N370FE, cancelled May 9, 2018
Service difficulty reports · 156
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 = 'N370FE' AND deregistration_id = 'N370FE-2018-05-09' 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 = 'N370FE' AND deregistration_id = 'N370FE-2018-05-09' 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 FDEA201609173291Former · crackedRIGHT WING L/E FORMER CRACKED AT XOS 703, LOWER END. REPAIRED L/E FORMER, WEB, ANGLE IAW SRM 57-00-01, FIG 10, VOL I. THIS REPAIR IS A CATEGORY-A,
MAJOR REPAIR.SDR FDEA201511113573Warning System · false activationWHEN CLOSING UP PRIOR TO PUSH, R1 DOOR DISARMED. LIGHT REMAINS ILLUMINATED WHEN DOOR IS ARMED.SDR FDEA201511013433Seat Track · damagedSEAT TRACK LOBE DAMAGED, INSTALLED NEW SEAT TRACK IAW SRM 53-70-00. INSTALLED FLOOR PANELS & CARGO LOADING SYS IAW AMM 53-21-08-2, ANCRA 25-50-66.SDR FDEA201507072163Combining Box · defectiveTWENTY MINUTES AFTER DEPARTURE STARTED TO NOTICE LIGHT SMOKE, HAZE & ODOR. DETERMINED SOURCE MOST LIKELY FROM HUD WITH EFVS ON. TURNED EFVS OFF & ODOR, SMOKE & HAZE STOPPED. RELEASED FOR SERVICE IAW MEL 31-61-04-01 CATEGORY C, EXPIRATION 17JUL 15. HUD SYSSDR FDEA201507032151Coalescer Bag · dirtyAT FL 380 WE ENCOUNTERED ACRID SMOKE IN THE COCKPIT. PERFORMED QRH PROCEDURE TO CLEAR SMOKE. SMOKED CLEARED AFTER 10 - 15 MINS. REPLACED OLD COALESCER BAGS WITH NEW BAGS IAW AMM 21-54-03-2. REFER TO WRI 26-12 4858 FOR FURTHER DETAILS & INSTRUCTIONS.SDR FDEA201506171915Battery · failedDURING EMER LIGHT TEST LEVEL 1, EMER BAT 1 LO. REMOVED & INSTALLED EMER LIGHTING BATTERY POWER SUPPLY. OK FOR CONTINUED SERVICE.SDR FDEA201506101744Adiru · failedNOTICED APPROXIMATELY 2000 FT DIFFERENCE BETWEEN NR 1 AND 2 MCDU DURING PROFILE DESCENT WITH F/O FLYING. SWITCHED AUTOPILOTS TO GET BACK ON PROFILE. AFTER BLOCK-IN IRU NR 2 SHOWED 14.8 DIRIFT & 15 GROUND SPEED. REPLACED THE NR 2 ADIRU, ACOMPLISHED TSDR FDEA201503211042Indicator · damagedSOCKET ASSEMBLY FOR R1, DOOR DISARM, LIGHT IS BROKEN. R & R INDICATOR ASSEMBLY IAW SMP 20-00-00. OPERATIONS NORMAL.SDR FDEA201503211041Indicator · damagedSOCKET ASSEMBLY FOR L1 DOOR DISARM LIGHT IS BROKEN. R & R LT FWD ENTRY DOOR DISARM LIGHT SOCKET ASSEMBLY IAW LMMS SM 52-11-0 S1-S2 & IPC 52-11--75-02 ITEM 420. TESTED NORMAL ON GND.SDR FDEA201502280614Charger · inoperativeEMERGENCY POWER TEST FAILED TWICE DURING PREFLIGHT. ASSOCIATED BATTERY CHARGER INOPERATIVE MINUTES LATER. REPLACED BATTERY CHARGER IAW MM 24-34-02-2-0. OPERATIONS CHECKED NORMAL.SDR FDEA201410072998Skin · chafedRIGHT OTBD FLAP VANE UPPER SURFACE OTBD OF OTBD TRACK HAS CHAFED. RT OTBD FLAP VANE UPPER SURFACE REPAIRED IAW SRM 57-53-01. EA 8-5750-T0312136 REV NO PS P1 TITLE WINGS FLIGHT SURFACES RT OTBD FLAP VANE UPPER SURFACE CHAFED RSC TRACKING ISSUED. MAJOR REPAISDR FDEA201410062991Skin · chafedRIGHT WING INBD FLAP VANE INBD UPPER SURFACE THE REPAIR DOUBLER IS CHAFED WITH PAINT OVER. REPAIRED RT WING INBD FLAP VANE UPPER SURFACE IAW SRM 57-00-01, SRM 51-71-00 & SRM 51-23-10. EA 8-5750-T0312137 REV NO PS P1 TITLE WINGS FLIGHT SURFACES RT WING INBD FSDR FDEA201410012883Panel · crackedNUMBER 1 PYLON PRE COOLER PANEL 437DR RIB STIFFENERS TOP & BOTTOM SIDES, INCLUDING FWD & AFT FLANGES, FOUND CRACKED WELDED AREAS. VERIFIED PANEL 437DR SECONDARY STRUCTURE IAW EA 8-5450-T0311730 STEP 1. WELDED RIB STIFFENERS TOP & BOTTOM SIDES & FWD & AFT FLASDR FDEA201410012882Duct · crackedPANEL 437DR, NR 1 PYLON HEAT EXCHANGE DUCT, INNER WALL CRACKED. REMOVED FASTENERS IAW SRM 51-35-01 FOR ACCESS TO WELD SUPPORT ANGLES. INSTALLED FASTENERS IAW SRM 51-35-01. WELDED NR 1 PYLON HEAT EXCHANGE DUCT ON T14 1095275 IAW EA 8-5450-T0311727 REV NR PS SDR FDEA201409302870Skin · dentedLEFT INBD ELEVATOR TE UPPER SURFACE HAS DENT. EVALUATED DENT FOUND TO BE OUT OF LIMITS IAW SRM 55-10-00 VOL 1 FIG 8 L = 2 INCHES, W = 4 INCHES. FABRICATED DOUBLER & FILLER IAW SRM 55-10-00 FIG 8 PG 15. INSTALLED FASTENERS IAW SRM 51-36-01. REPAIRED LT INBDSDR FDEA201409302867Panel · crackedNUMBER 3 ENG PYLON PANEL 487DL HAS CRACK LOWER LT CORNER OF PRE COOLER BOX, MARKED. REMOVED FASTENERS TO ACCESS CRACK IAW SRM 51-31-01. WELDED CRACK ON T14 1095277. REINSTALLED FASTENERS IAW SRM 51-31-01. ACCOMPLISHED WELD REPAIR IAW EA 8-5450-T0311731 REVSDR FDEA201409302866Panel · crackedNUMBER 3 ENG PYLON PANEL 487DL HAS CRACK FWD LOUVER RADIUS, MARKED. WELDED CRACK ON T14 1095278 ON NR 3 ENG PYLON PANEL 487DL MAT 321 DPS 10.225, AMS 5L80 ROD & ACCOMPLISHED IAW EA 8-5450-T0311732 REV NO PS P1. MINOR REPAIR.SDR FDEA201409292856Skin · damagedL1 DOOR OUTER SKIN BOTTOM FWD CORNER HAS A NOTCH CUT OUT. TEMP REPAIR, FABRICATED DOUBLER MAT 2024-T3 .071C, BATCH 2021540 IAW SRM 52-10-00 FIG 12A SHEET 1. INSTALLED DOUBLER IAW SRM 52-10-00. ACCOMPLISHED EA 8-5210-T0311872 RSC FOR TRACKING. MAJOR REPAIRSDR FDEA201409272827Doubler · damagedLEFT WING LE PANEL 518GB HAS ONE EACH ELONGATED FASTENER HOLE ON PANEL CUT OUT. R & R LT WING LE ACCESS PANEL 518GB LANDING DOUBLER WITH NEW PART. FABRICATED FROM 7075-T6, 0.090C BN 1885277 IAW 57-21-01 FIG 7 ITEM 33 & SRM 51-31-01. MAJOR REPAIR. .SDR FDEA201409242760Longeron · corrodedLOWER FWD CARGO COMPARTMENT LONGERON 52 CORRODED BETWEEN STATION 735 - 755. REPAIRED IAW SRM 53-10-00 FIG 2 SHEET 1. REMOVED CORROSION ON LONGERON & FOUND TO BE OUT OF LIMITS IAW SRM 53- 00-01 FIG 1 B. MAJOR REPAIR.SDR FDEA201409192688Floorbeam · corrodedAFT CARGO FLOORBEAM AFT FLANGE IS EXFOLIATED AT STATION 1841, PARALLEL TO LONGERON 51L. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01 FIG 1A. REPAIRED IAW SRM 53-00-01 FIG 7, MATERIAL USED 7075- T6 063 1498-200 PO 0002031082. MAJOR REPAIR.SDR FDEA201409172643Floorbeam · crackedMCD FLOORBOARD STATION 1909 - 2007, RBL 36 HAS CRACKS. FABRICATED FLOOR PANEL ON T14 1093394, BATCH 2663757 IAW SRM 51-61-01 / SRZ-25-005. MAJOR REPAIR.SDR FDEA201409142608Fitting · corrodedAFT CARGO DOOR FRAME LOWER FWD CORNER FITTING IS CORRODED. REMOVED AND REPLACED THE CORNER FITTING IAW SRM 51-31-01. ADJUSTED, SAFTIED OPS CHECKED GOOD IAW AMM 52-33-00-0. MAJOR REPAIR.SDR FDEA201408062101Light · inoperative1L DOOR LIGHT DOES NOT TEST. CHANGED BATTERIES IN L1 DOOR IAW SMP.SDR FDEA201406141450Skin · crackedDURING POST FLIGHT, FOUND A CRACK ON THE LT WING LE AT NR 4 SLAT, OTBD TRACK CUT OUT, LOWER, INBD RADIUS. HFEC INSPECTED SUSPECTED IAW NDTSPM 06-10 01 & VERIFIED THE CRACK TO BE A 3/8 - 1/2 INCH LONG. CUT OUT DAMAGED AREA IAW SRM. VERIFIED CRACK REMOVED USSDR FDEA201406141452Skin · crackedWHILE PERFORMING FCD, FOUND A CRACK ON NR 1 INBD SLAT TRACK SKIN CUT OUT LT WING. VERIFIED CRACK USING HFEC IAW NDTSPM 06-10-01. CRACK 1/2 INCH IN LENGTH. REMOVED CRACK. COMPLIED WITH HFEC INSPECTION, NO CRACKS FOUND. REPAIRED IAW EA 8-5710-F0308207. SDR FDEA201301180146Sensor · malfunctionedON GEAR RETRACTION, AFTER TAKEOFF, RT MAIN GEAR DID NOT INDICATE UP AND LOCK ON BOTH THE PRIMARY AND SECONDARY INDICATORS. ON TOUCHDOWN, IT FEELS LIKE RT GEAR BOTTOMS OUT AS THE AIRPLANE SETTLES TO THE RUNWAY. CHECK WIRES IAW WDM 32-61-01, 32-61-03 AND TROUSDR FDEA201301170125Sensor · inoperativeWITH THE LANDING GEAR HANDLE UP, THE RT GEAR INDICATION NOT UP AND LOCK IN BOTH THE PRIMARY AND SECNDARY INDICATORS. (LIGHT RED) PERFORMED VISUAL INSP OF RT MLG UPLOCK PROX SENSOR AND NO DEFECTS NOTED, PSEU RTS PASSES NORMALLY, CHECKED PSEU SENSOR READOUT UNSDR FDEA201206232320Fuel Control · malfunctionedFLEX PWR SET FOR 50 PERCENT, THROTTLES ADVANCED SMOOTHLY WHEN AUTOFLT SELECTED TO THE APPROPRIATE REDUCED PWR CHEVRON INDICATED SETTINGS ON THEN 1 GUAGE. THROTTLES CLAMPED NORMALLY PRIOR TO 80KTS. AFTER 80 KTS THE NR 3 ENGINE BEGAN NOTICEABLY SURGING WITH NSDR FDEA201108023064Door · inoperativeDOOR L1 HAD NO POWER TO CLOSE AT CLOSEUP AND PUSHBACK. DOOR OPS CHECKED GOOD IAW MM 52-10-01-2-0.SDR FDEA201108023063Lens · missingDURING SERVICE CHECK, FOUND L1 DOOR INSIDE FWD UPPER EMERGENCY LIGHT LENS COVER MISSING. INSTALLED NEW L1 DOOR INSIDE FWD UPPER EMERGENCY LIGHT LENS COVER IAW STANDARD PRACTICE.SDR FDEA201106152255Engine · malfunctionedRTO BELOW 80 KNOTS FOR LVL 1 ENG 2 EXCEEDANCE ALERT. MAX N2 101.1. PREVIEWED QRH FOR LVL1 AND RTO. ADVISED MX. RETURNED TO GATE. COMPLIED WITH VISUAL INSP OF NR 2 ENG EXHAUST AREA IAW AMM 72-00-00-6, NO DAMAGE NOTED. INSPECTED WHEELS TIRES BRAKES AND MLG DSDR FDEA201104261632Connector · corrodedWE RECEIVED AN ENG 2 OIL FILTER, LEVEL 2 ALERT. FOLLOWING QRH ENG 2 WAS SHUTDOWN. REMOVED AND REPLACED THE SCAVANGE AND MAIN LUBE OIL FILTERS, NO CONTAMINATION WAS FOUND REF. AMM MD10-79-20-02 AND 79-20-01, LEAK CHECK WAS GOOD. COMPLETED A 5 MINUTES GROUSDR FDEA201011234466Cable · bentSTARTED T/O ROLL NR 2 THROTTLE WAS SLOW TO ACHIEVE TAKEOFF POWER. AFTER ACHIEVING TAKEOFF POWER NR 2, N1 ROLLED BACK TO 10 O'CLOCK ON THE GAUGE AND ENGINE FAIL CAME ON AROUND 90 KTS. REMOVED AND REPLACED NR 2 ENGINE VSV FEEDBACK CABLE PER MM 75-31-01-2. REMSDR FDEA201011204432Mec · failedON TAKEOFF, NR 2 ENGINE DID NOT REACH T/O, N1 WITH THROTTLE ALIGNED WITH NR1 AND NR3. THROTTLE WAS MOVED SLIGHTLY FWD MANUALLY, AND N1 ROLLED BACK. ENGINE FAIL LIGHT ILLUMINATED, TAKEOFF REJECTED AT 85KTS. INSTALLED FUEL PUMP/MEC IAW MM 73-20-01-2. PERFOMESDR FDEA201010254166Floor Panel · puncturedAFT CARGO PIT FLOOR PANEL LT SIDE AT STA 1841 IS PUNCTURED. FABRICATED NEW FLOOR PANEL IAW DWG SRZ25-005, REV "H" AND DWG SRZ 25-011, REV "C". REMOVED AND RE-INSTALLED FLOOR PANEL IAW SRM 51- 31-01, VOL II.SDR FDEA201010214165Channel · corrodedCTR CARGO COMPARTMENT AT BS 1521, LBL 56, CHANNEL IS CORRODED. FABRICATED REPAIR ANGLES IAW SRM 53-00-01, FIG 9, VOL I. FABRICATED "J" CHANNEL IAW DAC DWG 2929469. ALODINED AND PRIMED REPAIR PARTS IAW SRM 51-21-01, VOL II. INSTALLED REPAIR PARTS IAW SRM SDR FDEA201010134043Floor Panel · crackedFWD CARGO PIT FLOOR PANEL 127 UF IS CRACKED. (BS. 791 - 2ND INBD) FABRICATED FLOOR PANEL 127 UF IAW SRZ 25-005, REV H. INSTALLED FLOOR PANEL 127 UF IAW SRM 51-31-01, VOL II.SDR FDEA201010124016Skin · dentedRT EXTERIOR FUSELAGE SKIN PRIMARY STATIC PORT CONTROLLED AREA HAS 5 EA DENTS. REPAIRED RT PRIMARY STATIC PORT CONTROLLED AREA DENTS, 5 EACH IAW EA 8-5330-123564, REV "IR" 10-1-10, ALL DENTS FOUND TO BE WITHIN LIMITS EA 8-5330-123564, REV "IR" 10-1- 10, ANDSDR FDEA201010073970Intercostal · corrodedCENTER CARGO COMPARTMENT BILGE AREA INTERCOSTAL IS CORRODED AT BS 1724; RBL 3. REMOVED ROLLER TRAY TO F.O.M. IAW MD/DC10 SRM 51-31-01, VOL II. REMOVED VHF ANTENNA TO F.O.M. REMOVED INTERCOSTAL TO F.O.M. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. ORSDR FDEA201010073969Tube · crackedNR1 ENG LT THRUST REVERSER GREEN COOLING TUBE IS CRACKED. R & R NR1 ENG LT THRUST REVERSER COOLING TUBE IAW AMM70-00-00; AMM 78-32-14; 70-32-01; SRM 51-21-01 AND SRM 51-41-01.SDR FDEA201010013853Floorboard · puncturedAFT PIT FLOOR BOARD 187 HF HAS SEVERAL PUNCTURES. FABRICATED NEW AFT PIT FLOORBOARD 187 HF IAW DWG SRZ 25-005, REV "H" AND SRZ 25-011, REV "C".SDR FDEA201010013852Floorboard · puncturedAFT PIT FLOORBOARD 187 GF HAS SEVERAL PUNCTURES. FABRICATED NEW AFT PIT FLOORBOARD PANEL 187 GF IAW DWG SRZ 25-005, REV "H" AND SRZ 25-011, REV "C".SDR FDEA201009303817Longeron · crackedFWD CARGO BAY LONGERON 52 BETWEEN STA 859 AND STA 755 HAS A CRACKED FASTENER HOLE. FABRICATED NEW LONGERON IAW DWG ADA 3064 AND SRM 51-10-02, FIG 1, VOL III. ALODINED, PRIMED AND PAINTED LONGERON 52 IAW SRM 51-21-01, VOL II. INSTALLED LONGERON 52 IAW SRM 5SDR FDEA201009293793Failsafe · corrodedCAC FRAME FAILSAFE ANGLE IS CORRODED STA 1119; LONGERON 51 RT. FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 53-00-01, FIG 1-B, VOL II. REMOVED INTERCOSTALS AT STA 1119 TO 1099; RBL 6 AND LONGERON 51 TO F.O.M. IAW SRM 51-30-0, VOL II. MATERIAL ID FOR REPAIR FSDR FDEA201009293795Seat Track · damagedMAIN CABIN SEAT TRACK SCALLOP IS BROKEN AT BS 775 RBL 8. REMOVED AND RE-INSTALLED FLOOR BOARD PANEL LBL 0 TO RBL 27 AT STA 615 - 775. MATERIAL ID NEW SEAT TRACK 49291150-12000, PO 617966.1. INSTALLED NEW SEAT TRACK IAW SRM 53-70-00. VOL I. OK TO PRIME, SDR FDEA201009293784Floor Panel · debondedCTR ACCESSORY COMPARTMENT LT STEP IS DEBONDED. REMOVED CENTER ACCESSORY COMPARTMENT LEFT STEP IAW SRM 51-31-01, VOL II. FABRICATED CENTER ACCESSORY COMPARTMENT LEFT STEP IAW DWG SRZ 25-005, REV "H". INSTALLED NEW PANEL IAW SRM 51-31-01, VOL II.SDR FDEA201009293792Skin · gougedFWD CARGO DOOR CUTOUT, AFT SKIN DOUBLER AT APPROXIMATELY STA 999; STRINGER 40 IS GOUGED AND MISSING MATERIAL. REMOVED DOUBLER IAW MD/DC10 SRM 51-31-01, VOL II. GENERATED RFTS N370FE-28-43009 MATERIAL ID TO FABRICATED A NEW DOUBLER IS 2024-T3 0.125, PO 674SDR FDEA201009233778Wedge · corrodedRT OTBD FLAP SEC WEDGE PANEL, INBD TOP SKIN REQUIRES REPLACEMENT BECAUSE OF CORROSION. REPAIRED SKIN IAW SRM 57-10-00, FIG 7, VOL I AND SRM 51-31-01, VOL II. FABRICATED 1 EA DOUBLER IAW DWG ARC 1953, REV "J". FABRICATED -34 AND -35 TEE CAPS IAW DWG ARC 1953SDR FDEA201009233689Gusset · crackedMAIN CABIN INTERNAL FRAME GUSSET IS CRACKED BETWEEN BS 1480 AND BS 1482, STRINGER 16R - STRINGER 17R. FABRICATED NEW CHANNEL IAW DWG 88277. HEAT TREATED CHANNEL FROM 7075-0 TO 7075-T6 PER DWG AWE 7017, REV "AH" AND IAW DPS 7.0. LOCATED AND DRILLED NEW CHA
Back to N370FE, cancelled May 9, 2018