N689FE
Service difficulty reports · 96
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 = 'N689FE' 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 = 'N689FE' 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 FDEA201511173668Floor Panel · crackedFLOORBOARD PANEL 241 LK HAS CRACKED. FABRICATED NEW PANEL ON T15 1172117 IAW DWG SRZ 25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.SDR FDEA201511173667Floor Panel · delaminatedMAIN DECK CARGO FLOOR PANEL 242 PF HAS DELAMINATED ON LT FWD EDGE CORNER. FABRICATED NEW PANEL ON T15 1172149 IAW DWG SRZ 25-005 REV L, CLASSIFIED AS MAJOR CAT A REPAIR.SDR FDEA201511173666Floor Panel · damagedFLOORBOARD PANEL 241 AJ HAS ELONGATED MOUNTING HOLE. FABRICATED NEW PANEL ON T15 1172144 IAW DWG SRZ 25-005 REV L CLASSIFIED AS MAJOR CAT A REPAIR.SDR FDEA201511173665Floor Panel · damagedFLOORBOARD PANEL 242QJ HAS PUNCTURED HOLE. FABRICATED NEW PANEL ON T15 1172048 IAW DWG SRZ 25-005 REV L. THIS REPAIR IS CLASSIFIED AS A CATEGORY A MAJOR REPAIR.SDR FDEA201511173664Floor Panel · damagedPANEL 242ZJ HAS A CUT, APPROX .5 INCHES. FABRICATED NEW PANEL ON T15 1172055 IAW DWG SRZ 25-005 REV L. REPAIR IS CLASSIFIED AS A CATEGORY A MAJOR REPAIR.SDR FDEA201511173663Floor Panel · damagedMAIN DECK FLOOR PANEL 251GF DAMAGED. FABRICATED NEW PANEL ON T15 1172147 IAW DWG SRZ 25-005 REV L. THIS REPAIR IS CLASSIFIED AS A CATEGORY A MAJOR REPAIR.SDR FDEA201511163652Floor Panel · delaminatedMAIN DECK FLOOR PANEL 251 HH IS DELAMINATED. FABRICATED NEW PANEL ON T15 1172064 IAW DWG SRZ 25-05 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.SDR FDEA201511163651Floor Panel · delaminatedMAIN DECK FLOOR PANEL 251 BH IS BROKEN. FABRICATED NEW PANEL ON T15 1172119 IAW DWG SRZ 25-05 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.SDR FDEA201511163650Floor Panel · delaminatedMAIN DECK FLOOR PANEL 252 BH, AFT, IS BROKEN DOT 135-5. FABRICATED NEW PANEL ON T15 1172116 IAW DWG SRZ 25-05 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.SDR FDEA201511143620Intercostal · crackedMDC FRAME 48, Y 0 TO -Y450, HAS CRACKED ON INTERCOSTAL. REMOVED INTERCOSTAL AT FRAME 48, BETWEEN 0 TO -Y450 IAW SRM 51-40-21. FABRICATED NEW INTERCOSTAL ON T15 1171512. INSTALLED NEW INTERCOSTAL AT FRAME 48, BETWEEN 0 TO -Y450 IAW SRM 51-40-21, MAJOR REPAIRSDR FDEA201511143614Intercostal · bentMDC FRAME 49 FROM Y 0 TO - Y450 HAS BENT INTERCOSTAL FEATURE. REMOVED INTERCOSTAL AT FRAME 49, BETWEEN 0 - TO -Y450 IAW SRM 51-40-21. FABRICATED NEW INTERCOSTAL ON T15 1171519. INSTALLED NEW INTERCOSTAL AT FRAME 49, BETWEEN 0 TO -Y450 IAW SRM 51-40-21, MAJOSDR FDEA201511143610Floor Support · corrodedMAIN DECK FLOOR SUPPORT BEAM, UPPER SURFACE HAS CORROSION AT FRAME 12, Y450. REMOVED DAMAGE IAW SRM 51-74-10 & CHECKED LIMITS, ORIGINAL MATERIAL = 0.079". REMOVED 0.20", NO ALLOWABLE DAMAGE LIMITS FOUND IN SRM TR 17450. REMOVED FLOOR SUPPORT AT FRAME 12, Y4SDR FDEA201511113558Fitting · crackedMDC FRAME 48, -Y1456 HAS CRACKED UNDER FLOOR BRACE LOWER FITTING. R & R ONE EACH FITTING AT FRAME 48, -Y1456 UNDER FLOOR LOWER BRACE IAW SRM 51-40-21. PN A5381206720001.SDR FDEA201501200231Lug · corrodedRIGHT MLG FWD LUG HAS CORROSION IN BORE & ON FWD & AFT FACES COMPLIED WITH EA T 6- 5710 T0303688 P6. TERMINATING ACTION OF RIB 5 FWD LUG RT. WINGS BASIC WING STRUCTURE. MAJOR REPAIR.SDR FDEA201501200230Lug · corrodedLEFT MLG FWD LUG HAS CORROSION IN BORE & ON FWD & AFT FACES COMPLIED WITH EA T 6- 5710 T0303688 P5. TERMINATING ACTION OF RIB 5 FWD LUG LT. WINGS BASIC WING STRUCTURE. MAJOR REPAIR.SDR FDEA201401080069Transmitter · inoperativeENROUTE AT FL370, WATCHED GREEN HYD RESERVOIR LEVEL DROP TO RED DOT. COMPLIED WITH QRH. LOSS OF GREEN SYS DID NOT REACH RED DOT IN YELLOW BAND. DURING LANDING, REPORTED THAT GREEN SYS RETURNED TO HAT BAND AREA. RAN GREEN HYD SYSTEM & OPERATED FLIGHT CONTRSDR FDEA201312152985Splice · crackedFUSELAGE FRAME 47, STRINGER 24 - 26R SPLICE FITTING FOUND CRACKED, COMPLIED WITH EO 6-5310-7-5017 P6.SDR FDEA201305070931Selector Valve · malfunctionedAT LEVEL OFF RECEIVED YELLOW HYD LOW PRESS THEN LOW QUANTITY. FOLLOWED QRH SECURED YELLOW SYSTEM AND CONTINUED TO DESTINATION. REPLACED MCD SELECTOR VALVE IAW MM 52-33-53-04. OPS AND LEAKS CHECKS NORMAL ACFT OK FOR SERVICE.SDR FDEA201109083766Skin · gougedRT INBD FLAP UPPER SURFACE APPROX 18" AFT OF L/E AND 1.5" OTBD OF RIB 6A; THERE IS A GOUGE APPROX 6 IN LONG X 2.5 INCHES WIDE AND 0.070 IN DEEP AT DEEPEST AREA. BLENDED DAMAGED AREA IAW SRM 51-73-10, CHECKED LIMITS - ORIGINAL .031, REMAINING .013, MATERIAL LSDR FDEA201109023636Skin · damagedFWD CARGO DOOR CUTOUT AT FR 20 APPROX 30" UP FROM SILL BEAM THERE IS A FIELD BLEND THAT MEASURES APPROX 1.5 IN L X .500 W X .100 IN D. REPAIRED IAW SRM 53-13-13, FIG 201-210.SDR FDEA201109013607Floorbeam · bentAFT CARGO COMPARTMENT RT SIDE FR 63 BETWEEN SEAT TRACK 4R AND 5R, UPPER FLOORBEAM IS BENT. ACCOMPLISHED REPAIR TO AFT CARGO FR C-63 DAMAGE IAW E.A. 6-5310-152428.SDR FDEA201108313602Stiffener · bentAFT CARGO UPPER CEILING AT FR 62 AT SEAT TRACK NR4 RT SIDE HAS A STIFFENER BENT. REMOVED ANGLE STIFFENER PER SRM 51-40-21 PARA 7. FABRICATED 1EA ANGLE STIFFENER PER DWG A53275446. REPROTECTED ANGLE STIFFENER PER SRM 51-21-10 AND SRM 51-75-10. LOCATED AND DSDR FDEA201108193387Floorboard · damagedFLOORBOARD 251JF HAS CORNER BROKEN OFF, FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRS 25-005, REV J.SDR FDEA201108183361Floor Panel · mismanufacturedFLOOR PANEL 2426F FABRICATED INCORRECTLY, MISSING 1 X 1.5 LEG ON END. FABRICATED PANEL 2426F IAW DWG SRZ 25-005 REV. J.SDR FDEA201108173320Floorboard · damagedMDCC FLOORBOARD 252 GF, NR2 IS BROKEN, 1 EA SECTION. FABRICATED REPLACEMENT FLOORBOARD 252, GF 2 IAW DWG SR2 25-005.SDR FDEA201108163295Floorboard · damagedMAIN CABIN CARGO ZONE 240 FLOORBOARD, 242RJ BROKEN AT CLEVIS ATTACH POINT. FABRICATED REPLACEMENT FLOORBOARD 242RJ.SDR FDEA201108123251Floorbeam · bentAFT CARGO FLOORBEAM AT FRAME 63 IS BENT, BS 4150. FABRICATED CHANNELS FOR FLOORBEAM REPAIR IAW SRM 53-10-15, FIG 207. REPAIR ACCOMPLISHED ON SNRM N00007 AND EA 6-5310-152428.SDR FDEA201108123250Floor Support · bentMAIN CARGO CABIN FRAME 48 TO FRAME 50 RT SIDE BETWEEN SEAT TRACKS 1 & 2 FLOOR SUPPORT BENT. REMOVED FLOOR SUPPORT IAW SRM 51-72-10. FABRICATED FLOOR SUPPORT IAW SRM 53-15-15 FIG.9 AND DWG A53813946. LOCATED AND DRILLED FLOOR SUPPORT . INSTALLED FLOOR SUPPORSDR FDEA201108113225Floor Panel · damagedMAIN DECK CARGO COMPARTMENT FLOOR PANEL 251BF IS BROKEN IN HALF ON BOTTOM SURFACE. FABRICATED REPLACEMENT FLOOR PANEL 251BF IAW DWG SRZ 25-005, REV J.SDR FDEA201108113224Floor Panel · damagedMAIN DECK CARGO COMPARTMENT FLOOR PANEL 242UF IS BROKEN. FABRICATED REPLACEMENT FLOOR PANEL 242UF IAW DWG SRZ 25-005, REV J.SDR FDEA201108113223Floor Panel · damagedMAIN DECK CARGO COMPARTMENT FLOOR PANEL 252DF TIP BROKEN OFF. FABRICATED REPLACEMENT FLOOR PANEL 252DF IAW DWG SRZ 25-005, REV J.SDR FDEA201108113221Floor Panel · crackedMAIN DECK CARGO COMPARTMENT FLOOR PANEL, 252GF CRACKED. FABRICATED REPLACEMENT PANEL 252GF IAW DWG SRZ 25-005, REV J.SDR FDEA201108113206Shear Plate · crackedGUSSET ON RT SIDE OF ACFT FUSELAGE FLOOR LEVEL BEHIND LOWER SIDEWALL AT FR 79, CRACKED. REMOVED SHEAR PLATE RT SIDE FLOOR LEVEL AT FR 79 IAW SRM'S 51-40-21 AND 51-72-10. LOCATED AND DRILLED NEW SHEAR PLATE IAW SRM 51-72-10. INSTALLED NEW PLATE IAW SRM'S 51-SDR FDEA201108113205Shear Plate · crackedGUSSET ON LT SIDE OF AFT FUSELAGE FLOOR LEVEL BEHIND LOWER SIDEWALL AT FR 79, CRACKED. REMOVED LT SIDE SHEAR PLATE AT FLOOR LEVEL AT FR 79 IAW SRM'S 51-40-21 AND 51-72-10. LOCATED AND DRILLED NEW SHEAR PLATE IAW SRM 51-72-10, INSTALLED NEW SHEAR PLATE IAW SDR FDEA201108103175Floor Panel · crackedFLOOR PANEL 242BF IS BROKEN IN HALF. FABRICATED REPLACEMENT FLOOR PANEL 242BF IAW DWG SRZ 25-005 REV. J.SDR FDEA201108103174Floor Panel · brokenFLOOR PANEL 242KF IS BROKEN IN HALF. FABRCATED REPLACEMENT PANEL 242KF IAW DWG SR2 25-005.SDR FDEA201108103176Floor Panel · crackedFLOOR PANEL 242GF HAS 1EA 9" CRACK ON BOTTOM SURFACE. FABRICATED REPLACEMENT FLOOR PANEL 242GF IAW DWG SRZ 25-005, REV. J.SDR FDEA201108093153Floor Panel · crackedFLOOR PANEL, 242SF, HAS 3 EA, 2" CRACKS ON BOTTOM SURFACE. FABRICATED REPLACEMENT PANEL 242SF IAW DWG SRZ-25-005, REV J AND IDENTIFIED REPLACEMENT PANEL 242SF IAW GMM 7-0-1001.SDR FDEA201108093151Floor Panel · damagedFLOOR PANEL 143DF IS OIL SOAKED. FABRICATED REPLACEMENT PANEL 143DF IAW DWG SRZ-25-005, REV J. IDENTIFIED REPLACEMENT PANEL IAW GMM 7-0-1001.SDR FDEA200912094394Smoke Detector · inoperativeWHEN LANDING GEAR WAS LOWERED AVIONICS SMOKE WARNING CAME ON - THERE WERE NO OTHER INDICATIONS OF SMOKE - WARNING WENT ON/OFF EVERY 5 SECONDS -AFTER LANDING AND TAXI - IN MECHANICS AND FIRE RESCUE FOUND NO EVIDENCE OF SMOKE - ALL WARINGS CEASED WHEN ENGINES SDR FDEA200903261071Seat Track · wornMDCC SEAT TRACK 5R 12 INCHES FWD OF FR 64 HAS A WORN SCALLOP REPAIRED SEAT TRACK IAW SRM 53-10-16 FIG 201.SDR FDEA200903231016Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK NR 2 RT, 6 INCHES FWD OF FR 64 HAS 1 WORN SCALLOPS. REMOVED DAMAGED SECTION OF NR 2 TRACK AND INSTALLED SEAT TRACK SPLICE REPAIR AT SEAT TRACK NR 2 RT BETWEEN FRAME 62 AND FRAME 64 IAW SRM 53-10-16, FIG 201, PAGE 207/208SDR FDEA200903130913Engine · failedON TAKEOFF HEAVY VIBRATION WITH NOISE AND ECAM ADVISORY FOR NR 1 ENGINE N1. NR 1 ENGINE N1 SHOWED MAX OF 3.6. N2 VIB NR 1 ENG 0.6. ALL OTHER ENGINE PARAMETERS NORMAL. COMPLETED INSTALLATION OF FIRST STAGE FAN BLADES ACCORDING TO AMM 72-21-00-4. REINSDR FDEA200812165181Unknown · unknownDURING CRUISE, RT OUTER FUEL TANK DROPPED AS LOW AS 7.04 LBS, WHILE LT OUTER TANK REMAINED AT 8.04 LBS & 2 CB'S WITH NO CORRECTION. ARRIVED AT ACFT, FOUND FUEL QTYS ALL NORMAL, L/O AT 8.3, R/O AT 8.3, ECAM AND OVERHEAD TOTALS AGREE WITH TANKS. PRESSURIZED ALSDR FDEA200812125132Relay · failedDURING T.O. ROLL NR 1 ENG N1 AND N2 SURGED AFTER TOGA, DROPPED 2 % 3 TIMES. NOTED EGT AND F.F. GAGES MIRRORED N1 AND N2. REJECTED TO AT 85 KTS. FOLLOWED QRH PROCEDURE. RETRIEVED FAULT CODE 351-18, 28 VDC POWER DISCONNECT FAULT. PER TSM REMOVED AND REPLACEDSDR FDEA200812125130Relay · surgesDURING TAKEOFF ROLL NR 1 ENG N1 AND N2 SURGED AFTER TOGA, DROPPED 2 3 PERCENT TIMES. NOTED EGT AND FF GAGES MIRRORED N1 AND N2. REJECTED TAKEOFF AT 85 KTS. FOLLOWED QRH PROCEDURE. REMOVED AND REPLACE RELAY 33KS.
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