N316FE

Service difficulty reports · 107

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR FDEA202211102747Line · splitON 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 ACCOMPLISHEDNov 10, 2022 · N316FE · Doug MD1030F · Hydraulic System, MainSDR FDEA202204301098None · nonePDIS 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 THEApr 30, 2022 · N316FE · Doug 600N · Trailing Edge Flap Control SystemSDR FDEA202201220117Skin · damagedINDY 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 8-5Jan 22, 2022 · N316FE · Doug MD1030F · Wing, Plate/SkinSDR FDEA202105291419Door Sill · crackedCENTER CARGO DOOR SILL, LOWER AFT SECTION HAS A CRACK REPAIRED PER SRM MD10 53-00-01 VOL I P40May 29, 2021 · N316FE · Doug MD1030F · Fuselage Miscellaneous StructureSDR FDEA202105211357Floor Panel · delaminatedMAIN 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 SRMMay 21, 2021 · N316FE · Doug MD1030F · Fuselage Floor PanelSDR FDEA202105201408Skin · dentedREWORK: 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 FMay 20, 2021 · N316FE · Doug MD1030F · Wing, Plate/SkinSDR FDEA202105171412Doubler · damagedRH 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 STRUCTMay 17, 2021 · N316FE · Doug MD1030F · Wing Main, Frame StructureSDR FDEA202105171261Fillet · gougedLH 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)May 17, 2021 · N316FE · Doug MD1030F · Leading Edge DevicesSDR FDEA202105151228Floor Panel · damagedMAIN 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-25-005May 15, 2021 · N316FE · Doug MD1030F · Fuselage Floor PanelSDR FDEA202105131214Floor Panel · delaminatedMAIN 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-25-005May 13, 2021 · N316FE · Doug MD1030F · Fuselage Floor PanelSDR FDEA202105121207Floor Panel · damagedMAIN 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)May 12, 2021 · N316FE · Doug MD1030F · Fuselage Floor PanelSDR FDEA202105121196Floor Panel · delaminatedMAIN DECK FLOOR PANEL FROM STA 600 TO STA 658 AT LBL 107 TO 75 DELAMED FABRICATED FLOOR PANEL REF. FEDEX DRAWING SRZ-25-005May 12, 2021 · N316FE · Doug MD1030F · Fuselage Floor PanelSDR FDEA202105121195Floor Panel · delaminatedMAIN 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-25-005May 12, 2021 · N316FE · Doug MD1030F · Cargo CompartmentsSDR FDEA202105111194Floor Panel · delaminatedMAIN 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-May 11, 2021 · N316FE · Doug MD1030F · Fuselage Floor PanelSDR FDEA202104281055Floor Panel · damagedAFT CARGO PIT FLOOR PANEL 187EF HAS MINOR DAMAGES ON TOP SURFACE FABRICATED NEW FLOOR PANEL REF FEDEX DRAWING SRZ-25-005Apr 28, 2021 · N316FE · Doug MD1030F · Fuselage Floor PanelSDR FDEA202104281054Floor Panel · damagedAFT CARGO PIT FLOOR PANEL 187EF HAS MINOR DAMAGES ON TOP SURFACE FABRICATED NEW FLOOR PANEL REF FEDEX DRAWING SRZ-25-005Apr 28, 2021 · N316FE · Doug MD1030F · Fuselage Floor PanelSDR FDEA202104261042Floor Panel · delaminatedAFT CARGO PIT FLOOR PANEL 187GF HAS MULTIPLE PUNCTURES AND SHOWS SIGNS OF DELAMINATION FABRICATED NEW FLOOR PANEL REF FEDEX DRAWING SRZ-25-005Apr 26, 2021 · N316FE · Doug MD1030F · Fuselage Main, StructureSDR FDEA202104261041Floor Panel · delaminatedAFT CARGO PIT FLOOR PANEL 187CF HAS MULTIPLE PUNCTURES AND SHOWS SIGNS OF DELAMINATION FABRICATED NEW FLOOR PANEL REF FEDEX DRAWING SRZ-25-005Apr 26, 2021 · N316FE · Doug MD1030F · Fuselage Floor PanelSDR FDEA202104261040Floor Panel · delaminatedAFT CARGO PIT FLOOR PANEL 187AF HAS MULTIPLE PUNCTURES AND SHOWS SIGNS OF DELAMINAION FABRICATED NEW FLOOR PANEL REF FEDEX DRAWING SRZ-25-005Apr 26, 2021 · N316FE · Doug MD1030F · Fuselage Floor PanelSDR FDEA202104261039Floor Panel · puncturedAFT CARGO PIT FLOOR PANEL 187BF HAS MULTIPLE PUNCTURES AND SHOWS SIGNS OF DEMLAMINATION FABRICATED NEW FLOOR PANEL REF FEDEX DRAWING SRZ-25-005Apr 26, 2021 · N316FE · Doug MD1030F · Fuselage Floor PanelSDR FDEA202104241193Skin · crackedR/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"Apr 24, 2021 · N316FE · Doug MD1030F · Wing, Plate/SkinSDR FDEA202104211215Skin · crackedLH 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.Apr 21, 2021 · N316FE · Doug MD1030F · Wing, Plate/SkinSDR FDEA202104201259Seal · crackedRH 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 ARC2148Apr 20, 2021 · N316FE · Doug MD1030F · Trailing Edge FlapsSDR FDEA202104191354Longeron · corrodedAFT 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.Apr 19, 2021 · N316FE · Doug MD1030F · Fuselage Main, Longeron/StringerSDR FDEA202104171312Door Frame · chafedLOWER 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.Apr 17, 2021 · N316FE · Doug MD1030F · Fuselage Main, StructureSDR FDEA202104171133Skin · damagedRIGHT 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-T0361351Apr 17, 2021 · N316FE · Doug MD1030F · Leading Edge DevicesSDR FDEA202104171132Skin · damagedRIGHT 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-T0361370Apr 17, 2021 · N316FE · Doug MD1030F · Leading Edge DevicesSDR FDEA202104161355Panel · corrodedL/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.Apr 16, 2021 · N316FE · Doug MD1030F · Wing, Plate/SkinSDR FDEA202104161131Seat Track · wornMAIN 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.Apr 16, 2021 · N316FE · Doug MD1030F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202104161050Seat Track · damagedMAIN 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"Apr 16, 2021 · N316FE · Doug MD1030F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202104151057Support · corrodedSTRUCTURES - 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 CLApr 15, 2021 · N316FE · Doug MD1030F · Fuselage Main, BulkheadSDR FDEA202104151136Bulkhead · crackedCENTER 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 LONGERApr 15, 2021 · N316FE · Doug MD1030F · Fuselage Main, BulkheadSDR FDEA202104150974Seat Track · wornMAIN 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.Apr 15, 2021 · N316FE · Doug MD1030F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202102240441Line · leakingPDIS 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/EFeb 24, 2021 · N316FE · Doug MD1030F · Hydraulic System, MainSDR FDEA202101010001Tee Fitting · cracked"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 ATJan 1, 2021 · N316FE · Doug MD1030F · Hydraulic System, MainSDR FDEA202011282986Lamp · inoperativeMDIS 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.Nov 28, 2020 · N316FE · Doug MD1030F · Emergency EquipmentSDR FDEA2019111542953Battery Pack · no testL1 DOOR SLIDE LIGHT WILL NOT TEST. REPLACED SLIDE INDICATOR BATTERIES, OPS CHECKS GOOD. REF MD10MM 25-61-02-2.Nov 14, 2019 · N316FE · Doug MD1030F · Emergency LightingSDR FDEA201906111271Engine · fluctuatesCLIMBOUT 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.Jun 11, 2019 · N316FE · Doug MD1030F · Engine (Turbine/Turboprop)SDR FDEA201905081015Panel · corrodedAUX 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 REPAIRMay 8, 2019 · N316FE · Doug MD1030F · Fuselage Main, BulkheadSDR FDEA2019042290865Seat Track · corrodedMAIN 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 Apr 19, 2019 · N316FE · Doug MD1030F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201811033089Switch · activatedAT 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. REMOVENov 3, 2018 · N316FE · Doug MD1030F · Pneumatic Indicating SystemSDR FDEA201807061643Probe · inoperative15 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 ANDJul 6, 2018 · N316FE · Doug MD1030F · Fuel Quantity SensorSDR FDEA201803230766Control Module · out of adjustDURING 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 Mar 23, 2018 · N316FE · Doug MD1030F · Trailing Edge Flap Control SystemSDR FDEA201707192004Wire · pulledEMERGENCY 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.Jul 19, 2017 · N316FE · Doug MD1030F · Light System WiringSDR FDEA201703150897Fitting · crackedRIGHT WING, OTBD FLAP INBD HINGE STRESS FITTING FOUND CRACKED. REMOVED AND REPLACED THE FITTING IAW EA 8-5740 -T0331942, AND DWG ARB0029.Mar 15, 2017 · N316FE · Doug MD1030F · Trailing Edge FlapsSDR FDEA201703120855Skin · crackedRT 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.Mar 12, 2017 · N316FE · Doug MD1030F · Wing, Plate/SkinSDR FDEA201703120854Skin · crackedRT 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.Mar 12, 2017 · N316FE · Doug MD1030F · Wing, Plate/SkinSDR FDEA201703090827Support · corrodedAFT 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.Mar 9, 2017 · N316FE · Doug MD1030F · Fuselage Miscellaneous StructureSDR FDEA201703080818Skin · crackedRT 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).Mar 8, 2017 · N316FE · Doug MD1030F · Trailing Edge FlapsSDR FDEA201703020753Skin · delaminatedRIGHT 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.Mar 2, 2017 · N316FE · Doug MD1030F · Trailing Edge Flaps
Back to N316FE