N681FE
Service difficulty reports · 339
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 = 'N681FE' 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 = 'N681FE' 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 FDEA202203280705None · crackedLH WING INTERNAL STRUCTURE FRONT SPAR LWR FLANGE FOUND 1EA CRACK JUST I/B OF RIB9 COMPLIED WITH FEDEX EA: 6-5710-T0367806 P1 REPAIRED LH WING INTERNAL STRUCTURE FRONT SPAR LWR FLANGE JUST I/B OF RIB9. THIS IS A CAT B REPAIR. THE FOLLOW UP INSPECTION REQSDR FDEA202203150509None · crackedRH WING CENTER FLAP RIB UPR FLANGE FOUND 1EA CRACK AT RIB19 STGR2.8 COMPLIED WITH EA 6-5750-T0367417 P1. TITLE: WING - FLIGHT SURFACES - RH CENTER FLAP, CRACKS IN UPPER FLANGES OF RIBS 11, 19, 25, 26 - ALI 575306-01-1A. REPAIRED THE RH WING CENTER FLAP RIBSDR FDEA202203150508None · crackedRH WING CENTER FLAP RIB UPR FLANGE FOUND 2EA CRACKS AT RIB25 STGR2.8, RIB26 STGR2.8 COMPLIED WITH EA 6-5750-T0367417 P1. TITLE: WING - FLIGHT SURFACES - RH CENTER FLAP, CRACKS IN UPPER FLANGES OF RIBS 11, 19, 25, 26 - ALI 575306-01-1A. REPAIRED THE RH WINGSDR FDEA202203150507None · crackedRH WING CENTER FLAP RIB UPR FLANGE FOUND 2EA CRACKS AT RIB11 STGR2.7, RIB 11 STGR2.8 COMPLIED WITH EA 6-5750-T0367417 P1. TITLE: WING - FLIGHT SURFACES - RH CENTER FLAP, CRACKS IN UPPER FLANGES OF RIBS 11, 19, 25, 26 - ALI 575306-01-1A. REPAIRED THE RH WINSDR FDEA202203150506None · crackedLH WING CENTER FLAP RIB UPR FLANGE FOUND 3EA CRACKS AT RIB26 STGR2.7, RIB26 STGR2.8, RIB27 STGR2.8 COMPLIED WITH EA 6-5750-T0367416 P1. TITLE: WING - FLIGHT SURFACES - LH CENTER FLAP, CRACKS IN UPPER FLANGES OF RIB26 AT STRINGERS 2.7 AND 2.8, RIB27 AT STRISDR FDEA202203150510None · noneRH WING #3 SPOILER CENTER O/B HINGE ARM O/B SIDE FOUND DELAMINATION . SIZE: 20MM*20MM, DEPTH: 1.35MM. COMPLIED WITH EA 6-5750-T0367302 P1. TITLE: WING - FLIGHT SURFACES - RH 3# SPOILER CENTER HINGE ARM OUTSIDE SURFACE DELAMINATION. REPAIRED THE RH WING #SDR FDEA202203090443None · noneMAIN DECK FR63 -Y2462 SEAT TRACK BROKEN. EAT TRACK PER A300-600F SRM53-10-16-201 PARA.4. THIS IS CATEGORY A REPAIR. MAJOR REPAIR IAW FEDEX GMM6-2-100SDR FDEA202203080439None · noneMAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CROSSBEAM CRACKED, AT FR58, BETWEEN Y1456 AND Y1959. REPAIRED THE MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE CRACKED CROSSBEAM AT FR58, BETWEEN Y1456 AND Y1959. THIS IS CATEGORY A REPAIR. MAJOR REPAIR IAW GMSDR FDEA2019101082493Skin · chafedLW O/B FLAP TOPSIDE SKIN HAS 2 CHAFED SPOTS REMOVED CHAFING AND FOUND TO BE OUT OF LIMITS IAW SRM 57-50-00. SURFACE PROTECTED BLEND AREAS IAW A300-600 SRM 51-21-10. REMOVED, FABRICATED, AND INSTALLED NEW CHAFING PLATES IAW EA NO: 6-5750-93355 A P2.SDR FDEA201910072486Frame · damagedRIGHT FRAME 47 HOLE "N" HAS INDICATION FOUND DUE TO HOLE OUT OF ROUND WITH SEALANT AT 6 O'CLOCK POSITION, VIEWED FROM AFT LOOKING FWD IN HOLE ACCOMPLISHED EA 6-5310-T0349502-P1.SDR FDEA201910072485Seat Track · crackedMAIN CANIN SEAT TRACK SUPPORT FITTING IS CRACKED FRAME 49, LBL 57. REMOVED AND REPLACED THE SEAT TRACK IAW DWG A53812067 ISSUE C AND SRM 51-40-21.SDR FDEA2019100762477Bumper · gougedNR 1 INBOARD THRUST REVERSER UPPER FWD BUMPER PAD STRUCTURE GOUGED BY CLAMP FOR BLEED VALVE. REMOVED AND REPLACED THE BUMPER PAD STRUCTURE IAW CMM 78-32-22. REPOSITIONED CLAMP AND CHECKED GOOD IAW AMM 36-11-14, AND 71-00-00.SDR FDEA201910042438Stiffener · gougedLEFT MAIN LANDING GEAR WHEEL WELL FRAME @ UPPER FWD SIDE OF LANDING GEAR UPLOCK IS GOUGED REMOVED AND REPLACED LT.MLG W/W FRAME STIFFENER FWD SIDE OF LANDING GEAR UPLOCK IAW A300-600 SRM 51-40-21 AB DWG A53812270 ISSUE BSDR FDEA201910042437Panel · worn#1 PYLON PANEL 413BL HAS MULTIPLE WORN SCREW HOLES AT TRAILING EDGE OF PANEL #1 PYLON PANEL 413BL REPAIRED IAW A300-600 SRM 54-50-00, REPAIR CSDR FDEA201910032432Intercostal · crackedTAIL SECTION, AFT OF ACCESS PANEL 312AR, INTERCOSTAL JUST AFT OF ACCESS PANEL IS CRACKED AND DEFORMED. REMOVED THE INTERCOSTAL IAW SRM 51-40-21. LOCATED AND DRILLED A NEW INTERCOSTAL IAW SRM 51-40-44. INSTALLED THE NEW INTERCOSTAL AND STRAP IAW IAW SRM 51SDR FDEA2019100322403Floor Panel · damagedFLOOR PANEL 221FF WAS DAMAGED. ACCOMPLISHED A PERMANENT REPAIR TO THE FLOOR PANEL IAW EA 6-5321-T0349655-P1. MAJOR REPAIR.SDR FDEA2019100312394Bracket · crackedLEFT WING NR 2 FLAP TRACK FAIRING OTBD ATTACH BRACKET CRACKED REMOVED AND REPLACED LT. WING #2 FLAP TRACK FAIRING OB ATTACH BRACKET IAW A300-600 SRM 51 600 SRM 51-40-21 AND AB DWG A57942502SDR FDEA201909282369Structure · corrodedAC BAY VAPOR SEAL 2EA EXTRUSION HAS EXFOLIATED CORROSION REMOVED AND REPLACED AC BAY VAPOR SEAL 2EA EXTRUSION PN: A2811035720700 PO#955582.1 AND PN:A2811035720600 PO#955375.1 PER A300 AMM 28-13-21-04 PARC(4)(A)SDR FDEA201909282368Panel · wornPARTS RACK:#2 PYLON PANEL 424CR WORN AROUND SCREW HOLE REPAIRED #2 PYLON PANEL 424CR IAW A300-600 SRM 54-52-51-FIG 201SDR FDEA201909272354Skin · dentedLEFT WING ALL SPEED UPPER SURFACE SKIN INBOARD TRAILING EDGE PROFILE IS DENTED ALL WORK ACCOMPLISHED ON S/O 283435 OPS N00344 IAW A300-600 SRM 57-61-11 AND A300- 600 SRM 51-77-12 MAJOR REPAIRSDR FDEA201909272353Skin · dentedLW ALLSPEED AILERON TOP SIDE HAS 3 DENTS REMOVED DAMAGED SKIN AT INBD, CENTER DENT AREA AS MARKED & REPAIRED IAW AIRBUS A300-600 SRM 57-61-11 FIG 1 ITEM 205, A300 -600 SRM 57-61-11 PAGE BLOCK 201 PARA 3E & A300- 600 SRM 51-77-12 PAPRA 4C REMOVED FINISH & SDR FDEA201909272366Floor Panel · delaminated(DISCREPANCY RACK) FWD CARGO COMPARTMENT FLOOR PANEL 132MG DAMAGED REPAIRED FLOOR PANEL 132MG BY FABRICATION IAW FEDEX SRZ-25-005 REV. R; A300-600 AMM 51-75-10 AND SRM 53-10-20 MAJOR REPAIRSDR FDEA201909272365Floor Panel · delaminated(DISCREPANCY RACK) FWD CARGO COMPARTMENT FLOOR PANEL 131QG DAMAGED REPAIRED FLOOR PANEL 131QG BY FABRICATION IAW FEDEX SRZ-25-005 REV. R, A300-600 AMM: 51-75-10 & SRM: 53-10-20 MAJOR REPAIRSDR FDEA201909272364Floor Panel · delaminated(DISCREPANCY RACK) FWD CARGO COMPARTMENT FLOOR PANEL 132NG DAMAGED REPAIRED FLOOR PANEL 132NG BY FABRICATION IAW FEDEX SRZ-25-005 REV. R, A300-600 AMM: 51-75-10 & SRM: 53-10-20 MAJOR REPAIRSDR FDEA201909272363Floor Panel · delaminated(DISCREPANCY RACK) FWD CARGO COMPARTMENT FLOOR PANEL 132PG DAMAGED REPAIRED FLOOR PANEL 132PG BY FABRICATION IAW FEDEX SRZ 25-005 REV. R; A300-600 AMM 51-75-10 AND 53-10-20. MAJOR REPAIRSDR FDEA201909272361Floor Panel · delaminated(DISCREPANCY RACK) FWD CARGO COMPARTMENT FLOOR PANEL 131MG DAMAGED REPAIRED FLOOR PANEL 131MG BY FABRICATION IAW FEDEX SRZ-25-005 REV. R, A300-600 AMM: 51-75-10 & SRM: 53-10-20 MAJOR REPAIRSDR FDEA2019093022350Plate · crackedNR 2 ENG PYLON OTBD FISH PLATE WAS CRACKED ABOVE OTBD THRUST REVERSER FWD SIDE OF PRECOOLER OPENING. REMOVED AND REPLACED THE NR 2 ENGINE PYLON OTBD FISH PLATE IAW DWG A54612368, AND SRM 51-40-21.SDR FDEA201909262348Skin · crackedCRACK FOUND:R/H WING UPPER SURFACE PANEL L/E,FWD OF #3 SPOILER 15.5" O/B OF PANEL I/B EDGE, 1" AFT OF L/E FASTENER ROW. MARKED LENGTH 1.5" LONG. REPAIRED #3 SPOILER SKIN SHROUD IAW A300-600 SRM 57-51-12 AND FED EX EA NO. 6-5730- T0349621 P1, WINGS-PLATES ANSDR FDEA201909262347Web · cracked#1 PYLON HAS CRACKED STRUCTURE AT PRESSURIZATION LINE ATTACH POINT UNDER PANEL 474CR. REMOVED AND REPLACE PANEL WEB IAW A300-600 SRM 51-40-21 AND AB DWG A54515063SDR FDEA201909262344Angle · damagedAFT CARGO COMPARTMENT LOWER DOOR CUTOUT @ FR63A ANGLE ASSY DAMAGED REMOVED AFT CARGO LOWER DOOR CUTOUT ANGLE IAW A300 SRM 51-40-21. RECIEVED NEW LOWER DOOR CUTOUT ANGLE P/N A25573798002 IAW A300 DAW #A2557378002. LOCATED AND DRILLED HOLES IAW A300 SRM 51-4SDR FDEA201909262343Depressor · damagedAFT CARGO DOOR CUTOUT SEAL DEPRESSOR IS DAMAGED AT THE AFT LOWER CORNER OF THE DOOR CUTOUT REMOVED AFT CARGO DOOR CUTOUT SEAL DEPRESSOR AND LOWER CORNER FITTING IAW A300 SRM 51-40-21. RECIEVED NEW SEAL DEPRESSOR P/N A5397822420401 AND LOWER CORNER FITTINSDR FDEA201909252341Floorboard · crackedFLOORBOARD PANEL 252 HH IS CRACKED. FABRICATED NEW FLOOR PANEL 252HH IAW DWG SRZ-25-005 REV P AND PART MARK PANEL IAW GMM 07-0-1000.SDR FDEA201909222316Trim Panel · crackedRT PYLON AFT SECTION RT SIDE TRIM HAS CRACK OR GOUGE. REMOVED AND REPLACED WITH NEW PART NR A5451532800103, PO # 954562.1 IAW SRM 51-40-21 AND DRAWING A54515327 REV D, TORQUED SCREWS IAW AMM 20-21-12-00.SDR FDEA201909212299Support · cracked#1 PYLON PANEL SUPPORT STRUCTURE UNDER PANEL 413BL CRACKED. REMOVED PANEL SUPPORT ARCH IAW SRM 51-40-21, LOCATED AND DRILLED NEW PANEL SUPPORT ARCH P/N A5461140900100 P/O 954576.1 IAW DWG A54010337; INSTALLED PANEL SUPPORT ARCH IAW DWG A54010337 ISSUE N AND ASDR FDEA201909212298Support Angle · damaged#1 PYLON TR SUPPORT ANGLE AT FWD LATCH PANEL HAS KNIFE EDGE. REMOVED AND REPLACED #1 TR SUPPORT ANGLE PER SRM 51-40-21 AND MRA IPC 78-32-22 FIG 15 PN 491B1313032-006 PO#954713.1.SDR FDEA201909212297Trim Panel · damagedRT PYLON AFT SECTION LT SIDE TRIM HAS CRACK OR GOUGE REMOVED AND REPLACED WITH NEW PART NR A5751532700103, PO#954846.1 IAW SRM 51-40-21 AND DRAWING 54515327 REV D, TORQUED SCREWS IAW AMM.SDR FDEA201909192289Skin · crackedCRACK FOUND: LT WING UPPER SURFACE PANEL LE FWD OF #3 SPOILER 16" OB OF PANEL EDGE .700" AFT OF LE FASTENER ROW. MARKED LENGTH 2.640" LONG REPAIRED CRACKED AREA ON THE LW UPPER SURFACE PANEL LE FWD OF #3 SPOILER IAW SRM 57-51-1212.SDR FDEA201909182277Floorboard · puncturedMAIN CABIN FLOOR BOARD PANEL 241 AJ PUNCTURED. FABRICATED NEW FLOOR PANEL 241 AJ IAW DWG SRZ-25-005 REV P AND PART MARKED PANEL IAW GMM 07-0-1000.SDR FDEA201909182276Floorboard · damagedMAIN CABIN FLOORBOARD 241 HK HAS 2EA MISSING INSERTS. FABRICATED NEW FLOOR PANEL 241 HK IAW DWG SRZ-25-005 REV P AND PART MARKED PANEL IAW GMM 07-0-1000.SDR FDEA201909182275Floor Support · crackedAVIONICS COMPARTMENT FLOOR SUPPORT WEB FR10@ RBL37 CORNER CRACKED. REMOVED CRACKED FLOOR SUPPORT IN AVIONICS COMPARTMENT AT FR10 RBL37 IAW SRM 51-40-21. RECEIVED NEW WEB P/N# 536119720201, PO# 954285.1 PER DWG A53611977. LOCATED AND DRILLED NEW WEB IAW SRM SDR FDEA201909172271Floorboard · crackedMAIN CABIN FLOOR BOARD PANEL 242AJ CRACKED ON EDGE. FABRICATED PANEL PER DRAWING SRZ-25-005 REV P.SDR FDEA201909172270Floorboard · damagedMAIN CABIN FLOORBOARD 252VF HAS EDGE DAMAGED AND CRACKED. FABRICATED NEW PANEL PER DRAWING SRZ-25-005 REV P.SDR FDEA201909172269Floorboard · damagedMAIN CABIN FLOOR BOARD PANEL 251 BH HAS DAMAGED CORNER AND EDGE FILLER. FABRICATED NEW PANEL PER DRAWING SRZ-25-005 REV P.SDR FDEA201909162258Cusp Web · crackedMAIN CABIN FLOOR AREA FR 77 RIGHT CUSP WEB CRACKED. REMOVED AND REPLACED CRACKED CUSP WEB FROM FRA 76 RT TO FRA 77 RT.SDR FDEA201909162257Cusp Web · crackedMAIN CABIN FLOOR AREA FR 79 RT CUSP WEB CRACKED. REMOVED AND REPLACED WEB PER SRM 51-40-21 AND DRAWING A53981360 ISSUE K.SDR FDEA201909152247Floorboard · damaged(PARTS RACK) MAIN CABIN FLOORBOARD 232NG IS DAMAGED. FABRICATED NEW FLOOR PANEL 232NG IAW DWG SRZ-25-005 REV P AND PART MARK PANEL IAW GMM 07-0-1000.SDR FDEA201909152246Floorboard · delaminatedFLOORBOARD 242UJ DELAMED. FABRICATED NEW FLOOR PANEL242UJ IAW DWG SRZ-25-005 REVP AND PART MARKED PANEL IAW GMM 07-0-1000.SDR FDEA201909152245Floorboard · damaged(PARTS RACK) MAIN CABIN FLOORBOARD 232TG IS DAMAGED. FABRICATED NEW FLOOR PANEL 232TG IAW DWG SRZ-25-005 REVP AND PART MARKED PANEL IAW GMM 07-0-1000.SDR FDEA201909142242Floor Panel · crackedMAIN CABIN FLOOR PANEL 262KF HAS CRACKED CORNER. FABRICATED NEW FLOOR PANEL IAW DWG SRZ-25-005 REV P AND GMM 07-0-1000.SDR FDEA201909132237Floorboard · puncturedMAIN CABIN FLOORBOARD FROM STA C74-C77 LT SIDE ROW B HAS PUCTURE. FABRICATED NEW FLOOR PANEL IAW DWG SRZ-25-005 REF P AND GMM 07-0-1000.
Back to N681FE