Airbus A318-111

Service difficulty reports · 353

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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 = 'A318111'
  ORDER BY difficulty_date DESC"

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SDR F3LA200800556Blanking Plate · corrodedDURING C-CHECK, INSP NOTED R2 AFT GIRT BAR BLANKING PLATE HAS CORROSION. MAINT REMOVED AND REPLACED BLANKING PLATE WITH NEW ONE FROM STOCK AND INSTALLED ON TASK CARD C5341032. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. (S)Aug 16, 2008 · N806FR · Airbus A318111 · Fuselage Miscellaneous StructureSDR F3LA200800555Blanking Plate · corrodedDURING C-CHECK INSP, NOTED R2 FWD GIRT BAR BLANKING PLATE HAS CORROSION. MAINT REMOVED AND REPLACED BLANKING PLATE WITH NEW ONE FROM STOCK AND INSTALLED ON TASK CARD C5341032. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. (S)Aug 16, 2008 · N806FR · Airbus A318111 · Fuselage Miscellaneous StructureSDR F3LA200800554Floor Panel · corrodedDURING C3 C-CHECK, INSP NOTED FLOOR PANEL 261FF HAS CORROSION ON LOWER SURFACE. MAINT REMOVED AND REPLACED FLOOR PANEL 261FF WITH A NEW PANEL AND INSTALLED ON TASK CARD C5341032. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. (S)Aug 16, 2008 · N806FR · Airbus A318111 · Fuselage Floor PanelSDR F3LA200800559Shear Plate · corrodedDURING C-CHECK INSP, NOTED CORROSION AROUND NUT CLIP HOLE APPROX 4.25 INCHES AFT OF FWD END ON RT SIDE FLOORBEAM ALONG Y1292 BETWEEN FR68 AND FR69. MAINTENANCE BLENDED AREA, FABRICATED FLANGE BUSHING AND INSTALLED IAW THE REQUIREMENTS OF ENGINEERING AUTHORIZAAug 16, 2008 · N806FR · Airbus A318111 · Fuselage Miscellaneous StructureSDR F3LA200800552Sill · corrodedDURING C3 C-CHECK, INSPECTION NOTED THE VERY AFT NUT PLATE HOLE ON L-2 DOOR SILL AT FRAME 68, JUST AFT OF GIRT BAR FITTING ASSEMBLY, WAS CORRODED. MAINTENANCE CUTOUT DAMAGE, MANUFACTURED REPAIR DOUBLER AND INSTALLED IAW THE REQUIREMENTS OF ENGINEERING AUTHORIAug 12, 2008 · N806FR · Airbus A318111 · Fuselage Miscellaneous StructureSDR F3LA200800553Floorbeam · corrodedDURING C-CHECK, INSP NOTED 3 OB NUT CLIP HOLES CORRODED ON FLOORBEAM Y1292 (L-2) AT FR 67. MAINT REMOVED AND REPLACED FLOORBEAM IAW SRM 51-42-11, PARAGRAPH 5. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. (S)Aug 12, 2008 · N806FR · Airbus A318111 · Fuselage Main, Floor BeamSDR F3LA200800550Floor Panel · gougedDURING C3 C-CHECK, INSPECTION NOTED THE FORWARD CARGO PIT RT AFT UPPER TRANSITION PANEL 132EG HAD A GOUGE. MAINTENANCE REPAIRED DAMAGED PANEL 132EG IAW THE REQUIREMENTS OF A319 SRM 53-02-00, PARAGRAPH 8C, FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPAug 11, 2008 · N806FR · Airbus A318111 · Fuselage Floor PanelSDR F3LA200800549Floor Panel · damagedDURING C3 C-CHECK, INSPECTION NOTED THE AFT CARGO PIT RT TRANSITION PANEL 162BF WAS DAMAGED. MAINTENANCE REPAIRED DAMAGED PANEL 162BF IAW THE REQUIREMENTS OF A319 SRM 53-02-00, PARAGRAPH 8C, FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUNAug 11, 2008 · N806FR · Airbus A318111 · Fuselage Floor PanelSDR F3LA200800548Floor Panel · damagedDURING C3 C-CHECK, INSPECTION NOTED THE FORWARD CARGO PIT LT TRANSITION PANEL 161CF WAS DAMAGED. MAINTENANCE REPAIRED DAMAGED PANEL 161CF IAW THE REQUIREMENTS OF A319 SRM 53-02-00, PARAGRAPH 8C, FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND Aug 11, 2008 · N806FR · Airbus A318111 · Fuselage Floor PanelSDR F3LA200800547Floor Panel · puncturedDURING C3 C-CHECK, INSPECTION NOTED THE FORWARD CARGO PIT FORWARD FLOOR PANEL 131CG HAS SEVERAL HOLES. MAINTENANCE REPAIRED DAMAGED PANEL 131CG IAW THE REQUIREMENTS OF A319 SRM 53-02-00, PARAGRAPH 8C, FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTEDAug 11, 2008 · N806FR · Airbus A318111 · Fuselage Floor PanelSDR F3LA200800546Floor Panel · puncturedDURING C3 C-CHECK, INSPECTION NOTED THE FORWARD CARGO PIT FORWARD FLOOR PANEL 131AF HAS SEVERAL HOLES. MAINTENANCE REPAIRED DAMAGED PANEL 131AF IAW THE REQUIREMENTS OF A319 SRM 53-02-00, PARAGRAPH 8C, FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTEAug 11, 2008 · N806FR · Airbus A318111 · Fuselage Floor PanelSDR F3LA200800551Floor Panel · damagedDURING C3 C-CHECK, INSPECTION NOTED THE AFT CARGO PIT LT TRANSITION PANEL 151HH WAS DAMAGED. MAINTENANCE REPAIRED DAMAGED PANEL 151HH IAW THE REQUIREMENTS OF A319 SRM 53-02-00, PARAGRAPSH 8C, FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUAug 11, 2008 · N806FR · Airbus A318111 · Fuselage Floor PanelSDR F3LA200800521Floor Panel · damagedLINE MAINT NOTED THE AFT CARGO COMPARTMENT TRANSITION PANEL 151FH WAS DAMAGED. MAINT REPAIRED TRANSITION PANEL 151FH IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)Jul 26, 2008 · N808FR · Airbus A318111 · Fuselage Floor PanelSDR F3LA200800522Floor Panel · damagedLINE MAINT NOTED THE AFT CARGO COMPARTMENT FLOOR PANEL 151DH WAS DAMAGED. MAINT REPAIRED FLOOR PANEL 151DH IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)Jul 26, 2008 · N808FR · Airbus A318111 · Fuselage Floor PanelSDR F3LA200800523Floor Panel · damagedLINE MAINT NOTED THE AFT CARGO COMPARTMENT FLOOR PANEL 151CH WAS DAMAGED. MAINT REPAIRED FLOOR PANEL 151CH IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)Jul 26, 2008 · N808FR · Airbus A318111 · Fuselage Floor PanelSDR F3LA200800519Support · crackedDURING SCHEDULED MAINT TASK CARD TC32711-02, INSP NOTED A CRACK ON THE FWD ANTI-ROTATION LUG. MAINT REMOVED AND REPLACED THE UPPER SUPPORT ASSEMBLY IAW THE REQUIREMENTS OF ENGINEERING AUTHORIZATION A8-32R-30496. UPON COMPLETION OF THE REPAIR IT WAS INSPECTEDJul 22, 2008 · N802FR · Airbus A318111 · Fuselage, Landing Gear Attach FittingsSDR F3LA200800507Floor Panel · puncturedLINE MAINTENANCE NOTED THE AFT CARGO PIT TRANSITION PANEL 151FG HAS PUNCTURE DAMAGE IN THREE PLACES ON UPPER SKIN. MAINTENANCE REPAIRED DAMAGE IN ACCORDANCE WITH A318 SRM 53-02-00, FIGURE 205.Jul 17, 2008 · N807FR · Airbus A318111 · Fuselage Floor PanelSDR F3LA200800506Floor Panel · puncturedLINE MAINTENANCE NOTED THE AFT CARGO PIT TRANSITION PANEL 151FH HAD PUNCTURE DAMAGE IN THREE PLACES ON THE UPPER SKIN. MAINTENANCE REPAIRED DAMAGE IN ACCORDANCE WITH A318 SRM 53-02-00, FIGURE 205.Jul 17, 2008 · N807FR · Airbus A318111 · Fuselage Floor PanelSDR F3LA200800441Girt Bar · out of adjustDURING CLIMB OUT THE L2 AND R2 DOOR DISARMED AT 8500 FT AND REARMED DURING DESCENT AT 10000 FT. MAINT ADJUSTED GIRT BAR FITTINGS ON THE L2 AND R2 DOORS AND OPS AND RIG CHECKED GOOD IAW AMM 52-11-00-820-001, AMM 25-62-44-400-006 AND AMM 05-53-00-780-003. UPON CJul 8, 2008 · N805FR · Airbus A318111 · Emergency EquipmentSDR F3LA200800423Floorbeam · corrodedDURING C-CHECK INSP NOTED FLOOR BEAM Y1292 HAS CORROSION AT NUTCLIP HOLE AT FRAME 68 OB SIDE JUST FWD OF GALLEY. MAINT BLENDED CORROSION AND OVERSIZED HOLE, INSTALLED FLANGE BUSHING TREATED PRIMED AND PAINTED IAW EA A8-53R-30435 AND SRM 51-75-12. UPON COMPLETIJul 7, 2008 · N805FR · Airbus A318111 · Fuselage Main, Floor BeamSDR F3LA200800422Floorbeam · corrodedDURING C-CHECK INSP NOTED FLOORBEAM Y1292 HAS CORROSION AT FWD OB NUTCLIP HOLE AT FRAME 66 JUST AFT OF LT LAVATORY. MAINT BLENDED CORROSION AND OVERSIZED HOLE, FABRICATED FLANGE BUSHING AND TREATED PRIMED AND PAINTED IAW EA A8-53R-30435 AND SRM 51-75-12. UPON Jul 7, 2008 · N805FR · Airbus A318111 · Fuselage Main, Floor BeamSDR F3LA200800421Shear Plate · corrodedDURING C-CHECK INSP NOTED CORROSION AROUND FAR RT NUTCLIP HOLE ON SHEAR PLATE ALONG FRAME 68 BETWEEN Y765 AND Y1292. MAINT REMOVED SHEAR CONNECTING PLATE, FABRICATED AND INSTALLED SHEAR CONNECTING PLATE IAW DRAWING D53670099 AND SRM 51-42-11. UPON COMPLETION OJul 7, 2008 · N805FR · Airbus A318111 · Fuselage Miscellaneous StructureSDR F3LA200800427Floorbeam · corrodedDURING C-CHECK INSP NOTED FLOORBEAM Y1292 LT HAS CORROSION AT FIRST, SECOND AND THIRD NUTCLIP HOLES. MAINT REMOVED AND REPLACED FLOORBEAM IAW SRM 51-72-00. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)Jul 7, 2008 · N805FR · Airbus A318111 · Fuselage Main, Floor BeamSDR F3LA200800426Shear Plate · corrodedDURING C-CHECK INSP, NOTED CORROSION AROUND FAR RT NUTCLIP HOLE ON SHEAR PLATE ALONG FRAME 68 BETWEEN Y765 AND Y1292. MAINT REMOVED, FABRICATED AND INSTALLED SERVICEABLE SHEAR PLATE AT FRAME 68 BETWEEN Y765 AND Y1292 IAW DRAWING O53670099, SRM 51-21-11, SRM 51Jul 7, 2008 · N805FR · Airbus A318111 · Fuselage Floor PanelSDR F3LA200800425Floor Panel · corrodedDURING C-CHECK INSP, FLOOR PANEL 262FF HAS CORROSION ON SURFACE. MAINT REMOVED AND REPLACED FLOOR PANEL 262FF IAW AMM 53-42-12-400-002. UPON COMPLETION OF THE REPAIR, INSPECTED AND FOUND ACCEPTABLE. (B)Jul 7, 2008 · N805FR · Airbus A318111 · Fuselage Floor PanelSDR F3LA200800424Floor Panel · corrodedDURING C-CHECK INSP NOTED FLOOR PANEL 261FF HAS CORROSION ON SURFACE. MAINT REMOVED AND REPLACED FLOOR PANEL 261FF IAW AMM 53-42-12-400-002. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)Jul 7, 2008 · N805FR · Airbus A318111 · Fuselage Floor PanelSDR F3LA200800419Plate · corrodedDURING C-CHECK INSP NOTED GIRT BAR BLANKING PLATE L2 AFT HAS CORROSION. MAINT REMOVED AND REPLACED CORRODED L2 AFT GIRT BAR BLANKING PLATES IAW WORK CARD C250001-03. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)Jul 3, 2008 · N805FR · Airbus A318111 · Fuselage Miscellaneous StructureSDR F3LA200800420Blanking Plate · corrodedDURING C-CHECK INSP, NOTED GIRT BAR BLANKING PLATE ON R2 DOOR AFT HAS CORROSION. MAINT REMOVED AND REPLACED R2 DOOR GIRT BAR BLANKING PLATES IAW WORK CARD C250001-03. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)Jul 3, 2008 · N805FR · Airbus A318111 · Fuselage Miscellaneous StructureSDR F3LA2009010800004Web · gougedDURING C-3 C-CHECK INSP, NOTED THAT THE LT NR 4 SPOILER ANTI-ROTATION LUG HAS A GOUGE. MX REPAIRED DAMAGED AREA IAW EA A8-57R-30431.Jul 2, 2008 · N805FR · Airbus A318111 · SpoilersSDR F3LA2009010800003Web · gougedDURING C-3 C-CHECK INSP, NOTED THAT THE RT NR 3 SPOILER ANTI-ROTATION FLAT HAS A GOUGE. MX REPAIRED DAMAGED AREA IAW EA A8-57R-30430.Jul 2, 2008 · N805FR · Airbus A318111 · SpoilersSDR F3LA200800414Panel · damagedREFERENCE NON ROUTINE C046424. DURING C-CHECK INSPECTION NOTED FWD CARGO PIT TRANSITION PANEL 132DG IS DAMAGED. MAINT REPAIRED FWD CARGO PIT TRANSITION PANEL 132DG IAW SRM 53-02-00 PARAGRAPH 8C FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUJul 1, 2008 · N805FR · Airbus A318111 · Fuselage Miscellaneous StructureSDR F3LA200800415Panel · damagedDURING C-CHECK INSP NOTED FWD CARGO PIT TRANSITION PANEL 131BF IS DAMAGED. MAINT REPAIRED FWD CARGO PIT TRANSITION PANEL 131BF IAW SRM 53-02-00 PARAGRAPH 8C, FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)Jul 1, 2008 · N805FR · Airbus A318111 · Fuselage Miscellaneous StructureSDR F3LA200800386Skin · damagedDURING WALK AROUND MAINT, NOTED LT FUSELAGE GOUGED AND DAMAGED FRAME 57 TO FRAME 58 AND STRINGER 30 LT TO STRINGER 31 LT. MAINT PERFORMED A PERMANENT REPAIR IAW SRM 53-00-11 FIGURE 203 AND E.A. A9-53R-30409. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED ANDJun 24, 2008 · N919FR · Airbus A318111 · Fuselage Main, Plate/SkinSDR F3LA200800382Lamp · burned outDURING A HEAVY MAINT CHECK INSP, NOTED ROWS 3 AND 11 AFT MOUNTED LAMP OF EMERGENCY LIGHT MOUNTED SEATS INOP. MAINT REMOVED AND REPLACED SEAT MOUNTED EMERGENCY LIGHT ASSEMBLY IAW AMM 33-51-19 PAGE BREAK 401. UPON COMPLETION OF THE MAINT IT WAS INSPECTED, FOUNDJun 23, 2008 · N810FR · Airbus A318111 · Emergency LightingSDR F3LA200800385Servo Control · inoperativeDURING TAXI OUT, THE FLIGHT CREW RECEIVED A NOSE WHEEL STEERING FAULT AND LOSS OF STEERING. MAINT REMOVED AND REPLACED NLG STEERING SERVO CONTROL VALVE IAW AMM 32-51-51 PAGE BREAK 401. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE AND OPJun 23, 2008 · N806FR · Airbus A318111 · Landing Gear Steering SystemSDR F3LA200800344Floor Panel · damagedDURING HEAVY SERVICE CHECK INSP, NOTED AFT CARGO COMPARTMENT FLOOR PANEL 151DH WAS DAMAGED. MAINT COMPLETED PERMANENT REPAIR ON PANEL 151DH IAW SRM 53-02-00. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A)Jun 17, 2008 · N809FR · Airbus A318111 · Fuselage Floor PanelSDR F3LA200800130Unknown · smokeDURING LANDING ROLL OUT, THE FLIGHT CREW REPORTED WHITE/GRAY SMOKE AND ACRID ODOR IN THE COCKPIT AND PASSENGER CABIN. MAINTENANCE PERFORMED IDLE LEAK CHECK OF BOTH ENGINES IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 71-00-00-710-006 AND PERFORMED A CHECK OF THMar 19, 2008 · N808FR · Airbus A318111 · Air Distribution SystemSDR F3LA200800077Cooling Fan · bindingDURING CRUISE, AT 35000, FLT CREW REPORTED LOUD NOISE AND VIBRATION FOLLOWED BY ACRID ODOR AND SMOKE IN COCKPIT. ECAM DISPLAYED BLOWER AND EXTRACTOR FAN FAULT. FLIGHT CREW DECLARED AN EMERGENCY, DIVERTED TO OKC AND PERFORMED AN UNEVENTFUL LANDING. MAINTENANMar 3, 2008 · N807FR · Airbus A318111 · Air Distribution FanSDR F3LA200800072Actuator · leakingDURING CLIMB, THROUGH 15000 FEET, THE FLIGHT CREW RECEIVED AN ECAM WARNING INDICATING THE GREEN SYSTEM HYDRAULIC QUANTITY WAS LOST. THE FLIGHT CREW PERFORMED AN AIR TURNBACK AND AFFECTED AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THEFeb 23, 2008 · N812FR · Airbus A318111 · Drag Control ActuatorSDR F3LA200800031Pressure Switch · inoperativeDURING C CHECK AND FUNCTIONAL TEST, THE ALTITUDE PRESSURE SWITCH FAILED ITS FUNCTIONAL TEST. MAINTENANCE REMOVED AND REPLACED THE ALTITUDE PRESSURE SWITCH IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 35-23-15 PB 401. FOLLOWING ITS INSTALLATION AND INSPECTION, Jan 23, 2008 · N804FR · Airbus A318111 · Cabin Pressure Control SystemSDR F3LA200800030Hinge Fitting · damagedDURING C CHECK INSPECTION, THE CENTER HINGE ANTI-ROTATION LUG FOR THE LEFT NUMBER 3 SPOILER WAS FOUND DAMAGED. MAINTENANCE REMOVED THE DAMAGED ASSEMBLY AND PERFORMED A "MAJOR REPAIR" IN ACCORDANCE WITH THE REQUIREMENTS OF EA A8-57R-12379. UPON COMPLETION OF Jan 23, 2008 · N804FR · Airbus A318111 · SpoilersSDR F3LA200800028Hinge Fitting · damagedDURING C CHECK INSPECTION, THE CENTER HINGE ANTI-ROTATION LUG FOR THE RIGHT NUMBER 3 SPOILER WAS FOUND DAMAGED. MAINTENANCE REMOVED THE DAMAGED ASSEMBLY AND PERFORMED A "MAJOR REPAIR" IN ACCORDANCE WITH THE REQUIREMENTS OF EA A8-57R-12379. UPON COMPLETION OFJan 23, 2008 · N804FR · Airbus A318111 · SpoilersSDR F3LA200800026Hinge Fitting · damagedDURING C CHECK INSPECTION, THE CENTER HINGE ANTI-ROTATION LUG FOR THE RIGHT NUMBER 4 SPOILER ACTUATOR BOLT WAS FOUND DAMAGED. MAINTENANCE REMOVED THE DAMAGED ASSEMBLY AND PERFORMED A "MAJOR REPAIR" IN ACCORDANCE WITH THE REQUIREMENTS OF EA A8-57R-12379. UPONJan 23, 2008 · N804FR · Airbus A318111 · SpoilersSDR F3LA200800029Hinge Bracket · damagedDURING C CHECK INSPECTION, THE CENTER HINGE ANTI-ROTATION BRACKET FOR THE LEFT NUMBER 2 SPOILER WAS FOUND DAMAGED. MAINTENANCE REMOVED THE DAMAGED ASSEMBLY AND PERFORMED A "MAJOR REPAIR" IN ACCORDANCE WITH THE REQUIREMENTS OF EA A8-57R-12381. UPON COMPLETIONJan 23, 2008 · N804FR · Airbus A318111 · SpoilersSDR F3LA200800027Hinge Fitting · damagedDURING C CHECK INSPECTION, THE CENTER HINGE ANTI-ROTATION LUG FOR THE LEFT NUMBER 4 SPOILER WAS FOUND DAMAGED. MAINTENANCE REMOVED THE DAMAGED ASSEMBLY AND PERFORMED A "MAJOR REPAIR" ON ACCORDANCE WITH THE REQUIREMENTS OF EA A8-57R-12379. UPON COMPLETION OF Jan 23, 2008 · N804FR · Airbus A318111 · SpoilersSDR F3LA200800025Pressure Switch · failedDURING C CHECK INSPECTION AND FUNCTIONAL TEST, THE CABIN PRESSURE SWITCH (16WR) FAILED TO DROP THE OXYGEN MASKS. MAINTENANCE REMOVED AND REPLACED THE CABIN PRESSURE SWITCH (16WR) IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 35-23-15-400-001. FOLLOWING ITS INSTJan 21, 2008 · N804FR · Airbus A318111 · Cabin Pressure Control SystemSDR F3LA200800024Release Cable · inoperativeDURING C CHECK INSPECTION AND FUNCTIONAL TESTING, THE RIGHT, OVERWING, EMERGENCY ESCAPE HATCH RELEASE CABLE WAS BINDING AND WOULD NOT RETRACT. MAINTENANCE REMOVED AND REPLACED THE CABLE IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 25-62-43-400-001. UPON REPLACJan 15, 2008 · N804FR · Airbus A318111 · Emergency ExitsSDR F3LA200800023Release Cable · inoperativeDURING C CHECK INSPECTION AND FUNCTIONAL TESTING, THE LEFT, OVERWING, EMERGENCY ESCAPE HATCH RELEASE CABLE WAS BINDING AND WOULD NOT RETRACT. MAINTENANCE REMOVED AND REPLACED THE CABLE IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 25-62-43-400-001. UPON REPLACEJan 15, 2008 · N804FR · Airbus A318111 · Emergency ExitsSDR F3LA200800022Floor Panel · corrodedDURING C CHECK INSPECTION, CARGO FLOOR PANEL 261FF, LOCATED BETWEEN FRAMES 66 AND 68, WAS FOUND TO HAVE CORROSION ON ITS LOWER SURFACE. MAINTENANCE REMOVED AND REPLACED THE FLOOR PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 53-42-12 PB 401. FOLLOWING THEJan 15, 2008 · N804FR · Airbus A318111 · Fuselage Floor PanelSDR F3LA200800018Floor Panel · corrodedDURING C CHECK INSPECTION, CARGO FLOOR PANEL 262FF, LOCATED BETWEEN FRAMES 66 AND 68, WAS FOUND TO HAVE CORROSION ON ITS LOWER SURFACE. MAINTENANCE REMOVED AND REPLACED THE FLOOR PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 53-42-12 PB 401. FOLLOWING THEJan 15, 2008 · N804FR · Airbus A318111 · Fuselage Floor Panel
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