# Service difficulty reports: N394FE, cancelled Mar 2, 2024

A list on [N394FE, cancelled Mar 2, 2024](https://openairdocs.org/deregistered/N394FE-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 2 · 99 reports

- [SDR FDEA2020031760571](https://openairdocs.org/sdr/FDEA2020031760571.md): Control Unit · malfunctioned · Mar 16, 2020 · N394FE · Doug MD1010F · Trailing Edge Flap Control System
  > PDIS 394 27-50 4766 15MAR20 MEM FACT U LOGPAGES:3200325 DECLARED EMERGENCY. UNRESPONSIVE FLAPS. UNABLE TO SELECT FLAPS BEYOND SLATS EXTENDED. USED DIAL-A-FLAP TO SELECT FLAPS 22 LANDING. PULLED CVR CB AND FLIGHT RECORDER CB PART 15MAR20 16:3
- [SDR FDEA2020031760570](https://openairdocs.org/sdr/FDEA2020031760570.md): Unknown · malfunctioned · Mar 16, 2020 · N394FE · Doug MD1010F · Trailing Edge Flap Control System
  > PDIS 394 27-50 4765 15MAR20 MEM FACT U DURING APPROACH REQUESTED "FLAPS 15", FO TRIED SELECTING FLAPS 15 UNSUCCESSFULLY. WE USED THE DIAL-A-FLAP TO SELECT FLAPS 22. SUSPECT JAMMED FLAPS. SHGN 15MAR20 21:36 MEM U WHILE TROUBELSHOOTING FLAPS
- [SDR FDEA201910312811](https://openairdocs.org/sdr/FDEA201910312811.md): Skin · cracked · Oct 31, 2019 · N394FE · Doug MD1010F · Trailing Edge Flaps
  > LH WING OUTBOARD FLAP UPPER SURFACE SKIN HAS TWO CRACKS LOCATED AT THE INBOARD HINGE AREA 0000608631: F - 01-NOV-2019 01:12 REPAIRED REF MD10 SRM 57-10-00 TRACKING EA 8-5750-T0350557 PART 1
- [SDR FDEA201906301440](https://openairdocs.org/sdr/FDEA201906301440.md): Warning System · false activation · Jun 30, 2019 · N394FE · Doug MD1010F · Landing Gear Brake System
  > AFTER LANDING ROLLOUT, THE LEVEL 1 BRAKE DIFF TEMP ALERTED, FOLLOWED BY THE LEVEL II (2) BRAKE OVERHEAT. BRAKES 5 & 6 PEAKED AT APPROX 600, BRAKES 1 & 2 PEAKED AT JUST BELOW 500. BRAKES 3-4, 7 & 8 NEVER EXCEEDED 200. MINIMAL BRAKING WAS USED FROM LANDING ROLLO
- [SDR FDEA201812183534](https://openairdocs.org/sdr/FDEA201812183534.md): Probe · out of limits · Dec 18, 2018 · N394FE · Doug MD1010F · Fuel Quantity Sensor
  > PDIS 394 28-40 3649 18DEC18 BNA OPEN U LOGPAGES:2876587 NR 2 FUEL QUANTITY DECREASED DISPROPORTIONATELY WITH NR 1 & NR 3 TANKS. POSSIBLE FUEL LEAK, OR SENSOR MALF (PREVIOUS WRITE UP). FACT 23DEC18 01:09 IAH ALL THE WORK DONE SERVICE WORK ORDER
- [SDR FDEA201810172932](https://openairdocs.org/sdr/FDEA201810172932.md): Cap · damaged · Oct 17, 2018 · N394FE · Doug MD1010F · Wing, Rib/Bulkhead
  > RT WING REAR UPPER SPAR AREA, APPROX XORS 402, INSIDE FUEL TANK UPPER RIB CAP HAS SMALL AREA OF DAMAGE. REPAIRED PER EA 8-5710-T0342036 PART 1.
- [SDR FDEA201808292262](https://openairdocs.org/sdr/FDEA201808292262.md): Rib · damaged · Aug 29, 2018 · N394FE · Doug MD1010F · Wing, Rib/Bulkhead
  > RIGHT WING, REAR UPPER SPAR AREA, XORS 402, INSIDE FUEL TANK UPPER RIB CAP HAD A SMALL AREA OF DAMAGE. REPAIRED IAW EA 8-5710-T0342036.
- [SDR FDEA201807121688](https://openairdocs.org/sdr/FDEA201807121688.md): Repair · damaged · Jul 12, 2018 · N394FE · Doug MD1010F · Trailing Edge Flaps
  > LT I/B FLAP VANE, I/B END HAS A DAMAGED REPAIR ON TOP SKIN. REPAIRED DAMAGE ON LT I/B FLAP VANE, I/B END TOP SIDE, IAW SRM 51-71-00 VOL 2, PAR 16.
- [SDR FDEA2018062981593](https://openairdocs.org/sdr/FDEA2018062981593.md): Skin · damaged · Jun 28, 2018 · N394FE · Doug MD1010F · Horizontal Stabilizer, Plate/Skin
  > RT DETACHABLE ELEVATOR HAD DAMAGE ON THE TOP INBD EDGE. REMOVED AND REPLACED THE SKIN IAW SRM 55-10-00, VOL 1, FIG 7, AND SRM 51-31-01, VOL 2.
- [SDR FDEA201805311403](https://openairdocs.org/sdr/FDEA201805311403.md): Spar · damaged · May 31, 2018 · N394FE · Doug MD1010F · Wing Spar
  > RT WING LOWER REAR SPAR REQUIRES SR10570049-60 REPAIR. PART TO BE FABRICATED PER EA 8-5710-T034000.
- [SDR FDEA201805311402](https://openairdocs.org/sdr/FDEA201805311402.md): Spar · damaged · May 31, 2018 · N394FE · Doug MD1010F · Wing Spar
  > RT WING LOWER REAR SPAR REQUIRES (2) SR10570048-38 REPAIR. PART TO BE FABRICATED PER EA 8-5710-T034000. REPAIRED PER ES 8-5710-T0340000.
- [SDR FDEA201805311401](https://openairdocs.org/sdr/FDEA201805311401.md): Spar · damaged · May 31, 2018 · N394FE · Doug MD1010F · Wing Spar
  > RT WING LOWER REAR SPAR REQUIRES SR10570048-6 REPAIR. PART TO BE FABRICATED PER EA 8-5710-T034000. REPAIRED PER EA 8-5710-T0340000.
- [SDR FDEA201805221371](https://openairdocs.org/sdr/FDEA201805221371.md): Flap System · cracked · May 22, 2018 · N394FE · Doug MD1010F · Wing Main, Frame Structure
  > REWORK REF N/R N00460 "LH WING ATTACH FITTING FOR O/B FLAP I/B HINGE HAS A.5 IN. CRACK ON THE O/B HALF AT THE FWD FASTENER. (MRKD)" REWORK PER QA REVIEW REJECTION. FITTING REPLACEMENT PART/MATERIAL NOT IDENTIFIED SNRM BLOCKS 23,24,25 AND NO RDR AND SDR GENE
- [SDR FDEA201805221447](https://openairdocs.org/sdr/FDEA201805221447.md): Frame · corroded · May 22, 2018 · N394FE · Doug MD1010F · Fuselage Main, Frame
  > CTR CARGO COMPT STA 1741 FRAME HAS CORROSION BY LONG 52. REMOVED AND REPLACED A SECTION OF CORRODED FRAME (CHANNEL) AT STA 1741 AT LONGERON 52 REF SRM 53-30-00 FIG 5 (SHEET 2) VOL I MAJOR REPAIR.
- [SDR FDEA201804301147](https://openairdocs.org/sdr/FDEA201804301147.md): Fitting · corroded · Apr 30, 2018 · N394FE · Doug MD1010F · Wing Main, Frame Structure
  > RIGHT WING OTBD FLAP, OTBD HINGE, SIDE LOAD FITTING ON THE AIRCRAFT SIDE, FOUND CORRODED AT THE FASTENER HOLES. REMOVED THE CORROSION. REMOVED AND REPLACED THE SIDE LOAD FITTING IAW SRM 51-33-01, VOL II, & DWG ARB0031.
- [SDR FDEA2018042601118](https://openairdocs.org/sdr/FDEA2018042601118.md): Seat Track · damaged · Apr 25, 2018 · N394FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > UPPER MAIN CARGO DECK LT SIDE, UNDER A BALLMAT AT BS 800, LBL 48 SEAT TRACK LOBE DAMAGED. REPAIRED THE SEAT TRACK IAW SRM 53-70-00, FIG 1, VOL 1.
- [SDR FDEA2018042601113](https://openairdocs.org/sdr/FDEA2018042601113.md): Skin · corroded · Apr 25, 2018 · N394FE · Doug MD1010F · Wing, Plate/Skin
  > LEFT UPPER WING SKIN HAS CORROSION AT FASTENER, XORS 423. AFT OF FRONT SPAR. REPAIRED IAW EA 8-5730-T0339577-P1. REPAIR CLASSIFIED AS MINOR.
- [SDR FDEA2018043001136](https://openairdocs.org/sdr/FDEA2018043001136.md): Rib · cracked · Apr 23, 2018 · N394FE · Doug MD1010F · Wing, Rib/Bulkhead
  > RIGHT WING L/E ACCESS PANEL 619DB, INSIDE UPPER RIB FLANGE IS CRACKED ABOVE PULLEY OTBD OF THE NR 10 SLAT TRACK.
- [SDR FDEA201804231101](https://openairdocs.org/sdr/FDEA201804231101.md): Skin · delaminated · Apr 23, 2018 · N394FE · Doug MD1010F · Wing, Plate/Skin
  > LEFT WING NR 3 SPOILER TOP SKIN HAS MULTIPLE AREAS OF DELAMINATION. REPAIRED IAW SRM 51-71-00, VOL II, PAR 16.
- [SDR FDEA201804191139](https://openairdocs.org/sdr/FDEA201804191139.md): Shear Tie · corroded · Apr 19, 2018 · N394FE · Doug MD1010F · Fuselage Internal Mounting Structure
  > AFT CARGO BAY, BS 1950, CORROSION ON THE FRAME SHEAR TIE BETWEEN LONGERONS 51 AND 52R. REPAIRED THE SHEAR TIE IAW SRM 53-30-00, PG 2, FIG 10, VOL 1.
- [SDR FDEA2018062981594](https://openairdocs.org/sdr/FDEA2018062981594.md): Skin · damaged · Apr 18, 2018 · N394FE · Doug MD1010F · Elevator, Plate/Skin
  > RT DETACHABLE ELEVATOR HAD DAMAGE ON THE TOP INBD EDGE. REMOVED AND REPLACED THE SKIN IAW SRM 55-10-00, VOL I, FIG 7, SRM 51-31-01, VOL II.
- [SDR FDEA201804111067](https://openairdocs.org/sdr/FDEA201804111067.md): Beam · cracked · Apr 11, 2018 · N394FE · Doug MD1010F · Fuselage Main, Structure
  > L3 DOOR, NR 1 BEAM AFT SIDE AT THE DOOR FRAME STOP WAS FOUND CRACKED. REMOVED AND REPLACED THE BEAM IAW DWG ADA 0006, AND SRM 51-31-01.
- [SDR FDEA2018042601128](https://openairdocs.org/sdr/FDEA2018042601128.md): Bulkhead Web · cracked · Apr 9, 2018 · N394FE · Doug MD1010F · Fuselage Main, Bulkhead
  > BS 595 BULKHEAD, RT FWD SIDE OF WEB HAS A 1 INCH CRACK THRU FASTENER HOLE AT RBL 60, Z100.00. PERFORMED A BULKHEAD REPAIR IAW SRM 53-40-00, FIG 25 V1.
- [SDR FDEA201804021245](https://openairdocs.org/sdr/FDEA201804021245.md): Spar Cap · cracked · Apr 2, 2018 · N394FE · Doug MD1010F · Wing Spar
  > RT WING REAR SPAR LOWER CAP AT XORS 446 HAS A 2.0 INCH CRACK AT THE AFT EDGE OF TEE CAP EXTENDING THROUGH THE RADIUS AND TERMINATING 1.0 IN UP THE VERTICAL LEG. REPAIRED PER EA 8-5710-T0340000.
- [SDR FDEA201804011123](https://openairdocs.org/sdr/FDEA201804011123.md): Frame · corroded · Apr 1, 2018 · N394FE · Doug MD1010F · Fuselage Main, Frame
  > CENTER CARGO BAY BS 1741 FRAME HAS CORROSION BY LONGERON 52. REPAIRED THE CORRODED FRAMED IAW SRM 53-30-00, VOL I, PAGE 31.
- [SDR FDEA201803280901](https://openairdocs.org/sdr/FDEA201803280901.md): Web · cracked · Mar 28, 2018 · N394FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > NOSE LANDING GEAR WW, RT SIDE FWD OF INNER WEB, BS 495, Z-65. CRACKED FROM FASTENER HOLES. REPAIRED IAW SRM 53-30-00, FIG 6, SH 8, VOL I. MAJOR REPAIR.
- [SDR FDEA201803271246](https://openairdocs.org/sdr/FDEA201803271246.md): Spar Cap · cracked · Mar 27, 2018 · N394FE · Doug MD1010F · Wing Spar
  > RT WING REAR SPAR LOWER CAP AT XORS 421 HAS A.200 INCH CRACK PROPAGATING FWD OF A PREVIOUS TRIM OUT REPAIR AND EXTENDING INTO THE RADIUS. REPAIRED PER EA 8-5710-T0340000.
- [SDR FDEA201803270974](https://openairdocs.org/sdr/FDEA201803270974.md): Skin · cracked · Mar 27, 2018 · N394FE · Doug MD1010F · Wing, Plate/Skin
  > RT WING SKIN AT THE INBOARD UPPER CORNER OF THE SLAT ANTI-ICE DUCT CUT OUT HAS A.500 INCH CRACK PROPAGATING THROUGH AN EXISTING STOP DRILL. INSTALLED A REPAIR DOUBLER PER SRM 57-10-00 FIG 103.
- [SDR FDEA201803270791](https://openairdocs.org/sdr/FDEA201803270791.md): Cargo Track · damaged · Mar 27, 2018 · N394FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CARGO TRACK BS 635 RBL 27.5 DAMAGED BEYOND LIMITS. REPAIRED THE TRACK IAW SRM 53-70-00, FIG 1, VOL 1.
- [SDR FDEA201803270790](https://openairdocs.org/sdr/FDEA201803270790.md): Cargo Track · gouged · Mar 27, 2018 · N394FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CARGO TRACK BS 879, RBL 8.5 GOUGED OUT OF LIMITS. REPLACED THE CARGO TRACK SRM 53-70-00, FIG 1, VOL 1.
- [SDR FDEA201803270788](https://openairdocs.org/sdr/FDEA201803270788.md): Cargo Track · worn · Mar 27, 2018 · N394FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CARGO BAY, BS 859, LBL 107.25 SEAT TRACK IS WORN OUT OF LIMITS. REPAIRED SEAT TRACK IAW SRM 53-70-00, FIG 1.
- [SDR FDEA201803261127](https://openairdocs.org/sdr/FDEA201803261127.md): Cap · cracked · Mar 26, 2018 · N394FE · Doug MD1010F · Fuselage Main, Bulkhead
  > RIGHT BS 595 BULKHEAD TEE CAP VERTICAL LEG AT LONGERON 43R HAS A.100 INCH CRACK THROUGH THE LOWER FASTENER HOLE. PERFORMED A TEE CAP REPAIR IAW DWG SR10530064.
- [SDR FDEA201803261112](https://openairdocs.org/sdr/FDEA201803261112.md): Cap · cracked · Mar 26, 2018 · N394FE · Doug MD1010F · Fuselage Main, Bulkhead
  > LEFT BS 595 BULKHEAD TEE CAP VERTICAL LEG AT LONGERON 41L HAS A 1 INCH CRACK THROUGH THE LOWER FASTENER HOLE. REPAIIRED THE TEE CAP IAW EA 8- 5310-T0339305 P1/P2. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201803160722](https://openairdocs.org/sdr/FDEA201803160722.md): Sensor · out of adjust · Mar 16, 2018 · N394FE · Doug MD1010F · Leading Edge Slat Position Indicating System
  > AFTER SELECTING FLAPS 35 ON FINAL AT ORD GOT SLAT DISAGREE ALERT. DUE TO TIME LAG BETWEEN SELECTING FINAL FLAPS AND ALERT ELECTED, A SECOND APPROACH IN NORMAL CONFIGURATION. NO DISAGREE, BUT SUSPECT LIMIT INDICATORS ARE OUT OF ADJUSTMENT. FOUND R2B SLAT
- [SDR FDEA201708152224](https://openairdocs.org/sdr/FDEA201708152224.md): Lever · binding · Aug 15, 2017 · N394FE · Doug MD1010F · Emergency Equipment
  > R1 ARMING LEVER VERY DIFFICULT TO MOVE, FEELS LIKE CABLE IS STRETCHING RATHER THAN PARTS ARE MOVING.
- [SDR FDEA201708052122](https://openairdocs.org/sdr/FDEA201708052122.md): Wire Harness · damaged · Aug 5, 2017 · N394FE · Doug MD1010F · Engine Indicating System Wiring
  > DURING CLIMBOUT, NOTICED THE NR 2 ENGINE EXCEEDENCE LEVEL 1 ALERT. EGT GAUGE FOR NR 2 SHOWED MAX 998. NORMAL EGT AT REDUCED POWER FOR LEVEL FLIGHT AT 7000 FT. ON ADVANCING POWER FOR CLIMB, NR 2 EGT CLIMBED RAPIDLY. PERFORMED GVI OF THE VSV FEED BACK CABLE
- [SDR FDEA201609263369](https://openairdocs.org/sdr/FDEA201609263369.md): Seat Track · damaged · Sep 26, 2016 · N394FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK FOUND DAMAGED BS 1388 RBL 75.25. REPAIRED IAW SRM 53-70-00.
- [SDR FDEA201609213367](https://openairdocs.org/sdr/FDEA201609213367.md): Seat Track · damaged · Sep 21, 2016 · N394FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > REPORTS A LOCK AT STA 1400, LOCK IN MAIN DECK CARGO IS NOT SECURE. PRIOR TO DEPARTURE, DISCOVERED SEAT TRACK DAMAGED WHERE LOCK IS LOCATED. NO DAMAGE TO LOCK WAS INDICATED. RELEASED FOR SERVICE IAW MEL: 25-57-02-A2, CATEGORY: A, EXPIRATION: 12OCT16, MEL 25-
- [SDR FDEA201605011439](https://openairdocs.org/sdr/FDEA201605011439.md): Longeron · corroded · May 1, 2016 · N394FE · Doug MD1010F · Fuselage Main, Longeron/Stringer
  > CENTER CARGO AREA LT SIDE AT BS 1781, STRINGER 43L HAS CORROSION. R & R THE LONGERON END CAP IAW SRM 51-31-01 VOL 2. FABRICATED NEW LONGERON END CAP ON T16 1202867, PN AFA3275-501 IAW SRM 53-15-01 PG 8B & 9 VOL 3. MAJOR REPAIR.
- [SDR FDEA201605011438](https://openairdocs.org/sdr/FDEA201605011438.md): Skin · corroded · May 1, 2016 · N394FE · Doug MD1010F · Fuel Storage
  > TOP SURFACE OF CTR WING TANK AT STATION 1224, LBL 90 - 105 HAS CORROSION. REMOVED CORROSION IAW SRM 51-21-01 VOL II FOUND TO BE OUT OF LIMITS IAW SRM 57-20-00 FIG 8A VOL I. INSPECTED AREA IAW NTSPM 06-10-01 & 06-00-03. NO DISCREPANCIES NOTED. COMPLIED WITH
- [SDR FDEA201605011437](https://openairdocs.org/sdr/FDEA201605011437.md): Skin · corroded · May 1, 2016 · N394FE · Doug MD1010F · Wing, Plate/Skin
  > CENTER WING UPPER SKIN AT STATION 1297, LBL 84 HAS CORROSION. REMOVED CORROSION IAW SRM 51-21-01 VOL 2, FOUND TO BE OUT OF LIMITS IAW SRM 57-20-00 FIG 8A VOL 1. INSPECTED AREA IAW NTSPM 06-10-01 & 06-00-03. NO DISCREPANCIES NOTED. COMPLIED WITH EA 8-5730-T
- [SDR FDEA201604281424](https://openairdocs.org/sdr/FDEA201604281424.md): Skin · corroded · Apr 28, 2016 · N394FE · Doug MD1010F · Wing, Plate/Skin
  > CENTER WING UPPER SKIN AT 1298, LBL 95, HAS CORROSION. REMOVED 6 EACH FASTENERS IAW SRM 51-30-01, VOL 2. REMOVED CORROSION IAW SRM 51-21-01 VOL 2. CHECKED LIMITS, ORIGINAL MATERIAL =.220, REMAINING MATERIAL =.182. FOUND OUT OF LIMITS IAW SRM 57-20-00 FIG
- [SDR FDEA201604281423](https://openairdocs.org/sdr/FDEA201604281423.md): Skin · dented · Apr 28, 2016 · N394FE · Doug MD1010F · Fuselage Main, Plate/Skin
  > TWO EACH DENTS ON UPPER FUSELAGE, EXTERNAL SURFACE AT FS 401, CLOSE TO L1 DOOR. COMPLIED WITH EA. 8-5330-T0324851 PT 1, DENTS AT FS 401 FWD OF L1 DOOR. APPLIED DENT DOT IAW GMM 06-3-101.
- [SDR FDEA201604271389](https://openairdocs.org/sdr/FDEA201604271389.md): Floorbeam · cracked · Apr 27, 2016 · N394FE · Doug MD1010F · Fuselage Main, Floor Beam
  > FLOORBEAM CRACKED AT STATION 1801, LBL 54 AT AFT CARGO DOOR CUT OUT. REPAIRED FLOORBEAM IAW SRM 53-60-01 FIG 3 VOL 1. MAJOR REPAIR.
- [SDR FDEA201604211331](https://openairdocs.org/sdr/FDEA201604211331.md): Floor Panel · damaged · Apr 21, 2016 · N394FE · Doug MD1010F · Fuselage Floor Panel
  > MAIN DECK AREA STATION 775, BL 0 FLOOR PANEL PUNCTURE. FABRICATED REPLACEMENT PANEL ON T16 1202347 IAW DWG SRZ-25-005. R & R FLOOR PANEL IAW 53-21-08-04, MAJOR REPAIR.
- [SDR FDEA201604151231](https://openairdocs.org/sdr/FDEA201604151231.md): Seat Track · gouged · Apr 15, 2016 · N394FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > GOUGES & MINOR DAMAGES ON SEAT TRACK SCALLOPS AT MAIN DECK CARGO COMPARTMENT, LBL 8.5 LT, BETWEEN FS 1521 & 1621. R & R SEAT TRACK AT LBL 8.5, FROM STATION 1531 - 1631, IAW SRM 51-01-01 VOL II, ON MAIN DECK CARGO, MAJOR REPAIR.
- [SDR FDEA201604131203](https://openairdocs.org/sdr/FDEA201604131203.md): Floorbeam · cracked · Apr 13, 2016 · N394FE · Doug MD1010F · Fuselage Main, Floor Beam
  > FLOORBEAM AT STATION 1821, HAS A CRACK AT LBL 54, INBD OF AFT CARGO DOOR CUT OUT. REPAIRED FLOORBEAM AT STATION 1821, LBL 54 IAW SRM 53-60-01 FIG 3 VOL 1 MAJOR REPAIR.
- [SDR FDEA201604101182](https://openairdocs.org/sdr/FDEA201604101182.md): Strap · defective · Apr 10, 2016 · N394FE · Doug MD1010F · Emergency Equipment
  > BOTH THE CAPTAIN & FIRST OFFICER ESCAPE STRAPS DO NOT REACH THE GND, AS REQUIRED BY STEPS 2 B 3 & 3 B 3 OF WC 25C6503. R & R CAPTAINS & FIRST OFFICERS ESCAPE STRAPS. OPERATIONS CHECKED GOOD IAW AMM 25-60-01-2.
- [SDR FDEA201512294101](https://openairdocs.org/sdr/FDEA201512294101.md): Light · inoperative · Dec 29, 2015 · N394FE · Doug MD1010F · Emergency Equipment
  > R1 DOOR PNEUMATIC PSI TEST FAILED. RELAMPED WITH CORRECT LIGHT BULBS. OPERATIONS CHECKED NORMAL IAW AMM 25-61-03-5-0.
- [SDR FDEA201502240591](https://openairdocs.org/sdr/FDEA201502240591.md): Switch · intermittent · Feb 24, 2015 · N394FE · Doug MD1010F · Passenger/Crew Doors
  > LEFT ENTRY DOOR FAILS TO MOVE UP OR DOWN, STUCK IN MID POSITION. DOOR SWITCH INTERMITTENT INTERIOR & EXTERIOR. REPLACED OPEN/CLOSE SOLENOID. ADJUST AND TEST CHECKS GOOD. IAW AMM 52-11-00-5 & 52-11-13-2.

Next page: https://openairdocs.org/deregistered/N394FE-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 = 'N394FE' AND deregistration_id = 'N394FE-2024-03-02'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N394FE-2024-03-02/reports

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