# Service difficulty reports: N390FE, cancelled Mar 2, 2024

A list on [N390FE, cancelled Mar 2, 2024](https://openairdocs.org/deregistered/N390FE-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 · 143 reports

- [SDR FDEA202001100107](https://openairdocs.org/sdr/FDEA202001100107.md): Unknown · malfunctioned · Jan 10, 2020 · N390FE · Doug MD1010F · Emergency Lighting
  > EMERGENCY LIGHT TEST FAIL ON POST FLIGHT. PERFORMED ADJUSTMENT/TEST OF EMERGENCY LIGHTING. EMERGENCY LIGHTING PASSED MULTIPLE TIMES(3) WITH NO FAULTS. REF AMM 33-50-00-5. OK FOR SERVICE.
- [SDR FDEA2019120433162](https://openairdocs.org/sdr/FDEA2019120433162.md): Warning Message · false activation · Dec 3, 2019 · N390FE · Doug MD1010F · Hydraulic System, Main
  > PDIS 390 29-02 9785 03DEC19 DEN FACT U LOGPAGES:3149673 AT FL 340, RECEIVED LEVEL 1 "HYD 3 ELEV OFF". SWITCHED FROM AUTOPILOT 2 TO AUTOPILOT 1. RECEIVED SUBSEQUENT "HYD 3 QTY LO", ACCOMPANIED BY " HYD 3 FAIL". FACT 03DEC19 04:39 DEN U SER
- [SDR FDEA201906181344](https://openairdocs.org/sdr/FDEA201906181344.md): Proximity Sensor · out of alignment · Jun 18, 2019 · N390FE · Doug MD1010F · Leading Edge Slat Control System
  > ON FINAL APP. WITH FLAPS 22*, EXTENDED GEAR AND GOT SLAT DISAG ALERT. PREFORMED GO-AROUND AND RETRACTED GEAR & FLAPS ONLY TO 15*. WENT TO QRH FOR SLAT DISAG. DID FLAP 22* LANDING AND LEFT FLAPS & SLATS IN 22* POSITION ALL THE WAY TO SHUTDOWN. ALERT DID GO
- [SDR FDEA201809252679](https://openairdocs.org/sdr/FDEA201809252679.md): Pseu · malfunctioned · Sep 25, 2018 · N390FE · Doug MD1010F · Leading Edge Slat Control System
  > PDIS 390 27-80 8566 25SEP18 MEM OPEN U "SLAT DISAG" LEVEL 2 ON APPROACH WHEN SELECTING FLAPS 35. NO ROLL NOTED. COMPLIED W/QRH LANDED WITH FLAPS 22/EXT. FACT 25SEP18 18:37 MEM REMOVED
- [SDR FDEA20180829005](https://openairdocs.org/sdr/FDEA20180829005.md): Shear Tie · corroded · Aug 7, 2018 · N390FE · Doug MD1010F · Fuselage Internal Mounting Structure
  > AFT CARGO BAY, BS 1987, JUST AFT OF THE SERVICE PANEL BETWEEN LONGERONS 51L & 51R CORRODED ON THE AFT SIDE OF FRAME ANGLE. REPAIRED THE SHEAR TIE IAW EA 8-5310-T0341752.
- [SDR FDEA2018080311881](https://openairdocs.org/sdr/FDEA2018080311881.md): Tee Fitting · corroded · Aug 1, 2018 · N390FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > CENTER WHEEL WELL AT STA 1521, RT SIDE CORROSION FOUND ON THE UPPER TEE ANGLE. REPAIRED "T" ANGLE PER EA 8-5310-T0341578.
- [SDR FDEA201807301857](https://openairdocs.org/sdr/FDEA201807301857.md): Floor Support · corroded · Jul 30, 2018 · N390FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > FWD CARGO COMPT DOOR SILL FWD FLOORBOARD SUPPORT CORRODED UNDER NUTPLATE AT STA 876. CLEANED CORROSION PER SRM 51-21-01 VOL 2.
- [SDR FDEA2018081492012](https://openairdocs.org/sdr/FDEA2018081492012.md): Floor Panel · corroded · Jul 29, 2018 · N390FE · Doug MD1010F · Fuselage Floor Panel
  > MAIN DECK, BS 495 LEFT SIDE FLOOR PANEL UNDER RCB HAD EXTENSIVE EXFOLIATION CORROSON ON THE SURFACE. FABRICATED A NEW FLOOR PANEL IAW DWG WSP0791-1.
- [SDR FDEA2018080751928](https://openairdocs.org/sdr/FDEA2018080751928.md): Shear Tie · corroded · Jul 25, 2018 · N390FE · Doug MD1010F · Fuselage Internal Mounting Structure
  > AFT CARGO BAY BILGE SHEAR TIE WAS FOUND CORRODED UNDER THE FRAME BS 1967, LONGERON 50R. REMOVED AND REPLACED THE SHEAR TIE IAW DWG AGA0021-65.
- [SDR FDEA2018073021820](https://openairdocs.org/sdr/FDEA2018073021820.md): Web · cracked · Jul 22, 2018 · N390FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > CENTER WHEEL WELL, HAS A CRACK ON RT UPPER SIDE WEB AT APROX STA 1501. INSTALLED REPAIR DOUBLER PER EA 8-5310-T0341389.
- [SDR FDEA2018080711927](https://openairdocs.org/sdr/FDEA2018080711927.md): Floor Support · cracked · Jul 21, 2018 · N390FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT BRACKET WAS CRACKED, BS 1501, LONGERON 50R. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-31-01, VOL 2.
- [SDR FDEA201803210746](https://openairdocs.org/sdr/FDEA201803210746.md): Fitting · corroded · Mar 21, 2018 · N390FE · Doug MD1010F · Wing, Landing Gear Attach Fittings
  > RIGHT MLG TRUNNION FWD FITTING FWD BEARING INNER DIAMETER SURFACE HAS PITTED CORROSION. COMPLIED WITH EA 8-5740-T0338917 WINGS - ATTACH FITTINGS RT MLG FWD TRUNNION FITTING HOLE CORRODED STEPS 1-8 DATED MAR 20, 2018 MAJOR REPAIR.
- [SDR FDEA201701260259](https://openairdocs.org/sdr/FDEA201701260259.md): Switch · malfunctioned · Jan 26, 2017 · N390FE · Doug MD1010F · Drag Control System
  > UNCOMMANDED GROUND SPOILER DEPLOYMENT DURING TAKEOFF. CHECKED BOTH FCC 1&2 FOR CURRENT OR PREVIOUS FAULTS, NONE FOUND. PERFORMED AGS RTS IN BOTH FCC'S, CHECKED GOOD. INSPECTED AGS ARM SWITCH S1-845 IT APPEARS TO MOVE FREELY AND HAS GOOD AUDIBLE CLICKS. RAN
- [SDR FDEA201608052821](https://openairdocs.org/sdr/FDEA201608052821.md): Bulkhead · cracked · Aug 5, 2016 · N390FE · Doug MD1010F · Fuselage Main, Bulkhead
  > RIGHT STA 595 BULKHEAD WEB LOWER FASTENER HOLE AT LONGERON 43R HAS A CRACK INDICATION. OPENED CRACK HOLE ON THE LOWER WEB TO.247 FOR NDT. PERFORMED OPEN HOLE HFEC. NO INDICATION FOUND IAW NDTSPM 93K0393. EA 8-5310-T0326599 FOR MORE INFORMATION.
- [SDR FDEA201608052820](https://openairdocs.org/sdr/FDEA201608052820.md): Skin · cracked · Aug 5, 2016 · N390FE · Doug MD1010F · Fuselage Main, Plate/Skin
  > RIGHT STA 595 FUSELAGE SKIN COMMON TO THE TEE CAP AT LONGERON 38R HAVE 2 EA. FASTENER HOLES WITH CRACK INDICATIONS. SAME HOLE LOCATIONS AS TEE CAP CRACK, OPENED FWD HOLE TO.247 AND AFT HOLE.262 AT LONGERON 38R ON THE FUSELAGE SKIN FOR NDT. PEFORMED OPEN H
- [SDR FDEA201608032791](https://openairdocs.org/sdr/FDEA201608032791.md): Frame · corroded · Aug 3, 2016 · N390FE · Doug MD1010F · Fuselage Main, Frame
  > FWD AVIONICS AREA THROUGH OPENING IN NLG WHEEL WELL UNDER SYSTEM NR 1 RAM AIR DUCT, FRAME AT BS 449, LBL 30 HAS DAMAGE AND SIGNS OF CORROSION. REMOVED LIGHT CORROSION IAW SRM 51-21-01VOL 2.
- [SDR FDEA201607302682](https://openairdocs.org/sdr/FDEA201607302682.md): Bulkhead · corroded · Jul 30, 2016 · N390FE · Doug MD1010F · Fuselage Main, Bulkhead
  > CENTER CARGO COMPARTMENT, FWD BULKHEAD LOWER WEB HAS EXFOLIATION CORROSION AT 42R, STA 1521, FOUND UNDER ROLLER TRAY. MARKED, 2016-07-30. R & R SMALL SECTION OF ANGLE WITH PN S2929469, S2933839 & S4931827 IN REF TO SRM 53-00-01, FIG 9, VOL 1.
- [SDR FDEA201607292659](https://openairdocs.org/sdr/FDEA201607292659.md): Skin · cracked · Jul 29, 2016 · N390FE · Doug MD1010F · Fuselage Main, Plate/Skin
  > NR 3 AIR CONDITIONING DOOR AFT UPPER CUT OUT CORNER HAS A.100 INCH CRACK. REPAIRED IAW SRM 53-50-00 FIG 3A VOL I.
- [SDR FDEA201607212588](https://openairdocs.org/sdr/FDEA201607212588.md): Angle · corroded · Jul 21, 2016 · N390FE · Doug MD1010F · Fuselage Main, Bulkhead
  > CENTER CARGO COMPARTMENT, AFT BULKHEAD LOWER WEB CORRODED. FOUND AT BS 1781, UNDER THE AFT END OF THE ENTRY WAY OMNI ROLLER TRAY. REMOVED AND REPLACED CORRODED ANGULAR SUPPORT BRACKET IAW SRM VOLUME 2 51-31-01,V2.
- [SDR FDEA201607132437](https://openairdocs.org/sdr/FDEA201607132437.md): Tee Fitting · cracked · Jul 13, 2016 · N390FE · Doug MD1010F · Fuselage Main, Bulkhead
  > RIGHT STA 595 BULKHEAD TEE CAP VERTICAL LEG HAS A 1.75" CRACK AT LONGERON 39R, MARKED.
- [SDR FDEA201607132436](https://openairdocs.org/sdr/FDEA201607132436.md): Tee Fitting · cracked · Jul 13, 2016 · N390FE · Doug MD1010F · Fuselage Main, Bulkhead
  > RIGHT STA 595, BULKHEAD TEE CAP VERTICAL LEG HAS A 1.75" CRACK AT LONGERON 39R, MARKED.
- [SDR FDEA201607132435](https://openairdocs.org/sdr/FDEA201607132435.md): Tee Fitting · cracked · Jul 13, 2016 · N390FE · Doug MD1010F · Fuselage Main, Bulkhead
  > RIGHT STA 595 BULKHEAD TEE CAP VERTICAL LEG HAS A 1.5" CRACK AT LONGERON 43R, MARKED.
- [SDR FDEA201607132434](https://openairdocs.org/sdr/FDEA201607132434.md): Tee Fitting · cracked · Jul 13, 2016 · N390FE · Doug MD1010F · Fuselage Main, Bulkhead
  > RT STA 595 BULKHEAD TEE CAP HAS A CRACK BETWEEN LONGERON 37R AND 38R ON THE VERTICAL AND FORWARD HORIZONTAL LEG EXTENDING THROUGH THE RADIUS, MARKED.
- [SDR FDEA201511013434](https://openairdocs.org/sdr/FDEA201511013434.md): Switch · malfunctioned · Nov 1, 2015 · N390FE · Doug MD1010F · Pneumatic Indicating System
  > ON CLIMB OUT, SELECT ENG & WING ANTI-ICE ON, AS SOON AS WING ANTI-ICE SELECTED, GOT AIR SYS 3 OFF WITH BLEED AIR 3 VLV & PACK 3 BEING TURNED OFF AUTOMATICALLY. R & R NR 3 SYS MANIFOLD FAILURE DETECTION SWITCH IAW AMM.
- [SDR FDEA201509202904](https://openairdocs.org/sdr/FDEA201509202904.md): Seat Track · damaged · Sep 20, 2015 · N390FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK LUG BROKEN, BETWEEN POS 2L & 3L LOCK ID IS Q758. REPAIRED DAMAGED SEAT TRACK IAW SRM 53-70-00 & SR 10-53-002. THIS IS A MAJOR REPAIR. REPLACED SEAT TRACK SEGMENT ONLY, PN 4929150-12000N. INSTALLED FLOORBOARDS & ROLLER SYS.
- [SDR FDEA201505131505](https://openairdocs.org/sdr/FDEA201505131505.md): Coalescer Bag · dirty · May 13, 2015 · N390FE · Doug MD1010F · Humidity Control System
  > IN CRUISE AT FLIGHT 350, AIR SYS SMELLS LIKE A GYM ROOM OR DIRTY SOCKS. PERFORMED REPLACEMENT OF PACK SYS 1, 2, & 3 CONICAL COALESCER BAGS. ODOR CLEARED UP & PACKS OPERATIONS CHECK GOOD. ACFT GOOD FOR SERVICE.
- [SDR FDEA201502010407](https://openairdocs.org/sdr/FDEA201502010407.md): Cable · frayed · Feb 1, 2015 · N390FE · Doug MD1010F · Passenger/Crew Doors
  > DURING SERVICE CHECK, FOUND L1 DOOR AFT UPPER DRIVE CABLE FRAYED. R & R L1 DOOR AFT UPPER DRIVE CABLE. RIG & OPS CHECKED OK.
- [SDR FDEA201409112615](https://openairdocs.org/sdr/FDEA201409112615.md): Dump Valve · failed · Sep 11, 2014 · N390FE · Doug MD1010F · Fuel Dump System
  > RIGHT WING DUMP VLV FAILED TO CLOSE AFTER DUMP TERMINATION. RIGHT FUEL DUMP VLV SYS WIRING CHECKED FROM RT FUEL DUMP VLV M1-89 TO FUEL SYS CONTROLLER. RT FUEL DUMP VLV TO FUEL SYS CONTROLLER, RT FUEL DUMP VLV TO 1, 2, 3 VIA CONTINUITY & INSULATION CHECKED NO
- [SDR FDEA201409092547](https://openairdocs.org/sdr/FDEA201409092547.md): Duct · cracked · Sep 9, 2014 · N390FE · Doug MD1010F · Engine Air Intake System
  > NR 2 NOSE COWL INLET DUCT, CRACKED THROUGHOUT CIRCUMFERENCE. R & R WITH NEW NOSE COWL ASSEMBLY IAW AMM 54-22-01-2.
- [SDR FDEA201409092545](https://openairdocs.org/sdr/FDEA201409092545.md): Skin · cracked · Sep 9, 2014 · N390FE · Doug MD1010F · Trailing Edge Flaps
  > LEFT OTBD FLAP UPPER SURFACE 2 CRACKS ON THE SKIN.120 TO.250 INCHES IN LENGTH APPROX XOF 560. REMOVED DAMAGE & INSTALLED DOUBLER IAW SRM 57-00-01 FIG 4 SHEET 2.
- [SDR FDEA201409082536](https://openairdocs.org/sdr/FDEA201409082536.md): Floorbeam · mechanic error · Sep 8, 2014 · N390FE · Doug MD1010F · Fuselage Main, Floor Beam
  > AFT CARGO COMPARTMENT STATION 1868 LT X=36.00 FLOOR LINE, FLOORBEAM HAS MULTIPLE HOLES WITH UNACCEPTABLE SPACING BETWEEN HOLES. FABRICATED & INSTALLED REPAIR ANGLE IAW SRM 53-00-01 FIG 9 SHT 7.
- [SDR FDEA201409082535](https://openairdocs.org/sdr/FDEA201409082535.md): Seat Track · damaged · Sep 8, 2014 · N390FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK STATION 1390 LT 75.5 SEAT TRACK IS DAMAGED. R & R DAMAGED SECTION OF SEAT TRACK IAW SRM 53-70-00 VOL 1.
- [SDR FDEA201409082534](https://openairdocs.org/sdr/FDEA201409082534.md): Seat Track · damaged · Sep 8, 2014 · N390FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK SEAT TRACK AT STATION 1381 LT 75.5 IS DAMAGED. R & R DAMAGED SECTION OF SEAT TRACK IAW SRM 53-70-00 VOL 1.
- [SDR FDEA201409012398](https://openairdocs.org/sdr/FDEA201409012398.md): Door · cracked · Sep 1, 2014 · N390FE · Doug MD1010F · Landing Gear Doors
  > LEFT MLG DOOR, CRACK EXISTS AT THE UPPER CTR HINGE PORTION OF THE DOOR. REMOVED DOOR AND REPLACED WITH NEW MLG DOOR IAW MM 32-14-01-2
- [SDR FDEA201311112747](https://openairdocs.org/sdr/FDEA201311112747.md): Bulkhead · cracked · Nov 11, 2013 · N390FE · Doug MD1010F · Fuselage Main, Bulkhead
  > TWO INCH CRACK LT MLG WW INBD BULKHEAD 30 INCHES FWD OF AFT BULKHEAD AND THREE INCHES DOWN FROM UPPER BULKHEAD. MARKED CRACK END HFEC. REPAIRED DAMAGED AREA, CRACK, REF SRM 53-00-01.
- [SDR FDEA201212154310](https://openairdocs.org/sdr/FDEA201212154310.md): O-Ring · failed · Dec 15, 2012 · N390FE · Doug MD1010F · Hydraulic System, Main
  > RECEIVED LEVEL 1 "HYD 3 ELEV OFF" ALERT. NR 3 SYS INDICATED 4.4 GALLONS AND OVER A 10 MIN PERIOD DECREASED TO 4.0, DIVERTED. DURING GEAR EXTENSION, NR 3 QTY DECREASED TO 1.7 GALLONS WITH "HYD 3 QTY LO". AFTER LT TURN OFF RUNWAY, MX TOW IN. FOUND O-RING TO
- [SDR FDEA201102220674](https://openairdocs.org/sdr/FDEA201102220674.md): Panel · corroded · Feb 22, 2011 · N390FE · Doug MD1010F · Wing Miscellaneous Structure
  > LT WHEEL WELL SLANT PANEL HAS SURFACE CORROSION ALONG THE LOWER EDGE IN SEVERAL AREAS. R & R LOWER SECTION OF SEAL RETAINER, REF SRM 51-35-01 AND 51-33-01.
- [SDR FDEA201102220673](https://openairdocs.org/sdr/FDEA201102220673.md): Angle · corroded · Feb 22, 2011 · N390FE · Doug MD1010F · Wing Miscellaneous Structure
  > LT WHEEL WELL SLANT PANEL INBD VERTICAL "L" ANGLE IS CORRODED AT LWR EDGE. R & R "L" ANGLE, REF SRM 51-35-01.
- [SDR FDEA201102220672](https://openairdocs.org/sdr/FDEA201102220672.md): Angle · corroded · Feb 22, 2011 · N390FE · Doug MD1010F · Fuselage Main, Bulkhead
  > LT MAIN WHEEL WELL, FWD BULKHEAD, CORROSION LOCATED AT OTBD LOWER CORNER OF SLANT PANEL. R & R ANGLE. REF DWG NPB6072 AND DPS 4.708.
- [SDR FDEA201102220680](https://openairdocs.org/sdr/FDEA201102220680.md): Web · cracked · Feb 22, 2011 · N390FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > SEVERAL CRACKS FOUND AT STA 1406 IN LT WHEEL WELL ON THE UNDERWING BARREL KEEL STRUCTURE. REPAIRED WEB AT STA 1406 IN LT WHEEL WELL ON THE UNDERWING KEEL STRUCTURE IAW EA 8-5310-148486.
- [SDR FDEA201102220671](https://openairdocs.org/sdr/FDEA201102220671.md): Structure · corroded · Feb 22, 2011 · N390FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > LT WHEEL WELL SLANT PANEL OTBD VERTICAL TEE IS CORRODED AT LWR END. R & R VERTICAL TEE SECTION.
- [SDR FDEA201102180623](https://openairdocs.org/sdr/FDEA201102180623.md): Angle · corroded · Feb 18, 2011 · N390FE · Doug MD1010F · Fuselage Main, Structure
  > RT MAIN WHEEL WELL REAR SPAR CAP ANGLE (APB7080-2) HAS 2 CRACKS (2' CRACK INDICATION AFTER BLEND OUT) REMOVED AND INSTALLED REPAIR ANGLE. SRM 53-40-00, FIG 11.
- [SDR FDEA201102180622](https://openairdocs.org/sdr/FDEA201102180622.md): Tee Fitting · corroded · Feb 18, 2011 · N390FE · Doug MD1010F · Fuselage Main, Attach Fittings
  > RT WHEEL WELL SLANT PANEL OTBD VERTICAL TEE IS CORRODED AT LWR CORNER. REMOVED CORROSION. REF EA 8-5340-148481.
- [SDR FDEA201010204119](https://openairdocs.org/sdr/FDEA201010204119.md): Floor Support · corroded · Oct 20, 2010 · N390FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT BILGE STA 1801 BETWEEN LONGERON 51 RIGHT AND LONGERON 52 FLOOR SUPPORT FRAME CLIP FOUND CORROSION. NEW SHEAR CLIP FABRICATED AS PER DOUGLAS DRAWING AFA0053, REVISION N. CORRODED SHEAR CLIP AT AFT CARGO COMPARTMENT BILGE STA 1801 BET
- [SDR FDEA201010113985](https://openairdocs.org/sdr/FDEA201010113985.md): Door Frame · damaged · Oct 11, 2010 · N390FE · Doug MD1010F · Fuselage Main, Structure
  > FORWARD DOOR CUTOUT FUSELAGE JAMB AFT BETWEEN LONGERON 39 AND LONGERON 42 DOUBLER REPAIR FOUND WITH EDGE DAMAGED. R & R IAW SRM 53-50-00, FIG 26, VOL I, REV 96. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.
- [SDR FDEA201010053930](https://openairdocs.org/sdr/FDEA201010053930.md): Hinge Bracket · corroded · Oct 5, 2010 · N390FE · Doug MD1010F · Wing, Control Surface Attach Fittings
  > RIGHT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE) BARREL NUT HOLE SURFACE FOUND CORRODED. REWORKED IAW CMM 20-11-02, REV 51. FOUND WITHIN DAC DWG ARC0503, SHEET 2, REV BG LIMIT AND CMM 57-44-09, REV 51, TABLE 601 IN-SERVICE REWORK LIMIT. SHIM FABRICATED
- [SDR FDEA201010053929](https://openairdocs.org/sdr/FDEA201010053929.md): Hinge Bracket · corroded · Oct 5, 2010 · N390FE · Doug MD1010F · Wing, Control Surface Attach Fittings
  > RIGHT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE) LOWER MOUNT OUTBOARD HOLE FWD AND AFT FACE FOUND CORRODED. REPAIR CARRIED OUT IAW EA 8-5750-143763, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.
- [SDR FDEA201010053928](https://openairdocs.org/sdr/FDEA201010053928.md): Hinge Bracket · corroded · Oct 5, 2010 · N390FE · Doug MD1010F · Wing, Control Surface Attach Fittings
  > RIGHT WING OUTBOARD FLAP HINGE (WING SIDE) LOWER MOUNT INBOARD HOLE FWD AND AFT FACE FOUND CORRODED. REPAIR CARRIED OUT IAW EA 8-5750-143763, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.
- [SDR FDEA201010053927](https://openairdocs.org/sdr/FDEA201010053927.md): Hinge Bracket · corroded · Oct 5, 2010 · N390FE · Doug MD1010F · Wing, Control Surface Attach Fittings
  > RIGHT WING OUTBOARD FLAP HINGE (WING SIDE) LOWER MOUNT OUTBOARD HOLE FOUND CORRODED. REPAIR CARRIED OUT IAW EA 8-5750-143763, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.
- [SDR FDEA201010053926](https://openairdocs.org/sdr/FDEA201010053926.md): Hinge Bracket · corroded · Oct 5, 2010 · N390FE · Doug MD1010F · Wing, Control Surface Attach Fittings
  > RIGHT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE) PIVOT BEARING HOLE FOUND CORRODED. REPAIR CARRIED OUT IAW EA 8-5750-143446, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.

Next page: https://openairdocs.org/deregistered/N390FE-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 = 'N390FE' AND deregistration_id = 'N390FE-2024-03-02'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N390FE-2024-03-02/reports

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