N396FE, cancelled Mar 2, 2024

Service difficulty reports · 124

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 = 'N396FE' AND deregistration_id = 'N396FE-2024-03-02'
  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.

SDR FDEA2020043090818Sensor · failedPDIS 396 27-80 8011 28APR20 ONT FACT U LOGPAGES:3164057 ON FINAL APPROACH " SLAT DISAG" RECV'D AS FLAPS MOVED FROM 22 TO 35. COMPLIED W/ QRH ACCOMPLISHED A 22 FLAP LANDING. SHGN 28APR20 06:15 ONT U REMOVED PANEL 516AB FOR ACCESS FOR TECH Apr 29, 2020 · N396FE · Doug MD1010F · Leading Edge Slat Position Indicating SystemSDR FDEA2019110752873Sensor · failedUPON SLAT RETRACT AFTER T/O CHECK LIST, SLAT DISAGREE ILLUMINATED, CYCLED SLAT EXTEND & BACK TO UP WITH NO FAULT. REMOVED AND REPLACED L2B SLAT POSITION SENSOR. OPS CHECKED SATISFACTORY. OK FOR SERVICE.Nov 5, 2019 · N396FE · Doug MD1010F · Leading Edge Slat Position Indicating SystemSDR FDEA2019093022367Slide · inoperativeMAIN ENTRY DOOR 1-L SLIDE RAFT INOP. REMOVED AND REPLACED L1 DOOR SLIDE AND CONTAINER IAW AMM 25-61-01-2. ALL OPS CHECKS AND PRESSURES GOOD. ACFT OK FOR SERVICE.Sep 28, 2019 · N396FE · Doug MD1010F · Escape SlideSDR FDEA201909042116Skin · cracked2" CRACK LT WING BELOW #1 SLAT SHGN 04SEP19 18:09 MEM U CHECKED THE GENERAL AREA FOR CRACKED MATERIAL. USING HFEC REF NDTSPM PART 6. LOCATED A FLAW INDICATING APPROXIMATLY 2 INCHES IN LENGTH. PAINT WILL NEED TO BE REMOVED TO DETERMINE THE ACTUAL LENGTH INSTSep 4, 2019 · N396FE · Doug MD1010F · Wing, Plate/SkinSDR FDEA201903160647Skin · crackedRT WING OB FLAP UPPER SUFACE SKIN CRACKED (EST 3" FRONT TO BACK) REPAIRED USING SRM 57-10-00 FIG 85 AS A REFERENCE.Mar 16, 2019 · N396FE · Doug MD1010F · Trailing Edge FlapsSDR FDEA2018102653004Truss · crackedNR 3 PYLON TRUSS FITTING INBOARD TRUSS HALF OUTBOARD EDGE HAS A CRACK INDICATION. REPAIRED PER E.A. 8-5450-T0342532. MAJOR REPAIR.Oct 25, 2018 · N396FE · Doug MD1010F · Nacelle/Pylon Miscellaneous StructureSDR FDEA201810232981Longeron · crackedNOSE WHEEL WELL, AFT DOOR ON THE LT SIDE IS BINDING ON THE SKIN WHEN CLOSING, 2018-10-23. REMOVED AND REPLACED THE LONGERON AT STA 548 TO STA 595 LONGERON 48L, NOSE WHEEL WELL PER DWG ACA 3796, EA 8-5310-T0327817 C, PART 3 & SRM 51-31-01 VOL 2.Oct 23, 2018 · N396FE · Doug MD1010F · Fuselage Main, Longeron/StringerSDR FDEA2018100542777Bracket · corrodedAFT CARGO COMPARTMENT FWD BULKHEAD STA.1781 LONGERON R42 L-ANGLE BRACKET SHOWING EXFOLIATING CORROSION. REMOVED & REPLACED "T-ANGLE BRACKET" AFB3883-505 AT STA. 1781 LONGERON R42 PER DWG AFA3878.Oct 4, 2018 · N396FE · Doug MD1010F · Fuselage Miscellaneous StructureSDR FDEA2018100532775Longeron · crackedNOSE W/W LT DOOR JAMB - LONGERON CRACKED PAST STOP DRILL AT STA.584. PART ACA3796-1 REQUIRES REPLACEMENT. REMOVED & REPLACED LONGERON AT STA. 548-STA.595 L48L NOSE W/W PER DWG ACA3796 & SRM 51-31-01 VOLIIOct 3, 2018 · N396FE · Doug MD1010F · Fuselage Main, Longeron/StringerSDR FDEA201810012758Skin · delaminatedLT WING NR 5 SPOILER UPPER SKIN HAS 5 3/4 " X 7 1/4" OF DELAMINATION. REPAIRED LT WING NR 5 SPOILER IAW SRM 51-71-00 VOL II PAR 16.Oct 1, 2018 · N396FE · Doug MD1010F · SpoilersSDR FDEA201809272716Shear Tie · crackedFWD CARGO COMPT STA 1099 SHEAR TIE CRACKED AT LEG. REPAIRED CRACKED SHEAR TIE AT STA 1099 PER SRM 53-30-00 VOL 1 PAGE 34.Sep 27, 2018 · N396FE · Doug MD1010F · Fuselage Internal Mounting StructureSDR FDEA201809252709Skin · corrodedR/H WING, TOP SKIN HAS CORROSION OUT OF LIMITS BETWEEN STR. -10 AND 11 XTA. XROS 346 REMOVED CORROSION PER SRM 57-10-00 FIG 61 VOL 1 AND EA# 8-5710-T0342487Sep 25, 2018 · N396FE · Doug MD1010F · Wing, Plate/SkinSDR FDEA201809192613Skin · delaminatedLT WING NR 5 SPOILER UPPER SKIN HAS 5 3/4" X 7 1/4" OF DELAMINATION. REPAIR LT WING NR 5 SPOILER IAW SRM 51-71-00 VOL II PAR 16.Sep 19, 2018 · N396FE · Doug MD1010F · SpoilersSDR FDEA2018091862556Seat Track · wornMAIN DECK SEAT TRACK STA 755 LT X=47.5 LBL WORN BEYOND LIMITS. REPLACED DAMAGED SEAT TRACK, FROM STA 745 - 765 REF SRM 53-70-00 FIG 1 V1 & DWG NCA6392.Sep 16, 2018 · N396FE · Doug MD1010F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA2018092542666Skin · unknownREPAIR ASSESSMENT: R/H DETACHABLE ELEVATOR, UPPER SURFACE, STA. XE 91, 28" FROM TRAILING EDGE, HAS AN EXISTING DOUBLER. APPROX 4" DIA. DOT 105 REPAIR WAS PREVIOUSLY INSTALLED PER SRM 55-00-01 FIG. 3 SH.2 VOL.1. REF. E.A. 8-5100- T034059 "STRUCTURES-REPAIR CSep 14, 2018 · N396FE · Doug MD1010F · Elevator, Plate/SkinSDR FDEA201809102631Skin · crackedRT LWR WING ACCESS DOOR CUTOUT FASTENER ATTACH HOLE 1 EA HAS A CRACK INDICATION AT FWD EDGE HOLE. REPAIRED AREA PER EA. 8-5730-T0342637.Sep 10, 2018 · N396FE · Doug MD1010F · Wing, Plate/SkinSDR FDEA2018091882551Skin · corrodedRT WING UPPER SKIN CORROSION AT FASTENER STA XORS 400 20 INCH FWD OF AFT SPAR. REMOVED CORROSION PER SRM 57-10-00.Sep 8, 2018 · N396FE · Doug MD1010F · Wing, Plate/SkinSDR FDEA2018091882554Skin · corrodedRT WING UPPER SKIN SURFACE CORROSION AT ROW OF FASTENERS AFT O/B OF PYLON CENTERLINE STA XORS 346. REMOVED CORROSION PER SRM 57-10-00.Sep 8, 2018 · N396FE · Doug MD1010F · Wing, Plate/SkinSDR FDEA2018091882552Skin · corrodedRT WING UPPER SKIN AT FASTENERS SURFACE CORROSION STA XORS 360. REMOVED CORROSION PER SRM 57-10-00.Sep 8, 2018 · N396FE · Doug MD1010F · Wing, Plate/SkinSDR FDEA2018091872557Seat Track · wornMAIN DECK SEAT TRACK STA 635 RT X = -8.50 LBL WORN BEYOND LIMITS. REPAIRED SEAT-TRACK SPLICE PER SRM 53-70-00 FIG 1 VOL I.Sep 7, 2018 · N396FE · Doug MD1010F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA2018091872553Seat Track · wornMAIN DECK SEAT TRACK STA 755 LT X = 8.50 LBL WORN BEYOND LIMITS. REMOVED AND REPLACED SEAT TRACK PER SRM 53-70-00 VOL I FROM STA 725-780.Sep 7, 2018 · N396FE · Doug MD1010F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201712193413Solenoid · corrodedL1 DOOR WILL ONLY OPEN 12 INCHES. DOOR CLOSED AND LOCKED. CND PROBLEM OPS CHECKED NORMAL SEVERAL TIMES, BUT DID NOTICE THE OPEN CLOSE SOLENOID WAS RUSTY, POSSIBLY INTERMITTENTLY CAUSING THE PROBLEM. REMOVED AND REPLACED OPEN - CLOSE LOCK SOLENOID.Dec 19, 2017 · N396FE · Doug MD1010F · Passenger/Crew DoorsSDR FDEA201712093352Switch · failedPDIS 396 52-10 5671 09DEC17 MEM OPEN U LOGPAGES:2767437 POST FLIGHT, UNABLE TO OPEN L1 DOOR. INDICATES DISARMED. REMOVED AND REPLACED L1 INTERIOR DOOR SWITCH S1-1205 PER MD10 WDM 52-10-01 AND SWPM CHAP 20. Dec 9, 2017 · N396FE · Doug MD1010F · Door Warning SystemSDR FDEA201705231472Coalescer Bag · odorSMOKE IN COCKPIT ON ARRIVAL AT FL 300. WHITE ACRID SMOKE DISSAPATED WITHIN 3-5 MINUTES. AIR TEMP KNOBS WERE TURNED DOWN AND NR 2 PACK TURNED OFF. NO ALERTS, BELLS, LIGHTS, OR WARNINGS OF ANY KIND. REMOVED AND REPLACED THE WATER SEPARATOR CONICAL COALESCERMay 23, 2017 · N396FE · Doug MD1010F · Humidity Control SystemSDR FDEA201701100113Unknown · malfunctionedON PREFLIGHT- SELECTING EMERGENCY POWER TO "ARM"- NO "ON" LIGHT. PERFORMED EPCU RTS IAW AMM 24-08-01-5, NO DEFECTS NOTED. PERFORMED ELECTRICAL EMERGENCY POWER SYSTEMS TEST IAW AMM 24-00-00-5, NO DEFECTS NOTED. AIRCRAFT OK FOR SERVICE.Jan 10, 2017 · N396FE · Doug MD1010F · AC Generation SystemSDR FDEA201609103174Floorbeam · corrodedFWD CARGO BS 979, BS 979 LBL 18 FLOORBEAM CORRODED. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED A REPAIR IAW SRM 53-60-01 FIG.3 SHEET 1.Sep 10, 2016 · N396FE · Doug MD1010F · Fuselage Main, Floor BeamSDR FDEA201609093175Floorbeam · corrodedFWD CARGO BS 979, RBL 16 FLOORBEAM HAS CORROSION 1.5 BY 3 INCHES. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR IAW SRM 53-60-01 FIG.3 SHEET 1.Sep 9, 2016 · N396FE · Doug MD1010F · Fuselage Main, Floor BeamSDR FDEA201609083148Doubler · crackedACM BAY 1, BS 594 APPROX LONGERON 33L IS CRACKED ON THE OUTER SKIN DOUBLER. REPAIRED THE DOUBLER IAW EA 8-5330-T0328088.Sep 8, 2016 · N396FE · Doug MD1010F · Fuselage Main, Plate/SkinSDR FDEA201609043117Cowling · crackedNR 2 ENGINE RT FAN COWL FORWARD LANDING, A/C SIDE, CRACKED AT LOWER SECTION, MARKED DOT 9, 2016-09-04. REPAIRED THE NR 2 ENGINE RT FAN COWL, FWD LANDING, A/C SIDE, IN REF TO SRM 54-10-00, FIG 20, SHEETS 1 THRU 5, VOL 1.Sep 4, 2016 · N396FE · Doug MD1010F · Engine Cowling SystemSDR FDEA201609033110Tee Fitting · crackedLT SIDE STA 595 T-CHORD AT LONGERON 39L HAS APPROXIMATELY 2" CRACK ON VERTICAL LEG, 2016-09-03 SECTION OF TEE CHORD WAS R & R AT STA 595 BETWEEN LONGERON 39L & 43L IN REF TO EA 8-5310-T0327401.Sep 3, 2016 · N396FE · Doug MD1010F · Fuselage Miscellaneous StructureSDR FDEA201609033108Skin · dentedDURING OVERSPEED INSPECTION, FOUND RT INBD DETACHABLE ELEVATOR UPPER SURFACE HAS SEVERAL DENTS. REPAIRED DENTS AREAS ON RT INBD DETACHABLE ELEVATOR UPPER SURFACE REF SRM 55-00-01, VOL 1.Sep 3, 2016 · N396FE · Doug MD1010F · Elevator, Plate/SkinSDR FDEA201608313097Floor Support · corrodedAFT CARGO COMPARTMENT: STA 1902-1967 CEILING, CENTERLINE SEAT TRACK UNDERSIDE HAS EXFOLIATION CORROSION AROUND SEVERAL NUTPLATES. AREAS MARKED, 2016-08-31. R & R FLOOR SUPPORT DUE TO CORROSION OUT OF LIMITS, PN: WSP0711-543 IAW SR DWG 10510131, INSTALLED FASAug 31, 2016 · N396FE · Doug MD1010F · Fuselage Miscellaneous StructureSDR FDEA201608313095Floor Support · corrodedAFT FUSE, WASTE TANK COMPARTMENT STA 1967-1980 CENTERLINE SEAT TRACK UNDERSIDE HAS EXFOLIATION CORROSION AROUND SEVERAL NUTPLATES. AREAS MARKED, 2016-08-31. R & R CENTERLINE FLOOR SUPPORT BECAUSE OF CORROSION OUT OF LIMITS, PN: WSP0711-555 IAW SR DWG 1051013Aug 31, 2016 · N396FE · Doug MD1010F · Fuselage Miscellaneous StructureSDR FDEA201608303082Floor Support · corrodedBS 374-395 75 RBL 107 FLOOR SUPPORT SHOWS LIGHT SURFACE CORROSION. REMOVED AND REPLACED THE FLOOR SUPPORT IAW DRAWING ABA7341 AND SRM 51-31-01 FIG 2 VOL 2.Aug 30, 2016 · N396FE · Doug MD1010F · Fuselage Miscellaneous StructureSDR FDEA201608283065Tee Fitting · crackedBS 595 BULKHEAD TEE CAP VERTICAL LEG AT LONGERON 43L HAS A 1.0 IN. CRACK. DAMAGED SECTION OF TEE CAP ON LT SIDE, STA 595 AT LONGERON 43L REPAIRED IAW EA 8-5310-T0327401 AND SRM 53-40-00, FIG 25, SHEET 1. SECTION OF TEE CHORD WAS R & R AT STA 595 BETWEEN LONGAug 28, 2016 · N396FE · Doug MD1010F · Fuselage Main, BulkheadSDR FDEA201608283064Bulkhead · crackedBS 595 PRESSURE BULKHEAD WEB AT LONGERON 43L HAS CRACK INDICATIONS. REPAIRED PRESSURE BULKHEAD WEB, 3 EA FASTENER HOLES IAW SRM 53-40-00, FIG 25, SHEET 2 AND SRM 51-39-01, VOL 1.Aug 28, 2016 · N396FE · Doug MD1010F · Fuselage Main, BulkheadSDR FDEA201608283062Bracket · crackedFWD CARGO COMPARTMENT TEE BRACKET HAS A CRACK. LT SIDE AT BS 595 BULKHEAD BETWEEN LONGERONS 44-45L. R & R TEE BRACKET, LT SIDE AT THE 595 BULKHEAD BETWEEN LONGERON 44L AND 45L, PN: NCA6044-187 IN REF TO DWG NCA6044.Aug 28, 2016 · N396FE · Doug MD1010F · Fuselage Miscellaneous StructureSDR FDEA201608283061Longeron · crackedNOSE GEAR WW .75 INCH CRACK LOCATED JUST BELOW THE LT TRUNNION AND ABOVE THE LT STRUT DOOR. CRACK WAS PREVIOUSLY STOP DRILLED BUT APPEARS NO REPAIR HAS BEEN ADDED. REPAIRED CRACK REF EA 8-5310-T0327817.Aug 28, 2016 · N396FE · Doug MD1010F · Fuselage Main, Longeron/StringerSDR FDEA201608283060Tee Fitting · crackedRIGHT STA 595 T-CHORD LONGERON 39R HAS APPROXIMATELY 2" CRACK IN VERTICAL FLANGE. SECTION OF TEE CHORD WAS R & R AT STA 595 BULKHEAD BETWEEN LONGERONS 39R AND 43R IN REF TO EA 8-5310-T0327400 AND SRM 53-40-00, FIG 25, SHEET 1 THRU 3.Aug 28, 2016 · N396FE · Doug MD1010F · Fuselage Main, BulkheadSDR FDEA201608283059Tee Fitting · crackedBS 595 BULKHEAD TEE CAP VERTICAL LEG AT LONGERON 43R HAS A ONE INCH CRACK. SECTION OF TEE CHORD R & R AT STA 595 BETWEEN LONGERONS 39R AND 43R IN REF TO EA 8-5310-T0327400 AND SRM 53-40-00, FIG 25, SHEET 1.Aug 28, 2016 · N396FE · Doug MD1010F · Fuselage Main, BulkheadSDR FDEA201608273051Seat Track · corrodedAFT FUSELAGE WASTE BAY CEILING BS 1980 LBL 24 SEAT TRACK UNDERSIDE NUT CLIP HOLE CORRODED. REMOVED AND REPLACED SEAT TRACK IAW DWG SP10510131.Aug 27, 2016 · N396FE · Doug MD1010F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201608263038Tee Fitting · crackedBS 595 RT SIDE TEE CAP ON THE UPPER FASTENER ROW OF THE VERTICAL LEG AT LONGERON 37 HAS CRACK INDICATIONS. REAMED IAW SRM 51-33-01, VOL 2 COMPLIED WITH HFEC INSPECTION IAW NDTSPM, TP-MDC-93KO393, NO DEFECTS NOTED. INSTALLED A BUSHING IAW SRM 51-39-01 VOL 2.Aug 26, 2016 · N396FE · Doug MD1010F · Fuselage Miscellaneous StructureSDR FDEA201608263028Tee Fitting · crackedSTA 595 RT SIDE T-CAP ON THE FORWARD FASTENER ROW OF THE HORIZONTAL LEG AT LONGERON 38 HOLE HAS CRACK INDICATIONS. REAMED HOLE LABELED-A REAMED HOLE A TO .277 ON THE FORWARD ROW OF HORIZONTAL LEG AT LONGERON 37R REF: SRM 51-39-01, FIG 1, VOL 2. INSTALLED REPAug 26, 2016 · N396FE · Doug MD1010F · Fuselage Miscellaneous StructureSDR FDEA201608263010Tee Fitting · crackedBS 595 RT SIDE T-CAP ON THE AFT FASTENER ROW OF THE HORIZONTAL LEG BETWEEN LONGERONS 38-39R HAVE CRACK INDICATIONS. REAMED THE HOLES ON THE AFT ROW OF HORIZONTAL LEG IAW SPM 51-39-01, VOL 2 AND DPS 1.33. INSTALLED BUSHINGS.Aug 26, 2016 · N396FE · Doug MD1010F · Fuselage Main, Attach FittingsSDR FDEA201608263009Tee Fitting · crackedSTA 595, RT SIDE T-CAP ON THE AFT FASTENER ROW OF THE HORIZONTAL LEG BETWEEN LONGERON 38-39, 3 HOLES HAVE CRACK INDICATIONS. REAMED 3 HOLES ON THE AFT ROW OF HORIZONTAL LEG BETWEEN LONGERON 38 & 39. HOLES LABLED B, C & D REAMED TO .277, REF SPM: 51-39-01, VAug 26, 2016 · N396FE · Doug MD1010F · Fuselage Miscellaneous StructureSDR FDEA201608242969Skin · dentedRIGHT WING INBD T/E FLAP UPPER SURFACE MID-SPAN AREA, SHOWING ONE DENT SPOT. REPAIRED IAW SRM 57-10-00 FIG 85 SHEET 2.Aug 24, 2016 · N396FE · Doug MD1010F · Wing, Control SurfacesSDR FDEA201606071870Coalescer Bag · dirtyPASSING 11,000 FT, DURING DESCENT AT 250 KTS AT 2, 45 AFTER TACKOFF, EXPERIENCED FUME EVENT. ALL 3 BLEEDS ON, ISOL VALVES CLOSED AND PACKS 1 AND 3 ON. FUME EVENT ODOR WAS VERY STRONG, HUMID MUSTY SMELL. R & R NR 1 AND NR 3 COALESCER BAGS IAW AMM 21-54-03-2.Jun 7, 2016 · N396FE · Doug MD1010F · Humidity Control SystemSDR FDEA201604201314Rivet · shearedON POST FLIGHT WALK AROUND FOUND NR 1 ENG CONICAL NOZZLE PLUG, AFT SECTION, MISSING. FOUND ALL RIVETS SHEARED AROUND AFT SECTION OF CONICAL NOZZLE PLUG. SEE ATTACHED PHOTOS. ONE REPLACED EXHAUST PLUG.Apr 20, 2016 · N396FE · Doug MD1010F · Engine Collector/Tailpipe/NozzleSDR FDEA201604071155Connector · defectiveAFTER TAKEOFF, RECEIVED LEVEL 2, BRAKE OVERHEAT, MAX TEMP 692. LEVELED OFF AT 17,000 SLOWED, LOWERED GEAR FOR 10 MINUTES. RAISED GEAR, TEMP STARTED TO RISE. DIVERTED & LOWERED GEAR AT FL 200, LANDED FLAPS 50. R & R NR 6 BRAKE TEMP CONNECTOR IAW AMM 20-30-0Apr 7, 2016 · N396FE · Doug MD1010F · Landing Gear Brake SystemSDR FDEA201511123571Warning System · false activationON DESCENT, DUE TO RNWY CHANGE, EXTENDED LG AT 235 KTS, ONCE ON DESCENT RETRACTED GEAR AT 220 KTS, BOTH MAIN GEAR INDICATED UNSAFE, UPON RETRACTION EXTENDED GEAR & GOT 3 GREEN. JACKED ACFT IAW AMM 07-11-00-2. PERFORMED MLG PROXIMITY SENSORS & TARGET TEST IAW Nov 12, 2015 · N396FE · Doug MD1010F · Landing Gear Position and Warning
Back to N396FE, cancelled Mar 2, 2024