Boeing 727-225

Service difficulty reports · 4,226

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  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = '727225'
  ORDER BY difficulty_date DESC"

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SDR 08FDEA01368Seat Track · corrodedMAIN CARGO COMPATRMENT, SEAT TRACK IC CORRODED FROM BS 870-848, LBL 25. REMOVED SEAT TRACK AT MAIN CARGO COMPARTMENT IAW SRM 51-30-2. LOCATED AND DRIILED NEW TRACK, DIM 16 INCH LONG IAW SRM 51-30-5 AND 53-10-2 FIG 7. TREATED AND PRIMED AFFECTED AREAS IAW CSApr 9, 2008 · N466FE · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR DHLA200800038Engine · vibrationFLT NR 155 ON TAKEOFF ROLL LOUD BANG AUTO PACK TRIP AND ENG FAIL LIGHTS ILLUMINATE AT 70KTS. RTO, ALL ENG RUNNING W/IN NORM, PARAMETER. CLEARED AUTO PACK TRIP AND PERFORMED RTO FLOW CHART. NOTIFY MX CNTRL. ON TAXI BACK ENG NR 1 LOW OIL PRESS LIGHT ILLUMINAApr 4, 2008 · N742DH · Boeing 727225 · Engine (Turbine/Turboprop)SDR 08FDEA01294Skin · dentedDENT RT AFT LWR FUSELAGE BS 1243 S21R CUT OUT DAMAGED AREA 3" BY 3/4" IAW SRM 53-30-3 FIG 1. FABRICATED DOUBLER REPAIR IAW SRM 53-30-3 FIG 1, AND 53-30-2 FIG 3. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED REPAIR DOUBLER IAW SRM 51-30-2.Apr 3, 2008 · N466FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR 08FDEA01293Seat Track · corrodedMAIN CARGO COMPARTMENT, CORROSION ON SEAT TRACK FORM STA 700-720 BL 0. REMOVED SEAT TRACK OUT LIMITS BTW STA 600-720 BL 0 IAW SRM 51-30-2. FABRICATED, LOCATED, AND DRILLED NEW SEAT TRACK IAW SRM EA-01-049 AND SRM 53-10-5 FIG 7. TREATED AND PRIMED IAW SRM 51Apr 3, 2008 · N466FE · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA01292Seat Track · corrodedMAI CARGO COMPARTMENT, SEAT TRACK CORRODED STA 570-580 RBL 45 REMOVED SEAT TRACK SECTION OUT OF LIMITS AT STA 530 TO 690 RBL 45 IAW SRM 51-30-2. FABRICATED, LOCATED AND DRILLED NEW SEAT TRACK IAW SRM ER-01-049 AND SRM 53-10-5 FIG 7. TREATED AND PRIMED PARTSApr 3, 2008 · N466FE · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA01291Seat Track · corrodedMAIN CARGO COMPARTMENT, SEAT TRACK CORRODED STA 950B BL 0. REMOVED SEAT TRACK-OUT OF LIMITS BETWEEN STA 890-950C BL 0 IAW SRM 51-30-2 LOCATED AND DRILLED NEW SEAT TRACK IAW SRM ER-01-049 AND 53-10-5 FIG 7. TREATED AND PRIMED PARTS IAW SRM 51-10-2. INSTALLEApr 3, 2008 · N466FE · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA01290Skin · delaminatedLT I/B FLAP HAS AN AREA OF DELAMINATION ON UPPER SURFACE, WS 275 CUT OUT DELAMINATED AREA 7 1/2 INCH BY 7 1/2 INCH ON LT I/B FORG FLAP UPPER SURFACE AND REMOVED DAMAGED CORE 7 1/2 BY 7 1/2. SHAPED SECTION OF CORE 7 1/2 INCH BY 7 1/2 INCH. FABRICATED DOUBLERApr 3, 2008 · N466FE · Boeing 727225 · Trailing Edge FlapsSDR 08FDEA01283Skin · dentedDENT LT AFT FUSELAGE STA 1350 STR 17L, FOUND OUT OF LIMITS IAW SRM, EVALUATED DENT AND FOUND OUT OF LIMITS. CUT OUT DAMAGED AREA DIM 1 1/2 BY 1 INCH AND FABRICATED REPAIRED DOUBLER IAW SRM 54-30-3 FIG7. TREATED AND PRIMED PARTS IAW SRM 51-10-2. INSTALLED Apr 3, 2008 · N466FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR 08FDEA01271Skin · crackedAFT LOWER CARGO DOOR LOWER AFT FUSELAGE EDGE BENT AND CRACKED AT STA 980-990. REPAIRED BY TRIMMING THE AFFECTED PER EA 7-5330-116976.Apr 2, 2008 · N466FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR 08FDEA01203Floorbeam · corrodedMAIN CARGO COMPARTMENT, FLOORBEAM CORRODED AT BS 560, RBL 0-25. REMOVED CORROSION IAW SRM 51-10-6, AND FOUND OUT OF LIMITS IAW SRM 53-10-1 FIG 4. REMOVED SPLICE ANGLE AND DISPLACED SEAT TRACK FOR ACCESS IAW SRM 51-30-2. CUT OUT DAMAGED SECTION FROM RBL 32 TMar 29, 2008 · N466FE · Boeing 727225 · Fuselage Main, Floor BeamSDR 08FDEA01171Vertical Beam · shearedSTA 1183 FWD SIDE VERTICAL BEAM AT APPROX LBL 12 HAS FASTENERS WITH NO EDGE DISTANCE. REPAIRED IAW EA 7-5310-116973.Mar 28, 2008 · N466FE · Boeing 727225 · Fuselage Miscellaneous StructureSDR 08FDEA01152Skin · dentedDENT RT AFT FUSELAGE STA 1050 STR 23R (DENT FOUND OUT OF LIMITS). CUT OUT DAMAGED AREA IAW SRM 53-30-1 FIG1. FABRICATED REPAIR DOUBLER TREATED AND PRIMED REPAIR PART AND AREA IAW SRM 51-10-2. INSTALLED DOUBLER IAW SRM 51-30-2.Mar 26, 2008 · N466FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR 08FDEA01112Seat Track · corrodedMAIN CABIN COMPARTMENT, SEAT TRACK CORRODED AT BS 950C, 8 BL 0. REMOVED SEAT TRACK SECTION- OUT OF LIMITS BL 0 STA 950C TO STA 1010 IAW SRM 51-30-2. FABRICATED, LOCATED AND DRILLED NEW SEAT TRACK IAW SRM ER 01-049 AND SRM 53-10-5 FIG7. TREATED AND PRIMED IAMar 23, 2008 · N466FE · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA01111Skin · wornLT FUSELAGE SKIN WORN AT BS 310 BTW S10L AND S11L, WORN BY FWD ENTRY DOOR MECHANISM LONG BOLT INSTALLED. REPAIRED FWD ENTRY DOOR MECHANISM IAW SRM 51-30-2 AND EA 7-5330-116972.Mar 23, 2008 · N466FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR 08FDEA01110Beam · crackedRT WING I/B T/E "J " BEAM AT WING STATION 92 CRACKED, WING T/E SUPPORT BEAM FOR NR 7 SPOILER. TRIMMED OUT CRACKED AREA LENGTH 0.75" IAW SRM 51-10-1. TREATED AND PRIMED AREA "J" BEAM IAW SRM 51-10-2 DRAWING SR27-57-025.Mar 22, 2008 · N466FE · Boeing 727225 · Wing Miscellaneous StructureSDR 08FDEA01109Shim · migratedMIGRATING SHIMS AND LOOSE HARDWARE AT LWR SIDE OF NR 8 SPOILER ACTUATOR SUPPORT BEAM FITTING, WS 198. REPAIRED SUPPORT BEAM FITTING IAW DRAWING SR27-57-038 REV "C".Mar 22, 2008 · N466FE · Boeing 727225 · Wing Miscellaneous StructureSDR 08FDEA01108Support Beam · crackedMIGRATING SHIMS AND LOOSE HARDWARES AT LWR SIDE OF NR 7 SPOILER SUPPORT BEAM FITTING WS 198. REPAIRED NR 7 SPOILER ACTUATOR SUPPORT BEAM FITTING IAW DRAWING SR27-57-038 REV "C".Mar 22, 2008 · N466FE · Boeing 727225 · Wing Miscellaneous StructureSDR 08FDEA01107Floorbeam · corrodedMAIN CARGO COMPARTMENT, FLOORBEAM CORRODED BETWEEN BL 0 BL 25L , B.S. 950DMar 22, 2008 · N466FE · Boeing 727225 · Fuselage Main, Floor BeamSDR 08FDEA01106Floorbeam · corrodedMAIN CARGO COMPARTMENT, FLOORBEAM CORRODED BETWEEN BL 0 BL 25L, BS 950D. CUT OUT DAMAGE IAW SRM 53-10-3 FIG 3 & SRM ER-01-049 REV E. FABRICATED SECTION, SUPPORT ANGLES AND REINFORCEMENT STRAPS IAW SRM 53-10-3 FIG 3 TREATED AND PRIMED IAW SRM 51-10-2. INSTALLMar 22, 2008 · N466FE · Boeing 727225 · Fuselage Main, Floor BeamSDR C1HA200879001Engine · overheatedON TAKEOFF ROLL, ENGINES WERE BROUGHT TO 1.4 EPR THEN WERE BEING ADVANCED TO FLEX THRUST WHEN NR 2 ENGINE MADE A LOUD NOISE, FE CONFIRMED NR 2 ENGINE WAS AT 1.65 EPR WHEN NOISE OCCURRED. NR 2 FUEL FLOW WENT TO 0, ENG FAIL LIGHTS ILLUMINATED, THRUST LEVERS WERMar 16, 2008 · N679MG · Boeing 727225 · Engine (Turbine/Turboprop)SDR C8GA20080011Switch · faultyFLT 738 FROM TOL TO SLW - DURING CLIMB-OUT, THE AFT AIRSTAIR LIGHT ILLUMINATED IN FLIGHT. THE AIRCRAFT RETURNED TO TOL WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION REVEALED THAT THE AFT AIRSTAIR CONTROL HANDLE MICROSWITCH WAS AT FAULT. THE AFT AMar 14, 2008 · N755DH · Boeing 727225 · Door Warning SystemSDR DHLA200800021Fire Warning · false activationDURING PUSH BACK ON GROUND, GOT INTERMITTENT FIRE BELL WARNING. FOUND LIGHT IN APU HANDLE ILLUMINATED. PERFORMED 1'S, PERFORMED CHECKLIST, CALL FIRE RESCUE AND HAD MX CHECK FOR FIRE. FIRE LIGHT IN HANDLE REMAIN ON. AS PER MAINT CONTROL APU OPERATION DEFERRMar 4, 2008 · N748DH · Boeing 727225 · Fire DetectionSDR DHLA200800017Fcu · out of adjustFLT NR 385, 1 ENG WOULD NOT PRODUCE TAKEOFF EPR RTO WT 174.9 24 DEGED C PA-70 BRAKE ENERGY ZONE NORMAL IAS LESS THAN 60 NTS SWAPPED NR 1 AND 2 EPR GAUGES FOR TROUBLESHOOTING RAN ENGINE, ALL ENGINE PARAMETER LOW ON NR 1 ENG. RETURN NR 1 AND 2 EPR GAUGES TO ORIFeb 26, 2008 · N743DH · Boeing 727225 · Fuel Control/Turbine EnginesSDR C8GA20080004Helicoil · missingFLT 716 FROM MEM TO HRL, ON DESCENT INTO HRL THE 1 ENGINE LOW OIL PSI LIGHT ILLUMINATED FOLLOWED BY A LOSS OF OIL QUALITY. THE NR 1 ENGINE WAS SHUT DOWN AND LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION REVEALED A MISSING HELI COIL ON THE GEARBOX. REMOVEDJan 31, 2008 · N801EA · Boeing 727225 · Accessory GearboxesSDR DHLA200800010Skin · damagedRT SIDE FUSELAGE HAS A 10 INCH GASH BY 1/4 INCH WIDE AT FUSELAGE STATION 720, 5 O'CLOCK POSITION. INSTALLED MAJOR REPAIR AT BS 700.00 AT RT STRINGER 27 IAW EVA B 253-00040 DTD 1/29/08 REV IR & IAW W/O 3473 TCN MXC10001 DTD 1-30-08. ACFT GROUNDED.Jan 28, 2008 · N742DH · Boeing 727225 · Fuselage Main, Plate/SkinSDR C1HA200878001Switch · malfunctionedAIRCRAFT (AT FL 290) CABIN ALT STARTED TO CLIMB. DESCENDED TO F200, THEN FL 160 DOWN TO 10,000 DIVERTED TO OKC. REMOVED AND REPLACED RT PACK VALVE REF MM 21-55-71, NO HELP. PROBLEM VERIFIED RT PACK SWITCH. REMOVED AND REPLACED RT PACK SWITCH. OPERATIONAL Jan 21, 2008 · N678MG · Boeing 727225 · Cabin Pressure ControllerSDR CA080121007Volt Regulator · odor(CAN) DURING FLIGHT CREW SHUTDOWN CHECKLIST, ON APU POWER, SMOKE ALARM SOUNDED IN THE AC LAVATORY. LAVATORY INSP REVEALED SOME SMOKE. ALARM SILENCED WHILE INSPECTING THE LAVATORY AREA. AFTER APPROXIMATELY 30 SECONDS, THE ALARM SOUNDED AGAIN, AND THE AC POWEJan 16, 2008 · Boeing 727225 · DC RegulatorSDR C8GA20080002Line · chafedFLT 246 FROM EWR TO BDA. DURING DESCENT INTO BDA, THE NR 2 HYDRAULIC "B" SYSTEM PUMP LOW PRESSURE LIGHT ILLUMINATED FOLLOWED BY A PRESSURE DROP TO ZERO PSIG. THE AIRCRAFT LANDED WITHOUT INCIDENT. POST FIGHT INSPECTION REVEALED THAT THE PRESSURE AND RETURN LIJan 7, 2008 · N755DH · Boeing 727225 · Hydraulic System, MainSDR C8GA20080001Rod · brokenFLT 1723 FROM ROC TO TOL, DURING GEAR RETRACTION AT POSITIVE CLIMB RATE CREW HEARD A LOAD "POP" FROM THE NOSE GEAR FOLLOWED BY THE ILLUMINATION OF THE RED DOOR INDICATOR LIGHT ON THE FRONT PANEL. THE AIRCRAFT RETURNED TO ROC WHERE IT LANDED WITHOUT INCIDENT. Jan 3, 2008 · N808EA · Boeing 727225 · Landing Gear Door Retract SectionSDR DHL2007742020Skin · corrodedCORROSION WITH EXFOLIATION, AFT PIT BS 950F + 4" STRINGER 29R. CORROSION FOUND OUT OF LIMIT IAW B-727 SRM 53-10-1 FIGURE 1. FABRICATED REPAIR DOUBLERS, FABRICATED FILLER IAW EDAE59-1 REV B. INSTALLED REPAIR DOUBLERS AT BS 950F TO BS 970, BS 970 TO BS 990 SDec 22, 2007 · N742DH · Boeing 727225 · Fuselage Main, Plate/SkinSDR DHL2007742067Seal Depressor · gougedC-1 DOOR SKIN GOUGED ALONG LOWER SURFACE. FOUND GOUGE OUT OF LIMITS IAW B-727 SRM 52-00-2. REMOVED C-1 DOOR LOWER SEAL DEPRESSOR IAW B-727 SRM 51-30-2. FABRICATED NEW DEPRESSOR FROM BAC 1496-383 2024-T3 PONR 7332283 (DIMENSION 44" LONG) IAW B-727 SRM 52-30-Dec 19, 2007 · N742DH · Boeing 727225 · Cargo/Baggage DoorsSDR C1HA200776001Blades · damagedAFTER 1.4 EPR CHECK, WHICH WAS COMPLETELY NORMAL, POWER WAS ADVANCED ON ALL ENGINES. AT APPROXIMATELY 1.6 EPR AND 60 KTS THE NR 1 PACK TRIP LIGHT ILLUMINATED FOLLOWED BY THE ENGINE FAIL LIGHTS. ABORTED THE TAKEOFF AT THAT POINT THE FLIGHT ATTENDANT HEARD A SERDec 18, 2007 · N676MG · Boeing 727225 · Engine (Turbine/Turboprop)SDR DHL2007742040Stringer · corrodedCORROSION WITH EXFOLIATION, AFT PIT BS 950E STRINGER 28R. CUT OUT DAMAGED AREA APPROXIMATE DIMENSION 15.5" LENGTH IAW COTNEY AEROSPACE, INC DRAWING NR AE59-53-R01 REV A. LOCATED AND DRILLED NEW STRINGER SECTION USING P/N 65-58387-2 PO NR 7332255 APPROXIMATE Dec 17, 2007 · N742DH · Boeing 727225 · Fuselage Main, Longeron/StringerSDR DHL2007742057Stringer · corrodedSURFACE CORROSION, AFT PIT BETWEEN BS 990 TO BS 970 STRINGER 29L. REMOVED CORROSION AFT PIT BETWEEN BS 990 TO BS 970 STRINGER 29L IAW B-727 SRM 51-10-6. FOUND CORROSION OUT OF LIMITS IAW B-727 SRM 53-10-1 FIGURE 1 AND 53-10-2 FIGURE 5. FABRICATED REPAIR PARDec 13, 2007 · N742DH · Boeing 727225 · Fuselage Main, Longeron/StringerSDR DHL2007742029Stringer · corrodedAFT CARGO COMPARTMENT STRINGER 29R IS CORRODED AT STATION 950E + 4". REMOVED FASTENERS AT AFT CARGO COMPARTMENT STRINGER 29R STATION 950E IAW B-727 SRM 51-30-2. REMOVED CORROSION STRINGER 29R STATION 950E + 4" IAW B-727 SRM 51-10-6. INSPECTED AREA, ORIGINALDec 13, 2007 · N742DH · Boeing 727225 · Fuselage Main, Longeron/StringerSDR DHL2007742031Stringer · crackedSTRINGER 18A RIGHT CRACKED AT BS 930. CUT OUT DAMAGED SECTION AT STRINGER 18A RIGHT FROM BS 940 AFT APPROXIMATE DIMENSION 21.375" IAW EVA:B253-00027. FABRICATED 2 EACH STEEL ANNEALED REPAIR ANGLES APPROXIMATE DIMENSION 21.5" BY 1" BY 1" FROM 4130 NORMALIZED Dec 11, 2007 · N742DH · Boeing 727225 · Fuselage Main, Longeron/StringerSDR DHL2007742061Floorbeam · crackedSPLICE PLATE (FLOORBEAM) AT LBL 65 BS 600 HAS CRACK FROM SLOT RADIUS. REMOVED CRACK FLOORBEAM SPLICE PLATE IAW B-727 SRM 51-30-2 AND AEI DRAWING NR AE727-3-A004. FABRICATED NEW SPLICE PLATE FROM 2024-T3 0.125" PO NR 9005802 APPROXIMATE DIMENSION 10.9375" BY Dec 9, 2007 · N742DH · Boeing 727225 · Fuselage Main, Floor BeamSDR DHL2007742060Floorbeam · crackedFLOORBEAM SPLICE PLATE AT LBL 65 BS 660 HAS CRACK FROM SLOT RADIUS. REMOVED CRACK FLOORBEAM SPLICE PLATE IAW B727 SRM 51-30-2 AND AEI DRAWING NR AE727-3-A004. FABRICATED NEW SPLICE PLATE FROM 2024-T3 0.125" PO NR 9005802 APPROXIMATE DIMENSION 10.9375" BY 6.7Dec 9, 2007 · N742DH · Boeing 727225 · Fuselage Main, Floor BeamSDR DHL2007742058Floorbeam · crackedFLOORBEAM SPLICE PLATE AT LBL 65 HAS CRACK FROM SLOT RADIUS BS 680. REMOVED CRACKED FLOORBEAM SPLICE PLATE IAW B-727 SRM 51-30-2 AND AEI DRAWING NR AE727-3-A004. FABRICATED NEW SPLICE PLATE FROM P/N 2024-T3 0.125 PO NR 9005802 APPROXIMATE DIMENSION 10.625" BYDec 9, 2007 · N742DH · Boeing 727225 · Fuselage Main, Floor BeamSDR DHL2007742030Skin · corrodedAFT CARGO COMPARTMENT SKIN EXFOLIATED CORROSION AT STATION 950E BETWEEN STRINGER 29R AND STRINGER 30 AFT SIDE OF FRAME. REMOVED CORROSION AT AFT CARGO COMPARTMENT SKIN STATION 950E BETWEEN STRINGER 29R AND 30 IAW B-727 SRM 51-10-6. INSPECTED AREA AND FOUND ODec 8, 2007 · N742DH · Boeing 727225 · Fuselage Main, Plate/SkinSDR DHL2007742017Seat Track · corrodedMAIN CABIN BS 740 TO BS 848.95 RBL 45 SEAT TRACK HAS CORROSION AT INBOARD FLANGE. REMOVED DAMAGED SEAT TRACK IAW B-727 SRM 51-30-2, FABRICATED IAW B-727 SRM 51-30-5 AND SRM 52-10-2 FIGURE 3 AND 5. INSTALLED EXTRUSION SEAT TRACK IAW B-727 SRM 51-30-2.Dec 7, 2007 · N742DH · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2007742063Stringer · corrodedFORWARD CARGO COMPARTMENT STRINGER 27L IS CORRODED AT STATION 620 WITH EXFOLIATION. REMOVED FASTENERS AND EXISTING SPLICE IAW B-727 SRM 51-30-2. CUT OUT DAMAGED AREA (DIMENSION 17.5" LONG) AND FABRICATED REPAIR FILLER FROM BAC 1493-513 7075-T6 PO NR 7332258 Dec 6, 2007 · N742DH · Boeing 727225 · Fuselage Main, Longeron/StringerSDR DHL2007742062Stringer · corrodedFORWARD CARGO COMPARTMENT STRINGER 27R IS CORRODED JUST AFT OF STATION 560 WITH EXFOLIATION. REMOVED SUPPORT FRAMES AT BS 564 AND BS 574 IAW B-727 SRM 51-30-2. CUT OUT DAMAGED SECTION (DIMENSION 18" LONG) AND FABRICATED NEW STRINGER SECTION FROM BAC 1498-147Dec 4, 2007 · N742DH · Boeing 727225 · Fuselage Main, Longeron/StringerSDR DHL2007742052Frame · damagedFUSELAGE FRAME STATION 420 FRAME AND STRAP HAVE NUMEROUS HOLES DRILLED THROUGH BETWEEN STRINGER 7R AND 8R. REMOVED STRAPS AND FRAME ATTACHED PARTS FOR ACCESS IAW B-727 SRM 51-30-2. CUT OUT DAMAGED SECTION OF FRAME (DIMENSION 40" BY 5") IAW B-727 SRM 51-10-1.Dec 4, 2007 · N742DH · Boeing 727225 · Fuselage Main, FrameSDR DHL2007742051Frame · damagedFUSELAGE FRAME STATION 380, FRAME AND STRAPS HAVE NUMEROUS HOLES DRILLED THROUGH FROM STRINGER 5R TO STRINGER 10R. REMOVED STRAPS AND FRAME ATTACHED PARTS FOR ACCESS IAW B-727 SRM 51-30-2. CUT OUT DAMAGED SECTION OF FRAME (DIMENSION 26" BY 5") IAW B-727 SRM Dec 4, 2007 · N742DH · Boeing 727225 · Fuselage Main, FrameSDR DHL2007742038Attach Angle · crackedNR 4 SLAT LOWER TRAILING EDGE ACCESS PANEL ATTACH "L" ANGLE IS CRACKED AT UPSTOP PAD. REMOVED OUTBOARD NR 4 SLAT ACCESS PANEL AND BUMP STOP IAW B-727 SRM 51-30-2. NDT CRACK FOR END VERIFICATION IAW B-727 NDT MANUAL CH. 51-00-0 PT 6 FIGURE 23. CUT OUT 4 INCHDec 4, 2007 · N742DH · Boeing 727225 · Wing, Attach FittingsSDR DHL2007742024Shear Tie · damagedBS 950C BETWEEN STRINGER 28L AND 29L FRAME SHEAR TIE DAMAGED. CUT OUT DAMAGED SECTION APPROXIMATE DIMENSION 6.75" BY 2" IAW B-727 SRM 53-10-4 FIGURE 15 AND SRM 51-10-1. FABRICATED SHEAR TIE REPAIR FROM 7075-O 0.071" APPROXIMATE DIMENSION 6.75" BY 2" IAW B-72Dec 4, 2007 · N742DH · Boeing 727225 · Fuselage Internal Mounting StructureSDR DHL2007742019Stringer · corrodedFOUND STRINGER 29L BS 950 - 950D CORRODED. REMOVED CORROSION FROM STRINGER 29L BS 950-950D IAW B-727 SRM 51-10-6, OUT BOARD FLANGE BS 950A-950B FOUND OUT OF LIMIT, BS 950B-950D FOUND WITHIN LIMIT, IAW B-727 SRM 53-10-1 FIGURE 1 AND SRM 53-10-2 FIGURE 5. FABRDec 4, 2007 · N742DH · Boeing 727225 · Fuselage Main, Longeron/StringerSDR DHL2007742069Stringer · corrodedE/E BAY, IN FUSELAGE LOWER LOBE STRINGER 28R BETWEEN STATION 460 TO 480 INSIDE HAT CHANNEL OF STRINGER RUNS THE LENGTH OF SURFACE CORROSION. REMOVED DAMAGED STRINGER BS 440 - BS 480 FROM PREVIOUS REPAIR SPLICE IAW B-727 SRM 51-30-2. FABRICATED NEW STRINGER FDec 3, 2007 · N742DH · Boeing 727225 · Fuselage Main, Longeron/StringerSDR DHL2007742066Support Beam · crackedCRACK AT RIGHT HORIZONTAL SUPPORT "I" BEAM AFT PIT BS 1183 INBOARD WL 196. REMOVED RIGHT HORIZONTAL SUPPORT BEAM BS 1183 IAW B-727 SRM 51-30-2. FABRICATED NEW "I" BEAM SUPPORT FROM BAC 1518-356 7075-T6 PO NR 7332188 APPROXIMATE DIMENSION 28.5" BY 3" IAW B-72Dec 3, 2007 · N742DH · Boeing 727225 · Fuselage Main, Structure
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