N656FE

Service difficulty reports · 243

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 = 'N656FE' 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 FDEA201310302654Rib · corrodedRT MLG RIB 5 CORROSION ON FWD LUG RT MLG RIB 5 CORROSION REMOVED AND BUSHES INSTALLED IAW REPAIR SCHEME R572-40425 AND EA 6-5710-T0303150.Oct 30, 2013 · N656FE · Airbus A300F4605R · Wing, Rib/BulkheadSDR FDEA201310302653Rib · corrodedLEFT MLG RIB 5 CORROED ON FWD LUG LT MLG RIB 5 CORROSION. REMOVED AND BUSHES INSTALLED IAW REPAIR SCHEME R572-40425 AND EA 6-5710-T0303149.Oct 30, 2013 · N656FE · Airbus A300F4605R · Wing, Rib/BulkheadSDR FDEA201310302652Door Frame · chafedAFT CARGO DOOR CUTOUT FORWARD LOWER FRAME SKIN SECTION HAS CHAFE DAMAGE. REPAIR CARRIED OUT IAW EA 6-5317-T03033344 AND RDAS 70584162/003/2013.Oct 30, 2013 · N656FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA201310302651Rib · corrodedRT WING, RIB 5 AFT LUG BUSH SHOWS EVIDENCE OF MIGRATION AND CORROSION. RT WING RIB 5 CORROSION REMOVED, NEW BUSHINGS INSTALLED IAW REPAIR INSTRUCTION R572-40425 AND EA 6-5710-T0303150.Oct 30, 2013 · N656FE · Airbus A300F4605R · Wing, Rib/BulkheadSDR FDEA201310292643Adapter · wornEVIDENCE OF WEAR ON CENTER FLANGE OF ADAPTER AT FRAME 27 BETWEEN Y1456 AND Y1959. DAMAGE REMOVED IAW SRM 51-23-10. ADAPTER PLATE REPLACED IAW SRM 51-40-21 AND DWG A53781920 .Oct 29, 2013 · N656FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201310292642Adapter · corrodedEVIDENCE OF CORROSION ON CENTER FLANGE OF ADAPTER AT FRAME 61 BETWEEN Y1456 AND Y1959. CORROSION REMOVED IAW SRM 51-40-21. ADAPTER PLATE REPLACED IAW SRM 51-40-21 AND DWG A53278286 .Oct 29, 2013 · N656FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201310292639Floorboard · damagedFLOORBOARD DAMAGED AT POSITION 9L. REPLACED FLOORBOARD FABRICATED IAW REPAIR SHEET SRZ-25-005. INSTALLED IAW 53-10-25.Oct 29, 2013 · N656FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201310292636Floor Panel · damagedFLOOR PANEL 242BF FOUND DAMAGED AT PANEL EDGE. FLOOR PANEL FABRICATED AND REFITTED IAW AMM 53-10-20/ REPAIR SHEET.Oct 29, 2013 · N656FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201310232599Skin · gougedFORWARD CARGO DOOR CUTOUT EDGE AND SKIN DAMAGE FOUND AT FORWARD LOWER CORNER FUSELAGE SKIN FRAMES 20-20A, S40-41R. BLENDED IAW SRM 53-13-12, FIG 109. FOUND TO BE OUT OF LIMITS. MAX DEPTH 1.44 MM LIMIT 1.0MM. REPAIR CARRIED OUT IAW EA 6-5314-T0303277.Oct 23, 2013 · N656FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA201310222585Skin · chafedAFT CARGO DOOR CUTOUT AFT FRAME UPPER SECTION HAS SKIN FRAME CHAFE DAMAGE. FUSELAGE SKIN FRAME 63A-64A, STG 27-STG 28R. BLENDED IAW SRM 53-17-12, FIG 104, SHEET 5. FOUND TO BE WITHIN LIMITS MAX DEPTH 0.4MM LIMIT 1.0MM SRM REQUIREMENT TO CARRY OUT INSPECTION Oct 22, 2013 · N656FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA201310222584Skin · gougedFORWARD CARGO DOOR CUTOUT EDGE AND SKIN, DAMAGE FOUND AT AFT LOWER CORNER FUSELAGE SKIN FRAMES 25A - 26, STR 39-42R. BLENDED IAW SRM 53-13-12, FIG 109. FOUND TO BE WITHIN LIMITS MAX DEPTH 0.24MM LIMIT 1MM.Oct 22, 2013 · N656FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA201310202563Skin · dentedLT WING CENTER FLAP TOP SKIN DAMAGED. REPAIRED IAW SRM 57-50-00, FIG 205.Oct 20, 2013 · N656FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA201310202562Skin · dentedLT WING CENTER FLAP DAMAGED. REPAIRED IAW SRM 57-50-00, FIG 208.Oct 20, 2013 · N656FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA201301170118O-Ring · leakingKRUGER NOT RETRACTED IN FLIGHT. REACTIVATED KRUEGER FLAP CONTROL REF AMM27-87-00-09. FOUND UNION ON RT NOTCH ACT LEAKING, TIGHTENED AND WAS NO HELP. R & R O-RING ON UNION, AND LEAKED CHECK GOOD. PERFORMED OPS CHECK OF SLAT SYS, REF AMM27-84-00. OK FOR SERJan 17, 2013 · N656FE · Airbus A300F4605R · Leading Edge Slat Control SystemSDR FDEA201301150098Warning Light · false activationON LEVEL OFF AT F320, NOTICED ENGINE NR 2 EGT HAD EXCEEDED LIMITS. EXCEEDANCE POINTER INDICATES 1050: ENG LIMITS N1 93.1, EGT 669, N2 97.9, OIL QTY 14.0 COMPLIED WITH QRH, LT THRUST AT IDLE. DID NOT NOTICE WHEN EGT EXCEEDED LIMITS. DFDR WAS DOWNLOADED ON Jan 15, 2013 · N656FE · Airbus A300F4605R · Engine Indicating SystemSDR FDEA201210173638Gcu · inoperativeON POWER UP FOR TAKEOFF STANDARD POWER SET LOST ALL EQPT ON AC BUSS NR 2 AND ALL F/O INSTRUMENTS. REJECTED TAKEOFF. SWAPPED APU'S GEN CONTROLLER UNIT(GCU) WITH NR 2 GCU, REF 24-22-12-04. RAN NR 2 ENG IAW JRH , NR 2 GEN OPS CHECKS NORMAL. R/I FROM FACT SWAOct 17, 2012 · N656FE · Airbus A300F4605R · AC Generator-AlternatorSDR FDEA201205111796Seat Track · corrodedFRAMES 20 - 26, SEAT TRACK 4L HAS FOUR GOUGES, FOUR SQUARE INCHES AND CHANNEL CORRODED THREE SPOTS, FOUR SQUARE INCHES. BLENDED CORROSION IAW SRM 51-74-10. CHECK LIMITS 1 EA AREA OUT OF LIMITS IAW SRM 53-10-16, FIG 102. REPAIRED AREA IAW EA 6-5310-157835. REMay 11, 2012 · N656FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201205111795Seat Track · corrodedFRAMES 19 - 26, SEAT TRACK 5L SCALLOP HAS GOUGES FOUR, TWO SQUARE INCHES AND CHANNEL CORRODED ONE SQUARE INCH. SMOOTHED AND BLENDED AREAS IAW SRM 51-73-10, CHECKED AND FOUND OUT OF LIMITS IAW SRM 53-10-16, FIG 102. REPAIRED SEAT TRACK IAW EA 6-5310-157835.May 11, 2012 · N656FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201205091776Angle · corrodedFWD CARGO BAY AT OVER HEAD FRAME 21 CEILING PANEL LAND BELOW SEAT TRACK 3L HAS .5" SQ" OF CORROSION AT FASTENER HOLE REMOVED CORROSION IAW SRM 51-74-10. AREA IS OUT OF LIMITS IAW A53781917 AND DAN11304. REPAIRED AREA IAW EA 6-5310-157838. REPROTECTED AREASMay 9, 2012 · N656FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201205091775Skin · gougedRT WING NR 1 SLAT LWR SURFACE 40" FROM OTBD AND .5" FWD OF T/E HAS .7" X 2" X .125 " DEPTH GOUGE. REPAIRED DAMAGE USING THE FILLER INSERT AND DOUBLER PATCH PLATE METHOD IAW EA 6-5750-157840, REF WRI 57504690.May 9, 2012 · N656FE · Airbus A300F4605R · Leading Edge DevicesSDR FDEA201205091773Skin · crackedNR 1 ENGINE AFT PYLON LOWER HORIZONTAL SKIN BETWEEN RIB 18 & 19 HAS 2 EA 1" CRACKS EXTENDING FROM HYD DRAIN PASS THRU FITTING. REMOVED AND REINSTALLED HYD PASS THRU FITTINGS & LINES TO FOM IAW AMM 29-00-00-04. R & R CRACKED WEB SUPPORT IAW SRM 51-40-21. REMay 9, 2012 · N656FE · Airbus A300F4605R · Nacelle/Pylon, Plate/SkinSDR FDEA201205091772Cargo Track · corrodedMAIN DECK CARGO TRACK 4L HAS 6 EA AREAS OF CORROSION BETWEEN FRAMES 31 AND 38 TOTAL DEFECT 4 SQ". AFTER REMOVAL OF LEVEL 1 CORROSION ON SEAT TRACK 4L IT WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16. R & R CARGO TRACK SECTION IAW SRM 53-10-16. REPROTECTEDMay 9, 2012 · N656FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201205071759Frame · crackedRIGHT MAIN DECK CARGO FRAME 24, BENT AT SPLICE AND MISSING ONE FASTENER BETWEEN STR 8R AND 9R DEFECT MEASURES 2.5 INCHES LONG. AFTER REMOVAL OF FASTENERS AND REFORMING BENT SPLICE IAW SRM 51-40-21, AND SRM 51-26-00 PG 1, NDT VERIFIED A 2 INCH CRACK IN PREVMay 7, 2012 · N656FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA201205051751Floor Support · damagedFLOORBOARD HOLES MISDRILLED THRU REPAIR TRACK AND THRUST PLATE. R & R THRUST PLATE FR 29-30 RT SEAT TRACK 3R IAW FSRM 51-40-21 PARA 6 AND 7. FABBED THRUST PLATE AT BETWEEN FR 29-30 AT SEAT TRACK 3R IAW DWG 10-A537-81894. TOP COATED THRUST PLATE AND FASTENERS May 5, 2012 · N656FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201205051750Bracket · corrodedFLOOR THRUST BRACKET BETWEEN FR 26 AND FR 27 UPPER SURFACE CORRODED 3 SQUARE INCHES BETWEEN SEAT TRACKS 4R AND 5R. REMOVED CORROSION IAW SRM 51-74-10, PARA 5, FOUND TO BE BEYOND LIMITS IAW DWG A53781984 AND TOLERANCES IAW ABS 5044 AND SRM 51-73-11 PARA 16. May 5, 2012 · N656FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201205051749Seat Track · corrodedSEAT TRACK 3R OTBD FLANGE HAS CORROSION AROUND BOLT HOLE 2 INCHES LONG AT FR 28, FABRICATED, LOCATED, AND DRILLED SEAT TRACK 3R IAW SRM 53-10-16. INSTALLED SEAT TRACK IAW SRM 53-10-16. TOP COATED FASTENERS ON SEAT TRACK 3R FR 27 THRU 31 IAW SRM 51-75-10.May 5, 2012 · N656FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201205041739Skin · chafedRIGHT WING INBD FLAP TOP SIDE MIDDLE FWD AREA HAS 2 EA .75 SQUARE INCH CHAFED AREAS WITH BARE METAL SHOWING. REPAIRED RT INBD FLAP UPPER SURFACE AT RIBS 14 TO 17 STR 2.1 TO 2.2 IAW FSRM 57-50-00, FIG 206.May 4, 2012 · N656FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA201205041737Skin · damagedLT WING CENTER FLAP TOP SKIN HAS AN EXISTING REPAIR DOUBLER WITH GOUGES. REMOVED DOUBLER IAW SRM 51-40-21 ID MATERIAL AS PO 13-11130 2024T3 CLAD .056 IAW FSRM 51-31-02. LOCATED AND DRILLED DOUBLER IAW FSRM 57-50-00. ALODINED AND PRIMED AND TOPCOATED IAW FSRM May 4, 2012 · N656FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA201205041735Skin · dentedLT WING CENTER FLAP L/E 7.5" FROM OTBD EDGE HAS DENT THAT MEASURES APPROX 3.7" X 1.2" X .22" VERIFIED LT WING CTR FLAP L/E DAMAGE OUT OF LIMITS IAW FSRM 57-50-00-101. REPAIRED L/E IAW FSRM 57-50-00.May 4, 2012 · N656FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA201205031731Skin · dentedLT WING OTBD FLAP L/E TOP EXTERNAL SKIN 77.5" FROM INBD EDGE HAS A DENT MEASURING APPROX 6.0" X 14". R & R REPAIR DOUBLER IAW SRM 57-50-00-21 PARA 4H, REPROTECTED AREAS IAW SRM 51-21-10 AND 51-75-10 LT WING OTBD FLAP L/E SKIN 75.5" FROM INBD EDGE.May 3, 2012 · N656FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA201204291668Frame · crackedTAIL CONE ASSY DOOR 317AL HOLD OPEN ROD BRACKET SUPPORT WEB HAS 4 EA FASTENERS PULLING THRU SKIN. REMOVED HOLD OPEN ROD FOR FOM IAW SRM 51-40-21. REMOVED INTERNAL CLOSE OUT SKIN IAW SRM 51-40-21. UPON REMOVAL OF CLOSE OUT SKIN 3" CRACK WAS FOUND ON FR 103A BEApr 29, 2012 · N656FE · Airbus A300F4605R · Aerodynamic FairingsSDR FDEA201204281663Adapter · corrodedMAIN CABIN BETWEEN SEAT TRACK 2R & 3R AT FR62 CLEVIS ADAPTER HAS APPROX 1 SQUARE INCH EXFOLIATED CORROSION. R & R CLEVIS ADAPTER ON MDCC BETWEEN SEAT TRACKS 2R & 3R AT FR 62 IAW SRM 51-72-10.Apr 28, 2012 · N656FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201204281662Adapter · corrodedMAIN CABIN BETWEEN SEAT TRACK 2R & 3R AT FR62 CLEVIS ADAPTER HAS APPROX 1 SQ IN EXFOLIATED CORROSION. R & R CLEVIS ADAPTER ON MDCC BETWEEN SEAT TRACKS 2R & 3R AT FR 62 IAW SRM 51-72-10.Apr 28, 2012 · N656FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201204271660Plate · crackedNR 2 PYLON STRUCTURE, JUST ABOVE PANEL 423CL CUT OUT HAS LOOSE FASTENER. FOUND FISHPLATE CRACKED. R & R FISHPLATE IAW SRM 51-72-10.Apr 27, 2012 · N656FE · Airbus A300F4605R · Nacelle/Pylon Miscellaneous StructureSDR FDEA201204251585Seat Track · corrodedMAIN DECK CARGO SEAT TRACK 2R HAS THREE AREAS OF CORROSION BETWEEN FR 31-38 TOTAL. REMOVED CORROSION, MATERIAL LOSS IS .057, .052, .009. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16 PG 105 FIG 102. REMOVED SEAT TRACK IAW SRM 53-10-16. LOCATED AND DRILLED NEWLApr 25, 2012 · N656FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201204241551Bracket · corrodedMAIN DECK CARGO, BETWEEN FR 25 AND FR 26, AND BETWEEN SEAT TRACKS 5L AND 6L, THRUST PLATE HAS CORROSION AT 11 SPOTS. REMOVED AND REPLACED IAW SRM 51-72-10 PG 3 PARA E.Apr 24, 2012 · N656FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201204241570Adapter · corrodedMAIN DECK CARGO AT FR 58 CLEVIS ADAPTER BETWEEN SEAT TRACK 2R & 3R 2 EA FASTENER HOLES. UPPER AND LOWER SURFACE CORRODED AND 1 EA FLOORBOARD SCREW & INSERT NOT REMOVED. R & R CLEVIS ADAPTER AT FR 58 BETWEEN SEAT TRACK 2R & 3R IAW FSRM 51-40-21, 51-40-44, ANApr 24, 2012 · N656FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201204241564Floorboard · corrodedCARGO FLOORBOARD 161CF HAS CORROSION ON BOTTOM SIDE, ALONG EDGE. FABRICATED REPLACEMENT FLOORBOARD IAW DWGS SRZ 25-005, REJ AND SRZ 25-011, REV D.Apr 24, 2012 · N656FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201204241559Plate · corrodedMAIN DECK CARGO, THRUST PLATES, BETWEEN FR 27 AND FR29 AND BETWEEN SEAT TRACKS 3R AND 4R HAS SURFACE CORROSION AT 5 EA AREAS (TOTAL 5 SQ IN). FABRICATED AND INSTALLED 2 EA THRUST PLATES IN UPPER FUSELAGE ZONE 230 AT FR27-FR29 BETWEEN SEAT TRACKS 3R AND 4R IApr 24, 2012 · N656FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201204241545Seat Track · corrodedMAIN DECK CARGO BETWEEN FR 67 AND FR 68, SEAT TRACK 3R INBD FLANGE CORRODED (2 SQ"). REMOVED CORROSION ON SEAT TRACK 3R BETWEEN FR 61 PLUS 5" & FR 69 IAW FSRM 51-74-10. CHECKED LIMITS AND FOUND TRACK OUT OF LIMITS IAW SRM 53-10-16 FIG 201. R & R SEAT TRACK Apr 24, 2012 · N656FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201204241544Bracket · corrodedMAIN DECK CARGO FLOOR THRUST BRACKET AFT OF FR 25 BETWEEN SEAT TRACKS 5R & 6R UPPER SURFACE CORRODED 2 SQUARE INCHES (LOCATION FR 25 3 INCHES). REMOVED CORROSION FROM THRUST PLATE BETWEEN FR25 AND FR 26, BETWEEN SEAT TRACKS 5R AND 6R IAW SRM 51-74-10. FOUNApr 24, 2012 · N656FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201204241543Bracket · corrodedMAIN DECK CARGO FLOOR THRUST BRACKET BETWEEN FR26 & FR27 UPPER SURFACE CORRODED 4 SQUARE INCHES BETWEEN SEAT TRACKS 2R & 3R. REMOVED FASTENERS TO FOM IAW FSRM 51-40-21. REMOVED CORROSION IAW FSRM 51-74-10. FOUND CORROSION BLENDED OUT AREA, OUT OF TOLERANCE IAApr 24, 2012 · N656FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201204241540Thrust Plate · corrodedMAIN DECK CARGO THRUST PLATES, BETWEEN FR 27 AND FR29 AND BETWEEN SEAT TRACKS 3R AND 4R HAVE SURFACE CORROSION. FABRICATED AND INSTALLED THRUST PLATES IAW FSRM 51-72-10 AND DWG 10-A537-81984. PROTECTED PARTS AND MATING AREAS IAW SRM 51-75-10.Apr 24, 2012 · N656FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201204231524Seat Track · corrodedMAIN DECK CARGO AT FR 19 - 27 SEAT TRACK 6L HAS CORROSION & GOUGED ON SCALLOP IAW AMM 53-10-16-6. REPLACED WITH NEW SEAT TRACK IAW SRM 51-40-21 PG 1 PARA 1. A. PARA 5 AND 7.Apr 23, 2012 · N656FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201204231538Adapter · bentMAIN DECK CARGO AT FR 28 BETWEEN SEAT TRACK 2L & 3L CLEVIS ADAPTER SCALLOP IS BENT. R & R CLEVIS ADAPTER IAW FSRM 51-72-10.Apr 23, 2012 · N656FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201204231528Floorboard · damagedMAIN DECK CARGO FLOORBOARD 241DF, 3 INSERTS MISSING, FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REVJ.Apr 23, 2012 · N656FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201204221521Seat Track · corrodedMAIN DECK CARGO AT FR 27 TO FR 30 SEAT TRACK 5L FLANGE HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-10. FOUND TO BE OUT OF LIMIT IAW SRM 53-10-16 PG.105. CUT OUT AND REMOVED SEAT TRACK 5L IAW SRM 53-10-16 FIG.201A FABRICATED SEAT TRACK AND ANGLES IAW SRM 5Apr 22, 2012 · N656FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201204211517Frame · bentMAIN DECK CARGO FRAME 22 BENT BETWEEN S8-9R REPAIR. REPAIRED IAW SRM 51-72-10 AND SRM 51-40-21 PG 7 PARA 6.Apr 21, 2012 · N656FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA201204211520Seat Track · corrodedMAIN DECK CARGO SEAT TRACK NR 1 UPPER SURFACE SCALLOPS CORRODED AT FRAME 773 AND 781 AND TWO SQUARE INCHES. SEAT TRACK UPPER SURFACE SCALLOPS CORRODED 2.5 SQUARE INCHES FR 73 12. REMOVED CORROSION, FOUND TO BE WITHIN LIMITS IAW FSRF 53-10-16, FIG 102. REMOApr 21, 2012 · N656FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201204211518Structure · bentMAIN DECK CARGO FR 21, STR 8 AND 9R BENT DEFECT MEASURES INCHES AT SPLICE REPAIR. REMOVED AND RE-INSTALLED NEW FABRICATED SPLICE REPAIR AT FR 21 BETWEEN STR'S 8R AND 9R IAW SRM 51-40-21, PG 7, PAR 6.Apr 21, 2012 · N656FE · Airbus A300F4605R · Fuselage Main, Structure
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