Boeing 757-2G5

Service difficulty reports · 557

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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 = '7572G5'
  ORDER BY difficulty_date DESC"

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SDR FDEA201010304196Transition Panel · corrodedAFT CARGO COMPT LT TRANSITION SIDE PANEL AT STA 1310 - STA 1410 FOUND CORRODED. R & R IAW SRM 51-40-02 REV 101. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.Oct 30, 2010 · N944FD · Boeing 7572G5 · Fuselage Miscellaneous StructureSDR FDEA201010264169Seat Track · chafedSEAT TRACK HAS CHAFED MARK GOUGES AND CORRODED AROUND HOLES BS 440 TO 640 RBL 45.50 REMOVED CORROSION AND GOUGES IAW SRM 51-10-02 . CHECKED LIMITS OF BLENDED AREA STA 450-660 RBL 45 MAT, LOSS .019 ON TOP OF CROWN AND .010 IN BOTTOM OF CROWN WITH IN LIMITS IAWOct 26, 2010 · N943FD · Boeing 7572G5 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201010264172Skin · gougedL4 DOOR INTERNAL SKIN PANEL AT APPROX STA 1660, STR 13-L HAS A GOUGE. REMOVED DAMAGE IAW SRM51-10-02. REMOVED GOUGE BY BLENDING IAW 52-10-01 PG 104 FIG 101, DETAIL V, L=2.0 W=1.0 D=0.008. ORIG MAT 0.063, AFTER REWORK 0.055 -OUT OF LIMITS IAW SRM52-10-01 PGOct 26, 2010 · N943FD · Boeing 7572G5 · Passenger/Crew DoorsSDR FDEA201010214136Seat Track · gougedSTA 418-440, RBL 45, SEAT TRACK GOUGED. REMOVED GOUGE, AFTER REWORK OUT OF LIMITS IAW SRM 53-00-52, FIG 101, DETAIL 7 ORIG MATL, .91, AFTER BLEND OUT, .37, ONLY 20 PERCENT OF MATL ALLOWED. REMOVED SEAT TRACK, BS 418-440, RBL 45, IAW SRM 51-40-02. FABRICATED NOct 21, 2010 · N943FD · Boeing 7572G5 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201010214135Seat Track · gougedSTA. 418-440, RBL 24, SEAT TRACK GOUGED. REMOVED GOUGE, AFTER REWORK OUT OF LIMITS IAW SRM 53-00-52, FIG.101, DETAIL 7, ORIG MATL .91, AFTER BLEND OUT, .30, LOST MORE THAN 20 PERCENT ALLOWED. REMOVED SEAT TRACK BS 418-440, RBL 24, IAW SRM 51-40-02. FABBED NEWOct 21, 2010 · N943FD · Boeing 7572G5 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201010154077Seat Track · gougedMAIN DECK SEAT TRACK STA 440- 680 LBL 45.5 GOUGED & CORRODED. REMOVED GOUGES AND CORROSION PER SRM 51-10-02. BLENDED AREA ; L=13.0",W=1.0",D=.030". OUT OF LIMITS, EXCEEDS THE MAX DEPTH OF .020", GIVEN IN SRM 53-00- 52, FIG.101, DETAIL 1. FABRICATED NEW SEOct 15, 2010 · N943FD · Boeing 7572G5 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201010144070Attach Bracket · crackedCABIN DOOR 4R SILL PLATE ATTACH BRACKET FOUND CRACKED ON REINSTALLATION. CRACKED R4 DOOR SILL PLATE BRACKET REMOVED AND REPLACED IAW SRM 51-40-02 REV.100. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.Oct 14, 2010 · N944FD · Boeing 7572G5 · Fuselage Main, Attach FittingsSDR FDEA201010144073Channel · corrodedWTB FAIRING STRUCTURE CHANNEL AT STA 1180 - STA 1200 RBL 6 FOUND WITH CORROSION. WTB FAIRING CHANNEL AT STA 1180 - STA 1200, RBL 6 REPLACED IAW SRM 51-40-02 REV 100. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100Oct 14, 2010 · N944FD · Boeing 7572G5 · Fuselage Miscellaneous StructureSDR FDEA201010144072Seat Track · corrodedCABIN, SEAT TRACK FROM BS 365.5 TO 640 RBL 45 CORRODED AT STN 365.5 TO 369 APPROX SEAT TRACK AT BS 365.5 TO 640 REPLACED IAW SRM 51-40-02 REV 100. REPAIR IS CLASSIFIED MINOR IAW GMM 6-2-100.Oct 14, 2010 · N944FD · Boeing 7572G5 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201010144071Intercostal · crackedCABIN INTERCOASTAL CRACKED AT STN 1320 TO 1340 LBL 454. R & R SRM 51-40-02 REV 101. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.Oct 14, 2010 · N944FD · Boeing 7572G5 · Fuselage Miscellaneous StructureSDR FDEA201010144069Retainer · corrodedRT MLG CUTOUT SEAL RETAINER UNDER DOOR WARNING LIGHT AFTER REMOVING SEAL FOUND CORROSION. CORRODED SEAL RETAINER AT RT MLG CUTOUT REPLACED IAW SRM 51-40-02, REV 100. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.Oct 14, 2010 · N944FD · Boeing 7572G5 · Wing Miscellaneous StructureSDR FDEA201010144068Retainer · corrodedRT MLG CUTOUT SEAL RETAINER UNDER DOOR WARNING LIGHT AFTER REMOVING SEAL FOUND CORROSION. CORRODED SEAL RETAINER AT RT MLG CUTOUT REPLACED IAW SRM 51-40-02, REV 100. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.Oct 14, 2010 · N944FD · Boeing 7572G5 · Wing Miscellaneous StructureSDR FDEA201010134040Floorbeam · corrodedMAIN CARGO COMPARTMENT FLOOR BEAM UPPER CHORD HAS CORROSION ENTIRE LENGTH BS 1660 CHECKED LIMITS STA 1660 FLOORBEAM AT LBL 55. TO RBL 59 L=6.0 W = 2.0 AND D = .038, FOUND TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-51, FIG.101, DETAIL 3 . REMOVED AND REPOct 13, 2010 · N943FD · Boeing 7572G5 · Fuselage Main, Floor BeamSDR FDEA201010134041Floorbeam · corrodedMAIN CARGO COMPARTMENT FLOORBEAM UPPER CHORD HAS CORROSION ENTIRE LENGTH BS 1660 CHECKED LIMITS STA 1660 FLOORBEAM AT LBL 55 TO RBL 59. L=6.0 W = 2.0 AND D =.038, FOUND TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-51 . R & R STA 1660 FLOORBEAM IAW SRM 51-40-Oct 13, 2010 · N943FD · Boeing 7572G5 · Fuselage Main, Floor BeamSDR FDEA201010134039Seat Track · gougedBS 418-440, LBL 24, SEAT TRACK IS GOUGED. REMOVED GOUGE IAW SRM 51-10-02. AFTER REWORK, FOUND OUT OF LIMITS IAW SRM 53-00- 52, FIG.101, DETAIL 7; L=1.5",W=1.0",D=.019". FABRICATED NEW SEAT TRACK, MATL ID BAC 1520-792, BATCH 1891618. INSTALLED NEW SEAT TRACK Oct 13, 2010 · N943FD · Boeing 7572G5 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201010083976Shear Web · corrodedMAIN CARGO COMPARTMENT SHEAR WEB UPPER SIDE HAS CORROSION AND NUT PLATES CORROED BS 1680 TO BS 1720 BL 0 TO RBL 62. REMOVED CORROSION AT MAIN CARGO COMP . SHEAR WEB UPPER SIDE BS 1680 TO BS 1720 BL 0 TO RBL 62 IAW SRM 51-10-02. BLENED AREA L = 17" W = 1Oct 8, 2010 · N943FD · Boeing 7572G5 · Fuselage Miscellaneous StructureSDR FDEA201010053947Crease Beam · corrodedMAIN DECK LT INBD CREASE BEAM BETWEEN STA.1200-1260 HAS NUT PLATE HOLE CORROSIONS AND SHEARED SCREWS, AS MARKED. REMONED CORROSION IAW SRM 51-10-02 BLENED AREA ORIG MAT .071 L= 4" W=2" D= .020 FOUND OUT OF LIMITS IAW SRM 53-60-13 FIG 101 DET VIII . Oct 5, 2010 · N943FD · Boeing 7572G5 · Fuselage Main, StructureSDR FDEA201010043899Crease Beam · corrodedMAIN CABIN STA 877 LBL 68 CORROSION ON CREASE BEAM REMOVED CORROSION, BLENED AREA L = 2.0" W= 1.5" D=.020 ORGI MAT, .070 REMAINING MAT. .050 OUT OF LIMITS IAW SRM 53-30-13 FIG 101 DET, VIII REPLACED CREASE BEAM STA 760-900 LBL 68 IAW SRM 51-40-02. Oct 4, 2010 · N943FD · Boeing 7572G5 · Fuselage Main, StructureSDR FDEA201010043900Structure · corrodedCORROSION MAIN CABIN STA 1610 WL 200 RBL 68.Oct 4, 2010 · N943FD · Boeing 7572G5 · Fuselage Miscellaneous StructureSDR FDEA201009283774Floorbeam · corrodedMAIN CARGO COMPARTMENT FLOORBEAM UPPER TEE HAS CORROSION BS 377 BLENED AREA IAW SRM 51-10-01. FOUND MUITIABLE AREA OUT OF LIMITS , EXCEEDS MAX OF 10% OF ORIG MAT IAW SRM 53-00-51 FIGURE 101 DETAIL III . REMOVED AND REPLACED UPPER TEE IAW SRM 51-10-01. ISep 28, 2010 · N943FD · Boeing 7572G5 · Fuselage Main, Floor BeamSDR FDEA201009283773Floorbeam · corrodedMAIN CARGO COMPARTMENT FLOORBEAM UPPER TEE HAS CORROSION BS 363.25. BLENDED DAMAGED AREAS IAW SRM 51-10-01. AREAS OUT OF LIMITS IAW SRM 53-00-51, FIG.101, DETAIL 3. R & R UPPER TEE AT RBL 18-60, BS 363.25, IAW SRM 53-00-51, FIG 201, AND SRM 51-40-02. INSTSep 28, 2010 · N943FD · Boeing 7572G5 · Fuselage Main, Floor BeamSDR FDEA201009223645Intercostal · corrodedMAIN CARGO COMPARTMENT INTERCOSTAL HAS CORROSION AROUND HOLES BS 324 TO 340 RBL 25.75. ( ELONGATED HOLES )Sep 22, 2010 · N943FD · Boeing 7572G5 · Fuselage Miscellaneous StructureSDR FDEA201009223639Floor Support · corrodedMAIN CARGO COMPARTMENT FLOOR SUPPORT HAS CORROSION BS 324 TO 325 RBL 43Sep 22, 2010 · N943FD · Boeing 7572G5 · Fuselage Miscellaneous StructureSDR FDEA201009223619Floorbeam · corrodedMAIN CARGO COMPARTMENT FLOORBEAM UPPER CHORD CORRODED AROUND HOLES BS 480. FLOORBEAM WITHIN LIMITS AND CONSIDERED A MINOR REPAIR.Sep 22, 2010 · N943FD · Boeing 7572G5 · Fuselage Main, Floor BeamSDR FDEA201009213603Stringer · corrodedCORROSION FOUND AT STRINGER 3R BETWEEN STA 310.5-324. REMOVED CORROSION IAW SRM 51-10-02. BLENDED AREA L=4",W=1",D=.020". ORIGINAL MATL.050", REMAINING MATL. .030". FOUND OUT OF LIMITS IAW SRM 53-00-03, FIG 101, DETAIL REPAIRED S4R, AT BS 310.5-324, IAW SRM Sep 21, 2010 · N943FD · Boeing 7572G5 · Fuselage Main, Longeron/StringerSDR FDEA201009213599Crease Beam · corrodedMAIN DECK CREASE BEAM, STA 664-776 LBL 60 HAS CORROSION. REMOVED CORROSION ON LT SIDE CREASE BEAM IB CHORD AT STA 664-776 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-30-15, FIG 101, DETAIL IV. ORIG MATERIAL .080 AFTER REWORK .043. R & R CHORD IAW SRM 51-40-02.Sep 21, 2010 · N943FD · Boeing 7572G5 · Fuselage Main, StructureSDR FDEA201009213593Crease Beam · corrodedMAIN CARGO COMPARTMENT CREASE BEAM INBD CHORD CORRODED BS 297 TO BS 324, RBL 62. REMOVED CORROSION AT MAIN CARGO COMPARTMENT CREASE BEAM, BS 297-324, RBL 62, PER SRM 51-10-02. BLENDED AREA; L=18",W=1",D=.049". ORIGINAL MATL .071", MATL. REMAINING; .022". FOSep 21, 2010 · N943FD · Boeing 7572G5 · Fuselage Main, StructureSDR FDEA201009203583Crease Beam · corrodedMAIN CARGO COMPARTMENT CREASE BEAM INBD CHORD HAS CORROSION BS 755 TO BS 900, RBL-62. REMOVED CORROSION ON RT SIDE INBD CREASE BEAM CHORD AND FOUND TO BE OUT OF LIMITS IAW SRM 53-30-13 FIG 101 DETAIL II. REMOVED AND REPLACED CREASE BEAM CHORD IAW SRM 51-40-02Sep 20, 2010 · N943FD · Boeing 7572G5 · Fuselage Main, StructureSDR FDEA201009203571Frame · corrodedMAIN CARGO COMPARTMENT BULKHEAD UPPER CHORD HAS CORROSION BS 324 ENTIRE LENGTH. REMOVED CORROSION UPPER CHORD IAW SRM 51-10-02 . BLENDED AREA L= 44" W=3.0 " D=.039, ORIG MAT .125 REMAINING . 086 OUT OF LIMITS IAW SRM 53-10-08, FIG 101, DET 9. R & R UPPESep 20, 2010 · N943FD · Boeing 7572G5 · Fuselage Main, FrameSDR FDEA201009203560Floorbeam · corrodedMAIN CARGO COMPARTMENT FLOORBEAM UPPER CHORD HAS CHAFED MARK AND CORRODED AROUND HOLES BS 740, RBL 42. REMOVED CORRSION IAW SRM 51-10-02 , CHECKED LIMITS OF BLENDED AREA L=3.01' W= 2.00', D = .015 ORIGINAL MATERIAL .125 , REMAINING. 110, OUT OF LIMITS IAWSep 20, 2010 · N943FD · Boeing 7572G5 · Fuselage Main, Floor BeamSDR FDEA201009203559Floorbeam · corrodedFLOORBEAM UPPER CHORD LOWER SURFACE BS-720 LBL-58 HAS CORROSION. REMOVED CORROSION ON FLOORBEAM UPPER CHORD AT STA 720, LBL 58 IAW SRM 51-10-02. BLEND OUT DIM. =3.5" L2.0" W .019"D, ORIG MATL THICKNESS = .125, FOUND OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DSep 20, 2010 · N943FD · Boeing 7572G5 · Fuselage Main, Floor BeamSDR FDEA201009163517Skin · corrodedNR1 ENG PYLON HAS CORROSION ON INBD INTERNAL SKIN SURFACE AT PP STA 153-168. NR1 ENGINE PYLON RT AFT SKIN PANEL R & R IAW SRM 51-40-02, REV 101. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.Sep 16, 2010 · N944FD · Boeing 7572G5 · Nacelle/Pylon, Plate/SkinSDR FDEA201009163516Panel · corrodedNR1 ENG PYLON STRUT INTERNAL LT SKIN HAS CORROSION INSIDE PANEL CUTOUT AREA 443AL AT PP STAS 106.00-119.00. R & R IAW SRM 51-40-02 REV. 101. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.Sep 16, 2010 · N944FD · Boeing 7572G5 · Nacelle/Pylon, Plate/SkinSDR FDEA201009163515Skin · corrodedNR 2 STRUT HAS CORROSION ON INTERNAL SKIN SURFACE LT BELOW PANEL CUTOUT 443J AT STA 154-171 PP WL 142.50. NR 2 PYLON LT AFT SKIN PANEL R & R IAW SRM 51-40-02, REV 101. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.Sep 16, 2010 · N944FD · Boeing 7572G5 · Nacelle/Pylon, Plate/SkinSDR FDEA201009163514Skin · corrodedNR 1 PYLON INTERNAL SKIN SURFACE OTBD SIDE HAS CORROSION BETWEEN PP STA 146.50-152.50 PP, WL 143.83. NR1 PYLON LT AFT SKIN PANEL R & R IAW SRM 51-40-02 REV.101. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.Sep 16, 2010 · N944FD · Boeing 7572G5 · Nacelle/Pylon, Plate/SkinSDR U2RA227DHN011Support Bracket · brokenAFT CARGO STA 1420 OTBD OF STR 29R, FLOOR SUPPORT CLIP BROKEN.Jul 29, 2010 · N151GX · Boeing 7572G5 · Fuselage Miscellaneous StructureSDR RYNA200903200006Battery Pack · dischargedDURING ROUTINE MAINTENANCE FOUND THE EMERGENCY EXIT LIGHTS AT THE AFT RT BULL NOSE INOPERATIVE. REMOVED AND REPLACED THE POWER PACK ASSEMBLY PER MM 33-51-07, ALL LIGHTS OPERATIONAL CHECK NORMAL.Mar 20, 2009 · Boeing 7572G5 · Emergency LightingSDR RYNA2009032000005Fseu · malfunctionedAFTER TAKEOFF FROM RFD UPON FLAP RETRACTION FROM 15 DEGREES TO 5 DEGREES T/E DISAGREE MESSAGE APPEARED. FOLLOWED CPM PROCEDURES FLAPS OPERATED NORMALLY, RETURNED TO RFD LANDING WEIGHT 76,0000 LBS. PERFORMED FIM 27-51-00/101 FIG 105 FOUND THE NR 1 FSEU FAULTYMar 18, 2009 · N151GX · Boeing 7572G5 · Trailing Edge Flap Control SystemSDR RYNA2009010700001Engine · malfunctionedON TAKE-OFF, AT MAX TAKEOFF POWER THE RT ENGINE COMPRESSOR STALLED. ENG PARAMETERS WERE EGT 886 FOR A TOTAL OF 6 SECONDS. ADDITIONALLY, DEADHEADING CREW REPORTEDLY OBSERVED FLAMES FROM RT ENG DURING COMPRESSOR STALL. INITIATED WO TO BOROSCOPE ENGINE IAW AMMJan 5, 2009 · N929RD · Boeing 7572G5 · Engine (Turbine/Turboprop)SDR RYNA2008121800045Warning System · false activationAFTER TAKEOFF FLIGHT CREW REPORTED A TRAILING EDGE FLAP DISAGREEMENT MESSAGE. AIRCRAFT RETURNED TO RFD MAINTENANCE TROUBLESHOT PERFORMED OPERATIONAL CHECKS PER AMM 27-51-00, NO DEFECTS NOTED. AIRCRAFT DEICED AND DISPATCHED. SYSTEM FAULT HAS NOT REPEATED IN Dec 16, 2008 · N151GX · Boeing 7572G5 · Trailing Flap Position Indicating SystemSDR RYN2008F00015Adi · failedF/O ADI BANKING OUT INTERMITTENTLY. REPLACED F/O ADI. (K0Oct 1, 2008 · N929RD · Boeing 7572G5 · Attitude and Direction Data SystemSDR RYN2008F00014Idg · failedIDG FAILED NO FREQUENCY OR VOLT. REPLACED IDG IAW AMM 24-11-1. CHECKED GOOD. (K)Oct 1, 2008 · N929RD · Boeing 7572G5 · AC Generator-AlternatorSDR RYN2008F00020Sense Line · brokenPILOT REPORT LT ENGINE NOT MAKING POWER AT FL 20000 WITH THE ENGINE POWER LEVER FULLY FWD AND N1 WAS ONLY 71 PERCENT. REPLACED THE LT ENGINE P1 PROBE BROKEN SENSE LINE. COMPLIED WITH HIGH POWER ENGINE RUN, NO DEFECT NOTED. (K)Sep 10, 2008 · N929RD · Boeing 7572G5 · Engine Indicating SystemSDR RYN2008F00013Antenna · failedAIR TURN BACK DUE TO WEATHER RADAR FAILED BEFORE ENTERING ETOPS AIRSPACE. REMOVED WATER FROM THE ANTENNA RESET THE SYSTEM OPS CHECKED NORMAL. (K)Sep 1, 2008 · N929RD · Boeing 7572G5 · Weather Radar SystemSDR RYN2008F00012Radar · failedWEATHER RADAR FAILED, AIRPLANE DIVERTED. TROUBLESHOOTING AND PARTS SOURCING IN WORK. (S)Jul 30, 2008 · N929RD · Boeing 7572G5 · Weather Radar SystemSDR RYN2008F00002Pump · failedAFTER TAKEOFF LT ENGINE DRIVEN HYDRAULIC PUMP LIGHT AND EICAS MESSAGE CAME ON. RETURNED TO AZA AND MADE OVERWEIGHT LANDING. PERFORMED AN OVERWEIGHT LANDING INSPECTION IAW AMM 08-51-38 AND PLACED THE LEFT ENGINE DRIVEN HYDRAULIC PUMP ON DEFERRAL PER MEL 29-31Jun 30, 2008 · N151GX · Boeing 7572G5 · Hydraulic Pump (Electric/Engine), MainSDR RYNA200800014Skin · crackedLOWER FUSELAGE, AFT CARGO DOOR OUTER SKIN IS CRACKED AT LOWER AFT CORNER. REPAIRED CRACK IAW B757-200 SRM 51-30-01.Jan 12, 2008 · N151GX · Boeing 7572G5 · Cargo/Baggage DoorsSDR RYNA200800010Skin · dentedLOWER FUSELAGE SKIN HAS A DENT AT BS 1712 BETWEEN STR 25L AND 26L. REPAIRED IAW EO C00-5-53-011-08.Jan 12, 2008 · N151GX · Boeing 7572G5 · Fuselage Main, Plate/SkinSDR RYNA200800009Skin · dentedUPPER FUSELAGE SKIN HAS A DENT AT BS 1712 BETWEEN STR 14L AND 15L. REPAIRED IAW EO C00-5-53-012-08.Jan 12, 2008 · N151GX · Boeing 7572G5 · Fuselage Main, Plate/SkinSDR RYNA200800008Skin · dentedLOWER FUSELAGE SKIN HAS A DENT AT BS 1696 BETWEEN STR 17L AND 18L. REPAIRED IAW EO C00-5-53-013-08.Jan 12, 2008 · N151GX · Boeing 7572G5 · Fuselage Main, Plate/Skin
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