N722FD

Service difficulty reports · 191

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 = 'N722FD' 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 FDEA201104281666Spar Cap · crackedCRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON THE CTR WING BOX CTR SPAR, AT RT CUT-OUT DOUBLE RUN OUT LT UPPER HOLE FIRST LAYER AT 12 O' CLOCK POSITION LOOKING FORWARD. REPAIRED AS PER EA 6-5710-150318. REPAIR CLASSIFIED AApr 28, 2011 · N722FD · Airbus A300B4622R · Wing SparSDR FDEA201104281665Spar Cap · crackedCRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON THE CTR WING BOX CTR SPAR, AT RT CUT-OUT DOUBLE RUN OUT LT UPPER HOLE SECOND LAYER AT 12 O' CLOCK POSITION LOOKING FORWARD. REPAIRED AS PER EA 6-5710-150318 PART 1. REPAIR CLASSApr 28, 2011 · N722FD · Airbus A300B4622R · Wing SparSDR FDEA201104281664Spar Cap · crackedCRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSP ON THE CTR WING BOX CTR SPAR, AT LT CUT-OUT DOUBLE RUN OUT RT UPPER HOLE SECOND LAYER AT 12 O' CLOCK POSITION LOOKING FWD. REPAIRED AS PER EA 6-5710-150318 PART 1. REPAIR CLASSIFIED AS MApr 28, 2011 · N722FD · Airbus A300B4622R · Wing SparSDR FDEA201104281663Spar Cap · crackedCRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSP ON THE CTR WING BOX CENTER SPAR, AT LT CUT-OUT DOUBLE RUN OUT UPPER HOLE SECOND LAYER AT 6 O' CLOCK POSITION LOOKING FWD. REPAIRED AS PER EA 6-5710-150318 PART 1. REPAIR CLASSIFIED AS Apr 28, 2011 · N722FD · Airbus A300B4622R · Wing SparSDR FDEA201104281662Skin · dentedRT FUSELAGE SKIN EXTERIOR SURFACE BETWEEN FRAME 48 TO FRAME 49A AND BETWEEN STRINGER 34 TO STRINGER 36 FOUND DENTED. REPAIRED AS PER EA 6-5310-149619 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 112.Apr 28, 2011 · N722FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA201104281661Skin · dentedFUSELAGE EXTERNAL SKIN BETWEEN FRAME 52 TO FRAME 53A, STRINGER 39 FOUND WITH SMALL DENT. REWORKED AND TRACKING REQUIRED AS PER EA 6-5310-149620 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 112.Apr 28, 2011 · N722FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA201104281660Skin · misrepairedLT FUSELAGE SKIN BETWEEN FRAME 40 AND FRAME 41 AT STRINGER 39 TO STRINGER 40 EXTERNAL SURFACE FOUND WITH SKIN REWORKED. REWORKED AS PER EA 6-5310-149618 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 112.Apr 28, 2011 · N722FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA201104261628Bracket · crackedCRACK INDICATION FOUND APPROXIMATELY 0.2 INCH IN LEGTH DURING HIGH FREQUENCY EDDY CURRENT INSPECTION ON CENTER HINGE OF RIGHT WING NR 1 SPOILER INBOARD LUG. RIGHT WING NR 1 SPOILER CENTER HINGE BRACKET REMOVED AND REPLACED AS PER EO 6-5710-7-3307 EOCN 04 PART Apr 26, 2011 · N722FD · Airbus A300B4622R · Wing, Control Surface Attach FittingsSDR FDEA201104261627Bracket · crackedCRACK INDICATION FOUND APPROXIMATELY 0.2 INCH IN LEGTH DURING HIGH FREQUENCY EDDY CURRENT INSPECTION ON CENTER HINGE OF LEFT WING NR 1 SPOILER OUTBOARD LUG. LEFT WING NR 1 SPOILER CENTER HINGE BRACKET REMOVED AND REPLACED AS PER EO 6-5710-7-3307 EOCN 04 PARTApr 26, 2011 · N722FD · Airbus A300B4622R · Wing, Control Surface Attach FittingsSDR FDEA201104251608Crossbeam · corrodedFORWARD CARGO COMPARTMENT CROSS BEAM AT FRAME 27, Y = 40, -Z = 26 FOUND SURFACE CORROSION ALONG FASTENERS AREA. REPAIRED AS PER E.A. 6-5310-150313 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 112.Apr 25, 2011 · N722FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR FDEA201104251607Crossbeam · corrodedFORWARD CARGO COMPARTMENT CROSS BEAM AT FRAME 25, Y = 40, -Z = 26 FOUND SURFACE CORROSION ALONG FASTENERS AREA. REPAIRED AS PER E.A. 6-5310-150312 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 112.Apr 25, 2011 · N722FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR FDEA201104251605Sill · misrepairedREPAIR AT AFT CARGO COMPARTMENT ENTRY AREA DOOR SILL BETWEEN FRAME 62 AND FRAME 63. REPAIR EVALUATED AND FOUND FASTENERS NOT INSTALLED PER APPROVED DATA. REPAIRED AS PER E.A. 6-5310-143890 PART 1 & E.O. 6-5100-7-5000C2 PART 1. REPAIR CLASSIFIED AS MAJOR PEApr 25, 2011 · N722FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201104231597Floor Support · corrodedMAIN DECK FWD UTILITY AREA, FLOOR BETWEEN FRAME 12 AND FRAME 13 LT APPROX Y700, SUPPORT STRUCTURE FOUND CORROSION. SUPPORT STRUCTURE ON MAIN DECK FORWARD UTILITY AREA FLOOR BETWEEN FRAME 12 AND FRAME 13 LEFT HAND APPROXIMATELY Y = 700, REMOVED AND REPLACED AApr 23, 2011 · N722FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201104231596Seat Track · corrodedMAIN DECK FWD UTILITY AREA, FLOOR SEAT TRACK ALONG Y -450 BETWEEN FRAME 18 AND FRAME 19 CORROSION FOUND ON CROWN. MAIN DECK FORWARD UTILITY AREA, FLOOR SEAT TRACK ALONG Y -450 BETWEEN FRAME 18 AND FRAME 19 REMOVED AND REPLACED AS PER SRM 51-40-21 REVISION 75.Apr 23, 2011 · N722FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201104231595Seat Track · corrodedMAIN DECK FWD UTILITY AREA, SEAT TRACK ALONG Y 450 BETWEEN FRAME 16 AND FRAME 19 CORROSION FOUND ON CROWN. MAIN DECK FORWARD UTILITY AREA, SEAT TRACK ALONG Y 450 BETWEEN FRAME 16 AND FRAME 19 REMOVED AND REPLACED AS PER SRM 51-40-21 REVISION 75. REPAIR CLASApr 23, 2011 · N722FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201104231594Seat Track · corrodedMAIN DECK FWD UTILITY AREA, FLOOR SEAT TRACK ALONG Y 953 BETWEEN FRAME 16 AND FRAME 19 CORROSION FOUND ON CROWN. MAIN DECK FORWARD UTILITY AREA, FLOOR SEAT TRACK ALONG Y 953 BETWEEN FRAME 16 AND FRAME 19 REMOVED AND REPLACED AS PER SRM 51-40-21 REVISION 75.Apr 23, 2011 · N722FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201104141480Frame · crackedDURING ACCOMPLISHMENT OF WORK CARD E6-5310-7-5013C PART 1, FUSELAGE FRAME NR 47 LT RADIUS FITTING FOUND CRACKED. REPAIRED AS PER E.O. 6-5310-7-5013C PART 1 &, SERVICE BULLITINS A300-53-6029 R08 AND A300-53-6144 R01. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-10Apr 14, 2011 · N722FD · Airbus A300B4622 · Fuselage Main, FrameSDR FDEA201104141477Mount · corrodedNR 2 PYLON ENGINE FWD MOUNT LT FWD BOLT HOLE FOUND WITH CORROSION. REPAIRED AS PER E.A. 6-5450-150314 PART 1. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REVISION 112.Apr 14, 2011 · N722FD · Airbus A300B4622R · Engine Mount SectionSDR FDEA201104141479Mount · corrodedNR 2 PYLON ENG AFT MOUNT LT FWD BOLT HOLE FOUND WITH CORROSION. REWORKED AS PER E.A. 6-5450-143900 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 112.Apr 14, 2011 · N722FD · Airbus A300B4622R · Engine Mount SectionSDR FDEA201104141478Mount · corrodedNR 2 PYLON ENGINE FWD MOUNT LT AFT BOLT HOLE FOUND WITH CORROSION. REPAIRED AS PER E.A. 6-5450-150314 PART 1. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REVISION 112.Apr 14, 2011 · N722FD · Airbus A300B4622R · Engine Mount SectionSDR FDEA201104141476Mount · corrodedNR 2 PYLON ENGINE AFT MOUNT LT AFT BOLT HOLE FOUND WITH CORROSION. REWORKED AS PER E.A. 6-5450-143900 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 112.Apr 14, 2011 · N722FD · Airbus A300B4622R · Engine Mount SectionSDR FDEA201104141475Window Frame · crackedONE CRACK FOUND ON LEFT FUSELAGE INTERNAL STRUCTURE FROM FRAME 2 TO 4 WINDSHIELD FRAME LOWER SECTION AT FASTENER HOLE NR 10 AFT SIDE DURING EDDY CURRENT ROTATING PROBE TEST PER NTM53-11-01. LEFT FUSELAGE INTERNAL STRUCTURE FROM FRAME 2 TO 4 WINDSHIELD FRAMEApr 14, 2011 · N722FD · Airbus A300B4622R · Fuselage Main, StructureSDR FDEA201104131464Stiffener · crackedPYLON NR 2, STIFFENER END BETWEEN RIB 6 AND RIB 7 FOUND CRACKED INDICATION APPROX 0.1 INCH DURING HIGH FREQUENCY EDDY CURRENT INSP. REPAIRED AS PER E.A. 6-5450-150310 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 112.Apr 13, 2011 · N722FD · Airbus A300B4622R · Nacelle/Pylon Miscellaneous StructureSDR FDEA201104051316Skin · misrepairedREPAIR DOUBLER FOUND AT FUSELAGE BELLY SKIN NEAR JACKPAD FRAME 87, STR 45. EVALUATED AND FOUND NOT INACCORDANCE WITH ANY REPAIR DATA. CARRIED OUT REPAIR AS PER SRM 53-10-12 FIGURE 225 REVISION 75. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 112.Apr 5, 2011 · N722FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA201103291241Fitting · crackedDURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSP ON FRAME 47 SPLICE FITTING BETWEEN STRINGER 24 AND STRINGER 26 IAW SB A300-53-6123R04, HOLE 'J' FOUND CRACKED. REPAIRED CARRIED OUT AS PER EO 6-5310-7-5017 A5 PART 5, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-1Mar 29, 2011 · N722FD · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA201103291240Fitting · crackedDURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSP ON FRAME 47 SPLICE FITTING BETWEEN STRINGER 24 AND STRINGER 26 IAW SB A300-53-6123R04, HOLE 'F' FOUND CRACKED. REPAIRED CARRIED OUT AS PER EO 6-5310-7-5017 A5 PART 5, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-10Mar 29, 2011 · N722FD · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA200909073265Door · missingACFT ARRIVED, MISSING MLG DOOR FAIRING. RELEASED FOR SERVICE IAW CDL: 52-13 CATEGORY: N CDL ITEM "CDL 52-13: MLG DOOR PANEL 732 - MISSING. REFER TO CDL 52-13 FOR RESTRICTIONS. ACFT RESTRICTED FROM OPERATING INTO KNOWN OR FORECAST ICING CONDITIONS."Sep 7, 2009 · N722FD · Airbus A300B4622R · Landing Gear DoorsSDR FDEA200812025039Skin · corrodedAFT CARGO DOOR INTERNAL SKIN CORRODED AT FWD LWR CORNER. THIS SDR IS GEN TO REFLECT CORRECTIONS MADE IN CORRECTIVE ACTION BLOCK FROM ORIG SDR 08-4756. REMOVED CORROSION IAW A300-600 SRM 51-74-10. FOUND TO BE OUT OF LIMITS IAW A300-600 SRM 51-30-00. ORIGINADec 2, 2008 · N722FD · Airbus A300B4622R · Cargo/Baggage DoorsSDR FDEA200811264988Rib · crackedLEFT WING RIB 5; HOLE "O" HAS A CRACK INDICATION. COMPLIED WITH FEDEX EA 6-5710-123674, WINGS, AD 99-16-01 - EO 6-5710-7-5005, LT WING REAR SPAR, RIB 5 FITTING BOLT HOLE "G", "I", "M", AND "O".Nov 26, 2008 · N722FD · Airbus A300B4622R · Wing, Rib/BulkheadSDR FDEA200811264987Rib · crackedLEFT WING RIB 5; HOLE "M" HAS A CRACK INDICATION. COMPLIED WITH FEDEX EA 6-5710-123674, WINGS - AD 99-16-01 - E.O. 6-5710-7-5005, LT WING REAR SPAR, RIB 5 FITTING BOLT HOLE "G", "I", "M" AND "O". ORGINAL EA IS ATTACHED TO SNRM N00846.Nov 26, 2008 · N722FD · Airbus A300B4622R · Wing, Rib/BulkheadSDR FDEA200811264986Rib · crackedLEFT WING RIB 5; HOLE "I" HAS A CRACK INDICATION. COMPLIED WITH FEDEX EA 6-5710-123674 WINGS, AD 99-16-01 - EO 6-5710-7-5005, LT WING REAR SPAR, RIB 5 FITTING BOLT HOLE "G", "I", "M", AND "O". ORIGINAL EA ATTACHED TO SNRM N00846.Nov 26, 2008 · N722FD · Airbus A300B4622R · Wing, Rib/BulkheadSDR FDEA200811264985Rib · crackedLEFT WING RIB 5; HOLE "G" HAS A CRACK INDICATION. COMPLIED WITH FEDEX EA 6-5710-123674 WINGS - AD 99-16-01 - EO 6-5710-7-5005 - LT WING REAR SPAR, RIB 5 FITTING BOLT HOLE "G", "I", "M", AND "O". ORIGINAL EA ATTACHED TO SNRM N00846.Nov 26, 2008 · N722FD · Airbus A300B4622R · Wing, Rib/BulkheadSDR FDEA200811264984Fitting · crackedRIGHT WING RIB 5; HOLE "L" SHOWS A CRACK INDICATION APPROX , WINGS - AD 99-16-01 EO 6-5710-7-5005-RT WING REAR SPAR, RIB 5 FITTING BOLT HOLE "L".Nov 26, 2008 · N722FD · Airbus A300B4622R · Wing Miscellaneous StructureSDR FDEA200811264982Fitting · crackedLEFT WING HOLE " D " OF EO 6-5710-7-5005 P1 SHOWS A CRACK INDICATION APPROX 1/16 LONG. COMPLIED WITH FEDEX EA 6-5710-123673, WINGS - AD 99-16-01 - EO 6-5710-7-5005 - LT WING REAR SPAR, MLG FWD PICK-UP FITTING BOLT HOLE "D".Nov 26, 2008 · N722FD · Airbus A300B4622R · Wing SparSDR FDEA200811264980Rib · damagedRIGHT WING RIB 5; HOLE "E", THE EXISTING HOLE SIZE IS LARGER THAN THE FINAL HOLE SIZE CALLED OUT IN FEDEX EO 6-5710-7-5005 P1. COMPLIED WITH FEDEX EA 6-5710-123672, WINGS - AD 99-16-01 - EO 6-5710-7-5005, RT WING REAR SPAR MLG FWD PICK-UP FITTING BOLT "E".Nov 26, 2008 · N722FD · Airbus A300B4622R · Wing, Rib/BulkheadSDR FDEA200811255074Skin · crackedRT WING LWR SKIN CRACKED APPROX 3/16 INCH BEYOND PREVIOUS STOP PLUG REPAIR. CRACK IS PROGRESSING AFT TOWARD FASTENER HOLE NR 19 AND TRANSITION RADIUS BETWEEN RIBS 8 AND 9. COMPLIED WITH EA 6-5730-123509 PART 1, WINGS CRACK IN RT BOTTOM SKIN AT FRONT SPAR, 63Nov 25, 2008 · N722FD · Airbus A300B4622R · Wing, Plate/SkinSDR 08FDEA04772Skin · crackedLT WING INBD FLAP AT RIB 25A, UPPER SKIN IS CRACKED. FABRICARED SKIN P/N A57960007200 & DOUBLER P/N A57960007202 IN REF TO FEDEX EA 6-5750-123671.Nov 6, 2008 · N722FD · Airbus A300B4622R · Trailing Edge FlapsSDR 08FDEA04757Skin · corrodedAFT CARGO DOOR INTERIOR SKIN IS CORRODED AT THE AFT LOWER CORNER. REMOVED CORROSION IAW SRM 51-74-01. FOUND TO BE OUT OF LIMITS IAW SRM 52-30-00. ORIGINAL MATERIAL 0.063. REMAINING MATERIAL 0.052. MATERIAL REMOVED 0.011. THE SKIN WAS REPLACED ON WORK CNov 5, 2008 · N722FD · Airbus A300B4622R · Cargo/Baggage DoorsSDR 08FDEA04686Floor Panel · delaminatedBULK PIT FLOOR PANEL IS DELAMINATED. REMOVED PANEL IAW AMM 53-10-35-4. FABRICATED NEW PANEL IAW FEDEX DWG SRZ 25-005. FABRICATED TOP SHEET IAW DWG SRZ 25-011. PART MARKED IAW GMM 7-0-1000. INSTALLED PANEL IAW AMM 53-10-35-4.Nov 3, 2008 · N722FD · Airbus A300B4622R · Fuselage Floor PanelSDR 08FDEA04685Floor Panel · delaminatedBULK PIT FLOOR PANEL IS DELAMINATED. REMOVED PANEL IAW AMM 53-10-35-4. FABRICATED NEW PANEL IAW DWG SRZ 25-005. FABRICATED TOP SHEET IAW DWG SRZ 25-011. PART MARKED IAW GMM 7-0-1000. INSTALLED PANEL IAW AMM 53-10-35-4.Nov 3, 2008 · N722FD · Airbus A300B4622R · Fuselage Floor PanelSDR 08FDEA04684Floor Panel · delaminatedBULK CARGO FLOOR PANEL IS DELAMINATED. REMOVED PANEL IAW AMM 53-10-35-4. FABRICATED NEW PANEL IAW DWG SRZ 25-005. FABRICATED TOP SHEET IAW DWG SRZ 25-011. PART MARKED IAW GMM 7-0-1000. INSTALLED PANEL IAW AMM 53-10-35-4.Nov 3, 2008 · N722FD · Airbus A300B4622R · Fuselage Floor PanelSDR 08FDEA04683Floor Panel · delaminatedBULK CARGO FLOOR PANEL IS DELAMINATED. REMOVED PANEL IAW AMM 53-10-35-4. FABRICATED NEW PANEL. FABRICATED TOP SHEET IAW DWG SRZ 25-011. PART MARKED IAW GMM 7-0-1000. INSTALLED PANEL IAW AMM 53-10-35-4.Nov 3, 2008 · N722FD · Airbus A300B4622R · Fuselage Floor PanelSDR 08FDEA04682Floor Panel · delaminatedBULK CARGO FLOOR PANEL IS DELAMINATED. REMOVED PANEL IAW AMM 53-10-35-4. FABRICATED NEW PANEL. FABRICATED TOP SHEET IAW DWG SRZ 25-011. PART MARKED IAW GMM 7-0-1000. INSTALLED PANEL 161 BF IAW AMM 53-10-35-4.Nov 3, 2008 · N722FD · Airbus A300B4622R · Fuselage Floor PanelSDR 08FDEA04681Floor Panel · delaminatedBULK CARGO FLOOR PANEL IS DELAMINATED. REMOVED PANEL IAW AMM 53-10-35-4. FABRICATED NEW PANEL. FABRICATED TOP SHEET IAW DWG SRZ 25-011. PART MARKED IAW GMM 7-0-1000. INSTALLED PANEL IAW AMM 53-10-35-4.Nov 3, 2008 · N722FD · Airbus A300B4622R · Fuselage Floor PanelSDR 08FDEA04680Floor Panel · delaminatedBULK CARGO FLOOR PANEL IS DELAMINATED. REMOVED PANEL IAW AMM 53-10-35-4. FABRICATED NEW PANEL. FABRICATED TOP SHEET IAW DWG SRZ 25-011. PART MARKED IAW GMM 7-0-1000. INSTALLED PANEL IAW AMM 53-10-35-4.Nov 3, 2008 · N722FD · Airbus A300B4622R · Fuselage Floor PanelSDR 08FDEA04679Floor Panel · puncturedBULK CARGO FLOOR PANEL DELAMINATED AND PUNCTURED. REMOVED PANEL IAW AMM 53-10-35-4. FABRICATED NEW PANEL. FABRICATED IAW DWG SRZ 25-005. PART MARKED IAW GMM 7-0-1000. INSTALLED PANEL IAW AMM 53-10-35-1.Nov 3, 2008 · N722FD · Airbus A300B4622R · Fuselage Floor PanelSDR 08FDEA04678Floor Panel · delaminatedBULK CARGO FLOOR PANEL IS DELAMINATED AND PUNCTURES. REMOVED PANEL IAW AMM 53-10-35-4. FABRICATED A NEW PANEL IAW FEDEX DWG SRZ 25-005. PART MARKED IAW GMM 7-0-1000.Nov 3, 2008 · N722FD · Airbus A300B4622R · Fuselage Floor PanelSDR 08FDEA04707Web · crackedLEFT WING INBD FLAP AT RIB 25A, WEB PLATE IS CRACKED. REMOVED AND REPLACED THE -220 WEB PLATE IN REF TO A300-600 SRM 51-40-21; PARA 7; PARA 14 AND FOKKER DWG A57960114, ISSUE E.Oct 31, 2008 · N722FD · Airbus A300B4622R · Trailing Edge FlapsSDR 08FDEA04706Web · crackedLEFT WING INBD FLAP AT RIB 25A THE WEB PLATE IS CRACKED. REMOVED AND REPLACED -218 WEB PLATE IN REF TO A300-600 SRM 51-40-21, PARA 7, PARA 14 AND FOKKER DWG A57960114, ISSUE E.Oct 31, 2008 · N722FD · Airbus A300B4622R · Trailing Edge FlapsSDR 08FDEA04648Web · damagedLEFT WING INBD FLAP AT RIB 25A, WEB PLATE IS CRACKED AND MISDRILLED. REMOVED & REPLACED THE WEB PLATE IN REF TO SRM 51-40-21& DWG A57960114.Oct 31, 2008 · N722FD · Airbus A300B4622R · Trailing Edge Flaps
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