# Service difficulty reports: N303FE

A list on [N303FE](https://openairdocs.org/aircraft/N303FE.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 · 207 reports

- [SDR FDEA202203120491](https://openairdocs.org/sdr/FDEA202203120491.md): None · none · Mar 12, 2022 · N303FE · Doug MD1030F · Landing Gear Retraction/Extension System
  > UNSAFE GEAR WARNING DURING EXTENSION FOR ALL 4 GEAR ON PRIMARY AND SECONDARY INDICATORS. AIRSPEED AT APPROXIMATELY 190 KNOTS. RETRACTED AND FOLLOWED QRH. RECEIVED NORMAL GEAR DOWN INDICATION AFTER THAT. CREW DEBREIF, CREW SUSPECTS GEAR HANDLE WAS POS
- [SDR FDEA202108212054](https://openairdocs.org/sdr/FDEA202108212054.md): O-Ring · damaged · Aug 21, 2021 · N303FE · Doug MD1030F · Fuel Boost Pump
  > PDIS 303 28-40 7724 21AUG21 IND OPEN U APPROXIMATELY 30 MIN INTO CRUISE TNK 1 FUEL QTY LO, TNK 1 TIP TRAPPED ALERTS ILLUMINATED. APPROXIMATELY 7700 LBS OF FUEL ACROSS EACH TANK.. TANK 1 STOPPED FEEDING AT 7500. SELECTED MANUAL, THEN AUTO, NO
- [SDR FDEA202102070298](https://openairdocs.org/sdr/FDEA202102070298.md): Connector · damaged · Feb 7, 2021 · N303FE · Doug MD1030F · Fire Protection System Wiring
  > DURING COCKPIT SET UP/PREFLIGHT & AFTER APU STARTED RECIEVED FIRE WARNING TONE, LWR CARGO FIRE, FLASHING DISCHARGE LIGHTS, PUSHED DISCHARGE, AFTER 2 MIN, STILL FLASHING, PUSH 2ND BOTTLE, CALLED FIRE& MX. EXITED AIRCRAFT. AFTER REPLACEMENT OF BOTTLES FOUN
- [SDR FDEA2020063081381](https://openairdocs.org/sdr/FDEA2020063081381.md): Via · failed · Jun 28, 2020 · N303FE · Doug MD1030F · Central Computers
  > ON TAKE OFF ROLL AT APPROX 120 KTS ALL DISPLAYS (DV'S) STARTED FLASHING EXCEPT FOR DV NR 1 (CAPTS). TAKEOFF WAS CONTINUED & WE HAD NUMEROUS ALERTS THAT FLASHED (CAC DOOR OPEN, A LIST OF YAW ALERTS) DURING OUR RETURN TO THE FIELD. THE FLASHING DISPLAYS CONI
- [SDR FDEA202004160754](https://openairdocs.org/sdr/FDEA202004160754.md): Seat Track · corroded · Apr 16, 2020 · N303FE · Doug MD1030F · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT 1290 LBL100 HAS CORROSION REQ REPAIR. REPLACED CORRODED SEAT TRACK AT STA 1290 LBL 100 REF SRM 53-70-00 FIG 1 VOL 1.
- [SDR FDEA2020041730746](https://openairdocs.org/sdr/FDEA2020041730746.md): Structure · damaged · Apr 13, 2020 · N303FE · Doug MD1030F · Nacelle/Pylon Miscellaneous Structure
  > DURING BOAT TAIL INSTALLATION, AFT SLING ATTACHMENT TO SKIN FAIRING CAP IS DAMAGED. REPAIRED DAMAGED AREA REFERENCE SRM 54-00-01 FIG. 11 SHT.1 VOL. 1 AND SRM 54-00-01 FIG. 13 SHT. 1 VOL. 1.
- [SDR FDEA2020041310732](https://openairdocs.org/sdr/FDEA2020041310732.md): Floorboard · gouged · Apr 11, 2020 · N303FE · Doug MD1030F · Fuselage Floor Panel
  > MAIN CARGO - FLOOR BOARD 233FF - GOUGE. REPAIRED FLOOR BOARD 233 FF. REF. FEDEX DRAWING SRZ-25-005
- [SDR FDEA2020040870704](https://openairdocs.org/sdr/FDEA2020040870704.md): Seat Track · damaged · Apr 7, 2020 · N303FE · Doug MD1030F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CARGO -SEAT TRACK DAMAGED AT STA. 798 LBL 8. PERFORMED REPAIR TO SEAT TRACK REF. SRM 53-70-00 FIG. 1 SHEET 1.VOL.1 FOR DAMAGED LOCATED AT STA 798 LBL 8 MAIN DECK.
- [SDR FDEA2020040100640](https://openairdocs.org/sdr/FDEA2020040100640.md): Skin · corroded · Mar 30, 2020 · N303FE · Doug MD1030F · Wing, Plate/Skin
  > MAIN CARGO DECK, STA 1241 102LBL TO 110LBL, CENTER WING UPPER SKIN CORROSION CENTRE WING TOP SKIN AT STRINGER 13, BETWEEN XCW 102 TO XCW110, CORROSION REWORK PERFORMED IAW EA 8-5710-T0353142 PART 1.
- [SDR FDEA2020032760608](https://openairdocs.org/sdr/FDEA2020032760608.md): Skin · corroded · Mar 26, 2020 · N303FE · Doug MD1030F · Wing, Plate/Skin
  > SMIS 303 57-30 6345 25MAR20 MEM OPEN U MOD TYPE T MOD NO. 8-5730-T0353169 REV NO. PS P1 WING, SKIN AND PLATES: CENTER WING UPPER, CENTER SKIN PANEL, STR 14 TO STR 15, COMPLY WITH E..A. 8-5730-T0353169 REV NO. POS. P1 INFO 25MAR20 14:44 **
- [SDR FDEA2020032760607](https://openairdocs.org/sdr/FDEA2020032760607.md): Skin · corroded · Mar 26, 2020 · N303FE · Doug MD1030F · Wing, Plate/Skin
  > SMIS 303 57-30 6346 25MAR20 MEM OPEN U MOD TYPE T MOD NO. 8-5730-T0353174 REV NO. PS P1 WING, SKIN AND PLATES: CENTER WING UPPER, FWD AND CENTER SKIN PANELS, STR 15, X COMPLY WITH E..A. 8-5730-T0353174 REV NO. POS. P1 INFO 26MAR20 11:54 *
- [SDR FDEA2020032530602](https://openairdocs.org/sdr/FDEA2020032530602.md): Skin · cracked · Mar 23, 2020 · N303FE · Doug MD1030F · Landing Gear Doors
  > RIGHT CENTER LANDING GEAR DOOR AFT DOOR HAS INNER SKIN CRACK APPROX.5" JUST FWD OF THE FWD HINGE. NDT VERIFIED AND MARKED END OF THE CRACK. REMOVED AND REPLACED FRAME SECTION PER DWG ANB7378 AND SRM 51-31-01,V2.
- [SDR FDEA2020040890717](https://openairdocs.org/sdr/FDEA2020040890717.md): Skin · corroded · Mar 19, 2020 · N303FE · Doug MD1030F · Fuselage Miscellaneous Structure
  > MAIN CARGO DECK, CENTER WING UPPER SKIN, STA 1229 100RBL HAS CORROSION ALONG EDGE (MARKED) CENTRE WING UPPER SKIN, STRINGER 15, XCW -89 TO XCW -105, CORROSION AT SKIN EDGES REWORKED IAW EA 8-5710-T0353281 PART 2
- [SDR FDEA2020040890716](https://openairdocs.org/sdr/FDEA2020040890716.md): Skin · corroded · Mar 19, 2020 · N303FE · Doug MD1030F · Fuselage Miscellaneous Structure
  > MAIN CARGO DECK, CENTER WING UPPER SKIN, STA1229 88RBL TO 100RBL HAS CORROSION AROUND MARKED FASTENERS CENTRE WING UPPER SKIN, STRINGER 15, XCW -89 TO XCW -105, CORROSION AT MARKED FASTENER AREAS REWORKED IAW EA 8-5710-T0353281 PART 2.
- [SDR FDEA2020032980613](https://openairdocs.org/sdr/FDEA2020032980613.md): Cap · corroded · Mar 18, 2020 · N303FE · Doug MD1030F · Fuselage Main, Bulkhead
  > MAIN CARGO AFT PRESSURE BULKHEAD TEE CAP HAS A CONFIRMED CRACKED ON RADIOUS STA 2007 APPROX BETWEEN X23-X25 REMOVED AND REPLACED DAMAGED SECTION OF TEE CAP REF. REPAIR SRM 53-40-00 VOL 1 FIG. 16, SRM 51-33-01 VOL 2.
- [SDR FDEA202003270605](https://openairdocs.org/sdr/FDEA202003270605.md): Fitting · cracked · Mar 17, 2020 · N303FE · Doug MD1030F · Fuselage Miscellaneous Structure
  > NLG WW RH SIDE BLKHD FITTING PN# ACA3837-2 REQUIRES FABRICATION DUE TO SHEET METAL REPAIR. REF NR# (225). INSTALLED ACA3837-2 FITTING I.A.W DWG. ACA3837. REF. N00225.
- [SDR FDEA2020040350654](https://openairdocs.org/sdr/FDEA2020040350654.md): Structure · corroded · Mar 15, 2020 · N303FE · Doug MD1030F · Fuselage Miscellaneous Structure
  > MAIN CARGO DECK, STA1227 83LBL TO 94LBL, CENTER UPPER WING SKIN HAS CORROSION (MARKED) CENTRE WING UPPER SKIN CORROSION AT STRINGER 15 BETWEEN XCW 83 TO XCW 94, REWORK PERFORMED IAW EA 8-5710-T0353281 PART 1
- [SDR FDEA2020040850724](https://openairdocs.org/sdr/FDEA2020040850724.md): Intercostal · corroded · Mar 15, 2020 · N303FE · Doug MD1030F · Fuselage Miscellaneous Structure
  > AVIONICS COMPARTMENT AT STA 464 LBL 28. LONGITUDIONAL STIFENNER, AND WEB AATACH ANGLE CORRODED (MARKED) FABRICATED AND INSTALLED -59 INTERCOSTAL PER DWG NBA6074 AND SRM 51-31-01 VOL. 2. WORK ACCOMPLISHED ON N/R 507.
- [SDR FDEA2020040840723](https://openairdocs.org/sdr/FDEA2020040840723.md): Intercostal · corroded · Mar 14, 2020 · N303FE · Doug MD1030F · Fuselage Miscellaneous Structure
  > AFT AVIONIC COMPARTMENT, STA.475, LOOKING IN THRU REFRIGERATOR DOOR, L/H BILGE AREA FLOOR SUPPORT ANGLE SHOWING CORROSION.(MARKED) FABRICATED AND INSTALLED -59 INTERCOSTAL PER DWG NBA6074 AND SRM 51-31-01 VOL. 2.
- [SDR FDEA2020040840708](https://openairdocs.org/sdr/FDEA2020040840708.md): Attach Fitting · chafed · Mar 14, 2020 · N303FE · Doug MD1030F · Leading Edge Devices
  > R/H WING OUTBD SLAT #6 SLAT TRACK INBD ATTACHED FITTING IS WORN DUE TO EXCESSIVE CHAFING OF SLAT TRACK LOWER INBD RAIL. REPAIRED DAMAGED AREA BY BLENDING OUT AREA, ALODINED AND PRIMED AREA REFERENCE E.A. 8-5710-TT0353271 P1 " WINGS RH WING SLAT TRACK #6 SU
- [SDR FDEA2020040340660](https://openairdocs.org/sdr/FDEA2020040340660.md): Floor Support · corroded · Mar 14, 2020 · N303FE · Doug MD1030F · Fuselage Miscellaneous Structure
  > MAIN CARGO COMPARTMENT UNDER FLOOR AREA, FLOOR SUPPORT BEAM CORRODED AT STATION 2006 RBL 23, VIEWED FROM AFT WASTE TANK COMPARTMENT. MARKED DOT #1. REAMOVED AND REPLACED WITH NEW FLOOR SUPPORT BEAM AGA 7087-506 REF. DWG AGA 7087, SRM 51-31-01 VOL 2.
- [SDR FDEA2020040340589](https://openairdocs.org/sdr/FDEA2020040340589.md): Web · cracked · Mar 14, 2020 · N303FE · Doug MD1030F · Fuselage Miscellaneous Structure
  > L/H NLG WHEEL WELL WEB HAS 2 EA. CRACKS AT FASTENER HOLES AT STA. 495 AND Z= -73. (MARKED) INSTALLED REPAIR DOUBLERS, FILLERS I.A.W SRM 53-30-00 FIG. 6.
- [SDR FDEA2020031940589](https://openairdocs.org/sdr/FDEA2020031940589.md): Web · cracked · Mar 14, 2020 · N303FE · Doug MD1030F · Fuselage Miscellaneous Structure
  > L/H NLG WHEEL WELL WEB HAS 2 EA. CRACKS AT FASTENER HOLES AT STA. 495 AND Z= -73. (MARKED) REPAIR CRACKED REF SRM 53-30-00 FIG. 6 VOL. 1, AND DAC DWG NCA6046.
- [SDR FDEA2020032730606](https://openairdocs.org/sdr/FDEA2020032730606.md): Support Bracket · cracked · Mar 13, 2020 · N303FE · Doug MD1030F · Fuselage, Landing Gear Attach Fittings
  > NOSE LANDING GEAR L/H RETRACT SUPPORT BRACKET LUG CRACKED. REMOVED AND REPLACED ACA007-1 FITTING REF. DAC DWG NCA6044 AND EO 8-5340-7-5000 D PT2.
- [SDR FDEA2023011620725](https://openairdocs.org/sdr/FDEA2023011620725.md): Seat Track · damaged · Mar 12, 2020 · N303FE · Doug MD1030F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CARGO - SEAT TRACK DAMAGED AT STA.1661 LBL 106. REPAIRED SEAT TRACK DAMAGE REF: SRM 53-70-00 FIG.1 SHT.1 PG.3
- [SDR FDEA2020041020725](https://openairdocs.org/sdr/FDEA2020041020725.md): Seat Track · damaged · Mar 12, 2020 · N303FE · Doug MD1030F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CARGO - SEAT TRACK DAMAGED AT STA.1661 LBL 106. REPAIRED SEAT TRACK DAMAGE REF: SRM 53-70-00 FIG.1 SHT.1 PG.3
- [SDR FDEA2020031920588](https://openairdocs.org/sdr/FDEA2020031920588.md): Bulkhead · cracked · Mar 12, 2020 · N303FE · Doug MD1030F · Fuselage Main, Bulkhead
  > NOSE LANDING GEAR WHEELWELL; X= -24 Y= 494 Z= -58 HAS 2EA. 1" CRACKS @ ADJACENT FASTENERS ON BULKHEAD. REPAIR CRACKED REF SRM 53-30-00 FIG. 6 VOL. 1, AND DAC DWG NCA6046. INSTALLED REPAIR DOUBLERS I.A.W SRM 53-30-00 FIG. 6. REF NON-ROUTINE N00225.
- [SDR FDEA2020031920587](https://openairdocs.org/sdr/FDEA2020031920587.md): Bulkhead · cracked · Mar 12, 2020 · N303FE · Doug MD1030F · Fuselage Main, Bulkhead
  > NOSE LANDING GEAR WHEELWELL; X= -24 Y= 486 Z= -48 2" CRACK ON BULKHEAD. REPAIR CRACKED REF SRM 53-30-00 FIG. 6 VOL. 1, AND DAC DWG NCA6046. INSTALLED REPAIR DOUBLERS I.A.W SRM 53-30-00 FIG. 6. REF. N00225.
- [SDR FDEA2020040810713](https://openairdocs.org/sdr/FDEA2020040810713.md): Web · corroded · Mar 11, 2020 · N303FE · Doug MD1030F · Fuselage Miscellaneous Structure
  > LH WHEEL WELL - WEB (P/N AEA0026-5) BETWEEN STA 1501 - 1521 IS CORRODED. (AREA MARKED) REMOVED AND REPLACED WITH FABRICATED PART FX AEA0026-5 PER DWG AEA0026 AND SRM 51-30-00 V.2
- [SDR FDEA2020031910585](https://openairdocs.org/sdr/FDEA2020031910585.md): Bulkhead · cracked · Mar 11, 2020 · N303FE · Doug MD1030F · Fuselage Main, Bulkhead
  > NLG WHEEL WELL RH BULKHEAD -Y= 24, APPROX STA. 470 AND 476, -X= 41. TWO 6" INCH CRACKS. REPAIR CRACKED REF SRM 53-30-00 FIG. 6 VOL. 1. AND DAC DWG NCA6046. INSTALLED REPAIR DOUBLER I.A.W SRM 53-30-00 FIG. 6.
- [SDR FDEA2020042390766](https://openairdocs.org/sdr/FDEA2020042390766.md): Stiffener · cracked · Mar 9, 2020 · N303FE · Doug MD1030F · Aerodynamic Fairings
  > AFT BULKHEAD TAIL CONE AT UPPER R/H SUPPORT STIFFNER (3RD FROM THE TOP, MARKED IN RED) O/B IS CRACKED. CUT OUT DAMAGED SECTION AND INSTALLED REPAIR HAT CHANNEL PER E.A. 8-5310- T0353336 AND SRM 51-31-01 VOL. 1.
- [SDR FDEA2020032590603](https://openairdocs.org/sdr/FDEA2020032590603.md): Doubler · gouged · Mar 9, 2020 · N303FE · Doug MD1030F · Fuselage Main, Plate/Skin
  > FWD CARGO CUT-OUT - LOWER AFT CORNER - DOUBLER/TRIPLER GOUGED. REMOVED DAMAGED DOUBLERS AND REPLACED WITH NEW DOUBLERS,REF SRM 53-50- 00,FIG26.
- [SDR FDEA2020012750228](https://openairdocs.org/sdr/FDEA2020012750228.md): Valve · malfunctioned · Jan 25, 2020 · N303FE · Doug MD1030F · Fuel Transfer Valve
  > PDIS 303 28-43 6202 25JAN20 LIT OPEN U LOGPAGES:3213631 "TNK 1 TIP TRAPPED" AT FL350 FOR 3 MINUTS. ALERT CLEARED ITSELF, THEN RETURNED CAUSING DIVERT INTO KLIT MEL 25JAN20 16:55 LIT U RELEASED FOR SERVICE PER MEL: 28-43-04-A CATEGORY
- [SDR FDEA201910302785](https://openairdocs.org/sdr/FDEA201910302785.md): Switch · defective · Oct 30, 2019 · N303FE · Doug MD1030F · Passenger/Crew Doors
  > IN CLT DURING TAXI "DOOR DISARMED" LIGHT ON PANEL TO THE RIGHT SIDE OF THE R1 DOOR ILLUMINATED. ALL DOORS SHOWED CLOSED IN COCKPIT, AND DOOR LEVER WAS IN THE "SLIDE AREMED" POSITION PDM-CONTROL NUMBER 7205681 - VERIFIED MEL 52-10-03: MAIN ENTRY DOOR OR S
- [SDR FDEA201910212728](https://openairdocs.org/sdr/FDEA201910212728.md): Skin · damaged · Oct 21, 2019 · N303FE · Doug MD1030F · Fuselage Main, Plate/Skin
  > AIRCRAFT FUSELAGE STRUCK BY CONTAINER DURING STORM, LEAVING HOLE IN SKIN JUST FORWARD AND BELOW BULK CARGO DOOR. INSTALLED REPAIR REF MD-10 SRM 53-20-00 FIG 6 AND E.A. 8-5330-T0350329 P1 FUSELAGE - PLATES & SKINS - CONTAINER STRIKE LWR AFT L/H FUSELAGE -
- [SDR FDEA201907261702](https://openairdocs.org/sdr/FDEA201907261702.md): Unknown · smoke · Jul 26, 2019 · N303FE · Doug MD1030F · Air Distribution System
  > PDIS 303 21-10 5616 25JUL19 MCI OPEN U LOGPAGES:3142593 TURNED ON #2 PACK IN CRUISE. GOT SMOKE IN COCKPIT ONLY, TURNED #2 PACK OFF SMOKE DISSIPATED. MEL 26JUL19 00:32 MCI U RELEASED FOR SERVICE PER MEL: 21-51-01-A CATEGORY: C EXPIRATION
- [SDR FDEA201907211649](https://openairdocs.org/sdr/FDEA201907211649.md): Power Supply · failed · Jul 21, 2019 · N303FE · Doug MD1030F · Emergency Lighting
  > MDIS 303 33-50 5599 21JUL19 JFK OPEN U ON PRE-FLIGHT CHKS "EMER LT BAT 1 LO" DISPLAYED DURING EMERGENCY LIGHT TEST. MEL 21JUL19 10:27 JFK U RELEASED FOR SERVICE PER MEL: 33-50-02 CATEGORY: C EXPIRATION: 31JUL19 "MEL 33-50-02: EMER LIGHT
- [SDR FDEA201902120413](https://openairdocs.org/sdr/FDEA201902120413.md): Hinge · cracked · Feb 12, 2019 · N303FE · Doug MD1030F · Landing Gear Doors
  > RIGHT MAIN GEAR DOOR CENTER HINGE CRACKED. REMOVED AND RE3PLACED DOOR HINGE AND INTERNAL TEE FITTINGS AND INSTALLED GEAR DOOR PAN REPAIR UISNG REF MD10 SRM 52-10-00 FIG 5 AND REINSTALLED ACCESS PANEL UISNG REF SRM MD10 51-35-02.
- [SDR FDEA201806201548](https://openairdocs.org/sdr/FDEA201806201548.md): Wire · damaged · Jun 20, 2018 · N303FE · Doug MD1030F · Light System Wiring
  > EMER LIGHTS BAT 1 LO ALERT. FOUND DAMAGED WIRE AT P1-1756A PIN 1 GND CAUSING ONLY 64 VAC TO PIN 6 CHARGING POWER. REPAIRED WIRE GND AT PIN 1 CKS GOOD AS WELL AS 115 VAC AT PIN 6 C/W EMER LIGHT TEST. OPS TESTS GOOD.
- [SDR FDEA2018052301266](https://openairdocs.org/sdr/FDEA2018052301266.md): Power Supply · failed · May 20, 2018 · N303FE · Doug MD1030F · Emergency Lighting
  > EMERGENCY LIGHT BATTERY 1 LOW ALERT. REPLACED THE POWER SUPPLY. OPS CHECKED GOOD.
- [SDR FDEA2018042601111](https://openairdocs.org/sdr/FDEA2018042601111.md): Skin · cracked · Apr 24, 2018 · N303FE · Doug MD1030F · Wing, Plate/Skin
  > LEFT INBD UPPER SURFACE CRACKED ON OTBD TRIM AT XIFH 310. REMOVED AND REPLACED THE SKIN IAW DWG ARC 2443, ZONE 8.
- [SDR FDEA201804171037](https://openairdocs.org/sdr/FDEA201804171037.md): Skin · cracked · Apr 17, 2018 · N303FE · Doug MD1030F · Trailing Edge Flaps
  > LEFT INBD FLAP UPPER SKIN CRACKED ON OUTBD TRIM AT XIFH 310. REMOVED & INSTALLED A FABRICATED OUTBD TRIM SKIN IAW SRM 57-52-01, FIG 1, PAGE 1 VOL I, DRAWINGS ARC3098 AND ARC2258.
- [SDR FDEA2018042601102](https://openairdocs.org/sdr/FDEA2018042601102.md): Seat Track · corroded · Apr 12, 2018 · N303FE · Doug MD1030F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK BS 1753, RBL 107 SEAT TRACK FLANGE HAS CORROSION. INSTALLED A NEW SEAT TRACK AND SPLICES IAW SRM 53-70-00, FIG 1, SHEET 1, VOL 1, DWG SR10-53-002, SRM 51-31-01, VOL II, SRM 51-41-01, VOL II, AND EA 8-5310-TO339630.
- [SDR FDEA201804121076](https://openairdocs.org/sdr/FDEA201804121076.md): Seat Track · corroded · Apr 12, 2018 · N303FE · Doug MD1030F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK, BS 1759, RBL 107 SEAT TRACK FLANGE HAS CORROSION. INSTALLED A NEW SEAT TRACK AND SPLICE IAW SRM 53-70-00, FIG 1, SHEET 1, VOL 1, DWG SR10-53-002, SRM 51-31-01, VOL 2, AND SRM 51-41-01, VOL 2.
- [SDR FDEA201804121075](https://openairdocs.org/sdr/FDEA201804121075.md): Seat Track · corroded · Apr 12, 2018 · N303FE · Doug MD1030F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK, BS 1738, RBL 107 SEAT TRACK FLANGE HAS CORROSION. INSTALLED A NEW SEAT TRACK AND SPLICE IAW SRM 53-70-00, FIG 1, SHEET 1, VOL 1, DWG SR10-53-002, SRM 51-31-01, VOL 2, AND SRM 51-41-01, VOL 2.
- [SDR FDEA201804111074](https://openairdocs.org/sdr/FDEA201804111074.md): Seat Track · corroded · Apr 11, 2018 · N303FE · Doug MD1030F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK, BS 1681, RBL 107 SEAT TRACK FLANGE HAS CORROSION. INSTALLED A NEW SEAT TRACK AND SPLICES IAW SRM 53-70-00, FIG 1, SHEET 1, VOL 1, DWG SR10-53-002, SRM 51-31-01, VOL 2, AND SRM 51-41-01, VOL 2.
- [SDR FDEA201804080998](https://openairdocs.org/sdr/FDEA201804080998.md): Stop Fitting · cracked · Apr 8, 2018 · N303FE · Doug MD1030F · Fuselage Main, Structure
  > NR 3 ACM DOOR FRAME STOP FITTING HAS A.250 INCH CRACK. REPAIRED STOP FITTING IAW SRM 53-00-01, FIG 2, SHEET 2, VOL 1, AND EA.
- [SDR FDEA201804070997](https://openairdocs.org/sdr/FDEA201804070997.md): Hinge · cracked · Apr 7, 2018 · N303FE · Doug MD1030F · Fuselage, Door Hinge
  > NR 3 PACK DOOR AFT HINGE CRACKED. REPAIRED IAW SRM 53-00-01, FIG 2, PAGE 15, VOL 1, AND EA.
- [SDR FDEA201804070918](https://openairdocs.org/sdr/FDEA201804070918.md): Shear Tie · corroded · Apr 7, 2018 · N303FE · Doug MD1030F · Fuselage Internal Mounting Structure
  > AFT CARGO BAY, BS 1967, LONGERON 48L SHEAR TIE CORRODED. REMOVED AND REPLACED THE SHEAR TIE IAW DWG AGA7058.
- [SDR FDEA201804051100](https://openairdocs.org/sdr/FDEA201804051100.md): Seat Track · corroded · Apr 5, 2018 · N303FE · Doug MD1030F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN BS 1761 - 1741 BETWEEN RBL 47 - 74, CORROSION FOUND ON THE SEAT TRACK. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 53-70-00, VOL 1, FIG 1, PAGE 3.

Next page: https://openairdocs.org/aircraft/N303FE/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 = 'N303FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N303FE/reports

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