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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR 08FDEA01562Rub Strip · damagedRIGHT WING INBD FLAP UPPER SKIN RUB STRIP IS WORN. REMOVED & REPLACED THE CHAFE / RUB STRIP IAW SRM 57-50-00.SDR 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 SDR 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. ALODINESDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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; APPSDR 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 EDGSDR 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 A300SDR 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.SDR 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.SDR 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.SDR 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.SDR 08FDEA01521Door Frame · crackedL-1 DOOR SLIDE ASSY; LOWER INTERNAL FRAME IS CRACKED AT THE FWD CORNER. NEW SERVICEABLE SLIDE RECEIVED. INSTALLED ON WIC 68S5001CP.SDR 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.SDR 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.SDR 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 SDR 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 51-75-1SDR 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.SDR 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 IAWSDR 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.SDR 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.SDR 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.SDR 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 & LSDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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 SDR 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.SDR 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.SDR 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.SDR 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 SDR 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 SSDR 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 PANSDR 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.SDR 08FDEA01473Depressor · gougedAFT CARGO DOOR FWD CUTOUT PRESSURE SEAL DEPRESSOR IS GOUGED FROM TOP TO BOTTOM. REMOVED & REPLACED SEAL DEPRESSOR IAW SRM 51-40-21.SDR 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.SDR 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.SDR 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.
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