# Service difficulty reports: N308FE

A list on [N308FE](https://openairdocs.org/aircraft/N308FE.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 2 · 98 reports

- [SDR FDEA202105041096](https://openairdocs.org/sdr/FDEA202105041096.md): O-Ring · failed · May 4, 2021 · N308FE · Doug MD1030F · Engine Oil Pressure
  > ON CLIMB OUT, #2 ENGINE OIL QUANTITY WENT TO 1 QT. SUBSEQUENTLY OIL PRESSURE BEGAN TO DROP BELOW THE GREEN BAND. FOLLOWED QRH TO SHUT DOWN #2 ENGINE AND LAND AT NEAREST SUITABLE FIELD. FOUND MAIN GEAR BOX OIL LINE CHIP DETECTOR O-RING TORN. R&R'D MAIN
- [SDR FDEA202103210738](https://openairdocs.org/sdr/FDEA202103210738.md): Unknown · smoke · Mar 21, 2021 · N308FE · Doug MD1030F · Air Distribution System
  > PDIS 308 21-50 7643 21MAR21 IND FACT U LOGPAGES:3203672 NOTE: AFTER STARTING APU AND TURNING ON PACKS AN ODD SMELL EMINATED FROM THE AIR VENTS. SMELLED LIKE TURPINTINE TO THE CAPT AND GASOLINE TO FO. HAPPENED TWICE. LASTED 5 MINS. SHGN 21MAR
- [SDR FDEA2020011310110](https://openairdocs.org/sdr/FDEA2020011310110.md): Pseu · malfunctioned · Jan 11, 2020 · N308FE · Doug MD1030F · Landing Gear Retraction/Extension System
  > ON FINAL FOR KMEM 18L AT 3000 FT, WE PUT THE GEAR HANDLE DOWN AND RECEIVED 4 RED GEAR UNSAFE INDICATIONS. WE EXECUTED A GO AROUND TO REENTER THE PATTERN AND RAN THE GEAR UNSAFE INDICATION WITH GEAR HANDLE DOWN CHECKLIST. AFTER RUNNING THE CHECKLIST WE WE
- [SDR FDEA2019082652015](https://openairdocs.org/sdr/FDEA2019082652015.md): Fitting · cracked · Aug 25, 2019 · N308FE · Doug MD1030F · Landing Gear Doors
  > CENTER LANDING GEAR LT AFT DOOR, AFT LOWER SUPPORT WAS CRACKED AT LOWER ATTACH LUG HOLE. REMOVED AND REPLACEED LT MLG DOOR LOWER AFT LINK FITTING IAW DRAWING ABN7451.
- [SDR FDEA2019082101972](https://openairdocs.org/sdr/FDEA2019082101972.md): Hinge Fitting · cracked · Aug 20, 2019 · N308FE · Doug MD1030F · Landing Gear Doors
  > CENTER LANDING GEAR LH AFT DOOR IS LOOSE AT FWD AND AFT HINGES. REMOVED AND REPLACED FITTING IAW DAC DWG ANB7451.
- [SDR FDEA201908091824](https://openairdocs.org/sdr/FDEA201908091824.md): Vane · worn · Aug 9, 2019 · N308FE · Doug MD1030F · Trailing Edge Flaps
  > LEFT WING INBOARD FLAP VANE WORN ON TOP INB INLINE WITH BUB STRIP APPROX. 4 INCHES. REPAIRED WORN AREA ON L/H I/B FLAP VANE AS REQUIRED REF. SRM 57-00-01 VOL.I PG.11 AND SRM 51-71-00 VOL.II.
- [SDR FDEA2019082181989](https://openairdocs.org/sdr/FDEA2019082181989.md): Rib · cracked · Aug 8, 2019 · N308FE · Doug MD1030F · Cargo/Baggage Doors
  > CENTER CARGO DOOR FWD RIB LOWER END IS CRACKED AND PIECE MISSING. REMOVED DAMAGED SECTION OF CENTER CARGO DOOR FWD RIB LOWER END AND INSTALLED REPAIR ANGLE AND FILLER REF. SRM 53-00-01 FIG. 8 VOL. 1.
- [SDR FDEA2019081281833](https://openairdocs.org/sdr/FDEA2019081281833.md): Floor Support · corroded · Aug 8, 2019 · N308FE · Doug MD1030F · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR AT STA 1845 RBL 7 UNDER FLOOR BOARD SUPPORT IS CORRODED AT NUT PLATE HOLE. (MKD) REPLACED PER DAC DWG AGA3814
- [SDR FDEA2019081571858](https://openairdocs.org/sdr/FDEA2019081571858.md): Floor Support · corroded · Aug 7, 2019 · N308FE · Doug MD1030F · Fuselage Miscellaneous Structure
  > INSIDE MAIN CABIN, AT BS 1885, RBL 20, UNDER FLOOR PANEL SUPPORT IS CORRODED AT NUT PLATE HOLES. REMOVED AND REPLACED THE FLOOR SUPPORT IAW DWG AGA7091, AND SRM 51-31-01,V2.
- [SDR FDEA2019081571857](https://openairdocs.org/sdr/FDEA2019081571857.md): Floor Support · corroded · Aug 7, 2019 · N308FE · Doug MD1030F · Fuselage Miscellaneous Structure
  > INSIDE MAIN CABIN, AT BS 1885, LBL 20 UNDER FLOOR PANEL, HAT SECTION SUPPORT IS CORRODED AT NUT PLATE HOLES. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-35-01,V2 AND DWG AGA7559.
- [SDR FDEA2019080971826](https://openairdocs.org/sdr/FDEA2019080971826.md): Floor Support · corroded · Aug 7, 2019 · N308FE · Doug MD1030F · Fuselage Miscellaneous Structure
  > INSIDE MAIN CABIN, AT STA 1885 LBL 44, UNDER FOOL SUPPORT HAT SECTION, IS CORRODED AT NUT PLATE HOLES. (MKD) AT STA. 1885, LBL 44, REMOVED AND REPLACED WITH NEW FLOOR SUPPORT AGA 7559-5 PER DAC. DWG. AGA 7559. INSTALLED FASTENERS PER SRM 51-31-01 VOL 2.
- [SDR FDEA2019080971825](https://openairdocs.org/sdr/FDEA2019080971825.md): Floor Support · corroded · Aug 7, 2019 · N308FE · Doug MD1030F · Fuselage Miscellaneous Structure
  > INSIDE MAIN CABIN, AT STA 1885 LBL 36, UNDER FLOOR PANEL SMALL HAT SECTION IS CORRODED AT NUTPLATE HOLE. (MKD) AT STA. 1885, LBL 36, REMOVED AND REPLACED WITH NEW FLOOR SUPPORT AGA 7559-5 PER DAC. DWG. AGA 7559. INSTALLED FASTENERS PER SRM 51-31-01 VOL 2.
- [SDR FDEA201908062189](https://openairdocs.org/sdr/FDEA201908062189.md): Frame · bent · Aug 6, 2019 · N308FE · Doug MD1030F · Fuselage Main, Frame
  > MAIN CARGO LT STA 1641 BETWEEN STR L13-L14. FRAME IS BENT. CUT OUT FRAME AND INSTALLED NEW FRAME SECTION PER SRM 53-30-00 FIG05 AND SRM 51- 38-01 VOL II.
- [SDR FDEA2019080531794](https://openairdocs.org/sdr/FDEA2019080531794.md): Skin · gouged · Aug 3, 2019 · N308FE · Doug MD1030F · Leading Edge Devices
  > R/H WING, L/E, I/B FLAP, APPROX. STA. XIFH280 FOUND A GOUGE UNDERNEATH RUB STRIP. INSTALLED REPAIR DOUBLER I.A.W. SRM57-00-01 FIG. 4 SHT.2 VOL. I
- [SDR FDEA2019100712483](https://openairdocs.org/sdr/FDEA2019100712483.md): Support · cracked · Jul 31, 2019 · N308FE · Doug MD1030F · Wing, Plate/Skin
  > RIGHT WING, LOWER LEADING EDGE WAS CRACKED ON PANEL LAND, AFT OF NR 9 SLAT TRACK. REMOVED AND REPLACED DAMAGED SUPPORT ARB2933-50 IAW DWG ARB2933 AND SRM 51-33-01 V2 AND SRM 51-35-01 V2 REMOVED DAMAGED DOUBLER ARB2933-50. REMOVED DOUBLER ARB2933-50 IAW
- [SDR FDEA2019081531893](https://openairdocs.org/sdr/FDEA2019081531893.md): Floor Support · corroded · Jul 31, 2019 · N308FE · Doug MD1030F · Fuselage Miscellaneous Structure
  > CENTER CARGO COMPARTMENT, FROM STATION 1541 TO STATION 1581, RBL-57 INTERCOSTALS CORRODED. REMOVED AND REPLACED CENTER CARGO COMPARTMENT INTERCOSTALS FROM STA.1541 TO STA. 1581,RBL-57. REF. SRM 51-31-02, VOL II; DAC DWG ACA7049.
- [SDR FDEA2019081528856](https://openairdocs.org/sdr/FDEA2019081528856.md): Seat Track · corroded · Jul 28, 2019 · N308FE · Doug MD1030F · Fuselage Main, Structure
  > MAIN DECK SEAT TRACK BS 1975 RBL 35 CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW DWG AGA7091, AND SRM 51-31-01,VOL 2.
- [SDR FDEA2019080581795](https://openairdocs.org/sdr/FDEA2019080581795.md): Floor Support · corroded · Jul 28, 2019 · N308FE · Doug MD1030F · Fuselage Miscellaneous Structure
  > MAIN CARGO DECK, STA1747 70RBL FLOOR SUPPORT HAS CORROSION (MARKED) REMOVED DAMAGED FLOOR SUPPORT AND REPLACED WITH NEW PER DWG AFA 3853 AND SRM 51-31-01,V2.
- [SDR FDEA2019080281789](https://openairdocs.org/sdr/FDEA2019080281789.md): Seat Track · cracked · Jul 28, 2019 · N308FE · Doug MD1030F · Fuselage, Seat/Cargo Attach Fittings
  > CTR. CARGO COMPT CEILING: STA. 1701 - 27.50 RBL, SEAT TRACK HAT SPLICE CRACKED (VIEWED LOOKING UP FROM CTR. CARGO COMPT.) MRKD. FABRICATED AND INSTALLED -20 SPLICE PLATE, PER DWG SR10-53-010.
- [SDR FDEA201907272231](https://openairdocs.org/sdr/FDEA201907272231.md): Channel · corroded · Jul 27, 2019 · N308FE · Doug MD1030F · Fuselage Miscellaneous Structure
  > CENTER CARGO COMPT: APPROX STA 1521 X=56.19. RT O/B CARGO RAIL. REF FWD ATTACH FASTENERS. (UNDERSIDE IN CHANNEL) FASTENER NUTS, WASHERS AND STRUCTURE CHANNEL CORRORED. REPAIRED CORRODED CHANNEL REF SRM 53-00-01, VOL I; FIG 7; SHEET 7.
- [SDR FDEA2019081671902](https://openairdocs.org/sdr/FDEA2019081671902.md): Support Web · cracked · Jul 27, 2019 · N308FE · Doug MD1030F · Fuselage Miscellaneous Structure
  > CTR CARGO COMPT: STA 1701 APPROX LONGERON 44L-47L - LOWER SUPPORT WEB CRACKED BELOW ROLLER TRAYS. (MRKD) REMOVED AND REPLACED CRACKED SECTION OF FLOOR BEAM IN CENTER CARGO, STA-1701, REF SRM 53-60-01, PG-7, FIG-3, SHEET-1, VOL-I; SRM 51-33-01, VOL-II; SR
- [SDR FDEA2019080871808](https://openairdocs.org/sdr/FDEA2019080871808.md): Floorbeam · corroded · Jul 27, 2019 · N308FE · Doug MD1030F · Fuselage Main, Floor Beam
  > CENTER CARGO COMPT: APPROX STA 1781, X=-16.5 FLOOR BOARD SUPPORT EXTRUSTION. 1 CLIPNUT HOLE SHOWS CORROSION. (UNDERSIDE) MARKED. INSTALLED FLOOR BOARD SUPPORT PER DAC DWG AFA7299.
- [SDR FDEA201907261894](https://openairdocs.org/sdr/FDEA201907261894.md): Floorbeam · corroded · Jul 26, 2019 · N308FE · Doug MD1030F · Fuselage Main, Floor Beam
  > AFT CARGO COMPT: APPROX STA 1841, FLOOR SUPPORT ANGLE HAS CORROSION AT NUT PLATES. (UNDERSIDE OF ANGLE). HEAVY AND LIGHT FROM RIGHT TO LEFT SIDE OF A/C. REMOVED AND REPLACED FLOOR SUPPORT AT STATION 1841 FROM RBL-1 TO RBL-63 REF DAC DWG AGA7170 AND SRM 51-
- [SDR FDEA2019080861806](https://openairdocs.org/sdr/FDEA2019080861806.md): Skin · gouged · Jul 26, 2019 · N308FE · Doug MD1030F · Wing, Plate/Skin
  > LT WING FIXED LEADING EDGE - REPAIR DOUBLER INBD SIDE OF ANTI-ICE DUCT HAS GOUGE CAUSED BY CONTACT WITH SLAT. REPAIRED L/H WING SKIN ATSLAT ANTI-ICE TELESCOPING DUCT CUT OUT REF SRM 57-10-00 FIG. 40 SHEETS 1-3 VOL. 1.
- [SDR FDEA2019080861805](https://openairdocs.org/sdr/FDEA2019080861805.md): Skin · cracked · Jul 26, 2019 · N308FE · Doug MD1030F · Wing, Plate/Skin
  > LT WING FIXED LEADING EDGE - REPAIR DOUBLER OUTBD SIDE OF ANTI-ICE DUCT HAS GOUGE CAUSED BY CONTACT WITH SLAT. (MARKED) REPAIRED L/H WING SKIN AT SLAT ANTI-CE TELESCOPING DUCT CUT OUT REF SRM 57-10-00 FIG 40 SHEETS 1-3 VOL. 1.
- [SDR FDEA2019101052497](https://openairdocs.org/sdr/FDEA2019101052497.md): Bulkhead · cracked · Jul 25, 2019 · N308FE · Doug MD1030F · Fuselage Main, Bulkhead
  > FUSELAGE AFT PRESSURE BULKHEAD, FWD SIDE, AT UPPER CANTED AREA, PREVIOUS REPAIR BLEND OUT HAS A "1/2" INCH CRACK INDICATION. INSTALLED A REPAIR IAW EA 8-5310-T0348800.
- [SDR FDEA2019081501851](https://openairdocs.org/sdr/FDEA2019081501851.md): Skin · cracked · Jul 25, 2019 · N308FE · Doug MD1030F · Leading Edge Devices
  > LEFT WING NR 8 SLAT, INBD LOWER SKIN WAS CRACKED. REMOVED AND REPLACED THE LT WING NR 8 SLAT, ADJUSTED AND OPS CHECKED GOOD IAW AMM 27-80-01-4, AND AMM 27-80-00-5.
- [SDR FDEA2019080721799](https://openairdocs.org/sdr/FDEA2019080721799.md): Frame Splice · cracked · Jul 25, 2019 · N308FE · Doug MD1030F · Fuselage Main, Frame
  > MAIN DECK STA 1741 FRAME SPLICE DOUBLER CRACKED. MRKD LH SIDEWALL BETWEEN L13L- L14L REMOVED AND REPLACED PER DWG AFA 0018
- [SDR FDEA2019080841804](https://openairdocs.org/sdr/FDEA2019080841804.md): Skin · worn · Jul 24, 2019 · N308FE · Doug MD1030F · Wing, Plate/Skin
  > RT WING DROOP L/E, INBD SIDE OF DROOP L/E SKIN HAS WEAR GROOVE/MARKS (MARKED AND DOT 4) PERFORMED DLE SKIN REPAIR I.A.W. SRM 57-10-00, PARA. 95 AND FIG. 97 VOL I
- [SDR FDEA2019081231832](https://openairdocs.org/sdr/FDEA2019081231832.md): Frame · cracked · Jul 23, 2019 · N308FE · Doug MD1030F · Fuselage Main, Frame
  > LH WHEEL WELL FRAME STA. 1501 APPROX STRINGER 33 - 1 INCH CRACK EMANATING FROM FASTENER HOLE AT FRAME. CRACK WAS CONFIRMED USING NDT HFEC. REPAIRED CRACKED FRAME REF DAC DWG AEA0439 AND SRM51-33-01 VOL. 2, SRM 53-00-01 FIG. 8 VOL. 1.
- [SDR FDEA2019081523876](https://openairdocs.org/sdr/FDEA2019081523876.md): Seat Track · worn · Jul 23, 2019 · N308FE · Doug MD1030F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK: SEAT TRACK WORN NEAR STA. 1122 AT RBL X=8.50. AREA MARKED RED REPLACED PER SRM CH 53-70-00,FIG 1,VOL 1.
- [SDR FDEA201903190684](https://openairdocs.org/sdr/FDEA201903190684.md): Unknown · odor · Mar 19, 2019 · N308FE · Doug MD1030F · Air Distribution System
  > FUME EVENT. ON TAKEOFF FROM CYMY WITH ENGINES SET TO TAKEOFF POWER AND ABOVE 80KNOTS, BOTH CREW MEMBERS SMELLED A MODERATELY INTENSE BURNED OIL ODOR. THE ODOR DISIPATED DURING CLIMB OUT AND WAS GONE BY 10,00FT MSL. RAN ALL 3 ENGINES AT IDLE PER JRH AND PERFORM
- [SDR FDEA201901100081](https://openairdocs.org/sdr/FDEA201901100081.md): Landing Gear · damaged · Jan 10, 2019 · N308FE · Doug MD1030F · Landing Gear Retraction/Extension System
  > AFTER TAKEOFF FROM 36L WITH GEAR HANDLE UP WE RECEIVED A UNSAFE CENTER GEAR INDICATION IN BOTH THE PRIMARY AND SECONDARY INDICATORS. CYCLED GEAR HANDLE PER QRH AND STILL HAD PRIMARY AND SECONDARY CENTER GEAR UNSAFE INDICATION W/GEAR HANDLE UP. GEAR HANDLE DOWN
- [SDR FDEA201801060034](https://openairdocs.org/sdr/FDEA201801060034.md): Door · inoperative · Jan 6, 2018 · N308FE · Doug MD1030F · Passenger/Crew Doors
  > L1 DOOR DID NOT WORK ELECTRICALLY.
- [SDR FDEA201709212666](https://openairdocs.org/sdr/FDEA201709212666.md): Skin · delaminated · Sep 21, 2017 · N308FE · Doug MD1030F · Spoilers
  > RIGHT WING NR 1 SPOILER OTBD TOP SECTION HAS A 2.75 X 3.5 INCHES OF DELAMINATION AT XORS 346. REPAIRED THE SPOILER IAW SRM 71-00-01, FIG 4, SHEET 1, VOL I.
- [SDR FDEA201709212665](https://openairdocs.org/sdr/FDEA201709212665.md): Panel · delaminated · Sep 21, 2017 · N308FE · Doug MD1030F · Aerodynamic Fairings
  > RIGHT WING TO FUSELAGE FIXED FAIRING, T/E AT INBD FLAP, PANEL ARC0288-504 R2, PREVIOUS REPAIR HAS COME OFF AND BOTTOM SIDE IS DELAMINATED. REPAIRED.
- [SDR FDEA201709192871](https://openairdocs.org/sdr/FDEA201709192871.md): Doubler · cracked · Sep 19, 2017 · N308FE · Doug MD1030F · Wing, Plate/Skin
  > RT WING LE XORS 562 INNER BEADED DOUBLER IS CRACKED. CONDITION CONFIRMED WITH HFEC. REPAIRED PER SRM 57-10-T0335748.
- [SDR FDEA201709132849](https://openairdocs.org/sdr/FDEA201709132849.md): Fitting · cracked · Sep 13, 2017 · N308FE · Doug MD1030F · Cargo/Baggage Doors
  > MAIN CARGO DOOR FRAME NR 7 LATCH SPOOL LOWER SUPPORT FITTING HAS A ONE INCH CRACK EMANATING FROM RETAINER HOLE AT THE FWD INBD SIDE OF FITTING. INSTALLED A NEW SPOOL SUPPORT FITTING IAW SRM 51-33-01, FIG 1, PAGE 1, VOL.2.
- [SDR FDEA201709112862](https://openairdocs.org/sdr/FDEA201709112862.md): Frame · cracked · Sep 11, 2017 · N308FE · Doug MD1030F · Wing, Rib/Bulkhead
  > RT WING LEADING EDGE FRAME ARB1161-15 AT STA XRS 269 IS CRACKED. RT LEADING EDGE FORMER REPAIRED PER EA 8-5710-T0335774.
- [SDR FDEA201709112861](https://openairdocs.org/sdr/FDEA201709112861.md): Floor Support · corroded · Sep 11, 2017 · N308FE · Doug MD1030F · Fuselage Miscellaneous Structure
  > AFT WASTE COMPT STA 2007 APPROX 24LBL UNDERSIDE OF FLOOR SUPPORT TRACK CORROSION. REMOVED AND INSTALLED NEW FLOORBOARD SUPPORT BEAM PER DRAWING AGA7087 AND SRM 53-70-00 FIG 1 VOL 1.
- [SDR FDEA201709082870](https://openairdocs.org/sdr/FDEA201709082870.md): Door Frame · cracked · Sep 8, 2017 · N308FE · Doug MD1030F · Fuselage Main, Structure
  > A/C COMPT PACK BAY NR 1, APPROX STA 553 LONG 36 REF PACK BAY DOOR (113DL). FWD FRAME OF DOOR CUTOUT. THE FRAME IS CRACKED. IT HAS APPROX A 2" CRACK NEAR TOP OF THE FRAME. REPAIRED FRAME PER EA 8-5310-T0335533.
- [SDR FDEA201709082778](https://openairdocs.org/sdr/FDEA201709082778.md): Seat Track · worn · Sep 8, 2017 · N308FE · Doug MD1030F · Fuselage, Seat/Cargo Attach Fittings
  > UPPER MAIN DECK SEAT TRACK WORN AT RBL 8.50 NEAR STA 675. REMOVED AND INSTALLED DAMAGED SEAT TRACK REF SRM 53-70-00 FIG 11 VOLUME 1.
- [SDR FDEA201709082699](https://openairdocs.org/sdr/FDEA201709082699.md): Seat Track · worn · Sep 8, 2017 · N308FE · Doug MD1030F · Fuselage, Seat/Cargo Attach Fittings
  > UPPER MAIN DECK, TWO SEAT TRACKS WORN AT LBL 47.50 NEAR BS 615. REPLACED THE SEAT TRACK IAW SRM 53-70-00, FIG 1, VOL I, SRM 51-4-01, VOL II, AND SR10-53-002A. MAJOR REPAIR.
- [SDR FDEA201607182499](https://openairdocs.org/sdr/FDEA201607182499.md): Warning Light · illuminated · Jul 18, 2016 · N308FE · Doug MD1030F · Emergency Lighting
  > RECIEVED AN EMERGENCY LIGHT BATTERY 1 LOW, ALERT DURING EMERGENCY LIGHT TEST.
- [SDR FDEA201604051144](https://openairdocs.org/sdr/FDEA201604051144.md): Door Frame · cracked · Apr 5, 2016 · N308FE · Doug MD1030F · Landing Gear Doors
  > DURING HYD LEAK CHECK INSPECTION, OPENED & CLOSED RT MAIN GEAR DOOR. WHEN CLOSING THE RT GEAR DOOR, THE DOOR WOULD NOT STAY UP. TROUBLE SHOT TO THE LATCH ACTUATOR. R & R RT MAIN GEAR DOOR LATCH CYLINDER IAW MM CH 32-34-02-2. OPS & LEAK CHECKED GOOD. RT GE
- [SDR FDEA201510203289](https://openairdocs.org/sdr/FDEA201510203289.md): Skin · cracked · Oct 20, 2015 · N308FE · Doug MD1030F · Air Conditioning Doors
  > SIX INCH CRACK ON EXTERNAL SKIN OF NR 3 ACM ACCESS DOOR. REPAIRED THE CRACK SKIN IAW EA 8-5240-T0320735 A.
- [SDR FDEA201510203287](https://openairdocs.org/sdr/FDEA201510203287.md): Bulkhead · dented · Oct 20, 2015 · N308FE · Doug MD1030F · Fuselage Main, Bulkhead
  > CENTER CARGO STATION 1841, LBL 6, BULKHEAD WEB HAS LARGE DENT. CUT OUT DENTED WEB AS REQUIRED IAW SRM 51-00-01 FIG 10. INSTALLED REPAIR DOUBLER IAW EA 8-5310-T0320825 PART 1.
- [SDR FDEA201510203286](https://openairdocs.org/sdr/FDEA201510203286.md): Bulkhead · dented · Oct 20, 2015 · N308FE · Doug MD1030F · Fuselage Main, Bulkhead
  > CENTER CARGO STATION 1841, RBL 6, BULKHEAD WEB HAS LARGE DENT. REPAIR DOUBLER IAW EA 8-5310-T0320825.
- [SDR FDEA201510173268](https://openairdocs.org/sdr/FDEA201510173268.md): Web · cracked · Oct 17, 2015 · N308FE · Doug MD1030F · Fuselage Miscellaneous Structure
  > RIGHT MLG WW NR 3 RESERVOIR, LOWER ATTACH STRUCTURE WEB CRACKED. REMOVED LOWER ATTACH STRUCTURE WEB, RT MLG WW IAW SRM 51-31-01 VOL 2. INSTALLED & FABRICATED STIFFENER PN AEA7035-10 IAW DWG AEA 7035.
- [SDR FDEA201510123179](https://openairdocs.org/sdr/FDEA201510123179.md): Structure · corroded · Oct 12, 2015 · N308FE · Doug MD1030F · Fuselage Miscellaneous Structure
  > CENTER WING LOWER BARREL, CTR AUXILIARY TANK, CORROSION UNDER RUB STRIPS OF UPPER INBD & OTBD STRIPS. STRUCTURE IS FOR CTR AUXILIARY FUEL TANK COVER. REMOVED LIGHT CORROSION AROUND HOLES IAW SRM 51-00-01 VOL II.

Next page: https://openairdocs.org/aircraft/N308FE/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 = 'N308FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N308FE/reports

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