# Service difficulty reports: N360FE, cancelled Mar 2, 2024

A list on [N360FE, cancelled Mar 2, 2024](https://openairdocs.org/deregistered/N360FE-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 · 149 reports

- [SDR FDEA202007161537](https://openairdocs.org/sdr/FDEA202007161537.md): Sensor · malfunctioned · Jul 16, 2020 · N360FE · Doug MD1010F · Landing Gear Brake System
  > AFTER TAKEOFF, LEVEL TWO BRAKE OVER TEMP. FOLLOWED QRH, MAX TEMP 996. CLEANED CONNECTOR TEMP READING GOOD. CONNECTED TO ORIGINAL SENSOR TEMP, READING GOOD. AFTER SAFETYING TEMP READING HIGH AND ERATIC AGAIN. CHECKED RESISTANCE OF SENSOR, RESISTANCE READIN
- [SDR FDEA2020071761537](https://openairdocs.org/sdr/FDEA2020071761537.md): Sensor · false indication · Jul 16, 2020 · N360FE · Doug MD1010F · Landing Gear Brake System
  > AFTER TAKEOFF, LEVEL TWO BRAKE OVER TEMP. FOLLOWED QRH. MAX TEMP 996. DEBRIEFED CREW UPON ARRIVAL INTO IND. AFTER TAKEOFF, TEMP CLIMBED TO 999 THEN "X'ED" OUT. USED THERMAL GUN TO CHECK BRAKE TEMP AFTER BLOCK IN. BRAKE TEMP WAS 147. NO OTHER ABNORMAL IND
- [SDR FDEA202002040265](https://openairdocs.org/sdr/FDEA202002040265.md): Access Door · missing · Feb 4, 2020 · N360FE · Doug MD1010F · Cargo/Baggage Doors
  > FOUND ACCESS DOOR (152RT) ON CENTER CARGO DOOR FAIRING FOR VENT DOOR HANDLE MISSING AT BLOCK-IN. INSTALLED SERVICEABLE DOOR OPS CHECK NORMAL REF MM CHAP 52-32-00-5.
- [SDR FDEA201910292779](https://openairdocs.org/sdr/FDEA201910292779.md): Floor Support · corroded · Oct 29, 2019 · N360FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > MAIN DECK STA 1900 RBL52 FLOOR SUPPORT WSP0711-552 UNDER NUTPLATE IS CORRODED REF PREVIOUS SDR #: 18-3003 REPAIRED FLOOR SUPPORT WSP0711-552 PER EA 8-5310-T0343200 P1 "FLOOR SUPPORT DOUBLER REPAIR AT STA 1895-1900" MAJOR REPAIR
- [SDR FDEA2019122089831](https://openairdocs.org/sdr/FDEA2019122089831.md): Engine · overtemp · Aug 9, 2019 · N360FE · Doug MD1010F · Engine (Turbine/Turboprop)
  > PDIS 360 77-20 6391 09AUG19 MEM OPEN U LOGPAGES:2977480 APPROXIMATELY 500 FEET AFTER TAKEOFF. WE RECEIVED A LEVEL 1 ENG 1 EXEEDANCE. TEMP SHOWED 1010?, THROTTLE 1 WAS PULLED BACK AND TEMP DECREASED INTO A NORMAL RANGE. WAS OVERTEMP FOR APPROX
- [SDR FDEA2019081291831](https://openairdocs.org/sdr/FDEA2019081291831.md): Engine · failed · Aug 9, 2019 · N360FE · Doug MD1010F · Engine (Turbine/Turboprop)
  > APPROXIMATELY 500 FEET AFTER TAKEOFF. WE RECEIVED A LEVEL 1 ENG 1 EXEEDANCE. TEMP SHOWED 1010, THROTTLE 1 WAS PULLED BACK AND TEMP DECREASED INTO A NORMAL RANGE. WAS OVERTEMP FOR APPROXIMATELY 2 SEC. ENGINE OPERATED NORMAL FOR THE REMAINDER OF FLIGHT RET
- [SDR FDEA201812213588](https://openairdocs.org/sdr/FDEA201812213588.md): Slat System · malfunctioned · Dec 21, 2018 · N360FE · Doug MD1010F · Leading Edge Slat Control System
  > PDIS 360 27-80 5760 21DEC18 SAN FACT U LOGPAGES:3057986 ON APPROACH WITH FLAPS 50, FULLY COFIGURED AT 2000' A/C SLOWING ON SPEED TO 148KNTS, GOT STICK SHACKER WITH SUBSEQUENT SLAT DISSAGREE WARNING LIGHT. WENT AROUND AND AFTER TROUBLESHOOTIN
- [SDR FDEA2018102953019](https://openairdocs.org/sdr/FDEA2018102953019.md): Doubler · cracked · Oct 25, 2018 · N360FE · Doug MD1010F · Wing, Plate/Skin
  > LT WING AT APPROX XORS 568, INTERNAL. WING BEADED DOUBLER HAS A 1" CRACK. REPAIRED REF SRM 57-10-00 VOL 1 FIG 71 PG 222. MAJOR REPAIR.
- [SDR FDEA2018110243073](https://openairdocs.org/sdr/FDEA2018110243073.md): Roller Tray · cracked · Oct 24, 2018 · N360FE · Doug MD1010F · Fuselage Floor Panel
  > FWD CARGO BS 919, RT OTBD OMNI ROLLER TRAY HAD A 5 INCH CRACK. FABRICATED AND INSTALLED A NEW ROLLER TRAY IAW DWG ADJ7005, AND SRM 51-31-01, VOL 2.
- [SDR FDEA201810202963](https://openairdocs.org/sdr/FDEA201810202963.md): Skin · delaminated · Oct 20, 2018 · N360FE · Doug MD1010F · Spoilers
  > LT WING NR 5 SPOILER, UPPER SKIN, PREVIOUS I/B REPAIR, HAS SMALL AREA DELAMINATION. REPAIRED NR 5 SPOILER PER SRM 57-10-00 VOL I AND SRM 51-71-00 VOL II.
- [SDR FDEA201810172936](https://openairdocs.org/sdr/FDEA201810172936.md): Bracket · cracked · Oct 17, 2018 · N360FE · Doug MD1010F · APU Cowling/Containment
  > APU INLET DOOR, LT BRACKET AT SHAFT CRACKED. WELDED DAMAGED AREA AS PER AMM 20-90-00-8 AND DPS 10.225 SECTIONS 4.5 TO 4.5.6 AND GENERAL WELD PROCEDURES 5.3 TO 5.3.5.
- [SDR FDEA2018102662991](https://openairdocs.org/sdr/FDEA2018102662991.md): Floor Support · corroded · Oct 16, 2018 · N360FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > CENTER CARGO STA 1841 FLOOR BOARD SUPPORT HAS CORROSION. INSTALLED NEW SUPPORT AGA7170-5 PER SRM 51-31-01 VOL. 2 AND DAC DWG AGA7170.
- [SDR FDEA2018102623014](https://openairdocs.org/sdr/FDEA2018102623014.md): Floor Support · corroded · Oct 12, 2018 · N360FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > MAIN DECK STA 1990 RBL 27 UNDER FLOOR HAS CORROSION AROUND NUT PLATE. MARKED NR 13 (ABOVE FLOOR) REMOVED DAMAGED FLOOR BOARD SUPPORT P/N WSP0711-554, FABRICATED FLOOR BOARD SUPPORT P/M WSP 0711-554 REF DWG WSP 0711, PROCESSED FLOOR BOARD SUPPORT P/N WSP 0711
- [SDR FDEA2018102623001](https://openairdocs.org/sdr/FDEA2018102623001.md): Floor Support · worn · Oct 12, 2018 · N360FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > MAIN DECK; STA. 440 26RBL FLOOR SUPPORT HAS UNDOCUMENTED MODIFICATION. DOT 47 REMOVED AND REPLACED AS REQUIRED FLOOR SUPPORT AT MAIN DECK; STA 440, RBL 19-26. REF. SRM 51-35-01 VOL 2 AND DWF: ABA8320 MAJOR REPAIR.
- [SDR FDEA201810122859](https://openairdocs.org/sdr/FDEA201810122859.md): Skin · delaminated · Oct 12, 2018 · N360FE · Doug MD1010F · Spoilers
  > RT WING NR 3 SPOILER UPPER SURFACE HAS SUSPECTED DELAMINATION AREA MARKED. REPAIRED DELAM AREA ON RT NR 3 SPOILER IAW SRM 51-71-00 VOL NR 2.
- [SDR FDEA2018102693000](https://openairdocs.org/sdr/FDEA2018102693000.md): Seat Track · cracked · Oct 9, 2018 · N360FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK - STA. 635 RBL 8. SEAT TRACK CRACKED LOWER FLANGE. NOTE: SEAT TRACK UNDER BALL MAT AREA. REPLACED DAMAGED SEAT TRACK FROM STA 635 TO STATION 615 REF SRM 53-70-00 FIG 1 VI, SRM 51-31-01 VOL, SRZ 10-53-002 DWG MAJOR REPAIR.
- [SDR FDEA2018102692997](https://openairdocs.org/sdr/FDEA2018102692997.md): Seat Track · cracked · Oct 9, 2018 · N360FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK; STA. 485 - 490 15RBL SEAT TRACK DAMAGED 4" SECTION MISSING ON IB LEG. DOT 43 NEW SEAT TRACK INSTALLED AT LOCATION NOTED WORKED ON NR 501 REF SRM 51-31-01 VII MAJOR REPAIR.
- [SDR FDEA201810092978](https://openairdocs.org/sdr/FDEA201810092978.md): Support · cracked · Oct 9, 2018 · N360FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > FWD CARGO COMPT STA 795 FLOOR SUPPORT IS CRACKED. REMOVED AND REPLACED CRACKED FLOOR SUPPORT AS REQUIRED REF SRM51-35-01 VOL 2 AND DAC DWG ADA0235, NEW FLOOR SUPPORT PART NUMBER FXADA0235-3.
- [SDR FDEA2018102682995](https://openairdocs.org/sdr/FDEA2018102682995.md): Seat Track · cracked · Oct 8, 2018 · N360FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK; STA. 485 75LBL SEAT TRACK DAMAGED - 4" OF MISSING MISSING OB LEG. DOT 42 NOTE: RCB AREA INSTALLED NEW SEAT TRACK @ NOTED LOCATION REF SRM 51-31-01 VOL II DWG WSP0826 REF NR500.
- [SDR FDEA201810073003](https://openairdocs.org/sdr/FDEA201810073003.md): Floor Support · corroded · Oct 7, 2018 · N360FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > MAIN DECK STA 1900 RBL52 FLOOR SUPPORT WSP0711-552 UNDER NUTPLATE IS CORRODED. REF SDR #: 19-2779 REPAIRED FLOOR SUPPORT WSP0711-552 PER EA 8-5310-T0343200 P1 FLOOR SUPPORT DOUBLER REPAIR AT STA 1895-1900" MAJOR REPAIR.
- [SDR FDEA201810263003](https://openairdocs.org/sdr/FDEA201810263003.md): Floor Support · corroded · Oct 7, 2018 · N360FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > MAIN DECK, BS 1900, RBL 52 FLOOR SUPPORT WAS CORRODED. REPAIRED THE FLOOR SUPPORT IAW EA 8-5310-T0343200 P1. MAJOR REPAIR.
- [SDR FDEA2018102673002](https://openairdocs.org/sdr/FDEA2018102673002.md): Floor Support · cracked · Oct 7, 2018 · N360FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > MAIN DECK STA 427 LBL 79 LEFT SIDE LATERAL FLOOR SUPPORT ABA7339-1 DAMAGED AT CLIP NUT LOCATION. REMOVED DAMAGED FLOOR SUPPORT AND FAB NEW PER DRAWING ABA7339 AND SRM 51-33- 01 VOL 2. MAJOR REPAIR.
- [SDR FDEA201810063086](https://openairdocs.org/sdr/FDEA201810063086.md): Intercostal · corroded · Oct 6, 2018 · N360FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > FORWARD AVIONICS COMPARTMENT STA 449 4 INCHES LEFT OF CENTERLINE CLIP HAS CORROSION. REMOVED AND REPLACED INTERCOSTAL AS REQUIRED IN REF DWG ABA7882 AND SRM-51-31-01 VOL II.
- [SDR FDEA201810063012](https://openairdocs.org/sdr/FDEA201810063012.md): Frame · corroded · Oct 6, 2018 · N360FE · Doug MD1010F · Fuselage Main, Frame
  > AFT CARGO COMPT, STA 1901 FRAME UNDERSIDE CORROSION BY NUTPLATE. ACCOMPLISH CORROSION REPAIR PER SRM 53-00-01 FIG 9 VOL 1.
- [SDR FDEA2018102662996](https://openairdocs.org/sdr/FDEA2018102662996.md): Seat Track · cracked · Oct 6, 2018 · N360FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > STA 488 RBL 17 SEAT TRACK WSP0826-513, TRACK DAMAGED AT FASTENER HOLE REMOVED AND REPLACED NOTED SEAT TRACK RF SRM 51-31-01 VOL II, DAC DWG WSP0826 MAJOR REPAIR.
- [SDR FDEA2018102662994](https://openairdocs.org/sdr/FDEA2018102662994.md): Seat Track · cracked · Oct 6, 2018 · N360FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > STA 488 LBL 82 SEAT TRACK WSP0826-509, FLANGE DAMAGED AT SCREW HOLE. INSTALLED NEW SEAT TRACK @ NOTED LOCATION REF SRN 51-31-01 VOL II DWG WSP0826.
- [SDR FDEA2018102652990](https://openairdocs.org/sdr/FDEA2018102652990.md): Bulkhead · damaged · Oct 5, 2018 · N360FE · Doug MD1010F · Fuselage Main, Bulkhead
  > CENTER CARGO COMPT STA1841 BULKHEAD SKIN DAMAGED (MARKED) REPLACED WEB AGA7170-3 AND AGA7170-4 PER SRM 51-31-01 VOL. 2. AND DAC DWG AGA7170.
- [SDR FDEA201810052972](https://openairdocs.org/sdr/FDEA201810052972.md): Bracket · loose · Oct 5, 2018 · N360FE · Doug MD1010F · Trailing Edge Flaps
  > RT WING TRAILING EDGE OUTBD FLAP, INBD HINGE, BULLET FAIRING (635EL) INTERNAL BRACKET HAS LOOSE FASTENERS. REMOVED AND REPLACED INTERNAL BRACKET ON FAIRING 635EL, RT WING T/E, O/B FLAP, I/B HINGE REF SRM 51-33-01 VOL 2.
- [SDR FDEA201810052971](https://openairdocs.org/sdr/FDEA201810052971.md): Bracket · cracked · Oct 5, 2018 · N360FE · Doug MD1010F · Trailing Edge Flaps
  > RT WING TRAILING EDGE OUTBD FLAP, INBD HINGE, BULLET FAIRING (635EL) INTERNAL BRACKET HAS LOOSE FASTENERS. FABRICATED NEW BRACKET AS REQ PER DWG ARC0504.
- [SDR FDEA2018102643013](https://openairdocs.org/sdr/FDEA2018102643013.md): Skin · worn · Oct 4, 2018 · N360FE · Doug MD1010F · Aerodynamic Fairings
  > TAIL CONE FOREWARD UPPER LEFT SKIN EDGE HAS WEAR MARKS MARKED NR 5 REPAIRED THE DAMAGE AREA AS REQUIRED REF SRM 53-00-01 FIG. 4 SHEET. 2 VOL. 1.
- [SDR FDEA201810042987](https://openairdocs.org/sdr/FDEA201810042987.md): Longeron · corroded · Oct 4, 2018 · N360FE · Doug MD1010F · Fuselage Main, Longeron/Stringer
  > A/C COMPT, PACK BAY NR 1. APPROX STA 565 TO 588, JUST O/B OF EXHAUST DOOR. RUSTED /CORRODED FASTENERS AND FRAME AND SKIN STRUCTURE. REMOVED AND REPLACED WITH LONGERON ACA3353-3 WITH SPLICE FROM STATION 561 TO STATION 590 REF SRM 53-00-01 FIG 7 SHEETS 5-7 DETAI
- [SDR FDEA201810033059](https://openairdocs.org/sdr/FDEA201810033059.md): Skin · corroded · Oct 3, 2018 · N360FE · Doug MD1010F · Wing, Plate/Skin
  > RT WING UPPER SURFACE AT APPROX XORS 387 STRINGER 5 CORROSION AROUND TWO (2) FASTENERS. REMOVED CORROSION REF SRM 57-10-00 FIG 60 SHEET 1 VOL 1. MATERIAL REMOVED WAS APPROX..034 INCH MAX ALLOWED IS 0.016 INCH PER SRM 57-10-00 FIG 61 SHEET 4 AREA IS OUT OF LIM
- [SDR FDEA201810033058](https://openairdocs.org/sdr/FDEA201810033058.md): Skin · corroded · Oct 3, 2018 · N360FE · Doug MD1010F · Wing, Plate/Skin
  > RT WING UPPER SURFACE AT APPROX XORS 264 STRINGER 13 CORROSION AROUND TWO (2) FASTENERS. REMOVED CORROSION REF SRM 57-10-00 FIG 60 SHEET 1 VOL 1. MATERIAL REMOVED WAS APPROX.022 INCH MAX ALLOWED IS 0.010 INCH PER SRM 57-10-00 FIG 64 SHEET 4. AREA IS OUT OF LI
- [SDR FDEA201810033057](https://openairdocs.org/sdr/FDEA201810033057.md): Skin · corroded · Oct 3, 2018 · N360FE · Doug MD1010F · Wing, Plate/Skin
  > LT WING UPPER SURFACE AT APPROX XORS 264 STRINGER 12 CORROSION AROUND ONE (1) FASTENER. REMOVED CORROSION REF SRM 57-10-00 FIG 60 SHEET 1 VOL 1. MATERIAL REMOVED WAS APPROX.023 INCH MAX ALLOWED IS 0.017 INCH PER SRM 57-10-00 FIG 61 SHEET 4. AREA IS OUT OF LIM
- [SDR FDEA201810033056](https://openairdocs.org/sdr/FDEA201810033056.md): Skin · corroded · Oct 3, 2018 · N360FE · Doug MD1010F · Wing, Plate/Skin
  > RT WING UPPER SURFACE AT APPROX XORS 264 BETWEEN STRINGERS 9 AND 10, CORROSION AROUND ONE (1) FASTENER. REMOVED CORROSION REF SRM 57-10-00 FIG 60 SHEET 1 VOL 1. MATERIAL REMOVED WAS APPROX.035-.157 INCH MAX ALLOWED IS 0.012-0.019 INCH PER SRM 57-10-00 FIG 61
- [SDR FDEA2018102632999](https://openairdocs.org/sdr/FDEA2018102632999.md): Seat Track · worn · Oct 3, 2018 · N360FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK: SEAT TRACK RBL X= 8.50 NEAR STA 755 WORN MARKED INSTALLED NEW SEAT TRACK SPLICE REF SRM 53-70-00 FIG 1 VOL I MAJOR REPAIR.
- [SDR FDEA2018102632998](https://openairdocs.org/sdr/FDEA2018102632998.md): Seat Track · worn · Oct 3, 2018 · N360FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK: SEAT TRACK RBL X= 107.25 NEAR STA 695 WORN MARKED REMOVED DAMAGE AND PLUGGED SEAT TRACK REF SRM 53-70-00 FIG 2 VOL. I MAJOR REPAIR.
- [SDR FDEA201810032854](https://openairdocs.org/sdr/FDEA201810032854.md): Seat Track · damaged · Oct 3, 2018 · N360FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK SEAT TRACK LBL X= 47.50 NEAR STA 755 WORN. REPLACED DAMAGED SEAT TRACK REF SRM 53-70-00, FIG 1, VOL 1 & SRM 51-31-01, VOL 2. MAJOR REPAIR.
- [SDR FDEA201807301850](https://openairdocs.org/sdr/FDEA201807301850.md): Connector · defective · Jul 30, 2018 · N360FE · Doug MD1010F · Landing Gear System Wiring
  > UPON EXTENDING GEAR ON FINAL WE RECEIVED A LEVEL 2 ANTISKID L FAIL ALERT. REMOVED NR 1 MLG WHEEL TRANSDUCER ASSY, REF AMM 32-45-03-2. FOUND FULLY PUSHED PIN ON NR 1 MLG WHEEL TRANSDUCER PLUG P1-1695, WIRE G89A20BL, PIN 2. FURTHER T/S REQUIRED. REMOVED AND
- [SDR FDEA2018073091840](https://openairdocs.org/sdr/FDEA2018073091840.md): Control Unit · failed · Jul 29, 2018 · N360FE · Doug MD1010F · Brake Anti-Skid Section
  > UPON PUTTING LANDING GEAR DOWN, GOT LEVEL 2 ANTI-SKID L FAIL ALERT. ON LAST LEG FAULTS FOUND ASCU INTERNAL FAULT CODE 324141. RTS FAILED. REMOVED AND REPLACED ANTI SKID CONTROL UNIT PER AMM 32-45-01-4, PERFORMED RETURN TO SERVICE TEST NO FAULTS NOTED. A/C OK
- [SDR FDEA201802140395](https://openairdocs.org/sdr/FDEA201802140395.md): Pump · failed · Feb 14, 2018 · N360FE · Doug MD1010F · Hydraulic Pump (Electric/Engine), Main
  > HYD 3 FAIL WHEN SELECTING GEAR DOWN. REMOVED AND REPLACED NR 3 ENGINE DRIVEN HYDRAULIC PUMPS LEFT AND RIGHT REF AMM 29-11-01-2. OPS AND LEAK CHECKS REQUIRED. REF AMM 29-12-02/201 REMOVED AND REPLACED NR 3 ENGINE HYDRAULIC PUMP PRESSURE LINE MANIFOLD FILTER ELE
- [SDR FDEA201801030004](https://openairdocs.org/sdr/FDEA201801030004.md): Light · malfunctioned · Jan 3, 2018 · N360FE · Doug MD1010F · Emergency Lighting
  > EMERGENCY TEST FAILED, ALERT DISPLAYED IAW AMM 24-00-00-5-0, DOWN POWERED ACFT, REPOWERED. RESET THE LT EMERGENCY BUSS SENSE BREAKER. SYSTEM OPS CHECKED GOOD IAW AMM 24-00-00-5. SUSPECT COLD WEATHER. OK FOR SERVICE.
- [SDR FDEA201712143383](https://openairdocs.org/sdr/FDEA201712143383.md): Wire · broken · Dec 14, 2017 · N360FE · Doug MD1010F · Fire Protection System Wiring
  > PDIS 360 26-10 4655 13DEC17 MEM FACT U LOGPAGES:2734383 ENG #3 FIRE INDICATION ON CLIMB OUT. COMPLIED WITH QRH PROCEDURES, INCLUDING DISCHARGE OF AGT 2. FIRE INDICATIONS STOPPED. CRASH CREW REPORTED NO INDICATIONS OF FIRE VISIBLE. RETURNED
- [SDR FDEA201707131934](https://openairdocs.org/sdr/FDEA201707131934.md): Duct · leaking · Jul 13, 2017 · N360FE · Doug MD1010F · Fire Detection
  > TWO HOURS INTO FLIGHT, HAD A QUICK FLASH ALERT LEVEL 2 FOR THE NR 2 ENGINE FIRE LOOP A, LASTED ONE SECOND AND WENT AWAY. 15 MINUTES LATER HAD STEADY LEVEL 2 ALERT FOR LOOP B. RAN QRH CHECKLIST, LOOP A TESTED GOOD. OPERATED IN LOOP A AT THAT POINT. ALL OT
- [SDR FDEA201703210964](https://openairdocs.org/sdr/FDEA201703210964.md): Actuator · inoperative · Mar 21, 2017 · N360FE · Doug MD1010F · Passenger/Crew Doors
  > 1L DOOR INOP. ELECTRIC DOOR ACTUATOR INOP. FOR EMERGENCY EGRESS, USE PNEUMATIC SYSTEM TO OPERATE DOOR. REPLACED L1 DOOR ACTUATOR ELECTRIC REF AMM 52-11-01-2. ADJUSTED CLUTCH CABLE REF AMM 52-11-00-5.
- [SDR FDEA201610313757](https://openairdocs.org/sdr/FDEA201610313757.md): Slide · inoperative · Oct 31, 2016 · N360FE · Doug MD1010F · Escape Slide
  > L1 DOOR SLIDE PRESSURE LIGHT ILLUMINATED. TROUBLE SHOT IAW FIM 25-61-00-2, TASK 25-61-00-810-802, PTT INDICATOR LIGHT DOESN`T GO OFF. CHECKED PLUG OUT OF JACK WITH OHM METER, READS ZERO. EVCUATION SLIDE IS INOPERATIVE. REMOVED AND REPLACED THE L1 DOOR S
- [SDR FDEA201610213667](https://openairdocs.org/sdr/FDEA201610213667.md): Skin · corroded · Oct 21, 2016 · N360FE · Doug MD1010F · Fuselage Main, Plate/Skin
  > LOWER FUSELAGE SKIN FOUND SURFACE CORROSION AT FWD DRAIN MAST LOCATION STA 665 APPROX. TRIMMED OUT SKIN DAMAGED, FABRICATED FILLER, DOUBLERS AND INSTALLED REF SRM 53-20-00 FIG 6 SHEET 7 VOL 1.
- [SDR FDEA201610133608](https://openairdocs.org/sdr/FDEA201610133608.md): Tee Fitting · cracked · Oct 13, 2016 · N360FE · Doug MD1010F · Fuselage Main, Bulkhead
  > LT STA 595 BULKHEAD TEE CAP VERTICAL LEG HAS A.5 INCH CRACK THROUGH THE LOWER FASTENER AT LONGERON 39L. REMOVED AND REPLACED SECTION OF TEE CHORD BETWEEN LONGERONS 36L AND 40L IN REF TO DWG SR10530064 AND EA 8-5310-T0328457.
- [SDR FDEA201610133604](https://openairdocs.org/sdr/FDEA201610133604.md): Tee Fitting · cracked · Oct 13, 2016 · N360FE · Doug MD1010F · Fuselage Main, Bulkhead
  > STA 595 BULKHEAD T CAP, LT FORWARD SIDE, HORIZONTAL LEG BETWEEN STR 38L AND STR 40L. 8 EA FASTENER HOLES SHOW CRACK INDICATION. REMOVED AND REPLACED SECTION OF TEE CHORD BETWEEN LONGERONS 36L AND 40L IN REF TO DWG SR10530064 AND EA 8-5310-T0328457.
- [SDR FDEA201610133594](https://openairdocs.org/sdr/FDEA201610133594.md): Skin · damaged · Oct 13, 2016 · N360FE · Doug MD1010F · Wing, Plate/Skin
  > LT WING FUEL TANK LANDING 536CB HAS 1 BLOWN HOLE. REPAIRED PER EA 8-5710-T0328817, LT WING LOWER SURFACE-TANK ACCESS PANELS.

Next page: https://openairdocs.org/deregistered/N360FE-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 = 'N360FE' AND deregistration_id = 'N360FE-2024-03-02'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N360FE-2024-03-02/reports

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