N726FD

Service difficulty reports · 237

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 = 'N726FD' 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 FDEA201002110398Wire Harness · damagedNR 2 ENGINE OUT OF 15000 AT CLIMB POWER W/ANTI-ICE ON GOT GREEN REVERSER LIGHT WITH ACCOMPANYING ECAM PULLED BACK ABOUT .4 LIGHT WENT OUT PUSHED POWER BACK UP TO 230 AND LIGHT AND ECAM RETURNED. ACFT ENGINES INDICATED NORMAL AND ACFT FLEW NORMALLY. NO SIGNFeb 11, 2010 · N726FD · Airbus A300B4622R · Engine Exhaust System WiringSDR FDEA201002050329Wire Harness · damagedDURING CLIMBOUT PASSING 12000 FT, THE GREEN NR 2 THRUST REVERSER LIGHT CAME ON AND THE ECAM INDICATED ENGINE REVERSER UNLOCKED. COMPLIED WITH ECAM PROCEDURE AND REVERSER LIGHT EXTINGUISHED AFTER NR 2 THROTTLE WAS PULLED TO IDLE. CONTINUE QRH AND MEL REVIEW. SFeb 5, 2010 · N726FD · Airbus A300B4622R · Engine Exhaust System WiringSDR FDEA200910283715Cylinder · wornPASSING 1000 AGL GOT AN ECAM ALERT "L/G DOOR SYS FAULT" NR1 SYS (FWD PANEL) SHOWED ALL UP, NR2 SYS (OVHD PANEL) SHOWED A NOSE GEAR DOOR FAULT. THERE WAS NO BUFFET. AT 12,500 AGL 290 KTS GOT STRONG VIBRATION, SLOWED TO 250 KTS AND DESCENDED. PULLING INTO TOct 28, 2009 · N726FD · Airbus A300B4622R · Landing Gear DoorsSDR FDEA200904211368Spar · damagedCENTER WING BOX REAR SPAR FR 47 OVERSIZED HOLES. COMPLIED WITH EA 6-5710-127940.Apr 21, 2009 · N726FD · Airbus A300B4622R · Wing SparSDR FDEA200904181359Skin · crackedCENTER WING JOINT AT FRAME 40; LEFT SIDE AT THE UPPER SKIN LEVEL TENSION BOLT JUNCTION; ALL THREE FASTENER HOLES HAVE CRACK INDICATIONS. REMOVED DAMAGE BY REAMING, TREATED BARE METAL AND INSTALLED OVERSIZED BOLTS IAW EA 6-5710-127939 " WINGS, CENTER WING JOINApr 18, 2009 · N726FD · Airbus A300B4622R · Wing, Plate/SkinSDR FDEA200904081228Hinge · chafedNR 2 ENGINE INBD FAN COWL DOOR AFT HINGE FITTING, FORWARD LUG HAS A CHAFING AREA. REMOVED DAMAGE IAW EA 6-7110-127945. FOUND TO BE WITHIN LIMITS IAW EA 6-7110-127945; ORIG THICKNESS 0.800. MATERIAL LOSS 0.100. MATERIAL REMAINING 0.700. PRIMED IAW A300-600Apr 8, 2009 · N726FD · Airbus A300B4622R · Nacelle/Pylon, Main FrameSDR FDEA200904061203Support · crackedRIGHT WING T/E SUPPORT IS CRACKED ABOVE RIB 9. REMOVED FASTENERS AND BUTT STRAP IAW SRM 51-40-21; PG 22. LOCATED AND DRILLED NEW BUTT STRAP IAW SRM 51-40-21; PARA 7 AND SRM 51-40-44; PARA 3. INSTALLED BUTT STRAP IAW SRM 51-40-21; PARA 7. OPENED AND CLOSED Apr 6, 2009 · N726FD · Airbus A300B4622R · Wing Miscellaneous StructureSDR FDEA200904061202Support · crackedRIGHT WING T/E UPPER PANEL SUPPORT PLATE IS CRACKED AT RIB 9. REMOVED SUPPORT PLATE IAW SRM 51-40-21; PG 22. FORMED A NEW SUPPORT PLATE IAW DWG A57242294; MOD "B". HEAT TREATED NEW SUPPORT PLATE IAW TPS 1003, REV "A". ALODINED, PRIMED AND PAINTED NEW Apr 6, 2009 · N726FD · Airbus A300B4622R · Wing Miscellaneous StructureSDR FDEA200904061201Intercostal · crackedRIGHT WING T/E SUPPORT INTERCOSTAL IS CRACKED ABOVE THE NR 4 FLAP BEAM; RIB 16. REMOVED PANEL SUPPORT IAW SRM 51-40-21; PARA 6 AND 7. FORMED A NEW SUPPORT REF DWG A57240194; ISSUE "A". ALODINED AND PRIMED IAW SRM 51-2110 PARA 2-B AND SRM 51-23-20; PG 23. Apr 6, 2009 · N726FD · Airbus A300B4622R · Wing Miscellaneous StructureSDR FDEA200904031178Skin · gougedTHE AFT PIT DOOR FRAME CUTOUT FWD LOWER CORNER IS GOUGED. REMOVED DAMAGE IAW A300-600 SRM 51-73-12 AND WAS FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR IAW A300-600 SRM 53-17-12; FIG 202. ALODINED IAW A300-600 SRM 51-21-10. PRIMED IAW A300-600 SRM 51-21-10Apr 3, 2009 · N726FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA200904021158Skin · gougedAFT LOWER FUSELAGE, FWD FRAME OF CARGO DOOR, SKIN GOUGED AND SCORED AT FRAME 58. REMOVED INTERCOSTAL AND STRAP IAW SRM 51-40-21, PARA 8. LOCATED AND DRILLED NEW STRAP IAW SRM 51-72-10. INSTALLED INTERCOSTAL AND STRAP IAW SRM 51-40-21, PARA 5.Apr 2, 2009 · N726FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA200904011134Beam · corrodedTHE BULK CARGO DOOR, LOWER CUTOUT SHIN PLATE, HAS CORROSION BELOW THE FASTENER HOLE AT FRAMES 68 - 69. REMOVED THE CORROSION ON THE LOWER CUTOUT SKIN PLATE IAW A300-600 SRM 51-74-10. MATERIAL THICKNESS IS 0.079. MATERIAL REMOVED 0.013. MATERIAL REMAINIApr 1, 2009 · N726FD · Airbus A300B4622R · Fuselage Main, StructureSDR FDEA200903251040Bracket · damagedLEFT WING FLAP TRACK FAIRING PANEL NR 533 BB MOUNT BRACKET SAFETY WIRE HOLES ON THE LT AND RT SIDES ARE RIPPED OUT. SAFETIED LT WING FLAP TRACK FAIRING 532 BB, LT AND RT AFT ATTACHED BOLTS REF AMM 20-11-11-0 AND EA 6-5750-127936.Mar 25, 2009 · N726FD · Airbus A300B4622R · Trailing Edge FlapsSDR FDEA200903251043Bracket · damagedLEFT WING FLAP TRACK FAIRING PANEL NR 536 BB, INBD MOUNT BRACKET SAFETY WIRE HOLE IS STRIPPED OUT. SAFETIED LT WING FLAP TRACK FAIRING 536 BB, LT AND RT AFT ATTACHED BOLTS REF AMM 20-11-11-0 AND EA 6-5750-127936.Mar 25, 2009 · N726FD · Airbus A300B4622R · Trailing Edge Flap Control SystemSDR FDEA200903251042Bracket · damagedLEFT WING FLAP TRACK FAIRING PANEL NR 535 BB MOUNT BRACKET SAFETY WIRE HOLES ON THE INBD SIDE IS STRIPPED OUT. SAFETIED LT WING FLAP TRACK FAIRING 535 BB, LT AND RT AFT ATTACHED BOLTS REF AMM 20-11-11-0 AND EA 6-5750-127936.Mar 25, 2009 · N726FD · Airbus A300B4622R · Trailing Edge Flap Control SystemSDR FDEA200903251041Bracket · damagedLEFT WING FLAP TRACK FAIRING PANEL NR 534 BB MOUNT BRACKET SAFETY WIRE HOLES ON THE LT AND RT SIDES ARE RIPPED OUT. SAFETIED LT WING FLAP TRACK FAIRING 534 BB, LT AND RT AFT ATTACHED BOLTS REF AMM 20-11-11-0 AND EA 6-5750-127936.Mar 25, 2009 · N726FD · Airbus A300B4622R · Trailing Edge Flap Control SystemSDR FDEA200903251039Bracket · damagedLEFT WING FLAP TRACK FAIRING PANEL NR 533 BB MOUNT BRACKET SAFETY WIRE HOLES ON THE LT AND RT SIDES ARE STRIPPED OUT. SAFETIED LEFT WING FLAP TRACK FAIRING 533 BB, LT AND RT AFT ATTACHED BOLTS REF AMM 20-11-11-0 AND E.A. 6-5750-127936, REV "A".Mar 25, 2009 · N726FD · Airbus A300B4622R · Trailing Edge FlapsSDR FDEA200903251038Floorbeam · corrodedTHE BULK CARGO COMPARTMENT FLOOR SUPPORT BEAM AT FRAME 67 AND RBL 46 HAS CORROSION (PITTING) IN THE AREA OF THE CARGO TIE DOWN. REMOVED CORROSION IAW SRM 51-74-10; PG 1. ANGLE WAS FOUND TO BE OUT OF LIMITS. LOCATED, DRILLED AND REPLACED NUT PLATES IAW SRMar 25, 2009 · N726FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR FDEA200903241028Intercostal · bentTHE INTERCOSTAL UPPER FLANGE IS BENT AT FRAME 86 AND STRINGER 39R REMOVED INTERCOSTAL AT FRAME 86 AND STRINGER 39R IAW SRM 51-40-21; PARA 6 AND 7. INSTALLED INTERCOSTAL IAW SRM 51-40-21; PARA 6 AND 7 AND SRM 51-72-10. APPLIED CIC IAW SRM 51-23-20.Mar 24, 2009 · N726FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA200903231014Floor Support · corrodedBULK CARGO COMPARTMENT FLOOR SUPPORT BETWEEN FRAME 68 AND FRAME 69 AT STRINGER 48R HAS CORROSION AROUND FASTENER HOLE. BLENDED CORROSION IAW SRM 51-74-10 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-00. INSTALLED NEW FLOOR SUPPORT P/N A5397426300000 IAW SRM Mar 23, 2009 · N726FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA200903231015Floor Panel · crackedFLOOR PANEL 242 HK IS CRACKED. FABRICATED NEW FLOOR PANEL USING THE OLD PANEL AS A TEMPLATE. MATERIAL ID; LOCATED AND COUNTERSUNK HOLES; POTTED INSERTS; POTTED EDGES; COMPLETED CURE; SANDED; APPLIED ANTI-SKID AND PART MARKED IAW DWG SRZ 25-005; REV "H".Mar 23, 2009 · N726FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA200903231013Floor Panel · delaminatedMAIN CARGO DECK FLOORBOARD 231 CF IS SPONGY FROM FRAMES 20-22 AND LBL Y 95 - Y 120. FABRICATED NEW FLOOR PANEL 231 CF IAW DWG SRZ 25-005; REV "H".Mar 23, 2009 · N726FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA200903231012Floor Panel · delaminatedMAIN CARGO DECK FLOORBOARD 231 HF IS SPONGY FROM FRAMES 22 - 24 AND LBL Y 95 - Y 120. FABRICATED NEW FLOOR PANEL 231 HF IAW DWG SRZ 25-005; REV "H".Mar 23, 2009 · N726FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA200903190972Floor Panel · dentedBULK CARGO PIT FLOOR PANEL 161GF HAS SEVERAL DENTS ON TOP SIDE. FABRICATED PER DWG SRZ 25-005; REV "H" AND DWG SRZ 25-011; REV "C".Mar 19, 2009 · N726FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA200903180954Hinge Fitting · bentLT WING AT NR 2 SPOILER CENTER HINGE FITTING BENT. REMOVED COVER, ANGLE AND BRACKET. LOCEATED, DRILLED, DEBURRED & LOCATED BRACKET. INSTALLED BRACKET IAW SRM 51-40- 21 PG 7 & 133. ALSO SRM 51-40-44 PG 1.Mar 18, 2009 · N726FD · Airbus A300B4622R · Wing, Control Surface Attach FittingsSDR FDEA200903180948Floor Panel · damagedFWD CARGO PIT FLOOR PANEL 132QF IS BROKE IN HALF. FABRICATED FWD PIT FLOOR PANEL 132QF PER A300-600 DRW SRZ-25-005 REV G.Mar 18, 2009 · N726FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA200903160930Support Bracket · crackedNR 2 PYLON PNEUMATIC BLEED DUCT, LT SIDE LOWER END, CRACKED SUPPORT BRACKET ATTACHED TO HEAT SHIELD. WELDED CRACKED SUPPORT BRACKET IAW AEROSPATIALE DWG A36115020 AND APA 01-04- 21. REMOVED AND INSTALLED IAW A300-600 AMM 36-11-00-01.Mar 16, 2009 · N726FD · Airbus A300B4622R · Nacelle/Pylon Miscellaneous StructureSDR FDEA200903130914Rib · crackedLT INBD FLAP RIB 25A HAS APPROX .125 INCH CRACK RIB 25A - RIB 25A. REMOVED THE UPPER SKIN, DAMAGED RIB, TWO CLOSE OUT PANELS, SIX STIFFENERS, TWO RUB STRIPS AND THE T/E FLAP TIP. LOCATED, DRILLED & DEBURRED RIB. INSTALLED ALL PARTS IAW SRM 51-40-21 PG 7 &Mar 13, 2009 · N726FD · Airbus A300B4622R · Trailing Edge FlapsSDR 07FDEA04714Outflow Valve · failedOVBD FLOW EXTRACT FAN FAULT WENT OVERBOARD THEN LOST PRESSURIZATION. DECLARED EMERGENCY DIVERTED TO MEMPHIS, WARNING HORN BREAKER H60 PULLED FOR MAINT PURPOSES. FOUND VENT-EXTRACT FAN AND VALVES CNTL C/B TRIPPED. RESETT. C/B TRIPPED WHEN VENT EXTRACT SELNov 2, 2007 · N726FD · Airbus A300B4622R · Pressure Regulator/Outflow ValveSDR 07FDEA04499Rib · crackedRT INBOARD FLAP RIB 25 FOUND CRACKED REMOVED SKIN AND STRINGERS. REMOVED DAMAGED RIB 25. INSTALLED NEW RIB 25 AND RE-INSTALLED SKIN AND STRINGERS. SEALED AND PAINTED.Oct 5, 2007 · N726FD · Airbus A300B4622R · Trailing Edge FlapsSDR 07FDEA04491Rib · crackedLT WING INBOARD FLAP RIB 25 FOUND CRACKED. REPLACED FLAP RIB 25 AND RUB AND ROLLER TRACK.Oct 5, 2007 · N726FD · Airbus A300B4622R · Wing, Rib/BulkheadSDR 07FDEA03041Angle · misrepairedFOUND SEVERAL MISDRILLED/ELONGATED HOLES BETWEEN FRAME 38.1-38.2, STGR. 31, LHS. REPAIR PERFORMED BY REPLACEMENT OF ANGLE WITH BUSHING REPAIR AND INSTALLING 4, 8MM DIA HI-LOKS TOGETHER WITH TWO SKIN PANELS AND A STRINGER IAW EA 6-5314-103278 AND RAS/DABRE/700Aug 22, 2007 · N726FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 07FDEA03040Stringer · misrepairedFOUND SEVERAL MISDRILLED/ELONGATED HOLES BETWEEN FRAME 38.1-38.2, STGR 31, LHS. REPAIR PERFORMED WITH BUSHING REPAIR AND INSTALLING 4, 8MM DIA HI-LOKS IAW EA 6-5314-103278 AND RAS/DABRE/7006911/2006 ISS "A".Aug 22, 2007 · N726FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR 07FDEA03039Skin Panel · misrepairedFOUND SEVERAL MISDRILLED/ELONGATED HOLES BETWEEN FRAME 38.1-38.2, STGR 31, LHS. REPAIR PERFORMED WITH BUSHING REPAIR AND INSTALLING 4,8MM DIA HI-LOKS IAW EA 6-5314-103278 AND RAS/DABRE/7006911/2006 ISS "A".Aug 22, 2007 · N726FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR 07FDEA03037Beam · chafedCHAFING MARKS ON VERTICAL WEB OF FLAP TRACK BEAM NR 4 RT, OUTBOARD SIDE. REPAIR PERFORMED BY BLEND OUT WITH NDT INSPECTION IAW EA 6-5720-103376 AND RAS/BAE/1003599/2006 ISSUE "A".Aug 22, 2007 · N726FD · Airbus A300B4622R · Wing Main, Frame StructureSDR 07FDEA03036Beam · chafedCHAFING MARKS FOUND ON VERTICAL WEB OF FLAP TRACK BEAM 3 OUTBOARD CHANNEL LHS, BEAM 3 INBOARD CHANNEL RHS. REPAIR PERFORMED BY BLEND OUT WITH NDT INSPECTION IAW EA 6-5720-103376 AND RAS/BAE/1003599/2006 ISSUE "A".Aug 22, 2007 · N726FD · Airbus A300B4622R · Wing Main, Frame StructureSDR 07FDEA03035Beam · chafedCHAFING MARKS FOUND ON VERTICAL WEB OF FLAP TRACK BEAM 2 INBOARD CHANNEL LHS. REPAIR PERFORMED BY BLEND OUT WITH NDT INSPECTION IAW EA 6-5720-103376 AND RAS/BAE/1003599/2006 ISSUE "A".Aug 22, 2007 · N726FD · Airbus A300B4622R · Wing Main, Frame StructureSDR 07FDEA03027Skin · damagedWING BOTTOM SKIN PANEL NR 1 LT, INCOMPLETE RECORDS OF EMBODIMENT OF DRW: R572-40179 AT FWD EDGE JUST OUTBOARD OF PYLON. IN ADDITION FOUND NUMEROUS DEVIATIONS (AT HOLE 7 & 9) AND CRACK IN HOLE 23 REPAIR PERFORMED BY RE-EMBODIMENT OF DRW: R572-40179 WITH CRACK Aug 22, 2007 · N726FD · Airbus A300B4622R · Wing, Plate/SkinSDR 07FDEA03026Skin Panel · unknownFOUND OLD DOUBLER REPAIR AT FRAME 26-27, STRG 24-26 RT. THE REPAIR WAS PERFORMED IAW DRW: R537B1730-002 BUT FOUR HOLES HAVE DIA: 7, 5MM INSTEAD OF 4,8MM. REPAIR PERFORMED BY REAM UP THE DIAMETERS TO 8, 8-9, 0MM AND INSTALL FOUR SHOULDERED BUSHES IAW EA 6-5Aug 22, 2007 · N726FD · Airbus A300B4622R · Aircraft StructuresSDR 07FDEA03025Rib · chafedCHAFING MARK AT END OF RIB 6-A, OUTBOARD SIDE RT WING T/E. REPAIR PERFORMED BY BLEND IAW EA 6-5751-103339 AND RAS/BAE/1003495/2006 ISS "A".Aug 22, 2007 · N726FD · Airbus A300B4622R · Wing, Rib/BulkheadSDR 07FDEA03024Frame · corrodedCORROSION AT CROSSBEAM FRAME 87 RT AFT FACE, OUT OF LIMIT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Aug 22, 2007 · N726FD · Airbus A300B4622R · Fuselage Main, FrameSDR 07FDEA03023Frame · chafedCHAFING MARK ON THE INNER FLANGE OF FRAME 38.2 BETWEEN STRG 14-15 LT. REPAIR PERFORMED BY BLEND OUT AND INSTALLING A REPAIR ANGLE AS PER SRM 53-10-13/FIG 202 IAW EA 6-5310-103329 AND RAS/DABRE/7006981/2006 ISS "A".Aug 22, 2007 · N726FD · Airbus A300B4622R · Fuselage Main, FrameSDR 07FDEA03021Frame · chafedCHAFING MARKS ON THE INNER FLANGE OF FRAME 22 BETWEEN STRG 14-15 RT. REPAIR PERFORMED BY BLEND OUT AND INSTALLING A REPAIR ANGLE AS PER SRM53-10-13/FIG 202 IAW EA 6-5310-103329 AND RAS/DABRE/7006981/2006 ISS "A".Aug 22, 2007 · N726FD · Airbus A300B4622R · Fuselage Main, FrameSDR 07FDEA03020Structure · damagedFOUND DAMAGED HOLES (COUNTERSUNK) IAW SB A300-53-6063 AT C40-41 RT, HOLE 24, 25, 26 AND 27. REPAIR PERFORMED BY REMOVING FASTENERS, ROTO-TEST AND INSTALLING FASTENERS HL13VF10 WITH NEW COUNTERSUNK IAW EA 6-5315-103324.Aug 22, 2007 · N726FD · Airbus A300B4622R · Fuselage Main, StructureSDR 07FDEA03019Beam · damagedTOOLING MARK WAS CAUSED IN THE EDGE OF FLANGE SPAR RADIUS AT BEAM 2 RT AT FRAME 42. REPAIR PERFORMED BY SMOOTH REWORK IAW EA 6-5710-103336 AND RAS/046790/014/2006 ISS "A".Aug 22, 2007 · N726FD · Airbus A300B4622R · Wing Main, Frame StructureSDR 07FDEA03018Fitting · damagedELONGATED HOLE IN CORNER FITTING OF CENTER WING TANK, FRAME 40, RIB 1 RHS. REPAIR PERFORMED BY REAM UP THE HOLE TO FINAL DIA 14,247-14,287 MM AND SPOT FACING IAW EA 6-5710-103331 AND RAS/047032/008/2006 ISS "A".Aug 22, 2007 · N726FD · Airbus A300B4622R · Wing Main, Frame StructureSDR 07FDEA03017Structure · damagedFOUND OLD TOOLING MARKS AT GANTRIES 4 AND 5 RT AND 5 LT, FRAME 47-48. REPAIR PERFORMED WITH SMOOTH REWORK AND INSTALLING CORNER ANGLES AND STRAPS IAW EA 6-5315-103326 AND RAS: 046958/010/2006 ISS "A".Aug 22, 2007 · N726FD · Airbus A300B4622R · Fuselage Main, StructureSDR 07FDEA03016Floorbeam · misrepairedOLD TOP CAP BEAM REPAIR FRAME 63 LT NOT CONFORM TO RAS/DAHAM/11513/1999 ISS. "A". SPLICE REPAIR RENEWED IAW RAS/DAHAM/11513/1999 ISS "A".Aug 22, 2007 · N726FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR 07FDEA03015Bulkhead · damagedHOLE FOUND ON PRESSURE BULKHEAD AT FRAME 39, Y-2244, Z-1425 CLOSE TO BRACKET A534-10096-204. REPAIR PERFORMED BY TRIMMING THE PRESSURE BULKHEAD AROUND THE DAMAGED AREA AND INSTALLATION OF REPAIR DOUBLER IAW EA 6-5314-103312 AND RAS: 046974/011/2006 ISS "A".Aug 22, 2007 · N726FD · Airbus A300B4622R · Fuselage Main, BulkheadSDR 07FDEA03014Skin Panel · damagedTWO SCRATCHES ON FRAME C25 AND C27, STRG 35 LHS. REPAIR PERFORMED WITH CUTOUT OF DAMAGED SKIN AND EXTERNAL DOUBLER, INSTALLATION IAW EA 6-5315-103323 AND RAS/DABRE/7006935/2006.Aug 22, 2007 · N726FD · Airbus A300B4622R · Fuselage Main, Plate/Skin
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