# N811PH: Mcdonnell Douglas DC-9-82, registration cancelled 2018-03-07 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: March 7, 2018 - Status when cancelled: Registration expired, pending cancellation - Airframe: [Mcdonnell Douglas DC-9-82](https://openairdocs.org/model/mcdonnell-douglas-dc-9-82) (registry code 3022084) - Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (OpenAirDocs) - Serial number: 53181 - Type of aircraft: Fixed wing multi engine - Certificate issued: April 18, 2013 - Last registry action: April 18, 2013 - Mode S code: AB0E60 - Owner when cancelled: [Engage Aviation LLC](https://openairdocs.org/faa-owner/ENGAGE%20AVIATION%20LLC) - Location: [Sarasota, FL](https://openairdocs.org/faa-place/FL/Sarasota) - Owner type: Corporation - Owner's area on the map: 27.3258° N, 82.5600° W: Placed by OpenAirDocs at the center of ZIP code 34236, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N811PH - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=811PH - Page: https://openairdocs.org/deregistered/N811PH-2018-03-07 From the FAA registry file of October 29, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Mcdonnell Douglas DC-9-82: https://openairdocs.org/model/mcdonnell-douglas-dc-9-82.md ## Service difficulty reports (21) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR 20000425SH041](https://openairdocs.org/sdr/20000425SH041), Mar 30, 2000: WIRE. SHORTED. WHILE C/W SB 8-28-31, SPECIAL INSP OF FUEL TANK BONDING, MECH RECEIVED ELEC SHOCK WHEN HE TOUCHED FUEL PROBE WIRING HARNESS CONDUIT LOCATED BETWEEN STA YW189.0 - [SDR QXEA9900420](https://openairdocs.org/sdr/QXEA9900420), Feb 25, 1999: WIRE. BROKEN. PDX- AFT SMOKE DETECTOR LIGHT STAYS ON. MAINTENANCE REPAIRED BROKEN WIRES 2612-4A22 AT CONNECTION 2612-P2. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE - [SDR QXEA9801754](https://openairdocs.org/sdr/QXEA9801754), Nov 28, 1998: BATTERY. DISCHARGED. LEFT FORWARD FUSELAGE EMERGENCY LIGHT INOP. REPLACED BATTERY FOR EMERGENCY LIGHTING, OPERATION CHECK GOOD. - [SDR QXEA9800936](https://openairdocs.org/sdr/QXEA9800936), Jul 7, 1998: BATTERY. DISCHARGED. PDX- LEFT HAND FORWARD EXTERIOR EMERGENCY LIGHT IS INOP. INSPECTED AND FOUND BATTERY PACK 3351-PS1 MALFUNCTION. REPLACED BATTERY PACK. OPERATIONAL CHECKS GOOD. - [SDR QXEA9700895](https://openairdocs.org/sdr/QXEA9700895), Dec 9, 1997: SPRING STRUT. BENT. PDX - MAIN CABIN DOOR WOULD NOT OPEN ALL THE WAY. DEPLANED PASSENGERS THROUGH THE EMERGENCY EXIT. FOUND AFT GAS SPRING STRUT BENT. REPLACED SNUBBER, OPERATIONAL - [SDR QXEA9700894](https://openairdocs.org/sdr/QXEA9700894), Dec 9, 1997: DIVIDER. MALFUNCTION. RETURNED TO GATE WITH NR 2 ENGINE FUEL PRESSURE WARNING. REPLACED NR 2 FUEL FLOW DIVIDER, OPERATIONAL CHECK GOOD. - [SDR QXEA9700892](https://openairdocs.org/sdr/QXEA9700892), Dec 5, 1997: GAP SEALS. WORN. DURING FLIGHT AIRCRAFT REQUIRED SOME AILERON AND RUDDER TRIM TO FLY COORDINATED. THIS CAUSED THE AIRCRAFT TO BE HARD TO TURN LEFT, WORSE AT HIGHER SPEEDS. CHECK - [SDR QXEA9700875](https://openairdocs.org/sdr/QXEA9700875), Dec 3, 1997: WARNING LIGHT. ILLUMINATED. BTM - RETURN TO FIELD, MAIN CABIN DOOR LIGHT CAME ON AFTER TAKEOFF. LANDED WITHOUT INCIDENT. INSPECTED DOOR OPERATION. TESTED GOOD PER MEL PROCEDURE 52-2. FORCE - [SDR QXEA9700740](https://openairdocs.org/sdr/QXEA9700740), Nov 5, 1997: LAMP. FAILED. PDX- ONE RED EMERGENCY FLOOR PATH LIGHT INOP. RELAMPED, OPERATIONAL CHECKS GOOD. - [SDR QXEA9700629](https://openairdocs.org/sdr/QXEA9700629), Oct 2, 1997: DOORS. CRACKED. PDX- BOTH NOSE LANDING GEAR DOORS ARE DAMAGED (FORWARD DOORS), AND CRACKED. REPLACED BOTH FORWARD NOSE GEAR DOORS, OPERATIONAL CHECKS GOOD. DOORS (S/N 22BAC083) - [SDR QXEA9700543](https://openairdocs.org/sdr/QXEA9700543), Sep 2, 1997: AUTOFEATHER TEST. FAILED. BOI - AUTO FEATHER TEST FAILED PRIOR TO DEPARTURE. NO ARM, OR UPTRIM, OR AUTO FEATHER LIGHTS. PERFORMED GROUND TEST OF AUTO FEATHER AND POWER UPTRIM. NO DEFECTS - [SDR QXEA9700189](https://openairdocs.org/sdr/QXEA9700189), May 16, 1997: LIGHT. INOPERATIVE. EMERGENCY HANDHELD OVERHEAD LIGHT INOP. REMOVED AND REPLACED COCKPIT HANDHELD LIGHT, OPERATIONAL CHECKS GOOD. - [SDR QXEA9700166](https://openairdocs.org/sdr/QXEA9700166), May 2, 1997: MECHANISM. OUT OF ADJUST. MAIN CABIN DOOR HANDLE UNLATCHED IN FLIGHT. FLIGHT ATTENDANT REPORTED THAT DOOR OPENED APPROX 1 INCH. ADJUSTED DOOR LIFT MECHANISM, DOOR STOP BOLTS, AND DOOR SE - [SDR QXEA9700156](https://openairdocs.org/sdr/QXEA9700156), Apr 26, 1997: POWER SUPPLY. INOPERATIVE. EMERGENCY EXIT LIGHTS ARE INOP. REPLACED 2 POWER SUPPLIES, OPERATIONAL CHECKS GOOD. - [SDR QXEA9700007](https://openairdocs.org/sdr/QXEA9700007), Jan 4, 1997: CONTROL BOX. MALFUNCTIONED. EMERGENCY LIGHTS WILL NOT SHUTOFF WITH COCKPIT SWITCH IN THE OFF POSITION. CONTROL BOX FOR THE EMERGENCY LIGHTS WAS REPLACED AND EMERGENCY LIGHTS OPS CHECKED GO - [SDR QXEA9600266](https://openairdocs.org/sdr/QXEA9600266), Jul 26, 1996: POWER SUPPLY. INOPERATIVE. SEA - SOME OF THE EMERGENCY LIGHTS WERE NOTED AS BEING DIM. POWER SUPPLY PS1 REPLACED AND LIGHTS OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. - [SDR QXEA9600263](https://openairdocs.org/sdr/QXEA9600263), Jul 23, 1996: CONNECTOR. DISCONNECTED. PSC - EMERGENCY STRIP LIGHTS DS1 THROUGH DS4 ARE INOPERATIVE. WIRE CONNECTOR FOUND DISCONNECTED, RECONNECTED AND LIGHTS OPS CHECKED GOOD. AIRCRAFT RETURNED TO S - [SDR QXEA9600182](https://openairdocs.org/sdr/QXEA9600182), May 28, 1996: WIRE. BROKEN. SEA - FLOOR PROXIMITY LIGHTING FORWARD LIGHT IS INOPERATIVE. WIRES AT LAMP SOCKET REPAIRED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. - [SDR QXEA9600150](https://openairdocs.org/sdr/QXEA9600150), Apr 16, 1996: POWER SUPPLY. INOPERATIVE. SEVERAL EMERGENCY LIGHTS FAILED TO ILLUMINATE. UPPER POWER SUPPLY IN COAT CLOSET REPLACED, LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. - [SDR QXEA9600148](https://openairdocs.org/sdr/QXEA9600148), Apr 13, 1996: POWER SUPPLY. FAILED. EMERGENCY LIGHT POWER SUPPLY IN COAT CLOSET THE LOWER PACK FAILED SHORTLY AFTER INSTALLATION. POWER SUPPLY AND BATTERY REPLACED AND POWER SUPPLY, OPS CHECKED GO - [SDR QXEA9600147](https://openairdocs.org/sdr/QXEA9600147), Apr 13, 1996: POWER SUPPLY. SHORTED. BURNT ELECTRICAL SMELL COMING FROM COCKPIT AND COAT CLOSET AREA. LOWER EMERGENCY LIGHT POWER SUPPLY IN THE COAT CLOSET REPLACED. POWER SUPPLY OPS, CHECKED GOOD. --- 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.