N727FD

Service difficulty reports · 185

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 = 'N727FD' 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 FDEA201104091413Skin · crackedFROM NDT REPORT EVIDENCE OF CRACK DISCREPENCIES FROM FASTENERS AT FR 54 STR 13 RT AND STR 5 RT. REPAIR CARRIED OUT IAW EA6-5330-149428. DAMAGE FOUND TO BE MECHANICAL DAMAGE AND NOT CRACKED.Apr 9, 2011 · N727FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA201104071381Skin · dentedINTERNAL DENT FOUND FWD OF MLG BAY CUT OUT FUSELAGE SKIN BETWEEN FR 48-49 RT SIDE. DENT DRESSED, SURFACE INSPECTION CARRIED OUT IAW EA6-5330-150104. NO CRACKS APPARENT AND REPROTECTED.Apr 7, 2011 · N727FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA201104061364Skin · damagedPREVIOUS DAMAGE OBSERVED RT FUSE FR 64-65, STA 4203-4256 STR 32-33. REPAIRED IAW EA6-5330-150107 SURFACE INSPECTION CARRIED OUT, NO CRACKS APPARENT. AREA REPROTECTED.Apr 6, 2011 · N727FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA201104061363Skin · dentedDENT AND GOUGE FR 18-19, STR 38-39, RT FUSELAGE SKIN BELOW FWD CARGO DOOR SELECTOR PANEL. REPAIRED IAW EA 6-5330-150105. DENT REWORKED SURFACE INSPECTION CARRIED OUT, NO CRACKS APPARENT AREA REPROTECTED.Apr 6, 2011 · N727FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA201104061362Skin · dentedINTERNAL DENT SEEN FROM EXTERIOR SKIN FR 17-18 LT SIDE. LEVEL WITH OUTFLOW BLANK 24" UP FROM SKIN EDGE. DAMAGE SITE REWORKED AS DETAILED ON EA 6-5330-150106. AREA BLENDED, ASSESSED, SURFACE FINISH INSPECTED AND REPROTECTED. NO DAMAGE APPARENT.Apr 6, 2011 · N727FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA201104061361Skin · dentedDENT, MLG BAY FUSE SKIN FOUND AT FR 51-52 AFT OF MLG BAY CUT OUT RT SIDE. REPAIRED IAW EA6-5330-150104. DENT DRESSED, SURFACE INSPECTION CARRIED OUT NO CRACKS APPARENT AND AREA REPROTECTED.Apr 6, 2011 · N727FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA201104061360Skin · dentedLT MLG DOOR EXT SKIN DENTS X2 FOUND TOWARDS THE TOP HALF OF THE DOOR AFT END. EA 6-3210-1499440 RAISED TO COVER MINOR DENTS IN DOOR SKIN.Apr 6, 2011 · N727FD · Airbus A300B4622R · Landing Gear DoorsSDR FDEA201104061359Skin · damagedBULK CARGO DOOR HANDLE RECESS SKIN EDGE DAMAGED/GOUGED. REWORKED AND CLASSED AS MINOR REPAIR IAW EA6-5230-150101Apr 6, 2011 · N727FD · Airbus A300B4622R · Cargo/Baggage DoorsSDR FDEA201104061358Skin · dentedDENT FOUND FWD OF MLG BAY CUT OUT FUSELAGE SKIN BETWEEN FR 48-49, LT SIDE. REPAIR CARRIED OUT IAW EA6-5330-150104 DENT DRESSED, SURFACE INSPECTION CARRIED NO CRACKS APPARENT. AREA REPROTECTED.Apr 6, 2011 · N727FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA201104061357Skin · gougedGOUGES LOCATED IN SCREW HOLE FOR RT THS MAN HOLE COVER 343GB, IN BOTTOM SKIN CUT OUT. REPAIR CARRIED OUT IAW EA6-5510-7-149430 AREAS BLENDED AND CLASSIFIED AS MINOR.Apr 6, 2011 · N727FD · Airbus A300B4622R · Horizontal Stabilizer, Plate/SkinSDR FDEA201104061356Skin · dentedDENT OBSERVED RT FUSE SKIN, FR 66-67, STA 4362-4309, STR 51-55. EA 6-5330-149434 RAISED TO COVER DENT, DEFINED AS IN LIMITS AND NO ACTION REQUIRED.Apr 6, 2011 · N727FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA201104061355Skin · dentedDENT FR 100-101 LT SIDE, AFT OF APU BAY VENT GRILL. EA 6-5330-149436 RAISED TO COVER DENT. NO REQUIREMENT TO REPAIR AFTER INSPECTION AND REPROTECTION.Apr 6, 2011 · N727FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA201104061354Skin · dentedDENT ON THE LT SIDE OF THE SAFETY STAND (TAIL STEADY) FITTING TO EMPENNAGE FUSEAGE SKIN FR 85. EA 6-5330-148539 RAISED TO ASSESS DENT AT FR 85 AND FOUND TO BE WITHIN LIMITS.Apr 6, 2011 · N727FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA201104061353Bulkhead · scratchedNLG BAY AFT BULKHEAD LT HAS SCRATCHES, INVESTIGATE AND RETREAT. SCRATCHES BLENDED AND REPROTECTED AS DETAILED ON EA 6-5310-149429. RELEASED BY RAS 70546062-005-2011 ISSUE AApr 6, 2011 · N727FD · Airbus A300B4622R · Fuselage Main, BulkheadSDR FDEA201104061352Skin · dentedDENT FR93-94 LT SIDE. TAILCONE AREA 9 O'CLOCK LOCATION ALF. EA 6-5330-149398 RAISED TO COVER DAMAGE SITE, AND FOUND TO BE WITHIN LIMITS.Apr 6, 2011 · N727FD · Airbus A300B4622R · Aerodynamic FairingsSDR FDEA201103311262Roller · corrodedROLLER TRACK Y805 FR60-63 HAS CORROSION TO THE AREAS ADJACENT TO THE FASTENER HOLES, CORROSION FOUND TO BE BEYOND SRM LIMITS. ROLLER TRACK CONSIDERED TO BE PRIMARY STRUCTURE. ROLLER TRACK FABRICATED IAW DRAWING A25775021 AND GMM 6-2-100 TRACK INSTALED IAW AMMar 31, 2011 · N727FD · Airbus A300B4622R · Fuselage Main, StructureSDR FDEA201103311261Roller · corrodedROLLER TRACK FR32-38.2 Y STATION 1470 IS CORRODED BEYOND SRM LIMITS 53-10-15 ROLLER TRACK CONSIDERED PRIMARY STRUCTURE. ROLLER TRACK FABRICATED IAW DRAWING A25771313 AND GMM 6-2-100 AND REFITTED IAW AMM 25-52-21 PB401.Mar 31, 2011 · N727FD · Airbus A300B4622R · Fuselage Main, StructureSDR FDEA201103311260Roller · corrodedROLLER TRACK FR 32-38.2 Y STATION -140 IS CORRODED BEYOND SRM LIMITS REF 53-10-15 ROLLER TRACK CONSIDERED PRIMARY STUCTURE. ROLLER TRACK FABRICATED IAW DRAWING A25771313 AND GMM 6-2-100 AND REFIITED 6-2-100Mar 31, 2011 · N727FD · Airbus A300B4622R · Fuselage Main, StructureSDR FDEA201103311259Roller · corrodedROLLER TRACK FR32-38.2 Y STATION -1470 IS CORRODED BEYOND SRM LIMITS REF 53-10-15. ROLLER TRACK CONSIDERED PRIMARY STRUCTURE. REPLACEMENT ROLLER TRACK FABRICATED IAW DRAWING A255771313 AND GMM 6-2-100. TRACK REFITTED IAW AMM 25-52-21 PB 401Mar 31, 2011 · N727FD · Airbus A300B4622R · Fuselage Main, StructureSDR FDEA201103311258Skin · dentedPREVIOUS FILLED DENT OBSERVED ON RH FUSE SKIN 9 INCH AFT OF FR76 BELOW STR 24. DENT FOUND TO BE OUT OF LIMITS. REPAIR CARRIED OUT IAW EA6-5330-149433 AND TD/K4/S1/34486/2011 ISSUE A. REPAIR RELEASED RAS / DAHAM / 4034486 / 2011 ISSUE B.Mar 31, 2011 · N727FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA201103311257Skin · dentedPREVIOUS DENT OBSERVED ON RH FUSE SKIN 15 INCH AFT FR77 17 INCH BELOW STR 24. REPAIR CARRIED OUT IAW SRM 53-10-12 REPAIR DOUBLER INSTALLED IAW SRM 53-10-10 FIG 225 ORIGINAL SKIN THICKNESS 0.063" REPAIR DOUBLER 0.071" THICK.Mar 31, 2011 · N727FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA201103251173Attach Angle · crackedRT MLG AT FR47/ STR42 REAR FACE ATTACH ANGLE EVIDENCE OF CRACK COMING FROM THE TOP FASTENER ON WEB. ON FURTHER INSP AND DUE TO NO SRM LIMITS A REPLACEMENT OF THE WEB WAS ACTIONED. REPLACEMENT WEB INSTALLED IAW SRM 51-40-21 AND DRAWING A53812215Mar 25, 2011 · N727FD · Airbus A300B4622R · Fuselage, Landing Gear Attach FittingsSDR FDEA201103251172Web · crackedLEFT MLG AT FR 41/ STR 42 REAR FACE ATTACH ANGLE, EVIDENCE OF CRACK COMING FROM THE TOP FASTENER ON WEB. ON FURTHER INSP AND DUE TO NO SRM LIMITS A REPLACEMENT OF THE WEB WAS ACTIONED. REPLACEMENT WEB FABRICATED IAW DRAWING A53812218 AND SRM 51-70-12, WEB INSMar 25, 2011 · N727FD · Airbus A300B4622R · Fuselage Main, Attach FittingsSDR FDEA201103181076Pin · crackedLEFT UNDERCARRAIGE HAS ONGOING REPORTS OF SHOCK STRUT LOOSING PRESSURE, DURING BASE MAINTENANCE INVESTIGATION OF PRESSURE LEAK RATE, LEFT HAND DRAG LINK BRACE AFT LOCATING SUPPORT PIN FOUND SHEARED 360 DEGREES INTERNALLY AND SLIGHT PIN MIGRATION NOTED. BOTHMar 18, 2011 · N727FD · Airbus A300B4622R · Main Landing GearSDR FDEA201103161015Skin · damagedFASTENERS ON AFT SIDE OF INBD END OF RT INBD SLAT CONTACTING L/E SKIN LEAVING DEEP WEAR MARKS FROM FASTENER HEADS. REPAIR CARRIED OUT IAW SRM 57-41-12 FIG 204 SCHEME BMar 16, 2011 · N727FD · Airbus A300B4622R · Leading Edge DevicesSDR FDEA201103161014Skin · misrepairedLT NR 2 SLAT LOWER SKIN TRACK 5-6 LOCATION STATES IN RECORDS, A FLUSH REPAIR IAW SRM 57-43-11, FIG 202. AIRCRAFT PHYSICALY HAS A DOUBLER REPAIR PATCH IN THIS POSITION WHICH IS NOT IAW STATED SRM. REPAIR DOUBLER INSTALLED IAW EA6-5750-149426.Mar 16, 2011 · N727FD · Airbus A300B4622R · Leading Edge DevicesSDR FDEA201103140967Hinge Fitting · corrodedBOTH LT AND RT KRUEGER FLAP BULL NOSE ASSY'S HAVE SEVERELY CORRODED HINGE ARM FITTINGS. THIS IS CONSIDERED PRIMARY STRUCTURE. KRUEGER FLAP HINGE ARMS REPLACED.Mar 14, 2011 · N727FD · Airbus A300B4622R · Leading Edge DevicesSDR FDEA201103140966Rib · misrepairedRE-EVALUATION OF EXISTING REPAIR ON RT WING CTR FLAP BULLNOSE RIBS 19-20 LOCATION CARRIED OUT USING ORIGINAL NRC 0003346 AND SRM 57-50-00, FIG 208. REPAIR SUSPECTED TO HAVE 1 ROW OF SPLICE FASTENERS MISSING FROM THE OTBD SPLICE. REPAIR WAS REMOVED AND SKMar 14, 2011 · N727FD · Airbus A300B4622R · Wing SparSDR FDEA201103090922Skin · misrepairedEXISTING DOUBLER AT FR72-73, STR 24-25 LT FOUND TO NOT BE IAW SRM 53-10-12, FIG 225. ONLY 2 ROWS OF FASTENERS HAVE PREVIOSLY BEEN INSTALLED EITHER SIDE OF CUTOUT, SRM REQUIRES 3 ROWS. REPAIR CARRIED OUT IAW EA6-5330-97590 AND SRM 53-10-12 FIG 225.Mar 9, 2011 · N727FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA201103080913Skin · misrepairedINCORRECT SKIN FASTENER USED DURING PREVIOUS REPLACEMENT OF INTERNAL DOUBLER BETWEEN FRS 12-12A LT FUSELAGE (FWD LAV SERVICE PANEL AREA) ALSO SKIN DAMAGE OBSERVED LOCAL TO FASTENER HOLES. FOUND DURING C2 CHECK, PREVIOUS REPAIR INTERNAL PRODUCTION DOUBLER REPLMar 8, 2011 · N727FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA201103080915Shear Tie · misrepairedDURING INSP AND REVIEW OF PREVIOUS OPERATORS RECORDS REPAIR FOUND TO BE CORRECT EXCEPT FRAME FOOT TO DOUBLER FASTENERS AT FR10A ARE INCORRECTLY INSTALLED, RIVET TAILS CHOPPED AND MISFORMED. FRAME FOOT TO DOUBLER FASTENERS REPLACED AT FR 10A IAW SRM 53-12-12.Mar 8, 2011 · N727FD · Airbus A300B4622R · Fuselage Internal Mounting StructureSDR FDEA201103080914Fitting · misrepairedEVALUATION OF PREVIOS REPAIR ON NLG CONNECTION FITTINGS AT FR13A-14. RT FOUND TO BE AS DETAILED BUT 2 LOWER FASTENERS THROUGH THE LOWER FITTING AND EXTERNAL SKIN ARE SITTING IN THE RADIUS THIS WAS CAUSING THE NUTS/ WASHERS TO NOT SIT FLUSH WITH THE FITTING. Mar 8, 2011 · N727FD · Airbus A300B4622R · Fuselage, Landing Gear Attach FittingsSDR FDEA201006232121Handle · malfunctionedLANDING GEAR WOULD NOT RETRACT ON EITHER SYSTEM. R & R LANDING GEAR CONTROL HANDLE AS PER MM32-31-11-4, R & R PROXIMITY SWITCH ELECTRONIC UNIT AS PER MM32-31-71-4, LUBED MAIN LANDING GEAR.Jun 23, 2010 · N727FD · Airbus A300B4622R · Landing Gear SelectorSDR FDEA200912184483Accumulator · failedDURING TAKEOFF ROLL,HAD ECAM WARNING FOR BLUE LO PRESS HYD SYS. ABORTED TAKEOFF ABOUT 80 KNOTS WITH NO PROBLEMS. DURING AFTER LANDING CHECKLIST NOTICED BLUE HYD SYS PRESSURE FLUCTUATED DOWN TO AS LOW AS 1950 PSI WHILE MOVING FLIGHT CONTROLS WITH NO LOADS RDec 18, 2009 · N727FD · Airbus A300B4622 · Hydraulic System, MainSDR FDEA200910263676Hose · leakingAIR TURNBACK FOR LOSS OF GREEN HYD QUANTITY. OCCURED AT 5000FT AGL AFTER TAKEOFF. RIGHT EICAM SHOWED 0 QUANTITY FOR GREEN SYSTEM. AFTER EXITING RWY 33R THE EMERGENCY RESPONDERS CONFIRMED FLUID LEAK. TURNED HY D PUMPS OFF WITHIN 2 MINUTES OF INDICATION. FOOct 26, 2009 · N727FD · Airbus A300B4622R · Hydraulic System, MainSDR FDEA200904151304Pressure Switch · failedDURING TAKEOFF LFPG AT 70KTS HYD BLUE SYSTEM LOW PRESSURE ECAM ALERT. REJECTED TAKE OFF. (PRESSURE A ND QUANTITIES APPEARED NORMAL,ECAM ALERT DISAPPEARED. UPON SUBSEQUENT FLT CONTROL CHECK ECAM ALERT REAPPEARED. T/S IN PROGRESS GOT BLUE SERVO LOW PRESSUREApr 15, 2009 · N727FD · Airbus A300B4622R · Hydraulic Indicating SystemSDR 08FDEA03316Skin · dentedTAIL CONE, FUSELAGE UPPER AREA WITH DENTS BETWEEN FR 100 AND 103 AND BETWEEN STGR 2 LT AND 2 RT. DENTED SKIN BETWEEN FR 100 AND FR 103 WAS REPAIRED AS PER FEDEX EA 6-5330-123347. FRAME SECTIONS OF FR 101 AND FR 102 WERE REPLACED AS PER SRM 51-72-10.Jul 29, 2008 · N727FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR 07FDEA04688Switch · dirtyAFTER TAKEOFF RECEIVED ECAM FOR LOWER ACCESS DOOR NOT CLOSED. FORWARD AND AFT LOWER ACCESS DOORS SWITCHES CLEANED. CHECKED INDICATION ON ECAM, NORMAL.Oct 26, 2007 · N727FD · Airbus A300B4622R · Door Warning SystemSDR 07FDEA03385Spar · corrodedDURING ACCOMPLISHMENT OF EO 6-5710-7-3301 A2 PART 1 FOUND CORRODED HOLE 'D (SEE SB A300-57-6063). REPAIR PERFORMED BY REAM UP AND OVERSIZING HOLE IAW EA 6-5710-95892 AND RAS/BAE/1002151/2006 ISSUE A.Sep 5, 2007 · N727FD · Airbus A300B4622R · Wing SparSDR 07FDEA03384Web · misrepairedFOUND OLD REPAIR AT WEB ON FLOOR STRUCTURE FRAME 13A-13B RT, Y-730, NOT CONFORM TO SRM (SPLICE MATERIAL). REPAIR RENEWED IAW SRM 53-12-15/FIG 207.Sep 5, 2007 · N727FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 07FDEA03383Web · misrepairedFOUND OLD REPAIR AT WEB ON FLOOR STRUCTURE FRAME 14A-14B, Y0, NOT CONFORM TO SRM (SPLICE MATERIAL). REPAIR RENEWED IAW SRM 53-12-15/FIG 207.Sep 5, 2007 · N727FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 07FDEA03382Panel · crackedCRACKED HOLES (8 MM) FOUND ON PYLON NR 1, RIB 8 INBOARD SIDE. REPAIR PERFORMED IAW SRM 54-51-31/FIG 201.Sep 5, 2007 · N727FD · Airbus A300B4622R · Nacelle/Pylon, Plate/SkinSDR 07FDEA03381Skin Panel · damagedFOUND ON CENTER WING BOX UPPER PANEL, UPPER SURFACE A NOTCH AT FRAME 47, BETWEEN TRACK 3-4 RT. REPAIR PERFORMED BY BLEND OUT DAMAGE IAW EA 6-5710-95852 AND RAS/AS/0003/2006 ISSUE A.Sep 5, 2007 · N727FD · Airbus A300B4622R · Wing, Plate/SkinSDR 07FDEA03380Skin Panel · failedOLD DOUBLER REPAIR ON SKIN AT FRAME 3 LT BELOW FLOOR LEVEL, NOT CONFORM TO RAS/AS/189/00 ISSUE A (SHIM IN THE CUT OUT IS MISSING). REPAIR RENEWED IAW. RAS/AS/189/00 ISSUE A.Sep 5, 2007 · N727FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR 07FDEA03379Stringer · damagedMISDRILLED HOLE FOUND AT STRG 53 RT, FRAME 54.3. STRINGER REPAIR PERFORMED IAW SRM 53-10-14/FIG 201A.Sep 5, 2007 · N727FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR 07FDEA03378Skin · crackedCRACKED HOLES (ABOUT 8 MM) ON PYLON NR 1, RIB 8 OUTBOARD SIDEWALL. REPAIR PERFORMED IAW SRM 54-51-31/FIG 201.Sep 5, 2007 · N727FD · Airbus A300B4622R · Nacelle/Pylon, Plate/SkinSDR 07FDEA03377Skin Panel · misrepairedOLD EXTERNAL REPAIR AT SKIN FRAME 65-66, STRG 33-34 RT, NOT CONFORM TO SRM 53-10-12/FIG 225. EXTERNAL DOUBLER REPAIR RENEWED IAW SRM 53-10-12/FIG 225.Sep 5, 2007 · N727FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR 07FDEA03376Support · crackedFOUND CRACKED SUPPORT BETWEEN FRAME 79-80, STRG 28 LT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Sep 5, 2007 · N727FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 07FDEA03375Beam · corrodedCORROSION ON BEAM NR 10, FRAME 67-69, STRG 45-47 RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Sep 5, 2007 · N727FD · Airbus A300B4622R · Fuselage Main, StructureSDR 07FDEA03374Frame · damagedFOUND ON DIAPHRAGM FRAME 47-54 AT BEAM 4-5 LT AND RT NICKS AND IMPACT DAMAGES. REPAIR PERFORMED BY SMOOTH REWORK OF DAMAGED AREA ON BEAM 4-5 LT IAW EA 6-5315-95840 AND RAS 041406/011/2005 ISSUE A AND CUT OUT THE DIAPHRAGM AND INSTALLING A REPAIR SPLICE ON BEASep 5, 2007 · N727FD · Airbus A300B4622R · Fuselage Main, Frame
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