N945AX, cancelled Dec 23, 2009

Service difficulty reports · 71

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 = 'N945AX' AND deregistration_id = 'N945AX-2009-12-23'
  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 ABXA050069Longeron · corrodedLONGERON 30 AT STA 945 WAS CORRODED BEYOND LIMITS. REPLACED LONGERON IAW DC-9 SRM 51-30-5 AND 51-30-2.Mar 8, 2005 · N945AX · Doug DC931 · Fuselage Main, Longeron/StringerSDR ABXA050070Skin · crackedDURING ROUTINE LINE MAINTENANCE AT ILN, FOUND THE FUSELAGE SKIN CRACKED 1 INCH LONG AT STA 897 AND LONGERON 29 RT. SKIN WAS FOUND TO BE CORRODED BEYOND LIMITS ON THE INTERIOR SURFACE UNDER LONGERON 30. INSTALLED SKIN SPLICE, REPAIRED IAW DC-9 SRM 53-04 FIG 1Mar 8, 2005 · N945AX · Doug DC931 · Fuselage Main, Plate/SkinSDR ABXA050003Pressure Switch · defectiveSHORTLY AFTER T/O, FLOW LIGHT ON AUTO PRESSURE CONTROLLER ILLUMINATED. TRANSFER LOCKOUT AND STANDBY LIGHT ALSO ON. RAN ABNORMAL PER MANUAL SECTION 21, CHAPTER 3. FLOW LIGHT, TRANSFER LOCKOUT AND STANDBY LIGHTS REMAINED ON. WENT TO MANUAL. STILL UNABLE TO CONTRJan 6, 2005 · N945AX · Doug DC931 · Cabin Pressure Control SystemSDR ABXA040267Frame · crackedLEFT FORWARD MAIN FRAME AT FUSELAGE STA 699 WAS CRACKED BEYOND LIMITS OF DC-9 S/B 53-131. CRACK RAN BETWEEN POINTS G - J. REPLACED FRAME IAW ABX EA 53400321-001-4, WO 600204273.Jul 29, 2004 · N945AX · Doug DC931 · Fuselage Main, FrameSDR ABXA040268Frame · crackedRIGHT FORWARD MAIN FRAME AT FUSELAGE STA 699 WAS CRACKED BEYOND LIMITS OF DC-9 S/B 53-131. CRACK RAN BETWEEN POINTS H - I. REPLACED FRAME IAW ABX EA 53400322-001-4, WO 600204273.Jul 29, 2004 · N945AX · Doug DC931 · Fuselage Main, FrameSDR ABXA040218Skin · crackedAFT LOWER CARGO DOOR SKIN WAS CRACKED AT THE DOOR HANDLE CUTOUT. REMOVED CRACKS, INSTALLED SCUFF PLATE IAW DC-9 SRM 52-05.Jun 7, 2004 · N945AX · Doug DC931 · Cargo/Baggage DoorsSDR ABXA040217Skin · crackedSKIN CRACKED ABOVE RIGHT PYLON AT RIVET, STA 1038, LONGERON 12 RIGHT. REPAIRED CRACK IAW DC-9 SRM 53-31-0.Jun 4, 2004 · N945AX · Doug DC931 · Fuselage Main, Plate/SkinSDR ABXA040216Skin · crackedSKIN CRACKED ABOVE LEFT PYLON AT RIVET, STA 1038, LONGERON 12 LEFT. REPAIRED CRACK IAW DC-9 SRM 53-31-0.Jun 4, 2004 · N945AX · Doug DC931 · Fuselage Main, Plate/SkinSDR ABXA040215Cusp Web · crackedCUSP WEB CRACKED IN TWO AREAS FS 237 TO FS 254, RIGHT BUTTLINE 45 TO RIGHT BUTTLINE 54. REPAIRED CUSP WEB IAW DC-9 SRM 53-01.Jun 4, 2004 · N945AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA040214Skin · crackedA .5 INCH CRACK COMING OUT OF FASTENER HOLE AT FORWARD LOWER CARGO DOOR UPPER CORNER FUSELAGE SKIN. INSTALLED REPAIR IAW EA 53100110-001.Jun 4, 2004 · N945AX · Doug DC931 · Fuselage Main, Plate/SkinSDR ABXA030084Structure · contaminatedUPON INITIAL GEAR EXTENSION, GEAR DID NOT EXTEND. AUX/ALT HYDRAULIC PUMPS WERE ON. ENGINE HYDRAULIC PUMPS WERE HIGH HYDRAULIC PRESSURE / QUANTITY WERE NORMAL. AFTER APPROXIMATELY 20 SECONDS, CREW RECYCLED LANDING GEAR AND GEAR EXTENDED NORMALLY. FOUND EXCEFeb 26, 2003 · N945AX · Doug DC931 · Landing Gear DoorsSDR ABXA030002Wire · unsecureFIRST OFFICERS YOKE LIGHT SPARKED WHEN LIFTED. SECURED WIRING TO CHART HOLDER IAW MM. OPS CHECKED GOOD.Jan 1, 2003 · N945AX · Doug DC931 · Light System WiringSDR ABXA020341Angle · corrodedRIGHT L ANGLE AT STA 965, LBL 30 - 52, HAD HEAVY CORROSION. REPLACED L ANGLE IAW DC-9 SRM.Nov 14, 2002 · N945AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA020340Doubler · crackedLEFT MAIN FRAME AT F.S. 699 WAS CRACKED IN FORWARD POCKET AT/BETWEEN "Z" CLIP ATTACH BOLTS. REPAIRED MAIN FRAME ON E.A. 53400110-001-1 AND DC-9 SRM.Nov 12, 2002 · N945AX · Doug DC931 · Fuselage Structure (General)SDR ABXA020339Fitting · crackedFORWARD SIDE OF AFT PRESSURE BULKHEAD RIGHT VENTRAL DOOR WEB SUPPORT ANGLE WAS CRACKED. REPLACED SUPPORT ANGLE IAW DC-9 SRM 51-10-4, 51-30-2 AND 51-30-5.Nov 12, 2002 · N945AX · Doug DC931 · Fuselage Main, BulkheadSDR ABXA020338Floorbeam · corrodedFLOORBEAM AT STA 995 WAS CORRODED ON THE TOP FLANGE AT LEFT BUTT LINE 46. REPAIRED FLOOR BEAM IAW DC-9 SRM.Nov 12, 2002 · N945AX · Doug DC931 · Fuselage Main, Floor BeamSDR ABXA020337Fitting · crackedAFT LOWER CARGO DOOR, #3 BEAM AFT END FITTING WAS CRACKED. REPLACED AFT LOWER CARGO DOOR IAW DC-9 MM AND NON ROUTINE #0345.Nov 11, 2002 · N945AX · Doug DC931 · DoorsSDR ABXA020336Clip · crackedAFT LOWER CARGO DOOR, INNER ANGLE AT #2 BEAM FITTING AREA WAS CRACKED. REPLACED AFT LOWER CARGO DOOR IAW DC-9 MM AND NON ROUTINE #0345.Nov 11, 2002 · N945AX · Doug DC931 · DoorsSDR ABXA020335Fitting · crackedAFT LOWER CARGO DOOR, #4 BEAM AFT END FITTING WAS CRACKED. REPLACED AFT LOWER CARGO DOOR IAW DC-9 MM AND NON ROUTINE #0345.Nov 11, 2002 · N945AX · Doug DC931 · DoorsSDR ABXA020334Fitting · crackedAFT LOWER CARGO DOOR, #2 BEAM FORWARD END FITTING WAS CRACKED. REPLACED AFT LOWER CARGO DOOR IAW DC-9 MM AND NON ROUTINE #0345.Nov 11, 2002 · N945AX · Doug DC931 · DoorsSDR ABXA020333Clip · crackedAFT LOWER CARGO DOOR, #5 BEAM FORWARD END FITTING WAS CRACKED. REPLACED AFT LOWER CARGO DOOR IAW DC-9 MM AND NON ROUTINE #0345.Nov 11, 2002 · N945AX · Doug DC931 · DoorsSDR ABXA020332Panel · crackedAFT LOWER CARGO DOOR, OUTER PAN CRACKED AT BLIND NUT AND BULGED OUT AT SAME LOCATION LOWER AFT CORNER. REPLACED AFT LOWER CORNER DOOR IAW DC-9 MM AND NON ROUTINE #0345.Nov 11, 2002 · N945AX · Doug DC931 · DoorsSDR ABXA020331Frame · corrodedLEVEL II CORROSION ON FRAME AT STA. 446, AFT SIDE, BETWEEN LONGERON 28 LEFT AND 28 RIGHT. REPAIRED FRAME IAW DC-9 SRM 53-03.Nov 11, 2002 · N945AX · Doug DC931 · Fuselage Structure (General)SDR ABXA020330Splice · crackedLONGERON 30 END FITTING BETWEEN F.S. 579 AND 596 CRACKED ON BOTH VERTICAL FLANGES. REPLACED END FITTINGS IAW DC-9 SRM.Nov 11, 2002 · N945AX · Doug DC931 · Fuselage Main, Longeron/StringerSDR ABXA020329Longeron · crackedLONGERON 29 LEFT CRACKED BETWEEN F.S. 579 AND 596. CRACKED ON BOTH VERTICAL FLANGES. REPAIRED LONGERON IAW REA D553-45780MR.Nov 11, 2002 · N945AX · Doug DC931 · Fuselage Main, Longeron/StringerSDR ABXA020328Skin · crackedRUDDER TOP RIGHT SIDE HAD LARGE CRACK. REPLACED RUDDER IAW DC-9 SRM.Nov 8, 2002 · N945AX · Doug DC931 · Rudder, Plate/SkinSDR ABXA020046Warning System · malfunctionedUPON SELECTING GEAR DOWN, NOSE GEAR UNSAFE LIGHT ILLUMINATED AND NOSE GEAR GREEN LIGHT DID NOT COME ON. GEAR WARNING HORN SOUNDED. RECYCLED GEAR, ALL INDICATIONS NORMAL. OPS CHECKED GOOD IAW DC-9 MM 32-60.Jul 9, 2002 · N945AX · Doug DC931 · Landing Gear Position and WarningSDR ABXA010651Battery · dischargedWHEN EMERGENCY LIGHTS WERE SELECTED ON, THE PEANUT LIGHTS DID NOT ILLUMINATE. REPLACED THE EMERGENCY LIGHT BATTERY/CHARGER PACK IAW DC-9 MM.Dec 25, 2001 · N945AX · Doug DC931 · Emergency LightingSDR ABXA9900807Outflow Valve · failedAUTO-PRESSURIZATION WAS INOPERATIVE. AIRCRAFT WOULD NOT DEPRESSURIZE UNTIL LANDING. OBSERVED STRONG ELECTRICAL SMELL. REPLACED OUTFLOW VALVE ACTUATOR.Nov 23, 1999 · N945AX · Doug DC931 · Pressure Regulator/Outflow ValveSDR ABXA9900670Cusp Web · crackedDURING C-CHECK, FOUND CUSP WEB RIGHT SIDE CRACKED AT STATION Y-945. REPLACED CUSP WEB IAW DC9 SRM 51-30-2 AND 51-30-5.Aug 25, 1999 · N945AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA9900669Bulkhead T-Cap · corrodedDURING C-CHECK, FOUND PRESSURE BULKHEAD T-CAP CORRODED AT STATION Y-617. REPAIRED T-CAP IAW ABX REA D953-32890 MR.Aug 25, 1999 · N945AX · Doug DC931 · Fuselage Main, BulkheadSDR ABXA9900668Web · crackedDURING C-CHECK, FOUND CUSP WEB CRACKED AT STATION 617 RIGHT SIDE. REPLACED CUSP WEB IAW DC9 SRM 51-30-1 AND 51-30-5.Aug 24, 1999 · N945AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA9900667Longeron · crackedDURING C-CHECK, FOUND LONGERON 30 FLANGE CRACKED UNDER AFT END CAP STATION Y-598. REPAIRED LONGERON IAW DC9 SRM 53-02-00.Aug 24, 1999 · N945AX · Doug DC931 · Fuselage Main, Longeron/StringerSDR ABXA9900685Frame · crackedDURING C-CHECK, FOUND FRAME CRACKED AT STATION 1076 AND LONGERON 13 RIGHT. REPLACED SECTION OF FRAME IAW DC9 SRM 53-03.Aug 23, 1999 · N945AX · Doug DC931 · Fuselage Main, FrameSDR ABXA9900684Fitting · crackedDURING C-CHECK, FOUND FITTING CRACKED BELOW LONGERON 16 LEFT ON THE AFT SIDE OF STATION 1076 FRAME. REPLACED FITTING IAW DC9 SRM 51-30-1 AND 51-30-5.Aug 23, 1999 · N945AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA9900683Hinge · crackedDURING C-CHECK, FOUND LEFT AILERON INBOARD HINGE FITTING CRACKED AT SPAR MOUNT HOLE. REPLACED HINGE IAW DACO DWG 5910515.Aug 20, 1999 · N945AX · Doug DC931 · Wing, Control Surface Attach FittingsSDR ABXA9900682Bulkhead Tee · crackedDURING C-CHECK, FOUND A CRACK INDICATION IN THE AFT PRESSURE BULKHEAD NR 6 TEE CAP. REPAIRED IAW ABX EA 53-120037-006.Aug 20, 1999 · N945AX · Doug DC931 · Fuselage Main, BulkheadSDR ABXA9900686Frame · crackedDURING C-CHECK, FOUND OUTBOARD END OF THE AFT PRESSURE BULKHEAD FRAME CRACKED AT LONGERON 15 LEFT. REPAIRED IAW DC9 SRM 51-30-5 AND 51-20-0.Aug 19, 1999 · N945AX · Doug DC931 · Fuselage Main, BulkheadSDR ABXA9900650Actuator · corrodedDURING C-CHECK, FOUND LEFT OUTBOARD SPOILER ACTUATOR VALVE BODY EXFOLIATED AND VALVE LINK MOUNT AREA CRACKED. REPLACED ACTUATOR IAW ABX EA 2760D019-001.Aug 18, 1999 · N945AX · Doug DC931 · Drag Control ActuatorSDR ABXA9900649Web · crackedDURING C-CHECK, FOUND CUSP WEB CRACKED FORWARD AND AFT OF FRAME AT STATION 598 RIGHT SIDE. REPLACED CUSP WEB IAW DC9 SRM 51-30-2 AND 51-30-1.Aug 18, 1999 · N945AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA9900648Doubler · corrodedDURING C-CHECK, FOUND DOUBLER FORWARD AND AFT OF STATION 718 CORRODED. REPLACED DOUBLER IAW DC9 SRM 51-30-5.Aug 18, 1999 · N945AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA9900647Longeron · corrodedDURING C-CHECK, FOUND LONGERON 14 LEFT CORRODED AT STATION 1089. REPLACED LONGERON SECTION IAW DC9 SRM 51-30-2.Aug 17, 1999 · N945AX · Doug DC931 · Fuselage Main, Longeron/StringerSDR ABXA9900644Web · crackedDURING C-CHECK, FOUND CUSP WEB CRACKED FORWARD AND AFT OF FRAME AT STATION 598, LEFT SIDE. REPLACED CUSP WEB IAW DC9 SRM 51-30-1 AND 51-30-2.Aug 16, 1999 · N945AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA9900643Panel · corrodedDURING C-CHECK, FOUND CORROSION ON LEFT LOWER SLANT PANEL CAP. REPAIRED IAW ABX REA D953-32811MR.Aug 13, 1999 · N945AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA9800080Doubler · corrodedDURING C-CHECK, FOUND CORROSION AT THE AFT END OF THE PRESSURIZATION OUTFLOW VALVE SCOOP. REPLACED DOUBLER IAW DC9 SRM 51-30-2.Feb 16, 1998 · N945AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA9800075Skin · crackedDURING C-CHECK, FOUND FUSELAGE SKIN BULGED AND CRACKED .125 AT FASTENER HOLE UNDER LONGERON 30 AT STA 897. REPAIRED IAW ABX REA D953-22433-MR.Feb 11, 1998 · N945AX · Doug DC931 · Fuselage Main, Plate/SkinSDR ABXA9800072Frame · corrodedDURING C-CHECK, FOUND EXFOLIATION CORROSION ON THE AFT FLANGE OF FRAME AT STA 851 BETWEEN LONGERON 29L AND 29R.Feb 10, 1998 · N945AX · Doug DC931 · Fuselage Main, FrameSDR ABXA9800071Fitting · crackedDURING C-CHECK, FOUND VERTICAL SUPPORT CRACKED AT LOWER END AT LONGERON 23R AND STA 560. REPAIRED SUPPORT FITTING IAW DC9 DWG NR K05159.Feb 10, 1998 · N945AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA9800066Angle · crackedDURING C-CHECK, FOUND LOWER PYLON TO FUSELAGE ATTACK ANGLE AT LEFT PYLON LEADING EDGE CRACKED. REPAIRED ANGLE IAW DC9 SRM 54-04.Feb 9, 1998 · N945AX · Doug DC931 · Nacelle/Pylon StructureSDR ABXA9800065Fitting · crackedDURING C-CHECK, FOUND RIGHT WING OUTBOARD FLAP HINGE FITTING CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-1.Feb 9, 1998 · N945AX · Doug DC931 · Trailing Edge Flaps
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