Boeing 727-2B7

Service difficulty reports · 290

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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 = '7272B7'
  ORDER BY difficulty_date DESC"

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SDR DHL2008760529Frame · dentedFABRICATED AND INSTALLED FRAME REPAIR AT BS 640, AND STR 16R, PER B727 SRM 53-10-2 FIG 3 AND SRM 51-40-3 FIG 1.Apr 2, 2008 · N760AT · Boeing 7272B7 · Fuselage Main, FrameSDR DHL2008760528Frame · dentedFABRICATED AND INSTALLED FRAME REPAIR AT BS 600, AND STR 16R, PER B727 SRM 53-10-2 FIG 3 AND SRM 51-40-3 FIG 1.Apr 2, 2008 · N760AT · Boeing 7272B7 · Fuselage Main, FrameSDR DHL2008760527Frame · dentedFABRICATED AND INSTALLED FRAME REPAIR AT BS 580, AND STR 16R, PER B727 SRM 53-10-2 FIG 3 AND SRM 51-40-3 FIG 1.Apr 2, 2008 · N760AT · Boeing 7272B7 · Fuselage Main, FrameSDR DHL2008760526Frame · dentedFABRICATED AND INSTALLED FRAME REPAIR AT BS 540, AND STR 16R, PER B727 SRM 53-10-2 FIG 3 AND SRM 51-40-3 FIG 1.Apr 2, 2008 · N760AT · Boeing 7272B7 · Fuselage Main, FrameSDR DHL2008760525Frame · dentedFABRICATED AND INSTALLED FRAME REPAIR AT BS 520, AND STR 16R, PER B727 SRM 53-10-2 FIG 3 AND SRM 51-40-3 FIG 1.Apr 2, 2008 · N760AT · Boeing 7272B7 · Fuselage Main, FrameSDR DHL2008760510Skin · crackedFABRICATED AND INSTALLED REPAIR DOUBLER AT R/WING NR 6 L/E SLAT O/B HOOK SEAL CUT-OUT, BETWEEN RWS 519 TO 546, PER B727 SRM 57-30-4 FIG 9.Apr 2, 2008 · N760AT · Boeing 7272B7 · Wing, Plate/SkinSDR DHLA200800007Battery · inoperativeFLT 152, EMERGENCY EXIT LIGHTS DON'T WORK. REMOVED AND REPLACED BATTERIES IN FWD AND AFT EMERGENCY EXIT LIGHTS, OPS CHECK GOOD IAW B727 MM 33-50-71, P/N 37067-001 4 EACH. ACFT GROUNDED.Jan 19, 2008 · N762AT · Boeing 7272B7 · Emergency LightingSDR DHLA200800005Light · dislodgedFLT 577, EMERGENCY EXIT LIGHT OVER MAIN ENTRY DOOR FELL OFF DURING TAKEOFF ROLL. REINSTALLED EMERGENCY EXIT LIGHT OVER MAIN ENTRY DOOR. OPS CK. GOOD PER MM 33-50-01. ACFT GROUNDED.Jan 18, 2008 · N762AT · Boeing 7272B7 · Emergency LightingSDR DHLA200700080Switch · malfunctionedAPPROXIMATLY 35 MIN, AFTER TAKEOFF NR 3 ENG OIL PRESSURE/BYPASS LIGHT ILLUMINATED. ABNORMAL PROCEDURE ACCOMPLISHED, DETERMINED THAT BYPASS MODE WAS RESPONSIBLE AND ENGINE WAS SHUT DOWN AT 0835Z. PRESSURE AND QUANTITY WAS NORMAL PRIOR TO SHUT DOWN. WINDMILL Dec 8, 2007 · N762AT · Boeing 7272B7 · Engine Oil Indicating SystemSDR DHL2007770Skin · delaminatedRT WING UPPER SURFACE HAS PANEL O/B OF APU EXH WITH 2 LARGE AREAS OF DELAMINATION APPROX W/S 224 TO 330. TWO AREAS EQUAL TO ABOUT 120 SQ IN.Dec 6, 2007 · N770AT · Boeing 7272B7 · Wing, Plate/SkinSDR DHLA200700059Transmitter · malfunctionedNR 2 ENG OIL TEMP GAGE REDUCED TO 0 DEG ENG OIL PRESS REDUCED TO 20 PSI OIL QUALITY GOOD COMPLETED APPROPRIATE PRECAUTIONARY ENG SHUT DOWN ENG OIL PRESSURE LIGHT FORWARD PANEL DID NOT ILLUMINATE. CK WIRING ON NR 2 ENG OIL TEMP AND OIL PRESSURE, CK WIRING FROMOct 25, 2007 · N770AT · Boeing 7272B7 · Engine Oil Indicating SystemSDR DHLA200700051Engine · malfunctionedREJECTED T/O ELP DUE TO NR 1 ENG PARAMETERS OUT OF NORMAL RANGE VS NR 2 AND NR 3 ENGS GW=147.9, SPEED EST .50 KNOTS, TEMP 29 DEGREES C PA 3950 REVERSE THRUST USED RAN NR 1 AND NR 3 ENG'S AND VERIFIED N1 AND N2 MATCHED. DEFERRED NR 1 ENG EPR GAUGE PER MEL 77-1Oct 4, 2007 · N770AT · Boeing 7272B7 · Engine (Turbine/Turboprop)SDR DHLA200700050Fitting · failedUPON FLAP RETRACTION FROM FLAPS 2 TO 0, SYSTEM A HYD QTY WENT TO 0. FOUND FITTING BLOWN OUT ON NR 7 SLAT SHUTTLE VALVE. REPLACED NR 7 SLAT ACTUATOR SHUTTLE VALVE PER M/M 27-81-71. SERVICED HYDRAULICS TO FULL PER 12-12-0. OPS CHECKS NORMAL.Oct 3, 2007 · N762AT · Boeing 7272B7 · Leading Edge Slat ActuatorSDR DHLA200700036Battery Pack · dischargedEMERGENCY EXIT LIGHTS (BOTH) WOULD NOT WORK DURING STBY TEST. REMOVED AND REPLACED BATTERIES IAW B727 MM 33-50-71, OPS CHECK GOOD.Jul 23, 2007 · N770AT · Boeing 7272B7 · Emergency LightingSDR DHLA200700033Battery · inoperativeDURING STBY PWR CHECK, THE EXIT LIGHTS WOULD NOT ILLUMINATE. REMOVED AND REPLACED FLIGHT COMPT AND MAIN ENTRY DOOR EMERGENCY LIGHT BATTERIES. OPS CHECKS OK IAW 727MM 33-50-71 PN OFF AND ON 37067-001.Jun 28, 2007 · N770AT · Boeing 7272B7 · Emergency LightingSDR DHL2007762502Support Angle · crackedFOUND CRACK IN LT AFT AIR STAIRS TORQUE BOX ON UPPER WEB SUPPORT ANGLE, APPROX BS 1253. MADE TWO EACH CUT OUTS FOR ACCESS, 4 BY 4 AT UPPER WEB IAW B727 SRM 51-10-1. REMOVED CRACKED SUPPORT ANGLE IAW B727 SRM 51-30-2. FABRICATED NEW SUPPORT ANGLE USING 7075TMar 23, 2007 · N762AT · Boeing 7272B7 · Fuselage Miscellaneous StructureSDR DHL2007762501Torque Box · gougedLEFT AFT AIR STAIRS TORQUE BOX LIGHTING HOLE GOUGED BS 1320. ROUTED OUT GOUGED AREA, MATERIAL LOSS .008 IAW B727 SRM 53-30-1 FIG 1. FAB REPAIR DOUBLER 4" BY 2.5" BY .050, 7075T6 IAW B727 SRM 53-10-2 FIG 6 AND 51-40-1, FIG 1. TREATED ALODINE AND PRIMED IAW BMar 23, 2007 · N762AT · Boeing 7272B7 · Fuselage Main, StructureSDR DHL2007760003Line · leakingA ENG 1/2 HYDRAULIC PUMP LOW PRESS LIGHTS ILLUMINATED IN FLT LOSS OF ALL A PRESS AND QUANTITY PERFORMED HYDRAULIC SYSTEM A FAILED ABNORMAL CHECKLIST. FOUND FLEX LINE AT ELEVATOR POWER CONTROL PACKAGE WITH HOLE IN IT REPLACED LINE WITH TEMP (17114-4CR-0240). Jan 24, 2007 · N760AT · Boeing 7272B7 · Aileron Control SystemSDR DHL2006770517Stringer · corrodedBS 950F, STR 29R, OB STR CLIP HAS CORROSION. REMOVED FASTENERS FOR CORROSION REMOVAL IAW SRM 51-30-2. AFTER CORROSION REMOVAL IAW SRM 51-10-6 ON STR CLIP FOUND OUT OF LIMITS IAW SRM 53-10-1 FIG 1. REMOVED DAMAGED STR CLIP IAW SRM 51-30-2. FAB PART FROM 60-Oct 16, 2006 · N770AT · Boeing 7272B7 · Fuselage Main, Longeron/StringerSDR DHL2006770519Tab · delaminatedLT WING, IB AILERON, TAB HAS T/E DAMAGE LWR IB SURFACE. REMOVED TAB IAW MM 27-10-11. CUT OUT DAMAGED AREA ON LWR SURFACE OF AILERON TAB APPOX 4.25 INCH BY 4.25 INCH IAW SRM 51-40-20 AND 51-30-2. FAB FILLER, 4.25 INCH BY 4.25 INCH AND DOUBLER 5.85 INCH BY 6 INOct 11, 2006 · N770AT · Boeing 7272B7 · AileronsSDR DHL2006770514Stringer Splice · corrodedAFT CARGO COMPARTMENT, BS 1138, STR 30, STRINGER CORROSION AT ATTACHMENT POINT C/T SHEAR TIE ANGLE. REMOVED CORROSION ON STR 30 IAW BOEING SRM 51-10-6. STR REMOVAL FOUND TO BE OUT OF LIMITS IAW BOEING SRM 53-10-1 FIG 1. CUT OUT DAMAGED STRINGER IAW BOEING SOct 6, 2006 · N770AT · Boeing 7272B7 · Fuselage Main, Longeron/StringerSDR DHL2006770518Stringer · gougedBS 334, STR 4L HAS DEEP GOUGE ON STRINGER, ABOVE AND AFT OF L1 DOOR EXIT LIGHT. CUT OUT DAMAGED AREA APPROX SIZE 2" LENGTH IAW B727 SRM 53-10-3 FIG 1. FAB REPAIR FILLER FROM BAC 1498-108, PO NR 6408112, APPROX 11 LONG IAW B727 SRM 53-10-3 FIG 1 AND 53-10-2 FOct 2, 2006 · N770AT · Boeing 7272B7 · Fuselage Main, Longeron/StringerSDR DHL2006770513Stringer · gougedBS 334, STR 4L HAS DEEP GOUGE ON STRINGER, ABOVE AND AFT OF L1 DOOR EXIT LIGHT. CUT OUT DAMAGED AREA APPOX SIZE 2 INCHES LENGTH IAW SRM 53-10-3 FIG.1. FAB REPAIR FILLER FROM BAC 1498-108, PO NR 6408112, APPOX 1 LONG IAW SRM 53-10-3 FIG.1 AND 53-10-2 FIG.9. Oct 2, 2006 · N770AT · Boeing 7272B7 · Fuselage Main, Longeron/StringerSDR DHL2006513Stringer · gougedASTAR NR 111564, DISCREPANCY: BS 334, STR 4L HAS DEEP GOUGE ON STRINGER, ABOVE AND AFT OF L1 DOOR EXIT LIGHT. CUT OUT DAMAGED AREA APPOX SIZE 2 INCH LENGTH IAW SRM 53-10-3 FIG.1. FAB REPAIR FILLER FROM BAC 1498-108, PO NR 6408112, APPOX 1 LONG IAW SRM 53-10-Oct 2, 2006 · N770AT · Boeing 7272B7 · Fuselage Main, Longeron/StringerSDR DHL2006770507Frame · dentedAFT CARGO COMPARTMENT, BS 1130 OVER STR 26R HAS FRAME WITH UPPER CHORD DENTED IN. CUT OUT DAMAGED AREA APPROX SIZE 1.875" BY 1.0" IAW B727 SRM 51-40-3 FIG 1. FAB DOUBLER REPAIR WITH 7075-0, .071, SIZE 8" BY 4", PO NR 9003817 IAW B727 SRM 53-10-2 FIG 3 AND 51Oct 2, 2006 · N770AT · Boeing 7272B7 · Fuselage Main, FrameSDR DHL2006770508Frame · corrodedAFT CARGO COMPARTMENT, BS 970, BETWEEN STR 28R AND 29R, FRAME LWR FLANGE BLOWN-UP WITH CORROSION. REMOVED FLOOR SUPPORT, VERTICAL STIFFENERS AND ANGLES FOR ACCESS IAW B727 SRM 51-30-2. CUT OUT DAMAGED AREA AT LWR FRAME FLANGE IAW B727 SRM 53-10-4 FIG 11. FAOct 2, 2006 · N770AT · Boeing 7272B7 · Fuselage Main, FrameSDR DHL2006760005Stringer · corrodedBROKEN RIVET HEAD ON RT FUSELAGE SKIN BS 445, STR 24R. CUT OUT DAMAGED SECTION OF STRINGER 11 INCHES, FABRICATED FILLER SECTION (11 INCHES), P/N 65-56236-6, PO 6348150 AND 2 EA SPLICE, BAC 1498-138, PO 6260178, (13 INCHES) IAW B727 SRM 53-10-3 FIG 1 AND 53-10Oct 2, 2006 · N760AT · Boeing 7272B7 · Fuselage Main, Longeron/StringerSDR DHL2006760004Skin · corrodedPILLOWING FASTENERS ON RIGHT FUSELAGE SKIN BS 990 STR 27R. REMOVED FLOORBOARD FROM BS 950E TO 990 IAW B727 SRM 51-30-2 FIG 15. REMOVED 3 EA FLOOR SUPPORT FOR ACCESS IAW B727 SRM 51-30-2. FOUND AREA WITH CORROSION OUT OF LIMITS IAW B727 SRM 53-30-1. CUT OUTOct 1, 2006 · N760AT · Boeing 7272B7 · Fuselage Main, Plate/SkinSDR DHL2006760003Stringer · corrodedFUSELAGE SKIN AT BS 1053, STR 30 HAS A BULGE BETWEEN AND AT FASTENERS. CLEANED AREA IAW B727 MM 12-40-0, EVAL AREA, FOUND STRINGER DAMAGED BEYOND ALLOWABLE LIMITS OF B727 SRM 53-10-1 FIG 1. CUT OUT DAMAGED SECTION, DIM 13 INCHES IAW B727 SRM 53-10-3 FIG 1, FOct 1, 2006 · N760AT · Boeing 7272B7 · Fuselage Main, Longeron/StringerSDR DHL2006770511Stringer · corrodedDISCREPANCY: FORWARD CARGO COMPARTMENT, BS 660, STR 28L, CORROSION ON STR 28L. REMOVED CORROSION AT STR, MATERIAL LOSS IS .022, ORIGINAL MATERIAL THICKNESS .063 AND MATERIAL REMAINING .041. FOUND TO BE OUT OF LIMITS IAW B727 SRM 53-10-1 FIG.1. CUT OUT DAMAGED Sep 30, 2006 · N770AT · Boeing 7272B7 · Fuselage Main, Longeron/StringerSDR DHL2006770506Frame · dentedFORWARD CARGO COMPARTMENT, BS 720C, STR 26R, DENT IN FRAME RADIUS. CUT OUT DAMAGED AREA SIZE 1.50 INCH BY 1.50 INCH IAW SRM 51-40-3 FIG 1. FAB DOUBLER WITH 7075-0, .071, SIZE 15 INCHES BY 4 INCHES, PO NR 9003817 IAW SRM 53-10-2 FIG.3 AND 51-40-3 FIG.1. HEAT TSep 30, 2006 · N770AT · Boeing 7272B7 · Fuselage Main, FrameSDR DHL2006770504Frame · dentedFORWARD CARGO COMPARTMENT, BS 660, STR 27R, DENT IN FRAME RADIUS. CUT OUT DAMAGED AREA SIZE 1.25" BY 1.625" IAW B727 SRM 51-40-3 FIG 1. FAB DOUBLER WITH 7075-0, .071, SIZE 15" BY 4", PO NR 9003817 IAW B727 SRM 53-10-2 FIG 3 AND 51-40-3 FIG 1. HEAT TREATED DSep 30, 2006 · N770AT · Boeing 7272B7 · Fuselage Main, FrameSDR DHL2006770510Frame · dentedFORWARD CARGO COMPARTMENT BS 680, STR 26R, DENT IN FRAME RADIUS. CUT OUT DAMAGED AREA IAW SRM 51-40-3 FIG.1. FABRICATED DOUBLER IAW SRM 53-10-2 FIG.3 AND 51-40-3 FIG.1. HEAT TREATED DOUBLER IAW ENGINEERING REPORT NR 2-37153-801 REV.IR. INSTALLED REPAIR PARTS Sep 30, 2006 · N770AT · Boeing 7272B7 · Fuselage Main, FrameSDR DHL2006770505Stringer · corrodedFORWARD CARGO COMPARTMENT, BS 660, STR 28L, CORROSION ON STR 28L. REMOVED CORROSION AT STR, MATERIAL LOSS IS .022, ORIGINAL MATERIAL THICKNESS .063 AND MATERIAL REMAINING .041. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1 FIG.1. CUT OUT DAMAGED APPOX 16 INCHES. Sep 30, 2006 · N770AT · Boeing 7272B7 · Fuselage Main, Longeron/StringerSDR DHL2006770503Frame · dentedFORWARD CARGO COMPARTMENT BS 680, STR 26R, DENT IN FRAME RADIUS. CUT OUT DAMAGED AREA IAW B727 SRM 51-40-3 FIG 1. FAB DOUBLER WITH 7075-0, .071, SIZE 15 INCHES BY 4 INCHES, PO 9003817 IAW B727 SRM 53-10-2 FIG 3 AND 51-40-3 FIG 1. HEAT TREATED DOUBLER FROM 7Sep 30, 2006 · N770AT · Boeing 7272B7 · Fuselage Main, FrameSDR DHL2006770515Floorbeam · corrodedLOWER LOBE AND WALKWAY BEAM LT SIDE, BS 294, CORROSION ON CHORD. REMOVED, FAB AND REPLACED CORRODED STIFFENER FROM P/N BAC 1505-29222, PO NR 9003865, IAW SRM 51-30-2, 51-30-5, 53-10-2 FIG 1 AND 51-20-1 FIG2. CUT OUT DAMAGED WEB AND FAB DOUBLER FROM 2024-0, .Sep 28, 2006 · N770AT · Boeing 7272B7 · Fuselage Main, Floor BeamSDR DHL2006770512Skin · corrodedASTAR NR# 111321, FUSLAGE SKIN EXTERIOR BS 1030 TO 1050, SURFACE CORROSION UNDER VHF3 ANTENNA. REMOVED SUPPORT ANGLES AND ANTENNA HARDWARE IAW B727 SRM 51-30-2, FIG 7. EVAL "U" CHANNEL FOUND OUT OF LIMITS DUE TO CORROSION IN HOLES IAW B727 SRM 51-10-2, FIG 1. Sep 28, 2006 · N770AT · Boeing 7272B7 · Fuselage Main, Plate/SkinSDR DHL2006770502Skin · delaminatedLEFT INBOARD FORE-FLAP, INBOARD LWR SURFACE DELAMINATED. CUT OUT DELAMINATED AREA ON LEFT INBOARD FOREFLAP, LWR SURFACE APPOX 5 INCHES BY 13 INCHES. FAB FILLER APPROX 5 INCHES BY 13 INCHES AND DOUBLER APPROX 3 INCHES BY 15 INCHES FROM 2024-T3, .016, PO 90031Sep 28, 2006 · N770AT · Boeing 7272B7 · Trailing Edge FlapsSDR DHL2006770501Attach Angle · crackedASTAR NR 111384: LT IB MID FLAP T/E LOWER STRUCTURE, WBL 70 TO 134 IS CRACKED FOUR PLACES IN CUT OUTS. CUT OUT DAMAGED AREA IAW SRM 51-30-2 AND 51-40-3, FIG.1. FAB NEW FROM AC 1003-100046-7075-T6, SIZE 68.75 INCH PO NR 6295115 AND ONE SPLICE WITH AC 1003-100Sep 28, 2006 · N770AT · Boeing 7272B7 · Trailing Edge FlapsSDR DHL2006770516Skin · dentedAFT AIRSTAIRS SKIN , BS 1263, STR 26R, DENT CLUSTER. EVALUATED DENTS, RATIOS ARE A: .30 AND Y: .008 A/Y: 37.5, A: .50, Y: .016, A/Y: 31.3, DENTS ARE WITHIN ALLOWABLE LIMITS IAW SRM 52-00-2 AND 53-10-1 FIG 1. ONE DENT FOUND OUT OF LIMITS, DIM., A: .70 , Y: .Sep 26, 2006 · N770AT · Boeing 7272B7 · Fuselage Main, Plate/SkinSDR DHL2006770509Stringer Splice · corrodedNR 111153, PILLOWING RT FUSELAGE SKIN BETWEEN STA.1110 AND STA.1130, STR.30. CUT OUT DAMAGED AREA APPOX 2.75 INCH IAW SRM 53-10-3 FIG.1. FAB REPAIR SPLICE FROM P/N BAC 1498-131, PO NR 9003866 AND FILLER FROM P/N BAC1498-131, PO NR 9003866, APPOX 2.75 INCH IAWSep 26, 2006 · N770AT · Boeing 7272B7 · Fuselage Main, Longeron/StringerSDR DHL2006770500Stringer Splice · corrodedASTAR NR 111153, PILLOWING RT FUSELAGE SKIN BETWEEN STA.1110 AND STA.1130, STR.30. CUT OUT DAMAGED AREA APPOX 2.75 INCH IAW SRM 53-10-3 FIG.1. FAB REPAIR SPLICE FROM P/N BAC 1498-131, PO NR 9003866 AND FILLER FROM PN BAC1498-131, PO NR 9003866, APPOX 2.75 INCSep 26, 2006 · N770AT · Boeing 7272B7 · Fuselage Main, Longeron/StringerSDR DHL2006770005Light · dislodgedEMERGENCY EXIT LIGHT OVER COCKPIT DOOR FELL OFF. RESECURED EMERGENCY EXIT LIGHT OVER COCKPIT DOOR AND OPS CKS GOOD IAW MM 33-50-91Sep 13, 2006 · N770AT · Boeing 7272B7 · Emergency LightingSDR DHL2006770004Warning Light · activatedESSENTIAL POWER FAIL LIGHT ILLUMINATED ON TAKEOFF. ABORTED TAKEOFF, -UNDER EXCITED SYSTEM 3- ON ELECTRICAL FAULT PANEL. TRANSFER TO DMI 26183 IAW MEL 24-1 CAT B DUE DATE 8-8-06, COMPLIED WITH PLACARDS INSTALLED. REF.DMI#26183 "ESSENTIAL POWER LIGHT NR 3 UAug 5, 2006 · N770AT · Boeing 7272B7 · AC Indicating SystemSDR DHL2006762511Seat Track · corrodedFOUND CABIN SEAT TRACK HAS CORROSION AT BS 650 LBL 45. REMOVED CORROSION AT MAIN CABIN SEAT TRACK BS 650 LBL 45, CORROSION IS OUT OF LIMITS IAW B727 SRM 51-10-1 AND 53-10-1 FIG 4. REMOVED SEAT TRACK FROM BS 620-710 LBL 45 IAW B727 SRM 51-30-2. FAB NEW SEAT Jul 12, 2006 · N762AT · Boeing 7272B7 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2006762512Seat Track · corrodedFOUND CABIN SEAT TRACK RBL 24 HAS CORROSION AT BS 480-620. REMOVED FLOORBOARDS FROM BL 0 - RBL 24 STA 480-690 IAW B727 SRM 51-30-2. REMOVED SEAT TRACK AT RBL 24 STA 480-660 IAW B727 SRM 51-30-2. FAB NEW SEAT TRACK OF BAC1520-792 DIM 17.5' PO NR 9003095 IAW Jul 8, 2006 · N762AT · Boeing 7272B7 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2006762510Seat Track · corrodedCABIN SEAT TRACK LBL 24 HAS CORROSION AT BS 480-620. REMOVED FLOORBOARDS FROM BL 0 TO LBL 45 FOR ACCESS IAW SRM 51-30-2, BS 480-690 SEAT TRACK CORROSION FOUND OUT OF LIMIT IAW SRM 51-10-1 & SRM 53-10-1 FIG. 4. REMOVED SEAT TRACK LBL24 BS 480-690 IAW SRM 51-30-Jul 8, 2006 · N762AT · Boeing 7272B7 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2006762508Mount · crackedNR 5 LE FLAP INBD ACTUATOR MOUNT BRACKET IS CRACKED BY THE LWR CORNER. REMOVED NR 5 LE FLAP ACTUATOR MOUNT WEB IAW B727 SRM 51-30-2. FAB NEW I/B MOUNT WEB IAW DWG NR 65-16263. TREATED AND PRIMED WEB MOUNT AND WORKING AREA IAW B727 SRM 51-10-2. INSTALLED I/Jul 6, 2006 · N762AT · Boeing 7272B7 · Wing, Attach FittingsSDR DHL2006762515Seat Track · corrodedCABIN SEAT TRACK HAS CORROSION AT BS 480-620 RBL 45" BALL MAT AREA. REMOVED CABIN FLOORBOARDS RBL 24-RBL 65 FOR ACCESS IAW B727 SRM 51-30-2. REMOVED SEAT TRACK RBL 45 STA 480-620 FOR REPAIR, CORROSION WAS FOUND OUT OF LIMITS IAW B727 SRM 51-30-2 AND SRM 53-1Jun 30, 2006 · N762AT · Boeing 7272B7 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2006762501Frame · crackedNR 6 SLAT AT ACT ROD END ATTACHMENT WS 515 HAS BOTH I/B & O/B FRAMES CRACKED FWD. REMOVED I/B & O/B NR 6 SLAT FRAMES AT WS 515 IAW B727 SRM 51-30-2, FAB NEW I/B & O/B FRAMES FROM 20024-0 .040 PO 9003230 DIM. FOR BOTH FRAMES 6 X 16 INCHES IAW B727 SRM 57-50-2Jun 30, 2006 · N762AT · Boeing 7272B7 · Leading Edge Devices
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