N676FE

Service difficulty reports · 178

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 = 'N676FE' 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 FDEA2020071761547Floor Panel · damagedBULK CARGO FLOOR PANEL 162HF HAS A PULLED THROUGH INSERT, MISSING. FABRICATED A FLOOR PANEL IAW DWG SRZ-25-005R. CATAGORY -A- MAJOR REPAIR.Jul 16, 2020 · N676FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA2020071761546Floor Panel · delaminatedBULK CARGO FLOOR PANEL 161GF WAS DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005R. CATAGORY -A- MAJOR REPAIR.Jul 16, 2020 · N676FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA2020071761545Floor Panel · delaminatedFLOOR PANEL 132QG WAS DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ-25-005R, CATAGORY -A- MAJOR REPAIR.Jul 16, 2020 · N676FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA2020071761544Floor Panel · delaminatedFLOOR PANEL 132SG WAS DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ-25-005R. A CATAGORY -A- MAJOR REPAIR.Jul 16, 2020 · N676FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA2020071761543Floor Panel · crackedFLOOR PANEL 152QF WAS CRACKED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ-25-005R. CATAGORY -A- MAJOR REPAIR.Jul 16, 2020 · N676FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA2020071761531Floor Panel · delaminatedFLOOR PANEL 132KG BROKEN. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ-25-005R. CATAGORY -A- MAJOR REPAIR.Jul 16, 2020 · N676FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202007161530Floor Panel · delaminatedFLOOR PANEL 131NG BROKEN. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ-25-005R, CATAGORY -A- MAJOR REPAIR.Jul 16, 2020 · N676FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA202007161529Floor Panel · delaminatedFLOOR PANEL 131SG DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ-25-005R. CATAGORY -A- MAJOR REPAIR.Jul 16, 2020 · N676FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA2020071761528Floor Panel · delaminatedFLOOR PANEL 131KG DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ-25-005R. CATAGORY -A- MAJOR REPAIR.Jul 16, 2020 · N676FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA2020073041510Rib · crackedFOUND CRACK ON RT CTR FLAP AT RIB 27 APPROX. 4.8" FWD OF REAR SPAR UPPER SKIN. REPAIRED RIB FLANGE IAW SRM 57-50-00, FIG. 205, CAT A MAJOR REPAIR.Jul 14, 2020 · N676FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA2020072341511Floor Panel · crackedFLOOR PANEL 152PF CRACKED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ-25-005R, CATEGORY -A- MAJOR REPAIR.Jul 14, 2020 · N676FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA2020072341509Floor Panel · crackedFLOOR PANEL 151MF CRACKED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ-25-005R, CAT A MAJOR REPAIR.Jul 14, 2020 · N676FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA202007141508Floor Panel · crackedFLOOR PANEL 152TF CRACKED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ-25-005R, CAT A MAJOR REPAIR.Jul 14, 2020 · N676FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA2020071741512Floor Panel · delaminatedBULK CARGO FLOOR PANEL 161CF DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ-25-005R, CATEGORY -A- MAJOR REPAIR.Jul 14, 2020 · N676FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA202007131503Floor Panel · brokenMAIN DECK FLOOR PANEL 252NG BROKEN. FABRICATED MAIN DECK FLOOR PANEL 252NG ON TD/000414 PER DRAWING SRZ-25-005R, CAT "A" AND MAJOR REPAIR.Jul 13, 2020 · N676FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA202007131502Floor Panel · brokenMAIN DECK FLOOR PANEL 231HG IS BROKEN. FABRICATED MAIN DECK FLOOR PANEL 231HG ON TD/000406 PER DRAWING SRZ-25-005R, CLASS CAT "A" AND MAJOR REPAIR.Jul 13, 2020 · N676FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA202007131501Floor Panel · brokenMAIN DECK FLOOR PANEL 231JG IS BROKEN. FABRICATED MAIN DECK FLOOR PANEL 231JG ON TD/000426 PER DRAWING SRZ-25-005R, CLASS CAT "A" AND MAJOR REPAIR.Jul 13, 2020 · N676FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA202007131500Floor Panel · brokenMAIN DECK FLOOR PANEL 241NJ IS BROKEN. FABRICATED MAIN DECK FLOOR PANEL 241NJ ON TD/000429 PER DRAWING SRZ-25-005R, CLASS CAT "A" AND MAJOR REPAIR.Jul 13, 2020 · N676FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA202007131499Floor Panel · brokenMAIN DECK FLOOR PANEL 251DF IS BROKEN. FABRICATED MAIN DECK FLOOR PANEL 251DF ON TD/000415 PER DRAWING SRZ-25-005R, CLASS CAT "A" AND MAJOR REPAIR.Jul 13, 2020 · N676FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA202007131498Floor Panel · brokenMAIN DECK FLOOR PANEL 241MJ BROKEN. FABRICATED MAIN DECK FLOOR PANEL 241MJ ON TD/000425 PER DRAWING SRZ-25-005R, CLASS CAT "A" AND MAJOR REPAIR.Jul 13, 2020 · N676FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA202007131497Floor Panel · brokenMAIN DECK FLOOR PANEL 231RG IS BROKEN. FABRICATED MAIN DECK FLOOR PANEL 231RG ON TD/000427 PER DRAWING SRZ-25-005R, CLASSIFIED CAT "A" AND MAJOR REPAIR.Jul 13, 2020 · N676FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA202007131496Floor Panel · brokenMAIN DECK FLOOR PANEL 251QH IS BROKEN. FABRICATED MAIN DECK FLOOR PANEL 251QH ON TD/000428 PER DRAWING SRZ-25-005R, CLASSIFIED CAT "A" AND MAJOR REPAIR.Jul 13, 2020 · N676FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201909242334Computer · faultedPDIS 676 28-40 8572 24SEP19 ELP FACT U LOGPAGES:3167557 CLIMBING THROUGH FL 200, ECAM MEMO PAGE SHOWED ALL XX'S ON GROSS WT CG, AND TOTAL FUEL INDICATION. ECAM FUEL PAGE SHOWED ALL XX'S ON ALL TANKS. THE FUEL PANEL ON THE OVERHEAD SHOWED QUANTITIES FOSep 24, 2019 · N676FE · Airbus A300F4605R · Fuel Indicating SystemSDR FDEA2019021410375Power Supply · malfunctionedRIGHT CABIN DOOR WILL NOT ARM NO SLIDE INDICATION ON ECAM AUTONOMOUS STANDBY POWER SUPPLY UNIT C/B RESET. AFTER RESET,DOOR ARMED AND INDICATION OPS SATIS ON ECAMFeb 11, 2019 · N676FE · Airbus A300F4605R · Emergency EquipmentSDR FDEA201810112860Power Unit · inoperativeL1 AND R1 DOORS ESCAPE SLIDES RELEASE WARNING LIGHT INOPERATIVE. REMOVED & REPLACED THE AUTONOMOUS STANDBY SUPPLY UNIT, 70 WN IAW AMM 52-73-18-04 AND THE BOTH EMERGENCY POWER SUPPLY BATTERY IAW AMM 33-51-14-04. PERFORMED AN OPS TEST IAW AMM 52-73-00-05-02, PAOct 11, 2018 · N676FE · Airbus A300F4605R · Door Warning SystemSDR FDEA201810112853Indication Sys · inoperativeR1 ENTRY DOOR ECAM SLIDE INDICATION SYSTEM INOP. DOOR ESCAPE SLIDE ARMING SYSTEM IS TO BE VERIFIED AS FULLY ARMED PRIOR TO EACH DEPARTURE. UNABLE TO HAVE BOTH L1 AND R1 DOOR ESCAPE SLIDE INDICATION WARNING LIGHT ILLUMINATED AND R1 SLIDE. ECAM INDICATION WHEN Oct 11, 2018 · N676FE · Airbus A300F4605R · Door Warning SystemSDR FDEA201803110652O-Ring · tornAT CRUISE OVER KTYS FL310 ECAM GRN HYD SYS LOW PSI, SPOILER NR 6 FAULT, THEN ECAM GRN HYD SYS LOW RSVR. GRN SYS HYD QUANTITY GAUGE ON OVERHEAD PANEL AT RED DOT. GRN SYS HYD QUANTITY INDICATOR ON ECAM IN AMBER. AFTER MANUAL GEAR EXTENSION, GRN SYS HYD QUANTITIEMar 11, 2018 · N676FE · Airbus A300F4605R · Hydraulic System, MainSDR FDEA201801280270Bracket · crackedANGLE BRACKET CRACKED, INBD OF SEAT TRACK -Y953, FRAME 47, REMOVED THE ANGLE BRACKET IAW SRM 51-40-21, FABRICATED NEW BRACKET IAW EA 6-5340-T0337966, AND INSTALLED IAW SRM 51-40-21, REPAIR CLASSIFED AS MAJOR.Jan 28, 2018 · N676FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201801200124Seat Track · brokenSEAT TRACK SCALOP BROKEN IN MDC BETWEEN FRAMES 57.1 AND 57.2, -Y450. FOUND SEAT TRACK TO BE OUT OF LIMITS IAW SRM 53-1--16, FIG 102. FABRICATED A NEW SEAT TRACK IAW SRM 53-10-16 FIG. 201 AND INSTALLED IAW SRM 53-10-16 FIG 201, MAJOR REPAIR.Jan 20, 2018 · N676FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201801180118Seat Track · corrodedCORROSION ON SEAT TRACK FLANGES UPPER AND LOWER SURFACES AT FRAME 69, Y0. CORROSION FOUND OUT OF LIMITS IAW SRM 53-10-16. REMOVED AND REPLACED THE SECTION IAW SRM 51- 27-11, AND SRM 51-40-44. INSTALLED THE SPLICES IAW SRM 53-10-16, FIG 201B, AND SRM 51-4Jan 18, 2018 · N676FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201801180117Seat Track · gougedSEAT TRACK SCALOPS GOUGED BETWEEN FRAMES 57 AND 57.1, Y950. CUT OUT DAMAGED SEAT TRACK SECTION IAW SRM 53-10-16, FIG 201. FABRICATED A NEW SEAT TRACK IAW SRM 53-10-16, FIG 201. INSTALLED IAW SRM 51-40-21. MAJOR REPAIR.Jan 18, 2018 · N676FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201801180116Floor Panel · damagedMAIN DECK FLOOR PANEL 241LH DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.Jan 18, 2018 · N676FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201801180114Floor Panel · brokenMAIN DECK FLOOR PANEL 241GJ BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.Jan 18, 2018 · N676FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201801180113Floor Panel · brokenMAIN DECK FLOOR PANEL 252CH BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.Jan 18, 2018 · N676FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201801180112Floor Panel · brokenMAIN DECK FLOOR PANEL 252NH BROKEN. FABRICAED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.Jan 18, 2018 · N676FE · Airbus A300F4605R · Fuselage Structure (General)SDR FDEA201801180111Floor Panel · brokenMAIN DECK FLOOR PANEL 252QH BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.Jan 18, 2018 · N676FE · Airbus A300F4605R · Fuselage Structure (General)SDR FDEA201801180110Floor Panel · damagedMAIN DECK FLOOR PANEL 241RJ BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIRJan 18, 2018 · N676FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201801180109Floor Panel · damagedMAIN CABIN FLOOR PANEL 241JF BROKEN. FABRCATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIRJan 18, 2018 · N676FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201510093131Doubler · wornAGING INSPECTION - EXISTING REPAIR ON LT INBD FLAP MAIN SECTION UPPER SKIN RIB 11A- RIB 14A STG 2.1-STG 2.2. WORN DAMAGE WAS FOUND ON THE EXTERNAL DOUBLE. REMOVED THE DAMAGED DOUBLER AND REPAIRED AGAIN PER A300-600F SRM 57-50-00 FIG 205 AND COMPLETED, TRACKIOct 9, 2015 · N676FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA201510043052Pressure Deck · crackedMDCC HORIZONTAL PRESSURE DECK FRAME 47, Y0 - -Y450, WEB CRACKED APPROX 0.5 INCH IN LENGTH. NDT FOUND THE LENGTH OF THE CRACK WAS OUT OF LIMITS IAW SRM 53-15-15-201 C2 & NTM 51-10-07, L=30 MM. FABRICATED THE NEW WEB IAW DWG A53832100 ISSUE G. PERFORMED THE ROct 4, 2015 · N676FE · Airbus A300F4605R · Fuselage Main, BulkheadSDR FDEA201510013015Frame · crackedCENTER WING, JOINT AT FRAME 40 RT UPPER HOLE HAS CRACK SIGNAL. PERFORMED THE REPAIR IAW EA 6-5710-T0320754 PT 1. THIS REPAIR WAS CATEGORY B & WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 129.Oct 1, 2015 · N676FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA201510013014Frame · crackedCENTER WING, JOINT AT FRAME 40 LT UPPER HOLE HAS CRACK SIGNAL. PERFORMED THE REPAIR IAW EA 6-5710-T0320754 PT 1. THIS REPAIR WAS CATEGORY B & WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 129.Oct 1, 2015 · N676FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA201510013012Frame · crackedCENTER WING, JOINT AT FRAME 40 LT LOWER HOLE HAS CRACK SIGNAL. PERFORMED THE REPAIR IAW EA 6-5710-T0320754 PT 1. THIS REPAIR WAS CATEGORY B & WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 129.Oct 1, 2015 · N676FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA201509272969Crossbeam · crackedMDCC CROSSBEAM CRACKED AT FRAME 58, Y1700. IAW SRM 53-10-15 FIGURE 211 REWORK THE STIFFENER & CUT OUT THE CRACK. PERFORM HFEC INSPECTION TO THE CUT OUT & REWORKED AREA IAW NTM 51-10-08 & NO CRACK FOUND. MANUFACTURED THE REPAIR ANGLE & DRILL THE FASTENER HOSep 27, 2015 · N676FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA201509212905Packing · damagedGREEN HYD QTY IN YELLOW BAND DURING CRUISE. FOUND BLEEDER PLUG ON SIDE OF GREEN MANIFOLD LEAKING. REPLACED PACKING ON BLEEDER PLUG, LEAK & OPERATIONS CHECKED GOOD IAW AMM 29-10-00-03 & 29-10-00-03.Sep 21, 2015 · N676FE · Airbus A300F4605R · Hydraulic System, MainSDR FDEA201401100082Coalescer Bag · dirtySMOKE APPEARED IN COCKPIT WITH NO ECAM INDICATIONS, DIVERTED. DURING TOUCHDOWN ECAM DISPLAYED AVIONICS SMOKE THEN EXTINGUISHED. FOUND EXCESSIVE DE-ICE FLUID IN MAIN WHEEL WHEEL WHILE ACCESSING AIR CONDITION PACK BAY AND CLEANED. INSPECTED BOTH LT & RT PACK CJan 10, 2014 · N676FE · Airbus A300F4605R · Humidity Control SystemSDR FDEA201310112476Fitting · corrodedLT MLG NR 5 RIB FWD LUG FITTING CORRODED REPAIR THE LUG FITTING IAW DWG:R57240425 AND EA 6-5710-T0302747.Oct 11, 2013 · N676FE · Airbus A300F4605R · Wing, Landing Gear Attach FittingsSDR FDEA201310112474Fitting · corrodedRT MLG NR 5 RIB FWD LUG FITTING CORRODED REPAIR THE LUG FITTING IAW DWG:R57240425 AND EA:6-5710-T0302748.Oct 11, 2013 · N676FE · Airbus A300F4605R · Wing, Landing Gear Attach FittingsSDR FDEA201307131552Pitot Tube · obstructedRTO AT 90 KTS AIRSPEED SPLIT ON TAKEOFF ROLL. F/O AND STBY AIRSPEED MATCHED AT 90 KTS, CAPTAIN`S AIRSPEED AT 50 KTS. REMOVED AND REPLACED CAPTAIN'S PITOT PROBE IAW MM 34-11-15-04. PITOT TUBE THAT WAS REMOVED HAD SMALL BLACK DEBRIS COME OUT OF IT.Jul 13, 2013 · N676FE · Airbus A300F4605R · Pitot/Static SystemSDR FDEA201303200625Computer · failedAVIONICS SMOKE DURING CLIMBOUT, WARNING WAS ACCOMPANIED BY ODOR. NO VISUAL SMOKE ONLY FUMES. FUMES WAS PHENOLIC BURNING ODOR. FLC SYS NR 2 CIRCUIT BREAKER WAS TRIPPED AND DISCOVERED BY MX AFTER BLOCK IN. R & R FLC NR 2 IAW AMM 27-23-26-04. OPS CHECKED GOOMar 20, 2013 · N676FE · Airbus A300F4605R · Rudder Tab Control System
Back to N676FE