# Service difficulty reports: N936AX, cancelled Feb 7, 2008 A list on [N936AX, cancelled Feb 7, 2008](https://openairdocs.org/deregistered/N936AX-2008-02-07.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 2 · 74 reports - [SDR ABXA040139](https://openairdocs.org/sdr/ABXA040139.md): Keelbeam · cracked · Apr 1, 2004 · N936AX · Doug DC931 · Fuselage Main, Keel > LEFT KEELBEAM TO VERTICAL WEB ATTACH FITTING CRACKED AT BOTTOM OF WING ATTACH POINT APPROXIMATELY STA 693 FORWARD OF GEAR DOOR ACTUATOR. REPLACED FITTING IAW DC-9 SRM. - [SDR ABXA020206](https://openairdocs.org/sdr/ABXA020206.md): Longeron · cracked · Aug 27, 2002 · N936AX · Doug DC931 · Fuselage Main, Longeron/Stringer > LONGERON 29 LEFT FORE AND AFT OF SPLICE CRACKED AT FS 408. REPLACED SECTION OF LONGERON IAW DC-9 SRM 53-02. - [SDR ABXA020205](https://openairdocs.org/sdr/ABXA020205.md): Angle · damaged · Aug 26, 2002 · N936AX · Doug DC931 · Fuselage Structure (General) > RIGHT DORSAL FIN ATTACH ANGLE HAD TOOLING DAMAGE IN THE RADIUS. REPLACED DORSAL FIN ATTACH ANGLE IAW DC-9 SRM 51-30-1, 51-30-2, 51-30-5, AND REA D953-44887. - [SDR ABXA020204](https://openairdocs.org/sdr/ABXA020204.md): Skin · cracked · Aug 26, 2002 · N936AX · Doug DC931 · Fuselage Main, Plate/Skin > FUSELAGE SKIN CRACKED AT UPPER/AFT STOP. REPAIRED UPPER AFT DOOR CUTOUT IAW DC-9 SRM 53-05. - [SDR ABXA010041](https://openairdocs.org/sdr/ABXA010041.md): Pan · cracked · Feb 9, 2001 · N936AX · Doug DC931 · Cargo/Baggage Doors > FORWARD LOWER CARGO DOOR LOWER PAN WAS CRACKED IN THE RADIOUS. MAINTENANCE INSPECTED AND REPAIRED THE CRACKED AREA IAW DC-9 SRM 52-03 FIG 8. - [SDR ABXA010045](https://openairdocs.org/sdr/ABXA010045.md): Shear Tie · cracked · Feb 9, 2001 · N936AX · Doug DC931 · Fuselage Main, Frame > SHEAR TIE AT FUSELAGE STATION 1087, LONGERON 2R WAS CRACKED. MAINTENANCE INSPECTED AND REPLACED THE SHEAR TIE IAW DC-9 SRM 51-30. - [SDR ABXA010044](https://openairdocs.org/sdr/ABXA010044.md): Longeron · cracked · Feb 9, 2001 · N936AX · Doug DC931 · Fuselage Main, Longeron/Stringer > LONGERON 2R WAS CRACKED. MAINTENANCE INSPECTED AND REPAIRED THE LONGERON IAW DC-9 SRM 53-01, 53-30. - [SDR ABXA010043](https://openairdocs.org/sdr/ABXA010043.md): Longeron · cracked · Feb 9, 2001 · N936AX · Doug DC931 · Fuselage Main, Longeron/Stringer > LONGERON 2L WAS CRACKED. MAINTENANCE INSPECTED AND REPAIRED THE LONGERON IAW DC-9 SRM 53-01, 51-30. - [SDR ABXA010042](https://openairdocs.org/sdr/ABXA010042.md): Frame · cracked · Feb 9, 2001 · N936AX · Doug DC931 · Fuselage Main, Frame > FUSELAGE FRAME AT STATION 617 WAS FOUND TO HAVE TWO CRACKS (1.25 AND.5 INCH LENGTHS). MAINTENANCE INSPECTED AND REPAIRED THE FRAME IAW ABX REA D953-39920-MR. - [SDR ABXA010136](https://openairdocs.org/sdr/ABXA010136.md): Bearing · worn · Jan 22, 2001 · N936AX · Doug DC931 · Stabilizer Control System > THE HORIZONTAL STABILIZER JACKSCREW BEARING FREE PLAY EXCEEDED LIMITATIONS. MAINTENANCE INSPECTED AND REPLACED THE JACKSCREW ASSEMBLY IAW DC-9 MM 27-40-01. - [SDR ABXA000107](https://openairdocs.org/sdr/ABXA000107.md): Switch · failed · Feb 9, 2000 · N936AX · Doug DC931 · Landing Gear Position and Warning > ON LANDING HAD TO RECYCLE GEAR BECAUSE NOSE GEAR GREEN LIGHT DID NOT ILLUMINATE. GEAR WAS SELECTED DOWN AGAIN AND ALL THREE GREEN LIGHTS ILLUMINATED. REPLACED NLG DOWNLOCK POSITION SWITCH IAW DC9 SMM 32-60-00. OPS CHECKED GOOD. - [SDR ABXA9900433](https://openairdocs.org/sdr/ABXA9900433.md): Frame · cracked · Jun 9, 1999 · N936AX · Doug DC931 · Fuselage Main, Frame > DURING C-CHECK, FOUND LEFT MAIN FRAME STATION 699 CRACKED. REPLACED LEFT MAIN FRAME IAW DC9 SRM 51-30-2 AND 51-30-1. - [SDR ABXA9900416](https://openairdocs.org/sdr/ABXA9900416.md): Pan · cracked · Jun 8, 1999 · N936AX · Doug DC931 · Cargo/Baggage Doors > DURING C-CHECK, FOUND FORWARD LOWER CARGO DOOR PAN CRACKED. REPAIRED IAW DC9 SRM 52-03 AND 51-30-1. - [SDR ABXA9900403](https://openairdocs.org/sdr/ABXA9900403.md): Longeron · cracked · Jun 7, 1999 · N936AX · Doug DC931 · Fuselage Main, Longeron/Stringer > DURING C-CHECK, FOUND LONGERON 26 LEFT CRACKED AT STATION 945. REPLACED LONGERON SECTION IAW DC9 SRM 51-30-2. - [SDR ABXA9900425](https://openairdocs.org/sdr/ABXA9900425.md): Longeron · cracked · Jun 4, 1999 · N936AX · Doug DC931 · Fuselage Main, Longeron/Stringer > DURING C-CHECK, FOUND LONGERON 17 LEFT CRACKED AT STATION 980. REPLACED LONGERON 17 LEFT IAW DC9 SRM 51-30-5. - [SDR ABXA9900424](https://openairdocs.org/sdr/ABXA9900424.md): Retainer · cracked · Jun 4, 1999 · N936AX · Doug DC931 · Fuselage Miscellaneous Structure > DURING C-CHECK, FOUND WINDOW RETAINER CRACKED AT STATION 698, LEFT SIDE. REPAIRED IAW ABX REA D953-31670. - [SDR ABXA9900423](https://openairdocs.org/sdr/ABXA9900423.md): Pan · cracked · Jun 4, 1999 · N936AX · Doug DC931 · Cargo/Baggage Doors > DURING C-CHECK, FOUND AFT LOWER CARGO DOOR PAN CRACKED. REPLACED DOOR PAN IAW DC9 SRM 51-30-2. - [SDR ABXA9701706](https://openairdocs.org/sdr/ABXA9701706.md): Vane · delaminated · Oct 21, 1997 · N936AX · Doug DC931 · Trailing Edge Flaps > DURING C-CHECK, FOUND THE LEFT WING CENTER FIXED VANE WAS DELAMINATED. REPLACED VANE. - [SDR ABXA9701705](https://openairdocs.org/sdr/ABXA9701705.md): Doubler · cracked · Oct 21, 1997 · N936AX · Doug DC931 · Fuselage Miscellaneous Structure > DURING C-CHECK, FOUND MAIN ENTRY DOOR CUTOUT INTERNAL UPPER FORWARD DOUBLER CRACKED. REPAIRED IAW DC-9 SRM 53-05. - [SDR ABXA9701704](https://openairdocs.org/sdr/ABXA9701704.md): Angle · cracked · Oct 21, 1997 · N936AX · Doug DC931 · Nacelle/Pylon Structure > DURING C-CHECK, FOUND THE RIGHT PYLON UPPER ATTACH ANGLE WAS CRACKED. REPAIRED IAW DC-9 SRM 54-04. - [SDR ABXA9701701](https://openairdocs.org/sdr/ABXA9701701.md): Vane · delaminated · Oct 21, 1997 · N936AX · Doug DC931 · Trailing Edge Flaps > DURING C-CHECK, FOUND THE LEFT WING INBOARD FIXED VANE WAS DELAMINATED. THE VANE WAS REPLACED IAW DC-9 M/M. - [SDR ABXA9701702](https://openairdocs.org/sdr/ABXA9701702.md): Bulkhead Angle · cracked · Oct 17, 1997 · N936AX · Doug DC931 · Fuselage Main, Bulkhead > DURING C-CHECK, FOUND ANGLE ON THE AFT SIDE OF THE AFT PRESSURE BULKHEAD WAS FOUND CRACKED. THE ANGLE WAS REPLACED IAW DC-9 SRM. - [SDR ABXA9701703](https://openairdocs.org/sdr/ABXA9701703.md): Angle · corroded · Oct 16, 1997 · N936AX · Doug DC931 · Fuselage Miscellaneous Structure > DURING C-CHECK, FOUND ANGLE CORRODED AT FORWARD OUTBOARD CORNER OF RIGHT WHEEL WELL. THE ANGLE WAS REPLACED IAW DC-9 SRM. - [SDR ABXA9700962](https://openairdocs.org/sdr/ABXA9700962.md): Gear Indication · inoperative · May 2, 1997 · N936AX · Doug DC931 · Landing Gear Position and Warning > NOSE LANDING GEAR INDICATION LIGHT APPEARS TO BE INOPERATIVE. VERIFIED DOWN BY TOWER FLY-BY. INSPECTED NOSE GEAR DOWN LOCK SWITCH AND GEAR HANDLE SWITCH. CYCLED NOSE GEAR 4 TIMES, OPS CHECKED GOOD IAW DC-9 MM 32-30-01. NO DEFECTS NOTED. - [SDR ABXA9600423](https://openairdocs.org/sdr/ABXA9600423.md): Power Supply · inoperative · Mar 30, 1996 · N936AX · Doug DC931 · Emergency Lighting > EMERGENCY LIGHTS INTERMITTENTLY STAY ON WITH POWER OFF. REPLACED EMERGENCY LIGHT POWER SUPPLY. - [SDR ABXA9600245](https://openairdocs.org/sdr/ABXA9600245.md): Power Supply · inoperative · Mar 8, 1996 · N936AX · Doug DC931 · Emergency Lighting > DURING PRE-DEPARTURE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY POWER SUPPLY. - [SDR ABXA9600244](https://openairdocs.org/sdr/ABXA9600244.md): Uplock Switch · defective · Mar 7, 1996 · N936AX · Doug DC931 · Landing Gear Position and Warning > AFTER GEAR RETRACTION, LEFT GEAR UNSAFE LIGHT REMAINED ILLUMINATED, RECYCLED GEAR, NO HELP. LIGHT EXTINGUISHED AFTER 2-3 MINUTES UPON ENTERING TURBULENCE. REPLACED LEFT GEAR UPLOCK SWITCH S1-79. - [SDR ABXA9600404](https://openairdocs.org/sdr/ABXA9600404.md): Pressure Panel · defective · Feb 14, 1996 · N936AX · Doug DC931 · Fuselage Miscellaneous Structure > DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE PRESSURE PANEL AT FS 37 HAD A ONE INCH DIAMETER HOLE ON THE RIGHT SIDE BELOW THE RADOME HINGE POINT. REPAIRED PRESSURE PANEL AT FS 37 IAW ABX REA D953-14357-MR. - [SDR ABXA9600403](https://openairdocs.org/sdr/ABXA9600403.md): Floor Panel · damaged · Feb 13, 1996 · N936AX · Doug DC931 · Fuselage Floor Panel > DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND A FLOOR PANEL DAMAGED FROM FS 237 TO 313. REPAIRED FLOOR PANEL IAW ABX REA D953-14339-MR. - [SDR ABXA9600387](https://openairdocs.org/sdr/ABXA9600387.md): Skin · cracked · Feb 7, 1996 · N936AX · Doug DC931 · Fuselage Main, Plate/Skin > DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE FUSELAGE SKIN AT FORWARD EDGE OF THE FORWARD CARGO COMPARTMENT DOOR JAMB HAD TWO CRACKS AND EXCESSIVE CORROSION BLENDOUTS. REPAIRED IAW ABX REA D953-13853-MR. - [SDR ABXA9600400](https://openairdocs.org/sdr/ABXA9600400.md): Door Pan · binding · Feb 6, 1996 · N936AX · Doug DC931 · Passenger/Crew Doors > DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND WHILE REPLACING THE LEFT FORWARD ENTRY DOOR, THE NEW DOOR REQUIRED EXCESSIVE TRIM OUT AROUND THE UPPER POCKET OF THE LOWER HINGE CAVITY. REPAIRED LEFT FORWARD ENTRY DOOR IAW REA D952-14205-MR. - [SDR ABXA9600402](https://openairdocs.org/sdr/ABXA9600402.md): Floor Beam · cracked · Feb 5, 1996 · N936AX · Doug DC931 · Fuselage Main, Floor Beam > DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE FLOOR BEAM WEB AT FS 996 AND BL 0 CRACKED AND CORRODED. REPAIRED FLOOR BEAM WEB AT FS 996 IAW ABX REA D953-14261-MR. - [SDR ABXA9600401](https://openairdocs.org/sdr/ABXA9600401.md): Skin · damaged · Jan 31, 1996 · N936AX · Doug DC931 · Fuselage Main, Plate/Skin > DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, AND EXISTING REPAIR ON THE SERVICE DOOR FORWARD JAMB UPPER CORNER INTERFERED WITH THE ACCOMPLISHMENT OF SID INSPECTION PSE 53-09-033A, IAW AD 94-03-1. VERIFIED REPAIR AND PLACED ON CARRYOVER FOR DACO TO PERFORM DTA - [SDR ABXA9600419](https://openairdocs.org/sdr/ABXA9600419.md): Te Panel · delaminated · Jan 26, 1996 · N936AX · Doug DC931 · Wing, Plate/Skin > DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE LEFT WING TRAILING EDGE PANEL AT XRS 91.0 DELAMINATED AND RIVETS SHEARED. REPLACED LEFT WING TRAILING EDGE PANEL IAW DC-9 SRM CHAPTERS 51-30-1 AND 51-30-2. - [SDR ABXA9600397](https://openairdocs.org/sdr/ABXA9600397.md): Web · corroded · Jan 26, 1996 · N936AX · Doug DC931 · Fuselage Main, Bulkhead > DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND A PREVIOUS REPAIR ON THE AFT PRESSURE BULKHEAD LOWER WEB THAT WAS CORRODED AND HAD DRILL STARTS. REPAIRED AFT PRESSURE BULKHEAD WEB IAW ABX REA D953-14176-MR. - [SDR ABXA9600399](https://openairdocs.org/sdr/ABXA9600399.md): Floor Beam Web · corroded · Jan 25, 1996 · N936AX · Doug DC931 · Fuselage Main, Floor Beam > DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND A FLOOR BEAM WEB CORRODED AT FS 996. REPAIRED FLOOR BEAM WEB AT FS 996 IAW ABX REA D953-14201-MR. - [SDR ABXA9600374](https://openairdocs.org/sdr/ABXA9600374.md): Skin · dented · Jan 25, 1996 · N936AX · Doug DC931 · Fuselage Main, Plate/Skin > DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE RIGHT AFT FUSELAGE SKIN HAD TWO DENTS BETWEEN FS 966 AND 987, BETWEEN LONGERONS 16R AND 18R. REPAIRED AFT FUSELAGE SKIN IAW ABX REA D953-13715-MR. - [SDR ABXA9600398](https://openairdocs.org/sdr/ABXA9600398.md): Skin · dented · Jan 24, 1996 · N936AX · Doug DC931 · Fuselage Main, Plate/Skin > DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND TWO DENTS IN THE RIGHT FORWARD FUSELAGE SKIN BETWEEN FS 351 AND 364 AND LONGERONS 24 AND 25R. REPAIRED FORWARD FUSELAGE SKIN IAW ABX REA D953-14200-MR. - [SDR ABXA9600381](https://openairdocs.org/sdr/ABXA9600381.md): Floor Beam · chafed · Jan 22, 1996 · N936AX · Doug DC931 · Fuselage Main, Floor Beam > DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE FLOOR BEAMS AT FS 389 AND 408 GOUGED AND CHAFED. REPAIRED FLOOR BEAMS IAW ABX REA D953-13826-MR. - [SDR ABXA9600380](https://openairdocs.org/sdr/ABXA9600380.md): Floor Beam · chafed · Jan 22, 1996 · N936AX · Doug DC931 · Fuselage Main, Floor Beam > DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE FLOOR BEAM AT FS 389 AND 408 GOUGED AND CHAFED. REPAIRED FLOOR BEAMS IAW ABX REA D953-13826-MR. - [SDR ABXA9600395](https://openairdocs.org/sdr/ABXA9600395.md): Floor Beam · chafed · Jan 20, 1996 · N936AX · Doug DC931 · Fuselage Main, Floor Beam > DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE FLOOR BEAM AT FS 980 HAD UPPER FLANGE CHAFE DAMAGE AT BL 40.0 AND 50.0. REPAIRED FLOOR BEAM AT FS 980 IAW ABX REA D953-14061-MR. - [SDR ABXA9600392](https://openairdocs.org/sdr/ABXA9600392.md): Frame · cracked · Jan 18, 1996 · N936AX · Doug DC931 · Fuselage Main, Frame > DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE LEFT FUSELAGE FRAME AT FS 658 HAD A PREVIOUS REPAIR THAT WAS CRACKED THROUGH THE STOP DRILL. REPAIRED LEFT FUSELAGE FRAME FS 658 IAW ABX REA D953-13924-MR. - [SDR ABXA9600391](https://openairdocs.org/sdr/ABXA9600391.md): Frame · cracked · Jan 18, 1996 · N936AX · Doug DC931 · Fuselage Main, Frame > DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE LEFT FUSELAGE FRAME AT FS 639 HAD A PREVIOUS REPAIR ON THE AFT SIDE AT LONGERON 18L THAT HAD CRACKED THROUGH THE PREVIOUS STOP DRILL. REPAIRED LEFT FUSELAGE FRAME AT FS 639 IAW ABX REA D953-13924-MR. - [SDR ABXA9600420](https://openairdocs.org/sdr/ABXA9600420.md): Te Panel · delaminated · Jan 16, 1996 · N936AX · Doug DC931 · Wing, Plate/Skin > DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE LEFT WING TRAILING EDGE PANEL BETWEEN STATION XRS 445.0 AND XRS 509 CORRODED AND DELAMINATED. REPLACED TRAILING EDGE PANEL IAW DC-9 SRM CHAPTERS 51-30-1 AND 51-30-2. - [SDR ABXA9600408](https://openairdocs.org/sdr/ABXA9600408.md): Frame · cracked · Jan 16, 1996 · N936AX · Doug DC931 · Fuselage Main, Frame > DURING C AND D-CHECK ACCEPTANCE INSPECTIONS WHILE COMPLYING WITH AD 78-07-05; SB 53-131 VISUAL INSPECTION OF LEFT AND RIGHT FUSELAGE FRAMES, FOUND THE FRAME AT FS 737L CRACKED IN TWO PLACES. REPLACED FRAME AT FS 737 IAW SB 53-131 AND DC-9 SRM CHAPTERS 51-30-1 - [SDR ABXA9600407](https://openairdocs.org/sdr/ABXA9600407.md): Frame · cracked · Jan 16, 1996 · N936AX · Doug DC931 · Fuselage Main, Frame > DURING C AND D-CHECK ACCEPTANCE INSPECTIONS WHILE COMPLYING WITH AD 78-07-05; SB 53-131, VISUAL INSPECTION OF LEFT AND RIGHT FUSELAGE FRAMES, FOUND THE LEFT FRAME CRACKED AT FS 718. REPLACED FRAME AT FS 718 IAW SB 53-131 AND DC-9 SRM CHAPTERS 51-30-1, 51-30-2 - [SDR ABXA9600394](https://openairdocs.org/sdr/ABXA9600394.md): Skin · chafed · Jan 15, 1996 · N936AX · Doug DC931 · Horizontal Stabilizer, Plate/Skin > DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE HORIZONTAL STABILIZER RIGHT AND LEFT UPPER SKIN PANELS CHAFED AND BLENDED BEYOND THE DC-9 SRM LIMITS. REPAIRED HORIZONTAL STABILIZER LEFT AND RIGHT UPPER SKIN PANELS IAW ABX REA D955-14035-MR. - [SDR ABXA9600393](https://openairdocs.org/sdr/ABXA9600393.md): Skin · chafed · Jan 15, 1996 · N936AX · Doug DC931 · Horizontal Stabilizer, Plate/Skin > DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE HORIZONTAL STABILIZER RIGHT AND LEFT UPPER SKIN PANELS CHAFED AND BLENDED BEYOND THE DC-9 SRM LIMITS. REPAIRED HORIZONTAL STABILIZER LEFT AND RIGHT UPPER SKIN PANELS IAW ABX REA D955-14035-MR. - [SDR ABXA9600396](https://openairdocs.org/sdr/ABXA9600396.md): Service Panel · cracked · Jan 12, 1996 · N936AX · Doug DC931 · Fuselage Miscellaneous Structure > DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE AFT LAVATORY SERVICE PANEL DAMAGED BETWEEN FS 965 AND FS 980 AT LONGERON 19L. REPAIRED LEFT AFT FUSELAGE SKIN PANEL IAW ABX REA D953-14063-MR. - [SDR ABXA9600389](https://openairdocs.org/sdr/ABXA9600389.md): Skin · dented · Jan 11, 1996 · N936AX · Doug DC931 · Fuselage Main, Plate/Skin > DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE RIGHT FORWARD FUSELAGE SKIN AT FS 148 AND LONGERON 19R HAD A SHARP DENT THAT EXCEEDED THE DC-9 SRM LIMITS. REPAIRED RIGHT FUSELAGE FORWARD SKIN IAW ABX REA D953-13887-MR. Next page: https://openairdocs.org/deregistered/N936AX-2008-02-07/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 = 'N936AX' AND deregistration_id = 'N936AX-2008-02-07' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N936AX-2008-02-07/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.