# N10791: 1973 Boeing 727-232, registration cancelled 2001-12-05 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: December 5, 2001 - 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-9 series](https://openairdocs.org/engine/pratt-whitney-jt8d-9-series) (registry code 52048) - Data sheets: [TCDS A3WE](https://openairdocs.org/tcds/A3WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs) - Serial number: 20645 - Year built: 1973 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: July 25, 1973 - Certificate issued: October 20, 1995 - Last registry action: October 16, 2001 - Mode S code: A02262 - Owner when cancelled: [Pacific Aircorp 791 Inc](https://openairdocs.org/faa-owner/PACIFIC%20AIRCORP%20791%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/N10791 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=10791 - Page: https://openairdocs.org/deregistered/N10791-2001-12-05 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 (78, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CALA9901477](https://openairdocs.org/sdr/CALA9901477), Nov 8, 1999: LIGHT. INOP. INSPECTION FOUND INTERIOR OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE AT ROW 22. THE LIGHT ASSEMBLY WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD. - [SDR CALA9901073](https://openairdocs.org/sdr/CALA9901073), Aug 19, 1999: FLOORBEAM. CORRODED. INSPECTION FOUND MAIN DECK FLOORBEAM IN AFT CARGO COMPARTMENT CORRODED AT STA 1130 FROM BL 0 TO RBL 30. REPAIRED IAW SRM 53-10-8 AND ECRA 5310-03898. - [SDR CALA9900621](https://openairdocs.org/sdr/CALA9900621), Jun 2, 1999: ACCESSORY UNIT. INOPERATIVE. WHEN GEAR WAS RETRACTED AFTER DEPARTURE A LOUD THUMP WAS HEARD WHEN NOSE GEAR RETRACTED. A LIGHT TEST WAS DONE AND THE NOSE GEAR GREEN LIGHT DID NOT COME ON. PR - [SDR CALA9900024](https://openairdocs.org/sdr/CALA9900024), Jan 16, 1999: STATOR. MIGRATED. ENGINE NUMBER THREE FAILED ON CLIMB-OUT. CONSTANT VIBRATION, OVER TEMP, ENGINE SHUT DOWN IN FLIGHT. AIRCRAFT RETURNED TO LAS. ENGINE AND DAMAGED COWLING REPLACE - [SDR CALA9800812](https://openairdocs.org/sdr/CALA9800812), May 7, 1998: BATTERY. DISCHARGED. MAIN CABIN O/H EMERGENCY LIGHT FLICKERING. RECHARGED BATTERY PACK PER MM 33-50-0. - [SDR CALA9800747](https://openairdocs.org/sdr/CALA9800747), May 3, 1998: FRAME. CRACKED. TOP FLANGE AT FRAME 520 HAS .5 INCH CRACK ABOVE STR 26R. STOP DRILLED CRACK PER SRM 51-10-1. FABRICATED AND INSTALLED REPAIR PER SRM 51-10-6. HEAT TREAT PER BAC - [SDR CALA9800746](https://openairdocs.org/sdr/CALA9800746), May 3, 1998: OXY CONTL UNIT. FAILED. FWD OXYGEN PASSENGER DROP FAILED FUNCTIONAL TEST. REPLACED OXYGEN CONTROL UNIT AND PERFORMED PNEUMATIC OXYGEN DROP PER MM 35-21-00. - [SDR CALA9800745](https://openairdocs.org/sdr/CALA9800745), May 3, 1998: WEB. CRACKED. VERT STAB INNER COMPARTMENT NR 1 CANTED STATION 1303 HAS CRACK (2.5) AT RT LOWER CORNER. ALSO, CRACK (1) AT RT UPPER CORNER. STOP DRILLED CRACKS, FABRICATED AND - [SDR CALA9800744](https://openairdocs.org/sdr/CALA9800744), May 3, 1998: STRINGER. CRACKED. VERT STAB INNER COMPARTMENT NR 7 STRINGER NR 2 AND NR 3 CRACKED (2) AT ATTACH BOLT. REPAIRED NR 7 RT STRINGER NR 2 AND NR 3 ON VERTICAL STAB PER SRM 55-30-4. - [SDR CALA9800743](https://openairdocs.org/sdr/CALA9800743), May 3, 1998: JAMB. CRACKED. C-1 DOOR JAMB BENT/TORN AT TWO PLACES. REMOVED AND REPLACED DOOR JAMB AS REQUIRED PER SRM 51-10-1. - [SDR CALA9800742](https://openairdocs.org/sdr/CALA9800742), May 3, 1998: FLANGE. CRACKED. TOP FLANGE RADIUS FS 700 ABOVE 24 L HAS 1.5 INCH CRACK. STOP DRILLED, FABRICATED DOUBLER AND INSTALLED PER SRM 51-30-2 AND 51-40-3. - [SDR CALA9800741](https://openairdocs.org/sdr/CALA9800741), May 3, 1998: WIRE. BROKEN. LT EXIT LIGHT INOP OVER EXIT IN CABIN. REPAIRED BROKEN WIRE AT EXIT IDENTIFIER, OPS CHECK PER 33-50-00. - [SDR CALA9800740](https://openairdocs.org/sdr/CALA9800740), May 3, 1998: FLANGE. CRACKED. A 1 INCH CRACK AT FRAME 500 TOP FLANGE RADIUS ABOVE 24 L. FABRICATED NEW DOUBLER AND INSTALLED IN ACCORDANCE WITH SRM 51-40-3. HEAT TREATED PER BAC 5602. - [SDR CALA9800739](https://openairdocs.org/sdr/CALA9800739), May 3, 1998: SKIN. CORRODED. FUSELAGE SKIN IN FORWARD BAG BIN FS 695.700 AT RBL HAS SURFACE CORROSION. REMOVED DAMAGED AREA AND INSTALLED DOUBLER PER SRM 53-30-03. - [SDR CALA9800738](https://openairdocs.org/sdr/CALA9800738), May 3, 1998: WIRE. BROKEN. ESCAPE PATH LIGHTS INOP ROW 24 TO 29. REPAIRED BROKEN WIRE GOING TO SEATS PER MM 33-50-00. - [SDR CALA9800701](https://openairdocs.org/sdr/CALA9800701), Apr 24, 1998: SUPPORT. CRACKED. INSPECTION FOUND A 2.5 CRACK IN VERTICAL STABILIZER STRINGER 4L SUPPORT WEB. THE SUPPORT WEB WAS REMOVED IAW SRM 51-30-2. A NEW SUPPORT WEB WAS FABRICATED AND I - [SDR CALA9800700](https://openairdocs.org/sdr/CALA9800700), Apr 24, 1998: SUPPORT. CRACKED. INSPECTION FOUND A 1 CRACK IN VERTICAL STABILIZER SUPPORT WEB AT STRINGER 3L AND STRINGER 3R. THE LT AND RT SUPPORT WEB WAS REMOVED. A NEW SUPPORT WEB WAS FABRI - [SDR CALA9800699](https://openairdocs.org/sdr/CALA9800699), Apr 24, 1998: FRAME. CRACKED. INSPECTION FOUND A 1 CRACK IN UPPER FLANGE RADIUS OF FRAME 640, RBL 8, FORWARD BAGGAGE BIN. THE CRACKED AREA WAS CUT OUT IAW SRM 51-40-3. A DOUBLER AND FITTING - [SDR CALA9800698](https://openairdocs.org/sdr/CALA9800698), Apr 24, 1998: FRAME. CRACKED. INSPECTION FOUND A .375 INCH CRACK WITH CORROSION IN FRAME 560 TO SKIN ATTACH FLANGE, BBL 0 TO LBL 6. THE CORRODED AREA OF FLANGE WAS CUT OFF IAW SRM 53-10-4. A - [SDR CALA9800697](https://openairdocs.org/sdr/CALA9800697), Apr 24, 1998: STRINGER. CORRODED. INSPECTION FOUND STRINGER 28L CORRODED AT STA 720D. THE CORRODED AREA OF STRINGER WAS REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 53-10-3 - [SDR CALA9800472](https://openairdocs.org/sdr/CALA9800472), Mar 17, 1998: HYD PUMP. LEAKING. THE 'A' SYSTEM HYDRAULIC RESERVOIR QUANTITY WENT TO ZERO AND LOW PRESSURE LIGHTS ILLUMINATED WHILE EN ROUTE FROM MSY TO IAH. THE HYDRAULIC QUANTITY LOSS AND HYD - [SDR CALA9701375](https://openairdocs.org/sdr/CALA9701375), Aug 31, 1997: BEAM. CRACKED. INSPECTION FOUND A .365 INCH AND .625 INCH CRACK IN RT WING UPPER TRAILING EDGE AFT OF MLG SUPPORT BEAM AT UPPER INBOARD CORNER OF NR 8 SPOILER ACTUATOR LINKAGE - [SDR CALA9701372](https://openairdocs.org/sdr/CALA9701372), Aug 26, 1997: DOUBLER. CORRODED. INSPECTION FOUND CORROSION AND POPPED RIVETS IN REPAIR DOUBLER AT FS 680, STRINGER 28R - 28L. THE EXISTING DOUBLER WAS REMOVED AND THE CORRODED AREA WAS CUT OUT - [SDR CALA9701374](https://openairdocs.org/sdr/CALA9701374), Aug 25, 1997: SKIN. PUNCTURED. INSPECTION FOUND A .25 INCH DIAMETER HOLE IN SKIN AT UPPER LEADING EDGE OF NR 7 SLAT. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-50-3. - [SDR CALA9701371](https://openairdocs.org/sdr/CALA9701371), Aug 25, 1997: BRACKET. CRACKED. INSPECTION FOUND A .5 CRACK IN UPPER AND LOWER RADIUS OF NR 5 KRUGER FLAP ACTUATOR SUPPORT BRACKET. A REPLACEMENT BRACKET WAS FABRICATED AND INSTALLED IAW SRM 5 - [SDR CALA9701369](https://openairdocs.org/sdr/CALA9701369), Aug 25, 1997: SKIN. CRACKED. INSPECTION FOUND A .375 INCH CRACK AT LEFT WING FIXED LEADING EDGE CUTOUT ABOVE NR 3 SLAT INBOARD TRACK. THE CRACK WAS STOP DRILLED. A DOUBLER WAS FABRICATED AN - [SDR CALA9701373](https://openairdocs.org/sdr/CALA9701373), Aug 24, 1997: SKIN. DENTED. INSPECTION FOUND TWO DENTS IN RT FUSELAGE SKIN AT STA 380. THE DENTED AREA WAS CUT OUT. FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 53-30-3. - [SDR CALA9701370](https://openairdocs.org/sdr/CALA9701370), Aug 24, 1997: BRACKET. CRACKED. INSPECTION FOUND A .75 CRACK IN BRACKET AT INBOARD AND OUTBOARD SIDE WHERE LEFT WING NR 1 L/E FLAP ACTUATOR MOUNTS (I/B LOWER AND O/B UPPER). REPLACEMENT BRACKE - [SDR CALA9700343](https://openairdocs.org/sdr/CALA9700343), Mar 16, 1997: ACTUATOR. LEAKING. AIRCRAFT LOST A-HYDRAULIC SYSTEM FLUID AFTER TAKEOFF. THE LOSS WAS ACCOMPANIED BY ILLUMINATION OF RUDDER SYSTEM A CAUTION LIGHT. THE AIRCRAFT WAS RETURNED TO IA - [SDR CALA9700125](https://openairdocs.org/sdr/CALA9700125), Jan 30, 1997: HYD PUMP. LEAKING. ACFT LOST THE A-HYDRAULIC SYSTEM FLUID QUANTITY ON APPROACH. THE FLUID LOSS WAS ACCOMPANIED BY THE PUMP LIGHT GOING ON AND OFF INTERMITTENTLY. THE AIRCRAFT LAND - [SDR CALA9601731](https://openairdocs.org/sdr/CALA9601731), Nov 19, 1996: SKIN. DAMAGED. THE RT INBOARD TRAILING EDGE MID FLAP LOWER SKIN SUSTAINED DAMAGE WHEN THE RT MLG TIRE BLEW. THE MID FLAP WAS REPAIRED IAW ECRA 5750-02565. - [SDR CALA9601378](https://openairdocs.org/sdr/CALA9601378), Oct 4, 1996: GEARBOX. LEAKING. THE NR 3 ENGINE LOST OIL QUANTITY AFTER TAKEOFF. THE LOSS OF OIL WAS ACCOMPANIED BY LOSS OF OIL PRESSURE AND ILLUMINATION OF FORWARD PANEL LIGHT. FUEL WAS DUMPE - [SDR CALA9601303](https://openairdocs.org/sdr/CALA9601303), Sep 11, 1996: DUCT. BLOWN. THE NR 2 ENGINE FAILED AFTER TAKEOFF. THE AIRCRAFT WAS RETURNED TO SJU WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 ENGINE 13TH STAGE DUCT BLOWN - [SDR CALA9601146](https://openairdocs.org/sdr/CALA9601146), Aug 7, 1996: AIRSTAIRS. OUT OF ADJUST. THE AFT AIRSTAIRS FELL DOWN WHILE TAXIING TO GATE AFTER LANDING AT IAH. THE AIRCRAFT WAS STOPPED AND THE STAIRS WERE SECURED. WHEN THE AIRSTAIRS WAS EXAMINED FO - [SDR CALA9600970](https://openairdocs.org/sdr/CALA9600970), Jul 6, 1996: ACTUATOR. LEAKING. THE A-SYSTEM HYDRAULIC QUANTITY WAS LOST DURING CLIMBOUT. FUEL WAS DUMPED AND THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOU - [SDR CALA9600956](https://openairdocs.org/sdr/CALA9600956), Jun 30, 1996: FLOORBEAM. CORRODED. INSPECTION FOUND THE FLOORBEAM CORRODED AT STA 1130, RBL 34 DURING FLIGHT PHONE INSTALLATION. THE FLOORBEAM WAS REPAIRED IAW SRM 5310-03300. - [SDR CALA9600913](https://openairdocs.org/sdr/CALA9600913), Jun 10, 1996: SHEAR TIE. CORRODED. INSPECTION FOUND SHEAR TIE CORRODED AT STA 580 BETWEEN STRINGER 27R AND 28R. THE SHEAR TIE WAS REMOVED AND A NEW SHEAR TIE WAS FABRICATED AND INSTALLED IAW SRM - [SDR CALA9600901](https://openairdocs.org/sdr/CALA9600901), Jun 5, 1996: STRINGER. CORRODED. INSPECTION FOUND STRINGER 28R FLANGE CORRODED AT F.S. 685. THE CORRODED SECTION OF STRINGER WAS REMOVED. A NEW STRINGER AND SPLICE WERE FABRICATED AND INSTALLED - [SDR CALA9600936](https://openairdocs.org/sdr/CALA9600936), Jun 2, 1996: STRINGER. CORRODED. INSPECTION FOUND STRINGER 28R CORRODED AT STA 520 T0 540. THE CORRODED STRINGER SECTION WAS REMOVED. A NEW STRINGER AND SPLICE WERE FABRICATED AND INSTALLED IAW - [SDR CALA9600938](https://openairdocs.org/sdr/CALA9600938), May 29, 1996: ANGLE. CORRODED. INSPECTION FOUND CORROSION ON SKIN ATTACH ANGLE AT STA 580, STRINGER 27L. A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 53-10-4, 51-30-2 AND MM 51-20-11. - [SDR CALA9600915](https://openairdocs.org/sdr/CALA9600915), May 28, 1996: SUPPORT. CORRODED. INSPECTION FOUND THE FORWARD CARGO COMPARTMENT FLOOR SUPPORT CORRODED AT STA 535, S28L TO S29L. A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-6, 51- - [SDR CALA9600919](https://openairdocs.org/sdr/CALA9600919), May 26, 1996: SHEAR TIE. CORRODED. INSPECTION FOUND SHEAR TIE CORRODED AT STA 265, S25R. A REPAIR WAS PERFORMED IAW SRM 53-10-4, 51-10-2, 51-30-2 AND MM 51-20-21. - [SDR CALA9600914](https://openairdocs.org/sdr/CALA9600914), May 26, 1996: SKIN. CORRODED. INSPECTION FOUND SKIN LAP CORRODED AT STA 720D TO 720E, STRINGER 27R. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3 AND 51-30-2. - [SDR CALA9600935](https://openairdocs.org/sdr/CALA9600935), May 25, 1996: ANGLE. CORRODED. INSPECTION FOUND ATTACH ANGLE CORRODED AT STA 540, S29R. THE ATTACH ANGLE WAS REMOVED. A REPAIR PART WAS FABRICATED IAW SRM 53-10-4, 53-10-1 AND 51-20-4. - [SDR CALA9600934](https://openairdocs.org/sdr/CALA9600934), May 25, 1996: FRAME. CORRODED. INSPECTION FOUND STA 540 FRAME ASSEMBLY CORRODED. A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM 53-10-4, PAGE 43. - [SDR CALA9600902](https://openairdocs.org/sdr/CALA9600902), May 25, 1996: ANGLES. CORRODED. INSPECTION FOUND SKIN ATTACH ANGLES(2) AT BILGE, STA 580, BL ZERO CORRODED. ANGLE DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10-2, 51-30-2, AND - [SDR CALA9600900](https://openairdocs.org/sdr/CALA9600900), May 24, 1996: FLOOR BEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT B.S. 1130, LBL 25. NEW PARTS WERE FABRICATED AND INSTALLED IAW SRM 53-10-1, 53-10-8, AND MM 51-20-11. - [SDR CALA9600923](https://openairdocs.org/sdr/CALA9600923), May 23, 1996: FLOOR BEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT STA 312, LBL 30. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 53-10-8, 51-10-2, 51-30-4 AND MM 51-20-11. - [SDR CALA9600912](https://openairdocs.org/sdr/CALA9600912), May 23, 1996: WEB. CRACKED. INSPECTION FOUND A FOUR INCH CRACK IN STIFFENER WEB INSIDE VERTICAL FIN ABOVE S-DUCT AT STA 1348. THE CRACK WAS STOPPED DRILLED, A DOUBLER WAS FABRICATED AND IN - [SDR CALA9600909](https://openairdocs.org/sdr/CALA9600909), May 23, 1996: SKIN. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN RT WING LEADING EDGE SKIN FORWARD OF OUTBOARD SLAT CARRIAGE, NR 5 SLAT. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-10 All 78: https://openairdocs.org/deregistered/N10791-2001-12-05/reports.md ## Other aircraft with N10791 - [Registered now](https://openairdocs.org/aircraft/N10791): Cameron Balloons US 0-105, S/N 6421 - [Cancelled 1932-12-28](https://openairdocs.org/deregistered/N10791-1932-12-28): Pitcairn PCA2, S/N B-25. Owner: [Pitcairn Aircraft Inc](https://openairdocs.org/faa-owner/PITCAIRN%20AIRCRAFT%20INC) - [Cancelled (date not recorded)](https://openairdocs.org/deregistered/N10791-undated): Cessna 150L, S/N 15075043. N-number assigned, not yet registered --- 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.