N669FE

Service difficulty reports · 320

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 = 'N669FE' 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 FDEA202604200487Elevator · not requiredEXISTING REPAIR ON RH ELEVATOR OUTBOARD OF ER2 85MM & IN FRONT OF T/E 810MM UPPER SKIN REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON RH ELEVATOR OUTBOARD OF ER2 85MM & IN FRONT OF T/E 810MM UPPER SKIN WAS EVALUATED AND FOUND IN CONFORMITY WITApr 20, 2026 · N669FE · Airbus A300F4605R · Elevator StructureSDR FDEA202604190482Hinge Arm · delaminatedRH WING #4 SPOILER CENTER HINGE ARM INBD ARM OUTBD SURFACE FOUND 2EA DELAMINATION (65MM*50MM*1.42MM,35MM*26MM*1.26MM). COMPLIED WITH EA 6-5750-T0387084 P1 REPAIRED THE DELAMINATION ON RH WING #4 SPOILER CENTER INBD HINGE ARM OUTBD SURFACE. EA TITLE: WING Apr 19, 2026 · N669FE · Airbus A300F4605R · SpoilersSDR FDEA202604180486Fitting · crackedUPPER FUSELAGE - RH "N" HOLD FOUND CRACKED AT FR47 BTW STGR25 AND STGR26. REPAIRED THE CRACKED RH HOLE N IN UPPER FUSELAGE FR47 BTW STGR25 AND STGR26 PER EA 6-5310-T0387082. TITLE: FUSELAGE - MAINFRAME - FR47 RH HOLE N CRACK REPAIR BETWEEN S-24R AND S-26RApr 18, 2026 · N669FE · Airbus A300F4605R · Fuselage Structure (General)SDR FDEA202604180485Seat Track · no discrepancyEXISTING REPAIR ON MAIN DECK FR40-45 -Y1959 SEAT TRACK REQUIRES EVALUATION FOR CONFORMITY. SEAT TRACK WAS EVALUATED AND FOUND IN CONFORMITY WITH DWG A53832020. NO RECORD FOUND. EO 6-5100-7-5000 D 07 PART 1 WAS COMPLETED. TITLE: STRUCTURES - REPAIR CATAApr 18, 2026 · N669FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202604180481Hinge Arm · delaminatedLH WING, NR 4 SPOILER CENTER HINGE ARM OUTBD SIDE ARM OTBD SURFACE DELAMINATED 40MM*25MM*1.66MM. COMPLIED WITH EA 6-5750-T0387083 P1 REPAIRED THE DELAMINATION ON LH WING #4 SPOILER CENTER OUTBD HINGE ARM OUTBD SURFACE. EA TITLE: WING - FLIGHT SURFACES - LApr 18, 2026 · N669FE · Airbus A300F4605R · SpoilersSDR FDEA202604170458Crossbeam · damagedEXISTING REPAIR ON MAIN DECK FR60 -Y1456~-Y1959 CROSSBEAM REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON MAIN DECK FR60 -Y1456~-Y1959 CROSSBEAM WAS EVALUATED AND FOUND NOT IN CONFORMITY WITH EA6-5310-T0306792 DUE TO A FASTENER HOLE MISS DRILL, Apr 17, 2026 · N669FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA202604170457Floor Support · misrepairedEXISTING REPAIR ON MAIN DECK FR11-FR12A Y0 FLOOR SUPPORT REQUIRES EVALUATION FOR CONFORMITY. EXISTING REPAIR ON MAIN DECK FR11-FR12A Y0 FLOOR SUPPORT REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MAIN DECK FR11-12A Y0 FLOOR SUPPORT WAS EVALUATApr 17, 2026 · N669FE · Airbus A300F4605R · Standard Practices/StructuresSDR FDEA202604160455Seat Track · no discrepancyEXISTING REPAIR ON MAIN DECK FR37-39 -Y450 SEAT TRACK REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON MAIN DECK FR37-39 -Y450 SEAT TRACK WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600F SRM 53-10-16-201 FIG.201, NO RECORD FOUND. EO 6-5100-7Apr 16, 2026 · N669FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202604160454Seat Track · no discrepancyEXISTING REPAIR ON MAIN DECK FR40-45 -Y953 SEAT TRACK REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON MAIN DECK FR40-45 -Y953 SEAT TRACK WAS EVALUATED AND FOUND IN CONFORMITY WITH DWG A53832020 (ISSUE: J00), NO RECORD FOUND. EO 6-5100-7-5000 D Apr 16, 2026 · N669FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202604160453Profile · no discrepancyEXISTING REPAIR ON BULK CARGO FR66-69 Y0~Y140 LONGITUDINAL PROFILE REQUIRES EVALUATION FOR CONFORMITY. LONGITUDINAL PROFILE WAS EVALUATED AND FOUND IN CONFORMITY WITH DWG A53974262 (ISSUE: D), NO RECORD FOUND. EO 6-5100-7-5000 D 07 PART 1 WAS COMPLETEDApr 16, 2026 · N669FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202604160451Seat Track · no discrepancyEXISTING REPAIR ON MAIN DECK FR11-15A Y953 SEAT TRACK REQUIRES EVALUATION FOR CONFORMITY. FLOOR SUPPORT WAS EVALUATED AND FOUND IN CONFORMITY WITH DWG: A53612519 (ISSUE: B00). NO RECORD FOUND. EO 6-5100-7- 5000 D07 PART 1 WAS COMPLETED. TITLE: STRUCTURESApr 16, 2026 · N669FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202604160450Seat Track · no discrepancyEXISTING REPAIR ON MAIN DECK FR57-57.2 -Y1456 SEAT TRACK REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON MAIN DECK FR57-57.2 -Y1456 SEAT TRACK WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600F SRM 53-10-16-201 FIG.201, NO RECORD FOUND. EO 6-Apr 16, 2026 · N669FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202604160449Seat Track · no discrepancyEXISTING REPAIR ON MAIN DECK FR26-28 Y0 SEAT TRACK REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON MAIN DECK FR26-28 Y0 SEAT TRACK WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600F SRM 53-10-16-201 FIG.201, NO RECORD FOUND. EO 6-5100-7-5000 Apr 16, 2026 · N669FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202604150452Seat Track · no discrepancyEXISTING REPAIR ON MAIN DECK FR15A-19 Y953 SEAT TRACK REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MAIN DECK FR15A-19 Y953 SEAT TRACK WAS EVALUATED AND FOUND IN CONFORMITY WITH DWG A53612524 (ISSUE: A00), NO RECORD FOUND. EO 6-5100-7-5000 D 07Apr 15, 2026 · N669FE · Airbus A300F4605R · Standard Practices/StructuresSDR FDEA202604140571Skin · crackedLH WING CENTER FLAP UPPER FLANGE FOUND 1EA CRACK AT RIB17 BETWEEN REAR SPAR AND STGR2.8 COMPLIED WITH EA 6-5750-T0387053 P1 TO REPAIR THE LH WING CENTER FLAP RIB UPPER FLANGE 1EA CRACK AT RIB17 BETWEEN REAR SPAR AND STGR2.8. TITLE: WINGS - FLIGHT SURFACEApr 14, 2026 · N669FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA202604140438Rib · crackedLH WING CENTER FLAP RIB UPPER FLANGE FOUND 1EA CRACK AT RIB27 BETWEEN REAR SPAR AND STGR2.8 COMPLIED WITH EA 6-5750-T0387053 P1 REPAIRED THE LH WING CENTER FLAP RIB27 UPPER CRACKED FLANGE BETWEEN REAR SPAR AND STGR2.8. CAT A REPAIR. MAJOR REPAIR IAW GMM 6Apr 14, 2026 · N669FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA202604140441Crossbeam · crackedMAIN DECK CARGO COMPARTMENT CROSSBEAM AT FR64 BETWEEN -Y1456 AND -Y1959 CRACKED. REPAIRED THE MAIN DECK CARGO COMPARTMENT CRACKED CROSSBEAM AT FR64 BETWEEN -Y1456 AND -Y1959 PER A300-600F SRM53-10-15-201 FIG.211. THIS IS A CATEGORY A REPAIR. MAJOR REPAIR Apr 14, 2026 · N669FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA202604140437Rib · crackedLEFT WING CENTER FLAP RIB UPPER FLANGE FOUND 1EA CRACK AT RIB17 BETWEEN REAR SPAR AND STGR2.8Apr 14, 2026 · N669FE · Airbus A300F4605R · Wing, Rib/BulkheadSDR FDEA202604120484Seat Track · damagedEXISTING REPAIR ON MAIN DECK FR18-22 Y2462 SEAT TRACK REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON MAIN DECK FR18-22 Y2462 SEAT TRACK WAS EVALUATED AND FOUND NOT IN CONFORMITY WITH A300-600F SRM53-10-16 FIG.201A. NO RECORD FOUND. RE-REPAIRED PApr 12, 2026 · N669FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202604120440Rib · crackedRH WING CENTER FLAP RIB UPPER FLANGE FOUND 1EA CRACK AT RIB26 BETWEEN STGR2.7 AND STGR2.8. REPAIRED RH WING CENTER FLAP RIB UPPER FLANGE CRACK AT RIB26 BETWEEN STGR2.7 AND STGR2.8 PER A300-600F SRM57-50-00-201 PARA.4.A & SRM57-50-00-201 FIG.205 & EA6-575Apr 12, 2026 · N669FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA202604120439Rib · crackedRH WING CENTER FLAP RIBS UPPER FLANGE FOUND 3EA CRACK AT RIB11 BETWEEN STGR2.7 AND STGR2.8. REPAIRED RH WING CENTER FLAP RIB UPPER FLANGE CRACK AT RIB11 BETWEEN STGR2.7 AND STGR2.8 PER A300-600F SRM57-50-00-201 PARA.4.A & SRM57-50-00-201 FIG.205 & EA6-5750Apr 12, 2026 · N669FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA202604110583Frame Splice · crackedMAIN FRAME, INSPECTION, HOLES IN FUSELAGE FRAME 47 SPLICE FITTING BETWEEN STR 24 & 26, LH /RH, AIRBUS SB A300-53-6123 COMPLIED WITH EO 6-5310-7-5017 P P6. TITLE: FUSELAGE - MAINFRAME - INSPECTION - HOLES IN FUSELAGE FRAME 47 SPLICE FITTING BETWEEN STR 24 Apr 11, 2026 · N669FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA202604100429Crossbeam · not reportedMAIN DECK CARGO COMPARTMENT CROSSBEAM AT FR67 BETWEEN Y1456 AND Y1959 CRACKED. REPAIRED THE MAIN DECK CARGO COMPARTMENT CRACKED CROSSBEAM AT FR67 BETWEEN Y1456 AND Y1959 PER A300-600F SRM53-10-15-201 FIG.211. THIS IS A CATEGORY A REPAIR. MAJOR REPAIR IAW GApr 10, 2026 · N669FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA202604070574Fitting · not reportedDOORS - CARGO DOOR/HYD SYS - DETAILED VISUAL INSPECTION OF THE MAIN DECK CARGO DOOR (MDCD) ACTUATOR BEARING FITTINGS 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 OApr 7, 2026 · N669FE · Airbus A300F4605R · Cargo/Baggage DoorsSDR FDEA202602180232Slide · damagedWHILE ACCOMPLISHING EA 6-2560-F0386375 REV A PART 1 FOR THE L1 DOOR SLIDE. FOUND THE EJECTOR BAG RELEASE CABLE HAD THE INCORRECT SAFETY WIRE INSTALLED. FACT 18FEB26 21:50 MEM AMM: 25-61-20-05-01 EA: 6-2560-F0386375 REV A PART 1 INSTALLED CAD PLATEDFeb 18, 2026 · N669FE · Airbus A300F4605R · Escape SlideSDR FDEA202602060141Power Supply · inoperativeON POST FLIGHT FOUND PASSENGER DOOR EMERGENCY EXIT LIGHT TEST INOPERATIVE. IAW AMM 33-51-14-04, REMOVED & INSTALLED THE POWER SUPPLY UNIT. OPS CHECK GOOD. NO DEFECTS NOTED.Feb 6, 2026 · N669FE · Airbus A300F4605R · Emergency LightingSDR FDEA202410251581Nut · looseABOUT TO DEPART BFM. TURNED ON APU BLEED. CURRIER AREA FILLED WITH SMOKE. TURNED OFF APU BLEED AND DEPARTED AC. FOUND OIL PUMP NUT LOOSE AT OIL COOLER INLET, TIGHTEN AS REQUIRE IAW A300-600 AMM CH 49-91-16-4 AND SERVICE APU OIL IAW AMM 12-13-49-00. REMOOct 25, 2024 · N669FE · Airbus A300F4605R · Airborne Auxiliary Power Unit (APU) SystemSDR FDEA202403130282Adc · failedSHORTLY AFTER TAKEOFF, PITCH TRIM 2 & YAW DAMPER 2 CLICKED OFF, FOLLOWED BY A ADC2 INOP MESSAGE. ONCE SLATS RETRACTED, FO FLYING & CONTINUED TIL 17,000 FT. REVIEWED QRH FOR ADC FAULT & NOTED WERE NO LONGER RVSM & FO PLACED AP 1 ON. AFTER 2 MINS, AP1 CLICKEDMar 13, 2024 · N669FE · Airbus A300F4605R · Air Data ComputerSDR FDEA202310021682Flap · corrodedLH WING O/B FLAP O/B END T/E SKIN CORRODED AND DISCHARGER FITTING FOUND BROKEN REPAIRED THE CORRODED SKIN AT LH WING O/B FLAP O/B END T/E PER EA:6-5750-T0376427 P1. TITLE: WINGS - FLIGHT SURFACES - LH O/B FLAP, OUTER TRAILING EDGE, UPPER SKIN CORROSION UOct 2, 2023 · N669FE · Airbus A300* · Trailing Edge FlapsSDR FDEA202309251644Crossbeam · crackedMDCC FLOOR CROSSBEAM FWD STIFFENER CRACKED AT FR31, BTW -Y450 - -Y953 REPAIRED THE CRACK ON THE MDCC FLOOR CROSSBEAM FWD STIFFENER AT FR31, BTW -Y450 - - Y953 PER A300-600F SRM53-10-15-201 PARA.15 & EA:6-5310-T0376313 P1. THE REPAIR IS CAT A REPAIR, MAJOR RESep 25, 2023 · N669FE · Airbus A300* · Fuselage Main, StructureSDR FDEA202309251643Seat Track · corrodedMDCC SEAT TRACK FOUND 2EA CORRODED BETWEEN FR73 - FR78, Y953 REPAIRED THE MDCC CORRODED SEAT TRACK BETWEEN FR73 - FR78, Y953 PER SRMA300-600F SRM53-10-16 FIG.201. THIS REPAIR IS CAT A REPAIR. MAJOR REPAIR IAW FEDEX GMM6-2-100.Sep 25, 2023 · N669FE · Airbus A300* · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202309251642Seat Track · corrodedMDCC SEAT TRACK FOUND CORROSION AT FR57.3 - FR58 Y-450 REPAIRED THE MDCC SEAT TRACK AT FR57.3 - FR58 Y-450, PER A300-600F SRM53-10-16 FIG.201, THIS REPAIR IS CAT A REPAIR. MAJOR REPAIR IAW FEDEX GMM6-2-100.Sep 25, 2023 · N669FE · Airbus A300* · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202304130635Unknown · unknownDOOR R1 ASSIST BOTTLE BLOWN. RELEASED FOR SERVICE PER MEL : 52-11-01-05 CATEGORY : C EXPIRATION : 23APR23 "MEL 52-11-01-05: CREW ENTRY DOOR R1 - INOP." SLIDE IS NOT BLOWN C/7356956. REMOVED AND REPLACED DIAPHRAGM IN R-1 FWD DOOR DAMPER AND EMERGENCY OPERAApr 13, 2023 · N669FE · Airbus A300* · Passenger/Crew DoorsSDR FDEA202201050011Packing · leakingL1 DOOR DAMPER ASSIST BOTTLE READING. 0 . RELEASED FOR SERVICE PER MEL : 52-11-01-05 CAT: C EXP: 15JAN22 "MEL 52-11-01-05: CREW ENTRY DOOR L1 - INOP." RELEASED FOR SERVICE PER MEL : 52-XX-XX-XX CATEGORY : C EXPIRATION : 15JAN22 . IDENTIFIED PARTS SEALJan 5, 2022 · N669FE · Airbus A300* · Passenger/Crew DoorsSDR FDEA202112133085Computer · damagedSUSPECTED FUEL LEAK DURING CLIMB OUT. PASSING FL200. LEFT INNER TANK WENT FROM 3K TO 200 POUNDS. COMPLIED WITH QRH. IMBALANCE AND FUEL DISCREPANCY STAYED AFTER RESETTING FUEL CHAN SUPPLY BREAKERS. FIRE CHIEF IN BNA SAID NO SIGNS OF A LEAK. LANDING AND TAXI IDec 13, 2021 · N669FE · Airbus A300F4605R · Fuel Indicating SystemSDR FDEA202109162318Damper · failedPDIS 669 32-30 3699 15SEP21 MKE OPEN U AFTER TAKE OFF KIND. LANDING GEAR HANDLE WOULD NOT COME UP IN SYS POS 1. POS SYS 2 WAS MEL. BUT TRIED POS SYS 2 AND IT WORKED. USED POS SYS 1 TO LOWER THE GEAR AT MKE. NO ISSUES. "MEL 32-30-01-A: LANDSep 16, 2021 · N669FE · Airbus A300F4605R · Landing Gear Retraction/Extension SystemSDR FDEA202103180760Adapter · damagedREPLACE ADAPTER TRACK UNDER LOCK STA1530 LOC. FLOOR STRUCTURE FR58 BTW -Y953 TO -Y450 FOR TERMINATING ACTION ON RUTINE CARD 000832 REPLACED ADAPTER TRACK UNDER LOCK STA1530 LOC. ON FLOOR STRUCTURE FR 58 BTW -Y953 TO -Y450 IAW SRM A300-600 FREIGHTER 51-40-21Mar 18, 2021 · N669FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202103160841Floor Support · corrodedCORROSION FLOOR BEAM Y450 BTW FR 11 TO FR 14 PASSENGER CABIN PERFORMED PERMANENT REPAIR ON FLOOR BEAM Y450 BTW FR11 TO FR 14 PASSENGER CABIN, THIS REPAIR IS CATEGORY B IAW A300-600 FREIGHTER SRM 53-12-15 STEP 5G FIG 207. AND INSPECTION THRESHOLD AT 42500FCMar 16, 2021 · N669FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202103130853Fitting · crackedCRACK INDICATION ON FRAME 47 RH SIDE ON CWB REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE AT OPEN FASTENER HOLE F (CRACK DIRECTION IS 7 OCLOCK) AT LOWER FUSELAGE (1EA) REPAIRED IAW EA 6-5710-T0360412 (P1) RELEASE DATE 06-APR-21 EA TITTLE: WINGS - BAMar 13, 2021 · N669FE · Airbus A300F4605R · Wing, Attach FittingsSDR FDEA202103090759Web · crackedCRACK WEB LOCATED AT LEVEL FR 47 AND Y450 TO Y0 IN PASSENGER CABIN (MAIN DECK) REPLACED WEB AT LEVEL FR47 AND Y450 TO Y0 IN MAIN DECK CABIN AS PER A300-600 SRM 51- 51-72-10 AND DRAWING A53810937 ISSUE B SHEET 01Mar 9, 2021 · N669FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202103090758Web · crackedCRACK WEB LOCATED AT LEVEL FR 47 AND Y0 TO -Y450 IN PASSENGER CABIN (MAIN DECK) REPLACED WEB LOCATED AT LEVEL FR47 AND Y0 TO -Y450 IN MAIN DECK CABIN AS PER A300- 600 SRM 51-72-10 AND DRAWING A53810937 ISSUE B SHEET 1Mar 9, 2021 · N669FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202103090741Web · crackedCRACK WEB LOCATED AT LEVEL FR 47 AND Y1456 TO Y953 IN PASSENGER CABIN (MAIN DECK) PERFORMED PERMANENT REPAIR ON WEB LOCATED AT LEVEL FR47 AND Y1456 TO Y953 IN PASSENGER CABIN (MAIN DECK) IAW A300-600 FREIGHTER SRM 53-15-15 PARAGRAPH 5A FIGURE 201 AND DWG# Mar 9, 2021 · N669FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202103090928Support Angle · crackedCRACK TRAILING EDGE SUPPORT ANGLE LOCATED AT LEVEL OF RIB 6A REAR SPAR INBOARD SIDE ON RH WING PERFORMED PERMANENT REPAIR ON TRAILING EDGE SUPPORT ANGLE LOCATED AT LEVEL OF OF RIB 6A REAR SPAR INBOARD SIDE ON RH WING IAW EA 6-5710-T0360731 TITTLE: WINGS- BAMar 9, 2021 · N669FE · Airbus A300F4605R · Wing Miscellaneous StructureSDR FDEA202103090739Web · crackedCRACK WEB LOCATED AT LEVEL FR 47 AND -Y1456 TO -Y953 IN PASSENGER CABIN (MAIN DECK) REPAIRED WEB LOCATED AT LEVEL FR47 AND -Y1456 TO -Y953 IN PASSENGER CABIN (MAIN DECK) IAW A300-600 FREIGHTER SRM 53-15-15 PARAGRAPH 5A(2) FIGURE 201 SHEET 1 AND 2 CONFIG. 2Mar 9, 2021 · N669FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202103080926Stringer · corrodedCORROSION STRUCTURE INTERNAL STRINGER 37L BETWEEN FR. 46 AND FR. 47 IN AIR CONDITIONING BAY PERFORMED REPAIR ON INTERNAL STRUCTURE STRINGER 37L BTW FR46 AND FR 47 IN AIR CONDITIONING BAY IAW EA# 6-5310-T0360467 P1 TITTLE: FUSELAGE MAINFRAME-CORROSION ON STMar 8, 2021 · N669FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA202103070890Skin · dentedSEVERAL DENTS ON AILERON UPPER AND LOWER SURFACE ON RH WING PERFORMED PERMANENT REPAIR LOC ON LOWER SURFACE BTW RIB 11 TO RIB 12 ON RH AILERON IAW EA 6-5750-T0360611 P1 TITLE WINGS FLIGHT SURFACES RIGHT HAND ALL SPEED AILERON UPPER AND LOWER SKINS MULTIPLEMar 7, 2021 · N669FE · Airbus A300F4605R · AileronsSDR FDEA202103070889Skin · dentedSEVERAL DENTS ON AILERON LOWER AND UPPER SURFACE ON LH WING PERFORMED PERMANENT REPAIR LOC LOWER SURFACE BTW RIB 9 AND RIB 11 ON LH AILERON IAW EA 6-5750-T0360573 P1 TITLE WINGS FLIGHT SURFACES LEFT HAND ALL SPEED AILERON UPPER AND LOWER SKINS MULTIPLE DENMar 7, 2021 · N669FE · Airbus A300F4605R · AileronsSDR FDEA202103030648Seat Track · corrodedEXISTING REPAIR ON MAIN DECK FR56-57.1 -Y1456 SEAT TRACK. REQUIRES EVALUATION PER ATTACHMENT B IAW EO 6-5100-7-5000 P1 THE EXISTING REPAIR ON MAIN DECK FR56-57.1 -Y1456 SEAT TRACK WAS NOT FOUND CONFORMITY WITH A300-600F SRM 53-10-16 FIG 201 AND EVALUATED PMar 3, 2021 · N669FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202103030628Seat Track · misrepairedEXISTING REPAIR ON SEAT TRACK Y0 LOCATED BETWEEN FR75 TO FR77 IN MAIN DECK. REQUIRES EVALUATION PER ATTACHMENT B. IAW EO 6-5100-7-5000 P1 THE EXISTING REPAIR ON SEAT TRACK Y0 LOCATED BETWEEN FR75 TO FR77 IN MAIN DECK WAS NOT FOUND CONFORMITY WITH A300-600FMar 3, 2021 · N669FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202103030627Seat Track · misrepairedEXISTING REPAIR FRAME ON UPPER FUSELAGE (EXISTING REPAIR ON MAIN DECK FR56-FR57.2 - Y953 SEAT TRACK. REQUIRES EVALUATION PER ATTACHMENT B IAW EO 6-5100-7-5000 P1) THE EXISTING REPAIR ON MAIN DECK FR56-FR57.2 -Y953 SEAT TRACK WAS NOT FOUND CONFORMITY WITH A3Mar 3, 2021 · N669FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
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