# Service difficulty reports: N14816, cancelled Jul 5, 2006 A list on [N14816, cancelled Jul 5, 2006](https://openairdocs.org/deregistered/N14816-2006-07-05.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 · 78 reports - [SDR P9RA20050079](https://openairdocs.org/sdr/P9RA20050079.md): Girt Bar · dirty · May 13, 2005 · N14816 · Doug DC982 · Escape Slide > SFB GATE ITEM P1, L2 DOOR WILL NOT DISARM. CLEANED AND LUBRICATED GIRT BAR IAW MM. OPERATIONAL CHECKED NORMAL. - [SDR P9RA20040058](https://openairdocs.org/sdr/P9RA20040058.md): Light · inoperative · Dec 23, 2004 · N14816 · Doug DC982 · Emergency Lighting > A/C IN SYR, PORTABLE E-LIGHT SWITCH NOT FUNCTIONAL. REMOVED AND REPLACED PORTABLE E-LIGHT PER MD-80 MM 33-50-00. OPS CHECK NORMAL. - [SDR P9RA](https://openairdocs.org/sdr/P9RA.md): Light · inoperative · Dec 23, 2004 · N14816 · Doug DC982 · Emergency Lighting > A/C IN SYR. PORTABLE E-LIGHT SWITCH NOT FUNCTIONAL. REMOVED AND REPLACED PORTABLE E-LIGHT PER MD-80 MM 33-50-00. OPS CHECK NORMAL. - [SDR P9RA20040047](https://openairdocs.org/sdr/P9RA20040047.md): Power Supply · inoperative · Oct 12, 2004 · N14816 · Doug DC982 · Emergency Lighting > AIRCRAFT IN MAINTENANCE, SYR. EMERGENCY LIGHT AT ROW 28 INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY IAW MM. - [SDR P9RA20040046](https://openairdocs.org/sdr/P9RA20040046.md): Power Supply · inoperative · Oct 12, 2004 · N14816 · Doug DC982 · Emergency Lighting > AIRCRAFT IN MAINTENANCE, SYR. EMERGENCY LIGHTS INOPERATIVE AT ROW 26. REMOVED AND REPLACED POWER SUPPLY IAW MM. - [SDR P9RA20040045](https://openairdocs.org/sdr/P9RA20040045.md): Battery · weak · Sep 29, 2004 · N14816 · Doug DC982 · Emergency Lighting > AIRCRAFT IN MAINTENANCE, SYR, 4 INTERIOR EMERGENCY LIGHTS ARE VERY DIM. REMOVED AND REPLACED BATTERIES IN 4 SEPARATE POWER SUPPLIES IAW MM. - [SDR P9RA20040023](https://openairdocs.org/sdr/P9RA20040023.md): Proximity Switch · sticking · Jul 29, 2004 · N14816 · Doug DC982 · Tail Cone Doors > IB FLIGHT, APPROXIMATELY 10 MINUTES BEFORE LANDING, TAIL CONE ANNUNCIATOR ILLUMINATED AND REMAINED ON. QRH PROCEDURE FOLLOWED. NO EMERGENCY DECLARED. UNEVENTFUL LANDING. FOUND DOOR PROXIMITY SWITCH STICKING. CLEANED AND LUBRICATED SWITCH.NO OTHER DEFECTS NO - [SDR P9RA20040020](https://openairdocs.org/sdr/P9RA20040020.md): Charger · inoperative · Jul 15, 2004 · N14816 · Doug DC982 · Emergency Lighting > IN INSPECTION, VARIOUS EMERGENCY EXIT LIGHTS OUT OVERHEAD. REMOVED AND REPLACED 3 BATTERY CHARGERS SERIAL NUMBERS 5227 15955 21872 AND AND 4 EMERGENCY BATTERIES PART NUMBER 5014. - [SDR P9RA20040014](https://openairdocs.org/sdr/P9RA20040014.md): Slide · out of position · May 31, 2004 · N14816 · Doug DC982 · Escape Slide > AT GATE IN CZM, THE L1 DOOR SLIDE FELL OUT OF ITS COVER. REINSTALLED L1 DOOR SLIDE COVER. - [SDR CALA0300280](https://openairdocs.org/sdr/CALA0300280.md): Compressor · failed · Jun 1, 2003 · N14816 · Doug DC982 · Engine (Turbine/Turboprop) > THE AIRFRAME SHUDDERED SLIGHTLY AND WAS ACCOMPANIED BY AN AUDIBLE BOOM AFTER TAKEOFF FROM IAH AT ABOUT 3,000 FEET. THE NR 1 ENGINE SUBSEQUENTLY AUTO SHUTDOWN. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. INITIAL FINDINGS REVEALED METAL - [SDR CALA0300169](https://openairdocs.org/sdr/CALA0300169.md): Frame · cracked · Apr 5, 2003 · N14816 · Doug DC982 · Fuselage Main, Frame > INSPECTION FOUND A 1 INCH CRACK IN FRAME AT STA 1418, L2L TO L2R. REMOVED AND REPLACED BELTFRAME IAW SRM 51-30-05. - [SDR CALA0100431](https://openairdocs.org/sdr/CALA0100431.md): Charger · inoperative · Apr 29, 2001 · N14816 · Doug DC982 · Emergency Lighting > EMERGENCY LIGHTS AT REAR GALLEY DOOR AND TAIL CONE DOOR INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY VASE PER MM 33-53-00 PG 407. - [SDR CALA0001870](https://openairdocs.org/sdr/CALA0001870.md): Skin · dented · Dec 7, 2000 · N14816 · Doug DC982 · Cargo/Baggage Doors > INSPECTION FOUND AFT CARGO DOOR OUTER SKIN DENTED AT CENTER OF DOOR 15 INCHES FROM FORWARD EDGE. THE DENTED AREA WAS REMOVED AND DOUBLER AND FILLER WERE INSTALLED IAW SRM 52-05, FIGURE 2 AND 51-10-3. - [SDR CALA0001851](https://openairdocs.org/sdr/CALA0001851.md): Doubler · damaged · Dec 2, 2000 · N14816 · Doug DC982 · Elevator, Plate/Skin > INSPECTION FOUND LT ELEVATOR TIP TRAILING EDGE DOUBLER DAMAGED. THE DOUBLER WAS REPLACED IAW SRM 51-10-2 AND 51-30-8. - [SDR CALA0001850](https://openairdocs.org/sdr/CALA0001850.md): Doubler · damaged · Dec 2, 2000 · N14816 · Doug DC982 · Elevator, Plate/Skin > INSPECTION FOUND LT ELEVATOR TIP TRAILING EDGE DOUBLER DAMAGED. THE DOUBLER WAS REPLACED IAW SRM 51-10-2 AND 51-30-8. - [SDR CALA0001841](https://openairdocs.org/sdr/CALA0001841.md): Skin · dented · Nov 29, 2000 · N14816 · Doug DC982 · Fuselage Main, Plate/Skin > INSPECTION FOUND FUSELAGE SKIN DENTED TWENTY INCHES BELOW LEFT PITOT PROBE AT FS 69.5. THE DENT WAS WORKED OUT TO ORIGINAL CONTOUR WITH NO CRACKS NOTED PER HFEC IAW MM 20-30-00. A PERMANENT REPAIR WAS ACCOMPLISHED IAW SRM 53-04, FIGURE 38. - [SDR CALA0001840](https://openairdocs.org/sdr/CALA0001840.md): Casting · cracked · Nov 28, 2000 · N14816 · Doug DC982 · Wing Miscellaneous Structure > INSPECTION FOUND LT WING TIP LEADING EDGE CASTING CRACKED WITH POPPED RIVETS AND GOUGES. THE CASTING PANEL WAS REMOVED AND A NEW CASTING PANEL WAS INSTALLED IAW SRM 51-30-2 AND 51-10-4. - [SDR CALA0001839](https://openairdocs.org/sdr/CALA0001839.md): Cargo Track · corroded · Nov 28, 2000 · N14816 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND AFT PIT LT CARGO TRACK CORRODED. THE CARGO TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-10-3, 51-30-1, AND 51-30-5. - [SDR CALA0001838](https://openairdocs.org/sdr/CALA0001838.md): Skin · corroded · Nov 28, 2000 · N14816 · Doug DC982 · Cargo/Baggage Doors > INSPECTION FOUND AFT CARGO DOOR INNER SKIN CORRODED AROUND RIVET NUTS. THE CORROSION WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 51-10-3 AND 52-05, FIGURE 7. - [SDR CALA0001836](https://openairdocs.org/sdr/CALA0001836.md): Floor Support · broken · Nov 24, 2000 · N14816 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND FORWARD CARGO COMPARTMENT LT FLOORBEAM SUPPORT BROKEN AT FS 294. THE FLOORBEAM SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-2, 51-30-5, AND 51-10-4. - [SDR CALA0001817](https://openairdocs.org/sdr/CALA0001817.md): Support Bracket · corroded · Nov 22, 2000 · N14816 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND AFT CARGO PIT LT VERTICAL SUPPORT TO FLOOR TRANSITION PANEL CORRODED AT STA 1155 - 1212. THE VERTICAL SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-10-3 AND 53-01, FIGURE 1. - [SDR CALA0001816](https://openairdocs.org/sdr/CALA0001816.md): Angle · cracked · Nov 21, 2000 · N14816 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND AN 8 INCH CRACK IN FORWARD CARGO DOOR SEAL FLANGE OPEN LOCK ANGLE. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2, 51-10-4, 51-10-3, AND 51-30-1. - [SDR CALA0001814](https://openairdocs.org/sdr/CALA0001814.md): Fitting · dented · Nov 20, 2000 · N14816 · Doug DC982 · Leading Edge Devices > INSPECTION FOUND LT WING NR 5 SLAT END FITTING DENTED. THE SLAT END FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51-10-4 AND 51-10-3. - [SDR CALA0001813](https://openairdocs.org/sdr/CALA0001813.md): Strap · corroded · Nov 20, 2000 · N14816 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND FORWARD CARGO COMPARTMENT DOOR JAMB FORWARD TORQUE BOX LINER RETAINING STRAP CORRODED AND WORN AT STA 370. THE STRAP WAS REMOVED AND A NEW STRAP WAS INSTALLED IAW SRM 51-30-1 AND 51-10-3. - [SDR CALA0001812](https://openairdocs.org/sdr/CALA0001812.md): Web · corroded · Nov 20, 2000 · N14816 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND CUSP WEB DOUBLER CORRODED AT STA 207-218, L18L. A NEW DOUBLER WAS INSTALLED IAW SRM 53-01-1, 51-10-3, AND 51-30-5. - [SDR CALA0001810](https://openairdocs.org/sdr/CALA0001810.md): Cargo Track · corroded · Nov 20, 2000 · N14816 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND MID CARGO LT TIE DOWN TRACK CORRODED AT STA 522 - 786. THE TIE DOWN TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-1, 51-10-4, AND 51-10-3. - [SDR CALA0001809](https://openairdocs.org/sdr/CALA0001809.md): Stiffener · cracked · Nov 20, 2000 · N14816 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND A 1.5 INCH CRACK IN APB VERTICAL STIFFENER AT BL 0 ABOVE AFT ENTRANCE DOOR AT UPPER CORNER. THE STIFFENER WAS REMOVED AND A NEW STIFFENER WAS INSTALLED IAW SRM 51-30-1, 51-10-4, 51-10-3, 51-30-5, 51-20-0, AND 51-30-2. - [SDR CALA0001807](https://openairdocs.org/sdr/CALA0001807.md): Cargo Track · corroded · Nov 20, 2000 · N14816 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND FORWARD CARGO COMPARTMENT RT CARGO TIE DOWN TRACK CORRODED AT STA 218 - 370. THE TIE DOWN TRACK WAS REMOVED AND A NEW TIE DOWN TRACK WAS INSTALLED IAW SRM 51-30-1, 51-10-4, AND 51-10-3. - [SDR CALA0001805](https://openairdocs.org/sdr/CALA0001805.md): Skin · cracked · Nov 19, 2000 · N14816 · Doug DC982 · Horizontal Stabilizer, Plate/Skin > INSPECTION FOUND A 1.5 INCH CRACK AND BEND IN LT HORIZONTAL STABILIZER TIP O/B LOWER AFT CORNER SKIN. A REPAIR DOUBLER WAS INSTALLED IAW SRM 55-11-0, 51-30-2, AND 51-30-3. - [SDR CALA0001804](https://openairdocs.org/sdr/CALA0001804.md): Frame · cracked · Nov 19, 2000 · N14816 · Doug DC982 · Fuselage Main, Structure > INSPECTION FOUND A 3 INCH CRACK IN FRAME FOR LEFT VENTRAL STAIRS SIDEWALL PANEL. THE SIDEWALL SUPPORT WAS REMOVED AND THE CRACK WAS STOP DRILLED IAW SRM 51-30-1, 51-30-2, AND 53-01. REPAIR ANGLES WERE INSTALLED IAW SRM 51-30-2. INSTALLED SIDEWALL SUPPORT IA - [SDR CALA0001803](https://openairdocs.org/sdr/CALA0001803.md): Doubler · bent · Nov 19, 2000 · N14816 · Doug DC982 · Landing Gear Doors > INSPECTION FOUND LEFT AFT NLG DOOR DOUBLER BENT AND SEPARATED AT AFT LOWER SECTION. THE DAMAGED DOUBLER WAS REMOVED AND A NEW DOUBLER WAS INSTALLED IAW SRM 51-30-2. - [SDR CALA0001802](https://openairdocs.org/sdr/CALA0001802.md): Skin · corroded · Nov 19, 2000 · N14816 · Doug DC982 · Cargo/Baggage Doors > INSPECTION FOUND MID CARGO DOOR INNER SKIN CORRODED AROUND RIVET NUTS. THE RIVET NUTS WERE REMOVED. A DOUBLER AND RIVET NUTS WERE INSTALLED IAW SRM 51-30-1, 52-01, FIGURE 2, AND 51-30-2. - [SDR CALA0001801](https://openairdocs.org/sdr/CALA0001801.md): Skin · gouged · Nov 18, 2000 · N14816 · Doug DC982 · Trailing Edge Flaps > INSPECTION FOUND RIGHT WING FLAP T/E PANEL 1613 SKIN GOUGED AND PITTED. THE SKIN SECTION WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 57-50-14. - [SDR CALA0001800](https://openairdocs.org/sdr/CALA0001800.md): Channel · torn · Nov 17, 2000 · N14816 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND AFT EMERGENCY EXIT RAMP UPPER LEFT RAIL CHANNEL EDGE TORN AT FS 1474 WITH A LARGE DENT 20 INCHES AFT. THE TORN EDGE WAS BLENDED OUT AND REPAIR DOUBLERS AND ANGLES WERE INSTALLED IAW SRM 53-01, FIGURE 1 & 2, 51-10-4, 51-10-3, AND 51-30-2. THE - [SDR CALA0001797](https://openairdocs.org/sdr/CALA0001797.md): Stop · chafed · Nov 17, 2000 · N14816 · Doug DC982 · Cargo/Baggage Doors > INSPECTION FOUND MID CARGO DOOR STOP NR 12 CHAFED. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5330-02819. - [SDR CALA0001796](https://openairdocs.org/sdr/CALA0001796.md): Rib · gouged · Nov 17, 2000 · N14816 · Doug DC982 · Wing, Rib/Bulkhead > INSPECTION FOUND LEFT WING O/B EDGE OF RIB GOUGED AT NR 15 SLAT TRACK CUTOUT. THE RIB WAS REMOVED AND A NEW RIB WAS INSTALLED IAW SRM 51-30-2, 51-30-6, 51-30-4, 51-10-3, AND 51-30-5. - [SDR CALA0001795](https://openairdocs.org/sdr/CALA0001795.md): Skin · gouged · Nov 17, 2000 · N14816 · Doug DC982 · Landing Gear Doors > INSPECTION FOUND LT FORWARD NLG DOOR SKIN GOUGED AT FORWARD UPPER CORNER. THE GOUGED AREA WAS REMOVED IAW SRM 52-01, FIGURE 1. REPAIR PARTS WERE INSTALLED IAW SRM 52-01, 52-84-0, 51-10-3, AND 51-30-2. - [SDR CALA0001794](https://openairdocs.org/sdr/CALA0001794.md): Floor Support · corroded · Nov 17, 2000 · N14816 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 180, RBL 12 - RBL 42. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2, 51-10-4, 51-10-3, AND 51-30-5. - [SDR CALA0001793](https://openairdocs.org/sdr/CALA0001793.md): Structure · corroded · Nov 17, 2000 · N14816 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND SUB FLOOR WEB CORRODED AT STA 165 - 200, LBL 52. THE SUB FLOOR WAS REMOVED AND A NEW SUB FLOOR WAS INSTALLED IAW SRM 53-01, FIGURE 1, 53-05, FIGURE 1, 51-10-3, 51-30-5, AND 51-30-2. - [SDR CALA0001792](https://openairdocs.org/sdr/CALA0001792.md): Floor Support · corroded · Nov 17, 2000 · N14816 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND FLOOR SUPPORT CORRODED ON LOWER SURFACE AT STA 218 - 256, LBL 14. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-5 AND 51-10-4. - [SDR CALA0001791](https://openairdocs.org/sdr/CALA0001791.md): Floor Support · corroded · Nov 17, 2000 · N14816 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 160 - 200, RBL 44 AND AT STA 148 - 200, RBL 7. THE FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW SRM 51-30-2, 51-30-5, 51-10-4, 51-10-3, AND 51-30-1. - [SDR CALA0001790](https://openairdocs.org/sdr/CALA0001790.md): Floor Support · corroded · Nov 17, 2000 · N14816 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 200, RBL 9 - RBL 45 AND AT LBL 5 - RBL 5. THE FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW SRM 51-30-5 AND 51-10-3. - [SDR CALA0001789](https://openairdocs.org/sdr/CALA0001789.md): Skin · gouged · Nov 17, 2000 · N14816 · Doug DC982 · Landing Gear Doors > INSPECTION FOUND RT MLG FORWARD DOOR SKIN GOUGED AT FORWARD UPPER CORNER. THE GOUGED AREA WAS REMOVED AND REPAIR PARTS WERE INSTALLED IAW SRM 52-01, FIGURE 1, 52-84-0, AND 51-10-3. - [SDR CALA0001788](https://openairdocs.org/sdr/CALA0001788.md): Stop · chafed · Nov 17, 2000 · N14816 · Doug DC982 · Cargo/Baggage Doors > INSPECTION FOUND MID CARGO DOOR STOPS NR 3, 4, 6 & 8 CHAFED. REPAIR DOUBLERS WERE INSTALLED IAW ECRA 5330-02819. - [SDR CALA0001787](https://openairdocs.org/sdr/CALA0001787.md): Fitting · corroded · Nov 17, 2000 · N14816 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND GALLEY SUPPORT FITTING CORRODED AT STA 216, RBL 55. THE FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51-30-2, 51-10-4, 51-10-3, 51-30-5. - [SDR CALA0001786](https://openairdocs.org/sdr/CALA0001786.md): Fitting · corroded · Nov 17, 2000 · N14816 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND RT FRAME TO FLOOR FITTING CORRODED AT STA 579, LONGERON 18R. THE FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51-10-3, 51-30-5, AND 51-30-1. - [SDR CALA0001785](https://openairdocs.org/sdr/CALA0001785.md): Skin · dented · Nov 17, 2000 · N14816 · Doug DC982 · Fuselage Main, Plate/Skin > INSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AT FS 1185, LONGERON 18L. A REPAIR DOUBLER WAS INSTALLED IAW EA 9-5331-2-A0800. - [SDR CALA0001777](https://openairdocs.org/sdr/CALA0001777.md): Angle · corroded · Nov 16, 2000 · N14816 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND FLOOR SUPPORT ANGLE AND PLATE CORRODED AT FS 148 - 200, RBL 55. THE ANGLE AND PLATE WERE REMOVED AND A NEW ANGLE AND PLATE WERE INSTALLED IAW SRM 51-30-2 AND 51-10-4. - [SDR CALA0001776](https://openairdocs.org/sdr/CALA0001776.md): Web · cracked · Nov 16, 2000 · N14816 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND TWO, 1 INCH CRACKS IN E&E COMPARTMENT CABIN PRESSURE WEB AT STA 190, RBL 48. A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-01, 51-30-3, AND 51-30-2. - [SDR CALA0001773](https://openairdocs.org/sdr/CALA0001773.md): Skin · gouged · Nov 15, 2000 · N14816 · Doug DC982 · Trailing Edge Flaps > INSPECTION FOUND RT WING NR 4 FLAP O/B TRAILING EDGE SKIN GOUGED. A DOUBLER WAS INSTALLED IAW SRM 57-01, FIGURE 3, 51-10-3, AND 51-30-2. Next page: https://openairdocs.org/deregistered/N14816-2006-07-05/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 = 'N14816' AND deregistration_id = 'N14816-2006-07-05' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N14816-2006-07-05/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.