA0600548Shear Tie · corrodedCORRSION FWD CARGO COMPT SHEAR TIE, CORRODED AT BS 742 BETWEEN STR 33R & 34R. REMOVED CORROSION FROM SHEAR TIE BS 742 BETWEEN STR 33R & 34R. FOUND SHEAR TIE TO BE OUT OF LIMITS PER SRM 53-00-07-1A-2 SHEET 1 NOTES B, D AND E. FABRICATED NEW SHEAR TIE FROM 70Jul 22, 2006 · N596HA · Boeing 767300 · Fuselage Internal Mounting StructureSDR HALA0600610Skin · gougedSKIN GOUGED BS 462 STR 32R. BLENDED DAMAGE. DAMAGE FOUND TO BE OUT OF LIMITS, CUT AND REMOVED DAMAGE AREA. INSTALLED REPAIR IAW SRM 53-00-01-4, SRM 53-00-01-2R-1.Jul 21, 2006 · N596HA · Boeing 767300 · Fuselage Main, Plate/SkinSDR HALA0600600Skin · lightning strikeLIGHTNING STRIKE DAMAGE ON FUSELAGE SKIN BETWEEN BS 1788 AND 1767 BETWEEN STRINGERS 39L AND 36L. BLENDED LIGHTNING STRIKES BS 1767 - 1788, STR 36-39L PER SRM 53-00-01-14-1. LIGHTNING STRIKES NR 1, 2, 3, 5, 6, 7 FOUND TO BE WITHIN LIMITS PER SRM 53-00-01-1A-1Jul 21, 2006 · N596HA · Boeing 767300 · Fuselage Main, Plate/SkinSDR HALA0600601Skin · gougedFUSELAGE EXTERIOR, BS 1530 TO 1702 STR 21L, SKIN HAS CONTINUED GOUGE. GOUGE AT BS 1530 - 1702 WAS BLENDED, FOUND TO BE ALL WITHIN LIMITS, 2EA EXTERNAL PATCHES WERE REMOVED AND REPLACED WITH 1EA INCORPORATING PATCH AT BS 1629 - 1654 BETWEEN STR 21L & 22L. ALLJul 21, 2006 · N596HA · Boeing 767300 · Fuselage Main, Plate/SkinSDR HALA0600570Channel · corrodedCORROSION (C53-221-02) LEFT AFT ENTRY DOOR, CHANNEL ON LOWER SURFACE OF STAINLESS STEEL THRESHOLD PLATE CORRODED. REMOVED AND REPLACED LEFT AFT ENTRY DOOR THRESHOLD PLATE CHANNEL PER SMP 51-40-02-06-0 STEP 4.Jul 21, 2006 · N596HA · Boeing 767300 · Fuselage Miscellaneous StructureSDR HALA0600550Plate · corrodedCORROSION C53-221-02 LEFT AFT ENTRY DOOR, CHANNEL ON LOWER SURFACE OF STAINLESS STEEL THRESHOLD PLATE CORRODED. REMOVED AND REPLACED LT AFT DOOR THRESHOLD PLATE CHANNEL PER SPM 51-40-02-06-00.Jul 21, 2006 · N596HA · Boeing 767300 · Fuselage Miscellaneous StructureSDR HALA0600549Mount · corrodedCORROSION C53-221-02, LT AFT ENTRY DOOR, FWD GIRT BAR FLOOR FITTING MOUNT PLATE CORRODED. REMOVED LT AFT ENTRY DOOR GIRTBAR DOOR BRACKET AND PLATE FITTING IAW SRM 51-40-2. REMOVED CORROSION FROM MOUNT PLATES FOUND TO BE OUT OF LIMITS IAW SRM 52-00-15. FABRICJul 21, 2006 · Boeing 767300 · Fuselage Main, Attach FittingsSDR HALA0600700Skin · chafedEMPENNAGE SKIN HAS A CHAFING DAMAGE AT RT HORIZONTAL STABILIZER SLIDE SEAL CUTOUT LWD LOWER CORNER. REMOVED DAMAGED AREA, FOUND TO BE OUT OF LIMITS PER SRM 53-00-01-1A-1. REMOVED DAMAGED SKIN AND INSTALLED NEW SKIN IAW SRM 51-40-02. LOCATED AT RT HORIZONTALJul 20, 2006 · N596HA · Boeing 767300 · Fuselage Main, Plate/SkinSDR HALA0600572Skin · crackedNR 5 SLAT LOWER SKIN TANG AT I/B MAIN TRACK IS CRACKED AND HAS PULLED FASTENERS. REPAIRED NR 5 SLAT LOWER SKIN TANG IAW SRM 57-43-01, SRM 51-70-17, AMM 51-21-10 AND 51-24-02.Jul 20, 2006 · N596HA · Boeing 767300 · Leading Edge DevicesSDR HALA0600496Light · unknownFLT DECK EXIT SIGN/EMERGENCY LIGHT INOP IN AUTO MODE, MANUAL MODE GOOD. TESTED COCKPIT EMERG LT PER MM 33-51-00-715-227 AND 33-51-00-725-247, AUTO FUNCTION CHECKS NORMAL W/EMERG LTS ARMED OPEN C/B B-6 ON PILOTS OVHD P-11, EMERG CHGR PORTABLE, CLOSED C/B ALL OJul 20, 2006 · N588HA · Boeing 767300 · Emergency LightingSDR HALA0600863Skin · damagedAFT BULK CARGO DOOR, INNER DOOR SKIN DAMAGED AT BOTTOM CENTER EDGE OF DOOR. REPAIRED AFT BULK CARGO DOOR INNER SKIN AT BOTTOM CENTER EDGE OF DOOR PER ER NR 06-3081 AND HAL M 105 NR 96038.Jul 19, 2006 · N596HA · Boeing 767300 · Cargo/Baggage DoorsSDR HALA0600660Stiffener · crackedNR 1 ENG STRUT - PYLON AFT BULKHEAD INTERIOR - HORIZONTAL STIFFENER CRACKED AT LOWER FLANGE, AT SECOND FASTENER FROM O/B END, APPROX 18 INCHES BELOW WING PLANK. REMOVED NR 1 ENG STRUT AFT FAIRING HORIZONTAL STIFFENER 18 INCHES BELOW WING PLANK ON AFT SIDE INTJul 19, 2006 · N596HA · Boeing 767300 · Nacelle/Pylon, Bulkhead/FirewallSDR HALA0600649Stiffener · crackedFOUND VERTICAL STIFFENER CRACKED I/B AFT RADIUS FWD SIDE OF CENTER FUEL TANK STA 785 LBL 11 WL 194. REPAIRED STA 785 RBL11 WL 194 VERTICAL STIFFENER I/B RADIUS SIDE OF CENTER FUEL TANK IAW HAL M 105 NR 59012.Jul 19, 2006 · N596HA · Boeing 767300 · Fuselage Miscellaneous StructureSDR HALA0600636Attach Angle · crackedNR 1 ENG STRUT ACCESS 447DB CUTOUT O/B SMALL ATTACH ANGLE LOOSE WITH POSSIBLE CRACK IN UPPER RADIUS, APPROX 8 INCHES AFT OF DIAGONAL BRACE AFT END. REMOVED NR 1 ENG STRUT ACCESS 447DB CUTOUT O/B SMALL ATTACH ANGLES. FABRICATED NEW ANGLES, HEAT TREATED, DRILLJul 19, 2006 · N596HA · Boeing 767300 · Nacelle/Pylon, Attach FittingsSDR HALA0600509Seat Track · corrodedFOUND CORROSION ON SEAT TRACK AT BS 753-814, LBL 88. REMOVED CORROSION ON SEAT TRACK AT BS 753-814 LBL 88. REMOVED 12" BY 1 BY 0.019" FOUND TO BE WITHIN THE ACCEPTABLE LIMITS AS PER SRM 53-00-52 1A-1. ALODINED, PRIMED AND PAINTED AS PER 51-22-01-0G-0.Jul 19, 2006 · N596HA · Boeing 767300 · Fuselage, Seat/Cargo Attach FittingsSDR HALA0600495Pump · unknownETOPS SIGNIFICANT SYSTEM, RIGHT AFT FUEL PUMP WOULD NOT TURN OFF WITH SWITCH. RIGHT AFT FUEL PUMP OPS CHK NORMAL PER AMM 28-22-00-715-001. COULD NOT DUPLICATE PROBLEM.Jul 19, 2006 · N584HA · Boeing 767300 · Fuel Boost PumpSDR HALA0600596Seat Track · corrodedCORROSION ON SEAT TRACK AT STA 933 - 977 LBL 55 WL 200. REPLACED SEAT TRACK AT BS 933-977 LBL 55, WL 200, IAW SRM 53-00-52 AND SRM 51-40-02.Jul 18, 2006 · N596HA · Boeing 767300 · Fuselage, Seat/Cargo Attach FittingsSDR HALA0600598Strap · bentTENSION STRAP BENT AT STA 1220, RBL 40, WL 193. REPAIRED TENSION STRAP BS 1220, RBL 40, WL 193 PER SRM 51-70-11, FIG 101.Jul 18, 2006 · N596HA · Boeing 767300 · Fuselage Miscellaneous StructureSDR HALA0600597Strap · bentTENSION STRAP BENT STA 1287, LBL 40 WL 194. REPAIRED TENSION STRAP BS 1287, LBL 40, WL 194 PER SRM 51-70-11 FIG 101.Jul 18, 2006 · N596HA · Boeing 767300 · Fuselage Miscellaneous StructureSDR HALA0600599Intercostal · crackedINTERCOSTAL UPPER ANGLE CRACKED AT STA 1087 - 1109 LBL 40. REMOVED AND REPLACED INTERCOSTAL UPPER ANGLE AT STATION 1087 - 1109, LBL 40, WL 200 AS PER SRM 51-40-02.Jul 18, 2006 · N596HA · Boeing 767300 · Fuselage Miscellaneous StructureSDR HALA0600575Seat Track · corrodedSTA 933 - 977 LBL 55, WL 200, CORROSION IN SEAT TRACK. REPLACED SEAT TRACK AT BS 933-977, LBL 55, WL 200, IAW SRM 53-00-52 AND SRM 51-40-02.Jul 18, 2006 · N596HA · Boeing 767300 · Fuselage, Seat/Cargo Attach FittingsSDR HALA0600551Intercostal · crackedINTERCOSTAL UPPER ANGLE CRACKED STATION 1241 - 1263 LBL 40 WL 200. REMOVED AND REPLACED INTERCOSTAL UPPER ANGLE STATION 1240 - 1263 LBL40 WL 200 AS PER SRM 51-40-02.Jul 18, 2006 · N596HA · Boeing 767300 · Fuselage Miscellaneous StructureSDR HALA0600510Skin · corrodedFOUND CORROSION ON AFT CARGO BAY LOWER LOBE SKIN AT BS 1518 - 1540, S-38L AND 39L. CLEANED UP THE SURROUNDING AREA, AFT CARGO BAY LOWER LOBE SKIN AT BS 1518 - 1540, S-38L AND S-39L. FOUND PAINT FLAKING UP AND NO CORROSION NOTED, IAW SRM 51-10-02.Jul 18, 2006 · N596HA · Boeing 767300 · Fuselage Main, Plate/SkinSDR HALA0600511Floorbeam · corrodedFOUND CORROSION ON FLOORBEAM LWR FLANGE AT NUTPLATE HOLES, STA 1480 LBL 55-RBL 60 WL193. REMOVED NUT PLATES, REMOVED CORROSION AT 13 NUTPLATE HOLES, 1" BY 1" TO MAXIMUM DEPTH OF .011 AT LBL 193. ORIGINAL THICKNESS IS .013", REMAINING MATERIAL THICKNESS IS .1Jul 18, 2006 · N596HA · Boeing 767300 · Fuselage Main, Floor BeamSDR HALA0600493Oven · malfunctionedDURING CLIMBOUT OF PHX OVEN LOCATED IN FWD GALLEY FACING LEFT SIDE OF FUSELAGE FURTHEST AFT STARTED EMITTING SMOKE AND SMELL OF OVERHEATED INSULATION ALL STOPPED WHEN POWER WAS REMOVED. WIRES AND CONNECTION INSPECTED AND CHECKED BY ELECTRIC SHOP FOUND OK. REJul 18, 2006 · N586HA · Boeing 767300 · Buffet/GalleysSDR HALA0600699Floor Support · corrodedFUSELAGE INTERIOR STRUCTURE, BS 342 LBL89 WL200, FLOOR SUPPORT CORRODED UNDERNEATH DRAIN PAN. REMOVED FLOOR STRUCTURE PER SRM 51-40-2. REMOVED CORROSION, A AREA OF 1.5" BY 2" BY 100% OF ORIGINAL THICKNESS IS .070 FOUND TO BE OUT OF LIMITS PER SRM 53-00-51. Jul 17, 2006 · N596HA · Boeing 767300 · Fuselage Miscellaneous StructureSDR HALA0600611Floorbeam · corrodedCORROSION AFT CARGO BAY TOP OF FRAME BS 1197+66, RBL 38, WL 125. BLENDED CORROSION ON FRAME INNER CHORD AT BS 1197+66 RBL 48 TO LBL48. PART FOUND TO BE OUT OF LIMITS PER SRM 5-00-07. REMOVED AND REPLACED INNER CHORD FRAME PER SRM 51-40-02-06-0.Jul 17, 2006 · N596HA · Boeing 767300 · Fuselage Main, Floor BeamSDR SUHALA0600595Floorbeam · corrodedFOUND CORROSION AFT CARGO BAY TOP FLANGE OF FLOORBEAM UNDER NUTPLATE BS 1219, RBL 42, WL125. REMOVED CORROSION AT BS 1219, RBL42, WL 125, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07-A1-1. REMOVED HANDLING SYSTEM ROLLER TRAY TO GAIN ACCESS IAW SRM 51-40-02. RJul 17, 2006 · N596HA · Boeing 767300 · Fuselage Main, Floor BeamSDR HALA0600595Frame · corrodedCORROSION AFT CARGO BAY TOP FLANGE OF FRAME UNDER NUT PLATE BS 1219, RBL 42, WL 125. REMOVED CORROSION AT BS 1219, RBL 42, WL 125, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07-1A-1. REMOVED HANDLING SYSTEM ROLLER TRAY TO GAIN ACCESS IAW SRM 51-40-02, REMOVED FJul 17, 2006 · N595HA · Boeing 767300 · Fuselage Main, FrameSDR HALA0600553Frame · corrodedCORROSION AFT CARGO BAY TOP FLANGE OF FRAME UNDER NUT PLATE BS 1197+110, LBL 42, WL 125. REMOVED AND REPLACED TOP FLANGE CHORD ON FRAME AT BS 1197+110 LBL 44 TO RBL 44 WL 125 IAW B767 SPM 51-40-02.Jul 17, 2006 · N596HA · Boeing 767300 · Fuselage Main, FrameSDR HALA0600552Frame · corrodedCORROSION, AFT CARGO BAY TOP FLANGE OF FRAME UNDER NUT PLATE BS 1197+132 LBL 42, WL 125. REMOVED UPPER CHORD BEAM/FLOOR SUPPORT ANGLE ON FRAME AT BS 1197+132 44 LBL 44 RBL. INSTALLED NEW UPPER CHORD ON FRAME AT WL 125 IAW B767 SRM 51-40-02.Jul 17, 2006 · N596HA · Boeing 767300 · Fuselage Main, FrameSDR HALA0600554Intercostal · crackedFWD CARGO COMP INTERCOSTAL UPPER FLANGE CRACKED BETWEEN BS 654+66 TO 654+88 RBL 39, WL 200. REMOVED INTERCOSTAL UPPER FRAME AT STATION 654+77 RBL 39 WL 200 PER SRM 51-40-02-0 FIG 8, FABRICATED NEW FLANGE FROM MATERIAL 7075-T6, 0.0050" LOT 674775 PER SRM 53-30Jul 16, 2006 · N596HA · Boeing 767300 · Fuselage Miscellaneous StructureSDR HALA0600491Engine · surgesNR 2 ENGINE SURGE IN CRUISE FL 340 DUE TO WAKE TURB BEHIND B767. PERF FIM 71-05-00 FIG 103 SHT 3 BLK 6, NO DEFECTS NOTED. ACCOMP BLK 7, 8, NO DEFECTS NOTED. ACCOMP 71-05-00 FIM 9, 10, 11, 12 TO ENTIRETY, ENG OPS CK NML. TEST 4 ACCOMP OPS CK NML.Jul 16, 2006 · N580HA · Boeing 767300 · Engine (Turbine/Turboprop)SDR HALA0600569Exhaust Port · lightning strikeAPU TAIL CONE HAS 9 LIGHTING STRIKES ON LEFT SIDE. REMOVED APU TAIL AND EXHAUST DUCT CONE PER MM 49-81-01 AND REPAIRED TAIL CONE. DISASSEMBLED AND FABRICATED NEW SKIN AND INSTALLED TAIL CONE SKIN PER SRM 51-40-02 & DWG 231770 AND INSTALLED APU TAIL CONE PER Jul 15, 2006 · N596HA · Boeing 767300 · APU Exhaust SystemSDR HALA0600555Crease Beam · corrodedCREASE BEAM SUPPORT HAS CORROSION AT BS 532 LBL 96.0. REMOVED AND REPLACED BEAM SUPPORT AT BS 532 LBL 96.0 IAW SRM 51-40-2.Jul 15, 2006 · N596HA · Boeing 767300 · Fuselage Main, Structure
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