Boeing 757-23A

Service difficulty reports · 1,397

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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 = '75723A'
  ORDER BY difficulty_date DESC"

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SDR FDEA200910123542Floorbeam · corrodedMAIN CABIN FLOORBEAM STA 337, BL 0 TO LBL 65 HAS AREAS OF CORROSION AROUND FASTENER HOLES. BLEND OUT FLOORBEAM IAW SRM 51-10-02 ,AND CHECK LIMITS, ORIG MAT .125 AFTER REWORK .085 FOUND OUT OF LIMITS IAW SRM 53-00-51 DET 3 CUT OUT DAMAGED AND FABRICATED NEOct 12, 2009 · N921FD · Boeing 75723A · Fuselage Main, Floor BeamSDR FDEA200910073498Slide · dislodgedRAMP CREW ATTEMPTED TO OPEN DOOR L1 WITH SLIDE ARMED, SLIDE FELL OUT OF DOOR. RELEASED FOR SERVICE IAW MEL: 52-11-01-A CATEGORY: B EXPIRATION: 10OCT09 "MEL 52-11-01-A: L1 DOOR SLIDE - INOP. " PLACED SLIDE IN CREW LUGGAGE AREA. INSTALLED SLIDE COVER BACK ONOct 7, 2009 · N917FD · Boeing 75723A · Escape SlideSDR FDEA200910023462Fuel/Oil Cooler · dirtyON CLIMBOUT, LT ENGINE LOST POWER AND WOULD NOT RESPOND TO THROTTLE MOVEMENT. WHEN THROTTLE ADVANCED ENGINE ROLLED BACK. THRUST MANAGEMENT COMPUTOR BEGAN RECYCLING THROUGH CON, GA, TO MODES. CTR AUTOPILOT BECAME VERY SLUGGISH AND WOULD NOT RESPOND ENGINE,Oct 2, 2009 · N917FD · Boeing 75723A · Engine Fuel/Oil CoolerSDR FDEA200909193333Switch · out of positionAFTER TAKEOFF AND PASSING 10,000 FT, AIRSPEED ZIPPER DID NOT INCREASE TO EXPECTED CLIMB AIRSPEED, MAX AIRSPEED 268 KTS AT FL 360, ZIPPER RESTRICTED AIRSPEED TO 238 KIAS. DURING DESCENT, PASSING FL300 ZIPPER INCREASED TO 268. DURING APPROACH ZIPPER INDICATIONSep 19, 2009 · N919FD · Boeing 75723A · Navigation SystemSDR FDEA200909083270Fitting · damagedRT TRUNNION,O/B SUPPORT BRACKET AND O/B HOLES IN TRUNNION AND ATTACH FITTING ASSY, HAS ELONGATED HOLES. FREEZE PLUGS FOR YOKE FABRICATED FREEZE PLUG FOR TRUNNION COMPLIED WITH E.A. F-5750-131116 AND FAA FORM 8100-9, DATED 09/01/2009. (INTERIM REPAIR DTA PESep 8, 2009 · N922FD · Boeing 75723A · Wing, Landing Gear Attach FittingsSDR FDEA200908203060Structure · crackedCRACK LWR CHORD RT WING INBD MIDFLAP OTBD SIDE. REMOVED PANEL AND RETAINER IAW SRM 51-30-2, CUT-OUT DAMAGE SECTION DIM: 40 INCH IAW SRM 51-40-4 FIG 1, FABRICATED SECTION FROM BAC 1503-100046 IAW SRM 57- 50-2 AND 51-40-4 PO NR 2909673 DIM: 40 INCH AND SPLICE Aug 20, 2009 · N207FE · Boeing 75723A · Trailing Edge FlapsSDR FDEA200908133012Seat Track · corrodedMAIN CABIN SEAT TRACK RBL 45 IS CORRODED AT BS 466 AND GOUGED AT BS 472. FABRICATED AND INSTALLED NEW SEAT TRACK FROM 602-6549/24 BATCH 0001541987 IAW SRM 53-30-52 AND SRM 51-40-02.Aug 13, 2009 · N922FD · Boeing 75723A · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200908133011Frame · damagedFRAME 1280 INBD FLANGE IS DAMAGED AT STRINGER 16RT. FABRICATED DOUBLER AND FILLER FROM 7075T6 .080 ON MAE TRAVELER T9/790596 IAW SRM 51-70-11 AND INSTALLED IAW SRM 51-70-11.Aug 13, 2009 · N922FD · Boeing 75723A · Fuselage Main, StructureSDR FDEA200908072934Switch · burnedFL 410 '160 MILES FROM ICT SMELLED ELECTRICAL SMOKE IN COCKPIT, AFTER 15 MINUTES SMOKE WENT AWAY. AT 240 ODOR OF SMOKE AGAIN. FOUND LIGHT OVERRIDE SWITCH STUCK. NO ICAS MESSAGES AND NO STATUS MESSAGE, NO C.B. POPPED. COMPLIED WITH FIM 21-00-01 PGS 101 THAug 7, 2009 · N920FD · Boeing 75723A · Flight Compartment LightingSDR FDEA200908062927Seat Track · gougedSEAT TRACK HAS GOUGE ON CROWN AREA AT STA 1064, LBL 24. REMOVED SEAT TRACK, FABRICATED NEW SEAT TRACK ON MAE TRAV T9/799981, INSTALLED SEAT TRACK AND PLATES IAW SRM 53-00-52. REPAIR 4, CATEGORY "A", MAJOR REPAIR.Aug 6, 2009 · N922FD · Boeing 75723A · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200907242736Frame · misalignedEXISTING HOLES IN FRAME AT STA 395, BETWEEN S3L-S3R, INTERFERES WITH INSTALLATION OF CABLE SHROUD MOD-. AT STA 395, S3L-S3R, FRAME REPAIR WAS ACCOMPLISHED , DUE TO DISCREPANCY EFFECTING THE PTF CONVERSION, ON MAE W/C 118450505AZD, AND MAE EA 757-2550-16-F2044,Jul 24, 2009 · N922FD · Boeing 75723A · Fuselage Main, FrameSDR FDEA200907242735Frame · misalignedEXISTING HOLES IN FRAME AT STA 418, BETWEEN S2L-S2R, INTERFERES WITH INSTALLATION, OF CABLE SHROUD MOD- AT STA 418, BETWEEN S2L-S2R, FRAME REPAIR WAS ACCOMPLISHED, DUE TO DISCREPANCY EFFECTING THE PTF CONVERSION ON MAE MOD W/C 118450505AZD, AND MAE EA NR 757Jul 24, 2009 · N922FD · Boeing 75723A · Fuselage Main, FrameSDR FDEA200907212689Floorbeam · noneMCD FLOORBEAM T-CHORD EXISTING REPAIR AT STA 324 FROM RBL 42, RBL 58, COMPLY WITH ATTACHMENT "B" OF EO F-5100-7-5001, P1. COMPLIED WITH ATTACHMENT "B" OF EO NR F-5100-7-5001, PT1. PREVIOUSLY INSTALLED REPAIR ON MCD FLOORBEAM T-CHORD AT STA 324, RBL42-RBL58, Jul 21, 2009 · N922FD · Boeing 75723A · Fuselage Main, Floor BeamSDR FDEA200907152644Wire · brokenAT APPLICATION OF STD TAKEOFF POWER ON TAKE OFF ROLL, RED CONFIG LIGHT AND RED EICAS MESSAGE "SPOILERS" ACCOMPANIED BY WARNING HORN. TAKEOFF ABORTED AT 50KTS. QRH PROCEDURES ACCOMPLISHED FOR BOTH ITEMS. FOUND B-BK WIRE FROM SPOILER HANDLE POSITION SWITCH SJul 15, 2009 · N920FD · Boeing 75723A · Flight Control System WiringSDR FDEA200907142643Relay · malfunctionedAT TAKEOFF POWER, EICAS MESSAGE "SPOILER" (RED MESSAGE) & RED "CONFIG" LIGHT. TAKE OFF ABORTED AT 56KTS. MOVED SPOILER HANDLE FULL-UP. TROUBLESHOT IAW FIM 31-51-00 & WDM 31-51-41. WHEN SPOILERS ACTUATED IN AUTO OR MANUAL NR 5, 6, 7, & 8 SPOILER PANELS DON`Jul 14, 2009 · N920FD · Boeing 75723A · Drag Control SystemSDR FDEA200907132611Floorbeam · misalignedDUE TO EXISTING FLOORBEAM REPAIR AT STA 1320, LBL 4-38, CAN NOT INSTALL MOD FITTING NR 657N3320-1 AT STA 1640, WL 208.10, LBL 24.75, A PREVIOUS REPAIR CONFLICTED WITH ACCOMPLISHMENT OF PTF CONVERSION. A NEW REPAIR WAS ACCOMPLISHED ON MAE W/C 118350521EZ2, ANDJul 13, 2009 · N922FD · Boeing 75723A · Fuselage Main, StructureSDR FDEA200907132610Intercostal · misalignedEXISTING INTERCOSTAL 146N5190-5, WAS PREVIOUSLY REPAIRED AND DOES NOT MATCH UP TO THE NEW FLOORBEAM AT STA 1661, RBL 10. REMOVED INTERCOSTAL, RECIEVED NEW ON MAE TRAV T9/796860, INSTALLED INTERCOSTAL AND SHEAR WEB, STA 1661, RBL 10, IAW SRM 51-40-05, 51-40-02Jul 13, 2009 · N922FD · Boeing 75723A · Fuselage Miscellaneous StructureSDR FDEA200907132609Channel · corrodedWHILE WORKING FLOORBEAM REPLACEMENT AT STA 1661, THE CHANNEL PN 146N5323-5, BL 0, STA 1661- 1681, WAS FOUND CORRODED. REMOVED CHANNEL, RECEIVED NEW CHANNEL PN 146N5323Y5, INSTALLED CHANNEL BL 0, STA 1661- 1681, IAW SRM 51-40-02. CATEGORY "A". MAJOR REPAIR.Jul 13, 2009 · N922FD · Boeing 75723A · Fuselage Miscellaneous StructureSDR FDEA200907092559Intercostal · crackedWHILE WORKING N/R N00657, 1660 FLOORBEAM REPLACEMENT. THE LOWER CHORD ON INTERCOSTAL AT STA 1640- 1660, RBL- 12, WAS FOUND TO BE CRACKED. REMOVED CRACKED LOWER CHORD, RECEIVED ON MAE TRAV NR T9/793657, INSTALLED NEW LOWER CHORD IAW SRM 51-40-05, 51-40-02, Jul 9, 2009 · N922FD · Boeing 75723A · Fuselage Miscellaneous StructureSDR FDEA200907092558Seat Track · crackedSEAT TRACK FLANGE CRACKED AT LBL-45, STA 1230. REMOVED, FABRICATED NEW TRACK WITH PN 60-6549/24, AND INSTALLED SEAT TRACK LBL-45, STA 1180- 1240, IAW SRM 51-40-02, CATEGORY "A" MAJOR REPAIR.Jul 9, 2009 · N922FD · Boeing 75723A · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200906302421Skin · unknownAPPROX STA 660, STR 6L TO 14L, EXCESSIVE CONTOUR MISMATCH. AT BS 660, S6L- S14L, NEW DSS SKIN WAS ACCOMPLISHED DUE TO DISCREPANCY EFFECTING THE PTF CONVERSION, ON MAE MOD W/C 118250277DSSR06, AMD MAE EA 757-5331-16-F2064, REV A, MAY 27, 2009. THIS NON ROUTINJun 30, 2009 · N922FD · Boeing 75723A · Standard Practices/StructuresSDR FDEA200906302420Splice · unknownDUE TO EXISTING FASTENER PITCH ON WEB AT STA 1620-1640, LBL 60. SPLICE CHANNEL (657N4308-1) CAN NOT BE LOCATED. REPLACED SPLICE CHANNEL (657N4308-1) BET STA 1620- 1640, LBL 60. ACCOMPLISHED DUE TO DISCREPANCY AFFECTING THE PTF CONVERSION ON MAE MOD W/C 1183Jun 30, 2009 · N922FD · Boeing 75723A · Standard Practices/StructuresSDR FDEA200906302419Stringer Splice · damagedFITTING PN 657N3250-18, STR 7L, STA 660, IF DRILLED WILL HAVE APPROX .300 ED ON MOST AFT FASTENER COMMON TO INBD EXISTING CHORD, ZWLG CALLOUT AT THIS LOCATION STA 660, S7L, STRINGER SPLICE REPAIR WAS ACCOMPLISHED DUE TO DISCREPANCY EFFECTING THE PTF CONVERSIONJun 30, 2009 · N922FD · Boeing 75723A · Fuselage Main, Longeron/StringerSDR FDEA200906302418Skin · dentedDENT AT BS 1640/ 1661, S23/ 28R COMPLIED WITH EA NR F-5330-124088- CATE "B", REPAIR WITH FOLLOW UP INP AT 37, 500, F/C, THEN REPEAT EVERY 3,000 F/C, METHOD- LFEC IAW NDT MANNUAL 53-00-06, PT 6. FUSE SKIN LWR LOBE DENT REPAIR STA 1640, STR 24R. MAJOR REPAIR.Jun 30, 2009 · N922FD · Boeing 75723A · Fuselage Main, Plate/SkinSDR FDEA200906242282Frame · damagedSTA 520 LWR FRAME INTG, SPLICE CHORD PN 657N3222-1, 4EA EXISTING FASTENER HOLES WHEN DRILLED THROUGH CHORD ARE TOO CLOSE TO RADIUS TO ALLOW PROPER INSTALLATION OF FASTENERS AT STA 520, LWR FRAME INTG, AREA STR 26L, DUE TO DISCREPANCY AFFECTING THE PTF CONVERSIJun 24, 2009 · N922FD · Boeing 75723A · Fuselage Main, FrameSDR FDEA200906242281Frame · activatedUPON REMOVAL OF FASTENERS FROM FRAME SPLICE 640, AT STR'S 8- 9L TO FOM. UNABLE TO INSTALL DUE TO FASTENERS, HOLES DO NOT ALIGN. AT STA 640, STR'S 8- 9L, A MAJOR ALTERATION WAS ACCOMPLISHED DUE TO THE DISCREPANCY AFFECTING THE P TO F CONVERSION, ON MAE MOD CARJun 24, 2009 · N922FD · Boeing 75723A · Fuselage Main, FrameSDR FDEA200906232246Floorbeam · corrodedMCD FLOORBEAM AT STA 310, BETWEEN RBL 25 TO RBL 60, HAS CORROSION AROUND FASTENER HOLES. COMPLIED WITH EA F-5310-123995. FUSE, MAIN FRAME BS 310, RBL25 TO RBL 60, FLOORBEAM MINOR CORROSION BLEND REPAIR. MAJOR REPAIR.Jun 23, 2009 · N922FD · Boeing 75723A · Fuselage Main, Floor BeamSDR FDEA200906222209Floorbeam · corrodedMAIN CABIN FLOORBEAM STA 720, LBL- 62, HAS AREA OF CORRODED FUSE, MAIN FRAME BS- 720 FLOORBEAM MINOR CORROSION BLEND REPAIR, COMPLIED WITH EA F-5310-123996, LBL- 62. CATEGORY "A", MAJOR REPAIR.Jun 22, 2009 · N922FD · Boeing 75723A · Fuselage Main, Floor BeamSDR FDEA200906222208Channel · damagedDUE TO EXISTING FASTENER PITCH ON WEB AT STA 1620-1640, RBL- 0, TO LBL- 60, SPLICE CHANNEL CAN NOT LOCATE AND DRILL. FABRICATED AND INSTALLED 2EA REPAIR SPLICE CHANNELS AT STA 1620- 1640, RBL-0 TO LBL, 60. IAW WORK CARD 118350448EZ2R04, AND EA NR 757-5361-16-FJun 22, 2009 · N922FD · Boeing 75723A · Fuselage Miscellaneous StructureSDR FDEA200906222205Frame · misalignedSTA 1640 RT, THERE ARE 5EA EXISTING FASTENERS HOLES THAT WILL INTERFERE WITH INSTALLATION OF MOD AT STA 1640, FRMAE RT SIDE , WL 200-208, REPAIR WAS ACCOMPLISHED DUE TO DISCREPANCY EFFECTING THE PTF CONVERSION, ON MAE MOD W/C NR 118350400EZ2R02, AND MAE EA NR Jun 22, 2009 · N922FD · Boeing 75723A · Fuselage Main, FrameSDR FDEA200906182155Crease Beam · corrodedAT STA 1370 LT CREASE BEAM CORRODED REMOVED CORROSION IAW SRM 51-10-06, FOUND TO BE OUT OF LIMITS IAW SRM 53-60-13 FIG 101 DETAIL 3, REMOVED INBD LT CREASE BEAM FROM STA 1370-1390 IAW SRM 51-40-02. FABRICATED REPAIR ANGLE AND BEAM IAW SRM 51-70-11 FIG. 1 AND Jun 18, 2009 · N922FD · Boeing 75723A · Fuselage Main, StructureSDR FDEA200906172135Web · crackedAFT CARGO FLOOR SUPPORT WEB AT BS 1520 TO 1540 LBL 28-29 CRACKED AT FASTENER HOLE. REMOVED WEB, RECEIVED NEW WEB. LOCATED AND DRILLED IAW SRM 51-40-05. TREATED AND PRIMED IAW SRM 51-20-01. INSTALLED WEB IAW SRM 51-40-02. THIS REPAIR IS CLASSIFIED AS CATEGJun 17, 2009 · N922FD · Boeing 75723A · Fuselage Miscellaneous StructureSDR FDEA200906102015Strap · corrodedAPU INTAKE FWD EDGE OF SURROUND, HAS HIDDEN CORROSION/APU COMPOSITE INTAKE PANEL, BULGING SKIN. CLEANED AREA FWD, AFT, UPPER AND LWR EDGE OF SURROUND APU INLET IAW SOPM 20-30-03. CORROSION FOUND ON FWD AND AFT STRAP, UPPER AND LOWER ANGLES. REMOVED CORROSION Jun 10, 2009 · N922FD · Boeing 75723A · APU Cowling/ContainmentSDR FDEA200906081954Cargo Track · damagedMAIN DECK CARGO TRACK IS DAMAGED & GOUGED AT BS 465 AND 475 LBL 45. BLENDED CARGO TRACK AND FOUND OUT OF LIMITS IAW SRM 53-00-52. REMOVED CARGO TRACK IAW SRM 51-40-02. FABRICATED NEW CARGO TRACK IAW SRM 53-30-52. TREATED AND PRIMED IAW SRM 51-20-01. INSTAJun 8, 2009 · N922FD · Boeing 75723A · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200905301855Intercostal · crackedMAIN CARGO DECK INTERCOSTAL IS CRACKED AT BS 1361, S10L. REMOVED INTERCOSTAL, IAW SRM 51-40-02. UPON FURTHER INSPECTION, VERIFIED INTERCOSTAL WAS CRACKED. FABRICATED INTERCOSTAL, LOCATED AND DRILLED IAW SRM 51-40-02. TREATED AND PRIMED IAW SRM 51-20-01. INSTAMay 30, 2009 · N922FD · Boeing 75723A · Fuselage Miscellaneous StructureSDR FDEA200905291849Floorbeam · corrodedMAIN DECK FLOORBEAM AT BS 1660, RBL 9, HAS TOOLING MARKS. REMOVED TOOLING MARKS IAW SRM 53-00-51 AND FOUND OUT OF LIMITS PER SRM 53-00-51. REMOVED FLOORBEAM IAW SRM 51-40-02. RECEIVED NEW FLOORBEAM, LOCATED AND DRILLED IAW SRM 51-40-05. INSTALLED NEW FLOORBEMay 29, 2009 · N922FD · Boeing 75723A · Fuselage Main, Floor BeamSDR FDEA200905291847Crease Beam · corrodedNR 3 LT EMERGENCY EXIT DOOR LOWER SILL BS 1343, HAS 1 RUSTY NUTPLATE. REMOVED NUTPLATE, CORROSION NOTED AT LOWER SILL TEE BRACKET & CREASE BEAM AT BS 1343. REMOVED CORROSION ON CREASE BEAM, FOUND OUT OF LIMITS IAW SRM 53-60-15. REMOVED CREASE BEAM AT BS 12May 29, 2009 · N922FD · Boeing 75723A · Fuselage Main, StructureSDR FDEA200905291850Skin · damagedAPPROX BS 650, LAP 26, BOTTOM ROW OF FASTENERS, 1 FASTENER HOLE HAS AN ELONGATED HOLE .270 INCH DIAMETER AT BS 650, LAP 26, (BS 646 / S26L), SKIN REPAIR WAS ACCOMPLISHED, DUE TO DISCREPANCY EFFECTING THE PTF CONVERSION, ON MAE MOD W/C NR 118250287DSSR08, AND MMay 29, 2009 · N922FD · Boeing 75723A · Fuselage Main, Plate/SkinSDR FDEA200905291848Floorbeam · corrodedMAIN DECK BS 1640 FLOORBEAM AT LBL 12, HAS AREA OF CORROSION. REMOVED CORROSION IAW SRM 53-00-51 AND FOUND OUT OF LIMITS IAW SRM 53-00-51. REMOVED FLOORBEAM AT BS 1640, LBL 65-RBL 65, IAW SRM 51-40-02. RECEIVED NEW FLOORBEAM, LOCATED AND DRILLED IAW SRM 51-May 29, 2009 · N922FD · Boeing 75723A · Fuselage Main, Floor BeamSDR FDEA200905281845Seat Track · gougedMAIN CARGO DECK SEAT TRACK HAS GOUGES FROM STA 480-510, LBL-45. REMOVED SEAT TRACK IAW SRM 51-40-02. FABED NEW SEAT TRACK MAT P/N 60-6549-24, IAW SRM 53-30-52. INSTALLED SEAT TRACK AT STA 440-680, LBL-45, IAW SRM 53-30-52, AND 51-40-02. CATEGORY "A" . MAJORMay 28, 2009 · N922FD · Boeing 75723A · Fuselage, Seat/Cargo Attach FittingsSDR CNMA20090151Access Panel · damagedKEELBEAM ACCESS PANEL NR 139 AL HAS EDGE DAMAGE ON RT AND LT SIDES. SANDED, CLEANED AND PREPED KEELBEAM PANEL NR 139 AL IAW SRM 51-70-03, PG 6-8, APPLIED REPAIR IAW SRM 51-70-03 PG 9-13 AND RESTORED FINISH IAW SRM 51-70-03 PG 13.May 27, 2009 · N549AX · Boeing 75723A · Fuselage Main, Plate/SkinSDR CNMA20090150Stanchion · crackedFWD PIT, AFT BULKHEAD CTR STANTION CRACKED. REMOVED AND INSTALLED FWD PIT, AFT BULKHEAD CTR STANTION IAW 51-40-02.May 27, 2009 · N549AX · Boeing 75723A · Fuselage Main, BulkheadSDR CNMA20090149Skin · damagedREPAIR DENT STA 1493 524L AND 25-L EXTERIOR SKIN. CUT OUT DAMAGED AREA OF EXTERIOR SKIN STA 1493 STR 24L AND 25L. FABRICATED REPAIR PARTS AND INSTALL IAW SRM 53-00-01, FIG 201, REPAIR NR 4.May 27, 2009 · N549AX · Boeing 75723A · Fuselage Main, Plate/SkinSDR CNMA20090148Angle · corrodedAFT LAV SERVICE DOOR ANGLE BETWEEN LATCHES IS CORRODED. REPLACED AFT LAV SERVICE DOOR ANGLE BETWEEN LATCHES IAW SRM 52-40-02-13.May 27, 2009 · N549AX · Boeing 75723A · Service DoorsSDR CNMA20090147Support · brokenECS DUCT SUPPORT BROKEN AT STA 1200 IN AFT CARGO COMPARTMENT ON LT SIDE . REPLACED ECS DUCT SUPPORT AT STA 1200 IAW 21-33-01.May 27, 2009 · N549AX · Boeing 75723A · Fuselage Miscellaneous StructureSDR CNMA20090146Scuff Plate · crackedL2 DOOR SCUFF PLATE CRACKED 2 PLACES. INSTALLED REPAIRED L2 DOOR SCUFF PLATE IAW MM 53-13-01-424-003.May 27, 2009 · N549AX · Boeing 75723A · Fuselage Miscellaneous StructureSDR FDEA200905271811Window · crackedAT LEVEL FLIGHT 340 CAPTAIN`S WINDOW CRACKED. RETURNED. WINDOW HAD ARCING AT TOP BEFORE WINDOW CRACKED. REMOVED AND REPLACED CAPT'S L1 WINDOW REF MM 56-11-01-4 AND SUPP 56-11-01-4. COMPLETED WINDOW INSTALL (SEALED AND TORQUED) AS PER MM 56-11-01-4. OPS CHMay 27, 2009 · N920FD · Boeing 75723A · Flight Compartment WindowsSDR FDEA200905271808Skin · corrodedNR 8 L/E SLAT, L/E HAS (3) AREAS OD INTERGRANULAR CORROSION AT WS 548.50, 32" OF I/B EDGE; WS 537.50, APPROX. 43" OF O/B EDGE AND WS 459.50, APPROX. 32" O/B OF I/B EDGE. ACCOMPLISHED CORRSION REPAIR IAW EA F-5740-123985. THIS REPAIR IS CLASSIFIED AS A CAT "May 27, 2009 · N917FD · Boeing 75723A · Leading Edge DevicesSDR FDEA200905271817Skin · corrodedRIGHT LOWER WING T/E HAS CORROSION AT WBL 740- 806.5 REMOVED CORRODED PANEL SKIN IAW SRM 51-40-02. INSTALLED NEW PANEL SKIN RT WING LOWER SURFACE AT WBL 775.5-740. IAW SRM 51-40-02. CATEGORY "A" MAJOR REPAIR.May 27, 2009 · N917FD · Boeing 75723A · Wing, Plate/SkinSDR FDEA200905271816Web · corrodedMCD INT FUSE WEB ON S17R BETWEEN STA 980- 1000, HAS CORR. REMOVED WEB IAW SRM 51-40-02. RECEIVED ON TRAV T9/792531, INSTALLED NEW WEB IAW SRM 51-40-02. CATEGORY "A", MAJOR REPAIR.May 27, 2009 · N922FD · Boeing 75723A · Fuselage Miscellaneous Structure
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