Boeing 727-227

Service difficulty reports · 5,082

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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 = '727227'
  ORDER BY difficulty_date DESC"

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SDR FDEA201003180896Seat Track · corrodedCORROSION SEAT TRACK LOBE SIDE WALL MAIN CABIN BS 610 - BS 620 RBL 45. REMOVED CORROSION IB FLANGE IAW SRM 51-10-6. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1, FIG 3 & 53-10-2. REMOVED SEAT TRACK SECTION SRM 51-30-2. FABRICATED SEAT TRACK SECTION MATERIAMar 18, 2010 · N479FE · Boeing 727227 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201003180894Seat Track · corrodedCORROSION ALONG WHOLE SEAT TRACK SECTION BS 480 - BS 690 LBL 45. REMOVED SEAT TRACK STA 480 - STA 690 LBL 45 IAW SRM 51-30-2. FABRICATED SEAT TRACK PN BAC 1520-792-7178T 65, PO 9006020, DIM: 204" X 8" STA 480 - 690 AND FABRICATE ANGLE PN 1503-100-122-7178T6,Mar 18, 2010 · N479FE · Boeing 727227 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201003180891Seat Track · corrodedCORROSION ALONG WHOLE SEAT TRACK SECTION MAIN CABIN BS 480- BS 690, LBL 24. EVALUATED AREA FOUND CORROSION AT SEAT TRACK SECTION BS 480 TO BS 700 OUT OF LIMITS IAW SRM 727-200 NOTED 5.4 AND SRM 53-10-5 FIG 1. R & R SEAT TRACK AT LBL 24 FROM BS 480 TO BS 690Mar 18, 2010 · N479FE · Boeing 727227 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201003180889Seat Track · corrodedCORROSION SEAT TRACK SECTION MAIN CABIN BS 360-480 BL 0. CLEANED AREA IAW BSOPM 20-30-03, EVALUATED AREA NO CORROSION NOTED IAW SRM 51-10-1 AT BS 360-440, REMOVED DAMAGED SECTION BS 430-600 IAW SRM 51-30-2 AND FABRICATED NEW SEAT TRACK SECTION FROM BAC 1520-7Mar 18, 2010 · N479FE · Boeing 727227 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201003180886Seat Track · corrodedCORROSION SEAT TRACK MAIN CABIN BS 370 -BS 390 LBL 45. CLEANED AREA IAW BSOPM 20-30-03 AND EVALUATED AREA NO CORROSION NOTED IAW SRM 51-10-1 AT BS 360- BS 399. EVALUATED AREA FROM BS 400 - BS 480 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1 FIG 3 AND SRM -20Mar 18, 2010 · N479FE · Boeing 727227 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201003180884Seat Track · corrodedCORROSION SEAT TRACK SECTION MAIN CABIN BS 360 -BS 480 LBL 24. CLEANED AREA FROM BS 360- BS 480 LBL 24 IAW BSOPM 20-30-03. EVALUATED AREA FOUND CORROSION AT BS 380- BS 480 IAW SRM 51-10-1 OUT OF LIMITS IAW SRM 53-10-1 AND SRM 727-200 9G NOT 5.4. REMOVED DAMMar 18, 2010 · N479FE · Boeing 727227 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201003180880Floorbeam · corrodedCORROSION WITH CRACKING/ LIFTED METAL -STA 1130 FLOORBEAM UPPER CHORD FWD FLANGE, LBL 25 - LBL 45. CUT-OUT DAMAGED AREA FROM 1130 FLOORBEAM UPPER CHORD FWD FLANGE IAW SRM 53-10-8 DETAIL III DIM 12.5 INCH LONG. PERFORMED HFEC ON CUT-OUT IAW NDTM 51-00-00 FIG Mar 18, 2010 · N479FE · Boeing 727227 · Fuselage Main, Floor BeamSDR FDEA201003180872Floorbeam · corrodedFLOORBEAM ABOVE RT MLG WHEEL WELL FWD SURFACE HAS CORROSION AT BS 880 RBL 44. REMOVED CORROSION ON FLOORBEAM BY MECHANICAL MEANS IAW SRM 51-10-6. AREA UT INSPECTED IAW NDTM 51-00-00 FIG 2, PART 4 WITH ORIGINAL MATERIAL OF .100", .002" REMOVED, REMAINING AMar 18, 2010 · N479FE · Boeing 727227 · Fuselage Main, Floor BeamSDR FDEA201003180871Floorbeam · crackedMAIN CABIN OVERWING FLOORBEAM T CHORD CRACKED AT LOWER RADIUS RBL 24 BS 760.9. REMOVED DAMAGED CHORD IAW SRM 51-30-2. FABRICATED NEW CHORD FROM BAC1506-1108 MATERIAL 7075T6 PO NR 20013162 DIM: 110" IAW SRM 51-30-5 & 51-10-1 AND DWG 65-16279 REV F DATED 04/19Mar 18, 2010 · N479FE · Boeing 727227 · Fuselage Main, Floor BeamSDR FDEA201003160962Support · crackedCRACK RT FWD STIFFNER NLG TRUNNION SUPPORT. REPLACEMENT OF STIFFENER ACCOMPLISHED ON SNRM NR N00463, WORK ORDER NR 00047694.Mar 16, 2010 · N479FE · Boeing 727227 · Fuselage, Landing Gear Attach FittingsSDR FDEA201003160961Support · crackedCRACK RT AFT STIFFNER NOSE TRUNNION SUPPORT. NO WORK ACCOMPLISHED ON THIS WORK CARD. REPLACEMENT OF STIFFENER ACCOMPLISHED ON SNRM NR N00463, WORK ORDER NR 00047694, SDR TRACKING NR 10-0807.Mar 16, 2010 · N479FE · Boeing 727227 · Fuselage, Landing Gear Attach FittingsSDR FDEA201003160843Floorbeam · corrodedFLOORBEAM ABOVE RT MLG WHEEL WELL CORRODED ON FWD SURFACE BS 890, RBL 22 TO RBL 28. CUT-OUT DAMAGED AREA AT BS 890 RBL 22 TO 28 DIM: 4.125" X 2.750" AND 2" X 2.9" IAW SRM 51-40-4, FIG 1. HFEC INSPECTED CUT-OUT IAW NDTM 51-00-00 FIG 23, PT 6 NO DEFECTS NOTED.Mar 16, 2010 · N479FE · Boeing 727227 · Fuselage Main, Floor BeamSDR FDEA201003160842Door Frame · crackedNR 1 CARGO DOORWAY FRAME, BS 620, STR 25R, WEB CRACKED, ORIGINATING FROM SEAL RETAINER FASTENER HOLE. REMOVED WEB AT BS 620 FRAME FROM STRINGER 16R TO 28R IAW SRM, REV 102, 51-30-2. FABRICATED NEW WEB USING 7075-T6, .071" X 24" X 139.5" IAW MFG DWG NR 65-5Mar 16, 2010 · N479FE · Boeing 727227 · Fuselage Main, StructureSDR FDEA201003160841Web · crackedNR 1 CARGO DOORWAY FRAME, BS 560, STR 19R, WEB CRACKED NEXT TO DOOR STOP FITTING. REMOVED WEB FROM C-1 DOOR CUT OUT FRAME AT BS 560 IAW SRM, REV 102, 51-30-2. FABRICATED NEW WEB USING 7075 -T6, .071" X 80" X 18" IAW SRM 53-10-2 FIG 3 AND DWG NR 65-56100,Mar 16, 2010 · N479FE · Boeing 727227 · Fuselage Main, StructureSDR FDEA201003130812Skin · gougedFUSELAGE SKIN GOUGED AT LAP SEAM, STR 19L, STA 720E. REMOVED FASTENERS AS REQUIRED AND CUT-OUT DAMAGED AREA ON UPPER AND LOWER LAP SEAM DIM: 3" X 4.3750" 2 EA IAW SRM 53-30-3 FIG 6. HEFC INSPECTED AREA IAW NDTM 51-00-00 FIG 23 PART 6, NO DEFECTS NOTED. FAMar 13, 2010 · N479FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR FDEA201003130811Skin · chafedFUSELAGE SKIN CHAFED AT LAP SEAM, STR 19R, STA 720E. CUT-OUT DAMAGED AREA DIM: 5.5" X 2.7500" IAW SRM 53-30-3 FIG 6. HFEC INSPECTED AREA IAW NDTM 51-00-00 FIG 23, PART 6, NO DEFECTS NOTED. FABRICATED DOUBLER FROM 2024T3 .071 DIM: 13" X 9" AND 2 EA TAPER FILMar 13, 2010 · N479FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR FDEA201003130814Skin · crackedRT INBD FOREFLAP CARRIAGE ATTACH FITTING AREA AT STA 224, SKIN CRACKED FWD OF ATTACH FITTING. CUT OUT DAMAGED AREA, DIMENSIONS .750" X .218" IAW SRM, REV 102, 57-50-4, FIG. 1. FABRICATED FILLER USING 2024 T-3, PO NR 9002222, DIMENSIONS .050" X .750" X .218" Mar 13, 2010 · N479FE · Boeing 727227 · Wing, Plate/SkinSDR FDEA201003130810Skin · dentedDENT BS 400 STR 17L - 19L EXTERIOR FUSELAGE. EVALUATED DENT AND FOUND TO BE OUT OF LIMITS IAW SRM 53-30-1 FIG 1. CUT-OUT DAMAGED AREA DIM: 2.6250" X 2.8750" IAW SRM 53-30-3 FIG 3. HFEC INSP CUT-OUT AREA IAW NDTM 51-00-00, FIG 23, PART 6, NO DEFECTS NOTED. FMar 13, 2010 · N479FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR FDEA201003130816Frame · damagedFRAME DAMAGED BY TOO LONG HARDWARE INSTALLED IN WIRE BUNDLE STAND OFF CLAMP, STA 500, STR 8R. REMOVED STAND OFF IAW SRM 51-30-2. DRILLED OUT DAMAGED AREA .125 DIA IAW SRM 53-10-1, FIG 1 INSTALLED .1250" SOLID FASTENER IAW SRM 53-10-1 FIG 1 & 51-30-2. INSTMar 13, 2010 · N479FE · Boeing 727227 · Fuselage Main, FrameSDR FDEA201003130815Frame · damagedWIRE BUNDLE STAND OFF BROKEN AND FRAME DAMAGED, STA 460, STR 8R. REMOVED DAMAGED STAND OFF IAW SRM 51-30-2. DRILLED OUT DAMAGE AT FRAME UP TO .125 DIA IAW SRM 53-10-1, FIG 1 AND INSTALLED .1250" SOLID FASTENER AT FRAME IAW SRM 51-30-2. INSTALLED NEW STAND OMar 13, 2010 · N479FE · Boeing 727227 · Fuselage Main, FrameSDR FDEA201003130813Frame · mismanufacturedFASTENERS WITH NO SPACING IN FRAME, STA 344, STR 4L. CUT-OUT DAMAGED AREA, FABRICATED REPAIR ANGLES FROM 7075-0 .050 PO NR 9009327 DIM: 7.4" X 3.3" & 7.4" X 3" HEAT TREATED TO 7075T6 IAW ENGINEERING REPORT NR 2-37153-801, REV A. TREATED AND PRIMED IAW SRM 51-Mar 13, 2010 · N479FE · Boeing 727227 · Fuselage Main, FrameSDR FDEA201003130807Structure · corrodedE/E COMPARTMENT, RT MID CHORD CORRODED AT STA 294.5. REMOVED CORROSION FROM RT MID CHORD AT STA 294.5 IAW SRM, REV 102, 51-10-6. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1, FIG 1. R & R MID CHORD PN 65-19862-20 AND 2 VERTICAL STIFFENERS, PN 65-19863-10 AND 65Mar 13, 2010 · N479FE · Boeing 727227 · Fuselage Main, StructureSDR FDEA201003110781Rib · crackedNR 5 SLAT RIB OTBD OF ACTUATOR FWD MOUNT, PREVIOUS REPAIR DOUBLER IS MISSSING 1 FASTENER AND DOUBLER IS INSTALLED ON TOP OF BUTTON HEAD RIVET. ACCOMPLISHED NR 5 SLAT RIBS REPLACEMENT ON NR N00260 SO 00047694, SDR 10-0780Mar 11, 2010 · N479FE · Boeing 727227 · Leading Edge DevicesSDR FDEA201003110780Rib · crackedNR 5 SLAT HAS ONE RIB CRACKED INBD SIDE OF ACTUATOR FWD MOUNT. REMOVED WEB PNL FOR ACCESS AND REINSTALLED IAW B727 SRM 51-30-2. REMOVED 2 EA. RIBS FOR CRACKS AND FABRICATED 1 RIB FROM 2024-0 .040 PO 24146179 DIMS: 16 3/4" X 6" IAW SRM 57-20-2 FIG 2 & 51-30-Mar 11, 2010 · N479FE · Boeing 727227 · Leading Edge DevicesSDR FDEA201003110784Rib · crackedNR 7 SLAT HAS 1 RIB CRACKED ON OTBD SIDE OF ACTUATOR FWD MOUNT.Mar 11, 2010 · N479FE · Boeing 727227 · Leading Edge DevicesSDR FDEA201003110783Angle · crackedNR 7 SLAT LOWER AFT CHORD ANGLE IS CRACKED BELOW T-DUCT.Mar 11, 2010 · N479FE · Boeing 727227 · Leading Edge DevicesSDR FDEA201003110782Rib · crackedNR 6 SLAT HAS 2 CRACKED RIBS AT ACTUATOR FWD MOUNT. NBD SIDE IS CRACKED AT AFT NUTPLATE AND OTBD SIDE CRACKED IN BOTTOM RADIUS. REMOVED ACCESS PANELS AND CRACKED RIBS AT NR 6 SLAT IAW SRM 51-30-2. LOCATED AND DRILLED NEW RIBS IAW SRM 51-30-5. INSTALLED NEWMar 11, 2010 · N479FE · Boeing 727227 · Leading Edge DevicesSDR FDEA201003110779Angle · crackedNR 2 SLAT LOWER T/E CHORD ANGLE IS CRACKED BELOW T-DUCT. R & R NR 2 SLAT ASSY ON NR NR N00252, WORK ORDER NR 00047694. NO MX PERFORMED ON THIS SNRM.Mar 11, 2010 · N479FE · Boeing 727227 · Leading Edge DevicesSDR FDEA201003110778Beam · mismanufacturedFWD BS 1183 BULKHEAD LBL 18 VERTICAL BEAM HAS FASTENER WITH NO SPACING. CUT-OUT DAMAGED AREA AT VERTICAL BEAM, FABRICATED REPAIR PARTS & INSTALLED. REPAIR PARTS AT BS 1183 LBL 18 VERTICAL BEAM IAW EA 7-5310-135529.Mar 11, 2010 · N479FE · Boeing 727227 · Fuselage Main, StructureSDR FDEA201003090707Actuator · failedAFTER TAKEOFF, DURING FLAP RETRACTION FROM FLAPS 2, DEG TO FLAPS 0 AMBER LE FLAP LIGHT REMAINED ILLUMINATED. COMPLIED WITH STABILIZER AND IDENTIFIED NR3 SLAT STILL DEPLOYED. EXECUTED RED TABS BUT UNABLE TO ATTAIN CLEAN ACFT CONFIG NR 3 SLAT. REMAINED DEPLOYEMar 9, 2010 · N485FE · Boeing 727227 · Trailing Edge Flap ActuatorSDR FDEA201003040634Valve · malfunctionedACFT WOULD NOT PRESSURIZE. TROUBLESHOOTING RAN NR 3 ENGINE PRESSURIZED AC PERFORMED CABIN DECAY. CHECK IAW JRH DECAY CHECK GOOD. PERFORMED BLEED SYS CHECK IAW JRH AND SYS CHECKED GOOD. AC PRESSURIZED TO 6 PSID NORMALLY NO FAULTS NOTED. LT FWD PACK VALVE WAS Mar 4, 2010 · N490FE · Boeing 727227 · Cabin Cooling SystemSDR FDEA201002260652Rib · crackedNR 8 SLAT SECOND RIB FROM INBD END IS CRACKED WING STA 355.4. REMOVED DAMAGED RIB, INSTALLED NEW RIB PN 65-17321-4 IAW SRM 51-30-2.Feb 26, 2010 · N482FE · Boeing 727227 · Leading Edge DevicesSDR FDEA201002190498Frame · corrodedAFT CARGO STATION 990 STUB FRAME CORRODED AT STR 29R. CUT OUT DAMAGED AREA IAW SRM 53-10-4 FIG 15 AND 51-10-1. FABRICATED DOUBLER, ANGLE AND SHIM IAW SRM 53-10-4 FIG 15. INSTALLED REAIR PARTS IAW SRM 51-30-2.Feb 19, 2010 · N482FE · Boeing 727227 · Fuselage Main, FrameSDR FDEA201002170441Shear Tie · corrodedAFT CARGO STATION 1110, STRINGER 27L, SHEAR TIE CORRODED. REMOVED SHEAR TIE TEE ANGLE AT BS 1110, STR 27L IAW SRM, REV 102, 51-30-2. FABRICATED REPLACEMENT SHEAR TIE FROM PM60-5632, 7075-T6511, 4.5" LONG IAW DRAWING NR. 65-16346 REV P. INSTALLED SHEAR TIE IFeb 17, 2010 · N482FE · Boeing 727227 · Fuselage Internal Mounting StructureSDR FDEA201002170445Web · crackedCRACK NOTED - RIGHT HAND LOWER TORQUE BOX WEB, RBL 20.5 AT BS 1223. UPPER LIGHTING HOLE, FORWARD OF PREVIOUS REPAIR RIVET LINE. REMOVED PREVIOUS REPAIR DOUBLER AT BS 1223, RBL 20.5 IAW SRM 51-30-2. ROUTED OUT DAMAGED AREA IAW SRM 51-10-1. FABRICATED NEW REPAFeb 17, 2010 · N482FE · Boeing 727227 · Fuselage Main, StructureSDR FDEA201002170444Floorbeam · corrodedAFT CARGO STATION 1070, BOTTOM OF FLOORBEAM, CORROSION AROUND SCREW HOLES. RBL 12-45. CUT OUT 2 DAMAGED AREAS IAW SRM 53-10-8 FIG 8. FABRICATED 2 REPAIR ANGLES AND 2 FILLERS IAW SRM 53-10-8 FIG 8. HEAT TREATED ANGLES TO T6 CONDITION IAW FASI ER 2-37153-801 RFeb 17, 2010 · N482FE · Boeing 727227 · Fuselage Main, Floor BeamSDR FDEA201002170438Floorbeam · damagedELONGATED HOLE MAIN CABIN FLOOR BEAM BS 1110 LBL 45. CUT OUT DAMAGED AREA IAW SRM 53-10-8 FIG 8. FABRICATED 2 ANGLE REPAIRS. IAW SRM 53-10-8 FIG. 8. FABRICATED 2 SHIMS. IAW SRM 53-10-8. FABRICATED CHANNEL. FABRICATED FILLER IAW SRM 53-10-8, 51-10-3, AND 51-Feb 17, 2010 · N482FE · Boeing 727227 · Fuselage Main, Floor BeamSDR FDEA201002160434Skin · damagedEVALUATE TRIM OUT EXTERIOR FUSELAGE LAP SEAM BS 178 STR 18R CUT OUT DAMAGE ON UPPER SKIN 2" X 2 1/8" AND REMOVED FASTENERS COMMON TO REPAIR DOUBLER IAW EA 7-5330-135526, FABRICATED REPAIR PARTS, DOUBLER AND FILLER USING 2024-T3, 0.071" PO NR 9009068 DIMENSION Feb 16, 2010 · N482FE · Boeing 727227 · Fuselage Main, Plate/SkinSDR FDEA201002160539Floorbeam · corrodedCORROSION FLOORBEAM MAIN CABIN BS 560, LBL10 CUT-OUT DAMAGED AREA IAW SRM 53-10-8 FIG 3, FABRICATED CHORD FAB 2 EA SUPPORT ANGLES, FAB 2 EA REINFORCEMENT STRAP IAW SRM 53-10-8 FIG REV 102, INSTALLED FLOORBEAM REPAIR AT BS 560 LBL 10 IAW SRM 51-30-2 REV 102.Feb 16, 2010 · N482FE · Boeing 727227 · Fuselage Main, Floor BeamSDR FDEA201002160437Skin · chafedLT ELEVATOR INSIDE NR 5 BALANCE BAY, GOUGE ON UPPER PANEL, OTBD END. REMOVED DAMAGE BY STOP DRILLING GOUGE ON UPPER PANEL INSIDE NR 5 BALANCE BAY FOR LT ELEVATOR IAW SRM 51-10-1, REV 102. COMPLIED WITH HFEC INSP IAW NDTM 51-00-00, FIGURE 23, WITH NO DEFECTSFeb 16, 2010 · N482FE · Boeing 727227 · Elevator, Plate/SkinSDR FDEA201002150433Structure · crackedLT INBD MID FLAP LOWER AFT CLOSE OUT CHORD WBL 106 IS CRACKED AT ACT ROD CUTOUT. CUT OUT DAMAGED SECTION DIM 47 1/4 " LONG IAW SRM 51-40-4 FIG 1. FABRICATED LOWER CHORD AND SPLICE IAW SRM 51-40-4 FIG 4. LOCATED AND DRILLED HOLES IAW SRM 51-30-5. INSTALLED LOWFeb 15, 2010 · N482FE · Boeing 727227 · Trailing Edge FlapsSDR FDEA201002150432Skin · crackedRT INBD FORE FLAP, STA 224, CRACK ON THE SKIN, L/E, FWD OF ATTACH FITTING. CUT OUT DAMAGED AREA IAW SRM 57-50-4 FIG 1. FABRICATED DOUBLER AND FILLER IAW SRM 57-50-4 FIG 1. INSTALLED DOUBLER AND FILLER IAW SRM 51-30-2.Feb 15, 2010 · N482FE · Boeing 727227 · Trailing Edge FlapsSDR FDEA201002150431Floorbeam · corrodedFWD LAV AREA - CORROSION ON FLOOR SUPPORT ANGLE AT BS 328 FROM BL 0 TO LBL 55, UPPER AND LOWER SURFACES. CUT OUT DAMAGED AREA APPROX DIM 2" IAW SRM 53-10-8 FIG 9. FABRICATED REPAIR FLOORBEAM. FABRICATED ANGLES 2. FABRICATED 2 ANGLES IAW SRM 53-10-8 FIG 9. Feb 15, 2010 · N482FE · Boeing 727227 · Fuselage Main, Floor BeamSDR FDEA201002150430Angle · crackedAFT AIRSTAIRS RT LOWER TORQUE BOX TEE ANGLE CRACKED AT BS 1263, AFT SIDE. REMOVED RT LOWER TORQUE BOX TEE ANGLE IAW SRM, REV 102, 51-30-2. LOCATED, DRILLED AND DEBURRED HOLES ON NEW TEE ANGLE IAW SRM 51-30-5. INSTALLED NEW TEE ANGLE IAW SRM 51-30-2.Feb 15, 2010 · N482FE · Boeing 727227 · Fuselage Miscellaneous StructureSDR FDEA201002130425Door Frame · crackedBS 783, RT OVERWING FRAME, STR 17R, CRACK ORIGINATING FROM FASTENER HOLE. STOP DRILLED CRACK, FABRICATED REPAIR ANGLE, STRAP, SPLICE ANGLE, NEW CHANNEL, AND INSTALLED REPAIR PARTS IAW SRM 51-10-1, SRM 51-30-2, SRM 51-30-5, SRM 51-10-2, ER NR 2-37153-0801 REVFeb 13, 2010 · N482FE · Boeing 727227 · Fuselage Main, StructureSDR FDEA201002130422Seat Track · corrodedCORROSION SEAT TRACK NUMEROUS AREAS MAIN CABIN BS 690 TO BS 720E 10 INCHES, RBL 45. REMOVED SEAT TRACK SECTION IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK, FABRICATED ANGLE SPLICES AND STRAP SPLICES IAW SRM 53-10-5 FIG 1. TREATED AND PRIMED REPAIR PARTS IAW Feb 13, 2010 · N482FE · Boeing 727227 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201002120418Floorbeam · corrodedAFT CARGO, BL 0 FLOORBEAM REPAIR, SCREW HOLES CORRODED, 3EA AT RBL5, STA 1070. REMOVED FLOORBEAM REPAIR LOWER STRAP IAW SRM 51-30-2. FABRICATED NEW STRAP IAW SRM 53-10-8 FIG 2. TREATED AND PRIMED NEW STRAP IAW SRM 51-10-2 INSTALLED NEW STRAP IAW SRM 53-10-Feb 12, 2010 · N482FE · Boeing 727227 · Fuselage Main, Floor BeamSDR FDEA201002120414Web · crackedAFT AIRSTAIR RT LOWER TORQUE BOX WEB IS CRACKED AT UPPER LIGHTING HOLE BS 1243. STOP DRILLED CRACK AT LOWER RIGHT LIGHTING HOLE IAW SRM 51-10-1 AND 51-40-2. COMPLIED WITH HFEC INSPECTION IAW NDTM PT6 51-00-00, FIG. 23, AND VERIFIED CRACK ENDS AT STOP DRILL.Feb 12, 2010 · N482FE · Boeing 727227 · Fuselage Miscellaneous StructureSDR FDEA201002120413Web · crackedAFT AIRSTAIR RT LOWER TORQUE BOX WEB IS CRACKED AT LOWER LIGHTING HOLE BS1223. STOP DRILLED CRACK AT RT LOWER LIGHTING HOLE IAW SRM 51-10-1 AND 51-40-2 FIG 1. HFEC INSP IAW NDTM PT6 51-00-00 FIG 23 VERIFIED CRACK ENDS AT STOP DRILL. FABRICATED NEW DOUBLER IAWFeb 12, 2010 · N482FE · Boeing 727227 · Fuselage Main, StructureSDR FDEA201002120417Support Angle · crackedAFT AIRSTAIR RT LOWER TORQUE BOX, SUPPORT ANGLE IS CRACKED AT FASTENER, BS 1263, ON AFT SIDE. REMOVED RT LOWER TORQUE BOX SUPPORT ANGLE IAW SRM, REV 102, 51-30-2. FORMED SUPPORT ANGLE IAW DWG NR 65-17517. HEAT TREATED GUSSET TO T-6 CONDITION IAW ENGINEERING RFeb 12, 2010 · N482FE · Boeing 727227 · Fuselage Miscellaneous Structure
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