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 95ZZZZ183Angle · corrodedDURING D-CHECK, CORROSION ON R/W FRONT SPAR LONGITUDINAL STIFFENER ANGLE JUST BELOW FUEL TANK ACCESS PLATE WS 193.0. REMOVED AND DISCARDED CORRODED ANGLE, FABRICATED AND INSTALLED NEW ANGLE PER SRM 51-10-1 AND 51-30-2. TOTAL CYCLES 29,577.Feb 28, 1995 · N740DH · Boeing 7272Q9 · Wing Miscellaneous StructureSDR 95ZZZZ182Frame · crackedDURING D-CHECK, FRAME UPPER FLANGE HAS DAMAGE AT BS 1090 STRINGER 25L. REMOVED PAINT, STOP DRILLED PER SRM 51-10-1, STRAIGHTENED DENTED FRAME PER SRM 51-40-1, INSTALLED FRAME REPAIR PER SRM 53-10-4. TOTAL CYCLES 29,577.Feb 28, 1995 · N740DH · Boeing 7272Q9 · Fuselage Main, FrameSDR 95ZZZZ181Skin · corrosionDURING D-CHECK, CORROSION IN 'S' DUCT ON SKIN INT AT RIB 27 BLR 3 INCHES. INSTALLED REPAIR 7075-T6 .080 INCH 4 INCHES BY 7 INCHES AS PER SRM 54-10-3. TOTAL CYCLES 29,577.Feb 28, 1995 · N740DH · Boeing 7272Q9 · Nacelle/Pylon, Plate/SkinSDR 95ZZZZ180Skin · corrosionDURING D-CHECK, CORROSION IN 'S' DUCT ON SKIN INT AT RIB 20 BLR 3 INCH. REMOVED CORROSION APPROX 3 INCH BY 3 INCH. INSTALLED DOUBLER REPAIR AS PER SRM 54-10-3, DOUBLER APPROX 6 INCHES BY 10 INCHES 7075-T6. TOTAL CYCLES 29,577.Feb 28, 1995 · N740DH · Boeing 7272Q9 · Nacelle/Pylon, Plate/SkinSDR 95ZZZZ179Floor Beam · corrosionDURING D-CHECK, CORROSION OF FLOOR BEAM UPPER FLANGE FROM RBL 24 TO BLO BS 440. PERFORMED REPAIR AS PER SRM 53-10-8 FROM LBL 24 TO LBL 0 STATION 440. MATERIAL REPAIR BAC1505-100617. TOTAL CYCLES 29,577.Feb 28, 1995 · N740DH · Boeing 7272Q9 · Fuselage Main, Floor BeamSDR 95ZZZZ178Seat Track · corrodedDURING D-CHECK, SEAT TRACK NR 5 HAS MANY SPOTS CORRODED STATION 980 TO 1130. REMOVED CORROSION (.002) PER SRM 51-10-06 AND CUT OUT AND INSTALLED NEW SECTION OF SEAT TRACK FROM STATION 1030 TO 1130 PER SRM 51-10-01. ALODINE AND PRIMED FROM STATION 980 TO 1030Feb 28, 1995 · N740DH · Boeing 7272Q9 · Fuselage, Seat/Cargo Attach FittingsSDR 95ZZZZ177Seat Track · corrodedDURING D-CHECK, SEAT TRACK NR 3 CORRODED AT STATION 960. REPLACED SEAT TRACK TRACK PER SRM 51-10-1 FROM STATION 960 TO 1136. TOTAL CYCLES 29,577.Feb 28, 1995 · N740DH · Boeing 7272Q9 · Fuselage, Seat/Cargo Attach FittingsSDR 95ZZZZ176Seat Track · corrodedDURING D-CHECK, SEAT TRACK NR 3 CORRODED FROM STATION 1000 TO 1030. REPLACED SEAT TRACK PER SRM 51-10-1 PG 4 FROM STATION 960 TO 1136. TOTAL CYCLES 29,577.Feb 28, 1995 · N740DH · Boeing 7272Q9 · Fuselage, Seat/Cargo Attach FittingsSDR 95ZZZZ175Seat Track · corrodedDURING D-CHECK, FABRICATE NEW SEAT TRACKS FROM BLANK STOCK BACB 20-792 AT RBL 45.50 BS 344 TO BS 480 DUE TO PITCH MISMATCH AND CORROSION BEYOND LIMITS. REPLACED TRACK IAW 51-10-1 PAR 4. TOTAL CYCLES 29,577.Feb 28, 1995 · N740DH · Boeing 7272Q9 · Fuselage, Seat/Cargo Attach FittingsSDR 95ZZZZ174Seat Track · corrodedDURING D-CHECK, SEAT TRACK NR 3 HAS MANY SPOTS CORRODED STATION 1090 TO 1136. REPLACED SEAT TRACK PER SRM 51-10-1 PG 4 FROM STATION 960 TO 1136. TOTAL CYCLES 29,577.Feb 28, 1995 · N740DH · Boeing 7272Q9 · Fuselage, Seat/Cargo Attach FittingsSDR 95ZZZZ173Skin · dentDURING D-CHECK, FUSELAGE EXTERIOR, DENT IN FUSELAGE SKIN AT FS 1380 APPROX AT STRINGER 5R AREA. CUT OUT DAMAGED AREA AS PER SRM 53-30-3. INSTALLED REPAIR DOUBLER AS PER SRM 53-30-3 7 INCHES BY 8 INCHES .063 7075-T6. TOTAL CYCLES 29,577.Feb 28, 1995 · N740DH · Boeing 7272Q9 · Fuselage Main, Plate/SkinSDR 95ZZZZ172Skin · corrosionDURING D-CHECK, FWD PASSENGER DOOR, FUSELAGE SKIN ABOVE TOP HINGE CUT OUT HAS GRIND OUT TO RIVET WITH NO EDGE DISTANCE. INSTALLED DOUBLER IAW SRM 53-30-3 FIG 1 DIM, 6 INCHES BY 3 INCHES 2024-T3 .125. TOTAL CYCLES 29,577.Feb 28, 1995 · N740DH · Boeing 7272Q9 · Fuselage Main, Plate/SkinSDR 95ZZZZ171Stringer · crackedDURING D-CHECK, STRINGER 26L BETWEEN STATION 620 TO 560 IN CTR OF STRINGER ABOVE OR OUTBOARD OF RIVETS HAS EVIDENCE OF CRACK AND HAS CORROSION. REPLACED STRINGER 26L FROM STATION 500 TO 680 IAW SRM 53-10-3 FIG 1. TOTAL CYCLES 29,577.Feb 28, 1995 · N740DH · Boeing 7272Q9 · Fuselage Main, Longeron/StringerSDR 95ZZZZ170Floor Support · crackedDRUING D-CHECK, FLOOR SUPPORT 'Z' ANGLE RBL 14 FWD OF STATION 600, AFT SIDE OF REPAIR DOUBLER, INNERSIDE OF TOP FLANGE DOES NOT EXTEND PAST AFT STOP DRILL, CHECK REPAIR COMFORMITY TO SRM. FABRICATED REPAIR IAW SRM 51-40-3. CRACK STOPS AT ORIGINAL STOP HOLE 1Feb 28, 1995 · N740DH · Boeing 7272Q9 · Fuselage Miscellaneous StructureSDR 95ZZZZ169Stringer · crackedDURING D-CHECK, STRINGER 26L JUST ABOVE THROUGH RIVETS HAS EVIDENCE OF CRACK AND HAS CORROSION STATION 620 TO JUST AFT OF STATION 680. REPLACED STRINGER 26L FROM STATION 500 TO 680 IAW SRM 53-10-3. TOTAL CYCLES 29,577.Feb 28, 1995 · N740DH · Boeing 7272Q9 · Fuselage Main, Longeron/StringerSDR 95ZZZZ168Floor Support · corrodedDURING D-CHECK, FLOOR SUPPORT 'Z' ANGLE JUST AFT OF STATION 640 HAS CORROSION RBL 15 TO LBL 15. REMOVED COROSION PER SRM 51-10-6. CUT OUT DAMAGE 2 CHANNELS 15 LBL AND 15 RBL. INSTALLED ANGLE REPAIRS PER SRM 51-40-3 8 INCHES BY 1 INCH BY 1 INCH .050 5 EACH. Feb 28, 1995 · N740DH · Boeing 7272Q9 · Fuselage Miscellaneous StructureSDR 95ZZZZ167Skin · corrosionDURING D-CHECK, FWD CARGO SKIN CORROSION STATION 680 STRINGER 28L-28R. REPLACED SKIN FROM STATION 680 TO 725 BETWEEN STRINGER 26L AND 26R PER SRM 53-30-3 IAW SB 727-53-A203 AND AD 91-09-09. TOTAL CYCLES 29,577.Feb 28, 1995 · N740DH · Boeing 7272Q9 · Fuselage Main, Plate/SkinSDR 95ZZZZ166Skin · corrosionDURING D-CHECK, FWD CARGO COMPARTMENT SKIN CORROISON STATION 685 STRINGER 28R. REPLACED SKIN FROM STATION 681-725 BETWEEN STRINGER 26L AND 26R PER SRM 53-30-3 IAW SB 727-53-A203 AND AD 91-09-09. TOTAL CYCLES 29,577.Feb 28, 1995 · N740DH · Boeing 7272Q9 · Fuselage Main, Plate/SkinSDR 95ZZZZ165Skin · corrodedDURING D-CHECK, FWD CARGO STATION 700 STR 28L-28R, SKIN CORROSION AT DOME NUTS. REPLACED SKIN FROM STATION 681 TO 725 STRINGER 26L AND 26R PER SRM 53-30-3. TOTAL CYCLES 29,577.Feb 28, 1995 · N740DH · Boeing 7272Q9 · Fuselage Main, Plate/SkinSDR 95ZZZZ164Bracket · crackedDURING D-CHECK, E/E COMPARTMENT DOOR SKIN GOUGED AND BULGED AT FWD END AND AFT END. REPLACED DAMAGED BRACKET ASSEMBLY AT FWD END PER SRM 51-10-1 PG 4. CUT OUT DAMAGED AFT END RT SIDE PER SRM 51-10-1. INSTALLED ANGLE REPAIR PER SRM 51-40-3. INSTALLED OUTER Feb 28, 1995 · N740DH · Boeing 7272Q9 · Electrical/Electronic Compartment DoorsSDR 95ZZZW321Skin · corrodedDURING D-CHECK, FUS EXTERIOR BULGE IN FUS SKIN AT FS 350, BETWEEN STR 26R AND STR 27R, O/B OF ACCESS PANEL. CUT OUT DAMAGED SECTION OF SKIN PER SRM 51-10-6. REMOVED CORROSION FROM LOWER SURFACE OF CHORD ANGLE PER SRM 51-10-6. INSTALLED SKIN REPAIR 16 INCHESFeb 28, 1995 · N740DH · Boeing 7272Q9 · Fuselage Main, Plate/SkinSDR 95ZZZW320Skin · corrodedDURING D-CHECK, FUS EXTERIOR SKIN BULGE AT FWD SIDE OF FUS FWD JACK PAD AT FS 348.2 AT STR 21R. CUT OUT DAMAGED SECTION OF SKIN AND REMOVED CORROSION FROM UNDERLYING SURFACES PER SRM 51-10-6. INSTALLED DOUBLER REPAIR 12 INCHES BY 20 INCHES .050 2024-T3 PER SFeb 28, 1995 · N740DH · Boeing 7272Q9 · Fuselage Main, Plate/SkinSDR 95ZZZW319Spar Cap · corrosionDURING D-CHECK, LT WING LOWER LE SPAR CAP HAS CORROSION UPPER SURFACE 10 INCHES AND 30 INCHES O/B OF NR 3 LE SLAT ACTUATOR IN TWO PLACES. REMOVED CORROSION IAW SRM 51-10-6, MATERIAL LOSS .040 AND .050. CORROSION GRIND OUT ON UPPER SURFACE IS WITHIN LIMITS PEFeb 28, 1995 · N740DH · Boeing 7272Q9 · Wing SparSDR 95ZZZW318Spar · corrodedDURING D-CHECK, LT WING LOWER LE SPAR HAS EXFOLIATED CORROSION LOWER SURFACE 15 INCHES O/B OF NR 1 LE SLAT ACTUATOR. REMOVED CORROSION PER SRM 51-10-6 MAX DEPTH REMOVED .070 OUT OF LIMITS. ALODINE AND PRIMED AREA PER SRM 51-10-2 AND INSTALLED REPAIR 7075-T6 Feb 28, 1995 · N740DH · Boeing 7272Q9 · Wing SparSDR 95ZZZW317Spar · corrodedDURING D-CHECK, LT WING LE LOWER SPAR CAP HAS CORROSION UPPER AND LOWER SURFACE 53 INCHES TO 60 INCHES O/B OF I/B END (JUST O/B OF NR 3 LE FLAP ACUTATOR MOUNT AND PREVIOUS GRIND OUT). REMOVED FASTENERS PER SRM 51-30-2, REMOVED CORROSION PER SRM 51-10-6 AT 43 Feb 28, 1995 · N740DH · Boeing 7272Q9 · Wing SparSDR 95ZZZW316Spar Cap · corrosionDURING D-CHECK, LT WING LE LOWER SPAR CAP LOWER SURFACE HAS EXFOLIATED CORROSION AFT OF NR 3 LE SLAT ACTUATOR AT 6 INCHES I/B OF ACTUATOR MOUNT BRACKET. REMOVED DAMAGED SECTION, FABRICATED NEW SPAR CAP, INSTALLED NEW SECTION PER SRM 51-40-4 AND 51-10-1, MATERFeb 28, 1995 · N740DH · Boeing 7272Q9 · Wing SparSDR 95ZZZW315Spar Chord · corrodedDURING D-CHECK, R/W FRONT SPAR LOWER CHORD CORRODED AT WS 383.0. REMOVED CORROSION PER SRM 51-10-6. CORROSION OUT OF LIMITS .093 REMOVAL PER SRM 51-20-1 FIG E. CUT OUT SPAR CHORD FROM WS 386 PER SRM 51-10-1, SPLICED IN NEW SECTION 24 INCHES PER SRM 51-40-4.Feb 28, 1995 · N740DH · Boeing 7272Q9 · Wing SparSDR 95ZZZW314Skin · burnedDURING D-CHECK, EXT FUS AT APPROX BS 950B STR 3L LIGHTENING STRIKE. REPAIRED LIGHTENING STRIKE AREA AS PER SRM 53-30-3. INSTALLATION OF DOUBLER 7 INCHES BY 12.5 INCHES 2024-T3 .090. TOTAL CYCLES 29577.Feb 28, 1995 · N740DH · Boeing 7272Q9 · Fuselage Main, Plate/SkinSDR 95ZZZW313Skin · dentedDURING D-CHECK, UPPER EXT FUS APPROX BS 333 JUST ABOVE AND ON STR 4L, DENT AND SCRATCH APPROX 3 INCHES L. CUT OUT DAMAGE SKIN PER SRM 53-30-3. INSTALLED EXTERNAL REPAIR AS PER SRM 53-30-3 FIG 3, 24 INCHES BY 30 INCHES 2024-T3 .070 IAW SRM 53-30-3 FIG 14. TOFeb 28, 1995 · N740DH · Boeing 7272Q9 · Fuselage Main, Plate/SkinSDR 95ZZZW312Skin · dentedDURING D-CHECK, UPPER EXT FUS APPROX BS 324 BETWEEN STR 3L AND 4L, DENT APPROX 1 INCH BY 2 INCH. CUT OUT OVERLAPPING SKIN PER SRM 53-30-3. INSTALLED DOUBLER REPAIR IAW SRM 53-30-3, 24 INCHES BY 30 INCHES 2024-T3 .070. TOTAL CYCLES 29577.Feb 28, 1995 · N740DH · Boeing 7272Q9 · Fuselage Main, Plate/SkinSDR 95ZZZW311Skin · corrodedDURING D-CHECK, FUS EXTERIOR HOLE CORRODED IN FUS SKIN AT FS STR 30. CUT OUT DAMAGED AREA PER SRM 53-30-3 AND INSTALLED REPAIR .71 7075-T6 6 INCHES BY 8 INCHES. TOTAL CYCLES 29577.Feb 28, 1995 · N740DH · Boeing 7272Q9 · Fuselage Main, Plate/SkinSDR 95ZZZW310Stringer · corrosionDURING D-CHECK, FUS EXTERIOR HAD SKIN BULGE AT FS 1150 AT STR 23R. REMOVED STRINGER AND FASTENER AS PER SRM 53-10-3. REMOVED SURFACE CORROSION ON SKIN IN SECTION AS PER SRM 51-10-6 LESS THAN .003. ALODINE AND PRIMED AS PER SRM 51-10-2. INSTALLED STR 23R BETFeb 28, 1995 · N740DH · Boeing 7272Q9 · Fuselage Main, Longeron/StringerSDR 95ZZZW309Skin · dentedDURING D-CHECK, FUS EXTERIOR HAD MANY SCRATCHES AND GOUGES IN FUS SKIN EXTERIOR SURFACE BETWEEN NEGATIVE PRESSURE RELIEF DOOR AND FS 1183 BETWEEN STR 18L AND STR 26L. REPAIRED GOUGES AT STA 1183 BETWEEN STA 18L AND STR 26L AS PER SRM 53-19-3, 19 INCHES BY 12 Feb 28, 1995 · N740DH · Boeing 7272Q9 · Fuselage Main, Plate/SkinSDR 95ZZZW308Skin · gougedDURING D-CHECK, FUS EXTERIOR HAD DEEP GOUGE IN FUS SKIN AT FS 1090 STR 18L. BURNISHED GOUGE BEYOND LIMITS PER SRM 51-10-1. CUT OUT DAMAGE PER SRM 53-30-3. FABRICATED AND INSTALLED DOUBLER PER SRM 53-30-3 19 INCHES BY 12 INCHES 2024-T3 .063. TOTAL CYCLES 29Feb 28, 1995 · N740DH · Boeing 7272Q9 · Fuselage Main, Plate/SkinSDR 95ZZZW307Skin · gougedDURING D CHECK, FUS SKIN EXTERIOR SURFACE GOUGED AND LIGHTLY CORRODED ALONG LOWER EDGE OF LT FUS BODY FAIRING MATING SURFACE FROM FS 950C TO FS 1010 BETWEEN STR 27L AND STR 20L. REPAIRED GOUGED WITH DOUBLER 17 INCHES BY 11 INCHES 2024-T3 PER SRM 53-30-3. TOTFeb 28, 1995 · N740DH · Boeing 7272Q9 · Fuselage Main, Plate/SkinSDR 95ZZZW306Skin · corrosionDURING D-CHECK, FUS EXTERIOR HAD SEVERAL AREAS OF SURFACE CORROSION AROUND NUTPLATES AT FUS FAIRING SKIN MATING AREAS BETWEEN STR 26L AND STR 26R, BETWEEN FS 700 AND FS 720. REPLACED SKIN FROM STA 681 TO 725 BETWEEN SRM 26L AND 26R PER SRM 53-30-3. TOTAL CYCFeb 28, 1995 · N740DH · Boeing 7272Q9 · Fuselage Main, Plate/SkinSDR 95ZZZW305Skin · corrosionDURING D-CHECK, FOUND CORROSION AND BULGE IN FUS SKIN BETWEEN FS 700 AND FS 720 APPROX BELOW STR 28L. REPLACED SKIN FROM STA 681 TO 725 BETWEEN STR 26L AND 26R PER SRM 53-30-3 IAW SB 727-53-A203 AND AD 91-09-09. TOTAL CYCLES 29577.Feb 28, 1995 · N740DH · Boeing 7272Q9 · Fuselage Main, Plate/SkinSDR 95ZZZW304Frame · corrodedDURING D-CHECK, FRAME HAD SEVERAL AREAS OF CORROSION BS 1148 BETWEEN STR 22L TO STR 27L ON TOP AND BOTTOM OF UPPER FLANGE. REMOVED CORROSION, MATERIAL REMOVED AT FRAME, NUTPLATE HOLE EXCESSIVE, OUT OF LIMITS. INSTALLED FRAME REPAIR AS PER SRM 51-10-6 AND 51-Feb 28, 1995 · N740DH · Boeing 7272Q9 · Fuselage Main, FrameSDR 95ZZZW303Skin · corrodedDURING D-CHECK, AFT CARGO DOOR FWD LOWER CORNER IS CHAPPED, ERODED AND CORRODED. INSTALLED DOUBLER SKIN REPAIR IAW SRM 52-00-3 8 INCHES BY 2 INCHES .063. TOTAL CYCLES 29577.Feb 28, 1995 · N740DH · Boeing 7272Q9 · Cargo/Baggage DoorsSDR 95ZZZW302Skin · dentedDURING D-CHECK, UPPER EXT FUS BS 328 BETWEEN STR 1 AND 3L, DEEP DENT AND SCRATCHES. CUT OUT DAMAGED AREA PER SRM 53-30-3. INSTALLED EXTERNAL REPAIR AS PER SRM 53-30-3 FIG 3 AND FIG 14, 24 INCHES BY 30 INCHES 2024-T3 .070. TOTAL CYCLES 29577.Feb 28, 1995 · N740DH · Boeing 7272Q9 · Fuselage Main, Plate/SkinSDR 95ZZZW301Stringer · corrodedDURING D-CHECK, FUS EXTERIOR - FUS SKIN BULGED AND LOOSE RIVETS AT FS 1050 AT STR 26L AND STR 28L. REMOVED DAMAGED PORTION OF STR 27L THAT WAS CAUSING SKIN BULGE. REINSTALLED STRINGER SPLICE AS PER SRM 53-10-3. STRINGER SPLICE APPROX 10 INCHES. TOTAL CYCLEFeb 28, 1995 · N740DH · Boeing 7272Q9 · Fuselage Main, Longeron/StringerSDR 95ZZZW300Stringer · corrodedDURING D-CHECK, BETWEEN STA 1183 AND 1166 STR 22L WAS CRACKED AND EXPLODED CORROSION. CUT OUT DAMAGED STR IAW SRM 53-10-3. INSTALLED NEW SECTION AND SPLICED STR REPAIR PER SRM 53-10-3 FROM STA 1183 TO 1154. TOTAL CYCLES 29577.Feb 28, 1995 · N740DH · Boeing 7272Q9 · Fuselage Main, Longeron/StringerSDR 95ZZZW299Floorbeam · corrosionDURING D CHECK, FLOORBEAM UPPER FLANGE HAS CORROSION BS 380 BETWEEN RBL 24 AND RBL 45. REMOVED BAD SECTION, ACCOMPLISHED REPAIR AS PER SRM 53-10-8 AND SRM 51-30-2 ON STA 380 BETWEEN RBL 24 AND RBL 45 7075-T3. TOTAL CYCLES 29577.Feb 28, 1995 · N740DH · Boeing 7272Q9 · Fuselage Main, Floor BeamSDR 95ZZZW298Floorbeam · corrodedDURING D CHECK, FOUND FLOORBEAM UPPER FLANGE BS 400 BETWEEN RBL 24 AND RBL 45 HAS CORROSION. ACCOMPLISHED REPAIR IAW SRM 51-10-6 AND SRM 53-10-8. TOTAL CYCLES 29577.Feb 28, 1995 · N740DH · Boeing 7272Q9 · Fuselage Main, Floor BeamSDR 95ZZZW297Floorbeam · corrosionDURING D-CHECK, FOUND CORROSION ON UPPER FLANGES OF FLOORBEAMS BS 400 AND BS 420 BETWEEN RBL 24 AND LBL 24. STA 420 - REMOVED CORROSION AS PER SRM 51-10-6 - MIN THICKNESS REMAINING .114 WITHIN LIMITS PER SRM 53-10-1 FIG 4. STA 400 - REMOVED CORROSION PER SRMFeb 28, 1995 · N740DH · Boeing 7272Q9 · Fuselage Main, Floor BeamSDR 95ZZZW296Frame · corrosionDURING D CHECK, FOUND CORROSION OF FRAME BS 380 FROM BL 0 TO RBL 24 UPPER FLANGE. REMOVED BAD SECTION. REPAIRED AS PER SRM 53-10-8 AND SRM 51-30-2. STA 380 FROM BL 0 TO RBL 24 7075-T73. TOTAL CYCLES 29577.Feb 28, 1995 · N740DH · Boeing 7272Q9 · Fuselage Main, FrameSDR 95ZZZW295Support · corrosionDURING D-CHECK, FLOORBEAM SUPPORT FROM BS 400 TO BS 420 RBL 55 UPPER ANGLE CORRODED AND HOLES DRILLED ON RADIUS. REPLACEMENT OF ANGLE AS PER SRM 51-10-1 PAR 4. TOTAL CYCLES 29577.Feb 28, 1995 · N740DH · Boeing 7272Q9 · Fuselage Miscellaneous StructureSDR 95ZZZW294Floorbeam · corrosionDURING D-CHECK, STA 344 UPPER FLOORBEAM CAP CORRODED FROM LBL 60 TO RBL 60. REMOVED OLD BAD BEAM CP. CLEANED AREA REMOVED SOME MILD CORROSION FROM WEB AS PER SRM 51-10-6. INSTALLED NEW CAP AS PER SRM 51-10-1 PAR 4 , 51-30-2 7075-T3. TOTAL CYCLES 29577.Feb 28, 1995 · N740DH · Boeing 7272Q9 · Fuselage Main, Floor BeamSDR 95ZZZW293Support · corrodedDURING D-CHECK, STA 314 FLOOR SUPPORT IS CORRODED FROM RBL 15 TO RBL 42. INSTALLED NEW SUPPORT ANGLE AS PER SRM 57-10-1 PAR 4 AND SRM 51-30-2 FROM RBL 15 - RBL 42 7075-T73 STA 314. TOTAL CYCLES 29577.Feb 28, 1995 · N740DH · Boeing 7272Q9 · Fuselage Miscellaneous StructureSDR 95ZZZW292Floorbeam · corrosionDURING D-CHECK, FOUND CORROSION ON FLOORBEAM FS 1110 FROM LBL 24 TO LBL 45 UPPER FLANGE. CUT OUT DAMAGED AREA AND INSTALLED REPAIR PER SRM 53-10-8. TREATED AND PRIMED AREA BEFORE INSTALLATION. FLANGE REPAIR 35 INCHES AND 2.5 INCHES - STRAPS 7085-T6. TOTAL Feb 28, 1995 · N740DH · Boeing 7272Q9 · Fuselage Main, Floor Beam
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