# Service difficulty reports: N597FE

A list on [N597FE](https://openairdocs.org/aircraft/N597FE.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 9 · 406 reports

- [SDR FDEA202407080967](https://openairdocs.org/sdr/FDEA202407080967.md): Packing · failed · Jul 8, 2024 · N597FE · Doug MD11F · Hydraulic System, Main
  > AFTER LEVEL OFF, LEVEL 1 HYD 3 ELEV OFF ALERT PROGRESSED TO HYD 3 QTY LOW TO HYD 3 FAIL. TOTAL LOSS OF HYD 3 FLUID. EMERGENCY DECLARED. ON ARRIVAL IN KIX, #3 HYD SYS REMAIN 0.3. T/S FOUND HYD LEAK FORM R/H L/G RETRACT ACT LINE. CHECKED EDPS AND #3 SY
- [SDR FDEA202403150292](https://openairdocs.org/sdr/FDEA202403150292.md): Fairing · damaged · Mar 15, 2024 · N597FE · Doug MD11F · Nacelle/Pylon, Main Frame
  > #3 ENGINE PYLON AFT FAIRINGS DAMAGED. AMM: 54-81-01-4 INSTALLED SERVICEABLE PYLON FAIRING
- [SDR FDEA202308151445](https://openairdocs.org/sdr/FDEA202308151445.md): Balance Weight · corroded · Aug 15, 2023 · N597FE · Doug MD11F · Aileron Control System
  > L/H AILERON HAS BALANCE WEIGHT CORRODED REMOVED AND REPLACED AILERON INCLUDING WEIGHTS
- [SDR FDEA202308151444](https://openairdocs.org/sdr/FDEA202308151444.md): Balance Weight · corroded · Aug 15, 2023 · N597FE · Doug MD11F · Aileron Control System
  > L/H O/B AILERON HAS BALANCE WEIGHT CORRODED. REMOVED AND REPLACED AILERON INCLUDING BALANCE WEIGHT N/R 329,
- [SDR FDEA202308151443](https://openairdocs.org/sdr/FDEA202308151443.md): Balance Weight · corroded · Aug 15, 2023 · N597FE · Doug MD11F · Aileron Control System
  > R/H O/B AILERON HAS CORROSION ON BALANCE WEIGHT REMOVED AND REPLACED AILERON INCLUDING ALL BALANCE WEIGHT, INCLUDING N/RS 477, 464, 463
- [SDR FDEA202308151442](https://openairdocs.org/sdr/FDEA202308151442.md): Balance Weight · corroded · Aug 15, 2023 · N597FE · Doug MD11F · Aileron Control System
  > R/H O/B AILERON HAS ALL BALANCE WEIGHT CORRODED. R/H O/B AILERON WAS REPLACED INCLUDING WEIGHTS
- [SDR FDEA202308151441](https://openairdocs.org/sdr/FDEA202308151441.md): Balance Weight · corroded · Aug 15, 2023 · N597FE · Doug MD11F · Aileron Control System
  > R/H O/B AILERON HAS ALL BALANCE WEIGHT CORRODED. REMOVED AND REPLACED 5 BALANCE WEIGHTS ON R/H O/B AILERON.
- [SDR FDEA202307261328](https://openairdocs.org/sdr/FDEA202307261328.md): Skin · gouged · Jul 26, 2023 · N597FE · Doug MD11F · Leading Edge Devices
  > R/H WING LEADING EDGE / BETWEEN I/B SLAT #1 & #2 AT SPLICE FOR TRACK #3 ( ON THE AIRCRAFT) HAS A DEEP GOUGE ( HIDDEN WHEN SLATS ARE RETRACTED) BLENDED GOUGE AND REPAIRED AREA ON LEADING EDGE OF RH WING XIS 247 (ABOVE SLAT TRACK 3) PER SRM 57-40-02-2R RE
- [SDR FDEA202307211457](https://openairdocs.org/sdr/FDEA202307211457.md): Skin · cracked · Jul 21, 2023 · N597FE · Doug MD11F · Leading Edge Devices
  > LH WING, LEADING EDGE, NO. 8 SLAT TRACK CUTOUT, OUTBD EDGE HAS HORIZONTAL CRACK APPROX.500", MARKED ORANGE DOT & RED GREASE PENCIL. REPAIRED PER EA # 1-5730-T0375548 P1.
- [SDR FDEA202307121452](https://openairdocs.org/sdr/FDEA202307121452.md): Stanchion · corroded · Jul 12, 2023 · N597FE · Doug MD11F · Fuselage Main, Structure
  > FWD CARGO COMPT, STA 6-73.5 RBL 9, AFT BULKHEAD, VERTICAL STANSION HAS CORROSION OUT OF LIMITS ON VERTICAL LEG AT NUTPLATE REPAIRED ATANCHION PER EA# 1-5310-T0375475 TITLE: FUSELAGE-FORWARD INTERMEDIATE- FORWARD CARGO COMPARTMENT AFT BULKHEAD, STANCHION AT
- [SDR FDEA202307121204](https://openairdocs.org/sdr/FDEA202307121204.md): Unknown · unknown · Jul 12, 2023 · N597FE · Doug MD11F · Wing Main, Frame Structure
  > PANEL 345BB DELAMED. REPAIRED DELAMINTED PANEL 345BB PER SRM 51-62-01-0G PG.44 REPAIR "J" STEP 1-9
- [SDR FDEA202307091189](https://openairdocs.org/sdr/FDEA202307091189.md): Tee Fitting · cracked · Jul 9, 2023 · N597FE · Doug MD11F · Wing Main, Frame Structure
  > RIGHTHAND INNER WING; STA. 1481 TRAILING EDGE STRUCTURE HAS CRACKED BRACKET @ HANGAR ASSEMBLY. AS VIEWED FROM WHEELWELL OUTER STRUCTURE NOTE: ARC0250 AND IPC 57-51. REMOVED FABERCATED AND INSTALLED NEW T CLIP ANB7535-127 IAW DWG ANB7535
- [SDR FDEA202307091188](https://openairdocs.org/sdr/FDEA202307091188.md): Tee Fitting · cracked · Jul 9, 2023 · N597FE · Doug MD11F · Wing Main, Frame Structure
  > LEFTHAND INNER WING; STA. 1481 TRAILING EDGE STRUCTURE HAS CRACKED BRACKET @ HANGAR ASSEMBLY. AS VIEWED FROM WHEELWELL OUTER STRUCTURE NOTE: ARC0250 AND IPC 57-51 REMOVED FABERCATED AND INSTALLES NEW T CLIP ANB7535-127 IAW DWG ANB7535
- [SDR FDEA202306251213](https://openairdocs.org/sdr/FDEA202306251213.md): Floorbeam · damaged · Jun 25, 2023 · N597FE · Doug MD11F · Fuselage Main, Floor Beam
  > FWD CARGO PIT FLOOR BEAM AT APPROX STA 6-10 CENTER BUTTLINE HAS AN IMPACT DAMAGE IN WHICH THE VERTICAL LEG WAS DEFORMED BEYOND ALLOWABLE LIMITS. REPAIRED FLOOR BEAM PER SRM 53-00-00-0G FIG 208 MAJOR REPAIR
- [SDR FDEA202306221078](https://openairdocs.org/sdr/FDEA202306221078.md): Unknown · unknown · Jun 22, 2023 · N597FE · Doug MD11F · Wing, Plate/Skin
  > DELAMINATION ON RH WING T/E XW899 REPAIRED DELAMINATION ON RH WING T/E XW899 PER SRM 57-00-01-2R REPAIR 2 FIG. 201 SHEET 1
- [SDR FDEA202306211093](https://openairdocs.org/sdr/FDEA202306211093.md): Support · corroded · Jun 21, 2023 · N597FE · Doug MD11F · Fuselage Main, Structure
  > FWD CARGO COMPT, AFT BULKHEAD, LOWER FLOOR BOARD SUPPORT STA RBL 10, HAS CORROSION ON VERTICAL LEG. INSTALLED TEE EXTRUSION AND REPAIR ANGLES AS REQUIRED. REF MD 11 SRM 53-00-00-2R FIGURE 208, SHEET 3, SRM 51-33-01-0G, DAC DWG ADA7667.
- [SDR FDEA202306151041](https://openairdocs.org/sdr/FDEA202306151041.md): Panel · delaminated · Jun 15, 2023 · N597FE · Doug MD11F · Wing, Plate/Skin
  > R/H HORIZ PANEL 345BB HAS DELAMINATION. REPAIRED DELAMINATED PANEL 345BB PER SRM55-20-80-2R PG.25-27.
- [SDR FDEA202306151040](https://openairdocs.org/sdr/FDEA202306151040.md): Panel · delaminated · Jun 15, 2023 · N597FE · Doug MD11F · Wing, Plate/Skin
  > PANEL 345BB DELAMED. REPAIRED DELAMINATED PANEL 345BB PER SRM55-20-80-2R PG.25-27
- [SDR FDEA202306050996](https://openairdocs.org/sdr/FDEA202306050996.md): Floorboard · damaged · Jun 5, 2023 · N597FE · Doug MD11F · Fuselage Floor Panel
  > LWR FWD CARGO FLOORBOARD 127EF HAS HOLE DAMAGE AND EDGE DAMAGE FABRICATED FLOORBOARD 127EF REF FEDEX DWG SRZ-25-005 MAJOR REPAIR
- [SDR FDEA202306050994](https://openairdocs.org/sdr/FDEA202306050994.md): Floorboard · damaged · Jun 5, 2023 · N597FE · Doug MD11F · Fuselage Floor Panel
  > LWR FWD CARGO FLOORBOARD 127NF HAS PUNCTURES FABRICATED PANEL REF FEDEX DWG SRZ-25-005 MAJOR REPAIR
- [SDR FDEA202306041205](https://openairdocs.org/sdr/FDEA202306041205.md): Unknown · unknown · Jun 4, 2023 · N597FE · Doug MD11F · Fuselage Main, Plate/Skin
  > L/H FUSELAGE SKIN AT #1 PACK EXHAUST DOOR UPPER AFT CORNER HAS A.200 IN. CRACK PROPAGATING OUT OF FASTENER HOLE. (MARKED) INSTALLED FILLER, DOUBLER, AND TRIPLER REF MD11 SRM 53-20-15-2R REPAIR 3. MAJOR REPAIR
- [SDR FDEA202305300975](https://openairdocs.org/sdr/FDEA202305300975.md): Unknown · unknown · May 30, 2023 · N597FE · Doug MD11F · Standard Practices/Structures
  > LH WING-BETWEEN UPPER AND LOWER REAR SPAR: ARC7199-529 BRACKET AT XORS 1088 HAS CRACK APROX. 3 INCHES REPAIRED NOTED LH WING-BETWEEN UPPER AND LOWER REAR SPAR: ARC7199-529 BRACKET AT XORS 1088 HAS CRACK APROX. 3 INCHES PER SRM 51-62-01-0G REPAIR"J" PG.44
- [SDR FDEA202305300974](https://openairdocs.org/sdr/FDEA202305300974.md): Bracket · damaged · May 30, 2023 · N597FE · Doug MD11F · Standard Practices/Structures
  > LEFT WING -- BETWEEN UPPER AND LOWER REAR SPAR - COMPOSITE ANGLE BRACKET AT XORS 1088 HAS 2 DAMAGED HOLES REPAIRED NOTED LEFT WING -- BETWEEN UPPER AND LOWER REAR SPAR - COMPOSITE ANGLE BRACKET AT XORS 1088 HAS 2 DAMAGED HOLES PER SRM 51-62-01-0G REPAIR "A
- [SDR FDEA202305270985](https://openairdocs.org/sdr/FDEA202305270985.md): Skin · corroded · May 27, 2023 · N597FE · Doug MD11F · Fuselage Main, Plate/Skin
  > H AFT FUSELAGE, APPROX STA 2140-2164, BOTTOM EDGE OF FAIRING AJC7897-1, HAS SURFACE CORROSION. REPAIRED LH AFT FUSELAGE BOTTOM EDGE AT APRROX STA 2140-2164, REF SRM 53-70-01 2R REPAIR 3 FIG 201 SHEET 1-5, MD-11 SRM 51-33-01-0G, DAC DWG AJC7059. "MAJOR
- [SDR FDEA202305250969](https://openairdocs.org/sdr/FDEA202305250969.md): Channel · corroded · May 25, 2023 · N597FE · Doug MD11F · Fuselage Miscellaneous Structure
  > FWD CARGO COMPT, STA 6-60 6LBL, CORROSION ON THE CENTER ROLLER TRAY/ FLOOR SUPPORT LAND. REMOVED AND REPLACED A6J7003-1 CHANNEL ASSEMBLY WITH NEWLY FABRICATED A6J7003-1 CHANNEL ASSEMBLY REF DAC DWGS A6J7003, N6J6715, AND NBJ6735 MAJOR REPAIR
- [SDR FDEA202305241330](https://openairdocs.org/sdr/FDEA202305241330.md): Nose Cowl · dented · May 24, 2023 · N597FE · Doug MD11F · Horizontal Stabilizer Structure
  > NO. 2 ENG INLET LEADING EDGE - APPROX 3:00 OCLOCK POSITION (LOOKING FWD)- DENT APPROX 1 INCH DIA. DOT #18 REPAIR NOSE COWL REF. EA # 1-5430-T0375346.
- [SDR FDEA202305241133](https://openairdocs.org/sdr/FDEA202305241133.md): Frame · chafed · May 24, 2023 · N597FE · Doug MD11F · Fuselage Main, Attach Fittings
  > TAIL CONE FWD SECTION. FWD L/H UPPER GUIDE PIN LOOSE. REPAIRED DAMAGE PER SRM 53-80-07-2R REPAIR 1 FIG 201 SHEET 1.
- [SDR FDEA202305241132](https://openairdocs.org/sdr/FDEA202305241132.md): Frame · cracked · May 24, 2023 · N597FE · Doug MD11F · Fuselage Main, Attach Fittings
  > TAIL CONE FWD SECTION. FWD END APPROX 1-0CLOCK POSITION (UPPER R/H) GUIDE PIN LOOSE REPAIRED DAMAGE PER SRM 53-80-07-2R REPAIR 1 FIG 201 SHEET 1.
- [SDR FDEA202305241131](https://openairdocs.org/sdr/FDEA202305241131.md): Frame · cracked · May 24, 2023 · N597FE · Doug MD11F · Fuselage Main, Attach Fittings
  > TAIL CONE FWD SECTION."FWD END" APPROX. 3-O CLOCK POSITION GUIDE PIN ATTACHING STRUCTURE (FRAME) CRACKED. "MARKED" REPAIRED PER SRM 53-80-07-2R REPAIR 1 FIG 201 SHEET 1.
- [SDR FDEA202305241069](https://openairdocs.org/sdr/FDEA202305241069.md): Shim · damaged · May 24, 2023 · N597FE · Doug MD11F · Wing Main, Frame Structure
  > #3 PYLON AFT BULKHEAD TO UPPER SPAR CHORD ANGLE T/E SHIM HAS MIGRATED OUT OF POSITION. (MKD) WORK WITH N/R 641 LOOSE BOLTS NOTE: THESE LOOSE BOLTS MAY REQUIRE REMOVAL FOR NDT CHECK FOR CONDITION OF HOLES PRIOR TO REPLACEMENT. 0000098319: NAVARRO, ENRIQU
- [SDR FDEA202305240987](https://openairdocs.org/sdr/FDEA202305240987.md): Skin · cracked · May 24, 2023 · N597FE · Doug MD11F · Fuselage Main, Structure
  > RH AIR COND COMPT OPENING EXTERNAL STRUCTURE - AFT UPPER CORNER - VISUAL INDICATION FROM PAINT OF SKIN CRACK EMINATING THRU 2EA. RIVETS - NDT HFEC INSPECTION CONFIRMED INDICATIONS. REPAIRED AFT UPPER CORNER SKIN AT RH AIR COND COMPT,REF MD-11 SRM 53-20-15
- [SDR FDEA202305240931](https://openairdocs.org/sdr/FDEA202305240931.md): Floorboard · damaged · May 24, 2023 · N597FE · Doug MD11F · Fuselage Floor Panel
  > CTR CARGO FLOORBOARD 183EB HAS EVIDENCE OF IMPACT DAMAGE FABRICATED FLOORBOARD 183EB REF FEDEX DWG SRZ-25-005 MAJOR REPAIR
- [SDR FDEA202305221228](https://openairdocs.org/sdr/FDEA202305221228.md): Spar Cap · corroded · May 22, 2023 · N597FE · Doug MD11F · Wing Spar
  > LEFT WING -- LOWER REAR SPAR AT XORS 1048 HAS CORROSION REMOVED CORROSION AND REPAIRED LH WING LOWER REAR SPAR AT XORS 1048 PER SRM SRM 57-00-00-2R FIG.202 SHT.3 AND EA T 1-5710-T0374723 WING - BASIC WING STRUCTURE - LH WING REAR SPAR LOWER CAP XORS 1042
- [SDR FDEA202305201047](https://openairdocs.org/sdr/FDEA202305201047.md): Skin · corroded · May 20, 2023 · N597FE · Doug MD11F · Wing, Plate/Skin
  > MAIN DECK, CENTER TANK, TOP SKIN AT STA 1275 AND RBL 106 HAS CORROSION MARKED #2 BLENDED AND REMOVED CORROSION IAW 51-21-01-0G. APPLIED DOUBLER REPAIR OVER BLEND OUT AREA IAW EA# 1- 5730-T0374766
- [SDR FDEA202305191163](https://openairdocs.org/sdr/FDEA202305191163.md): Spar · corroded · May 19, 2023 · N597FE · Doug MD11F · Wing Spar
  > LEFT WING REAR SPAR AT APPROX XORS 1042 HAS 3 SPOTS OF CORROSION MARKED #6 #7 #8. BLENDED CORROSION AND REWORKED SPAR REF E.A. #1-5710-T0374802 TITLE: WING-LH OUTER WING-REAR SPAR BETWEEN XORS1030 TO XORS 1045-REWORK.
- [SDR FDEA202305161075](https://openairdocs.org/sdr/FDEA202305161075.md): Skin · delaminated · May 16, 2023 · N597FE · Doug MD11F · Wing Main, Frame Structure
  > RIGHTHAND WING; TRAILING EDGE XW=899 OB OF OB AILERON 4" MODERATE CORROSION @ WING EDGE. MARKED REPAIRED TRAILING EDGE XW=899 FOUND APPROX 4" BY 2" AREA OF DELAMINATION AS REQ REF 51-43-01-0G PG 6 PAR 10
- [SDR FDEA202212212976](https://openairdocs.org/sdr/FDEA202212212976.md): Brake Disc · deteriorated · Dec 21, 2022 · N597FE · Doug MD11F · Landing Gear Brake System
  > LEVEL 1 BRAKE DIFF TEMP AFTER TAKEOFF. #3 TEMP 59 AND #4 TEMP 395. AFTER LANDING AT THE GATE, MAINTENANCE ADVISED #4 BRAKE GLOWING RED HOT. AIRCRAFT CHOCKED AND BRAKES RELEASED. REMOVED #4 TIRE,INSPECTED #4 BRAKE FOUND CARBON DISKS DISNITEGRATED AND
- [SDR FDEA202210252657](https://openairdocs.org/sdr/FDEA202210252657.md): Warning Message · false activation · Oct 25, 2022 · N597FE · Doug MD11F · Landing Gear Position and Warning
  > UNSAFE CENTER GEAR INDICATION ON BOTH GEAR LIGHTS AND SYNOPTIC ON INITIALLY LOWER THE GEAR. RECYCLED TO GEAR HANDLE AND GOT 4 GREEN ON BOTH SYNOPTIC AND GEAR LIGHTS. REMOVED AND REPLACED CENTER LANDING GEAR DOWNLOCKCYLINDER RESTRICTOR PER MD-11 AMM 32-38-0
- [SDR FDEA202209092259](https://openairdocs.org/sdr/FDEA202209092259.md): Line · leaking · Sep 9, 2022 · N597FE · Doug MD11F · Hydraulic System, Main
  > HYD 2 FAIL LEVEL 2 ALERT APPROXIMATELY 5:45 INTO FLIGHT. HYDRAULIC SYSTEM 2 QUANTITY DECREASED RAPIDLY TO ZERO. QRH PROCEDURE COMPLETED ***EMERGENCY DECLARED*** FOUND LEAK COMING FROM LINE FROM #2 ENGINE HYD MANIFOLD "PRESS IN LWR PUMP" REPLACED LINE
- [SDR FDEA202206261564](https://openairdocs.org/sdr/FDEA202206261564.md): Brake Assy · delaminated · Jun 26, 2022 · N597FE · Doug MD11F · Brake
  > MDIS 597 32-40 5376 26JUN22 STN FACT U ON POST FLIGHT INSPECTION FOUND NUMBER 10 BRAKE ASSY FAILED. BRAKE DISCS FAILED (SPLINTERED). R/I 26JUN22 01:47 STN U REASON CODE: PREMATURE REMOVAL/INSTALLATION OFF MPN: 2609472-4B
- [SDR FDEA202204130973](https://openairdocs.org/sdr/FDEA202204130973.md): Attach Fitting · cracked · Apr 13, 2022 · N597FE · Doug MD11F · Wing, Control Surfaces
  > FOUND CRACK 1.75 INCHS LONG ON I/B UPPER WINGLET L/E ATTACH FLANGE ON RIGHT-HAND WING REPAIR IAW EA 1-5750-T0368013 PART 1
- [SDR FDEA202204130960](https://openairdocs.org/sdr/FDEA202204130960.md): Fairing · chafed · Apr 13, 2022 · N597FE · Doug MD11F · Wing Miscellaneous Structure
  > RH WINGLET LOWER FAIRING 628XW HAS SIGNS OF WIND EROSION 0000355851: MITROVICH, DAVID T - 14-APR-2022 23:27 REPAIRED R/W WINGLET LOWER PANEL REF: MD11 SRM 51-62-01. REPAIRED METALIZED COATING REF: MD11 SRM 51-43-06-0G. PREPPED & PAINTED REF: MD11 AMM 51-22
- [SDR FDEA202203010442](https://openairdocs.org/sdr/FDEA202203010442.md): Fitting · corroded · Mar 1, 2022 · N597FE · Doug MD11F · Wing Miscellaneous Structure
  > SMIS 597 57-20 5046 05MAR22 MEM FACT U MOD TYPE T MOD NO. 1-5720-T0367318 REV NO. A PS P1 WING - SECONDARY WING STRCT - R/H MLG TRUNNION UPPER / LOWER PAD WHERE A-FRAME COMPLY WITH E..A. 1-5720-T0367318 REV NO. A POS P11 INFO 06MAR22 00:27
- [SDR FDEA202111022722](https://openairdocs.org/sdr/FDEA202111022722.md): Fuel Tank · corroded · Nov 2, 2021 · N597FE · Doug MD11F · Fuel Storage
  > MAIN DECK CARGO COMPARTMENT - CABIN, FOUND CENTRE WING TANK TOP SURFACE AT STATION 1224, X = 7 TO X = -7 CORRODED. MAIN DECK CARGO COMPARTMENT - CABIN AT CENTER WING TANK TOP SURFACE STATION 1224, X = 7 TO X = - 7 CORRODED AREA REPAIRED AS PER E.A.#: 1-
- [SDR FDEA202110192571](https://openairdocs.org/sdr/FDEA202110192571.md): Doubler · none · Oct 19, 2021 · N597FE · Doug MD11F · Wing, Plate/Skin
  > WORK ORDER 69707 SPECIAL/NONROUTINE MAINTENANCE FORM NUMBER N00331 MAJOR REPAIR, REQUIRED INSPECTION ITEM, JOB PROGRESS FORM ITEMS 3 TO 4 AND 8 TO 11 DO NOT HAVE REQUIRED INSPECTION ITEM BLOCK MARKED. EXISTING REPAIR REMOVED AT LEFT HAND WING FIXED LEADIN
- [SDR FDEA202110192570](https://openairdocs.org/sdr/FDEA202110192570.md): Doubler · unknown · Oct 19, 2021 · N597FE · Doug MD11F · Wing, Plate/Skin
  > WORK ORDER 69707 SPECIAL/NONROUTINE MAINTENANCE FORM NUMBER N00328 MAJOR REPAIR, REQUIRED INSPECTION ITEM, JOB PROGRESS FORM ITEMS 4 TO 5 AND 7 TO 10 DO NOT HAVE REQUIRED INSPECTION ITEM BLOCK MARKED. EXISTING DOUBLER REMOVED AS PER SRM 51-33-01-0G AT LEF
- [SDR FDEA202110192569](https://openairdocs.org/sdr/FDEA202110192569.md): Doubler · unknown · Oct 19, 2021 · N597FE · Doug MD11F · Wing, Plate/Skin
  > WORK ORDER 69707 SPECIAL/NONROUTINE MAINTENANCE FORM NUMBER N00585 MAJOR REPAIR, REQUIRED INSPECTION ITEM, JOB PROGRESS FORM ITEMS 2 TO 6 DO NOT HAVE REQUIRED INSPECTION ITEM BLOCK MARKED. REMOVED EXISTING DOUBLER AT LEFT HAND WING FIXED LEADING EDGE LOWE
- [SDR FDEA202110182565](https://openairdocs.org/sdr/FDEA202110182565.md): Track · unknown · Oct 18, 2021 · N597FE · Doug MD11F · Fuselage Floor Panel
  > WORK ORDER 69707 SPECIAL/NONROUTINE MAINTENANCE FORM NUMBER N00518 MAJOR REPAIR, REQUIRED INSPECTION ITEM. JOB PROGRESS FORM ITEMS 5 TO 8 DO NOT HAVE REQUIRED INSPECTION ITEM BLOCK MARKED. EXISTING SEAT TRACK REPAIR SECTION REMOVED AT EXISTING SPLICES STA
- [SDR FDEA202110142533](https://openairdocs.org/sdr/FDEA202110142533.md): Fuel Cell · corroded · Oct 14, 2021 · N597FE · Doug MD11F · Fuel Storage
  > MAIN DECK CARGO COMPARTMENT FOUND CENTRE WING TANK TOP SURFACE AT STATION 1228, X = 7 TO X = - 7 CORRODED. MAIN DECK CARGO COMPARTMENT - CABIN AT CENTER WING TANK TOP SURFACE STATION 1228 X = 7 TO X= - 7 CORRODED AREA REPAIRED AS PER E.A.#: 1-5730-T036478
- [SDR FDEA202110142534](https://openairdocs.org/sdr/FDEA202110142534.md): None · none · Oct 14, 2021 · N597FE · Doug MD11F · Fuselage Main, Plate/Skin
  > AGING AIRCRAFT - EXISTING REPAIR EXTERNAL DOUBLERS AT FUSELAGE SKIN STATION 285 Z=- 33. EXISTING REPAIR EXTERNAL DOUBLERS AT FUSELAGE SKIN STATION 285 Z=-33 RIGHT HAND SIDE EVALUATED AND FOUND REPAIR DEVIATION TO SRM 53-00-01-2R REPAIR 1 FIGURE 201 CLASS

Next page: https://openairdocs.org/aircraft/N597FE/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 = 'N597FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N597FE/reports

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