N661FE

Service difficulty reports · 318

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 = 'N661FE' 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 08FDEA01562Rub Strip · damagedRIGHT WING INBD FLAP UPPER SKIN RUB STRIP IS WORN. REMOVED & REPLACED THE CHAFE / RUB STRIP IAW SRM 57-50-00.Apr 25, 2008 · N661FE · Airbus A300F4605R · Trailing Edge FlapsSDR 08FDEA01628Skin · dentedRT WING INBD FLAP LWR SKIN HAS A NUMBER OF DENTS. MEASURED DEEPEST DENT TO BE D= .028 INCH DEEP AND X= .500" WIDE. FOUND TO BE WITHIN LIMITS PER SRM 57-50-00 PG 101 DEPTH GAUGE NR T8492F. GOUGE BLENDED ORIG MAT .031" REMAINING .021, REMOVED .010" FOUND TO Apr 24, 2008 · N661FE · Airbus A300F4605R · Trailing Edge FlapsSDR 08FDEA01627Skin · dentedRT WING INBD AILERON HAS NUMEROUS HAIL DENTS ON UPPER SKIN. DENT FOUND TO BE OUT OF LIMITS IAW SRM 57-61-11, MAT ID 2024-T3 PO NR 605306.1 IAW SRM 57-61-11 AND 51-21-00, PAGE 23-24 TABLE 3 SHEET 3, FABBED DOUBLER AND FILLER IAW SRM 57-61-11, FIG 206. ALODINEApr 24, 2008 · N661FE · Airbus A300F4605R · AileronsSDR 08FDEA01537Structure · damagedNR 2 ENGINE OUTBD T/R TRANSLATING COWL HAS EXPOSED COMPOSITE CORE. REPLACED THE NR 2 ENGINE OUTBD THRUST REVERSER TRANSLATOR COWL IAW AMM 78-32-11-4. REFERRED ALL WORK TO NON-ROUTINE N01042.Apr 24, 2008 · N661FE · Airbus A300F4605R · Engine Thrust ReverserSDR 08FDEA01536Skin · erodedNR 2 ENGINE OUTBD T/R, ALL BLOCKER DOORS HAVE EXPOSED COMPOSITE CORE, SKIN IS ERODED. REPLACED THR NR 2 ENGINE THRUST REVERSER TRANSLATOR COWL IAW AMM 78-32-11-4. REFERRED ALL WORK TO NON-ROUTINE N01042.Apr 24, 2008 · N661FE · Airbus A300F4605R · Engine Thrust ReverserSDR 08FDEA01535Structure · looseNR 2 ENGINE OUTBD T/R UPPER T/E COMPOSITE REPAIR EDGES ARE LOOSE. REPLACED NR 2 ENGINE OUTBOARD THRUST REVERSER TRANSLATOR COWL IAW A300-600 AMM 78-32-11-4. REFERRED ALL WORK TO NON-ROUTINE N01042.Apr 24, 2008 · N661FE · Airbus A300F4605R · Engine Thrust ReverserSDR 08FDEA01533Structure · looseNR 2 ENGINE OUTBD T/R T/E HAS LOOSE COMPOSITE REPAIR EDGE. REPLACED THE NR 2 ENGINE OUTBOARD TRANSLATOR COWL IAW AMM 78-32-11-4. REFERRED ALL WORK TO NON-ROUTINE N01042.Apr 24, 2008 · N661FE · Airbus A300F4605R · Engine Thrust ReverserSDR 08FDEA01532Panel · delaminatedAIR CONDITION EXTERNAL FAIRING PANEL NR 144 GR IS DELAMINATING ON THE INTERNAL SKIN. REPAIRED PANEL 144 GR BY REMOVING THE DAMAGE AND APPLYING A WET LAY UP IAW SRM 51-77-12 AND RESTORED THE FINISH IAW SRM 51-75-10.Apr 24, 2008 · N661FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR 08FDEA01531Panel · delaminatedAIR CONDITION EXTERNAL FAIRING PANEL NR 144 HR IS DELAMINATING ON THE INTERNAL SKIN. REPAIRED PANEL BY REMOVING THE DAMAGE AND APPLYING A WET LAY UP IAW SRM 51-77-12 AND RESTORED THE FINISH IAW SRM 51-75-10.Apr 24, 2008 · N661FE · Airbus A300F4605R · Aerodynamic FairingsSDR 08FDEA01530Fairing · delaminatedAIR CONDITIONING EXTERNAL FAIRING NR 143 GL IS DELAMINATED. REMOVED THE DAMAGE; PREPPED AREA FOR REPAIR; APPLIED A LAY-UP REPAIR; REFINISHED SURFACE IAW SRM 51-77-12 & SRM 53-15-73.Apr 24, 2008 · N661FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR 08FDEA01529Floorboard · delaminatedEMPENAGE ACCESS THRU 312 AR, THE FLOORBOARD ON THE LEFT SIDE OF THE A/C AFT OF THE PNEUMATIC DUCT AT FRAME 84 IS DELAMINATED. FABRICATED NEW PANEL; LOCATED & DRILLED NEW HOLES; INSTALLED INSERTS; POTTED & CURED BOARD EDGES. SANDED EDGES AS NEEDED; APPApr 24, 2008 · N661FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA01528Floorboard · delaminatedEMPENNAGE ACCESS THRU 312 AR, THE FLOORBOARD ON THE LEFT SIDE OF THE A/C FWD OF THE PNEUMATIC DUCT AT FRAME 84 IS DELAMINATED. FABRICATED NEW PANEL. LOCATED & DRILLED NEW HOLES USING OLD FLOORBOARD AS A TEMPLATE; INSTALLED INSERTS; POTTED & CURED BOARD EDGApr 24, 2008 · N661FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA01524Web · crackedLEFT AIR CONDITION FAIRING SUPPORT WEB FOR FAIRING 143 FL; AFT WEB OUTER ATTACH POINT TO BODY IS CRACKED. REMOVED SUPPORT AND WEB REF FEDEX A300-600 SRM 51-40-21. MATERIAL ID IS 2024-T3, 0.050 REF FEDEX A300-600 SRM 53-15-73. FORMED DOUBLER REF FEDEX A300Apr 24, 2008 · N661FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR 08FDEA01526Skin · gougedRIGHT WING ROOT AREA EXTERNAL SKIN HAS NUMEROUS GOUGED PLACES BETWEEN FRAME 51 AND FRAME 52. REMOVED THE DAMAGE & FOUND SKIN TO BE OUT OF LIMITS. COMPLIED WITH E.A. 6-5310-118492.Apr 24, 2008 · N661FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR 08FDEA01525Attach Angle · crackedNR 2 PYLON ATTACH ANGLE AND RIB 3-A (OUTBD) IS CRACKED. REMOVED SHIM IAW A300-600 SRM 51-40-21 PG 7. PART IS IDENTIFIED AS A SHIM WITH A CRACK 1 INCH LONG IAW SRM 54-52-31 FIG 2 ITEM 15. FABRICATED SHIM. SHIM IS INSTALLED IAW SRM 51-40-2 PG 7.Apr 24, 2008 · N661FE · Airbus A300F4605R · Nacelle/Pylon, Attach FittingsSDR 08FDEA01523Slide · crackedR-1 DOOR SLIDE ASSY, BOX IS CRACKED ON THE OUTER SURFACE, UPPER FWD SIDE. RECEIVED SERVICEABLE SLIDE TO BE INSTALLED ON W/C 68S1500CP; STEP 5-B.Apr 24, 2008 · N661FE · Airbus A300F4605R · Escape SlideSDR 08FDEA01522Connector · missingL-1 DOOR SLIDE ASSY, BATTERY TEST CONNECTOR IS MISSING. RECEIVED SERVICABLE SLIDE FOR FR 15B (L-1 DOOR) TO BE INSTALLED ON WIC 68S5001CP.Apr 24, 2008 · N661FE · Airbus A300F4605R · Equipment/Furnishings WiringSDR 08FDEA01521Door Frame · crackedL-1 DOOR SLIDE ASSY; LOWER INTERNAL FRAME IS CRACKED AT THE FWD CORNER. NEW SERVICEABLE SLIDE RECEIVED. INSTALLED ON WIC 68S5001CP.Apr 24, 2008 · N661FE · Airbus A300F4605R · Escape SlideSDR 08FDEA01520Slide · damagedL-1 DOOR SLIDE ASSY, UPPER EXTERNAL FRAME INSERTS ARE PULLED OUT OF THE BOX AT THE FWD END. NEW SERVICEABLE SLIDE RECEIVED INSTALLED ON WIC 68S5001CP.Apr 24, 2008 · N661FE · Airbus A300F4605R · Passenger/Crew DoorsSDR 08FDEA01519Frame · crackedR-1 DOOR SLIDE ASSY, LOWER INTERNAL FRAME IS CRACKED AT THE AFT CORNER. RECEIVED SERVICEABLE SLIDE TO BE INSTALLED ON W/C 68S5001CP.Apr 24, 2008 · N661FE · Airbus A300F4605R · Passenger/Crew DoorsSDR 08FDEA01518Fairing · dentedLEFT WING FLAP FAIRING 535 AT IS DENTED. REPAIR BY REMOVING THE DAMAGE & APPLYING A CORE; CLOSING PLIES AND A FIBERGLASS OVERLAY REPAIR IAW SRM 57-20-35. APPLIED AN ANTI-STATIC COATING IAW SRM 51-23-20. APPLIED PORE FILLER & PRIMER IAW SRM 51-75-10. PREPPED Apr 23, 2008 · N661FE · Airbus A300F4605R · Trailing Edge FlapsSDR 08FDEA01517Fairing · delaminatedLEFT WING FLAP FAIRING 535 AT IS DELAMINATED. REPAIRED BY REMOVING THE DAMAGE & APPLYING A CORE; CLOSING PLIES AND A FIBERGLASS OVERLAY REPAIR IAW SRM 57-20-35. APPLIED THE ANTI-STATIC COATING IAW SRM 51-23-20. APPLIED PORE FILLER & PRIMER IAW SRM 51-75-1Apr 23, 2008 · N661FE · Airbus A300F4605R · Trailing Edge FlapsSDR 08FDEA01516Fairing · erodedLEFT WING FLAP FAIRING 534 AB L/E IS ERODED IN 2 AREAS. REMOVED DAMAGE & LAYED UP REPAIR PLIES & STARTED CURE. COMPLETED CURE & SANDED. APPLIED ANTI-STATIC COATING; APPLIED FR PRIMER & APPLIED PAINT.Apr 23, 2008 · N661FE · Airbus A300F4605R · Trailing Edge FlapsSDR 08FDEA01515Fairing · erodedLEFT WING FLAP FAIRING 535 AB L/E IS ERODED IN 2 AREAS. REMOVED FINISH & DAMAGE AT 2 AREAS TOP & BOTTOM OF THE FAIRING IAW SRM 57-20-35. LAYED UP; BAGGED & CURED REPAIRS IAW SRM 57-20-35. REINSTALLED SEAL PARTIALLY REMOVED TO F.O.M. & RESTORED FINISH IAWApr 23, 2008 · N661FE · Airbus A300F4605R · Trailing Edge FlapsSDR 08FDEA01514Panel · erodedLEFT WING FLAP FAIRING 532 BB LEADING EDGE IS ERODED. REMOVED DAMAGE AND REPAIRED BY APPLYING FIBERGLASS WET LAY UP IAW SRM 57-20-35 & E.A. 6-5720-118496.Apr 23, 2008 · N661FE · Airbus A300F4605R · Trailing Edge FlapsSDR 08FDEA01513Fairing · puncturedLEFT WING FLAP FAIRING 535 BB IS PUNCTURED ON THE FWD LOWER SECTION. REMOVED DAMAGE & APPLIED A WET LAY-UP IAW SRM 57-20-35.Apr 23, 2008 · N661FE · Airbus A300F4605R · Trailing Edge FlapsSDR 08FDEA01512Fairing · dentedLEFT WING FLAP FAIRING 534 BB IS DENTED ON THE LOWER FWD SECTION. REMOVED DAMAGE AND APPLIED A WET LAY-UP IAW SRM 57-20-35 & RESTORED FINISH IAW SRM 57-75-10 & AMM 51-23-10-0.Apr 23, 2008 · N661FE · Airbus A300F4605R · Trailing Edge FlapsSDR 08FDEA01511Fairing · puncturedLEFT WING FLAP FAIRING 533BB FWD SECTION IS PUNCTURED INTERNALLY. REMOVED DAMAGE FROM PANEL; FABRICATED REPLACEMENT CORE PLUG; POTTED CORE & STARTED CURE; COMPLETED CURE & SANDED; LAYED UP REPAIR PLYS UNDER VAC BAG & STARTED CURE; COMPLETED CURE & LApr 23, 2008 · N661FE · Airbus A300F4605R · Trailing Edge FlapsSDR 08FDEA01510Panel · damagedA/C FAIRING LEFT PANEL 143 FL IS DAMAGED FROM FRETTING. REMOVED DAMAGE; PREPPED THE AREA FOR REPAIR; APPLIED LAY-UP REPAIR & REFINISHED THE SURFACE IAW A300-600 SRM 51-77-12 & SRM 53-15-73.Apr 23, 2008 · N661FE · Airbus A300F4605R · Aerodynamic FairingsSDR 08FDEA01509Rub Strip · chafedLEFT WING INBD FLAP UPPER SURFACE CHAFING PLATE IS PEELING AND WORN. REMOVED &B REPLACED THE CHAFE STRIPS IAW SRM 57-50-00; PARA 3-G; FIG 207.Apr 23, 2008 · N661FE · Airbus A300F4605R · Trailing Edge FlapsSDR 08FDEA01508Rub Strip · delaminatedRIGHT WING FLAP UPPER SKIN RUB STRIP IS DELAMINATED AT 3 SPOTS. REMOVED & REPLACED THE CHAFE / RUB STRIP IAW SRM 57-50-00; PARA 3-G FIG 207.Apr 23, 2008 · N661FE · Airbus A300F4605R · Trailing Edge FlapsSDR 08FDEA01507Skin · damagedNR 2 ENGINE OUTBD T/R CORE COWL SKIN IS PEELING. REPAIRED BY REMOVING THE PEELING WIRE MESH & SEALING THE EDGES IAW CMM 78-32-02; REPAIR NR 13.Apr 23, 2008 · N661FE · Airbus A300F4605R · Engine Thrust ReverserSDR 08FDEA01506Skin · chafedNR 2 ENGINE INBD FAN COWL INNER SKIN DOUBLER IS WORN AND CHAFED. REMOVED AND REPLACED DAMAGED CHAFE PLATE ITEM 9 IAW SRM 54-02-01 & 54-20-00. RESTORED THE SURFACE FINISH IAW SRM 54-20-00.Apr 23, 2008 · N661FE · Airbus A300F4605R · Engine Air Intake SystemSDR 08FDEA01505Skin · delaminatedNR 2 ENGINE INBD FAN COWL INNER SKIN IS DELAMINATED. REMOVED DAMAGED INNER SKIN AND REPAIRED IAW SRM 54-20-00. RESTORED FINISH IAW SRM 54-20-00 & SRM 51-75-10.Apr 23, 2008 · N661FE · Airbus A300F4605R · Engine Air Intake SystemSDR 08FDEA01504Cowling · dentedNR 2 ENGINE INBD FAN COWL IS DENTED. REMOVED DAMAGE, PREPED FOR THE APPLICATION OF FILLER MATERIAL. APPLIED FILLER, CURED, SANDED & PREPPED FOR PRIMER. APPLIED PRIMER & PAINTED IAW SRM 54-10-00, 54-20-00 & 51-75-10.Apr 23, 2008 · N661FE · Airbus A300F4605R · Engine Air Intake SystemSDR 08FDEA01503Nose Cowl · dentedNR 2 ENGINE INBD FAN COWL IS DENTED. REMOVED DAMAGE, PREPPED FOR THE APPLICATION OF FILLER MATERIAL. APPLIED FILLER, CURED, SANDED & PREPPED FOR PRIMER. APPLIED PRIMER & PAINTED IAW SRM 54-10-00, SRM 54-20-00 & SRM 51-75-10.Apr 23, 2008 · N661FE · Airbus A300F4605R · Engine Air Intake SystemSDR 08FDEA01502Nose Cowl · delaminatedNR 1 ENGINE NOSE COWL IS DELAMINATED AT THE FWD LOWER END. REMOVED & REPLACED THE NR 1 NOSE COWL IAW AMM 71-11-00-4. FAN COWL DOORS TO BE ADJUSTED & CLOSED ON THE NR 1 ENGINE INSTALLATION W/C 64T0700-1.Apr 23, 2008 · N661FE · Airbus A300F4605R · Engine Air Intake SystemSDR 08FDEA01501Fairing · delaminatedRIGHT WING FLAP FAIRING 636 AB LEFT SIDE UPPER POINT IS DELAMINATED. REMOVED FINISH AND DAMAGE IAW SRM 57-20-35. LAYED UP & CURED REPAIR PLYS IAW SRM 57-20-35 PAPAGRAPHS 5; G-M. APPLIED FINISH IAW SRM 51-75-10.Apr 23, 2008 · N661FE · Airbus A300F4605R · Trailing Edge FlapsSDR 08FDEA01500Door · gougedNLG LEFT MAIN DOOR IS GOUGED ON THE EDGE. REPAIRED LEFT NOSE; LEFT MAIN GEAR DOOR BY REMOVING DAMAGED AREA & BONDING CARBON WET LAY UP REPAIR IAW A300-600 SRM 52-82-11 & 51-77-10 PARA 3.0; FIG 209. REMOVED FINISH AT SECOND DAMAGE LOCATION AFTER FURTHER Apr 23, 2008 · N661FE · Airbus A300F4605R · Landing Gear DoorsSDR 08FDEA01499Fairing · dentedLEFT WING FLAP FAIRING 536 AB RIGHT SIDE HAS A DENT. REPAIRED THE DENT BY REMOVING THE DAMAGED AREA, POTTING THE CORE, APPLYING A WET LAY UP REPAIR AND REFINISHING THE AREA IAW SRM 57-20-35.Apr 23, 2008 · N661FE · Airbus A300F4605R · Trailing Edge FlapsSDR 08FDEA01498Panel · puncturedBULK CARGO PANEL 161 BW IS PUNCTURED IN 2 PLACES. REPAIRED BY REMOVING THE DAMAGE. APPLYING A WET LAY UP, CURING THE WET LAY UP AND PAINTING THE REPAIRED SURFACE.Apr 23, 2008 · N661FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR 08FDEA01497Panel · crackedAFT CARGO PANEL 151 PW IS CRACKED IN 3 PLACES. REMOVED DAMAGE, STOPPED DRILLED THE CRACKS & PREPPED AREA FOR REPAIRS TO BE LAYED UP, 3 EA FIBERGLASS WET LAY UP REPAIRS & APPLIED THE FINISH COAT IAW DWG SRZ 25-013.Apr 23, 2008 · N661FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR 08FDEA01492Skin · bentRIGHT APU DOOR SKIN IS BENT AND THE EDGE IS CRACKED AT THE CENTER LINE OF THE A/C WITH THE DOOR CLOSED. REMOVED BENT & CRACKED EDGE DAMAGE IAW SRM 51-27-00. FOUND EDGE DISTANCE TO FASTENERS TO BE 2-D & WITHIN LIMITS IAW SRM 51-40-50. PRIMED AREA IAW A300-600 Apr 23, 2008 · N661FE · Airbus A300F4605R · APU Cowling/ContainmentSDR 08FDEA01491Panel · chafedNR 2 PYLON; RIGHT FWD LOWER FAIRING; PANEL 486R IS CHAFED AT THE ATTACHMENT POINTS. REMOVED PANEL AND CHECKED LIMITS. STIFFENER WAS OUT OF LIMITS. FABBED A NEW STIFFENER ON N/R N01140. INSTALLED STIFFENER IAW SRM 51-40-21; PG 7 AND REINSTALLED PANEL IAW SApr 23, 2008 · N661FE · Airbus A300F4605R · Nacelle/Pylon Miscellaneous StructureSDR 08FDEA01490Panel · chafedNR 2 PYLON LEFT FWD LOWER FAIRING; PANEL 485BL IS CHAFED AT THE ATTACHMENT POINTS. REMOVED PANEL AND CHECKED THE LIMITE. THE STIFFENER WAS OUT OF LIMITS. FABBED A NEW STIFFENER ON N/R N01141 & INSTALLED THE STIFFENER IAW SRM 51-40-21. INSTALLED THE PANApr 23, 2008 · N661FE · Airbus A300F4605R · Nacelle/Pylon Miscellaneous StructureSDR 08FDEA01476Shear Plate · crackedSHEAR PLATE IS CRACKED AT FRAME 79 BETWEEN STRINGER 16L AND 17L. REMOVED AND REPLACED THE SHEAR PLATE IAW A300 SRM 51-40-21.Apr 22, 2008 · N661FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR 08FDEA01473Depressor · gougedAFT CARGO DOOR FWD CUTOUT PRESSURE SEAL DEPRESSOR IS GOUGED FROM TOP TO BOTTOM. REMOVED & REPLACED SEAL DEPRESSOR IAW SRM 51-40-21.Apr 22, 2008 · N661FE · Airbus A300F4605R · Cargo/Baggage DoorsSDR 08FDEA01472Retainer · gougedAFT CARGO DOOR AFT CUTOUT; PRESSURE SEAL DEPRESSOR IS GOUGED FROM TOP TO BOTTOM. REMOVED AND REPLACED THE DAMAGED SEAL DEPRESSOR IAW SRM 51-40-21.Apr 22, 2008 · N661FE · Airbus A300F4605R · Cargo/Baggage DoorsSDR 08FDEA01471Retainer · bentAPU ACCESS CUTOUT AFT SEAL RETAINER IS BENT AND THE SEAL IS TORN. REMOVED SEAL RETAINER & ANGLE IAW SRM 51-40-21. INSTALLED ANGLE & RETAINER IAW SRM 51-40-21.Apr 22, 2008 · N661FE · Airbus A300F4605R · APU Cowling/ContainmentSDR 08FDEA01470Drain Mast · bentAPU DRAIN MAST RIGHT UPPER FLANGE IS BENT AND THE MAST IS DENTED AND BENT. REMOVED AND REPLACED THE DRAIN MAST IAW SRM 51-40-21.Apr 22, 2008 · N661FE · Airbus A300F4605R · Airborne Auxiliary Power Unit (APU) System
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