Boeing 727-233

Service difficulty reports · 3,034

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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 = '727233'
  ORDER BY difficulty_date DESC"

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SDR FDEA201007072397Shear Tie · corrodedCORROSION ON SHEAR TIE AT BS 970 BETWEEN STRINGERS 30 AND 29R. CUT OUT DAMAGED AREA OF SHEAR TIE AT BS 970 STR 29-30R IAW SRM 53-10-4 FIG 12 DIM 4 1/2" X 3" FABRICATED REPAIR PARTS USING 7075 O .071" DIM 10 1/4" X 7 1/4" 7075T6 .063" DIM 4 1/2" X 2 3/8" AJul 7, 2010 · N265FE · Boeing 727233 · Fuselage Internal Mounting StructureSDR FDEA201007062380Stringer · corrodedCORROSION - STRINGER 27L, STATION 740 INSIDE CHANNEL. CUT OUT STRINGER 27L AT BS 740, 8 5/8" LONG AND 2 STRINGER TIES ANGLES IAW SRM REV 103 53-10-3 FIG 1 51-30-2. FABRICATED STRINGER SECTION FROM BAC1498-147, 7075T6, 8 5/8" LONG SPLICE FROM BAC1498-131 707Jul 6, 2010 · N265FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR FDEA201007062372Rib · crackedNR 6 SLAT I/B & O/B ACTUATOR ATTACH RIBS CRACKED. REMOVED I/B AND O/B RIBS TO NR 6 SLAT IAW SRM 51-30-2 FABRICATED, LOCATED AND DRILLED NEW I/B AND O/B RIBS, 2024 0 MATERIAL PO 29126300 DIM 16 1/2" X 6" IAW SRM 57-50-2 FIG 2 INSTALLED NEW RIBS 2 EACH IAW SJul 6, 2010 · N266FE · Boeing 727233 · Wing, Rib/BulkheadSDR FDEA201007062371Skin · corrodedCORROSION - UPPER SKIN, EXTERIOR SURFACE OF WING CTR SECTION FUEL TANK. APPROX BS 825, RBL 12. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 51-10-6 AND 57-30-1 FIG 4. REPAIRED AREA IAW EA 7-5730-142035.Jul 6, 2010 · N265FE · Boeing 727233 · Wing, Plate/SkinSDR FDEA201007052391Web · crackedAFT STAIR AREA, RIGHT LOWER TORQUE BOX WEB CRACKED AT LIGHTING HOLE BS 1223. CUTOUT DAMAGED AREA, DIMENSION 1/4" AFT AIRSTAIR AREA RT BS 1223 IAW SRM 51-40- 2 FIG 1, FABRICATED 2 EA. REPAIR PLATES FROM 2024T3 .040, DIM: 5 1/8" X 1 3/4" IAW SRM 51-40-2 FIG 1Jul 5, 2010 · N265FE · Boeing 727233 · Fuselage Main, StructureSDR FDEA201007052390Web · crackedAFT STAIR AREA, RIGHT LOWER TORQUE BOX WEB CRACKED 2 EA AT LIGHTING HOLE BS 1236. CUTOUT DAMAGED AREA DIM: 1/4" AT AFT AIRSTAIR AREA RH BS 1236 IAW SRM 51-40-2 FIG 1. FABRICATED 2 EA. REPAIR PLATES FROM 2024T3 .040 DIMENSION 4 1/2" X 1 5/8" IAW SRM 51-40-2 FIJul 5, 2010 · N265FE · Boeing 727233 · Fuselage Main, StructureSDR FDEA201007052369Skin · bulgedBULGE EXTERIOR FUSELAGE BS 660 BETWEEN STR 28L TO 28R. CUT OUT DAMAGED AREA 3" X 1.375" AND 1.75" X 1.5" IAW SRM 53-30-3. FABRICATED DOUBLER FROM 2024T3 .080" DIM. 17.50" X 10.50" IAW SRM 53-30-3 AND 53-30-2. INSTALLED REPAIR PARTS IAW SRM 53-30-3 AND 51-30-Jul 5, 2010 · N266FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA201007032343Stringer · corrodedCORROSION ON STRINGER 29L FROM BS 950F TO 970. REMOVED CORROSION ON STR 29L FROM 950F TO 970 IAW SRM 51-10-6. CW UT. THICKNESS IAW NDTM 51-00-00 PT 4 FIG 2, ORIGINAL AREA .140, REMAINING .111. EVALUATED AREA FOUND TO BE WITHIN LIMITS IAW EA 7-5330-135567. TRJul 3, 2010 · N265FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR FDEA201006302310Attach Bracket · crackedNR 8 SLAT ACTUATOR IB & OB ATTACH BRACKETS INSIDE PLATES ARE CRACKED. REMOVED I/B AND O/B BRACKETS IAW SRM 51-30-2. FABRICATED BRACKETS FROM 7075-0 .063" DIM. 9" X 4.80 " (2 EA) AND I/B PLATE FROM 7075T6 .125" DIM. 3.8" X 7.5" IAW DWG. 65-17255. HEAT TREATED BJun 30, 2010 · N266FE · Boeing 727233 · Leading Edge DevicesSDR FDEA201006302309Attach Bracket · crackedNR 8 SLAT ACT. IB & OB ATTACH BRACKETS INSIDE PLATES ARE CRACKED. REMOVED I/B AND O/B BRACKETS FROM NR 8 SLAT IAW SRM 51-30-2. FABRICATED I/B AND O/B BRACKETS FROM 7075-0 .063" DIM. 9" X 4.80 " (2 EA) AND I/B PLATE FROM 7075T6 .125" DIM. 3.8" X 7.5" IAW DWG. 6Jun 30, 2010 · N266FE · Boeing 727233 · Leading Edge DevicesSDR FDEA201006302272Skin · dentedDENT EXTERIOR FUSELAGE BS 1060 STR 20L. CUT OUT DAMAGED AREA DIM. 3.375" X 2.625" IAW SRM 53-30-3. FABRICATED DOUBLER FROM 2024T3 .071" DIM. 13.25" X 9.25" AND FILLER FROM 2024T3 .063" DIM. 14.75" X 6.5" IAW SRM 53-30-3. INSTALLED REPAIR PARTS IAW SRM 53-30-3.Jun 30, 2010 · N266FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA201006282269Web · crackedAFT AIRSTAIR AREA - RT LOWER TORQUE BOX WEB LIGHTNING HOLE IS CRACKED AT BS 1223. TRIMMED OUT DAMAGED AREA DIM. .5" X .25" IAW SRM 51-10-1, FABRICATED REPAIR WEB DOUBLER FROM 2024T3 .040" DIM. 4" X 2.625" IAW SRM 51-40-2 AND INSTALLED DOUBLER IAW SRM 51-30-2Jun 28, 2010 · N266FE · Boeing 727233 · Fuselage Main, StructureSDR FDEA201006282271Web · crackedAFT AIRSTAIR AREA - RT LOWER TORQUE BOX WEB LIGHTNING HOLE IS CRACKED AT BS 1243 TRIMMED OUT DAMAGED AREAS DIM. .375" X .5" AND .5" X .75" IAW SRM 51-10-1, FABRICATED WEB REPAIR DOUBLER FROM 2024T3 .040" DIM 2.375" X 6.625" IAW SRM 51- 40-2, FIG 1 AND INSTAJun 28, 2010 · N266FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR FDEA201006282270Web · crackedAFT AIRSTAIR AREA - RT LOWER TORQUE BOX WEB LIGHTNING HOLE IS CRACKED AT BS 1225 TRIMMED OUT DAMAGED AREA DIM. .5" X .375" IAW SRM 51-10-1, FABRICATED WEB REPAIR DOUBLER FROM 2024T3 .040" DIM. 4" X 2.25" IAW SRM 51-40-2, FIG 1 AND INSTALLED WEB REPAIR DOUBLER Jun 28, 2010 · N266FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR FDEA201006262202Web · crackedAFT AIRSTAIR AREA - RT LOWER TORQUE BOX LIGHTNING HOLE IS CRACKED AT BS 1230 REMOVED DAMAGED AREA IAW SRM 51-40-2 AND 51-10-1, REV 103. FABRICATED DOUBLER IAW SRM 51-40-2 FIG 1 AND 53-10-2. INSTALLED DOUBLER IAW SRM 51-30-2.Jun 26, 2010 · N266FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR FDEA201006252194Bulkhead · crackedAFT PIT CRACK IN BS 1183 BULKHEAD AT APPROX. RBL 24 & WL 167. CUT OUT WEB AROUND THE CRACK APPROX. 2.875" X 1.875" IAW EA 7-5310-135559. FABRICATED FILLER FROM 2024T3 .050" DIM. 2.75" X 1.75", DOUBLER FROM 2024T3 .071" DIM. 7.125" X 6", 3 EACH FILLERS FROM Jun 25, 2010 · N266FE · Boeing 727233 · Fuselage Main, BulkheadSDR FDEA201006252193Doubler · gougedGOUGE ON MCD INNER DOUBLER STA. 560 S4L. REMOVED MCD INNER SKIN UPPER CENTER PANEL IAW SRM 51-30-2. FABRICATED NEW MCD INNER SKIN UPPER CENTER PANEL FROM 2024T3 .090" DIM. 88" X 34" IAW SRM 53-10-2 FIGURE 3A. INSTALLED NEW MCD INNER SKIN UPPER CENTER PANEL IAWJun 25, 2010 · N266FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA201006252145Skin · damagedL-1 DOOR RAIN GUTTER INSTALLED WITH BLIND FASTENERS THROUGH FUSELAGE SKIN WITH NO E.D. WITH SOLID FASTENERS. DRILLED DAMAGED AREAS (3 EACH) TO MINIMUM DIAMETER IAW SRM 51-30-2 AND EA 7-5330-135558. FABRICATED REPAIR DOUBLER FROM 2024T3 .090" DIM. 33" X 22.25",Jun 25, 2010 · N266FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA201006242135Skin · crackedFORWARD GALLEY DOOR CUTOUT, CRACKED ON LOWER AFT CORNER. CUT OUT DAMAGED AREA OF SKIN APPROX. 2.5" X 1" IAW FEDEX EO 7-5313-7-2304 PT2. FABRICATED REPAIR FILLER FROM 2024T3 .080" DIM. 2.5" X 1" AND DOUBLER FROM 2024T3 .080" DIM. 26.125" X 20.125" IAW EO 7-Jun 24, 2010 · N266FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA201006242144Skin · gougedGOUGE ON MCD INNER DOUBLER STA. 640 STR. 5L. REMOVED INNER SKIN AFT UPPER PANEL IAW SRM 51-30-2. FABRICATED NEW INNER SKIN FROM 2024T3 .125" DIM. 48" X 79" IAW SRM 53-10-2 FIGURE 3A. INSTALLED INNER SKIN IAW SRM 51-30-2Jun 24, 2010 · N266FE · Boeing 727233 · Cargo/Baggage DoorsSDR FDEA201006232143Skin · gougedGOUGE ON MCD INNER DOUBLER STA. 480 STR. 4L. REMOVED FORWARD UPPER INNER SKIN IAW SRM 51-30-2. FABRICATED NEW INNER SKIN FROM 2024T3 .125" DIM. 48" X 79" IAW SRM 53-10-2 FIGURE 3A. INSTALLED FORWARD UPPER INNER SKIN IAW SRM 51-30-2.Jun 23, 2010 · N266FE · Boeing 727233 · Cargo/Baggage DoorsSDR FDEA201006232123Doubler · gougedGOUGES ON MCD INNER DOUBLER STATION 620, STRINGER 9L. REMOVED INNER SKIN DOUBLER "SPLICE" IAW SRM 51-30-2. FABRICATED NEW INNER SKIN DOUBLER "SPLICE" FROM 2024T3 .125" DIM. 11" X 22" IAW SRM 53-10-2 FIGURE 3A. INSTALLED INNER SKIN DOUBLER "SPLICE" IAW SRM Jun 23, 2010 · N266FE · Boeing 727233 · Cargo/Baggage DoorsSDR FDEA201006232276Doubler · gougedGOUGE ON MCD INNER DOUBLER STA 640, STR 11L. CUT OUT DAMAGED AREA DIM. 28" X 22 IAW EA 7-5330-135557. FABRICATED NEW WEB FROM 2024T3 .125" DIM. 28" X 22" AND SPLICE STRAP FROM 2024T3 .125" DIM. 22" X 4" IAW EA 7-5330-135557. INSTALLED REPAIR PARTS IAW FEDEXJun 23, 2010 · N266FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA201006232275Skin · gougedGOUGE ON MCD INNER DOUBLER STA 620 STR 16L CUT OUT DAMAGED AREA DIM. 2" X 1" IAW EA 7-5330-135557. FABRICATED FILLER FROM 2024T3 .125" DIM. 2" X 1" AND DOUBLER FROM 2024T3 .125" DIM. 6" X 3" IAW EA 7-5330-135557. INSTALLED REPAIR PARTS IAW IAW EA 7-5330-13555Jun 23, 2010 · N266FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA201006232116Engine · stalledNR 2 ENGINE COMPRESSOR STALL/SURGE AT LEVEL OFF - FL340 EPR WAS OBSERVED TO GO DOWN TO 1.6 EPR WITH ENGINE VIBRATION NOISE ASSOCIATED WITH COMPRESSOR STALL. AIRTURN BACK. R & R NR 2 ENGINE AS PER WORK CARD 70T0002 AND TESTED PER WORK CARD 70T0301-02. ALLJun 23, 2010 · N220FE · Boeing 727233 · Engine (Turbine/Turboprop)SDR FDEA201006192073Battery Pack · inoperativeEMERGENCY EXIT LIGHT ON BOTH DOORS INOP. REPLACED EMERGENCY EXIT LIGHT BATTERIES. OPS CHECK GOOD FOR SERVICE AT THIS TIME. FINAL CLOSED.Jun 19, 2010 · N278FE · Boeing 727233 · Emergency LightingSDR FDEA201006152020Stringer · corrodedCORROSION IN CHANNEL -STRINGER 27L, STA 950 - 950C. CUT OUT SECTION OF STRINGER 27L FROM BS 950A PLUS 10" TO 950C PLUS 10", 38 3/4" IN LENGTH, IAW SRM, REV 103, 51-10-1 AND 53-10-3 FIG 1. FABRICATED (2) STRINGER SECTIONS USING BAC1498-147, 7075-T6, 19" LOJun 15, 2010 · N267FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR FDEA201006152014Fire Warning · false activationON CLIMBOUT, GLARESHIELD FIRE WARNING LIGHTS ILLUMINATED DIMLY, FOLLOWED A MINUTE LATER BY AN APU FIRE WARNING LIGHT. FIRE WARNING LIGHTS STAYED ON APPROX 15-20 SECONDS. APU FIRE WARNING REMAINED ON UNTIL IN CHOCKS. PULLED APU FIRE HANDLE, DISCHARGED APU FIRJun 15, 2010 · N284FE · Boeing 727233 · Smoke DetectionSDR FDEA201006142002Rib · gougedUPON REMOVAL OF NO. 7 SLAT, FOUND OB END CAP RIB CHAFFED AND GOUGED, EXTERIOR SURFACE. REMOVED DAMAGE OB RIB AND FABRICATED NEW RIB FROM 2024O .040 HEATED TREATED TO T4 CONDITION IAW FAS ENGINEERING REPORT 2-37153-801 REV A APPROX DIM: 15 3/4" X 7" & INJun 14, 2010 · N267FE · Boeing 727233 · Leading Edge DevicesSDR FDEA201006142000Rib · gougedUPON REMOVAL OF NR 7 SLAT FOUND IB END CAP RIB CHAFED AND GOUGED, EXTERIOR SURFACE REMOVED DAMAGED IB RIB, FABRICATED NEW RIB FROM 2024O .040 APPROX DIM: 15 3/4" X 7" HEATED TREATED TO T4 CONDITION IAW FAS ENGINEERING REPORT 2-37153-801 REV A & INSTALLED Jun 14, 2010 · N267FE · Boeing 727233 · Leading Edge DevicesSDR FDEA201006121972Skin · damagedUPON REMOVAL OF BLIND FASTENER AT BS 950E, AT STRINGER 26L TO 25L, FOUND DOUBLE DRILLED HOLE. CUT OUT DAMAGED AREA OF SKIN, DIMENSIONS 4" X 4" IAW SRM 53-30-3 FIG 5 AND 51-10-1. FABRICATED STRUCTURAL FILLER USING 2024 T3 .080", PO NR 9009585, DIMENSIONSJun 12, 2010 · N267FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA201006101937Web · crackedAFT AIRSTAIRS RT LOWER TORQUE BOX WEB AT BS 1243 HAS UPPER LIGHTNING HOLE CRACKED. CUTOUT DAMAGED AREA APPROX DIM: 5/8" X 3/8", FABRICATED REPAIR DOUBLER FROM 7075T6 .032 APPROX DIM: 4" X 1 1/4" & INSTALLED REPAIR DOUBLER AT BS 1243 RH LOWER TORQUE WEB IJun 10, 2010 · N267FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR FDEA201006101936Web · crackedAFT AIRSTAIR RT LOWER TORQUE BOX WEB AT BS 1243 HAS LOWER LIGHTNING HOLE CRACKED. CUTOUT DAMAGED AREA APPROX DIM: 5/8" X 3/8", FABRICATED REPAIR DOUBLER FROM 7075T6 .032 APPROX DIM: 4" X 1 1/4" & INSTALLED REPAIR DOUBLER AT BS 1243 RH AFT AIRSTAIR TORQUE BOXJun 10, 2010 · N267FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR FDEA201006101946Shear Tie · crackedCRACKED SHEAR TIE - STA 950E AT STR 26L. REMOVED SHEAR TIE 26L IAW SRM, REV 103, 51-30-2. FABRICATED SHEAR TIE USING BAC1505-100261 7075-T6511, 7 3/8" LONG IAW DWG 65-56123 REV A. INSTALLED SHEAR TIE IAW DWG 65-56123 REV A AND SRM 51-30- 2.Jun 10, 2010 · N267FE · Boeing 727233 · Fuselage Internal Mounting StructureSDR FDEA201006091908Stringer · crackedRT WING, WS 629 STR 9 HAS A CRACK. STOP DRILLED CRACK DIM: .0187" IAW EO 7-5710-7-4322 PART 1. FABRICATED REPAIR ANGLES FROM AND10134-2001 7075T6 DIM: 10.6" X 2" AND 3.4" X 2" AND FABRICATED 2 EA. RADIUS FILLER FROM AND 10137-3004 DIM: 3" X 1" IAW EO 7-5710Jun 9, 2010 · N267FE · Boeing 727233 · Wing, Longeron/StringerSDR FDEA201006091917Skin · corrodedCORROSION IN SKIN BS 600, STR 28L. CUTOUT DAMAGED AREA APPROX DIM: 2.5" X 1" AND FABRICATED REPAIR DOUBLER FROM 2024T3 .100 APPROX DIM: 8 3/4" X 12 5/8". INSTALLED REPAIR DOUBLE AT BS 600 STR 28L IAW SRM 53-30-3 FIG 1, SRM 51-30-2, SRM 51-10-2, & SRM 51-10-6Jun 9, 2010 · N267FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA201006081873Seat Track · corrodedCORROSION SEAT TRACK SECTION BS 1130-BS 1176, RBL 25. REMOVED CORRODED SEAT TRACK AT BS 1130 - BS 1176 RBL 25 IAW SRM 51-30-2 FOUND CORROSION OUT- OF-LIMITS IAW SRM 53-10-1 FIG 3. FABRICATED SEAT TRACK PN RCV 7075T65105X4IN DIM: 44" 3/4 IAW DWG 53FX976 REV Jun 8, 2010 · N267FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201006081871Skin · gougedMAIN CARGO AREA, MAIN CARGO INNER SKIN, BS 620 - 640, STR 4L GOUGED. REMOVED DAMAGE MAIN CARGO DOOR INNER SKIN FROM BS 594- BS 642 STR 9L - STR 4L, FABRICATED NEW SKIN FROM 2024T3 .125 APPROX DIM: 79" X 48" & INSTALLED NEW SKIN AT MAIN CABIN CARGO DOOR CJun 8, 2010 · N267FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA201006081900Intercostal · corrodedCORROSION IN STR 28L AT BS 600. CUTOUT DAMAGED AREA APPROX DIM: 17" IN LENGTH, AND FABRICATED NEW STRINGER SECTION FROM BAC 1498-141 APPROX DIM: 17" IN LENGTH AND FAB'D 2 EA. SPLICES FROM BAC 1498-132 APPROX DIM: 12", ALSO FAB'D NEW INTERCOSTAL FROM 7075 O Jun 8, 2010 · N267FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR FDEA201006071859Skin · corrodedCORROSION ON SKIN UNDER INTERCOSTAL AT BS 970 BETWEEN STR 28L AND 27L. CUT OUT DAMAGE, 15 1/4" X 2 7/8" ON SKIN AT BS 950E TO 970 BETWEEN STRINGER 28L AND 27L IAW SRM, REV 103, 53-30-3 FIG 3. FABRICATED DOUBLER USING 2024 T3, .125" X 27 1/4" X 11 1/2" IAW SRMJun 7, 2010 · N267FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA201006051840Floorbeam · corrodedCORROSION TOP OF FLOORBEAM MAIN CABIN BS 620 BETWEEN LBL 25 - LBL 45. CUT-OUT DAMAGED AREA AT TOP OF FLOOR BEAM BS 620 LBL 25 -LBL 45 APPROX DIM: 3" 5/8 X 1". FABRICATED ANGLES REPAIR HEAT TREATED TO T6, FIRST ANGLE DIM: 22" 1/4 X 3" AND SECOND ANGLE DIM:Jun 5, 2010 · N267FE · Boeing 727233 · Fuselage Main, Floor BeamSDR FDEA201006051839Floorbeam · corrodedCORROSION FLOORBEAM TOP FLANGE BS 1130, RBL 35. CUT-OUT DAMAGED AREA APPROX DIM: 3" X 1" 1/4, FABRICATED REPAIR PARTS, ANGLE APPROX DIM 11" 1/8 X 3", FABRICATED STRAP DIM 11" 1/4 X 2", FABRICATED FILLER DIM 2" 7/8 X 1" 3/8, FABRICATED RADIUS FILLER DIM: 11Jun 5, 2010 · N267FE · Boeing 727233 · Fuselage Main, Floor BeamSDR FDEA201006041825Fitting · corrodedCORROSION ON LOWER CHORD AT BS 950, STRINGER 30. REMOVED LOWER CHORD SPLICE AT BS950, BL 0, IAW SRM, REV 103, 51-30-2. LOCATED, DRILLED AND DEBURRED LOWER CHORD SPLICE FITTING IAW SRM 51-30-5. INSTALLED LOWER CHORD SPLICE FITTING IAW SRM 51-30-2.Jun 4, 2010 · N267FE · Boeing 727233 · Fuselage Main, Attach FittingsSDR FDEA201006041821Stringer · corrodedCORROSION ON STR 27L BETWEEN BS 950F AND 970. REMOVED SECTION OF STRINGER 38 1/2" IN LENGTH IAW B727 SRM, REV 103, 53-10-3 FIG 1. FABRICATED (2)EA. STRINGER SECTIONS USING BAC1498-146, 7075-T6, 19 1/4" IN LENGTH, AND (3)EA. SPLICES USING BAC1498-131, 7075-TJun 4, 2010 · N267FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR FDEA201006031833Skin · damagedMAIN CARGO AREA, BS 660, BETWEEN STR 3L -4L. FASTENERS WITH NO SPACING. DAMAGED AT TEAR STRAP AND SKIN BS 660 STR 3L - 4L DIM: 3" X 2" 1/2 - 2" 1/2 X 1". FABRICATED DOUBLER APPROX DIM: 12" 1/8 X 11" 1/8, FABRICATED TRIPLER APPROX DIM: 9" 3/4 X 9", FABRICATJun 3, 2010 · N267FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA201006031812Stringer · corrodedCORROSION ON STRINGER 29L, FROM BS 950B TO 950C. REMOVED FASTENERS IAW SRM 51-30-2. REMOVED CORROSION FROM STR 29L IAW SRM 51-10-6. UT INSPECTED AREA IAW NDTM 51-00-00, FIG 3 PART 4, ORIGINAL .150", REMAINING .136". FOUND MATERIAL LOSS OF .014" TO BE WITHJun 3, 2010 · N267FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR FDEA201006031810Angle · crackedRT WING INBD MID FLAP LOWER T/E CHORD ANGLE IS CRACKED, 2 PLACES, WBL 100. R & R DUE TO DELAMINATION ON SNRM NR N00544, WO NR00048343.Jun 3, 2010 · N267FE · Boeing 727233 · Trailing Edge FlapsSDR FDEA201006031809Structure · crackedNR 7 SLAT T/E CHORD CRACKED AT INBD UP STOP. REMOVED NR 7 SLAT LOWER CHORD IAW SRM 51-30-2. FABRICATED NEW CHORD USING BAC1514-1559, 2024-T3511, 113.7500", IAW SRM 57-50-2 FIG 2 AND 51-30-5. INSTALLED LOWER CHORD IAW SRM 51-30-2.Jun 3, 2010 · N267FE · Boeing 727233 · Leading Edge DevicesSDR FDEA201006031801Seat Track · corrodedCORROSION SEAT TRACK FLANGE MAIN CABIN BS 680 TO BS 620, LBL 45. REMOVED DAMAGED SEAT TRACK SECTION FROM BS 480 - 690 LBL 45 AND FABRICATED NEW SEAT TRACK SECTION FROM BAC 1520-792 APPROX DIM: 209" .5, FABRICATED SPLICE ANGLES FROM BAC 1503-100122 APPROX DIJun 3, 2010 · N267FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201006022027Fitting · damagedTAIL STAND FITTING AFT SIDE OF 1183 BULKHEAD, LBL19 HAS A DRILL START REPAIRED TAIL STAND FITTING AFT SIDE OF BS 1183 BULKHEAD, LBL19 IAW EA 7-5310- 135541 ( FUSELAGE AD 98-11-03 R1, BS1183 AFT PRESSURE BULKHEAD VERTICAL BEAM WITH INSUFFICIENT FASTENER SPACINJun 2, 2010 · N268FE · Boeing 727233 · Fuselage Main, Structure
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