N612AX

Service difficulty reports · 31

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 = 'N612AX' 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.

SDR ZTRR20200910002Hinge · departed2020-08-30 UPON LANDING DURING MX WALK-AROUND NR 2 ENGINE RIGHT CORE COWL WAS NOTICED TO HAVE FAILED DURING FLIGHT, PI-REP ENG 2 CORE COWL DAMAGED AND PIECES MISSING. CONCLUSIVE FAILURE IS UNDETERMINED, TWO POSSIBILITIES WHICH COULD RESULT IN SUCH FAILURE AREAug 30, 2020 · N612AX · Doug DC1030 · Nacelle/Pylon, Main FrameSDR CNMA20110007Pan · corrodedFWD P17, STA 870, LWR BILGE LAV DUMP PAN HAS SEVERAL AREAS OF CORROSION ON TOP AND RT SIDE OF PAN. REMOVED CORROSION FROM RT SIDE OF PAN FOUND TO BE WITHIN LIMITS IAW SRM VOL 1 53-00-01, FIG 1A, PG 6. REPLACED TOP PANEL IAW SRM VOL I 51-31-01 PG 1 AND REPLMar 24, 2011 · N612AX · Doug DC1030 · Fuselage Miscellaneous StructureSDR CNMA20110011Intercostal · corrodedSUPPORT ANGLE AND INTERCOSTAL AT APPROX LONGERON 44L HAS AREAS OF CORROSION AND FASTENER HEADS POPPED FROM STA 535 TO 595. REPAIRED INTERCOSTAL IAW SRM VOL I 53-00-01, FIG 8, PG 27. REMOVED CORR IAW SRM VOL II 51-21-01, PG 28 AND REMOVED BAD FASTNER IAW SRM VMar 19, 2011 · N612AX · Doug DC1030 · Fuselage Miscellaneous StructureSDR CNMA20110006Attach Angle · corrodedCORROSSION ON FUSELAGE FRAME ATTACH ANGLE AT LONGERON 51L STA. 1119. REMOVED CORROSSION FOUND OUT OF LIMITS FABRICATED REPAIR DOUBLER FROM .080 7075-0 HEAT TREATED TO T6 IAW SRM VOL I 53-30-00, FIG 8, PG 31.Mar 19, 2011 · N612AX · Doug DC1030 · Fuselage Main, Attach FittingsSDR CNMA20110005Door Frame · corrodedSURFACE CORROSSION ON AFT PIT DOOR FWD SIDE OF FRAME ON LOWER AFT SIDE AT LONGERON 42L TO 46L AT STA 1957. R & R FRAME AT STA 1957 IAW SRM VOL II 51-35-01, PG 1 AND 51-33-01, PG 34.Mar 19, 2011 · N612AX · Doug DC1030 · Fuselage Main, StructureSDR CNMA20110004Bulkhead · crackedNR 3 PYLON HAS CRACK ON AFT BULKHEAD UPPER INBD FLANGE COMING OUT OF RADIUS AT PYLON STA 418. REMOVED NR 3 PYLON REPLACED AFT PYLON BULKHEAD IAW DWG NR AWB70125 RE-INSTALLED PYLON IAW MM 54-00-01 LEAK AND OPS CHECK GOOD.Mar 19, 2011 · N612AX · Doug DC1030 · Nacelle/Pylon, Bulkhead/FirewallSDR CNMA20100035Strainer · cloggedENG 3 OIL STRAINER CLOG LIGHT ILLUMINATED STEADY IN FLIGHT, ACCOMPLISHED QRH PROCEDURE NR3 ENGINE SHUTDOWN. C/A: REPLACED ENGINE.Dec 29, 2010 · N612AX · Doug DC1030 · Turbine Engine Oil SystemSDR CNMA20100019Decoder · failedF/A'S BROUGHT TO ATTENTION OF COCKPIT THAT IF READING LIGHTS, CALL LIGHTS AND AUDIO INOP IN B ZONE MAY EFFECT O2 GENERATORS, MAINT CONTROL CONFIRMED RETURNED TO DEPARTURE. R&R SECTION TIMER DECODER IN ZONE "B", OTBD IAW AMM 23-33 CHK OPS NORMAL. ACCOMPLISHEMay 8, 2010 · N612AX · Doug DC1030 · Entertainment SystemSDR CNMA20100004Indicator · defectiveFL300 PRESSURE DIFF INDICATING 4 PSID, ALT INDICATED 3500' DECREASED CABIN TO 1800' PRESS RELIEF LIGHT ON, NEITHER DIFF INDICATION OR ALT WERE GIVING CORRECT INFORMATION OPERATING IN STBY MODE. R & R CABIN ALT DIFF PRESS INDICATOR IAW MM 21-33-01, AND PERFORMFeb 9, 2010 · N612AX · Doug DC1030 · Cabin Pressure IndicatorSDR CNMA20100001Retract Cylinder · defectiveUPON GEAR RETRACTION, LT MLG RED LIGHT ON LOOKED THRU VIEWER, SAW GROUND LIGHTS, FELT VIBRATION. REMOVED AND REPLACED LT MLG RETRACT ACTUATOR. OPS CHECKS GOOD IAW MM 32-33.Jan 7, 2010 · N612AX · Doug DC1030 · Landing Gear Retraction/Extension SystemSDR CNMA20090001Engine · power lossNR 2 ENGINE COMPRESSOR STALL CLIMBING THRU 320 NO THROTTLE MOVEMENT SMOOTH WEATHER. N1 DROPPED TO 90%, EGT 850 WITH VIBRATION. CORRECTIVE ACTION REPLACED ENGINE.Mar 28, 2009 · N612AX · Doug DC1030 · Engine (Turbine/Turboprop)SDR CNMA20090102Panel · crackedNR1 PYLON PRE-COOLER EXHAUST GRILL PANEL HAS 4 INCH CRACK AT 3RD INBD SCREW HOLE. PERFROMED A REPAIR IAW SRM VOL 1, 54-00-01, FIG 2B. INSTALLED FASTENERS IAW SRM VOL II, 51-31-01.Jan 22, 2009 · N612AX · Doug DC1030 · Engine Bleed Air SystemSDR CNMA20090101Channel · damagedRT WING L/E LWR PANEL XORS 917 -949 DEEP ABRASION ON INNER CHANNEL C/TO PANEL. DAMAGED CHANNEL WAS REMOVED NEW CABLE GUARD WAS FABRICATED AND INSTALLED IAW DWG ARB2946 AND GMM 4.45. INSTALLEDFASTENERS IAW SRM VOL 2, 51-31-01.Jan 22, 2009 · N612AX · Doug DC1030 · Wing Miscellaneous StructureSDR CNMA20090100Skin · crackedBS 515-535, STR 32L, THERE IS A CRACK ON AIR CON BAY DOOR SKIN UPPER EDGE. DAMAGED AREA WAS TRIMMED OUT. DOOR WAS REINFORCED WITH 2 DOUBLERS AND 1 FILLER PN N612AX-NRC914-1/ -02/ -03 IAW SRM VOL 1, 52-10-00, FIG 2 AND INSTALLED USING FASTENERS BACR15CE5D7 B/NJan 22, 2009 · N612AX · Doug DC1030 · Air Conditioning DoorsSDR CNMA20090099Floor Support · corrodedB/T STA 824 AND STA 859, LBL 38 CORROSION ON FLOOR SUPPORT. CORROSION WAS BLENDED OUT IAW SRM VOL 2, 51-21-01 AREA WAS REINFORCED WITH A STRAP IAW SRM VOL 1, 53-00-01, FIG 7. INSTALLED FASTENERS IAW SRM 51-31-01.Jan 22, 2009 · N612AX · Doug DC1030 · Fuselage Miscellaneous StructureSDR CNMA20090098Floor Support · corrodedSTA 889, LBL 38, CORROSION ON FLOOR SUPPORT. CORROSION WAS BLENDED OUT IAW SRM VOL 2, 51-21-01 AREA WAS REINFORCED WITH A STRAP IAW SRM VOL 1, 53-00-01, FIG 7. INSTALLED FASTENERS IAW SRM 51-31-01.Jan 22, 2009 · N612AX · Doug DC1030 · Fuselage Miscellaneous StructureSDR CNMA20090097Floor Support · damagedDOUBLE HOLE ON FLOOR SUPPORT STA 1884, LBL 4. DAMAGED FLOOR SUPPORT WAS REMOVED. NEW FLOOR SUPPORT FABRICATED AND INSTALLED IAW SRM VOL 3, 53-16-01 AND GMM 4.45. INSTALLED FASTENERS IAW SRM 51-31-01, VOL 2.Jan 22, 2009 · N612AX · Doug DC1030 · Fuselage Miscellaneous StructureSDR CNMA20090095Channel · damagedLT WING L/E LWR 4TH PANEL FROM TIP INNER CHANNEL TORN. DAMAGED CHANNEL REMOVED. FABRICATED NEW CHANNEL IAW DWG ARB2946-24 AND GMM 4.45. INSTALLED FASTENERS IAW SRM VOL 2 51-31-01.Jan 22, 2009 · N612AX · Doug DC1030 · Fuselage Miscellaneous StructureSDR CNMA20090094Fitting · damagedCTR CARGO COMP AFT WALL IN FRONT OF AFT FUEL TANK ON EACH BREAKER (NOT SURE CAN'T READ WORD?) FOUND CRACKED. DAMAGED FITTING WAS REMOVED. A NEW FITTING WAS FABRICATED IAW DWG AFA 7725 AND GMM 4.45 AND INSTALLED FASTENERS IAW SRM VOL 2, 51-35-01.Jan 22, 2009 · N612AX · Doug DC1030 · Fuselage Main, Attach FittingsSDR CNMA20090093Skin · damagedLT OTBD FLAP VANE HAS A SMALL HOLE AT UPPER SKIN ABOVE FLAP OTBD FAIRING. HOLE ON OTBD FLAP VANE REPAIRED WITH EXTERNAL DOUBLER IAW SRM 51-71-00, PAR 16B.Jan 22, 2009 · N612AX · Doug DC1030 · Trailing Edge FlapsSDR CNMA20090092Strap · damagedBS 1931, LBL 27, DOUBLE HOLE ON STRAP WITH NUT PLATES. DAMAGED AREA TRIMMED OUT. REINFORCED AREA WITH ANGLE IAW SRM VOL 1, 53-00-01, FIG 8 INSTALLED FASTENERS IAW SRM VOL 2, 51-31-01.Jan 22, 2009 · N612AX · Doug DC1030 · Fuselage Miscellaneous StructureSDR CNMA20090091Frame · corrodedBS 1902, FROM BL 0.0 TO LBL15, CORROSION ON FRAME LWR CHORD. CORRODED SECTION OF CHORD WAS TRIMMED OUT. CHORD WAS REINFORCED WITH A REPAIR ANGLE, STRAP AND FILLER PN N612AX-NRC562-1/-2/-3 FABRICATED AND INSTALLED IAW SRM VOL 1, 53-00-00, FIG 8. USING FASTEJan 22, 2009 · N612AX · Doug DC1030 · Fuselage Main, FrameSDR CNMA20090090Intercostal · crackedBS 1701-1721, STR 38L-39L, THERE IS A CRACK ON THE INTERCOSTAL. CRACK WAS DRILLED OUT, INTERCOSTAL WAS REINFORCED WITH AN ANGLE AND INSTALLED IAW SRM VOL 1, 53-00-01, FIG 8. INSTALLED FASTENERS IAW SRM VOL 2, 51-35-01.Jan 22, 2009 · N612AX · Doug DC1030 · Fuselage Miscellaneous StructureSDR CNMA20090089Intercostal · brokenBS 1741-1761, STR 38L-39L, INTERCOSTAL IS BROKEN. BROKEN EDGE WAS TRIMMED OUT, INTERCOSTAL WAS REINFORCED WITH AN ANGLE. FABRICATED AND INSTALLED IAW SRM VOL 1 53-00-01, FIG 8. INSTALLED FASTENERS IAW SRM VOL 2, 51-35-01.Jan 22, 2009 · N612AX · Doug DC1030 · Fuselage Miscellaneous StructureSDR CNMA20090088Support · brokenBS 999, LBL 13, CABLE ANGLE SUPPORT IS BROKEN. DAMAGED SUPPORT REMOVED AND NEW FABRICATED IAW DWG AAP8000-1077, GMM 4.45 INSTALLED FASTENERS IAW SRM VOL 2, 51-31-01.Jan 22, 2009 · N612AX · Doug DC1030 · Fuselage Miscellaneous StructureSDR CNMA20090087Support · brokenBS979, LBL13, CABLE ANGLE SUPPORT IS BROKEN. DAMAGED SUPPORT REMOVED AND INSTALLED IAW DWG AAP8000-1077, GMM 4.45. INSTALLED FASTENERS IAW SRM VOL 2, 51-31-01.Jan 22, 2009 · N612AX · Doug DC1030 · Fuselage Miscellaneous StructureSDR CNMA20090086Bracket · brokenBS 959, LBL 13, CABLE ANGLE SUPPORT IS BROKEN C/T INTERCOSTAL. DAMAGED BRACKET REMOVED AND NEW PN OAI-53-0001 IAW DWG AAP 8000 -1077, GMM 4.45 USING FASTENERS IAW SRM VOL 2, 31-31-01, MS20470D5-4 B/N 03000.Jan 22, 2009 · N612AX · Doug DC1030 · Fuselage Miscellaneous StructureSDR CNMA20090085Channel · crackedBS 879, RBL 16, THERE IS A CRACK ON U-CHANNEL. DAMAGED CHANNEL WAS REMOVED. A NEW FLOOR SUPPORT WAS FABRICATED IAW SRM VOL 3, 53-13-01, FIG 12 AND GMM 4.45 AND INSTALLED FASTENERS IAW SRM VOL 2, 51-33-01.Jan 22, 2009 · N612AX · Doug DC1030 · Fuselage Miscellaneous StructureSDR CNMA20090084Support · crackedBS 1341, STR 31L, THERE IS A CRACK ON OVERWING FAIRING SUPPORT. CRACKED AREA TRIMMED OUT. REINFORCED AREA WITH DOUBLER PN NG12AX-NRC454-1 IAW SRM VOL 1, 53-00-01 FIG 4 USING FASTENERS IAW SRM VOL 2, 51-31-01 BACR15BB4D4C B/N 08877.Jan 22, 2009 · N612AX · Doug DC1030 · Fuselage Miscellaneous StructureSDR CNMA20090083Floor Support · damagedBS 1741, LBL 40 DOUBLE-MOLE ON CARGO FLOOR SUPPORT. REMOVED DAMAGED FLOOR SUPPORT AND NEW FLOOR SUPPORT PN AOI-53-0015 ARE INSTALLED IAW SRM VOL III 53-15-01 AND GMM 4.45 WITH FASTENER IAW SRM VOL II 51-31-01.Jan 22, 2009 · N612AX · Doug DC1030 · Fuselage Miscellaneous StructureSDR CNMA20090082Floor Support · damagedBS1741, RBL 40 DOUBLE HOLE ON FLOOR SUPPORT. REMOVED DAMAGED FLOOR SUPPORT AND NEW FLOOR SUPPORT PN OAI - 53-0014 IAW SRM VOL III 53-15-01 AND GMM 4.45.Jan 22, 2009 · N612AX · Doug DC1030 · Fuselage Miscellaneous Structure
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