Boeing 767-300

Service difficulty reports · 2,161

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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 = '767300'
  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 HALA0600537Spar · damagedLT HORIZONTAL STABILIZER FWD AUXILIARY SPAR, UPPER MATING SURFACES FOR REMOVABLE LEADING EDGE HAS NUMEROUS SCRATCH MARKS. BLENDED NUMEROUS SCRATCH MARKS ON L/H HORIZONTAL STAB. FWD, AUX SPAR, UPPER SPAR MATING SURFACE FOR REMOVABLE LE. DEEPEST MEASUREMENT OBTJul 15, 2006 · N596HA · Boeing 767300 · Horizontal Stabilizer, Spar/RibSDR HALA0600508Skin · lightning strikeLIGHTING STRIKES(15) ON APU COMPARTMENT LEFT DOOR OUTER SKIN. REPAIRED LT APU DOOR (15 EA LIGHTNING STRIKES) IAW SRM 53-01-2R-8.Jul 15, 2006 · N596HA · Boeing 767300 · Auxiliary Power Unit (APU) DoorsSDR HALA0600490Circuit Card · failedL ENG FIRE LP 2 DISPLAYED. REPLACED L ENG FIRE DETECTION CARD M682 PER 767 FIM 26-11-00 FIG 104, OPS CHECK OK PER AMM 767 26-10-01.Jul 15, 2006 · N589HA · Boeing 767300 · Fire DetectionSDR HALA0600488Computer · malfunctionedETOPS SIGNIFICANT SYSTEM, EICAS STATUS MSG "ELEV FEEL" DISPLAYED. ACCOMPLISHED FIM 27-31-00. DISCONNECTED ELEV FEEL COMPUTER PER MM 27-31-19-024-001 (HAL5897 07/16/06). REMOVED AND INSTALLED ELEV FEEL COMPUTER PER AMM 27-31-19 UP TO STEP 3F10 COMPLETED INSTJul 15, 2006 · N583HA · Boeing 767300 · Elevator Control SystemSDR HALA0600593Floor Support · looseFUSELAGE INTERIOR FLOOR, BS 927 LBL 31 TO LBL 50 WL 200, FLOOR SUPPORT LOOSE AND CHAFING AT FASTENER HOLES. REPLACED FLOOR SUPPORT AT BS 927 LBL 31 TO LBL 50 WL 200 IAW SRM 51-40-02 AND DWG 140T0530.Jul 14, 2006 · N596HA · Boeing 767300 · Fuselage Miscellaneous StructureSDR HALA0600594Floor Support · looseFUSELAGE INTERIOR FLOOR, BS 977 LBL 56 TO LBL 72 WL 200, FLOOR SUPPORT LOOSE AND CHAFING AT FASTENER HOLES. REPLACED FLOOR SUPPORT AT BS 977 56 TO LBL 56 TO LBL 72 WL 200 IAW SRM 51-40-02 AND BOEING DWG 140T0530.Jul 14, 2006 · N596HA · Boeing 767300 · Fuselage Miscellaneous StructureSDR HALA0600592Floor Support · looseFUSELAGE INTERIOR FLOOR, BS 977 LBL 34 TO LBL 51 WL 200, FLOOR SUPPORT LOOSE AND CHAFING AT FASTENER HOLES. REPLACED FLOOR SUPPORT AT BS 977 LBL 34 TO LBL 51 WL 200 IAW SRM 51-40-02, IAW SRM 51-40-02 AND DWG 140T0530.Jul 14, 2006 · N596HA · Boeing 767300 · Fuselage Miscellaneous StructureSDR HALA0600565Acoustic Panel · puncturedNR 1 ENGINE INBOARD T/R ACOUSTIC PANEL HAS 2 PUNCTURES 5 INCHES FROM T/E 5 O`CLOCK POSITION. REPAIRED NR 1 ENGINE INBOARD T/R ACOUSTIC PANEL 2 PUNCTURED AREA 5 INCHES T/E 5 O`CLOCK POSITION IAW SRM 54-00-01-2R1.Jul 14, 2006 · N596HA · Boeing 767300 · Engine Thrust ReverserSDR HALA0600556Plate · crackedLEFT WING LOWER T/E WIFFLE PLATE IS CRACKED AT WS 455. REMOVED LEFT WING LWR T/E WIFFLE PLATE AT WS 455. FABRICATED AND INSTALLED IAW SRM 51-40-2 AND BOEING DRAWING 113T1661.Jul 14, 2006 · N596HA · Boeing 767300 · Wing, Attach FittingsSDR HALA0600487Pump · leakingETOPS SIGNIFICANT SYSTEM, DURING WALK AROUND FUEL NOTED DRIPPING FROM R. ENG. OPENED ENGINE, TRACED LEAKAGE TO MAIN FUEL PUMP DRIVE PAD. LEAKAGE RATE 2-3 DROPS PER MINUTE, WITHIN ALLOWABLE LEAKAGE RATE PER MM 71-71-00. OK FOR CONTINUED SERVICE. CLOSED AND Jul 14, 2006 · N586HA · Boeing 767300 · Engine Fuel PumpSDR HALA0600489Radio · malfunctionedETOPS SIGNIFICANT SYSTEM, NR 1 HF RADIO WILL NOT TUNE. PERFORMED OPERATION CK OF NR 1 HF RADIO-SYS, OPS CK OK PER AMM 23-11-03.Jul 14, 2006 · N588HA · Boeing 767300 · VHF Communications SystemSDR HALA0600589Crease Beam · corrodedCREASE BEAM FITTING CORRODED AT STR 20R, BS 456 TO 478. REPLACED CREASE BEAM FITTING AT BS 456 TO 478 RBL 88 IAW SRM 51-40-02.Jul 13, 2006 · N596HA · Boeing 767300 · Fuselage Main, StructureSDR HALA0600591Crease Beam · corrodedCRASED BEAM FITTING CORRODED AT STR 20R, BS 654+66 TO 654+88. REPLACED CREASE BEAM FITTING AT BS 654+66 TO 654+88, IAW SRM 51-40-02.Jul 13, 2006 · N596HA · Boeing 767300 · Fuselage Main, StructureSDR HALA0600566Skin · corrodedLEFT O/B AILERON O/B COUNTER BALANCE WEIGHT ARM SKIN IS CORRODED AT FWD UPPER TIP. REMOVED AND REPLACED LEFT AILERON BALANCE MAST ASSY, IAW SRM 51-40-02, SRM 51-40-04 AND DWG 1177106 & 113T7100. REMOVAL, REINSTALLED & BALANCED.Jul 13, 2006 · N596HA · Boeing 767300 · AileronsSDR HALA0600536Crease Beam · corrodedCREASE BEAM FITTING CORRODED AT STA 20R, BS 654+88 TO 654+110.//REMOVED CORROSION FROM CREASE BEAM FITTING AT STR 20R BS 654+88 TO 654+110. REMOVED 1.00"X2.00" X .030" DEEP ORGINAL THICKNESS .050". FOUND TO BE OUT OF LIMITES PER SRM 53-00-51/101SHT 1-3 DETAIL Jul 13, 2006 · N596HA · Boeing 767300 · Fuselage Main, StructureSDR HALA0600535Fitting · corrodedCREASE BEAM FITTING CORRODED AT STR-20L, BS 588 TO 610.// REPLACED CREASE BEAM FITTING SPAN BS 588 TO 610 STR 20 L/H.Jul 13, 2006 · N596HA · Boeing 767300 · Fuselage Main, Attach FittingsSDR HALA0600506Crease Beam · corrodedFOUND CORROSION ON CREASE BEAM FITTING AT STR 20R, BS 654+44 TO 654+66. REMOVED CORROSION AT CREASE BEAM FITTING AT STR 20R, BS 654+44 TO 654+66. AN AREA 1.00" BY 2.00" BY 0.005" DEEP. ORIGINAL THICKNESS 0.90". REMAINING THICKNESS IS 0.85" FOUND TO BE IN LJul 13, 2006 · N596HA · Boeing 767300 · Fuselage Main, StructureSDR HALA0600507Crease Beam · corrodedFOUND CORROSION ON CREASED BEAM FITTING AT STR-20L, BS 566 TO 588. REMOVED AND REPLACED CORRODED CREASE BEAM FITTING AT STR 20L, BS 566 TO BS 588, IAW SRM 51-40-02 AND SRM 51-20-01.Jul 13, 2006 · N596HA · Boeing 767300 · Fuselage Main, StructureSDR HALA0600486Engine · malfunctionedBTB - ABNORMAL START ON NR 2 ENGINE ALL NORMAL UNTIL EGT HUNG AT 420 FOR APPROX 10 SEC. THEN EGT COOLED THEN HEATED BACK UP TO 420 DEG. THEN N1 WENT BLANK. GROUND CREW NOTICED NO N1 ROTATION AND SAID THE ENG DIDN'T SOUND RIGHT. FA'S ALSO SAID ENGINE START Jul 13, 2006 · N584HA · Boeing 767300 · Engine (Turbine/Turboprop)SDR HALA0600567Web · corrodedCORROSION ON FUSELAGE INTERIOR FLOOR STRUCTURE, BS 406 RBL 62 WL 200, ON FLOOR WEB. BLENDED AREA 2" X 2" X .026", ORIGINAL THICKNESS IS .063" OUT OF LIMITS. FABRICATED REPLACEMENT WEB FOR BS 396 TO 412 RBL 54 TO 88.5 WL 200. REMOVED AND REPLACED WEB, MATERIJul 12, 2006 · N596HA · Boeing 767300 · Fuselage Miscellaneous StructureSDR HALA0600534Floorbeam · damagedFLOORBEAM IS CHAFED A FASTNER HOLES AT BS 978-999, RBL 35, WL 200. FOUND DAMAGED HOLES TO BE OUT OF LIMITES, IAW SRM 53-50-1A-0. REPAIRED DAMAGE IAW SRM 53-00-51-2R-3.Jul 12, 2006 · N596HA · Boeing 767300 · Fuselage Main, Floor BeamSDR HALA0600505Seat Track · corrodedFOUND CORROSION ON SEAT TRACK AT BS-611 TO BS-785, RBL-88 WL-200. REMOVED CORROSION ALODINED, PRIMED AND RESTORED FINISH ON SEAT TRACK AT BS-611 TO BS-785, RBL 88 WL-200 IAW SRM 53-00-52, 51-20-00-0G-0 AND SRM 51-10-02-0G-0.Jul 12, 2006 · N596HA · Boeing 767300 · Fuselage, Seat/Cargo Attach FittingsSDR HALA0600484Switch · openETOPS SIGNIFICANT SYSTEM, PER FLT CREW APU WILL NOT START ON TAXI IN HNL. REPLACED APU AIR INTAKE DOOR OPEN SWITCH PER AMM 49- 15-02-404-13. OPS CHECK OF APU PER AMM49-15-02-404-13 OK.Jul 12, 2006 · N581HA · Boeing 767300 · APU Start/Ignition SystemSDR HALA0600557Pan · corrodedCORROSION FWD CARGO COMPT PDU 11R PAN HAS CORROSION AT BS 654+108 RBL 36. UPON FURTHER INVESTIGATION FOUND CRACK WITHIN CORRODED AREA. TRIMMED OUT CRACK AND CORROSION. TRIM OUT AREA .4" X .28" WITHIN LIMITS. HY FREQ INSPECTION REVEALED NO CRACKS. FORMED AJul 10, 2006 · N596HA · Boeing 767300 · Fuselage Miscellaneous StructureSDR HALA0600708Intercostal · corrodedFOUND CORROSION AFT CARGO BAY ON BOTTOM OF INTERCOSTAL STA 1307-1329, RBL 82 WL 193. REMOVED CORROSION ON INTERCOSTAL IN AFT CARGO BAY BS 1307- BS 1329 RBL 32 WL 193 IN2 AREAS, 1.5" BY.8" BY .010 DEEP AND .8"Z.3" BY .004 DEEP. BOTH AREAS OUT OF LIMITS PER SRJul 8, 2006 · N598HA · Boeing 767300 · Fuselage Miscellaneous StructureSDR HALA0600637Door Frame · corrodedCORROSION BULK CARGO DOOR CUTOUT AFT FRAME WEB STA 1461 BETWEEN STR 31L - 33L. REMOVED CORROSION, BULK CARGO DOOR CUTOUT AFT FRAME WEB STA 1461 BETWEEN STR 31 L - 33L, FOUND TO BE WITHIN LIMITS. TREATED, PRIMED, APPLIED ORIGINAL FINISH IAW SRM 53-00-07/101, Jul 8, 2006 · N598HA · Boeing 767300 · Fuselage Main, StructureSDR HALA0600504Skin · gougedFOUND GOUGES, AT FWD SIDE OF FORWARD CARGO BAY DOOR CUTOUT FROM S26R TO S32R FROM EDGE TO 12"FWD. BLENDED NUMEROUS GOUGES AT THE FWD SKIN, FWD SIDE OF FORWARD CARGO BAY DOOR CUTOUT S22 TO S41 AND S26R TO S32R IAW SRM 51-10-02. MAX MATERIAL REMOVED AT THE TAPJul 8, 2006 · N596HA · Boeing 767300 · Fuselage Main, Plate/SkinSDR HALA0600704Frame · corrodedFOUND CORROSION AFT CARGO BAY, ON FRAME UPPER CHORD 1197 RBL 38 WL 126. REMOVED CORROSION UPPER CHORD STA 1197, WL 126, IN AN AREA 2" BY 3" BY .041 PER SRM 51-10-2. ORIGINAL THICKNESS IS .100" OUT OF LIMITS PER SRM 53-00-07, FIG 101, SHEET 2. REMOVED OLD CHOJul 7, 2006 · N598HA · Boeing 767300 · Fuselage Main, FrameSDR HALA0600703Frame · corrodedCORROSION AFT CARGO BAY, ON FRAME UPPER CHORD STA 1197 + 132 LBL 8 - 19 WL 126. REMOVED CORROSION ON FRAME UPPER CHORD STA 1197 + 132 LBL 8-19 WL 126 IN SEVERAL AREAS. LARGEST AREA REMOVED WAS .065 IN IN A 3" BY .9 " AREA. ORIGINAL THICKNESS TO BE .100 OUT Jul 7, 2006 · N598HA · Boeing 767300 · Fuselage Main, FrameSDR HALA0600702Floor Support · corrodedCORROSION AFT CARGO COMPT FLOOR SUPPORT CORRODED AT BS 1413 TO 1418, 15 RBL WL 127. REMOVED CORROSION ON FLOOR SUPPORT AT BS 1413 TO 1418. CORROSION WAS OUT OF LIMITS PER SRM 51-10-02, AND 53-00-03. REMOVED FLOOR SUPPORT AND REPLACED WITH NEW, IAW SRM 51-40Jul 7, 2006 · N598HA · Boeing 767300 · Fuselage Miscellaneous StructureSDR HALA0600658Structure · crackedNLG WHEEL WELL LEFT AFT STRUCTURE IS CRACKED AT WL 178 STA 287. REPAIRED NLG WHEEL WELL LEFT AFT STRUCTURE AT BS 287 WL 178 LBL 25 PER SRM 51-70-12-00-0 FIG 1.Jul 7, 2006 · N596HA · Boeing 767300 · Fuselage Miscellaneous StructureSDR HALA0600659Floorbeam · corrodedCORROSION (767-3-229003) STA 347 FLOORBEAM CORRODED BL 0 TO RBL 55 WL 208. FOUND CORROSION TO BE OUT OF LIMITS, PER SRM 53-00-51. REPAIRED FLOORBEAM AT BS 347, BC 0 TO RBC 34 IAW SRM 53-00-51-22-1. CORROSION .0%. 100% NEW MATERIAL, ORIGNINAL THICKNESS IS .0Jul 7, 2006 · N596HA · Boeing 767300 · Fuselage Main, Floor BeamSDR HALA0600588Seat Track · corrodedCORROSION (767-3-249004) SEAT TRACK CORODDED STA 754 TO 808 RBL 88 WL 200. BS 754 TO 808 RBL WL 200, FABRICATED NEW SEAT TRACK PER SRM 53-00-52-2R-3 FIG 201. INSTALLED SEAT TRACK PER SRM 51-40-02-00-0. INSTALLED FASTENERS IN FWD SPLICE CHANNEL VERTICAL FLANJul 7, 2006 · N596HA · Boeing 767300 · Fuselage, Seat/Cargo Attach FittingsSDR HALA0600503Support Beam · crackedFOUND CRACK ON RT L/E SUPPORT BEAM AT AFT END OF PANEL 661BB I/B SUPPORT ANGLE. REMOVED CRACKED ANGLE F/W T/E AT AFT END OF PANEL 661BB I/B SUPPORT BEAM AND INSTALLED NEW REPLACEMENT ANGLE, FABRICATED FRAME MATERIAL LOT #704851 EXTRUSION BAC 1505-10054 #7075TJul 7, 2006 · N596HA · Boeing 767300 · Wing Miscellaneous StructureSDR HALA0600483Apu · overservicedETOPS SIGNIFICANT SYSTEM, CREW REPORTS APU AUTO SHUT DOWN, NO MESSAGE. FOUND OIL QTY OVERSERVICED BY .25 QTS DRAINED. APU OPS NORMAL.Jul 6, 2006 · N581HA · Boeing 767300 · APU System WiringSDR HALA0600475Actuator · failedSPOILER LIGHT AND SPOILER EICAS MESSAGE AFTER ENGINE START. ACCOMPLISHED FIM 27-05-00 FIG 105A. REPLACED LT SPOILER CTL MODULE. COND SAME. REINSTALLED SCM, FOUND M307 PIN 571/K11 SHORTED. REPLACED NR 2 O/B SPOILER PCA PER AMM 27-61-02. OPS/LEAK CHKS GOODJul 6, 2006 · N581HA · Boeing 767300 · Drag Control ActuatorSDR HALA0600471Indication Sys · malfunctionedETOPS SIGNIFICANT SYSTEM, INTERMITTENT LEFT QUANTITY GAUGE BLANKS AND TOTAL QUANTITY BLANK. DID NOT TEST FUEL QUANTITY. ACCOMPLISHED FIM 28-41-00 TABLE 101, FAULT CODE 59 NOTED, INDICATING LEFT TANK UNIT NR 9. ACCOMPLISHED TABLE 127 THRU D. NO FAULT INDICATJul 4, 2006 · N583HA · Boeing 767300 · Fuel Quantity IndicatorSDR HALA0600638Skin · corrodedCORROSION AT AFT CARGO DOOR INNER SKIN 16 INCHES FROM TOP OF DOOR AND 41 INCHES FROM FWD OF DOOR. REMOVED CORROSION OF 1"X 1", 1"X 1" AND 1" X 3" ON AFT DOOR INNER SKIN 16 INCHES FROM TOP AND 41 INCHES FROM FWD EDGE AT DOOR, ORIGINAL THICKNESS .040", THICKNESJul 3, 2006 · N598HA · Boeing 767300 · Cargo/Baggage DoorsSDR HALA0600469Warning Message · illuminatedBTB - ATT DISAGREE ON EICAS. RESET INST COMP C/B, ACCOMP FIM PER 34-21-00 ALL TEST PASS ACCOMPLISHED TEST 30 LMP REMAINS IN LAND 3 STATUS.Jul 3, 2006 · N584HA · Boeing 767300 · Independent Position Determining SystemSDR HALA0600723Shear Tie · corrodedCORROSION FWD CARGO COMPT SHEAR TIE CORRODED AT BS 742, BETWEEN STR 36L - 37L. CORROSION WAS FOUND TO BE OUT OF LIMITS ON SHEAR TIE VERTICAL FLANGE PER DETAIL 5 AT BS 742 BETWEEN STR 36L -37L PER SRM 53-00-07-1A-2. REMOVED AND REPLACED SHEAR TIE PER SRM 51-4Jul 2, 2006 · N598HA · Boeing 767300 · Fuselage Internal Mounting StructureSDR HALA0600724Shear Tie · corrodedCORROSION FWD CARGO COMPT SHEAR TIE CORRODED AT BS 762 BETWEEN STR 35R - 36R. REMOVED OUT OF LIMITS SHEAR TIE. FABRICATED, ALODINED, PRIMED HEAR TIE FROM 70750 CLAD,LOT 2339/09, DOC NR 140T2102. INSTALLED NEW FABRICATED SHEAR TIE, IAW SRM 51-40-02/801, AMM Jul 2, 2006 · N598HA · Boeing 767300 · Fuselage Internal Mounting StructureSDR HALA0600722Channel · crackedBIN SUPPORT CHANNEL CRACKED STA 1197 + 44, BETWEEN 11R - 12R. REMOVED AND REPLACED BIN SUPPORT CHANNEL STA 1197+44 BETWEEN STR 11R - 12R PER SRM 51-40-02/801 PG 1 DETAIL 1, AND SRM 51-42-02-08-0 PG 1, PA 2 B (1).Jul 2, 2006 · N598HA · Boeing 767300 · Fuselage Miscellaneous StructureSDR HALA0600652Shear Tie · corrodedFOUND FWD CARGO COMPARTMENT SHEAR TIE CORRODED AT BS 742 BETWEEN STR 39L AND 39R. REMOVED AND REPLACED (WITH NEW) FWD CARGO COMPT SHEAR TIE AT BS 742 BETWEEN STR 39L - 39R IAW SRM 51-40-02.Jul 2, 2006 · N598HA · Boeing 767300 · Fuselage Internal Mounting StructureSDR HALA0600617Floorbeam · damagedFOUND FLOORBEAM WORN AT NUTPLATE HOLES STA 654 LBL 22 - 53, WL 200. REMOVED DAMAGE ON UPPER CHORD OF FLOORBEAM STA 654, LBL 22-53 WL 200 PER B767-300 SRM 51-10-02. UPPER CHORD AFT FLANGE FOUND TO BE WITHIN LIMITS PER B767-300 SRM 53-00-51. UPPER CHORD FWD FJul 2, 2006 · N598HA · Boeing 767300 · Fuselage Main, Floor BeamSDR HALA0600616Floorbeam · damagedFLOORBEAM WORN AT NUTPLATE HOLES STA 1197 RBL 78 WL 200. BLENDED FWD FLANGE OF UPPER CHORD ON FLOOR AT STR 1197 RBL 78 PER B767-300, SRM STEP 5A, FOUND TO BE OUT OF LIMITS PER B767-300 SRM, 53-00-51 DETAIL 2 AND 3, CUT OUT DAMAGE PER B767-300 SRM 53-00-51 FIGJul 1, 2006 · N598HA · Boeing 767300 · Fuselage Main, Floor BeamSDR HALA0600615Floorbeam · damagedFLOORBEAM WORN AT NUTPLATE HOLES STA 1197 RBL 35 - 53. BLENDED DAMAGE AT NUTPLATE HOLES IAW SRM 51-40-02. BLENDED HOLE AT RBL 35 IN AN AREA OF .08" BY .09 BY .073". REMOVED .012", IN LIMITS, BLENDED HOLE AT RBL 40 IN AN AREA OF .95" BY .70" BY .077". REMOVJul 1, 2006 · N598HA · Boeing 767300 · Fuselage Main, Floor BeamSDR HALA0600614Failsafe · corrodedCORROSION FWD CARGO COMPT FRAME FAIL SAFE ANGLE CORRODED AT BS 654+44 BETWEEN STR 37L - 37R. REMOVED CORROSION ON FWD CARGO COMPT FRAME FAIL/SAFE ANGLE AT BS 654+44 BETWEEN STR 37L - 37R. FOUND TO BE WITHIN LIMITS, RESTORED ORIGINAL PER SRM 53-00-07, SRM 53-Jul 1, 2006 · N598HA · Boeing 767300 · Fuselage Main, FrameSDR HALA0600721Frame · corrodedAFT CARGO BAY, CORROSION ON FRAME, FWD FLANGE UPPER SURFACE, BS 1219, LBL 35. REMOVED NUTPLATES ON AFT CARGO BAY FRAME UPPER CHORD FWD FLANGE, BS1219,LBL35, IAW SRM 51-40-02-06-0. REMOVED CORROSION IN A 1.3 INCH X .90 INCH X .42 INCH AREA IAW SRM 51-10-02, OJun 30, 2006 · N598HA · Boeing 767300 · Fuselage Main, FrameSDR HALA0600663Floorbeam · corrodedCORROSION (CP53-252-011) CORROSION ON FLOORBEAM STA 1518 RBL 25 WL 200. REPAIRED FLOORBEAM CORROSION IN AREA OF FS 1518, RBL 25, WL 200 PER SRM 53-00-51/201. INSTALLED FLOORBEAM IAW SRM 51-40-02-06-0.Jun 30, 2006 · N598HA · Boeing 767300 · Fuselage Main, Floor BeamSDR HALA0600662Floor Support · crackedFWD CARGO COMPT FLOOR SUPPORT LOWER SURFACE ATTACH ANGLE CRACKED BS 478 LBL 47 WL 125. ATTACH ANGLE AT BS 478 LBL 47 WL 125 CRACKED 100 PERCENT ACROSS. MATERIAL OUT OF LIMITS IAW SRM 53-00-04-1A-1, NOTE (B), CRACKS NOT PERMITTED. FABRICATED NEW ATTACH ANGLEJun 30, 2006 · N598HA · Boeing 767300 · Fuselage Miscellaneous Structure
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