# Service difficulty reports: N389FE, cancelled Feb 3, 2024

A list on [N389FE, cancelled Feb 3, 2024](https://openairdocs.org/deregistered/N389FE-2024-02-03.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 4 · 175 reports

- [SDR FDEA201901190175](https://openairdocs.org/sdr/FDEA201901190175.md): Slide · unserviceable · Jan 19, 2019 · N389FE · Doug MD1010F · Escape Slide
  > MDIS 389 52-20 8452 19JAN19 MEM OPEN U DOOR SLIDE ASSEMBLY FELL OUT OF L1 DOOR, SLIDE DID NOT INFLATE HOWEVER CANVAS CASING LACES WERE PULLED. DISCONNECTED ATTACHMENT FITTINGS AND REMOVED ENTIRE SLIDE ASSY FROM DOOR. RELEASED FOR SERVICE PER MEL: 52-1
- [SDR FDEA201901020006](https://openairdocs.org/sdr/FDEA201901020006.md): Cable · broken · Jan 2, 2019 · N389FE · Doug MD1010F · Passenger/Crew Doors
  > WHILE ARMING THE L1 DOOR, FO REPORTS A CABLE SNAPPED AND BROKE. NOW A CABLE IS HANGING FROM THE DOOR. DOOR IS AVAILABLE FOR EMERGENCY USEONLY. REMOVED AFT DRIVE CABLE REF AMM 52-11-09-2-0.
- [SDR FDEA201802100335](https://openairdocs.org/sdr/FDEA201802100335.md): Spring · missing · Feb 10, 2018 · N389FE · Doug MD1010F · Landing Gear Position and Warning
  > UNSAFE GEAR INDICATION ILLUMINATED DURING DESCENT FOR THE RIGHT MAIN GEAR, UNSAFE INDICATION ON BOTH THE GEAR PANEL AND SYNOPTIC. COMPLIED WITH QRH, INDICATION WENT AWAY AFTER SLOWING BELOW 230KTS. NORMAL EXTENSION DURING APPROACH AND LANDING. PSEU T
- [SDR FDEA201710102889](https://openairdocs.org/sdr/FDEA201710102889.md): Slat System · malfunctioned · Oct 10, 2017 · N389FE · Doug MD1010F · Leading Edge Slat Control System
  > ON SLECTION OF FLAPS 35 FOR LANDING, A LEVEL 2 ALERT FOR SLAT DISAGREE CAME ON. DUE TO PROXIMINTY TO AIRPORT, A GO AROUND WAS INITIATED AND THEN THE ALERT WENT AWAY. F/O ALSO SUSPECTS FLAP/SLAT HANDLE DID NOT FULLY SETTLE IN DETENT. PERFORMED GVI OF THE
- [SDR FDEA201706201717](https://openairdocs.org/sdr/FDEA201706201717.md): Power Supply · inoperative · Jun 20, 2017 · N389FE · Doug MD1010F · Emergency Lighting
  > DURING EMERGENCY LIGHT TEST, HAD A LEVEL ONE EMERGENCY LIGHT BATTERY 1 LOW. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY POWER SUPPLY IAW AMM 33-51-01-4. OPS CHECKED GOOD. ACFT OK FOR SERVICE.
- [SDR FDEA201706071590](https://openairdocs.org/sdr/FDEA201706071590.md): Loop · worn · Jun 7, 2017 · N389FE · Doug MD1010F · Pneumatic System Wiring
  > LEVEL 3 AIR MANIFOLD NR 2 FAILED DURING CLIMBOUT. TROUBLESHOT THE NR 2 LOOP MANIFOLD IAW FIM 36-23-00-2, AND SSM 36-23-00. CHECKED RESISTANCE ON D1-17 AND FOUND GOOD. LOOP IS DISCONNECTED BETWEEN LOOP D1-17 AND LOOP D1-13 FOR TROUBLESHOOTING. FOUND D1-38
- [SDR FDEA201702210606](https://openairdocs.org/sdr/FDEA201702210606.md): Fuel Control · failed · Feb 21, 2017 · N389FE · Doug MD1010F · Fuel Control/Turbine Engines
  > AFTER SHUTTING DOWN THE NR 1 ENGINE FOR A FUNCTIONAL CHECK. FUEL FLOW EGT AND N2 PROGRESSED NORMAL DURING START, BUT THE N1 WOULD NOT ADVANCE PAST 28%. ADVANCING THROTTLE DID NOT CHANGE ANY NR 1 ENGINE PARAMETERS UNTIL REACHING 10,000 FT, AT WHICH TIME THE
- [SDR FDEA201702090481](https://openairdocs.org/sdr/FDEA201702090481.md): Seat Track · worn · Feb 9, 2017 · N389FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK SEAT TRACK DAMAGED BS 1089 TO 1169, LBL 9. REPAIRED SEAT TRACK IAW SRM 53-70-00 FIG 1 VOL 1.
- [SDR FDEA201702090480](https://openairdocs.org/sdr/FDEA201702090480.md): Seat Track · worn · Feb 9, 2017 · N389FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK LBL 9 SEAT TRACK DAMAGED FROM BS 1089 TO 1169. REPAIRED IAW SRM 53-70-00 FIG 1 VOL 1.
- [SDR FDEA201702060447](https://openairdocs.org/sdr/FDEA201702060447.md): Skin · cracked · Feb 6, 2017 · N389FE · Doug MD1010F · Wing, Plate/Skin
  > LEFT WING NR 10 SLAT TRACK CUT OUT AFT INBOARD DOOR CORNER HAS A.200 INCH CRACK. REPAIRED THE SKIN IAW SRM 57-10-00 FIG 68 SHEET 2/3 VOL 1
- [SDR FDEA201702040576](https://openairdocs.org/sdr/FDEA201702040576.md): Access Door · cracked · Feb 4, 2017 · N389FE · Doug MD1010F · Wing, Plate/Skin
  > LEFT WING SLAT ACTUATOR ACCESS DOOR, FWD INBOARD CONER HAS A.100 INCH CRACK. REPAIRED IAW SRM 57-10-00, VOL I, FIG 104, SHEET 2. MAJOR REPAIR.
- [SDR FDEA201702030575](https://openairdocs.org/sdr/FDEA201702030575.md): Skin · cracked · Feb 3, 2017 · N389FE · Doug MD1010F · Wing, Plate/Skin
  > LEFT WING NR 10 SLAT TRACK CUTOUT AFT INBD DOOR CORNER HAS A.200 INCH CRACK. REPAIRED IAW SRM 57-10-00, VOL I, FIG 68, SHEET 2 & 3.
- [SDR FDEA201702020412](https://openairdocs.org/sdr/FDEA201702020412.md): Hinge · cracked · Feb 2, 2017 · N389FE · Doug MD1010F · Landing Gear Doors
  > LEFT MAIN GEAR DOOR CENTER HINGE IS CRACKED. REMOVED AND REPLACED THE HINGE ASSY IAW SRM 51-31-01, VOL 2, & DRAWING ANB7093.
- [SDR FDEA201701290281](https://openairdocs.org/sdr/FDEA201701290281.md): Structure · corroded · Jan 29, 2017 · N389FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > UPPER MAIN DECK, BS 1273 AND LBL TO RBL OF CENTER WING TOP BOX SHOWS NUMEROUS CORRODED SPOTS. REPAIRED IAW EA. 8-5730-T0331280.
- [SDR FDEA201701250411](https://openairdocs.org/sdr/FDEA201701250411.md): Skin · cracked · Jan 25, 2017 · N389FE · Doug MD1010F · Landing Gear Doors
  > LEFT MAIN GEAR DOOR INNER SKIN IS CRACKED. REMOVED AND REPLACED THE SKIN IAW SRM 52-00-01, FIG 9, SHEET 1, VOL 1.
- [SDR FDEA201701250410](https://openairdocs.org/sdr/FDEA201701250410.md): Fitting · cracked · Jan 25, 2017 · N389FE · Doug MD1010F · Landing Gear Doors
  > LEFT MAIN GEAR DOOR FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-31-05, VOL 2, AND DRAWING ANB7134.
- [SDR FDEA201701250251](https://openairdocs.org/sdr/FDEA201701250251.md): Seat Track · corroded · Jan 25, 2017 · N389FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CARGO DECK, STA 1962 RT O/B FLOOR TRACK CORRODED. REPAIRED TRACK PER SRM 53-70-00 FIG 18.
- [SDR FDEA201701230241](https://openairdocs.org/sdr/FDEA201701230241.md): Seat Track · worn · Jan 23, 2017 · N389FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK BS 1140 9LBL SEAT TRACK DAMAGED. R & R SEAT TRACK SPLICE IAW SRM 53-70-00, FIG 1.
- [SDR FDEA201701230240](https://openairdocs.org/sdr/FDEA201701230240.md): Seat Track · worn · Jan 23, 2017 · N389FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK, BS 1135, LBL 9 SEAT TRACK DAMAGED. R & R THE SEAT TRACK SPLICE IAW SRM 53-70-00.
- [SDR FDEA201701210234](https://openairdocs.org/sdr/FDEA201701210234.md): Access Panel · delaminated · Jan 21, 2017 · N389FE · Doug MD1010F · Wing, Plate/Skin
  > RIGHT WING, ACCESS PANEL 641LB IS DELAMINATED. REPAIRED THE ACCESS PANEL IAW SRM 51-71-00, VOLUME 2, PAGE 39, PARAGRAPH 3, AND DRAWING ARC0357.
- [SDR FDEA201701170571](https://openairdocs.org/sdr/FDEA201701170571.md): Skin · damaged · Jan 17, 2017 · N389FE · Doug MD1010F · Horizontal Stabilizer, Plate/Skin
  > UPPER RT HORIZ STAB, SHOW HAILS / TOOL MARK APPROX 1" X 1" X.25" 5121819. CUT OUT DAMAGE AND INSTALLED A DOUBLER AND FILLER IAW SRM 55-00-01 VOL I FIG 3 SHEET 2.
- [SDR FDEA201701170215](https://openairdocs.org/sdr/FDEA201701170215.md): Seat Track · worn · Jan 17, 2017 · N389FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN, SEAT TRACK AT STA 630 IS DAMAGED. REPAIRED PER SRM 53-70-00 FIG 1A VOL1.
- [SDR FDEA201701170214](https://openairdocs.org/sdr/FDEA201701170214.md): Seat Track · damaged · Jan 17, 2017 · N389FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK, SEAT TRACK AT STA 637, RBL 9 IS DAMAGED. REPAIRED PER SRM 53-70-00 FIG 1A VOL1.
- [SDR FDEA201701120261](https://openairdocs.org/sdr/FDEA201701120261.md): Access Door · cracked · Jan 12, 2017 · N389FE · Doug MD1010F · Wing, Plate/Skin
  > LEFT WING SLAT ACTUATOR ACCESS DOOR FWD INBOARD CORNER HAS A.100 INCH CRACK. REPAIRED IAW SRM 57-10-00 VOL1 FIG 104 SHEET 2.
- [SDR FDEA201701110409](https://openairdocs.org/sdr/FDEA201701110409.md): Door Frame · cracked · Jan 11, 2017 · N389FE · Doug MD1010F · Fuselage Main, Structure
  > LEFT MLG DOOR INBD INTERIOR LANDING IS CRACKED NEAR ACTUATOR ATTACH FITTING. REMOVED AND REPLACED THE LANDING IAW SRM 52-00-01, FIG 9, SHEET 1, VOL 1, PG.42.
- [SDR FDEA201601070078](https://openairdocs.org/sdr/FDEA201601070078.md): Shaft · sheared · Jan 7, 2016 · N389FE · Doug MD1010F · Stabilizer Control System
  > RIGHT SIDE HORIZONTAL STABILIZER, CONSTANT BEARING INSPECTION REVEALED, OTBD SIDE LOAD STRUT NUT & LUBE WASHER ARE LOOSE & OUT OF POSITION. R & R THE SHAFT, SLEEVE & LUBE WASHER.
- [SDR FDEA201601010004](https://openairdocs.org/sdr/FDEA201601010004.md): Stowage Box · faulty · Jan 1, 2016 · N389FE · Doug MD1010F · Crew Oxygen System
  > ON PREFLIGHT, FIRST OFFICERS OXYGEN MASK FAILED MIC TEST. R & R MASK STOWAGE BOX IAW MM 35-13-04-4, OPERATIONS NORMAL.
- [SDR FDEA201510143189](https://openairdocs.org/sdr/FDEA201510143189.md): Switch · inoperative · Oct 14, 2015 · N389FE · Doug MD1010F · Emergency Equipment
  > R1 DOOR SLIDE REMOTE PRESS INDICATOR TEST LIGHT INOPERATIVE. RELEASED FOR SERVICE IAW MEL 25-61-01 CATEGORY C. VERIFY & RECORD IN THE AML, EVAC SLIDE SYS PRESS ONCE EACH FLIGHT DAY. DEFERRED R1 SLIDE INDICATOR LIGHT C 7023854. R & R SWITCH IAW AMM 25-61-03
- [SDR FDEA201505051383](https://openairdocs.org/sdr/FDEA201505051383.md): Warning Light · illuminated · May 5, 2015 · N389FE · Doug MD1010F · Landing Gear Position and Warning
  > RT LANDING GEAR RED LIGHT ILLUMINATED AT FL330. DESCENDED TO FL270 & SLOWED TO 230 KTS IAW QRH. LIGHT REMAINED ON UNTIL PASSING FL20.5, GOOD INDICATIONS ON LANDING LIGHTS, 3 GREEN. FAULTED 317074 INTERMITTENT RT GEAR UP & LATCHED, AB SENSOR DISAGREE, FOUND
- [SDR FDEA201502060458](https://openairdocs.org/sdr/FDEA201502060458.md): Light · inoperative · Feb 6, 2015 · N389FE · Doug MD1010F · Emergency Equipment
  > DURING PREFLIGHT CREW INFORMED MX L1 DOOR EMER SLIDE PUSH TO TEST DOOR LIGHT INOPERATIVE. REPLACED L1 REMOTE SLIDE PRESSURE INDICATOR AND BATTERY PACK ASSY.
- [SDR FDEA201412224163](https://openairdocs.org/sdr/FDEA201412224163.md): Aileron · corroded · Dec 22, 2014 · N389FE · Doug MD1010F · Ailerons
  > POPPED FASTENERS & SIGN OF CORROSION 24 INCHES OTBD OF THE INBD EDGE OF THE OTBD AILERON ON THE RT WING. REMOVED CORROSION & INSTALLED REPAIR DOUBLER IAW SRM 57-10-00 FIG 85.
- [SDR FDEA201412114105](https://openairdocs.org/sdr/FDEA201412114105.md): Panel · delaminated · Dec 11, 2014 · N389FE · Doug MD1010F · Nacelle/Pylon, Plate/Skin
  > PANEL 364 DR RT PICKLE BARREL HAS MINOR DAMAGE. REPAIRED PANEL 364 DR RT PANEL IAW SRM 51-71-00 VOL II.
- [SDR FDEA201412084084](https://openairdocs.org/sdr/FDEA201412084084.md): Angle · cracked · Dec 8, 2014 · N389FE · Doug MD1010F · Wing Miscellaneous Structure
  > RIGHT WING LE SLAT DRIVE ACCESS DOOR OTBD LANDING IS CRACKED AT PREVIOUS REPAIR DOUBLER. R & R ANGLE ARB1286-14 IAW DWG ARB1286 & SRM 51-31-01 VOL II.
- [SDR FDEA201412084083](https://openairdocs.org/sdr/FDEA201412084083.md): Skin · cracked · Dec 8, 2014 · N389FE · Doug MD1010F · Wing, Plate/Skin
  > RIGHT WING LE PANEL LAND CRACKED BEHIND SLAT NR 3 NEXT TO SLAT TRACK NR 8. R & R LAND STRAP IAW DWG ARB1180 & SRM 51-31-01 VOL II.
- [SDR FDEA201412044064](https://openairdocs.org/sdr/FDEA201412044064.md): Skin · cracked · Dec 4, 2014 · N389FE · Doug MD1010F · Wing, Plate/Skin
  > RIGHT WING, LE PANEL LAND CRACKED BEHIND SLAT NR 4 NEXT TO SLAT TRACK NR 9. REMOVED CRACKED LAND RT WING LE PANEL AS REQUIRED. INSTALLED NEW LAND RT WING LE PANEL IAW DWG ARB1180 & SRM 51-31-01 VOL II.
- [SDR FDEA201412044063](https://openairdocs.org/sdr/FDEA201412044063.md): Floor Support · corroded · Dec 4, 2014 · N389FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > MAIN CABIN RT APPROX STATION 1219 RBL 80 FLOOR SUPPORT CORRODED. FABRICATED & INSTALLED FLOOR SUPPORT AEA0394-504 RT APPROX STATION 1129, RBL 80 IAW DWG NEA6018 & SRM 51-31-01 VOL II.
- [SDR FDEA201412034051](https://openairdocs.org/sdr/FDEA201412034051.md): Seat Track · damaged · Dec 3, 2014 · N389FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK STATION 1385 & 1395 RT 75.50 SEAT TRACK DAMAGED. REPAIRED DAMAGED SEAT TRACK AREA IAW SRM 53-70-00 FIG 1.
- [SDR FDEA201412034049](https://openairdocs.org/sdr/FDEA201412034049.md): Seat Track · damaged · Dec 3, 2014 · N389FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK STATION 1384 & 1389 LT 75.50 SEAT TRACK DAMAGED. WORK WITH NR 209. REPAIRED SEAT TRACK IAW SRM 53-70-00 FIG 1.
- [SDR FDEA201412034048](https://openairdocs.org/sdr/FDEA201412034048.md): Seat Track · damaged · Dec 3, 2014 · N389FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN STATION 1270 SEAT TRACK DAMAGED AT LBL 75. REPAIRED IAW SRM 53 FIG 2 SHEET 1.
- [SDR FDEA201412034047](https://openairdocs.org/sdr/FDEA201412034047.md): Seat Track · damaged · Dec 3, 2014 · N389FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK SEAT TRACK STATION 1250 LT 75.50 DAMAGED. REPAIRED IAW SRM 53-70-00 FIG 2 SHEET 1.
- [SDR FDEA201408132159](https://openairdocs.org/sdr/FDEA201408132159.md): Link · faulty · Aug 13, 2014 · N389FE · Doug MD1010F · Landing Gear Door Retract Section
  > LEFT MAIN GEAR SHOWED UNSAFE RED LIGHT AFTER TAKEOFF FOR BOTH PRIMARY & SECONDARY INDICATIONS. LG WAS CYCLED AT ALTITUDE IAW THE QRH WITH NO IMPROVEMENT. FOUND LT MAIN GEAR DOOR UP LATCH LINK NOT RETURNING TO LATCH POSITION. R & R LT MLG DOOR LINK, LINK BO
- [SDR FDEA201407191870](https://openairdocs.org/sdr/FDEA201407191870.md): Pivot · lack of lube · Jul 19, 2014 · N389FE · Doug MD1010F · Landing Gear Position and Warning
  > WHEN GEAR WAS RETRACTED AFTER TAKEOFF BOTH THE RED LT LIGHT ABOVE THE GEAR HANDLE & THE LIGHT ON THE CONFIG PAGE SHOWED AN INDICATION THAT THE LT MAIN GEAR WAS NOT EXTRACTED. HOWEVER THERE WAS NO DRAG OR ADVERSE HANDLING CHARACTERISTICS. SPEED WAS KEPT BELOW
- [SDR FDEA201407171840](https://openairdocs.org/sdr/FDEA201407171840.md): Landing Gear · lack of lube · Jul 17, 2014 · N389FE · Doug MD1010F · Landing Gear Retraction/Extension System
  > LEFT MAIN GEAR WOULD NOT GIVE A SAFE UP INDICATION ON EITHER THE PRIMARY OR SECONDARY INDICATORS. COMPLIED WITH QRH WITH SAME RESULT. LUBRICATED LT & RT MLG IAW AMM 12-21-01-3-2. JACKED ACFT IAW AMM 07-11-00-2. PERFORMED EXTENSION & RETRACTION OF GEAR FOR
- [SDR FDEA201405182091](https://openairdocs.org/sdr/FDEA201405182091.md): Skin · cracked · May 18, 2014 · N389FE · Doug MD1010F · Wing, Plate/Skin
  > LEFT WING FIXED LE SKIN CRACKED AT THE PRESS REFUELING DOORWAY PANEL 518FB INBD FWD. REPAIRED IAW SRM 57-10-00 & EA 8-5710-T0308261 SEQ 231.
- [SDR FDEA201405182089](https://openairdocs.org/sdr/FDEA201405182089.md): Skin · cracked · May 18, 2014 · N389FE · Doug MD1010F · Wing, Plate/Skin
  > RIGHT WING NR 3 SLAT ANTI-ICE TELESCOPING DUCT CUT OUT IS CRACKED AT UPPER INBD & OTBD CORNERS. REPAIRED IAW EA 8-5710-T0308270.
- [SDR FDEA201405182088](https://openairdocs.org/sdr/FDEA201405182088.md): Skin · cracked · May 18, 2014 · N389FE · Doug MD1010F · Wing, Plate/Skin
  > LEFT WING FIXED LE SKIN CRACKED AT THE TAI DUCT CUT OUT TOP OTBD CORNER. REPAIRED IAW EA 8-5710-T0308271 PART 1.
- [SDR FDEA201308121832](https://openairdocs.org/sdr/FDEA201308121832.md): Pump · failed · Aug 12, 2013 · N389FE · Doug MD1010F · Engine Fuel/Oil Cooler
  > NR 2 ENGINE FUEL FILTER ALERTED AT 80 KTS DURING TAKEOFF ROLL. ALERT OCCURED AT 98 PERCENT N1. REJECTED TAKEOFF. ALERT EXTINQUISHED AT THROTTLE REDUCTION. REMOVED FUEL FILTER AND DEBRIS SCREEN IAW 73-12-01-2. NR 2 ENGINE FUEL PUMP, MEC, AND FUEL OIL COOL
- [SDR FDEA201306031345](https://openairdocs.org/sdr/FDEA201306031345.md): Bulkhead · cracked · Jun 3, 2013 · N389FE · Doug MD1010F · Fuselage Main, Bulkhead
  > 2 INCH CRACK LT MLG WW INBD BULKHEAD 30 INCHES FWD OF AFT BULKHEAD AND 3 INCHES DOWN FROM UPPER BULKHEAD. REPAIRED PER SRM 53-00-01, FIG 10, VOLUME I.
- [SDR FDEA201212024227](https://openairdocs.org/sdr/FDEA201212024227.md): Spar Cap · cracked · Dec 2, 2012 · N389FE · Doug MD1010F · Horizontal Stabilizer, Spar/Rib
  > HORZIONTAL STAB CONSTANT SECTION RT SIDE AFT UPPER SPAR CAP FITTING, HAS A CRACK APPROX 1" IN LENGTH, JUST INBD OF ATTACH BOLT. R & R SECTION OF UPPER SPAR CAP REF EA 8-5510-163913.
- [SDR FDEA201204011217](https://openairdocs.org/sdr/FDEA201204011217.md): Regulator · inoperative · Apr 1, 2012 · N389FE · Doug MD1010F · Pneumatic Indicating System
  > FLIGHT LEVEL 340, LEVEL 3 AIR MANIFOLD 2 FAIL. DIVERTED AND LANDED WITHOUT INCIDENT. REPLACED NR 2 ENGINE PRESSURE REGULATOR VALVE, REF AMM 36-12-01-4.

Next page: https://openairdocs.org/deregistered/N389FE-2024-02-03/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 = 'N389FE' AND deregistration_id = 'N389FE-2024-02-03'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N389FE-2024-02-03/reports

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