N315FE
Service difficulty reports · 212
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 = 'N315FE' 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.
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 = 'N315FE' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR FDEA201407141776Skin · gougedRIGHT INBD FLAP UPPER SKIN GOUGED AT NUMEROUS LOCATIONS, XIFH 250 - 295. BLENDED UPPER SKIN DAMAGE AREA DIM L=.100", W=.050", D=.002". L=.100", W=.050", D=.002". L=.150", W=.100", D=.003". L=.100", W=.080", D=.002". L=.100", W=.080", D=.002". FOUND TO BSDR FDEA201407141774Skin · damagedMULTIPLE LIGHTNING STRIKES AT LT SIDE OF UPPER AFT RUDDER NEAR THE TIP. REMOVED, RE-INSTALLED & PERFORMED FUNCTIONAL CHECK UPPER AFT RUDDER IAW AMM 27-20-02-4, CHECKED GOOD. FABRICATED DOUBLER STRAP & SKIN REPAIR IAW SRM 55-10-00 & 55-31-01 & CHECKED CLEARANSDR FDEA201407141773Plate · gougedLEFT WING INBD TE ADJACENT TO OTBD FLAP VANE. METAL STRIKE PLATE HAS GOUGE. BLENDED LT WING INBD TE METAL STRIKE PLATE. LENGTH = 3.3 INCHES, WIDTH = 1.9 INCHES & DEPTH = 0.0295 INCHES. FOUND ACCEPTABLE IAW EA 8-5750-T0309660 PS P1. MINOR REPAIR.SDR FDEA201407141771Skin · gougedGOUGED MARK ON FUSELAGE SKIN AT FWD CARGO DOOR CUT OUT LOWER FWD CORNER. NO ALLOWABLE DAMAGE ON AN EXISTING REPAIR. R & R NR 1 DOUBLER ON EXISTING REPAIR IAW SRM VOL I 53-50-00 FIG 26 SHT 3. MATERIAL IS 2024-T3 .090C BATCH 2540972. SKIN PN IS ADA3139-501SDR FDEA201407131755Panel · chafedRIGHT HORIZONTAL STAB PNL 352BZ HAS CHAFING WEAR. EVALUATED CHAFE, FOUND CHAFE MARK LESS THAN 2D FROM FASTENER HOLE. FOUND TO BE OUT OF LIMITS IAW SRM VOL 1, 55-00-01, FIG 1A SHT 1. FABRICATED NEW PANEL ON TR T14 1078626, 7075-T6, BATCH 0001689641. TRANSFSDR FDEA201407121753Stiffener · crackedNUMBER 3 ENG PYLON AFT LOWER FAIRING HAS CRACK ON LAST TWO STIFFENERS. REMOVED CRACKED RIBS TWO EACH IAW SRM VOL II 51-31-01. GENERATED & REVISED EA 8-5480-T0309537 P1. WELDED CRACKS ON TRAVELER'S T14 1079877 & T14 1079876. LOCATED, DRILLED & INSTALLED TWOSDR FDEA201407121752Skin Panel · dentedFUSELAGE SKIN AFT OF AFT CARGO DOOR CUT OUT LOWER CORNER HAS THREE EACH DENTS. MEASURED DENTS IN SKIN L 087 X D 040, L 087 X D 039, L1.10 X D.10 FOUND ALL THREE ARE OUT OF LIMITS IAW SRM 53-20-00, FIG 13 TABLE A VOL 1. CUT OUT DAMAGE IAW SRM 53-50-00 FIG 26 SDR FDEA201407091679Skin · chafedRIGHT INBD AILERON, LOWER SECTION OF INBD END LE HAVE CHAFED MARK. R & R SKIN & SUPPORT BRACKET IAW SRM 51-31-01 PG 1 ON RT INBD AILERON LOWER SECTION OF INBD LE. SKIN FABRICATED ON T14 1078081 IAW SRM 57-51-01. MAJOR REPAIR.SDR FDEA201407091676Skin · wornAFT FUSELAGE ACCESS DOOR 311AB CUT OUT UPPER SURFACE HAS WEAR MARKS. OUT OF LIMITS IAW SRM 53-00-01 FIG 1A. PERFORMED REPAIR BY COMPLYING WITH EA 8-5330-T0309419 DATE JUL 03, 2014. MAJOR REPAIR.SDR FDEA201407061637Stiffener · crackedUPON REMOVAL & REPLACEMENT OF R2 DOOR BEAM NR 2, A FWD UPPER STIFFENER WAS CRACKED AT LOWER END DURING RIVET REMOVAL. R & R ONE EACH STIFFENER AT FWD UPPER R2 DOOR BEAM NR 2 IAW SRM 51-31-01. STIFFENER WAS FABRICATED ON T14 1078173 IAW SRM 52-12-01. PN ADA3SDR FDEA201407051634Floor Panel · puncturedMAIN DECK FLOOR PANEL PUNCTURED BS 1900 RBL 50. R & R MAIN DECK FLOOR PANEL AT BS 1900, RBL - 50 IAW AMM 53-21-08-04. FABRICATED NEW FLOOR PANEL ON T14/1077523. MAJOR REPAIR.SDR FDEA201407011599Support · corrodedAFT CARGO FRAME STATION 1841 UPPER CHORD HAS CORROSION UNDER NUTPLATES FROM LONGERON 43L TO 43R. REMOVED CORROSION FROM -43 SUPPORT AT FS 1841 IAW SRM 51-21-01. ORIGINAL THICKNESS .125, .079 MATERIAL REMAINING. OUT OF LIMIT IAW SRM 53-00-01, FIG 1B, PG 12. SDR FDEA201406301589Floorboard · damagedMAIN DECK FLOORBOARD DAMAGED BS 765 BLO RECEIVED NEW FLOOR PANEL ON MAIN DECK BS 765 BL0 ON T14/1077527. INSTALLED FLOOR PANEL IAW SRM 51-31-01 & AMM 53-21-08-04. MAJOR REPAIR.SDR FDEA201406301588Floorboard · puncturedMAIN DECK FLOORBOARD PUNCTURED BS 655 - 735 BL0 FOUR LOCATIONS. RECEIVED NEW MAIN DECK FLOOR PANEL BS 655 - 735 BL0 ON T14/1077525. INSTALLED FLOOR PANEL IAW SRM 51-31-01 & AMM 53-21-08-04. MAJOR REPAIR.SDR FDEA201406301587Floorboard · puncturedMAIN DECK FLOORBOARD PUNCTURED AT SEVERAL SPOTS BS 791 - 840 LBL 76 - 106. RECEIVED NEW MAIN DECK FLOOR PANEL BS 791 - 840 LBL 76 - 106 ON T141077528. INSTALLED FLOOR PANEL IAW SRM 51-31-01 & AMM 53-21-08-04. MAJOR REPAIR.SDR FDEA201406281582Floor Panel · damagedCABIN FLOOR PANEL 283CF HAS MISSING EDGE SEALANT. FABRICATED FLOOR PANEL 283CF IAW SRM VOL II 51-62-01 & DWG SRZ-25-005. MAJOR REPAIR.SDR FDEA201406281581Floor Panel · delaminatedCABIN FLOOR PANEL 283JF DELAMINATED. FABRICATED NEW CABIN FLOOR PANEL 283JF ON T141077202 IAW SRZ-25-005 IAW VOL II SRM 51-62-01 AT RBL 27 - 46 BS 1741 - 1821. MAJOR REPAIR.SDR FDEA201406281580Floorboard · damagedMAIN DECK FLOORBOARD DAMAGED BS 695 LBL 85. FABRICATED NEW MAIN DECK FLOORBOARD AT BS 695 LBL 85 ON T141076888 IAW SRZ-25-005 IAW VOL II SRM 51-62-01. MAJOR REPAIR.SDR FDEA201406281579Floor Panel · crackedMAIN CARGO DECK FLOOR PANEL 293HF TOP SKIN, AFT END CRACKED. FABRICATED MAIN CARGO DECK FLOOR PANEL 293HF ON T141076890 PER SRZ-25-005 IAW VOL II SRM 51-62-01 AT RBL 4 - RBL 4 BS 1910-2007. MAJOR REPAIR.SDR FDEA201406281577Floorboard · damagedCABIN FLOOR PNL 252FF HAVE DAMAGED SEALANT ON EDGES. FABRICATED NEW CABIN FLOOR PANEL 252FF ON T14 1077204 IAW SRZ-25-00 IAW VOL II SRM 51-62-01 AT RBL 46- RBL 74 BS 1099 - 1159. MAJOR REPAIRSDR FDEA201406281575Floorboard · puncturedMAIN DECK FLOORBOARD PUNCTURED BS 1039 LBL 10. FABRICATED NEW FLOOR PANEL AT BS 1039 LBL 10 IAW SRZ-25-005 & SRM VOL II 51-22-01 ON VTAM T14/1076889.SDR FDEA201309142225Display · failedTHIRTY MINUTES INTO FLIGHT, MCDU 1 SHOWED LSK 1L BLANK (NO FMC) 100 MINS LATER MCDU 2 WENT BLANK AND FMC-2 DROPPED OFF NEVER GOT "MAP FAIL" ON MAP DISPLAY. WHEN ENG'S WERE SHUTDOWN IN PARKING GROUND POWER TOOK OVER, MCDU 2 CAME BACK UP.SDR FDEA201303250670Battery Pack · failedDURING PRE FLIGHT CHECK, EMERGENCY LIGHT DID NOT TEST, EMERGENCY LIGHT BATTERY 1 LOW MESSAGE DISPLAYED REPLACED FORWARD EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-01-4. OPS GOOD. ACFT OK FOR SERVICE.SDR FDEA201206112179Light · malfunctionedCOCKPIT OVERHEAD EMERGENCY LIGHT DOES NOT COME ON WITH LOSS OF POWER. SWITCH IS IN ARM, GO TO "ON" LIGHT WILL COME ON. PERFORMED EMERGENCY LIGHTING ADJUSTMENT AND TEST IAW MM 33-50-00-5. OPS CHECKED OK.SDR FDEA201205221934Control Valve · looseHORIZONTAL STABILIZER LOWER PRIMARY TRIM CONTROL VALVE FOUND FLOW CONTROL VALE BORE .75" PRESSURE PASSAGE BORE WITH A METAL ORIFICE PLUG STUCK IN IT. THIS IS AREA OF HFEC INSP AND WAS UNABLE TO COMPLY WITH THIS PROCEDURE DUE TO BLOCKAGE. REPLACED LOWER PRIMASDR FDEA201205031730Landing Light · damagedON POST FLIGHT WALK AROUND, FOUND RT FUSELAGE LANDING LIGHT MISSING, AND WIRING TO LIGHT EXPOSED. PULLED AND TAGGED RT LANDING LT CONTROL & LAMP CB'S. FOUND NO EVIDENCE OF DAMAGE TO ACFT FROM MISSING LANDING LIGHT. REPLACED LANDING LIGHT ASSY IAW AMM 33-SDR FDEA201106032105Bulb · inoperativeRT CABIN DOOR DISARM LIGHT INOP. R & R 2 EA BULBS IN DISARM LIGHT. FINAL CLOSED.SDR FDEA201105031709Warning Light · false activationAT 98 KTS GOT A NR 2 ENG EXCEEDANCE ALERT REJECT TAKEOFF. PERFORMED FAN (N1) OVERSPEED INSP, FAN BLADES MOTOR FREE FOR ROTATION FIRST STAGE FAN SHROUD WITHOUT RUB TRACES AND INLET AND EXHAUST NOZZLES FREE FROM PARTICLES IAW AMM 72-00-00-6-2. ACFT OK FOR SESDR FDEA201104271646Cable · out of positionCAPT'S LT SLIDING WINDOW WOULD NOT OPEN. FOUND WINDOW CRANK CABLE OFF TRACK ON MOST AFT PULLEY. REINSTALLED CABLE AND PROPERLY POSITIONED CABLE GUIDE PIN. WINDOW OPS CHECK NORMAL. REF: MM 56-12-01-2, FINAL CLOSED.SDR FDEA201104121459Indicator · stickingON SHORT FINAL RECEIVED FUEL QTY/USED CK LEVEL 2 ALERT LANDED-CLEARED RUNWAY-HAD FIRE DEPT CK FOR LEAKS-NONE WERE SEEN-TAXIED TO BLOCKS. ONCE PARKED, ALERT CLEARED. EXPECTED FUEL QTY=24.4 ACTUAL FUEL QTY=23.6 RELEASED FOR SERVICE IAW MEL: 28-01-01 CATEGOSDR FDEA201102040468Unknown · odorAFTER APU START, WHEN PACKS TURNED ON HAD FUEL ODOR FOR APROX 20 SECONDS. CONDUCTED A NORMAL APU START, REF JRH, 3-5,3-6 3-7, RAN PACKS, NO ABNORMAL ODORS NOTED, PACK OPS GOOD REF MM 21-00-00, COULD NOT DUPLICATE.SDR FDEA201101080076Engine · bird ingestionMULTIPLE BIRD STRIKES, FRONT WINDSCREEN AND NR 3 ENGINE. MODERATE VIBRATION, DECLARED AN EMERGENCY, COMPLIED WITH QRH, DIVERTED. (DEPARTED 16R BIRD STRIKE AT 2,500 FT MSL) FIRED BOTH BOTTLES INTO NR 3 ENGINE. LOST "B" LOOPS.SDR FDEA201008112919Engine · inoperativeMANUAL FUEL/PUMPS ON HAD PROBLEM STARTING NR2. 1ST ATTEMPT-ENGINE ROLLED BACK AFTER 40 PERCENT, N1. SECOND ATTEMPT SLOW BUT STARTED OK. CHECKED POWER SEVERAL TIMES ON TAXI-ALL OK. PASSING 19K ENG 2 FLAMED OUT. RAN CHECKLIST,RECYCLED PUMP SWITCHES, RESTARTESDR FDEA201006252146Skin · gougedEXISTING GOUGE IN FUSELAGE SKIN ADJACENT TO NOSE JACK POINT ALIGNMENT HOLE REPAIRED IAW EA 8-5330-123164.SDR FDEA201004291395Skin · wornRT WING L/E DROOPED EXT FOUND DEEP WEAR ON SKIN. REPAIRED AREA IAW SRM 57-10-00, VOL I, FIG 39.SDR FDEA201002180448Skin · wornLT WING L/E DEEP WEARS & 4 EA FASTENERS U/S ON LOWER SKIN. REPAIRED AREA IAW EA 8-5710-137482 & SRM 57-10-00 FIG 83, VOL I.SDR FDEA201002150426Skin · crackedLT WING INBD FLAP UPPER SURFACE FOUND CRACK ON SKIN. REPAIRED SKIN IAW SRM 57-10-00, FIG 85, SHT 2 & 4 VOL I.SDR FDEA201002120402Skin · wornLT WING, SLAT NR 2 FOUND DEEP WEAR ON LOWER SKIN. REPAIRED SKIN IAW SRM 57-10-00, FIG 31, VOL I.SDR FDEA201001130100Skin · damagedMAIN CABIN LOCATED AND DRILLED OUT GATELINK ANTENNA DOUBLER IN WRONG POSITION, BTWN LONG NR 2 RT & LONG NR 3 RT IN LIEU OF LONG NR 3 RT & LONG NR 4 RT REF DWG 72749-504. REPAIRED AREA IAW SRM 53-20-00 VOL I, FIG 13.SDR FDEA200912234511Stiffener · crackedAFT FUSELAGE INT FOUND CRACK ON TEE CAP VERTICAL STIFFENER. REPAIRED AREA IAW SRM 53-00-01, FIG 19, VOL I.SDR FDEA200912234509Skin · corrodedDURING INSP LT WING LWR SURFACE FOUND SUSPECT CORROSION UNDER SKIN OF OTBD AILERON AND AROUND HEADS OF FASTENERS. REPAIRED AREA IAW SRM 57-10-00, FIG 85, SHT 3, VOL I.SDR FDEA200912234508Support Angle · crackedDURING INSP, AFT FUSELAGE UPPER ATTIC AREA FOUND CRACK ON ANGLE SUPPORT. REPAIRED AREA IAW SRM 53-30-00 FIG 2B VOL I.SDR FDEA200912234507Bulkhead · dentedDURING INSP AFT FUSELAGE EXT FOUND DEEP NICK ON BULKHEAD SKIN LOWER SIDE. REPAIRED AREA IAW SRM 53-00-01, FIG 10 & SRM 51-00-01, FIG 100, VOL I.SDR FDEA200912224494Frame · wornMAIN CABIN DEFORMATION AND WEAR ON FRAME. REPAIRED AREA IAW SRM 53-30-00, FIG 4, VOL I.SDR FDEA200912044355Frame · crackedLT AIR CONDITIONING COMPT FOUND CRACK ON FRAME. REPAIRED FRAME IAW SRM 53-30-00, FIG 4, VOL I.SDR FDEA200912034338Membrane · crackedCOCKPIT FLOOR STRUCTURE HAVE BEEN FOUND CRACK ON MEMBRANE AND ON STIFFENERS. REPAIRED MEMBRANE IAW SRM 53-00-01 FIG 4 SHT 2 VOL I.SDR FDEA200911234121Channel · corrodedFWD CARGO COMPT DURING MOD, REMOVED PART FOUND 6 EA MODERATELY CORRODED CHANNELS UNDER SHOE BRAKES. REPAIRED AREA IAW SRM 53-70-00 FIG 7, SHT 5, VOL I.SDR FDEA200911234120Channel · corrodedFWD CARGO COMPT DURING MOD REMOVED ACTION FOUND MODERATE CORROSION UNDER THE SHOE BRAKE CHANNEL. REPAIRED AREA IAW SRM 53-70-00, FIG 7, SHT 5, VOL I.SDR FDEA200911043841Skin · crackedDURING INSP OF HORIZ STABILIZER, FOUND SKIN PANEL PLANKS CRACKED. IAW EO NR 8-5510-7-2307 PT1, SECT. C, STEP 1 AND 2 VERIFY APPLICABILITY OF EO NR 8-5510-7-4308 PT 2. REPAIRED AREA IAW EA 8-5510-133464 & EA 8-5510-133465.SDR FDEA200911033801Support · corrodedAFT CARGO COMPT, SEVERE CORROSION WITH EXFOLIATION ON SUPPORT. REPAIRED AREA IAW SRM 53-70-00 FIG 13 SHT 1 VOL I.
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