N307FE
Service difficulty reports · 140
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 = 'N307FE' 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 = 'N307FE' 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 FDEA202211292863Fairing · cracked#3 ENGINE PYLON HAS CRACKED PANEL,LOCATED AT LOWER SURFACE AFT OF EXUAST NOZZLE AND FORWARD OF V PANEL. REPAIRED PYLON PANEL ASREQUIRED IAW SRM 54-00-01 FIG. 2B SHEET 2.SDR FDEA202202080248None · failedPDIS 307 73-20 9023 08FEB22 DEN OPEN U ON TAKEOFF ROLL , NUMBER 3 ENGINE VERY SLOW TO SPOOL UP. AFTER MAX THRUST WAS SET NUMBER 2 STARTING ROLLING BACK AND WE GOT THE RED ENG FAIL LIGHT. REJECTED TAKEOFF. REMOVED AND REPLACED THE MEC, FUEL PSDR FDEA202112253139None · noneLPE ACTIVATED AFTER ROTATION, GO AROUND/TAIL STRIKE LANDING PERFORMANCE ENHANCEMENT FACT 25DEC21 01:19 YYZ U TAIL STRIKE PART A INSPECTION CARRIED OUT I.A.W AMM 05-51-12-6. NO DAMAGE NOTED .A/C OK FOR SERVICE. TALE STRIKE PART A INSPECTION CARRIED OUT SDR FDEA202110032448Paint · wornRH OB ELEVATOR BARE METAL AT LOWER SURFACE AFT OF ACTUATOR FOUND RH OB ELEVATOR LOWER SURFACE AFT OF INB ACTUATOR (PANEL 346BB) HAS MARKED MISSING PAINT, PREPPED AND PAINTED PER MD10-30 SRM 51-21-02 VOL 2 PARAGRAPH 2 STEPS A-J. PERFORMED WEIGHT AND BALANCESDR FDEA202110022486Skin · damagedNUMBER ONE R/H SLAT HAS SKIN DAMAGED FORWARD SIDE. REPAIRED DAMAGE IN REFERENCE TO MD-10-30 SRM 57-10-00 FIG 43 VOL 1SDR FDEA202109232395Panel · damagedLEFT WING OUTBOARD FLAP PANEL ABOVE OUTBOARD END OF FLAPMISDRILLED HOLE AT I/B CORNER OF OUTBOARD END. REPAIRED PANEL PER E.A. 8-5710-T0364140(P1)- BASIC WING STRUCTURE - LH WING TE HONEYCOMB PANEL P/N ARC0616-501 (MAJOR REPAIR)SDR FDEA202109232394Panel · damagedLEFT WING OUTBOARD FLAP PANEL ABOVE OUTBOARD END OF FLAPS HAS MISDRILLED HOLES. REPAIRED PANEL PER E.A. 8-5710-T0364140 (P1)-BASIC WING STRUCTURE - LH WING TE HONEYCOMB PANEL P/N ARC0616-501(MAJOR REPAIR)SDR FDEA202109232387Floorboard · damagedAFT CARGO COMPARTMENT FLOOR BOARD 187EF DAMAGED FABRICATED NEW FLOOR BOARD SRZAGA3876-3SDR FDEA202109142302Floorboard · delaminatedDELAMINATED FABRICATE NEW AKC7082-3 FLOOR BOARD PER FEDEX DRAWING SRZ-25-005SDR FDEA202109132296Floorboard · delaminatedDELAMINATED FABRICATE NEW AKC 7082-19 FLOOR BOARD PER FEDEX DRAWING SRZ-25-005SDR FDEA202109112298Floor Support · corrodedMAIN DECK FLOORBOARD SUPPORT ANGLE STA. 1581 LBL=15 EXFOLIATED/CORRODED. REMOVED EXFOLIATED/CORRODED FLOOR SUPPORT ANGLE P/N AFA3853-15 AT STA 1581 LBL 15. FABRICATED , PROCESSED ,TREATED, PRIMED, AND INSTALLATED NEW FABRICATED FLOOR SUPPORT ANGLE. REF.SDR FDEA202109112315Floorbeam · corrodedMAIN DECK FLOOR PANEL SUPPORT ANGLE AT STA 1661 RBL 75 TO 107 CORRODED AROUND SEVERAL CLIPNUTS REMOVED AND REPLACE FLOOR SUPPORT REF DOUGLAS DRAWING AFA-3853.SDR FDEA202109112316Floorbeam · corrodedMAIN DECK FLOORBOARD SUPPORT ANGLE STA. 1661 LBL=107.25 EXFOLIATED/CORRODED. (MRKD) REMOVED AND REPLACED WITH NEW FABRICATED FLOOR BOARD SUPPORT P/N AFA3853-501 REF DAC DWG AFA3853 AND SRM 51-33-01 VOL. 2SDR FDEA202109112303Floorbeam · corrodedMAIN DECK FLOOR SUPPORT ANGLE AT STA 1901 RBL 08 TO RBL 27 CORRORED MAIN DECK FLOOR SUPPORT ANGLE AT STA 1901 RBL 08 TO RBL 27 HAS BEEN REPAIRED PER DWG # AGA7559.SDR FDEA202109112290Floorboard · delaminatedDELAMINATED FABRICATED NEW ARC7082-55 FLOOR PANEL PER SRZ-25-005SDR FDEA202109072246Panel · delaminatedDELAMINATION ON AJC7001-149 STEP FABRICATED NEW AJC7001-149 STEP PER SRZ-25-005SDR FDEA202109032517None · damagedTEE FITTING HOLES DAMAGED. FABRICATE NEW FITTING PER DWG ARB3280 0000832258 : PUTZ, JARED J - 28-SEP-2021 16:44 FABRICATED TEE-TENSION BEVEL ARB3280-2 REF DWG ARB3280 0000097667 : SEVERJIN, DAVE H - 28-SEP-2021 17:59 C/W.SDR FDEA202109032279Skin · dentedMAIN CARGO DOOR OPENING, FWD LOWER CORNER DAMAGE TO SKIN LAYERS (MARKED) 0003882689 : CARREDANO, CHRISTOPHER - 24-SEP-2021 00:24 REPAIRED MAIN CARGO DOOR CORNER REF MD10-30 SRM 53-50-00, VOL I, FIG 26, SHEET 6, PG 178, NOTES 1-14 0000858546 : KAYA, KEVINSDR FDEA202108302167Floorboard · damagedMAIN CARGO DECK STA.1437 DAMAGED FLOOR BOARD. ON PANEL DOOR #271GF (LH) AREA (MARKED) FABRICATED NEW FLOOR BOARD PANEL PER SRZ-25-005SDR FDEA202108222455Angle · crackedRIGHT WING SLAT #2 OUTBOARD END UNDER STAINLESS SEAL BY DLE HAS CRACKED L-ANGLE MARKED #1 REMOVED AND REPLACED CRACKED ANGLE ARB1647-6 IN REFERENCE TO DOUGLAS DRAWING ARB1647 AND MD-10-30 SRM 51-31-01 VOL2SDR FDEA202108222189Rub Strip · crackedLH WING: #1 SLAT UPPER SURFACE O/B - T/E RUBSTRIP UNDERSIDE CRACKED. (MRKD) REMOVED AND INSTALLED RUBSTRIP PER E.A 8-5750-T0363959, & REF MD10-30 SRM 51-35-01 VOL II, & REF DAC DWG NRB6224 REF. JPF ITEMS 2,3, AND 4SDR FDEA202108302166Floorboard · damagedMAIN DECK CARGO STA. 1437 DAMAGED FLOOR BOARD. ON PANEL DOOR #271GF LH AREA (MARKED). FABRICATED NEW FLOOR BOARD PANEL PER FEDEX DRAWING SRZ-25-005SDR FDEA202108212053Floorbeam · crackedMAIN CARGO COMPT. FLOOR BOARD SUPPORT AT STA. 1199 AT APPROX. X=98 TO X=104 CRACKED REMOVED AND REPLACED FLOOR BOARD SUPPORT P/N ACA3763-1 ON MAIN CARGO COMPT. AT NOTED LOCATION REF SRM 51-33-01 VOL 2SDR FDEA202108192052Floorbeam · corrodedMAIN CARGO COMPT. FLOOR BOARD SUPPORT AT STA. 1219 AT APPROX. X=89 TO X=105 HAS CORROSION REMOVED CORRODED FLOOR BOARD SUPPORT AND FABRICATED NEW FLOOR BOARD SUPPORT P/N AEA0394-501 IAW DOUGLAS DRAWING AEA0394 USING S2929169 EXTRUSION MP5630208 AND INSTASDR FDEA202108192051Floorbeam · crackedMAIN CARGO COMPT. FLOOR BOARD SUPPORT AT STA. 1481 AT APPROX. X=-10 TO X=-16 CRACKED REMOVED AND REPLACED FLOOR BOARD SUPPORT P/N ACA3763-1 ON MAIN CARGO COMPT. AT NOTED LOCATION REF SRM 51-33-01 VOL 2SDR FDEA202108192050Floorbeam · crackedMAIN CARGO COMPT. FLOOR BOARD SUPPORT AT STA. 1461 AT APPROX. X=29 TO X=35 CRACKED REMOVED AND REPLACED FLOOR BOARD SUPPORT P/N ACA3763-1 ON MAIN CARGO COMPT. AT NOTED LOCATION REF SRM 51-33-01 VOL 2SDR FDEA202108192049Floorbeam · crackedMAIN CARGO COMPT. FLOOR BOARD SUPPORT AT STA. 1441 AT APPROX. X=10 TO X=16 CRACKED REMOVED AND REPLACED FLOOR BOARD SUPPORT P/N ACA3763-1 ON MAIN CARGO COMPT. AT NOTED LOCATION REF SRM 51-33-01 VOL 2SDR FDEA202108182319Fitting · crackedL/H STA. 595 BULKHEAD TEE CAP VERT LEG AT LONG 43L HAS A .700 IN. CRACK. (MARKED) INSTALLED REPAIR DOUBLERS PER EA8-5310-T0363663SDR FDEA202108182059Floorbeam · crackedFUSELAGE MAINFRAME OVERWING FLOOR BEAM L/H SIDE AT STA 1256 LBL 112 IS CRACKED APPROX. ONE INCH IN LENGHT. (MKD) REPAIRED FUSELAGE MAINFRAME OVERWING FLOOR BEAM AT STA 1256 LBL112 REF BOEING SERVICE BULLETIN DC10-53-172 FIG 5, DWG SR10530081, EA 8-5310-T03SDR FDEA202108182278Stiffener · corrodedAFT CARGO COMPARTMENT R/H TUNNEL VERTICAL STIFFNER CORRODED UNDER NUT PLATE ON LOWER AREA AT STA 1841. (DOT 5) 0004092897 : REECE JR., RONALD S - 10-SEP-2021 17:49 WEB ASSEMBLY REPAIRED IAW SRM 53-00-01 GENERAL REPAIR #8 FIGURE 8 SHEETS 1-3 AND DRAWING ASDR FDEA202108182277Beam · crackedFOREWARD CARGO AT 595 BULKHEAD LOWER BEAM BEHIND NOSE GEAR P/N NCA6044-29 HAS 4 CRACKS VERIFIED AND MARKED. 0000911637 : STEPHENS, NATHAN M - 09-SEP-2021 19:14 STOP DRILLED ENDS OF CRACKS AND APPLIED DOUBLER REPAIR IAW SRM 53-40-00 V1 FIG36SDR FDEA202108172170Seat Track · corrodedAFT WASTE COMPT: STA 1967 LBL 107.25 - SEAT TRACK UNDERSIDE HAS EXFOLIATION CORROSION (VIEWED FROM LH SIDE AFT WASTE COMPT. LOOKING UP). REMOVED AND INSTALLED NEW SEAT TRACK EXTRUSION S4929148 REF SRM 53-70-00 VOL 1 FIG 16, SHEET 1, PG 59 PAR. 1C, SRM 57-SDR FDEA202108172320Tee Fitting · crackedFWD CARGO, L/H SIDE "T" CAP CRACKED ON VERTICAL LEG, LOCATED BY STRINGER 45. CORRECTION: LOCATED BY STRINGER 39. INSTALLED REPAIR DOUBLERS PER EA. 8-5310-T0363663SDR FDEA202108172029Floorbeam · crackedMAIN CABIN OVERWING FLOOR BEAM, R/H SIDE, AT STA 1275 RBL 104, HAS A SEVERED BEAM. (MKD) INSTALLED NEW FABRICTED EXTRUSION SPLICE IAW SRM 51-38-01 PAR 4.D VOL 2 AND DWG VZZ7071(-1) SHEET 2 ZN17 VIEW G-G AND SRM 51-33-01 VOL.2SDR FDEA202108162188Skin · crackedLH LEADING EDGE, SLAT ANTI ICE TELESCOPING DUCT CUTOUT, PERFORMED NDT HFEC INSP PER NDTSPM PART 6. CRACK INDICATION AT UPPER INBD CORNER APPROX .250 IN LENGTH, MARKED DOT#39 AND RED GREASE PENCIL. NOTE: LOCATION IS CORNER #1 PER SEQ 1015, PG 22, FIG 2. RSDR FDEA202108152424Doubler · wornAFT FUSELAGE; 311AB DOOR LAND WORN THRU SKIN @ LH AFT LATCH CONTACT POINT. DOT #11 REPAIRED PER EA 8-5330-T0364309.SDR FDEA202108132292Floor Panel · delaminatedMAIN DECK FLOOR PANEL DELAM. FROM STA 1561-1661.BETWN LBL 8.50-27.50 MARKED RED FABRICATED NEW FLOOR BOARD PER FDX DWG SRZ-25-005SDR FDEA202108132221Floorboard · damagedUPPER MAIN CARGO FLOORBOARD 282BF IS MISSING MULTIPLE INSERTS. STA 1561-1661 FABRICATED NEW FLOOR BOARD PER FEDEX DRAWING SRZ-25-005SDR FDEA202108132017Seat Track · wornMAIN DECK: STA 1029 (R) X = -47.50 SEAT TRACK WORN BEYOND (GO-NOGO GAUGE)LIMITS. (MRKD) REMOVED AND REPLACED SEAT TRACK FROM STA 949-1030 RBL 47.50 MAIN DECK MPN S4929405-13500N MP3266343 REF SRM 53-70-00 FIG 1 VOL.1 AND SRM 51-31-01 VOL. 2 "MAJOR REPAISDR FDEA202105041137Skin · crackedLH UPPER A/C PACK EXHAUST CUTOUT HAS SUSPECTED CRACK IN UPPER AFT CORNER THRU FASTENER HOLE. REPAIRED FUSELAGE SKIN PER MD10-30 SRM 53-50-00 FIG 3ASDR FDEA2020082011858Power Supply · no testDURING AN EMERGENCY LIGHTS TEST, FOUND THE EMERGENCY LIGHTS BATTERY 1 LOW. REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY POWER SUPPLY IAW AMM 33-51-01-4-1, AND OPS CHECKED OK. ACFT OK FOR SERVICE.SDR FDEA2020081211858Battery Pack · no testDURING EMERGENCY LIGHTS TEST, FOUND THE BATTERY 1 LOW.SDR FDEA202007031439Valve · failedTNK 3 TIP TRAPPED ALERT DURING CRUISE. 5800 LBS TRAPPED IN #3 TANK. EMERGENCY DECLARED WITH ATC. IN REF TO FFC ERO 5200247 REMOVED REPLACED AND OPS CHECKED #3 MOTIVE SHUTOFF VALVE IRW FE MD10- 30 AMM 28-21-13-2 AND FE MD10-30 FIM 28-14-00-810-803. OPS CHSDR FDEA2020070631439Unknown · malfunctionedTANK 3 TIP TRAPPED ALERT DURING CRUISE. 5800 LBS TRAPPED IN NR 3 TANK. EMERGENCY DECLARED WITH ATC.SDR FDEA2020061961263Float Valve · malfunctionedAT L/O , FL 360 GOT LVL 1 ALERT FOR " TNK 3 TIP TRAPPED" WITH APPX 8.0 K FUEL IN #3, MEANING WE ONLY HAD 8.0 - 5.8 = 2.2 IN NR 3 TANK , AND INSUFFICIENT FUEL TO MAKE DESTINATION , ALERT WENT AWAY AFTER 2 MIN BUT ON DESCENT, GOT TNK 3 FUEL QTY LO ALERT WITHSDR FDEA202003290628Indicator · malfunctionedL1 DOOR EVACUATION SLIDE REMOTE PRESSURE PRESS-TO-TEST INDICATING SYS NOT TESTING. REMOVED AND REPLACED REMOTE SLIDE PACK PRESSURE INDICATOR. OPERATIONAL CHECKS GOODSDR FDEA201910282765Spoiler Sys · malfunctionedPDIS 307 27-60 6896 28OCT19 PDX FACT U LOGPAGES:3144742 DURING DESCENT WHEN SPOILERS DEPLOYED THE AIRCRAFT HAD A SIGNIFICANT ROLL TO THE RIGHT. FACT 28OCT19 05:05 PDX U C/W FIM 27-60-09-00 . FULLY DEPLOYED SPOILERS AND INSPECTED SURFACES SDR FDEA201909032081Floor Support · corrodedCORROSION UNDER NUT PLATES AFT CARGO FLOOR SUPPORT STA 1907, END TO END. REMOVED & REPLACED NUT PLATES IAW SRM 51-31-01 VOL II, REMOVED CORROSION STA 1902 L- 40 TO R-40 IAW SRM 51-21-01 VOL I. CHECK LIMITS ORIG MAT. .063" MAT. LOSS .026": MAT REM .037", FOUND SDR FDEA201909032080Access Panel · corrodedLWR AUX TANK REAR SPAR ACCESS WEB HAS CORROSION ON BOTH UPPER AND LOWER SURFACES. (PANEL RACK) REMOVED CORR IAW SRM 51-81-00 VOL II. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01 FIG 1A. SH 3 ORIG .190 AFTER REWORK .152 TR# 14401. FABRICATED WEB ON TR # T19/14360SDR FDEA201909032082Skin · chafedLT WING FIXED L/E UPPER SKIN IS CHAFED UNDER SLAT #1 AND 2 JOINT. CHECK FIT / FAIR GAP CLEARANCE AFTER REPAIR. BLENDED AREA IAW SRM 57-00-01 FIG I. VOL I. REMAINING MAT ON LT WING FIXED L/E UPPER SKIN UNDER SLAT #1 AND 2 JOINT WAS FOUND TO BE OUT OF LIMITS IAW
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