N728FD

Service difficulty reports · 266

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 = 'N728FD' 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 08FDEA03249Skin · gougedRIGHT CREW/COURIER EXTERIOR DOOR SKIN IS GOUGED AT THE LOWER FWD CORNER. BLENDED AND FOUND TO BE OUT OF LIMITS IAW A300-600 SRM 52-11-00; DIF 102. ACCOMPLISHED A DOUBLER REPAIR IAW A300-600 SRM 52-11-00, FIG 206. ALODINED AND PAINTED IAW A300-600 SRM 51-21-Aug 4, 2008 · N728FD · Airbus A300B4622R · Passenger/Crew DoorsSDR 08FDEA03214Floor Panel · damagedMAIN DECK FLOOR BOARD 232 LG IS PUNCTURED. REMOVED DAMAGE; PREPPED FOR LAY UP. MAT ID'D; LAYED UP REPAIR PLYS AND STARTED CURE. COMPLETED CURE AND SANDED IAW A300-600 SRM 53-10-21.Aug 1, 2008 · N728FD · Airbus A300B4622R · Fuselage Floor PanelSDR 08FDEA03136Skin · gougedTHE LEFT WING CENTER FLAP UPPER SKIN IS GOUGED. AREA IS OUT OF LIMITS IAW SRM 57-50-00; FIG 102; SHEET 5. FABRICATED IAW SRM 57-50-00; PG 219. ALODINED AND PRIMED IAW AMM 51-22-00-0, PG 1. INSTALLED IAW SRM 57-50-00, PG 219.Jul 29, 2008 · N728FD · Airbus A300B4622R · Trailing Edge FlapsSDR 08FDEA03125Housing · corrodedAFT LOWER EXTERIOR FUSELAGE; RADIO ALTIMETER ANTENNA DOME NUT RING IS CORRODED IN SEVERAL AREAS. REMOVED ANTENNA HOUSING IAW A300-600 SRM 51-40-21. LOCATED & DRILLED NEW ANTENNA HOUSING P/N A5397355400400, PO 627058.2 IAW SRM 53-17-12 & SRM 51-40-44. INSTAJul 29, 2008 · N728FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR 08FDEA02998Duct · crackedRT WING INBD FIXED L/E INLET SCOOP IS CRACKED ON THE FWD END APPROX 2 INCHES LONG. REMOVED PANEL IAW SRM 51-40-21, PG 7; SECT 5. WELDED CRACK IN THE RIGHT WING L/E INLET SCOOP IAW DWG A21040014. INSTALLED IAW SRM 51-40-21; PG 7.Jul 21, 2008 · N728FD · Airbus A300B4622R · Wing Miscellaneous StructureSDR 08FDEA02996Support Angle · crackedVERTICAL STABILIZER RIGHT TRAILING EDGE SUPPORT IS CRACKED BELOW THE NR 2 RUDDER HINGE FITTING. REMOVED DAMAGE IAW SRM 51-70-10, REPAIR I. FABRICATED A REPAIR ANGLE AND FILLER IAW SRM 51-70-10, REPAIR I. ALODINED AREA AND REPAIR PARTS IAW SRM 51-21-10. PRIJul 21, 2008 · N728FD · Airbus A300B4622R · Vertical StabilizerSDR 08FDEA02995Angle · crackedTHE APU COMPARTMENT AFT BULKHEAD HAS A PUNCTURE JUST BELOW THE LEFT LATCH RECEPTICLE. REMOVED PUNCTURED BULKHEAD ANGLE IAW A300-600 SRM 51-40-21. REMOVED THE INTERCOSTAL FOR ACCESS IAW A300-600 SRM 51-40-21. LOCATED, DRILLED AND INSTALLED A NEW ANGLE P/N AJul 21, 2008 · N728FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 08FDEA02997Support Angle · crackedVERTICAL STABILIZER RIGHT TRAILING EDGE SUPPORT IS CRACKED BELOW THE NR 2 RUDDER HINGE FITTING. REMOVED DAMAGE IAW SRM 51-70-10, REPAIR I. FABRICATED A REPAIR ANGLE AND FILLER IAW SRM 51-70-10, REPAIR I. ALODINED AREA AND REPAIR PARTS IAW SRM 51-21-10. PRIJul 21, 2008 · N728FD · Airbus A300B4622R · Vertical StabilizerSDR 08FDEA02950Angle · crackedAPU COMPARTMENT AFT BULKHEAD LOWER ANGLE IS CRACKED & BENT. REMOVED CRACKED ANGLE IAW SRM 51-40-21. LOCATED & DRILLED NEW ANGLE IAW SRM 51-72-10. INSTALLED THE ANGLE IAW SRM 51-72-10.Jul 17, 2008 · N728FD · Airbus A300B4622R · APU Cowling/ContainmentSDR 08FDEA02903Shear Web · crackedCRACKED SHEAR WEB BETWEEN FRAME 79 AND FRAME 80/82 RIGHT SIDE AT MAIN CABIN DECK FLOOR LEVEL. REMOVED AND REPLACED SHEAR WEB IAW A300-600 SRM 51-40-21.Jul 15, 2008 · N728FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 07FDEA04372Rib · crackedDURING SCHEDULED B CHECK, RT INBOARD FLAP RIB 25, P/N A5796011320100 WAS FOUND TO HAVE A 3 INCH CRACK IN THE FWD UPPER RADIUS, REF: N00030. REMOVED AND REPLACED DAMAGED RIB REF: A300 SRM 51-40-21.Sep 28, 2007 · N728FD · Airbus A300B4622R · Wing, Rib/BulkheadSDR 07FDEA04373Rib · crackedDURING SCHEDULED B CHECK, LT INBOARD FLAP RIB 25, P/N A 5796011320000 WAS FOUND TO CRACKED IN TWO PLACES, A 1.5 INCH CRACK WAS FOUND IN THE FWD UPPER RADIUS AND A 1.5 INCH CRACK WAS FOUND IN THE AFT UPPER RADIUS AND FLANGE, REF: N00029. REMOVED AND REPLACESep 28, 2007 · N728FD · Airbus A300B4622R · Wing, Rib/BulkheadSDR 07FDEA04319Rib · crackedLT RIB 25 AND RT RIB 25 FOUND CRACKED IN "B" CHECK. REPLACED RIB 25 LEFT AND RIGHT INBOARD FLAPS.Sep 26, 2007 · N728FD · Airbus A300B4622R · Trailing Edge FlapsSDR 07FDEA03630Pump · faultedAT 30000 FT, FUEL TRANSFERED TO TRIM TANK. AUTO FEED FAULT WITH CENTER TANK PUMPS FAULT. TURNED OFF CENTER PUMPS AS PER ECAM. FOLLOWED QRH FOR PUMPS FAULTS AND MANUAL FEED. CENTER TANK PUMPS WILL NOT COME ON, PUMPS KEEP FAULTING. TRAPPED FUEL OF 7000 RESep 12, 2007 · N728FD · Airbus A300B4622R · Fuel Boost PumpSDR 07FDEA03557Skin Panel · misrepairedOLD DOUBLER REPAIR AT FRAME 36-37, STRG 29-30 LT. DISAGREEMENT IN SRM REFERENCE IN OUTER RIVET ROW IS IAW SRM 53-10-12/FIG 207. REPAIR PERFORMED CONFORM TO VALID REFERENCE: SRM 53-10-12/FIG 225.Sep 11, 2007 · N728FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR 07FDEA03563Stringer · failedFOUND TWO OLD PILOTHOLES WITHOUT RIVETS AT FRAME 44, STRG 1 RT. PILOTHOLES CLOSED WITH RIVETS 2 4MM DIA IAW EA 6-5315-95894 AND RAS/DATLS/0002966/2006 ISSUE C.Sep 11, 2007 · N728FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR 07FDEA03562Rib · corrodedFOUND CORROSION IN MLG RIB 5 FWD LUG ON BOTH WINGS. REPAIR PERFORMED BY SPOT FACING AND OVERSIZING WITH NEW BUSHES IAW REPAIR DRW R572-40221 ISSUE E, APPROVED BY EA 6-5751-95903 AND RAS/BAE/1002238/2006 ISSUE A.Sep 11, 2007 · N728FD · Airbus A300B4622R · Wing, Rib/BulkheadSDR 07FDEA03560Frame · chafedCHAFING MARKS AT FRAME 34 BETWEEN STRG 14-15 LHS, OUT OF LIMIT. REPAIR PERFORMED IAW SRM 53-10-13/FIG 202. FRAME COUPLING INSTALLED.Sep 11, 2007 · N728FD · Airbus A300B4622R · Fuselage Main, FrameSDR 07FDEA03558Bracket · crackedCRACKED BRACKET AT STRG 26 LT BETWEEN FRAME 75-75A. REPLACEMENT OF AFFECTED PART IAW SRM 51-72-10.Sep 11, 2007 · N728FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 07FDEA03556Skin Panel · failedOLD DOUBLER REPAIR AT FRAME 36, STRG 32-33 LT. DISAGREEMENT IN SRM REFERENCE IN OUTER RIVET ROW. REPAIR PERFORMED IAW SRM 53-10-12/FIG 207. REPAIR SOLUTION WITH SRM 53-10-12/FIG 225.Sep 11, 2007 · N728FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR 07FDEA03555Stringer · corrodedFOUND HEAVY CORRODED STRINGER 46 RT BETWEEN FRAME 63-63A, TORSION BOX. STRINGER REPAIR PERFORMED IAW SRM 53-10-14/FIG 201 AND TORSION BOX-SPLICE REPAIR IAW SRM 53-17-18/FIG 206/SH 2.Sep 11, 2007 · N728FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR 07FDEA03550Floorbeam · misrepairedOLD CROSSBEAM REPAIR IN AFT CARGO FLOOR COMPARTMENT, FRAME 63 LT IS NOT CONFORM TO SRM 53-10-15/FIG 207 (REPAIR PROFIL THICKNESS). REPAIR RENEWED IAW SRM 53-10-15/FIG 207.Sep 11, 2007 · N728FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR 07FDEA03549Floorbeam · misrepairedOLD CROSSBEAM REPAIR IN AFT CARGO FLOOR COMPARTMENT, FRAME 63 LT IS NOT CONFORM TO SRM 53-10-15/FIG 207 (REPAIR PROFIL THICKNESS). REPAIR RENEWED IAW SRM 53-10-15/FIG 207.Sep 11, 2007 · N728FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR 07FDEA03548Frame · crackedFOUND CRACK (17 MM) IN FRAME 44 RT. REPAIR MOD PERFORMED IAW FEDEX WIC 6-5310-7-5015 FROM FRAME 41-46.Sep 11, 2007 · N728FD · Airbus A300B4622R · Fuselage Main, FrameSDR 07FDEA03543Flange · damagedFOUND SEVERAL MISDRILLED HOLES AT FLANGE FOR AOA SENSOR BETWEEN FRAME 18-19 LHS (PTOF DRW. R537B1311). REPAIR PERFORMED BY REPLACEMENT OF FLANGE IAW SRM 51-72-10.Sep 11, 2007 · N728FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 07FDEA03540Bracket · crackedFOUND TWO CRACKED BRACKETS BETWEEN CROSSBEAM FRAME 29-30 AND 30-31, Y-2462 RHS. REPAIR PERFORMED BY REPLACEMENT OF PARTS IAW SRM 51-72-10.Sep 11, 2007 · N728FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 07FDEA03539Frame · damagedDAMAGED FRAME 12A RT (BENT PARTITIONS, IMPACTS AT RIVET HOLES, OVERSIZED HOLES), STRG 24-27. REPAIR PERFORMED BY REPLACEMENT IAW SRM 51-72-10.Sep 11, 2007 · N728FD · Airbus A300B4622R · Fuselage Main, FrameSDR 07FDEA03537Fitting · damagedDAMAGED FITTING AT FRAME 12A, Z-177, STRG 26 RHS. REPAIR PERFORMED BY REPLACEMENT IAW SRM 51-72-10.Sep 11, 2007 · N728FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 07FDEA03535Fitting · damagedDAMAGED FITTING AT FRAME 13, STR 26 RT. REPAIR PERFORMED BY REPLACEMENT IAW SRM 51-72-10.Sep 11, 2007 · N728FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 07FDEA03533Skin Panel · dentedFOUND DENT BETWEEN FRAME 19-20, STRG 36 LT, BELOW THE BUTT JOINT STRG 35. REPAIR PERFORMED BY CUT OUT AND INSTALLING EXTERNAL DOUBLER FOLLOWING SRM 53-10-12/FIG 224/SH 2, APPROVED BY EA 6-5313-95878 AND RAS/DABRE/7006162/2006 ISSUE A.Sep 11, 2007 · N728FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR 07FDEA03527Support · crackedCRACKED SUPPORT AT FRAME 79-80, STRG 28 LHS. REPLACEMENT OF SUPPORT IAW SRM 51-72-10.Sep 11, 2007 · N728FD · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR 07FDEA03525Frame · damagedFOUND OVERSIZED HOLES AT CROSSBEAM, FRAME CONNECTION, FRAME 77 BETWEEN STRG 27-28 LHS. REPLACMENT OF FRAME SEGMENT IAW SRM 51-72-10.Sep 11, 2007 · N728FD · Airbus A300B4622R · Fuselage Main, FrameSDR 07FDEA03523Shear Tie · crackedCRACKED SHEAR PLATES BETWEEN FRAME 79-80, STRG 26. REPAIR PERFORMED BY REPLACEMENT OF PART SRM 51-72-10.Sep 11, 2007 · N728FD · Airbus A300B4622R · Fuselage Internal Mounting StructureSDR 07FDEA03521Skin Panel · wornELONGATED HOLES AT PYLON SUPPORT BRACKET AND BOTTOM SKIN OF LT WING. REPAIR PERFORMED BY OVERSIZING HOLES AND INSTALLING BUSHES IAW EA 6-5720-95870 AND RAS/BAE/1002289/2006 ISSUE A.Sep 11, 2007 · N728FD · Airbus A300B4622R · Wing, Plate/SkinSDR 07FDEA03520Frame · damagedDAMAGED FRAME 12A LT (BENT PARTITIONS, IMPACTS AT RIVET HOLES, OVERSIZED HOLES), STRG 24-27. REPAIR PERFORMED BY REPLACEMENT IAW SRM 51-72-10.Sep 11, 2007 · N728FD · Airbus A300B4622R · Fuselage Main, FrameSDR 07FDEA03519Fitting · damagedDAMAGED FITTING AT FRAME 13, STRG 26 LHS. REPAIR PERFORMED BY REPLACEMENT IAW SRM 51-72-10.Sep 11, 2007 · N728FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 07FDEA03517Fitting · damagedDAMAGED FITTING AT FRAME 12A, Z-177, STRG 26 LT. REPAIR PERFORMED BY REPLACEMENT IAW SRM 51-72-10.Sep 11, 2007 · N728FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 07FDEA03514Frame · scratchedFOUND SCRUBMARKS AT FRAME 55 LT & RT, BETWEEN STR 14-15. REPAIR PERFORMED BY REWORK AND INSTALLING REINFORCEMENT PLATE IAW TD/K4/S1/20292/2005/A AND SRM 53-10-13 / FIG 202, APPROVED BY EA 6-5316-95880 AND RAS/DAHAM/4020292/2005 ISSUE A.Sep 11, 2007 · N728FD · Airbus A300B4622R · Fuselage Main, FrameSDR 07FDEA03503Frame · crackedFOUND CRACKED FRAME SEGMENT ON RT AND LT AFT PAX DOOR (ZONE 843 / 833 ). FRAME SEGMENT REPLACED IAW SRM 52-13-00 AND SRM 51-72-10.Sep 10, 2007 · N728FD · Airbus A300B4622R · Passenger/Crew DoorsSDR 07FDEA03502Diaphragm · damagedFOUND SEVERAL DAMAGES AN DIAPHRAGM BETWEEN TRACK 4/5 RT AND LT, DENT-NICK- SCRATCHES AROUND FASTENERS. REPAIR PERFORMED BY BLEND OUT SCRATCHES AROUND FASTENERS, DRILLING HOLES FOR NICK (FULL FILLED WITH FASTENER), LETTING DENT IN STATE AND HFEC/ROTOTEST/DVI.Sep 10, 2007 · N728FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 07FDEA03501Fitting · corrodedHEAVY CORROSION ON FITTING AT FRAME 63 LT, STRG 43-46. REPLACED FITTING IAW SRM 51-72-10.Sep 10, 2007 · N728FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR 07FDEA03500Stringer · corrodedCORROSION ON STRINGER 44 LT BETWEEN FRAME 16A-17. STRINGER REPAIR PERFORMED IAW SRM 53-12-14 / FIG 201.Sep 10, 2007 · N728FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR 07FDEA03499Stringer · corrodedHEAVY CORROSION ON STRINGER 49 RT BETWEEN FRAME 57.3-58. STRINGER REPAIR PERFORMED IAW SRM 53-10-14 / FIG 201.Sep 10, 2007 · N728FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR 07FDEA03498Skin Panel · chafedFOUND TWO CHAFE MARKS AND ONE IMPACT DAMAGE ON FIXED L/E 'D' NOSE SKIN BETWEEN TRACK 3-4 RT WING. REPAIR PERFORMED BY BLEND OUT OF CHAFING MARKS AND DRILLING 1/4INCH DIA HOLE WITH CSK AND INSTALLING A SOLID ALUMINUM RIVET IAW TD/J1/S1/02044/2005 ISSUE B, APPRSep 10, 2007 · N728FD · Airbus A300B4622R · Wing, Plate/SkinSDR 07FDEA03497Structure · crackedFOUND CRACKED PICK UP MEMBER ON PYLON NR 2. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 54-54-11.Sep 10, 2007 · N728FD · Airbus A300B4622R · Nacelle/Pylon, Main FrameSDR 07FDEA03496Panel · wornFOUND WORN HOLES ON RIB 8 INBOARD AND OUTBOARD PANEL, PYLON NR 2 RHS. REPAIR PERFORMED IAW SRM 54-51-31/CONF 02/FIG 201.Sep 10, 2007 · N728FD · Airbus A300B4622R · Nacelle/Pylon, Plate/SkinSDR 07FDEA03495Gusset · crackedFOUND CRACKED GUSSET ON FWD PAX DOOR LT (DOOR ZONE 831) AT FWD LOWER CORNER. REPAIR PERFORMED BY REPLACEMENT OF GUSSET IAW SRM 52-11-00-C1.Sep 10, 2007 · N728FD · Airbus A300B4622R · Passenger/Crew DoorsSDR 07FDEA03493Panel · wornFOUND WORN HOLES ON RIB 8 INBOARD AND OUTBOARD PANEL, PYLON NR 1 LHS. REPAIR PERFORMED IAW SRM 54-51-31/CONF 02/FIG 201.Sep 10, 2007 · N728FD · Airbus A300B4622R · Nacelle/Pylon, Plate/SkinSDR 07FDEA03490Skin · dentedLT ALL SPEED AILERON LOWER SKIN, DENTS IN TRAILING EDGE HONEYCOMB AREA. REPAIR PERFORMED BY CUT OUT DENTED SKIN AND APPLY WITH EXTERNAL PATCHES IAW EA 6-5761-95884 AND RAS/FOK/199/2005 ISSUE B.Sep 10, 2007 · N728FD · Airbus A300B4622R · Wing, Control SurfacesSDR 07FDEA03489Structure · corrodedHEAVY CORROSION ON LOWER T-SECTION AT FRAME 92 BETWEEN STRG 21 LT TO STRG 21 RT. REPAIR PERFORMED CUT OUT T-SECTION AND INSTALLING NEW PORTION OF T-SECTION AND A REPAIR ANGLE IAW EA 6-5319-95861 AND RAS/DAHAM/4020299/2005 ISSUE A.Sep 10, 2007 · N728FD · Airbus A300B4622R · Fuselage Main, Structure
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