N655FE

Service difficulty reports · 219

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 = 'N655FE' 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 FDEA201701310296Shear Tie · crackedFWD CARGO COMP RT SIDE SHEAR TIE BETWEEN FR 36 AND 37 IS CRACKED. REMOVED AND REPLACED FWD CARGO RT SHEAR TIE BETWEEN FR 36 AND 37 PER SRM 51-40-21 AND SRM 51-40-44.Jan 31, 2017 · N655FE · Airbus A300F4605R · Fuselage Internal Mounting StructureSDR FDEA201701310295Floorboard · damagedFWD CARGO COMPARTMENT FLOORBOARD 132MG HAS EDGE DAMAGE AND MISSING INSERTS. FABRICATED FWD CARGO COMPARTMENT FLOORBOARD 132MG PER DWG SRZ-25-005.Jan 31, 2017 · N655FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201701310294Floorboard · damagedFWD CARGO COMPARTMENT FLOORBOARD 132KG LOWER SKIN IS PUNCTURED. FABRICATED FWD CARGO COMPARTMENT FLOORBOARD 132KG PER DWG SRZ-25-005 005.Jan 31, 2017 · N655FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201701310293Floorboard · damagedFWD CARGO COMPARTMENT FLOORBOARD 131RG UPPER AND LOWER SURFACE IS DAMAGED. FABRICATED FWD CARGO COMPARTMENT FLOORBOARD 131RG PER DWG SRZ-25-005 005.Jan 31, 2017 · N655FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201701310292Floorboard · puncturedFWD CARGO COMPARTMENT FLOORBOARD 131KG LOWER SKIN IS PUNCTURED. FABRICATED FWD CARGO COMPARTMENT FLOORBOARD 131KG PER DWG SRZ-25-005 005.Jan 31, 2017 · N655FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201701310291Floorboard · damagedFWD CARGO COMPARTMENT FLOORBOARD 132SG HAS DAMAGE ON LOWER SKIN. FABRICATED FWD CARGO COMPARTMENT FLOORBOARD 132SG PER DWG SRZ-25-005 005.Jan 31, 2017 · N655FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201701310290Floorboard · damagedMAIN CABIN FLOORBOARD 241PF IS DAMAGED. FABRICATED MAIN CABIN FLOORBOARD 241PF PER DWG SRZ-25-005.Jan 31, 2017 · N655FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201701310289Floorboard · damagedAFT CARGO COMP FLOORBOARD 152TF IS DAMAGED ON LOWER SKIN. FABRICATED AFT CARGO COMPARTMENT FLOORBOARD 152TF PER DWG FX-25-005.Jan 31, 2017 · N655FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201701310288Floorboard · damagedAFT CARGO COMPARTMENT FLOORBOARD 151SF HAS EDGE DAMAGE. FABRICATED AFT CARGO FLOORBOARD 151SF PER DWG FX-SRZ-25-005.Jan 31, 2017 · N655FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201701310287Floorboard · damagedAFT CARGO FLOORBOARD 152QF HAS DAMAGE ON LOWER SURFACE. FABRICATED AFT CARGO FLOORBOARD 152QF PER DWG SRZ-25-005.Jan 31, 2017 · N655FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201701250250Floorboard · puncturedFWD CARGO BAY FLOORBOARD 131LG UPPER SKIN IS PUNCTURED. REPAIRED THE FLOORBOARD IAW SRM 53-10-20 PARA 8B.Jan 25, 2017 · N655FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201701250249Floorboard · damagedFWD CARGO BAY FLOORBOARD 131SG IS DAMAGED ON UPPER AND LOWER SURFACE. REPAIRED IAW SRM 53-10-20 PARA 8B.Jan 25, 2017 · N655FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201701230237Floorbeam · corrodedMAIN CABIN FLOOREAM AT FRAME 31 RBL 40 HAS CORROSION AT NUTPLATE ON LOWER FLANGE. REMOVED CORROSION, FOUND TO BE IN LIMITS IAW SRM 53-10-15 FIG 106, TREATED, PRIMED AND TOPCOATED IAW SRM 51-75-10.Jan 23, 2017 · N655FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA201511273801Contactor · faultyAT LIFT OFF ON TAKEOFF, THE FOLLOWING OCCURRED. FCP WENT BLANK. ATS LEVER TRIPPED OFF. INSTRUMENTATION ON BOTH SIDES DISAPPEARED, EXCEPT FOR ADI'S & SPEED SCALES. FMS ON BOTH SIDES WENT TO INDEPENDENT OPERATIONS, FCP INTERMITTENTLY RE-ILLUMINATED, BUT SETTNov 27, 2015 · N655FE · Airbus A300F4605R · AC Generator-AlternatorSDR FDEA201505041384Warning Buzzer · inoperativeL1 DOOR ESCAPE SLIDE BUZZER WILL NOT TEST. WARNING LIGHT WORKS OK. L1 CREW ENTRY DOOR ESCAPE SLIDE WARNING SYS BUZZERS INOPERATIVE. TROUBLE SHOT IAW TSM 52-73-00 FIG 101. WIRING CHECKED AT TEST SW GOOD. CLEANED WARNING HORN TERMINALS & TIGHTENED CONNECTIOMay 4, 2015 · N655FE · Airbus A300F4605R · Escape SlideSDR FDEA201410133135Skin · wornLT WING BOTTOM SKIN PANELWORN. REPAIRED IAW EA 6-5730-T0312234 PT1. MAJOR REPAIR IAW GMM6-2-100.Oct 13, 2014 · N655FE · Airbus A300F4605R · Wing, Plate/SkinSDR FDEA201410123119Skin · wornNR 1 ENGINE PYLON TO WING AREA HOLE FOR HYD PIPE NR 3 WORN. LT WING BOTTOM SKIN PANEL 2 PYLON SYS HOLE NR 3 WORN. REPAIRED IAW EA.6-5730-T0312234 A PT1. MAJOR REPAIR IAW GMM6-2-100.Oct 12, 2014 · N655FE · Airbus A300F4605R · Wing, Plate/SkinSDR FDEA201409292851Adapter · corrodedMAIN DECK CARGO BAY FRAME 47 BETWEEN Y-450 & Y-953 FLOORBEAM ADAPTER CORRODED. REPAIRED IAW AMM 20-21-12-00. MAJOR REPAIR IAW GMM6-2-100.Sep 29, 2014 · N655FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA201409252766Support Beam · crackedFORWARD CARGO BAY UPPER CUT OUT BETWEEN FRAMES 22 - 23 Y-1456 & Y-1959 CYLINDER ASSEMBLY SUPPORT BEAM CRACKED. SUPPORT BEAM REPLACED IAW SRM 51-40-21. MAJOR REPAIR IAW GMM6-2-100.Sep 25, 2014 · N655FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA201409252768Rib · crackedRIGHT PYLON CANTILEVER BEAM ON RIB J08 - RIB A11 FOUND CRACKED. REPAIRED IAW SRM 54-52-11 FIG.201. MAJOR REPAIR IAW GMM6-2-100.Sep 25, 2014 · N655FE · Airbus A300F4605R · Nacelle/Pylon, Frame/Spar/RibSDR FDEA201409252767Rib · crackedLEFT PYLON CANTILEVER BEAM ON RIB J08 - RIB A11 FOUND CRACKED. REPAIRED IAW SRM 54-52-11 FIG.201. MAJOR REPAIR IAW GMM6-2-100.Sep 25, 2014 · N655FE · Airbus A300F4605R · Nacelle/Pylon, Frame/Spar/RibSDR FDEA201407221923Lug · corrodedLEFT RIB 5 FWD LUG HAS CORROSION IN BORE & IN FWD & AFT FACES. COMPLIED WITH EA 6-5710-T0309888 P 1 WINGS BASIC WING STRUCTURE LT MLG RIB 5 FWD LUG CORROSION.Jul 22, 2014 · N655FE · Airbus A300F4605R · Wing, Rib/BulkheadSDR FDEA201406081360Damper · failedLANDING GEAR FAILED TO RETRACT AFTER TAKE OFF. TRIED TO RAISE GEAR USING BOTH SYS 1 & SYS 2 & BOTH FAILED. COULD NOT GET GEAR HANDLE PAST NEUTRAL. AFTER LT PITCH DAMPER WAS REMOVED & REPLACED IAW AMM 32-31-00-05, PERFORMED FUNCTIONAL TEST 3.A.(4) GEAR RETJun 8, 2014 · N655FE · Airbus A300F4605R · Landing Gear Retraction/Extension SystemSDR FDEA201309092164Monitor · failedPASSING APPROX 10,000', MESSAGE ECAM WARNING OF BLUE HYD SYS OVERHEAT, COMPLIED WITH QRH. INDICATION REMAINED ON REMAINDER OF FLIGHT AND TAXI. R & R RESERVOIR OVERHEAT MONITOR UNIT, 38GR, REF AMM 29-33-12. OPS CHECKS GOOD. RAN ENGINES AND MOVED FLIGHT CONTRSep 9, 2013 · N655FE · Airbus A300F4605R · Hydraulic Indicating SystemSDR FDEA201210183665Uplock · brokenOPEN RT NOSE GEAR DOOR WOULD NOT CLOSE AT GEAR RETRACTION. FOUND LT NOSE GEAR DOOR NOT FULLY CLOSED WHEN ACFT ARRIVED AT THE GATE. LEFT NOSE GEAR DOOR UPLOCK LATCH MECHANISM BROKEN R & R UPLOCK ASSY IAW AMM 32-31-14-04. GROUND DOOR OPENING AND CLOSING TEOct 18, 2012 · N655FE · Airbus A300F4605R · Landing Gear Door Retract SectionSDR FDEA201206142234Skin · misrepairedFUSELAGE SKIN FR 64-65 S35-38 RT MEASURED THE DOUBLER THICKNESS IAW NTM 51-10-04. THE SUBJECT REPAIR IS NOT IAW SRM 53-10-12, FIG 209, REMOVED THE DOUBLER AND REPAIR AGAIN IAW EA 6-5330-158065.Jun 14, 2012 · N655FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA201206122205Skin · misrepairedSKIN FR25-26, S38R MISREPAIRED. REPAIRED IAW EA 6-5330-158063. THE REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jun 12, 2012 · N655FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA201206042071Seat Track · corrodedMAIN DECK FR 45 - 49 Y953 SEAT TRACK CORRODED. REMOVED THE CORRODED SEAT TRACK PER SRM 51-40-21. FABRICATED REPAIR SEAT TRACK PER DWG A53810087. INSTALLED THE REPAIR SEAT TRACK PER SRM 51-40-21. APPLIED PAINT PER SRM 51-75-10. COMPLIED WITH EA 6-5310-Jun 4, 2012 · N655FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201206042072Seat Track · corrodedSEAT TRACK UPPER FLANGE FOUND DELAMINATION AT FR 38.2. REMOVED THE CORRODED SEAT TRACK IAW SRM 51-40-21. DRILLED FASTENER HOLES ON THE NEW SEAT TRACK IAW SRM 51-40-44. INSTALLED THE NEW SEAT TRACK IAW SRM 51-40-21 APPLIED PAINT IAW SRM 51-75-10.Jun 4, 2012 · N655FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201206032069Floor Support · corrodedMAIN DECK CARGO FLOOR SUPPORT UPPER FLANGE FOUND CORROSION BETWEEN FR 12 - 13. REMOVED THE CORRODED FLOOR SUPPORT IAW SRM 51-40-21. DRILLED FASTENER HOLES ON THE NEW FLOOR SUPPORT IAW SRM 51-40-44, INSTALLED THE NEW FLOOR SUPPORT IAW SRM 51-40-21. APPLIEDJun 3, 2012 · N655FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201206032068Seat Track · corrodedMAIN DECK FR 54-55, Y953 SEAT TRACK CORRODED. REMOVED THE CORRODED SEAT TRACK IAW SRM 51-40-21. DRILLED FASTENER HOLES ON THE NEW SEAT TRACK IAW SRM 51-40-40 INSTALLED THE NEW SEAT TRACK IAW SRM 51-40-21. APPLIED FINISH TO THE FASTENER HEADS IAW SRM 51-75-1Jun 3, 2012 · N655FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201206032066Floor Support · corrodedMAIN DECK CARGO FLOOR SUPPORT UPPER FLANGE FOUND CORRODED BETWEEN FR12-13 , Y730. REMOVED CORRODED FLOOR SUPPORT IAW SRM 51-40-21. DRILLED FASTENER HOLES ON THE NEW FLOOR SUPPORT IAW SRM 51-40-44. INSTALLED THE NEW FLOOR SUPPORT IAW SRM 51-40-21. APPLIED FJun 3, 2012 · N655FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA201206032065Seat Track · corrodedMAIN DECK FR 40-45 -Y450 SEAT TRACK FOUND CORROSION AROUND FASTENER HOLES REMOVED THE CORRODED SEAT TRACK IAW SRM 51-40-21. DRILLED FASTENER HOLES ON THE NEW SEAT TRACK IAW SRM 51-40-40. INSTALLED THE NEW SEAT TRACK IAW SRM 51-40-21 APPLIED FINISH TO THE FJun 3, 2012 · N655FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201206032064Seat Track · corrodedMAIN DECK FR40-45 Y953 SEAT TRACK CORRODED. REMOVED THE CORRODED SEAT TRACK IAW SRM 51-40-21. DRILLED FASTENER HOLES ON THE NEW SEAT TRACK IAW SRM 51-40-40. INSTALLED THE NEW SEAT TRACK IAW SRM 51-40-21. APPLIED FINISH TO THE FASTENER HEADS IAW SRM 51-75-1Jun 3, 2012 · N655FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201206032063Structure · crackedAT B-CHECK, FOUND LOWER FWD CARGO DOOR UPPER CORNER CRACKED AT FASTENER. REPAIRED UPPER AFT CORNER OF LWR FWD CARGO DOOR SKIN IAW SRM 52-31-00, FIG 202.Jun 3, 2012 · N655FE · Airbus A300F4605R · Cargo/Baggage DoorsSDR FDEA201205302010Frame · deformedFRAME 60 S13 - 14R DEFORMED. REPAIRED THE FRAME IAW SRM 53-10-13-201, PARA 5.May 30, 2012 · N655FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA201205302009Frame · deformedFRAME 74 S11 - 12R DEFORMED. REPAIRED THE FRAME IAW SRM 53-10-13-201, PARA 5.May 30, 2012 · N655FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA201205302008Frame · chafedFRAME 58 CHAFED & DISTORTED B/W S12-13 L. REPAIRED THE FRAME IAW SRM 53-10-13-201, PARA 5.May 30, 2012 · N655FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA201205281996Floor Support · corrodedLONGITUDINAL FLOOR SUPPORT UPPER FLANGE CORRODED BETWEEN FR13-14. CUT OUT CORRODED FLOOR SUPPORT IAW SRM 53-12-15-201, C2 PARA 5G. FABRICATED REPAIR PARTS IAW SRM 53-12-15-201, C2 PARA 5G, DYE PENETRANT INSPECTION FOR REPAIR PARTS IAW NTM 51-90-20, NO CRACMay 28, 2012 · N655FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201205281995Skin · chafedFUSELAGE SKIN EXTERIOR SURFACE CHAFED AT FR33-4" STR40 RT SIDE LOCATION. BLENDED OUT AND SMOOTHED CHAFING AREA IAW SRM 51-74-10. EXCEED LIMIT IAW SRM 53-10-12-101. PERFORMED DOUBLER REPAIR IAW SRM 53-10-12/201, FIG 208.May 28, 2012 · N655FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA201202150586Manifold · leakingDURING PREFLIGHT, OIL QUANTITY 18 QUARTS. AT LEVEL FLIGHT OIL QUANTITY NR 2 WAS 13 QUARTS. OIL QUANTITY DECREASED TO 7 QUARTS IN CRUISE. AT BLOCK-IN OIL QUANTITY INDICATED 13 QUARTS. FOUND OIL PUDDLING UNDER NR 2 ENGINE FAN BLADES AT BOTTOM OF FAN COWL. OILFeb 15, 2012 · N655FE · Airbus A300F4605R · Turbine Engine Oil SystemSDR FDEA201110124449Warning Light · false activationON TAKEOFF ROLL APPROX 80 KNOTS GOT MASTER WARNING LIGHT AND CRC. NO INDICATIONS ON ECAM. ABORTED TAKEOFF AT APPROX 90 KNOTS. R & R FLIGHT WARNING COMPUTER NR 1 & NR 2 IAW MM 31-53-34-04. VERIFIED NR 1 & NR 2 FWC CONTAINS IDENTICAL SOFTWARE CODES. PERFORMEDOct 12, 2011 · N655FE · Airbus A300F4605R · Central WarningSDR FDEA201107313048Rib · corrodedRT WING MLG RIB 5, FWD LUG, FWD BUSHING IS CORRODED AND PITTED. COMPLIED WITH EA 6-5710-14562 WING RT RIB 5 FWD LUG CORROSION REF N00008 AFTER THE REMOVAL OF LEVEL 1 CORROSION.Jul 31, 2011 · N655FE · Airbus A300F4605R · Wing, Rib/BulkheadSDR FDEA200912214489Seat Track · crackedAFT CARGO COMPARTMENT, DUMMY SEAT TRACK OVERHEAD MAIN FLOOR STRUCTURE IS CRACKED AT THE OTBD END LOCATED AT FRAME 60; RBL 64. REMOVED FLOOR PANELS 252 RT AND 252 WH IAW AMM 53-10-25-4. REMOVED CRACKED DUMMY SEAT TRACK IAW SRM 51-40-21, PARA 7. INSTALLED NEW Dec 21, 2009 · N655FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200912174478Seat Track · crackedAFT CARGO COMPARTMENT DUMMY SEAT TRACK, OVERHEAD MAIN CABIN FLOOR STRUCTURE, LOCATED AT FRAME 61; RBL 42 IS CRACKED IN THE RADIUS. REMOVED AND REPLACED DUMMY SEAT TRACK PN R5370617920400 SRM 51-40- 40, PG 21 AND SRM 51-40-21, PARA 5 AND 6.Dec 17, 2009 · N655FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200912144463Skin · damagedACCESS DOOR 312 AR FWD UPPER CORNER IS DAMAGED. CHECKED LIMITS AND FOUND TO BE OUT OF LIMITS IAW SRM 52-41-00, PARA 5, FIG 102. CUT OUT DAMAGE AND FABBED REPAIR PART FILLER AND DOUBLER IAW SRM 52-41-12, FIG 202. ALODINED IAW SRM 51-21-10, PG 1. PRIMED IAW Dec 14, 2009 · N655FE · Airbus A300F4605R · Service DoorsSDR FDEA200912114414Frame · crackedRT WING FRAME 47, HOLE "E" HAS A CRACK INDICATION AT 6 O'CLOCK AT DEPTH 15/32. COMPLIED WITH EA 6-5710-135118.Dec 11, 2009 · N655FE · Airbus A300F4605R · Wing SparSDR FDEA200912114413Floorbeam · crackedAFT PIT CROSSBEAM IS CRACKED JUST BELOW THE SEAT ADAPTER FITTING AT FRAME 60; RBL 48. REMOVED CRACKED SECTION OF CROSSBEAM IAW SRM 53-10-15, FIG 204 AND SRM 51-40-21, PARA 7. INSTALLED REPAIR PARTS IAW SRM 53-10-15, FIG 207, SHEET 18, PGS 291 / 292 AND SRM 5Dec 11, 2009 · N655FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA200912094389Floor Panel · damagedBULK CARGO COMPARTMENT 2ND TO AFT LONG FLOOR PANEL IS DAMAGED AT THE AFT RT SIDE. REMOVED FLOOR PANEL 161 GF IAW AMM 53-40-25-4, PARA 1 TO FOM. FABRICATED NEW FLOOR PANEL IAW DWG SRZ 25-005, REV "H" AND SRZ 25-011, REV "C". INSTALLED FLOOR PANEL 161 GF IAW Dec 9, 2009 · N655FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200912084378Support · crackedAVIONICS COMPARTMENT BATTERY RACK SUPPORT TRANSVERSE INTERCOSTAL IS CRACKED AT THE FASTENER HOLE AT FRAME 15.Dec 8, 2009 · N655FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
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