# N936PG: 1980 Boeing 727-225, registration cancelled 2011-04-28 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: April 28, 2011 - Status when cancelled: Valid registration - Airframe: [Boeing 727-225](https://openairdocs.org/model/boeing-727-225) (registry code 1384077) - Engine: [Pratt & Whitney JT8D-15](https://openairdocs.org/engine/pratt-whitney-jt8d-15) (registry code 52051) - Data sheets: [TCDS A3WE](https://openairdocs.org/tcds/A3WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs) - Serial number: 22441 - Year built: 1980 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: March 5, 2000 - Certificate issued: October 29, 2008 - Last registry action: October 31, 2008 - Mode S code: ACFD3F - Owner when cancelled: [Stewart Industries International LLC](https://openairdocs.org/faa-owner/STEWART%20INDUSTRIES%20INTERNATIONAL%20LLC) - Location: [Guthrie, OK](https://openairdocs.org/faa-place/OK/Guthrie) - Owner type: Corporation - Owner's area on the map: 35.8679° N, 97.4344° W: Placed by OpenAirDocs at the center of ZIP code 73044, within about 9 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N936PG - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=936PG - Page: https://openairdocs.org/deregistered/N936PG-2011-04-28 From the FAA registry file of November 4, 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 727-225: https://openairdocs.org/model/boeing-727-225.md ## Service difficulty reports (33) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR GAIA04042OP](https://openairdocs.org/sdr/GAIA04042OP), Feb 27, 2004: FIRE LOOP. OUT OF POSITION. FLT 714 - FWA-MIA - NR 1 ENGINE FIRE DETECTION CIRCUIT GROUND LIGHT ILLUMINATED IN FLIGHT. FOUND DETECTOR CHAFING AT COWL DOOR. REPOSITIONED NR 1 ENGINE FIRE LO - [SDR GAIA04036OP](https://openairdocs.org/sdr/GAIA04036OP), Feb 26, 2004: FIRE LOOP. OUT OF ADJUST. FLT 213 - ATL-FWA - DURING CRUISE, THE NR 1 ENGINE FIRE DETECTION LIGHT ILLUMINATED ON THE FLIGHT ENGINEERS PANEL. REPOSITIONED NR 1 ENGINE FIRE LOOP OPERATIONA - [SDR GAIA04033AOP](https://openairdocs.org/sdr/GAIA04033AOP), Feb 21, 2004: WARNING LIGHT. ILLUMINATED. NR 1 ENGINE FIRE DETECTION CIRCUIT GROUND LIGHT ILLUMINATED. (M) - [SDR GAIA04033BOP](https://openairdocs.org/sdr/GAIA04033BOP), Feb 21, 2004: FIRE LOOP. OUT OF ADJUST. NR 1 ENGINE FIRE DETECTION CIRCUIT GROUND LIGHT ILLUMINATED. REPOSITIONED NR 1 ENGINE FIRE LOOP. GROUND FAULT LIGHT EXTINGUISHED. AIRCRAFT WAS RETURNED TO SERVI - [SDR GAIA04023OP](https://openairdocs.org/sdr/GAIA04023OP), Feb 19, 2004: FIRE LOOP. GROUNDED. THE NR 1 ENGINE GROUND FAULT LIGHT CAME ON AFTER LANDING IN FWA. NR 1 ENGINE FIRE LOOP WAS FOUND GROUNDED OUT. REPOSITIONED LOOP AND THE SYSTEM OPERATIONALLY CH - [SDR GAIA04009OP](https://openairdocs.org/sdr/GAIA04009OP), Jan 30, 2004: RELAY. INOPERATIVE. DURING TAXI OUT, IT WAS DISCOVERED THAT THE TAKE OFF WARNING HORN WOULD NOT TEST. REMOVED AND REPLACED THE TIME DELAY RELAY. OPERATIONALLY CHECKED GOOD. THE AIR - [SDR GAIA03110OP](https://openairdocs.org/sdr/GAIA03110OP), Oct 17, 2003: ACCESSORY UNIT. LOOSE. ON APPROACH TO PHX, THE RIGHT MLG DOWN AND LOCKED LIGHT DID NOT ILLUMINATE ON GEAR EXTENTION. THE SECONDARY MLG LIGHTS INDICATED DOWN AND LOCKED. THE CREW PERFO - [SDR GAIA03108OP](https://openairdocs.org/sdr/GAIA03108OP), Sep 12, 2003: BRAKE ASSY. DRAGGING. FLT 372 - LAX-PHX-FWA, DURING TAXI TO DEPARTURE, THE FLIGHT CREW NOTICED THE NR 3 BRAKE DRAGGING. REMOVED AND REPLACED THE NR 3 BRAKE AND THE NR 3 AND NR 4 MAIN - [SDR GAIA02155OP](https://openairdocs.org/sdr/GAIA02155OP), Nov 12, 2002: ACTUATOR. CRACKED. DURING CLIMB-OUT OF SCHEDULE FLIGHT NR 705 FROM IAH-FWA, THE CREW NOTICED THE LOSS OF SYSTEM 'A' HYDRAULIC QUANTITY, AND PRESSURE WENT TO ZERO. THE CREW DECLARE - [SDR GAIA02151ST](https://openairdocs.org/sdr/GAIA02151ST), Oct 24, 2002: SKIN. CRACKED. DURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE RIGHT WING UPPER OUTBOARD LEADING EDGE AT WS 430 HAD A ROW OF FASTENERS WITH CRACKS RUNNING FROM HEAD HO - [SDR GAIA02150ST](https://openairdocs.org/sdr/GAIA02150ST), Oct 24, 2002: DOOR FRAME. CRACKED. DURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE C-1 DOOR CUTOUT AFT RIGHT FRAME HAD A CRACK IN THE SKIN IN TWO PLACES AT STRINGER S26R. REPAIR WAS ACCOM - [SDR GAIA02149ST](https://openairdocs.org/sdr/GAIA02149ST), Oct 24, 2002: FRAME. DENTED. DURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE FRAME AT BS 560, STRINGER S25L WAS DENTED. REPAIR WAS ACCOMPLISHED IAW BOEING 727 SRM 51-40-3, FIGURE 1. - [SDR GAIA02148ST](https://openairdocs.org/sdr/GAIA02148ST), Oct 24, 2002: FRAME. DENTED. DURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE FRAME AT BS 580, AND IN BETWEEN STRINGER S24L AND S25L WAS DENTED. REPAIR WAS ACCOMPLISHED IAW BOEING 72 - [SDR GAIA02147ST](https://openairdocs.org/sdr/GAIA02147ST), Oct 24, 2002: BUSHING. DETERIORATED. DURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE LEFT AFT BOTTLE PIN BUSHINGS WERE DETERIORATED. THE BUSHINGS WERE REPLACED IAW THE BOEING 727 MM 57-41-1 - [SDR GAIA02146ST](https://openairdocs.org/sdr/GAIA02146ST), Oct 24, 2002: SKIN. CRACKED. DURING A ROUTINE INSPECTION AT FLIGHTSTAR IN JAX, IT WAS DISCOVERED THAT THE C-1 DOOR CUT OUT INNER SKIN WAS CRACKED AT BS 620, STRINGER S25R. REPAIR WAS ACCOMP - [SDR GAIA02145ST](https://openairdocs.org/sdr/GAIA02145ST), Oct 24, 2002: SKIN. CRACKED. DURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE VENTRAL STAIR CUTOUT, FORWARD RIGHT SIDE HAD A CRACK IN THE RADIUS. REPAIR WAS ACCOMPLISHED IAW BOEING 7 - [SDR GAIA02144ST](https://openairdocs.org/sdr/GAIA02144ST), Oct 24, 2002: SKIN. DENTED. DURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE LEFT WING NR 2 SLAT NOSE UPPER SURFACE SHOWS A LARGE DENTED AREA ON THE SKIN. REPAIR WAS ACCOMPLISHED IA - [SDR GAIA02143ST](https://openairdocs.org/sdr/GAIA02143ST), Oct 24, 2002: RIB. CRACKED. DURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE LEFT WING NR 4 SLAT INTERIOR RIB WAS CRACKED AT WS 410, OUTBOARD OF THE ACTUATOR ATTACH POINT. REPAIR WA - [SDR GAIA02142ST](https://openairdocs.org/sdr/GAIA02142ST), Oct 24, 2002: SKIN. CRACKED. DURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE LEFT WING LEADING EDGE UPPER SKIN AT THE NR 3 SLAT GUIDE FITTING CUT OUT WAS CRACKED AND HAD LOOSE FASTE - [SDR GAIA02141ST](https://openairdocs.org/sdr/GAIA02141ST), Oct 24, 2002: SKIN. DELAMINATED. DURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE LEFT WING NR 7 GROUND SPOILER PANEL WAS DELAMINATED AND HAD HOLES ON THE BOTTOM SIDE OF THE PANEL. REPAI - [SDR GAIA02140ST](https://openairdocs.org/sdr/GAIA02140ST), Oct 24, 2002: SKIN. CRACKED. DURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE FUSELAGE SKIN WAS CRACKED AT THE FORWARD ENTRY DOOR LOWER HINGE CUT OUT. REPAIR WAS ACCOMPLISHED IAW BOE - [SDR GAIA02139ST](https://openairdocs.org/sdr/GAIA02139ST), Oct 24, 2002: FRAME. DENTED. DURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT IN THE FORWARD CARGO LOWER BILGE BS 600, IN BETWEEN STRINGER S28L AND S29L, THE FRAME WAS DENTED. REPAIR ACC - [SDR GAIA02137ST](https://openairdocs.org/sdr/GAIA02137ST), Oct 24, 2002: WEB. CRACKED. DURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE LEFT WING LEADING EDGE WEB AT WING STATION 130.7 UPPER CHORD IS CRACKED ABOUT 10 INCHES LONG. REPAIRED A - [SDR GAIA02136ST](https://openairdocs.org/sdr/GAIA02136ST), Oct 24, 2002: STIFFENER. CRACKED. DURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE LEFT WING FRONT SPAR AT FSS 106.8 VERTICAL STIFFENER IS CRACKED AT THE FORWARD END. REPAIR ACCOMPLISHED - [SDR GAIA02152ST](https://openairdocs.org/sdr/GAIA02152ST), Oct 24, 2002: STRINGER. CHAFED. DURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE STRINGER AT BS 720E, S19R HAD CHAFE DAMAGE FROM FAIRING AT THE LAP JOINT. REPAIR WAS ACCOMPLISHED IAW BO - [SDR GAIA01308OP](https://openairdocs.org/sdr/GAIA01308OP), Sep 8, 2001: LIGHT. INOPERATIVE. DURING MAINTENANCE AT TOL, IT WAS DISCOVERED THAT THE L1 DOOR EMERGENCY EXIT LIGHT WAS INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT. THE SYSTEM OP - [SDR GAIA01307OP](https://openairdocs.org/sdr/GAIA01307OP), Sep 8, 2001: CONTACTOR. DIRTY. DURING MAINTENANCE AT TOL, IT WAS DISCOVERED THAT THE COCKPIT EMERGENCY EXIT LIGHT WAS INOPERATIVE. INSPECTION FOUND THE EMERGENCY EXIT LIGHT CONNECTIONS DIRTY. - [SDR GAIA01302OP](https://openairdocs.org/sdr/GAIA01302OP), Aug 28, 2001: CONNECTOR. DIRTY. DURING MAINTENANCE AT TOL, IT WAS DISCOVERED THAT THE COCKPIT EMERGENCY EXIT LIGHT WAS INOPERATIVE. INSPECTION FOUND THE EMERGENCY EXIT LIGHT CONNECTIONS DIRTY - [SDR GAIA01124OP](https://openairdocs.org/sdr/GAIA01124OP), Apr 9, 2001: BATTERY. DISCHARGED. DURING MAINTENANCE, IT WAS DISCOVERED THAT THE EMERGENCY LIGHT ASSEMBLY AT THE L1 DOOR APPEARS TO BE DISCHARGED. REMOVED AND REPLACED THE L1 DOOR EMERGENCY LIGH - [SDR GAIA00260A](https://openairdocs.org/sdr/GAIA00260A), Apr 28, 2000: FIRE LOOP. MALFUNCTIONED. DURING SCHEDULED FLIGHT 1760, FWA-MEM, ON CLIMB-OUT, ENGINE NR 3 FIRE WARNING GROUND DETECTION SYSTEM LIGHT CAME ON. NR 3 FIRE WARNING DETECTION WAS DEFERRED. A - [SDR GAIA00260](https://openairdocs.org/sdr/GAIA00260), Apr 27, 2000: WARNING LIGHT. ILLUMINATED. DURING SCHEDULED FLIGHT 1760 FROM FWA TO MEM, ON CLIMB-OUT, ENGINE NR 3 FIRE WARNING GROUND DETECTION SYSTEM LIGHT CAME ON. NR 3 FIRE WARNING DETECTION WAS DEFE - [SDR GAIA00162](https://openairdocs.org/sdr/GAIA00162), Mar 31, 2000: LINE. LEAKING. DURING SCHEDULED FLIGHT 509, MCO-TOL, ON CLIMB-OUT, ENGINE NR 1 STRUT OVERHEAT LIGHT CAME ON. THE AIRCRAFT RETURNED TO MCO AND MADE A ROUTINE LANDING. MAINTENAN - [SDR GAIA00161](https://openairdocs.org/sdr/GAIA00161), Mar 31, 2000: ANTI-ICE VALVE. LEAKING. DURING SCHEDULED FLIGHT 509, MCO-TOL, ON CLIMB-OUT, ENGINE NR 3 STRUT OVERHEAT LIGHT CAME ON. THE AIRCRAFT RETURNED TO MCO AND MADE A ROUTINE LANDING. FOUND AIR --- 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.