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 FDEA200912304559Crease Beam · corrodedUPPER CABIN RT SIDE INBD CREASE BEAM CORRODED FS 590 TO FS 660. R & R RT INBD CREASEBEAM FROM BS 450-664, IAW SRM 51-40-02. CORROSION REMOVAL WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53, FIG. 101, DETAIL 4; ORIGINAL THICKNESS: .070", AFTER REWORK: .045", Dec 30, 2009 · N914FD · Boeing 75728A · Fuselage Main, StructureSDR FDEA200912304558Crease Beam · corrodedUPPER CABIN INBD LT CREASE BEAM FS 1370 TO 1640 HAS NUMEROUS AREAS OF CORROSION. BLENDED AND FOUND TO BE OUT OF LIMITS, IAW SRM 53-60-13, FIG 101, PG 105. REMOVED CREASE BEAM, IAW SRM 51-40-02. FABED NEW CREASE BEAM IAW SRM 51-10-02, 53-60-13. INSTALLED CDec 30, 2009 · N914FD · Boeing 75728A · Fuselage Main, StructureSDR FDEA200912304557Seat Track · corrodedNUMERIOUS GOUGES AND CORROSION FOUND ON SEAT TRACK FROM STA 1080 TO STA 1120 AT LBL 46. REMOVED SEAT TRACK IAW SRM 51-40-02. FABRICATED NEW SEAT TRACK , IAW SRM 53-00-52. INSTALLED SEAT TRACK IAW SRM 51-40-02, 53-00-52. CATEGORY "A", MAJOR REPAIR.Dec 30, 2009 · N914FD · Boeing 75728A · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200912294548Panel · corrodedUPPER SKIN SURFACE OF CTR TANK HAS CORROSION JUST UNDER STA 960 RT INTERCOSTAL. REMOVED CORROSION ON UPPER SURFACE OF CTR WING TANK STA 960, RBL 57, IAW SRM 51-10-02. ORIG MAT .180", MAT LOSS .028", L= .200", W= .100", MAT REMAIN .152", FOUND OUT OF LIMITS Dec 29, 2009 · N914FD · Boeing 75728A · Fuel StorageSDR FDEA200912294547Panel · corrodedUPPER SKIN SURFACE OF CTR TANK HAS CORROSION JUST UNDER STA 980 INTRECOSTAL. REMOVED CORROSION ON UPPER SURFACE OF CTR WING TANK STA 980, RBL 59, IAW SRM 51-10-02. ORIG MAT .180", MAT LOSS- .034", L= .100", W= .050", MAT REMAIN .146". FOUND OUT OF LIMITS IAW Dec 29, 2009 · N914FD · Boeing 75728A · Fuel StorageSDR FDEA200912294546Fuel Tank · corrodedUPPER SKIN SURFACE OF CTR TANK HAS CORROSION JUST UNDER STA 1000 LT INTERCOSTAL.Dec 29, 2009 · N914FD · Boeing 75728A · Fuel StorageSDR FDEA200912294545Panel · corrodedUPPER SKIN OF CTR TANK HAS CORROSION JUST UNDER STA 960 LT INTERCOSTAL. REMOVED CORROSION ON UPPER SKIN SURFACE OF CTR WING TANK STA 960, LBL 59, IAW SRM 51-10-02, ORIG MAT .180", MAT LOSS .028" L=.100", W= 100". MAT REMAIN .152" FOUND OUT OF LIMITS IAW SRMDec 29, 2009 · N914FD · Boeing 75728A · Fuel StorageSDR FDEA200912294544Fuel Tank · corrodedUPPER SKIN SURFACE OF CTR TANK HAS CORROSION JUST UNDER STA 1000 RT INTERCOSTAL.Dec 29, 2009 · N914FD · Boeing 75728A · Fuel StorageSDR FDEA200912294542Seat Track · corrodedNUMEROUS CORROSION FOUND ON MCD SEAT TRACK FASTENER HOLES LWR SURFACE APPROX BETWEEN STA. 480 TO 560 AT LBL 46. SEAT TRACK FOUND TO BE OUT OF LIMITS "AS IS", ORIGINAL MATL .100", "AS IS" .090", .010" MATL. LOSS, BEYOND LIMITS IAW SRM 53-00-52, DETAIL 1, FIGDec 29, 2009 · N914FD · Boeing 75728A · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200912294541Seat Track · corrodedUPPER CABIN SEAT TRACK FS 1320 TO 1540 LBL 45.5 HAS SCRATCHES AND TOOL MARKS WITH CORROSION IN NUMEROUS AREAS. REMOVED CORROSION ON SEAT TRACK AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52. REMOVED SEAT TRACK IAW SRM 51-40-02. REMOVED ANGLE, IAW SRM 51-40-Dec 29, 2009 · N914FD · Boeing 75728A · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200912294539Seat Track · corrodedCABIN SEAT TRACK RBL 24 STA 1320-1340 HAS CORROSION. REMOVED CORROSION ON SEAT TRACK, AFTER REWORK FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52. REMOVED SEAT TRACK. FABRICATED NEW SEAT TRACK ON MAE TRAVELER NR T10/816707. LOCATED AND DRILLED HOLES IAW SRM 51-1Dec 29, 2009 · N914FD · Boeing 75728A · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200912284537Crease Beam · corrodedUPPER CABIN RT SIDE, FS 755 INBD CREASE BEAM CORRODED. REMOVED CREASE BEAM IAW SRM 51-40-02. FABRICATED NEW CREASE BEAM BAC1515-553, IAW SRM 51-40-05. INSTALLED NEW CREASE BEAM AT STA 755- 900, IAW SRM 51-40-02. CATEGORY "A", MAJOR REPAIR.Dec 28, 2009 · N914FD · Boeing 75728A · Fuselage Main, StructureSDR CA091229003Pressure Switch · defective(CAN) IN CRUISE, EICAS MESSAGE ANNUNCIATION "LT ENG HYD PUMP". IN-FLIGHT TURNBACK INITIATED TO YYZ FOR COMPANY CONVENIENCE. THE LEFT ENGINE HYDRAULIC PUMP PRESSURE SWITCH WAS FOUND DEFECTIVE. (TC NR 20091229003)Dec 27, 2009 · Boeing 75728A · Hydraulic Pump (Electric/Engine), MainSDR NOCA07209Eec · malfunctionedNR 2 ENG EEC AND NR 2 ENG LIMITER EICAS MSG ILLUMINATED AFTER ENG START. PERFORMED FIM 73-21-00 FIG 115 AND FIG 103. NO FAULTS NOTED ON RT EEC, RAN ENGS. NO MSGS NOTED.Dec 21, 2009 · N755NA · Boeing 75728A · Fuel Control/Turbine EnginesSDR FDEA200912184485Floorbeam · corrodedCABIN FLOORBEAM STA 365 FROM BL 0- RBL 60 UPPER TEE HAS CORROSION AROUND HOLES. REMOVED CORROSION & FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL 3. FABRICATED UPPER TEE, RECEIVED -2 AND -3 ANGLES. RECEIVED -4 AND -5 STRAPS. LOCATED, DRILLED RDec 18, 2009 · N914FD · Boeing 75728A · Fuselage Main, Floor BeamSDR FDEA200912154472Skin · dentedLT WING, NR 3 SLAT, T/E WEDGE UPPER SURFACE HAS SEVERAL DENTS FROM MID SECTION TO INBD EDGE. SEVERAL DENTS FOUND TO BE OUT OF LIMITS IAW SRM 57-43-01, PAGE 103, PARA. M, DUE TO PROXIMITY TO EACH OTHER. DENTED AREA REPAIRED IAW SRM 51-70-10, BONDED DOUBLER, AT Dec 15, 2009 · N921FD · Boeing 75728A · Leading Edge DevicesSDR FDEA200912154471Frame · gougedFRAME AT STA 1280 RT, STR 14-10 HAS GOUGES. REPLACED FRAME SEGMENT FROM STR 7R TO 14R IAW SRM 51-40-05. FRAME SEGMENT FABRICATED ON MAE TR T/9/812786, CHANNEL 1 FABRICATED ON MAE TR T9/812787, CHANNEL 2 FABRICATED ON MAE TR T9/812788. ORIG MAT'L .071 AFTER Dec 15, 2009 · N912FD · Boeing 75728A · Fuselage Main, FrameSDR FDEA200912144464Skin · corrodedSTRUT NR 2 INBD SKIN SURFACE IS EXFOLIATED JUST FWD LWR OF PANEL 443 JL. R & R STRUT NR 2 INBD SKIN PN 311N5046Y53 IAW DWG 311N5002 SH 14 REV E, AND SRM 51-40-02. CATEGORY "A", MAJOR REPAIR.Dec 14, 2009 · N914FD · Boeing 75728A · Nacelle/Pylon, Plate/SkinSDR CNMA20090155Warning Light · illuminatedRUDDER RATIO LIGHT ILLUMINATED ON GROUND, EICAS MSG - RUDDER RATIO DISPLAYED. PERFORMED FIM 27-09, FOUND LT AND RT CONTROL UNITS DISPLAYED PCA FAULT. RESET IAW FIM, EICAS MESSAGE CLEARED. PERFORMED RESISTANCE CHECK ON CONNECTORS D381 AND D461, CHECKED GOOD.Dec 10, 2009 · N639AX · Boeing 75728A · Central WarningSDR NOCA06909Light · inoperativeEMERGENCY LIGHT INOP AT OVERHEAD BIN 1 ABC. REPLACED LIGHT AS PER MM 33-51-05.Nov 25, 2009 · N750NA · Boeing 75728A · Emergency LightingSDR NOCA06709Light · brokenEMERGENCY FLOOR PATH LIGHT ASSY LOCK BROKEN AT 26C. REPLACED EMERGENCY FLOOR PATH LIGHT ASSY AS PER MM 33-51-11.Nov 25, 2009 · N750NA · Boeing 75728A · Emergency LightingSDR NOCA06609Connector · looseEMERGENCY LIGHT INOP L1 DOOR. RESECURED LOOSE CONNECTOR OPS CHECK OK AS PER MM 33-51-05Nov 25, 2009 · N750NA · Boeing 75728A · Light System WiringSDR NOCA06509AALamp · burned outEMERGENCY LIGHT INOP AT OVERHEAD BIN 1 ABC. REPLACED LIGHT AS PER MM 33-51-05.Nov 25, 2009 · N750NA · Boeing 75728A · Emergency LightingSDR NOCA06509BBEngine · power lossAPPROX 5+00 INTO FLT AT FL350 EXPERIENCED PARTIAL POWER LOSS ON RT ENGINE. ALL PARAMETERS NORMAL EXCEPT LOSS OF POWER (PARTIAL) ON EPR. ADVANCED THROTTLE TO FULL WITH NO FURTHER INCREASE IN EPR (POWER). ENGINE STABLE WITH NO FLUX. CONT FLT WITH PARTIAL POWNov 15, 2009 · N754NA · Boeing 75728A · Engine (Turbine/Turboprop)SDR FDEA200910223647Frame Splice · damagedMAIN CABIN DECK STA 1280, STR 12 & 13, LT HAS A FRAME REPAIR SPLICE DAMAGE. REMOVED REPAIR ANGLES IAW SRM 51-40-02, RECIEVED NEW FROM FAB SHOP 2EA REPAIR ANGLES, MAE TRAV T9/805465, INSTALLED NEW REPAIR PARTS STA 1280, STR 12 & 13, LT IAW SRM 53-00-07, FIGOct 22, 2009 · N913FD · Boeing 75728A · Fuselage Main, FrameSDR FDEA200910223646Frame Splice · damagedMAIN CABIN DECK STA 1280, STR 12 & STR 13, RT HAS FRAME REPAIR SPLICE DAMAGE. REMOVED REPAIR ANGLES, FABRICATED NEW SPLICE REPAIR ANGLES, MAE TRAV T9/805464, INSTALLED REPAIR PARTS AT STA 1280, STR 12 & 13 RT, IAW SRM 53-00-07, FIG 201, REPAIR 2. MAJOR REPAIOct 22, 2009 · N913FD · Boeing 75728A · Fuselage Main, FrameSDR FDEA200910133554Skin · corrodedNR 1 PYLON, INBD AFT SKIN ASSY HAS CORROSION. REMOVED CORROSION, REMOVED SKIN IAW SRM 54-50-01. FABRICATED NEW SKIN ON MAE TRAV NR T9/803805. INSTALLED NEW SKIN PANEL ASSY INBD AFT IAW EA NR F-5450-131114. MAJOR REPAIR.Oct 13, 2009 · N913FD · Boeing 75728A · Nacelle/Pylon, Plate/SkinSDR FDEA200910063486Skin · delaminatedDELAMINATION ON SLAT NR 6, TRAILING WEDGE, ABOUT 30" FROM INBD EDGE. ACCOMPLISHED REPAIR OF RT WING, NR 6 L/E SLAT, T/E WEDGE, ABOUT 30" FROM INBD END IAW EA F5750-133518, SRM 51-70-10, REPAIR NR 4, AND SRM 57-43-02. THIS REPAIR IS CLASSIFIED AS A CAT "A" MAJOOct 6, 2009 · N913FD · Boeing 75728A · Leading Edge DevicesSDR FDEA200909303446Skin · dentedPROTRUDING DENT BETWEEN STA 324- 333.45, STR 22- 23 LT SIDE FUSLAGE. AFTER EVAL, DENT OUT OF LIMITS IAW SRM 53-00-01, FIG 101, DET III, CUT OUT DAMAGE AREA, FABRICATED REPAIR DOUBLER AND FILLER, INSTALLED REPAIR IAW SRM 51-40-02, AND SRM 53-00-01, FIG 201, Sep 30, 2009 · N913FD · Boeing 75728A · Fuselage Main, Plate/SkinSDR FDEA200909233372Floorbeam · corrodedFWD CABIN, FLOORBEAM (BULKHEAD) AT BS 324, RBL 26-RBL 60, UPPER SURFACE HAS SEVERAL AREAS OF CORROSION. REMOVED CORROSION IAW SRM 51-10-02. ORIGINAL MATERIAL THICKNESS .125, AFTER REWORK .106 INCH, REMOVED .019 INCH; L=2 INCHES, W=2 INCHES, D=.019 INCH, FOUNSep 23, 2009 · N913FD · Boeing 75728A · Fuselage Main, Floor BeamSDR FDEA200909223365Skin · damaged3 EA LIGHTENING STRIKES FOUND DURING SCRIBELINE LAP SEEM INSP LOCATED AT BS 1440.125 S-4R AND BS 1449.500 S-4R IN THE LAP SEAM. EACH MARKED WITH DOT. DOT 137-001 ACCOMPLISHED EA F-5330-131525. THIS IS A CAT B REPAIR WITH INSPECTIONS EVERY 3000 FC'S INCLUDINSep 22, 2009 · N913FD · Boeing 75728A · Fuselage Main, Plate/SkinSDR FDEA200909163310Panel · debondedLT WING UPPER INBD FIXED PANEL EXT- SKIN AT RSTA 177.5, PANEL MOUNTING HOLES ELONGATED SKIN BULGING / DISBONDED. ACCOMPLISHED EA F- 5730-131110, THIS REPAIR HAS RECEIVED FIRST STAGE APPROVAL, THE DTA WILL BE TRACKED VIA ENMDS, 24 MONTHS FROM FAA FORM 8100-9Sep 16, 2009 · N913FD · Boeing 75728A · Wing, Plate/SkinSDR 22AA200900024Adc · inoperativeON TAKE OFF, NO AIRSPEED, CA'S ASI. REMOVED AND REPLACED, AIR DATA COMPUTER IAW AMM 34-12-01, PERFORMED LOW RANGE PITOT STATIC LEAK CHECK IAW 34-11-00, SYS WORKS NORMAL GMM 1-4-3.Sep 15, 2009 · N822PB · Boeing 75728A · Air Data ComputerSDR FDEA200909123293Skin · crackedNR 1 PYLON OTBD AFT 311N5046-31 SKIN ASSY HAS 2 EA FASTENER HOLES WITH VISIBLE CRACKS AT APROX PPS 153.90 NDT HFEC INSPECTED VERIFIED CRACKS IAW NTM, 51-00-19 PART 6, (CRACK LENGTHS ARE 1=0.250 INCH, 2= .0200 INCH, 3= 0.198 INCH, STOP DRILLED CRACKS IAW EA F-5Sep 12, 2009 · N913FD · Boeing 75728A · Nacelle/Pylon, Plate/SkinSDR FDEA200909123292Skin · corrodedRT NAC- FWD INBD SKIN INNER WALL CORRODED, JUST AFT OF 443 GL ACCESS PANEL CUT-OUT. REMOVED CORROSION IAW SRM 54-50-01 FIG 101 L=1.0 INCH, W=1.0 INCH, D=0.035 INCH, ORIGINAL MAT. 0.90 INCH, MAT REMAINING 0.055 INCH FOUND TO BE OUT OF LIMITS IAW SRM 54-50-01 FISep 12, 2009 · N913FD · Boeing 75728A · Nacelle/Pylon, Plate/SkinSDR FDEA200909123291Skin · corrodedLT PYLON EXT LWR OTBD SKIN JUST BELOW MID SPAR FUSE PIN (APROX PP-185 TO PPS-196 ) HAS CORROSION. REMOVED CORROSION IAW SRM 54-50-01, DETAIL 1 AND FIG 101. ORIGINAL MAT 0.090 INCH, REMAINING MAT. 0.074 INCH, L=12.0 INCH, W=1.75 INCH, D=0.016 INCH FOUND TO BESep 12, 2009 · N913FD · Boeing 75728A · Nacelle/Pylon, Plate/SkinSDR FDEA200909123290Skin · corrodedNR 1 PYLON OTBD AFT 311N5046-31 SKIN ASSY HAS CORROSION ON INTERIOR SURFACE BETWEEN FWD ACCESS DOOR OPENING AND PRECOOLER OPENING. REMOVED CORROSION FROM INTERIOR SURFACE IAW SRM 54-50-01 ORIGINAL MATERIAL 0.90 INCH, MATERIAL LOSS 0.013", MAT REMAINING 0.077 Sep 12, 2009 · N913FD · Boeing 75728A · Nacelle/Pylon, Plate/SkinSDR FDEA200909093278Skin · misrepairedPREVIOUSLY INSTALLED REPAIR IDENTIFIED AT BS 1610, S-17L/18L, HAS UNDERSIZED FASTENERS. REMOVED EXISTING DOUBLER IAW SRM 51-40-02. CUT OUT DAMAGED AREA IAW SRM 53-00-01. REPAIR 3 FIG 201. INSPECTED CUT OUT AND OPEN HOLES FOR CRACKS, NO CRACKS FOUND IAW NSep 9, 2009 · N913FD · Boeing 75728A · Fuselage Main, Plate/SkinSDR FDEA200909013210Pressure Panel · corrodedON PRESSURE DECK UPPER SURFACE FWD OF BS 1040, BELOW CREASE BEAM STR- 18L. ACCOMPLISHED EA NR F-5710-131109, WING CTR SECTION - UPPER SKIN CORROSION REPAIR, LBL 62, STA 1040, AND REAR SPAR , FAA FOR 8100-9, DATED 08/21/2009 ATTACHED.Sep 1, 2009 · N913FD · Boeing 75728A · Wing, Rib/BulkheadSDR FDEA200909013209Crease Beam · misalignedWHILE PERFORMING PTF SECTION 46 RT CREASE BEAM MOD, PRODUCTION FOUND A MISMATCH INBD TO OUTBD BETWEEN THE CREASE BEAM INNER CHORD AT THE PRODUCTION SPLICE AT APPROX STA 1628, RBL 63. A REPAIR WAS ACCOMPLISHED AT STA 1590-1628, RBL 63, CREASE BEAM INNER CHORDSep 1, 2009 · N913FD · Boeing 75728A · Fuselage Main, StructureSDR FDEA200908313190Splice · misalignedSPLICE 657N3338-35, WILL HAVE SHORTED AT THE FWD MOST FASTENER HOLE COMMON TO IT'S VERTIVLE LEG IF DRILLED. DUE TO THE DISCREPANCY EFFECTING THE PTF MOD A REPAIR WAS ACCOMPLISHED ON MAE MOD W/C 118350452CZ2R01, MAE EA 757-5341-16-F2256, REV-, AT STA 1150-118Aug 31, 2009 · N913FD · Boeing 75728A · Fuselage Main, StructureSDR FDEA200908283115Bracket · misalignedTV MONITOR BRACKETS INTERFERES WITH PROVISIONS INSTALLATION FROM FS-377 TO FS-1640, STR 3L TO STR 3R. AT BS-760-800, 980-1020, 1100-1140, 1320-1360, AND 1440-1460, B/T STR 3L-3R, FRAME REPAIR WAS ACCOMPLISHED, DUE TO DISCREPANCY EFFECTING THE PTF CONVERSION, OAug 28, 2009 · N913FD · Boeing 75728A · Fuselage Main, StructureSDR FDEA200908273112Floorbeam · failedTHE INCOMING FLOORBEAM REPAIR AT STA 1661 WILL INTERFERE WITH THE INSTALLATION OF SEAT TRACKS AND CREASE BEAMS. REMOVED FLOORBEAM AT STA 1661 IAW SRM 51-40-02, FABRICATED NEW BEAM FROM BAC 1518-338 BATCH NR 0001674883 IAW DWG 146N5090, ANODIZED IAW BAC 5019 REAug 27, 2009 · N913FD · Boeing 75728A · Fuselage Main, Floor BeamSDR FDEA200908273111Floorbeam · failedTHE INCOMING FLOORBEAM REPAIRS AT STA 1640 WILL INTERFERE WITH THE INSTALLATION OF SEAT TRACKS AND CREASE BEAM MODS. REMOVED FLOORBEAM AT STA 1640 IAW SRM 51-40-02, FABRICATED NEW FLOORBEAM FROM BAC1518-338 BATCH NR 0001674883 IAW DWG 146N5089, ANODIZED IAW BAug 27, 2009 · N913FD · Boeing 75728A · Fuselage Main, Floor BeamSDR FDEA200908263107Frame · damagedSTA 418, FRAME B/T STR 3L-3R, NUMEROUS MISDRILLED HOLES. (INCOMING CONDITION) AT BS 418, B/T STR 3L-3R, FRAME REPAIR WAS ACCOMPLISHED, DUE TO DISCREPANCY EFFECTING THE PTF CONVERSION, ON MAE W/C NR 118450524AZD, AND MAE EA 757-5332-16-F2172, REV A, DATED 08/17Aug 26, 2009 · N913FD · Boeing 75728A · Fuselage Main, FrameSDR FDEA200908263106Frame · damagedFRAME STA 395 B/T STR 3L-3R, NUMERIOUS MISDRILLED HOLES, (INCOMING CONDITION). REPAIR WAS ACCOMPLISHED,DUE TO DISCREPANCY EFFECTING THE PTF CONVERSION, ON MAE MOD W/C 118450524AZD, AND MAE EA 757-5332-16-F2172, REV A, DATED AUG 17, 2009, THIS NON ROUTINE ISAug 26, 2009 · N913FD · Boeing 75728A · Fuselage Main, FrameSDR FDEA200908263105Frame · damagedFRAME STA 377.7, B/T STR 3L-3R, NUMERIOUS MISDRILLED HOLES. (INCOMING CONDITION) AT BS 377.7, B/T STR 3L-3R, NUMERIOUS MISDRILLED HOLES, FRAME REPAIR WAS ACCOMPLISHED DUE TO DISCREPANCY AFFECTING THE PTF CONVERSION, OM MAE W/C NR 118450524AZD, AND MAE EA RN 7Aug 26, 2009 · N913FD · Boeing 75728A · Fuselage Main, FrameSDR FDEA200908253084Frame · damagedBS. 560, FRAME LWR FLANGE OUTBD OF STR 26L, OTBD HOLE ED, WILL NOT ALLOW ACCOMPLISHMENT OF PTF, COVERSION, PRE- EXISTING INSTALL. BS. 560, FRAME, LWR FLANGE OTBD OF STR 26L, O/B HOLE SED WAS ACCOMPLISHED ON MAE MOD W/C NR 118250287DSSRO8, AND MAE EA NR 75Aug 25, 2009 · N913FD · Boeing 75728A · Fuselage Main, FrameSDR FDEA200908253083Frame · damagedBS 620, FRAME LWR FLANGE OUTBD OF STR 26L, OUTBD HOLE E.D. WILL NOT ALLOW ACCOMPLISHMENT OF PTF CONVERSION, PRE- EXISTING INSTALL. BS. 620, FRAME, LOWER FLANGE O/B OF S26L, O/B HOLE S.E.D. WAS ACCOMPLISHED ON MAE MOD W/C NR 118250287DSSR08, AND MAE EA NR Aug 25, 2009 · N913FD · Boeing 75728A · Fuselage Main, FrameSDR FDEA200908253082Frame · misalignedBS 580 FRAME LWR FLANGE OTBD OF STR 26L OTBD HOLE ED WILL NOT ALLOW ACCOMPLISH OF PTF CONVERSION - PREEXISTING INSTALL BS 580 FRAME, LWR FLANGE OTBD OF STR 26L O/B HOLE SED WAS ACCOMPLISHED ON MAE MOD W/C 118250287 DSSR08, AND MAE EA NR 757-5332-16-F2205 REV-,Aug 25, 2009 · N913FD · Boeing 75728A · Fuselage Main, Frame
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