N744FD

Service difficulty reports · 271

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 = 'N744FD' 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 FDEA201308181930Lug · corrodedRIB 5 RT FWD LUG BORE CORRODED, REMOVED CORROSION IAW EA 6-5750-T0301639, PT1. R & R RT MLG SUPPORT, RIB 5.Aug 18, 2013 · N744FD · Airbus A300B4622R · Wing, Attach FittingsSDR FDEA201308151892Skin · delaminatedWATER TRAPPED AREA WAS FOUND AT RH RUDDER TRAILING EDGE FASTENERS ROW 37 SCREW. OUTER SKIN CUT OUT 3.5" AND DRY THE AREA, AND PERFORMED A TAP-TEST FOR DAMAGE FREE IAW SRM 55-41-12 STEP 1. INSTALLED INNER SKIN WITH RESIN IAW SRM 51-77-10 PARAGRAPH 2 H. INSTAug 15, 2013 · N744FD · Airbus A300B4622R · Rudder, Plate/SkinSDR FDEA201308151891Skin · delaminatedWATER TRAPPED AREA WAS FOUND AT LT RUDDER T/E FASTENERS ROW NR 20 SCREW. THE OUTER SKIN CUT OUT 3.5" AND DRY THE AREA IAW SRM 55-41-12 STEP1. PERFORMED A TAP-TEST FOR DAMAGE FREE IAW SRM 55-41-12, STEP 1. INSTALLED INNER SKIN WITH RESIN IAW SRM 51-77-10, PAAug 15, 2013 · N744FD · Airbus A300B4622R · Rudder, Plate/SkinSDR FDEA201308151890Skin · delaminatedWATER TRAPPED AREA WAS FOUND AT RT RUDDER T/E FASTENERS ROW NR 19 SCREW. OUTER SKIN CUT OUT 3.5" AND DRY THE AREA IAW SRM 55-41-12, STEP 1. PERFORMED A TAP-TEST FOR DAMAGE FREE IAW SRM 55-41-12, STEP 1. INSTALLED INNER SKIN WITH RESIN IAW SRM 51-77-10, PARAug 15, 2013 · N744FD · Airbus A300B4622R · Rudder, Plate/SkinSDR FDEA201308151889Skin · delaminatedWATER TRAPPED IN LT RUDDER. THE OUTER SKIN CUT OUT 4.8" AND DRY THE AREA IAW SRM 55-41-12 STEP 1. PERFORMED A TAP-TEST FOR DAMAGE FREE IAW SRM 55-41-12, STEP 1. INSTALLED INNER SKIN WITH RESIN IAW SRM 51-77-10, PARA 2H. INSTALLED REPLACEMENT CORE AND FILLEAug 15, 2013 · N744FD · Airbus A300B4622R · Rudder, Plate/SkinSDR FDEA201308151888Skin · delaminatedWATER TRAPPED IN LT RUDDER. THE OUTER SKIN CUT OUT 4.5" AND DRY THE AREA IAW SRM 55-41-12, STEP 1. PERFORMED A TAP-TEST FOR DAMAGE FREE IAW SRM 55-41-12, STEP 1. INSTALLED INNER SKIN WITH RESIN IAW SRM 51-77-10, PARA 2H. INSTALLED REPLACEMENT CORE AND FILLAug 15, 2013 · N744FD · Airbus A300B4622R · Rudder, Plate/SkinSDR FDEA201308091816Stringer · corrodedAVIONICS BAY STRINGER CORRODED BETWEEN FRAMES 15 AND 15A, S44R. REPAIRED IAW EA 6-5310-T0301799.Aug 9, 2013 · N744FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR FDEA201308091815Seat Track · chafedAFT MAIN DECK CENTER LINE SEAT TRACK FLANGE CHAFED. CUT SEAT TRACK IAW SRM 51-27-11. PERFORMED SEAT TRACK SPLICE REPAIR IAW SRM 53-10-16, FIG 202. REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Aug 9, 2013 · N744FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201308091814Seat Track · chafedAFT MAIN DECK NR 2 SEAT TRACK FLANGE CHAFED. CUT OUT SEAT TRACK IAW SRM 51-27-11. REPAIRED IAW SRM SUPPLEMENT 53-10-16, FIG 202.3. REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Aug 9, 2013 · N744FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201208173061Indicator · failedFIRST OFFICER`S ALTIMETER INOPERATIVE, STICKS AND JUMPS CONSTANTLY TRIED FIRST OFFICER SWITCH TO CAPTAIN`S ADC, SAME PROBLEM. NOT RVSM. FOUND INDICATOR REPEATED EXACTLY THE SAME FAULT THAT IT EXHIBITED ON THE LAST ACFT IT WAS INSTALLED ON. R & R FIRST OFFIAug 17, 2012 · N744FD · Airbus A300B4622R · Altimeter, Barometric/EncoderSDR FDEA201203020730Gcu · failedNR 2 GENERATOR FAULTED ON INTIAL TAKEOFF ROLL. REJECTED TAKEOFF AND COMPLIED WITH QRH PROCEDURES. ON ATTEMPTED GEN RESET, GEN AND ELEC LIGHTS FLICKERED RAPIDLY, WOULD NOT RESET. RETURNED TO GATE. REMOVED AND REPLACED NR 2 GCU IAW AMM 24-22-12-04-0. RANMar 2, 2012 · N744FD · Airbus A300B4622R · AC Generator-AlternatorSDR FDEA201202170610Power Supply · inoperativeBOTH L1 AND R1 DOORS WILL NOT TEST, LIGHT AND HORN. DOOR WARNING CONTROL UNIT SHOWS 28 VOLTS NOT AVAILABLE. R & R AUTONOMOUS STANDBY POWER SUPPLY UNIT AND BATTERIES REF AMM 52-73-18-04-0. RED 28 VDC LIGHT STILL ILLUMINATED WHEN A TEST OF THE SYS IS PERFORFeb 17, 2012 · N744FD · Airbus A300B4622R · Door Warning SystemSDR FDEA201202170609Power Supply · inoperativePAX DOORS WILL NOT TEST, LIGHT AND HORN. DOOR WARNING CONTROL UNIT SHOWS 28 VOLTS NOT AVAILABLE. R & R AUTONOMOUS STANDBY POWER SUPPLY UNIT AND BATTERIES REF AMM 52-73-18-04-0. RED 28 VDC LIGHT STILL ILLUMINATED WHEN A TEST OF THE SYS IS PERFORMED. R &Feb 17, 2012 · N744FD · Airbus A300B4622R · Door Warning SystemSDR FDEA201202170608Power Supply · inoperativePAX DOORS WILL NOT TEST, LIGHT AND HORN. DOOR WARNING CONTROL UNIT SHOWS 28 VOLTS NOT AVAILABLE. R & R AUTONOMOUS STANDBY POWER SUPPLY UNIT AND BATTERIES REF AMM 52-73-18-04-0. RED 28, VDC LIGHT STILL ILLUMINATED WHEN A TEST OF THE SYS IS PERFORMED. RFeb 17, 2012 · N744FD · Airbus A300B4622R · Door Warning SystemSDR FDEA201202170607Power Supply · inoperativePAX DOORS WILL NOT TEST, LIGHT AND HORN. DOOR WARNING CONTROL UNIT SHOWS 28 VOLTS NOT AVAILABLE. R & R AUTONOMOUS STANDBY POWER SUPPLY UNIT AND BATTERIES REF AMM 52-73-18-04-0. RED 28 VDC LIGHT STILL ILLUMINATED WHEN A TEST OF THE SYS IS PERFORMED. R & RFeb 17, 2012 · N744FD · Airbus A300B4622R · Door Warning SystemSDR FDEA201202170606Battery · failedPAX DOORS WILL NOT TEST, LIGHT AND HORN. DOOR WARNING CONTROL UNIT SHOWS 28 VOLTS NOT AVAILABLE. R & R AUTONOMOUS STANDBY POWER SUPPLY UNIT AND BATTERIES REF AMM 52-73-18-04-0. RED 28 VDC LIGHT STILL ILLUMINATED WHEN A TEST OF THE SYS IS PERFORMED. R & R AFeb 17, 2012 · N744FD · Airbus A300B4622R · Door Warning SystemSDR FDEA201202170605Battery · failedPAX DOORS WILL NOT TEST, LIGHT AND HORN. DOOR WARNING CONTROL UNIT SHOWS 28 VOLTS NOT AVAILABLE. R & R AUTONOMOUS STANDBY POWER SUPPLY UNIT AND BATTERIES REF AMM 52-73-18-04-0. RED 28 VDC LIGHT STILL ILLUMINATED WHEN A TEST OF THE SYS IS PERFORMED. R & RFeb 17, 2012 · N744FD · Airbus A300B4622R · Door Warning SystemSDR FDEA201202170604Power Supply · failedPAX DOORS WILL NOT TEST, LIGHT OR HORN. DOOR WARNING CONTROL UNIT SHOWS 28 VOLTS NOT AVAILABLE. R & R AUTONOMOUS STANDBY POWER SUPPLY UNIT AND BATTERIES REF AMM 52-73-18-04-0. RED 28 VDC LIGHT STILL ILLUMINATED WHEN A TEST OF THE SYS IS PERFORMED. R & RFeb 17, 2012 · N744FD · Airbus A300B4622R · Door Warning SystemSDR FDEA201112065210Computer · failedDURING GO AROUND AND REPEATEDLY SELECTING GO AROUND WITH THROTTLE AND TRP, THROTTLES DID NOT ADVANCE. MINIMAL THRUST RESPONSE TO MANUAL THROTTLE MOVEMENT. FCP STUCK IN LAND MODE EVEN AFTER MOVING VNI SWITCHES TO NAV AND CHANGING ILS FREQ WITH AUTOPILOT DISCDec 6, 2011 · N744FD · Airbus A300B4622R · Auto Throttle SystemSDR FDEA201104301684Skin · gougedNR 2 SPOILER OTBD EDGE HAS GOUGE 1.5 IN. (1) HOLE FASTENER NO HAS EDGE DISTANCE. RT WING REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER, SHIM AND FILLER IAW EA 6-5750-145598 (OTBD FACE OF SPAR).Apr 30, 2011 · N744FD · Airbus A300B4622R · SpoilersSDR FDEA201104301682Skin · dentedLT WING NR 1 SLAT HAS A 2 SQ IN DEFORMATION DENT AND 0.25 DEEP ON THE INSIDE SURFACE 48 INCH OUTSIDE OF ITS INBD EDGE. NDT CHECK C/W NO CRACK NOTED IAW NTM 51-10-8. REMOVED DAMAGED SECTION, FABRICATED REPAIR PARTS AND REPAIRED IAW SRM 57-42-11, FIG 206, PApr 30, 2011 · N744FD · Airbus A300B4622R · Leading Edge DevicesSDR FDEA201104251617Skin · dentedRIGHT WING CENTER FLAP LE OB END (16" FROM OB END) LE DENTED. PERFORMED NOSE SKIN FLUSH REPAIR IAW SRM 57-50-00 FIG. 208 PG234 AND E.A. 6-5750-150228.Apr 25, 2011 · N744FD · Airbus A300B4622R · Trailing Edge FlapsSDR FDEA201104211543Seat Track · corrodedFWD CABIN SEAT TRACK 2L CORRODED AT FR 16A 10 SQ IN REMOVED LEVEL 1 CORROSION IAW SRM 51-74-10, CHECKED LIMITS FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16, REMOVED SEAT TRACK IAW SRM 51-40-21. FABRICATED NEW SEAT TRACK IAW SRM 51-40-44 , INSTALLED FABBED SEAT Apr 21, 2011 · N744FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201104191522Seat Track · corrodedMDCC FWD CBN SEAT TRACK 2 R FR 16A HAS EXFOLIATION CORROSION 10SQN. REMOVED LEVEL 1 CORROSION. REMOVED DAMAGED SEAT TRACK BETWEEN FR15A AND 19. REPLACE SEAT TRACK WITH NEW SECTION IAW SRM 53-12-16 AND 51-40-01.Apr 19, 2011 · N744FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201104131470Seat Track · damagedMAIN DECK SEAT TRACK 2R HAS DAMAGE INSIDE THE LUG CUTOUT AND A GOUGE AT THE TOP OF THE LUG AFT OF IT BETWEEN FRAME 71 AND 72. REMOVED DAMAGED SEAT TRACK SECTION AND REPAIRED IAW SRM 53-10-16, PAGE 249.Apr 13, 2011 · N744FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201104011292Skin · crackedLT WING L/E COMPT AT STA XORS 536 FOUND FINGER DOUBLER WITH APPROX (8) IS CRACKED. TRIMMED OFF IAW SRM 57-40-02, REV 46, REPAIR 9, FIG 203. HFEC INSP CARRIED OUT ON REPAIR AREA FOUND NO CRACK EVIDENT. REPAIR DOUBLER, ANGLE AND FILLER FABRICATED AND INSTALApr 1, 2011 · N744FD · Airbus A300B4622R · Wing, Plate/SkinSDR FDEA201103311264Rib · crackedRIGHT INBOARD FLAP RIB 25A CRACKED REMOVED AND REPLACED RIB 25A AT RT FLAP IAW SRM 51-40-21 PARA.7 AND 51-40- 44 PAGE 6, TABLE 4 FOR LOCATED AND DRILLED.Mar 31, 2011 · N744FD · Airbus A300B4622R · Trailing Edge FlapsSDR FDEA201009233661Idg · failedON T/O ROLL AT 70 KIAS ECAM WARN NR1 LOW OIL PRESS. REJECT T/O QRH CK LIST. RELEASED FOR SERVICE IAW MEL: 79-36-01 CATEGORY: C EXPIRATION: 03OCT10 "MEL 79-36-01: ECAM OIL INDICATION (IDENTIFY) NR1 INOP." RAN ENGINES IAW JRH, ALL OIL PRESSURE INDICATIONSSep 23, 2010 · N744FD · Airbus A300B4622R · AC Generator-AlternatorSDR FDEA201009213612Seal · out of positionCAPTAINS SLIDING WINDOW VERIFIED CLOSED AND LOCKED PRIOR TO BLOCKOUT. EXTREMELY LOUD AIR NOISE AFTER ROTATION, INCREASINGLY LOUDER DURING ACCELERATION. FOUND CAPT SLIDING WINDOW SEAL OUT OF POSITION. REPOSITIONED INTO PROPER LOCATION REF AMM 56-12-13-04-0Sep 21, 2010 · N744FD · Airbus A300B4622R · Flight Compartment WindowsSDR FDEA200905301856Tire · failedDISCOVERED NR 2 TIRE HAD TREAD PEELING OFF AND CAUSING DAMAGE TO WING ROOT, LEFT SIDE OF AIRCRAFT. COMPLIED WITH INTERIM ACTION OF E.A 6-5720-130840. REMOVED 2 EACH LOCK FASTENERS AND BUSHINGS THAT WERE PULLED THROUGH PANEL.May 30, 2009 · N744FD · Airbus A300B4622R · TireSDR 08FDEA04037Splice · damagedFOUND DURING SKIN PANEL REPAIR IAW DR 187 SIX OVERSIZED HOLES ON FUSELAGE SKIN, C 39-40, P 27-28 LT IN SPLICE A538-31283-202. REPAIR PERFORMED BY INSTALLATION OF SHOULDERED BUSHES IAW RAS/70512709/008/2008, APPROVED BY EA 6-5315-123058.Sep 25, 2008 · N744FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR 08FDEA04036Skin Panel · corrodedFOUND CORROSION ON FUSELAGE SKIN, C 39-40, P 27-28 RT AT KRUEGER FLAP AREA. REPAIR PERFORMED BY REPLACEMENT OF SKIN PANEL IAW RAS/70512709/008/2008, APPROVED BY EA 6-5315-123058.Sep 25, 2008 · N744FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR 08FDEA04035Skin Panel · corrodedFOUND CORROSION ON FUSELAGE SKIN , C39-40, P 27-28 LT AT KRUEGER FLAP AREA. REPAIR PERFORMED BY REPLACEMENT OF SKIN PANEL IAW RAS/70512709/008/2008, APPROVED BY EA 6-5315-123058.Sep 25, 2008 · N744FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR 08FDEA04034Skin · delaminatedFOUND ON RUDDER LT SIDE NEAR HOISTING POINTS FLUID INGRESS (SEVERAL AREAS) WITH DEBONDING. REPAIR PERFORMED BY BONDING REPAIRS IAW RAS/DAHAM/4025347/2008 ISS A, APPROVED BY EA 6-5541-123055.Sep 25, 2008 · N744FD · Airbus A300F4622R · Rudder, Plate/SkinSDR 08FDEA04033Skin · delaminatedFOUND ON RUDDER RT SIDE NEAR RIB 0 FLUID INGRESS (4 AREAS) WITH DEBONDING. REPAIR PERFORMED BY BONDING REPAIRS IAW RAS/DAHAM/4025347/2008 ISS A, APPROVED BY EA 6-5541-123055.Sep 25, 2008 · N744FD · Airbus A300B4622R · Rudder, Plate/SkinSDR 08FDEA04032Plate · corrodedFOUND ON RUDDER RT SIDE THE LIGHTNING PROTECTION PLATE CORRODED. REPAIR PERFORMED BY REPLACEMENT OF LIGHTNING PROTECTION PLATE IAW RAS/DAHAM/4025347/2008 ISS A, APPROVED BY EA 6-5541-123055.Sep 25, 2008 · N744FD · Airbus A300B4622R · Rudder StructureSDR 08FDEA04031Panel · chafedFOUND CHAFING ON PANEL 471AT, LT WING, RIB 7-8 PANEL REPLACED IAW DRAWING R572-40275, APPROVED BY RAS/BAE/1007905/2008 ISS A AND EA 6-5741-123099.Sep 25, 2008 · N744FD · Airbus A300B4622R · Wing, Plate/SkinSDR 08FDEA04030Window Frame · corrodedFOUND CORRODED FASTENER HOLES IN WINDSHIELD FRAME. REPAIR PERFORMED BY REAM UP THE CORRODED HOLES, NDT FOR CORROSION FREE CONDITION AND INSTALL FASTENER IAW RAS/70512884/015/2008 ISS A, APPROVED BY EA 6-5311-123131.Sep 25, 2008 · N744FD · Airbus A300B4622R · Fuselage Main, StructureSDR 08FDEA04029Panel · delaminatedFOUND DELAMINATION ON RT OUTBOARD TRAILING EDGE PANEL REPAIR PERFORMED IAW SRM 57-51-12 PAGE 201 PARA 4, FIG 216, APPROVED BY RAS/1007710/2008 ISS A AND EA 6-5751-123095.Sep 25, 2008 · N744FD · Airbus A300B4622R · Wing, Plate/SkinSDR 08FDEA04003Fitting · corrodedFOUND CORROSION ON PYLON NR 2 UPPER AND LOWER SPIGOT FITTING AROUND BEARING SEAT. REPAIR PERFORMED BY INSTALLATION OF CORROSION RESISTENT FITTING IAW SB A300-54-6017, APPROVED BY EA 6-5451-123011.Sep 23, 2008 · N744FD · Airbus A300B4622R · Nacelle/Pylon, Attach FittingsSDR 08FDEA04002Fitting · corrodedFOUND CORROSION ON PYLON NR 1 UPPER AND LOWER SPIGOT FITTING AROUND BEARING SEAT. REPAIR PERFORMED BY INSTALLATION OF CORROSION RESISTENT FITTING IAW SB A300-54-6017, APPROVED BY EA 6-5451-123011.Sep 23, 2008 · N744FD · Airbus A300B4622R · Nacelle/Pylon, Attach FittingsSDR 08FDEA04001Skin · corrodedFOUND ON AFT CARGO DOOR CORROSION ON SKIN PLATES (P/N A523-74263-212, A523-74263-214, A523-74160-208) REPAIR PERFORMED BY CORROSION REWORK, NDT FOR CORROSION FREE CONDITION IAW RAS/DAHAM/4025425/2008 ISS A, APPROVED BY EA 6-5232-123072.Sep 23, 2008 · N744FD · Airbus A300B4622R · Cargo/Baggage DoorsSDR 08FDEA03998Fitting · damagedFOR A REPAIR THE NEW PYLON SPIGOT FITTING FOR PYLON NR 2 HAVE BEEN DELIVERED WITHOUT ATTACHMENT HOLES AND SURFACE PROTECTION. REPAIR PERFORMED BY DRILL SPIGOT FITTING BY COPY OF OLD PART, PERFORM SPRAYING SURFACE PROTECTION AND INSTALL FITTING PER DRAWING RSep 23, 2008 · N744FD · Airbus A300B4622R · Nacelle/Pylon, Attach FittingsSDR 08FDEA03997Fitting · damagedFOR A REPAIR THE NEW PYLON SPIGOT FITTING FOR PYLON NR 1 HAVE BEEN DELIVERED WITHOUT ATTACHMENT HOLES AND SURFACE PROTECTION. REPAIR PERFORMED BY DRILL SPIGOT FITTING BY COPY OF OLD PART, PERFORM SPRAYING SURFACE PROTECTION AND INSTALL FITTING PER DRAWING RSep 23, 2008 · N744FD · Airbus A300B4622R · Nacelle/Pylon, Attach FittingsSDR 08FDEA03978Fitting · damagedFOUND DAMAGED HOLES DURING ACCOMPLISHMENT OF SB A300-57-6086 (HOLE G,T) ON HORIZONTAL FLANGE, C47, RT. REPAIR PERFORMED BY OVERSIZING THE HOLES, NDT FOR DAMAGE FREE CONDITION AND INSTALLING A CONICAL WASHER IN HOLE T IAW RAS/70512903/024/2008 ISS A, APPROVESep 22, 2008 · N744FD · Airbus A300B4622R · Wing Main, Frame StructureSDR 08FDEA03977Fitting · damagedFOUND DAMAGED HOLES DURING ACCOMPLISHMENT OF SB A300-57-6086 (HOLE E, F, P) ON HORIZONTAL FLANGE, C 47, LT. REPAIR PERFORMED BY OVERSIZING THE HOLES AND NDT FOR DAMAGE FREE CONDITION IAW RAS/70512903/024/2008 ISS A, APPROVED BY EA 6-5710-123133.Sep 22, 2008 · N744FD · Airbus A300B4622R · Wing Main, Frame StructureSDR 08FDEA03976Fitting · damagedFOUND DAMAGED HOLES DURING ACCOMPLISHMENT OF SB A300-57-6049 (HOLE I, L, N, U) ON VERTICAL FLANGE, C 47, RHS. REPAIR PERFORMED BY OVERSIZING THE HOLES, EXTERNAL FITTING CUT OUT AT HOLE I AND NDT FOR DAMAGE FREE CONDITION IAW RAS/70512903/024/2008 ISS A, APPROSep 22, 2008 · N744FD · Airbus A300B4622R · Wing Main, Frame StructureSDR 08FDEA03975Fitting · damagedFOUND DAMAGED HOLES DURING ACCOMPLISHMENT OF SB A300-57-6049 (HOLE N, Y, U) ON VERTICAL FLANGE, C 47, LHS. REPAIR PERFORMED BY OVERSIZING THE HOLES OF EXTERNAL FITTING AND INSTALL A CONICAL WASHER AT HOLE U IAW RAS/70512903/024/2008 ISS A, APPROVED BY EA 6-57Sep 22, 2008 · N744FD · Airbus A300B4622R · Wing Main, Frame StructureSDR 08FDEA03965Skin · chafedFOUND 2 AREAS OF CHAFING MARKS ON LT CENTER FLAP TOP SKIN, RIB 13-15 AND 20-21. REPAIR PERFORMED BY BLEND OUT THE CHAFING MARKS IAW RAS/FOK/229/2008 ISS A, APPROVED BY EA 6-5753-123084.Sep 22, 2008 · N744FD · Airbus A300B4622R · Trailing Edge FlapsSDR 08FDEA03964Skin · chafedFOUND 2 AREAS OF CHAFING MARKS ON LT OUTER FLAP TOP SKIN, RIB 4-5 AND 15-17. REPAIR PERFORMED BY BLEND OUT THE CHAFING MARKS IAW RAS/FOK/227/2008 ISS A, APPROVED BY EA 6-5754-123065.Sep 22, 2008 · N744FD · Airbus A300B4622R · Trailing Edge Flaps
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