# N995UA: 1980 Boeing 737-291, registration cancelled 2004-06-04

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: June 4, 2004
- Exported to: Indonesia
- Status when cancelled: Valid registration
- Airframe: [Boeing 737-291](https://openairdocs.org/model/boeing-737-291) (registry code 138448W)
- Engine: [Pratt & Whitney JT8D-17 series](https://openairdocs.org/engine/pratt-whitney-jt8d-17-series) (registry code 52049)
- Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs)
- Serial number: 22399
- Year built: 1980
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: December 15, 1980
- Certificate issued: May 7, 2004
- Last registry action: May 7, 2004
- Mode S code: ADE6F9
- Owner when cancelled: [Fort Lauderdale Aerospace Inc](https://openairdocs.org/faa-owner/FORT%20LAUDERDALE%20AEROSPACE%20INC)
- Location: [Plantation, FL](https://openairdocs.org/faa-place/FL/Plantation)
- Owner type: Corporation
- Owner's area on the map: 26.1125° N, 80.2749° W: Placed by OpenAirDocs at the center of ZIP code 33324, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N995UA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=995UA
- Page: https://openairdocs.org/deregistered/N995UA-2004-06-04

From the FAA registry file of November 7, 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 Boeing 737-291: https://openairdocs.org/model/boeing-737-291.md

## Service difficulty reports (11)

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

- [SDR 2001UALA01876](https://openairdocs.org/sdr/2001UALA01876), Aug 30, 2001: LINKAGE. DAMAGED. NR 1 ENGINE SHUTDOWN DUE TO THROTTLE CONTROL PROBLEM. *S/D* FOUND THE THROTTLE LINKAGE DISCONNECTED. REINSTALLED THE LINKAGE AND TRIMMED THE FUEL CONTROL.
- [SDR 2001UALA00369](https://openairdocs.org/sdr/2001UALA00369), Mar 29, 2001: KEELBEAM. DAMAGED. DAMAGED AREAS AT KEEL BEAM STA 680 AND STA 708. REPLACES FASTENERS AT DAMAGED AREAS. MAJOR REPAIR ACCOMPLISHED.
- [SDR 2001UALA00321](https://openairdocs.org/sdr/2001UALA00321), Mar 26, 2001: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT HAS CORROSION AROUND FASTENER HOLES AT RBL 20 AND BETWEEN STA 967 AND STA 986. REMOVED CORRODED FLOOR SUPPORT. FABRICATED, ALODINED, PRIMED, AND I
- [SDR 2000UALA00806](https://openairdocs.org/sdr/2000UALA00806), Dec 23, 2000: BULLET. SEPARATED. ENGINE COMPRESSOR STALL ON TAKEOFF. *S/D* THE STALL WAS CAUSED BY THE NR 2 ENGINE NOSE DOME BEING LIBERATED FROM THE FRONT ACCESSORY SUPPORT. THE ACCESSORY SUPP
- [SDR 2000UALA00680](https://openairdocs.org/sdr/2000UALA00680), Nov 13, 2000: COALESCER BAG. CONTAMINATED. SMOKE SMELL IN THE PASSENGER CABIN. SUPPLEMENTAL DATA UPDATE NO FAULT FOUND. REPLACED COALESCER BAG AS PRECAUTION.
- [SDR 2000UALA00488](https://openairdocs.org/sdr/2000UALA00488), Aug 17, 2000: LIGHT. INOPERATIVE. SERVICE DOOR EMERGENCY EXIT LIGHT INOPERATIVE. FOUND EMERGENCY LIGHT ASSEMBLY DETACHED. RE-INSTALLED EMERGENCY LIGHT.
- [SDR 96UAL900630](https://openairdocs.org/sdr/96UAL900630), Aug 14, 1996: CONTROL UNIT. FAILED. ENGINE WOULD NOT DEVELOP TAKEOFF THRUST, WOULD GO NO HIGHER THAN 96.5 PERCENT N-1. ABORTED TAKEOFF. *S/D* FUEL CONTROL UNIT FAILED. REPLACED FUEL CONTROL UNIT C
- [SDR 96UAL900521](https://openairdocs.org/sdr/96UAL900521), Jul 11, 1996: BOOST PUMP CB. TRIPPED. THE LEFT HAND CENTER TANK FUEL BOOST PUMP PREVIOUSLY INOP ON CLIMB DUE TO POPPED CIRCUIT BREAKER, THE RIGHT CENTER TANK BOOST PUMP CIRCUIT BREAKER POPPED. RETUR
- [SDR 96UAL900304](https://openairdocs.org/sdr/96UAL900304), May 1, 1996: YAW COUPLER. MALFUNCTION. DURING TEN DEGREE RIGHT TURN EXPERIENCED FULL YAW DAMPER DEFLECTION TO THE LEFT. AUTOPILOT WAS ON, RUDDER AND AILERON TRIM WERE SET AT ZERO. SIGNIFICANT AILERON
- [SDR 95UAL900190](https://openairdocs.org/sdr/95UAL900190), Oct 10, 1995: CIRCUIT BREAKERS. HOT. AFTER PUSH-BACK ON ENGINE START, HAD A HOT ELECTRICAL SMELL FROM GALLEY AREA. SMELL CAME FROM AREA OF CIRCUIT BREAKERS ON FORWARD WALL OF AFT GALLEY. WALL WAS W
- [SDR 95UAL737030](https://openairdocs.org/sdr/95UAL737030), Mar 17, 1995: SEAL PLATE. FAILED. B-SYSTEM HYDRAULIC LOW QUANTITY LIGHT CAME ON AND A SYSTEM QUANTITY DROPPED TO 1.25 GALLONS. B-SYSTEM LOW PRESSURE LIGHT DID NOT COME ON, BUT AUTO PILOT WOULD N

## FAA accident and incident reports (1)

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 19910929054839I](https://openairdocs.org/incident/19910929054839I), Sep 29, 1991: Boeing 737200 (N995UA), Wichita, KS. Oil pressure drop on NR2 engine. Declared emergency. Shut engine down. ATC vectored pilot to Wichita.

## Other aircraft with N995UA

- [Registered now](https://openairdocs.org/aircraft/N995UA): Tuffwing UAV MAPPER, S/N TWF-02

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