N655FE

Service difficulty reports · 219

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 = 'N655FE' 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 FDEA202510061904Bottle · low pressureR1 DOOR EMERGENCY DAMPENER BELOW MIN NITROGEN CHARGE. AMM 52-10-14-03-02 SERVICED R1 DOOR EMERGENCY DAMPENER CYLINDER TO WITHIN LIMITS PER PLACARD AND AMM 52-10-14-03-02 STEP 3.D.(12) OKAY TO CONTINUE.Oct 6, 2025 · N655FE · Airbus A300F4605R · Service DoorsSDR FDEA202409131400Rib · corrodedTHE UPPER BORE OF INBD JACK RIB(LOCATION#1) WAS CORRODED ON L5 SPLR. ACCOMPLISHED THE REINFORCEMENT REPAIR AT LH #5 SPOILER INBD JACK RIB I.A.W FEDEX EA NO: T6-5740-T0380719 P1, SEQ NO:790, TITLE: WINGS- ATTACH FITTINGS- LH WING #5 SPOILER JACK RIB AT STA Sep 13, 2024 · N655FE · Airbus A300F4605R · Wing, Rib/BulkheadSDR FDEA202409131385Rib · corrodedTHE UPPER BORE OF INBD JACK RIB(LOCATION#1) WAS CORRODED ON L5 SPLR. ACCOMPLISHED THE REINFORCEMENT REPAIR AT LH #5 SPOILER INBD JACK RIB I.A.W FEDEX EA NO: T6-5740-T0380719 P1, SEQ NO:790, TITLE: WINGS- ATTACH FITTINGS- LH WING #5 SPOILER JACK RIB AT STA Sep 13, 2024 · N655FE · Airbus A300F4605R · Wing, Rib/BulkheadSDR FDEA202409121488Rib · corrodedRH SPOILER 3 OUTBOARD JACK RIB UPPER BORE CORRODED ACCOMPLISHED THE REINFORCEMENT REPAIR AT RH #3 SPOILER OUTBD JACK RIB UPPER BORE I.A.W FEDEX EA NO: T6-5740-T0380720 P1, SEQ NO:791, TITLE: WINGS- ATTACH FITTINGS- RH WING #3 SPOILER JACK RIB AT STA ABX 40Sep 12, 2024 · N655FE · Airbus A300F4605R · Wing, Rib/BulkheadSDR FDEA202409121399Rib · corrodedTHE LWR BORE OF INBD JACK RIB WAS CORRODED ON L5 SPLR(LOCATION #3). ACCOMPLISHED THE REINFORCEMENT REPAIR AT LH #5 SPOILER INBD JACK RIB I.A.W FEDEX EA NO: T6-5740-T0380719 P1, SEQ NO:790, TITLE: WINGS- ATTACH FITTINGS- LH WING #5 SPOILER JACK RIB AT STA ASep 12, 2024 · N655FE · Airbus A300F4605R · Wing, Rib/BulkheadSDR FDEA202409121396Rib · corrodedRH SPOILER 5 OUTBOARD JACK RIB UPPER BORE CORRODED ACCOMPLISHED THE REINFORCEMENT REPAIR AT RH #5 SPOILER OUTBD JACK RIB I.A.W FEDEX EA NO: T6-5740-T0380713 P1, SEQ NO:789, TITLE: WINGS- ATTACH FITTINGS- RH WING #5 SPOILER JACK RIB AT STA ABX 175.875 AND ASep 12, 2024 · N655FE · Airbus A300F4605R · Wing, Rib/BulkheadSDR FDEA202409121395Rib · corrodedRH SPOILER 5 INBD JACK RIB UPPER BORE CORRODED ACCOMPLISHED THE REINFORCEMENT REPAIR AT RH #5 SPOILER INBD JACK RIB I.A.W FEDEX EA NO: T6-5740-T0380713 P1, SEQ NO:789, TITLE: WINGS- ATTACH FITTINGS- RH WING #5 SPOILER JACK RIB AT STA ABX 175.875 AND ABX184Sep 12, 2024 · N655FE · Airbus A300F4605R · Wing, Rib/BulkheadSDR FDEA202409121394Rib · corrodedRH SPOILER 3 OUTBOARD JACK RIB UPPER BORE CORRODED ACCOMPLISHED THE REINFORCEMENT REPAIR AT RH #3 SPOILER OUTBD JACK RIB I.A.W FEDEX EA NO: T6-5740-T0380720 P1, SEQ NO:791, TITLE: WINGS- ATTACH FITTINGS- RH WING #3 SPOILER JACK RIB AT STA ABX 40.425- BEAM Sep 12, 2024 · N655FE · Airbus A300F4605R · Wing, Rib/BulkheadSDR FDEA202409121393Rib · gougedTHE UPPER BORE OF INBD JACK RIB (LOCATION #1) GOUGE ON L4 SPOILER ACCOMPLISHED THE REINFORCEMENT REPAIR AT LH #4 SPOILER INBD JACK RIB I.A.W FEDEX EA NO: T6-5740-T0380723 P1, SEQ NO:792, TITLE: WINGS- ATTACH FITTINGS- LH WING #4 SPOILER JACK RIB AT STA ABXSep 12, 2024 · N655FE · Airbus A300F4605R · Wing, Rib/BulkheadSDR FDEA202409121392Rib · gougedTHE UPPER BORE OF INBD JACK RIB (LOCATION #1) GOUGE ON L4 SPOILER ACCOMPLISHED THE REINFORCEMENT REPAIR AT LH #4 SPOILER INBD JACK RIB I.A.W FEDEX EA NO: T6-5740-T0380723 P1, SEQ NO:792, TITLE: WINGS- ATTACH FITTINGS- LH WING #4 SPOILER JACK RIB AT STA ABXSep 12, 2024 · N655FE · Airbus A300F4605R · Wing, Rib/BulkheadSDR FDEA202409121386Rib · corrodedTHE LWR BORE OF INBD JACK RIB WAS CORRODED ON L5 SPLR(LOCATION #3). ACCOMPLISHED THE REINFORCEMENT REPAIR AT LH #5 SPOILER INBD JACK RIB I.A.W FEDEX EA NO: T6-5740-T0380719 P1, SEQ NO:790, TITLE: WINGS- ATTACH FITTINGS- LH WING #5 SPOILER JACK RIB AT STA ASep 12, 2024 · N655FE · Airbus A300F4605R · Wing, Rib/BulkheadSDR FDEA202409121370Seat Track · corrodedMAIN DECK SEAT TRACK A POINT GOT CORROSION AT FR15B Y953 REPLACED THE SEAT TRACK WITH NEW PART. I.A.W A300-600F SRM 51-72-10-001, P2. THIS REPAIR CLASSIFIED AS MINOR, PER GMM 06-2-100. AT FR15A~19, Y953Sep 12, 2024 · N655FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202409121332Seat Track · corrodedMAIN DECK SEAT TRACK A POINT GOT CORROSION AT FR15B Y953 REPLACED THE SEAT TRACK WITH NEW PART. I.A.W A300-600F SRM 51-72-10-001, P2. THIS REPAIR CLASSIFIED AS MINOR, PER GMM 06-2-100. AT FR15A~19, Y953 NOTE: 5.(C), P/N TYPE ERROR, CREATED A NEW SDR NO:24-Sep 12, 2024 · N655FE · Airbus A310300 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202409111407Fitting · crackedLOWER RH FRAME 46 BASE FITTING FOUND AREA 1 CRACK ACCOMPLISHED THE DOUBLER REPAIR AT FRAME FOOT FR 46, STGR36R~38R. I.A.W FEDEX EO NO:E6-5310-E0330747 D P26, SEQ NO:784, TITLE: FUSELAGE- MAINFRAME- INSPECTION OF LOWER FRAME BASE FITTING BETWEEN FRAMES 41 ASep 11, 2024 · N655FE · Airbus A300F4605R · Fuselage Main, Attach FittingsSDR FDEA202409111406Fitting · crackedLOWER LH FRAME 46 BASE FITTING FOUND AREA 1 CRACK ACCOMPLISHED THE DOUBLER REPAIR AT FRAME FOOT FR 46, STGR36L~38L. I.A.W FEDEX EO NO:E6-5310-E0330747 D P25, SEQ NO:783, TITLE: FUSELAGE- MAINFRAME- INSPECTION OF LOWER FRAME BASE FITTING BETWEEN FRAMES 41 ASep 11, 2024 · N655FE · Airbus A300F4605R · Fuselage Main, Attach FittingsSDR FDEA202409111405Fitting · crackedLOWER LH FRAME 45 BASE FITTING FOUND AREA 1 CRACK ACCOMPLISHED THE DOUBLER REPAIR AT FRAME FOOT FR 45, STGR36L~38L. I.A.W FEDEX EO NO:E6-5310-E0330747 D P23, SEQ NO:782, TITLE: FUSELAGE- MAINFRAME- INSPECTION OF LOWER FRAME BASE FITTING BETWEEN FRAMES 41 ASep 11, 2024 · N655FE · Airbus A300F4605R · Fuselage Main, Attach FittingsSDR FDEA202409111404Fitting · crackedLOWER RH FRAME 44 BASE FITTING FOUND AREA 1 CRACK ACCOMPLISHED THE TRIMMED OUT AND FILLED THE GAP UNDER THE ANGLE WITH SHIM AT FR 44, STGR36R~37R I.A.W FEDEX EO NO:E6-5310-E0330747 D P22, SEQ NO: 781, TITLE: FUSELAGE- MAINFRAME- INSPECTION OF LOWER FRAME BSep 11, 2024 · N655FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA202403020227Slide · detachedR1 DOOR ESCAPED SLIDE FELL OUT OF DOOR WHEN DOOR WAS OPENED. DOOR DID NOT BLOW WHEN IT FELL OUT. REPLACED SLIDE IAW AMM 25-61-21-4.Mar 2, 2024 · N655FE · Airbus A300F4605R · Escape SlideSDR FDEA202206161441None · unknownMDIS 655 32-42 4886 16JUN22 LRD OPEN U # 5 MLG TIRE COMPLETELY MISSING FROM AIRCRAFT AT BLOCK IN. *************************************************** TFOA CATEGORY: 1 SHGN 19JUN22 22:36 LRD Jun 16, 2022 · N655FE · Airbus A300* · BrakeSDR FDEA202204181076Seat Track · damagedMAIN DECK COMPT - SEAT TRACK CROWN LIP AREA FOUND ENLARGED AT FR20 6" AND -Y450 CUT OUT AND INSTALLED NEW SEAT TRACK PORTION & REPAIR ANGLES I.A.W EA NO:6-5310- T0367804 P1, SEQ NO:001135, TITLE:FUSELAGE-MAINFRAME- MAIN DECK SEAT TRACKS AT -Y450 & -Y1456 WOApr 18, 2022 · N655FE · Airbus A300* · Fuselage Main, StructureSDR FDEA202204181075Seat Track · damagedMAIN DECK COMPT - SEAT TRACK CROWN LIP AREA FOUND ENLARGED AT FR20 6" AND -Y1456 CUT OUT AND INSTALLED NEW SEAT TRACK PORTION & REPAIR ANGLES I.A.W EA NO:6-5310- T0367804 P1, SEQ NO:001135, TITLE:FUSELAGE-MAINFRAME- MAIN DECK SEAT TRACKS AT -Y450 & -Y1456Apr 18, 2022 · N655FE · Airbus A300* · Fuselage Main, StructureSDR FDEA202203290828Floor Panel · noneAT THE TIME OF AGING AIRCRAFT INSPECTION FOUND MAIN DECK FLOOR PANEL 242BF IS SHOWING SIGNS OF DELAMINATION REPAIRED WITH RESIN COMPOUND AND FIBER GLASS I.A.W A300-600F SRM 53-10-20-201, PARA.8B, P209-211, FIG203(SHEET 1)Mar 29, 2022 · N655FE · Airbus A300* · Fuselage Floor PanelSDR FDEA202203210618None · wornFR38.2/FR40 RH NO.2 DUMMY SEAT TRACK SLOT GAP OVER GAP VALUE(A) 0.0393INCH(1.0MM) BUT LESS THAN 0.0846INCH(2.15MM). I.A.W A300-600 SRM 53-15-16-201 PARA 5A P201-210 FIG.201 PERFORM REPAIR ACCOMPLISHED.Mar 21, 2022 · N655FE · Airbus A300* · Fuselage Main, Floor BeamSDR FDEA202203210617None · wornFR38.2/FR40 CENTER NO.1 DUMMY SEAT TRACK SLOT GAP OVER GAP VALUE(A) 0.0393INCH(1.0MM) BUT LESS THAN 0.0846INCH(2.15MM). I.A.W A300-600 SRM 53-15-16-201 PARA 5A P201-210 FIG.201 PERFORM REPAIR ACCOMPLISHED.Mar 21, 2022 · N655FE · Airbus A300* · Fuselage Main, Floor BeamSDR FDEA202203210616None · wornFR38.2/FR40 LH NO.2 DUMMY SEAT TRACK SLOT GAP OVER GAP VALUE(A) 0.0393INCH(1.0MM) BUT LESS THAN 0.0846INCH(2.15MM). I.A.W A300-600 SRM 53-15-16-201 PARA 5A P201-210 FIG.201 PERFORM REPAIR ACCOMPLISHED.Mar 21, 2022 · N655FE · Airbus A300* · Fuselage Main, Floor BeamSDR FDEA202203210615None · wornFR54/FR54.2 LH NO.4 DUMMY SEAT TRACK SLOT GAP OVER GAP VALUE(A) 0.0393INCH(1.0MM) BUT LESS THAN 0.0846INCH(2.15MM). I.A.W A300-600 SRM 53-15-16-201 PARA 5A P201-210 FIG.201 PERFORM REPAIR ACCOMPLISHED.Mar 21, 2022 · N655FE · Airbus A300* · Fuselage Main, Floor BeamSDR FDEA202203210614None · wornFR54/FR54.2 LH NO.5 DUMMY SEAT TRACK SLOT GAP OVER GAP VALUE(A) 0.0393INCH(1.0MM) BUT LESS THAN 0.0846INCH(2.15MM). I.A.W A300-600 SRM 53-15-16-201 PARA 5A P201-210 FIG.201 PERFORM REPAIR ACCOMPLISHED.Mar 21, 2022 · N655FE · Airbus A300* · Fuselage Main, Floor BeamSDR FDEA202203200893None · unknownAIRCRAFT REPAIR ASSESSMENT:EXISTING EXTERNAL DOUBLER FOUND ON R/H WING LWR SURFACE L/E PANEL 613AB CUTOUT FWD O/B AREA. COMPLIED WITH ATTCHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE:A300/A310 RPR IDENT & SUPPLEMENTAL MX REQ(SMP) TRK, INSPECTION OF EXISTIMar 20, 2022 · N655FE · Airbus A300* · Wing StructureSDR FDEA202203200892None · noneAIRCRAFT REPAIR ASSESSMENT:EXISTING EXTERNAL DOUBLER FOUND ON L/H WING LWR SURFACE L/E PANEL 513AB CUTOUT FWD O/B AREA. COMPLIED WITH ATTCHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE:A300/A310 RPR IDENT & SUPPLEMENTAL MX REQ(SMP) TRK, INSPECTION OF EXISTIMar 20, 2022 · N655FE · Airbus A300* · Wing StructureSDR FDEA202203200891Seat Track · noneAIRCRAFT REPAIR ASSESSMENT:EXISTING REPAIR OF SPLICE FOUND ON MAIN DECK SEAT TRACK BTW FR67-FR70,Y450 POSITIOS. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: A300/A310 RPR IDENT & SUPPLEMENTAL MX REQ(SMR) TRK, INSPECTION OF EXISTING REPAMar 20, 2022 · N655FE · Airbus A300* · Fuselage Structure (General)SDR FDEA202203200671Seat Track · corrodedMAIN DECK COMPT FLOOR - SEAT TRACK , FLANGE AREA GOT CORROSION POS FROM FR 55 11" TO FR 56 10" AND Y0. PERFORMED SEAT TRACK SPLICE REPAIR ON CORROSION SECTION I.A.W. A300-600F SRM 53- 10-16-201, PARA.4, PAGE.203-208, FIG.201. "MAJOR REPAIR"Mar 20, 2022 · N655FE · Airbus A300* · Fuselage Main, StructureSDR FDEA202203180724Floor Support · corrodedMAIN DECK FLOOR SUPPORT GOT CORROSION POS AROUND HARDPOINT AREA FROM FR13 TO FR13A AND Y953 ACCOMPLISHED THE CATE.B FLOOR STRUCTURE REPAIR I.A.W A300-600F SRM 53-12-15-201-2, PARA.5G, PAGE.239-244, FIG.207 & SRI:53-12-15-201, IIR:53-12-15-2-004-00, PARA.Mar 18, 2022 · N655FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202203150817None · wornLH SPL#2 O/B EDGE WEB CHAFING. ACCOMPLISHED THE REPAIR WITH FILLER AND REPAIR SHIM I.A.W EA NO:6-5750-T0367548 P1, SEQ NO:001119, TITLE:WING -FLIGHT SURFACES- LH SPOILER #2 -WEAR MARK ON OUTBOARD FACE OF FRONT SPAR AT LEVEL OF RIB18 & A300-600F SRM 51-27Mar 15, 2022 · N655FE · Airbus A300* · Wing, Control SurfacesSDR FDEA202203150695Plate · crackedAVIONICS COMP'T DOOR AFT EDGE PANEL SUPPORT FRAME CRACK ABOUT0.2". REPLACED THE PLATE BENT WITH NEW ONE I.A.W A300-600F SRM 51-72-10-001, PAGE2Mar 15, 2022 · N655FE · Airbus A300* · Fuselage Floor PanelSDR FDEA202203100652Floor Panel · damagedTHE FWD CARGO FLOOR PANEL #131QG #131LG #131RG #131SG WAS FOUND DAMAGED AS MARKER. ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W A300-600F SRM 53-10-20-201 PARA8B FIG203 SHEET1 P209-211Mar 10, 2022 · N655FE · Airbus A300* · Fuselage Floor PanelSDR FDEA202203100628Skin · damaged1EA WATER TRAPPED AREA WAS FOUND AT L/H ELEVATOR UPPER SKIN PANEL NO.14(130MM X 85MM) SCREW AREA. ACCOMPLISHED THE WATER TRAPPED AREA CAT.A REPAIR I.A.W A300-600F SRM 55-21-12-201 PARA.5J P268-270 FIG 212 (SHEET 3)Mar 10, 2022 · N655FE · Airbus A300* · Horizontal Stabilizer StructureSDR FDEA202203100627Skin · damaged1EA WATER TRAPPED AREA WAS FOUND AT L/H ELEVATOR UPPER SKIN PANEL NO.19(120MM X 80MM) SCREW AREA. ACCOMPLISHED THE WATER TRAPPED AREA CAT.A REPAIR I.A.W A300-600F SRM 55-21-12-201 PARA.5J P268-270 FIG 212 (SHEET 3)Mar 10, 2022 · N655FE · Airbus A300* · Horizontal Stabilizer StructureSDR FDEA202203100626Skin · damaged1EA WATER TRAPPED AREA WAS FOUND AT L/H ELEVATOR UPPER SKIN PANEL NO.20(150MM X 90MM) SCREW AREA. ACCOMPLISHED THE WATER TRAPPED AREA CAT.A REPAIR I.A.W A300-600F SRM 55-21-12-201 PARA.5J P268-270 FIG 212 (SHEET 3)Mar 10, 2022 · N655FE · Airbus A300* · Horizontal Stabilizer StructureSDR FDEA202111182892None · corrodedAFTER REMOVAL OF THE RH RIB 5, FWD LUG AFT FACE BUSHING, FOUND CORROSION IN BORE AND ON LUG FACE. REPAIRED IAW EA T6-5710-T0365559, PARTS 1, THRU 5. RH RIB 5 FWD LUG BORE & AFT FACE WEAR DAMAGE DUE TO IMPROBERILY INSTALLED MLG BUSHING- SB A300-57-6106 Nov 18, 2021 · N655FE · Airbus A300F4605R · Wing, Rib/BulkheadSDR FDEA202102230600Bulkhead · damagedNLG WHEEL WELL BULKHEAD DAMAGE (STIFFENER CRACK/DEFORMAT COMPLY WITH E..A. 6-5310-T0360151 REV NO. POS. P1 INFO 07MAR21 01:32 ** ATTACHED TO WORK ORDER 00079413 ** STRP 07MAR21 03:12 MEM U FACT 07MAR21 03:12 MEM U COMPLIED WITH EA 6-5310-T0360151 Feb 23, 2021 · N655FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA202011032765Arming Lever · unknownPDIS 655 52-10 3248 03NOV20 MEM FACT U. UPON CLOSE UP OF A/C 655 THE CABIN ENTRY DOOR ON THE RIGHT SIDE OF THE AIRPLANE WOULD NOT ARM SLIDE. IT ILLUMINATED BRIEFLY, FLASHED ON AND OFF AND THEN STAYED OFF. WE OPENED AND CLOSED DOOR AND ATTEMPTED TO REARM TO Nov 3, 2020 · N655FE · Airbus A300F4605R · Emergency EquipmentSDR FDEA202010232621Transmitter · failedPDIS 655 29-30 3219 23OCT20 CLE OPEN U LOGPAGES:3236545 ENROUTE TO CLE AT 350, GOT A ECAM WARNING FOR GREEN HYDRAULIC LO QUANTITY. THE GEEN HYDRAULIC GAUGE SHOWED FLUID BELOW RED DOT. ECAM GAUGE WAS AT THE BOTTOM OF THE SCALE. DIDN'T RECEIVE Oct 23, 2020 · N655FE · Airbus A300F4605R · Hydraulic Indicating SystemSDR FDEA202008292065Tire · failedON APPROACH, GOT A LEFT MAIN DOOR LIGHT. ALL GEAR INDICATIONS WERE ALL GREEN(DOWN AND LOCKED) ADHERED TO QRH. ON LANDING ROLLOUT, HAD AN APPARENT BLOWN TIRE. COMPLIED WITH EA 6-3212-T0356228 REV A PART 2. GEAR SWING TEST GOOD, REF AMM 32-31-00-5 LANDING GAug 29, 2020 · N655FE · Airbus A300F4605R · TireSDR FDEA2019120193152Adapter · damagedRESTRAINT ID C1509 IS UNABLE TO PROVIDE RESTRAINT DUE TO SEAT TRACK DAMAGE. REMOVED AND REPLACED DAMAGED ADAPTER REF SRM 51-40-20 AND SRM 30-53-003. RE-INSTALLED LATCH/RESTRAINT IN 8L.Nov 19, 2019 · N655FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA2019120183153Adapter · damagedSEAT TRACK ADAPTER ON MAIN CARGO DECK AT POSITION C1509 HAS A BROKEN LOBE. REMOVED AND REPLACED DAMAGED ADAPTER REF SRM 51-40-20 AND SR30-53-003.Nov 8, 2019 · N655FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201910312796Actuator · malfunctionedPDIS 655 27-80 2283 30OCT19 FSD OPEN U LOGPAGES:2284251 ON APPROACH FSD - NO KRUGER FLAP EXTENTION - RUN ECAM - QRH - NORMAL LANDING. SHGN 31OCT19 12:53 FSD U FOUND LEFT KRUGER FLAP WITH MOVEABLE VANE ABOVE FLAP. COMPLIED WITH EA. 6-2780Oct 31, 2019 · N655FE · Airbus A300F4605R · Leading Edge Slat ActuatorSDR FDEA201909052104Skin · corrodedFROM INSIDE TO OUTSIDE NR 1 STATIC DISCHARGER RETAINER AND SKIN SEPARATION ON THE RT WING TRAILING EDGE. COMPLIED WITH EA:6-5750-T0349278 P1 REPAIRED FROM INSIDE TO OUTSIDE NR 1 STATIC DISCHARGER RETAINER AND SKIN SEPARATION ON THE RT WING TRAILING EDGE. EA TISep 5, 2019 · N655FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA201908302041Support Beam · crackedAFT CARGO DOOR SUPPORT BEAM FOUND CRACKED FR61 TO FRAMES 62 TO 62. REPLACED AFT CARGO DOOR SUPPORT BEAM IAW SRM 51-40-21. MAJOR REPAIR IAW GMM 6-2-100.Aug 30, 2019 · N655FE · Airbus A300B4605R · Fuselage Miscellaneous StructureSDR FDEA201908262017Floorbeam · crackedAFT CARGO COMPARTMENT DOOR CUTOUT AREA, FLOOR BEAM ABOUT FRAME 60 FOUND CRACKED. COMPLIED WITH EA:6-5310-T0348991 P1, REPAIRED AFT CARGO COMPARTMENT DOOR CUTOUT AREA, FLOORBEAM ABOUT FRAME 60. MAJOR REPAIR IAW GMM 6-2-100.Aug 26, 2019 · N655FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA201908221998Crossbeam · crackedCROSSBEAM ON NLG FR15A WEB FACE AT ATTACHMENT FITTING OF RACK 107VU FOUND CRACKED. COMPLIED WITH EA 6-5310-T0348838 P1, REPAIRED THE CROSSBEAM. MAJOR REPAIR IAW GMM 6-2-100.Aug 22, 2019 · N655FE · Airbus A300F4605R · Fuselage Main, Structure
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