Boeing 727-214

Service difficulty reports · 296

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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 = '727214'
  ORDER BY difficulty_date DESC"

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SDR DHL2007785007Shear Tie · corrodedSURFACE CORROSION ON FORWARD PIT SHEAR TIE BS 520 BETWEEN STRINGER 28L AND 28R. REMOVED FASTENERS IN AREA TO GAIN ACCESS IAW B-727 SRM 51-30-2. REMOVED CORROSION IAW B-727 SRM 51-10-6, FOUND OUT OF LIMITS IAW B-727 SRM 53-10-1 FIGURE 1. FABRICATED SHEAR TIEOct 17, 2007 · N785AT · Boeing 727214 · Fuselage Internal Mounting StructureSDR DHL2007785011Frame · gougedC-1 DOOR CUT OUT AFT FRAME BS 620, WEB HAS DEEP GOUGE ON THE FORWARD SURFACE BETWEEN STRINGER 26R AND 27R. BLEND OUT AREA IAW B-727 SRM 51-10-1. OUT OF LIMITS IAW B-727 SRM 53-10-1 FIGURE 1 AND 53-10-2 FIGURE 3. REMOVED FASTENERS FROM AREA IAW B-727 SRM 51-Oct 17, 2007 · N785AT · Boeing 727214 · Fuselage Main, FrameSDR DHL2007785009Shear Tie · corrodedSURFACE CORROSION ON FORWARD PIT SHEAR TIE BS 520 BETWEEN STRINGER 28L AND 28R. REMOVED FASTENERS IN AREA TO GAIN ACCESS IAW B-727 SRM 51-30-2. REMOVED CORROSION IAW B-727 SRM 51-10-6, FOUND OUT OF LIMITS IAW B-727 SRM 53-10-1 FIGURE 1. FABRICATED SHEAR TIEOct 17, 2007 · N785AT · Boeing 727214 · Fuselage Internal Mounting StructureSDR DHL2007785049Seat Track · corrodedMAIN CABIN SEAT TRACKS LBL 45 BS 480-BS 690 HAVE LIGHT CORROSION. REMOVED CABIN FLOOR PANELS BETWEEN BS 480 AND 700 LBL 22 LBL65-LBL22 FOR ACCESS IAW B-727 MM 53-30-11. REMOVED SEAT TRACK OUT OF LIMITS FROM BS 480 TO 700 LBL45 IAW B-727 SRM 51-30-2. FABRICAOct 16, 2007 · N785AT · Boeing 727214 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2007785024Skin · damagedRIGHT FUSELAGE UPPER SKIN HAS LIGHTNING STRIKE AT BS 700 + 8" STRINGER 9R. BLEND OUT DAMAGE IAW B-727 SRM 53-30-2 FIGURE 2 AND 53-30-1 FIGURE 1 AND 2. CUT OUT DAMAGED AREA (DIMENSION .875" DIAMETER) AND FABRICATED REPAIR DOUBLER FROM 2024-T3 0.063" PO NR 900Oct 15, 2007 · N785AT · Boeing 727214 · Fuselage Main, Plate/SkinSDR DHL2007785030Skin · bulgedVERTICAL STABILIZER RIGHT SIDE ABOVE UPPER RUDDER HAS BULGING SKIN (FIN WL 168 AT FIN STA 305). CUT OUT DAMAGE AREA AND FABRICATED REPAIR DOUBLER AND REPAIR FILLER IAW B-727 SRM 55-30-3 FIGURE 6 AND 55-30-2 FIGURE 1. TREATED AND PRIMED PARTS IAW B-727 SRM 51Oct 12, 2007 · N785AT · Boeing 727214 · Vertical Stabilizer, Plate/SkinSDR DHL2007785023Skin · damagedSCRATCH ON UPPER FUSELAGE SKIN BS 1090 STRINGER 4R TO STRINGER 5R. BLENDED OUT DAMAGE AREA IAW B-727 SRM 51-10-4. FOUND OUT OF LIMITS IAW B-727 SRM 53-30-2 FIGURE 2 AND 53-30-1 FIGURE 1 AND 2. DISPLACED GILLINER CABIN LINER FOR ACCESS BETWEEN BS 1030 AND BSOct 11, 2007 · N785AT · Boeing 727214 · Fuselage Main, Plate/SkinSDR DHLA200700054Skin · damagedDURING PUSHBACK TOWBAR BROKE AND A/C HIT TUG. REPAIRED DAMAGED SKIN AREA IAW BOEING 727 SRM 53-30-03. REPLACED 2 INTERCOSTALS IAW BOEING 727SRM 51-30-02. FABRICATED INTERCOSTALS PER BOEING DWG 69-16996.Oct 10, 2007 · N788AT · Boeing 727214 · Fuselage Main, Plate/SkinSDR DHL2007785006Radome · crackedAT COMPLETION OF PUSH BACK, GROUND CREW UNABLE TO REMOVE TOW BAR. WHEN TOW BAR RELEASED, WITH PARKING BRAKE SET, ACFT MOVED FORWARD. VISIBLE DAMAGE NOTED TO RADOME ASSY.Aug 25, 2007 · N785AT · Boeing 727214 · Aerodynamic FairingsSDR GAIA07012OPLight · inoperativeDURING PS CHECK, FOUND CONTROL CABIN EMERGENCY EXIT LIGHT WOULD STAY ON WITH THE SWITCH IN THE OFF POSITION. REMOVED AND REPLACED EMERGENCY EXIT LIGHT. OPS CHECK NORMAL. AIRCRAFT WAS RETURNED TO SERVICE. (M)Aug 2, 2007 · N751US · Boeing 727214 · Emergency LightingSDR GAIA0711OPFire Detector · false indicationFLT 706 - DFW-IAH - DURING CLIMB, THE FLIGHT CREW HAD AN INDICATION OF AN APU FIRE. THE APU FIRE HANDLE WAS PULLED AND THE FIRE BOTTLE WAS DISCHARGED. THE AIRCRAFT CONTINUED TO IAH AND AN UNEVENTFUL LANDING WAS MADE. INSPECTED APU AREA AND FOUND NO EVIDENCEAug 2, 2007 · N750US · Boeing 727214 · Fire DetectionSDR DHL2007785005Support Fitting · crackedNR 8 SPOILER ACTUATOR SUPPORT FITTING IS CRACKED. REMOVED FITTING AND REPLACED WITH NEW FITTING PER B727 SRM 51-30-2 FIG 1, FIG 15, AND B727 MM 27-61-91.Jun 27, 2007 · N785AT · Boeing 727214 · Wing, Attach FittingsSDR DHL2007785004Spar · crackedRIGHT WING T/E AT RWBL 120, HAS A 1.5" CRACK IN RADIUS OF FALSE SPAR LOWER CHORD ANGLE. CUT OUT DAMAGED CHORD AND WEB SECTIONS, FABRICATED NEW WEB SECTION FROM 7075-T6, .032" BY 12" BY 9.5", PO NR 9003458; REPAIR DOUBLER FROM 2024-T3, .050" BY 11" BY 12", POJun 27, 2007 · N785AT · Boeing 727214 · Wing SparSDR DHL2007785003Beam · crackedRT WING T/E UPPER EXTRUDED "I" BEAM HAS A .375" CRACK AT RWBL 114. ROUTED OUT CRACK; MATERIAL REMOVED BEYOND SERVICE LIMITS PER B727 SRM 57-20-1 FIG 2. REMOVED "I" BEAM, FABRICATED NEW BEAM FROM BAC1506-1659 EXTRUSION, 85.5" IN LENGTH, PO NR 72485, PER B727 Jun 27, 2007 · N785AT · Boeing 727214 · Wing Main, Frame StructureSDR DHL2007785002Web · crackedWHILE IN "A" CHECK, CRACK ON AFT AIRSTAIR AREA TORQUE BOX WEB AT LIGHTENING HOLE BS 1303. STOP DRILLED CRACK IAW B727 SRM 51-10-1 PARA 10. FAB REPAIR DOUBLER FROM 7075T6 .040 PO NR 9004940 APPROX DIM 4" BY 2" IAW B727 SRM 51-40-2 FIG 1 AND 53-10-2 FIG 6. IMay 19, 2007 · N785AT · Boeing 727214 · Fuselage Main, StructureSDR DHL2007785001Skin · chafedWHILE IN "A" CHECK, RT INBD TE FLAP PREVIOUS REPAIR HAS CHAFFING ON LE OF FOREFLAP. REMOVED PREVIOUS REPAIR IAW B727 SRM 51-30-2. FABRICATED NEW DOUBLER FROM 2024T3 .063 PO NR 9005138 DIM 5 1/4" BY 4 1/4' IAW B727 SRM 57-50-04 FIG 1 AND 57-50-2 FIG 3. TREATMay 19, 2007 · N785AT · Boeing 727214 · Trailing Edge FlapsSDR DHL2007788526Nose Cowl · wornWHILE IN C CHECK AT FLIGHT STAR, NR 1 ENG NOSE COWLING 9:00 POS AFT END COWLING FAYING SURFACE IS WORN AWAY AND KNIFE EDGED. CUT OUT DAMAGED AREA ON NR 1 ENGINE NOSE COWLING AFT END 9:00 POSITION IAW B727 SRM 54-10-03 FIG3. CUTOUT AREA 5" BY 75", FABRICATED May 18, 2007 · N788AT · Boeing 727214 · Nacelle/Pylon, Main FrameSDR DHL2007788525Skin · gougedWHILE AT C CHECK AT FLIGHTSTAR, RT I/B FORE FLAP I/B UPPER SURFACE GOUGED. REMOVED DAMAGED AREA 5" DIA CLEANED AND PREPPED REPAIR AREA, FABRICATED FILLER 5" AND DOUBLER 8" FROM .016" 2024-T3 PO NR 9003189 ALODINED, PRIMED AND APPLIED ADHESIVE FILM IAW B727 SRMay 17, 2007 · N788AT · Boeing 727214 · Trailing Edge FlapsSDR DHL2007788528Skin · dentedWHILE IN "C" CHECK, 3 DENTS ON R/W I/B AFT FLAP UPPER SURFACE 31", 55", AND 82" FROM I/B END. EVALUATED 3 DENTS AT 31" A=1.5, Y=.032, A/Y=46.37. 55" A=1.5", Y=.038, A/Y=39.47. 82" A=1.8, Y=.028, A/Y=64.28. AREA FOUND WITHIN LIMITS IAW B727 SRM 53-10-1 FIG 1.May 10, 2007 · N788AT · Boeing 727214 · Trailing Edge FlapsSDR DHL2007788517Skin · crackedRT IB AFT FLAP IS CRACKED 3 PLACES. CUT OUT 3 CRACKED AREAS ON RT IB AFT FLAP UPPER SKIN (1) 1.2" DIA. (2) 1" DIA (3) 1.8" DIA. CUTOUT 2 DELAMINATED AREAS ON LOWER SKIN (1) 8" BY 8" (2) 8 1/2" BY 23". FABRICATED UPPER DOUBLERS (1) 4.2" DIA (2) 4" DIA. (3) 4May 9, 2007 · N788AT · Boeing 727214 · Trailing Edge FlapsSDR GAI2007F00001Connector · dirty(REF NR: GAIA 07-05 OP) DURING CLIMB THE FLIGHT CREW RETRACTED THE FLAPS NORMALLY HOWEVER, AT ZERO DEGREES FLAPS THE AMBER LIGHT REMAINED ILLUMINATED ON THE FRONT PANEL. FE PANEL INDICATED NR 4 SLAT EXTENDED. FOLLOWED OPS PROCEDURE AND CYCLED FLAPS WITH SAMEMay 4, 2007 · N750US · Boeing 727214 · Flight Control System WiringSDR DHL2007788510Stringer · corrodedEXFOLIATION ON STRINGER 27R STA 510. CUT OUT DAMAGED AREA OF STR 27R 7 INCHES IN LENGTH IAW B727 SRM 53-10-3, FIG 1. FABRICATED STRINGER FILLER FROM 7075T6, 7" BY.040", CHORD FROM BAC 1493-412-7075T6, 15 INCHES LONG TWO EACH, ANGLE FROM BAC 1498-140-7075T6,May 4, 2007 · N788AT · Boeing 727214 · Fuselage Main, Longeron/StringerSDR DHL2007788511Skin · delaminatedLEFT WING INBD FORE FLAP, LWBL 74 UPPER SURFACE DELAMINATED AT EXISTING REPAIR. REMOVED DELAMINATED AREA 2.5" BY 7" CLEANED AND PREPPED AREA TO BOND IAW B727 SRM 51-40-20, PAR 7, FIG 3. FABRICATED DOUBLER 10" BY 5.7" AND FILLER 2.5" BY 7" FROM .016, 2024T3, May 3, 2007 · N788AT · Boeing 727214 · Trailing Edge FlapsSDR DHL2007788516Skin · delaminatedLT OB AILERON TAB HAS AREA OF DELAMINATION AT OB END UPPER SURFACE. CUTOUT DELAMINATED AREA ON LT OB AILERON TAB UPPER OB END APPROX 1" BY 3 1/2". FABRICATED FILLER APPROX 1" BY 3 1/2" AND DOUBLER APPROX 2 1/2" BY 5" FROM 2024T3 PO NR 9003621. CLEANED, PREPMay 1, 2007 · N788AT · Boeing 727214 · AileronsSDR DHL2007788515Door Frame · corrodedC2 DOOR CUTOUT AFT FRAME INNER CHORD IS CHORDED WITH EXFOLIATION BETWEEN STR 25R-26R. CUTOUT DAMAGED AREA IAW AD39-53-101 IR. FABRICATED NEW STRAP, FILLER, AND TWO ANGLES IAW DWG AD39-53-101IR. TREATED AND PRIMED ALL REPAIR PARTS AND AREA IAW B727 SRM 51-10Apr 29, 2007 · N788AT · Boeing 727214 · Fuselage Main, StructureSDR DHL2007788512Skin · delaminatedLEFT WING, INBD FORE FLAP LOWER SURFACE DELAMINATED AT LWBL 125. CUT OUT DELAMINATED AREA 8.4" BY 9.4" CLEANED AND PREPPED AREA TO BOND IAW B727 SRM 51-40-20, PAR 7, FIG 3 AND 51-40-24, FIG 1. FABRICATED DOUBLER 10" BY 12.4" AND FILLER 8.4" BY 9.4" FROM .016Apr 29, 2007 · N788AT · Boeing 727214 · Trailing Edge FlapsSDR GAI2007F00000Torque Box · crackedDURING INSPECTION IT WAS DISCOVERED THAT THE AFT AIRSTAIRS WOULD NOT TRAVEL TO THE FULLY CLOSED POSITION. FURTHER INSPECTION FOUND A CRACK IN SECTION 48 LOWER AFT TORQUE BOX BY THE AIRSTAIR ACTUATOR FITTING. THE CRACK WAS REPAIRED IAW SB 727-53-0129. THE AIApr 27, 2007 · N750US · Boeing 727214 · Fuselage Main, StructureSDR DHL2007788522Cargo Track · corrodedMAIN CARGO DECK SEAT TRACK BBL 24L FROM BS 790 - 840 SHOWS CORROSION. FOUND SEAT TRACK CORRODED OUT OF LIMITS IAW B727 SRM 53-10-1 FIG 3. REMOVED SEAT TRACK SECTION AT MAIN CARGO DECK STA 759.45L - 852.45L BBL24L IAW B727 SRM 51-30-2. FABRICATED NEW SEAT TRApr 24, 2007 · N788AT · Boeing 727214 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2007788514Skin · delaminatedLEFT WING, INBD FORE FLAP, LOWER SURFACE NEAR TRACK FITTING, LWBL 90, AREA DELAMINATED. CUT OUT DELAMINATED AREA 13" BY 15.5" FABRICATED FILLER, 13" BY 15.5" AND DOUBLER, TWO EACH, 3" BY 15.5" FROM .016, 2024T3. ANODIZED, PRIMED AND APPLIED ADHESIVE FILM IAWApr 24, 2007 · N788AT · Boeing 727214 · Trailing Edge FlapsSDR DHL2007788507Seat Track · corrodedMAIN CARGO DECK, SEAT TRACK LBL 45L, FROM BS 850 TO 950C, SURFACE CORROSION, STA 868 TO 950C REMOVED .009 MATERIAL, ORIGINAL MATERIAL THICKNESS .230, MATERIAL REMAINING .221 WITHIN LIMITS IAW B727 SRM 53-10-1, FIG 3. TREATED AND PRIMED AREA IAW B727 SRM 51-10Apr 24, 2007 · N788AT · Boeing 727214 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2007788508Seat Track · corrodedMAIN CARGO DECK, SEAT TRACK LBL 45L, AT 750F, SURFACE CORROSION. REMOVED SEAT TRACK BS 690 TO 740 IAW B727 SRM 51-30-2. FABRICATED TWO NEW SEAT TRACKS FROM BAC 1520-792-7178T6511, 7'.8" LONG AND 6'.8" LONG AND TWO ANGLES FROM BAC 1503-100122-7178T6311, 1'.2"Apr 24, 2007 · N788AT · Boeing 727214 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2007788501Skin · gougedRIGHT WING, INBD FOREFLAP, INBD UPPER SURFACE GOUGED, WS 198, RWBL 84. REMOVED DAMAGED AREA APPROX 5" DIA IAW B727 SRM 51-40-20,PAR 7, FIG 3. FABRICATED FILLER 5" DIA AND DOUBLER 8" DIA FROM 2024T6 IAW B727 SRM 51-40-24, FIG 1 AND 57-50-2 FIG 3. CLEANED, PRApr 24, 2007 · N788AT · Boeing 727214 · Trailing Edge FlapsSDR DHL2008788501Skin · gougedRIGHT WING, INBD FOREFLAP, INBD UPPER SURFACE GOUGED, WS 198, RWBL 84. REMOVED DAMAGED AREA APPROX 5" DIA IAW B727 SRM 51-40-20, PAR 7, FIG 3. FABRICATED FILLER 5" DIA AND DOUBLER 8" DIA FROM 2024T6 IAW B727 SRM 51-40-24, FIG 1 AND 57-50-2 FIG 3. CLEANED, PApr 24, 2007 · N788AT · Boeing 727214 · Trailing Edge FlapsSDR DHL2007788513Skin · delaminatedRIGHT WING, LWS 383.5, L/E SLAT AERO FENCE, LOWER AFT COMPOSITE SURFACE AREA IS CRACKED, LAYERS ARE SPLITTING. SANDED, CLEANED AND PREPPED 9" BY 5" DAMAGED AREA IAW B727 SRM 51-40-9, PAR 4, FIG 1. FABRICATED, IMPREGNATED (7781-50) FIBERGLASS AND 50A RESIN. Apr 23, 2007 · N788AT · Boeing 727214 · Leading Edge DevicesSDR DHL2007788505Skin · crackedRIGHT WING FIXED L/E NR 5 SLAT, INBD TRACK CUTOUT FOR SLAT TRACK SEAL, AFT INBD RADIUS, .5"-.75" LONG CRACK W/S 383.5. CUTOUT DAMAGED AREA 7" BY 2.25" IAW B727 SRM 57-30-4. FABRICATED NEW DOUBLER 7" BY 5.375 BY .040, 301 1/2 HARD AND FILLER 7" BY 2.25 BY .04Apr 23, 2007 · N788AT · Boeing 727214 · Wing, Plate/SkinSDR DHL2007788506Skin · gougedLEFT W/S 464, OUTBD FOREFLAP, INBD L/E AT PREVIOUS REPAIR DOUBLER GOUGED. REMOVED GOUGED DOUBLER IAW B727 SRM 51-30-2. FABRICATED REPAIR DOUBLER 5" BY 6" BY .063 FROM 2024T3 AND FILLER 2.20" BY 1.90" BY .063 FROM 2024T3 IAW B727 SRM 57-50-4, FIG 4. TREATED Apr 21, 2007 · N788AT · Boeing 727214 · Trailing Edge FlapsSDR DHL2007788502Stringer · corrodedFWD LWR CARGO COMPARTMENT BS 700-720, STR 28L CORROSION ON STR. CUTOUT DAMAGED STR APPROX 30.25" LONG IAW B727 SRM 53-10-3 FIG 1. FABRICATED REPAIR PARTS, 2 HAT SECTIONS 12" AND 18.25" LONG FROM BAC1498-131-7075T6 AND 2 EACH SPLICES 12.25 AND 12.625" LONG FRApr 20, 2007 · N788AT · Boeing 727214 · Fuselage Main, Longeron/StringerSDR DHL2007788503Hinge Fitting · crackedLEFT WING UPPER T/E, NR 3 SPOILER PANEL, CENTER OUTBD HINGE FITTING IS CRACKED. STOP DRILLED CRACK .250 DIA AT END OF CRACK IAW B727 SRM 51-10-1, VERIFIED WITH NTD HFEC IAW B727 NDTM PT6-51-00-00, FIG 23, CRACK TERMINATED IN STOP DRILL HOLE. FABRICATED 6' BYApr 19, 2007 · N788AT · Boeing 727214 · SpoilersSDR DHL2007788509Skin · crackedLEFT INBD MID FLAP LWBL 85-100, LOWER T/E CHORD CRACKED THREE PLACES ON CUTOUTS. CUTOUT DAMAGE AREA 46.625" BY 2" IAW B727 SRM 51-40-3, FIG 1. FABRICATED NEW ANGLE FROM BAC1503-100046-7075T6, 46.625" BY 2" AND TWO EACH SPLICES FROM BAC 1503-100046-7075T6, 7.Apr 18, 2007 · N788AT · Boeing 727214 · Trailing Edge FlapsSDR DHL2007788504Skin · debondedLEFT INBD AFT FLAP, UPPER SURFACE LWBL 244, UPPER SURFACE CRACKED AND DISBONDED. REMOVED DAMAGED AREA 12.5" BY 15", CLEANED, PREPPED AREA IAW B727 SRM 51-40-20, PAR 7, FIG 3. FABRICATED DOUBLER 3" BY 15" AND SKIN 12.5" BY 15" FROM 7075T6, .012, PRIMED, APPLIApr 18, 2007 · N788AT · Boeing 727214 · Trailing Edge FlapsSDR DHL2007788521Panel · crackedVERTICAL LE PANEL NR 9502 LOWER INTERIOR PANEL BENT AND CRACKED. REMOVED PREVIOUS REPAIR ON PANEL NR 9502 IAW B727 SRM 51-30-2. FABRICATED REPAIR DOUBLER 7075T6 .025 (16.5" BY 8.5") PO NR 9004219 IAW B727 SRM 55-30-2 FIG 2 AND 51-40-2 FIG 1. TREATED AND PRIApr 17, 2007 · N788AT · Boeing 727214 · Horizontal Stabilizer, Plate/SkinSDR DHL2007788519Nose Cowl · crackedNR 1 ENG NOSE COWL 7:30 POS AFT EDGE SKIN IS WORN AND CRACKED. CUTOUT DAMAGED AREA (3.50" BY .90"). FABRICATED REPAIR DOUBLER 2024T3 .050 PO 9004690 (11.25" BY 3.50") AND FILLER 2024T3 .040 PO NR 9004779 (3.50" BY .90") IAW B727 SRM 54-30-3 FIG 8. TREATED AApr 17, 2007 · N788AT · Boeing 727214 · Nacelle/Pylon, Main FrameSDR DHL2007788518Skin · damagedNR 1 ENG NOSE COWL 9:00 POSITION AFT EDGE SKIN IS BROKEN OUT. CUTOUT DAMAGED AREA (3.50" BY .90"). FABRICATED REPAIR DOUBLER 2024T3 .050 PO NR 9004690 (8.25" BY 2.65") AND FILLER 2024T3 .040 PO NR 9004779 (3.50" BY .90") IAW B727 SRM 54-30-3 FIG 8. TREATED Apr 17, 2007 · N788AT · Boeing 727214 · Nacelle/Pylon, Main FrameSDR DHL2007788527Torque Box · crackedWHILE IN "C" CHECK, AFT STAIRWELL RT TORQUE BOX HAS CRACK AT INBD WEB LIGHTENING HOLE STA 1223. STOP DRILLED CRACK IAW B727 SRM 51-10-1, FABRICATED REPAIR DOUBLER 7075T6 .025 PO NR 9004219 6.6" BY 3.75" IAW B727 SRM 53-10-2 FIG 6. TREATED AND PRIMED IAW B727Apr 14, 2007 · N788AT · Boeing 727214 · Fuselage Main, StructureSDR DHL2007786529Structure · crackedNR 1 SLAT ASSY CRACK WHERE SLAT ACTUATOR ATTACHES TO SLAT INTERNAL. REMOVED NR 1 SLAT ASSY TO FOM REPAIR IAW B727 M/M 27-81-11. REMOVED 2 RIBS INBD AND OUTBD FROM NR 1 SLAT ASSY IAW B727 SRM 51-30-2. LOCATED AND DRILLED RIBS IAW B727 SRM 51-30-2. INSTALLEDMar 30, 2007 · N786AT · Boeing 727214 · Leading Edge DevicesSDR DHL2007786503Web · crackedCRACK AT LIGHTENING HOLE, RT LOWER TORQUE BOX STA 1329. STOP DRILLED 0.250" DIAMETER HOLE AT LIGHTENING HOLE RT LOWER TORQUE BOX STA 1329 IAW B727 SRM 51-40-2. NDT C/W HFEC FOR CRACK STOP VERIFED, IAW B727 NDTM, PT6 51-00-00 FIG 23. FABRICATED DOUBLER REPAIMar 28, 2007 · N756AT · Boeing 727214 · Fuselage Miscellaneous StructureSDR DHL2007786505Rib · crackedNR 3 SLAT IB AND OB RIBS WS 515 AT ACT ATTACH ARE CRACKED IN THE AFT LOWER CORNERS. REMOVED AND REPLACED RIBS I/B AND O/B AT NR 3 SLAT WS 515 IAW B727 SRM 51-30-2.Mar 28, 2007 · N786AT · Boeing 727214 · Leading Edge DevicesSDR DHL2007786504Torque Box · crackedCRACK AT LIGHTENING HOLE, RT LOWER TORQUE BOX STA 1329. STOPPED DRILLED 0.250" DIAMETER HOLE AT LIGHTENING HOLE RT LOWER TORQUE BOX STA 1329 IAW B727 SRM 51-40-2. NDT C/W HFEC FOR CRACK STOP VERIFED, IAW B727 NDTM, PT6 51-00-00 FIG 23. FABRICATED DOUBLER REMar 28, 2007 · N756AT · Boeing 727214 · Fuselage Main, StructureSDR DHL2007786530Skin · gougedRIGHT WING INBD MID FLAP GOUGED 3 FROM INBD EDGE, WBL 73.597. CUTOUT DAMAGED AREA 1 BY 1.875. FABRICATED INTERNAL DOUBLER FROM 2024T3, .040, 7.75 BY 5.625 AND FILLER 2024T3, .040, 1 BY 1.875. TREATED, ALODINED AND PRIMED PARTS IAW B727 SRM 51-10-2. INSTALLMar 27, 2007 · N786AT · Boeing 727214 · Trailing Edge FlapsSDR DHL2007786524Skin · dentedA/C IN "C" CHECK AT FLIGHTSTAR A/C SERVICES, REF ASTAR NR 112921, LT WING OB FORE FLAP ASSY HAS 1 DENT UPPER SKIN. CUT OUT DENT 1" DIA ON LT OB FORE FLAP UPPER SURFACE AND APPLIED POTTING COMPOUND. FABRICATED FILLER 4" DIA FROM .016 2024T3 PO NR 9004174. BOMar 27, 2007 · N786AT · Boeing 727214 · Trailing Edge Flaps
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