N397FE, cancelled Jan 29, 2024
Service difficulty reports · 78
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 = 'N397FE' AND deregistration_id = 'N397FE-2024-01-29' 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 = 'N397FE' AND deregistration_id = 'N397FE-2024-01-29' 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 FDEA201408052077Skin · crackedRIGHT WING LE IS CRACKED NR 3 SLAT ANTI-ICE DUCT CUT OUT TOP SIDE. BOTH CORNERS REPAIR COMPLIED WITH USING EA 8-5710-T0308474.SDR FDEA201309132206Fire Loop · false indicationNR 2 ENGINE LOOP, A LEVEL 2 ON 10 MILE FINAL. POSSIBLE ENG FIRE. INSPECTED FAN, REVERSER AND TURBINE COWLS AND PERFORMED GVI OF NR 2 ENGINE. NO EVIDENCE OF FIRE OR PNUEMATIC DUCT LEAK. NO EVIDENCE OF DAMAGE TO FIRE LOOPS NOTED. NO EVIDENCE OF FIRE IN TAISDR FDEA201302120472Bulkhead · crackedINBD BULKHEAD CRACKED 32 INCHES FWD OF BS 1521 AND 3 INCHES DOWN FROM UPPER BULKHEAD. REPAIRED IAW SRM 53-00-01, FIG 10.SDR FDEA201302120470Bulkhead · crackedRT BULKHEAD HAS ONE CRACK 51 INCHES FWD OF BS 1521 AND 31 INCHES UP FROM BELLY SKIN. REPAIRED IAW SRM 53-00-01.SDR FDEA201302120471Bulkhead · crackedINBD BULKHEAD ONE CRACK 14 INCHES AFT OF BS 1381 AND 14 INCHES DOWN FROM UPPER BULKHEAD. CRACK VERIFIED USING HFEC. REPAIRED THE DAMAGED TO THE RT SIDE WHEEL WELL BULKHEAD IAW EA 8-5310-157380.SDR FDEA201302120469Bulkhead · crackedLT BULKHEAD HAS THREE CRACKS 12 INCHES AFT OF BS 1381 AND 3 INCHES DOWN FROM UPPER BULKHEAD, AND ONE IS 13 INCHES AFT BS 1381 AND 3 INCHES DOWN, AND LAST CRACK IS 17 INCHES. AFT BS 1381 AND 3 INCHES DOWN. ALL THREE CRACKS HAVE BEEN VERIFIED USING HFEC. REPASDR FDEA201302120468Bulkhead · crackedINBD BULKHEAD HAS TWO CRACKS 21 INCHES AFT OF BS 1381 AND 7 AND 9 INCHES DOWN FROM UPPER BULKHEAD. TWO CRACKS VERIFIED USING HFEC. COMPLETED REPAIR OF AREA USING EA 8-5310-157381 AND REPAIR SKETCH 201302130091-001 AS REF.SDR FDEA201301020003Angle · corrodedNR 3 ACM BAY FOUND THE ACA3796-2 TEE ANGLE CORRODED BEYOND LIMIT AT BS 585, LONGERON 47R. R & R TEE ANGLE IAW REF 51-33-00 AND 51-35-01, VOL II.SDR FDEA201212314406Tee Fitting · crackedRT FWD PRESSURE BULKHEAD AT BS 595, RT LONGERON 43, FOUND CRACKED AT THE WEB AND TEE FITTING. SERVICABLE TEE FITTING INSTALLED IAW EA 8-5310-163797.SDR FDEA201204081302Cover · brokenR1 DOOR LOWER FWD EXIT LIGHT COVER BROKEN. REPLACED LIGHT COVER. OK FOR SERVICE.SDR FDEA201106262431Power Supply · dischargedDURING PREFLIGHT, OBSERVED EMGERENCY LIGHT BATTERY 1 LOW. REPLACED EMERGENCY LIGHTS POWER SUPPLYSDR FDEA201105031704Battery · inoperativeDURING PRE FLIGHT GOT EMERGENCY LIGHT BATTERY LOW ALERT. R & R EMERGENCY LIGHT BATTERY IAW MM 33-51-01-4. OPS CHECKS NORMAL IAW MM 33-51-01-5.SDR FDEA201012204728Switch · failedNR 2 ENG OIL FILTER LEVEL II ALERT. INFLT SHUT DOWN AS PER FLT CREW WITH LEVEL II ALERT, ENG HAD NORMAL OIL PRESSURE. INSPECTED FILTER ELEMENT FOR CLOGGING, ELEMENT FOUND CLEAN AND NOT CLOGGED. INSTALLED NEW FILTER ELEMENT AS PER MM 79, RAN ENG AS PER JRHSDR FDEA200910283716Manifold · dirtyDURING DESCENT, LVL 1 HYD 3 ELEV OFF-NR3 HYD LEVEL AT 4.5 GALLONS. RAN CHECKLIST SHORTLY FOLLOWED BY HYD 3, QTY LO AND THEN HYD 3 FAIL SGN - REPLACED NR3 ENG HYD SYS MANIFOLD FILTERS IAW AMM 29-12-02-2, NO METAL OR DEBRIS FOUND IN OLD FILTERS. STILL REDQUIRESSDR FDEA200812195245Wire · brokenNR 3 ENGINE HUNG START AT FL 25.0 AND DESCENDED TO 10000 FT STILL WOULD NOT ACCELERATE; SHUT DOWN ENGINE. IDLE READINGS: ENGINE 1 N1 38 PERCENT; EGT 362; N2 71.1 PERCENT, ENGINE 2 N1 39 PERCENT; EGT 362; N2 72.6 - ENGINE 3 N1 29 PERCENT; EGT 372; N2 50.5 SDR FDEA200812175189Skin · dentedRT FUSELAGE AT STA 1776 BETWEEN LONGERONS 39R AND 40R THE SKIN IS DENTED. REPAIR SKIN IAW E.A. 8-5330-123532 TITLE (FUSELAGE DENT IN GROSS WEIGHT MOD DOUBLER AT STA 1816, L39R - L40R ). REMOVED AND REINSTALLED ACCESS PANELS IN THE PIT IAW SRM 57-31-01; VOL ISDR FDEA200812085106Sleeve · dentedNR 2 ENGINE LEFT TRANSLATING COWL OUTER SKIN IS DENTED. REPAIRED NR 2 LEFT TRANSLATING SLEEVE/COWL OUTER SKIN BY DRILLING INJECTED HOLES AND INJECTING EA 934 ADHESIVE AND FILLING THE DENT WITH POTTING COMPOUND AND CURING IAW CF6-6 ENGINE MANUAL 78-00-32; REPASDR FDEA200811254972Solenoid · defectiveL-1 DOOR TORQUE TUBE SOLENOID NOT OPERATING PROPERLY. REMOVED AND REPLACED L-1 DOOR TORQUE TUBE SOLENOID AND ADJUSTED. OPS CHECKED GOOD IAW FEDEX MD 10 AMM 52-11-13-2 AND 52-11-00-5.SDR FDEA200811124864Skin · gougedLT WING INBD SLAT GOUGED OTBD TOP CORNER. REMOVED AND RE-INSTALLED THE LEFT NR 2 SLAT. BLENDED AREA IAW SRM 57-00-01; FIG 1-A; SHEET 3; PG 5; VOL I AND 57-55-01. FABRICATED SKIN AND SPLICE PLATES THEN INSTALLED RTEF SRM 57-10-00; VOL I; FIG 3-1. GAP CHECKSSDR FDEA200811124865Spar Cap · crackedAPPROX 2.75 INCH CRACK EXISTS IN RT WING LOWER SPAR CAP (PSE 57.10.008) AT XORS = 411. CRACK RUNS FROM AFT EDGE OF SPAR CAP AFT TANG, FWD APPROX 1.625 INCH TO RADIUS, THEN UPWARDS AND INBOARD APPROX 1.125 INCH AND TERMINATES AT VERTICAL LEG FASTENER AT APPROXSDR 08FDEA04865Spar Cap · crackedAPPROX 2.75 INCH CRACK EXISTS IN RT WING LOWER SPAR CAP (PSE 57.10.008 ) AT XORS = 411. CRACK RUNS FROM AFT EDGE OF SPAR CAP AFT TANG, FWD APPROX 1.625 INCH TO RADIUS, THEN UPWARDS AND INBOARD APPROX 1.125 INCH AND TERMINATES AT VERTICAL LEG FASTENER AT APPROSDR FDEA200811044709Skin · wornAFT NACELLE, FIREWALL SEAL PLANE AT FS Y2166 AND LEFT SIDE OF THE TRAILING EDGE OF THE DIVERTER, HAS WORN SKIN. REPAIR WORN SKIN AREA IAW SRM 51-31-01; VOL II; PG 1; SRM 55-35-04; VOL III AND DWG AJC7415, REV "BK". ALODINED AND PRIMED IAW SRM 51-21-01; VOLSDR 08FDEA04708Skin · wornAFT NACELLE, FIREWALL SEAL PLANE AT FS Y2166 AND RIGHT SIDE OF THE TRAILING EDGE OF THE DIVERTER; HAS WORN SKIN AND IS CRACKED. REMOVED AND FABRICATED NEW SKIN SECTION IAW SRM 51-35-01 VOL II AND DWG AJC7415 REV BK, ALODINED AND PRIMED IAW SRM 51-21-01 VOL I SDR 08FDEA04771Skin · corrodedCENTER LANDING GEAR WHEEL WELL, FS 1481 TO FS 1501 BETWEEN STR R50 TO L49 HAS CORROSION ON SKIN. REMOVED CORROSION IAW SRM 51-21-01 PG 28 A VOL II. SKIN ORIG THICKNESS 0.125 IAW DWG AYB 7030; REV "E". REMAINING MATERIAL THICKNESS 0.090. MATERIAL REMOVED 0.SDR 08FDEA04770Skin · corrodedCENTER LANDING GEAR WHEEL WELL, FS 1501 TO FS 1521 AT STR R50 TO L48 HAS CORROSION AND BARE METAL. REMOVED CORROSION IAW SRM 51-21-01 PG. 28 VOL. II. ORIGINAL THICKNESS ON SKIN IS .125 IAW DWG AYB7030 REV E. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01 PG. 6SDR 08FDEA04709Skin · wornAFT NACELLE, FIREWALL SEAL PLANE AT FS Y2166 AND LEFT SIDE OF THE TRAILING EDGE OF THE DIVERTER, HAS WORN SKIN.SDR 08FDEA04658Fitting · corrodedMAIN CARGO DOOR LOWER JAMB NR 7 FITTING HAS CORROSION IN HOLES "A"; "C" AND "D". REMOVED & REPLACED AFA 7132-1 FITTING & REPAIRED THE LOWER JAMB IN REF TO DC/MD-10 SRM 53-50-00 FIG 17 VOL I & DC/MD-10 SRM 51-33-01 VOL II.SDR 08FDEA04657Fitting · corrodedMAIN CARGO DOOR LOWER JAMB NR 6 FITTING HAS CORROSION IN HOLES "A"; "B"; "C" AND "D". REMOVED & REPLACED AFA 7132-1 FITTING & REPAIRED THE LOWER JAMB IN REF TO DC/MD-10 SRM 53-50-00; FIG 17 VOL I & DC/MD-10 SRM 51-33-01 VOL II.SDR 08FDEA04656Fitting · corrodedMAIN CARGO DOOR LOWER JAMB NR 5 FITTING HAS CORROSION IN HOLES "C" AND "D". REMOVED & REPLACED AFA 7132-1 FITTING & REPAIRED THE LOWER JAMB IN REF TO DC/MD-10 SRM 53-50-00 FIG 17 VOL I & DC/MD-10 SRM 51-33-01 VOL II.SDR 08FDEA04655Fitting · corrodedMAIN CARGO DOOR LOWER JAMB NR 4 FITTING HAS CORROSION IN HOLES "A"; "B" AND "D". REMOVED & REPLACED AFA 7132-1 FITTING & REPAIRED THE LOWER JAMB IN REF TO DC/MD-10 SRM 53-50-00 FIG 17 VOL I & DC/MD-10 SRM 51-33-01 VOL II.SDR 08FDEA04654Fitting · corrodedMAIN CARGO DOOR LOWER JAMB NR 3 FITTING HAS CORROSION IN HOLES "A" AND "D". REMOVED & REPLACED AFA 7132-1 FITTING & REPAIRED THE LOWER JAMB IN REF TO DC/MD-10 SRM 53-50-00 FIG 17 VOL I & DC/MD-10 SRM 51-33-01 VOL II.SDR 08FDEA04653Fitting · corrodedMAIN CARGO DOOR LOWER JAMB NR 2 FITTING HAS CORROSION IN HOLES "B" AND "C". REMOVED & REPLACED AFA 7131-1 FITTING & REPAIRED THE LOWER JAMB IN REF TO DC/MD-10 SRM 53-50-00 FIG 17 VOL I & DC/MD-10 SRM 51-33-01 VOL II.SDR FDEA200810274845Structure · corrodedRT MLG W/W BS 1381 RBL 116 OTBD LOWER CORNER OF SLANT PANEL VERTICAL TEE CAP HAS CORROSION. DISPLACED SLANT PANEL IAW SRM 51-31-01; VOL I. REMOVED 7, REPLACED ANGLE IAW SRM 51-33-01; VOL II AND DWG NR AEA0471; REV "A". FABBED AND INSTALLED NEW ANGLE IAW DACSDR 08FDEA00289Wire Harness · out of positionMAIN GEAR WOULD NOT RETRACT ON AFTER TAKEOFF CHECKLIST CYCLED GEAR AS PER QRH GEAR WENT DOWN 3 GREEN BUT MAIN GEAR STILL WOULD NOT RETRACT CONFIG PAGE CONFIRMED ALL THE ABOVE. FOUND LEFT AND RIGHT UPLATCH SENSOR WIRE HARNESS INTERFERING WITH TRAVEL OF LINK ASDR 08FDEA00291Wire Harness · out of positionMAIN GEAR WOULD NOT RETRACT ON AFTER TAKEOFF CHECKLIST CYCLED GEAR AS PER QRH GEAR WENT DOWN 3 GREEN BUT MAIN GEAR STILL WOULD NOT RETRACT CONFIG PAGE CONFIRMED ALL THE ABOVE. FOUND LEFT AND RIGHT UPLATCH SENSOR WIRE HARNESS INTERFERING WITH TRAVEL OF LINK ASDR 07FDEA01813Skin · crackedMODIFICATION AND REPAIR ASSESSMENT ON 13 APRIL 2007, DURING PNEUMATIC TESTS WITH AIR, AT 9:30 A.M. THE PRESSURIZED AIR FLEXIBLE HOSE COLLAPSED CAUSING THE END CONNECTING TO THE HANGAR UNDERFLOOR MANIFOLD TO HIT THE LOWER FUSELAGE JUST FWD OF C.A.C. THE IMPASDR 07FDEA01730Skin · dentedACF MODIFICATION AND REPAIR ASSESSMENT HORIZONTAL STABILIZER LT SIDE DENTS, NICKS, DEFORMATION RIB AND SKIN AND 10 EA RIVETS LOOSE ON LOWER SKIN B/T STA 48.500 TO STA XE 67.225 AND STA XE 88.625 TO STA XE 100.455. REMOVED DETACHABLE ELEVATOR , REMOVED LWR SDR 07FDEA01729Shear Tie · corrodedMD 10-10 ACF MODIFICATION AND REPAIR ASSESSMENT AFT CARGO COMPARTMENT: MISSING MATERIAL AND CORROSION ON SHEAR CLIP STA 1956 B/T L 48 TO L 50 LT SIDE REMOVED CLIPS ATTACHING FOR ACCESS: REMOVED INTERCOSTAL AND RIVETS, CUT OUT SHEAR CLIP DAMAGED, CLEANED EXCESSSDR 07FDEA01728Longeron · damagedACF MODIFICATION AND REPAIR ASSESSMENT\AFT CARGO COMPT TUNNEL SIDE RT: STA 1801-1821 NICK ON THE LONGERON 27 PERFORMED BLEND-OUT AND CHECK LIMITS IAW SRM 53-00-01 FIG 1 B. INSTALLED ANGLE AND EXISTING STRAP IAW SRM 53-00-01 FIG 7 AND SRM 51-33-01 VOL. II. PRSDR 07FDEA01727Longeron · crackedACF MODIFICATION AND REPAIR ASSESSMENT LT MLG WHEEL WELL: AT STA 1510, AT X = 30 FOUND LONG WITH CRACK THE 1 INCH ACCOMPLISHED CRACK STOP DRILL 1/4 '' DIA AND REPAIRED LONGERON IAW SRM 53-00-01 FIG 9 VOL I.SDR 07FDEA01724Skin · crackedMD 10-10 ACF MODIFICATION AND REPAIR ASSESTMENT RT WING LEADING EDGE STA XORS 506 LOWER SIDE CLOSE TO PANEL FUEL PANEL, SKIN WITH CRACK OF ABOUT 2 INCH REMOVED ACCESS DOOR, REPAIRED FIXED L.E IAW SRM 57-10-00 FIG 68 SHEETS 2 AND 3. INSTALLED ACCESS DOOR. SDR 07FDEA01633Frame · corrodedMD 10-10 ACF MODIFICATION AND REPAIR ASSESSMENT AFT FUSE WASTE TANK COMPT STA 1996 RT SIDE TO L 47 FROM L 50 REPAIR EXISTING WITH LIGHT CORROSION. PERFORMED REPAIR WITH NRC NR 1202.SDR 07FDEA01632Frame · corrodedACF MODIFICATION AND REPAIR ASSESSMENT AFT FUSE WASTE TANK COMPT STA 1996 LT SIDE TO L. 50 FROM L. 52 REPAIR EXISTING WITH LIGHT CORROSION. REMOVED EXISTING REPAIR, PERFORMED INSPECTION, CUP ANGLE B/T L46 AND L48 RT SIDE AND B/T L 48 TO L 50 LT SIDE IAW SRM 5SDR 07FDEA01585Door Frame · crackedMODIFICATION AND REPAIR ASSESSMENT R3 DOOR ON JAMB STA 1305 SIDE LOWER FOUND WEB WITH EXISTING REPAIR REMOVED EXISTING REPAIR NOT IN COMPLIANCE WITH SRM 53-50-00 FIG 19.SDR 07FDEA01580Skin · crackedMODIFICATION AND REPAIR ASSESTMENT RT WING INBOARD AILERON FRONT SPAR WITH EXISTING REPAIR STA XIA 372 TO 374 REMOVED DOUBLER (EXISTING REPAIR), FOUND CRACKS. REMOVED AILERON RT INBOARD. REPAIRED SKIN DOUBLER. INSTALLED FILLER AND COVER IAW MM 20-50-02. ISDR 07FDEA01574Skin · damagedMODIFICATION AND REPAIR ASSESSMENT RT WING DROP LEADING EDGE WITH WORN AND MISSING MATERIAL ON EXISTING REPAIR. REMOVED INNER SKIN AND EXISTING REPAIR IAW SRM 51-31-01 VOL II. REPAIR DOUBLER, INSTALLED IAW SRM 57-10-00 FIG 55 VOL I. REINSTALLED HINGE, FWSDR 07FDEA01518Skin · corrodedDURING MD10-10 ACF MODIFICATION AND REPAIR ASSESSMENT PROG EXISTING REPAIR ON SKIN STA 1039 RT SIDE BETWEEN L 50 TO L 51. REMOVED EXISTING REPAIR IAW SRM 51-35-01 VOL II . CUT DAMAGED SKIN AND REMOVED CORROSION. PERFORMED CHECK LIMITS AND TREATED IAW SRM 51SDR 07FDEA01512Skin · damagedDURING MD10-10 ACF MODIFICATION AND REPAIR ASSESSMENT RT WING INBOARD FLAP UPPER SIDE WITH EXISTING REPAIR STA XIFH 219.550 REPAIR CARRIED OUT IAW SRM 57-10-00 FIG 85.SDR 07FDEA01510Skin · misrepairedDURING MD10-10 ACF MODIFICATION AND REPAIR ASSESMENT PROG EXITING REPAIR ON EXTERNAL SKIN STA 603 TO STA 617 RT SIDE BETWEEN L 43 TO L 45. REMOVED OLD REPAIR (BECAUSE IS NOT COMPLIANCE WITH SRM 53-20-00 FIG 6) AND INSTALLED NEW REPAIR IAW SRM 53-20-00 FIG SDR 07FDEA01504Skin · dentedDURING MD10-10 ACF MODIFICATION FOUND 3 DENTS ON EXTERNAL SKIN BETWEEN STA 1797 TO 1804 RT SIDE LONGERON 29 TO LONGERON 30, DENT 0.32" BY 2" BY 1" STA 1802 TO 1804, DENT 0.32" BY 1" BY .050" STA 1801, DENT 0.32" 1.80" BY 1" STA 1797 TO 1799. PERFORMED REPAIR
Back to N397FE, cancelled Jan 29, 2024