# Service difficulty reports: N306FE

A list on [N306FE](https://openairdocs.org/aircraft/N306FE.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 4 · 167 reports

- [SDR FDEA202211292851](https://openairdocs.org/sdr/FDEA202211292851.md): Engine · fire · Nov 29, 2022 · N306FE · Doug MD1030F · Engine (Turbine/Turboprop)
  > DURING ENGINE 1 START SEQUENCE, ENGINE TOOK LONGER THAN NORMAL TO START. IGNITER USED WAS B, SWITCHED TO A DURING START. ENGINE APPEARED TO START NORMALLY, BUT GROUND CREW ANNOUNCED OVER HEADSET THAT THE AIRPLANE WAS ON FIRE AND TO EVACUATE THE AIRPLANE
- [SDR FDEA202209222357](https://openairdocs.org/sdr/FDEA202209222357.md): Bulb · no test · Sep 22, 2022 · N306FE · Doug MD1030F · Emergency Equipment
  > ON ARRIVAL EVACUATE SLIDE REMOTE PRESS TO TEST INDICATION SWITCH L1 DOOR LIGHT INOP. REPLACED BULBS IN L1 DOOR INDICATOR PRESS TO TEST SWITCH IN REF TO AMM 25-61-03-5-0, OPS CHECKS GOOD AT THIS TIME, LIGHTS WORKED FINE, NO PROBLEM NOTED BY MX AT THIS TIME,
- [SDR FDEA202206071399](https://openairdocs.org/sdr/FDEA202206071399.md): Warning Message · illuminated · Jun 7, 2022 · N306FE · Doug MD1030F · Central Warning
  > UNEVENTFUL FLIGHT FROM SMF UNTIL ALERT. LEVEL AT FL310 APROX 2 30 INTO FLIGHT. COST INDEX 200 GAVE US.837MACH. GOT TRI-TONE AND MASTER WARNING LIGHT, WITH "LWR AFT CRG FIRE". DECLARED EMERGENCY AND DIVERTED TO CLOSEST FIELD KTUL. 13MIN FROM DECLARATION
- [SDR FDEA202202180321](https://openairdocs.org/sdr/FDEA202202180321.md): None · none · Feb 18, 2022 · N306FE · Doug MD1030F · Fuel Indicating System
  > DESCENDING INTO KMEM WITH FSC IN MANUAL, WE RECIEVED LEVEL 1 ALERT, TANK 3 QTY LO. FUEL WAS 7.1/6.2/5.2. THE QRH SAID TO TREAT AS REAL SO WE DECLARED AN EMERGENCY AND LANDED. AT SHUTDOWN FUEL QTYS WERE 5.9/5.3/3.9. RETERMINTATED WIRES 3E901Z22BL, 3E901AA
- [SDR FDEA202111282943](https://openairdocs.org/sdr/FDEA202111282943.md): None · none · Nov 28, 2021 · N306FE · Doug MD1030F · Fuselage Main, Plate/Skin
  > THIS CARD IS CREATED FOR TRACKING PURPOSES TO CREATE A RDR/SDR FOR THE REPAIR DONE TO MCD LOWER JAMB AT STA. 697.87 UNDER E.A.8-5330-T0365660 B PART 2 CREATED RDR/SRD FOR MCD LOWER JAMB REPAIR USING E.A. 8-5330-T0365660 B PART 2.
- [SDR FDEA202107291917](https://openairdocs.org/sdr/FDEA202107291917.md): Rib · cracked · Jul 29, 2021 · N306FE · Doug MD1030F · Wing, Rib/Bulkhead
  > RIGHT HAND WING - LOWER SURFACE - SECONDARY STRUCTURE IS CRACKED AFT/OUTBOARD OF FUELING PANEL (MARKED). REPAIRED RIB PER EA.8-5710-T0363338
- [SDR FDEA202107191817](https://openairdocs.org/sdr/FDEA202107191817.md): Panel · corroded · Jul 19, 2021 · N306FE · Doug MD1030F · Wing, Plate/Skin
  > L/H WING PANEL 541LB L/E LAND CORROSION AROUND SCREW HOLE.(MARKED) REMOVED CORROSION,.118 REMAINING THICKNESS,.132 ORIGINAL THICKNESS,.012 MATERIAL REMOVED PER SRM 57-00-01 VOL I, WITHIN LIMITS. TREATED AND PAINTED SRM REF 51-21-01 VOL II.
- [SDR FDEA202107031710](https://openairdocs.org/sdr/FDEA202107031710.md): Support · worn · Jul 3, 2021 · N306FE · Doug MD1030F · Leading Edge Devices
  > RIGHT WING L/E #6 SLAT TRACK SUPPORT STRUCTURE GOUGED BY FWD O/B RUB BLOCK. (DOT 4) ACCOMPLISHED EA 8-5710-T0362811 WINGS - BASIC WING STRUCTURE - RH WING SLAT TRACK #6 SUPPORT OUTBD RIB AT XOS431 - GOUGE.
- [SDR FDEA202107011645](https://openairdocs.org/sdr/FDEA202107011645.md): Panel · cracked · Jul 1, 2021 · N306FE · Doug MD1030F · Cargo/Baggage Doors
  > PANEL ACA3213 (231LF) CRACK ALONG ONE OF THE HOLES. FABRICATED A NEW PANEL.
- [SDR FDEA202107011646](https://openairdocs.org/sdr/FDEA202107011646.md): Floor Panel · delaminated · Jul 1, 2021 · N306FE · Doug MD1030F · Fuselage Floor Panel
  > DELAMINATED FLOOR PANEL, MAIN UPPER CARGO [L/H, O/B ][STA 600-695]. REMOVED AND REPLACED DELAMINATED FLOOR PANEL REF SRM 51-31-01 VOL2
- [SDR FDEA202106291615](https://openairdocs.org/sdr/FDEA202106291615.md): Rib · cracked · Jun 29, 2021 · N306FE · Doug MD1030F · Fuselage Main, Structure
  > RIB CRACKED REMOVED AND FABRICATED NEW RIB AND INSTALLED PER DOUGLAS DWG ANB7143 AND SRM 51-31-00 VOL 2
- [SDR FDEA202106281614](https://openairdocs.org/sdr/FDEA202106281614.md): Skin · worn · Jun 28, 2021 · N306FE · Doug MD1030F · Wing, Plate/Skin
  > R/H WING FIX L/E O/B SIDE HAS WORN MARK FROM SLAT # 2 RUBBING AGAINST IT. LOCATION OF DAMAGE IS ON TOP I/B SIDE STA. XORS 160. REPAIRED PER SRM 57-10-00 VOL 1 FIG 15A.
- [SDR FDEA202106271609](https://openairdocs.org/sdr/FDEA202106271609.md): Skin · corroded · Jun 27, 2021 · N306FE · Doug MD1030F · Fuselage Main, Plate/Skin
  > CORROSION AT STA.1926-1942 L47-49 BELOW AFT CARGO DOOR. REPAIRED CORROSION AT STA.1926-1942 L47-49 PER EA #T 8-5310-T0362734 TITLED: FUSELAGE - MAINFRAME - SKIN STA 1910-1942, L48 - L44 AFT CARGO DOOR UNDER SCUFF PLATE - CORRSION
- [SDR FDEA202106251589](https://openairdocs.org/sdr/FDEA202106251589.md): Floor Panel · delaminated · Jun 25, 2021 · N306FE · Doug MD1030F · Fuselage Floor Panel
  > LOWER FUSELAGE AFT CARGO PANEL 187FF DELAMINATED P/N AGA3877-15 FABRICATED NEW LOWER FUSELAGE AFT CARGO COMPARTMENT PANEL 187FF P/N AGA3877- 15 REF FEDEX DRAWING SRZ-25-005 AND SRZ-25-011
- [SDR FDEA202106211577](https://openairdocs.org/sdr/FDEA202106211577.md): Floorboard · damaged · Jun 21, 2021 · N306FE · Doug MD1030F · Fuselage Floor Panel
  > FLOORBOARD SR84852-125 DAMAGED. FABRICATED FLOORBOARD SR84852-125 PER FEDEX DRW SRZ-25-001
- [SDR FDEA202106181625](https://openairdocs.org/sdr/FDEA202106181625.md): Bracket · cracked · Jun 18, 2021 · N306FE · Doug MD1030F · Fuselage Main, Structure
  > #3 ACM RAM AIR INLET SHELL BRACKET THAT IS MOUNTED BELOW THE AVIONINCS RACK IS BROKEN. REMOVED & REPLACED BRACKET REF ABA7221 & MD10-30 SRM 51-33-01 VOL II.
- [SDR FDEA202106171565](https://openairdocs.org/sdr/FDEA202106171565.md): Floor Panel · delaminated · Jun 17, 2021 · N306FE · Doug MD1030F · Fuselage Floor Panel
  > LOWER FUSELAGE AFT CARGO PANEL 187CF DELAMINATED P/N AGA7429-9 FABRICATED LOWER FUSELAGE AFT CARGO COMPARTMENT PANEL 187CF P/N AGA7429-9 REF FEDEX DRAWING SRZ-25-005 AND SRZ-25-011
- [SDR FDEA202106171560](https://openairdocs.org/sdr/FDEA202106171560.md): Floor Panel · delaminated · Jun 17, 2021 · N306FE · Doug MD1030F · Fuselage Floor Panel
  > LOWER FUSELAGE AFT CARGO FLOOR BOARD PANEL 187BF P/N AGA7428-7 IS DELAMINATED AND MISSING INSERTS FABRICATED LOWER FUSELAGE AFT CARGO FLOOR PANEL 187BF P/N AGA7428-7 REF FEDEX DRAWING SRZ-25-005 AND SRZ-25-011
- [SDR FDEA202106151549](https://openairdocs.org/sdr/FDEA202106151549.md): Floorboard · delaminated · Jun 15, 2021 · N306FE · Doug MD1030F · Fuselage Floor Panel
  > LWR FWD PIT FLOOR BOARD 123KF DAMAGED FABRICATED PANEL PER FEDEX DRAWING SRZ-25-005
- [SDR FDEA202106141706](https://openairdocs.org/sdr/FDEA202106141706.md): Skin · dented · Jun 14, 2021 · N306FE · Doug MD1030F · Cargo/Baggage Doors
  > AFT-INTERMEDIATE/CENTER CARGO - AT APX STA 1790 L34 AFT OF CTR CARGO DOOR, DENT IS PRESENT (TOP DENT). 0000098319: NAVARRO, ENRIQUE S - 08-JUL-2021 18:25 REPAIRED DENT IN REFERENCE TO MD10-30 SRM 53-20-00 FIG 6 SHEET 7 VOL 1. MAJOR REPAIR.
- [SDR FDEA202106121510](https://openairdocs.org/sdr/FDEA202106121510.md): Floor Panel · damaged · Jun 12, 2021 · N306FE · Doug MD1030F · Fuselage Floor Panel
  > CENTER CARGO FLOOR BOARD 183YF IS DAMAGED FABRICATED CENTER CARGO FLOOR PANEL 183YF REF FEDEX DRAWING SRZ-25-005
- [SDR FDEA202106111505](https://openairdocs.org/sdr/FDEA202106111505.md): Floorboard · delaminated · Jun 11, 2021 · N306FE · Doug MD1030F · Fuselage Floor Panel
  > DELAMINATION ADA0244-13 (127EF). FABRICATED PER FEDEX DRAWING SRZ-25-005.
- [SDR FDEA202106111503](https://openairdocs.org/sdr/FDEA202106111503.md): Floorboard · delaminated · Jun 11, 2021 · N306FE · Doug MD1030F · Fuselage Floor Panel
  > DELAMINATION ADA0238-9 (127BF). FABRICATED PER FEDEX DRAWING SRZ-25-005.
- [SDR FDEA202106111502](https://openairdocs.org/sdr/FDEA202106111502.md): Floorboard · damaged · Jun 11, 2021 · N306FE · Doug MD1030F · Fuselage Floor Panel
  > DAMAGED FLOORBOARD ADA8349-3 (242DF) FABRICATED PER FEDEX DRAWING SRZ-25-005.
- [SDR FDEA202106091623](https://openairdocs.org/sdr/FDEA202106091623.md): Nut Plate · damaged · Jun 9, 2021 · N306FE · Doug MD1030F · Vertical Stabilizer
  > NUMEROUS NUT PLATES DAMAGED INSIDE ZONE 316 R/H UPPER SIDE. AFTER FURTHER INSPECTION CORROSION WAS FOUND AND DETERMINED OUT OF LIMITS. INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 53-20-00 #24 AND EA NO. 8-5330-T0362493. REPLACED NUT-PLATES IAW SRM 51-31-01
- [SDR FDEA202106091478](https://openairdocs.org/sdr/FDEA202106091478.md): Floorboard · damaged · Jun 9, 2021 · N306FE · Doug MD1030F · Fuselage Floor Panel
  > DAMAGE FLOOR BOARD AGA7078-70(292EF). FABRICATED NEW FLOOR BOARD PER FEDEX DRAWING SRZ-25-005.
- [SDR FDEA202106091475](https://openairdocs.org/sdr/FDEA202106091475.md): Skin · delaminated · Jun 9, 2021 · N306FE · Doug MD1030F · Wing, Plate/Skin
  > R/H TRAILING EDGE PANEL 641HB FOUND TO HAVE DELAMINATION AFTER REMOVAL, MARKED AREA IN RED REPAIRED R/H TRAILING EDGE PANEL 641HB AT THE MARKED DELAMINATED AREA REF SRM 51-71-00 VOL 2 PAGE 3 TO PAGE 47 AND DOUGLAS DRAWING ARC0258
- [SDR FDEA202106081619](https://openairdocs.org/sdr/FDEA202106081619.md): Bracket · cracked · Jun 8, 2021 · N306FE · Doug MD1030F · Fuselage Miscellaneous Structure
  > LH WING UPPER SURFACE, FUSELAGE STA.1341 - LOWER BRACKET FOR FAIRING SUPPORT/FRAME CRACKED. BRACKET UNDER PANEL 151FT. REMOVED & REPLACED BRACKET REF DAC DWG ANB7142 & MD 10-30 SRM 51-33-01 VOL II
- [SDR FDEA202106081599](https://openairdocs.org/sdr/FDEA202106081599.md): Bracket · cracked · Jun 8, 2021 · N306FE · Doug MD1030F · Aerodynamic Fairings
  > LH WING UPPER SURFACE, FUSELAGE STA.1298 - LOWER BRACKET FOR FAIRING SUPPORT/FRAME CRACKED. BRACKET UNDER PANEL 151ET. REMOVED AND REPLACED BRACKET REF DAC DWG ANG7139.
- [SDR FDEA202106081598](https://openairdocs.org/sdr/FDEA202106081598.md): Bracket · cracked · Jun 8, 2021 · N306FE · Doug MD1030F · Aerodynamic Fairings
  > LH WING UPPER SURFACE, FUSELAGE STA.1321 - LOWER BRACKET FOR FAIRING SUPPORT/FRAME CRACKED. BRACKET UNDER PANEL 151FT. REMOVED & REPLACED BRACKET REF DAC DWG ANB7141 & MD10-30 SRM 51-33-01 VOL II
- [SDR FDEA202106081597](https://openairdocs.org/sdr/FDEA202106081597.md): Bracket · cracked · Jun 8, 2021 · N306FE · Doug MD1030F · Aerodynamic Fairings
  > LH WING UPPER SURFACE, FUSELAGE STA.1273 - LOWER BRACKET FOR FAIRING SUPPORT/FRAME CRACKED. BRACKET UNDER PANEL 151ET. REMOVED AND REPLACED BRACKET REF ANB7138 DAC DWG.
- [SDR FDEA202106081588](https://openairdocs.org/sdr/FDEA202106081588.md): Floor Support · corroded · Jun 8, 2021 · N306FE · Doug MD1030F · Fuselage Miscellaneous Structure
  > AFT CARGO COMPT RH TUNNEL STA 1853 RBL 85 MAIN DECK FLOORBOARD SUPPORT CORRODED. MRKD REMOVED, FABRICATED AND INSTALLED REPLACEMENT FLOOR SUPPORT AGA3814-34 REF. DRAWING AGA3814 AND SRM 51-33-01 VOL.2.
- [SDR FDEA202106081550](https://openairdocs.org/sdr/FDEA202106081550.md): Skin · worn · Jun 8, 2021 · N306FE · Doug MD1030F · Wing, Plate/Skin
  > R/H WING DROOP LEADING EDGE FLEX SKIN ASSY (PN:ARB2404-3) HAS WORN SLOT HOLE ON SKIN (MARKED). 0004002945: FICKES, KYLE S - 15-JUN-2021 23:15 REMOVED DAMAGED SLOTTED FLEX SKIN AND REPLACED WITH NEW FABRICATED SKIN REF. MD10-30 SRM 57-10-00 VOL.1 PG.191 F
- [SDR FDEA202106071774](https://openairdocs.org/sdr/FDEA202106071774.md): Striker · worn · Jun 7, 2021 · N306FE · Doug MD1030F · Fuselage Miscellaneous Structure
  > AFT FUSELAGE COMPT DOOR, LATCH INNER STRIKER SURFACE WORN AT MARKED POSITIONS. REPAIRED PER REF E.A 8-5330-T-0362904:FUSELAGE- PLATES & SKINS - ACCESS DOOR 311AB CUTOUT- DAMAGED DOUBLER. REF MD10-30 SRM VOL II 51-31-01 & MD10-30 SRM 10-30 VOL II 51- 33-0
- [SDR FDEA202106071865](https://openairdocs.org/sdr/FDEA202106071865.md): Skin · worn · Jun 7, 2021 · N306FE · Doug MD1030F · Fuselage Main, Plate/Skin
  > LH FUSELAGE STA 695 SKIN HAS GOUGE AT MAIN CARGO DOOR CUTOUT. MRKD AT LWR JAMB AFT OF LATCH SPOOL #4 REPAIRED PER EA # 8-5330-T0362732 P1
- [SDR FDEA202106071591](https://openairdocs.org/sdr/FDEA202106071591.md): Doubler · cracked · Jun 7, 2021 · N306FE · Doug MD1030F · Wing, Plate/Skin
  > RH WING LE INTERNAL STRUCTURE AT APPROX XORS 555 - BEADED DOUBLER IS CRACKED AT SEVERAL LOCATIONS. CRACKS HAVE BEEN CONFIRMED WITH NDT HFEC AND ENDS MARKED. INSTALLED REPAIR DOUBLER, REF EA: # 8-5710-T0362282.
- [SDR FDEA202106071509](https://openairdocs.org/sdr/FDEA202106071509.md): Skin · cracked · Jun 7, 2021 · N306FE · Doug MD1030F · Wing, Plate/Skin
  > L/H WING SKIN AT THE SLAT ANTI-ICE DUCT CUT OUT UPPER INBOARD CORNER HAS A.400 IN. CRACK (MARKED) REPAIRED NOTED CRACK AS REQUIRED PER SRM REQUIREMENTS REF SRM 57-10-00 VOL 1 FIG 103 PG 483-488
- [SDR FDEA202106071556](https://openairdocs.org/sdr/FDEA202106071556.md): Doubler · cracked · Jun 7, 2021 · N306FE · Doug MD1030F · Wing, Plate/Skin
  > RH WING LE INTERNAL STRUCTURE AT XORS 683 - BEADED DOUBLER IS CRACKED AT TWO (2) LOCATIONS. CRACKS HAVE BEEN CONFIRMED WITH HFEC AND ENDS MARKED. INSTALLED REPAIR DOUBLER, REF SRM 57-10-00 FIG 71, VOL 1.
- [SDR FDEA202106071461](https://openairdocs.org/sdr/FDEA202106071461.md): Floorboard · damaged · Jun 7, 2021 · N306FE · Doug MD1030F · Fuselage Floor Panel
  > AFA3200-2 DAMAGED FABRICATED PER DRAWING SRZ-25-005
- [SDR FDEA202106061570](https://openairdocs.org/sdr/FDEA202106061570.md): Former · cracked · Jun 6, 2021 · N306FE · Doug MD1030F · Wing Spar
  > LH WING LE INTERNAL STRUCTURE AT XORS 562 AND APPROX 18" AFT OF LE - FORMER/FRAME IS CRACKED APPROX.750" IN LENGTH. CRACKED CONFIRMED WITH HFEC AND ENDS MARKED. REPLACED DOUBLER REF DAC DWG ARB3954 & SRM 51-33-01 VOL II MD10-30
- [SDR FDEA202106061541](https://openairdocs.org/sdr/FDEA202106061541.md): Beam · cracked · Jun 6, 2021 · N306FE · Doug MD1030F · Fuselage Main, Structure
  > FWD LWR CARGO COMPT STA 595 BULKHEAD BEAM NCA 6044 CRACKED 4 PLACES. MRKD X DIM -5 AND 5 TWO PLACES EACH. Z DIM -59.38 CORRECTION Z DIM SHOULD REA -80 REPAIRED BULKHEAD BEAM NCA6044-29 AT NOTED LOCATION REF. SRM 53-40-00 VOL. 1 FIG. 36 SHEETS 1-4 PGS. 143-
- [SDR FDEA202106061566](https://openairdocs.org/sdr/FDEA202106061566.md): Doubler · cracked · Jun 6, 2021 · N306FE · Doug MD1030F · Wing Main, Frame Structure
  > LH WING LE INTERNAL STRUCTURE AT XORS 562 - BEADED DOUBLER IS CRACKED AT SEVERAL LOCATIONS. CRACKS HAVE BEEN CONFIRMED WITH HFEC AND ENDS MARKED. INSTALLED DOUBLER REF MD10-30 SRM 57-10-00 VOL 1 PG 222 FIG 71 MAJOR REPAIR
- [SDR FDEA202106021450](https://openairdocs.org/sdr/FDEA202106021450.md): Web · cracked · Jun 2, 2021 · N306FE · Doug MD1030F · Fuselage Miscellaneous Structure
  > NOSE W/W, STA 472, RH WEB NCA6046-3 IS CRACKED JUST BELOW THE REPAIR DOUBLER / ABOVE HORIZONTAL STIFFENER(MARKED). THE CORRECT PART NUMBER FOR THE WEB IS NCA6246-3 0005108155: SHERWIN, SAMUEL M - 14-JUN-2021 07:28 REPAIRED NOSE W/W, STA 472, RH WEB REF SRM
- [SDR FDEA202106021520](https://openairdocs.org/sdr/FDEA202106021520.md): Seat Track · worn · Jun 2, 2021 · N306FE · Doug MD1030F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CARGO DECK, STA. 1265, LBL 27.50", SEAT TRACK APROX 16" SECTION WORN. DOT #79 REPLACED DAMAGED SEAT TRACK FROM STA 1255 TO 1310 LBL 27.5 REF SRM 53-70-00 FIG 1 VOL 1, SRM 51-31-01 VOL 2, SRM 51-41-01 VOL 2, AND SR10-53-002. MAJOR REPAIR
- [SDR FDEA202106021477](https://openairdocs.org/sdr/FDEA202106021477.md): Seat Track · worn · Jun 2, 2021 · N306FE · Doug MD1030F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CARGO DECK, STA. 1265, LBL 8.50", SEAT TRACK WORN. DOT #9 REPLACED DAMAGED SEAT TRACK FROM STA 1269 TO 1334 AT LBL 8.50 REF SRM 53-70-00 FIG 1 VOL 1, SRM 51-31-01 VOL 2, SRM 51-41-01 VOL 2, AND SR10-53-002. MAJOR REPAIR
- [SDR FDEA202106021476](https://openairdocs.org/sdr/FDEA202106021476.md): Seat Track · worn · Jun 2, 2021 · N306FE · Doug MD1030F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CARGO DECK, STA. 1255, LBL 8.50", SEAT TRACK WORN. DOT #67. REPLACED DAMAGED SEAT TRACK FROM STA 1269 TO 1334 AT LBL 8.50 REF SRM 53-70-00 FIG 1 VOL 1, SRM 51-31-01 VOL 2, SRM 51-41-01 VOL 2, AND SR10-53-002. MAJOR REPAIR
- [SDR FDEA2020061641236](https://openairdocs.org/sdr/FDEA2020061641236.md): Wire Harness · defective · Jun 14, 2020 · N306FE · Doug MD1030F · Engine Indicating System Wiring
  > ON DESCENT NR 2 ENGINE EGT EXCEEDANCE 1007*C, PRECAUTIONARY SHUT DOWN. NO OTHER EXCEEDANCES, EGT GAUGE "X'D" OUT SEVERAL TIMES. WHEN TROUBLESHOOTING EGT HARNESS PER AMM 77-21-01-2, FOUND UPPER HARNESS LEAD HAD NORMAL, THEN HIGH THEN OPEN RESISTANCE WHEN SHAK
- [SDR FDEA2020062300884](https://openairdocs.org/sdr/FDEA2020062300884.md): Skin · dented · May 3, 2020 · N306FE · Doug MD1030F · Fuselage Main, Plate/Skin
  > ON WALK AROUND FOUND DENT ON R/H SIDE OF AIRCRAFT JUST AFT RADOME. FABRICATED DOUBLER, TRIPLER AND FILLER. DRILLED AND COUNTERSINK. ALODINED AND PRIMED IAW SRM 53-20-00 CLASS 2 REPAIR FIG 6. INSTALLED REPAIR PARTS IAW SR
- [SDR FDEA2020050430884](https://openairdocs.org/sdr/FDEA2020050430884.md): Skin · damaged · May 3, 2020 · N306FE · Doug MD1030F · Fuselage Main, Plate/Skin
  > ON WALK AROUND FOUND DENT ON R/H SIDE OF AIRCRAFT JUST AFT RADOME. FABRICATED DOUBLER, TRIPLER AND FILLER. DRILLED AND COUNTERSINK. ALODINED AND PRIMED IN R
- [SDR FDEA201909072132](https://openairdocs.org/sdr/FDEA201909072132.md): Switch · faulty · Sep 7, 2019 · N306FE · Doug MD1030F · Landing Gear Position and Warning
  > UPON GEAR RETRACTION ALL THE PRIMARY GEAR AND SECONDARY LIGHTS ILLUMINATED WITH THE GEAR HANDLE UP. FOLLOWED QRH PROCEDURES AND THE GEAR RETRACTED. TROUBLESHOOT IAW FIM 32-30-00-2, PIN A AND B, DID NOT READ CONTINUITY ON SW S1-392. REMOVED AND REPLACED LANDING

Next page: https://openairdocs.org/aircraft/N306FE/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 = 'N306FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N306FE/reports

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