Boeing 727-225

Service difficulty reports · 4,226

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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 = '727225'
  ORDER BY difficulty_date DESC"

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SDR DHL2007742039Wedge · delaminatedRIGHT INBOARD MID FLAP INBOARD TRAILING EDGE DELAMINATED WBL80. FOUND WEDGE OUT OF REPAIRABLE LIMITS IAW B-727 SRM 57-50-1 FIGURE 3. REMOVED WEDGE, LOCATED AND INSTALLED NEW WEDGE IAW B-727 SRM 51-30-2 AND 51-30-5.Dec 3, 2007 · N742DH · Boeing 727225 · Trailing Edge FlapsSDR DHL2007742027Shear Tie · corrodedBS 720F BETWEEN STRINGER 26L AND 27L FRAME SHEAR TIE HAS CORROSION. CUT OUT DAMAGED AREA APPROXIMATE DIMENSION 5.5" BY 2.125" IAW B-727 SRM 53-10-3 FIGURE 11. FABRICATED REPAIR DOUBLER FROM 7075-T6 0.071 PO NR 9005482 APPROXIMATE DIMENSION 4.25" BY 5.375" IADec 3, 2007 · N742DH · Boeing 727225 · Fuselage Internal Mounting StructureSDR DHL2007742023Stringer · corrodedFUSELAGE LOWER LOBE (E/E BAY) STATION 480-460 STRINGER 28L INSIDE HAT CHANNEL OF STRINGER RUNS THE LENGTH OF LIGHT SURFACE CORROSION. REMOVED STRINGER FROM BS 460 - BS 480 PREVIOUS SPLICE IAW B-727 SRM 51-30-2. FABRICATED NEW STRINGER FILLER FROM BAS 1498-13Dec 3, 2007 · N742DH · Boeing 727225 · Fuselage Main, Longeron/StringerSDR DHL2007742046Skin · delaminatedLEFT WING INBOARD FOREFLAP HAS TWO AREAS OF DELAMINATION ON LOWER SURFACE, WBL 130. CUT OUT DELAMINATED AREA OF LEFT WING INBOARD FOREFLAP WBL 130 10" BY 11". REMOVED DAMAGED CORE 10" BY 11". CUT AND TRIMMED NEW CORE PLUG 10" BY 11" FROM PED3.1 3/16 5052 NADec 1, 2007 · N742DH · Boeing 727225 · Trailing Edge FlapsSDR DHL2007742036Attach Angle · misrepairedNR 2 SLAT LOWER TRAILING EDGE ACCESS PANEL, ATTACH "L" ANGLE REPAIR AT UPSTOP PAD IS IMPROPER. REMOVED ACCESS PANELS AND IMPROPER REPAIR IAW B-727 SRM 51-30-2. CUT OUT ANGLE DAMAGED SECTION (DIMENSION 26.75 BY 2") AND FABRICATED NEW ANGLE FILLER SECTION FROMNov 29, 2007 · N742DH · Boeing 727225 · Leading Edge DevicesSDR DHL2007742026Shear Tie · damagedBS 950E BETWEEN STRINGER 28L AND 29L FRAME SHEAR TIE DAMAGED. CUT OUT DAMAGED SHEAR TIE (DIMENSION 6.75" BY 2") IAW B-727 SRM 53-10-4 FIGURE 15 AND 51-10-1. FABRICATED SHEAR TIE REPAIR FROM 7075-0 0.071" PO NR 7247111 (DIMENSION 6.75" BY 2") IAW B-727 SRM 53Nov 28, 2007 · N742DH · Boeing 727225 · Fuselage Internal Mounting StructureSDR DHL2007742025Shear Tie · damagedBS 950D BETWEEN STRINGER 28L AND 29L FRAME SHEAR TIE DAMAGED. CUT OUT DAMAGED SECTION (DIMENSION 6.75" BY 2") IAW B-727 SRM 53-10-4 FIGURE 15 AND SRM 51-10-1. FABRICATED SHEAR TIE REPAIR FROM 7075-0 0.071" PO NR 7247111 (DIMENSION 6.75" BY 2") IAW B-727 SRM Nov 28, 2007 · N742DH · Boeing 727225 · Fuselage Internal Mounting StructureSDR 07FDEA04959Stringer · crackedRT EXT FUSELAGE SKIN STRINGER IS CRACKED, BS 940-946, STR 18A R REMOVED DAMAGE SECTION OF STR 18A RT. DRILLED UP REPAIR ANGLES, RADIUS FILLERS AND AND SHIMS, AND NEW STR SECTION. INSTALLED ALL REPAIR PARTS AND INSTALLED W/B PLN NR 3118 AND 3116. REF FED EX Nov 28, 2007 · N464FE · Boeing 727225 · Fuselage Main, Longeron/StringerSDR DHL2007742028Stringer · corrodedFORWARD CARGO COMPARTMENT STRINGER 27L SHOWS CORROSION AT BS 720F + 10". CUT OUT DAMAGED AREA APPROXIMATE DIMENSION 7.375" LENGTH IAW B-727 SRM 53-10-3 FIGURE 1. FABRICATED REPAIR FILLER FROM BAC 1498-147 0.090" PO NR 7332258 APPROXIMATE DIMENSION 7.875" LENNov 27, 2007 · N742DH · Boeing 727225 · Fuselage Main, Longeron/StringerSDR DHL2007742054Frame · dentedDENT, AFT PIT AT FRAME BS 1070 ABOVE STRINGER 26R. CUT OUT DAMAGED AREA APPROXIMATE DIMENSTION 1: BY 1: IAW B-727 SRM 51-40-2 FIGURE 1. FABRICATED FRAME REPAIR DOUBLER FROM 7075-0 0.071" PO NR 724711 APPROXIMATE DIMENSION 10" BY 4.5" IAW B-727 SRM 51-40-2 FINov 26, 2007 · N742DH · Boeing 727225 · Fuselage Main, FrameSDR DHL2007742045Stringer · corrodedFORWARD CARGO COMPARTMENT STRINGER 26R IS HEAVILY CORRODED BETWEEN STATION 720F TO 740. CUT OUT DAMAGE AREA 9.5" AT STRINGER 26R BETWEEN STATION 720F - 740 IAW B-727 SRM 53-10-3 FIGURE 1. FABRICATED NEW SECTION, MATERIAL USED BAC 1498-147 0.090" 7075-T6 PO NNov 26, 2007 · N742DH · Boeing 727225 · Fuselage Main, Longeron/StringerSDR DHL2007742044Stringer · corrodedFORWARD CARGO COMPARTMENT STRINGER 27R IS HEAVILY CORRODED BETWEEN STATION 720F AND 740. CUT OUT DAMAGED AREA 10.5" STRINGER 27R BETWEEN STATION 720F-740 IAW B-727 SRM 53-10-3 FIGURE 1. FABRICATED NEW SECTION MATERIAL USED BAC 1498-147 0.090" 7075-T6 DIMENSINov 26, 2007 · N742DH · Boeing 727225 · Fuselage Main, Longeron/StringerSDR DHL2007742042Hinge · crackedMCD AFT HINGE ON FUSELAGE SIDE HAS AFT LOBE CRACKED. REMOVED DAMAGED SECTION OF MCD HINGE AEI CH 52 REV G FIGURE 5201 B/A. LOCATED AND DRILLED NEW SECTION OF MCD HINGE APPROXIMATE DIMENSION 18" BY 1.75" P/N 14520001-16-7200 PO NR 724546 IAW AEI B-727 MM CH 5Nov 26, 2007 · N742DH · Boeing 727225 · Fuselage, Door HingeSDR C1HA200778002Wire · chafedWHILE WAITING FOR PASSENGER AIRCRAFT HAD SOME SORT OF POWER SURGE OR INTERRUPTION IN POWER. GASPER FAN CIRCUIT BREAKER POPPED, COOLING DOOR BREAKER POPPED, LEFT PACK FAN CIRCUIT BREAKER POPPED, LEFT DUCT OVERHEATED, FOLLOWED BY LEFT PACK TRIP. NR 1 GENERATORNov 26, 2007 · N678MG · Boeing 727225 · Electrical Power System WiringSDR DHL2007742068Skin · corrodedBS 710 RIGHT AND LEFT FAIRINGS HAS CORROSION ON NUT PLATES (AC BAY AREA). CUT OUT DAMAGED AREA AT LOWER FUSELAGE BS 710 APPROXIMATE DIMENSION 1.25" BY .75" IAW B-727 SRM 53-30-3 FIGURE 1. REMOVED DAMAGED SHEAR TIE CLIP ON AFT SIDE OF FRAME BS 710 IAW B-727 SNov 25, 2007 · N742DH · Boeing 727225 · Fuselage Main, Plate/SkinSDR DHL2007742050Frame · corrodedEXFOLIATED CORROSION AFT PIT FRAME BS 1050 ABOVE STRINGER 22L ALSO ABOVE 21L. CUT OUT DAMAGED AREA (DIMENSION 4.5" BY 3.5"). FABRICATED REPAIR ANGLE FROM 7075-0 0.071" PO NR 7247111 (DIMENSION 15.25" BY 4.5") AND REPAIR FILLER FROM 7075-T6 0.063" PO NR 90059Nov 24, 2007 · N742DH · Boeing 727225 · Fuselage Main, FrameSDR 07FDEA04921Floor Support · corrodedFWD PIT FLOOR SUPPORT PNL IS CORRODED BS 480-720D, LBL 20-26, WL 157. BLENDED CORROSION AT BS 480 TO 720C +10. MAX MATERIAL LOSS OF 16 PERCENT OF .050 ORIG "T". WITHIN LIMITS REF SRM 53-10-1 PG 31. BLENDED CORROSION AT BS 720C+10 TO BS 720D. MATERIAL LOSNov 24, 2007 · N464FE · Boeing 727225 · Fuselage Miscellaneous StructureSDR 07FDEA04920Bracket · cracked2" CRACK THROUGH FASTENER ON ANGLE BRACKET, FS 1303, LBL 20, WL 273, ON FWD SIDE OF BULKHEAD, ABOVE S-DUCT, BRACKET CONNECTS BULKHEAD TO FUSELAGE SKIN. REMOVED AND INSTALLED NEW BRACKET AT FS 1303, LBL 20, WL 273 ON FWD SIDE OF BULKHEAD ABOVE S-DUCT REF 51-3Nov 24, 2007 · N464FE · Boeing 727225 · Fuselage Miscellaneous StructureSDR 07FDEA04919Floor Support · corrodedFWD PIT FLR SPPT Z-CHANNEL IS CORRODED BS 720B TO 720C PLUS 10, LBL 20, WL 156 BLENDED CORROSION ON FLOOR SUPPORT. MATERIAL OF .025" OF .063' ORIG "T" FOUND TO BE OUT OF LIMITS REF 53-10-1 PG 2. FABRICATED NEW FLOOR SUPPORT Z-CHANNEL FROM EXTRUSION BAC1517-1Nov 24, 2007 · N464FE · Boeing 727225 · Fuselage Miscellaneous StructureSDR 07FDEA04918Pan · crackedDITCHING PAN IS CRACKED LOCATED AT RBL 27 STA 1183, WL 208 REMOVED GILL LINER SUPPORT PLUS DITCHING PAN REF SRM51-30-2 PG 1-16. FABRICATED NEW DITCHING PAN REF DWG 65-29567. TREATED AND PRIMED DITCHING PAN SRM 51-30-02. REMOVED FLAPPER VALVE SRM 51-30-2. Nov 24, 2007 · N464FE · Boeing 727225 · Fuselage Miscellaneous StructureSDR 07FDEA04917Skin · corrodedRT FUSELAGE SKIN UNDER WING TO BODY TO FAIRING 3442 HAS CORROSION AROUND NUTPLATE HOLES AND FRETTING ALONG MATING SURFACE REMOVED CORROSION REF SRM 51-10-6, ORIGINAL MATERIAL THICKNESS "T" .060" AFTER BLENDING, REMAINING MATERIAL THICKNESS IS .043" AND IS OUT Nov 24, 2007 · N464FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR 07FDEA04916Frame · crackedFWD PIT, PREVIOUS UNREPAIRED DAMAGE FRAME CRACKED AT BS 700 AND BETWEEN STR 18R AND 19R REPAIRED FRAME 700 AT STRINGER 18 TO19 RT REF FED EX EA NR 7-5310-113118 AND BOEING DWG 65-15938, 65-82614-9, 65-17664-50. TREATED AND PRIMED PARTS REF SRM 51-10-2. IDENTNov 24, 2007 · N464FE · Boeing 727225 · Fuselage Main, FrameSDR 07FDEA04915Frame · crackedAFT PIT BODY FRAME WEB IS CRACKED AT TOOLING HOLE BS 970, STR 26L - 27L REMOVED ASSOCIATED PARTS TO FRAME 970 SECTION, REMOVED DAMAGE SECTION OF FRAME FROM STR 27R TO STR 24L AND 25L. FABRICATED NEW FRAME SECTION, HEAT TREATED, ALODINED AND PRIMED, PAINTED ANNov 24, 2007 · N464FE · Boeing 727225 · Fuselage Main, FrameSDR 07FDEA04914Pan · crackedDITCHING PAN AT STA 1183 BETWEEN RBL46 TO 49, WL 208 IS CRACKED, ALONG WITH AFT SUPPORT CLIP. REMOVED GILLINER SUPPORT PLUS DITCHING PAN SRM 51-30-20 PG 16. FABBED NEW DITCHING PAN REF DWG 65-29567. TREATED AND PRIMED REPAIR PARTS 51-10-02 PG 7. INSTALLED Nov 24, 2007 · N464FE · Boeing 727225 · Fuselage Miscellaneous StructureSDR 07FDEA04913Angle · corrodedAFT CARGO BS 970 LOWER FRAME ANGLE CRACKED BETWEEN STR 26L-27L REMOVED LOWER FRAME ANGLE. FABRICATED REPAIR ANGLE AND REINSTALLED LOWER FRAME REPAIR AND INSTALLED LOWER REPAIR ANGLE. REF SRM 51-40-3/ FIG NR 1/ PAGES 1-6 AND SRM 51-30-02. REPAIR IS CLASSIFNov 24, 2007 · N464FE · Boeing 727225 · Fuselage Main, FrameSDR 07FDEA04912Pan · crackedDITCHING PAN IS CRACKED, LOCATED AT STA 1183, WL 20/8, LBL 27. REMOVED DITCHING PAN, STA 1183, LBL 27 REF SRM 51-30-02. FABRICATED DITCHING PAN REF BOEING DRAWING 65-29567-5 DITCHING PAN. HEAT TREATED REF BOEING DRAWING 65-29567-5. TREATED AND PRIMED DITCHNov 24, 2007 · N464FE · Boeing 727225 · Fuselage Miscellaneous StructureSDR 07FDEA04911Bracket · corrodedAFT LOWER CARGO DOOR, LOWER AFT CORNER WEB CORRODED INSTALLED NEW BRACKET PER DWG 65-57204 AND APPLIED LEVELING COMPOUND TO THE LOWER AREA AROUND BRACKET PER BOHM 52-36-22 PG 407.Nov 24, 2007 · N464FE · Boeing 727225 · Cargo/Baggage DoorsSDR 07FDEA04910Frame · crackedFWD PIT, PREVIOUS UNREPAIRED DAMAGE FRAME CRACKED AT BS 720, STR 19R REPAIRED FRAME 720 BTW STR 18R AND 19R REF FED EX EA 7-5310-113119, SRM 51-40-3 FIG 1 SRM 51-30-2 PG 2 51-30-5 PG 1 BOEING DWG 65-82614-12, 65-17664-50. TREATED AND PRIMED REF SRM 51-10-2 PNov 24, 2007 · N464FE · Boeing 727225 · Fuselage Main, FrameSDR DHL2007742049Angle · corrodedEXFOLIATED CORROSION AFT PIT FRAME BS 1070 JUST ABOVE STRINGER 22L. CUT OUT DAMAGED AREA (DIMENSION 2.25" BY 2.25"). FABRICATED REPAIR ANGLE FROM 7075-0 0.071" PO NR 7247111 (DIMENSION 13" BY 3.5") AND REPAIR FILLER FROM 7075-T6 0.063" PO NR 9005922 (DIMENSINov 23, 2007 · N742DH · Boeing 727225 · Fuselage Miscellaneous StructureSDR DHL2007742021Intercostal · crackedAFT PIT INTERCOSTAL BETWEEN BS 1148 - 1166 JUST BELOW STRINGER 26R HAS LOWER ANGLE CRACKED AND CORRODED. REMOVED TRANSITION PANEL SECTION FROM BS 1135 TO 1166 RIGHT, INTERCOSTAL AND CRACKED LOWER ANGLE IAW B-727 SRM 51-30-3. FABRICATED NEW ANGLE FROM 7075-T6Nov 23, 2007 · N742DH · Boeing 727225 · Fuselage Miscellaneous StructureSDR DHL2007742041Skin · gougedSTRINGER 19L HAS GOUGE IN SKIN AT LAP SEAM AT BS 720E. CUT OUT DAMAGE AREA APPROXIMATE 2.75" BY 4.25" ON STRINGER 19L AT BS 720E IAW B-727 SRM 53-30-3 FIGURE 6. FABRICATED REPAIR DOUBLER 2024-T3 0.071" PO NR 9005922 DIMENSION 12.5" BY 9", STRUCTURAL FILLER 2Nov 21, 2007 · N742DH · Boeing 727225 · Fuselage Main, Plate/SkinSDR DHL2007742032Skin · chafedRIGHT FUSELAGE CHAFFED AT BS 720D + 10" STRINGER 19R. CUT OUT DAMAGED AREA 6.75" BY 2.75" IAW B-727 SRM 53-30-3 FIGURE 6. FABRICATED DOUBLER REPAIR 2024-T3 0.071" PO NR 9005922 DIMENSION: 15.5" BY 9", STRUCTURAL FILLER 2024-T3 0.063" PO NR 9006027 DIMENSION:Nov 21, 2007 · N742DH · Boeing 727225 · Fuselage Main, Plate/SkinSDR DHL2007742070Skin · dentedDENT ON RIGHT FUSELAGE SKIN BS 460 2" ABOVE STRINGER 20R. CUT OUT DAMAGE (DIMENSION 2.25" BY 1.125") IAW B-727 SRM 51-10-1 AND 53-30-3 FIGURE 1. FABRICATED REPAIR DOUBLER FROM 2024-T3 0.063" PO NR 9006027 (DIMENSION 10" BY 6.5") AND REPAIR FILLER FROM 2024-TNov 20, 2007 · N742DH · Boeing 727225 · Fuselage Main, Plate/SkinSDR DHL2007742065Shear Tie · corrodedCORROSION AFT PIT ON SHEAR TIE BS 1148 ABOVE STRINGER 26R. REMOVED CORROSION IAW SRM 51-10-6, FOUND OUT OF LIMITS IAW SRM 53-10-1 FIGURE 1 AND 53-10-2 FIGURE 5. REMOVED SHEAR TIE IAW SRM 51-30-2. FABRICATED NEW SHEAR TIE IAW SRM 53-10-2 FIGURE 5 AND 51-30-Nov 20, 2007 · N742DH · Boeing 727225 · Fuselage Internal Mounting StructureSDR DHL2007742059Frame · crackedFUSELAGE STATION 303.9 FRAME WEB IS CRACKED AT STRINGER 15 WEB CUT OUT AND STRINGER 16 WEB CUT OUT AND CRACK INDICATION AT INBOARD CHORD WEB CUT OUT VERIFIED BY NDT. REMOVED CRACKED PARTS IAW B-727 SRM 51-30-2 AND SB727-53A-0153 REV 7. LOCATED AND DRILLED NENov 20, 2007 · N742DH · Boeing 727225 · Fuselage Main, FrameSDR DHL2007742016Skin · crackedEXTERIOR FUSELAGE SURFACE BS 615 ON STRINGER 27L 1 SKIN STRINGER FASTENER HOLE IS CRACKED, VERIFIED WITH HFEC. CUT OUT DAMAGED AREA, FABRICATED REPAIR DOUBLER AND REPAIR FILLER IAW B-727 SRM 53-30-2 FIGURE 2 AND 53-30-3 FIGURE 3. TREATED AND PRIMED REPAIR PANov 20, 2007 · N742DH · Boeing 727225 · Fuselage Main, Plate/SkinSDR DHL2007742014Tear Strap · corrodedAFT CARGO COMPARTMENT TEAR STRAP AT BS 1148 AT STRINGER 26R TO 25R IS EXFOLIATED. CUT OUT DAMAGED TEAR STRAP SECTION, FABRICATED TEAR STRAP REPAIR IAW B-727 SRM 53-30-4 FIGURE 9 AND 51-10-1. TREATED AND PRIMED PART IAW B-727 SRM 51-10-2 AND INSTALLED REPAIR Nov 20, 2007 · N742DH · Boeing 727225 · Fuselage Main, StructureSDR DHL2007742056Frame · dentedDENT AT FRAME BS 950D ABOVE STRINGER 26L. CUT OUT DAMAGED AREA IAW SRM 53-10-4 FIGURE 1. FABRICATED NEW FRAME REPAIR IAW SRM 53-10-4 FIGURE 1. HEAT TREATED FRAME REPAIR TO T6 CONDITION IAW FORM 1115 REV 11. LOCATED AND DRILLED NEW FRAME REPAIR IAW SRM 53-Nov 19, 2007 · N742DH · Boeing 727225 · Fuselage Main, FrameSDR DHL2007742053Frame · dentedDENT AFT PIT AT FRAME BS 1050 ABOVE STRINGER 26R. REMOVED FASTENERS AS REQUIRED FOR ACCESS IAW SRM 51-30-2. CUT OUT DAMAGED AREA DIMENSION 1" BY 1.5: AND FABRICATED REPAIR ANGLE IAW SRM 51-40-3 AND M/I 53-10-2 FIGURE 9. HEAT TREATED MATERIAL TO T6 0.071 CONov 19, 2007 · N742DH · Boeing 727225 · Fuselage Main, FrameSDR DHL2007742047Skin · crackedNR 6 SLAT SKIN CRACKED AT INBOARD SLAT HOOK UPPER MOUNT SCREW. C/W HFEC IAW B-727 NDT PT 6 51-00-00 FIGURE 23. CRACK TERMINATES IN FASTENER HOLE. FABRICATED DOUBLER REPAIR WITH 7075-T6 0.125" SIZE 7.5" BY 3.25" PO NR 9005685 IAW B-727 SRM 57-50-3 FIGURE 10.Nov 19, 2007 · N742DH · Boeing 727225 · Leading Edge DevicesSDR DHL2007742037Rib · crackedNR 3 SLAT RIB HAS SMALL CRACK ON INBOARD SIDE OF ACTUATOR ATTACHMENT, VERIFIED BY NDT. REMOVED 3 RIBS FROM NR 3 SLAT IAW B-727 SRM 51-30-2. INSTALLED 2 NEW RIBS IN PLACE, LOCATED AND DRILLED IAW B-727 SRM 51-30-5. REINSTALLED 1 RIB (REMOVED FOR ACCESS) IAW Nov 19, 2007 · N742DH · Boeing 727225 · Leading Edge DevicesSDR DHL2007742034Skin · damagedRIGHT ELEVATOR TAB HAS LARGE LIGHTNING STRIKE ON UPPER TRAILING EDGE. CUT OUT LIGHTNING STRIKE DAMAGE 0.5" BY 0.75". FABRICATED FILLER 0.5" BY 0.75" AND DOUBLER 2" BY 4" FROM 0.010" 2024-T3 PO NR 9003189 IAW B-727 SRM 55-20-2. BONDED FILLER AND DOUBLER, CLENov 19, 2007 · N742DH · Boeing 727225 · Elevator, Plate/SkinSDR DHL2007742018Frame · dentedDENT AT FRAME BS 950D ABOVE STRINGER 26L AFT PIT. CUT OUT DAMAGE AREA DIMENSION IAW B-727 SRM 53-10-4 FIGURE 1. FABRICATED NEW FRAME REPAIR IAW FORM FAS 1115 REV 11. LOCATED AND DRILLED NEW FRAME REPAIR IAW B-727 SRM 53-10-4 FIGURE 1 AND 51-30-5. TREATED ANov 19, 2007 · N742DH · Boeing 727225 · Fuselage Main, FrameSDR DHL2007742015Intercostal · crackedMAIN CARGO INTERCOSTAL AT BS 361 STRINGER 8R HAS FORWARD EDGE CRACKED. REMOVED CRACKED INTERCOSTAL IAW B-727 SRM 51-30-2. FABRICATED NEW INTERCOSTAL IAW B-727 SRM 51-20-1 AND 53-10-2 FIGURE 3. TREATED AND PRIMED NEW INTERCOSTAL IAW B-727 SRM 51-10-2 AND INSNov 19, 2007 · N742DH · Boeing 727225 · Fuselage Miscellaneous StructureSDR DHL2007742055Frame · dentedMULTIPLE DENTS AFT PIT FRAME BS 950F BETWEEN STRINGER 26L AND 25L. CUT OUT DAMAGED AREAS (2 EACH DIMENSION 1" BY 1"). FABRICATED REPAIR ANGLE FROM 7075-0 0.080" PO NR 9005665 (DIMENSION 17" BY 5.5") IAW B-727 SRM 53-10-2 FIGURE 5 AND 51-40-3 FIGURE 1. HEAT Nov 18, 2007 · N742DH · Boeing 727225 · Fuselage Main, FrameSDR DHL2007742064Frame · dentedDENTED FRAME AFT PIT BS 1110 ABOVE STRINGER 25R. REMOVED PREVIOUS REPAIR IAW B-727 SRM 51-30-2. CUT OUT DAMAGE (DIMENSION 1" BY 1") AND FABRICATED REPAIR ANGLE FROM 7075-0 0.071" PO NR 7247111 (DIMENSION 16" NR 4.25") IAW B-727 SRM 51-40-3 FIGURE 1 AND 53-10Nov 17, 2007 · N742DH · Boeing 727225 · Fuselage Main, FrameSDR 07FDEA04825Frame · crackedFWD PIT BODY FRAME, UPPER CHORD ANGLE, DOUBLER IS CRACKED, BS 720B, STR 26L-27L. REMOVED DAMAGE, FORMED REPAIR ANGLE AND FILLER, HEAT TREATED TO T-6 CONDITION, DRILLED AND TRIMMED REPAIR PARTS, ALODINED AND PRIMED. INSTALLED REPAIR REF SRM 51-40-3, 51-20-02Nov 17, 2007 · N464FE · Boeing 727225 · Fuselage Main, FrameSDR 07FDEA04824Frame · corrodedBODY FAIRING FRAME LOCATED BETWEEN PANELS 3358 AND 3458, FORWARD END HAS CORROSION. REPLACED FAIRING FRAME, REF BOEING DWG 65-59318 AND SRM 51-30-2, TREATED AND PRIMED REF MM 51-20-021-7, THIS IS CLASSIFIED AS A MINOR REPAIR.Nov 17, 2007 · N464FE · Boeing 727225 · Aerodynamic FairingsSDR DHL2007742022Strap · gougedFRAME INNER CHORD, UPPER STRAP HAS GOUGES FROM STRINGER 27R TO STRINGER 23R BS 560 AFT EDGE C-1 DOOR AREA. CUT OUT DAMAGED AREA APPROXIMATE DIMENSION 13" BY 5" IAW B-727 SRM 51-40-2 FIGURE 1. FABRICATED REPAIR DOUBLER FROM 2024-T3 0.050" PO NR 9005773 APPROXNov 16, 2007 · N742DH · Boeing 727225 · Fuselage Main, FrameSDR DJL2007742048Skin · crackedNR 7 SLAT SKIN CRACKED AT OUTBOARD SLAT HOOK UPPER MOUNT SCREW. C/W HFEC IAW B-727 NDTM PT 6 51-00-00 FIGURE 23. CRACK TERMINATES IN FASTENER HOLE. FABRICATED DOUBLER REPAIR USING 7075-T6 0.125 PO NR 9005685 DIMENSION 7.5" BY 3" IAW B-727 SRM 57-50-3 FIGURENov 15, 2007 · N742DH · Boeing 727225 · Leading Edge Devices
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