# Service difficulty reports: N307FE

A list on [N307FE](https://openairdocs.org/aircraft/N307FE.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 · 140 reports

- [SDR FDEA202211292863](https://openairdocs.org/sdr/FDEA202211292863.md): Fairing · cracked · Nov 29, 2022 · N307FE · Doug MD1030F · Nacelle/Pylon Miscellaneous Structure
  > #3 ENGINE PYLON HAS CRACKED PANEL,LOCATED AT LOWER SURFACE AFT OF EXUAST NOZZLE AND FORWARD OF V PANEL. REPAIRED PYLON PANEL ASREQUIRED IAW SRM 54-00-01 FIG. 2B SHEET 2.
- [SDR FDEA202202080248](https://openairdocs.org/sdr/FDEA202202080248.md): None · failed · Feb 8, 2022 · N307FE · Doug MD1030F · Fuel Controlling System
  > PDIS 307 73-20 9023 08FEB22 DEN OPEN U ON TAKEOFF ROLL, NUMBER 3 ENGINE VERY SLOW TO SPOOL UP. AFTER MAX THRUST WAS SET NUMBER 2 STARTING ROLLING BACK AND WE GOT THE RED ENG FAIL LIGHT. REJECTED TAKEOFF. REMOVED AND REPLACED THE MEC, FUEL P
- [SDR FDEA202112253139](https://openairdocs.org/sdr/FDEA202112253139.md): None · none · Dec 25, 2021 · N307FE · Doug MD1030F · Fuselage Miscellaneous Structure
  > LPE ACTIVATED AFTER ROTATION, GO AROUND/TAIL STRIKE LANDING PERFORMANCE ENHANCEMENT FACT 25DEC21 01:19 YYZ U TAIL STRIKE PART A INSPECTION CARRIED OUT I.A.W AMM 05-51-12-6. NO DAMAGE NOTED.A/C OK FOR SERVICE. TALE STRIKE PART A INSPECTION CARRIED OUT
- [SDR FDEA202110032448](https://openairdocs.org/sdr/FDEA202110032448.md): Paint · worn · Oct 3, 2021 · N307FE · Doug MD1030F · Elevator, Plate/Skin
  > RH OB ELEVATOR BARE METAL AT LOWER SURFACE AFT OF ACTUATOR FOUND RH OB ELEVATOR LOWER SURFACE AFT OF INB ACTUATOR (PANEL 346BB) HAS MARKED MISSING PAINT, PREPPED AND PAINTED PER MD10-30 SRM 51-21-02 VOL 2 PARAGRAPH 2 STEPS A-J. PERFORMED WEIGHT AND BALANCE
- [SDR FDEA202110022486](https://openairdocs.org/sdr/FDEA202110022486.md): Skin · damaged · Oct 2, 2021 · N307FE · Doug MD1030F · Powerplant System
  > NUMBER ONE R/H SLAT HAS SKIN DAMAGED FORWARD SIDE. REPAIRED DAMAGE IN REFERENCE TO MD-10-30 SRM 57-10-00 FIG 43 VOL 1
- [SDR FDEA202109232395](https://openairdocs.org/sdr/FDEA202109232395.md): Panel · damaged · Sep 23, 2021 · N307FE · Doug MD1030F · Trailing Edge Flaps
  > LEFT WING OUTBOARD FLAP PANEL ABOVE OUTBOARD END OF FLAPMISDRILLED HOLE AT I/B CORNER OF OUTBOARD END. REPAIRED PANEL PER E.A. 8-5710-T0364140(P1)- BASIC WING STRUCTURE - LH WING TE HONEYCOMB PANEL P/N ARC0616-501 (MAJOR REPAIR)
- [SDR FDEA202109232394](https://openairdocs.org/sdr/FDEA202109232394.md): Panel · damaged · Sep 23, 2021 · N307FE · Doug MD1030F · Trailing Edge Flaps
  > LEFT WING OUTBOARD FLAP PANEL ABOVE OUTBOARD END OF FLAPS HAS MISDRILLED HOLES. REPAIRED PANEL PER E.A. 8-5710-T0364140 (P1)-BASIC WING STRUCTURE - LH WING TE HONEYCOMB PANEL P/N ARC0616-501(MAJOR REPAIR)
- [SDR FDEA202109232387](https://openairdocs.org/sdr/FDEA202109232387.md): Floorboard · damaged · Sep 23, 2021 · N307FE · Doug MD1030F · Fuselage Floor Panel
  > AFT CARGO COMPARTMENT FLOOR BOARD 187EF DAMAGED FABRICATED NEW FLOOR BOARD SRZAGA3876-3
- [SDR FDEA202109142302](https://openairdocs.org/sdr/FDEA202109142302.md): Floorboard · delaminated · Sep 14, 2021 · N307FE · Doug MD1030F · Fuselage Floor Panel
  > DELAMINATED FABRICATE NEW AKC7082-3 FLOOR BOARD PER FEDEX DRAWING SRZ-25-005
- [SDR FDEA202109132296](https://openairdocs.org/sdr/FDEA202109132296.md): Floorboard · delaminated · Sep 13, 2021 · N307FE · Doug MD1030F · Fuselage Floor Panel
  > DELAMINATED FABRICATE NEW AKC 7082-19 FLOOR BOARD PER FEDEX DRAWING SRZ-25-005
- [SDR FDEA202109112298](https://openairdocs.org/sdr/FDEA202109112298.md): Floor Support · corroded · Sep 11, 2021 · N307FE · Doug MD1030F · Fuselage Miscellaneous Structure
  > MAIN DECK FLOORBOARD SUPPORT ANGLE STA. 1581 LBL=15 EXFOLIATED/CORRODED. REMOVED EXFOLIATED/CORRODED FLOOR SUPPORT ANGLE P/N AFA3853-15 AT STA 1581 LBL 15. FABRICATED, PROCESSED,TREATED, PRIMED, AND INSTALLATED NEW FABRICATED FLOOR SUPPORT ANGLE. REF.
- [SDR FDEA202109112315](https://openairdocs.org/sdr/FDEA202109112315.md): Floorbeam · corroded · Sep 11, 2021 · N307FE · Doug MD1030F · Fuselage Main, Floor Beam
  > MAIN DECK FLOOR PANEL SUPPORT ANGLE AT STA 1661 RBL 75 TO 107 CORRODED AROUND SEVERAL CLIPNUTS REMOVED AND REPLACE FLOOR SUPPORT REF DOUGLAS DRAWING AFA-3853.
- [SDR FDEA202109112316](https://openairdocs.org/sdr/FDEA202109112316.md): Floorbeam · corroded · Sep 11, 2021 · N307FE · Doug MD1030F · Fuselage Main, Floor Beam
  > MAIN DECK FLOORBOARD SUPPORT ANGLE STA. 1661 LBL=107.25 EXFOLIATED/CORRODED. (MRKD) REMOVED AND REPLACED WITH NEW FABRICATED FLOOR BOARD SUPPORT P/N AFA3853-501 REF DAC DWG AFA3853 AND SRM 51-33-01 VOL. 2
- [SDR FDEA202109112303](https://openairdocs.org/sdr/FDEA202109112303.md): Floorbeam · corroded · Sep 11, 2021 · N307FE · Doug MD1030F · Cargo Compartments
  > MAIN DECK FLOOR SUPPORT ANGLE AT STA 1901 RBL 08 TO RBL 27 CORRORED MAIN DECK FLOOR SUPPORT ANGLE AT STA 1901 RBL 08 TO RBL 27 HAS BEEN REPAIRED PER DWG # AGA7559.
- [SDR FDEA202109112290](https://openairdocs.org/sdr/FDEA202109112290.md): Floorboard · delaminated · Sep 11, 2021 · N307FE · Doug MD1030F · Fuselage Floor Panel
  > DELAMINATED FABRICATED NEW ARC7082-55 FLOOR PANEL PER SRZ-25-005
- [SDR FDEA202109072246](https://openairdocs.org/sdr/FDEA202109072246.md): Panel · delaminated · Sep 7, 2021 · N307FE · Doug MD1030F · Vertical Stabilizer, Plate/Skin
  > DELAMINATION ON AJC7001-149 STEP FABRICATED NEW AJC7001-149 STEP PER SRZ-25-005
- [SDR FDEA202109032517](https://openairdocs.org/sdr/FDEA202109032517.md): None · damaged · Sep 3, 2021 · N307FE · Doug MD1030F · Wing Main, Frame Structure
  > TEE FITTING HOLES DAMAGED. FABRICATE NEW FITTING PER DWG ARB3280 0000832258: PUTZ, JARED J - 28-SEP-2021 16:44 FABRICATED TEE-TENSION BEVEL ARB3280-2 REF DWG ARB3280 0000097667: SEVERJIN, DAVE H - 28-SEP-2021 17:59 C/W.
- [SDR FDEA202109032279](https://openairdocs.org/sdr/FDEA202109032279.md): Skin · dented · Sep 3, 2021 · N307FE · Doug MD1030F · Cargo/Baggage Doors
  > MAIN CARGO DOOR OPENING, FWD LOWER CORNER DAMAGE TO SKIN LAYERS (MARKED) 0003882689: CARREDANO, CHRISTOPHER - 24-SEP-2021 00:24 REPAIRED MAIN CARGO DOOR CORNER REF MD10-30 SRM 53-50-00, VOL I, FIG 26, SHEET 6, PG 178, NOTES 1-14 0000858546: KAYA, KEVIN
- [SDR FDEA202108302167](https://openairdocs.org/sdr/FDEA202108302167.md): Floorboard · damaged · Aug 30, 2021 · N307FE · Doug MD1030F · Fuselage Floor Panel
  > MAIN CARGO DECK STA.1437 DAMAGED FLOOR BOARD. ON PANEL DOOR #271GF (LH) AREA (MARKED) FABRICATED NEW FLOOR BOARD PANEL PER SRZ-25-005
- [SDR FDEA202108222455](https://openairdocs.org/sdr/FDEA202108222455.md): Angle · cracked · Aug 22, 2021 · N307FE · Doug MD1030F · Wing Main, Frame Structure
  > RIGHT WING SLAT #2 OUTBOARD END UNDER STAINLESS SEAL BY DLE HAS CRACKED L-ANGLE MARKED #1 REMOVED AND REPLACED CRACKED ANGLE ARB1647-6 IN REFERENCE TO DOUGLAS DRAWING ARB1647 AND MD-10-30 SRM 51-31-01 VOL2
- [SDR FDEA202108222189](https://openairdocs.org/sdr/FDEA202108222189.md): Rub Strip · cracked · Aug 22, 2021 · N307FE · Doug MD1030F · Leading Edge Devices
  > LH WING: #1 SLAT UPPER SURFACE O/B - T/E RUBSTRIP UNDERSIDE CRACKED. (MRKD) REMOVED AND INSTALLED RUBSTRIP PER E.A 8-5750-T0363959, & REF MD10-30 SRM 51-35-01 VOL II, & REF DAC DWG NRB6224 REF. JPF ITEMS 2,3, AND 4
- [SDR FDEA202108302166](https://openairdocs.org/sdr/FDEA202108302166.md): Floorboard · damaged · Aug 22, 2021 · N307FE · Doug MD1030F · Fuselage Floor Panel
  > MAIN DECK CARGO STA. 1437 DAMAGED FLOOR BOARD. ON PANEL DOOR #271GF LH AREA (MARKED). FABRICATED NEW FLOOR BOARD PANEL PER FEDEX DRAWING SRZ-25-005
- [SDR FDEA202108212053](https://openairdocs.org/sdr/FDEA202108212053.md): Floorbeam · cracked · Aug 21, 2021 · N307FE · Doug MD1030F · Fuselage Main, Floor Beam
  > MAIN CARGO COMPT. FLOOR BOARD SUPPORT AT STA. 1199 AT APPROX. X=98 TO X=104 CRACKED REMOVED AND REPLACED FLOOR BOARD SUPPORT P/N ACA3763-1 ON MAIN CARGO COMPT. AT NOTED LOCATION REF SRM 51-33-01 VOL 2
- [SDR FDEA202108192052](https://openairdocs.org/sdr/FDEA202108192052.md): Floorbeam · corroded · Aug 19, 2021 · N307FE · Doug MD1030F · Fuselage Main, Floor Beam
  > MAIN CARGO COMPT. FLOOR BOARD SUPPORT AT STA. 1219 AT APPROX. X=89 TO X=105 HAS CORROSION REMOVED CORRODED FLOOR BOARD SUPPORT AND FABRICATED NEW FLOOR BOARD SUPPORT P/N AEA0394-501 IAW DOUGLAS DRAWING AEA0394 USING S2929169 EXTRUSION MP5630208 AND INSTA
- [SDR FDEA202108192051](https://openairdocs.org/sdr/FDEA202108192051.md): Floorbeam · cracked · Aug 19, 2021 · N307FE · Doug MD1030F · Fuselage Main, Floor Beam
  > MAIN CARGO COMPT. FLOOR BOARD SUPPORT AT STA. 1481 AT APPROX. X=-10 TO X=-16 CRACKED REMOVED AND REPLACED FLOOR BOARD SUPPORT P/N ACA3763-1 ON MAIN CARGO COMPT. AT NOTED LOCATION REF SRM 51-33-01 VOL 2
- [SDR FDEA202108192050](https://openairdocs.org/sdr/FDEA202108192050.md): Floorbeam · cracked · Aug 19, 2021 · N307FE · Doug MD1030F · Fuselage Main, Floor Beam
  > MAIN CARGO COMPT. FLOOR BOARD SUPPORT AT STA. 1461 AT APPROX. X=29 TO X=35 CRACKED REMOVED AND REPLACED FLOOR BOARD SUPPORT P/N ACA3763-1 ON MAIN CARGO COMPT. AT NOTED LOCATION REF SRM 51-33-01 VOL 2
- [SDR FDEA202108192049](https://openairdocs.org/sdr/FDEA202108192049.md): Floorbeam · cracked · Aug 19, 2021 · N307FE · Doug MD1030F · Fuselage Main, Floor Beam
  > MAIN CARGO COMPT. FLOOR BOARD SUPPORT AT STA. 1441 AT APPROX. X=10 TO X=16 CRACKED REMOVED AND REPLACED FLOOR BOARD SUPPORT P/N ACA3763-1 ON MAIN CARGO COMPT. AT NOTED LOCATION REF SRM 51-33-01 VOL 2
- [SDR FDEA202108182319](https://openairdocs.org/sdr/FDEA202108182319.md): Fitting · cracked · Aug 18, 2021 · N307FE · Doug MD1030F · Fuselage Main, Bulkhead
  > L/H STA. 595 BULKHEAD TEE CAP VERT LEG AT LONG 43L HAS A.700 IN. CRACK. (MARKED) INSTALLED REPAIR DOUBLERS PER EA8-5310-T0363663
- [SDR FDEA202108182059](https://openairdocs.org/sdr/FDEA202108182059.md): Floorbeam · cracked · Aug 18, 2021 · N307FE · Doug MD1030F · Fuselage Main, Floor Beam
  > FUSELAGE MAINFRAME OVERWING FLOOR BEAM L/H SIDE AT STA 1256 LBL 112 IS CRACKED APPROX. ONE INCH IN LENGHT. (MKD) REPAIRED FUSELAGE MAINFRAME OVERWING FLOOR BEAM AT STA 1256 LBL112 REF BOEING SERVICE BULLETIN DC10-53-172 FIG 5, DWG SR10530081, EA 8-5310-T03
- [SDR FDEA202108182278](https://openairdocs.org/sdr/FDEA202108182278.md): Stiffener · corroded · Aug 18, 2021 · N307FE · Doug MD1030F · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT R/H TUNNEL VERTICAL STIFFNER CORRODED UNDER NUT PLATE ON LOWER AREA AT STA 1841. (DOT 5) 0004092897: REECE JR., RONALD S - 10-SEP-2021 17:49 WEB ASSEMBLY REPAIRED IAW SRM 53-00-01 GENERAL REPAIR #8 FIGURE 8 SHEETS 1-3 AND DRAWING A
- [SDR FDEA202108182277](https://openairdocs.org/sdr/FDEA202108182277.md): Beam · cracked · Aug 18, 2021 · N307FE · Doug MD1030F · Fuselage Main, Structure
  > FOREWARD CARGO AT 595 BULKHEAD LOWER BEAM BEHIND NOSE GEAR P/N NCA6044-29 HAS 4 CRACKS VERIFIED AND MARKED. 0000911637: STEPHENS, NATHAN M - 09-SEP-2021 19:14 STOP DRILLED ENDS OF CRACKS AND APPLIED DOUBLER REPAIR IAW SRM 53-40-00 V1 FIG36
- [SDR FDEA202108172170](https://openairdocs.org/sdr/FDEA202108172170.md): Seat Track · corroded · Aug 17, 2021 · N307FE · Doug MD11F · Fuselage Main, Structure
  > AFT WASTE COMPT: STA 1967 LBL 107.25 - SEAT TRACK UNDERSIDE HAS EXFOLIATION CORROSION (VIEWED FROM LH SIDE AFT WASTE COMPT. LOOKING UP). REMOVED AND INSTALLED NEW SEAT TRACK EXTRUSION S4929148 REF SRM 53-70-00 VOL 1 FIG 16, SHEET 1, PG 59 PAR. 1C, SRM 57-
- [SDR FDEA202108172320](https://openairdocs.org/sdr/FDEA202108172320.md): Tee Fitting · cracked · Aug 17, 2021 · N307FE · Doug MD1030F · Fuselage Main, Attach Fittings
  > FWD CARGO, L/H SIDE "T" CAP CRACKED ON VERTICAL LEG, LOCATED BY STRINGER 45. CORRECTION: LOCATED BY STRINGER 39. INSTALLED REPAIR DOUBLERS PER EA. 8-5310-T0363663
- [SDR FDEA202108172029](https://openairdocs.org/sdr/FDEA202108172029.md): Floorbeam · cracked · Aug 17, 2021 · N307FE · Doug MD1030F · Fuselage Main, Floor Beam
  > MAIN CABIN OVERWING FLOOR BEAM, R/H SIDE, AT STA 1275 RBL 104, HAS A SEVERED BEAM. (MKD) INSTALLED NEW FABRICTED EXTRUSION SPLICE IAW SRM 51-38-01 PAR 4.D VOL 2 AND DWG VZZ7071(-1) SHEET 2 ZN17 VIEW G-G AND SRM 51-33-01 VOL.2
- [SDR FDEA202108162188](https://openairdocs.org/sdr/FDEA202108162188.md): Skin · cracked · Aug 16, 2021 · N307FE · Doug MD1030F · Wing, Plate/Skin
  > LH LEADING EDGE, SLAT ANTI ICE TELESCOPING DUCT CUTOUT, PERFORMED NDT HFEC INSP PER NDTSPM PART 6. CRACK INDICATION AT UPPER INBD CORNER APPROX.250 IN LENGTH, MARKED DOT#39 AND RED GREASE PENCIL. NOTE: LOCATION IS CORNER #1 PER SEQ 1015, PG 22, FIG 2. R
- [SDR FDEA202108152424](https://openairdocs.org/sdr/FDEA202108152424.md): Doubler · worn · Aug 15, 2021 · N307FE · Doug MD1030F · Vertical Stabilizer
  > AFT FUSELAGE; 311AB DOOR LAND WORN THRU SKIN @ LH AFT LATCH CONTACT POINT. DOT #11 REPAIRED PER EA 8-5330-T0364309.
- [SDR FDEA202108132292](https://openairdocs.org/sdr/FDEA202108132292.md): Floor Panel · delaminated · Aug 13, 2021 · N307FE · Doug MD1030F · Fuselage Floor Panel
  > MAIN DECK FLOOR PANEL DELAM. FROM STA 1561-1661.BETWN LBL 8.50-27.50 MARKED RED FABRICATED NEW FLOOR BOARD PER FDX DWG SRZ-25-005
- [SDR FDEA202108132221](https://openairdocs.org/sdr/FDEA202108132221.md): Floorboard · damaged · Aug 13, 2021 · N307FE · Doug MD1030F · Fuselage Floor Panel
  > UPPER MAIN CARGO FLOORBOARD 282BF IS MISSING MULTIPLE INSERTS. STA 1561-1661 FABRICATED NEW FLOOR BOARD PER FEDEX DRAWING SRZ-25-005
- [SDR FDEA202108132017](https://openairdocs.org/sdr/FDEA202108132017.md): Seat Track · worn · Aug 13, 2021 · N307FE · Doug MD1030F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK: STA 1029 (R) X = -47.50 SEAT TRACK WORN BEYOND (GO-NOGO GAUGE)LIMITS. (MRKD) REMOVED AND REPLACED SEAT TRACK FROM STA 949-1030 RBL 47.50 MAIN DECK MPN S4929405-13500N MP3266343 REF SRM 53-70-00 FIG 1 VOL.1 AND SRM 51-31-01 VOL. 2 "MAJOR REPAI
- [SDR FDEA202105041137](https://openairdocs.org/sdr/FDEA202105041137.md): Skin · cracked · May 4, 2021 · N307FE · Doug MD1030F · Fuselage Main, Structure
  > LH UPPER A/C PACK EXHAUST CUTOUT HAS SUSPECTED CRACK IN UPPER AFT CORNER THRU FASTENER HOLE. REPAIRED FUSELAGE SKIN PER MD10-30 SRM 53-50-00 FIG 3A
- [SDR FDEA2020082011858](https://openairdocs.org/sdr/FDEA2020082011858.md): Power Supply · no test · Aug 11, 2020 · N307FE · Doug MD1030F · Emergency Lighting
  > DURING AN EMERGENCY LIGHTS TEST, FOUND THE EMERGENCY LIGHTS BATTERY 1 LOW. REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY POWER SUPPLY IAW AMM 33-51-01-4-1, AND OPS CHECKED OK. ACFT OK FOR SERVICE.
- [SDR FDEA2020081211858](https://openairdocs.org/sdr/FDEA2020081211858.md): Battery Pack · no test · Aug 11, 2020 · N307FE · Doug MD1030F · Emergency Lighting
  > DURING EMERGENCY LIGHTS TEST, FOUND THE BATTERY 1 LOW.
- [SDR FDEA202007031439](https://openairdocs.org/sdr/FDEA202007031439.md): Valve · failed · Jul 3, 2020 · N307FE · Doug MD1030F · Aircraft Fuel Distribution System
  > TNK 3 TIP TRAPPED ALERT DURING CRUISE. 5800 LBS TRAPPED IN #3 TANK. EMERGENCY DECLARED WITH ATC. IN REF TO FFC ERO 5200247 REMOVED REPLACED AND OPS CHECKED #3 MOTIVE SHUTOFF VALVE IRW FE MD10- 30 AMM 28-21-13-2 AND FE MD10-30 FIM 28-14-00-810-803. OPS CH
- [SDR FDEA2020070631439](https://openairdocs.org/sdr/FDEA2020070631439.md): Unknown · malfunctioned · Jul 3, 2020 · N307FE · Doug MD1030F · Fuel Indicating System
  > TANK 3 TIP TRAPPED ALERT DURING CRUISE. 5800 LBS TRAPPED IN NR 3 TANK. EMERGENCY DECLARED WITH ATC.
- [SDR FDEA2020061961263](https://openairdocs.org/sdr/FDEA2020061961263.md): Float Valve · malfunctioned · Jun 16, 2020 · N307FE · Doug MD1030F · Fuel Storage
  > AT L/O, FL 360 GOT LVL 1 ALERT FOR " TNK 3 TIP TRAPPED" WITH APPX 8.0 K FUEL IN #3, MEANING WE ONLY HAD 8.0 - 5.8 = 2.2 IN NR 3 TANK, AND INSUFFICIENT FUEL TO MAKE DESTINATION, ALERT WENT AWAY AFTER 2 MIN BUT ON DESCENT, GOT TNK 3 FUEL QTY LO ALERT WITH
- [SDR FDEA202003290628](https://openairdocs.org/sdr/FDEA202003290628.md): Indicator · malfunctioned · Mar 29, 2020 · N307FE · Doug MD1030F · Emergency Exits
  > L1 DOOR EVACUATION SLIDE REMOTE PRESSURE PRESS-TO-TEST INDICATING SYS NOT TESTING. REMOVED AND REPLACED REMOTE SLIDE PACK PRESSURE INDICATOR. OPERATIONAL CHECKS GOOD
- [SDR FDEA201910282765](https://openairdocs.org/sdr/FDEA201910282765.md): Spoiler Sys · malfunctioned · Oct 28, 2019 · N307FE · Doug MD1030F · Drag Control System
  > PDIS 307 27-60 6896 28OCT19 PDX FACT U LOGPAGES:3144742 DURING DESCENT WHEN SPOILERS DEPLOYED THE AIRCRAFT HAD A SIGNIFICANT ROLL TO THE RIGHT. FACT 28OCT19 05:05 PDX U C/W FIM 27-60-09-00. FULLY DEPLOYED SPOILERS AND INSPECTED SURFACES
- [SDR FDEA201909032081](https://openairdocs.org/sdr/FDEA201909032081.md): Floor Support · corroded · Sep 3, 2019 · N307FE · Doug MD1030F · Fuselage Miscellaneous Structure
  > CORROSION UNDER NUT PLATES AFT CARGO FLOOR SUPPORT STA 1907, END TO END. REMOVED & REPLACED NUT PLATES IAW SRM 51-31-01 VOL II, REMOVED CORROSION STA 1902 L- 40 TO R-40 IAW SRM 51-21-01 VOL I. CHECK LIMITS ORIG MAT..063" MAT. LOSS.026": MAT REM.037", FOUND
- [SDR FDEA201909032080](https://openairdocs.org/sdr/FDEA201909032080.md): Access Panel · corroded · Sep 3, 2019 · N307FE · Doug MD1030F · Fuel Storage
  > LWR AUX TANK REAR SPAR ACCESS WEB HAS CORROSION ON BOTH UPPER AND LOWER SURFACES. (PANEL RACK) REMOVED CORR IAW SRM 51-81-00 VOL II. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01 FIG 1A. SH 3 ORIG.190 AFTER REWORK.152 TR# 14401. FABRICATED WEB ON TR # T19/14360
- [SDR FDEA201909032082](https://openairdocs.org/sdr/FDEA201909032082.md): Skin · chafed · Sep 3, 2019 · N307FE · Doug MD1030F · Wing, Plate/Skin
  > LT WING FIXED L/E UPPER SKIN IS CHAFED UNDER SLAT #1 AND 2 JOINT. CHECK FIT / FAIR GAP CLEARANCE AFTER REPAIR. BLENDED AREA IAW SRM 57-00-01 FIG I. VOL I. REMAINING MAT ON LT WING FIXED L/E UPPER SKIN UNDER SLAT #1 AND 2 JOINT WAS FOUND TO BE OUT OF LIMITS IAW

Next page: https://openairdocs.org/aircraft/N307FE/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 = 'N307FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N307FE/reports

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