# Service difficulty reports: Bombardier DHC-8-101 A list on [Bombardier DHC-8-101](https://openairdocs.org/model/bombardier-dhc-8-101.md). Newest first. General aviation reporting is voluntary. Page 1 of 3 · 137 reports - [SDR 7C7A201805140414](https://openairdocs.org/sdr/7C7A201805140414.md): Plate · corroded · May 8, 2018 · N880EA · Dhav DHC8101 · Entrance Stairs > PAX DOOR STRAIRCASE FWD AND AFT BACKING PLATED CORRODED. REPLACED THE PLATE. - [SDR HNAA2017042100132](https://openairdocs.org/sdr/HNAA2017042100132.md): Connector · inoperative · Apr 17, 2017 · N814EX · Dhav DHC8101 · Light System Wiring > RH THRESHOLD AND EXIT EMERGENCY LIGHT FOR RT FWD EXIT INOPERATIVE ALSO FWD CEILING OUT. - [SDR HNAA2017042100133](https://openairdocs.org/sdr/HNAA2017042100133.md): Light · inoperative · Apr 17, 2017 · Dhav DHC8101 · Emergency Lighting > RIGHT OTBD AFT EMERGENCY LIGHT INOPERATIVE, - [SDR HNAA2016012500021](https://openairdocs.org/sdr/HNAA2016012500021.md): Oil System · overserviced · Jan 25, 2016 · N808EX · Dhav DHC8101 · APU Oil System > BURNING ODOR COMING FROM APU BLEEDS. INSPECTED APU COMPARTMENT WITH NO DEFECTS OR SIGNS OF ANYTHING BURNED. FOUND APU OIL SLIGHTLY OVER SERVICED. DRAINED OIL TO PROPER LEVEL. RAN APU BLEEDS FOR 30 MINUTES WITH NO BURNING ODOR NOTICED. OK FOR SERVICE. - [SDR CA140630021](https://openairdocs.org/sdr/CA140630021.md): Engine · overtorqued · Jun 19, 2014 · Dhav DHC8101 · Engine (Turbine/Turboprop) > (CAN) THE RT ENGINE TORQUE WENT TO 113 PERCENT FOR 3 SECONDS AND BACK TO NORMAL DURING TAXI. ACFT TAXI BACK TO GATE UNEVENTFULLY. TROUBLESHOOTING ONGOING. - [SDR CA140620008](https://openairdocs.org/sdr/CA140620008.md): Engine · warning light · Jun 11, 2014 · Dhav DHC8101 · Engine (Turbine/Turboprop) > (CAN) DURING CRUISE AT FL170 THE MANUAL CAUTION LIGHT ILLUMINATED AND COULD NOT BE RESET. THE PILOT DECIDED TO RETURN TO THE DEPARTURE AIRPORT WHERE IT LANDED SAFETY. POST FLIGHT TROUBLESHOOTING LED TO THE REPLACEMENT OF THE ENGINE ELECTRONIC CONTROL. - [SDR CA140604001](https://openairdocs.org/sdr/CA140604001.md): Line · ruptured · May 11, 2014 · Dhav DHC8101 · Hydraulic System, Main > (CAN) DURING CRUISE THE NR 1 MAIN HYDRAULIC SYS LOST ALL FLUID. ACFT DIVERTED TO BASE. AFTER LANDING, SMOKE WAS NOTICED COMING FROM THE LT ENGINE AND AIRFIELD SERVICES WAS REQUESTED. THE HYDRAULIC PRESSURE LINE RUNNING FROM PRESSURE MANIFOLD IN THE NACELLE, O - [SDR CA130905001](https://openairdocs.org/sdr/CA130905001.md): Oil Cooler · leaking · Aug 20, 2013 · Dhav DHC8101 · Engine Oil Cooler > (CAN) THE PILOT SHUTDOWN THE ENGINE DUE TO MAIN OIL PRESSURE FLUCTUATION FOLLOWED BY LOSS OF OIL PRESSURE. AN AIRFRAME COOLER OIL LEAKAGE WAS DETERMINED AS THE CAUSE OIL PRESSURE LOSS. - [SDR CA130620005](https://openairdocs.org/sdr/CA130620005.md): Link · broken · Jun 20, 2013 · Dhav DHC8101 · Landing Gear Retraction/Extension System > (CAN) DURING C-CHECK, TECHS HAD PROBLEM WITH MLG ALTERNATE RELEASE SYS, RT MAIN GEAR REFUSED TO EXTEND. AFTER INVESTIGATION TECH FOUND A BROKEN D-LINK, PN 83231032-101 IPC REF 32-10-00, FIG 46, ITEM 120 IN THE RT MLG DOOR RELEASE MECHANISM IN THE RT NACELLE G - [SDR CA130521001](https://openairdocs.org/sdr/CA130521001.md): Landing Gear · malfunctioned · May 18, 2013 · Dhav DHC8101 · Landing Gear Retraction/Extension System > (CAN) DURING APPROACH, LT MLG WOULD NOT FULLY EXTEND, ALTERNATE EXTENSION WAS ATTEMPTED TO NO AVAIL. CREW RETRACTED ALL GEAR AND LANDED ON THE BELLY. CREW AND PASSENGERS EXITED SAFELY ON THE RUNWAY AND WERE BUSED TO THE TERMINAL. MAINTENANCE CREW PULLED THE - [SDR CA130410015](https://openairdocs.org/sdr/CA130410015.md): Proximity Sensor · malfunctioned · Mar 28, 2013 · Dhav DHC8101 · Landing Gear Position and Warning > (CAN) DURING CRUISE, AFTER TAKEOFF AND CLIMBOUT, THE WEIGHT ON WHEELS, CAUTION LIGHT ILLUMINATED. AFTER CONSULTING THE QRH, THE CAPTAIN DECIDED TO RETURN TO BASE FOR RECTIFICATION. EXTENSIVE TESTING OF THE ACFT PROXIMITY SENSOR SYS WAS CARRIED OUT AND THE NR - [SDR CA130212011](https://openairdocs.org/sdr/CA130212011.md): Shaft · cracked · Jan 7, 2013 · Dhav DHC8101 · Propeller Assembly > (CAN) PROPELLER SHAFT FOUND WITH A CRACK INDICATION AT THE INNER BORE AT THE NR 19 BEARING LOCATION DURING THE NORMAL MAGNETIC PARTICLES INSPECTION WHILE THE RGB WAS BEING REPAIRED FOR METAL IN OIL, MIO, CONDITION. A REQUEST WAS RAISED TO RETURN THE SHAFT URG - [SDR CA121121005](https://openairdocs.org/sdr/CA121121005.md): Oil Cooler · split · Nov 7, 2012 · Dhav DHC8101 · Engine Oil Cooler > (CAN) ACFT REPORTED TO HAVE DIMINISHING OIL PRESSURE DURING FLIGHT ON THE RT ENGINE. ENGINE SHUTDOWN AND ACFT RETURNED TO BASE SAFELY. PILOTS DEBRIEFED AND ESTABLISHED THAT THE ENGINE WAS SHUTDOWN WHEN PRESSURE JUST WENT INTO THE TOP OF THE AMBER RANGE TO SAV - [SDR HNAA2012081300915](https://openairdocs.org/sdr/HNAA2012081300915.md): Door · open · Aug 10, 2012 · N938HA · Dhav DHC8101 · Landing Gear Retraction/Extension System > GEAR FAILED TO RETRACT AFTER TAKEOFF. MAINT INSPECTED AND FOUND OVERHEAD BYPASS DOOR OPEN. MAINT CLOSED DOOR AS REQUIRED. - [SDR CA120314001](https://openairdocs.org/sdr/CA120314001.md): Actuator · failed · Mar 14, 2012 · Dhav DHC8101 · Drag Control Actuator > (CAN) A/C LOST HYDRAULIC PRESSURE DUE TO FAILURE OF THE L/H OB SPOILER ACTUATOR. ON DESCENT TO POM, THE CREW COMPLETED A MANUAL ALTERNATE GEAR EXTENSION, WITH ALL THREE OF THE ALT GEAR LIGHTS INDICATING GREEN. HOWEVER THE CREW HEARD A GRINDING NOISE FROM THE N - [SDR KPVA2012030802](https://openairdocs.org/sdr/KPVA2012030802.md): Connector · burned · Mar 3, 2012 · N805W · Dhav DHC8101 · Light System Wiring > FLIGHT ATTENDANT NOTICED STRONG "BURN" SMELL IN THE MIDDLE OF THE CABIN SHORTLY AFTER SHUTTING DOWN. FOUND OVERHEAD LIGHT AT FLIGHT ATTENDANT STATION BURNED OUT WITH BURNT CONNECTOR. - [SDR CA111114001](https://openairdocs.org/sdr/CA111114001.md): Oil System · low pressure · Nov 3, 2011 · Dhav DHC8101 · Engine Oil Indicating System > (CAN) DURING CRUISE, THE CREW RECEIVED A LOW OIL PRESSURE WARNING. THE PROPELLER WAS FEATHERED AND THE POWER BROUGHT BACK TO IDLE. THE OIL PRESSURE CONTINUED TO DECREASE AND THE PILOT SHUT THE ENGINE DOWN BEFORE DIVERTING THE FLIGHT, WHERE AN UNEVENTFUL SINGL - [SDR CA110307003](https://openairdocs.org/sdr/CA110307003.md): Landing Gear · collapsed · Mar 4, 2011 · Dhav DHC8101 · Main Landing Gear > (CAN) AN ACFT HAD AN INCIDENT UPON LANDING WHEN THE RT MAIN GEAR COLLAPSED DUE TO A HEAVY LANDING. THE ACFT SKIDDED OF THE SIDE OF THE RUNWAY BEFORE COMING TO REST. THE 31 PASSENGERS AND 3 CREW MEMBERS ONBOARD WERE NOT HURT. INVESTIGATION IS ON-GOING. - [SDR CA110221003](https://openairdocs.org/sdr/CA110221003.md): Actuator · cracked · Feb 16, 2011 · Dhav DHC8101 · Drag Control Actuator > DURING A WALK AROUND, A HYD LEAK WAS NOTICED FROM THE LT WING. ENGINEERING FOUND THE LT OTBD SPOILER ACTUATOR LEAKING FROM THE ACTUATOR HSG, HSG THREADS HAD FRACTURED ABOUT THE CYLINDER END CAP OF THE ACTUATOR. THE ACTUATOR WAS SUBSEQUENTLY REPLACED BY A SERV - [SDR CA110110010](https://openairdocs.org/sdr/CA110110010.md): Socket · burned · Jan 8, 2011 · Dhav DHC8101 · Passenger Compartment Lighting > A CABIN SIDEWALL LIGHT WAS REPORTED AS BEING UNSERVICEABLE. THE FLUORESCENT TUBE LAMP HOLDER WAS FOUND BURNT AND PARTIALLY MELTED AT ONE OF THE RECEPTACLES ENDS. - [SDR CA101019004](https://openairdocs.org/sdr/CA101019004.md): Fuel Control · failed · Oct 6, 2010 · Dhav DHC8101 · Fuel Control/Turbine Engines > VIBRATIONS/IFSD, DURING CLIMB AFTER T/O, THE PILOT HAD ENGINE VIBRATIONS AND HE ELECTED TO SHUT THE ENGINE DOWN BEFORE RETURNING TO THE DEPARTURE AIRPORT FOR AN UNEVENTFUL SINGLE ENGINE LANDING. TROUBLESHOOTING LED TO REPLACEMENT OF THE FUEL CONTROL, FUEL PUM - [SDR P4YA201061100002](https://openairdocs.org/sdr/P4YA201061100002.md): Autofeather Sys · no test · Jun 10, 2010 · N801LR · Dhav DHC8101 · Propeller Feathering/Reversing > AUTOFEATHER TEST FAILED NR 1 ENGINE. OPERATIONS CONTINUED IAW MEL NR 61-2 ITEM A, CAT B, DUE 13 JUN 2010. - [SDR P4YA201061100001](https://openairdocs.org/sdr/P4YA201061100001.md): Cable · broken · Jun 7, 2010 · N801LR · Dhav DHC8101 · Landing Gear Retraction/Extension System > MLG RELEASE CABLE BROKEN. REPLACED MLG ALTERNATE RELEASE FIXED LENGTH NON-ADJUSTABLE CABLE WITH NEW CABLE PN: 83200506-003 IAW AMM 32-15-00. - [SDR CA100610001](https://openairdocs.org/sdr/CA100610001.md): Actuator · leaking · Apr 30, 2010 · Dhav DHC8101 · Drag Control Actuator > FLT CREW REPORTED LOSS OF NR 1 HYD SYS PRESSURE AT TAKEOFF. ABORTED TAKEOFF AND RETURNED TO GATE WITHOUT FURTHER INCIDENT. MX FOUND THE RT INBD SPOILER ACTUATOR LEAKING DUE TO FAILURE OF THE HSG. SPOILER ACTUATOR REPLACED. OPS CHECKS AND LEAK CHECKS CARRIE - [SDR CA090909001](https://openairdocs.org/sdr/CA090909001.md): Bearing · damaged · Aug 29, 2009 · Dhav DHC8101 · Propeller Blade Section > FLT CREW REPORTED ABNORMAL VIBRATION THROUGHOUT ACFT IN ALL PHASES OF FLIGHT. VIBRATION BECAME WORSE WITH PROPS AT MAX AND HIGHER TORQUE SETTINGS. ACFT LANDED WITHOUT FURTHER INCIDENT. AFTER LANDING, RT ENG NACELLE WAS FOUND TO BE COATED WITH FLUID. ALL ENG - [SDR CA081128001](https://openairdocs.org/sdr/CA081128001.md): Turbine · failed · Nov 25, 2008 · Dhav DHC8101 · Turbine Section > (CAN) PRIOR TO TAKEOFF, THE CREW FELT A THUD AND GRINDING NOISE FROM THE NR 2 ENGINE AT 70 PERCENT TORQUE. THE ENGINE WAS IMMEDIATELY SHUTDOWN, BUT BY THE TIME THE TORQUE REDUCED TO ZERO PSI AND THE ITT OF THE ENG REACHED UP TO 1200 DEGREE CELSIUS. ENG WAS IMM - [SDR FDKA200708388](https://openairdocs.org/sdr/FDKA200708388.md): Wire · damaged · Aug 15, 2007 · N926HA · Dhav DHC8101 · Light System Wiring > FDM 6014 JFK-SYR (0951 PHX LCL) - OVERHEAD CEILING ENERGENCY LIGHT INOP. MX REPAIRED WIRING TO LIGHT ASSY. - [SDR FDKA200708378](https://openairdocs.org/sdr/FDKA200708378.md): Light · inoperative · Aug 9, 2007 · N926HA · Dhav DHC8101 · Emergency Lighting > FDM 6175 ALB-JFK (0459 PHX LCL) - 2 FLOOR EMERGENCY STRIP LIGHTS INOP. MX RELAMPED LIGHT STRIPS. - [SDR FDKA200708358](https://openairdocs.org/sdr/FDKA200708358.md): Indicator · malfunctioned · Aug 2, 2007 · N802LR · Dhav DHC8101 · Trailing Flap Position Indicating System > FDM 6205 JFK-PVD (0555 PHX LCL) - PILOT REPORTED THAT THE FLAPS ONLY GO TO 4 DEGREES ON INDICATOR. MX REPLACED THE FLAP INDICATOR. - [SDR FDKA200708357](https://openairdocs.org/sdr/FDKA200708357.md): Flap System · malfunctioned · Aug 2, 2007 · N802LR · Dhav DHC8101 · Trailing Edge Flap Control System > FDM 6204 PVD-JFK (0555 PHX LCL) - PILOT ABORTED TAKEOFF DUE TO TAKEOFF CONFIG WANRING HORN ON ROLLOUT. MX RESET SYSTEM AND PERFORMED OPS CK OF FLAPS AND INDICATION SYSTEM; SYSTEM OPS CK GOOD AND NO DEFECTS WERE NOTED. - [SDR FDKA200707339](https://openairdocs.org/sdr/FDKA200707339.md): Ballast · malfunctioned · Jul 17, 2007 · N809LR · Dhav DHC8101 · Passenger Compartment Lighting > FDM 6023 JFK-BWI (1544 PHX LCL) - CAPTAIN REPORTED BURNING SMELL IN REAR CABIN. REMOVED AND REPLACED ROW 7DF SIDEWALL BALLAST AND OPS CHECKED GOOD. - [SDR HNAA0700144](https://openairdocs.org/sdr/HNAA0700144.md): Mount · broken · Jul 12, 2007 · N942HA · Dhav DHC8101 · Engine Mount Section > ENGINE REMOVED FROM A/C 942 HA IN MDT ON 7-3-07 RECEIVED AT SBY MAINTANCE SHOP. FOUND TORQUE MOUNT END BROKEN OFF. ENG S/N 12-42. - [SDR FDKA200707333](https://openairdocs.org/sdr/FDKA200707333.md): Bulb · burned out · Jul 9, 2007 · N808LR · Dhav DHC8101 · Emergency Lighting > FDM 6180 ALB-JFK. DURING GEAR EXTENSION INTO JFK, NLG DOWN AND LOCKED INDICATOR DID NOT ILLUMINATE. MX FOUND INDICATOR BULB BURNED OUT AND REPLACED. - [SDR CA070718001](https://openairdocs.org/sdr/CA070718001.md): Regulator · fluctuates · Jul 8, 2007 · Dhav DHC8101 · Engine Oil Pressure > (CAN) DURING FLIGHT, THE OIL PRESS INDICATOR NR 1 ENGINE, DROPPED TO 50 PSI. QRH DRILL COMPLETED, UNSCHEDULED LANDING COMPLETED. OIL PRESSURE REGULATOR ASSEMBLY REPLACED IAW AMM 71-01-50, SYSTEM TESTED SERVICEABLE AND AIRCRAFT RETURNED TO SERVICE. (TC NR 20070 - [SDR FDKA200707323](https://openairdocs.org/sdr/FDKA200707323.md): Arm · broken · Jul 4, 2007 · N806LR · Dhav DHC8101 · Passenger/Crew Doors > FDM 6023 JFK (1746 PHX LCL) - PASSENGER DOOR LT ARM BROKEN. MX RESECURED. - [SDR FDKA200706299](https://openairdocs.org/sdr/FDKA200706299.md): Plunger · lack of lube · Jun 23, 2007 · N802LR · Dhav DHC8101 · Gust Lock Damper System > FDM 6285 JFK (1100 PHX LCL) CREW REPORTED A GUST LOCK INOP. MX LUBED GUSTLOCK PLUNGER OPS GOOD. - [SDR FDKA200706260](https://openairdocs.org/sdr/FDKA200706260.md): Light · inoperative · Jun 4, 2007 · N809LR · Dhav DHC8101 · Emergency Lighting > FDM 6182 PVD (1732 PHX LCL) - REAR EMERGENCY ESCAPE PATH LIGHT OUT. MX RELAMPED. - [SDR FDKA200705255](https://openairdocs.org/sdr/FDKA200705255.md): Switch · dirty · May 30, 2007 · N802LR · Dhav DHC8101 · Trailing Flap Position Indicating System > FDM 6184 BWI-JFK (0428 PHX LCL). TAKEOFF CONFIG WARNING HORN ON TAKEOFF ROLL. MX CLEANED FLAP SWITCHES, OPS CHECKED GOOD. - [SDR FDKA200705221](https://openairdocs.org/sdr/FDKA200705221.md): Light · inoperative · May 22, 2007 · N809LR · Dhav DHC8101 · Emergency Lighting > FDM 6182 JFK (1309 PHX LCL) - CREW REPORTED THE FLOOR AFT FLOOD LIGHT INOP. MX RELAMPED. - [SDR FDKA200705216](https://openairdocs.org/sdr/FDKA200705216.md): Connector · dirty · May 20, 2007 · N808LR · Dhav DHC8101 · Flight Control System Wiring > FDM 6178 JFK (1415 PHX LCL) RETURNED TO GATE DUE TO RUDDER PRESS LIGHT FAILED TO ILLUMINATE. MX CLEANED CONNECTOR. - [SDR FDKA200705215](https://openairdocs.org/sdr/FDKA200705215.md): Relay · failed · May 20, 2007 · N808LR · Dhav DHC8101 · Rudder Control System > FDM 6205 RUDDER PRESS LIGHT FAILED TO ILLUMINATE. ACFT FERRIED TO JFK WHERE MX REPLACED RELAY, OPS CHECK WAS GOOD. - [SDR FDKA200705212](https://openairdocs.org/sdr/FDKA200705212.md): Switch · dirty · May 18, 2007 · N802LR · Dhav DHC8101 · Central Warning > FDM 6189 BDL. ABORTED T/O DUE TO T/O WARNING HORN GOES OFF ON T/O ROLL. MX CLEANED THROTTLE AND FLAP MICRO SWITCHES, OP CHECKS GOOD. - [SDR FDKA200705209](https://openairdocs.org/sdr/FDKA200705209.md): Switch · faulty · May 17, 2007 · N807LR · Dhav DHC8101 · Rudder Control System > FDM 6159 ALB-JFK (0500 PHX LCL). FLIGHT CREW REPORTED RUDDER FULL PRESS, RUDDER PRESS, & NR 2 RUDDER HYD CAUTION LIGHTS ILLUMINATED IN FLT. MX REMOVED AND REPLACED RUDDER HYD CUTOFF SWITCH. - [SDR FDKA200705198](https://openairdocs.org/sdr/FDKA200705198.md): Hydraulic System · contaminated · May 11, 2007 · N806LR · Dhav DHC8101 · Hydraulic System, Main > UPON FLAP EXTENSION RUD PRESS, RUD FULL PRESS, FLAP DRIVE & NR 1 ENG HYD PUMP CAUTION LIGHTS & FLAPS ARE SLOW TO EXTEND. MX BLED AIR FROM SYSTEM AND OPS CHECKED GOOD. - [SDR FDKA200705196](https://openairdocs.org/sdr/FDKA200705196.md): Light · broken · May 9, 2007 · N807LR · Dhav DHC8101 · Emergency Lighting > FDM RON JFK (1330 PHX LCL) - ROW 4 C/D EMERGENCY EXIT LIGHT BROKEN. MX REMOVED AND REPLACED EMERGENCY LIGHT ASSY. - [SDR FDKA200705190](https://openairdocs.org/sdr/FDKA200705190.md): Unknown · unknown · May 7, 2007 · N802LR · Dhav DHC8101 · Central Warning > ABORTED TAKEOFF DUE TO CONFIG WARN. CREW CYCLED ALL PARAMETERS, FAULT CLEARED. - [SDR FDKA200705189](https://openairdocs.org/sdr/FDKA200705189.md): Relay · inoperative · May 6, 2007 · N808LR · Dhav DHC8101 · Airfoil Anti/De-ice System > PITOT HEAT NR 1 LIGHT ILLUM AND BURNING ODOR IN THE FLIGHT DECK. MX REMOVED AND REPLACED RELAY CURRENT SENSOR. - [SDR FDKA200705182](https://openairdocs.org/sdr/FDKA200705182.md): Electronic Unit · malfunctioned · May 4, 2007 · N808LR · Dhav DHC8101 · Landing Gear Retraction/Extension System > FDM 6144 BWI-JFK (1103 PHX LCL) - CREW REPORTED THE NOSE POS IND LIGHT ILLUMINATED GEAR DIS LIGHT CAME ON DURING FLIGHT AND THE WOW FAIL LIGHT ILLUMINATED. MAINTENANCE REMOVED AND REPLACED PSEU. - [SDR FDKA200705183](https://openairdocs.org/sdr/FDKA200705183.md): Ground Wire · broken · May 4, 2007 · N805LR · Dhav DHC8101 · Emergency Lighting > FDM 6198 JFK-BTV (1247 PHX LCL). ROW 2 OVERHEAD EMERGENCY LIGHT INOP. MX REPAIRED BROKEN GROUND WIRE. - [SDR FDKA200704159](https://openairdocs.org/sdr/FDKA200704159.md): Indicator · failed · Apr 17, 2007 · N802LR · Dhav DHC8101 · Trailing Flap Position Indicating System > FDM 6208 PHL-JFK (1732 PHX LCL). AIRCRAFT RETURNED TO THE GATE DUE TO RIGHT STALL WARNING LIGHT. MX REMOVED AND REPLACED FLAP POSITION INDICATOR. Next page: https://openairdocs.org/model/bombardier-dhc-8-101/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 aircraft_model_key = 'DHC8101' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/model/bombardier-dhc-8-101/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.