Boeing 727-2Q9

Service difficulty reports · 830

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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 = '7272Q9'
  ORDER BY difficulty_date DESC"

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SDR 95ZZZW291Skin · crackedDURING D-CHECK, FUS EXTERIOR GOUGE IN FUS SKIN EXTERIOR STR FS 950B AT STR 24L ('B' SYSTEM HYDRAULIC AREA). BURNISHED AREA PER SRM 51-10-1, NO CRACK NOTED, NDT TERMINATION BEYOND LIMITS. INSTALLED DOUBLER REPAIR PER SRM 53-30-3 18 INCHES BY 10 INCHES .071. Feb 28, 1995 · N740DH · Boeing 7272Q9 · Fuselage Main, Plate/SkinSDR 95ZZZW290Skin · corrosionDURING D-CHECK, FUS EXTERIOR - FUS SKIN BULGE AT EXTERNAL DOUBLER AT FS 1085 STR 30. CUT OUT DAMAGED SKIN BULGE PER SRM 53-30-3 AND INSTALLED DOUBLER SKIN REPAIR IAW SRM 53-30-3 9 INCHES BY 18 INCHES .071. TOTAL CYCLES 29577.Feb 28, 1995 · N740DH · Boeing 7272Q9 · Fuselage Main, Plate/SkinSDR 95ZZZW289Support · corrosionDURING D-CHECK, FOUND CORROSION ON 'T' ANGLE FLOOR SUPPORT RBL 41 JUST FWD OF STA 312 FLOORBEAM. REPLACED ANGLE AND INSTALLED PER SRM 51-10-1 PG 4 AND 5, 51-30-2. TOTAL CYCLES 29577.Feb 28, 1995 · N740DH · Boeing 7272Q9 · Fuselage Miscellaneous StructureSDR 95ZZZW288Intercostal · corrosionDURING D-CHECK, FOUND CORROSION ON INTERCOSTAL RBL 12 JUST FWD OF STA 312 FLOORBEAM. REPLACED DAMAGED INTERCOSTAL AS PER SRM 51-10-1 PAR 4. TOTAL CYCLES 29577.Feb 28, 1995 · N740DH · Boeing 7272Q9 · Fuselage Miscellaneous StructureSDR 95ZZZW287Seat Track · corrodedDURING D-CHECK, FOUND NR 2 SEAT TRACK CORRODED FROM STA 480 TO FWD END. REPLACED SEAT TRACK AS PER MODIFICATION STC SA 179750 AND SRM 51-10-1. TOTAL CYCLES 29577.Feb 28, 1995 · N740DH · Boeing 7272Q9 · Fuselage, Seat/Cargo Attach FittingsSDR 95ZZZW286Seat Track · corrodedDURING D-CHECK, FOUND NR 3 SEAT TRACK CORRODED FROM STA 480 TO FWD END. REPLACED SEAT TRACK AS PER MODIFICATION STC - S4179750 AND SRM 51-10-1. TOTAL CYCLES 29577.Feb 28, 1995 · N740DH · Boeing 7272Q9 · Fuselage, Seat/Cargo Attach FittingsSDR 95ZZZW285Seat Track · corrodedDURING D-CHECK, FOUND NR 5 SEAT TRACK CORRODED FROM STA 480 TO FWD END. REPLACED SEAT TRACK AS PER MODIFICATION STC SA 17750 AND SRM 51-10-1. TOTAL CYCLES 29577.Feb 28, 1995 · N740DH · Boeing 7272Q9 · Fuselage, Seat/Cargo Attach FittingsSDR 95ZZZW284Stringer · corrodedDURING D-CHECK, AFT CARGO HAD EVIDENCE OF SURFACE CORROSION ALONG O/B EDGE OF STR 29L BETWEEN FS 950 AND FS 950A. REMOVED CORROSION IAW SRM 51-10-6, BEYOND LIMITS, INSTALLED REPAIR IAW SRM 51-40-4, ALODINE PRIMER PER SRM 51-10-2 2024-T3, .100 10.5 BY 6.25. TFeb 28, 1995 · N740DH · Boeing 7272Q9 · Fuselage Main, Longeron/StringerSDR 95ZZZW283Stringer · corrosionDURING D-CHECK, AFT CARGO HAD EVIDENCE OF CORROSION AROUND FASTENERS AT O/B SIDE OF STR 29L BETWEEN FS 950D AND FS 950E. REMOVED CORROSION PER SRM 51-10-6, BEYOND LIMITS. INSTALLED ANGLE REPAIR PER SRM 51-40-4, 2 INCHES BY 2 INCHES .100, FS 950D IS WITHIN LFeb 28, 1995 · N740DH · Boeing 7272Q9 · Fuselage Main, Longeron/StringerSDR 95ZZZW282Stringer · corrodedDURING D-CHECK, AFT CARGO HAD CORROSION ON O/B SIDE OF STR 29R AROUND FASTENERS BETWEEN FS 950D AND FS 950E. REMOVED CORROSION PER SRM 51-10-6, CORROSION OUT OF LIMIT. FABRICATED EXIT STRAP AND INSTALLED PER SRM 51-40-4 9.5 INCHES BY 4 INCHES .125 2024-T3. Feb 28, 1995 · N740DH · Boeing 7272Q9 · Fuselage Main, Longeron/StringerSDR 95ZZZW281Stringer · corrosionDURING D-CHECK, AFT CARGO HAD CORROSION ALONG O/B ROW OF FASTENERS ON STR 29L BETWEEN FS 950E AND FS 950F. REMOVED CORROSION PER SRM 51-10-6, TREATED ALODINE AND PRIMED PER SRM 51-10-2, BEYOND LIMITS, INSTALLED ANGLE REPAIR PER SRM 51-40-4 12 INCHES BY 1 INCHFeb 28, 1995 · N740DH · Boeing 7272Q9 · Fuselage Main, Longeron/StringerSDR 95ZZZW280Stringer · corrosionDURING D-CHECK, AFT CARGO HAS SEVERAL AREAS OF SURFACE CORROSION AROUND FASTENERS AT O/B SIDE OF STR 29L BETWEEN FS 970 AND FS 990. REMOVED CORROSION PER SRM 51-10-6, BEYOND LIMITS. INSTALLED ANGLE REPAIR PER SRM 51-40-4 12 INCHES BY 1 INCH .100. TOTAL CYCFeb 28, 1995 · N740DH · Boeing 7272Q9 · Fuselage Main, Longeron/StringerSDR 95ZZZW279Stringer · corrosionDURING D-CHECK, AFT CARGO AREA OF SURFACE CORROSION IN STR 29R CHANNEL AND ON STR SPLICE APPROX 6 INCHES AFT OF FS 1010 FRAME. REMOVED FASTENERS AND FABRICATED SPLICE PLATE. REPLACED SPLICE AS PER SRM 51-10-1 PAR 4. INSTALLED FASTENERS PER SRM 51-30-2. TOTFeb 28, 1995 · N740DH · Boeing 7272Q9 · Fuselage Main, Longeron/StringerSDR 95ZZZW419Angle · corrosionDURING D-CHECK, CABIN INTERIOR HAS SURFACE CORROSION ON I/B AND O/B SIDES OF CABIN FLOOR ANGLE AT FS 370, AT APPROX STR 17R. REMOVED ANGLE PER SRM 51-30-2. REMOVED CORROSION AROUND ANGLE AREA PER SRM 51-10-6. MAT LOSS 0.002, FABRICATED ANGLE PER SRM 51-10-1Feb 20, 1995 · N741DH · Boeing 7272Q9 · Fuselage Miscellaneous StructureSDR 95ZZZW418Angle · corrosionDURING D-CHECK, HEAVY CORROSION RIGHT O/B END OF BS 1176.9 CHORD. REMOVED CHORD ANGLE PER SRM 51-30-2. REMOVED CORROSION PER SRM 51-10-6 MAT LOSS .002 INCH. REPLACED CHORD ANGLE PER SRM 51-10-1 PAR 4 AND INSTALLED PER SRM 51-30-2. TOTAL CYCLES 29235.Feb 20, 1995 · N741DH · Boeing 7272Q9 · Fuselage Miscellaneous StructureSDR 95ZZZW416Skin · dentedDURING D-CHECK, E AND E DOOR EXTERIOR SKIN DENTED AT AFT CENTER EDGE. STRAIGHTEN SKIN PER SRM 51-40-1. DYE CHECK PER SRM 20-20-2. STOP DRILLED CRACK PER SRM 51-10-1. INSTALLED DOUBLER REPAIR AS PER SRM 52-00-3. TOTAL CYCLES 29235.Feb 20, 1995 · N741DH · Boeing 7272Q9 · Electrical/Electronic Compartment DoorsSDR 95ZZZW415Frame · crackedDURING D-CHECK, UPPER LOBE STA 720F STR 15F, CRACKED AT FRAME. STOP DRILLED PER SRM 51-10-1. INSTALLED ANGLE REPAIR AS PER SRM 51-40-3 7075-T6 .071 1 INCH BY 1 INCH BY 10 INCH. TOTAL CYCLES 29235.Feb 20, 1995 · N741DH · Boeing 7272Q9 · Fuselage Main, FrameSDR 95ZZZW414Frame · crackedDURING D-CHECK, UPPER LOBE STA 804 STR 14R, CRACK IN FRAME, STOP DRILLED PER SRM 51-10-1. INSTALLED ANGLE REPAIR AS PER SRM 51-40-3 SIZE 1 INCH BY 1 INCH BY 9 INCH MAT 7075-T6 .071. TOTAL CYCLES 29235.Feb 20, 1995 · N741DH · Boeing 7272Q9 · Fuselage Main, FrameSDR 95ZZZW413Skin · crackedDURING D-CHECK, CRACK ON FUS SKIN STA 690 AND 700 BETWEEN STR 27L TO 28L. REPLACED SECTION OF SKIN 35 INCH BY 50 INCH 2024-T3 .071 AS PER SRM 53-30-3 FIG 12, SPLICE 7 INCH BY 50.5 INCH 2024-T3 .080. TOTAL CYCLES 29235.Feb 20, 1995 · N741DH · Boeing 7272Q9 · Fuselage Main, Plate/SkinSDR 95ZZZW412Skin · corrosionDURING D-CHECK, CORROSION STA 700 BETWEEN STA 700 TO 720 STR 26L TO 26R ON PNL ATTACH ANCHOR NUTS. REPLACED SECTION OF SKIN AS PER SRM 53-30-3 FIG 12. TOTAL CYCLES 29235.Feb 20, 1995 · N741DH · Boeing 7272Q9 · Fuselage Main, Plate/SkinSDR 95ZZZW411Floorbeam · corrosionDURING D-CHECK, HEAVY CORROSION CABIN FLOORBEAM BS 344. REMOVED OLD BAD UPPER CAP. CLEANED AREA WITH ALODINE AND PRIMED BARE PLACES AS PER SRM 51-10-6. INSTALLED NEW CAP AS PER SRM 51-10-1 PAR 4 AND SRM 51-30-2. TOTAL CYCLES 29235.Feb 20, 1995 · N741DH · Boeing 7272Q9 · Fuselage Main, Floor BeamSDR 95ZZZW410Support · corrosionDURING D-CHECK, CORROSION ON CABIN FLOOR SUPPORT LBL 12 BS 1020 TO BS 1070. REPLACED FLOOR SUPPORTS LBL 12 FROM 1030 TO 1050 AND FROM 1050 TO 1070 PER SRM 51-10-1 PAR 4. TOTAL CYCLES 29235.Feb 20, 1995 · N741DH · Boeing 7272Q9 · Fuselage Miscellaneous StructureSDR 95ZZZW409Track · corrosionDURING D-CHECK, CORROSION ON CABIN SEAT TRACK 24L STA 1020 TO STA 1130. REMOVED AND REPLACED TRACK SECTION PER SRM 51-10-4 PAR 4 FROM STA 1030 TO STA 1130. REMOVED CORROSION AND TREATED FROM STA 1020 TO 1030 PER SRM 51-10-6. MAT REMOVED .003. TOTAL CYCLES Feb 20, 1995 · N741DH · Boeing 7272Q9 · Fuselage, Seat/Cargo Attach FittingsSDR 95ZZZW408Seat Track · corrosionDURING D-CHECK, CORROSION ON CABIN SEAT TRACK 48L STA 1020 TO STA 1130. INSTALLED SEAT TRACK AS PER SRM 53-1-5 STA 1030 TO STA 1130. TOTAL CYCLES 29235.Feb 20, 1995 · N741DH · Boeing 7272Q9 · Fuselage, Seat/Cargo Attach FittingsSDR 95ZZZW407Skin · corrosionDURING D-CHECK, BARE METAL AND FRAT CORROSION LEFT AFT FUS FAIRING CONTACT AREA ON FUSELAGE. BURNISHED WORN AREA PER SRM 51-10-1, INSTALLED INTERNAL REPAIR PER SRM 53-30-3 FIG 4. ALSO, INSTALLED AN EXTERNAL REPAIR 2 INCHES BY 1 INCH AS PER SRM 53-30-3 FIG 5 Feb 20, 1995 · N741DH · Boeing 7272Q9 · Fuselage Main, Plate/SkinSDR 95ZZZW406Skin · wornDURING D-CHECK, FUS SKIN EXT SURFACE WORN DOWN BY CHAFING, STA 720 AT STR 19L. REPAIRED AS PER SRM 53-30-3 DETAIL IV. INSTALLED DOUBLER .090 2024-T3 14 INCHES BY 10 INCHES AND FILLER 2024-T3 14 INCHES BY 5 INCHES .071. TOTAL CYCLES 29235.Feb 20, 1995 · N741DH · Boeing 7272Q9 · Fuselage Main, Plate/SkinSDR 95ZZZW405Skin · dentedDURING D-CHECK, ON THE NR 2 ENG TORQUE BOX LT SIDE, SKIN HAS FILLER COVERING DAMAGE JUST AFT OF STA 1343 ABOVE RAIN GUTTER. REMOVED FILLER AND PAINT FROM SKIN AFT OF STA 1343, FAB REPAIR PLATE APPROX 12 INCHES BY 14 INCHES .063 2024-T3. TREATED AND PRIMED PEFeb 20, 1995 · N741DH · Boeing 7272Q9 · Fuselage Main, Plate/SkinSDR 95ZZZW404Floorbeam · corrosionDURING D-CHECK, CORROSION AROUND HOLES TOP FLANGE OF FLOORBEAM BS 328 AT LBL 20 AND LBL 46. REMOVED CORROSION PER SRM 51-10-6. CUT 0UT DAMAGED AREAS AND INSTALLED 2 EACH ANGLE REPAIRS 10 INCHES BY 1 INCH BY 1 INCH AT LBL 20 AND LBL 46, MATERIAL USED 7075-T6 Feb 20, 1995 · N741DH · Boeing 7272Q9 · Fuselage Main, Floor BeamSDR 95ZZZW403Floorbeam · corrosionDURING D-CHECK, CORROSION OF FLOORBEAM SUPPORT BETWEEN BS 344 AND BS 360 TOP FLANGE RBL 12. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-10-1 PAR 4 AND INSTALLED PER SRM 51-30-2. TOTAL CYCLES 29235.Feb 20, 1995 · N741DH · Boeing 7272Q9 · Fuselage Main, Floor BeamSDR 95ZZZW402Angle · corrosionDURING D-CHECK, FLOOR BOARD ATTACHMENT ANGLE RBL 64 FROM BS 400 TO BS 420 HAS CORROSION. REMOVED ANGLE PER SRM 51-30-2. REMOVED CORROSION AROUND ANGLE AREA PER SRM 51-10-6. MATERIAL LOSS 0.002 FABRICATED ANGLE PER SRM 51-10-1. MATERIAL 1014-T3 .063 84 INCHFeb 20, 1995 · N741DH · Boeing 7272Q9 · Fuselage Miscellaneous StructureSDR 95ZZZW401Floorbeam · corrosionDURING D-CHECK, CORROSION ON TOP AND BOTTOM SIDES OF FLOORBEAM UPPER FLANGE BS 400 FROM BL 0 TO RBL 64. CUT OUT DAMAGED AREA, FABRICATED PARTS AND INSTALLED REPAIR PER SRM 53-10-8. REPLACED 37 INCHES OF UPPER CHORD SPLICE OF 12 INCHES BY 2 INCHES BY 1 INCH IFeb 20, 1995 · N741DH · Boeing 7272Q9 · Fuselage Main, Floor BeamSDR 95ZZZW400Floorbeam · corrosionDURING D-CHECK, CORROSION ON FLOORBEAM BS 380 UPPER FLANGE TOP AND BOTTOM SIDES FROM BL 0 TO RBL 64. CUT OUT DAMAGED AREA AND INSTALLED REPAIR PER SRM 53-10-8 AT RBL 16 STA 380. ANGLE 1 INCH BY 2 INCH BY 15 INCH 7075-T6 .050 AND ANGLE 1 INCH BY 2 INCH BY 15 Feb 20, 1995 · N741DH · Boeing 7272Q9 · Fuselage Main, Floor BeamSDR 95ZZZW398Support · corrosionDURING D-CHECK, CORROSION ON CABIN FLOOR SUPPORT RBL 12 BS 1070 TO BS 1090. INSTALLED ANGLE REPAIR PER SRM 51-40-4 FIG 3 16 INCHES .050 2024-T3. TOTAL CYCLES 29235.Feb 20, 1995 · N741DH · Boeing 7272Q9 · Fuselage Miscellaneous StructureSDR 95ZZZW397Support · corrosionDURING D-CHECK, CORROSION ON CABIN FLOOR SUPPORT BLR 12 STA 990 TO 1130. REMOVED CORROSION BLR 12 STA 990 TO 1130 PER SRM 51-10-6. MATERIAL REMOVED .003, ALODINE AND PRIMED PER SRM 51-10-2. REPLACED FLOOR SUPPORT FROM STA 1030 TO 1050 AND FROM STA 1050 TOFeb 20, 1995 · N741DH · Boeing 7272Q9 · Fuselage Miscellaneous StructureSDR 95ZZZW396Floorbeam · corrosionDURING D-CHECK, CORROSION ON CABIN FLOORBEAM AT BS 1070 BLL 24 TO BLL 65. REMOVED CORROSION PER SRM 51-10-6. ALODINED AND PRIMED PER SRM 51-10-2. CUT OUT DAMAGED AREA PER SRM 53-10-8. FABRICATED ANGLE 12 INCHES BY 2 INCHES 7075-T6 0.80. TOTAL CYCLES 29235Feb 20, 1995 · N741DH · Boeing 7272Q9 · Fuselage Main, Floor BeamSDR 95ZZZW395Floorbeam · corrosionDURING D-CHECK, CORROSION ON CABIN FLOORBEAM AT BS 1050 BLL 65. REMOVED CORROSION PER SRM 51-10-6. ALODINE AND PRIMED CUT OUT DAMAGED AREA PER SRM 51-40-4. FABRICATED ANGLE REPAIR PER SRM 53-10-8, ANGLE SIZE 15 INCHES BY .8750 INCH BY 2 INCHES 7075-T6 0.50Feb 20, 1995 · N741DH · Boeing 7272Q9 · Fuselage Main, Floor BeamSDR 95ZZZW394Support · corrosionDURING D-CHECK, UPPER LOBE RT STA 304 TO 380 RBL 57 HAS CORROSION FLOOR TO SIDE WALL SUPPORT ANGLE. REMOVED CORROSION IN AREA PER SRM 51-10-6 AND 51-10-2. REPLACED FLOOR SUPPORT ANGLE PER SRM 51-10-1. TOTAL CYCLES 29235.Feb 20, 1995 · N741DH · Boeing 7272Q9 · Fuselage Miscellaneous StructureSDR 95ZZZW393Floorbeam · corrosionDURING D-CHECK, FLOORBEAM STA 310 LBL 3 HAS CORROSION ON TOP UNDERSIDE. REMOVED CORROSION PER SRM 51-10-6. CUT OUT DAMAGED AREA PER SRM 51040-4. INSTALLED ANGLE REPAIR AS PER SRM 51-40-4 9.5 INCHES BY 1 INCH BY 1 INCH. TOTAL CYCLES 29235.Feb 20, 1995 · N741DH · Boeing 7272Q9 · Fuselage Main, Floor BeamSDR 95ZZZW392Support · corrosionDURING D-CHECK, UPPER LOBE R/B STA 320 TO 340 RBL 42, FLOOR SUPPORT HAS CORROSION. REMOVED CORROSION FLOOR SUPPORT PER SRM 51-10-6, BEYOND LIMITS. REPLACED FLOOR SUPPORT STA 320 TO 340 RBL 42 PER SRM 51-10-1 PAR 4. TOTAL CYCLES 29235.Feb 20, 1995 · N741DH · Boeing 7272Q9 · Fuselage Miscellaneous StructureSDR 95ZZZW391Floorbeam · material lossDURING D-CHECK, FLOORBEAM STA 360 RBL 4, TOP FWD HAS A CUT OUT 'CHECK FOR SRM COMFORMANCE'. CUT OUT DAMAGED AREA, FABRICATED PARTS AND INSTALLED REPAIR PER SRM 53-10-8. REPLACED 34.5 INCHES OF UPPER CHORD SPLICE 12.5 INCHES BY 2 INCHES BY 1 INCH O/B END, ANDFeb 20, 1995 · N741DH · Boeing 7272Q9 · Fuselage Main, Floor BeamSDR 95ZZZW390Floorbeam · hole oversizedDURING D-CHECK, UPPER LOBE RT STA 340 AT TOP OF FLOORBEAM RBL 33, BRACKET TOP AFT RIVET HOLE OVERSIZED. REPLACED FLOORBEAM AS PER SRM 51-10-1 PAR 4. UPPER CAP REPLACED ONLY. TOTAL CYCLES 29235.Feb 20, 1995 · N741DH · Boeing 7272Q9 · Fuselage Main, Floor BeamSDR 95ZZZW389Skin · dentedDURING D-CHECK, EXT FUS SKIN AREA WITHIN BS 1030 AND BS 1183 BETWEEN STR 21R AND 17R HAS MULTIPLE DENTS AND SCRATCHES. BURNISHED AREA PER SRM 51-10-1, STRAIGHTENED DENTS PER SRM 51-40-1 AND CHECKED LIMITS OF DENTS PER SRM 53-30-1. ALSO, REPAIRED DENTS AT STR Feb 20, 1995 · N741DH · Boeing 7272Q9 · Fuselage Main, Plate/SkinSDR 95ZZZW388Skin · dentedDURING D-CHECK, SKIN AREA BS 1070 AND BS 1183 BETWEEN STR 17L AND STR 21L DENTED AND SCRATCHED. BURNISHED MINOR SCRATCHES PER SRM 51-10-1, CHECKED DEPTH TO LENGTH RATIO OF DENTS. DENTS WITHIN LIMITS PER SRM 53-30-1. REPAIRED DENT AT STA 1080 JUST ABOVE STR Feb 20, 1995 · N741DH · Boeing 7272Q9 · Fuselage Main, Plate/SkinSDR 95ZZZW387Skin · wornDURING D-CHECK, FUS SKIN AT EDGE OF ACCESS PANELS 3519, 3520, AND 3521, PANELS HAVE WORN INTO THE SKIN. BURNISHED WORN AREAS PER SRM 51-10-1, INSTALLED INTERNAL REPAIR PER SRM 53-30-3 FIG 4. INSTALLED EXTERNAL REPAIR PER SRM 53-30-3 FIG 5, ON AREA FOUND TO BFeb 20, 1995 · N741DH · Boeing 7272Q9 · Fuselage Main, Plate/SkinSDR 95ZZZW386Frame · corrosionDURING D-CHECK, AFT CARGO HAS CORROSION ON AFT SIDE OF FUS FRAME 950E AT FWD LOWER CORNER OF DOOR FRAME AT APPROX STR 27R. REMOVED CORROSION PER SRM 51-10-6, CUT OUT DAMAGED SECTION OF WEB AND INSTALLED NEW SECTION PER SRM 51-40-2, 6 INCH BY 18 INCH 7075-T6 .Feb 20, 1995 · N741DH · Boeing 7272Q9 · Fuselage Main, FrameSDR 95ZZZW385Skin · corrosionDURING D-CHECK, APPROX BS 690 STR 30 FLUSH PATCH REPAIR APPEARS BULGED, CORROSION IND. REPLACED SECTION OF SKIN AS PER SRM 53-30-3 FIG 12. TOTAL CYCLES 29235.Feb 20, 1995 · N741DH · Boeing 7272Q9 · Fuselage Main, Plate/SkinSDR 95ZZZW384Frame · corrosionDURING D-CHECK, AREA EXPOSED BY REMOVAL OF ACCESS PANEL 1104, APPROX BET BS 330 TO 350 FRAME AT APPROX BS 350 HAS EXFOLIATION OF FWD FRAME (APPROX BR 3 INCHES TO BLL 10 INCHES), CORROSION AROUND FASTENERS, CORROSION AT LONG FASTENERS (LT AND RT), CORROSION AT Feb 20, 1995 · N741DH · Boeing 7272Q9 · Fuselage Main, FrameSDR 95ZZZW383Frame · corrosionDURING D-CHECK, THE RT FWD GALLEY SERVICE DOOR FRAME HAS CORROSION ON FUS FRAME AT APPROX FS 375 AT I/B FLANGE, FWD AND AFT SIDES AT STR 17R. INSTALLED ANGLE REPAIR AS PER SRM 51-40-3 MAT 7075-T6 .071 5 INCHES BY 6 INCHES. TOTAL CYCLES 29235.Feb 20, 1995 · N741DH · Boeing 7272Q9 · Fuselage Main, FrameSDR 95ZZZW382Frame · corrosionDURING D-CHECK, RT FORWARD GALLEY SERVICE DOOR FRAME, EXFOLIATED CORROSION ON STRINGER 17R AT AFT LOWER CORNER OF GALLEY DOOR CUTOUT AT FS 415 APPROXIMATELY. REMOVED ANGLE, FOUND OUT OF LIMTI CORROSION, FABRICATED NEW ANGLE 2024-T3.040 AS PER SRM 51-10-1 AND Feb 20, 1995 · N741DH · Boeing 7272Q9 · Fuselage Main, FrameSDR 95ZZZW381Skin · crackedDURING D-CHECK, RT GALLEY SERVICE DOOR FORWARD EXTERNAL DOUBLER REPAIR ON EXTERIOR SKIN AT LOWER HINGE CUTOUT, IS BROKEN AT FWD CORNER. INSTALLED DOUBLER AS PER SRM 51-10-1 4 INCHES BY 4 INCHES PER SRM 51-40-2. TOTAL CYCLES 29,235.Feb 20, 1995 · N741DH · Boeing 7272Q9 · Galley Doors
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