Boeing 737-282

Service difficulty reports · 303

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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 = '737282'
  ORDER BY difficulty_date DESC"

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SDR BJNA030211Floor Support · corrodedDURING A SCHEDULED MAINTENANCE VISIT, LEVEL 2 CORROSION WAS DISCOVERED ON A CABIN FLOOR SUPPORT ANGLE LOCATED AT BS 277 BL 10L WL 208.1. REMOVED THE CORRODED SECTION OF FLOOR SUPPORT, FABRICATED AND INSTALLED REPLACEMENT PARTS IAW BOEING 737 SRM 53-10-9 FIGURFeb 12, 2003 · N789TM · Boeing 737282 · Fuselage Miscellaneous StructureSDR BJNA030210Floor Support · corrodedDURING A SCHDULED MAINTENANCE VISIT, LEVEL 2 CORROSION WAS DISCOVERED ON AN AFT RIGHT CABIN FLOOR SUPPORT LOCATED AT FS 957. TIMCO REMOVED THE CORRODED SECTION OF FLOOR SUPPORT, FABRICATED AND INSTALLED REPLACEMENT FLOOR SUPPORT AND FILLER MADE FROM 7075-T6 .Feb 11, 2003 · N789TM · Boeing 737282 · Fuselage Miscellaneous StructureSDR BJNA03029Seat Track · corrodedDURING A SCHEDULED MAINTENANCE VISIT, LEVEL 2 CORROSION WAS DISCOVERED ON A PASSENGER CABIN SEAT TRACK LOCATED AT BS 360 LEFT OUTBOARD SIDE. REMOVED THE CORRODED SECTION OF SEAT TRACK AND REPLACED WITH A NEW SECTION MADE OUT OF BOEING EXTRUSION P/N BAC 1520-7Feb 11, 2003 · N789TM · Boeing 737282 · Fuselage, Seat/Cargo Attach FittingsSDR BJNA03028Seat Track · corrodedDURING A SCHEDULED MAINTENANCE VISIT, LEVEL 2 CORROSION WAS DISCOVERED ON THE SCALLOPS AND WELLS OF A PASSENGER CABIN SEAT TRACK LOCATED AT BS 344-360 LEFT INBOARD SIDE. REMOVED THE CORRODED SECTION OF SEAT TRACK AND REPLACED WITH A NEW SECTION MADE OUT OF BOFeb 11, 2003 · N789TM · Boeing 737282 · Fuselage, Seat/Cargo Attach FittingsSDR BJNA03027Floorbeam · corrodedDURING A SCHEDULED MAINTENANCE VISIT, LEVEL 2 CORROSION WAS DISCOVERED ON A FLOORBEAM LOCATED IN THE FORWARD CARGO COMPARTMENT AT FS 500 PLUS 40 INCH BL 12R, AREA OF CORROSION IS APPROXIMATELY 3 INCHES BY 1 INCH ON THE FRAME LOWER FORWARD FLANGE. REMOVED THE Feb 11, 2003 · N789TM · Boeing 737282 · Fuselage Main, Floor BeamSDR BJNA03026Floor Support · corrodedDURING A SCHEDULED MAINTENANCE VISIT, LEVEL 2 CORROSION WAS DISCOVERED ON A FLOOR SUPPORT LOCATED IN THE AFT PIT AT FS 1000 LBL 17. REMOVED THE SUPPORT FITTING, FABRICATED AND INSTALLED NEW REPAIR PART IAW BOEING 737-200 SRM 51-10-2, AND 51-30-2. (M)Feb 9, 2003 · N789TM · Boeing 737282 · Fuselage Miscellaneous StructureSDR BJNA03025Floor Support · corrodedDURING A SCHEDULED MAINTENANCE VISIT, LEVEL 2 CORROSION WAS DISCOVERED ON A FLOOR SUPPORT ANGLE LOCATED AT BS 285, BL 12L, WL 208.1. REMOVED CORRODED SECTION, FABRICATED AND INSTALLED A REPLACEMENT FLOOR SUPPORT ANGLE FROM BAC 1510-335 EXTRUSION. DIMENSION OFeb 6, 2003 · N789TM · Boeing 737282 · Fuselage Miscellaneous StructureSDR BJNA03024Support Bracket · corrodedDURING A SCHEDULED MAINTENANCE VISIT, LEVEL 2 CORROSION WAS DISCOVERED ON AN APU BLEED AIR SUPPORT BRACKET LOCATED IN THE AFT PIT ACCESSORY COMPARTMENT AT STA 1016. REMOVED AND REPLACED THE CORRODED SUPPORT BRACKET IAW SRM.Feb 5, 2003 · N789TM · Boeing 737282 · Fuselage Miscellaneous StructureSDR BJNA03021Panel · corrodedDURING A SCHEDULED MAINTENANCE VISIT, LEVEL 2 CORROSION, AND BROKEN RIVETS WERE DISCOVERED AROUND AIR CONDITIONING GROUND SERVICE PANEL AT FS 520 STRINGER 29L-28R. TIMCO REMOVED CORRODED SKIN SECTION, FABRICATED AND INSTALLED FILLER AND REPAIR DOUBELR OUT OF Feb 3, 2003 · N789TM · Boeing 737282 · Fuselage Main, Plate/SkinSDR BJNA03022Panel · corrodedDURING A SCHEDULED MAINTENANCE VISIT, LEVEL 2 CORROSION WAS DISCOVERED ON THE FORWARD RIGHT SIDE OF THE FUSELAGE TO WING FILLET PANEL NR 3479R, AFT SUPPORT. REMOVED AND REPLACED THE CORRODED TAPERED SHIMS IAW BOEING 737-200 SRM 51-10-1 PAGE 8. (M)Feb 3, 2003 · N789TM · Boeing 737282 · Fuselage Main, Plate/SkinSDR BJNA03023Skin · crackedDURING A SCHEDULED MAINTENANCE VISIT, A CRACK WAS DISCOVERED IN FUSELAGE SKIN OF THE FORWRAD ENTRY DOOR LOWER HINGE CUTOUT. CRACK EXTENDS FROM THE RADIUS OF THE HINGE CUTOUT FORWARD 1.9 INCHES, TERMINATING AT A FASTENER HOLE. CRACK IS SIMILAR TO THOSE SHOWN Feb 3, 2003 · N789TM · Boeing 737282 · Fuselage Main, Plate/SkinSDR BJNA021202Battery Pack · dischargedLT EXTERIOR EMERGENCY EXIT LIGHTS INOPERATIVE AT OVERWING EXIT. REPLACE LT EXTERIOR EMERGENCY BATTERY PACK POWER SUPPLY IN THE AFT CARGO PIT IAW MM.Dec 30, 2002 · N344TM · Boeing 737282 · Emergency LightingSDR BJNA021201Battery Pack · dischargedAFT EMERGENCY FLASH LIGHT BATTERY CONDITION INDICATOR NOT BLINKING. REPLACED BATTERY PACK, NORMAL MAINTENANCE. (M)Nov 29, 2002 · N233TM · Boeing 737282 · Emergency EquipmentSDR BJNA021016Power Supply · dischargedRIGHT OVER WING EXTERIOR EMERGENCY EXIT LIGHTS INOPERATIVE ON TEST. REPLACED POWER SUPPLY PER BMM 33-51-31. (M)Oct 30, 2002 · N789TM · Boeing 737282 · Emergency LightingSDR TSAA0253236Pressure Panel · damagedPERFORMED MODIFICATION TO THE WEB AND DOUBLER OF THE MAIN WHEEL WELL PRESSURE FLOOR TRANSVERSE BEAM BETWEEN BS 650 AND BS 727 AND BETWEEN RT AND LT BBL 45. FABRICATED WEB FILLER AND REPAIR DOUBLER IAW FIGURE 7. REPLACED ANGLE, CHANNEL AND DOUBLER WITH PARTS Oct 27, 2002 · N824AL · Boeing 737282 · Fuselage Main, BulkheadSDR TSAA0253235Beam · damagedOVERSIZED 4 HOLES IN THE RIGHT MLG LOWER BEAM CHORD FLANGE. FABRICATED FOUR FREEZE PLUGS. FABRICATED FOUR 1 INCH DIAMETER RETAINING WASHERS. INSTALLED FREEZE PLUGS AND OPENED ID HOLES TO THE EXISTING .1875 INCH DIAMETER PANEL ATTACH BOLTS. INSTALLED RETAINOct 27, 2002 · N824AL · Boeing 737282 · Wing, Landing Gear Attach FittingsSDR TSAA0253232Structure · crackedTRIMMED OUT THE DAMAGE OF THE HOLES TO A RECTANGULAR SHAPE. VERIFIED CRACK REMOVED USING HFEC. FABRICATED CIRCULAR DOUBLERS FOR EACH HOLE. REPAIR COMPLETED IAW ECO 3302. AIRCRAFT RETURNED TO SERVICE. (M)Oct 27, 2002 · N824AL · Boeing 737282 · Fuselage Miscellaneous StructureSDR TSAA0253231Fitting · damagedREMOVED DAMAGE FROM THE NR 2 AND NR 7 FLAP TRACK ATTACHMENT FITTING HOLE. FABRICATED A 'NEW' REPLACEMENT TUBE AND BUSHING INCREASING THE OUTSIDE DIAMETER .0015 TO .0020 INCH INTERFERENCE FIT ON THE FINISHED DIAMETER OF THE HOLE. INSTALLED NEW TUBE AND BUSHINOct 27, 2002 · N824AL · Boeing 737282 · Trailing Edge FlapsSDR BJNA021010Floorbeam · corrodedCORROSION ADJACENT TO WATER DRAIN LINE FORWARD UNDER SIDE OF R2 DOOR SCUFF PLATE AREA BS 958 RBL 53. REMOVED CORROSION FROM LOWER OUTBOARD FLOORBEAM SUPPORT, CORROSION WENT OUT OF LIMITS. FABRICATED REPAIR DOUBLER AND INSTALLED IAW B737 SRM 51-40-3, 51-10-2,Oct 23, 2002 · N233TM · Boeing 737282 · Fuselage Main, Floor BeamSDR BJNA021005Floorbeam · corrodedDURING A SCHEDULED C-CHECK INSPECTION DISCOVERED LEVEL 2 CORROSION ADJACENT TO WATER DRAIN LINE FORWARD UNDER SIDE OF R2 DOOR SCUFF PLATE AREA BS 958 RBL 53. REMOVED CORROSION FROM LOWER OUTBOARD FLOORBEAM SUPPORT, CORROSION WENT OUT OF LIMITS. FABRICATED REOct 23, 2002 · N233TM · Boeing 737282 · Fuselage Main, Floor BeamSDR BJNA021017Floor Support · corrodedDURING SCHEDULED C-CHECK INSPECTION DISCOVERED, L1 DOOR AFT GIRTH BAR ATTACH FITTING AND OUTBOARD FLOORBOARD SUPPORT AT BS 346 LBL 60 CORRODED. FOUND GIRTH BAR FITTING AND FLOORBOARD SUPPORT CORRODED OUT OF LIMITS FORMED REPAIR FLOORBOARD SUPPORT AND GIRTH BAOct 20, 2002 · N233TM · Boeing 737282 · Fuselage Miscellaneous StructureSDR BJNA021009Floor Support · corrodedDURING SCHEDULED C-CHECK INSPECTION DISCOVERED FLOOR SUPPORT BETWEEN FRAME 947-967 RIGHT APPROX BL40R HAS FLAKING CORROSION. FLOOR SUPPORT CORRODED OUT OF LIMITS. FABRICATED REPLACEMENT SUPPORT AND INSTALLED IAW B737 SRM 53-10-1, 51-10-2 AND 51-30-2. (M)Oct 19, 2002 · N233TM · Boeing 737282 · Fuselage Miscellaneous StructureSDR BJNA021004Stringer · corrodedDURING A SCHEDULED C-CHECK INSPECTION OF THE AFT CARGO COMPARTMENT BILGE AREA, DISCOVERED LEVEL 2 CORROSION. ON THE FORWARD END OF STRINGERS 25L AT STATION 967. CUT OUT DAMAGED SECTION, IAW BOEING SRM 53-10-3 FIGURE 1. FABRICATED AND INSTALLED STRINGER REPAOct 19, 2002 · N233TM · Boeing 737282 · Fuselage Main, Longeron/StringerSDR BJNA021002Floor Support · corrodedDURING A SCHEDULED C-CHECK INSPECTION, DISCOVERED AFT FUSELAGE FLOOR SUPPORT FRAME AT STATION 951 FROM LBL 20 TO LBL 36 HAS LEVEL 2 CORROSION. REMOVED FLOOR SUPPORT FRAME, FABRICATED AND INSTALLED FRAME REPAIR IAW BOEING SRM 53-10-2 AND 51-30-2. (M)Oct 19, 2002 · N233TM · Boeing 737282 · Fuselage Miscellaneous StructureSDR BJNA021003Stringer · corrodedDURING A SCHEDULED C-CHECK INSPECTION OF THE FORWARD CARGO COMPARTMENT, DISCOVERED A TWO INCH SPOT OF LEVEL 2 CORROSION ON STRINGER 27L AT STATION 389. FABRICATED AND INSTALLED STRINGER REPAIR IAW BOEING 737 SRM 51-10-2, 51-10-6, 51-30-2, 53-10-01 FIGURE 1 ANOct 19, 2002 · N233TM · Boeing 737282 · Fuselage Main, Longeron/StringerSDR TSAA0253234Structure · corrodedBLENDED THE DAMAGE ON THE LUG. SPOTFACED THE INBOARD AND OUTBOARD SURFACES. OVERSIZED THE TAPERED/ELONGATED HOLE OF THE INBOARD LUG ON THE ORIGINAL CENTERLINE TO OBTAIN A ROUND AND TRUE CONDITION. FABRICATED NEW REPAIR SLEEVE BUSHING TO FIT THE OVERSIZED INOct 18, 2002 · N824AL · Boeing 737282 · Horizontal Stabilizer Miscellaneous StructureSDR TSAA0253233Structure · crackedTRIM OUT ALL THREE HOLES IN THE DAMAGED ZONE. HFEC THE EDGE OF THE TRIM. FABRICATED A DOUBLER AND A TRIPLER. INSTALLED DOUBLER AND TRIPLER. REPAIR COMPLETED IAW ECO 3250, FIGURE 24. AIRCRAFT RETURNED TO SERVICE. (M)Oct 18, 2002 · N824AL · Boeing 737282 · Fuselage Miscellaneous StructureSDR BJNA021007Floorbeam · corrodedDURING SCHEDULED C-CHECK INSPECTION DISCOVERED FORWARD LAVATORY FLOOR STATION 294.5 WL 208 LBL 12 FLOORBEAM HAS 12 INCHES OF CORROSION. FLOORBEAM CORRODED MORE THAN 50 PERCENT, OUT OF LIMITS. REMOVED CORRODED FLOORBEAM UPPER T-CAP AND SPLICE. FABRICATED REPOct 18, 2002 · N233TM · Boeing 737282 · Fuselage Main, Floor BeamSDR BJNA021008Angle · crackedLEFT CENTER HORIZONTAL STABILIZER REAR STABILIZER FITTING HAS CRACKED ANGLE STATION 1170, BELOW LEFT HORIZONTAL STABILIZER PIN/AFT. REMOVED CRACKED ANGLE IAW B737 SRM 51-30-2. TRIMMED TO FIT NEW SUPPORT ANGLE IAW B737 SRM 51-30-5, 51-10-1, 51-20-1 FIG 1/2. Oct 15, 2002 · N233TM · Boeing 737282 · Horizontal Stabilizer Miscellaneous StructureSDR BJNA021101Skin · delaminatedDURING SCHEDULED C-CHECK INSPECTION DISCOVERED RIGHT WING INBOARD AFT FLAP LOWER SKIN DELAMINATED AT T/E SECTION. CUT OUT DELAMINATED AREA .5 INCH BY 1 INCH. FABRICATED AND INSTALLED SKIN SECTION AND DOUBLER. BONDED AND APPLIED FIBERGLASS REPAIR IAW B737 SROct 10, 2002 · N233TM · Boeing 737282 · Trailing Edge FlapsSDR BJNA021014Skin · gougedRIGHT WING OUTBOARD FLAP, LOWER FORE FLAP LEADING EDGE SKIN GOUGED, FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR DOUBLER IAW B737 SRM 57-50-4 FIG 2, 51-10-2 AND 51-30-8. (M)Oct 10, 2002 · N233TM · Boeing 737282 · Trailing Edge FlapsSDR BJNA021013Stringer Clip · corrodedAFT FUSELAGE FLOORBEAM STATION 967 LEFT SIDE WHERE MEETS CIRCUMFERENTIAL FRAME HAS CORRODED STRINGER TIE. REMOVED STRINGER TIE CLIP, FABRICATED AND INSTALLED REPAIR CLIP IAW B737 SRM 51-10-2, 51-30-2 AND 51-20-1. (M)Oct 10, 2002 · N233TM · Boeing 737282 · Fuselage Miscellaneous StructureSDR BJNA021011Intercostal · corrodedNOSE WHEEL WELL LEFT SIDE AT AFT ACCESS PANEL SUPPORT BEAMS, THREE EACH HAS EXFOLIATED CORROSION FS 280. REMOVED AND REPLACED TWO EXFOLIATED INTERCOSTALS IAW B737 SRM 51-30-2, 51-20-1, B737 MM 51-21-0. REMOVED CORROSION FROM THIRD VERICAL BEAM FOUND TO BE WIOct 10, 2002 · N233TM · Boeing 737282 · Fuselage Miscellaneous StructureSDR BJNA021015Skin · crackedLEFT WING NR 2 SLAT TRAILING EDGE CHAFED AND CRACKED AT OUTBOARD AUX SLAT TRACK. REPAIRED CRACKED AND CHAFED LEFT WING NR 2 SLAT TRAILING EDGE AT OUTBOARD AUX SLAT TRACK BY CUTTING OUT DAMAGED SECTION, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW B7Oct 9, 2002 · N233TM · Boeing 737282 · Leading Edge DevicesSDR BJNA021012Floorbeam · corrodedFLOORBEAM BS 976, LBL 53 HAS EXFOLIATED CORROSION. REMOVED FLOORBEAM, FABRICATED AND INSTALLED FLOORBEAM REPAIR 55 INCHES BY 1.5 INCHES BAC1505-100617, IAW TIMCO REO-L00597 REV A. (M)Oct 9, 2002 · N233TM · Boeing 737282 · Fuselage Main, Floor BeamSDR BJNA021006Stringer · corrodedDURING SCHEDULED C-CHECK INSPECTION DISCOVERED AFT LOWER BILGE STATION 1006, STRINGER 23L, CLIP CORRODED. REMOVED CLIP AND S23L IN THE AFT LOWER BILGE BS 1006. FORMED REPAIR STRINGER AND CLIP AND INSTALLED IAW B737 SRM 53-10-3 AND 51-10-2. (M)Oct 9, 2002 · N233TM · Boeing 737282 · Fuselage Main, Longeron/StringerSDR BJNA021001Case · damagedON TAKEOFF ROLL AT 115 KNOTS AIRCRAFT VEERED TO THE LT, CAPTAIN REPORTED HEARING A LOUD BANG. ABORTED TAKEOFF. MAINTENANCE REPORTED MAJOR DAMAGE TO TURBINE SECTION OF ENGINE. UPON FURTHER INSPECTION REVEALED THAT ALL DAMAGE WAS TOTALLY CONTAINED TO THE ENGIOct 9, 2002 · N344TM · Boeing 737282 · Turbine Engine Compressor SectionSDR BJNA020832Spar · corrodedFOUND LT HORIZONTAL STAB CENTER SECTION REAR SPAR TOP CHORD FORWARD LUG HAS LEVEL 2 CORROSION INSIDE BORE. REMOVED CORROSION BORED I/D OF LUG TO 1.564 INCH, ROTO TREATED AND INSTALLED BUSHING. (M)Aug 27, 2002 · N344TM · Boeing 737282 · Horizontal Stabilizer, Spar/RibSDR BJNA020828Frame · corrodedFOUND LEVEL 2 CORROSION UNDER 3 EACH SCREW HOLES AT FRAME RBL 28 BETWEEN BS 955 TO BS 967. REMOVED FRAME ORDERED AND RECEIVED NEW FRAME (BEAM) DRILLED, DEBBARRD, TREATED PRIMED AND INSTALLED IAW B737-200 SRM 51-10-6 PAGE 12, 51-30-2 PAGE 3, AND B737 MM 51-21-Aug 16, 2002 · N344TM · Boeing 737282 · Fuselage Main, FrameSDR BJNA020827Beam · corrodedFOUND LEVEL 2 CORROSION 4 EACH PLACES ON UPPER SURFACE OF BEAM 294.5 BETWEEN LBL 10 TO RBL 20. REMOVED CORROSION AND TREAT. REPAINT SURFACE CHECK LIMITS. (M)Aug 15, 2002 · N344TM · Boeing 737282 · Fuselage Main, StructureSDR BJNA020824Frame · corrodedFOUND FRAME AT STATION 328 HAS SURFACE CORROSION AROUND FASTENER HOLES ON UNDER SIDE OF FRAME. LEVEL 2 CORROSION. REMOVED CORROSION AT 328 FABRICATED REPAIR ANGLES IAW B737 SRM 53-10-9 PAGE 26. (M)Aug 15, 2002 · N344TM · Boeing 737282 · Fuselage Main, FrameSDR BJNA020818Panel · corrodedFOUND CORROSION IN FORWARD PIT LEFT SIDE TRANSITION PANEL FROM STATION 500B TO 520, LEVEL 2 CORROSION. REMOVED OLD TRANSITION PANEL, FABRICATED NEW SECTION OF PANEL, INSTALLED NEW SECTION OF TRANSITION PANEL LEFT STATION 500B TO 520 IAW B737 SRM 51-402 FIGUREAug 14, 2002 · N344TM · Boeing 737282 · Fuselage Main, Plate/SkinSDR BJNA020833Skin · corrodedFORWARD FRAME OF THE C-2 DOOR CUT OUT ABOVE TRANSITION PANEL HAS LEVEL 2 CORROSION. REMOVED CORRODED FRAME IAW 737 SRM 51-30-2 AND REO L00 588. REPAIRED FRAME IAW REO L00 588 REV IR. FABRICATED FRAME SPLICES AND INSTALLED IAW REO L00588 AND B737 SRM 51-20-1Aug 12, 2002 · N344TM · Boeing 737282 · Fuselage Main, Plate/SkinSDR BJNA020831Frame · corrodedFOUND LEVEL 2 CORROSION FORWARD PIT STATION 500 RBL 12 FRAME LOWER LEG. CORROSION REMOVED AND FOUND REMAINING MATERIAL OUT OF LIMITS, FABRICATED, TRIMMED DRILLED, ALODINED PRIMED AND INSTALLED REPAIR IAW B737 SRM 51-10-6, 53-10-1, 53-10-4 FIGURE 6 PAGE 13-15.Aug 10, 2002 · N344TM · Boeing 737282 · Fuselage Main, FrameSDR BJNA020813Door Frame · gougedFOUND RIGHT SIDE FORWARD EDGE OF AFT CARGO DOOR OPENING IS GOUGED AND TORN. CUT OUT DAMAGED AREA AND FABRICATED STACKED DOUBLER REPAIR PER B737 SRM 53-30-3 FIG 46. INSTALLED REPAIR PER B737 SRM 31-30-2, 51-20-4, 53-30-3 FIG 46. (M)Aug 9, 2002 · N344TM · Boeing 737282 · Fuselage Main, StructureSDR BJNA020810Seat Track · corrodedSURFACE CORROSION ON SEAT TRACK AT RBL 32 AT BS 328, LEVEL 2 CORROSION. FOUND CORROSION ON SEAT TRACK OUT OF LIMITS, CUT NEW TRACK FROM BAC1520-792 16 INCH INSTALLED IAW 727 SRM 51-10-2, 51-10-1 AND 51-30-2. (M)Aug 8, 2002 · N344TM · Boeing 737282 · Fuselage, Seat/Cargo Attach FittingsSDR BJNA020825Stringer · corrodedAFT AIRCRAFT INSIDE RIGHT SIDE STRINGER 17 AT FS 986.5 UNDER CUSP LONGERON HAS LEVEL 2 CORROSION. REMOVED CORROSIN FABRICATED AND INSTALLED NEW CUSP WEB IAW B737 SRM 51-20-1, 53-10-2, FIGURE 5, 53-10-1 FIGURE 1 AND 51-10-6. (M)Aug 7, 2002 · N344TM · Boeing 737282 · Fuselage Main, Longeron/StringerSDR BJNA020812Tie Clip · crackedFOUND TENSION TIE FITTING AT STA 104 STR 19L AND 20L CRACKED ON CORNER. LEVEL 2 CORROSION. REMOVED SECTION OF STATION 19L AT FS 104 FABRICATED REPAIR SECTION OF STATION AND TIE CLIP AT 19L AND 1104 TREATED, PRIMED AND INSTALLED STRINGER, SPLICES SECTION AND Aug 6, 2002 · N344TM · Boeing 737282 · Fuselage Miscellaneous StructureSDR BJNA020811Shear Tie · corrodedFOUND CORROSION IN FORWARD PIT AT STA 500 LBL 2 TO RBL 2 FRAME LOWER LEG, LEVEL 2 CORROSION. CUT AND REMOVED CORROSION FROM SHEAR TIE LEG. FABRICATED AND INSTALLED SHEAR TIE REPAIR AND DOUBLER IAW SRM.Aug 6, 2002 · N344TM · Boeing 737282 · Fuselage Main, StructureSDR BJNA020820Floor Support · corrodedFORWARD PIT FLOOR SUPPORT BS 520 LBL 17 TO LBL 20 LEVEL 2 CORROSION AROUND 4 EACH NUT CLIPS AND 1 MISSING. REMOVED CORROSION FABRICATED AND INSTALLED FLOOR SUPPORT REPAIR IAW 737 SRM 51-10-2, 51-30-2, 51-40-4, FIGURE 1 AND 53-10-1. (M)Aug 6, 2002 · N344TM · Boeing 737282 · Fuselage Miscellaneous Structure
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