Boeing 757-2B7

Service difficulty reports · 3,730

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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 = '7572B7'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR FDEA201008203059Rib · chafedLT WING INBD T/E FLAP INBD SUPPORT FITTING HAS WORN/CHAFED SPOT. CHECKED AREA L = 1.5 W = .060 D =.042, ORIGINAL MATERIAL THICKNESS = .090, MATERIAL REMAINING = .048 AND OUT OF LIMITS IAW SRM 57-53-02 FIG. 101 DETAIL VIII. R & R SUPPORT FITTING AND RIB ASSY Aug 20, 2010 · N902FD · Boeing 7572B7 · Wing, Control Surface Attach FittingsSDR FDEA201008173031Floor Panel · corrodedMAIN CABIN AREA AT BS. 1720 LBL 35 FLOOR PANEL WITH CORROSION. REMOVED CORROSION AT BS 1720, LBL 35 FLOOR PANEL, BLENDED OUT DAMAGE L= 4.00 X W=3.00 X D.016, ORIGINAL MATERIAL =.071, MATERIAL REMAINING = .055 IS OUT OF LIMITS IAW SRM 53-00-51 FIG. 101 DETAIAug 17, 2010 · N902FD · Boeing 7572B7 · Fuselage Floor PanelSDR FDEA201008163011Skin · dentedEXTERNAL FUSELAGE SKIN STA 1620- 1640 S-22R TO S-23R HAS 2EA OUTWARD DENTS. EVALUATED (2EA) DENTS, NR1 A/Y=26.47, NR2 A/Y=20.37, BOTH DENTS FOUND OUT OF LIMITS IAW SRM 53-00-01, FIG 101, DET III. REPAIRED SKIN AT STA 1620-1640, BET S22R TO S23R IAW SRM 53-00-Aug 16, 2010 · N902FD · Boeing 7572B7 · Fuselage Main, Plate/SkinSDR USAA2010081891703Skin Panel · debondedCLT - C2 - MAJOR REPAIR - DISBOND ON RIGHT INBOARD MID FLAP TRAILING EDGE COVE PANEL LOWER SKIN 46 INCHES FROM INBOARD END & 10 INCHES FROM AFT EDGE. REPAIRED RIGHT INBOARD MID FLAP TRAILING EDGE COVE PANEL LOWER SKIN IAW EA 102112 & B757 SRM 51-70-07.Aug 14, 2010 · N201UU · Boeing 7572B7 · Trailing Edge FlapsSDR FDEA201008132995Seat Track · gougedCABIN FLOOR SEAT TRACK AT LBL 45.50 AT STA 700-780 SEVERAL NICKS. BLENDED OUT SEVERAL NICKS ON CABIN FLOOR SEAT TRACK AND FOUND TO BE OUT OF LIMIT. REMOVED SEAT TRACK FROM STA 700-780 IAW SRM 51-49-02 REPLACED WITH THE NEW SEAT TRACK WITH BATCH NR 1869949 ANDAug 13, 2010 · N902FD · Boeing 7572B7 · Fuselage, Seat/Cargo Attach FittingsSDR USAA2010081891702Crease Beam · corrodedCLT - C2 - MAJOR REPAIR - CORROSION ON CREASE BEAM BETWEEN BS 1250 TO BS 1270, S17R, RBL 60. REPAIRED CREASE BEAM BETWEEN BS 1250 TO BS 1270, S17R, RBL 60 IAW EA 102116.Aug 11, 2010 · N201UU · Boeing 7572B7 · Fuselage Main, StructureSDR USAA20100812BB048Line · low pressureFLL - THE L1 DOOR EMERGENCY POWER RESERVOIR PRESSURE WAS FOUND BELOW LIMITS. REMOVED AND REPLACED THE EMERGENCY POWER RESERVOIR AT L1 DOOR. FOUND BOURDON TUBE IN PRESSURE GAUGE LEAKING. REPLACED PRESSURE GAUGE AND SERVICED THE UNIT.Aug 11, 2010 · N941UW · Boeing 7572B7 · Passenger/Crew DoorsSDR FDEA201008102912Crease Beam · corrodedMAIN DECK STA 665-755, WL 208, LBL 65 CREASE BEAM INBD CHORD IS CORRODED. REMOVED CORROSION ON INBD CREASE BEAM CHORD STA 665-755 LBL65 IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-30-15, FIG 101, DETAIL IV ORIG MATERIAL .080 AFTER REWORK .055 L=60"Aug 10, 2010 · N902FD · Boeing 7572B7 · Fuselage Main, StructureSDR USAA20100812BB047Fuse · blownPHX - THE EMERGENCY LIGHT AT ROW 15DEF WAS INOPERATIVE. REPLACED THE FUSE IN EPSU BASE 10699.Aug 9, 2010 · N939UW · Boeing 7572B7 · Emergency LightingSDR FDEA201008072872Seat Track · corrodedMAIN CABIN SEAT TRACK STA 900-1040 RBL 25 IS GOUGED AND HAS CORROSION . REMOVED CORROSION ON SEAT TRACK STA 900-1040, RBL 25 IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 101, DETAIL I. DEPTH EXCEEDS MAX REMOVAL .020. L=10" W=1.0 D=.028. Aug 7, 2010 · N902FD · Boeing 7572B7 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201008042811Floor Support · corrodedFLOOR SUPPORT STA 377-418 RBL 25 CORRODED AND GOUGED REMOVED CORROSIN AND GOUGES AT STA 377-418 RBL 24 IAW SRM 51-10-02. REMOVED .010" FROM .071 ORIGINAL MATERIAL, OUT OF LIMITS IAW SRM 53-00-52 FIG 101 DET VIII,REMOVED AND REPLACED SUPPORT AT RBL 24,STA 365Aug 4, 2010 · N902FD · Boeing 7572B7 · Fuselage Miscellaneous StructureSDR USAA20100804BB046Bearing · failedANC FLT 900 EN ROUTE, EICAS MESSAGE EQUIP OVERHEAT DISPLAYED. OVERHEAT LIGHT ILLUMINATED. EICAS MESSAGE EQUIP CLG FAN DISPLAYED. OVERHEAT LIGHT EXTINGUISHED WHEN AUTO WAS SELECTED (QRH). GOT STRONG ELECTRICAL ODOR THROUGHOUT THE AIRCRAFT. ODOR DISSIPATEAug 3, 2010 · N200UU · Boeing 7572B7 · Air Distribution FanSDR FDEA201007312744Floorbeam · damagedREMOVED FLOORBEAM STA 1640 IAW SRM 51-40-02, FABRICATED NEW FLOORBEAM STA 1640, FROM MAT TYPE PN BAC 1518-338/18A, BATCH 1783535 IAW DWG NR 146N5089, SH 3, REV B. INSTALLED FLOORBEAM IAW SRM 51-40-02. MAJOR REPAIR.Jul 31, 2010 · N902FD · Boeing 7572B7 · Fuselage Main, Floor BeamSDR FDEA201007312748Seat Track · corrodedSEAT TRACK, STA 418-440, RBL 24 GOUGED, REMOVED GOUGE AT STA 418-440, RBL 24 IAW SRM 51-10-02. BLENDED AREA DIM L=2.5 W=.8 D=.026. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52 FIG 101 DETAIL VII. ORIG MATERIAL .080 AFTER REWORK .054. R & R SEAT TRACK IAW SRMJul 31, 2010 · N902FD · Boeing 7572B7 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201007312745Crease Beam · corrodedMAIN CABIN STA 1440-1460, RT SIDE CREASE BEAM WEB HAS CORROSION. REMOVED CORROSION AT MAIN CABIN STA 1440-1460 RT SIDE CREASE BEAM IAW SRM 51-10-02. BLENDED AREA L= 1.75",W=1.45",D=.008" ORIGINAL MAT. .040". MAT REMAINING .032" FOUND OUT LIMITS IAW SRM 53-00-Jul 31, 2010 · N902FD · Boeing 7572B7 · Fuselage Main, StructureSDR FDEA201007312743Seat Track · gougedSEAT TRACK STA 418-440, RBL 45 IS GOUGED. BLENDED DAMAGED AREA ORIG MAT .080, AFTER BLEND, L-2.00, W-.900, D-.022, REMAINING MAT .058. FOUND TO BE OUT OF LIMIT IAW SRM 53-00-52, FIG 101, DET VII, FAB NEW SEAT TRACK OF PN 60-6549/24 BATCH NR 1541987 IAW SRMJul 31, 2010 · N902FD · Boeing 7572B7 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201007292726Web · corrodedAFT PIT FLOOR STRUCTURE WEBS (2EA) BS 1500-1520 BL0-RBL 5.5 LOWER SECTION HAS CORROSION. REMOVED CORROSION FROM WEB STA 1500-1520 BL0 TO RBL 5.5 IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53, FIG 101 DETAIL V. ORIGINAL MATERIAL .032 AFTER REWOJul 29, 2010 · N902FD · Boeing 7572B7 · Fuselage Miscellaneous StructureSDR FDEA201007292718Support · corrodedSTA 365-418 RBL-45 SEAT TRACK SUPPORT. REMOVED CORROSION FROM SEAT TRACK SUPPORT IAW SRM 51-10-02. BLENDED AREA IS .011" DEEP, .5" WIDE, 1" LONG. ORIGINAL MATERIAL IS .070" OUT OF LIMITS IAW SRM 53-00-52 FIG 101 DET VIII. INSTALLED NEW SEAT TRACK SUPPORT AJul 29, 2010 · N902FD · Boeing 7572B7 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201007282698Floor Support · corrodedAFT PIT FLOOR SUPPORT WEB BS 1600-1620 RBL 5.5 LOWER SECTION CORRODED. BLENDED OUT CORROSION ON WEB IN AFT CARGO STA 1600- 1620 AND CHECKED LIMITS, MATERIAL THICKNESS- 0.40, L=15", W=0.075, D=.10", AND FOUND OUT OF LIMIT IAW SRM 53-00-04, FIG 101. INSTALLJul 28, 2010 · N902FD · Boeing 7572B7 · Fuselage Miscellaneous StructureSDR FDEA201007282696Shear Tie · corrodedINTERNAL LOWER FUSELAGE SKIN SHEAR TIE BS 1620 BL0 CORRODED. REMOVED CORROSION ON SHEAR TIE, STA 1620, BL0 IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-60-04, FIG 101, DETAIL II. ORIG MATERIAL .050 AFTER REWORK .040 L=1.0 W=1.0. R & R SHEAR TJul 28, 2010 · N902FD · Boeing 7572B7 · Fuselage Internal Mounting StructureSDR FDEA201007272683Crease Beam · corrodedMAIN CABIN STA 1260, RT SIDE IB CREASE BEAM CHORD HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02 BLEND AREA ORIG. MAT. .070 MAT. REMAINING .050 OUT OF LIMITS IAW SRM 53-30-13 FIG. 101 DET. 3, REMOVED AND REPLACED CREASE BEAM FROM STA 1180-1300 IAW SRM 51Jul 27, 2010 · N902FD · Boeing 7572B7 · Fuselage Main, StructureSDR FDEA201007272682Frame · gougedMAIN CABIN, STA 1280, STR 10R TO STR 14R, FRAME HAVE 4 EA GOUGES. BLENDED GOUGES BET 10R & 14R AT STA 1280 FRAME. BLEND OUT DM= L=28",W=1.0", D=.009" ORIGINAL MAT'L THICKNESS .071", FOUND OUT OF LIMITS IAW 53-00-07 FIG. 101 DET, II REPAIR IAW SRM 53-00-07 FIJul 27, 2010 · N902FD · Boeing 7572B7 · Fuselage Main, StructureSDR FDEA201007242658Frame · gougedMAIN CABIN, INTERNAL STRUCTURE FRAME BS 180, STRG 14L, STRG 10L, HAVE GOUGES. REPAIR FRAME BS 1280 LT IAW SRM 53-00-07, FIG 201, REPAIR NR 1.THIS IS A CAT B REPAIR WITH SUPPLEMENTAL INSPECTIONS REQUIRED IAW TABLE 203 OF SRM 53-00-07, FIG 201, REPAIR NR 1. MAJJul 24, 2010 · N902FD · Boeing 7572B7 · Fuselage Main, FrameSDR FDEA201007242657Crease Beam · corrodedMAIN CABIN BETWEEN STA 740-760, RT SIDE CREASE BEAM WEB HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02 BLEANDED AREA AL 2" X 0.5" XD=.008 MAT ORIG .056 REMAINING .048 OUT OF LIMITS IAW SRM 53-00-04 FIG 101 DET IV. REMOVED AND REPLACED CREASE WEB STA ATJul 24, 2010 · N902FD · Boeing 7572B7 · Fuselage Main, StructureSDR USAA20100723BB044Filter · dirtyCLT - FLT 1422 EN ROUTE SXM TO CLT. AN ACRID SMELL WAS NOTED IN THE COCKPIT, IT SMELLED LIKE DUCTS. TURNED OFF THE LEFT BLEED SWITCH AND THE SMELL DISSIPATED. MAINTENANCE WAS UNABLE TO DUPLICATE. RAN BOTH ENGINES, ISOLATED THEM FOR SMELL, NO SMELLS NOTED.Jul 22, 2010 · N937UW · Boeing 7572B7 · Air Distribution SystemSDR FDEA201007202620Crease Beam · corrodedMAIN CABIN CREASE BEAM WEB BS 1380 S17L LOWER SURFACE HAS CORROSION. REMOVED CORROSION AT MAIN CREASE BEAM WEB STA 1380 S17L LOWER SURFACE IAW SRM 51-10-02. BLENDED AREA L=1",W=1.5",D=.023",ORIGINAL MAT. .063" MAT REMAINING .040" FOUND OUT THE LIMITS IAW SRMJul 20, 2010 · N902FD · Boeing 7572B7 · Fuselage Main, StructureSDR FDEA201007202628Crease Beam · corrodedMAIN CABIN, STA 1380-1400, STR 17R, WL 208, CREASE BEAM WEB HAS CORROSION. REMOVED CORROSION ON BETWEEN STA 1380-1400 RT IAW SRM 51-10-02 BLENDED AREA L=1.6",W=1.0" D=.021" ORIG. MATERIAL .063 MAT REMAINING .042 FOUND OUT LIMITS IAW B757 SRM 53-40-13 FIG Jul 20, 2010 · N902FD · Boeing 7572B7 · Fuselage Main, StructureSDR FDEA201007152539Frame · damagedUNABLE TO TRIM THE FRAME AT BS 1645, LBL 63.125 - EXISTING REPAIR DOUBLER WILL INTERFERE WITH PTF MOD. AT BS 1645, LBL 62.125, WL 208, FRAME ALTERATION WAS ACCOMPLISHED DUE TO DISCREPANCY EFFECTING THE PTF CONVERSION ON MAE W/C 118350399EZ2R02, AND MAE EA 75Jul 15, 2010 · N904FD · Boeing 7572B7 · Fuselage Main, FrameSDR FDEA201007152538Frame · damagedPOTENTIAL SHORT EDGE MARGIN FOUND ON FRAME AT BS 480, BETWEEN S26L / 27L. AT BS 480, S26L / 27L, FRAME ALTERATION WAS ACCOMPLISHED DUE TO DISCREPANCY EFFECTING THE PTF CONVERSION, ON MAE W/C 118250068DSSR07 AND MAE EA 757-5332-16-F2619, REV NEW, DATED 04/07/Jul 15, 2010 · N904FD · Boeing 7572B7 · Fuselage Main, FrameSDR FDEA201007152537Stringer Splice · damagedSHORT EDGE MARGIN IN THE 657N3250-18 STRINGER SPLICE AT BS 667, S7L CONDITION COMMON TO THE 657N3250-18 STRINGER SPLICE WAS DETERMINED TO BE ACCEPTABLE TO ENGINEERING IAW MAE EA 757-5331-16-F2599 AND MAE PTF W/C NR 118250277DSSR07, REF EA F-5310-139198 AND FJul 15, 2010 · N904FD · Boeing 7572B7 · Fuselage Main, Longeron/StringerSDR FDEA201007142513Skin · misinstalledMCD-STA 460 BETWEEN S-1 AND S-2L AND S-3L AND S-4L FASTNERS IN (2) AREAS ARE FOUND TO BE MISLOCATED DEVIATION TO SKIN FASTNER PATTERN AT STA 460 FROM S-1 TO S-4L WAS DETERMINED TO BE STRUCTURALLY ACCEPTABLE IAW NON CONFORMITY/REJECTION REPORT MAE/AIDC/118, Jul 14, 2010 · N904FD · Boeing 7572B7 · Fuselage Main, Plate/SkinSDR FDEA201007142512Bracket · misalignedSTA 365, LBL 20-24 CABLE PULLEY BRACKET THAT NEEDS TO SHIMMED DUE TO EXISTING FLOORBEAM REPAIR AT STA 365, LBL 20-24 CABLE PULLEY BRACKET REPAIR WAS ACCOMPLISHED DUE TO DISCREPANCY EFFECTING THE P TO F CONVERSION ON MAE W/C NR 118350472RCBR10 AND MAE EA 757-53Jul 14, 2010 · N904FD · Boeing 7572B7 · Fuselage Miscellaneous StructureSDR FDEA201007142510Filler · misalignedPOTENTIAL BREAK OUT CONDITION ON 143N5407-11 AND 143N5407-16 FILLERS LOCATED AT STA 460, LT SIDE, WL 208.1 AT STA 460 LT SIDE, WL 208.1 POTENTIAL BREAK OUT CONDITION REPAIR WAS ACCOMPLISHED DUE TO DISCREPENCY EFFECTING THE P TO F CONVERSION ON MAE MOD W/C 1183Jul 14, 2010 · N904FD · Boeing 7572B7 · Fuselage Miscellaneous StructureSDR FDEA201007142509Floorbeam · damagedELONGATED HOLES IN FLOORBEAM WEB AT STA 680 LBL 24.75 AT STA 680 LBL 24.75 FLOORBEAM WEB REPAIR WAS ACCOMPLISHED DUE TO DISCREPANCY EFFECTING THE P TO F CONVERSION ON MAE MOD W/C 118350497BZ2R04 AND MAE EA NR 757-5335-16-F2674 REV - DATED MAY 11, 2010. THIS Jul 14, 2010 · N904FD · Boeing 7572B7 · Fuselage Main, Floor BeamSDR FDEA201007132501Floorbeam · corrodedSTA 365, FLOORBEAM CORRODED AND GOUGED FROM BL 0 RBL 55. REMOVED CORROSION AND GOUGES FROM FLOOR BEAM UPPER CHORD STA 365 BL0-RBL55 IAW SRM 51-10-02. BOTH FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51 FIG 101 DETAIL III. ORIG MATERIAL .125 REMOVED 0.017. L=1.0 Jul 13, 2010 · N902FD · Boeing 7572B7 · Fuselage Main, Floor BeamSDR USAA20100716BB042Circuit Board · faultedPHL FLT 740 EN ROUTE SJU TO PHL. DURING APPROACH, RECEIVED "L ENG LP PUMP" MESSAGE. THE LEFT ENGINE UNSPOOLED AND THE LEFT ENGINE OIL PRESSURE WENT TO 16 PSI AND WITHIN 45 SECONDS CAME BACK TO ALL NORMAL INDICATIONS. THE FLIGHT LANDED WITHOUT FURTHER INCIJul 13, 2010 · N939UW · Boeing 7572B7 · AC RegulatorSDR FDEA201007132503Floorbeam · corrodedCABIN FLOORBEAM TEE AT STA 345.0 BETWEEN LBL 24.75 AND LBL 45.5 HAS CORROSION. REMOVED CORROSION FROM T-CAP STA 345, LBL24-45, IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL III. ORIG MATERIAL .125 AFTER REWORK .106. L=20" W=.Jul 13, 2010 · N902FD · Boeing 7572B7 · Fuselage Main, Floor BeamSDR FDEA201007132502Floorbeam · corrodedCABIN FLOOR FRAME T-CAP AT STA 377.7 FROM LBL 50.22 TO BL-0 CORRODED. REMOVED CORROSION STA 377 UPPER CHORD IAW SRM 51-10-02. REMOVED .017 FROM ORIG MATERIAL .125 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL III. L=2.0 W=.1.5. R & R UPPER CHOJul 13, 2010 · N902FD · Boeing 7572B7 · Fuselage Main, Floor BeamSDR FDEA201007132498Fitting · misinstalledPOTENTIAL SHORT EDGE MARGIN CONDITIONS ON 657N4320-4 FITTING AT BS 460, LBL 62.50. AT BS 460, LBL 62.50, POTENTIAL SHORT EDGE MARGIN CONDITION WAS REWORKED REPAIRED ON MAE PTF W/C 118350028BZ2R04 AND MAE EA 757-5335-16-F2611, REV NEW, DATED 04/01/2010 AND FOJul 13, 2010 · N904FD · Boeing 7572B7 · Fuselage Main, Attach FittingsSDR USAA2010071491418Fastener · shearedCLT - C2 - MAJOR REPAIR - FASTENER SHEARED AT RIGHT PYLON OUTBOARD UPPER VERTICAL FLANGE FOR STRUT TO DIAGONAL BRACE FITTING AT PPS209.5. REPLACED DAMAGED FASTENER IAW EA 102029A.Jul 12, 2010 · N938UW · Boeing 7572B7 · Nacelle/Pylon, Attach FittingsSDR USAA2010071391410Slat · debondedPHX - B-CHECK - MAJOR REPAIR - NR 8 LEADING EDGE SLAT INBOARD END/TRAILING EDGE CORNER DISBONDED 22 (APPROX) WEDGE. REPLACED NR 8 LEADING EDGE SLAT IAW JOB CARD 19L52027002.Jul 9, 2010 · N942UW · Boeing 7572B7 · Leading Edge DevicesSDR USAA2010071391409Slat · debondedPHX - B-CHECK - MAJOR REPAIR - NR 5 LEADING EDGE SLAT- OUTBOARD END 18 INCHES INBOARD X 6 INCHES FROM TRAILING EDGE DISBONDED (APPROX) WEDGE. REPLACED NR 5 LEADING EDGE SLAT IAW JOB CARD 19C51227001.Jul 9, 2010 · N942UW · Boeing 7572B7 · Leading Edge DevicesSDR FDEA201007082420Floorbeam · corrodedCABIN FLOORBEAM AT STA 700 IN BETWEEN LBL 45.50 AND 58.22 CORRODED. REMOVED CORROSION IAW SRM 51-10-02 BLENDED AREA ORIG. MAT. .125 MAT LOSS .009", L=.014", W=2.050", D=.009". FOUND TO BE WITHIN LIMIT IAW SRM 53-00-51 FIG 101 DETAIL II. TREATED & PRIMED FLOOJul 8, 2010 · N902FD · Boeing 7572B7 · Fuselage Main, Floor BeamSDR FDEA201007082419Floorbeam · corrodedCABIN FLOORBEAM PANEL HOLES AT STA 740 BETWEEN LBL-24.75 AND LBL-58-22 HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02. BLEND OUT DIM L=8.0 W=2.0 D=.016. ORIG MATERIAL .125 AFTER REWORK .109 FOUND OUT OF LIMITS IAW SRM 53-00-51 FIG 101 DETAIL III. REPAJul 8, 2010 · N902FD · Boeing 7572B7 · Fuselage Main, Floor BeamSDR FDEA201007072392Crease Beam · corrodedMAIN CABIN AREA. LT SIDE BET BS 1260-1280 INBD CREASE BEAM CHORD WITH CORROSION. REMOVED CORROSION IAW SRM 51-10-02, BLENDED AREA L=40'", W=2.0" D=.013 ORIG. MAT. .070, REMAINING .057 OUT OF LIMITS, IAW SRM 53-60-13 FIG 101 DET. III. REMOVED REPLACE CREASE BJul 7, 2010 · N902FD · Boeing 7572B7 · Fuselage Main, StructureSDR USAA2010070991392Skin Panel · delaminatedCLT - C2 - MAJOR REPAIR - DELAMINATION ON APU TAIL CONE INTERIOR SKIN PANEL AT BS1990, BL 0. REPAIRED APU TAIL CONE INTERIOR SKIN PANEL AT BS 1990, BL 0 IAW EA 132039.Jul 3, 2010 · N938UW · Boeing 7572B7 · Aerodynamic FairingsSDR FDEA201007032342Stand Off · corrodedMAIN CABIN, BETWEEN STA. 1580-1600, STR. 17R, WL 208, 1EA STAND-OFF HAS CORROSION. (ATTACHED TO CREASE BEAM)Jul 3, 2010 · N902FD · Boeing 7572B7 · Fuselage Main, Attach FittingsSDR FDEA201007022317Stringer · crackedSTRINGER 9L AT STA 439 IS CRACKED. REMOVED STR 9L AL STA 439 AND STRINGER CLIP AT STA 418 ON S-9L FOR ACCESS IAW: SRM 51-40-02. ROUTED AND RECEIVED FROM FAB SHOP, REPAIR STRINGER TRAV NR T10/843350. LOCATED AND DRILLED REPAIR STRINGER 9L AT STA 439 AND STJul 2, 2010 · N902FD · Boeing 7572B7 · Fuselage Main, Longeron/StringerSDR FDEA201006302277Skin · dentedEXTENAL SKIN DENTED AT R-4 DOOR BELOW SCUFFPLATE AT BS 1661,S18R. EVALUATED DENT AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01, FIG. 101, DETAIL 3, DUE TO PROXIMITY TO SHEAR TIE AT BS 1661, S18R. ACCOMPLISHED DENT REPAIR IAW EA F-5330-139159, DATED 06/03/20Jun 30, 2010 · N904FD · Boeing 7572B7 · Fuselage Main, Plate/SkinSDR USAA20100630BB038Selector · shortedSTT - THE CAPTAIN'S VOR/DME SELECTOR REPORTED BY CREW TO HAVE ELECTRICAL SHORT. PANEL HAD SMOKE AND ODOR FROM FRONT OF UNIT. CREW REPORT: CREW REMOVED MAN/AUTO SWITCH AND PROBLEM STOPPED. MAINTENANCE FOUND A LIGHT BULB AT THE BOTTOM OF THE SWITCH. REPLACEJun 29, 2010 · N937UW · Boeing 7572B7 · Localizer/VOR System
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