N320FE
Service difficulty reports · 183
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 = 'N320FE' 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 = 'N320FE' 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 FDEA201002030312Floor Support · corrodedAFT CARGO COMPT BILGE FOUND NR 4 HOLES ON NUTPLATE CORROSION ON ANGLE SUPPORT FLOOR PANEL. REPAIRED AREAS IAW SRM 53-00-01 FIG.9 SH.7 VOL.1SDR FDEA201002030311Skin · wornRT WING L/E SLAT DROOPED FOUND DEEP WEAR ON EXT SKIN. REPAIRED SKIN IAW SRM 57-00-01 FIG.4 VOL.1SDR FDEA201002030310Skin · dentedDURING INSP LT HOR STAB INBD ELEVATOR FOUND DEEP DENT 1.50" X 1.50" DEEP.068" ON UPPER SKIN. REPAIRED SKIN IAW SRM 55-10-00 FIG.8 VOL.1SDR FDEA201001290286Skin · crackedRT HORIZ STAB FOUND CRACK ON UPPER SKIN OF DETACHABLE ELEVATORS. REPAIRED SKIN IAW SRM 55-00-01 FIG.3 VOL1SDR FDEA201001280280Frame · corrodedAFT CARGO COMPT BILGE FOUND CORROSION ON CAP FRAME AND FRAME LONGERON. TRMIMED AND REPLACED FRAME SECTION, SPLICE IAW SRM 53-30-00 FIG.5 VOL.1 & 53-00-01 FIG.10 VOL.1 & DWG AGA7125.SDR FDEA201001270271Skin · dentedDURING INSP RT HOR STAB L/E EXT SURFACE FOUND 1 EA DEEP DENT 1" X 1" DEEP .118" ON SKIN ( REMOVED PART ). REPAIRED L/E SKIN IAW SRM 55-10-00 FIG.13 SH.1-2-3 VOL.1SDR FDEA201001250244Web · crackedMAIN CABIN R3 DOOR UPPER JAMB CRACK ON WEB. REPAIRED WEB IAW SRM 53-50-00 FIG.19 VOL1SDR FDEA201001250243Bulkhead · crackedRT MLG WHEEL WELL FOUND CRACK ON HORIZONTAL WEB. REPAIRED IAW SRM 53-00-01 FIG.10 SH.1 VOL.1SDR FDEA201001250242Cargo Track · crackedFWD CARGO COMPT FOUND CRACK ON TRACK. REPLACED TRACK SECTION, USED EXISTING SPLICES IAW SRM 53-70-00 FIG.1 SH.1 VOL.1.SDR FDEA201001250241Cargo Track · crackedFWD CARGO COMPT FOUND CRACK ON TRACK. REMOVED AND REPLACED SECTION OF TRACK IAW SRM 53-70-00 FIG.1 SH.1 VOL.1.SDR FDEA201001250240Frame · crackedRT MLG WHEEL WELL, FOUND CRACK ON FRAME. TRIMMED OUT DAMAGED SECTION OF FRAME IAW SRM 53-30-00 FIG.5 VOL.1. INSTALLED NEW SECTION OF FRAME & SPLICE IAW SRM 53-00-01 FIG.10 SH.5 VOL.1SDR FDEA201001250239Intercostal · crackedMAIN CABIN COCKPIT FOUND CRACK ON HORIZONTAL INTERCOSTAL. REPAIRED INTERCOSTAL IAW SRM 53-00-01 FIG.2 SH.2 VOL.1SDR FDEA201001250238Intercostal · crackedMAIN CABIN, COCKPIT FOUND CRACK ON HORIZONTAL INTERCOSTAL. REPAIRED INTERCOSTAL IAW SRM 53-00-01 FIG.2 SH.2 VOL.1.SDR FDEA201001250236Skin · crackedDURING INSP OF HORIZONTAL STAB CONSTANT SECTION, FOUND 2 PANELS CRACKED PN 7229-1 POS NR3 & 7226-1 POS NR18, PLEASE VERIFY APPLICABILITY & REVISION OF EO 8-5510-7-4308 IAW SECTION C. ACCOMPLISHED E.A.8-5510-133497 IAW SB DC10-55-016. REMOVED AND REPLACED SDR FDEA201001130099Web · crackedMAIN CABIN CRACK ON WEB L3 DOOR LOWER JAMB. REPAIRED CRACK IAW SRM 53-50-00 FIG.19 SH.2 VOL.1SDR FDEA201001110069Intercostal · crackedLT WING L/E FOUND CRACK ON OLD REPAIR OF INTERNAL INTERCOSTAL. REPAIRED INTERNAL INTERCOSTAL IAW SRM 57-00-01 FIG.10 SH.1 VOL.1SDR FDEA201001110076Skin · crackedRT WING L/E FOUND CRACKS ON SKIN DOUBLER UPPER INT SKIN L/E. REPAIRED BEADED DOUBLER IAW SRM 57-10-00 FIG.71 VOL.1.SDR FDEA201001110075Skin · crackedRT WING L/E FOUND CRACK ON DOUBLER UPPER INT SKIN L/E. REPAIRED DOUBLER IAW SRM 57-10-00, FIG 71, VOL I.SDR FDEA201001110074Skin · crackedRT WING L/E FOUND CRACK ON SKIN DOUBLER UPPER INT SKIN. REPAIRED DOUBLER IAW SRM 57-10-00, FIG 71, VOL I.SDR FDEA201001110073Skin · crackedRT WING L/E FOUND CRACK ON DOUBLER UPPER INT SKIN. REPAIRED DOUBLER IAW SRM 57-10-00, FIG 71, VOL I.SDR FDEA201001110072Skin · crackedRT WING L/E FOUND CRACK ON SKIN DOUBLER UPPER INT SKIN L/E. REPAIRED DOUBLER IAW SRM 57-10-00, FIG 71, VOL I.SDR FDEA201001110071Skin · crackedRT WING LWR SURFACE FOUND CRACK ON SKIN OF WING TIP. REPAIRED SKIN IAW SRM 57-00-01 FIG.4 SH.2 VOL.1SDR FDEA201001110070Skin · crackedRT WING L/E FOUND CRACK ON LWR EXT SKIN L/E. REPAIRED SKIN IAW SRM 57-10-00, FIG 68, SHT 2, VOL I.SDR FDEA201001110068Rib · crackedRT WING L/E FOUND CRACK ON INT RIB L/E. REPAIRED RIB IAW SRM 57-00-01 FIG.10 SH.1 VOL.1.SDR FDEA201001110067Strut · corrodedAFT FUSE WASTE TANK, SEVERE CORROSION ON STRUT. REPAIRED STRUT IAW SRM53-00-01 FIG.9 VOL.1SDR FDEA200912234510Beam · crackedFWD CARGO COMPT, FOUND CRACK ON BEAM. PERFORMED REPAIR ON BEAM IAW SRM 53-60-01 FIG.3 VOL.1SDR FDEA200912234506Frame · crackedDURING INSPECTION CAC INT. FOUND CRACK ON FRAME. REPAIRED FRAMES IAW SRM 53-30-00 FIG.7 VOL.1.SDR FDEA200912224498Panel · crackedLT WING L/E FOUND CRACK ON CHORD FIXED PANEL. REPAIRED L/E LOWER STRINGER IAW SRM 57-10-00 FIG.49 VOL.1.SDR FDEA200912224497Doubler · crackedLT WING L/E FOUND CRACK ON INTERNAL DOUBLER. REPAIRED DOUBLER IAW SRM 57-10-00 FIG.71 VOL.1SDR FDEA200912224496Intercostal · crackedLT WING L/E FOUND CRACK ON INTERNAL INTERCOSTAL. REPAIRED INTERCOSTAL IAW SRM 57-00-01 FIG.10 SH.1 VOL.1SDR FDEA200912224495Channel · corrodedLWR CTR CARGO COMPT, SEVERE CORROSION ON CHANNEL.SDR FDEA200911264201Skin · crackedLT WING OTBD FLAP FOUND CRACK ON UPPER SKIN. REPAIRED SKIN IAW SRM 57-00-01 FIG 4, SHT 2, VOL I.SDR FDEA200911264200Skin · crackedLT WING OTBD FLAP FOUND CRACK ON UPPER SKIN. REPAIRED SKIN IAW SRM 57-00-01 FIG 4, SHT 2, VOL I.SDR FDEA200911264199Skin · dentedLT WING OTBD FLAP LWR SKIN FOUND MANY DEEP NICKS. REPAIRED SKIN IAW SRM 57-10-00, FIG 85, VOL I.SDR FDEA200911173995Skin · dentedEXT FUSELAGE LWR SURFACE FOUND 1 EA DENT ON SKIN 1"X 1" DEEP 0.060". PERFORMED HFEC INSPECTION IAW NDTSPM 06, NO CRACK FOUND. INSTALLED FINGER DOUBLER IAW SRM 53-20-00 FIG.13 SH.2 & SH.5 VOL.1.SDR 07FDEA04624Seat Track · gougedMAIN CARGO COMPT SEAT TRACK HAS GOUGED AREAS AT F/S 615-635 RBL 48. REMOVED AND REPLACED SEAT TRACK IAW SRM 53-70-00 VOL 1 FIG 1.SDR 07FDEA04623Seat Track · gougedMAIN CARGO COMPT SEAT TRACK HAS GOUGED AREAS AT F/S 615-635 RBL 8. REMOVED AND REPLACED SEAT TRACK IAW SRM 53-70-00 VOL 1 FIG 5.SDR 07FDEA04622Seat Track · gougedMAIN CARGO COMPT SEAT TRACK HAS GOUGED AREAS AT F/S 735-755 LBL 8. REMOVED AND REPLACED SEAT TRACK IAW SRM 53-70-00 VOL 1 FIG 1 SHEET 4.SDR 07FDEA02832Motor · burnedUPON TAKING RUNWAY, FUMES NOTICED IN THE COCKPIT. TAXIED CLEAR BACK TO THE RAMP. FUMES INCREASED, DECLARED EMERGENCY, EVACUATED THE AIRCRAFT. UPON FURTHER INSPECTION, FOUND S/O'S SEAT CONTROL C/B POPPED, AND STRONG ODOR FROM SEAT MOTOR. UPON FURTHER INSPECSDR 06FDEA1446Engine · damagedNR 2 ENG S/N 530393, RT LPT CASE 3 O'CLOCK POSITION BURN THRU HOLE APPROX .500" DIAMETER, AND HEAT DISTRESS AROUND LPT TURBINE CASE. REMOVED AND REPLACED NR 2 ENG PER FEDEX W/C 71T1101, W/C 71T1701 AND N/R 563.SDR 05FDEA00885Sensor · faultySLAT DISAGREE LIGHT ILLUMINATED WITH FLAP EXTENSION FROM 22 TO 35 AND REMAINED ON. PERFORMED RED TABS. LANDED WITH 22/EXT CONFIGURATION. ACCOMPLISHED DETAILED VISUAL INSPECTION OF THE SLAT CABLES BOTH LEFT AND RIGHT WING, PERFORMED PCU BITE TEST ALL CHANNELSDR 04FDEA03171Skin · canningRIGHT INBOARD FLAP INBOARD AFT SEGMENT UPPER SURFACE HAS A LARGE SKIN SECTION OIL CANNING. REPLACED SKIN PNL ASSY IAW DC-10 SRM 51-31-01 AT MAE ON N/R N01147.SDR 04FDEA03050Door Frame · gougedFUSELAGE CORROSION/GOUGES ON MAIN CARGO DOOR FRAME. COMPLIED WITH EA 8-5310-82067. FUSELAGE CORROSION GOUGES ON MAIN CARGO DOOR FRAME.SDR 04FDEA03004Seat Track · corrodedMAIN CARGO DECK SHORT SEAT TRACK FITTING IS CORRODED AT RBL 89 STA 1821 TO 1853. REMOVED CORROSION IAW SRM 53-70-00 VOL 1, FOUND TO BE OUT OF LIMITS IAW SRM 53-70-00. REMOVED FLOOR PANELS IAW M/M 53-21-04-2. REMOVED DAMAGED TRACK IAW SRM 51-31-01. NEW SEATSDR 03FDEA00601Hinge · corrodedNR S 32 C/W E.A.8-5740-68784. RT I/B FLAP HINGE ASSY CORROSION REWORK. CLOSING ACTION ON 04/18/03. COMPLIED WITH E.A.8-5740-68784. RT I/B FLAP HINGE ASSY CORROSION REWORK.SDR 03FDEA00600Hinge · corrodedNR S 31 C/W E.A.8-5740-68783-L/H I/B FLAP HINGE ASSY CORROSION REWORK. CLOSING ACTION .COMPLIED WITH E.A.8-5740-68783. ON 04/18/03.SDR 03FDEA00566Bracket · wornNR S-27 COMPLY WITH EA8-5331-68781 FUSELAGE-WING TO BODY FILLET- ATTACH BRACKET WEAR REPAIR P/N ANB7245. COMPLIED WITH EA8-5331-68781 FUSELAGE-WING TO BODY FILLET- ATTACH BRACKET WEAR REPAIR P/N ANB7245.SDR 03FDEA00568Finger Doubler · corrodedMAIN DECK UNDER F/R STRUCTURE STA 515 TO 535 LBL 8.5 TO RBL 8.5 FINGER DOUBLER CORRODED AND FASTENER HEADS CORRODED AND BROKEN OFF. CLOSING ACTION ON 04/20/03. REMOVED AND REPLACED FINGER DOUBLER IAW SRM 53-12-01 AND SRM 51-31-01. FAB NEW DOUBLER IAW SRM 53SDR 03FDEA00569Seat Track · corrodedMAIN CARGO DECK SEAT TRACK STA 675 TO 735 RBL 75 AT TRACK FLANGE CLIP NUT HOLES TOP AND BOTTOM CORRODED. CLOSING ACTION ON 04/14/03. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-70-00. REMOVED AND REINSTALLED NEW SEAT TRACK IAW SRM 51-31-01, FABSDR 03FDEA00570Support · crackedRIGHT O/B FLAP I/B HINGE FAIRING SUPPORT STRUCTURE CRACKED LWR AFT END OF HINGE. CLOSING ACTION ON 04/15/03. REMOVED SUPPORT STRUCTURE IAW SRM 51-31-01, FOUND -T- ANGLE CRACKED. REMOVED -T- ANGLE IAW SRM 51-31-01. SENT TO FAB, FAB SUPPORT AND -T- ANGLE O
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