N631FE
Service difficulty reports · 360
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 = 'N631FE' 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 = 'N631FE' 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 FDEA2019102182700Seat Track · crackedUPPER CARGO COMPARTMENT - STA.758/LBL-8.5 - SEAT TRACK DAMAGED (MARKED). REPAIRED DAMAGED SEAT TRACK REF SRM 53-00-52 FIG 201 SH.1, SR 10-53-002, SRM 51-31-01 , SRM 51-41-01 MAJOR REPAIR SEE JPFSDR FDEA2019101842684Skin · chafed#2 ENGINE - LOWER RIGHT AFT INLET - SKIN WORN THROUGH AT APPROXIMATELY 5:45 POSITION, WHERE THE RIGHT FAN COWL MAKES CONTACT WITH SKIN SURFACE (MARKED). REPAIRED WORN SKIN PER SRM 54-20-15-2R SHT.3.SDR FDEA2019100732478Doubler · crackedRIGHT WING - INBOARD LEADING EDGE - FORWARD LEADING EDGE PANEL LAND IS CRACKED, INBOARD OF NR 9 SLAT TRACK. R & R THE DOUBLER PER DWG ARB1180, AND SRM 51-31-01.SDR FDEA2019101092500Intercostal · crackedLEFT WING L/E FIXED WING PANEL AT WING ROOT AREA, HAS A SMALL CRACK ON THE INTERCOSTAL, DIRECTLY BEHIND PANEL. FABRICATED A NEW INTERCOSTAL IAW DRAWING ARB7127.SDR FDEA201909222317Skin · corrodedAFT ACCESSORY COMPARTMENT STA 2144 TO STA 2164 RT LONGERON 39 - 43 EXFOLIATION CORROSION ON SKIN AND AROUND NUTPLATES. PERFORMED FUSELAGE SKIN REPAIR IN REF TO SRM 53-70-01, REPAIR # 3.SDR FDEA2019101762676Former · crackedLEFT WING - FORWARD SPAR - SUPPORTING STRUCTURE IS CRACKED AFT/OUTBOARD OF FUELING PANEL (MARKED). STOP DRILLED CRACK AND INSTALLED A .090 REPAIR DOUBLER IAW SRM 57-00-00 FIG 209 SHEET 1.SDR FDEA201909122228Frame · crackedFWD CARGO, APPROX STA 939 RBL 70 SUPPORT FRAME CRACKED. REPAIRED THE FWD CARGO COMPARTMENT FLOOR SUPPORT FRAME AT STA 939 AND RBL 70 IN REF TO DWG # ADA7145 & SRM 53-50-51, REPAIR 1 FIG 201.SDR FDEA201908282152Seat Track · wornMAIN DECK SEAT TRACK STA1261-1301 RBL=75.25 HAS () AREAS WORN. REPLACE NOTED MAIN DECK SEAT TRACK IAW SRM 53-00-52 REPAIR-1 FIG-201.SDR FDEA2019101732675Stringer · crackedLEFT WING - LOWER SURFACE - FORWARD PANEL LAND IS CRACKED AFT OF #9 SLAT TRACK (MARKED). CORRECTIVE ACTION: INSTALLED REPAIR DOUBLER PER MD11 SRM 57-40-03-2R & SRM 51-31- 01.SDR FDEA201908212337Spar Cap · cracked#2 PYLON RT UPPER SPAR CAP FWD EDGE AT THE OUTER RADIUS HAS A .100 IN CRACK PROPAGATING AFT AT YID 408.600. REPAIRED #2 PLYON UPPER SPAR CAP AVB7506 PER EA 1-5450-T0349293 (MANUFACTURING JOINT FATIGUE CRACK IN RT UPER SPAR) MAJOR REPAIR.SDR FDEA2019082101959Hinge · wornFWD CARGO DOOR, DOOR SIDE, HINGE SEGMENT IS WORN REMOVED REPLACED HINGE SEGMENT PER DWG. ADA0253 AND SRM 51-33-01SDR FDEA2019082101958Hinge · wornFWD CARGO DOOR, DOOR SIDE HAS A WORN HINGE. P/N ADA0253-509 REMOVED AND REPLACED HINGE SEGMENT PER DWG. ADA0253 AND SRM 51-33-01SDR FDEA2019082101957Hinge · wornFWD CARGO DOOR HINGE , DOOR SIDE IS WORN P/N ADA0253-505 REMOVED AND REPLACE DOOR HINGE SEGMENT PER DWG. ADA0253 ANDSRM 51-33-01.SDR FDEA201908182238Skin · chafedRT WING: DROOP L/E, OUTBD EDGE HAS WEAR GROOVE INTO SKIN (MARKED) REPAIRED PER SRM 57-40-01 FIG 202, REP 15.SDR FDEA2019101082487Hinge · corrodedUNDERSIDE OF HINGE SEGMENT NR 3 AT ATTACH POINT WITH MCD HAS CORROSION. AREAS. REMOVED CORROSION FROM NOTED HINGE SEGMENT MATERIAL REMAINING AFTER BLENDOUT IS .079 IS OUT OF LIMITS IAW SRM 52-30-16-1A. C/W REPAIR IAW EA 1-5230-T0349272 PT 1.SDR FDEA2019101062540Repair · crackedNR 1 ACM EXHAUST OUTLET DOOR CUTOUT, PREVIOUS DOUBLER REPAIR, IS CRACKED AT LOWER FWD CORNER AREA. REMOVED AND REPLACED THE REPAIR DOUBLER IAW DWG ACA3850 AND SRM 51-31-01.SDR FDEA2019101082488Hinge · corrodedMCD: UNDERSIDE OF HINGE SEGMENT #5 AT ATTACH POINT WITH MCD HAS CORROSION. AREAS MRKD IN RED (DOT 5) 5121818: CONSIGNADO, FREDERICK J - 19-SEP-2019 02:20 REMOVED CORROSION FROM NOTED HINGE SEGMENT MATERIAL REMAINING IS .066 IS OUT OF LIMITS PER SRM 52-30-SDR FDEA201908162280Hinge · corrodedMCD: UNDERSIDE OF HINGE SEGMENT #4 AT ATTACH POINT WITH MCD HAS CORROSION. AREAS MRKD IN RED (DOT 4) REMOVED CORROSION FROM NOTED HINGE SEGMENT. MATERIAL REMAINING IS .036 IS OUT OF LIMITS PER SRM 52-30-16-1A. C/W REPAIR PER EA 1-5230-T0349272 PT 2. TITLE DOORSDR FDEA201908152279Hinge · corrodedUPPER MCD: UPPER DOOR FRAME/CHORD HAS EXFOLIATION CORROSION ON MULTIPLE AREAS FROM LE TO TE. (AREAS MARKED - VIEWED FROM INSIDE A/C) C/W REPAIRS PER EA 1-5230-T0349272 PT.2 TITLE: DOORS- MAIN CARGO DOOR-UPPER DOOR HINGE SEGMENTS RUSTED. REFER TO N/R #625,626,6SDR FDEA201908302039Rib · crackedLEFT NR 1 SLAT CRUISE PERFORMANCE FAIRING ARB7105-3 CRACKED AT UPPER ATTACHMENT STUD. REPAIRED THE RIB IAW SRM 57-40-71 FIG 201 SH. 1 MAJOR REPAIR.SDR FDEA2019082832035Rib · crackedRT NR 1 SLAT CRUISE PERFORMANCE FAIRING CRAKED AT UPPER ATTACH STUD. REPAIRED THE RIB IAW SRM 57-40-71-2R FIG 201SDR FDEA201908122505Structure · corrodedCTR WING AREA UPPER SURFACE APPROX. STA 1229 LBL 98 TO 102 CORROSION FOUND ON UPPER TANK SURFACE AND AROUND SEVERAL FASTENERS MECHANICALLY REMOVED SURFACE CORROSION IAW SRM 57-00-01 AND BLEND OUT ACCEPTABLE PER EA 1-5730-T0348981SDR FDEA2019101081504Fuel Tank · corrodedCENTER FUEL TANK UPPER SURFACE, BS 1229, LBL 75 TO 79 CORRODED. MECHANICALLY REMOVED SURFACE CORROSION IAW SRM 57-00-01 AND BLENDED OUT IAW EA 1-5730-T0348981.SDR FDEA2019101082512Floorboard · damagedMAIN DECK: FLOOR PANEL FROM APPROX BS 791-840 BETWEEN SEAT TRACKS LBL 75 AND LBL 108 WAS DAMAGED AND WORN. REPLACED FLOOR BOARD IAW DWG SRZ-25-005.SDR FDEA201910102509Floorboard · damagedMAIN DECK FLOOR PANEL AT STA 6-70 BETWEEN RBL 75-107 POSITION 8R IS WORN THROUGH TOP SURFACE OUTLINING LOADING RAIL. REPLACED THE FLOOR PANEL IAW DWG ACA3209.SDR FDEA2019101082507Floorboard · damagedMAIN DECK FLOOR PANEL FROM APPROX STA 791-840 BETWEEN SEAT TRACKS RBL 75 AND RBL108 WAS DAMAGED AND WORN. REPLACED THE DAMAGED FLOORBOARD WITH A NEW FLOORBOARD IAW DRAWING SRZ-25-005.SDR FDEA2019101082503Fuel Tank · corrodedCENTER TANK AREA UPPER SURFACE, APPROX. BS 1229, LBL15 - 20 CORRODED. FOUND ON UPPER TANK SURFACE AND AROUND SEVERAL FASTENERS. REMOVED SURFACE CORROSION IAW SRM 57-00-01 AND BLENDED OUT IAW EA 1-5730-T0348981.SDR FDEA201908112151Seat Track · wornMAIN DECK SEAT TRACK: STA 1261-1301 - LBL = 75.25 HAS (2) AREAS WORN BEYOND LIMITS. (MRKD) REPLACED DAMAGED SEAT TRACK SECTION AT STA 1229 TO 1285 LBL-75.25 REF SRM 53-00-52-2R REPAIR-1 FIG-201.SDR FDEA201908112087Floor Panel · damagedMAIN DECK: FLOOR PANEL FROM APPROX STA 840-899 BETWEEN SEAT TRACKS LBL75 AND LBL108 IS DAMAGED AND WORN (MARKED AND DOT 24) REPLACED DAMAGED FLOOR PANEL AS REQ REF DWG SRZ-25-005.SDR FDEA2019082111949Skin · corrodedRH WING UPPER SURFACE - APPROX XORS 331 STINGER 17 - CORROSION AROUND TWO FASTENERS. REPAIRED PER SRM 57-00-01 FIG.101 SHT. 1-10.SDR FDEA201905041007Retract Cylinder · failedAPPROXIMATELY 2 HRS INTO FLIGHT RECIEVED LVL-1 HYD 3 ELEV OFF ALERT WITH HYDRAULIC QUANTITY OF 4.9 GAL. QTY LEVEL CONTINUED TO DROP SLOWLY UNTIL SYSTEM DEPRESSURIED AS A RESULT OF QTY TRIGGERING THE HYD 3 OFF ALERT UPON CONFIGURING WE LOST ALL HYD FLUID RESULSDR FDEA201902210472Deu · failedIN CRUISE FL300 DEU NR 1, ''NO COMPARE'' ALERT. ON PFD ON FIRST. REMOVED AND REPLACED DEU NR 2 AS PER AMM 31-61-02-4. ALL TESTS SATIS.SDR FDEA201802030295Frame · corrodedRT MLG TRUNNON SUPPORT FAYING SURFACE CORRODED. REPAIRED IAW 1-3210-T0338223, REV A , POS P11. REPAIRED THE FRAME IAW SRM 57-20-14-2R. REPAIR 2 AND EA 1-3210-T0338223 A, PART 1.SDR FDEA201801050028Fitting · unsecureDURING TAKEOFF, RECEIVED AN UNRELIABLE AIRSPEED ON FIRST OFFICER'S SIDE. FOLLOWED QRH PROCEDURES AND LANDED. MX FOUND THE BAYONET FOR AIR SYSTEM OF THE NR 2 CADC NOT SECURE. SECURED IAW SMP, TESTED SYSTEM IAW MM 34-16-01-700-802, THE SYSTEM PRESSURE HOSDR FDEA201707282066Doubler · crackedLT WING LEADING EDGE CAVITY BEADED DOUBLER AT STA XOS 653 - XOS 659 FOUND CRACKED. BEADED DOUBLER REPAIRED AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201707282065Doubler · crackedLEFT WING LEADING EDGE CAVITY BEADED DOUBLER AT XOS 698 - 703 FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201707282064Doubler · crackedRIGHT WING LEADING EDGE CAVITY BEADED DOUBLER AT XOS 626 FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201707282063Skin · crackedDURING HFEC OPEN HOLE INSPECTION OF THE RT WING CORNER NR 2 OF SLAT ANTI -ICE TELESCOPING DUCT CUTOUT, UPPER OTBD CORNER, A CRACK WAS FOUND APPROX. 1/2 INCH IN LENGTH, AT XOS 470. REPAIRED IAW SRM 57-40-01-2R, FIGURE 202, REPAIR 10. REPAIR CLASSIFIED MAJOR SDR FDEA201707282062Skin · crackedDURING HFEC OPEN HOLE INSPECTION ON THE RT WING CORNER NR 5 OF SLAT ACTUATOR ACCESS DOOR, THE FORWARD INBD CORNER WAS FOUND CRACKED APPROX. 1/2 INCH IN LENGTH, AT XOS 490. REPAIRED IAW SRM 57-40-01-2R, FIGURE 201, REPAIR 17. REPAIR CLASSIFIED AS MAJOR IAWSDR FDEA201707272054Structure · damagedCENTER CARGO DOOR EXTERIOR FWD LOWER EDGE DAMAGED REPAIREDTIAW EA 1-5230-T0332581, B PT 4.SDR FDEA201707262048Frame · chafedMAIN DECK CARGO FRAME CHAFED AT BS 535, LONGERON 19L. REPAIRED IAW SRM 53-20-07-2R, FIGURE 202, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201707262047Frame · chafedMAIN DECK CARGO FRAME CHAFED AT BS 535, LONGERON 24L. REPAIRED IAW SRM 53-20-07-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201707262045Cargo Track · damagedMAIN DECK CARGO TRACK CROWN AREA DAMAGED AT BS 1426, LBL 8.5. REPAIRED THE SEAT TRACK IAW SRM 53-00-52, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201707262044Seat Track · damagedCABIN MAIN DECK CARGO COMPT SEAT TRACK CROWN AREA DAMAGED AT LT STA 1541, X=47.5. SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 1571 TO EXISTING SPLICE STA 1531, X=47.5. AS PER SRM 53-00-52 FIG 201 REPAIR 1. REPAIR CLASSIFIED MAJOR AS PER GMSDR FDEA201701230239Rib · crackedRIGHT WING L/E NR 6 SLAT HAS A CRACKED NR 7 RIB. REMOVED AND REPLACED THE SLAT IAW AMM 27-80-30-5.SDR FDEA201701230238Rib · crackedLEFT WING L/E SLAT NR 6 HAS A CRACKED RIB NR 6. THE RIB WAS REMOVED AND REPLACED IAW AMM 27-80-30-5.SDR FDEA201701170213Skin · chafedRIGHT NR 8 SLAT COVE PANEL INNER SKIN IS CHAFED AT OUTBOARD RIB XOS 1185. BLENDED OUT CHAFED AREA IAW SRM 57-00-00-2R FOUND TO BE OUT OF LIMITS, PERFORMED A DOUBLER REPAIR IAW SRM 57-40-01-2R AND EA 1-5750-T0330795.SDR FDEA201612274581Fairing · damagedRIGHT OTBD FLAP, INBD AFT FAIRING DAMAGED. REPAIRED IAW SRM 51-31-01.SDR FDEA201606292192Pitot Line · contaminatedLOST FLIGHT DIRECTORS AND AUTOPILOT/ATS PASSING 16000. F/O AIRSPEED 10 KNOTS LESS THAN CAPTAIN AND STANDBY A/S. ALSO RECEIVED, SELECT ELEVATOR FEEL MANUAL AND SELECT FLAP LIMIT OVER RIDE INDICATIONS. ENTERED A/S UNRELIABLE CHECKLIST. F/O SELECTED AUXILIARSDR FDEA201508242692Fitting · corrodedRIGHT WING OTBD FLAP VANE FITTING F BUSHING BORE CORRODED. FOUND OUT OF LIMITS IAW SRM 57-50-02-2R. REPAIR BUSHING FABRICATED IAW EA 1-5750-T0319728 P 1 STEP 1. BUSHING INSTALLED IAW AMM 27-50-32-4. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
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