# N45793: 1973 Boeing 727-232, registration cancelled 2003-10-25 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: October 25, 2003 - Status when cancelled: Triennial form not returned - Airframe: [Boeing 727-232](https://openairdocs.org/model/boeing-727-232) (registry code 1384082) - Engine: [Pratt & Whitney JT8D-1](https://openairdocs.org/engine/pratt-whitney-jt8d-1) (registry code 52044) - Data sheets: [TCDS A3WE](https://openairdocs.org/tcds/A3WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs) - Serial number: 20647 - Year built: 1973 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: August 28, 1973 - Certificate issued: August 2, 2000 - Last registry action: August 19, 2003 - Mode S code: A58FCC - Owner when cancelled: [Pegasus Aviation Inc](https://openairdocs.org/faa-owner/PEGASUS%20AVIATION%20INC) - Location: [San Francisco, CA](https://openairdocs.org/faa-place/CA/San%20Francisco) - Owner type: Corporation - Owner's area on the map: 37.7984° N, 122.3992° W: Placed by OpenAirDocs at the center of ZIP code 94111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N45793 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=45793 - Page: https://openairdocs.org/deregistered/N45793-2003-10-25 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 Boeing 727-232: https://openairdocs.org/model/boeing-727-232.md ## Service difficulty reports (94, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CALA9901588](https://openairdocs.org/sdr/CALA9901588), Dec 10, 1999: BATTERY PACK. DISCHARGED. INSPECTION FOUND THE EMERGENCY LIGHT AT AFT AIRSTAIR INOPERATIVE. THE BATTERY PACK WAS REMOVED, RECHARGED, REINSTALLED, OPERATION CHECKED GOOD IAW MM 33-51-01, - [SDR CALA9901587](https://openairdocs.org/sdr/CALA9901587), Dec 10, 1999: WIRE. BROKEN. INSPECTION FOUND THE EMERGENCY PATH LIGHTS IN SECTION 3 AND 4 INOPERATIVE. BROKEN WIRES AT SECTION 3 AND 4 WERE REPAIRED IAW MM 33-10-00 AND OPERATIONAL CHECK W - [SDR CALA9901586](https://openairdocs.org/sdr/CALA9901586), Dec 10, 1999: BATTERY PACK. DISCHARGED. THE RT OVERWING EMERGENCY EXIT LIGHTS IN THE MID AND AFT POSITIONS WERE FOUND INOPERATIVE. THE BATTERY PACK WAS REMOVED, RECHARGED, REINSTALLED AND OPERATION CH - [SDR CALA9901585](https://openairdocs.org/sdr/CALA9901585), Dec 10, 1999: BATTERY. DISCHARGED. INSPECTION FOUND MID CABIN FIXED EMERGENCY LIGHT INOPERATIVE. THE BATTERY PACK WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD IAW MM 33-51-00, PAGE 6. - [SDR CALA9901584](https://openairdocs.org/sdr/CALA9901584), Dec 10, 1999: WIRE. CHAFED. INSPECTION FOUND THE LT OVERWING EMERGENCY LIGHTS IN MID AND AFT POSITIONS INOPERATIVE. MAINTENANCE FOUND A CHAFED WIRE BEHIND WHEEL WELL FAIRING PANEL AREA. TH - [SDR CALA9901583](https://openairdocs.org/sdr/CALA9901583), Dec 10, 1999: BATTERY PACK. DISCHARGED. INSPECTION FOUND THE L-1 AND L-2 DOOR EXIT SIGNS INOPERATIVE. THE BATTERY PACK FOR EACH SIGN WAS REMOVED, RECHARGED, REINSTALLED AND OPERATION CHECKED GOOD IAW - [SDR CALA9901581](https://openairdocs.org/sdr/CALA9901581), Dec 9, 1999: LIGHT. INOPERATIVE. INSPECTION FOUND THE EMERGENCY EXIT LIGHT AT AFT ENTRY INOPERATIVE. THE LIGHT ASSEMBLY WAS REPLACED AND OPERATION CHECKED IAW MM 33-50-01. - [SDR CALA9901283](https://openairdocs.org/sdr/CALA9901283), Sep 23, 1999: STRINGER. CRACKED. INSPECTION FOUND A 5 INCH CRACK AT ATTACH POINT IN LT WING UPPER FORWARD STRINGER AT WING STA 629.0. THE CRACKED AREA WAS CUT OUT, REPAIR PARTS WERE INSTALLED I - [SDR CALA9901273](https://openairdocs.org/sdr/CALA9901273), Sep 20, 1999: SKIN. DELAMINATED. INSPECTION FOUND O/B END UPPER SURFACE OF LT WING NR 7 SPOILER DELAMINATED. THE NR 7 SPOILER WAS REMOVED AND REPLACED IAW MM 27-62-1. - [SDR CALA9901272](https://openairdocs.org/sdr/CALA9901272), Sep 20, 1999: SEAT TRACK. CORRODED. INSPECTION FOUND G-1 GALLEY SEAT TRACK CORRODED AT STA 344-380. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 51-30-1, - [SDR CALA9901271](https://openairdocs.org/sdr/CALA9901271), Sep 20, 1999: SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED AT CENTERLINE FLOORBEAM, STA 1035. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-10-2 AND 51- - [SDR CALA9901251](https://openairdocs.org/sdr/CALA9901251), Sep 17, 1999: WIRE. DISCONNECTED. THE EMERGENCY EXIT LIGHT WIRING WAS FOUND PULLED OUT OF CONDUIT AND DISCONNECTED AT ROW 11. THE WIRING WAS RECONNECTED AND PLACED BACK INTO CONDUIT IAW MM 20-00 - [SDR CALA9901250](https://openairdocs.org/sdr/CALA9901250), Sep 17, 1999: INTERCOSTAL. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN INTERCOSTAL AT STA 990, STRINGER 23L. THE INTERCOSTAL WAS REMOVED AND A NEW INTERCOSTAL WAS INSTALLED IAW SRM 51-30-2 AND 51- - [SDR CALA9901232](https://openairdocs.org/sdr/CALA9901232), Sep 15, 1999: FRAME. CORRODED. INSPECTION FOUND FRAME CORRODED AT STA 580, STRINGER 26R-27R. THE CORRODED AREA WAS REMOVED IAW SRM 53-10-4 AND A REPAIR WAS INSTALLED IAW SRM 51-10-1 AND 53-10 - [SDR CALA9901231](https://openairdocs.org/sdr/CALA9901231), Sep 15, 1999: FRAME. CORRODED. INSPECTION FOUND FRAME AND WEB CORRODED AT STA 1148 FROM STRINGER 27L-27R. THE WEB WAS REMOVED, REPAIRED, AND REINSTALLED IAW SRM 51-10-6, 53-10-4, FIGURE 45, A - [SDR CALA9901230](https://openairdocs.org/sdr/CALA9901230), Sep 15, 1999: STRINGER. CORRODED. INSPECTION FOUND STRINGER 29R CORRODED AT STA 344. THE SKIN WAS CUT AND CORRODED STRINGER WAS REMOVED. A FILLER, DOUBLER, AND STRINGER REPAIR WERE INSTALLED IAW - [SDR CALA9901229](https://openairdocs.org/sdr/CALA9901229), Sep 15, 1999: WEB. CORRODED. INSPECTION FOUND WEB SKIN CORRODED AT STA 1142-1148, STRINGER 26R TO 20R. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-30-2 AND 51-40-2. - [SDR CALA9901228](https://openairdocs.org/sdr/CALA9901228), Sep 15, 1999: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT STA 380, RBL 15. THE FLOORBEAM WAS REPAIRED IAW SRM 53-10-8 AND 51-30-2. - [SDR CALA9901227](https://openairdocs.org/sdr/CALA9901227), Sep 15, 1999: SHEAR TIE. CORRODED. INSPECTION FOUND FRAME SHEAR TIES CORRODED AT STA 720B, STRINGER 28L-28R, STA 720C, S28L-28R, AND STA 720F, S25R-27R. THE SHEAR TIES WERE REMOVED AND REPLACED I - [SDR CALA9901226](https://openairdocs.org/sdr/CALA9901226), Sep 15, 1999: SHEAR TIE. CORRODED. INSPECTION FOUND SHEAR TIE CORRODED AT STA 1148, STRINGER 24R TO 27R. REPAIRED SHEAR TIE IAW SRM 53-10-4. - [SDR CALA9901225](https://openairdocs.org/sdr/CALA9901225), Sep 15, 1999: ANGLE. CORRODED. INSPECTION FOUND THREE ANGLES CORRODED IN KEEL BEAM AREA FROM STA 759-824. THE ANGLES WERE REMOVED AND REPLACED IAW SRM 51-40-4, 51-30-2, AND 51-10-1. - [SDR CALA9901224](https://openairdocs.org/sdr/CALA9901224), Sep 15, 1999: INTERCOSTAL. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN INTERCOSTAL BETWEEN STA 990 AND 1010 AT S24L. THE CRACK WAS STOP DRILLED AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 51-10-1, - [SDR CALA9901223](https://openairdocs.org/sdr/CALA9901223), Sep 15, 1999: ANGLE. CORRODED. INSPECTION FOUND KEEL BEAM ANGLES AT STA 750, RT SIDE AND STA 850, RBL 5 TO LBL 5 CORRODED. THE ANGLES WERE REMOVED AND NEW ANGLES WERE INSTALLED IAW SRM 51-30- - [SDR CALA9901222](https://openairdocs.org/sdr/CALA9901222), Sep 15, 1999: STRINGER. CORRODED. INSPECTION FOUND STRINGER S28R AND S27L CORRODED AT STA 660-680. THE CORRODED SECTION OF STRINGERS WERE REMOVED AND NEW SECTIONS WERE INSTALLED IAW 51-30-2, 53- - [SDR CALA9901221](https://openairdocs.org/sdr/CALA9901221), Sep 15, 1999: FRAME. CRACKED. INSPECTION FOUND A 4 INCH CRACK IN FRAME AT STA 500, STRINGER 21L. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. A DOUBLER WAS INSTALLED IAW SRM 51-40-3. - [SDR CALA9901220](https://openairdocs.org/sdr/CALA9901220), Sep 15, 1999: SHEAR TIE. CORRODED. INSPECTION FOUND SHEAR TIES CORRODED AT STA 990, S29R AND STA 1090, S29R. NEW SHEAR TIES WERE INSTALLED IAW SRM 53-10-4, 51-30-2, AND 51-10-2. - [SDR CALA9901219](https://openairdocs.org/sdr/CALA9901219), Sep 15, 1999: KEEL BEAM. CORRODED. INSPECTION FOUND KEEL BEAM WEB CORRODED AT STA 801, LT SIDE. THE CORRODED WEB AREA WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-10-1. - [SDR CALA9901169](https://openairdocs.org/sdr/CALA9901169), Sep 9, 1999: STRINGER. CORRODED. INSPECTION FOUND FORWARD CARGO STRINGER 27L CORRODED AT FS 660-640, FS 720C-720B, AND 720B-720A. THE CORRODED AREAS WERE CUT OUT AND A REPAIR WAS INSTALLED IAW - [SDR CALA9900021](https://openairdocs.org/sdr/CALA9900021), Jan 14, 1999: WIRE. SHORTED. EMERGENCY EXIT LIGHT RIGHT HAND CONTROL CIRCUIT BREAKER POPPED AND WOULD NOT RESET. FOUND WIRE SHORTED IN AFT LEFT TAIL COMPARTMENT. SECURED WIRES AND PROTECTED - [SDR CALA9802132](https://openairdocs.org/sdr/CALA9802132), Dec 2, 1998: FLOOR. CORRODED. INSPECTION FOUND CABIN FLOOR PAN CORRODED AT AFT ENTRY STA 1177 TO 1171, BL 0 TO LBL 18. THE FLOOR PAN WAS REMOVED AND A NEW FLOOR PAN WAS INSTALLED IAW SRM 53- - [SDR CALA9802125](https://openairdocs.org/sdr/CALA9802125), Nov 30, 1998: FLOOR. CORRODED. INSPECTION FOUND CORROSION ON RT AFT LAV FLOOR PAN AT BS 1111 TO 1183. THE FLOOR PAN WAS REMOVED AND A NEW PAN WAS INSTALLED IAW SRM 51-30-2, 51-40-2 FIGURE 1, - [SDR CALA9802038](https://openairdocs.org/sdr/CALA9802038), Nov 4, 1998: SKIN. DELAMINATED. INSPECTION FOUND RT WING O/B TE AFT FLAP O/B END UPPER SURFACE DELAMINATED AT SPAR. THE AFT FLAP WAS REMOVED AND REPLACED IAW MM 27-51-11. - [SDR CALA9802037](https://openairdocs.org/sdr/CALA9802037), Nov 4, 1998: FUSE. BLOWN. INSPECTION FOUND LT AFT EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED A BLOWN FUSE AND OPERATION CHECKED GOOD IAW MM 33-51-00. - [SDR CALA9802036](https://openairdocs.org/sdr/CALA9802036), Nov 4, 1998: SKIN. DELAMINATED. INSPECTION FOUND TOP SURFACE OF NR 8 SPOILER DELAMINATED. THE NR 8 SPOILER WAS REMOVED AND REPLACED IAW MM 27-62-81. - [SDR CALA9802019](https://openairdocs.org/sdr/CALA9802019), Nov 3, 1998: STIFFENER. CORRODED. INSPECTION FOUND RT WING FRONT SPAR VERTICAL STIFFENER CORRODED AT STA 244. THE STIFFENER WAS REPLACED IAW SRM 51-10-1 PAGE 4 AND 6A, SRM 51-10-2 AND 51-30-2. - [SDR CALA9802018](https://openairdocs.org/sdr/CALA9802018), Nov 2, 1998: SPAR. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN LT ELEVATOR REAR SPAR. THE LT ELEVATOR WAS REMOVED AND REPLACED IAW MM 27-30-1, PAGE 401 AND 402. RIG AND OPERATIONAL CHECK - [SDR CALA9802017](https://openairdocs.org/sdr/CALA9802017), Nov 2, 1998: FRAME. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN FLOOR LEVEL RIB AT RT SIDE OF STA 344. A STRAP WAS INSTALLED IAW SRM 51-10-2 AND 53-10-8 FIGURE 6. - [SDR CALA9802016](https://openairdocs.org/sdr/CALA9802016), Nov 2, 1998: ANGLE. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN C-3 DOOR T-ANGLE AT LOWER AFT DOOR STOP AREA. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-101. - [SDR CALA9802015](https://openairdocs.org/sdr/CALA9802015), Nov 2, 1998: CHORD. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN LT WING AFT FALSE SPAR LOWER CHORD AT WBL 135.2. THE CRACKED AREA WAS CUT OUT AND SPLICE ANGLE AND STRAPS WERE INSTALLED IAW - [SDR CALA9802011](https://openairdocs.org/sdr/CALA9802011), Nov 2, 1998: BRACKET. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN INBOARD SUPPORT BRACKET AT LOWER END WHERE LT WING NR 1 L/E FLAP ACTUATOR IS MOUNTED. A NEW SUPPORT BRACKET WAS INSTALLED IA - [SDR CALA9802010](https://openairdocs.org/sdr/CALA9802010), Nov 2, 1998: SKIN. PUNCTURED. INSPECTION FOUND TWO .25 INCH DIAMETER HOLES IN RT ELEVATOR UPPER SKIN JUST AFT OF NR 3 ATTACH HINGE. A DOUBLER REPAIR WAS INSTALLED IAW SRM 55-20-3, PAGE 9. - [SDR CALA9801992](https://openairdocs.org/sdr/CALA9801992), Oct 27, 1998: TERMINAL. INOP. INSPECTION FOUND L-1 OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REPAIRED TERMINAL AT LIGHT SOCKET ASSEMBLY AND OPERATIONAL CHECKS WERE GOOD AT MM 33 - [SDR CALA9801991](https://openairdocs.org/sdr/CALA9801991), Oct 27, 1998: WIRE. LOOSE. INSPECTION FOUND THE L-2 OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE FOUND A LOOSE WIRE IN HARNESS. THE WIRE WAS REPQIRED AND OPERATIONAL CHECKS WERE - [SDR CALA9800842](https://openairdocs.org/sdr/CALA9800842), May 9, 1998: NUT. LEAKING. ON TAKEOFF DURING GEAR RETRACTION, A-SYSTEM HYDRAULICS FAILED. FOUND LEAK AT A-SYSTEM RETURN LINE T-FITTING AT FWD KEEL BEAM RT WHEEL WELL. TIGHTENED B-NUT AND - [SDR CALA9800002](https://openairdocs.org/sdr/CALA9800002), Jan 4, 1998: HYD LINE. RUPTURED. THE AIRCRAFT LOST A-SYSTEM HYDRAULIC QUANTITY DURING GEAR EXTENSION WHILE ON APPROACH TO IAH. ABNORMAL AND EMERGENCY PROCEDURES WERE FOLLOWED AND THE AIRCRAFT L - [SDR CALA9701752](https://openairdocs.org/sdr/CALA9701752), Dec 12, 1997: RELAY. INOPERATIVE. THE NR 1 ENGINE FIRE DETECTION FAULT LIGHT AT B POSITION ILLUMINATED INTERMITTENTLY WHILE IN FLIGHT. TROUBLESHOOTING THE NR 1 ENGINE FIRE DETECTION SYSTEM FOUND - [SDR CALA9701502](https://openairdocs.org/sdr/CALA9701502), Oct 24, 1997: POWER SUPPLY. INOPERATIVE. INSPECTION FOUND LEFT OVERWING EXIT AFT LIGHT INOPERATIVE. THE LEFT OVERWING EXIT LIGHT POWER SUPPLY WAS REMOVED AND REPLACED. OPERATION OF THE LIGHT CHECKED GO - [SDR CALA9701397](https://openairdocs.org/sdr/CALA9701397), Sep 29, 1997: BATTERY PACK. DISCHARGED. INSPECTION FOUND OVERHEAD EMERGENCY LIGHTS AT ROW 17 INOPERATIVE. THE BATTERY PACK WAS REPLACED. - [SDR CALA9701186](https://openairdocs.org/sdr/CALA9701186), Jul 28, 1997: STRINGER. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN UPPER AREA OF RT WING STRINGER, SECOND FROM AFT AT STA 686.5. THE CRACK WAS STOP DRILLED, A REPAIR WAS FABRICATED AND INSTALL - [SDR CALA9701183](https://openairdocs.org/sdr/CALA9701183), Jul 28, 1997: RIB. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN RT WING FUEL TANK RIB AT WS 760. THE CRACK WAS STOP DRILLED, A REPAIR WAS INSTALLED IAW SRM 57-10-5. All 94: https://openairdocs.org/deregistered/N45793-2003-10-25/reports.md ## Other aircraft with N45793 - [Cancelled 1952-08-25](https://openairdocs.org/deregistered/N45793-1952-08-25): Luscombe 8A, S/N 2320, built 1946. Exported to Mexico. Owner: [Anderson Carl](https://openairdocs.org/faa-owner/ANDERSON%20CARL), [Springfield, MO](https://openairdocs.org/faa-place/MO/Springfield) --- 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.