N394FE, cancelled Mar 2, 2024
Service difficulty reports · 99
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 = 'N394FE' AND deregistration_id = 'N394FE-2024-03-02' 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 = 'N394FE' AND deregistration_id = 'N394FE-2024-03-02' 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 FDEA2020031760571Control Unit · malfunctionedPDIS 394 27-50 4766 15MAR20 MEM FACT U LOGPAGES:3200325 DECLARED EMERGENCY. UNRESPONSIVE FLAPS. UNABLE TO SELECT FLAPS BEYOND SLATS EXTENDED. USED DIAL-A-FLAP TO SELECT FLAPS 22 LANDING. PULLED CVR CB AND FLIGHT RECORDER CB PART 15MAR20 16:3SDR FDEA2020031760570Unknown · malfunctionedPDIS 394 27-50 4765 15MAR20 MEM FACT U DURING APPROACH REQUESTED "FLAPS 15", FO TRIED SELECTING FLAPS 15 UNSUCCESSFULLY. WE USED THE DIAL-A-FLAP TO SELECT FLAPS 22. SUSPECT JAMMED FLAPS. SHGN 15MAR20 21:36 MEM U WHILE TROUBELSHOOTING FLAPSSDR FDEA201910312811Skin · crackedLH WING OUTBOARD FLAP UPPER SURFACE SKIN HAS TWO CRACKS LOCATED AT THE INBOARD HINGE AREA 0000608631 : F - 01-NOV-2019 01:12 REPAIRED REF MD10 SRM 57-10-00 TRACKING EA 8-5750-T0350557 PART 1SDR FDEA201906301440Warning System · false activationAFTER LANDING ROLLOUT, THE LEVEL 1 BRAKE DIFF TEMP ALERTED, FOLLOWED BY THE LEVEL II (2) BRAKE OVERHEAT. BRAKES 5 & 6 PEAKED AT APPROX 600, BRAKES 1 & 2 PEAKED AT JUST BELOW 500. BRAKES 3-4, 7 & 8 NEVER EXCEEDED 200. MINIMAL BRAKING WAS USED FROM LANDING ROLLOSDR FDEA201812183534Probe · out of limitsPDIS 394 28-40 3649 18DEC18 BNA OPEN U LOGPAGES:2876587 NR 2 FUEL QUANTITY DECREASED DISPROPORTIONATELY WITH NR 1 & NR 3 TANKS. POSSIBLE FUEL LEAK, OR SENSOR MALF (PREVIOUS WRITE UP). FACT 23DEC18 01:09 IAH ALL THE WORK DONE SERVICE WORK ORDERSDR FDEA201810172932Cap · damagedRT WING REAR UPPER SPAR AREA, APPROX XORS 402, INSIDE FUEL TANK UPPER RIB CAP HAS SMALL AREA OF DAMAGE. REPAIRED PER EA 8-5710-T0342036 PART 1.SDR FDEA201808292262Rib · damagedRIGHT WING, REAR UPPER SPAR AREA, XORS 402, INSIDE FUEL TANK UPPER RIB CAP HAD A SMALL AREA OF DAMAGE. REPAIRED IAW EA 8-5710-T0342036.SDR FDEA201807121688Repair · damagedLT I/B FLAP VANE, I/B END HAS A DAMAGED REPAIR ON TOP SKIN. REPAIRED DAMAGE ON LT I/B FLAP VANE, I/B END TOP SIDE, IAW SRM 51-71-00 VOL 2, PAR 16.SDR FDEA2018062981593Skin · damagedRT DETACHABLE ELEVATOR HAD DAMAGE ON THE TOP INBD EDGE. REMOVED AND REPLACED THE SKIN IAW SRM 55-10-00, VOL 1, FIG 7, AND SRM 51-31-01, VOL 2.SDR FDEA201805311403Spar · damagedRT WING LOWER REAR SPAR REQUIRES SR10570049-60 REPAIR. PART TO BE FABRICATED PER EA 8-5710-T034000.SDR FDEA201805311402Spar · damagedRT WING LOWER REAR SPAR REQUIRES (2) SR10570048-38 REPAIR. PART TO BE FABRICATED PER EA 8-5710-T034000. REPAIRED PER ES 8-5710-T0340000.SDR FDEA201805311401Spar · damagedRT WING LOWER REAR SPAR REQUIRES SR10570048-6 REPAIR. PART TO BE FABRICATED PER EA 8-5710-T034000. REPAIRED PER EA 8-5710-T0340000.SDR FDEA201805221371Flap System · crackedREWORK REF N/R N00460 "LH WING ATTACH FITTING FOR O/B FLAP I/B HINGE HAS A .5 IN. CRACK ON THE O/B HALF AT
THE FWD FASTENER. (MRKD)" REWORK PER QA REVIEW REJECTION. FITTING REPLACEMENT PART/MATERIAL NOT IDENTIFIED
SNRM BLOCKS 23,24,25 AND NO RDR AND SDR GENESDR FDEA201805221447Frame · corrodedCTR CARGO COMPT STA 1741 FRAME HAS CORROSION BY LONG 52. REMOVED AND REPLACED A SECTION OF CORRODED FRAME (CHANNEL) AT STA 1741 AT LONGERON 52 REF SRM 53-30-00 FIG 5 (SHEET 2) VOL I MAJOR REPAIR.SDR FDEA201804301147Fitting · corrodedRIGHT WING OTBD FLAP, OTBD HINGE, SIDE LOAD FITTING ON THE AIRCRAFT SIDE, FOUND CORRODED AT THE FASTENER HOLES. REMOVED THE CORROSION. REMOVED AND REPLACED THE SIDE LOAD FITTING IAW SRM 51-33-01, VOL II, & DWG ARB0031.SDR FDEA2018042601118Seat Track · damagedUPPER MAIN CARGO DECK LT SIDE, UNDER A BALLMAT AT BS 800, LBL 48 SEAT TRACK LOBE DAMAGED. REPAIRED THE SEAT TRACK IAW SRM 53-70-00, FIG 1, VOL 1.SDR FDEA2018042601113Skin · corrodedLEFT UPPER WING SKIN HAS CORROSION AT FASTENER, XORS 423. AFT OF FRONT SPAR. REPAIRED IAW EA 8-5730-T0339577-P1. REPAIR CLASSIFIED AS MINOR.SDR FDEA2018043001136Rib · crackedRIGHT WING L/E ACCESS PANEL 619DB, INSIDE UPPER RIB FLANGE IS CRACKED ABOVE PULLEY OTBD OF THE NR 10 SLAT TRACK.SDR FDEA201804231101Skin · delaminatedLEFT WING NR 3 SPOILER TOP SKIN HAS MULTIPLE AREAS OF DELAMINATION. REPAIRED IAW SRM 51-71-00, VOL II, PAR 16.SDR FDEA201804191139Shear Tie · corrodedAFT CARGO BAY, BS 1950, CORROSION ON THE FRAME SHEAR TIE BETWEEN LONGERONS 51 AND 52R. REPAIRED THE SHEAR TIE IAW SRM 53-30-00, PG 2, FIG 10, VOL 1.SDR FDEA2018062981594Skin · damagedRT DETACHABLE ELEVATOR HAD DAMAGE ON THE TOP INBD EDGE. REMOVED AND REPLACED THE SKIN IAW SRM 55-10-00, VOL I, FIG 7, SRM 51-31-01, VOL II.SDR FDEA201804111067Beam · crackedL3 DOOR, NR 1 BEAM AFT SIDE AT THE DOOR FRAME STOP WAS FOUND CRACKED. REMOVED AND REPLACED THE BEAM IAW DWG ADA 0006, AND SRM 51-31-01.SDR FDEA2018042601128Bulkhead Web · crackedBS 595 BULKHEAD, RT FWD SIDE OF WEB HAS A 1 INCH CRACK THRU FASTENER HOLE AT RBL 60, Z100.00. PERFORMED A BULKHEAD REPAIR IAW SRM 53-40-00, FIG 25 V1.SDR FDEA201804021245Spar Cap · crackedRT WING REAR SPAR LOWER CAP AT XORS 446 HAS A 2.0 INCH CRACK AT THE AFT EDGE OF TEE CAP EXTENDING THROUGH THE RADIUS AND TERMINATING 1.0 IN UP THE VERTICAL LEG. REPAIRED PER EA 8-5710-T0340000.SDR FDEA201804011123Frame · corrodedCENTER CARGO BAY BS 1741 FRAME HAS CORROSION BY LONGERON 52. REPAIRED THE CORRODED FRAMED IAW SRM 53-30-00, VOL I, PAGE 31.SDR FDEA201803280901Web · crackedNOSE LANDING GEAR WW, RT SIDE FWD OF INNER WEB, BS 495, Z-65. CRACKED FROM FASTENER HOLES. REPAIRED IAW SRM 53-30-00, FIG 6, SH 8, VOL I. MAJOR REPAIR.SDR FDEA201803271246Spar Cap · crackedRT WING REAR SPAR LOWER CAP AT XORS 421 HAS A .200 INCH CRACK PROPAGATING FWD OF A PREVIOUS TRIM OUT REPAIR AND EXTENDING INTO THE RADIUS. REPAIRED PER EA 8-5710-T0340000.SDR FDEA201803270974Skin · crackedRT WING SKIN AT THE INBOARD UPPER CORNER OF THE SLAT ANTI-ICE DUCT CUT OUT HAS A .500 INCH CRACK PROPAGATING THROUGH AN EXISTING STOP DRILL. INSTALLED A REPAIR DOUBLER PER SRM 57-10-00 FIG 103.SDR FDEA201803270791Cargo Track · damagedMAIN CARGO TRACK BS 635 RBL 27.5 DAMAGED BEYOND LIMITS. REPAIRED THE TRACK IAW SRM 53-70-00, FIG 1, VOL 1.SDR FDEA201803270790Cargo Track · gougedMAIN CARGO TRACK BS 879, RBL 8.5 GOUGED OUT OF LIMITS. REPLACED THE CARGO TRACK SRM 53-70-00, FIG 1, VOL 1.SDR FDEA201803270788Cargo Track · wornMAIN CARGO BAY, BS 859, LBL 107.25 SEAT TRACK IS WORN OUT OF LIMITS. REPAIRED SEAT TRACK IAW SRM 53-70-00, FIG 1.SDR FDEA201803261127Cap · crackedRIGHT BS 595 BULKHEAD TEE CAP VERTICAL LEG AT LONGERON 43R HAS A .100 INCH CRACK THROUGH THE LOWER FASTENER HOLE. PERFORMED A TEE CAP REPAIR IAW DWG SR10530064.SDR FDEA201803261112Cap · crackedLEFT BS 595 BULKHEAD TEE CAP VERTICAL LEG AT LONGERON 41L HAS A 1 INCH CRACK THROUGH THE LOWER FASTENER HOLE. REPAIIRED THE TEE CAP IAW EA 8- 5310-T0339305 P1/P2. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201803160722Sensor · out of adjustAFTER SELECTING FLAPS 35 ON FINAL AT ORD GOT SLAT DISAGREE ALERT. DUE TO TIME LAG BETWEEN SELECTING FINAL FLAPS AND ALERT ELECTED, A SECOND APPROACH IN NORMAL CONFIGURATION. NO DISAGREE, BUT SUSPECT LIMIT INDICATORS ARE OUT OF ADJUSTMENT. FOUND R2B SLAT SDR FDEA201708152224Lever · bindingR1 ARMING LEVER VERY DIFFICULT TO MOVE, FEELS LIKE CABLE IS STRETCHING RATHER THAN PARTS ARE MOVING.SDR FDEA201708052122Wire Harness · damagedDURING CLIMBOUT, NOTICED THE NR 2 ENGINE EXCEEDENCE LEVEL 1 ALERT. EGT GAUGE FOR NR 2 SHOWED MAX 998. NORMAL EGT AT REDUCED POWER FOR LEVEL FLIGHT AT 7000 FT. ON ADVANCING POWER FOR CLIMB, NR 2 EGT CLIMBED RAPIDLY. PERFORMED GVI OF THE VSV FEED BACK CABLE SDR FDEA201609263369Seat Track · damagedSEAT TRACK FOUND DAMAGED BS 1388 RBL 75.25. REPAIRED IAW SRM 53-70-00.SDR FDEA201609213367Seat Track · damagedREPORTS A LOCK AT STA 1400, LOCK IN MAIN DECK CARGO IS NOT SECURE. PRIOR TO DEPARTURE, DISCOVERED SEAT TRACK DAMAGED WHERE LOCK IS LOCATED. NO DAMAGE TO LOCK WAS INDICATED. RELEASED FOR SERVICE IAW MEL: 25-57-02-A2, CATEGORY: A, EXPIRATION: 12OCT16, MEL 25-SDR FDEA201605011439Longeron · corrodedCENTER CARGO AREA LT SIDE AT BS 1781, STRINGER 43L HAS CORROSION. R & R THE LONGERON END CAP IAW SRM 51-31-01 VOL 2. FABRICATED NEW LONGERON END CAP ON T16 1202867, PN AFA3275-501 IAW SRM 53-15-01 PG 8B & 9 VOL 3. MAJOR REPAIR.SDR FDEA201605011438Skin · corrodedTOP SURFACE OF CTR WING TANK AT STATION 1224, LBL 90 - 105 HAS CORROSION. REMOVED CORROSION IAW SRM 51-21-01 VOL II FOUND TO BE OUT OF LIMITS IAW SRM 57-20-00 FIG 8A VOL I. INSPECTED AREA IAW NTSPM 06-10-01 & 06-00-03. NO DISCREPANCIES NOTED. COMPLIED WITHSDR FDEA201605011437Skin · corrodedCENTER WING UPPER SKIN AT STATION 1297, LBL 84 HAS CORROSION. REMOVED CORROSION IAW SRM 51-21-01 VOL 2, FOUND TO BE OUT OF LIMITS IAW SRM 57-20-00 FIG 8A VOL 1. INSPECTED AREA IAW NTSPM 06-10-01 & 06-00-03. NO DISCREPANCIES NOTED. COMPLIED WITH EA 8-5730-TSDR FDEA201604281424Skin · corrodedCENTER WING UPPER SKIN AT 1298, LBL 95, HAS CORROSION. REMOVED 6 EACH FASTENERS IAW SRM 51-30-01, VOL 2. REMOVED CORROSION IAW SRM 51-21-01 VOL 2. CHECKED LIMITS, ORIGINAL MATERIAL = .220, REMAINING MATERIAL = .182. FOUND OUT OF LIMITS IAW SRM 57-20-00 FIGSDR FDEA201604281423Skin · dentedTWO EACH DENTS ON UPPER FUSELAGE, EXTERNAL SURFACE AT FS 401, CLOSE TO L1 DOOR. COMPLIED WITH EA. 8-5330-T0324851 PT 1, DENTS AT FS 401 FWD OF L1 DOOR. APPLIED DENT DOT IAW GMM 06-3-101.SDR FDEA201604271389Floorbeam · crackedFLOORBEAM CRACKED AT STATION 1801, LBL 54 AT AFT CARGO DOOR CUT OUT. REPAIRED FLOORBEAM IAW SRM 53-60-01 FIG 3 VOL 1. MAJOR REPAIR.SDR FDEA201604211331Floor Panel · damagedMAIN DECK AREA STATION 775, BL 0 FLOOR PANEL PUNCTURE. FABRICATED REPLACEMENT PANEL ON T16 1202347 IAW DWG SRZ-25-005. R & R FLOOR PANEL IAW 53-21-08-04, MAJOR REPAIR.SDR FDEA201604151231Seat Track · gougedGOUGES & MINOR DAMAGES ON SEAT TRACK SCALLOPS AT MAIN DECK CARGO COMPARTMENT, LBL 8.5 LT, BETWEEN FS 1521 & 1621. R & R SEAT TRACK AT LBL 8.5, FROM STATION 1531 - 1631, IAW SRM 51-01-01 VOL II, ON MAIN DECK CARGO, MAJOR REPAIR.SDR FDEA201604131203Floorbeam · crackedFLOORBEAM AT STATION 1821, HAS A CRACK AT LBL 54, INBD OF AFT CARGO DOOR CUT OUT. REPAIRED FLOORBEAM AT STATION 1821, LBL 54 IAW SRM 53-60-01 FIG 3 VOL 1 MAJOR REPAIR.SDR FDEA201604101182Strap · defectiveBOTH THE CAPTAIN & FIRST OFFICER ESCAPE STRAPS DO NOT REACH THE GND, AS REQUIRED BY STEPS 2 B 3 & 3 B 3 OF WC 25C6503. R & R CAPTAINS & FIRST OFFICERS ESCAPE STRAPS. OPERATIONS CHECKED GOOD IAW AMM 25-60-01-2.SDR FDEA201512294101Light · inoperativeR1 DOOR PNEUMATIC PSI TEST FAILED. RELAMPED WITH CORRECT LIGHT BULBS. OPERATIONS CHECKED NORMAL IAW AMM 25-61-03-5-0.SDR FDEA201502240591Switch · intermittentLEFT ENTRY DOOR FAILS TO MOVE UP OR DOWN, STUCK IN MID POSITION. DOOR SWITCH INTERMITTENT INTERIOR & EXTERIOR. REPLACED OPEN/CLOSE SOLENOID. ADJUST AND TEST CHECKS GOOD. IAW AMM 52-11-00-5 & 52-11-13-2.
Back to N394FE, cancelled Mar 2, 2024