Cameron Balloons U S A-300

Service difficulty reports · 3,457

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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 = 'A300'
  ORDER BY difficulty_date DESC"

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SDR 2026FA0000414Seal · wrong partDURING THE DISASSEMBLY OF RR XWB-97K EGB EG0527, THE PRESENCE OF A DYNAMIC SEAL P/N NOT LISTED IN THE APPROVED DATA FOR XWB 97K AT POSITION 14-320 WAS OBSERVED. THE MOUNTED P/N IS: 90C24604 "JOINT ASSEMBLY, ROTATING EE361628-1". THE P/NS SPECIFIED IN RR XWBMay 20, 2026 · Airbus A300* · Turbine Engine Accessory DriveSDR 6HUY202605180001Slide · fodON 6 MAY 2026, ESCAPE SLIDE ASSEMBLY P/N 62292-108 WITH S/N C0975 WAS RECEIVED FOR MAINTENANCE FROM AIR FRANCE UNDER CUSTOMER REPAIR ORDER NO. 6D224308HKR. THE UNIT WAS BOOKED UNDER INTERNAL WORK ORDER WHU2603936. DURING THE INSPECTION AND TESTING PHASE OF THMay 6, 2026 · Airbus A300* · Escape SlideSDR 2025F00091Gearbox · misoverhauledWHILE DISASSEMBLING RR TRENTXWB EGB P/N 90500-02 S/N EG1048, 2 SCREWS (AS3237-14) WERE FOUND AMONG THE 4 TGB BEARING SUPPORT FIXTURES. THESE SCREWS ARE NOT INCLUDED IN THE EGB BOM. THESE SCREWS SHOULD BE AS3237-12. THIS COMPONENT WAS MOUNTED ON ENGINE RR TRENApr 11, 2025 · Airbus A300* · Turbine Engine Accessory DriveSDR FDEA202405050579Static Wick · corrodedRH WING OUTER FLAP OUTBOARD AREA 1EA STATIC DISCHARGER BASE CORRODED COMPLIED WITH EA 6-5750-T0379031 P1 REPAIRED THE RH WING O/B FLAP OUTER T/E CORRODED UPPER SKIN. TITLE: WINGS - FLIGHT SURFACES - RH O/B FLAP, OUTER TRAILING EDGE, UPPER SKIN CORROSION UNMay 5, 2024 · N670FE · Airbus A300* · Pitot/Static SystemSDR FDEA202405050578None · noneEXISTING REPAIR ON FUSELAGE FRAME FR20A S37R-S42R REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON FUSELAGE FRAME FR20A S37R-S42R WAS EVALUATED AND FOUND NOT IN CONFORMITY WITH A300-600F SRM53-13-13-201 FIG.201. COMPLIED WITH EA 6-5310-54559 B P2May 5, 2024 · N670FE · Airbus A300* · Standard Practices/StructuresSDR FDEA202404260296None · noneEXISTING REPAIR FOUND ON M/D CROSSBEAM AT FR29, BTW Y1456 TO -Y1456 COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707, INSPECTION OF EXISTIApr 26, 2024 · N661FE · Airbus A300* · Standard Practices/StructuresSDR FDEA202401050039Indicator · failedENGINE FIRE AND MULTIPLE SYSTEMS WARNINGS AND CAUTIONS AFTER ROTATION IN LIGHT RAIN. ENGINE TEMPERATURE INDICATIONS WERE NORMAL AUTOPILOT AUTOMATION WAS NOT AVAILABLE. EMERGENCY DECLARED. INDICATOR WERE ALL REPLACED AND ALL OPS CHECKS BEING SATISFACTORY. Jan 5, 2024 · N721FD · Airbus A300* · Fire DetectionSDR FDEA202401040036Crossbeam · crackedMAIN DECK CARGO COMPARTMENT - CRACK FOUND ON CROSSBEAM AT FR64 BETWEEN -Y1456 AND -Y1959 JUST BELOW THE EXISTING REPAIR COMPLIED WITH EA 6-5310-T0377782 P1 REPAIRED THE MAIN DECK CARGO CRACKED CROSSBEAM AT FR64 BETWEEN -Y1456 AND -Y1959. THIS IS CAT B REPJan 4, 2024 · N659FE · Airbus A300* · Fuselage Main, StructureSDR FDEA202401030012Unknown · unknownLH WING CENTER FLAP RIB UPR FLANGE FOUND CRACKS AT RIB17 BETWEEN STGR2.8 AND REAR SPARJan 3, 2024 · N659FE · Airbus A300* · Trailing Edge FlapsSDR FDEA202401020007Coalescer Bag · failedDURING DESCENT WHEN THROTTLES REDUCED TO IDLE, STRONG BURST OF SMOKE SMELL AND SLIGHT HAZE IN THE COCKPIT. IMMEDIATELY CLEARED AND DID NOT REOCCUR. REMOVED AND REPLACED BOTH COALESCER BAGS IAW A300 AMM 21-51-16-03. ITEM CLOSED. GROUND RUN CARRIED OUT ASJan 2, 2024 · N653FE · Airbus A300* · Humidity Control SystemSDR FDEA202312211950Engine · leakingENG 1 OIL LO PRESS. PRESSURE INDICATED NORMAL ON ENG PAGE AND GAUGE. HOWEVER, WE NOTICED OIL QUANTITY DECREASING. DECREASING APPROX 2 QUARTS PER 10 MINUTES. AFTER LANDING BACK AT KMEM WE HAD 5 QUARTS REMAINING. 8 QUARTS AFTER ENG SHUTDOWN. ADDED 12 QTS OIDec 21, 2023 · N682FE · Airbus A300* · Engine Oil Indicating SystemSDR FDEA202312161943Unknown · unknownR1 SLIDE INDICATION NOT SHOWING ON ECAM WHEN DOOR IS CLOSED AND ARMED, ALL OTHER DOOR CLOSED AND LOCKED INDICATIONS ARE FINE. PERFORMED T/S FOUND NO R1" SLIDE" INDICATION ON ECAM. PERFORMED TEST OF AUTOMOMOUS STBY PWR UNIT AND R1 "SLIDE" INDICATION RETURDec 16, 2023 · N682FE · Airbus A300* · Escape SlideSDR FDEA202312141938Power Supply · failed"EMERG TEST" P/BSW (25WL) DOES NOT ILLUMINATE & EMERGENCY LIGHTS REMAIN ILLUMINATED WHEN TEST CYCLE IS ENERGIZED. FACT 14DEC23 14:10 MSN U AMM: 33-51-14-04-0 RED LED FAULT LIGHT ILLUMINATED ON EPSU REMOVED AND REPLACED POWER SUPPLY UNIT (29WL) IAW Dec 14, 2023 · N650FE · Airbus A300* · Emergency LightingSDR FDEA202312061926Lens · inoperativeAPU FIRE WARNING LIGHT INDICATOR AT NOSE GEAR STEERING BYPASS IS MISSING. RELEASED FOR SERVICE PER MEL : 26-XX-XX CAT C EXP : 16DEC23 APU GROUND AUTO FIRE EXTINGUISHING SYSTEM - INOP. APU OPERATION MUST BE MONITORED FROM COCKPIT WHILE APU IS RUNNING." Dec 6, 2023 · N745FD · Airbus A300* · Central WarningSDR FDEA202312051925Switch · inoperativeFOUND DOOR INTERIOR EMERGENCY EXIT LIGHTS ALWAYS ILLUMINATED. NOTICED RED EMERGENCY LIGHT SWITCH FWD OF L1 DOOR IS STUCK INSIDE. RELEASED FOR SERVICE PER MEL : 33-XX-XX-XX CAT: C EXP: 15DEC23 "MEL 33-XX-XX-XX: COURIER COMPARTMENT INTERIOR EMERGENCY LIGHTSDec 5, 2023 · N671FE · Airbus A300* · Emergency LightingSDR FDEA202311281918Rib · damagedL/H MLG RIB 5 FWD LUG HAS MINOR IMPACT DAMAGE ON FWD AND AFT SIDES. REPAIRED PER E.A. 6-5710-T0377239 PT 1.Nov 28, 2023 · N659FE · Airbus A300* · Fuselage Structure (General)SDR FDEA202311261927Pin · looseTHERE IS A RED FLAG PROTRUDING FROM UNDER THE R1 DOOR SLIDE. 26NOV23 - REMOVED RED TAG LABELED - REMOVE BEFOREINSTALLATION - ON R1 DOOR SLIDE REF ABOVE AMM REFERENCE. A/C OK FOR SERVICE. PER MOC PERF INSP / CHECK OF R1 DOOR SLIDE. AMM: 25-61-20-06-1 PERNov 26, 2023 · N658FE · Airbus A300* · Equipment/Furnishings WiringSDR FDEA202311251898Elevator · unknownAIRCRAFT REPAIR ASSESSMENT : EXISTING COMPOSITE REPAIR FOUND ON LH ELEVATOR UPR SKIN AT ER5-14", T/E-6" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFRNov 25, 2023 · N660FE · Airbus A300* · Elevator StructureSDR FDEA202311201956Header · crackedAFT CGO DOOR UPPER L/H SIDE CORNER FOUND PATCH CRACKED. REPLACED THE CRACK PART WITH NEW PART I.A.W A300-600F SRM 51-72-10-001 PAGE 2.Nov 20, 2023 · N660FE · Airbus A300* · Fuselage Miscellaneous StructureSDR FDEA202311201930Dummy Rail · damagedM/D CARGO COMPARTMENT FOUND NO.1 DUMMY SEAT TRACK (NO.1) CROWN BROKEN AT FR54.1 PLUS 4",RBL0 POS. ACCOMPLISHED THE DUMMY SEAT TRACK REPLACEMENT I.A.W A300-600F SRM 51-72-10-001, PAGE.2 & 51-40-21-001, PARA.7, PAGE.24-50Nov 20, 2023 · N660FE · Airbus A300* · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202311161866Skin · unknownEXISTING DOUBLER REPAIR FOUND ON FUSELAGE SKIN BETWEEN STRINGER 6~8L, FRAME 84~85,EVALUATE TO DETERMINE WHETHER IT IS MAJOR OR MINOR AND WHETHER ACCOMPLISHED PER APPROVED DATA COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES-REPAINov 16, 2023 · N660FE · Airbus A300* · Standard Practices/StructuresSDR FDEA202311151966Rib · corrodedR5 SPLR JACK RIB BOLT BORE CORRODED AT LOACTION NO.1, NO.3 AND NO.4 ACCOMPLISHED THE REINFORCING REPAIR AT RH #5 SPOILER I/B & O/B JACK RIB I.A.W FEDEX EA NO:T6-5740-T0377191 P1,SEQ NO:760,TITLE: WINGS-ATTACH FITTINGS-RH WING #5 SPOILER JACK RIB AT STA ABXNov 15, 2023 · N660FE · Airbus A300* · Wing, Rib/BulkheadSDR FDEA202311151963Rib · corrodedR7 SPLR JACK RIB BOLT BORE CORRODED AT LOACTION NO.1 ACCOMPLISHED THE REINFORCING REPAIR AT RH #7 SPOILER O/B JACK RIB I.A.W FEDEX EA NO:T6-5740-T0377209 P1,SEQ NO:763,TITLE: WINGS-ATTACH FITTINGS-RH WING #7 SPOILER JACK RIB AT STA SP2X 40.425-BEAM ATTACHMNov 15, 2023 · N660FE · Airbus A300* · Wing, Rib/BulkheadSDR FDEA202311151962Rib · corrodedR4 SPLR JACK RIB BOLT BORES CORRODED AT LOCATION NO.1 AND NO.2 ACCOMPLISHED THE REINFORCING REPAIR AT RH #4 SPOILER I/B & O/B JACK RIB I.A.W FEDEX EA NO:T6-5740-T0377195 P1,SEQ NO:766,TITLE: WINGS-ATTACH FITTINGS-RH WING #4 SPOILER JACK RIB AT STA ABX 103.Nov 15, 2023 · N660FE · Airbus A300* · Wing, Rib/BulkheadSDR FDEA202311151961Rib · corrodedR3 SPLR JACK RIB BOLT BORES CORRDED AT LOCATION NO.2 AND NO.3 ACCOMPLISHED THE REINFORCING REPAIR AT RH #3 SPOILER I/B & O/B JACK RIB I.A.W FEDEX EA NO:T6-5740-T0377189 P1,SEQ NO:765,TITLE: WINGS-ATTACH FITTINGS-RH WING #3 SPOILER JACK RIB AT STA ABX 31.67Nov 15, 2023 · N660FE · Airbus A300* · Wing, Rib/BulkheadSDR FDEA202311151960Rib · corrodedR6 SPLR JACK RIB BOLT BORE CORRODED AT LOCATION NO.1. ACCOMPLISHED THE REINFORCING REPAIR AT RH #6 SPOILER O/B JACK RIB I.A.W FEDEX EA NO: T6-5740-T0377208 P1, SEQ NO:761, TITLE: WINGS-ATTACH FITTINGS-RH WING #6 SPOILER JACK RIB AT STA SP1X 40.425 - BEAM ANov 15, 2023 · N660FE · Airbus A300* · Wing, Rib/BulkheadSDR FDEA202311141965Rib · corrodedLH WING SPOILER NO.5 I/B JACK RIB BOLT HOLES CORRODED AT BEAM ATTACHMENT BOLT LOCATION #1 & #3 ACCOMPLISHED THE REINFORCING REPAIR AT LH #5 SPOILER I/B JACK RIB I.A.W FEDEX EA NO:T6- 5740-T0377193 P1,SEQ NO:764,TITLE: WINGS-ATTACH FITTINGS-LH WING #5 SPOILENov 14, 2023 · N660FE · Airbus A300* · Wing, Rib/BulkheadSDR FDEA202311141964Rib · corrodedLH WING SPOILER NO.5 O/B JACK RIB BOLT HOLES CORRODED AT BEAM ATTACHMENT BOLT LOCATION #2 & #4 ACCOMPLISHED THE REINFORCING REPAIR AT LH #5 SPOILER O/B JACK RIB I.A.W FEDEX EA NO:T6-5740-T0377193 P1,SEQ NO:764,TITLE: WINGS-ATTACH FITTINGS-LH WING #5 SPOILENov 14, 2023 · N660FE · Airbus A300* · Wing, Rib/BulkheadSDR FDEA202311141959Rib · corrodedLH WING SPOILER NO.3 O/B JACK RIB BOLT HOLE CORRODED AT BEAM ATTACHMENT BOLT LOCATION #2 ACCOMPLISHED THE REINFORCING REPAIR AT LH #3 SPOILER O/B JACK RIB I.A.W FEDEX EA NO:T6-5740-T0377187A P1,SEQ NO:762,TITLE: WINGS-ATTACH FITTINGS-LH WING #3 SPOILER JACNov 14, 2023 · N660FE · Airbus A300* · Wing, Rib/BulkheadSDR FDEA202311131953Stringer Splice · corrodedAVIONICS COMPT BILGES GOT A STRINGER CORRODED AT FR19-2", STR-52L REPLACED THE SPLICE WITH NEW ONE I.A.W A300-600F SRM 51-72-10-001, PAGE.2 & 51-40-21-001, PARA.6, PAGE.7B~23Nov 13, 2023 · N660FE · Airbus A300* · Fuselage Main, Longeron/StringerSDR FDEA202311131895Skin · dentedFUSELAGE TAIL SKIN FOUND 1EA BULGED AT FR93 PLUS 5.3",S-16R PLUS 3.5",POS. CUT OUT DAMAGE AREA,FABRICATED THE REPAIR DOUBLER,WET INSTALLED REPAIR DOUBLER WITH FASTENERS. I.A.W A300-600F SRM 53-19-12-201,PARA.6B,FIG202,PAGE213~PAGE218. "MAJOR REPAIR"Nov 13, 2023 · N660FE · Airbus A300* · Fuselage Main, Plate/SkinSDR FDEA202311131894Skin · dentedFUSELAGE TAIL SKIN FOUND 5EA BULGEDS AT FR92 PLUS 4.4", S-16R PLUS 1.8", FR92 PLUS 3", S- 16R PLUS 2.4", FR92 PLUS 5.5", S-17R PLUS 0.9", FR92 PLUS 5.4", S-17R PLUS 2.5", FR92 PLUS 2.8", S-17R PLUS 4.7" POS. CUT OUT DAMAGE AREA, FABEICATED THE REPAIR DOUBLNov 13, 2023 · N660FE · Airbus A300* · Fuselage Main, Plate/SkinSDR FDEA202311120003Retainer · corrodedFR40 BULKHEAD T/E LWR SURFACE RETAINER CORRODED. ACCOMPLISHED THE DOUBLER REPAIR TO THE DAMAGE AREA I.A.W FEDEX EA NO:T6-5310- T0377351 P1, SEQ NO:774,TITLE:FUSELAGE - MAINFRAME - PRESSURE FLOOR PANEL REPAIR AT FR40 BETWEEN Y953 AND -Y1456 DUE TO HEAVY EXFONov 12, 2023 · N660FE · Airbus A300* · Fuselage Structure (General)SDR FDEA202311121897Slat · gougedR1 SLAT CHAFING AT RIB20 PLUS 3", T/E -13". ACCOMPLISHED THE BONDED REPAIR WITH SKIN FILLER PIECE AND REPAIR PATCH I.A.W FEDEX EA NO:T6-5750-T0377084 P1, SEQ NO:752, TITLE:WING-FLIGHT SURFACES-RH #1 SLAT-GOUGE DAMAGE FOUND ON TAIL SECTION OUTBOARD LOWER SKNov 12, 2023 · N660FE · Airbus A300* · Leading Edge DevicesSDR FDEA202311100008Slat · damagedLH WING #1 SLAT "D" NOSE SKIN EXTERNAL SURFACE FOUND SLIGHT CREASED AT JACK RIB 1 LOWER SECTION ACCOMPLISHED THE EXTERNAL DOUBLER REPAIR AT JACK RIB 1 I.A.W FEDEX EA NO:T6-5750- T0377059 P1, SEQ NO:775, TITLE:WING - FLIGHT SURFACES - LH #1 SLAT - 02EA CREASNov 10, 2023 · N660FE · Airbus A300* · Leading Edge DevicesSDR FDEA202311100002Slat · damagedLH WING #1 SLAT "D" NOSE SKIN EXTERNAL SURFACE FOUND SLIGHT CREASED AT JACK RIB 1 LOWER SECTION ACCOMPLISHED THE EXTERNAL DOUBLER REPAIR AT JACK RIB 1 IAW FEDEX EA T6-5750- T0377059 P1, SEQ NO:775, TITLE:WING - FLIGHT SURFACES - LH #1 SLAT - 02EA CREASE LINNov 10, 2023 · N660FE · Airbus A300* · Leading Edge DevicesSDR FDEA202311100001Slat · damagedLH WING #1 SLAT "D" NOSE SKIN EXTERNAL SURFACE FOUND CREASED AT TRACK RIB 1 LWR SECTION ACCOMPLISHED THE FLUSH REPAIR AT TRACK RIB 1 I.A.W FEDEX EA NO:T6-5750-T0377059 P1, SEQ NO:775, TITLE:WING - FLIGHT SURFACES - LH #1 SLAT - 02EA CREASE LINES FOUND ON Nov 10, 2023 · N660FE · Airbus A300* · Leading Edge DevicesSDR FDEA202311101946Slat · damagedR3 SLAT LWR SURFACE PROTUDER AT RIB37-3", T/E-6.5". ACCOMPLISHED THE COLD WORK TO THE PROTUDED LWR SKIN I.A.W FEDEX EA NO:T6-5750- T0377056 P1, SEQ NO:768, TITLE:WING-FLIGHT SURFACES-RH WING-#3 SLAT UPPER SKIN PUNCTURE BETWEEN RIB36 AND 37 "MAJOR REPAIR"Nov 10, 2023 · N660FE · Airbus A300* · Leading Edge DevicesSDR FDEA202311101945Slat · damagedR3 SLAT UPPER SURFACE PUNTURED AT RIB37-3", T/E-6.5" CUT OUT THE DAMAGE AREA AND INSTALLED THE EXTERNAL PATCH I.A.W FEDEX EA NO:T6-5750- T0377056 P1, SEQ NO:768, TITLE:WING-FLIGHT SURFACES-RH WING-#3 SLAT UPPER SKIN PUNCTURE BETWEEN RIB36 AND 37 "MAJOR REPNov 10, 2023 · N660FE · Airbus A300* · Leading Edge DevicesSDR FDEA202311101935Flap · cracked8EA CRACKS (MAX 27MM) WERE FOUND AT LH WING CENTER FLAP RIB12 FWD, 15 FWD, 18 AFT, 27 FWD, 27 AFT AND 25 AFT(3EA) AREA OF TOP SURFACE RIB FLANGE ACCOMPLISHED THE RIB FLANGE REPAIRS AND EXTERNAL DOUBLER REPAIRS I.A.W FEDEX EA NO:T6-5750-T0377102 P1, SEQ NO:Nov 10, 2023 · N660FE · Airbus A300* · Trailing Edge FlapsSDR FDEA202311081879Fitting · crackedFLOOR CROSSBEAM 10 PICK-UP FITTING CRACK AT Y-953 POSITION REMOVED CRACK PICK-UP FITTING,THEN INSTALLED NEW ONE WITH FASTENERS I.A.W A300-600F SRM 51-72-10-001,PAGE 2 & 51-40-21-001, PARA.6,PAGE 7B~23Nov 8, 2023 · N660FE · Airbus A300* · Fuselage Main, StructureSDR FDEA202311081878Angle · crackedFLOOR CROSSBEAM 10 ANGLE FITTING CRACK AT Y-953 POSITION REMOVED CRACK ANGLE FITTING,THEN INSTALLED NEW ONE WITH FASTENERS I.A.W A300-600F SRM 51-72-10-001,PAGE 2 & 51-40-21-001, PARA.6,PAGE 7B~23Nov 8, 2023 · N660FE · Airbus A300* · Fuselage Miscellaneous StructureSDR FDEA202311081877Strap · crackedFUSELAGE INNER S-39R PLATE WEB FOUND STRAP CRACK BETWEEN FR86 & FR87 AREA CRACKED STRAP REPLACED NEW PART,INSTALLED WITH RIVETS I.A.W A300-600F SRM 51-72-10- 001,PAGE 2 AND 51-40-21-001,PARA 6,PAGE 7B-PAGE 23Nov 8, 2023 · N660FE · Airbus A300* · Fuselage Miscellaneous StructureSDR FDEA202311071851Flap · unknownAIRCRAFT REPAIR ASSESSMENT : EXISTING DOUBLER REPAIR FOUND ON RH O/B FLAP UPR SKIN AT RIB 26A,T/E-2" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 12Nov 7, 2023 · N660FE · Airbus A300* · Trailing Edge FlapsSDR FDEA202311071840Unknown · unknownPDIS 749 05-50 7037 07NOV23 MEM MULTIPLE BIRD STRIKES AT LIFTOFF. ***EMERGENCY DECLARED**** FACT 07NOV23 19:05 MEM AMM: 05-51-14-00 PERFORMED BIRD STRIKE INSPECTION REF. AMM 05-51-14-00 ,CLEANED BLOOD STAIN ON NOSE RADOME AND BOTH ENGINES, Nov 7, 2023 · N749FD · Airbus A300* · Standard Practices/StructuresSDR FDEA202311051827Actuator · inoperativePDIS 683 32-20 2696 03NOV23 CAN FACT U L/G DOOR NOT CLOSED ECAM AFTER GEAR RETRACTION. AMBER LIGHTS ILLUMINATED ON BOTH GEAR INDICATION PANELS. COMPLIED WITH QRH. DISCUSSED WITH GOC & MOC. WHEN GEAR WAS EXTENDED, THE AMBER DOOR LIGHTS REMAINov 5, 2023 · N683FE · Airbus A300* · Nose/Tail Landing GearSDR FDEA202311021823Hinge · delaminatedLH WING #5 SPOILER CENTER O/B HINGE LOWER SURFACE (17MM*12MM, DEPTH: 1.7MM) AND O/B SIDE (30MM*10MM, DEPTH: 1.1MM) FOUND DELAMINATION REPAIRED LH WING #5 SPOILER CENTER O/B HINGE O/B SIDE DELAMINATION PER SB A300-57-6082 R03 FIGURE 2 SHEET 2&4 AND FIGURE 5Nov 2, 2023 · N688FE · Airbus A300* · SpoilersSDR FDEA202311021822Hinge · delaminatedRH WING #5 SPOILER CENTER O/B HINGE LOWER SURFACE (25MM*15MM, DEPTH: 2.1MM) & O/B SIDE (20MM*15MM, DEPTH: 1.4MM) AND CENTER I/B HINGE O/B SIDE (20MM*15MM, DEPTH: 1.07MM) FOUND DELAMINATION RH WING #5 SPOILER CENTER O/B HINGE LOWER SURFACE DELAMINATION WAS Nov 2, 2023 · N688FE · Airbus A300* · SpoilersSDR FDEA202311021821Hinge · delaminatedRH WING #3 SPOILER CENTER I/B HINGE O/B SIDE FOUND DELAMINATION (15MM*15MM, DEPTH: 1.22MM) REPAIRED RH WING #3 SPOILER CENTER I/B HINGE O/B SIDE DELAMINATION PER SB A300-57-6082 R03 FIGURE 2 SHEET 2&4 AND FIGURE 5 & EA 6-5750-T0376848 P1. MAJOR REPAIR INov 2, 2023 · N688FE · Airbus A300* · SpoilersSDR FDEA202310281808Slat · unknownEXISTING REPAIR ON RH WING #1 SLAT END RIB 2A, FROM I/B EDGE ABOUT 7" REQUIRES EVALUATION FOR CONFORMITY COMPLIED WITH EA 6-5750-T0376898 A P1. REPAIRED THE RH WING #1 SLAT EXISTING REPAIR AT INBOARD EDGE CLOSE TO RIB 2A. THIS IS CAT A REPAIR AND THIS REPOct 28, 2023 · N688FE · Airbus A300* · Leading Edge Devices
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