N660FE

Service difficulty reports · 227

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
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 n_number = 'N660FE' AND registry_match = 'registration'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR FDEA202605310657Door · crackedMAIN DECK CARGO DOOR UPR EDGE AT PT1 BETWEEN FR22 AND FR25 FOUND CRACK SIGNAL ON 6EA FASTENER HOLES. REPAIRED THE CRACKED FASTENER HOLES AT MAIN DECK CARGO DOOR UPR EDGE AT PT1 BETWEEN FR22 AND FR25 PER EA 6-5230-T0387491 P1. CRACKED HOLES ON MAIN DECK CARMay 31, 2026 · N660FE · Airbus A300F4605R · Cargo/Baggage DoorsSDR FDEA202605290658Frame · crackedRH CENTER BOX REAR SPAR FR47 BOTTOM PANEL "D" HOLE FOUND CRACKED SIGNAL. REPAIRED THE "D" HOLE ON RH CENTER WING BOX REAR SPAR FR47 BOTTOM PANEL PER EA 6- 5710-T0387476 P1. EA TITLE: WINGS - BASIC WING STRUCTURE - CRACK HOLE D AT FR47 RHS DURING SB57-6086 May 29, 2026 · N660FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA202605280664Skin · crackedRH WING INNER FLAP TOP SKIN FOUND CARCKED BTW RIB16 AND RIB17, STGR 2.1 AND STGR 2.2. REPAIRED THE CRACKED SKIN AT RH WING INNER FLAP BTW RIB16 AND RIB17, STGR 2.1 AND STGR 2.2 PER SRM57-50-00-201 PARA.4E FIG.205. RSC TRACKING EA 6-5750-T0387591 WAS RAISEMay 28, 2026 · N660FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA202605230659Floor Support · corrodedMAIN DECK - FWD COURIER AREA FR11-FR14 Y1456 LONGITUDINAL FLOOR SUPPORT CORRODEDMay 23, 2026 · N660FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202605230649Web · crackedMDC - UNDER FLOOR WEB CRACKED AT FR47 Y-953 - Y-1456. REPAIRED THE CRACKED WEB ON MDC - UNDER FLOOR AT FR47 Y-953 - Y-1456 PER A300-600F SRM53-15-15-201 FIG.201. THIS IS A CATEGORY B REPAIR AND IT MUST BE INSPECTED AT DEFINED INTERVAL PER A300-600F SRI53-1May 23, 2026 · N660FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202605230636Web · crackedMDC - UNDER FLOOR WEB CRACKED AT FR47 Y0 - Y-450. REPAIRED THE CRACKED WEB ON MDC - UNDER FLOOR AT FR47 Y0 - Y-450 PER A300-600F SRM53- 15-15-201 FIG.201. THIS IS A CATEGORY B REPAIR AND IT MUST BE INSPECTED AT DEFINED INTERVAL PER A300-600F SRI53-15-15-2-May 23, 2026 · N660FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202605220635Skin · delaminatedRH WING NR 5 SPOILER CENTER HINGE ARM INBD SIDE ARM OUTBD SURFACE DELAMINATED. 38MM*13MM*0.98MM. COMPLIED WITH EA 6-5750-T0387449 P1 REPAIRED THE DELAMINATION ON RT WING NR 5 SPOILER CENTER HINGE ARM INBD SIDE ARM OUTBD SURFACE. EA TITLE: WING - FLIGHT SUMay 22, 2026 · N660FE · Airbus A300F4605R · SpoilersSDR FDEA202605210634Door Frame · crackedRH PAX DOOR FRAME SEGMENT AT FR14C FOUND 2EA CRACKS. REPLACED THE CRACKED SEGMENT ON RH PAX DOOR FRAME AT FR14C PER A300-600F SRM51- 40-21 AND DWG: F52181299(ISSUE: G). RSC TRACKING EA: 6-5210-T0387549 RAISED AND ACCOMPLISHED. TITLE: DOORS - PASSENGER/CREWMay 21, 2026 · N660FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA202605190780Rib · crackedLH WING CENTER FLAP RIB UPPER FLANGE FOUND 1EA CRACK AT RIB26 BETWEEN STGR2.7 AND STGR2.8 COMPLIED WITH EA 6-5750-T0377102 A P2 PERFORMED HFEC INSPECTION TO CONFIRM THE CRACK IN LH WING CENTER FLAP RIB26 UPR FLANGE BETWEEN STGR2.7 AND STGR2.8 AND REMOVEDMay 19, 2026 · N660FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA202605190633Rib · crackedLH WING CENTER FLAP RIB UPPER FLANGE FOUND 2EA CRACKS AT RIB13 BETWEEN STGR2.6 AND STGR2.7 & RIB15 BETWEEN STGR2.7 AND STGR2.8. COMPLIED WITH EA 6-5750-T0377102 A P2 TO REPAIR THE LH WING CENTER FLAP RIB UPPER FLANGE 2EA CRACKS AT RIB3 BETWEEN REAR SPAR AMay 19, 2026 · N660FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA202605190632Rib · crackedLH WING CENTER FLAP RIB UPPER FLANGE FOUND 2EA CRACKS AT RIB11 BETWEEN REAR SPAR AND STGR2.8 & BETWEEN STGR2.7 AND STGR2.8. COMPLIED WITH EA 6-5750-T0377102 A P2 TO REPAIR THE LH WING CENTER FLAP RIB UPPER FLANGE 2EA CRACKS AT RIB11 BETWEEN REAR SPAR AND May 19, 2026 · N660FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA202605190631Rib · crackedLH WING CENTER FLAP RIB UPPER FLANGE FOUND 2EA CRACKS AT RIB13 BETWEEN STGR2.6 AND STGR2.7 & RIB15 BETWEEN STGR2.7 AND STGR2.8. COMPLIED WITH EA 6-5750-T0377102 A P2 TO REPAIR THE LH WING CENTER FLAP RIB UPPER FLANGE 2EA CRACKS AT RIB13 BETWEEN STGR2.6 ANMay 19, 2026 · N660FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA202605190630Rib · crackedLH WING CENTER FLAP RIB UPPER FLANGE FOUND 2EA CRACKS AT RIB19 & RIB20 BETWEEN STGR2.8 AND REAR SPAR. COMPLIED WITH EA 6-5750-T0377102 A P2 TO REPAIR THE LH WING CENTER FLAP RIB UPPER FLANGE 2EA CRACKS AT RIB19 & RIB20 BETWEEN STGR2.8 AND REAR SPAR. EA TIMay 19, 2026 · N660FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA202605150792Bearing Fitting · damagedCARGO DOOR/HYD SYS - DETAILED VISUAL INSPECTION OF THE MAIN DECK CARGO DOOR (MDCD) ACTUATOR BEARING FITTING AT FRAME 23 AND 24 - AOT A52W016-24 COMPLIED WITH EO 6-5230-E0378588 C P5. TITLE: DOORS - CARGO DOOR/HYD SYS - DETAILED VISUAL INSPECTION OF THE MAIMay 15, 2026 · N660FE · Airbus A300F4605R · Cargo/Baggage DoorsSDR FDEA202605150622Stringer · corrodedFWD CARGO COMPARTMENT S44R STRINGER CORRODED AT FR38.2 - FR39. REPAIRED THE CORRODED S44R STRINGER AT FWD CARGO COMPARTMENT FR38.2 - FR39 IAW SRM 53-10-14-201, FIG 208 & EA 6-5310-T0387401, P1. THE FOLLOW UP INSPECTION REQUIREMENT IAW SRI/IIR 53-10-14-2-008-May 15, 2026 · N660FE · Airbus A300F4605R · Fuselage Main, Longeron/StringerSDR FDEA202602140196Safety Wire · wrong partWHILE PERFORMING F.E.A. 6-2560-F0386375 A P1 FOUND SAFETY WIRE FOR EJECTOR BAG RELEASE CABLE INCORRECT. R1 DOOR AMM: 25-61-20-05-01 REMOVED AND REPLACED SAFETY WIRE WITH MS20995CY16 CAD-PLATED COPPER WIRE. OPS CHK GOOD. A/C OK FOR SERVICE. INSPECTED Feb 14, 2026 · N660FE · Airbus A300F4605R · Escape SlideSDR FDEA202602140195Safety Wire · wrong partWHILE PERFORMING F.E.A. 6-2560-F0386375 A P1 FOUND SAFETY WIRE FOR PACKBOARD CABLE WIRE INCORRECT. R1 DOOR - AMM: 25-61-20-05-01 REMOVED AND REPLACED SAFETY WIRE FROM PACKBOARD RELEASE CABLE WITH MS20995C15 STAINLESS STEEL WIRE. INSPECTED BY VENDOR. OPFeb 14, 2026 · N660FE · Airbus A300F4605R · Escape SlideSDR FDEA202509251831Computer · failedAFTER DEPARTURE, APPROXIMATELY 1,000 FEET MSL, AVIONICS SMOKE OVERHEAD ALERT, MASTER WARNING BELL AND ECAM ALERT. COMPLIED WITH ECAM AND QRH. EMERGENCY DECLARED. NO REFERENCE REQUIRED PER CREW INPUT NO SMOKE WAS NOTICED IN THE COCKPIT, ONLY THE INDICATISep 25, 2025 · N660FE · Airbus A300F4605R · Fire DetectionSDR FDEA202507011086Seat Track · damagedWHILE EVALUATING SEAT TRACK DAMAGE UNDER WRI 25-50/8707, FOUND THAT WRONG LOCK WAS IDENTIFIED AND PLACED ON MEL WRI 25-50/8709. DAMAGE TO SEAT TRACK IS UNDER LOCK ID MB0828. LOCK IS STILL LOCATED IN COAT CLOSET. CREATING NEW WRI FOR WRI 25-50/872 OIL. REFJul 1, 2025 · N660FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202501240134Rib · corrodedLEFT RIB 5 AFT PINTLE BETWEEN BUSH "D" AND "E" HAS EVIDENCE OF CORROSION. PERFORMED REPAIR ON EA# 6-5710-T0381764 PT1. EA TITLE: WINGS - BASIC WING STRUCTURE - L/H MAIN LANDING GEAR RIB 5, FWD LUG CORROSION. MAJOR REPAIRJan 24, 2025 · N660FE · Airbus A300F4605R · Wing, Rib/BulkheadSDR FDEA202403190314Bottle · failedR1 DOOR DAMPER AND EMERGENCY OPERATING CYLINDER PRESSURE BELOW DISPATCH MINIMUMS. SERVICED R1 DOOR DAMPER/EMERGENCY OPERATION CYLINDER REF A300 AMM 52-10-14-03-02 AND PLACARD. ACFT OK TO CONTINUE.Mar 19, 2024 · N660FE · Airbus A300F4605R · Emergency EquipmentSDR FDEA202403110270Switch · faultedR1 CABIN DOOR UNSAFE INDICATION ON DEPARTURE. CABIN PRESSURE INDICATIONS WERE NORMAL THROUGHOUT CLIMB. IN CRUISE, PUSHED HANDLE IAW QRH AND UNSAFE INDICATION WENT OUT FOR REMAINDER OF FLIGHT. RELEASED FOR SERVICE PER MEL 52-11-01-05 CATEGORY : C. R & Mar 11, 2024 · N660FE · Airbus A300F4605R · Passenger/Crew DoorsSDR 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 FDEA202108122008Check Valve · dirtyAFTER BLOCKOUT AT ENGINE START WHEN BLEEDS OPENED WITH BOTH PACKS RUNNING, GOT SMOKE (HYDRALIC FLUID) OUT OF VENTS. ON ENTRY INTO ARCFT, AFTER ENGINE SHUTDOWN, CABIN HAD DISTINCT ODOR OF HYD FLUID. REMOVED AND REPLACED APU PRESSURIZATION LINE ISOLATION CHAug 12, 2021 · N660FE · Airbus A300F4605R · Hydraulic System, Main
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