Boeing 757-2G7

Service difficulty reports · 502

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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 = '7572G7'
  ORDER BY difficulty_date DESC"

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SDR AWXA200700245Windshield · arcedFLIGHT 432: PHX - OGG - ATB - PRIOR TO REACHING THE COAST, THE CREW NOTICED AN ELECTRICAL SMELL IN THE FLIGHT STATION. THE CREW SHUT DOWN THE LEFT PACK AND THE SMELL WENT AWAY. BASED ON THE REQUIREMENTS TO HAVE BOTH PACKS OPERATING FOR ETOPS OPERATION, THE CFeb 21, 2007 · N909AW · Boeing 7572G7 · Flight Compartment WindowsSDR AWXA200700114Skin · crackedMCN - CRACK FOUND ON COVE SKIN OF RIGHT WING NR 9 SLAT INBOARD PANEL 624CB, WS 574.8 - 605.3. REPAIRED COVE SKIN OF RIGHT WING NR 9 SLAT INBOARD PANEL 624CB, WS 574.8 - 605.3 IAW BOEING DWG 114N4076, B757 SRM 51-40-02-06 PAR 4-7/4-9, FIG 8-12/8-16, AND B757 Jan 19, 2007 · N909AW · Boeing 7572G7 · Leading Edge DevicesSDR AWXA200700099Clamp · dislodgedFLIGHT 320: PHX - LAS - AT FL 240 NR 2 ENGINE (RT OVHT) ILLUM, EICA AND LOWER PANEL MSG. THE CREW COMPLIED W/QRH, SHUTDOWN NR 2 ENG, (CAPT STATED LIGHT EXTINGUISHED AFTER THROTTLE REDUCTION, AND ILLUMINATED AFTER POWERED BACK UP, THAT'S WHEN INITIATED AN IN-FJan 15, 2007 · N908AW · Boeing 7572G7 · Pneumatic Distribution SystemSDR AWXA200700060Engine · shutdown908 - IFSD - KOA - PHX - DURING CLIMB, THE CREW NOTICED THE NR 1 ENGINE HAD SHUTDOWN IN-FLIGHT. THE CREW DECLARED AN EMERGENCY AND RETURNED TO KOA. MX FOUND PINS 2 AND 5 SHORTED IN CON. D2142, FOUND DAMAGED WIRING IN SHIELD TERMINATION FOR WIRE W3306/R/Y/B-2Jan 11, 2007 · N908AW · Boeing 7572G7 · Fuel Controlling SystemSDR AWXA200700084Attach Angle · crackedMCN - MAIN CABIN INTERCOSTAL UPPER ATTACH ANGLE CRACKED, BS 1520 - BS 1540, BL 0. REPLACED MAIN CABIN INTERCOSTAL UPPER ATTACH ANGLE CRACKED, BS 1520 - BS 1540, BL 0 IAW B737-300SRM 51-40-02.Jan 9, 2007 · N909AW · Boeing 7572G7 · Fuselage Main, Attach FittingsSDR AWXA200700083Attach Angle · crackedMCN - MAJOR REPAIR - MAIN CABIN INTERCOSTAL UPPER ATTACH ANGLE CRACKED, BS 1420 - BS 1440, BL 0. REPLACED MAIN CABIN INTERCOSTAL UPPER ATTACH ANGLE CRACKED, BS 1420 - BS 1440, BL 0 IAW B737-300SRM 51-40-02.Jan 7, 2007 · N909AW · Boeing 7572G7 · Fuselage Main, Attach FittingsSDR AWXA200700061Floorbeam · crackedMCN - MAJOR REPAIR - C-02 CHECK - CRACKS ON TEE CAP, AFT CLIP, BS 1320, LBL 45.5, WL 208.10. REPLACED T-CAP, AFT CLIP, BS 1320, LBL 45.5, WL 208.10 IAW B757-200 SRM 51-40-02.Dec 28, 2006 · N909AW · Boeing 7572G7 · Fuselage Main, Floor BeamSDR AWXA200700062Floorbeam · crackedMCN - MAJOR REPAIR - C-02 CHECK - FLOORBEAM SUPPORT CLIP, BS 1300, RBL 48.5, WL 208. REPLACED FLOORBEAM SUPPORT CLIP CRACKED, BS 1300, RBL 48.5, WL 208 I/A/W B757-200 SRM 51-40-02.Dec 26, 2006 · N909AW · Boeing 7572G7 · Fuselage Main, Floor BeamSDR AWXA200700105Floor Support · corrodedMCN - CORROSION ON MAIN CABIN SUPPORT, BS 1664 - BS 1681.8, RBL 56, WL 208. REPLACED MAIN CABIN SUPPORT, BS 1664 - BS 1681.8, RBL 56, WL 208 IAW B757-200 SRM 51-40-02.Dec 21, 2006 · N909AW · Boeing 7572G7 · Fuselage Miscellaneous StructureSDR AWXA200700089Wedge · delaminatedMCN - MAJOR REPAIR - LEFT WING NR 1 SLAT OUTBOARD TRAILING EDGE WEDGE DELAMINATED, WS 799 - WS 801. REPAIRED LEFT WING NR 1 SLAT OUTBOARD TRAILING EDGE WEDGE, WS 799 - WS 801 IAW B757-200 SRM 51-70-10-2R4, REPAIR 4, FIG 201.Dec 20, 2006 · N909AW · Boeing 7572G7 · Leading Edge DevicesSDR AWXA200700082Skin · crackedMCN - MAJOR REPAIR - LEFT WING NR 2 SLAT LOWER SURFACE SKIN CRACKED, SS 574. REPLACED LEFT WING NR 2 SLAT LOWER SURFACE SKIN, SS 574 IAW B737-300 SRM 51-40-04 AND 51-40-02.Dec 20, 2006 · N909AW · Boeing 7572G7 · Leading Edge DevicesSDR AWXA200700063Skin · corrodedMCN - CORROSION ON FUSELAGE EXTERIOR SKIN, BS 1556, S30, UNDER THE AFT AIRPHONE ANTENNA. REPAIRED FUSELAGE EXTERIOR SKIN, BS 1556, S30 IAW B757-200 SRM 53-00-01-2R3.Dec 20, 2006 · N909AW · Boeing 7572G7 · Fuselage Main, Plate/SkinSDR AWXA200700039Wedge · delaminatedMCN - LEFT WING NR 5 SLAT INBOARD AND OUTBOARD TRAILING EDGE WEDGES DELAMINATED, WS 177.50 AND WS 258.50. REPAIRED LEFT WING NR 5 SLAT INBOARD AND OUTBOARD TRAILING EDGE WEDGES, WS 177.50 AND WS 258.50 IAW B757-200 SRM 51-70-10-2R2, REPAIR 2, FIGURE 203.Dec 20, 2006 · N909AW · Boeing 7572G7 · Leading Edge DevicesSDR AWXA200700050Skin · crackedMCN - RIGHT WING NR 9 SLAT INNER COVE SKIN CRACKED, SS 594.50 - SS 623.50. REPLACED RIGHT WING NR 9 SLAT INNER COVE SKIN, SS 594.50 - SS 623.50 IAW B757-200 SRM 51-40-02 AND BOEING DRAWING 114N4076.Dec 12, 2006 · N909AW · Boeing 7572G7 · Leading Edge DevicesSDR AWXA200601946Skin · damagedFUSELAGE BS 800 BETWEEN S14 AND S15L HAS TWO PLUGGED HOLES THAT WERE R/R THE SHEAR TIE UNDERNEATH. COUNTER SANK THE INNER SKIN AT BS 800 BETWEEN S-14L AND S-15L TO ACCOMODATE THE RIVETS BUTTON. PLUGGED THE TWO HOLES USING BACR15CE AND DOUBLE FLUSHED THE RIVENov 17, 2006 · N910AW · Boeing 7572G7 · Fuselage Main, Plate/SkinSDR AWXA200601936Oxygen Mask · leakingPHX - APPROXIMATELY 1 HR INTO FLIGHT, STATUS PAGE INDICATED O2 PRESS OF 110 NR. THE CREW DECLARED AN EMERGENCY AND RETURNED TO PHX. THE PAX DID NOT BRACE. THE LANDING WAS UNEVENTFUL. MAINTENANCE REMOVED AND REPLACED THE O2 BOTTLE PER TC NR R2A35601. NO LENov 13, 2006 · N908AW · Boeing 7572G7 · Crew Oxygen SystemSDR AWXA200601742Skin · bulgedPHX - MAJOR REPAIR - 4-DAY CHECK - FUSELAGE SKIN HAS POPPED RIVET AND BULGING SKIN, BS 1378 - 1380, S28R.Oct 10, 2006 · N908AW · Boeing 7572G7 · Fuselage Main, Plate/SkinSDR AWXA200601672Support · corrodedMCN - FOUND CORROSION ON R4 DOORWAY LOWER SILL INNER CHORD (SUPPORT), BS 1640 - BS 1661, RBL 57, WL 208. REPLACED CORROSION ON R4 DOORWAY LOWER SILL INNER CHORD (SUPPORT), BS 1640 - BS 1661, RBL 57, WL 208 IAW B757-200 SRM 51-40-02 FIGURE 12.Sep 22, 2006 · N908AW · Boeing 7572G7 · Fuselage Miscellaneous StructureSDR AWXA200601671Support · corrodedMCN - FOUND CORROSION ON L-4 DOORWAY LOWER SILL INNER CHORD (SUPPORT), BS 1661, LBL 57, WL 208. REPLACED L-4 DOORWAY LOWER SILL INNER CHORD (SUPPORT), BS 1661, LBL 57, WL 208 IAW B757-200 SRM 51-40-02 FIGURE 12.Sep 22, 2006 · N908AW · Boeing 7572G7 · Fuselage Miscellaneous StructureSDR AWXA200601637Support Fitting · corrodedMCN - CORROSION ON R-4 DOOR SILL UPPER SURFACE OF LOWER SILL AFT INNER CHORD, B/S 1661-1681, RBL 57, WL 208. REPLACED R-4 DOOR SILL AFT INNER CHORD B/S1661-1681, RBL 57, WL 208 IAW B757-200 SRM 51-40-02-0G PARA 7D FIG 12.Sep 22, 2006 · N908AW · Boeing 7572G7 · Fuselage Miscellaneous StructureSDR AWXA200601632Door Frame · crackedC-02 CHECK - NR 5934562, FWD CARGO COMPARTMENT, UPPER DOOR FRAME 3RD FROM AFT, ANGLE BRACKET CRACKED. REMOVED AND REPLACED FWD CARGO COMPARTMENT, UPPER DOOR FRAME 3RD FROM AFT, ANGLE BRACKET IAW SRM 51-40-02-0G F IG 12 PAR 7D.Sep 18, 2006 · N908AW · Boeing 7572G7 · Cargo/Baggage DoorsSDR AWXA200601631Door Frame · crackedC-02 CHECK - NR 5934564, FWD CARGO COMPARTMENT DOOR UPPER AFT FRAME ANGLE BRACKET CRACKED. REMOVED AND REPLACED FWD CARGO COMPARTMENT DOOR UPPER AFT FRAME ANGLE BRACKET IAW SRM 51-40-02-0G FIG 8 AND SRM 51-40-02-0G FIG 13. Sep 18, 2006 · N908AW · Boeing 7572G7 · Cargo/Baggage DoorsSDR AWXA200601707Stiffener · corrodedMCM - MAJOR REPAIR-C-02 CHECK-NR 5934085, CORROSION UNDER R-4 DOOR LOWER SILL SCUFF PLATE ATTACH FITTING (STIFFENER) BS 1669. REMOVED AND REPLACED ATTACH FITTING AT R-4 DOOR BS 1669 IAW SRM 51-40-02-0G PARA 7D FIG 12.Sep 15, 2006 · N908AW · Boeing 7572G7 · Fuselage Miscellaneous StructureSDR AWXA200601628Bracket · crackedC-2 CHECK - NR 5934563, FWD CARGO COMPARMENT DOOR, FWD FRAME UPPER ANGLE BRACKET CRACKED. REPLACED FWD CARGO COMPARMENT DOOR, FWD FRAME UPPER ANGLE BRACKET IAW SRM 51-40-02, FIGURES 8 & 12.Sep 12, 2006 · N908AW · Boeing 7572G7 · Fuselage Miscellaneous StructureSDR AWXA200601595Life Raft · failedMCN - EMERGENCY EQUIPMENT LIFE RAFT FAILED TO DEPLOY AND INFLATE COMPLETELY, P/N 63800-101 S/N L6037. ROTATABLE PARTS CHANGE WAS INDICATED.Aug 31, 2006 · N908AW · Boeing 7572G7 · Life RaftSDR AWXA200601309Control Unit · out of toleranceTHE CREW ADVANCED THE NR 2 THRUST LEVER TO TAXI AND THE NR 2 ENGINE SHUT DOWN. EGT REACHED 620C. ENGINE SHUTDOWN WAS NOT INITIATED BY THE CREW. THE NR 2 ENGINE BLEED VALVE CONTROL UNIT DISPLAYED A VOLTAGE FAULT. MX REMOVED AND REPLACED THE NR 2 BLEED VALVEJul 22, 2006 · N910AW · Boeing 7572G7 · Compressor Bleed ControlSDR AWXA200601055Wire · brokenPHX - EEL - NR - 4104203 - DURING OVERNIGHT MAINTENANCE IT WAS DISCOVERED THAT ROW 29L SEAT EMERGENCY LIGHT WAS INOP. MAINTENANCE REPAIRED THE BROKEN WIRES TO THE LIGHT IAW 20-10-3.Jun 28, 2006 · N908AW · Boeing 7572G7 · Light System WiringSDR AWXA200601031Controller · inoperativeHNL - DIVERSION - FLT 931 - DURING CLIMB-OUT OF OGG EN ROUTE TO PHX, THE CREW NOTICED THAT THE CABIN WAS CLIMBING WITH THE AIRCRAFT IN AUTO 1 POSITION. RECEIVED CABIN ALT MASTER CAUTION AND SWITCHED TO AUTO 2, THERE WAS NO CHANGE. RECEIVED CABIN ALT 1 AND 2 Jun 24, 2006 · N909AW · Boeing 7572G7 · Cabin Pressure ControllerSDR AWXA200600926Wire · brokenPHX - EEL - DURING OVERNIGHT MAINTENANCE DISCOVERED BOTH RED EMERGENCY LIGHTS WERE INOPERATIVE AT ROW 27. MAINTENANCE REPAIRED BROKEN WIRE AT ROW 27L FOR EMERGENCY ESCAPE PATH LIGHTING. OPERATIONAL CHECKS WERE GOOD.Jun 9, 2006 · N909AW · Boeing 7572G7 · Light System WiringSDR AWXA200600887Pin · burnedOGG - EEL - LG 7250100 & 7250101 - OVERHEAD EMERGENCY LIGHTS BETWEEN SEAT ROWS 4 AND 5 DO NOT ILLUMINATE ON GROUND TEST. M731 POWER SUPPLY BAD. OGG MAINTENANCE REMOVED AND REPLACED POWER SUPPLY AND BATTERY PACK IAW MM 33-51-07. AIRCRAFT WAS FERRIED BACK TO Jun 1, 2006 · N910AW · Boeing 7572G7 · Emergency LightingSDR AWXA200600814Connector · damagedPHX - FLT 7832 - DURING REPO FLIGHT CREW REPORTED THAT INBOUND TO PHX RECEIVED LEADING EDGE FLAP ASYMMETRY AND DISAGREE LIGHT. QRH PROCEDURES WERE FOLLOWED. LANDED IN PHX WITHOUT FURTHER EVENT. MAINTENANCE CHECKED WIRING BETWEEN FSEU 1, FSEU 2 AND RT SLATMay 13, 2006 · N910AW · Boeing 7572G7 · Leading Edge Slat Control SystemSDR AWXA200600805Transmitter · faultyHNL - FLT 920 - CREW REPORTED THAT AFTER SELECTING FLAPS 1 ON APPROACH INTO HNL, RECEIVED "LE SLAT DISAGREE" CAUTION MSG. CREW FOLLOWED QRH CHECK LIST AND THEN RECEIVED "LE SLAT ASYMMETRY" CAUTION MSG. CREW FOLLOWED QRH AND PERFORMED ALL FLAPS/SLATS UP LANDIMay 11, 2006 · N910AW · Boeing 7572G7 · Leading Edge Slat Control SystemSDR AWXA200600759Battery Pack · overheatedGYR - EEL - NR 5919942 - DURING C12 CHECK DISCOVERED THE EMERGENCY LIGHTS BATTERY PACK, JUST AFT OF FWD ENTRY LIGHT, WAS OVERHEATING. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK IAW BOEING 757-200 AMM 33-51-07-2. OPERATIONAL CHECKS WERMay 1, 2006 · N910AW · Boeing 7572G7 · Emergency LightingSDR AWXA200600720Pump · malfunctionedCREW REPORTED RECEIVING "HYD QTY EICAS MESSAGE PRIOR TO DEP L HYD QTY DROPPED TO 0.26, RT HYD PRESS DROPPED TO 2940 PSI." CREW DIVERTED TO PHX AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE FOUND METAL IN LT CASE DRAIN PRESSURE MODULE FILTER. ALSO, FOUND THEApr 21, 2006 · N908AW · Boeing 7572G7 · Hydraulic Pump (Electric/Engine), MainSDR AWXA200600795Channel · crackedGYR - DURING C12 CHECK DISCOVERED CHANNEL ASSEMBLY CRACKED ON THE L4 DOOR. MAINTENANCE REMOVED AND INSTALLED NEW L4 DOOR CHANNEL ASSEMBLY IAW BOEING 757-200 SRM 51-40-02-06 PAGE 8.Apr 20, 2006 · N910AW · Boeing 7572G7 · Passenger/Crew DoorsSDR AWXA200600790Gate · corrodedGYR - DURING C12 CHECK DISCOVERED LEVEL 2 CORROSION ON THE R2 DOOR UPPER GATE HINGE AREA, ALONG FULL LENGTH. MAINTENANCE REMOVED AND INSTALLED NEW UPPER GATE IAW MM 52-11-38-4. GATE WAS ADJUSTED IAW MM 52-11-00-5.Apr 19, 2006 · N910AW · Boeing 7572G7 · Passenger/Crew DoorsSDR AWXA200600749Attach Fitting · galledDURING C12 CHECK DISCOVERED RT WING INBOARD STRUT ATTACH FITTING FOR PYLON GALLED FROM BUSHING CONTACT ON THE INBOARD AND OUTBOARD SIDES OF LUG AT WBL 248R. MAINTENANCE REMOVED OUTBOARD BUSHING IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 19-5704-06114-RC2Mar 29, 2006 · N910AW · Boeing 7572G7 · Nacelle/Pylon, Attach FittingsSDR AWXA200600748Attach Fitting · galledDURING C12 CHECK DISCOVERED RT WING OUTBOARD STRUT ATTACH FITTING LUGS FOR PYLON GALLED FROM BUSHING CONTACT ON THE INBOARD AND OUTBOARD SIDES OF LUG AT WBL 263R . MAINTENANCE REMOVED OUTBOARD BUSHING IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 19-5704-06Mar 29, 2006 · N910AW · Boeing 7572G7 · Nacelle/Pylon, Attach FittingsSDR AWXA200600648Shim · migratedGYR - DURING C12 CHECK DISCOVERED NR 1 PYLON DIAGONAL BRACE FITTING SHIMS MIGRATING LEFT SHIM HORIZONTAL MOVEMENT 0.400 INCHES AND VERTICAL MOVEMENT 0.900 INCHES. MAINTENANCE REPAIRED PER AWA ER 19-5453-06060-BA1 AND BOEING SB 757-54-0035 FIG. 21, STEPS 8, 12Mar 29, 2006 · N910AW · Boeing 7572G7 · Nacelle/Pylon Miscellaneous StructureSDR AWXA200600647Shim · migratedGYR - DURING C12 CHECK DISCOVERED NR 2 ENGINE PYLON DIAGONAL BRACE ATTACH FITTING VERTICAL SHIMS MIGRATED LT 0.200 INCHES AND R/H 0.030 INCHES. MAINTENANCE REMOVED AND REPLACED LEFT AND RIGHT DIAGONAL BRACE ATTACH FITTING SHIMS PER AWA ER 19-5453-06060-BA1.Mar 29, 2006 · N910AW · Boeing 7572G7 · Wing Miscellaneous StructureSDR AWXA200600750Attach Fitting · galledDURING C12 CHECK DISCOVERED LT WING OUTBOARD STRUT ATTACH FITTING FOR PYLON GALLED FROM BUSHING CONTACT ON THE INBOARD AND OUTBOARD SIDES OF LUG AT WBL 263L. MAINTENANCE REMOVED OUTBOARD BUSHING IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 19-5704-06114-RCMar 28, 2006 · N910AW · Boeing 7572G7 · Nacelle/Pylon, Attach FittingsSDR AWXA200600747Attach Fitting · galledDURING C12 CHECK DISCOVERED LUG SURFACES GALLED FROM BUSHING CONTACT ON THE INBOARD AND OUTBOARD SIDES OF LEFT WING INBOARD STRUT ATTACH FITTING FOR PYLON AT WBL 248L. MAINTENANCE REMOVED INBOARD BUSHING IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 19-5704Mar 28, 2006 · N910AW · Boeing 7572G7 · Wing, Attach FittingsSDR AWXA200600664Floorbeam · corrodedGYR - DURING C12 CHECK DISCOVERED LEVEL 2 GALVANIC CORROSION ON THE MAIN CABIN FLOORBEAM UPPER EDGE AT BS 365 FROM BL 15R TO BL 35R. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW BOEING 757-200 SRM 53-00-51-2A. MAINTENANCE CUT OUT AND REMOVED DAMAGED AREA IAWMar 27, 2006 · N910AW · Boeing 7572G7 · Fuselage Main, Floor BeamSDR AWXA200600616Floorbeam · corrodedGYR - DURING C12 CHECK DISCOVERED LEVEL 2 GALVANIC CORROSION ON FLOORBEAM AT BS 740 FROM BL 45.5R TO BL 55.5R, WL 208. MAINTENANCE CUT OUT DAMAGED AREA AT BS 740 BL 45.5R IAW SRM 53-00-51-2R. CORROSION FOUND TO BE OUT OF SRM LIMITS. FABRICATED REPAIR ANGLEMar 26, 2006 · N910AW · Boeing 7572G7 · Fuselage Main, Floor BeamSDR AWXA200600789Support · corrodedGYR - DURING C12 CHECK DISCOVERED LEVEL 2 CORROSION ON FASTENER HOLE AT BOTTOM SURFACE OF FLOOR PANEL SUPPORT ANGLE AT BL 60R AND BS 684.5. CORROSION WAS FOUND TO BE OUT OF LIMITS. INSTALLED NEW FLOOR PANEL SUPPORT ANGLE AT BL 60R AND BS 684.5.Mar 25, 2006 · N910AW · Boeing 7572G7 · Fuselage Miscellaneous StructureSDR AWXA200600712Web · corrodedGYR - DURING C12 CHECK DISCOVERED CORROSION, LEVEL 2 INTERGRANULAR, ON R3 LOWER DOOR EMERGENCY LOWER WEB FROM BS 1340 TO BS 1360, WL 208.1, STR 17R, FROM BL 70R TO BL 79R. MAINTENANCE REMOVED CORROSION FROM WEB LOWER SIDE FROM BS 1340 TO BS 1360, WL 208.1, STMar 24, 2006 · N910AW · Boeing 7572G7 · Fuselage Miscellaneous StructureSDR AWXA200600711Web · corrodedGYR - DURING C12 CHECK DISCOVERED CORROSION, LEVEL 2 INTERGRANULAR, ON L3 DOOR EMERGENCY LOWER WEB FROM BS 1340 TO BS 1360 AT STR 17L. MAINTENANCE REMOVED CORROSION FROM LOWER WEB FROM BS 1340 TO BS 1360 AT STR 176 IAW BOEING 757-200 SRM 51-10-02. CORROSION Mar 24, 2006 · N910AW · Boeing 7572G7 · Fuselage Miscellaneous StructureSDR AWXA200600752Floorbeam · crackedDURING C12 CHECK DISCOVERED FLOORBEAM CRACKED IN TWO PLACES AT BS 700, ONE CRACK AT BL 24R AND THE OTHER AT BL 46R. EACH CRACK WAS APPROXIMATELY 1 INCH LONG. MAINTENANCE CUT OUT DAMAGED AREA. FABRICATED SUPPORT ANGLES, REINFORCEMENT STRAPS, AND FILLER IAW AMar 23, 2006 · N910AW · Boeing 7572G7 · Fuselage Main, Floor BeamSDR AWXA200600751Skin · delaminatedDURING C12 CHECK DISCOVERED 2 SQUARE INCH AREA OF DELAMINATION ON THE UPPER SURFACE OF THE NR 8 SLAT, TRAILING EDGE WEDGE AT THE INBOARD END AT WBL 440R. MAINTENANCE REMOVED DAMAGED AREA IAW BOEING 757-200 SRM 51-70-10-2R. FABRICATED FILLER AND DOUBLER IAW BMar 20, 2006 · N910AW · Boeing 7572G7 · Leading Edge DevicesSDR AWXA200600653Wedge · delaminatedGYR - DURING C12 CHECK DISCOVERED ONE SQUARE INCH DELAMINATION AREA ON TOP SURFACE OF NR 7 L/E SLAT 28 INCHES FROM OB EDGE. MAINTENANCE CUT OUT DAMAGED AREA. FABRICATED FILLER AND DOUBLER. BONDED FABRICATED PARTS TO TOP SURFACE OF NR 7 L/E SLAT 28 INCHES FRMar 20, 2006 · N910AW · Boeing 7572G7 · Leading Edge Devices
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