# Service difficulty reports: N359FE, cancelled Mar 2, 2024

A list on [N359FE, cancelled Mar 2, 2024](https://openairdocs.org/deregistered/N359FE-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 · 94 reports

- [SDR FDEA202012173172](https://openairdocs.org/sdr/FDEA202012173172.md): Switch · failed · Dec 17, 2020 · N359FE · Doug MD1010F · Pneumatic System
  > DURNING CRUISE AFTER TURNING OFF WING ICE THE RED MANF LIGHT ILLUMINATED ON #3 WITH ASSOCIATED "MAN 3 FAIL" LEVEL 1 ALERT. FOUND PRESSURE SWITCH FAULT BALL DROPPED IN WINDOW ON PNEUMATIC MANIFOLD FAULT INDICATOR. RESET FAULT BALL. SUPPLIED PNEUMATIC AIR USIN
- [SDR FDEA202009022081](https://openairdocs.org/sdr/FDEA202009022081.md): Transducer · failed · Sep 2, 2020 · N359FE · Doug MD1010F · Landing Gear Position and Warning
  > PDIS 359, 2-44, 6863, 02SEP20, ORD OPEN U. LEVEL 2 ANTI-SKID L FAIL, SHGN 02SEP20 03:09. ORD U CREW ENTERED WRI 32-44/6864 (EMERGENCY DECLARED) DUE TO LEVEL 2 ANTI-SKID L FAIL. FAILED TO ENTER IN ORIGINAL PDIS WRITEUP SO UPDATING HERE. MEL 02SEP20 05:15 O
- [SDR FDEA202008071779](https://openairdocs.org/sdr/FDEA202008071779.md): Frame · cracked · Jul 28, 2020 · N359FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > BS 1159 AFT UPPER LT CORNER STRUCTURE SUSPECTED CRACK MWT REPAIRED PER FEDEX EA 8-5310-T03555599 PART 1. INSTALLED REPAIR DOUBLERS.
- [SDR FDEA2020080581769](https://openairdocs.org/sdr/FDEA2020080581769.md): Web · cracked · Jul 28, 2020 · N359FE · Doug MD1010F · Fuselage Main, Structure
  > CLG WHEEL WELL SIDE WALL HAS A CRACK IN THE AFT LEFT CORNER. REPAIRED CLG WHEEL WELL SIDE WALL CRACK IN ACCORDANCE WITH EA 8-5330-T0355551. INSTALLED REPAIR DOUBLER.
- [SDR FDEA202002140338](https://openairdocs.org/sdr/FDEA202002140338.md): Throttle · malfunctioned · Feb 14, 2020 · N359FE · Doug MD1010F · Power Lever
  > PDIS 359 76-10 6450 14FEB20 ONT OPEN U LOGPAGES:3200450 DURING DESCENT NUMBER 2 THROTTLE WOULD NOT DECREASE BELOW APPROXIMATELY 71% N1. DURING ATTEMPTED THROTTLE MOVEMENTS IN AUTO AND MANUAL THROTTLE NUMBER 2 THROTTLE WOULD ADVANCE ON IT'S O
- [SDR FDEA201903190681](https://openairdocs.org/sdr/FDEA201903190681.md): Fire Warning · false activation · Mar 19, 2019 · N359FE · Doug MD1010F · Fire Detection
  > UPON ARRIVAL AFTER A/C WAS PARKED AT GATE WAS NOTIFIED BY FLT CREW THEY HAD A FIRE INDICATION IN THE FWD LWR CARGO COMPT BUT DID NOT DISCHARGE FIRE BOTTLE. HAVE FWD AGENT DISCH LIGHT FLASHING ON OVER HEAD PNL ALSO HAVE ON AIR PAGE DISCH CARGO AGENT. INSP'D LWR
- [SDR FDEA201903180670](https://openairdocs.org/sdr/FDEA201903180670.md): Latch · out of adjust · Mar 18, 2019 · N359FE · Doug MD1010F · Landing Gear Door Retract Section
  > AFTER LEVEL OFF AT FL 350 THE RIGHT MAIN PRIMARY AND SECONDARY INDICATIORS WENT RED WITH GEAR HANDLE UP. RAN QRH AND ALL LITES WERE GREEN WITH HANDLE DOWN. WHEN HANDLE RAISED IAW QRH LIGHTS ILLUMINATED. LIGHTS REMAINED ON WITH HANDLE UP UNTIL DESCENDING T
- [SDR FDEA201812213593](https://openairdocs.org/sdr/FDEA201812213593.md): Shear Tie · corroded · Dec 21, 2018 · N359FE · Doug MD1010F · Fuselage Internal Mounting Structure
  > FWD CARGO BILGE STA 825 49R TO 50R CORRODED SHEAR CLIP. REMOVED AND REPLACED SHEAR CLIP AT STA 825 STR 49R TO 50R IAW SRM 51-31-01. CORROSION FOUND OUT OF LIMITS IAW SRM 51-40-02. MAJOR REPAIR
- [SDR FDEA201812213592](https://openairdocs.org/sdr/FDEA201812213592.md): Shear Tie · corroded · Dec 21, 2018 · N359FE · Doug MD1010F · Fuselage Internal Mounting Structure
  > FWD CARGO BILGE AREA AT STA 808 SHEAR CLIP SECTON CORRODED AND ANGLE. REMOVED CORROSION FROM SHEAR CLIP AND ANGLE CLIP FOUND TO BE OUT OF LIMITS IAW SRM 51-40-02. REMOVED AND REPLACED BOTH SHEAR CLIPS AND ANGLE CLIP AT STA 808 48R TO 47R IAW SRM 51-31-01.
- [SDR FDEA2018122103586](https://openairdocs.org/sdr/FDEA2018122103586.md): Skin · chafed · Dec 20, 2018 · N359FE · Doug MD1010F · Cargo/Baggage Doors
  > LOWER FWD CARGO DOOR AFT FRAME SIDEWALL HAS CHAFE MARK. REMOVED AND REPLACED DOUBLER AND TRIPLER PER SRM 53-50-00. CAT "A" MAJOR REPAIR
- [SDR FDEA2018122103585](https://openairdocs.org/sdr/FDEA2018122103585.md): Floor Support · corroded · Dec 20, 2018 · N359FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > WASTE TANK COMPARTMENT STA 2007 CEILING AREA BL0 FLOOR STRUCTURE HAS CORROSION REMOVED FLOOR SUPPORT IAW SRM 51-31-01. CHECK LIMITS. EXCEEDS 10% ALLOWABLE DAMAGE IAW SRM 53-00-01 FIG 1A. LOCATED AND DRILLED NEW FLOOR SUPPORT P/N WSP0711-543 BATCH # 00033
- [SDR FDEA2018122103584](https://openairdocs.org/sdr/FDEA2018122103584.md): Skin · corroded · Dec 20, 2018 · N359FE · Doug MD1010F · Fuselage Main, Plate/Skin
  > WASTE TANK COMPARTMENT STA 1997-2007 LONGERON 46R - 47R FUSELAGE SKIN HAS CORROSION REMOVED CORROSION IAW SRM 53-20-00 FIG 4 OUT OF LIMITS FABRICATED AND INSTALLED DOUBLER REPAIR. IAW SRM 53-20-00 FIG 4 AT STA 1997 - 2007. CAT "A" MAJOR REPAIR.
- [SDR FDEA2018122103583](https://openairdocs.org/sdr/FDEA2018122103583.md): Seat Track · gouged · Dec 20, 2018 · N359FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK COMPARTMENT STA 1191-1531 SEAT TRACK X=75.25 HAS SCRATCHES AND GOUGES AS MARKED. REPAIRED MAIN DECK COMPARTMENT STA 1191 - 1531 X= 75.25 IAW SRM 53-70-00 FIG 1. (SEAT TRACK REPLACED). MAJOR REPAIR
- [SDR FDEA2018122193562](https://openairdocs.org/sdr/FDEA2018122193562.md): Chain · missing · Dec 19, 2018 · N359FE · Doug MD1010F · Passenger/Crew Doors
  > L1 DOOR EMERGENCY PNEUMATIC ACTUATION CHECK FAILED. FOUND L1 EMERGENCY AIR MOTOR CHAIN MISSING. REPLACED CHAIN IAW CMM 52-11-09. PNEUMATIC TEST CHECK GOOD IAW AMM 52-10-01-2
- [SDR FDEA201812153508](https://openairdocs.org/sdr/FDEA201812153508.md): Seat Track · cracked · Dec 15, 2018 · N359FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > AFT CARGO SEAT TRACK UPPER SURFACE HAS SCRATCHES, GOUGES, AND CORROSION AS MARKED. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-31-01 CAT "A" MAJOR REPAIR. SEAT TRACK FOUND OUT OF LIMITS FOR CRACK.
- [SDR FDEA201812083481](https://openairdocs.org/sdr/FDEA201812083481.md): Seat Track · gouged · Dec 8, 2018 · N359FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CARGO SEAT TRACK AT STA 999 POSITION X=-47.5 HAS MULTIPLE GOUGES. REMOVED DAMAGE ON SEAT TRACK STA 999 X= -47.5 IAW SRM 53-70-00 FIG 5. CHECKED LIMITS. MAXIMUM MATERIAL REMOVE IS.025 AFTER REWORK MATERIAL LOSS IS.045 FOUND TO BE OUT OF LIMITS IAW SRM 53
- [SDR FDEA201812073465](https://openairdocs.org/sdr/FDEA201812073465.md): Door Sill · corroded · Dec 7, 2018 · N359FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR SILL LOWER SURFACE HAS CORROSION UNDER NUT PLATES 5 PLACES. REMOVED AND REPLACED AFT CARGO DOOR SILL LOWER SURFACE IAW SRM 51-31-01 AND SRM 51-35-01. MAJOR REPAIR.
- [SDR FDEA201811123184](https://openairdocs.org/sdr/FDEA201811123184.md): Fire · detected · Nov 12, 2018 · N359FE · Doug MD1010F · APU Core Engine
  > APU TAIL PIPE FIRE. SMOKE REPORTED BY OTHER AIRCRAFT. FIRE CRASH RESCUE INSPECTED AND FOLLOWED BACK TO RAMP. AFTER BLOCK IN AND CREW DEBRIEF INSPECTED AFT ENG AND APU COMPARTMENT. WITH NO SMOKE OR DAMAGED NOTED, BUT COULD SMELL A SMOKE ODOR. RESTARTED APU, DUR
- [SDR FDEA2018080311861](https://openairdocs.org/sdr/FDEA2018080311861.md): Pitot Tube · dirty · Jul 31, 2018 · N359FE · Doug MD1010F · Pitot/Static System
  > "SEL ELEV FEEL MAN" AND "SEL FLAP LIMIT OVRD" LVL MSGS CAME UP AFTER T/O. WE RAN AND COMPLIED WITH QRH. FO AIRSPEED WAS UNRELIABLE. FOUND BOTH CAPTAINS AND FO'S PITOT TUBES TO HAVE PLUGGED DRAIN HOLES. REMOVED AND REPLACED BOTH IAW MM 34-11-02-2. ALSO REF EA
- [SDR FDEA201806121463](https://openairdocs.org/sdr/FDEA201806121463.md): Power Supply · failed · Jun 12, 2018 · N359FE · Doug MD1010F · Emergency Lighting
  > EMER LT BAT 1 LO. T/S USING FIM 33-50-00-810 FOUND EMERG PWR SUPPLY AT FAULT. REMOVED AND REPLACED PWR SUPLY IAW MM 33-51-01-4 AND OPS CHECK PER 33-51-01-5 OPS VERIFED NORMAL. A/C OK FOR SERVICE.
- [SDR FDEA201611043826](https://openairdocs.org/sdr/FDEA201611043826.md): Skin · nicked · Nov 4, 2016 · N359FE · Doug MD1010F · Trailing Edge Flaps
  > LEFT WING INBD FLAP LOWER SURFACE NICKED. REPAIRED LOWER FLAP SKIN IAW SRM 57-10-00 FIG 85. MAJOR REPAIR.
- [SDR FDEA201610293752](https://openairdocs.org/sdr/FDEA201610293752.md): Longeron · corroded · Oct 29, 2016 · N359FE · Doug MD1010F · Fuselage Main, Longeron/Stringer
  > MAIN DECK AREA LEFT SIDE BETWEEN STATION 1381-1401 STRINGER 17L LONGERON HAS CORROSION. LONGERON FOUND OUT OF LIMITS IAW SRM VOL I 53-00-01 FIG 1B. REMOVED AND REPLACED LONGERON IAW SRM VOLII 51-31-01 AND 51-33-01 AND DRAWING AEA 0220-1. LONGERON FABRICATED
- [SDR FDEA201610293751](https://openairdocs.org/sdr/FDEA201610293751.md): Longeron · corroded · Oct 29, 2016 · N359FE · Doug MD1010F · Fuselage Main, Longeron/Stringer
  > MAIN DECK AREA LEFT SIDE BETWEEN STATION 1401-1421 STRINGER 19L LONGERON HAS CORROSION. LONGERON FOUND OUT OF LIMITS IAW SRM VOL I 53-00-01 FIG 1B. REMOVED AND REPLACED LONGERON IAW SRM VOL II 51-33-01 AND 51-31-01 AND DRAWING AEA0222. LONGERON FABRICATED O
- [SDR FDEA201610293750](https://openairdocs.org/sdr/FDEA201610293750.md): Floor Panel · delaminated · Oct 29, 2016 · N359FE · Doug MD1010F · Fuselage Floor Panel
  > MAIN DECK CARGO BS 1501, RBL 68 FLOOR PANEL DELAMINATED & DENTED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.
- [SDR FDEA201610273710](https://openairdocs.org/sdr/FDEA201610273710.md): Longeron · corroded · Oct 27, 2016 · N359FE · Doug MD1010F · Fuselage Main, Longeron/Stringer
  > MAIN DECK AREA, LT SIDE BETWEEN BS 1321 AND 1341 LONGERON 17L HAS CORROSION. REMOVED THE CORROSION IAW SRM 51-21-01 VOL II. FOUND OUT OF LIMITS IAW SRM 51-00- 01 VOL I. REMOVED AND REPLACED THE LONGERON IAW SRM 51-31-01 VOL II. MAJOR REPAIR.
- [SDR FDEA201610273709](https://openairdocs.org/sdr/FDEA201610273709.md): Floorbeam · corroded · Oct 27, 2016 · N359FE · Doug MD1010F · Fuselage Main, Floor Beam
  > BROKEN NUTPLATES AND CORROSION UNDER NUTPLATES AT AFT CARGO FLOORBEAM UPPER TEE BS 1841 LT TO RT END. REMOVED CORROSION IAW SRM 51-00-01. AND FOUND TO BE OUT OF LIMITS. FABRICATED A REPAIR IAW SRM 53-00-01 FIG. 7. INSTALLED THE REPAIR IAW SRM 51-31-01. MAJOR R
- [SDR FDEA201609273382](https://openairdocs.org/sdr/FDEA201609273382.md): Fire Warning · false activation · Sep 27, 2016 · N359FE · Doug MD1010F · Fire Detection
  > DURING ENGINE SHUTDOWN WE RECEIVED A FIRE WARNING IN THE LOWER FORWARD CARGO COMPARTMENT. FIRED THE AGENT. THERE WAS NO EVIDENCE OF A FIRE/SMOKE IN THE FWD LOWER COMPARTMENT. THERE WAS A OVERVOLTAGE MSG IN THE EPCU CURRENT FAULTS. FIREX DISCHARGE SQUIB MPN
- [SDR FDEA201602260689](https://openairdocs.org/sdr/FDEA201602260689.md): Skin · cracked · Feb 26, 2016 · N359FE · Doug MD1010F · Fuselage Main, Plate/Skin
  > DURING WALK AROUND, FOUND WHAT APPEARS TO BE 1/2 CRACK & PUNCTURE IN FUSELAGE, LOCATED ABOUT 8 FEET AFT OF AFT LOWER CARGO DOOR. CRACK & PUNCTURE IS PROTRUDING OUTWARD. REMOVED CORROSION DAMAGE IAW SRM 53-20-00. REQUIRES HFEC OF CUT OUT AREA TO INSURE ALL D
- [SDR FDEA201512174025](https://openairdocs.org/sdr/FDEA201512174025.md): Fire Warning · false activation · Dec 17, 2015 · N359FE · Doug MD1010F · Fire Detection
  > DURING COCKPIT SET UP, HAD FWD AGENT DISCHARGE LIGHT FLASHING ALONG WITH DISCHARGE AGENT ON EAD, FOLLOWED BY FIRE ALERT. FIRED BOTH BOTTLES, ACFT WAS LOADED UNABLE TO VERIFY. TROUBLE SHOT & FOUND THAT THE MSC SOFTWARE HAD GLITCHED. PULLED & RESET CB'S FOR M
- [SDR FDEA201502210574](https://openairdocs.org/sdr/FDEA201502210574.md): Panel · damaged · Feb 21, 2015 · N359FE · Doug MD1010F · Passenger/Crew Doors
  > SMALL DAMAGE, APPROX 1.5" X 1.5", FOUND ON UPPER AFT SIDE OF COVER PANEL INSIDE OF L1 DOOR. REPAIRED DAMAGE TO L1 DOOR COVER.
- [SDR FDEA201411073567](https://openairdocs.org/sdr/FDEA201411073567.md): Fuse · cracked · Nov 7, 2014 · N359FE · Doug MD1010F · Hydraulic System, Main
  > HYD 3 FAIL LEVEL 2 AFTER GEAR DOWN ON APPROACH, ALL HYD FLUID EMPTIED & LEAKED FROM HYD SYS 3 AFTER GEAR LOWERED. PUMPS NOT TURNED OFF. R & R TRIM CYLINDER INTERLOCK FUSE IAW AMM32-31-06-2.
- [SDR FDEA201410123128](https://openairdocs.org/sdr/FDEA201410123128.md): Seat Track · damaged · Oct 12, 2014 · N359FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK SEAT TRACK AT STATION 1140 RBL 48 HAS DAMAGE. R & R NEW SEAT TRACK IAW SRM 53-70-00 FIG 2.
- [SDR FDEA201410072994](https://openairdocs.org/sdr/FDEA201410072994.md): Longeron · corroded · Oct 7, 2014 · N359FE · Doug MD1010F · Fuselage Main, Longeron/Stringer
  > MAIN DECK RT SIDEWALL STATION 1401 - 1421 L17 LONGERON HAS EXFOLIATION CORROSION. REPLACED LONGERON AEA0220-521 IAW DWG AZA0220.
- [SDR FDEA201410072993](https://openairdocs.org/sdr/FDEA201410072993.md): Longeron · corroded · Oct 7, 2014 · N359FE · Doug MD1010F · Fuselage Main, Longeron/Stringer
  > MAIN DECK RT SIDEWALL STATION 1361 - 1381 L17 LONGERON HAS EXFOLIATION CORROSION. REPLACED LONGERON AEA 0220-503 IAW DWG AZA0220.
- [SDR FDEA201410042960](https://openairdocs.org/sdr/FDEA201410042960.md): Longeron · corroded · Oct 4, 2014 · N359FE · Doug MD1010F · Fuselage Main, Longeron/Stringer
  > MAIN DECK RT SIDEWALL STATION 1441 - 1461 L17 LONGERON HAS EXFOLIATION CORROSION. INSTALLED LONGERON IAW DWG AEA0220, REPLACED LONGERON.
- [SDR FDEA201410042959](https://openairdocs.org/sdr/FDEA201410042959.md): Longeron · corroded · Oct 4, 2014 · N359FE · Doug MD1010F · Fuselage Main, Longeron/Stringer
  > MAIN DECK RT SIDEWALL STATION 1381 - 1401 L17 LONGERON HAS EXFOLIATION CORROSION. INSTALLED LONGERON IAW DWG AEA0220, REPLACED LONGERON.
- [SDR FDEA201410042958](https://openairdocs.org/sdr/FDEA201410042958.md): Longeron · corroded · Oct 4, 2014 · N359FE · Doug MD1010F · Fuselage Main, Longeron/Stringer
  > MAIN DECK RT SIDEWALL STATION 1461 - 1481 L17 LONGERON HAS EXFOLIATION CORROSION. INSTALLED LONGERON IAW DWG AEA0220, REPLACED LONGERON.
- [SDR FDEA201410032947](https://openairdocs.org/sdr/FDEA201410032947.md): Bracket · cracked · Oct 3, 2014 · N359FE · Doug MD1010F · Fuselage Main, Attach Fittings
  > LEFT LG WELL HYD LINE SUPPORT, CRACK IS EMANATING FROM MOUNT BOLT LOCATED FWD OF THE GEAR STRUT UP STOP. REMOVED CRACKED BRACKET & INSTALLED A NEW SERVICEABLE BRACKET IAW SRM 51-31-01 VOL II.
- [SDR FDEA201409302872](https://openairdocs.org/sdr/FDEA201409302872.md): Structure · cracked · Sep 30, 2014 · N359FE · Doug MD1010F · Nacelle/Pylon Miscellaneous Structure
  > NUMBER 2 ENG INLET NOSE COWL CRACKED AT INNER STRUCTURE BETWEEN 3 & 4 O'CLOCK POSITION. R & R NOSE COWL IAW AMM 54-22-01-2.
- [SDR FDEA201409272826](https://openairdocs.org/sdr/FDEA201409272826.md): Web · cracked · Sep 27, 2014 · N359FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > CENTER CARGO BS 1841, RT WEB HAS SMALL CRACK. REMOVED, FABRICATED & INSTALLED NEW WEB.
- [SDR FDEA201409242745](https://openairdocs.org/sdr/FDEA201409242745.md): Longeron · corroded · Sep 24, 2014 · N359FE · Doug MD1010F · Fuselage Main, Longeron/Stringer
  > MAIN DECK RT SIDEWALL LONGERON 17, EACH FRAME BAY HAS A SEPARATE LONGERON, CORRODED, A TOTAL OF 10 LONGERONS FROM STATION 1159 TO 1481. REMOVED CORROSION WITHIN LIMITS PER SRM 53-00-01 FIG 1B AND REPLACED LONGERONS THAT EXCEEDED LIMITS IAW BLUEPRINT SPECIFIC
- [SDR FDEA201409232744](https://openairdocs.org/sdr/FDEA201409232744.md): Skin · gouged · Sep 23, 2014 · N359FE · Doug MD1010F · Leading Edge Devices
  > LEFT WING NR 4 SLAT LOWER TE SURFACE HAS DEEP GOUGE BY NR 9 TRACK. REPAIRED GOUGE IAW SRM 57-00-01 FIGURE 4 SHEET 2.
- [SDR FDEA201409212697](https://openairdocs.org/sdr/FDEA201409212697.md): Frame · corroded · Sep 21, 2014 · N359FE · Doug MD1010F · Fuselage Main, Frame
  > FORWARD CARGO BILGE CORROSION AT BS 970 STRINGER 51L. REMOVED AND REPLACED THE FRAME IAW DWG ADA0078 AND SRM 53-10-00 FIG. 2 VOL 1.
- [SDR FDEA201409202691](https://openairdocs.org/sdr/FDEA201409202691.md): Longeron · corroded · Sep 20, 2014 · N359FE · Doug MD1010F · Fuselage Main, Longeron/Stringer
  > FORWARD CARGO BILGE BS 979 LONGERON 51L HAS CORROSION. REPAIRED LONGERON 51L IAW SRM 53-10-00 FIG 2 VOL 1
- [SDR FDEA201409192677](https://openairdocs.org/sdr/FDEA201409192677.md): Longeron · corroded · Sep 19, 2014 · N359FE · Doug MD1010F · Fuselage Main, Longeron/Stringer
  > MAIN DECK BS 1481 - 1501 LONGERON 18R HAS CORROSION. REMOVED CORROSION WITHIN LIMITS IAW SRM 53-00-01 FIG 1B
- [SDR FDEA201409182661](https://openairdocs.org/sdr/FDEA201409182661.md): Frame · corroded · Sep 18, 2014 · N359FE · Doug MD1010F · Fuselage Main, Frame
  > CENTER CARGO BILGE FRAME HAS CORROSION AT BS 1781 JUST ABOVE LONGERON 45R, BENEATH AFT END OF ROLLER TRAY. REPAIRED IAW SRM 53-60-01 AND SRM 53-60-01.
- [SDR FDEA201409182662](https://openairdocs.org/sdr/FDEA201409182662.md): Frame · corroded · Sep 18, 2014 · N359FE · Doug MD1010F · Fuselage Main, Frame
  > CENTER CARGO BILGE FRAME HAS CORROSION AT BS 1841 JUST ABOVE LONGERON 46L. REMOVED CORROSION IAW SRM 51-21-01, VOL II
- [SDR FDEA201409182666](https://openairdocs.org/sdr/FDEA201409182666.md): Skin · corroded · Sep 18, 2014 · N359FE · Doug MD1010F · Fuselage Main, Plate/Skin
  > AFT CARGO BAY BILGE BS 1841, SKIN HAS A LIGHT SURFACE CORROSION AROUND FINGER DOUBLER BETWEEN L47-48R. CLEANED CORROSION IAW SRM 51-21-01 VOL II. PERFORMED UT NDT INSPECTION & VERIFIED REMAINING MATERIAL THICKNESS FOUND TO BE WITHIN IAW SRM 53-20-00 VOL 1.
- [SDR FDEA201409182665](https://openairdocs.org/sdr/FDEA201409182665.md): Skin · corroded · Sep 18, 2014 · N359FE · Doug MD1010F · Fuselage Main, Plate/Skin
  > AFT CARGO BAY BILGE, CORROSION FOUND BETWEEN LONGERON 47-48R BS 1841. CLEANED & TREATED SURFACE CORROSION IAW SRM 51-21-01 VOL II. PERFORMED UT NDT & VERIFIED REMAINING MATERIAL FOUND TO BE WITHIN LIMITS IAW SRM 53-20-00 VOL 1 FIG 13 SHEET 28.
- [SDR FDEA201404100708](https://openairdocs.org/sdr/FDEA201404100708.md): Pump · bypassing · Apr 10, 2014 · N359FE · Doug MD1010F · Pneumatic Distribution System
  > NR 2 AIR MANIFOLD FAIL ILLUMINATED AT 17,000 FT DURING CLIMB OUT WITH CLIMB POWER SET. FOLLOWED QRH PROCEDURE, LIGHT EXTINGUISHED WITH THROTTLE RETARDED BELOW 95%. PERFORMED NR 2 PNEUMATIC SYS DECAY CHECK IAW MM 36-00-01-5, SYS FAILED TEST. SHOULD BE 20 SE

Next page: https://openairdocs.org/deregistered/N359FE-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 = 'N359FE' AND deregistration_id = 'N359FE-2024-03-02'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N359FE-2024-03-02/reports

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