# N686CA: 1980 Boeing 727-2S7, registration cancelled 2013-05-03 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: May 3, 2013 - Status when cancelled: Registration expired, pending cancellation - Airframe: [Boeing 727-2S7](https://openairdocs.org/model/boeing-727-2s7) (registry code 138407Z) - Engine: [Pratt & Whitney JT8D-17 series](https://openairdocs.org/engine/pratt-whitney-jt8d-17-series) (registry code 52049) - Data sheets: [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs) - Serial number: 22021 - Year built: 1980 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: July 9, 1999 - Certificate issued: October 29, 2008 - Last registry action: October 29, 2008 - Mode S code: A919B4 - Owner when cancelled: [Csds Aircraft Sales & Leasing Inc](https://openairdocs.org/faa-owner/CSDS%20AIRCRAFT%20SALES%20%26%20LEASING%20INC) - Location: [Torrance, CA](https://openairdocs.org/faa-place/CA/Torrance) - Owner type: Corporation - Owner's area on the map: 33.8079° N, 118.3480° W: Placed by OpenAirDocs at the center of ZIP code 90505, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N686CA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=686CA - Page: https://openairdocs.org/deregistered/N686CA-2013-05-03 From the FAA registry file of October 31, 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 727-2S7: https://openairdocs.org/model/boeing-727-2s7.md ## Service difficulty reports (44) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR C1HA200786006](https://openairdocs.org/sdr/C1HA200786006), Oct 8, 2007: RELIEF VALVE. FAILED. UNABLE TO CONTROL CABIN PRESSURE WITH ANY MODE OF CONTROLLER. REMOVED AND REPLACED OUT FLOW VALVE IAW MM 21-31-11, PERFORMED ADJ TEST IAW MM 21-31-00, OPS CHECK - [SDR C1HA200786005](https://openairdocs.org/sdr/C1HA200786005), Oct 1, 2007: FLOORBEAM. CORRODED. CORROSION ON FLOORBEAM AT BS 1035 LBL 24-45. REMOVED EXISTING PART, FABRICATED NEW PART; TREATED AND PRIMED AND INSTALLED NEW PART IAW B727 SRM 51-30-2 FIG 1 AN - [SDR C1HA200786004](https://openairdocs.org/sdr/C1HA200786004), Oct 1, 2007: SEAT TRACK. CORRODED. CORROSION ON TRACK ANGLE AT BS 1033 LBL 54.5. REMOVED EXISTING PART, FABRICATED NEW PART; TREATED AND PRIMED AND INSTALLED NEW PART IAW B727 SRM 51-30-2 FIG 1 A - [SDR C1HA200786003](https://openairdocs.org/sdr/C1HA200786003), Oct 1, 2007: FLOORBEAM. CORRODED. NUMEROUS AREAS OF CORROSION ON FLOOR BEAM AT BS 344 LBL 25 - RBL 6. CUT OUT DAMAGED AREA. FABRICATED REPAIR PARTS AND INSTALLED REPAIR PARTS IAW B727 SRM 53-10- - [SDR C1HA200786002](https://openairdocs.org/sdr/C1HA200786002), Oct 1, 2007: FLOORBEAM. CORRODED. BS 1030 FLOORBEAM CORROSION LBL 25 - RBL 25 TOP SURFACE UPPER CHORD. REMOVED AND REPLACED PREVIOUS UPPER "T" CHORD REPAIR IAW B727 SRM 53-10-8 FIG 3. - [SDR C1HA200786001](https://openairdocs.org/sdr/C1HA200786001), Oct 1, 2007: FLOORBEAM. CORRODED. BS 1110 FLOORBEAM CORROSION LBL 45 - RBL 45 TOP SURFACE UPPER CHORD. REPAIR BS 1110 FLOORBEAM IAW B727 SRM 53-10-8 FIG 3. - [SDR C1HA200686001](https://openairdocs.org/sdr/C1HA200686001), Jan 2, 2006: SUPPORT FITTING. CRACKED. NR 3 ENGINE PYLON; DURING OPEN HOLE HFEC OF FWD SUPPORT FITTING PER TASK CARD AD 2005-19-24-02, FOUND CRACK IN HOLE P OF ANGLE 69-16977-2. REMOVED AND REPLACED - [SDR C1HA200568004](https://openairdocs.org/sdr/C1HA200568004), Sep 27, 2005: FRAME. CORRODED. UPPER FRAME CHORD CORRODED ON LWR SURFACE IN AFT PIT BS 990 OVER STR 27R JUST BEHIND AFT DOOR CUTOUT. CUT OUT DAMAGED AREA FABBED AND INSTALLED FILLER 2" BY 1" - [SDR C1HA200568003](https://openairdocs.org/sdr/C1HA200568003), Sep 27, 2005: CHANNEL. CRACKED. NLG LOCK ACTUATOR SUPPORT CHANNEL IS CRACKED BY LWR INB SUCTION VISUAL AND HFEC CONFIRMED. REMOVED AND REPLACED NLG LOCK ACTUATOR SUPPORT CHANNEL PN 69-19122-2 - [SDR C1HA200586001](https://openairdocs.org/sdr/C1HA200586001), Sep 27, 2005: SUPPORT BRACKET. CORRODED. RT NLG LOCK ACTUATOR SUPPORT BRACKET HAS NUMEROUS GOUGES CORROSION IN ONE OF THE BOLT HOLES AND WORN BUSHING. REMOVED AND REPLACED RT AND LT NLG LOCK ACTUATOR S - [SDR C1HA200586002](https://openairdocs.org/sdr/C1HA200586002), Sep 27, 2005: FRAME. CORRODED. FRAME LEG CORRODED IN FWD PIT AT FRAME 700 BETWEEN STRINGERS 28L AND 29L. CUT OUT DAMAGED AREA FABBED AND INST REPAIR DOUBLER AND ANGLE MADE FROM 7075 T6 .050 P - [SDR C1HA200568005](https://openairdocs.org/sdr/C1HA200568005), Sep 27, 2005: STIFFENER. CRACKED. RT WHEEL WELL BS 870 AND KEEL BEAM VERTICAL STIFFENER CRACKED NOT CONFIRMED. REMOVED AND REPLACED DAMAGED ANGLE PN 65-18636-378 PO NR 535322 IAW 727 SRM 51-30-2 - [SDR C1HA200386014](https://openairdocs.org/sdr/C1HA200386014), Sep 10, 2003: SEAT TRACK. CORRODED. AFT CABIN SEAT TRACK IS CORRODED AT BS 1034 LBL 25 - [SDR C1HA200386013](https://openairdocs.org/sdr/C1HA200386013), Sep 10, 2003: SUPPORT. CORRODED. CORROSION IN SEVERAL AREAS OF LT AFT LAV INBOARD WALL SUPPORT AT BS 1138/1164. - [SDR C1HA200386012](https://openairdocs.org/sdr/C1HA200386012), Sep 9, 2003: SEAT TRACK. CORRODED. CORROSION ON SEAT TRACK BS 1130 LBL 25. - [SDR C1HA200386011](https://openairdocs.org/sdr/C1HA200386011), Sep 9, 2003: SEAT TRACK. CORRODED. SEAT TRACK CORRODED BS 1090/1130 RBL 25. - [SDR C1HA200386010](https://openairdocs.org/sdr/C1HA200386010), Sep 9, 2003: SEAT TRACK. CORRODED. LITE CORROSION ON SEAT TRACK BS 990-1030 LBL 22. - [SDR C1HA200386009](https://openairdocs.org/sdr/C1HA200386009), Sep 9, 2003: SEAT TRACK. GOUGED. SEAT TRACK GOUGED AND SCRATCHED AT BS 344 RBL 50. - [SDR C1HA200386008](https://openairdocs.org/sdr/C1HA200386008), Sep 9, 2003: SEAT TRACK. CORRODED. CORROSION AROUND SEAT TRACK FASTENERS AT BS 420-480 RBL 50. - [SDR C1HA200386007](https://openairdocs.org/sdr/C1HA200386007), Sep 8, 2003: SEAT TRACK. CORRODED. BS 480 LBL 25 SEAT TRACK HAS CORROSION AROUND FASTENER. - [SDR C1HA200386006](https://openairdocs.org/sdr/C1HA200386006), Sep 8, 2003: FLOORBEAM. CORRODED. CORROSION ON FLOORBEAM UPPER CHORD AT BS 1166 RBL 45. - [SDR C1HA200386005](https://openairdocs.org/sdr/C1HA200386005), Sep 8, 2003: FLOORBEAM. CORRODED. CORROSION ON FLOORBEAM UPPER CHORD AT BS 312. - [SDR C1HA200386004](https://openairdocs.org/sdr/C1HA200386004), Sep 8, 2003: WEDGE. GOUGED. NR 3 SLAT TRAILING EDGE WEDGE GOUGED. - [SDR C1HA200386003](https://openairdocs.org/sdr/C1HA200386003), Sep 8, 2003: WEDGE. GOUGED. NR 7 SLAT TRAILING EDGE WEDGE GOUGED. - [SDR C1HA200386002](https://openairdocs.org/sdr/C1HA200386002), Sep 8, 2003: FLOORBEAM. CORRODED. CORROSION ON FLOORBEAM UPPER CHORD AT BS 344. - [SDR C1HA200386001](https://openairdocs.org/sdr/C1HA200386001), Sep 8, 2003: STRINGER. CORRODED. CORROSION ON STRINGER 29 LT AT BS 950B+8. - [SDR C1HA200286006](https://openairdocs.org/sdr/C1HA200286006), Sep 2, 2002: BATTERY. Cockpit emergency exit light is INOP.Replaced 1 battery and cleaned contact. - [SDR C1HA200286007](https://openairdocs.org/sdr/C1HA200286007), Sep 2, 2002: CONTACTOR. DIRTY. AFT AIRSTAIR EMERGENCY AREA LIGHT IS INOP. CLEANED CONTACTS ON BATTERY PACK. - [SDR C1HA200286005](https://openairdocs.org/sdr/C1HA200286005), Aug 29, 2002: POWER SUPPLY. INOPERATIVE. LT OVERWING FLOOR TRACK LIGHT POWER SUPPLY INOP. REMOVED AND REPLACED FLOOR TRACK LIGHT POWER SUPPLY. - [SDR C1HA200286004](https://openairdocs.org/sdr/C1HA200286004), Jul 26, 2002: BATTERY. R1 DOOR EMERGENCY EXIT LIGHT ( ABOVE DOOR ) INOPR&R PORBITABLE EMERGENCY EXIT LIGHT ASSEMBLY & BATTERYS IAW 73-27 MM 33-50-101 ( R1 DOOR ) - [SDR C1HA200286003](https://openairdocs.org/sdr/C1HA200286003), May 29, 2002: PUMP. STANDBY HYD FLUID DECREASED TO ZERO & GREEN ON LOGHT ON ENG PANEL EXTINGUISHED INFLIGHT. POST FLIGHT REVEALED EVIDENCE OF LEAK ON AROUND STBY PUMP IN WING ROOT. - [SDR C1HA200286002](https://openairdocs.org/sdr/C1HA200286002), May 24, 2002: CHARGER. INOPERATIVE. LEFT OVERWING EXIT SIGNS INOP. FOUND BATTERY CHARGER AND BATTERY CARTRIDGE FAULTY AT OVERWING CEILING PANEL STA 840. REMOVED AND REPLACED BATTERY CARTRIDGE AND - [SDR C1HA200286001](https://openairdocs.org/sdr/C1HA200286001), May 18, 2002: BATTERY. LOOSE. EMERGENCY EXIT LIGHT ON LEFT OVERWING INOPERATIVE. RESECURED EMERGENCY EXIT LIGHT BATTERY. OPS CHECKS GOOD IAW MM. - [SDR C1HA200186009](https://openairdocs.org/sdr/C1HA200186009), Nov 9, 2001: BATTERY. INOPERATIVE. Emergency Exit Light Inop between aft lavs. Action Taken: Removed and replaced emergency exit light battery between aft lavs. Ops check normal per 727 MM 33-50. - [SDR C1HA200196015](https://openairdocs.org/sdr/C1HA200196015), Sep 29, 2001: CAP. MISSING. EMERGENCY FLOOR TRACK LIGHTING FROM ROW 32 EXIT IS OFF. INSTALLED MISSING END CAP EMERGENCY FLOOR TRACK AT ROW 32 AS REQUIRED. - [SDR C1HA200186008](https://openairdocs.org/sdr/C1HA200186008), Jul 29, 2001: FAN. FAILED. RIGHT PACK TRIPPED OFF AT 180 DEGREES. EXPERIENCED HEAVY SMOKE IN CABIN. PAX USED O2 BELOW LIMITS. REMOVED AND REPLACED PACK FAN, OPS CHECKED NORMAL. REPLACED P - [SDR C1HA200186007](https://openairdocs.org/sdr/C1HA200186007), Jun 30, 2001: ENGINE. FOD. #2 eng EPR dropped from 2.19 to 2.12 after liftoff #2 power lever @ firewall 3 to 4 inches further than 1 or 3. Air return/Return to block.Action Taken:Inspecti - [SDR C1HA200186006](https://openairdocs.org/sdr/C1HA200186006), Jun 22, 2001: CONNECTOR. FAULTY. APU fire system will not test.ACTION TAKEN:Replaced connector at sensor responder checks good. - [SDR C1HA200186005](https://openairdocs.org/sdr/C1HA200186005), Jun 6, 2001: CONNECTOR. LOOSE. RIGHT AFT LAV SMOKE DETECTOR INOP. FOUND POWER PLUG LOOSE TIGHTENED PLUG, OPS CHECKED GOOD. - [SDR C1HA200186004](https://openairdocs.org/sdr/C1HA200186004), Apr 2, 2001: BATTERY. DISCHARGED. AFT AIRSTAIR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERIES, OPS CHECK GOOD. - [SDR C1HA200186003](https://openairdocs.org/sdr/C1HA200186003), Mar 31, 2001: CONTROL UNIT. LEAKING. LOST BOTH B-SYSTEM HYDRAULIC PUMPS, LOW PRESS LIGHTS CAME ON IN FLT. AT FL260 B-QUANTITY NORMAL LOSS OF A-QUANTITY. FLIGHT DIVERTED. AUTOBRAKE CONTROL MODULE DI - [SDR C1HA200186002](https://openairdocs.org/sdr/C1HA200186002), Feb 9, 2001: LIGHT. INOPERATIVE. AFT AIRSTAIR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED AFT AIRSTAIR EXIT LIGHT. - [SDR C1HA200186001](https://openairdocs.org/sdr/C1HA200186001), Jan 27, 2001: GASPER FAN. FAILED. IN CRUISE FLIGHT F/A NOTICED BURNING SMELL IN AFT CABIN NEAR FORWARD GALLEY. TURNED GASPER FAN OFF, SMELL DISAPPEARED. CONTINUES FLIGHT WITH GASPER FAN OFF. REM - [SDR C1HA200086001](https://openairdocs.org/sdr/C1HA200086001), Dec 30, 2000: FIRE LOOP. OUT OF POSITION. NR 2 FIRE DETECTION CIRCUIT GROUND LIGHT ILLUMINATED ON DESCENT. REPOSITIONED FIRE LOOP OPS NORMAL. ## Other aircraft with N686CA - [Registered now](https://openairdocs.org/aircraft/N686CA): Piper PA-28-181, S/N 2881130, built 2019 --- 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.