# Service difficulty reports: N79750, cancelled Jan 24, 2018 A list on [N79750, cancelled Jan 24, 2018](https://openairdocs.org/deregistered/N79750-2018-01-24.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 · 60 reports - [SDR 2004F00174](https://openairdocs.org/sdr/2004F00174.md): Line · cracked · Jun 15, 2004 · N79750 · Boeing 727224 · Hydraulic System, Main > DURING FINAL APPROACH HYDRAULIC SYSTEM A QUANTITY DROPPED TO ZERO LANDED SAFELY WITHOUT INCIDENT. FOUND NR 2 ENGINE SUPPLY LINE CRACKED REPLACED SAME PER MM 29-00. OPS CHECK GOOD AIRCRAFT RETURNED TO SERVIEC WITHOUT FURTHER INCIDENT. (M) - [SDR 2004F00301](https://openairdocs.org/sdr/2004F00301.md): Actuator · inoperative · Jan 29, 2004 · N79750 · Boeing 727224 · Leading Edge Slat Actuator > DURING THE AFTER T/O CHECKLIST, NR 2 LEADING EDGE SLAT EXTENDED INDICATION REMAINED ON BOTH FORWARD AND AFT ANNUNCIATOR LIGHTS DUMPED FUEL AND RETURNED TO KCVG WITHOUT INCIDENT. REPLACED NR 2 LEADING EDGE SLAT ACTUATOR PER MM 27-81-32. AIRCRAFT RETURNED TO S - [SDR 2004F00219](https://openairdocs.org/sdr/2004F00219.md): Steering Sys · out of adjust · Jan 28, 2004 · N79750 · Boeing 727224 · Landing Gear Steering System > DISCONTINUED TAKEOFF ROLL, DUE TO LACK OF STEERING CONTROL TO THE RIGHT. RETURNED TO RAMP WITHOUT INCIDENT. ADJUSTED RUDDER PEDAL STEERING MECHANISM PER MM 32-51-0. OPS CHECK GOOD. (M) - [SDR 2002F01029](https://openairdocs.org/sdr/2002F01029.md): Ballast · malfunctioned · Sep 26, 2002 · N79750 · Boeing 727224 · Passenger Compartment Lighting > DURING CLIMB, SMOKE ALARMS IN BOTH AFT LAVATORIES WENT ON, SMOKE WAS NOTICED. AFTER 20 OR 3 MINUTES IT WAS CLEAR, AFT GALLEY POWER WAS SWITCHED OFF AS PRECAUTIONARY A/C CONTINUED TO MIAMI. ON THE GROUND, FOUND AFT CABIN CEILING LIGHTS DUAL FILTER BALLAST BUR - [SDR 2002F00402](https://openairdocs.org/sdr/2002F00402.md): Switch · worn · Mar 23, 2002 · N79750 · Boeing 727224 · Leading Edge Slat Position Indicating System > ON TAXI-OUT WITH FLAPS 15 F/E AUX PANEL SHOWED NR 4 LE DEVICE NOT DOWN AND LOCKED A/C RETURNED TO GATE. REMOVED AND REPLACED NR 4 L/E DEVICE SWITCH PER MM 27-82-31. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR 2001F00643](https://openairdocs.org/sdr/2001F00643.md): Hydraulic Line · leaking · Oct 15, 2001 · N79750 · Boeing 727224 · Hydraulic System, Main > FLT 523 - ARRIVING FROM SVMI, AFTER LANDING INTO MIA, HYDRAULIC SYSTEM 'A' PRESSURE AND QUANTITY INDICATION DROPPED TO 0. AIRCRAFT CONTINUED TO GATE WITHOUT INCIDENT. MAINTENANCE T/S AND FOUND THE HYDRAULIC SYSTEM 'A' RETURN LINE FROM THE ENGINE NR 2 HYDRAUL - [SDR FX72001F00003](https://openairdocs.org/sdr/FX72001F00003.md): Heat Exchanger · cracked · Aug 20, 2001 · N79750 · Boeing 727224 · Cabin Cooling System > AFTER TAKEOFF AIRCRAFT WOULD NOT PRESSURIZE. BOTH AIRCRAFT PACKS DID NOT WORK AND AFTER RESETTING BOTH PACKS TO (ON) AIRCRAFT WILL NOT PRESSURIZE. RETURNED TO AIRPORT WITHOUT INCIDENT. TROUBLESHOT AIRCRAFT PRESSURE SYSTEM, FOUND CRACKED PRIMARY HEAT EXCHANGE - [SDR 20010320SG001](https://openairdocs.org/sdr/20010320SG001.md): Indicator · malfunctioned · Feb 11, 2001 · N79750 · Boeing 727224 · Engine Pressure Ratio (EPR) > ABORTED TAKEOFF DUE TO A LOW EPR INDICATION AT REDUCED POWER ON ENGINE NR 2. INSPECTED AND CREW RAN ENGINE UP TO MAX POWER. NR 2 ENGINE OPS PROPERLY ON GROUND ENGINE RUN AND ALL ENGINE INDICATIONS READ NORMAL AS PER TRIM CHART 71-00-87. AIRCRAFT RETURNED TO - [SDR 20000614AP003](https://openairdocs.org/sdr/20000614AP003.md): Switch · out of adj · Apr 7, 2000 · N79750 · Boeing 727224 · Landing Gear Position and Warning > ON FAE FLIGHT NR 153, DBWI TO KIAD, DURING CLIMB AND GEAR RETRACTION, THE TAIL SKID LIGHT REMAINED ILLUMINATED. AIRCRAFT PERFORMED AN AIR RETURN TO KBWI. ON GROUND MAINTENANCE ADJUSTED THE TAILS SKID SWITCH AND GROUND OPS CHECKED OK IAW 32-71-01. AIRCRAFT W - [SDR 20000614AP004](https://openairdocs.org/sdr/20000614AP004.md): Seal · misaligned · Feb 26, 2000 · N79750 · Boeing 727224 · Doors > ON FAE FERRY FLIGHT 981 - KMIA-KFLL - DURING CLIMB, CREW HEARD LOUD NOISE FROM L1 DOOR. AIRCRAFT RETURNED TO KMIA. ON GROUND MAINTENANCE, FOUND DOOR SEAL LOWER HINGE MISALIGNED. SEAL WAS REPOSITIONED IAW MM 52-11-71. AIRCRAFT WAS PRESSURIZED IAW MM 21-31-0 - [SDR 99ZZZM732](https://openairdocs.org/sdr/99ZZZM732.md): Pdu · binding · Sep 29, 1999 · N79750 · Boeing 727224 · Trailing Edge Flap Control System > FLT 201 - KMIA-SDQ - DURING CLIMB AND WHILE RETRACTING FLAPS, OUTBOARD FLAPS STAYED AT 5 DEGREES. RECYCLING BY NORMAL MEANS DID NOT WORK. A/C AIR RETURNED BACK TO KMIA. NO FUEL WAS DUMPED, A/C ACCOMPLISHED NORMAL OVERWEIGHT LANDING. WHILE EXTENDING FLAPS FO - [SDR CALA9901168](https://openairdocs.org/sdr/CALA9901168.md): Megaphone · inop · Sep 9, 1999 · N79750 · Boeing 727224 · Emergency Equipment > INSPECTION FOUND AFT CABIN MEGAPHONE INOPERATIVE. THE MEGAPHONE WAS REPLACED. - [SDR 2000ZZZM204](https://openairdocs.org/sdr/2000ZZZM204.md): B-Nut · loose · Aug 16, 1999 · N79750 · Boeing 727224 · Fuel Control/Turbine Engines > ON FAE - FLT 945 - KMEM TO NBJ, DURING CLIMB, THROUGH FL260 NR 3 ENGINE STARTED FLUCTUATING INTERMITTENT AT FIRST THEN STEADY. AFTER LEVEL OFF AT FL290, NR 3 ENGINE CONTINUED TO FLUCTUATE. AIRCRAFT RETURNED TO KMEM. ON GROUND MAINTENANCE INSPECTED NR 3 ENGI - [SDR 99ZZZX1758](https://openairdocs.org/sdr/99ZZZX1758.md): Seat Track · corroded · Mar 23, 1999 · N79750 · Boeing 727224 · Fuselage, Seat/Cargo Attach Fittings > DURING A C-CHECK, CORROSION WAS NOTED ON SEAT TRACK STA 1060 - STA 1110, LBL 45. - [SDR 99ZZZX1757](https://openairdocs.org/sdr/99ZZZX1757.md): Stringer · corroded · Mar 23, 1999 · N79750 · Boeing 727224 · Fuselage Main, Longeron/Stringer > DURING A C-CHECK, CORROSION WAS NOTED ON STR 28R, STA 950F - STA 990. - [SDR 99ZZZX1756](https://openairdocs.org/sdr/99ZZZX1756.md): Channel · corroded · Mar 23, 1999 · N79750 · Boeing 727224 · Fuselage Miscellaneous Structure > DURING A C-CHECK, CORROSION WAS NOTED ON A SECTION OF HAT CHANNEL LEFT AFT LAVATORY STA 1137 - STA 1176. - [SDR 99ZZZX1755](https://openairdocs.org/sdr/99ZZZX1755.md): Hinge · corroded · Mar 23, 1999 · N79750 · Boeing 727224 · Passenger/Crew Doors > DURING A C-CHECK, CORROSION WAS NOTED ON R-1 DOOR'S LOWER HINGE. - [SDR 99ZZZX1754](https://openairdocs.org/sdr/99ZZZX1754.md): Skin · corroded · Mar 23, 1999 · N79750 · Boeing 727224 · Leading Edge Devices > DURING A C-CHECK, CORROSION WAS NOTED ON NR 1 NOSE FLAP OF NR 1 KREUGER FLAP AT BUSHING FLANGE ATTACH POINT. - [SDR 99ZZZX1753](https://openairdocs.org/sdr/99ZZZX1753.md): Beam · corroded · Mar 23, 1999 · N79750 · Boeing 727224 · Horizontal Stabilizer Structure > DURING A C-CHECK, CORROSION WAS NOTED ON RT HORIZONTAL STABILIZER UPPER TRAILING EDGE BEAM. - [SDR 99ZZZX1752](https://openairdocs.org/sdr/99ZZZX1752.md): Strap · corroded · Mar 23, 1999 · N79750 · Boeing 727224 · Fuselage Miscellaneous Structure > DURING A C-CHECK, CORROSION WAS NOTED ON STRAP IN C-1 PIT FLOOR AREA JUST FORWARD OF STA 540 THAT CROSSES FLOORBEAM. - [SDR 99ZZZX1751](https://openairdocs.org/sdr/99ZZZX1751.md): Floorbeam · corroded · Mar 23, 1999 · N79750 · Boeing 727224 · Fuselage Main, Floor Beam > DURING A C-CHECK, CORROSION WAS NOTED AT STA 720L, STR 27. - [SDR CALA9801961](https://openairdocs.org/sdr/CALA9801961.md): Battery · discharged · Sep 19, 1998 · N79750 · Boeing 727224 · Emergency Lighting > AFT GALLEY OVERHEAD EMERGENCY LIGHT NOT WORKING. REMOVED AND REPLACED BATTERY PACK AND POWER SUPPLY. - [SDR CALA9801051](https://openairdocs.org/sdr/CALA9801051.md): Fitting · cracked · Jun 11, 1998 · N79750 · Boeing 727224 · Passenger/Crew Doors > INSPECTION FOUND A 2 INCH CRACK ON L-1 DOOR UPPER HINGE FITTING. THE CRACKED AREA WAS CUT OUT, AN ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-30-2, AND 51-40-5. - [SDR CALA9801050](https://openairdocs.org/sdr/CALA9801050.md): Fitting · corroded · Jun 11, 1998 · N79750 · Boeing 727224 · Fuselage, Landing Gear Attach Fittings > INSPECTION FOUND LT MLG TRUNNION FITTING CORRODED. THE TRUNNION FITTING WAS REPAIRED IAW ECRA 5340-01320. - [SDR CALA9800995](https://openairdocs.org/sdr/CALA9800995.md): Skin · delaminated · Jun 5, 1998 · N79750 · Boeing 727224 · Trailing Edge Flaps > INSPECTION FOUND A 4 X 2 AREA OF RT WING TRAILING EDGE INBOARD FOREFLAP LOWER SURFACE DELAMINATED. THE FOREFLAP WAS REMOVED AND REPLACED IAW MM 27-51-12. - [SDR CALA9800948](https://openairdocs.org/sdr/CALA9800948.md): Shear Tie · corroded · Jun 2, 1998 · N79750 · Boeing 727224 · Fuselage Miscellaneous Structure > INSPECTION FOUND SHEAR TIE CORRODED AT STA 500, STRINGER 27R-28R. THE CORRODED AREA WAS CUT OUT, A NEW SHEAR TIE WAS FABRICATED AND INSTALLED IAW SRM 51-30-4, FIGURE 15, REPAIR 3. - [SDR CALA9800930](https://openairdocs.org/sdr/CALA9800930.md): Intercostal · corroded · Jun 1, 1998 · N79750 · Boeing 727224 · Fuselage Miscellaneous Structure > INSPECTION FOUND INTERCOSTAL CORRODED IN FORWARD BAGGAGE BIN AT STA 500, RBL 9. THE INTERCOSTAL WAS REMOVED AND CORRODED STRINGER WAS CUT OUT IAW SRM 53-10-3. NEW STRINGER AND SPLICES WERE FABRICATED IAW SRM 53-10-5 AND 51-10-2. THE STRINGER, SPLICES AND IN - [SDR CALA9800929](https://openairdocs.org/sdr/CALA9800929.md): Skin · corroded · Jun 1, 1998 · N79750 · Boeing 727224 · Fuselage Main, Plate/Skin > INSPECTION FOUND FUSELAGE SKIN CORRODED AT STA 480 TO 500, STRINGER 28R. THE CORRODED AREA WAS CUT OUT IAW SRM 53-30-3. DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 53-30-3, 51-10-2, AND 51-30-2. - [SDR CALA9800928](https://openairdocs.org/sdr/CALA9800928.md): Wire · broken · Jun 1, 1998 · N79750 · Boeing 727224 · Light System Wiring > INSPECTION FOUND THE EMERGENCY PATH LIGHTING INOPERATIVE FROM ROW 22 AND AFT. BROKEN WIRING WAS REPAIRED AND A FUSE WAS REPLACED IAW MM 33-50-00 AND OPERATION OF THE LIGHTS CHECKED GOOD. - [SDR CALA9800927](https://openairdocs.org/sdr/CALA9800927.md): Bracket · cracked · Jun 1, 1998 · N79750 · Boeing 727224 · Leading Edge Slat Actuator > INSPECTION FOUND A 1 INCH CRACK IN LT WING NR 2 LEADING EDGE FLAP ACTUATOR ATTACH BRACKET AT LOWER INBOARD CORNER INSIDE LEADING EDGE AREA. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-10-1, AND 51-10-2. - [SDR CALA9800926](https://openairdocs.org/sdr/CALA9800926.md): Bracket · cracked · Jun 1, 1998 · N79750 · Boeing 727224 · Leading Edge Slat Actuator > INSPECTION FOUND A 1 INCH CRACK AT LOWER INBOARD AND OUTBOARD CORNERS OF LT WING NR 1 LEADING EDGE FLAP ACTUATOR ATTACH BRACKET. THE BRACKETS WERE REMOVED AND NEW BRACKETS WERE FABRICATED AND INSTALLED IAW SRM 51-10-1 AND 51-10-6. - [SDR CALA9800925](https://openairdocs.org/sdr/CALA9800925.md): Cowling · corroded · Jun 1, 1998 · N79750 · Boeing 727224 · Engine Cowling System > INSPECTION FOUND NR 2 ENGINE INLET COWLING RING CORRODED. THE CORRODED AREA WAS CUT OUT. FILLER AND DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 54-30-3, 51-10-2, 51-40-5 AND 51-30-2. - [SDR CALA9800586](https://openairdocs.org/sdr/CALA9800586.md): Battery Pack · discharged · Mar 25, 1998 · N79750 · Boeing 727224 · Emergency Lighting > INSPECTION FOUND CEILING EMERGENCY EXIT LIGHT BETWEEN R-2 DOOR AND L-2 DOOR INOPERATIVE. THE BATTERY PACK WAS REMOVED AND REPLACED. - [SDR CALA9800099](https://openairdocs.org/sdr/CALA9800099.md): Structure · damaged · Jan 22, 1998 · N79750 · Boeing 727224 · Fuselage Main, Structure > THE AIRCRAFT SUSTAINED GROUND DAMAGE TO THE FUSELAGE SKIN, STRINGER, AND FRAMES AT STA 440-480, STRINGERS 14-19L. THE FUSELAGE SKIN AND STRINGER WERE REPAIRED IAW ECRA 5330-02621. THE FRAMES WERE REPAIRED IAW ECRA 5310-03656, SRM 51-40-3, AND 53-10-3. - [SDR CALA9701513](https://openairdocs.org/sdr/CALA9701513.md): Power Supply · inoperative · Oct 29, 1997 · N79750 · Boeing 727224 · Emergency Lighting > INSPECTION FOUND RIGHT AFT CARGO DOOR EMERGENCY EXIT LIGHT INOPERATIVE. THE BATTERY POWER SUPPLY WAS REMOVED AND REPLACED. - [SDR CALA9701431](https://openairdocs.org/sdr/CALA9701431.md): Fuse · blown · Oct 10, 1997 · N79750 · Boeing 727224 · Emergency Lighting > EMERGENCY TRACK LIGHTS INOP ROW 10 FORWARD. REMOVED AND REPLACED FUSES. - [SDR CALA9700423](https://openairdocs.org/sdr/CALA9700423.md): Support · corroded · Mar 19, 1997 · N79750 · Boeing 727224 · Fuselage Miscellaneous Structure > INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 1033, RBL 26. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-1. - [SDR CALA9700422](https://openairdocs.org/sdr/CALA9700422.md): Support · corroded · Mar 19, 1997 · N79750 · Boeing 727224 · Fuselage Miscellaneous Structure > INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 1067, RBL 26. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-10-1. - [SDR CALA9700418](https://openairdocs.org/sdr/CALA9700418.md): Stiffener · cracked · Mar 19, 1997 · N79750 · Boeing 727224 · Fuselage Miscellaneous Structure > INSPECTION FOUND A.75 INCH CRACK IN STIFFENER AT BS 348, STRINGER 10R. THE STIFFENER WAS REPAIRED IAW SRM 51-30-2. - [SDR CALA9700417](https://openairdocs.org/sdr/CALA9700417.md): Floorbeam · corroded · Mar 19, 1997 · N79750 · Boeing 727224 · Fuselage Main, Floor Beam > INSPECTION FOUND FLOORBEAM CORRODED AT STA 344, LBL 10 AND RBL 10. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED. A NEW SECTION WAS FABRICATED AND INSTALLED USING REPAIR ANGLES AND FILLERS IAW SRM 53-10-8, FIGURE 9. - [SDR CALA9700416](https://openairdocs.org/sdr/CALA9700416.md): Circumferential · cracked · Mar 19, 1997 · N79750 · Boeing 727224 · Fuselage Main, Frame > INSPECTION FOUND A 1 INCH CRACK IN CIRCUMFERENTIAL AT STA 930, STRINGER 14R. THE CRACKED AREA WAS REMOVED AND REPAIR PARTS WERE INSTALLED IAW EC 5310-01397, PAGE 5. - [SDR CALA9700415](https://openairdocs.org/sdr/CALA9700415.md): Circumferential · cracked · Mar 19, 1997 · N79750 · Boeing 727224 · Fuselage Main, Frame > INSPECTION FOUND A 1 INCH CRACK IN CIRCUMFERENTIAL AT STA 804, STRINGER 14L. THE CRACK WAS STOP DRILLED. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-40-3. - [SDR CALA9700414](https://openairdocs.org/sdr/CALA9700414.md): Support · broken · Mar 19, 1997 · N79750 · Boeing 727224 · Fuselage Miscellaneous Structure > INSPECTION FOUND FLOOR SUPPORT BROKEN AT STA 758, BL 0. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-10-1. - [SDR CALA9700413](https://openairdocs.org/sdr/CALA9700413.md): Support · corroded · Mar 19, 1997 · N79750 · Boeing 727224 · Fuselage Miscellaneous Structure > INSPECTION FOUND INBOARD END OF FLOOR SUPPORT CORRODED AT STA 342, RBL 17. THE SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-2. - [SDR CALA9700412](https://openairdocs.org/sdr/CALA9700412.md): Stringer · deformed · Mar 19, 1997 · N79750 · Boeing 727224 · Fuselage Main, Longeron/Stringer > INSPECTION FOUND SKIN BULGED IN STRINGER 2-3L AREA AT STA 420 WITH STRINGER DEFORMED. A STRINGER REPAIR WAS INSTALLED IAW SRM 53-10-3. - [SDR CALA9700421](https://openairdocs.org/sdr/CALA9700421.md): Support · corroded · Mar 17, 1997 · N79750 · Boeing 727224 · Fuselage Miscellaneous Structure > INSPECTION FOUND FLOOR SUPPORT CORRODED FROM STA 1070 TO 1140, RBL 66. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-1 AND 51-10-6. - [SDR CALA9700420](https://openairdocs.org/sdr/CALA9700420.md): Floorbeam · corroded · Mar 17, 1997 · N79750 · Boeing 727224 · Fuselage Main, Floor Beam > INSPECTION FOUND FLOORBEAM CORRODED AT BS 1050, RBL 26 TO 66. THE CORRODED AREA WAS REMOVED AND A NEW SECTION WAS FABRICATED AND INSTALLED IAW SRM 53-10-8, 51-40-5, 51-10-2, AND 51-30-2. - [SDR CALA9700419](https://openairdocs.org/sdr/CALA9700419.md): Floor Pan · corroded · Mar 17, 1997 · N79750 · Boeing 727224 · Fuselage Floor Panel > INSPECTION FOUND LEFT AFT LAV FLOOR PAN CORRODED. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2 AND 51-10-6. - [SDR CALA9700344](https://openairdocs.org/sdr/CALA9700344.md): Floorbeam · corroded · Mar 10, 1997 · N79750 · Boeing 727224 · Fuselage Main, Floor Beam > INSPECTION FOUND FLOORBEAM CORRODED AT STA 300, RBL 12 TO RBL 40. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED, A NEW SECTION WAS FABRICATED AND INSTALLED IAW SRM 53-10-8. - [SDR CALA9700340](https://openairdocs.org/sdr/CALA9700340.md): Floor Support · broken · Mar 10, 1997 · N79750 · Boeing 727224 · Fuselage Miscellaneous Structure > INSPECTION FOUND FLOOR SUPPORT BROKEN AT STA 758, BL ZERO. THE FLOOR SUPPORT WAS REMOVED. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-10-1. Next page: https://openairdocs.org/deregistered/N79750-2018-01-24/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 = 'N79750' AND deregistration_id = 'N79750-2018-01-24' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N79750-2018-01-24/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.