Pratt & Whitney JT8D-15

Service difficulty reports · 2,710

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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 engine_model_key = 'JT8D15'
  ORDER BY difficulty_date DESC"

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SDR FDEA201011224459Stringer · corrodedCORROSION STRINGER 30 AT STA 1166, EXTERIOR SIDE OF LT CHANNEL RISER. REMOVED STRINGER SECTION FROM STATION 1142 TO 1183 AND 1EA SPLICE IAW SRM 51-30-2. FABRICATED 2 STRINGER REPAIR SECTIONS USING BAC1498-147 7075T6 19" LONG AND 19 1/2" LONG AND 2 SPLICES UNov 22, 2010 · N233FE · Boeing 727247 · Fuselage Main, Longeron/StringerSDR FOTR2019813717Floorbeam · damagedBS 1110, FLOORBEAM AT LBL 60 HAS NUTPLATE FASTENER AT EDGE OF PLUGED HOLE. CUT OUT DAMAGE SECTION 14.2500" X 2" IAW SRM 53-10-8. FABRICATED UPPER CORD FROM BAC1505-100617 7075-T6 PO 20172139, 20.1250"X 2.1250", 2EA ANGLES SUPPORTS FROM BAC1490-2785 7075-T6, PONov 20, 2010 · N713AA · Boeing 727223 · Fuselage Main, Floor BeamSDR FOTR/20198/13037Rib · damagedREPAIR LT L/E WING BETWEEN WINGTIP LENS AND NR 1 SLAT. REMOVED PANEL & RIB AT LT L/E WING BETWEEN WINGTIP & NR 1 SLAT IAW SRM 51-30-2. HEAT TREATED RIB FROM 2024-0 .040" TO 2024-T4 IAW FASI ENG REPORT NR2-371-53-801 REV A. NEW RIB MATERIAL USED 2024-0 .040" Nov 20, 2010 · N713AA · Boeing 727223 · Wing, Rib/BulkheadSDR FOTR2019813724Seat Track · corrodedBS 960, RBL 24, SEAT TRACK HAS GOUGE. REMOVED CORROSSION FOUND TO BE OUT OF LIMITS IAW SRM 51-10-6 & 53-10-1 FIG 3. FABRICATED SEAT TRACK AND SPLICE FROM BAC1503-100122-7178T6 AND BAC1520-792-7178T6511 AND 7075-T6 .250 TREATED AND PRIMED PARTS IAW SRM 51-10-2Nov 20, 2010 · N713AA · Boeing 727223 · Fuselage, Seat/Cargo Attach FittingsSDR FOTR2019813689Seat Track · corrodedBS 1070-1010, SEAT TRACK LBL 48 IS CORRODED. REMOVED CORROSION ON UPPER FLANGE OF LBL 48, SEAT TRACK SECTION EVALUATED ARE FOUND AREA TO BE OUT OF LIMITS. REMOVED SEAT TRACK SECTION FROM BS 1010-1130 LBL48. FABRICATED NEW SEAT TRACK SECTION FROM BAC1520-792-7Nov 20, 2010 · N713AA · Boeing 727223 · Fuselage, Seat/Cargo Attach FittingsSDR Y2PA2010112400031Battery · dischargedROW 12, LT & RT EMERGENCY EXIT SIGN FWD OF OVERWING HATCH IS INOPERATIVE. DISCREPANCY FOUND DURING SERVICE CHECK. MX RECHARGED THE BATTERY SUPPLY. SYS OPERATIONALLY CHECKED GOOD IAW THE MM 33-53-0. ACFT RETURNED TO SERVICE.Nov 20, 2010 · N934US · Doug DC934 · Emergency LightingSDR FDEA201011204439Frame · dentedFWD PIT FRAME REPAIR DOUBLER IS DENTED AT BS 600, BETWEEN STR 25-26L. REMOVED FRAME REPAIR DOUBLER AT BS600 BETWEEN STRINGER 25L AND 26L IAW SRM, REV 103, 51-30-2. FABRICATED FRAME REPAIR USING 7075-0, .063" X 6.6" X 4.0" IAW DRAWING NR 69-43674. INSTALLED DNov 20, 2010 · N233FE · Boeing 727247 · Fuselage Main, FrameSDR FDEA201011204440Seat Track · corrodedCORROSION SEAT TRACK STA 950, PLUS 10" TO STA 1010, RBL 25. REMOVED CORROSION FOUND OUT OF LIMITS IAW SRM 53-10-1 FIG 1, REMOVED SEAT TRACK IAW SRM 51-30-2, FABRICATED NEW SEAT TRACK FROM BAC 1520-792-7178-T6511 DIM: 20' X 3 3/8" IAW SRM 53-10-5 FIG 1, TREATENov 20, 2010 · N233FE · Boeing 727247 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201011204647Floorbeam · corrodedCORROSION TOP TEE CAP FLOORBEAM MAIN CABIN STA 950F RBL 25 - RBL 45 CUT OUT DAMAGED AREA, FABRICATED REPAIR FILLER, ANGLES AND STRAPS, INSTALLED. REPAIR PARTS AT BS 950F, RBL 25 TO RBL 55 IAW SRM 51-30-2, SRM 51-10-2 AND SRM 53-10-8, FIG 1.Nov 20, 2010 · N233FE · Boeing 727247 · Fuselage Main, Floor BeamSDR FOTR2019813627Stringer · corroded(FOTR) BS 1130, STR 27 L HAS CORROSION AT STRINGER FITTING. CUT & REMOVED STRINGER 14 .7500" LONG FROM 1120 TO 1135 STR 27L. FABRICATED STRINGER REPAIR HAT SECTION MAT USED BAC 1498-145-7075-T6, PO 90010545 DIM 14.7500 LONG. SPLICE MAT. USED BAC 1498-131-7075-Nov 19, 2010 · N713AA · Boeing 727223 · Fuselage Main, Longeron/StringerSDR FOTR2019813655Skin · punctured(FOTR) ON THE LT INBD MID FLAP SKIN IS PUNCTURED NEAR INBD END ON LWR SURFACE WHERE AFT FLAP MATES WITH MID FLAP. REMOVED DAMAGED AREA CUT OUT SIZE 4.5" X 4.0" LT MID FLAP INBD AFT LOWER T/E SKIN, IAW SRM 51-10-1 AND 57-50-4. OBTAINED MAT FOR FILLER 2024-T3 .0Nov 19, 2010 · N713AA · Boeing 727223 · Trailing Edge FlapsSDR FDEA201011194430Skin · dentedDENT EXTERIOR FUSELAGE STA 405 STR 16-17L. CUTOUT DAMAGED AREA DIM: APPROX 1" DIAMETER IAW SRM 53-30-3 FIG 1 AND FABRICATED REPAIR DOUBLER FROM 2024T3 .063 DIM: 11 1/8" X 8 3/4" IAW SRM 53-30-3 FIG 1, INSTALLED COUNTERSINK WASHERS IAW SRM 53-30-1 FIG 1, TNov 19, 2010 · N233FE · Boeing 727247 · Fuselage Main, Plate/SkinSDR FDEA201011194428Floorbeam · corrodedCORROSION TOP "T" CAP FLOORBEAM MAIN CABIN STA 380 RBL45 - RBL 61. REMOVED PREVIOUS REPAIR. FABRICATED NEW T-CAP USING BAC1505-100617 7075T7 DIMS 76 5/8", FABRICATED 1 EACH SPLICE ANGLE USING BAC1490-2785 7075T6 DIMS 13 1/2", FABRICATED 1 EACH SPLICE ANNov 19, 2010 · N233FE · Boeing 727247 · Fuselage Main, Floor BeamSDR FDEA201011194424Shear Tie · corrodedCORROSION FRAME SHEAR TIE FWD LOWER FLANGE STATION 950B, BETWEEN STR 29L TO STR 28L. CUT OUT DAMAGED SHEAR TIE BS 950B FRAME BETWEEN STRINGER 29L AND 28L, 6 3/8" X 3 5/8" IAW SRM, REV 103, 53-10-4 FIG 12. FABRICATED SHEAR TIE USING 7075-0, .080" X 10 5/16Nov 19, 2010 · N233FE · Boeing 727247 · Fuselage Internal Mounting StructureSDR FOTR2019813362Angle · damagedCRACK INBD AILERON, RT WING UPPER PANEL. REMOVED PANEL & CRACKED ANGLE AT INBD AILERON RT WING UPPER PNL IAW SRM 51-30-2. FABRICATED NEW ANGLE FROM 2024-T3. PO 900997 DIM. 5" X 2" IAW SRM 51-20-1, FIG 7 AND SRM 51-10-3 & SRM 51-30-6. TREATED AND PRIMMED IAWNov 18, 2010 · N713AA · Boeing 727223 · Wing Miscellaneous StructureSDR FOTR2019813847Floorbeam · corrodedSTA 1130, FLOORBEAM LBL 0-9 FOUND CORRODED. CUT DAMAGE AREA AT LWR CHORD OF FLOORBEAM STA 1130 DIM. 5.75" X 2" IAW SRM 53-10-8, FIG 10. C/W HFEC INSP IAW NDTM PT6 51-00-00, FIG 23. DO DEFECTS NOTED. EXTENDED CUTOUT .040" NEW DIM 5.79 X 2" FAB 2EA ANGLES FRONov 18, 2010 · N713AA · Boeing 727223 · Fuselage Main, Floor BeamSDR FDEA201011184411Air Duct · contaminatedSTRONG ODOR OF FUEL FUMES IN COCKPIT, INCREASED AFTER TAKEOFF DURING CLIMB. UPON ARRIVAL, NOTICED STRONG DIESEL ODOR IN ACFT EE AND PIT AREAS ALSO IN FLT DECK. OUR HEAT DUCTING WAS ALSO STRONG ODOR. CHECKING COALASTER BAGS. SUSPECT HEAT CART CONTAMINATION Nov 18, 2010 · N487FE · Boeing 727227 · Air Distribution SystemSDR FOTR2019813826Intercostal · damagedINTERCOSTAL IS BENT AT FLOOR SUPPORT RBL 4 IN AFT CARGO. REMOVED INTERCOSTAL AT STA 950F-970, RBL 4, IAW SRM 51-30-2. FABRICATED FROM 7075-T6 .040" PO 9009608 IAW SRM 53-10-2 TREATED AND PRIMED PART IAW SRM 51-10-2 INSTALLED INTERCOSTAL IAW SRM 51-30-2.Nov 17, 2010 · N713AA · Boeing 727223 · Fuselage Miscellaneous StructureSDR FOTR/20198/13827Intercostal · damagedBS 970-990 INTERCOSTAL IS BENT AT FLOOR SUPPORT RBL 4 IN AFT CARGO. REMOVED INTERCOSTAL AT STA 897-990, RBL 4 IAW SRM 51-30-2. FABRICATED INTERCOSTAL FROM 7075-T6 .040". PO 9009608 IAW SRM 53-10-2. TREATED AND PRIMED PART IAW SRM 51-10-2. INSTALLED INTERCOSTNov 17, 2010 · N713AA · Boeing 727223 · Fuselage Miscellaneous StructureSDR FOTR2019813583Intercostal · damagedBS 950E-950F INTERCOSTAL IS BENT AT FLOOR SUPPORT RBL 4 AFT CARGO. REMOVED INTERCOSTAL AT STA 950E-950F RBL4 IAW SRM 51-30-2. FABRICATED INTERCOSTAL FROM 7075-T6 .040". PO 9009608. IAW SRM 53-10-2. TREATED AND PRIMED PART IAW SRM 51-10-2. INSTALLED INTERCOSTANov 17, 2010 · N713AA · Boeing 727223 · Fuselage Structure (General)SDR FOTR2019813595Web · damagedLT SIDE OF AIRSTAIR AREA, INSIDE FUSELAGE TORQUE BOX, WEB AT BS.1223 HAS DRILL DAMAGE IN UPPER INBD CORNER. CUT OUT DAMAGE AREA DIM. 1" X 1" IAW SRM 51-40-2. FABRICATED FILLER PO 9009504 AND DOUBLER FROM PO 9008186. TREATED AND PRIMED PARTS IAW SRM 51-10-2. INov 17, 2010 · N713AA · Boeing 727223 · Fuselage Miscellaneous StructureSDR FOTR2019813648Skin · gougedDEEP GOUGE MARKS ON LT OTBD FORE FLAP AT INBD END L/E. BLENDED GOUGE OUT OF LIMITS IAW SRM 57-50-1 FABRICATED AND INSTALLED DOUBLER REPAIR IAW SRM 57-50-4. MATERIAL USED 2024-T3 .063" PO 90010274 SIZE 3.5" X 4.25".Nov 17, 2010 · N713AA · Boeing 727223 · Wing, Plate/SkinSDR FOTR2019813819Skin · damagedEVALUATE EXISTING DENT AT LT INBD FORE FLAP LOWER SURFACE, 28" FROM INBD EDGE. EVALUATED DENT ON LT INBD FOREFLAP LOWER SURFACE & DENT WAS FOUND TO HAVE SHARP CREASE & BEYOND ALLOWABLE LIMITS IAW SRM 57-50-1 FIG 3. REMOVED DAMAGE/ CLEANED & PREPARED AREA IAW Nov 17, 2010 · N713AA · Boeing 727223 · Wing, Plate/SkinSDR FOTR2019813259Skin · damagedLT WING INBD FLAP, AFT FLAP HAS TEMP REPAIR C/W PERMINENT REPAIR IAW CUSTOMER REQUEST. REMOVED DAMAGED AREA; SANDED, CLEANED AND PREPPED AREA IAW SRM 51-40-20 PAR 7. REPAIRED LT WING INBD AFT FLAP UPPER SURFACE BY HOT BONDING REPAIR ON IAW SERM 51-40-20, PARNov 17, 2010 · N713AA · Boeing 727223 · Trailing Edge FlapsSDR FDEA201011174409Actuator · failedNR7 LED WOULD NOT RETRACT ON CLIMBOUT. RAN QRH AND IT WOULD NOT CLEAR. REPLACED THE NR 7 SLAT ACTUATOR WITH AND OVERHAULED UNIT PER MM 27-81-032-4. OPS CHECK AND LEAK CHECK GOOD. LEAK AND OPS CHECK NORMAL PER MM 27-81-032-4.Nov 17, 2010 · N282FE · Boeing 727233 · Leading Edge Slat ActuatorSDR FDEA201011174406Seat Track · corrodedCORROSION SEAT TRACK FLANGE STA 344 TO STA 480, LBL 45. REMOVED SEAT TRACK SECTION FROM BS 344 TO BS 480 LBL 45, FABRICATED NEW SEAT TRACK SECTION & INSTALLED NEW SEAT TRACK IAW SRM 51-30-2, SRM 53-10-5 FIG 1 & SRM 51-10-2.Nov 17, 2010 · N233FE · Boeing 727247 · Fuselage, Seat/Cargo Attach FittingsSDR FOTR/20198/13440Frame · damagedSTA 720, FRAME HAS FASTENER W/NO ED IN WINDOW AREA ON LT SIDE. CUTOUT DAMAGE AREA DIM. 1" X .7500", FABRICATED FRAME REPAIR 2EA PARTS, MATERIAL USED 7075-0. PO 90016396, DIM 13" X 3" & 13" X 4" IAW. SRM 53-10-4. HEAT TREATED PART FROM 7075-0 TO 7075-T6. IAWNov 16, 2010 · N713AA · Boeing 727223 · Fuselage Main, FrameSDR FOTR20198913427Frame · damagedSTA 720E FRAME HAS FASTENERS W/ NO ED IN RT SIDE WINDOW AREA. CUTOUT DAMAGED AREA DIM. 1" X 3/4" IAW SRM 53-10-4, FIG 1. FAB. FRAME REPAIR 2EA PARTS MAT. USED 7075-0 .071" PO 90016396 DIM 13.5" X 3" & 13.5 X 4" IAW SRM 53-10-4, FIG 1 HEAT TREATED PARTS FROM 7Nov 16, 2010 · N713AA · Boeing 727223 · Fuselage Main, FrameSDR FOTR2019813271Frame Splice · chafedBS 1166 BETWEEN STRINGER 5 & 6 R GILLINER SUPPORT IS CHAFING AGAINST FRAME SPLICE. REMOVED FRAME SPLICE IAW SRM 51-30-2. FABRICATED FRAME SPLICE APPROX. DIM 8.3750" X 4.3750" IAW SRM 53-10-2, FIG 5 AND SRM 51-20-1, FIG 7. INSTALLED FRAME SPLICE AT BS 1166 BENov 16, 2010 · N713AA · Boeing 727223 · Fuselage Main, FrameSDR FDEA201011164387Seat Track · corrodedCORROSION SEAT TRACK FLANGE STA 380 - STA 480, RBL 45. REMOVED DAMAGED SEAT TRACK FABRICATED NEW SECTION USING BAC1520-792, 7178-T65 DIMS 135" AND INSTALLED IAW SRM 53-10-2 AND SRM 51-30-2.Nov 16, 2010 · N233FE · Boeing 727247 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201011164388Seat Track · corrodedFWD PIT CABIN SEAT TRACK AT BL 0 IS CORRODED BETWEEN BS 500 - 540. REMOVED SEAT TRACK SECTION AND SPLICES IAW SRM 51-30-2. FABRICATED, LOCATED AND DRILLED SEAT TRACK SECTION IN LENGTH USING BAC1520-792 7178-T6511, AND INSTALLED SEAT TRACK SECTION AND SPLICES Nov 16, 2010 · N233FE · Boeing 727247 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201011164389Seat Track · corrodedCORROSION SEAT TRACK FLANGE STA 600 - STA 690, RBL 45. REMOVED SEAT TRACK IAW SRM 51-30-2 AND FABRICATED NEW SEAT TRACK FROM BAC1520-792-7178-T6511, DIM: APPROX 172" IAW SRM 53-10-5, FIG 1. TREATED AND PRIMED SEAT TRACK IAW SRM 51-10-2 AND INSTALLED IAW SRM 5Nov 16, 2010 · N233FE · Boeing 727247 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201011164390Seat Track · corrodedCORROSION SEAT TRACK FLANGE MAIN CABIN STA 480 - STA 690, LBL 25. REMOVED SEAT TRACK SECTION AND SPLICE IAW SRM 51-30-2, LOCATED AND DRILLED SEAT TRACK SECTION, BAC 1520-792 7178 T6 DIM 210" LONG. FABRICATED SPLICE MAT USED 2EA ANGLES BAC 1503-100122 7178-4Nov 16, 2010 · N233FE · Boeing 727247 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201011164393Seat Track · corrodedCORROSION SEAT TRACK FLANGE STA 706 - 740, RBL 25. REMOVED DAMAGED SEAT TRACK SECTION, FABRICATED NEW SEAT TRACK AND SPLICE SECTION, INSTALLED NEW SEAT TRACK AND SPLICE IAW SRM 51-30-2, REV 103, SRM 51-10-2 AND 53-10-5, FIG 1.Nov 16, 2010 · N233FE · Boeing 727247 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201011164394Seat Track · corrodedCORROSION SEAT TRACK & SPLICE MAIN CABIN STA 460 - STA 480, LBL 25. REMOVED DAMAGED SEAT TRACK SECTION. FABRICATED NEW SECTION USING BAC1520-792, 7178 T6511 DIMS 136" AND INSTALLED IAW SRM 53-10-2 AND SRM 51-30-2.Nov 16, 2010 · N233FE · Boeing 727247 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201011164391Skin · dentedDENT EXTERIOR FUSELAGE STA 378, STR 21L. CUTOUT DAMAGED AREA IAW SRM 53-30-3, FABRICATED DOUBLER REPAIR AND FILLER IAW SRM 53-30-2 FIG 2 AND SRM 53-30-3 FIG 3, INSTALLED FILLER AND REPAIR DOUBLER AT BS 378 STR 21L IAW SRM 53-30-3 FIG 3 AND SRM 51-30-2.Nov 16, 2010 · N233FE · Boeing 727247 · Fuselage Main, Plate/SkinSDR FDEA201011164482Stringer · damagedSTRINGER 4L AT BS 1180 TENSION TIE DAMAGED. CUT-OUT DAMAGED AREA ON STRINGER 4L FROM 1160 TO 1181.1250, DIM 21.1250", FABRICATED AND INSTALLED REPAIR AND STRINGER SECTION FROM STR. BAC 1498-145 7075T6-2, DIM 21.1250" AND 5EA REPAIR PLATES NR1 FROM 2024T3 0.250Nov 16, 2010 · N488FE · Boeing 727227 · Fuselage Main, Longeron/StringerSDR FDEA201011164392Seat Track · corrodedCORROSION SEAT TRACK FLANGE MAIN CABIN STA 480 - STA 690, LBL 45. REMOVED SEAT TRACK SECTION STA. 480 - STA. 690 LBL 45 IAW SRM 51-30-2 AND FABRICATED NEW SEAT TRACK SECTION FROM BAC1520-7927178T6 511 APPROX DIM: 209" IAW SRM 53-10-5 FIG 1. INSTALLED NEW SEANov 16, 2010 · N233FE · Boeing 727247 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201011164402Spar · crackedCRACKED ANGLE CHORD FALSE SPAR RT WING AT NR8 SPOILER ACTUATOR SUPPORT MOUNT TRIMMMED WEB 12.2500" X 9.7500" AND LOWER CHORD 31" IN LENGTH AT RT WING FALSE SPAR IAW REPAIR DWG NR SR27-57-038, REV C. FABRICATED 2 SPLICE ANGLES USING 7075- 0, .071" X 16.2500" Nov 16, 2010 · N233FE · Boeing 727247 · Wing SparSDR FDEA201011164403Seat Track · corrodedCORROSION SEAT TRACK FLANGE STA 1030 - STA 950, PLUS 10" LBL 45. REMOVED DAMAGED SEAT TRACK SECTION. FABRICATED NEW SECTION USING BAC1520-792 7178 T6511 DIMS 210 3/8" AND INSTALLED IAW SRM 53-10-5 AND SRM 51-30-2.Nov 16, 2010 · N233FE · Boeing 727247 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201011164384Seat Track · corrodedCORROSION SEAT TRACK FLANGE STA 482-680, RBL 25. REMOVED SEAT TRACK SECTION FROM BS 480-690 RBL 25, FABRICATED NEW SEAT TRACK SECTION AND INSTALLED SEAT TRACK AT BS 480-690 RBL 25 IAW SRM 51-30-2; SRM 53-10-5 FIG 1 AND SRM 51-10-2, REV 103.Nov 16, 2010 · N233FE · Boeing 727247 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201011154369Stringer Splice · corrodedAFT PIT STRINGER SPLICE CORRODED BS 1124 TO 1136, STR 30. CUT OUT DAMAGED STRINGER, FABRICATED NEW STRINGER SECTION AND SPLICES AND INSTALLED IAW SRM 53-10-3, SRM 51-10-2 AND SRM 51-30-2.Nov 15, 2010 · N233FE · Boeing 727247 · Fuselage Main, Longeron/StringerSDR FDEA201011134348Skin · gougedINNER SKIN GOUGED STA 1177, STR 4L. CUT-OUT DAMAGED AREA AT BS 1177 ON STR 4L DIM. 1.125" DIA., FABRICATED REPAIR DOUBLER AND LAP FILLER FROM 2024T3 0.063" DIM. DOUBLER 10" X 6.8750" FILLER 11" X 4.5", AND INSTALLED DOUBLER AND FILLER IAW EA 7-5330-143918.Nov 13, 2010 · N488FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR FDEA201011134351Frame · gougedFRAME GOUGED STA 1070 STR 27L, AT RADIUS OF UPPER CHORD FLANGE CUT OUT DAMAGED SECTION OF UPPER FRAME DIM 3/4" X 2 1/2 " IAW SRM 51-40-3, FIG 1. FABRICATED REPAIR DOUBLER, MATERIAL USED 7075 O .071" DIM 14" X 6" IAW SRM 53-10-2, FIG 5 AND 51-40-3, FIG 1 LNov 13, 2010 · N488FE · Boeing 727227 · Fuselage Main, FrameSDR FDEA201011124668Seat Track · corrodedSEAT TRACK CORRODED STA 950 PLUS 10" TO STA 1010, RBL 45. REMOVED DAMAGED SEAT TRACK SECTION, FABRICATED NEW SECTION AND INSTALLED IAW SRM 53-10-2, 51-30-2 AND 53-10-5 FIG 7.Nov 12, 2010 · N233FE · Boeing 727247 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201011074441Structure · misinstalledL1 DOOR RAIN GUTTER FWD ATTACMENT HAS 2 FASTENERS WITH IMPROPER SPACING STA 300 TO STA 312. CUT-OUT AFFECTED AREAS IAW EA 7-5330-143916. FABRICATED FREEZE PLUGS, FILLERS, AND DOUBLER IAW EA 7-5330-143916. INSTALLED REPAIR PARTS IAW EA 7-5330-143916 AT L-1 DONov 7, 2010 · N488FE · Boeing 727227 · Fuselage Miscellaneous StructureSDR C8GA2010000059Web · dentedDURING HEAVY MX PERFORMING INSPECTIONS IT WAS NOTED THAT THE FWD CARGO COMPARTMENT RT SIDE OF CARGO DOOR FRAME CUT-OUT AT BS 560 BETWEEN STR 23R & 25R. REMOVED DAMAGE AND FABRICATED WEB REPAIR FROM 7075 T6 .050 DIM. 15.5" X 5". INSTALLED REPAIR, NO OTHER DEFENov 6, 2010 · N715AA · Boeing 727223 · Fuselage Miscellaneous StructureSDR C8GA2010000064Floorbeam · corrodedDURING HEAVY MX INSP IT WAS NOTED THAT THE AFT CARGO FLOORBEAM STA 1030, RBL 20 IS CORRODED. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR. NO OTHER DEFECTS WERE NOTED. ACFT WAS RETURNED TO SERVICE.Nov 6, 2010 · N715AA · Boeing 727223 · Fuselage Main, Floor BeamSDR C8GA2010000065Floorbeam · corrodedDURING HEAVY MX INSP IT WAS NOTED THAT THE AFT CARGO FLOORBEAM STAT 1010, LBL 10 IS CORRODED. CUT OUT DAMAGE, FABRICATED REPAIR PARTS FROM 7075 T6 .063" DIM 18" X 3", STRAP FROM 7075 T6 .100" DIM. 18" X 2" FILLER FROM BAC1505-100797 DIM. 7.25" X 2.25" AND INSTNov 6, 2010 · N715AA · Boeing 727223 · Fuselage Main, Floor BeamSDR C8GA2010000067Shear Tie · corrodedDURING HEAVY MX INSP IT WAS NOTED THAT THE AFT CARGO STA 1148, BL 0 SHEAR-TIE IS CORRODED. REMOVED SHEAR-TIE AND FABRICATED NEW FROM 2024 T3 .050". INSTALLED REPAIR, NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE.Nov 6, 2010 · N715AA · Boeing 727223 · Fuselage Internal Mounting Structure
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