# N8911E: 1966 Douglas DC-9-14, registration cancelled 2013-08-16

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: August 16, 2013
- Status when cancelled: Sale reported, canceled
- Airframe: [Douglas DC-9-14](https://openairdocs.org/model/douglas-dc-9-14) (registry code 3022034)
- Engine: [Pratt & Whitney JT8D-1](https://openairdocs.org/engine/pratt-whitney-jt8d-1) (registry code 52044)
- Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs)
- Serial number: 45825
- Year built: 1966
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: November 23, 1966
- Last registry action: February 7, 2012
- Mode S code: AC4B8B
- Location: [Mcminnville, OR](https://openairdocs.org/faa-place/OR/Mcminnville)
- Owner type: Individual
- Owner's area on the map: 45.2117° N, 123.2817° W: Placed by OpenAirDocs at the center of ZIP code 97128, within about 6 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N8911E
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=8911E
- Page: https://openairdocs.org/deregistered/N8911E-2013-08-16

From the FAA registry file of November 3, 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 Douglas DC-9-14: https://openairdocs.org/model/douglas-dc-9-14.md

## Service difficulty reports (41)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR 0400099152](https://openairdocs.org/sdr/0400099152), Jan 11, 2004: LINE. LEAKING. THE RT HYDRAULIC SYSTEM FLUID QUANTITY WAS LOST DURING THE TAKEOFF ROLL. THE TAKEOFF WAS ABORTED SAFELY AT 100 KTS AT IND. MAINTENANCE FOUND THE PRESSURE LINE O
- [SDR 0201189152](https://openairdocs.org/sdr/0201189152), Apr 18, 2002: INSULATION. OUT OF POSITION. JUST PRIOR TO THE FLIGHT LEVELING OFF AT FL290, THE CABIN PRESSURE WARNING LIGHT ILLUMINATED. CABIN ALTITUDE WAS 10,500 FEET WITH THE DIFFERENTIAL AT 5 PSI. CRE
- [SDR 9904269152](https://openairdocs.org/sdr/9904269152), Oct 12, 1999: BATTERIES. DISCHARGED. DURING LINE MAINTENANCE INSPECTION, FOUND CATWALK EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK NORMAL.
- [SDR 9904139152](https://openairdocs.org/sdr/9904139152), Oct 4, 1999: BATTERIES. DISCHARGED. FORWARD CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL.
- [SDR 9902079152](https://openairdocs.org/sdr/9902079152), Jun 13, 1999: BATTERY PACK. DISCHARGED. DURING LINE CHECK, FOUND CATWALK EMERGENCY EXIT PATH LIGHTING INOPERATIVE. MAINTENANCE REPLACED BATTERY PACK, OPERATIONAL CHECK OK.
- [SDR 9901719152](https://openairdocs.org/sdr/9901719152), May 10, 1999: BATTERY PACK. DISCHARGED. DURING LINE MAINTENANCE INSPECTION, FOUND PATHWAY CATWALK EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL.
- [SDR 9900329152](https://openairdocs.org/sdr/9900329152), Feb 5, 1999: FRAME. CRACKED. DURING PERIODIC CHECK, FOUND FRAME UPPER RIGHT CORNER SIDE CRACKED FS 83.5. REPAIRED PER EA 91-164891, REV A (P/N 9911505-7).
- [SDR 9804889152](https://openairdocs.org/sdr/9804889152), Mar 24, 1998: BATTERY. DISCHARGED. FLIGHT ATTENDANT REPORTED, EMERGENCY FLASHLIGHT AT ENTRY DOOR 1L INOPERATIVE. MAINTENANCE REPLACED BATTERY, OPERATIONAL CHECK OK.
- [SDR 9804899152](https://openairdocs.org/sdr/9804899152), Mar 23, 1998: BATTERY PACK. DISCHARGED. DURING LINE CHECK, FOUND LEFT NACELLE EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REPLACED BATTERY PACK, OPERATIONAL CHECK OK.
- [SDR 9802329152](https://openairdocs.org/sdr/9802329152), Feb 7, 1998: POWER SUPPLY. FAILED. DURING INSPECTION, THE EMERGENCY FLOOR PROXIMITY LIGHTS LOCATED IN FIRST CLASS SECTION WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHTS P
- [SDR 9800819152](https://openairdocs.org/sdr/9800819152), Jan 14, 1998: BATTERY PACK. DISCHARGED. DURING LINE MAINTENANCE INSPECTION, FOUND LEFT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY AND POWER SUPPLY, OPERATIONAL CHECK NORMAL.
- [SDR 9800809152](https://openairdocs.org/sdr/9800809152), Jan 14, 1998: BATTERY PACK. DISCHARGED. DURING LINE MAINTENANCE INSPECTION, FOUND OVERHEAD EMERGENCY LIGHT AT ROW 16 INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL.
- [SDR 9719289152](https://openairdocs.org/sdr/9719289152), Oct 15, 1997: POWER SUPPLY. INOPERATIVE. DURING LINE CHECK, FOUND COVE PANEL NOT INSTALLED AND EMERGENCY LIGHT POWER ASSEMBLY FAULTY. INSTALLED EMERGENCY LIGHT POWER ASSEMBLY AND INSTALLED COVE PANEL. 
- [SDR 9719779152](https://openairdocs.org/sdr/9719779152), Oct 11, 1997: PRESS PANEL. CRACKED. DURING L CHECK, FOUND CRACK IN NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE PANEL FS 83 INBOARD OF FRAME FITTING. REPAIRED PER EA 91-151749.
- [SDR 9719739152](https://openairdocs.org/sdr/9719739152), Oct 11, 1997: PRESS PANEL. CRACKED. DURING L CHECK, FOUND CRACKS IN THE NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE PANEL FS 110 AT THE INBOARD AND OUTBOARD VERTICAL FRAME ATTACH FITTINGS. RE
- [SDR 9710879152](https://openairdocs.org/sdr/9710879152), Jun 7, 1997: O-RING. DAMAGED. AFTER TAKEOFF, THE TOWER REPORTED THE LEFT ENGINE WAS SMOKING. ALL ENGINE INDICATIONS WERE NORMAL. AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT FURTHER INCIDENT.
- [SDR 9710759152](https://openairdocs.org/sdr/9710759152), Jun 3, 1997: BATTERIES. DISCHARGED. DURING LINE CHECK, FOUND OVERHEAD EMERGENCY LIGHTS VERY WEAK ON THE RIGHT REAR OF THE AIRCRAFT. REPLACED BATTERIES IN POWER PACK, OPERATIONAL CHECK OK.
- [SDR 9703199152](https://openairdocs.org/sdr/9703199152), Feb 4, 1997: CLIPS. OUT OF ADJUST. DURING LINE CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE TAILCONE RELEASE HANDLE FROM CLIPS. ALSO, FOUND SIX BEARING PLATES WORN. REPLACED BEARING
- [SDR 9625539152](https://openairdocs.org/sdr/9625539152), Nov 29, 1996: BATTERY. DISCHARGED. DURING LINE CHECK, FOUND FLOOR PROXIMITY LIGHTS FROM ROW 2 TO ROW 7 STAY ON FOR ONLY TEN SECONDS. REPLACED BATTERY AND OPERATION CHECKS GOOD.
- [SDR 9623989152](https://openairdocs.org/sdr/9623989152), Nov 3, 1996: BATTERIES. DISCHARGED. DURING LINE CHECK, FOUND AFT RIGHT HAND AISLE OVERHEAD LIGHT AND TAIL COMPARTMENT OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERIES IN POWER SUPPLY, OPER
- [SDR 9613299152](https://openairdocs.org/sdr/9613299152), Jun 16, 1996: BATTERY PACK. DISCHARGED. DURING LINE CHECK, FOUND TAIL COMPARTMENT OVERHEAD EMERGENCY LIGHTS AND AFT RIGHT AISLE OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK B5-28. ALL E
- [SDR 9611449152](https://openairdocs.org/sdr/9611449152), May 27, 1996: AMPLIFIER. MALFUNCTIONED. DURING CLIMBOUT, CABIN PRESSURE WARNING LIGHT ILLUMINATED WITH CABIN DECOMPRESSION. MASKS DEPLOYED, CABIN CONTROLLED MANUALLY AND ACFT RETURNED TO DSM AND LANDE
- [SDR 9607849152](https://openairdocs.org/sdr/9607849152), Apr 5, 1996: POWER SUPPLY. INOPERATIVE. DURING LINE CHECK, FOUND FORWARD EMERGENCY PATHWAY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY, OPERATIONAL CHECK GOOD.
- [SDR 9605119152](https://openairdocs.org/sdr/9605119152), Mar 4, 1996: VERT GYRO. FAILED. DURING CLIMBOUT, FIRST OFFICER'S VERTICAL GYRO FAILED. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED THE NR 2 VERTICAL GYRO AND CHECKED OK.
- [SDR 9604319152](https://openairdocs.org/sdr/9604319152), Feb 20, 1996: INDICATION. MALFUNCTIONED. ON APPROACH INTO MSP, THE LEFT MAIN GEAR SHOWED NO GREEN LIGHT UPON EXTENSION. RECYCLED GEAR AND INDICATIONS WERE NORMAL. AIRCRAFT LANDED WITHOUT INCIDENT. MAIN
- [SDR 9604569152](https://openairdocs.org/sdr/9604569152), Feb 16, 1996: LONGERON. CORRODED. DURING H-CHECK, FOUND CORROSION IN THE RIGHT WING STRINGERS 18, 21 AND 22 APPROXIMATELY STA 69 TO 91. REPAIRED PER EA 91-109380.
- [SDR 9604559152](https://openairdocs.org/sdr/9604559152), Feb 16, 1996: SKIN. CRACKED. DURING H-CHECK, FOUND A .375 INCH CRACK IN THE FORWARD ENTRY DOOR JAMB FS 199 AT THE 5TH STOP HOLE FROM THE BOTTOM. REPAIRED JAMB SKIN (P/N 5911406-59) PER EA 9
- [SDR 9604549152](https://openairdocs.org/sdr/9604549152), Feb 16, 1996: DOUBLER. CORRODED. DURING H-CHECK, FOUND CORROSION ON THE LEFT FUSELAGE WINDOW BELT DOUBLER AT FS 536 BETWEEN THE SKIN AND THE WINDOW RETAINER. REPAIRED DOUBLER (P/N 9911535) PER 
- [SDR 9604539152](https://openairdocs.org/sdr/9604539152), Feb 15, 1996: BLKHD DOOR JAMB. CRACKED. DURING H-CHECK, FOUND TWO CRACKS IN THE AFT CABIN DOOR JAMB SEAL RETAINER RING LEFT AND RIGHT SIDES AT APPROXIMATELY THE 3 AND 9 O'CLOCK POSITIONS. REPAIRED JAM
- [SDR 9603939152](https://openairdocs.org/sdr/9603939152), Feb 13, 1996: FITTING. CORRODED. DURING H-CHECK, FOUND CORROSION ON THE INTERCOSTAL END FITTING LOCATED IN THE FORWARD CARGO BIN FS 484 OUTBOARD OF LONGERON 28R. REPLACED FITTING PER SRM 51-30-
- [SDR 9603879152](https://openairdocs.org/sdr/9603879152), Feb 9, 1996: FITTING. CRACKED. DURING H-CHECK, FOUND A CRACK IN THE LONGERON 28R END FITTING AT FS 470. REPLACED FITTING PER SRM 51-30-2.
- [SDR 9604469152](https://openairdocs.org/sdr/9604469152), Feb 8, 1996: FITTING. CRACKED. DURING H-CHECK, FOUND A CRACK IN THE LOWER WING TO FUSELAGE ATTACH FITTING AT FS 494 BETWEEN LONGERONS 22L TO 23L. REPLACED FITTING (P/N 5910006-43) PER EA 91-1
- [SDR 9520999152](https://openairdocs.org/sdr/9520999152), Dec 13, 1995: TRAPEZOIDAL FTG. CRACKED. DURING SPECIAL MAINTENANCE VISIT, FOUND A CRACK IN THE RIGHT REAR SPAR TRAPEZOIDAL ATTACH FITTING. REPLACED FITTING (P/N 3912073-502) PER EM 5710-00028, SECTION
- [SDR 9520969152](https://openairdocs.org/sdr/9520969152), Dec 12, 1995: LONGERON. CORRODED. DURING SPECIAL MAINTENANCE VISIT, FOUND CORROSION ON THE LEFT WING STRINGER 12 LOWER FLANGE BETWEEN WS 91-111. REPAIRED STRINGER PER EA 91-104032.
- [SDR 9520939152](https://openairdocs.org/sdr/9520939152), Dec 11, 1995: CLIPS. CRACKED. DURING SPECIAL MAINTENANCE VISIT, FOUND CORROSION ON THE LEFT WING STATION 69 RIB TO STRINGER LOWER ATTACH CLIPS BETWEEN STRINGERS 15-17 AND A CRACK IN THE LEFT
- [SDR 9518989152](https://openairdocs.org/sdr/9518989152), Nov 23, 1995: EEL WIRE. BROKEN. THE EMERGENCY EXIT LIGHTS WOULD NOT ILLUMINATE IN FORWARD CABIN AREA. REPAIRED SPLICE AT ROW 1, OPERATIONAL CHECK OK.
- [SDR 9518829152](https://openairdocs.org/sdr/9518829152), Nov 17, 1995: EEL TRACK. OUT OF ADJUST. DURING PREFLIGHT CHECK, FOUND EMERGENCY FLOOR LIGHTING AT FORWARD CABIN GALLEY INOPERATIVE. FOUND FLOOR LIGHTING TRACK OUT OF ALIGNMENT, ADJUSTED TRACK AND OPER
- [SDR 9518409152](https://openairdocs.org/sdr/9518409152), Oct 19, 1995: CONNECTOR. CORRODED. DURING APPROACH AT 5,000 FEET, 160 KNOTS, AND FLAPS AT 20 DEGREES, STALL WARNING STICK SHAKER ACTIVATED. EXECUTED GO-AROUND PROCEDURES AND AN UNEVENTFUL LANDING
- [SDR 9506489152](https://openairdocs.org/sdr/9506489152), Apr 23, 1995: UPLOCK SWITCH. MALFUNCTIONED. DURING APPROACH INTO DTW, GEAR DOOR OPEN LIGHT REMAINED ON AFTER GEAR WAS EXTENDED FOR LANDING. EXECUTED GO-AROUND PROCEDURES AND PERFORMED EMERGENCY EXTENSION 
- [SDR 9506479152](https://openairdocs.org/sdr/9506479152), Apr 22, 1995: DOOR SWITCHES. CONTAMINATED. DURING APPROACH INTO RIC, LANDING GEAR DOOR OPEN LIGHT REMAINED ON AFTER GEAR EXTENSION. RECYCLED GEAR AND LIGHT STAYED ON. PERFORMED EMERGENCY GEAR EXTENSION P
- [SDR 9503379152](https://openairdocs.org/sdr/9503379152), Feb 28, 1995: TRANSMITTER. MALFUNCTIONED. THE NR 2 ENGINE OIL PRESSURE INDICATOR EXCEEDED NORMAL LIMITS ON TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AT 80 KTS AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENA

## FAA accident and incident reports (3)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 19901024055889I](https://openairdocs.org/incident/19901024055889I), Oct 24, 1990: Doug DC914 (N8911E), Detroit, MI. Lost pressurization en route. Made emergency descent. Replaced outflow valve and controller.
- [Incident 19850730041379I](https://openairdocs.org/incident/19850730041379I), Jul 30, 1985: Doug DC914 (N8911E), Memphis, TN. Returned to airport after engine shutdown due to oil screen light and high oil temperature. Metal in oil screen.
- [Incident 19830404028689I](https://openairdocs.org/incident/19830404028689I), Apr 4, 1983: Doug DC914 (N8911E), Milwaukee, WI. Taxied off ramp area into soft ground. Had to be towed onto the hard surface ramp.

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