Boeing 727-223

Service difficulty reports · 5,313

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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 = '727223'
  ORDER BY difficulty_date DESC"

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SDR DHL2008753509Attach Angle · cracked"C" CHECK 1 ENG PYLON OB UPPER ATTACH ANGLE CRACKED AT SECOND HOLE, VERIFIED BY NDT. REMOVED DAMAGED ANGLE AT NR 1 ENGINE (PYLON) OB UPPER IAW B727 SRM 51-30-2. LOCATED HOLE, DRILLED AND DEBURRED ANGLE WITH P/N 69-16977-1 PO NR 738094 IAW B727 SRM 51-30-5 ANFeb 27, 2008 · N753DH · Boeing 727223 · Nacelle/Pylon, Attach FittingsSDR DHL2008753508Beam · damaged"C" CHECK, LT WING UPPER T/E PANEL SUPPORT "J" BEAM WBL 124 HAS DOUBLER REPAIR. REMOVED "J" BEAM IAW B727 SRM 51-30-2. FABRICATED NEW "J" BEAM PER DRAWING 65-21655 REV J AND EC-00829-001 FROM BAC1506-860 7075T6 DIM.81" PO NR 738052. TREATED AND PRIMED IAW BFeb 27, 2008 · N753DH · Boeing 727223 · Wing Miscellaneous StructureSDR DHL2008753501Structure · crackedDURING "C" RT I/B MID FLAP LOWER T/E CHORD AT CUTOUT WBL 102 IS CRACKED. OPENED SECTION OF LOWER PANEL RT I/B MID FLAP T/E IAW SRM 51-30-2. REMOVED SEAL AND SEL RETAINER FOR ACCESS IAW SRM 51-30-2. CUTOUT DAMAGE AREA AT CHORD APPROX 70 INCH. FAB NEW CHORD Feb 27, 2008 · N753DH · Boeing 727223 · Trailing Edge FlapsSDR DHL2008753502Support · crackedDURING "C" RT WING UPPER T/E WBL 124 "J" BEAM PANEL SUPPORT IS CRACKED FWD OF SPOILER ACTUATOR. REMOVED "J" BEAM IAW B727 SRM 51-30-2. FABRICATED NEW "J" BEAM PER DRAWING 65-21655 REV J AND EC-00829-001 FROM BAC1506-860 7075T6 DIM.81" PO NR 738738052. TREATFeb 27, 2008 · N753DH · Boeing 727223 · Wing Miscellaneous StructureSDR DHL2008752511Skin · crackedNR 3 NOSE COWL O/B T/E SKIN CRACKED ABOVE COWL LATCH. INSTALLED REPAIR IAW B727 SRM 54-30-2 FIG 1.Feb 26, 2008 · N752DH · Boeing 727223 · Engine Cowling SystemSDR DHL2008753506Skin · cracked"C" CHECK LT WING L/E CRACKED AT NR 4 SLAT O/B TRACK CUTOUT. REMOVED PAINT LT WING L/E NR 4 SLAT O/B TRACK IAW MM 51-20-1. STOP DRILLED WITH .250 AT THE END OF THE CRACK IAW SRM 51-10-1. FAB DOUBLER REPAIR IAW SRM 57-30-4 FIG 11 AND SRM 51-20-1 FIG 7. TREAFeb 26, 2008 · N753DH · Boeing 727223 · Wing, Plate/SkinSDR DHL2008752609Skin · crackedNR 3 NOSE COWL O/B T/E SKIN CRACKED ABOVE COWL LATCH. INSTALLED REPAIR IAW B727 SRM 54-30-2 FIG 1.Feb 26, 2008 · N752DH · Boeing 727223 · Engine Air Intake SystemSDR DHL2008753504Intercostal · corrodedDURING "C" CHECK FWD E/E COMPT BS 227.8 CORROSION ON WEB AND ANGLE BBL "0". REMOVED INTERCOSTAL DAMAGE, STIFFENER AND ANGLE FOR ACCESS IAW SRM 51-30-2. REMOVED CORROSION, FOUND OUT OF LIMITS IAW SRM 53-10-1 FIG 1. CUTOUT DAMAGED AREA APPROX 11 INCHES. FAB Feb 25, 2008 · N753DH · Boeing 727223 · Fuselage Miscellaneous StructureSDR DHL2008752509Flap · delaminatedRT INBD MIDFLAP HAS DELAM AT LOWER OUTBD TRAILING EDGE (AT WBL 238.0). CUT OUT DELAMINATED AREA ON RT I/B MIDFLAP APPROX 1.5 INCH DIAMETER APPLIED POTTING COMPOUND AND CURED AND SANDED SMOOTH. FABRICATED DOUBLER APPROX 3.5 DIAMETER FROM 7075T6 .020 PO NR 728Feb 23, 2008 · N752DH · Boeing 727223 · Trailing Edge FlapsSDR DHL2008752508Rib · crackedNR 1 SLAT ACTUATOR INBD ATTACHING RIB (AT SLAT) CRACKED. REMOVED RIB AND "U" CHANNEL FOUND CRACK IAW B727SRM 51-30-2 LOCATED, DRILLED AND DEBURRED RIB P/N 65-17327U3 PO 7375239 IAW B727 SRM 51-30-5. FABRICATED CHANNEL USING 2024-T3 .071 PO 9005922 DIM 6.5 INFeb 23, 2008 · N752DH · Boeing 727223 · Leading Edge DevicesSDR DHL2008752606Attach Fitting · crackedNR 1 SLAT ACTUATOR INBD ATTACHING RIB (AT SLAT) CRACKED. REMOVED RIB AND "U" CHANNEL FOUND CRACK IAW B727 SRM 51-30-2. LOCATED, DRILLED AND DEBURRED RIB P/N 65-17327U3 PO 7375239 IAW B727 SRM 51-30-5. FABRICATED CHANNEL USING 2024-T3 .071 PO 9005922 DIM 6.5Feb 23, 2008 · N752DH · Boeing 727223 · Wing, Attach FittingsSDR DHL2008752607Attach Fitting · crackedNR 1 SLAT ACTUATOR INBD ATTACHING RIB (AT SLAT) CRACKED. REMOVED RIB AND "U" CHANNEL FOUND CRACK IAW SRM 51-30-2. LOCATED, DRILLED AND DEBURRED RIB IAW SRM 51-30-5. FABRICATED CHANNEL IAW BDW NR 65-17327 AND SRM 51-20-01, 51-20-2, 51-30-5. INSTALLED RIB ANFeb 23, 2008 · N752DH · Boeing 727223 · Leading Edge DevicesSDR DHL2008752506Frame · dentedAFT PIT STA1130 HAS DENT IN RADIUS OF FRAME AT S-26L. CUTOUT DAMAGED AREA AT AFT CARGO COMP STA 1130 STR 26L DIMENSION 3/4 INCH BY 1/2 INCH IAW B727SRM 51-40-3 FIG 1. FABRICATED FRAME REPAIR MATERIAL USED 7075-O .071 PO NR 9006377 DIMENSION 9" BY 4" IAW B727Feb 8, 2008 · N752DH · Boeing 727223 · Fuselage Main, FrameSDR DHL2008752512Angle · crackedRT WING I/B L/E AREA AT FSS 107.2 FWD WING SPAR TERMINAL JOINT ANGLE CRACK AT BOTTOM. STOP DRILLED CRACK DIM .250 IAW B727 SRM 51-10-1 HFEC VERIFIED THAT CRACK END ON STOP DRILL HOLE IAW B727 NDTM PT6 51-00-00 FIG 23. FABRICATED NEW ANGLE USING 7075-T6 .063 Feb 8, 2008 · N752DH · Boeing 727223 · Wing Miscellaneous StructureSDR DHL2008752505Frame · dentedAFT PIT STA1130 HAS DENT IN RADIUS OF FRAME AT S-26L. CUTOUT DAMAGED AREA AT AFT CARGO COMP STA 1130 STR 26L DIMENSION 3/4 INCH BY 1/2 INCH IAW B727SRM 51-40-3 FIG1. FABRICATED FRAME REPAIR MATERIAL USED 7075-O .071 PO NR 9006377 DIMENSION 9 INCH BY 4 INCH IFeb 8, 2008 · N752DH · Boeing 727223 · Fuselage Main, FrameSDR DHL2008752610Spar · crackedRT WING INBOARD L/E AREA AT FSS 107.2 FWD WING SPAR TERMINAL JOINT ANGLE CRACK AT BOTTOM. STOP DRILLED CRACK DIM .250 IAW B727 SRM 51-10-1. HFEC VERIFIED THAT CRACK END ON STOP DRILL HOLE IAW B727 NDTM PT6 51-00-00 FIG 23. FABRICATED NEW ANGLE USING 7075-T6Feb 8, 2008 · N752DH · Boeing 727223 · Wing SparSDR DHL2008752603Frame · dentedAFT PIT STA1130 HAS DENT IN RADIUS OF FRAME AT S-26L. CUTOUT DAMAGED AREA AT AFT CARGO COMP STA 1130 STR 26L DIMENSION 3/4" BY 1/2" IAW B727 SRM 51-40-3 FIG 1. FABRICATED FRAME REPAIR MATERIAL USED 7075-O .071 PO NR 9006377 DIMENSION 9 INCH BY 4 INCHES IAW BFeb 8, 2008 · N752DH · Boeing 727223 · Fuselage Main, FrameSDR DHL2008752604Frame · dentedAFT PIT STA1130 HAS DENT IN RADIUS OF FRAME AT S-26L. CUTOUT DAMAGED AREA AT AFT CARGO COMP STA 1130 STR 26L DIMENSION 3/4" BY 1/2" IAW B727 SRM 51-40-3 FIG 1. FABRICATED FRAME REPAIR MATERIAL USED 7075-O .071 PO NR 9006377 DIMENSION 9" BY 4" IAW B727 SRM 51Feb 8, 2008 · N752DH · Boeing 727223 · Fuselage Main, FrameSDR DHL2008749019Angle · corrodedDURING C CHECK, EXFOLIATION NOTED AT C2 DOOR CUT OUT, BS 990 (FRAME) BETWEEN STRINGERS 26R AND 27R. REMOVED CORROSION AT C2 DOOR CUT OUT BS 990 IAW SRM 51-10-6, ORIGINAL THICKNESS 0.100, MATERIAL LOSS 0.35, MATERIAL REMAINING 0.65, FOUND OUT OF LIMITS IAW SRMFeb 6, 2008 · N749DH · Boeing 727223 · Fuselage Main, StructureSDR DHL2008752510Skin · delaminatedLT OB AILERON TAB UPPER SURFACE HAS DELAMINATED AREA. CUTOUT DELAMINATED AREA 2 INCHES DIA ON LT O/B AIL TAB UPPER SURFACE. FABRICATED FILLER AND DOUBLER IAW B727SRM 57-50-2, BONDED FILLER AND DOUBLER IAW B727SRM 51-40-20.Feb 6, 2008 · N752DH · Boeing 727223 · Aileron TabsSDR DHL2008752507Structure · crackedLT WING UPPER T/E WBL 320 NR 4 SPOILER INBOARD CENTER HINGE CUTOUT IS CRACKED FWD. REMOVED FASTENERS AT LT WING UPPER T/E WBL 320 NR 4 SPOILER INBOARD CENTER HINGE CUTOUT IAW B727SRM 51-30-2. STOP DRILLED 0.250" DIA AT END OF CRACK IAW B727 SRM 57-30-4 FIG 1Feb 6, 2008 · N752DH · Boeing 727223 · Wing Miscellaneous StructureSDR DHL2008752608Skin · delaminatedLT OB AILERON TAB UPPER SURFACE HAS DELAMINATED AREA. CUTOUT DELAMINATED AREA 2 INCHES DIA ON LT O/B AILERON. TAB UPPER SURFACE FABRICATED FILLER AND DOUBLER IAW B727 SRM 57-50-2, BONDED FILLER AND DOUBLER IAW B727SRM 51-40-20.Feb 6, 2008 · N752DH · Boeing 727223 · Aileron TabsSDR DHL2008752605Skin · crackedLT WING UPPER T/E WBL 320 NR 4 SPOILER INBOARD CENTER HINGE CUTOUT IS CRACKED FWD. REMOVED FASTENERS AT LT WING UPPER T/E WBL 320 NR 4 SPOILER INBOARD CENTER HINGE CUTOUT IAW B727 SRM 51-30-2. STOP DRILLED 0.250" DIA AT END OF CRACK IAW B727 SRM 57-30-4 FIG Feb 6, 2008 · N752DH · Boeing 727223 · Wing, Plate/SkinSDR DHL2008752601Web · crackedLT SIDE OF AIRSTAIR WEB CRACKED AT LIGHTING HOLE BS 1223. CUTOUT DAMAGED AREA AT LT SIDE OF AIRSTAIR WEB SAT 1223 IAW B727 SRM 51-40-2 FIG1. FABRICATED DOUBLER MAT USED 7075T6 0.032 DIMENSION 2.5" BY 2.5" PO NR 9006457 IAW B727 SRM 51-40-2 FIG 1 AND B727 SRMFeb 4, 2008 · N752 · Boeing 727223 · Entrance StairsSDR DHL2008752502Structure · crackedRT WING NR 5 L/E SLAT WING L/E I/B BULKSEAL HAS SURFACE CRACKED. REMOVED FASTENERS AT RT WING NR 5 L/E SLAT WING L/E I/B BULK SEAL IAW SRM 51-30-2. STOP DRILLED 0.250 AT END OF CRACK IAW SRM 51-10-1. FABRICATED DOUBLER REPAIR AT L/E SLAT MATERIAL USED 2024TFeb 4, 2008 · N752DH · Boeing 727223 · Leading Edge DevicesSDR DHL2008752504Web · crackedLT SIDE OF AIRSTAIR WEB CRACKED AT LIGHTING HOLE BS 1223. CUTOUT DAMAGED AREA AT LT SIDE OF AIRSTAIR WEB SAT 1223 IAW SRM 51-40-2 FIG 1. FABRICATED DOUBLER MAT USED 7075T6 0.032 DIMENSION 2.5 INCH BY 2.5 INCH PO NR 9006457 IAW SRM 51-40-2 FIG 1 AND SRM 53-10Feb 4, 2008 · N752DH · Boeing 727223 · Entrance StairsSDR DHL2008752503Structure · crackedRT WING NR 5 L/E SLAT WING L/E I/B BULKSEAL HAS SURFACE CRACKED. REMOVED FASTENERS AT RT WING NR 5 L/E SLAT WING L/E I/B BULK SEAL IAW SRM 51-30-2. STOP DRILLED 0.250 AT END OF CRACK IAW SRM 51-10-1. FABRICATED DOUBLER REPAIR AT NR 5 L/E SLAT MATERIAL USED Feb 4, 2008 · N752DH · Boeing 727223 · Leading Edge DevicesSDR DHL2008752501Structure · crackedRT WING NR 5 L/E SLAT WING L/E I/B BULKSEAL HAS SURFACE CRACKED. REMOVED FASTENERS AT RT WING NR 5 L/E SLAT WING L/E I/B BULK SEAL IAW SRM 51-30-2. STOP DRILLED 0.250 AT END OF CRACK IAW SRM 51-10-1. FABRICATED DOUBLER REPAIR AT L/E SLAT MATERIAL USED 2024TFeb 4, 2008 · N752DH · Boeing 727223 · Leading Edge DevicesSDR DHL2008752570Structure · crackedRT WING NR 5 L/E SLAT WING L/E I/B BULKSEAL HAS SURFACE CRACKED. REMOVED FASTENERS AT RT WING NR 5 L/E SLAT WING L/E I/B BULK SEAL IAW B727 SRM 51-30-2. STOP DRILLED 0.250 AT END OF CRACK IAW B727 SRM 51-10-1. FABRICATED DOUBLER REPAIR AT L/E SLAT MATERIAL Feb 4, 2008 · N752DH · Boeing 727223 · Leading Edge DevicesSDR DHL2008752550Structure · crackedRT WING NR 5 L/E SLAT WING L/E I/B BULKSEAL HAS SURFACE CRACKED. REMOVED FASTENERS AT RT WING NR 5 L/E SLAT WING L/E I/B BULK SEAL IAW B727 SRM 51-30-2. STOP DRILLED 0.250 AT END OF CRACK IAW B727 SRM 51-10-1. FABRICATED DOUBLER REPAIR AT L/E SLAT MATERIAL Feb 4, 2008 · N752DH · Boeing 727223 · Leading Edge DevicesSDR DHL2008752500Structure · crackedRT WING NR 5 L/E SLAT WING L/E I/B BULKSEAL HAS SURFACE CRACKED. REMOVED FASTENERS AT RT WING NR 5 L/E SLAT WING L/E I/B BULK SEAL IAW B727 SRM 51-30-2. STOP DRILLED 0.250 AT END OF CRACK IAW B727 SRM 51-10-1. FABRICATED DOUBLER REPAIR AT L/E SLAT MATERIAL Feb 4, 2008 · N752DH · Boeing 727223 · Leading Edge DevicesSDR DHL2008749013Stringer · crackedAFT PIT STRINGER 29R CRACKED AT SPLICE AFT OF BS 950. REMOVED AFT PIT STRINGER 29R, LOCATED AND DRILLED NEW STRINGER 29L P/N 65-52441-8 PO NR 7370104. INSTALLED NEW STRINGER 29L FROM BS 950 TO BS 1010 IAW B-727 SB 727-53-0179.Feb 4, 2008 · N749DH · Boeing 727223 · Fuselage Main, Longeron/StringerSDR DHL2008752602Web · crackedLT SIDE OF AIRSTAIR WEB CRACKED AT LIGHTING HOLE BS 1223. CUTOUT DAMAGED AREA AT LT SIDE OF AIRSTAIR WEB STA 1223 IAW SRM 51-40-2 FIG1. FABRICATED DOUBLER IAW SRM 51-40-2 FIG1 AND SRM 53-10-2 FIG 6. TREATED AND PRIMED AREA IAW SRM 51-10-2. INSTALLED DOUBLEFeb 4, 2008 · N752DH · Boeing 727223 · Fuselage Miscellaneous StructureSDR DHL2008752600Slat · crackedRT WING NR 5 L/E SLAT WING L/E I/B BULKSEAL HAS SURFACE CRACKED. REMOVED FASTENERS AT RT WING NR 5 L/E SLAT WING L/E I/B BULK SEAL IAW SRM 51-30-2. STOP DRILLED 0.250 AT END OF CRACK IAW SRM 51-10-1. FABRICATED DOUBLER REPAIR AT L/E SLAT MATERIAL USED 2024TFeb 4, 2008 · N752DH · Boeing 727223 · Wing, Plate/SkinSDR DHL2008752515Beam · crackedRT WING T/E UPPER "J" BEAM IS CRACKED AT WBL 118. ACCOMPLISHED REPAIR TO CRACKED RT WING T/E UPPER "J" BEAM WBL 118. REPLACED MATERIAL USED J BEAM P/N BAC1506-860 7075T6 DIM 80.625" IAW EC-00795-001, DWG NR 65-21655 REV J DATED 12/4/78, B727 SRM 51-30-2.Feb 3, 2008 · N752DH · Boeing 727223 · Wing Miscellaneous StructureSDR DHL2008752513Angle · crackedCRACK AT RT MLG WHEEL WELL STATION 870 FWD INBD LWR BULKHEAD 18: LEFT OF LOAD CONTROL VALVE 8 INCHES RIGHT OF CENTER. REMOVED AND REPLACED ANGLE AT RT MLG W/W STA 870 FWD I/B LOWER BULKHEAD IAW B727SRM 51-30-2.Feb 3, 2008 · N752DH · Boeing 727223 · Fuselage Miscellaneous StructureSDR DHL2008752611Angle · crackedCRACK AT RT MLG WHEEL WELL STATION 870 FWD INBD LWR BULKHEAD 18: LEFT OF LOAD CONTROL VALVE 8" RIGHT OF CENTER. REMOVED AND REPLACED ANGLE AT RT MLG W/W STA 870 FWD INBOARD LOWER BULKHEAD IAW B727 SRM 51-30-2.Feb 3, 2008 · N752DH · Boeing 727223 · Fuselage Miscellaneous StructureSDR DHL2008780002Flap · cracked1 INCH CRACK ON I/B LOWER SIDE OF NR 3 K FLAP JUST ABOVE BULL NOSE.Jan 30, 2008 · N780DH · Boeing 727223 · Trailing Edge FlapsSDR DHL2008780001Flap · delaminatedLT WING I/B FORE FLAP DELAMINATED BEHIND I/B FLAP TRACK AREA 7 INCH BY 3 INCH.Jan 29, 2008 · N780DH · Boeing 727223 · Trailing Edge FlapsSDR DHL2008749009Angle · crackedRIGHT ELEVATOR LOWER SKIN INTERIOR SUPPORT ANGLE IS CRACKED ELEVATOR STATION 20 VIEW THROUGH ACCESS 9405. REMOVED ANGLE IAW SRM 51-30-2. FABRICATED NEW ANGLE IAW SRM 51-20-1, 51-20-2, 51-30-5, 55-20-2 FIGURE 7. ALODINE AND PRIMED ANGLE IAW SRM 51-10-2. INSJan 23, 2008 · N749DH · Boeing 727223 · Elevator Miscellaneous StructureSDR DHL2008749008Attach Fitting · crackedRT WING NR 5 SLAT ACTUATOR ATTACH FITTING CRACKED AT INBOARD SIDE, INSIDE LEADING EDGE STRUCTURE. FABRICATED NEW RIBS (2 EACH) IAW SRM 57-50-2 FIGURE 2, 51-20-1 FIGURE 1 AND SRM 51-20-1 FIGURE 2. IAW ER 2-37163-801 REV A. INSTALLED NEW RIBS AT NR 5 SLAT IJan 22, 2008 · N749DH · Boeing 727223 · Leading Edge DevicesSDR DU4R2008191Skin · corrodedS/O 304002 N/R NR26444 CORROSION FWD CARGO BILGE AREA BS 660 S-28L - S-28R. REPAIRED BY CUTTING OUT CORRODED AREA BS 661 TO BS 664.5, NDT VERIFIED NO CRACKS IAW NPTM PT. 6 51-00-00 FIG. 23. FABRICATED AND INSTALLED REPAIR DOUBLER 11.6 INCH X 16.25 INCH FROM 2Jan 19, 2008 · N289MT · Boeing 727223 · Fuselage Main, Plate/SkinSDR DHL2008749018Angle · corrodedDURING C CHECK, EXFOLIATION AT FASTENER ON "L" ANGLE ON UPPER SURFACE OF LONGITUDINAL FRAME, BS 919 RWBL 70.5. FABRICATED NEW "L" ANGLE IAW SRM 51-30-5, 51-10-3 AND 53-10-2 FIG 4. INSTALLED IAW SRM 51-30-2. NR 033718Jan 15, 2008 · N749DH · Boeing 727223 · Fuselage Miscellaneous StructureSDR DHL2008749007Seat Track · corrodedMAIN CABIN SEAT TRACK CORRODED FROM BS 500 TO 520 LBL25. FABRICATED NEW SEAT TRACK SECTION FROM P/N BAC 1520-792 7178-T6 PO NR 9006152 APPROXIMATE LENGTH 210" IAW B-727 SRM 53-10-5 FIGURE 1 AND SRM 53-10-2 FIGURE 7. INSTALLED NEW SEAT TRACK SECTION USING PREJan 15, 2008 · N749DH · Boeing 727223 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2008749006Seat Track · corrodedSEAT TRACK CORRODED IN MAIN CARGO COMPARTMENT BS 480 - 620 LBL 45. FABRICATED NEW SEAT TRACK IAW SRM 53-10-2 FIGURE 7 AND SRM 53-10-5 FIGURE 1. INSTALLED NEW SEAT TRACK IAW SRM 53-10-5 FIGURE 1 USING PREVIOUS GOOD CONDITION SPLICE PARTS.Jan 15, 2008 · N749DH · Boeing 727223 · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA00132Connector · burnedAT ROTATION OFF FLAG IN CAPT'S ALTIMETER AND ALT SELECT WINDOW APPEARED. FOUND RACK CONNECTOR D609 CENTER SECTION, BEHIND NR 1 CADC BLACK FROM ELECTRICAL DAMAGE. INSTALLED WIRE NUMBERS W0007-162-22 AND W0007-9069-2 2 IN D609A PIN 12 PER BOEING HOOK UP LIST.Jan 15, 2008 · N223FE · Boeing 727223 · Navigation System WiringSDR DHL2008749005Angle · crackedC-1 DOOR FORWARD FRAME REINFORCEMENT 3RD ANGLE CRACKED BS 500. REMOVED ANGLE IAW SRM 51-30-2. FABRICATED NEW ANGLE IAW SRM 51-20-2, 51-30-5 AND 52-30-1 FIGURE 4. ALODINE AND PRIMED ANGLE IAW SRM 51-10-2. INSTALLED ANGLE IAW SRM 51-30-2 AND 51-40-3 FIGURE 1Jan 14, 2008 · N749DH · Boeing 727223 · Cargo/Baggage DoorsSDR DHL2008749004Shear Tie · corrodedFORWARD CARGO COMPARTMENT SHEAR TIE CORRODED AT FORWARD SIDE OF BS 680 FRAME AND STRINGER 26R. REMOVED CORRODED SHEAR TIE IAW SRM 51-30-2. CLEANED AREA AROUND SHEAR TIE IAW SOPM 20-30-3. NO DEFECTS NOTED IAW SRM 51-10-6 PARA 3. FABRICATED NEW SHEAR TIE IAWJan 14, 2008 · N749DH · Boeing 727223 · Fuselage Internal Mounting StructureSDR DHL2008749003Shear Tie · corrodedFORWARD CARGO COMPARTMENT SHEAR TIE AND FRAME CORRODED AT FORWARD SIDE OF BS 720F STRINGER 25L. REMOVED SHEAR TIE IAW SRM 51-30-2. CLEANED SKIN AREA IAW MM 12-40-00, NO CORROSION NOTED. FABRICATED NEW SHEAR TIE IAW SRM 53-10-2 FIGURE 3, 51-20-2 AND 53-10-4 Jan 14, 2008 · N749DH · Boeing 727223 · Fuselage Internal Mounting StructureSDR DHL2008749002Stringer Clip · corrodedFORWARD CARGO COMPARTMENT STRINGER CLIP CORRODED AT STRINGER 26L BS 740. REMOVED STRINGER CLIP IAW SRM 51-30-2. CORROSION OUT OF LIMITS IAW SRM 53-10-1 FIGURE 1. CLEANED LOWER AREA IAW MM 12-40-00 NO CORROSION NOTED. FABRICATED NEW PART IAW SRM 53-10-2 FIJan 12, 2008 · N749DH · Boeing 727223 · Fuselage Main, Attach Fittings
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