# Service difficulty reports: N396FE, cancelled Mar 2, 2024

A list on [N396FE, cancelled Mar 2, 2024](https://openairdocs.org/deregistered/N396FE-2024-03-02.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 3 · 124 reports

- [SDR FDEA2020043090818](https://openairdocs.org/sdr/FDEA2020043090818.md): Sensor · failed · Apr 29, 2020 · N396FE · Doug MD1010F · Leading Edge Slat Position Indicating System
  > PDIS 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
- [SDR FDEA2019110752873](https://openairdocs.org/sdr/FDEA2019110752873.md): Sensor · failed · Nov 5, 2019 · N396FE · Doug MD1010F · Leading Edge Slat Position Indicating System
  > UPON 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.
- [SDR FDEA2019093022367](https://openairdocs.org/sdr/FDEA2019093022367.md): Slide · inoperative · Sep 28, 2019 · N396FE · Doug MD1010F · Escape Slide
  > MAIN 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.
- [SDR FDEA201909042116](https://openairdocs.org/sdr/FDEA201909042116.md): Skin · cracked · Sep 4, 2019 · N396FE · Doug MD1010F · Wing, Plate/Skin
  > 2" 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 INST
- [SDR FDEA201903160647](https://openairdocs.org/sdr/FDEA201903160647.md): Skin · cracked · Mar 16, 2019 · N396FE · Doug MD1010F · Trailing Edge Flaps
  > RT WING OB FLAP UPPER SUFACE SKIN CRACKED (EST 3" FRONT TO BACK) REPAIRED USING SRM 57-10-00 FIG 85 AS A REFERENCE.
- [SDR FDEA2018102653004](https://openairdocs.org/sdr/FDEA2018102653004.md): Truss · cracked · Oct 25, 2018 · N396FE · Doug MD1010F · Nacelle/Pylon Miscellaneous Structure
  > NR 3 PYLON TRUSS FITTING INBOARD TRUSS HALF OUTBOARD EDGE HAS A CRACK INDICATION. REPAIRED PER E.A. 8-5450-T0342532. MAJOR REPAIR.
- [SDR FDEA201810232981](https://openairdocs.org/sdr/FDEA201810232981.md): Longeron · cracked · Oct 23, 2018 · N396FE · Doug MD1010F · Fuselage Main, Longeron/Stringer
  > NOSE 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.
- [SDR FDEA2018100542777](https://openairdocs.org/sdr/FDEA2018100542777.md): Bracket · corroded · Oct 4, 2018 · N396FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > AFT 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.
- [SDR FDEA2018100532775](https://openairdocs.org/sdr/FDEA2018100532775.md): Longeron · cracked · Oct 3, 2018 · N396FE · Doug MD1010F · Fuselage Main, Longeron/Stringer
  > NOSE 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 VOLII
- [SDR FDEA201810012758](https://openairdocs.org/sdr/FDEA201810012758.md): Skin · delaminated · Oct 1, 2018 · N396FE · Doug MD1010F · Spoilers
  > LT 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.
- [SDR FDEA201809272716](https://openairdocs.org/sdr/FDEA201809272716.md): Shear Tie · cracked · Sep 27, 2018 · N396FE · Doug MD1010F · Fuselage Internal Mounting Structure
  > FWD 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.
- [SDR FDEA201809252709](https://openairdocs.org/sdr/FDEA201809252709.md): Skin · corroded · Sep 25, 2018 · N396FE · Doug MD1010F · Wing, Plate/Skin
  > R/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-T0342487
- [SDR FDEA201809192613](https://openairdocs.org/sdr/FDEA201809192613.md): Skin · delaminated · Sep 19, 2018 · N396FE · Doug MD1010F · Spoilers
  > LT 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.
- [SDR FDEA2018091862556](https://openairdocs.org/sdr/FDEA2018091862556.md): Seat Track · worn · Sep 16, 2018 · N396FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN 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.
- [SDR FDEA2018092542666](https://openairdocs.org/sdr/FDEA2018092542666.md): Skin · unknown · Sep 14, 2018 · N396FE · Doug MD1010F · Elevator, Plate/Skin
  > REPAIR 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 C
- [SDR FDEA201809102631](https://openairdocs.org/sdr/FDEA201809102631.md): Skin · cracked · Sep 10, 2018 · N396FE · Doug MD1010F · Wing, Plate/Skin
  > RT 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.
- [SDR FDEA2018091882551](https://openairdocs.org/sdr/FDEA2018091882551.md): Skin · corroded · Sep 8, 2018 · N396FE · Doug MD1010F · Wing, Plate/Skin
  > RT WING UPPER SKIN CORROSION AT FASTENER STA XORS 400 20 INCH FWD OF AFT SPAR. REMOVED CORROSION PER SRM 57-10-00.
- [SDR FDEA2018091882554](https://openairdocs.org/sdr/FDEA2018091882554.md): Skin · corroded · Sep 8, 2018 · N396FE · Doug MD1010F · Wing, Plate/Skin
  > RT 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.
- [SDR FDEA2018091882552](https://openairdocs.org/sdr/FDEA2018091882552.md): Skin · corroded · Sep 8, 2018 · N396FE · Doug MD1010F · Wing, Plate/Skin
  > RT WING UPPER SKIN AT FASTENERS SURFACE CORROSION STA XORS 360. REMOVED CORROSION PER SRM 57-10-00.
- [SDR FDEA2018091872557](https://openairdocs.org/sdr/FDEA2018091872557.md): Seat Track · worn · Sep 7, 2018 · N396FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN 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.
- [SDR FDEA2018091872553](https://openairdocs.org/sdr/FDEA2018091872553.md): Seat Track · worn · Sep 7, 2018 · N396FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN 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.
- [SDR FDEA201712193413](https://openairdocs.org/sdr/FDEA201712193413.md): Solenoid · corroded · Dec 19, 2017 · N396FE · Doug MD1010F · Passenger/Crew Doors
  > L1 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.
- [SDR FDEA201712093352](https://openairdocs.org/sdr/FDEA201712093352.md): Switch · failed · Dec 9, 2017 · N396FE · Doug MD1010F · Door Warning System
  > PDIS 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.
- [SDR FDEA201705231472](https://openairdocs.org/sdr/FDEA201705231472.md): Coalescer Bag · odor · May 23, 2017 · N396FE · Doug MD1010F · Humidity Control System
  > SMOKE 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 COALESCER
- [SDR FDEA201701100113](https://openairdocs.org/sdr/FDEA201701100113.md): Unknown · malfunctioned · Jan 10, 2017 · N396FE · Doug MD1010F · AC Generation System
  > ON 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.
- [SDR FDEA201609103174](https://openairdocs.org/sdr/FDEA201609103174.md): Floorbeam · corroded · Sep 10, 2016 · N396FE · Doug MD1010F · Fuselage Main, Floor Beam
  > FWD 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.
- [SDR FDEA201609093175](https://openairdocs.org/sdr/FDEA201609093175.md): Floorbeam · corroded · Sep 9, 2016 · N396FE · Doug MD1010F · Fuselage Main, Floor Beam
  > FWD 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.
- [SDR FDEA201609083148](https://openairdocs.org/sdr/FDEA201609083148.md): Doubler · cracked · Sep 8, 2016 · N396FE · Doug MD1010F · Fuselage Main, Plate/Skin
  > ACM BAY 1, BS 594 APPROX LONGERON 33L IS CRACKED ON THE OUTER SKIN DOUBLER. REPAIRED THE DOUBLER IAW EA 8-5330-T0328088.
- [SDR FDEA201609043117](https://openairdocs.org/sdr/FDEA201609043117.md): Cowling · cracked · Sep 4, 2016 · N396FE · Doug MD1010F · Engine Cowling System
  > NR 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.
- [SDR FDEA201609033110](https://openairdocs.org/sdr/FDEA201609033110.md): Tee Fitting · cracked · Sep 3, 2016 · N396FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > LT 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.
- [SDR FDEA201609033108](https://openairdocs.org/sdr/FDEA201609033108.md): Skin · dented · Sep 3, 2016 · N396FE · Doug MD1010F · Elevator, Plate/Skin
  > DURING 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.
- [SDR FDEA201608313097](https://openairdocs.org/sdr/FDEA201608313097.md): Floor Support · corroded · Aug 31, 2016 · N396FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > AFT 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 FAS
- [SDR FDEA201608313095](https://openairdocs.org/sdr/FDEA201608313095.md): Floor Support · corroded · Aug 31, 2016 · N396FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > AFT 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 1051013
- [SDR FDEA201608303082](https://openairdocs.org/sdr/FDEA201608303082.md): Floor Support · corroded · Aug 30, 2016 · N396FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > BS 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.
- [SDR FDEA201608283065](https://openairdocs.org/sdr/FDEA201608283065.md): Tee Fitting · cracked · Aug 28, 2016 · N396FE · Doug MD1010F · Fuselage Main, Bulkhead
  > BS 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 LONG
- [SDR FDEA201608283064](https://openairdocs.org/sdr/FDEA201608283064.md): Bulkhead · cracked · Aug 28, 2016 · N396FE · Doug MD1010F · Fuselage Main, Bulkhead
  > BS 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.
- [SDR FDEA201608283062](https://openairdocs.org/sdr/FDEA201608283062.md): Bracket · cracked · Aug 28, 2016 · N396FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > FWD 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.
- [SDR FDEA201608283061](https://openairdocs.org/sdr/FDEA201608283061.md): Longeron · cracked · Aug 28, 2016 · N396FE · Doug MD1010F · Fuselage Main, Longeron/Stringer
  > NOSE 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.
- [SDR FDEA201608283060](https://openairdocs.org/sdr/FDEA201608283060.md): Tee Fitting · cracked · Aug 28, 2016 · N396FE · Doug MD1010F · Fuselage Main, Bulkhead
  > RIGHT 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.
- [SDR FDEA201608283059](https://openairdocs.org/sdr/FDEA201608283059.md): Tee Fitting · cracked · Aug 28, 2016 · N396FE · Doug MD1010F · Fuselage Main, Bulkhead
  > BS 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.
- [SDR FDEA201608273051](https://openairdocs.org/sdr/FDEA201608273051.md): Seat Track · corroded · Aug 27, 2016 · N396FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > AFT FUSELAGE WASTE BAY CEILING BS 1980 LBL 24 SEAT TRACK UNDERSIDE NUT CLIP HOLE CORRODED. REMOVED AND REPLACED SEAT TRACK IAW DWG SP10510131.
- [SDR FDEA201608263038](https://openairdocs.org/sdr/FDEA201608263038.md): Tee Fitting · cracked · Aug 26, 2016 · N396FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > BS 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.
- [SDR FDEA201608263028](https://openairdocs.org/sdr/FDEA201608263028.md): Tee Fitting · cracked · Aug 26, 2016 · N396FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > STA 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 REP
- [SDR FDEA201608263010](https://openairdocs.org/sdr/FDEA201608263010.md): Tee Fitting · cracked · Aug 26, 2016 · N396FE · Doug MD1010F · Fuselage Main, Attach Fittings
  > BS 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.
- [SDR FDEA201608263009](https://openairdocs.org/sdr/FDEA201608263009.md): Tee Fitting · cracked · Aug 26, 2016 · N396FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > STA 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, V
- [SDR FDEA201608242969](https://openairdocs.org/sdr/FDEA201608242969.md): Skin · dented · Aug 24, 2016 · N396FE · Doug MD1010F · Wing, Control Surfaces
  > RIGHT WING INBD T/E FLAP UPPER SURFACE MID-SPAN AREA, SHOWING ONE DENT SPOT. REPAIRED IAW SRM 57-10-00 FIG 85 SHEET 2.
- [SDR FDEA201606071870](https://openairdocs.org/sdr/FDEA201606071870.md): Coalescer Bag · dirty · Jun 7, 2016 · N396FE · Doug MD1010F · Humidity Control System
  > PASSING 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.
- [SDR FDEA201604201314](https://openairdocs.org/sdr/FDEA201604201314.md): Rivet · sheared · Apr 20, 2016 · N396FE · Doug MD1010F · Engine Collector/Tailpipe/Nozzle
  > ON 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.
- [SDR FDEA201604071155](https://openairdocs.org/sdr/FDEA201604071155.md): Connector · defective · Apr 7, 2016 · N396FE · Doug MD1010F · Landing Gear Brake System
  > AFTER 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 20-30-0
- [SDR FDEA201511123571](https://openairdocs.org/sdr/FDEA201511123571.md): Warning System · false activation · Nov 12, 2015 · N396FE · Doug MD1010F · Landing Gear Position and Warning
  > ON 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

Next page: https://openairdocs.org/deregistered/N396FE-2024-03-02/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/deregistered/N396FE-2024-03-02/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.