N480FE, cancelled Dec 18, 2013
Service difficulty reports · 45
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 = 'N480FE' AND deregistration_id = 'N480FE-2013-12-18' 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 = 'N480FE' AND deregistration_id = 'N480FE-2013-12-18' 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 05FDEA01234Skin · damagedLOWER FUSELAGE BETWEEN STRINGER 27R AND 28R, STA 1065 TO 1074. EVALUATED REPAIR, FOUND TO END ON A STRINGER AND THEREFORE A CAT-B REPAIR. REMOVED DOUBLER IAW SRM 51-30-2. FABRICATED NEW DOUBLER IAW SRM 53-30-3. LOCATED & DRILLED DOUBLER REPAIR IAW 51-30-5.SDR 05FDEA00579Pad · corrodedPITTING AND CORROSION ON AFT MOUNTING PAD ON RT WING FOR NR 6 FLAP TRACK. REMOVED CORROSION IAW SRM 51-10-6 PG 5 FIG 4, FOUND TO BE WITHIN LIMITS ORIGINAL DRWG SPECS IAW DWG 66-14734. TREATED & PRIMED IAW SRM 51-10-2, ORIGINAL MAT THICKNESS .600, REMOVED .00SDR 05FDEA00196Floorbeam · corrodedMCD, STA 480, RBL 24.50 TO BL 0.00, FLOORBEAM HAS CORROSION. REMOVED CORROSION IAW SRM 53-10-1 FIG 4, PAGE 19, ORIG MATERIAL .140 AFTER REWORK .085 FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED AREA IAW SRM 53-10-8. MATERIAL ID AS BAC 1518-338 7075-T6 511 FABBSDR 05FDEA00146Floorbeam · corrodedSTA 340, FLOORBEAM HAS DENT & CORROSION IN DIFFERENT AREAS. REMOVED DAMAGED AREA & REPAIR PARTS IAW SRM 51-30-2. FABRICATED NEW T-CAP FROM 60- 893/18 BATCH 833835 & REPAIR SPLICES FROM 60-3408/18 BATCH 812526 & 7075-T6 .063C BATCH 784273 IAW SR 27-53-007. SDR 05FDEA00145Bracket · crackedLEFT WING L/E, LOWER SURFACE SUPPORT BRACKET IS CRACKED AT WS 165 (INBOARD OF NR 3 K-FLAP ACTUATOR). REMOVED BRACKET IAW SRM 51-30-2. FABRICATED NEW BRACKET FROM 2024-T3 .050 BATCH 0000837762 IAW SRM 51-10-1. INSTALLED NEW BRACKET IAW SRM 51-30-2.SDR 04FDEA00376Cable · damagedRED DOORS WARNING LIGHT ILLUMINATED ON GEAR RETRACTION S/O'S PANEL. NOSE GEAR DOOR LIGHT ALSO ILLUMINATED AFTER FOLLOWING QRH PROCEDURES. THE LIGHTS REMAINED ILLUMINATED. RETURN TO MEM. REMOVED AND REPLACED BOTH DOOR CABLE, ADJ AND RIGGED NOSE GEAR FWD DOOSDR 03FDEA00336Switch · failedMAIN CARGO DOOR LIGHT CAME ON INFLT . BOTH PACKS TURNED OFF . ALT 6000 FT PSI DIFF. 2.8 . LIGHT WENT OUT ONCE DEPRESS. COMPLIED WITH CHECKLIST RETURN TO MCO . OPERATED MCD OPEN/CLOSED SEVERAL TIMES. CLOSED DOOR AND PRESSURIZED A/C. WAS ABLE TO GET DOOR WARNSDR 03FDEA00121Roller · failedDURING CLIMBOUT HEARD (LOUD) BANG AS IF SOMEONE HIT AIRCRAFT WITH HAMMER. SOUND OCCURRED AGAIN ABOUT 2 MINUTES LATER (BANG) WERE SO VIOLENT IT COULD BE FELT THROUGH SEATS. AFTER LANDING FOUND UPPER AFT ROLLER CAM ASSEMBLY ON FORWARD ENTRY DOOR BROKEN. BOSDR 03FDEA00115Structure · damagedPASSING APPROX 10,000 FT MSL NOTICED CABIN VVI FLUCTUATED BETWEEN CLIMB AND DESCENT. AROUND 13,000 FT HEARD AND FELT 2 LOAD BANGS COMING FROM VICINITY OF FORWARD ENTRY DOOR. DOOR WAS DIFFICULT TO CLOSE AND OPEN. *S/D* REPAIRED L1 DOOR UPPER AFT CORNER PER SDR 02FDEA00791Frame · gougedGOUGE IN 1176 CHORD AT RBL 28, WL 208. R&R CHORD PER EA 7-5310-67046.SDR 02FDEA00793Frame · dentedBS 950C FRAME IS DENTED AT STR 25R UPPER FLANGE. R&R FRAME PER SRM 51-40-3 FIG 3 & EA 7-5310-67053.SDR 02FDEA00787Frame · dentedFRAME IS BENT AT BS 1010, LBL 30, WL 146. REPAIRED FRAME BS 1010 LBL 30 WL 146 IAW EA 7-5310-67044 AND SRM 51-40-3 FIG 1.SDR 02FDEA00779Keelbeam · corrodedCORROSION AT BS 950C=12, STR 29R. REPAIRED KEELBEAM BS 950C+12 STR 29R IAW FEDEX DWG SR 27-53-023.SDR 02FDEA00790Shear Tie · corrodedCORROSION ON SHEAR TIE AT BS 950B, STR 29R. R&R SHEAR TIE PER SRM 53-10-4 & EA 7-5310-67049.SDR 02FDEA00785Shear Tie · corrodedCORROSION ON SHEAR TIE AT BS 950B, STR 29R.SDR 02FDEA00770Frame · wornBS 1352 T-CHORD AFT FLANGE IS WORN IN SEVERAL LOCATIONS FROM 3-9 O'CLOCK AND KNIFE EDGED AT 5 O'CLOCK. R&R BS 1352 T-CHORD PER SRM 51-30-2.SDR 02FDEA00780Keelbeam · corrodedCORROSION ON KEELBEAM AT BS 950D TO 950E, STR 29 LT. REPAIRED KEEL BEAM STA 950D TO 950I STR 29L IAW FEDEX DWG SR 27-53-023.SDR 02FDEA00763Web · corrodedCORROSION ON WEB AT BS 1166, LBL 10, WL 140. R&R WEB PER SRM 53-10-1, 51-30-2, 51-20-1.SDR 02FDEA00764Web · corrodedCORROSION ON WEB AT BS 1166, RBL 10, WL 140. R&R WEB PER SRM 53-10-1, 51-30-2, 51-20-1.SDR 02FDEA00792Frame · dentedFRAME DENTED AT 970, LBL 30, STR 26L. R&R FRAME PER SRM 51-40-3 FIG & EA 7-5310-67055.SDR 02FDEA00761Frame · dentedFRAME DENTED AT STR 950F, LBL 30, STR 26L. REPAIRED FRAME IAW SRM 51-40-3 FIG 1 SHEET 3 & EA 7-5310-67056.SDR 02FDEA00762Frame · dentedFRAME IS DENTED AT BS 990, LBL 30, WL 146. R&R FRAME PER SRM 53-10-1.SDR 02FDEA00759Floorbeam · corrodedBULGE IN COCKPIT FLOOR. R&R BEAM PER SRM 51-30-2, 51-30-5, 51-30-8.SDR 02FDEA00760Skin · dentedEXTERNAL SKIN DENTED WITH TWO GOUGES AT BS 365, ABOVE STR 17L.SDR 00FDEA00394Rib · crackedDURING INSPECTION, NR 4 L/E SLAT WAS FOUND CRACKED AT INBOARD ACTUATOR ATTACH RIB. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR IAW SRM 51-40-3 & 51-30-2.SDR 00FDEA00393Rib · crackedDURING INSPECTION, NR 5 L/E SLAT WAS FOUND CRACKED AT INBOARD ACTUATOR ATTACH RIB. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR IAW SRM 51-40-3 & 51-30-2.SDR 00FDEA00392Rib · crackedDURING ROUTINE INSP, NR 5 L/E SLAT WAS FOUND CRACKED AT O/B ACTUATOR ATTACH RIB. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR IAW SRM 51-40-3 & 51-30-2.SDR 00FDEA00349Skin · crackedDURING ROUTINE INSPECTION, FUSELAGE SKIN FOUND CRACKED AT FWD ENTRY DOOR LOWER HINGE CUTOUT APPROX 0.4 INCH. REMOVED AND REPLACED PER IAW FEDEX EO 7-5330-7-2345.SDR 00FDEA00348Fitting · corrodedDURING ROUTINE INSPECTION, FITTING ON LOWER SIDE OF DOOR JAMB AREA AT BS 620 BETWEEN STR 25R AND 26R. REMOVED AND REPLACED PER IAW SRM 51-30-2.SDR 00FDEA00347Angle · crackedDURING ROUTINE INSPECTION, ANGLE FOUND CRACKED AT BS 560, FROM STR 25R IN DOOR JAMB AREA. REMOVED, FABRICATED AND INSTALLED PER IAW SRM 51-20-1 & SRM 51-30-2.SDR 00FDEA00346Fitting · corrodedDURING ROUTINE INSPECTION, FITTING ON LWR SIDE DOOR JAMB AREA AT BS 620 BETWEEN STR 25R & 26R CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING PER IAW SRM 51-30-2.SDR 00FDEA00344Skin · crackedDURING ROUTINE INSPECTION, EXTERIOR SKIN LEFT SIDE VERTICAL STABILIZER CRACKED AT FIN STA 87, WL 290. REMOVED AND REPLACED PER IAW SRM 51-40-2 & SRM 51-30-2.SDR 00FDEA00343Angle · corrodedDURING ROUTINE INSPECTION, ANGLE ON LWR SIDE OF DOOR JAMB BS 620 CORRODED BEYOND LIMITS FROM STR 27R - 28R. REMOVED AND REPLACED PER IAW SRM 51-40-4.SDR 00FDEA00342Angle · corrodedDURING ROUTINE INSPECTION, FLOOR SUPPORT ANGLE ABOVE STR 29R AT BS 642 CORRODED BEYOND LIMITS. REMOVED AND REPLACED PER IAW SRM 53-10-5 & SRM 51-40-3.SDR 00FDEA00341Skin · gougedDURING ROUTINE INSPECTION, AFT AIRSTAIR EXTERIOR SKIN FOUND GOUGED BEYOND LIMITS AT BS 1300. REMOVED AND REPLACED PER IAW SRM 52-10-2.SDR 00FDEA00340Beltframe · crackedDURING ROUTINE INSPECTION, CRACK IN FWD UPPER FLANGE BELTFRAME BS 1010 BETWEEN STR 26L AND 27L. REMOVED AND REPLACED PER IAW SRM 51-40-3.SDR 00FDEA00339Angle · corrodedDURING ROUTINE INSPECTION, FLOOR SUPPORT ABOVE STR 30 AT BS 1035 CORRODED BEYOND LIMITS. REMOVED AND REPLACED PER IAW SRM 51-40-3.SDR 00FDEA00338Floorboard · crackedDURING ROUTINE INSPECTION, CRACKS FOUND IN FLOOR WEB FWD OF BS 1183 BULKHEAD BL 0 TO LBL 45. REMOVED AND REPLACED WEB PER IAW SRM 51-20-1 AND SRM 51-30-2.SDR 00FDEA00337Floorboard · crackedDURING ROUTINE INSPECTION, CRACKS FOUND IN FLOOR WEB FWD BS 1183 BULKHEAD FROM BL 0 TO RBL 45. REMOVED, FABRICATED AND INSTALLED WEB IAW SRM 51-20-1 & 51-30-2.SDR 96FDEA01386Engine · damagedADVANCED POWER FOR TAKEOFF AND HAD LARGE AIRFRAME VIBRATION. THROTTLES RETARDED AND TAKEOFF ABORTED. EPR MADE IT AS FAR AS 1.3, BUT NOT UP TO 1.4. SUBSEQUENT POST FLIGHT INSPECTION REVEALED DAMAGE TO THE NUMBER ONE ENGINE. REMOVED AND REPLACED THE NUMBER OSDR 95FDEA01112Stringer · crackedSTR 7R CRACKED IN 2 PLACES BETWEEN STA 530 TO 540R. INSTALLED STR REPAIR AS PER SRM 53-10-3.SDR 95FDEA01111Stringer · corrodedSTR 28R IS CORRODED IN 2 PLACES BETWEEN STA 490 TO 500. REPAIRED DAMAGED AREA PER SRM 53-30-3 PG 140 AND 53-10-3 PG 1.SDR 95FDEA01110Seat Track · wornSEAT TRACK WORN STA 740 LBL 45. SPLICED IN NEW SECTION OF SEAT TRACK PER SRM 53-10-5 PG 1 TO 4.SDR 95FDEA01109Rib Chord · crackedFS 760 RT RIB CHORD UPPER VERTICAL FLANGE FWD UPPER FASTENER HOLE AND FWD LOWER FASTENER HOLE HAVE CRACKS UP AND DOWN FROM HOLES. REMOVED END OF CRACK PER 51-10-1, NFRC INSP SPOTFREE OF CRACK REMOVED, REPAIRED BY INSTALLING DOUBLER PER EO 7-5710-7-23084 PART SDR 95FDEA01108Seat Track · corrodedCORROSION TOP LT FLANGE OF NR 3 TRACK LBL 25 STA 740. THE NR 3 TRACK STA 740 IS OUT OF LIMITS 53-10-1 PG 616. REPLACED SEAT TRACK PER SRM 53-10-5.
Back to N480FE, cancelled Dec 18, 2013