# Service difficulty reports: N550FE, cancelled Mar 2, 2024

A list on [N550FE, cancelled Mar 2, 2024](https://openairdocs.org/deregistered/N550FE-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 5 · 205 reports

- [SDR FDEA202105271414](https://openairdocs.org/sdr/FDEA202105271414.md): Engine · malfunctioned · May 27, 2021 · N550FE · Doug MD1010F · Engine (Turbine/Turboprop)
  > AT FL380 ALL ENGINES WERE OPERATING NORMALLY. AS WE BEGAN OUR DESCENT AND THROTTLES CAME BACK TOWARDS IDLE ECS SURGED FOLLOWED BY A LEVEL 2 AIRSYS 2 PRES LO AND CONFIRM ENG OUT PROMPT. AIR PRESSURE OUT OF THE NUMBER 2 ENGINE WAS 9 PSI. THE NUMBER 2 THROTT
- [SDR FDEA202012103114](https://openairdocs.org/sdr/FDEA202012103114.md): Support · corroded · Dec 10, 2020 · N550FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT BILGE, CORROSION ON VERTICAL FRAME SUPPORT BELOW FLOOR AT FWD BULKHEAD STA 1781 L-52, MARKED NR 2, 2020-12-10. REMOVED AND REPLACED THE STANCHION, IAW SRM 53-15-01, FIG 9A VOL 3 & DWG AFA 3225.
- [SDR FDEA202012060010](https://openairdocs.org/sdr/FDEA202012060010.md): Attach Angle · cracked · Dec 6, 2020 · N550FE · Doug MD1010F · Fuselage Main, Attach Fittings
  > AT CAC BAY LT SIDE, A CRACK FOUND ON 'ATTACHMENT ANGLE' FOR SUGAR SCOOP FITTING (P/N-NYB6042-7) AT FUS STA-1156. REMOVED AND REPLACED SUGAR SCOOP ATTACHMENT ANGLE AS REQUIRED, PER DWG NYB6042.
- [SDR FDEA202012030015](https://openairdocs.org/sdr/FDEA202012030015.md): Stop Fitting · cracked · Dec 3, 2020 · N550FE · Doug MD1010F · Passenger/Crew Doors
  > L-1 DOOR UPPER FWD CORNER STOP APPEARS TO BE CRACKED. REMOVED DAMAGED ABA7191-506 STOP ASSEMBLY AND INSTALLED NEW PART REFERENCE DRAWING ABA7191 AND EA NR 8-5210-T0358597. REWORK FROM ABA7191-1.
- [SDR FDEA202011183198](https://openairdocs.org/sdr/FDEA202011183198.md): Skin · cracked · Nov 18, 2020 · N550FE · Doug MD1010F · Horizontal Stabilizer, Plate/Skin
  > LT HORIZ LEADING EDGE CENTER SECTION (INTERAL) MULTIPLE CRACKS AT BEADED DOUBLE, APPROXIMATELY 27" OUTBOARD OF INBOARD EDGE (BETWEEN FRAMES 5-6). CRACKS WERE CONFIRMED WITH NDT HFEC. REPAIRED PER EA 8-5510-T0358321.
- [SDR FDEA202011032903](https://openairdocs.org/sdr/FDEA202011032903.md): Skin · corroded · Nov 3, 2020 · N550FE · Doug MD1010F · Fuselage Main, Plate/Skin
  > AFT FUSELAGE, RT SIDE STA 2163 LONG 33 NUTPLATE HOLE CORRODED OUT OF LIMITS. CONFIRMED WITH NDT. COMPLIED WITH FUSELAGE SKIN REPAIR, PER MD-10 SRM 53-20-00 PG 197-205 FIG 22.
- [SDR FDEA202011012876](https://openairdocs.org/sdr/FDEA202011012876.md): Stiffener · cracked · Nov 1, 2020 · N550FE · Doug MD1010F · Nacelle/Pylon Miscellaneous Structure
  > REWORK NR 343 FABRICATED PART NOT ACCEPTED: NR 3 ENGINE PYLON INTERNAL STRUCTURE/BOX AFT ANGLE SUPPORT FOR ACCESS DOOR 488BL COMPLETELY BROKEN OFF AND CRACKED VIEWING THRU ACCESS DOOR 488BR. (DOT 9) REMOVED AND REPLACED ANGLE SUPPORT FX AUB7087-15, AS REQUI
- [SDR FDEA202010292835](https://openairdocs.org/sdr/FDEA202010292835.md): Access Panel · corroded · Oct 29, 2020 · N550FE · Doug MD1010F · Horizontal Stabilizer, Plate/Skin
  > RIGHT HAND LEADING EDGE INBOARD SIDE P/N ACL7051-2-401 HAS CORROSION UNDER STRINGERS AROUND ACCESS PANEL 341, AT MARKED NR 14 (REQ RDR SDR). REPLACED DOUBLER P/N ALC7273-11, PER DOUGLAS DRW ALC7273 AND MD10 SRM 51-31-01 VOL II.
- [SDR FDEA202010283006](https://openairdocs.org/sdr/FDEA202010283006.md): Skin · cracked · Oct 28, 2020 · N550FE · Doug MD1010F · Horizontal Stabilizer Structure
  > RT HORIZONTAL STABILIZER, AFT BODY FAIRING, HAS THREE DAMAGED NUTPLATES, AREA MARKED. COMPLIED WITH DOUBLER REPAIR INSTALLATION AT FUSELAGE SKIN STA 2163 BETWEEN LONGERON 12 & 13 RT, REF MD-10 SRM 53-00-01 FIG 4 (SHEET 2) VOL 1.
- [SDR FDEA202010262657](https://openairdocs.org/sdr/FDEA202010262657.md): Support · cracked · Oct 26, 2020 · N550FE · Doug MD1010F · Wing Miscellaneous Structure
  > RT WING NR 3 FUEL TANK REFUELING/DEFUELING T-LINE SUPPORT BRACKET CRACKED P/N ARL0501-44. FABRICATED NEW SUPPORT BRACKET, REF DAC DWG ARL0501.
- [SDR FDEA202010242768](https://openairdocs.org/sdr/FDEA202010242768.md): Doubler · corroded · Oct 24, 2020 · N550FE · Doug MD1010F · Vertical Stabilizer, Plate/Skin
  > LEFT HORIZONTAL LEADING EDGE INBOARD SECTION ALC7051-1-401 HAS EXTENSIVE CORROSION. INSIDE AND OUTSIDE SKIN IS SWOLLEN AROUND FASTENERS, MARKED NR 15 AND NR 16. FOUND CORROSION TO BE ON ACCESS PANEL DOUBLER P/N ALC7273-13. REPLACED DOUBLER AND INSTALLED NE
- [SDR FDEA202010242631](https://openairdocs.org/sdr/FDEA202010242631.md): Drive Chain · broken · Oct 24, 2020 · N550FE · Doug MD1010F · Emergency Equipment
  > L1 DOOR EMERGENCY OPERATION CHECK FAILED FOUND DRIVE CHAIN BROKEN. REPLACED CHAIN, PER CMM 52-11-09 AND GMM 52-10-01-2. OPERATIONS CHECKED EMERGENCY DOOR, PER WORK CARD 52C1301.
- [SDR FDEA202010223228](https://openairdocs.org/sdr/FDEA202010223228.md): Fitting · cracked · Oct 22, 2020 · N550FE · Doug MD1010F · Fuselage Main, Structure
  > LT FUSELAGE STRUCTURE, STA 1156 L39, SUGER SCOOP FITTING (AYB 7000) CRACKED APPROX 1 INCH BEYOND PREVIOUS STOP DRILL, MARKED. REMOVED AND REPLACED SUGAR SCOOP FITTING AYB7000-1, REFERENCE DOUGLAS DRAWING NYB6042.
- [SDR FDEA202010183191](https://openairdocs.org/sdr/FDEA202010183191.md): Frame · corroded · Oct 18, 2020 · N550FE · Doug MD1010F · Fuselage Main, Frame
  > CENTER CARGO BILGE-STR 52 STA 1641-CORROSION AT FRAME, LOWER ANGLE AFT. REPAIRED CENTER CARGO BILGE STR 52 STA 1641 FRAME, REF SRM 53-30-00 FIG 5 (SHEET 1) VOL 1. MAJOR REPAIR AMT NR JG3884010 11/13/20 RII BUY BACK QC NR 439384 11/13/20. SEE ATTACHMENTS FOR
- [SDR FDEA202010172610](https://openairdocs.org/sdr/FDEA202010172610.md): Frame · corroded · Oct 17, 2020 · N550FE · Doug MD1010F · Fuselage Main, Frame
  > AFT CARGO COMPT BILGE, CORROSION ON FRAME, LOWER HAT SECTION, AT STA 1921 L-52 (MARKED #10) STA 1921, FRAME AGA7130-11, LOWER HAT, BETWEEN LONG L51 TO R51 REMOVED CORROSION REF MD10-10 SRM 51-21-01 VOL 2. DUE TO BLENDOUT PAST 20 PERCENT OF ORIGINAL THICKN
- [SDR FDEA202010172608](https://openairdocs.org/sdr/FDEA202010172608.md): Frame · corroded · Oct 17, 2020 · N550FE · Doug MD1010F · Fuselage Main, Frame
  > AFT CARGO COMPT BILGE, CORROSION ON FRAME, LOWER HAT SECTION, AT STA 1853 L-52 (MARKED #7) REMOVED CORROSION ON FRAME AGA0016-3, LOWER HAT SECTION, AT STA 1853 BETWEEN LONG L51 TO R51 REF MD10-10 SRM 51-21-01 VOL 2. INSTALLED NESTED CHANNEL REPAIR REF MD
- [SDR FDEA202010172607](https://openairdocs.org/sdr/FDEA202010172607.md): Frame · corroded · Oct 17, 2020 · N550FE · Doug MD1010F · Fuselage Main, Frame
  > AFT CARGO COMPT BILGE, CORROSION ON FRAME, LOWER HAT SECTION, AT STA 1841 L-52 (MARKED #11) CORROSION ON FORMER/FRAME (2 PIECE) LWR CHANNEL AT STA 1841, LONG 50L TO 50R IS ON A PREVIOUS SPLICE REPAIR. REMOVED PREVIOUS SPLICE REPAIR IAW MD10-10 SRM 51-33-
- [SDR FDEA202010160017](https://openairdocs.org/sdr/FDEA202010160017.md): Cap · cracked · Oct 16, 2020 · N550FE · Doug MD1010F · Fuselage Main, Structure
  > LT WING, FUSELAGE STRUCTURE SEEN THROUGH WING BODY FAIRING 154AB, STA 1156 STRINGER 39, FITTING CRACKED, MARKED. REPAIRED AREA REFERENCE EA 8-5310-T0357883.
- [SDR FDEA202010162691](https://openairdocs.org/sdr/FDEA202010162691.md): Fitting · cracked · Oct 16, 2020 · N550FE · Doug MD1010F · Fuselage Main, Frame
  > RT FUSELAGE AT STA 1156, FRAME FITTING (SUGAR SCOOP) CRACKED (CRACK CONTINUE PROPOGATE FROM PREVIOUS STOP DRILL INBOARD, VIEW FROM OUTSIDE. INSTALLED NEW EXTERNAL REPAIR DOUBLER, FILLER AND SHIM, PER EA: T8-5310-T0357791 P1.
- [SDR FDEA202010162689](https://openairdocs.org/sdr/FDEA202010162689.md): Skin · cracked · Oct 16, 2020 · N550FE · Doug MD1010F · Fuselage Main, Plate/Skin
  > RT FUSELAGE APPROXIMATELY AT STA 1156 SKIN HAS A 3" CRACK, PROPAGATING FROM EXTERNAL DOUBLER FORWARD BETWEEN STRINGER 38 AND 37, INSTALLED NEW EXTERNAL REPAIR DOUBLER, FILLER AND SHIM, PER EA: T8-5310-T0357791.
- [SDR FDEA202010152582](https://openairdocs.org/sdr/FDEA202010152582.md): Stiffener · cracked · Oct 15, 2020 · N550FE · Doug MD1010F · Nacelle/Pylon Miscellaneous Structure
  > NR 3 ENGINE PYLON INTERNAL STRUCTURE/BOX AFT ANGLE SUPPORT FOR ACCESS DOOR 488BL COMPLETLY BROKEN OFF AND CRACKED WING THRU ACCESS DOOR 488BR. (DOT 9) REMOVED AND REPLACED STIFFENER AUB7087-505, REF DAC DWG AUB7300 AND SRM 51-31-01 VOL 2.
- [SDR FDEA202010142885](https://openairdocs.org/sdr/FDEA202010142885.md): Skin · dented · Oct 14, 2020 · N550FE · Doug MD1010F · Fuselage Main, Plate/Skin
  > RT FUSELAGE EXTERIOR APPROXIMATELY STA 1853 BETWEEN LONGERON 37R-38R DENT. ENTERED IN ERROR.
- [SDR FDEA202010142789](https://openairdocs.org/sdr/FDEA202010142789.md): Doubler · cracked · Oct 14, 2020 · N550FE · Doug MD1010F · Fuselage Main, Structure
  > CENTER WHEEL WELL FWD BULKHEAD RT OUTBOARD SPOILER PUSH/PULL M.J RODS FEED THROUGH DOUBLER LOWER AFT CORNER CRACKED. P/N AEA0526. R & R THE DOUBLER (P/N-AEA0526U2) WITH HI-LOK, PER SRM 51-33-01 VOL-II.
- [SDR FDEA202010142662](https://openairdocs.org/sdr/FDEA202010142662.md): Stiffener · cracked · Oct 14, 2020 · N550FE · Doug MD1010F · Wing Miscellaneous Structure
  > RT WING FIXED LEADING, INNER SURFACE, SKIN STIFFENER IS CRACKED AT STA XOS 697. REPAIRED STIFFENER, PER EA 8-5710-T0357549 "WINGS-BASIC WING STRUCTURE-RT WING LEADING EDGE UPPER STRINGER CRACKED AT XOS 696-REPAIR".
- [SDR FDEA202010142661](https://openairdocs.org/sdr/FDEA202010142661.md): Doubler · cracked · Oct 14, 2020 · N550FE · Doug MD1010F · Wing, Plate/Skin
  > RT WING FIXED LEADING EDGE, INNER UPPER SURFACE, PILLOW DOUBLER IS CRACKED AT STA XOS 697. REPAIRED CRACKED DOUBLER, PER SRM 57-10-00 FIG 71 VOL 1.
- [SDR FDEA202010142601](https://openairdocs.org/sdr/FDEA202010142601.md): Skin · cracked · Oct 14, 2020 · N550FE · Doug MD1010F · Wing, Plate/Skin
  > RT WING FIXED LEADING EDGE, INNER SURFACE, PILLOW DOUBLER IS CRACKED AT STA XOS 669. INSTALLED REPAIR DOUBLER AS REQUIRED, REF SRM 57-10-00 VOL 1 FIG 71 AND SRM 51-31-01 VOL 2.
- [SDR FDEA202010132690](https://openairdocs.org/sdr/FDEA202010132690.md): Skin · cracked · Oct 13, 2020 · N550FE · Doug MD1010F · Fuselage Main, Plate/Skin
  > CENTER CARGO DOOR AFT SKIN CUT-OUT AT APPROXIMATELY STA 1787 BETWEEN LONGERON 39L-41L. REPAIR DOUBLERS DAMAGED AT CENTER CARGO DOOR LOWER AFT CORNER STA 1787 BETWEEN LONGERON 39L-41L. REMOVED DAMAGED DOUBLERS NR 1 & NR 2 AND MADE NEW REPLACEMENT DOUBLERS NR
- [SDR FDEA202010132731](https://openairdocs.org/sdr/FDEA202010132731.md): Skin · damaged · Oct 13, 2020 · N550FE · Doug MD1010F · Fuselage Main, Plate/Skin
  > FWD CARGO DOOR CUT-OUT SKIN AT APPROXIMATELY STA 959 BETWEEN LONGERONS 40-41-REPAIR DOUBLERS ARE DAMAGED. R & R REPAIR DOUBLERS AND FILLER, REF SRM 53-50-00 VOL I FIGURE 26 PG 175 AND DWG ADA0237.
- [SDR FDEA202010122533](https://openairdocs.org/sdr/FDEA202010122533.md): Doubler · cracked · Oct 12, 2020 · N550FE · Doug MD1010F · Wing, Plate/Skin
  > RT WING, FWD LOWER LEADING EDGE: CRACK ON INTERCOSTAL. OUTBOARD OF NR 12 SLAT TRACK, STA XOS 790. REMOVED AND REPLACED CRACKED ARB1249-28, REF SRM 51-33-01 VOL 2 AND SRM 51-35-01 PG 40 VOL. 2 AND DWG ARB1249.
- [SDR FDEA2020041380734](https://openairdocs.org/sdr/FDEA2020041380734.md): Web · dented · Apr 8, 2020 · N550FE · Doug MD1010F · Nacelle/Pylon Miscellaneous Structure
  > #2 ENGINE AFT PYLON CENTER SECTION VERTICAL WEB R/H SIDE IS DENTED. FABRICATED/INSTALLED #2 ENG PYLON WEB USING DOUGLAS DRW AVB7318, AVB7023 & AVB7050 AS A REFERENCE.
- [SDR FDEA2020042750698](https://openairdocs.org/sdr/FDEA2020042750698.md): Fire Detector · malfunctioned · Apr 5, 2020 · N550FE · Doug MD1010F · Fire Detection
  > DURING QRH FOR COMPRESSOR STALL WE RECEIVED LEVEL 2 ENG 2 LOOP A ALERT/ POSSIBLE ENGINE FIRE. THE QRH PROCEDURES SHOWED NO FIRE SO WE LEFT ENG 2 AT IDLE WITH ENG 2 LOOP SWITCH IN B POSITION. #2 ENGINE FIRE DETECT SYSTEM OPS CHECK GOOD IAW MD10-10 MM 26-
- [SDR FDEA2020040650698](https://openairdocs.org/sdr/FDEA2020040650698.md): Fire Warning · false activation · Apr 5, 2020 · N550FE · Doug MD1010F · Fire Detection
  > DURING QRH FOR COMPRESSOR STALL WE RECEIVED LEVEL 2 ENG 2 LOOP A ALERT/ POSSIBLE ENGINE FIRE. THE QRH PROCEDURES SHOWED NO FIRE SO WE LEFT ENG 2 AT IDLE WITH ENG 2 LOOP SWITCH IN B POSITION.
- [SDR FDEA2020042730686](https://openairdocs.org/sdr/FDEA2020042730686.md): Engine · malfunctioned · Apr 3, 2020 · N550FE · Doug MD1010F · Engine (Turbine/Turboprop)
  > CLIMBING THRU FL340 WITH ENGINES ALL AT CLIMB POWER WE FELT A BUMP LIKE MINOR TURBULENCE. THEN ANOTHER AND ANOTHER. WE SAW ENG 2 N1 FLUCTUATING SO WE SUSPECTED A COMPRESSOR STALL. AS WE WERE RUNNING THE QRH FOR ENG COMPRESSOR STALL WE RECEIVED LEVEL 2 ENG
- [SDR FDEA2020040630686](https://openairdocs.org/sdr/FDEA2020040630686.md): Engine · unknown · Apr 3, 2020 · N550FE · Doug MD1010F · Engine (Turbine/Turboprop)
  > CLIMBING THRU FL340 WITH ENGINES ALL AT CLIMB POWER WE FELT A BUMP LIKE MINOR TURBULENCE. THEN ANOTHER AND ANOTHER. WE SAW ENG 2 N1 FLUCTUATING SO WE SUSPECTED A COMPRESSOR STALL. AS WE WERE RUNNING THE QRH FOR ENG COMPRESSOR STALL WE RECEIVED LEVEL 2 ENG
- [SDR FDEA201904270941](https://openairdocs.org/sdr/FDEA201904270941.md): Bracket · damaged · Apr 27, 2019 · N550FE · Doug MD1010F · Emergency Equipment
  > MDIS 550 25-60 7274 27APR19 OAK OPEN U UPON ENTERING THROUGH L1 DOOR, FOUND GIRT BAR HANGING AND DISCOVERED FWD ATTACHED BRACKET INDEX PIN SHEARED. REPLACED GIRT BAR BRACKET (HOOK), AND PERFORMED ADJ/TEST REF AMM 52-11-00. ALL CHECKS OK. BRAC
- [SDR FDEA201901180172](https://openairdocs.org/sdr/FDEA201901180172.md): Skin · cracked · Jan 18, 2019 · N550FE · Doug MD1010F · Passenger/Crew Doors
  > R1 DOOR FWD LOWER CORNER DENTED. REPLACED LOWER SKIN OF R1 DOOR REF. SRM 52-10-00 FIG. 4A PAGE 14A VOL. 1, AND RSC TRACKING EA # 8-5210-T0344731.
- [SDR FDEA201811163266](https://openairdocs.org/sdr/FDEA201811163266.md): Lead · defective · Nov 16, 2018 · N550FE · Doug MD1010F · Engine EGT/TIT Indicating System
  > AS AUTO THROTTLES WENT TO CLIMB TRUST, NR 1 EGT WENT TO 1018' WITH "ENG 1 EXCEEDANCE" ALERT. C/W MTSI, R&R ALL NR 1 EGT THERMOCOUPLE PROBES AND FWD AND AFT LEADS I/R/T MM 77-21-01-2. RAN ENGINE NR 1 AND NR 3 FOR COMPARISON. ENGINE NR 1 START EGT 560, EGT 375 A
- [SDR FDEA201811033103](https://openairdocs.org/sdr/FDEA201811033103.md): Skin · dented · Nov 3, 2018 · N550FE · Doug MD1010F · Passenger/Crew Doors
  > R1 FORWARD PASSENGER / CREW DOOR HAS DENTS IN SKIN ACROSS 4 FRAME BAYS, COMPLIED WITH EA 8-5210-T0340776 AND IAW SRM 52-10-00 FIG 12B. SECTIONAL SKIN REPLACEMENT REPAIR. MAJOR REPAIR.
- [SDR FDEA201810313066](https://openairdocs.org/sdr/FDEA201810313066.md): Skin · corroded · Oct 31, 2018 · N550FE · Doug MD1010F · Trailing Edge Flaps
  > BULGING SKIN AT LT INBD FLAP LOWER SURFACE MID AREA 22" INBD OF FLAP HINGE ARM. CORROSION FOUND TO BE BEYOND LIMITS AT BULGING SKIN AT LT INBD FLAP LOWER SURFACE MID AREA 22" INBD OF FLAP HINGE ARM IAW SRM 57-00-01 FIG 1A. REMOVED AND REPLACED LOWER SKIN AND
- [SDR FDEA201810293045](https://openairdocs.org/sdr/FDEA201810293045.md): Angle · corroded · Oct 29, 2018 · N550FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > CENTER CARGO COMPT, FWD WALL LOWER SECTION, FWD OF LT END ATTACHMENT OF LT ROLLER TRAY ALONG STA 1521 HAS CORROSION. REMOVED CORROSION IAW SRM 51-21-01 AND SRM 53-00-01 VOL I. MATERIAL LOSS.100 OUT OF LIMITS IAW SRM 53-00-01 VOL 1. REMOVED AND REPLACED ANGLE
- [SDR FDEA201810263015](https://openairdocs.org/sdr/FDEA201810263015.md): Door Sill · corroded · Oct 26, 2018 · N550FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > CORROSION ON WEB IN CENTER CARGO COMPT DOOR SILL AREA BS 1701 TO BS 1705 UNDER FLOOR LEVEL. REMOVED CORROSION IAW SRM 51-21-01. MATERIAL LOSS.098 FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG 1A. REMOVED AND REPLACED WEB IAW SRM 53-31-01. MAJOR REPAIR.
- [SDR FDEA201810263016](https://openairdocs.org/sdr/FDEA201810263016.md): Floorbeam · cracked · Oct 26, 2018 · N550FE · Doug MD1010F · Fuselage Main, Floor Beam
  > CRACKED CABIN FLOORBEAM BELOW LT OVERWING DOOR STA 1301. REPAIRED CABIN FLOORBEAM AT LT STA 1301 IAW REPAIR DWG SR10530081-7003. PERFORM REPETITIVE NDI INSPECTION AT LANDING INTERVALS 5000 LANDINGS. IAW SRM 51-50-01 VOL II. MAJOR REPAIR
- [SDR FDEA201810222969](https://openairdocs.org/sdr/FDEA201810222969.md): Seat Track · corroded · Oct 22, 2018 · N550FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK BS 1481, X75.50 SEAT TRACK FLANGE HAD CORROSION. REMOVED THE CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-70-00. FABRICATED A NEW SEAT TRACK REPAIR SPLICE. INSTALLED THE REPAIR IAW SRM 53-70-00, PAGE3. MAJOR REPAIR.
- [SDR FDEA201807181772](https://openairdocs.org/sdr/FDEA201807181772.md): O-Ring · damaged · Jul 18, 2018 · N550FE · Doug MD1010F · Hydraulic System, Main
  > LEVEL ONE HYD 3 ELEV OFF W/ SLOW LEAK TO HYD 3 QTY LO LEVEL ONE ON DESCENT AND GEAR EXTENDED. ON TAXI IN LEVEL 2 HYD 3 FAIL. BLOCK IN QTY 1.2. QTY DECREASED THROUGHOUT REMAINDER OF FLIGHT, QRH PROCEDURES FOLLOWED. QTY NEVER DECREASED TO THE POINT OF ENG PUMP D
- [SDR FDEA201802070332](https://openairdocs.org/sdr/FDEA201802070332.md): Torque Tube · failed · Feb 7, 2018 · N550FE · Doug MD1010F · Cargo/Baggage Doors
  > MAIN CARGO DOOR WOULD NOT LATCH, WHEN CLOSED. FOUND TORQUE TUBE CRACKED AND BROKEN. REMOVED THE MAIN CARGO DOOR TORQUE TUBE ON FWD SIDE OF DOOR IAW CMM 52-34-04. INSTALLED A NEW TORQUE TUBE IAW CMM 52-34-04.
- [SDR FDEA201705101381](https://openairdocs.org/sdr/FDEA201705101381.md): Warning Light · false activation · May 10, 2017 · N550FE · Doug MD1010F · Landing Gear Position and Warning
  > AFTER TAKEOFF, NOTICED THREE RED GEAR LIGHTS. LEVELED AT 5000 FT, SLOWED TO 200KTS, COMPLIED WITH QRH, CYCLED GEAR. LIGHTS WENT OUT WITH NO FURTHER PROBLEMS. TROUBLESHOT FAULT IAW FIM 32-30-00-2-0, TASK 32-30-00-810-801, NO CURENT PSEU FAULTS OR FAULT HIST
- [SDR FDEA201612104372](https://openairdocs.org/sdr/FDEA201612104372.md): Trim System · malfunctioned · Dec 10, 2016 · N550FE · Doug MD1010F · Rudder Tab Control System
  > RUDDER TRIM WHEEL WILL NOT TURN PAST 1R OR 1L. INSPECTED CABLES AND PULLEYS NO DEFECTS NOTED. APPLIED ICE PREVENTION COMPOUND TO AFT PRESSURE SEALS. RAN RUDDER TRIM FULL TRAVEL LEFT AND RIGHT WITH NO BINDING. ALL WORK DONE IAW AMM 20-20-07-2-0.
- [SDR FDEA201612034313](https://openairdocs.org/sdr/FDEA201612034313.md): Access Panel · punctured · Dec 3, 2016 · N550FE · Doug MD1010F · Wing, Plate/Skin
  > LEFT WING, BOTTOM ACCESS PANEL 541EB HAS A DAMAGED CORNER AND A PUNCTURE. PREPPED AND BONDED THE ACCESS PANEL IAW SRM 57-71-00 VOL 2 PAGE 64 PARA.16 A2.
- [SDR FDEA201612014303](https://openairdocs.org/sdr/FDEA201612014303.md): Skin · cracked · Dec 1, 2016 · N550FE · Doug MD1010F · Wing, Plate/Skin
  > RIGHT WING UPPER SKIN HAS CRACKS. INSTALLED A REPAIR DOUBLER IAW SRM 57-10-00 FIG 55
- [SDR FDEA201611234234](https://openairdocs.org/sdr/FDEA201611234234.md): Spar Cap · cracked · Nov 23, 2016 · N550FE · Doug MD1010F · Wing Spar
  > RIGHT WING, LOWER REAR SPAR CAP AFT EDGE AT STA. XORS 404 HAS A.150 IN. CRACK PROPAGATING UP FROM THE LOWER EDGE. REPAIR IAW EA. 8-5710-T0329826

Next page: https://openairdocs.org/deregistered/N550FE-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 = 'N550FE' AND deregistration_id = 'N550FE-2024-03-02'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N550FE-2024-03-02/reports

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