# Service difficulty reports: N316FE

A list on [N316FE](https://openairdocs.org/aircraft/N316FE.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 · 107 reports

- [SDR FDEA202211102747](https://openairdocs.org/sdr/FDEA202211102747.md): Line · split · Nov 10, 2022 · N316FE · Doug MD1030F · Hydraulic System, Main
  > ON CLIMB OUT, RECEIVED A HYD 3 OFF LEVEL 1 ALERT, FOLLOWED BY A LOSS OF HYD FLUID LEADING TO A HYD 3 FAIL LVL 2 ALERT. A COMPLETE LOSS OF HYD FLUID & PRESSURE. RAN QRH, COMPLIED WITH QRH. LANDED AT KMEM. DECLARED AN EMERGENCY. ALT GEAR EXT ACCOMPLISHED
- [SDR FDEA202204301098](https://openairdocs.org/sdr/FDEA202204301098.md): None · none · Apr 30, 2022 · N316FE · Doug 600N · Trailing Edge Flap Control System
  > PDIS 316 27-50 7006 30APR22 SLC OPEN U UPON FLAPS 35 SELECTION, RECEIVED LEVEL 2 SLAT DISAG. ALERT. INITIATED GO AROUND, AND THEN RECEIVED LEVEL 2 FLAP DISAG. ALERT. AIRSPEED WAS 146 IAS. AIRCRAFT DID NOT HAVE ANY ROLL MOMENT WHEN GETTING THE
- [SDR FDEA202201220117](https://openairdocs.org/sdr/FDEA202201220117.md): Skin · damaged · Jan 22, 2022 · N316FE · Doug MD1030F · Wing, Plate/Skin
  > INDY LINE FOUND ON NRC6053-509 TOP SKIN OF WEDGE ARC1953-503 (ARC1953-4, 2024-T3 0.025 TH, AND THE ARC1953-7 DOUBLER 0.016 TH) PULLING BACK FROM IB EDGE (XOF 511.260 TO XOF 522.276), DAMAGED SKIN MEASURES 12" X 35" APPROX. REPAIRED FLAP WEDGE USING EA 8-5
- [SDR FDEA202105291419](https://openairdocs.org/sdr/FDEA202105291419.md): Door Sill · cracked · May 29, 2021 · N316FE · Doug MD1030F · Fuselage Miscellaneous Structure
  > CENTER CARGO DOOR SILL, LOWER AFT SECTION HAS A CRACK REPAIRED PER SRM MD10 53-00-01 VOL I P40
- [SDR FDEA202105211357](https://openairdocs.org/sdr/FDEA202105211357.md): Floor Panel · delaminated · May 21, 2021 · N316FE · Doug MD1030F · Fuselage Floor Panel
  > MAIN DECK L-1 DOOR AREA FLOOR PANEL, RIGHT NEXT TO MAIN CARGO DOOR CONT, SHOWING SPONGY AND SUSPECTING DELAM. R/R THE FLOOR PANEL#223AF WITH SCREW PER SRM
- [SDR FDEA202105201408](https://openairdocs.org/sdr/FDEA202105201408.md): Skin · dented · May 20, 2021 · N316FE · Doug MD1030F · Wing, Plate/Skin
  > REWORK: REFERENCE SNRM 467..L/H WING UPPER SURFACE-L/E SKIN DENTED AT APPROX. STA. XDLE 309,INBD OF #3 SLAT FIXED WING LEADING EDGE IS PRIMARY STRUCTURE. "MAJOR REPAIR" CUTOUT DAMAGED AREA 1IN DIAMETER AND REPAIRED AREA PER. MD10-30 SRM 57-00-01 VOL.1 F
- [SDR FDEA202105171412](https://openairdocs.org/sdr/FDEA202105171412.md): Doubler · damaged · May 17, 2021 · N316FE · Doug MD1030F · Wing Main, Frame Structure
  > RH WING INTERNAL LE - ABOVE ANTI-ICE TELESCOPE DUCT(ACCESS, PANEL 613AB)- BEADED DOUBLER IS DAMAGED. 0000575467: WRAY, BASIL P. B. - 03-JUN-2021 13:20 TRIMMED OUT DAMAGED AREA AND INSTALLED REPAIR. REFERENCE E.A. 8-5710- T0361809. "WINGS-BASIC WING STRUCT
- [SDR FDEA202105171261](https://openairdocs.org/sdr/FDEA202105171261.md): Fillet · gouged · May 17, 2021 · N316FE · Doug MD1030F · Leading Edge Devices
  > LH WING # 1 SLAT FILLET ASSY LOWER SURFACE TRAILING EDGE GOUGE REPAIRED # 1 SLAT FILLET ASSY LOWER SURFACE TRAILING EDGE DAMAGED PER SRM 51-43- 01 VOL 2 PARAGRAPH 11.A STEPS ( 1)-(7)
- [SDR FDEA202105151228](https://openairdocs.org/sdr/FDEA202105151228.md): Floor Panel · damaged · May 15, 2021 · N316FE · Doug MD1030F · Fuselage Floor Panel
  > MAIN DECK FLOOR PANEL FROM STA 1561 TO 1650 AT LBL 107 TO LBL 75 HAS GOUGES IN SEVERAL AREAS (MARKED) FABRICATED NEW FLOOR PANEL REF FEDEX DRAWING SRZ-25-005
- [SDR FDEA202105131214](https://openairdocs.org/sdr/FDEA202105131214.md): Floor Panel · delaminated · May 13, 2021 · N316FE · Doug MD1030F · Fuselage Floor Panel
  > MAIN DECK FLOOR PANEL FROM STA 1099 TO 1029 AT LBL 107 TO LBL 75 POSSIBLY DELAMED (MARKED) FABRICATED NEW FLOOR PANEL REF FEDEX DRAWING SRZ-25-005
- [SDR FDEA202105121207](https://openairdocs.org/sdr/FDEA202105121207.md): Floor Panel · damaged · May 12, 2021 · N316FE · Doug MD1030F · Fuselage Floor Panel
  > MAIN DECK: FLOOR PANEL AT APPROX STA 1503 BETWEEN RBL 8 AND LBL 8 IS DAMAGED (MARKED AND DOT 44 IN 2 PLACES) REPAIRED MAIN DECK: FLOOR PANEL AT APPROX STA 1503 BETWEEN RBL 8 AND LBL 8 PER SRM 53-60-00 VOL I PG 6 FIG 6 (MAJOR REPAIR)
- [SDR FDEA202105121196](https://openairdocs.org/sdr/FDEA202105121196.md): Floor Panel · delaminated · May 12, 2021 · N316FE · Doug MD1030F · Fuselage Floor Panel
  > MAIN DECK FLOOR PANEL FROM STA 600 TO STA 658 AT LBL 107 TO 75 DELAMED FABRICATED FLOOR PANEL REF. FEDEX DRAWING SRZ-25-005
- [SDR FDEA202105121195](https://openairdocs.org/sdr/FDEA202105121195.md): Floor Panel · delaminated · May 12, 2021 · N316FE · Doug MD1030F · Cargo Compartments
  > MAIN DECK FLOOR PANEL FROM STA 600 TO STA 658 AT LBL 47 TO LBL 75 HAS SEVERAL GOUGES - POSSIBLE DELAMED FABRICATED FLOOR PANEL REF. FEDEX DRAWING SRZ-25-005
- [SDR FDEA202105111194](https://openairdocs.org/sdr/FDEA202105111194.md): Floor Panel · delaminated · May 11, 2021 · N316FE · Doug MD1030F · Fuselage Floor Panel
  > MAIN DECK FLOOR PANEL FROM APPROX STA 1481-1561 BETWEEN RBL 75-RBL107 IS WORN THROUGH TOP LAYER AT APPROX STA 1511 RBL 75 SIDE (MARKED AND DOT 41) FABRICATED NEW FLOOR PANEL ACA0126-4 FROM STA 1481-1561, RBL 75 TO RBL 107 AS REQ'D REF FEDEX DRAWING SRZ-25-
- [SDR FDEA202104281055](https://openairdocs.org/sdr/FDEA202104281055.md): Floor Panel · damaged · Apr 28, 2021 · N316FE · Doug MD1030F · Fuselage Floor Panel
  > AFT CARGO PIT FLOOR PANEL 187EF HAS MINOR DAMAGES ON TOP SURFACE FABRICATED NEW FLOOR PANEL REF FEDEX DRAWING SRZ-25-005
- [SDR FDEA202104281054](https://openairdocs.org/sdr/FDEA202104281054.md): Floor Panel · damaged · Apr 28, 2021 · N316FE · Doug MD1030F · Fuselage Floor Panel
  > AFT CARGO PIT FLOOR PANEL 187EF HAS MINOR DAMAGES ON TOP SURFACE FABRICATED NEW FLOOR PANEL REF FEDEX DRAWING SRZ-25-005
- [SDR FDEA202104261042](https://openairdocs.org/sdr/FDEA202104261042.md): Floor Panel · delaminated · Apr 26, 2021 · N316FE · Doug MD1030F · Fuselage Main, Structure
  > AFT CARGO PIT FLOOR PANEL 187GF HAS MULTIPLE PUNCTURES AND SHOWS SIGNS OF DELAMINATION FABRICATED NEW FLOOR PANEL REF FEDEX DRAWING SRZ-25-005
- [SDR FDEA202104261041](https://openairdocs.org/sdr/FDEA202104261041.md): Floor Panel · delaminated · Apr 26, 2021 · N316FE · Doug MD1030F · Fuselage Floor Panel
  > AFT CARGO PIT FLOOR PANEL 187CF HAS MULTIPLE PUNCTURES AND SHOWS SIGNS OF DELAMINATION FABRICATED NEW FLOOR PANEL REF FEDEX DRAWING SRZ-25-005
- [SDR FDEA202104261040](https://openairdocs.org/sdr/FDEA202104261040.md): Floor Panel · delaminated · Apr 26, 2021 · N316FE · Doug MD1030F · Fuselage Floor Panel
  > AFT CARGO PIT FLOOR PANEL 187AF HAS MULTIPLE PUNCTURES AND SHOWS SIGNS OF DELAMINAION FABRICATED NEW FLOOR PANEL REF FEDEX DRAWING SRZ-25-005
- [SDR FDEA202104261039](https://openairdocs.org/sdr/FDEA202104261039.md): Floor Panel · punctured · Apr 26, 2021 · N316FE · Doug MD1030F · Fuselage Floor Panel
  > AFT CARGO PIT FLOOR PANEL 187BF HAS MULTIPLE PUNCTURES AND SHOWS SIGNS OF DEMLAMINATION FABRICATED NEW FLOOR PANEL REF FEDEX DRAWING SRZ-25-005
- [SDR FDEA202104241193](https://openairdocs.org/sdr/FDEA202104241193.md): Skin · cracked · Apr 24, 2021 · N316FE · Doug MD1030F · Wing, Plate/Skin
  > R/H WING ANTI ICE TELESCOPING DUCT CUT OUT, TOP O/B CORNER CRACKED (MARKED) REPAIRED CRACK ON CORNER OF SKIN CUT-OUT FOR ANTI-ICE DUCT PER SRM 57-10-00 VOL.1 FIG. 103 SHEET 5. "MAJOR REPAIR"
- [SDR FDEA202104211215](https://openairdocs.org/sdr/FDEA202104211215.md): Skin · cracked · Apr 21, 2021 · N316FE · Doug MD1030F · Wing, Plate/Skin
  > LH WING TIP LOWER SURFACE, 1" CRACK IN SKIN - APPROX. XW987, OUTBD OF STROBE LIGHT CONTROLLER ACCESS DOOR. REPAIRED WINGTIP SKIN CRACK REF: SRM 57-00-01 VOL 1, FIG 4.
- [SDR FDEA202104201259](https://openairdocs.org/sdr/FDEA202104201259.md): Seal · cracked · Apr 20, 2021 · N316FE · Doug MD1030F · Trailing Edge Flaps
  > RH WING OUTBD FLAP OUTBD HINGE XW638 - METAL SEAL CRACKED AT PANEL 636JL. REMOVED AND INSTALLED NEW METAL SEAL PN ARC2148-9 ON ARC2148-504(636JL)FAIRING REF SRM 51-31-01 VOL 2 AND DWG ARC2148
- [SDR FDEA202104191354](https://openairdocs.org/sdr/FDEA202104191354.md): Longeron · corroded · Apr 19, 2021 · N316FE · Doug MD1030F · Fuselage Main, Longeron/Stringer
  > AFT CARGO COMPT BILGE STA 1854-1864 CORROSION AT L48R. MRKD 0003884010: GUTZWEILER, JOHN - 22-MAY-2021 05:37 REMOVED AND REPLACED DISCREPANT LONGERON SPLICE ASSEMBLY AFT CARGO COMPARTMENT BILGE STA 1854 - 1864 LONGERON 48R REF DWG NGA6314.
- [SDR FDEA202104171312](https://openairdocs.org/sdr/FDEA202104171312.md): Door Frame · chafed · Apr 17, 2021 · N316FE · Doug MD1030F · Fuselage Main, Structure
  > LOWER CENTER CARGO DOOR, LOWER AFT JAMB EDGE DAMAGED, MARKED. REMOVED DAMAGE AND COMPLIED WITH DOOR JAMB REPAR AT LOWER CENTER CARGO DOOR LOWER AFT EDGE PER MD10-30 SRM 53-53-00 FIG 26 VOL 1.
- [SDR FDEA202104171133](https://openairdocs.org/sdr/FDEA202104171133.md): Skin · damaged · Apr 17, 2021 · N316FE · Doug MD1030F · Leading Edge Devices
  > RIGHT WING #3 SLAT AFT SIDE HAS MANY DAMAGED, MISSING AND LOOSE RIVETS. 0000435071: HARPER, RICHARD R - 05-MAY-2021 19:03 REMOVED AND REPLACED FASTNERS ON R/H WING SLAT#3 INNER SKIN PER SRM 57-10-00 PARA.90, PG.387 ALSO TRACKING EA 8-5750-T0361351
- [SDR FDEA202104171132](https://openairdocs.org/sdr/FDEA202104171132.md): Skin · damaged · Apr 17, 2021 · N316FE · Doug MD1030F · Leading Edge Devices
  > RIGHT WING #4 SLAT AFT SIDE HAS MANY DAMAGED, MISSING AND LOOSE RIVETS. 0000435071: HARPER, RICHARD R - 05-MAY-2021 18:58 REMOVED AND REPLACED FASTNERS ON R/H WING SLAT#4 INNER SKIN PER SRM 57-10-00 PARA.90 PG.387 AND TRACKING EA 8-5750-T0361370
- [SDR FDEA202104161355](https://openairdocs.org/sdr/FDEA202104161355.md): Panel · corroded · Apr 16, 2021 · N316FE · Doug MD1030F · Wing, Plate/Skin
  > L/H WING TRAPERZOID PANEL ARC0269-503 SHOWS SIGNS OF CORROSION AND DELAMINATION PERFORMED REPAIR BONDING ON PNL ARC0269-503 PER SRM 51-71-00 VII PARAGRAPH 18.
- [SDR FDEA202104161131](https://openairdocs.org/sdr/FDEA202104161131.md): Seat Track · worn · Apr 16, 2021 · N316FE · Doug MD1030F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CARGO COMPT, APPROX STA 1199 X= 47.50, SEAT TRACK WORN. FOUND SEAT TRACK TO BE WORN OUT OF LIMITS. REPLACED SEAT TRACK SECTION AT APPROX STA 1213 TO 1261 X 47.5 PER SRM 53-70-00 FIG 1 VOL 1.
- [SDR FDEA202104161050](https://openairdocs.org/sdr/FDEA202104161050.md): Seat Track · damaged · Apr 16, 2021 · N316FE · Doug MD1030F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CARGO COMPT, APPROX STA 959-969 X= -27.50, SEAT TRACK WORN AT TWO LOCATIONS. REMOVED DAMAGE AND INSTALLED PLUG REPAIR. REF. SRM 53-70-00 FIG. 2 VOL.1 "MAJOR REPAIR"
- [SDR FDEA202104151057](https://openairdocs.org/sdr/FDEA202104151057.md): Support · corroded · Apr 15, 2021 · N316FE · Doug MD1030F · Fuselage Main, Bulkhead
  > STRUCTURES - FUSELAGE SEALS AND DRAINS: DURING FUSELAGE PRESSURIZATION, AT R/H MAIN LANDING GEAR WHEEL WELL R/H UPPER T-CORD FWRD BULKKHEAD LEAKING, SHOWING SHOWING WHITE POWDERY SUBSTANCE UNDER 4 EACH CLAMPS/CLIPS & RUB STRIP MIGRATED MIGRATED BETWEEN CL
- [SDR FDEA202104151136](https://openairdocs.org/sdr/FDEA202104151136.md): Bulkhead · cracked · Apr 15, 2021 · N316FE · Doug MD1030F · Fuselage Main, Bulkhead
  > CENTER LANDING GEAR WHEEL WELL, L/H FWD VERTICAL BULKHEAD, AT TRANSITION HOLE FOR SPOILER/AILERON CONTROL RODS, STA 1381 Z=-76 TO -87. DOUBLER FITTING AEA0486 HAS A FOUR INCH CRACK ALONG THE VERTICAL FASTENER ROW, TOP AREA. (MKD) REMOVE AND REPLACE LONGER
- [SDR FDEA202104150974](https://openairdocs.org/sdr/FDEA202104150974.md): Seat Track · worn · Apr 15, 2021 · N316FE · Doug MD1030F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK SEAT TRACK AT APROX STA 1640 RBL 47.50 WORN (MARKED) REMOVED WORN SEAT TRACK SECTION AND SPLICED IN NEW SECTION OF SEAT TRACK. REF. SRM 53-70-00 FIG. 1 VOL.1 AND FEDEX DRAWING SR10-53-002.
- [SDR FDEA202102240441](https://openairdocs.org/sdr/FDEA202102240441.md): Line · leaking · Feb 24, 2021 · N316FE · Doug MD1030F · Hydraulic System, Main
  > PDIS 316 29-02 5970 23FEB21 MEM FACT U "ENROUTE TO KMEM LEVEL 1 "HYD 3 ELEV OFF" ALERT ILLUMINATED. HYD 3 WAS AT 4.3 AT THE TIME. HYD 3 CONTINUED TO DECREASE TO 3.0. GEAR EXTENDED W/GEAR HANDLE AND FLAPS & SLATS DEPLOYED OKAY. MADE FLAPS 35/E
- [SDR FDEA202101010001](https://openairdocs.org/sdr/FDEA202101010001.md): Tee Fitting · cracked · Jan 1, 2021 · N316FE · Doug MD1030F · Hydraulic System, Main
  > "HYD 3 ELEV OFF" ALERT CAME ON. WE NOTICED HYD 3 QUANTITY SLOWLY DECLINE. WE LATER HAD HYD QUANTITY LOW. WE EXTENDED THE LANDING GEAR NORMALLY. WE THEN HAD HYD 3 FAIL. AFTER BLOCK IN FOUND HYDRAULIC QTY NR 3 SYSTEM AT 3.5 GAL. FOUND HYD LINE CRACKED AT
- [SDR FDEA202011282986](https://openairdocs.org/sdr/FDEA202011282986.md): Lamp · inoperative · Nov 28, 2020 · N316FE · Doug MD1030F · Emergency Equipment
  > MDIS 316 25-60 5669 28NOV20 MEM OPEN U. L1 DOOR SLIDE PRESS TO TEST LIGHT INOPERABLE. RELAMPED AND R & R BATTERIES, PER AMM 25-61-03-2. TROUBLESHOOTING IS REQUIRED PRIOR TO INSTALLING PARTS.
- [SDR FDEA2019111542953](https://openairdocs.org/sdr/FDEA2019111542953.md): Battery Pack · no test · Nov 14, 2019 · N316FE · Doug MD1030F · Emergency Lighting
  > L1 DOOR SLIDE LIGHT WILL NOT TEST. REPLACED SLIDE INDICATOR BATTERIES, OPS CHECKS GOOD. REF MD10MM 25-61-02-2.
- [SDR FDEA201906111271](https://openairdocs.org/sdr/FDEA201906111271.md): Engine · fluctuates · Jun 11, 2019 · N316FE · Doug MD1030F · Engine (Turbine/Turboprop)
  > CLIMBOUT OUT OFF FL230"ENG 3 EXCEEDANCE"LVL ALERT DISPLAYED.EGT OBSERVERED AT 964 WITH PWR EQUAL OTHER PARAMETERS EQUAL.DURING CRUISE HAD #3 ENG PULLED BACK 10-15% N1 TO KEEP BELOW YELLOW ARC.NOTICED SLOW FLUCTUATIONS FROM 590 EGT TO 800 DURING LVL FLT.
- [SDR FDEA201905081015](https://openairdocs.org/sdr/FDEA201905081015.md): Panel · corroded · May 8, 2019 · N316FE · Doug MD1030F · Fuselage Main, Bulkhead
  > AUX FUEL TANK PANEL AT REAR SPAR HAS CORROSION AT MANY LOCATIONS. FABRICATED FUEL TANK BULKHEAD PANEL ON T19/1410809. REINSTALLED 6EA STIFFNERS IAW SRM 51-31-01. BULKHEAD REMOVED / REPLACED ON WORK CARD 53SI1520-01. MAJOR REPAIR
- [SDR FDEA2019042290865](https://openairdocs.org/sdr/FDEA2019042290865.md): Seat Track · corroded · Apr 19, 2019 · N316FE · Doug MD1030F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK SEAT TRACK AT X8.5 STA 1601 TO STA 1661 HAS GOUGES AND SURFACE CORROSION AT 3EA LOCATIONS. REMOVED AND REINSTALLED 2EA FLOOR PANELS FOR ACCESS IAW MD10-30 AMM 53-21-01-2. REPAIRED DAMAGED FLOOR PANELS (2EA) IAW SRM 53-60-00 FIG 6. REMOVED AND
- [SDR FDEA201811033089](https://openairdocs.org/sdr/FDEA201811033089.md): Switch · activated · Nov 3, 2018 · N316FE · Doug MD1030F · Pneumatic Indicating System
  > AT FL280 ABOUT TO DESCEND INTO ICING WE TURNED ON WING ANTI-ICE. RECEIVED LVL 1 AIR SYS 3 OFF WITH RED MANIFOLD NR 3 INDICATION BOTH ON SCHEMATIC AND AIR SYSTEM CONTROL PANEL BLEED AIR 3 MANIFOLD LIGHT. CONSULTED WITH MOCC DIVERTED TO AVOID KNOWN ICING. REMOVE
- [SDR FDEA201807061643](https://openairdocs.org/sdr/FDEA201807061643.md): Probe · inoperative · Jul 6, 2018 · N316FE · Doug MD1030F · Fuel Quantity Sensor
  > 15 MIN ENROUTE. JUST LEVELED AT FL350. GOT LVL 2 FUEL QTY/USED CHK. COMPLIED WITH QRH. TOTAL QTY INDICATED. 9.0 LBS LESS THAN REQUIRED. ( SHOULD OF HAD 57.0, INDICATED 48.0) RTB KMEM. POSSIBLE FUEL LEAK. FOUND PROBE NR 3 ON RT INOP, REMOVED AND REPLACED AND
- [SDR FDEA201803230766](https://openairdocs.org/sdr/FDEA201803230766.md): Control Module · out of adjust · Mar 23, 2018 · N316FE · Doug MD1030F · Trailing Edge Flap Control System
  > DURING TAKEOFF THE FLAP/SLAT HANDLE WOULD NOT MOVE OUT OF TAKEOFF FLAP SETTING 15.5. INITIALLY COULD NOT MOVE FLAP SELECTOR WHEEL EITHER. EVENTUALLY USED THE FLAP SELECTOR WHEEL TO SELECT FLAPS 24 FOR LANDING, COULD NOT MOVE FLAP HANDLE OR GET SELECTOR TO
- [SDR FDEA201707192004](https://openairdocs.org/sdr/FDEA201707192004.md): Wire · pulled · Jul 19, 2017 · N316FE · Doug MD1030F · Light System Wiring
  > EMERGENCY LIGHTS BATTERY 1 LOW ALERT. FOUND WIRE FOR PIN 8 OF P1-1756A PULLED OUT OF CONTACT. TERMINATED THE WIRE. EMERGENCY LIGHTS OPS CHECKED GOOD. PERFORMED IAW M/M 33-51-01-5 AND WDM 33-51-01.
- [SDR FDEA201703150897](https://openairdocs.org/sdr/FDEA201703150897.md): Fitting · cracked · Mar 15, 2017 · N316FE · Doug MD1030F · Trailing Edge Flaps
  > RIGHT WING, OTBD FLAP INBD HINGE STRESS FITTING FOUND CRACKED. REMOVED AND REPLACED THE FITTING IAW EA 8-5740 -T0331942, AND DWG ARB0029.
- [SDR FDEA201703120855](https://openairdocs.org/sdr/FDEA201703120855.md): Skin · cracked · Mar 12, 2017 · N316FE · Doug MD1030F · Wing, Plate/Skin
  > RT WING, FWD OF FUEL ACCESS PANEL CUT OUT, L/E SKIN HAS A CRACKED.075 LENGTH. REMOVED CRACKED, INSTALLED FILLER AND DOUBLER PER SRM 57-10-00 VOL 1 FIGURE 106 SHEET 2.
- [SDR FDEA201703120854](https://openairdocs.org/sdr/FDEA201703120854.md): Skin · cracked · Mar 12, 2017 · N316FE · Doug MD1030F · Wing, Plate/Skin
  > RT WING, FWD OF FUEL ACCESS PANEL CUT OUT, L/E SKIN HAS A CRACKED.075 LENGTH. REMOVED CRACK AND INSTALLED DOUBLER AND FILLER PER SRM 57-10-00 FIG 106 VOL2 SHEET 2.
- [SDR FDEA201703090827](https://openairdocs.org/sdr/FDEA201703090827.md): Support · corroded · Mar 9, 2017 · N316FE · Doug MD1030F · Fuselage Miscellaneous Structure
  > AFT WASTE COMP STA 1967 LOWER CENTER SUPPORT STRUCTURE AFT SIDE HAS EXFOLIATION CORROSION AROUND SEVERAL NUTPLATES. REMOVED AND REPLACED SUPPORT PER DWG AGA 3857-1.
- [SDR FDEA201703080818](https://openairdocs.org/sdr/FDEA201703080818.md): Skin · cracked · Mar 8, 2017 · N316FE · Doug MD1030F · Trailing Edge Flaps
  > RT I/B FLAP VANE LOWER SURFACE HAS DEEP DENT, FOUND AN 3/8" CRACK. REPAIRED CRACK IAW SRM 51-71-00 VOL II PAGE 9 PAR 5 (A).
- [SDR FDEA201703020753](https://openairdocs.org/sdr/FDEA201703020753.md): Skin · delaminated · Mar 2, 2017 · N316FE · Doug MD1030F · Trailing Edge Flaps
  > RIGHT OTBD FLAP VANE SKIN BENEATH NR 6 RUBSTRIP IS DELAMINATED. REPAIRED THE SKIN IAW SRM 51-71-00, VOL II, PAGE 9, PAR 5 (A), PAR 15.

Next page: https://openairdocs.org/aircraft/N316FE/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 = 'N316FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N316FE/reports

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