Boeing 757-28A

Service difficulty reports · 2,000

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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 = '75728A'
  ORDER BY difficulty_date DESC"

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SDR FDEA201003240976Skin · corrodedAFT PIT SKIN STA 1195, BL0 2EA SMALL CUT-OUT FOR LAVATORY SERVICE HAS CORROSION. KIN REPAIR WAS ACCOMPLISHED ON MAE W/C 118510305WWS AND MAE EA 757-5362-16-F2582, DATED APR 20, 2010. T THIS IS A MAJOR REPAIR.Mar 24, 2010 · N914FD · Boeing 75728A · Fuselage Main, Plate/SkinSDR NOCA02510Support Fitting · corrodedAFT MID LAV, AFT IND LOWER CORNER HAS EVIDENCE OF CORROSION. CLEANED LOWER AFT I/B CORNER OF MID LAV FOUND OUT OF LIMITS IAW B757 AMM 51-00-53. REMOVED LOWER SUPPORT FITTING FROM MID LAV AFT LWR SIDE IAW B757 SRM 51-40-02. REMOVED CORROSION FROM SUPPORT FITMar 12, 2010 · N750NA · Boeing 75728A · Fuselage Miscellaneous StructureSDR FDEA201003100777Crease Beam · corrodedUPPER CABIN, FS 900R TO 1040R INBD CREASE BEAM CORRODED AND HAS NUMEROUS DAMAGED NUT PLATES. REMOVED CORROSION FROM CREASE BEAM FOUND TO BE OUT OF LIMITS, ORIG. MAT .071, MAT. LOSS .018, MAT. REMAINING .053 PER SRM 53-40-13, FIG. 101, DETAIL VII. REMOVED AMar 10, 2010 · N914FD · Boeing 75728A · Fuselage Main, StructureSDR FDEA201003100854Frame · crackedBS 395 FRAME CRACKED AT STR 12R. REPAIR WAS ACCOMPLISHED ON MAE NON ROUTINE NR 43024860001, MAE EA NR757-5312-16-F2588, DATED MARCH 23, 2010. THIS NON - ROUTINE IS FOR TRACKING PURPOSES ONLY. MAJOR ALTERATION.Mar 10, 2010 · N914FD · Boeing 75728A · Fuselage Main, FrameSDR FDEA201003100738Floorbeam · damagedDECK FLOORBEAM TOP FLANGE BS 780 HAS ELONGATED HOLE LBL 24.5. COMPLIED WITH EA F-5310- 131582. REF FORM 8110-3, DATED MAR 25, 2010. MAJOR REPAIR.Mar 10, 2010 · N914FD · Boeing 75728A · Fuselage Main, Floor BeamSDR FDEA201003100737Rib · crackedLT WING T/E RIB AT WS 650 HAS A CRACK. FOUND OUT OF LIMITS IAW SRM 57-51-09 PAGE 105, NOTE D, FIG 101 REPLACED RIB TRACK AT LT WING STA 650 IAW SRM 51-40-02. FABRICATED ON TRAV T10/826717.Mar 10, 2010 · N914FD · Boeing 75728A · Wing, Rib/BulkheadSDR FDEA201003100736Stringer · damagedSTA 839, STRINGER 2R HAS TOOL MARKS. REWORKED/REPAIRED TOOL MARKS AT STA 839, STR 2R, IAW SRM 53-00-03, FIG 201, REPAIR 1, AND EA F-5330-131586. REPAIR IS CLASSIFIED AS A CAT "B" REPAIR WITH SUPPLEMENTAL INSP REQUIRED. INITIAL - 32,940 FC, REPEAT EVERY 3,000 Mar 10, 2010 · N914FD · Boeing 75728A · Fuselage Main, Longeron/StringerSDR FDEA201003100735Door Frame · crackedR2 DOOR FWD FRAME STA 690 STR 11R FRAME CRACKED AFTER REMOVAL OF DOOR MECHANISM FITTING. REPAIRED ON MAE NON-ROUTINE NR 43024520001, AND MAE EA 757-5332-16-F2606, DATED 03/30/10, DUE TO DISCREPANCY EFFECTING THE PTF CONVERSION. THIS NON-ROUTINE IS FOR TRACMar 10, 2010 · N914FD · Boeing 75728A · Fuselage Main, StructureSDR FDEA201003040643Seat Track · misinstalledAT BS 365-418, RBL 45, SEAT TRACK DOES NOT MATCH -107 RCB INSTALLATION. AT BS 365-418, RBL 45.50, SEAT TRACK REINFORCEMENT WAS ACCOMPLISHED, DUE TO DISCREPANCY EFFECTING PTF CONVERSION, ON MAE MOD W/C 118350535RCBR02, AND MAE EA 757-5315-16-F2473, DATED 12/2Mar 4, 2010 · N914FD · Boeing 75728A · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201003040642Seat Track · misinstalledAT BS 365-418, RBL 24, SEAT TRACK DOES NOT MATCH -107 RCB INSTALLATION. AT BS 365-418, RBL 24, SEAT TRACK REINFORCEMENT WAS ACCOMPLISHED, DUE TO DISCREPANCY EFFECTING PTF CONVERSION, ON MAE MOD W/C 118350535RCBR02 AND MAE EA 757-5315-16-F2473, DATED 12/28/09Mar 4, 2010 · N914FD · Boeing 75728A · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201003030624Failsafe · corrodedMAIN CABIN STA 940 FWD SIDE OF AFT FRAME, ANGLE APPROX 2' UP FROM CREASE BEAM WEB CORRODED. CORRODED FAILSAFE CHORD FOUND OUT OF LIMITS IAW SRM 53-00-07, PG 103, FIG 101, DETAIL II. ORIG. MAT .125 AFTER REWORK .111, MAT. LOSS .014 (1/2"X3/4") STA 940, S-16Mar 3, 2010 · N914FD · Boeing 75728A · Fuselage Main, StructureSDR FDEA201003030623Failsafe · corrodedFUSELAGE FRAME BS 980 ABOVE S17R OUTER CHORD HAS CORROSION OUTER CHORD FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07, FIG. 101, DET. II, PG. 101-103, ORIGINAL MAT. THICKNESS IS .090', REM. THICKNESS IS .073", MAT. REM. .017'. REMOVED AND REPLACED FAILSAFE IAWMar 3, 2010 · N914FD · Boeing 75728A · Fuselage Main, StructureSDR FDEA201003030627Support · misrepairedL-2 DOOR SILL SUPPORT ANGLE HAS IMPROPER REPAIR INSTALL IAW SRM APPROX BETWEEN STA 700 TO STA 720. AFTER RESEARCH FOUND REPAIR DOES NOT COMPLY WITH SRM. R & R CREASE BEAM PN 143N8328-53 BTW STA 675 TO 775 AT LBL 64 IAW SRM 51-40-02 AND 51-20- 05. MAJOR REMar 3, 2010 · N914FD · Boeing 75728A · Fuselage Miscellaneous StructureSDR FDEA201003030625Fitting · misalignedACFT DOES NOT MATCH DWG NR 657N3160, SHEET 2, REV. D, FOR PART NR 657N3161-11 FITTING. AT BS 1640, S14L-18L, PLUGGING OF HOLES IN FITTING AT BS 1640/S14L-18L, WAS ACCOMPLISHED, DUE TO DISCREPANCY EFFECTING THE PTF CONVERSION, ON MAE MOD W/C 118350399EZR02, ANMar 3, 2010 · N914FD · Boeing 75728A · Fuselage Main, Attach FittingsSDR FDEA201003030620Frame · damagedSTA 1600 LBL 19.25 STR 3L FRAME HAS A DOUBLE DRILLED HOLE R & R FRAME SECTION STA 1600 STR 5L-5R IAW SRM 51-40-02 AND 53-00-07 PG 203, FIG 201 DET II. FABRICATED NEW FRAME SECTION W/TRAVELER T10/819092, FABBED CHANNELS NR 1 &NR 2 W/ TRAVELER'S T10/819080, T10/Mar 3, 2010 · N914FD · Boeing 75728A · Fuselage Main, FrameSDR FDEA201003020595Frame · crackedUPPER FUSELAGE INTERIOR STA 377.7 AND STRINGER 6R FRAME IS CRACKED AND GOUGED. REMOVED GOUGE, OUT OF LIMITS, CUT AND REMOVED DAMAGED FRAME SECTION IAW SRM 53-00-07, 51-70-11. FABRICATED NEW FRAME ON TRAV NR T10/816878, CHANNEL ON TRAV NR T10/81687, CHANNEL OMar 2, 2010 · N914FD · Boeing 75728A · Fuselage Main, FrameSDR NOCA02210Unknown · malfunctionedON INITIAL TAKEOFF ROLL AT ABOUT 40 KNOTS RT RECIRC FAN ANNUNCIATED FOLLOWED BY RIGHT AND LEFT UTILITY BUSES OFF ON EICAS ABORTED TAKEOFF. ACCOMPLISHED FIM 24-51-00 FIG 103 RIGHT GEN SYS AUX CONTACTOR FAULT ON BPCU RESET. RAN BOTH ENGINES AND CYCLED EACH GENFeb 28, 2010 · N750NA · Boeing 75728A · AC Indicating SystemSDR FDEA201002200478Structure · crackedAPU RT DOOR NR 4 LATCH HOLE IS DEFORMED WITH CRACKS ON EDGE REMOVED CRACK BY BLENDING AREA SMOOTH ON EDGE AND STOP DRILLED EDGE CRACKS IAW SRM 52-40-01, FIG 201 REPAIR V. INSTALLED REPAIR DOUBLER ON DOOR IAW SRM 52-40- 01 FIG 201 REPAIR V. CLASSIFIED AS MAJOFeb 20, 2010 · N914FD · Boeing 75728A · Auxiliary Power Unit (APU) DoorsSDR FDEA201002190475Floorbeam · damagedEXISTING FLOORBEAM REPAIR AT STA 1661 LBL 61-RBL 61 WILL INTERFERE WITH INSTALLATION OF 4EA MOD SEAT TRACKS. REMOVED/INTERFERING FLOORBEAM AT BS 1661, PER SRM 51-40-02, DUE TO INTERFERING WITH PTF MOD SEAT TRACK INSTALLATIONS (4EA.). REPLACED BS 1661 FLOOFeb 19, 2010 · N914FD · Boeing 75728A · Fuselage Main, Floor BeamSDR FDEA201002170440Door · damagedRIGHT APU DOOR SKIN LWR EDGE CHIPPED 2 PLACES FWD CORNER WITHIN LIMITS IAW SRM 52-40-01 FIG 101 PG 103. AFT CORNER DAMAGE OUT OF LIMITS IAW SRM 52-40-01 FIG 101 DET.VI, PG 103, INSTALLED DOUBLER TO RT APU DOOR AFT CORNER IAW SRM 52-40-01 FIG 201, REPAIR CLASSFeb 17, 2010 · N914FD · Boeing 75728A · Auxiliary Power Unit (APU) DoorsSDR FDEA201002150429Skin · damagedAPPROX STA 438 STR 8R, 1 EA EXISTING FASTENER HOLE, IF DRILLED IN THE NEW STRINGER SPLICE WILL LAND IN RADIUS OF SPLICE. AT BS 439F, STR 8R PREVIOUSLY INSTALLED REPAIR CONFLICTED WITH ACCOMPLISHMENT OF PTF CONVERSION, NEW REPAIR WAS ACCOMPLISHED BS 439F, STR.Feb 15, 2010 · N914FD · Boeing 75728A · Fuselage Main, Plate/SkinSDR FDEA201002120406Frame · damagedBS 640, S26L/R, FRAME HAS AN EXISTING ELONGATED HOLE AT BS 640 FRAME, S26L, PREVIOUS ELONGATED HOLE CONFLICTED WITH ACCOMPLISHMENT OF PTF CONVERSION. A NEW FRAME REPAIR WAS ACCOMPLISHED AT BS 640 FRAME, S25L / 26L, DURING PTF CONVERSION ON MAE MOD W/C NR 11Feb 12, 2010 · N914FD · Boeing 75728A · Fuselage Main, FrameSDR NOCA01910Light · inoperativeE-PATH LIGHT BY SEAT ROW 12 INOP. REMOVED AND REPLACED E-PATH FLOOR LIGHT ASSY AT ROW 12 AS PER THE AMM 33-51-11. SYSTEM OPERATIONAL CHECKS OK.Feb 12, 2010 · N754NA · Boeing 75728A · Emergency LightingSDR FDEA201002100380Support Bracket · misinstalledFRAME STA 1340 AT S-2L, EXISTING TV MONITOR SUPPORT BRACKET FASTNER HOLES HAVE SHORT E.D. REMOVED DAMAGED FRAME SECTION IAW SRM 53-00-07 FIG 202 DET 1 AND INSTALLED FRAME. REPAIR IAW SRM 53-00-07 REPAIR 1 ON FSTA 1340 FROM STR. 5L TO STR. 5R, REPAIR PARTS.Feb 10, 2010 · N914FD · Boeing 75728A · Fuselage Miscellaneous StructureSDR FDEA201002050337Floorbeam · damagedMC DECK FLOORBEAM BS. 860 LBL-24.5 HAS ENLOGATED HOLE IN TOP FLANGE. REMOVED FLOORBEAM CHORD, FOUND TO BE OUT OF LIMITS, IAW SRM 53-00-51, IAW SRM 51-40-02. FABRICATED NEW FLOORBEAM CHORD IAW SRM 53-00-51. INSTALLED FLOOR BEAM CHORD REPAIR PARTS ANGLES, STFeb 5, 2010 · N914FD · Boeing 75728A · Fuselage Main, Floor BeamSDR FDEA201002030315Structure · crackedEXISTING 146N8732-22 OTBD CHORD AT STA 1620-1640 S-16, CRACKED IN RADIUS. R & R OTBD CHORD PN 146N8736-22 IAW SRM 51-40-02. MAJOR REPAIR.Feb 3, 2010 · N914FD · Boeing 75728A · Fuselage Main, StructureSDR FDEA201002020300Floorbeam · failedEXISTING FLOORBEAM REPAIR AT STA. 1640 LBL 61- RBL61 WILL INTERFERE WITH THE INSTALLATION OF 4 EA MOD, SEAT TRACKS. REMOVED FLOORBEAM IAW SRM 51-40-02, LOCATED AND DRILLED IAW SRM 51-40- 05,TREATED AND PRIMED AND PAINTED IAW SRM 51-20-01 INSTALLED FLOORBEAMFeb 2, 2010 · N914FD · Boeing 75728A · Fuselage Main, Floor BeamSDR NOCA01310Light · inoperativeLEFT AFT LAV FLOOR EMERGENCY LIGHT OUT. DEFERRED PER MEL 33-51-3. REPLACED EMERGENCY FLOOR LIGHT ASSY, AS PER MM 33-51-11, OPS CHECK GOOD ITEM CLOSED.Jan 31, 2010 · N750NA · Boeing 75728A · Emergency LightingSDR FDEA201001290289Floorbeam · corrodedFLOORBEAM (UNDERSIDE) AT STA 345 LBL 64, HAS CORROSION. REMOVED CORROSION ON FLOORBEAM STA 345, LBL 64. ORIG MAT .125, MAT. LOSS .040, REMAINING MAT .085 OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL VI. REMOVED AND INSTALLED FLOORBEAM REPAIR CHORD ATJan 29, 2010 · N914FD · Boeing 75728A · Fuselage Main, Floor BeamSDR FDEA201001270276Landing Gear · malfunctionedLANDING GEAR FAILED TO COME UP. RAN QRH PROCEDURE USING LOCK OVERIDE AND GEAR CAME UP. UNCOVERD AND SELECTED TO ALTN POSITION. ALL 3 MLG PINS INSTALLED AND SAFETIED. GEAR LEVER LOCK CB ON P11 PANEL FOUND PULLED AND COLLARED. UNCOLLARED LEVER LATCH CB, ERAJan 27, 2010 · N912FD · Boeing 75728A · Landing Gear Retraction/Extension SystemSDR FDEA201001260265Floor Support · corrodedCABIN FLOOR SUPPORT L-1 DOOR LOWER SILL AREA BS 345-365 HAS CORROSION UNDER NUTPLATES. CORROSION OUT OF LIMITS. REMOVED AND FABRICATED NEW FLOOR SUPPORT ON MAE FAB TRAV NR T10/817695, PN BAC1517-2238 HT T6 IAW SRM 51-10-02. INSTALLED NEW FLOOR SUPPORT AT LJan 26, 2010 · N914FD · Boeing 75728A · Fuselage Miscellaneous StructureSDR NOCA01210Mount Fitting · corrodedAFT GALLEY RIGHT AFT TIE DOWN FITTING CORRODED. REPLACED MOUNT FITTING PER SRM 51-10-02.Jan 25, 2010 · N752NA · Boeing 75728A · Fuselage, Equipment Attach FittingsSDR NOCA01110Mount Fitting · corrodedAFT GALLEY LEFT AFT TIE DOWN MOUNT FITTING CORRODED. REPLACED MOUNT FITTING PER SRM 51-10-02.Jan 25, 2010 · N752NA · Boeing 75728A · Fuselage, Equipment Attach FittingsSDR NOCA01010Mount Fitting · corrodedAFT GALLEY CENTER TIE DOWN FITTING CORRODED. REPLACED MOUNT FITTING PER SRM 51-10-02.Jan 25, 2010 · N752NA · Boeing 75728A · Fuselage, Equipment Attach FittingsSDR FDEA201001230228Crease Beam · corrodedMAIN CABIN, STA 960-980 CREASE BEAM WEB CORRODED AT AFT OTBD CORNER.Jan 23, 2010 · N914FD · Boeing 75728A · Fuselage Main, StructureSDR NOCA00810Sill · corroded4L DOOR SILL CORROSION AT BS 1674 LBL 56. REPLACED GUTTER SUPPORT BRACKET PER SRM 51-10-02.Jan 22, 2010 · N753NA · Boeing 75728A · Fuselage Miscellaneous StructureSDR NOCA00910Support · corrodedTHE 4L DOOR SILL CORROSION AT BS 1667 LBL 56. REPLACED GUTTER SUPPORT PER SRM 51-10-02.Jan 22, 2010 · N752NA · Boeing 75728A · Fuselage Miscellaneous StructureSDR FDEA201001210209Valve · failedON APPROACH, PUT GEAR LEVER DOWN. GOT NO NOSE GEAR INDICATION. HAD GEAR DISAGREE MESSAGE, GEAR AND DOOR LIGHTS. RAN CHECKLIST AND LOWERED GEAR WITH ALT IXT SWITCH. COULD HEAR NOSE GEAR EXTENDING. GOT 3 GREEN INDICATIONS AND DOOR LIGHT. LANDED NORMALLY.Jan 21, 2010 · N912FD · Boeing 75728A · Landing Gear Retraction/Extension SystemSDR NOCA00410Light · inoperativeEMERGENCY LIGHT AT SEAT 1C (FLOOR PATH) 1 LIGHT INOP. REPLACED 1 EA LIGHT ASSEMBLY AMM 33-51-1, OPS OK.Jan 16, 2010 · N754NA · Boeing 75728A · Emergency LightingSDR FDEA201001150155Crease Beam · corrodedUPPER CABIN INBD CREASE BEAM FS 665 RT CORRODED. REMOVED CORROSION ON INBD CREASE BEAM, AND FOUND TO BE OUT OF LIMITS IAW 53-30-13, DETAIL 8, FIG. 101. REMOVED INBD CREASE BEAM IAW SRM 51-40-02. INSTALLED NEW INBD CREASE BEAM, IAW SRM 51-40-02, THIS REPAIR ISJan 15, 2010 · N914FD · Boeing 75728A · Fuselage Main, StructureSDR FDEA201001150154Crease Beam · corrodedCABIN LT FLOOR/ CREASE BEAM SUPPORT ANGLE STA 1240-1280 HAS CORROSION. REMOVED CORROSION AND CHECKED LIMITS. FOUND TO BE OUT OF LIMITS IAW SRM 53-60-13. REMOVED CREASE BEAM AT BS 1180-1295, LBL 60 IAW SRM 51-40-02. FABRICATED NEW CREASE BEAM, BAC1515-553. Jan 15, 2010 · N914FD · Boeing 75728A · Fuselage Main, StructureSDR FDEA201001150153Panel · corrodedFS 755 TO 635 RT TRANSITION PANEL CORRODED WITH AND DRILLER OFF SCREWS.Jan 15, 2010 · N914FD · Boeing 75728A · Fuselage Miscellaneous StructureSDR FDEA201001140149Seat Track · damagedEXSITING SEAT TRACK HAS SCALLOPS PREVIOUSLY REMOVED AT STA 1635-1640, LBL 45 WHICH WILL INTERFERE WITH INSTALLATION OF CARGO HANDLING SYS. R & R SEAT TRACK IAW SRM 51-40-02. FABRICATED NEW SEAT TRACK ON MAE TRAVELER NR T10/819328. CLASSIFIED CATEGORY "A" MJan 14, 2010 · N914FD · Boeing 75728A · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201001140148Seat Track · damagedEXISTING SEAT TRACK HAS SCALLOPS PREVIOISLY REMOVED AT STA 1635-1640 LBL 24 WHICH WILL INTERFERE WITH INSTALLATION OF CARGO HANDLING SYS. R & R SEAT TRACK AT LBL 24, STA 1540 TO 1640 IAW SRM 51-40-02 AND 51-40-05. SEAT TRACK FABRICATED ON MAE FAB TRAV, T10/8Jan 14, 2010 · N914FD · Boeing 75728A · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201001140147Seat Track · damagedEXISTING SEAT TRACK HAS SCALLOPS PREVIOUSLY REMOVED AT STA 1635-1640, RBL 24 WHICH WILL INTERFERE WITH INSTALLATION OF CARGO HANDLING SYS. R & R SEAT TRACK BETWEEN STA 1540 TO 1640, RBL 24.75 IAW SRM 51-40- 02. MAJOR REPAIR.Jan 14, 2010 · N914FD · Boeing 75728A · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201001140145Crease Beam · corrodedMAIN CABIN STA 1140 I.B CREASE BEAM CORRODED. REMOVED DAMAGED CREASE BEAM IAW SRM 51-40-02. FABRICATED NEW CREASE BEAM IAW SRM 51-40-02. INSTALLED NEW CREASE BEAM AT RT STA 1040 TO 1180, IAW SRM 51-40-02 AND 51-20-05. MAJOR REPAIR.Jan 14, 2010 · N914FD · Boeing 75728A · Fuselage Main, StructureSDR FDEA201001140135Support · corrodedNR 2 CARGO DOOR LWR SILL SUPPORT FRAME STA 1380-1440 HAS CORROSION UNDER NUTPLATES. REMOVED CORROSION IAW SRM 53-60-15 CHECKED LIMITS ORIG 0.220 MAT REMAIN 0.190, LOSS 0.030 AT LOWEST FOUND OUT OF LIMITS IAW SRM 53-60-15. REMOVED AND REPLACED TEE FITTING IAJan 14, 2010 · N914FD · Boeing 75728A · Fuselage Miscellaneous StructureSDR FDEA201001140132Floor Support · corrodedMCD FLOOR SUPPORT WEB SURFACE IS CORRODED BETWEEN STA 700 TO STA 720 AT LBL 64. R & R GUTTER SUPPORT. CHECKED LIMITS, FOUND OUT OF LIMITS IAW SRM 53-00-51, PG. 103, FIG. 101, DETAIL II. MINOR REPAIR.Jan 14, 2010 · N914FD · Boeing 75728A · Fuselage Miscellaneous StructureSDR FDEA201001140131Crease Beam · corrodedCORROSION FOUND ON LOWER SURFACE OF MCD CREASE BEAM BETWEEN STA 680 TO STA 700 AT LBL 64. ORIG MAT THICKNESS .050 MAT LOSS .008 MAT REMAIN .042, FOUND AREA OUT OF LIMITS IAW SRM 53-00-51, FIG 01, DETAIL VI, PAG 103. R & R CHANNEL PN 143N5410-1, IAW SRM 51-40-Jan 14, 2010 · N914FD · Boeing 75728A · Fuselage Main, StructureSDR FDEA201001140130Floorbeam · corrodedFLOORBEAM 1681.18 UPPER CAP LOWER SURFACE BOTH FWD AND AFT FLANGES HAVE CORROSION ON AND AROUND NUTPLATE ASSY. REMOVED NUT PLATE ASSY IAW SRM 51-40-02. FABRICATED NEW NUT PLATE ASSY IAW SRM 51-40-01. INSTALLED NEW NUT PLATE ASSY STA 1681.8, IAW SRM 51-40-0Jan 14, 2010 · N914FD · Boeing 75728A · Fuselage Main, Floor Beam
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