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 DHL2003742530Stiffener · crackedDURING C-CHECK, RT WING L/E BL 92 INT FRAME VERT STIFFENER IS CRACKED ON BOTTOM THRU FASTENER HOLE. CUT OUT DAMAGED AREA DIM 2.5 X 2 INCH IAW B-727 SRM 51-40-4. FABRICATED NEW FILLER IAW B-727 SRM 51-40-4. TREATED AND PRIMED IAW B-727 SRM 51-10-2 AND INSTALNov 24, 2003 · N742DH · Boeing 727225 · Wing Miscellaneous StructureSDR DHL2003742521Doubler · crackedDURING C-CHECK, RT WING L/E STA 130 INT FRAME DOUBLER TO UPPER SURF IS CRACKED ABOVE FASTENER. REMOVED DAMAGED AREA IAW B-727 SRM 51-30-2. FABRICATED NEW DOUBLER IAW SRM MAT ID 7075 T6 .050 PO 90096 DIM 10 X 1.75 INCH IAW B-727 SRM 51-40-4 FIG 1. TREATED PNov 24, 2003 · N742DH · Boeing 727225 · Wing Main, Frame StructureSDR DHL2003742515Skin · crackedDURING C-CHECK, NR 5 SLAT OUTBOARD HOOK CUTOUT IN UPPER L/E SKIN AFT OUTBOARD CORNER IS CRACKED. REMOVED PAINT AT AFFECTED AREA IAW MM 51-20-1 AND STOP DRILLED CRACK IAW SRM 51-10-1 HFEC VERIFIED STOP DRILL IAW B-727 NDT MM PT 6 51-00-00 FIG 23. FABRICATED PNov 24, 2003 · N742DH · Boeing 727225 · Leading Edge DevicesSDR DHL2003742566Seat Track · damagedDURING C-CHECK, NR 5 SEAT TRACK AT BS 480 IS DAMAGED. REMOVED DAMAGED SEAT TRACK AND FABED NEW FROM BAC1520-792 PO 902203 DIM 158.5 INCH AND TWO SPLICE ANGLES FROM BAC1503-100122 PO 900221 DIM 14 X 2.5 INCH AND 1 EA SPLICE PLATE FROM 7075-T6 .250 PO 99112793Nov 23, 2003 · N742DH · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2003742564Door Frame · corrodedDURING C-CHECK, MAIN E&E COMPARTMENT DOOR CUTOUT FWD FRAME CORRODED/EXFOLIATED 100 PERCENT MATERIAL LOSS BS 424, BL 0-RBL 5 WL 150. REMOVED FASTENERS FOR ACCESS AS REQUIRED, FABRICATED NEW FWD FRAME IAW B727 SRM 51-30-2, FABRICATED NEW FWD FRAME AT BS 424 BLNov 23, 2003 · N742DH · Boeing 727225 · Fuselage Main, StructureSDR DHL2003742563Floorbeam · corrodedDURING C-CHECK, CORROSION ON BS 344 FLOORBEAM UPPER CHORD AROUND NUT PLATES ATTACHING 9G BULKHEAD TO FLOORBEAM, LBL 50 RBL 50,WL 208,AS VIEWED FROM NWW DOGHOUSE AREA. REMOVED 9G BULKHEAD,AND SHEAR WEB FOR ACCESS, IAW B727 SRM 51-30-2 AND MM 53-20-11. REMOVENov 23, 2003 · N742DH · Boeing 727225 · Fuselage Main, Floor BeamSDR DHL2003742562Skin · dentedDURING C-CHECK, NR 1 CARGO DOOR AFT SIDE SKIN BEHIND THE REPAIR IS DENTED. CUT OUT DAMAGED LWR SECTION OF SKIN & FABED NEW FROM 2024-T3 .040, PO 900355 DIM 58.5 X 14.375 INCH AND DOUBLERS 6 EA FROM 2024-T3 .063, PO 900355, DIM 5 X 8 INCH, 5.5 X 4.5 INCH, 8.87Nov 23, 2003 · N742DH · Boeing 727225 · Cargo/Baggage DoorsSDR DHL2003742550Floorbeam · corrodedDURING C-CHECK AT FLIGHTSTAR AIRCRAFT SERVICES IN JACKSONVILLE, FLORIDA DISCREPANCY IS AS FOLLOWS; N/R 60029 CORROSION ON BS 344 FLOORBEAM UPPER CHORD AROUND NUT PLATES ATTACHING 9G BULKHEAD TO FLOORBEAM LBL 50 RBL 50 WL 208, AS VIEWED FROM NWW DOGHOUSE AREA. Nov 23, 2003 · N742DH · Boeing 727225 · Fuselage Main, Floor BeamSDR DHL200374266Seat Track · damagedDURING C-CHECK, NR 5 SEAT TRACK AT BS 480 IS DAMAGED. REMOVED DAMAGED SEAT TRACK AND FABBED NEW FROM BAC1520-792 PO 902203 DIM 158.5 INCH AND TWO SPLICE ANGLES FROM BAC1503-100122 PO 900221 DIM 14 INCH X 2.5 INCH AND 1 EA SPLICE PLATE FROM 7075-T6 .250 PO 991Nov 23, 2003 · N742DH · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR DHL200374264Door Frame · corrodedDURING C-CHECK, MAIN E&E COMPARTMENT DOOR CUTOUT FWD FRAME CORRODED/EXFOLIATED, 100 PERCENT MATERIAL LOSS BS 424, BL 0 - RBL 5 WL 150. REMOVED FASTENERS FOR ACCESS AS REQUIRED, FABRICATED NEW FWD FRAME IAW B727 SRM 51-30-2, FABRICATED NEW FWD FRAME AT BS 424 Nov 23, 2003 · N742DH · Boeing 727225 · Fuselage Main, StructureSDR DHL200374263Floorbeam · corrodedDURING C-CHECK, CORROSION ON BS 344 FLOORBEAM UPPER CHORD AROUND NUT PLATES ATTACHING 9G BULKHEAD TO FLOORBEAM, LBL 50 - RBL 50, WL 208, AS VIEWED FROM NWW DOGHOUSE AREA. REMOVED 9G BULKHEAD, AND SHEAR WEB FOR ACCESS IAW B727 SRM 51-30-2 AND MM 53-20-11, REMONov 23, 2003 · N742DH · Boeing 727225 · Fuselage Main, Floor BeamSDR DHL200374262Skin · dentedDURING C-CHECK, NR 1 CARGO DOOR AFT SIDE SKIN BEHIND THE REPAIR IS DENTED. CUT OUT DAMAGED LWR SECTION OF SKIN & FABED NEW FROM 2024-T3 .040, PO 900355 DIM 58.5 X 14.375 INCH AND DOUBLERS 6 EA FROM 2024-T3 .063, PO 900355, DIM 5 X 8 INCH, 5.5 X 4.5 INCH, 8.87Nov 23, 2003 · N742DH · Boeing 727225 · Cargo/Baggage DoorsSDR DHL200374250Floorbeam · corrodedDURING C-CHECK, CORROSION ON BS 344 FLOORBEAM UPPER CHORD AROUND NUT PLATES ATTACHING 9G BULKHEAD TO FLOORBEAM LBL 50 - RBL 50 WL 208, AS VIEWED FROM NWW DOGHOUSE AREA. REMOVED 9G BULKHEAD, FLOORBOARDS AND SHEAR WEB FOR ACCESS IAW B727 SRM 51-30-2 AND MM 53-2Nov 23, 2003 · N742DH · Boeing 727225 · Fuselage Main, Floor BeamSDR DHL2003742555Structure · corrodedDURING C-CHECK, CORROSION ON LOWER SURFACE OF LEFT NOSE WHEEL WELL MID-CHORD BS 296, LBL 20, WL 165 AS VIEWED THROUGH FWD LEFT DOGHOUSE FLOOR PRESSURE PANEL. REMOVED AND REPLACED LT NOSE WHEEL WELL AND CHORD BS 296 USING P/N 65-19862-19 PO3348224 IAW B-727 SRNov 23, 2003 · N742DH · Boeing 727225 · Fuselage Main, StructureSDR DHL2003742509Floorbeam · corrodedDURING C-CHECK, CORROSION ON BS 360 FLOORBEAM UPPER CHORD SPLICE LBL 20, WL 208. REMOVED DAMAGED PARTS AND FABBED NEW T-SPLICE FROM BAC 1505-100617 PO 90041 DIM 12 INCHES LONG AND 2 EACH SPLICE ANGLES FROM BAC 1505-29222 PO 9912219 DIM 12 INCHES AND 8.5 INCHENov 23, 2003 · N742DH · Boeing 727225 · Fuselage Main, Floor BeamSDR DHL200374277Skin · gougedDURING C-CHECK, FUSELAGE SKIN TWO LIGHT GOUGES STA 670 BETWEEN STR 5R TO 6R. CLEANED GAUGE AT BS 670 STR 5R TO 6R MATERIAL LOSS 0.010 FOUND TO BE OUT OF LIMITS IAW B727 SRM 53-30-3 FIG 1. CUT OUT DAMAGED AREA DIM APPROX 4 X 1 INCH IAW B727 SRM 53-30-3 FIG 1.Nov 22, 2003 · N742DH · Boeing 727225 · Fuselage Main, Plate/SkinSDR DHL200374276Skin · dentedDURING C-CHECK, FUSE SKIN TWO DENTS STA 430 BETWEEN STR 2R AND 3R. MEASURED DENT AND FOUND TO BE OUT OF LIMITS IAW B727 SRM 53-30-1 FIG 1. REMOVED FASTENERS FOR ACCESS AND CUT OUT DAMAGED AREA, DIM 4 X 1.375 INCH AND FABRICATED ONE DOUBLER DIM 14 X 9.5 INCH Nov 22, 2003 · N742DH · Boeing 727225 · Fuselage Main, Plate/SkinSDR DHL200374275Skin · dentedDURING C-CHECK, UPPER FUSELAGE EXTERIOR SKIN BS 390 BETWEEN STR 6L AND 7L SKIN IS DENTED. DENT AT BS 390 STR 6L TO STR 7L FOUND OUT OF LIMITS IAW B727 SRM 53-30-1 FIG 1. REMOVED FASTENERS FOR ACCESS AND CUT OUT DAMAGED AREA, DIMENSIONS 3 X 2 INCH IAW B727 SRNov 22, 2003 · N742DH · Boeing 727225 · Fuselage Main, Plate/SkinSDR DHL200374274Skin · damagedDURING C-CHECK, FUSELAGE EXTERIOR BS 620 STR 10R LAP SEAM VERIFIED REPAIRS DONE FOR STRUCTURAL REPAIRS MANUAL COMPLIANCE. EVALUATED REPAIR AND FOUND IT TO BE NON-COMPLIANT IAW 727 SRM 53-30-3 FIG 24. REMOVED PREVIOUS REPAIR AND FABBED NEW STRUCTURAL FILLER FNov 22, 2003 · N742 · Boeing 727225 · Fuselage Main, Plate/SkinSDR DHL2003742568Skin · dentedDURING C-CHECK, UPPER FUSELAGE EXTERIOR SKIN BS 390 BETWEEN 6TH LEFT AND 7TH SKIN IS DENTED. DENT AT BS 390 STR 6L TO STR 7L FOUND OUT OF LIMITS IAW B727 SRM 53-30-1 FIG 1. REMOVED FASTENERS FOR ACCESS AND CUT OUT DAMAGED AREA DIM 3 X 2 INCH IAW B727 SRM 53-Nov 22, 2003 · N742DH · Boeing 727225 · Fuselage Main, Plate/SkinSDR DHL200374268Skin · dentedDURING C-CHECK, UPPER FUSELAGE EXTERIOR SKIN BS 390 BETWEEN 6TH LEFT AND 7TH SKIN IS DENTED. DENT AT BS 390 STR 6L TO STR 7L FOUND OUT OF LIMITS IAW B727 SRM 53-30-1 FIG 1. REMOVED FASTENERS FOR ACCESS AND CUT OUT DAMAGED AREA DIM 3 X 2 INCH IAW B727 SRM 53-Nov 22, 2003 · N742DH · Boeing 727225 · Fuselage Main, Plate/SkinSDR DHL2003742534Skin · gougedDURING C-CHECK, FUSELAGE SKIN TWO LIGHT GAUGES STA 670 BETWEEN STR 5 R TO STR 6 R. CLEANED GAUGES AT BS 670 STR 5 R TO 6 R MATERIAL LOSS 0.010 FOUND TO BE OUT OF LIMITS IAW B-727 SRM 53-30-3 FIG (1). CUT OUT DAMAGED AREA DIM APPROX 4 BY 1 INCH IAW B-727 SRM Nov 22, 2003 · N742DH · Boeing 727225 · Fuselage Main, Plate/SkinSDR DHL2003742508Skin · misrepairedDURING C-CHECK, FUSELAGE EXTERIOR BS 620 STR 10R LAP SEAM VERIFY REPAIR DONE FOR STRUCTURAL REPAIRS MANUAL COMPLIANCE. EVALUATED REPAIR AND FOUND IT TO BE NON-COMPLIANT IAW B-727 SRM 53-30-3 FIG 24. REMOVED PREVIOUS REPAIR AND FABBED NON STRUCTURAL FILLER FRNov 22, 2003 · N742DH · Boeing 727225 · Fuselage Main, Plate/SkinSDR DHL2003742500Skin · dentedDURING C-CHECK, FUSELAGE SKIN TWO DENTS STA 430 BETWEEN STR 2R AND STR 3R. MEASURE DENT AND FOUND TO BE OUT OF LIMITS IAW B-727 SRM 53-30-1 FIG 1. REMOVED FASTENERS FOR ACCESS AND CUT OUT DAMAGE AREA DIM 4 INCH X 1.375 INCH AND FABRICATED ONE DOUBLER DIM 14 Nov 22, 2003 · N742DH · Boeing 727225 · Fuselage Main, Plate/SkinSDR DHL2003748011Light · inoperativeEMERGENCY LIGHT OVER FORWARD ENTRY DOOR INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMBLY IAW BMM CHAPTER 33-50-00, OPS CHECKED GOOD.Nov 22, 2003 · N748DH · Boeing 727225 · Emergency LightingSDR DHL2003742565Floorbeam · bentDURING C-CHECK, AFT CARGO FLOOR SUPPORT BENT STA 955E LBL12. REMOVED DAMAGED FLOOR SUPPORT STA 955E LBL 12 AND MADE NEW FROM BAC1500-6199.7075-T6 (68.5 X .75 X 1.25 X 1.25 X 1.25 X .75 INCH) PO 335824 AS PER SAMPLE IAW B727 SRM 53-10-2 FIG 8, PART TREATED ANDNov 21, 2003 · N742DH · Boeing 727225 · Fuselage Main, Floor BeamSDR DHL200374265Floorbeam · bentDURING C-CHECK, AFT CARGO FLOOR SUPPORT BENT STA 955E LBL 12. REMOVED DAMAGED FLOOR SUPPORT STA 955E LBL 12 AND MADE NEW FROM BAC1500-6199.7075-T6 (68.5 X .75 X 1.25 X 1.25 X 1.25 X .75 INCH) PO 335824 AS PER SAMPLE IAW B727 SRM 53-10-2 FIG 8, PART TREATED ANNov 21, 2003 · N742DH · Boeing 727225 · Fuselage Main, Floor BeamSDR DHL2003742544Stringer · corrodedDURING C-CHECK, DISCREPANCY IS AS FOLLOWS; N/R 59972 STR 27 L BETWEEN STA 620-640 AT POWER CABLE STAND-OFF. REMOVED FASTENERS FOR ACCESS AS REQ'D IAW B727 SRM 51-30-2. CUT OUT DAMAGED AREA AT STA 630 STR 27L, CORROSION OUT OF LIMITS IAW B727 SRM 53-10-1 FIG Nov 21, 2003 · N742DH · Boeing 727225 · Fuselage Main, Longeron/StringerSDR DHL2003742542Intercostal · bentDURING C-CHECK, UPPER LOBE INTERIOR STIFFENER BUCKLED AT STA 360 STR 5 R. REMOVED UPPER LOBE INTERCOSTAL BS 360 STR 5 RT AS REQUIRED FOR FAB NEW IAW B727 SRM 51-30-02, FABRICATED NEW WEB INTERCOSTAL MAT IDENTIFICATION 7075-T6 .032 PO 991238 DIMENSIONS 19 X 5.Nov 21, 2003 · N742DH · Boeing 727225 · Fuselage Miscellaneous StructureSDR DHL200342544Stringer · corrodedDURING C-CHECK, STR 27 L BETWEEN STA 620-640 AT POWER CABLE STAND-OFF. REMOVED FASTENERS FOR ACCESS AS REQ'D IAW B727 SRM 51-30-2. CUT OUT DAMAGED AREA AT STA 630 STR 27 L, CORROSION OUT OF LIMITS IAW B727 SRM 53-10-1 FIG 1AREA OF CUT OUT 3 INCHES AND FABRICNov 21, 2003 · N742DH · Boeing 727225 · Fuselage Main, Longeron/StringerSDR DHL200342542Intercostal · bentDURING C-CHECK, UPPER LOBE INTERIOR STIFFENER BUCKLED AT STA 360 STR 5 R. REMOVED UPPER LOBE INTERCOSTAL BS 360 STR 5 R AS REQUIRED FOR FAB NEW IAW B727 SRM 51-30-02, FABRICATED NEW WEB INTERCOSTAL MAT IDENTIFICATION 7075-T6 .032 PO 991238 DIMENSIONS 19 X 5.5Nov 21, 2003 · N742DH · Boeing 727225 · Fuselage Miscellaneous StructureSDR DHL2003742520Seat Track · corrodedDURING C-CHECK DISCREPANCY AS FOLLOWS, NR 59977 FWD CARGO COMPARTMENT, CABIN SEAT TRACK AND SPLICE PARTS ARE CORRODED BETWEEN STA 680-700 RBL 24. REMOVED SPLICE OF SEAT TRACK BETWEEN STA 680 TO 700 RBL 24 IAW B-727 SRM 51-30-2. REMOVED LITE CORROSION OF SEATNov 21, 2003 · N742DH · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2003742519Floor Support · bentDURING C-CHECK, AFT CARGO STA 1110 BLL O FLOOR SUPPORT BENT AND TWO SHEARED FASTENERS. REMOVED FASTENERS AS REQUIRED FOR ACCESS IAW B-727 SRM 51-30-2. CUT OUT DAMAGE AREA 2.25 X .875 INCH AND FABRICATED REPAIR ANGLE FROM BAC 1517-1360, EXTRUSION 10.5 X .75 Nov 21, 2003 · N742DH · Boeing 727225 · Fuselage Miscellaneous StructureSDR DHL2003742517Seat Track · corrodedDURING C-CHECK, FWD CARGO COMPT CABIN SEAT TRACK AND SPLICE PARTS ARE CORRODED BETWEEN STA 680-700 RBL 45. REMOVED SPLICE OF SEAT TRACK BETWEEN STA 680-700 RBL 45 AND FABRICATED NEW SPLICE FROM MAT 7075-T6 .250 PO 9911344 DIM 6.75 X 2 INCH IAW B-727 SRM 53-1Nov 21, 2003 · N742DH · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2003742512Frame · dentedDURING C-CHECK, UPPER LOBE INTERIOR FRAME HAS DENT STA 500 ABOVE 17 RT. CUT OUT DAMAGED AREA UPPER LOBE INTERIOR FRAME HAS DENT STA 500 ABOVE 17RT AND FABRICATED NEW ANGLE WITH MATERIAL 7075 T6 .071 PO 9912917 DIMENSION 8 X 4 X 1 INCH IAW B727 SRM 53-10-4 FINov 21, 2003 · N742DH · Boeing 727225 · Fuselage Main, FrameSDR DHL2003742511Frame · dentedDURING C-CHECK, UPPER LOBE INTERIOR BS 520 FRAME HAS DENT ABOVE 17 RT. CUT OUT DAMAGED AREA DIM 1.5 X 1 INCH AND FABBED REPAIR ANGLE FROM 7075 T6 .071 PO 9912917 DIM 9 X 5 X 1 INCH IAW B-727 SRM 53-10-2 FIG 3 AND 53-10-4 FIG 1. PART TREATED AND PRIMED IAW BNov 21, 2003 · N742DH · Boeing 727225 · Fuselage Main, FrameSDR DHL2003742570Frame · damagedDURING C-CHECK, NR 1 CARGO DOOR FUSELAGE FRAME LOWER FWD, CORNER AREA WITH DENTS. DAMAGE FOUND TO BE OUT OF LIMITS IAW B727 SRM 51-10-1 FIG 1. CUT OUT DAMAGED UPPER CHORD AND FABBED NEW ONE FROM BAC 1503-100274 PO 3344880 DIM 42 INCHES & SPLICE ANGLE DIM 9 INov 20, 2003 · N742DH · Boeing 727225 · Fuselage Main, StructureSDR DHL2003742571Skin · damagedDURING D-CHECK, LOWER FUSELAGE EXTERIOR BS 277 TO 178 AREAS SKIN DEEP BLEND OUTS STR 25R TO 26R. STRIPPED PAINT IAW B-727 MM 51-20-01 AND FOUND LIGHTNING STRIKES DRILLED 6 EACH AREAS TO .250 AND INSTALLED FASTENERS IAW B-727 SRM 53-30-3 FIG 20. ONE EACH AREANov 20, 2003 · N742DH · Boeing 727225 · Fuselage Main, Plate/SkinSDR DHL200374270Door Frame · dentedDURING C-CHECK, NR 1 CARGO DOOR FUSELAGE FRAME LOWER FWD, CORNER AREA WITH DENTS. DAMAGE FOUND TO BE OUT OF LIMITS IAW B727 SRM 51-10-1 FIG 1. CUT OUT DAMAGED UPPER CHORD AND FABED NEW ONE FROM BAC 1503-100274 PO 3344880 DIM 42 INCHES & SPLICE ANGLE DIM 9 INov 20, 2003 · N742DH · Boeing 727225 · Fuselage Main, StructureSDR DHL2003742543Frame · dentedDURING C-CHECK, NR 1 CARGO DOOR FUSELAGE FRAME LOWER FWD CORNER AREA WITH DENTS. DAMAGED FOUND TO BE OUT OF LIMITS IAW B727 SRM 51-10-1 FIG 1. CUT OUT DAMAGED UPPER CHORD AND FABED NEW ONE FROM BAC1503-100274 PO334880 DIM 42 INCHES & SPLICE ANGLE 9 INCHES IANov 20, 2003 · N742DH · Boeing 727225 · Fuselage Main, FrameSDR DHL2003742537Support Fitting · damagedDURING C-CHECK, LT MLG SUPPORT FITTING RETAINER BOLT LUGS ELONGATED. ACCOMPLISHED REPAIR TO LT MLG SUPPORT FITTING IAW B727 S/B 57-0153 REV 4, LEAK CHECK GOOD.Nov 20, 2003 · N742DH · Boeing 727225 · Fuselage, Landing Gear Attach FittingsSDR DHL200342543Frame · dentedDURING C-CHECK, NR 1 CARGO DOOR FUSELAGE FRAME LOWER FWD CORNER AREA WITH DENTS. DAMAGED FOUND TO BE OUT OF LIMITS IAW B727 SRM 51-10-1 FIG 1. CUT OUT DAMAGED UPPER CHORD AND FABED NEW ONE FROM BAC1503-100274 PO334880 DIM 42 INCHES & SPLICE ANGLE 9 INCHES INov 20, 2003 · N742DH · Boeing 727225 · Fuselage Main, FrameSDR DHL200342537Fitting · damagedDURING C-CHECK , N/R 59858 LEFT MLG SUPPORT FITTING RETAINER BOLT LUGS ELONGATED. ACCOMPLISHED REPAIR TO LEFT MLG SUPPORT FITTING IAW B727 S/B 57-0153 REV 4, LEAK CHECK GOOD.Nov 20, 2003 · N742DH · Boeing 727225 · Wing, Landing Gear Attach FittingsSDR DHL2003742531Skin · wrinkledDURING C-CHECK, FUSELAGE EXTERNAL SKIN BS 400 TO 420 STR 24R TO 23R SKIN WRINKLE. REMOVED PREVIOUS REPAIR AND ADJACENT FASTENERS IAW B-727 SRM 51-30-2. CUT OUT DAMAGED AREA IAW B-727 SRM 53-20-3 FIG 23, SHEET 10, DETAIL IX (19 X 1.5 INCH). FABRICATED NEW DONov 20, 2003 · N742DH · Boeing 727225 · Fuselage Main, Plate/SkinSDR DHL2003742529Skin · lightning strikeDURING C-CHECK, LOWER FUSELAGE EXTERIOR BS 277 TO BS 178 AREAS SKIN DEEP BLEND OUTS BETWEEN STR 25R TO 26R. STRIPPED PAINT AND FOUND LIGHTNING STRIKES. DRILLED 6 EACH AREAS TO .250 AND INSTALLED FASTENERS IAW B-727 SRM 53-30-3 FIG 20. ONE EACH AREA FOUND TONov 20, 2003 · N742DH · Boeing 727225 · Fuselage Main, Plate/SkinSDR DHL2003742527Frame · bentDURING C-CHECK, CABIN CRACK FILLER AND BENT FRAME STA 372 STR 5R. REMOVED FASTENERS FOR ACCESS IAW B-727 SRM 51-30-2. CUT OUT DAMAGED AREA AS REQUIRED FOR REPAIR DIMENSION 3.5 X 3.5 INCH IAW B-727 SRM 57-40-3 FIG 1. FABRICATED ANGLE REPAIR IAW B-727 SRM 53-Nov 20, 2003 · N742DH · Boeing 727225 · Fuselage Main, FrameSDR DHL2003742516Skin · dentedDURING C-CHECK, FUSELAGE EXTERNAL SKIN BS 630 STR 23R WITH A DENT. CUT DAMAGE AREA DIM 1 X 1 .125 X .75 INCH IAW B-727 SRM 53-30-3. FABRICATED DOUBLER REPAIR DIM 11.5625 X 8.5 INCH USING 2024 T3 .080 PO 90013 IAW B-727 SRM 53-30-3 FIG 1. ALODINED AND PRIMENov 20, 2003 · N742DH · Boeing 727225 · Fuselage Main, Plate/SkinSDR DHL2003742510Frame · crackedDURING C-CHECK, CABIN CRACK FRAME STA 380 ATTACH TO TOP OF R1 DOOR FRAME. REMOVED FASTENERS FOR ACCESS AS REQUIRED FOR REPAIR IAW B-727 SRM 51-30-2. CUT OUT DAMAGE AREA DIMENSION 2 INCH X 1 INCH IAW B-727 SRM 53-10-4 FIG 1. FABRICATED REPAIR MAT USED 7075 TNov 20, 2003 · N742DH · Boeing 727225 · Fuselage Main, FrameSDR DHL2003742502Stringer · crackedDURING C-CHECK, N/R 59873 CABIN STR 15 R CRACK STA 724D. REMOVED FASTENERS AS REQUIRED FOR ACCESS STR 15R STA 724D IAW B-727 SRM 51-30-2. CUT OUT DAMAGE END OF STR 15R DIM 7 INCHES AND FABRICATED ONE U-CHANNEL DIMENSIONS 1 INCH X 1 INCH X 1 INCH X 4 INCHES UNov 20, 2003 · N742DH · Boeing 727225 · Fuselage Main, Longeron/StringerSDR DHL2003742501Stringer · crackedDURING C-CHECK, CABIN STRINGER 15 RT CRACKED STA 736D. REMOVED FASTENERS AS REQUIRED FOR ACCESS STRINGER 15R STA 736D IAW B-727 SRM 51-30-2. CUT OUT DAMAGED END OF STRINGER 15R DIM 7 INCHES AND FABRICATED ONE U-CHANNEL DIM 1 INCH X 1 INCH X 1 INCH X 4 INCH Nov 20, 2003 · N742DH · Boeing 727225 · Fuselage Main, Longeron/Stringer
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