# N696CA: 1981 Boeing 727-2J4, registration cancelled 2018-01-23

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: January 23, 2018
- Status when cancelled: Registration expired, pending cancellation
- Airframe: [Boeing 727-2J4](https://openairdocs.org/model/boeing-727-2j4) (registry code 138400L)
- 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: 22574
- Year built: 1981
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: December 7, 1997
- Certificate issued: November 5, 2008
- Last registry action: May 18, 2010
- Mode S code: A94133
- Owner when cancelled: [Paxair LLC](https://openairdocs.org/faa-owner/PAXAIR%20LLC)
- Location: [Chicago, IL](https://openairdocs.org/faa-place/IL/Chicago)
- Owner type: Corporation
- Owner's area on the map: 41.8667° N, 87.6149° W: Placed by OpenAirDocs at the center of ZIP code 60605, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N696CA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=696CA
- Page: https://openairdocs.org/deregistered/N696CA-2018-01-23

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 727-2J4: https://openairdocs.org/model/boeing-727-2j4.md

## Service difficulty reports (82, newest 50)

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

- [SDR C1HA200796013](https://openairdocs.org/sdr/C1HA200796013), Oct 21, 2007: FLAP SYSTEM. MALFUNCTIONED. UPON FLAP RETRACTION LE FLAP NR 6 DID NOT RETRACT. DISPATCH AND MC NOTIFIED. RETURN TO STL, REMOVED AND REPLACED NR 6 FLAP ACT IAW 27-81-22. OPS AND LEAK CK NOR
- [SDR C1HA200796012](https://openairdocs.org/sdr/C1HA200796012), Jul 22, 2007: WHEEL. FRACTURED. WHILE PERFORMING MX TAXI I/B ANTISKID LIGHT ILLUMINATED A/C TAXIED DIFFICULT STOPPED A/C AND FOUND NR 1, 2, 4 TIRES FLAT NR 3 TIRE MISSING AC REMOVED FROM SERVI
- [SDR C1HA200796007](https://openairdocs.org/sdr/C1HA200796007), May 29, 2007: STRINGER. CORRODED. CORROSION STRINGER 26R TENSION FITTING AT 1183. REMOVED AND REPLACED BS 1183 STR 26L TENSION FITTING PN 65-24276-24 IAW B727 SRM 51-30-2.
- [SDR C1HA200796006](https://openairdocs.org/sdr/C1HA200796006), May 29, 2007: STRINGER. CORRODED. CORROSION STRINGER 26L TENSION FITTING AT 1183. REMOVED AND REPLACED BS 1183 STR 26L TENSION FITTING PN 65-24276-24 PO NR 720764 IAW B727 SRM 51-30-2.
- [SDR C1HA200796002](https://openairdocs.org/sdr/C1HA200796002), May 29, 2007: SKIN. CORRODED. LT LOWER WING SURFACE APPROX BS 800 IN RAM AIR AREA IS CORRODED (PLENUM). BLENDED OUT DAMAGED AREA AND REPAIRED IAW EO-727-5710-04 REV IR.
- [SDR C1HA200796001](https://openairdocs.org/sdr/C1HA200796001), May 29, 2007: ATTACH FITTING. CORRODED. LEFT WING NR 2 FLAP TRACK FWD ATTACH FITTING CORRODED AT LUG FACE. REMOVED L/W NR 2 FLAP TRACK FWD ATTACH FITTING AND MACHINED FITTING CORRODED FACE PER SOPM 20
- [SDR C1HA200796003](https://openairdocs.org/sdr/C1HA200796003), May 29, 2007: PAN. CORRODED. AFT LAV SERVICE PAN AT RT BS 1170 IS DAMAGED AND CORRODED BEYOND LIMITS. DRILLED NEW PAN PN 65-25815-2 AND INSTALLED PAN IAW B727 MM 51-30-*2 FIG 1 AND 15. LEAK
- [SDR C1HA200796011](https://openairdocs.org/sdr/C1HA200796011), May 29, 2007: FRAME. CORRODED. CORROSION STA 312 AT DOGHOUSE, RT. REPAIRED FRAME AS REQUIRED IAW B727 SRM 53-10-4 FIG 14.
- [SDR C1HA200796005](https://openairdocs.org/sdr/C1HA200796005), May 29, 2007: STRINGER. CORRODED. CORROSION STRINGER 27R AT STA 740. REPAIRED STRINGER 27R AT STA 740 IAW B727 SRM 53-10-3 FIG 7.
- [SDR C1HA200796010](https://openairdocs.org/sdr/C1HA200796010), May 29, 2007: STRINGER. CORRODED. CORROSION STA 312 ON STRINGER 21R. CUT OUT DAMAGED AREA OF STR 21R AND REPAIRED STRINGER 21R IAW B727 SRM 53-10-3 FIG 1.
- [SDR C1HA200796009](https://openairdocs.org/sdr/C1HA200796009), May 29, 2007: TENSION TIE. CORRODED. AFT CARGO AT BS 1186 TENSION TIE FITTING AT STR 22L IS CORRODED. REMOVED DAMAGED FITTING AND INSTALLED NEW TENSION TIE FITTING PN 65-24276-26, IAW B727 SRM 51-3
- [SDR C1HA200796008](https://openairdocs.org/sdr/C1HA200796008), May 29, 2007: STRINGER. CORRODED. AFT CARGO STR 22L AT BS 1183 IS CORRODED. CUT OUT DAMAGED SECTION OF STRINGER 22L AND REPAIRED IAW B727 SRM 53-10-3 FIG 1.
- [SDR C1HA200796004](https://openairdocs.org/sdr/C1HA200796004), May 29, 2007: SUPPORT BRACKET. CRACKED. AFT AIRSTAIR AREA STA 1263 RT ANGLE SUPPORT BRACKET IS CRACK APPROX 1/2 INCH LONG INSIDE LIGHTNING HOLE. REMOVED CRACKED SUPPORT ANGLE ON AFT AIRSTAIR STA 1263 
- [SDR C1HA200596010](https://openairdocs.org/sdr/C1HA200596010), May 6, 2005: SHEAR TIE. CORRODED. STA 304 LOWER LT FRAME SHEAR TIE HAS CORROSION. REPAIRED SHEAR TIE PER SRM 53-10-4.
- [SDR C1HA200596011](https://openairdocs.org/sdr/C1HA200596011), Apr 27, 2005: LONGERON. CORRODED. E&E COMPT STA 440 LONGERON 26R, CORRODED. CENTER AND BOTTOM OF LONGERON UNDER FRAME REPLACED STRINGER FROM STA 429 TO 431 IAW SRM 53-10-2 FIG 1.
- [SDR C1HA200596009](https://openairdocs.org/sdr/C1HA200596009), Apr 26, 2005: FRAME. CORRODED. FUSELAGE INTERIOR STA 312 LOWER LT HORIZONTAL WALKBEAM, AND FRAME CORRODED (GENERATING ITEM C53-111-03-02) FUSELAGE INTERIOR STA 304 - LOWER LT FRAME HAS CORROS
- [SDR C1HA200596007](https://openairdocs.org/sdr/C1HA200596007), Apr 25, 2005: FLOORBEAM. CORRODED. MAIN PASSENGER CABIN STA 344 LBL 19 TO 57 FLOORBEAM TOP CORRODED.
- [SDR C1HA200596006](https://openairdocs.org/sdr/C1HA200596006), Apr 23, 2005: FLOOR SUPPORT. CORRODED. MAIN PASSENGER CABIN B/L 15L STA 1137 FLOOR SUPPORT CORRODED.
- [SDR C1HA200596005](https://openairdocs.org/sdr/C1HA200596005), Apr 22, 2005: FLOORBEAM. CORRODED. MAIN PASSENGER CABIN STA 1030 LBL 24 TO RBL 24 TOP OF FLOORBEAM CORRODED.
- [SDR C1HA200596004](https://openairdocs.org/sdr/C1HA200596004), Apr 22, 2005: FLOORBEAM. CORRODED. MAIN PASSENGER CABIN STA 1130 LBL 26 TO 46 TOP OF FLOORBEAM CORRODED.
- [SDR C1HA200596003](https://openairdocs.org/sdr/C1HA200596003), Apr 22, 2005: INTERCOSTAL. CORRODED. MAIN PASSENGER CABIN STA 304 TO 312 RBL 45, UNDER CONTROL CABIN BULKHEAD BOTTOM ANGLE, INTERCOSTAL CORRODED FWD END.
- [SDR C1HA200596002](https://openairdocs.org/sdr/C1HA200596002), Apr 22, 2005: INTERCOSTAL. CORRODED. MAIN PASSENGER CABIN STA 304 TO 312 RBL 55, UNDER CONTROL CABIN BULKHEAD BOTTOM ANGLE, INTERCOSTAL CORRODED FWD END.
- [SDR C1HA200596008](https://openairdocs.org/sdr/C1HA200596008), Apr 21, 2005: SKIN. BULGED. LOWER FUSELAGE BULGE IN SKIN FWD EDGE OF NOSE JACK PAD FOUND CORROSION ON THE INTERNAL DOUBLER. REMOVED AND REPLACED INTERNAL DOUBLER AT THE NOSE JACK PAD SRM 5
- [SDR C1HA200596012](https://openairdocs.org/sdr/C1HA200596012), Apr 13, 2005: STRINGER. CORRODED. FWD ASSY COMP STA 312, STRINGER 27L IS CORRODED UNDER FRAME (C53-111-03-02) STRINGER SPLICE REPAIR IAW SRM 53-10-3 FIG 3.
- [SDR CIHA200596001](https://openairdocs.org/sdr/CIHA200596001), Feb 24, 2005: INDICATOR. MALFUNCTIONED. CAPTAINS ADI SHOWED A 5 DEG BANK TURN TO THE LEFT WITH AIRCRAFT NOT IN A TURN ATTITUDE FLAG IN VIEW, WHEN DUMP VALVES WERE OPENED TANK NR 2 RT FWD AND LF AFT BO
- [SDR C1HA200396020](https://openairdocs.org/sdr/C1HA200396020), Dec 5, 2003: ENGINE. LEAKING. OIL QUANTITY DECREASED TO .1 GALLONS IN FLIGHT. OIL TEMP 112 AT POWER PRESSURE 49. AIRCRAFT DIVERTED INTO DFW. MAINTENANCE FOUND OIL COMING OUT OF THE COMBUSTIO
- [SDR C1HA200396019](https://openairdocs.org/sdr/C1HA200396019), Oct 26, 2003: DOOR. NOT CLOSED. SHORTLY AFTER TAKEOFF A LOUD NOISE FROM AIRCRAFT FORWARD WAS HEARD. THE AIRCRAFT WAS NOT PRESSURIZING. THE 1R DOOR APPEARED NOT TO BE PROPERLY SEALED. NO DOOR L
- [SDR C1HA200396018](https://openairdocs.org/sdr/C1HA200396018), Aug 29, 2003: MODULE. MALFUNCTIONED. ON DEP NOSEGEAR UNSAFE LT REMAINED ILLUM ON GEAR RETRACT. CYCLED GEAR, THEN TO OFF POSITION, NO CHANGE. VISUALLY VERIFIED NOSEGEAR DOOR CLOSED. THROUGH TELE CON
- [SDR C1HA200396017](https://openairdocs.org/sdr/C1HA200396017), Aug 28, 2003: ACCESSORY UNIT. MALFUNCTIONED. ON GEAR RETRACTION AT STL, RED NOSE GEAR LIGHT REMAINED ILLUMINATED. CYCLED GEAR HANDLE UP - LIGHT REMAINED ON (CONT) ON ARRIVAL AT LAS. RED LIGHT EXTINGUSHIED 
- [SDR C1HA200396016](https://openairdocs.org/sdr/C1HA200396016), Aug 28, 2003: WIRE. CHAFED. RED (NOSE GEAR) DISAGREEMENT LIGHT REMAINED ILLUMINATED AFTER RETRACTION IN MDJ. LIGHT EXTINGUISHED WHEN GEAR LEVER WAS PLACED TO OFF FOUND CHAFFED WIRE COMING 
- [SDR C1HA200396015](https://openairdocs.org/sdr/C1HA200396015), Aug 28, 2003: SWITCH. CONTAMINATED. BOTH RED (NOSE GEAR) DISAGREEMENT LIGHT AND GREEN (NOSE GEAR) DOWN/LOCKED LIGHT ILLUMINATED. NOSE GEAR LOCK AND POS SWITCHES ADJUSTMENT TEST DONE AFTER FOUND SW
- [SDR C1HA200396013](https://openairdocs.org/sdr/C1HA200396013), Aug 4, 2003: BATTERY. INOPERATIVE. AFT AIRSTAIRS OVERHEAD EMERGENCY LIGHT INOP. REMOVED AND REPLACED AFT BATTERY, OPS CHECK NORMAL.
- [SDR C1HA200396014](https://openairdocs.org/sdr/C1HA200396014), Aug 4, 2003: BATTERY. INOPERATIVE. AFT AIRSTAIRS OVERHEAD EMERGENCY LIGHT INOP. REMOVED AND REPLACED FWD BATTERY, OPS CHECK NORMAL.
- [SDR C1HA200396010](https://openairdocs.org/sdr/C1HA200396010), May 20, 2003: SEAT TRACK. CORRODED. PITTING CORROSION AND GOUGING ON NR 3 SEAT TRACK AT RBL 22 BETWEEN BS 690 & 740.
- [SDR C1HA200396009](https://openairdocs.org/sdr/C1HA200396009), May 20, 2003: SEAT TRACK. CORRODED. PITTING CORROSION AND GOUGING ON NR 2 SEAT TRACK AT LBL 22 BETWEEN BS 480 & 620.
- [SDR C1HA200396008](https://openairdocs.org/sdr/C1HA200396008), May 20, 2003: SEAT TRACK. CORRODED. PITTING CORROSION AND GOUGING ON NR 1 SEAT TRACK AT LBL 44 BETWEEN BS 380 & 480.
- [SDR C1HA200396007](https://openairdocs.org/sdr/C1HA200396007), May 20, 2003: SEAT TRACK. GOUGED. GOUGING ON NR 1 SEAT TRACK AT LBL 44 BETWEEN BS 344 & 380.
- [SDR C1HA200396011](https://openairdocs.org/sdr/C1HA200396011), May 20, 2003: SEAT TRACK. CORRODED. PITTING CORROSION AND GOUGING ON NR 4 SEAT TRACK AT RBL 44 BETWEEN BS 690 & 740
- [SDR C1HA200396012](https://openairdocs.org/sdr/C1HA200396012), May 20, 2003: SEAT TRACK. CORRODED. AFT CABIN SEAT TRACK RBL 45 HAS NUMEROUS AREAS OF PITTING CORROSION BETWEEN BS 955F AND 1070
- [SDR C1HA200396006](https://openairdocs.org/sdr/C1HA200396006), May 20, 2003: SEAT TRACK. GOUGED. LT OTBD SEAT TRACK GOUGED BETWEEN BS 954 & 956
- [SDR C1HA200396005](https://openairdocs.org/sdr/C1HA200396005), May 19, 2003: SEAT TRACK. CORRODED. PITTING CORROSION AND GOUGING ON NR 2 SEAT TRACK AT LBL22, BETWEEN BS 480 & 620.
- [SDR C1HA200396003](https://openairdocs.org/sdr/C1HA200396003), Feb 27, 2003: SWITCH. MALFUNCTIONED. DURING TAXI IN LAS NOSE GEAR DOOR LIGHT ILLUMINATED. OPENED NOSE GEAR DOORS AND INSPECTED DOOR LOCK SWITCH. ADJUSTED NOSE GEAR DOOR ADJ. STRUT & OPS CHECKED DOO
- [SDR C1HA200396004](https://openairdocs.org/sdr/C1HA200396004), Feb 12, 2003: SWITCH. BURNED. LEAVING 12000 FT SMELLED STRONG ELECTRICAL BURNING ODOR F/O NOTICED FIRST. NO SMOKE WAS SEEN. NOTICED AUTO COOLING DOOR BEGAN TO OPEN. FOUND 2 POSTS AND WIRES T
- [SDR C1HA200396002](https://openairdocs.org/sdr/C1HA200396002), Feb 10, 2003: WIRE. SHORTED. LEAVING 15,000 FT SMELLED STRONG ELETRICAL ODOR, STRONG ELECTRICAL BURNING ODOR. F/O NOTICED FIRST. NO SMOKE WAS SEEN. REPOSITIONED WIRE CONTACTING GROUND ON AN
- [SDR C1HA200396001](https://openairdocs.org/sdr/C1HA200396001), Jan 5, 2003: WARNING LIGHT. ILLUMINATED. AFTER GEAR RETRACTION, THE FWD DOOR LIGHT AND F/E'S RT GEAR DOOR LIGHT REMAINED ILLUMINATED. PERFORMED COM PROCEDURE 2.32.29 AND BOTH LIGHTS EXTINGUISHED. INSTA
- [SDR C1HA200296017](https://openairdocs.org/sdr/C1HA200296017), Dec 14, 2002: OIL FILTER. BYPASSING. ABORTED TAKEOFF DUE TO NR 2 ENGINE OIL BYPASS LIGHT ILLUMINATED. REMOVED AND INSPECTED NR 2 ENGINE MAIN OIL FILTER IAW M/M 72-61-08, LEAK AND OPS CHECK GOOD. FO
- [SDR C1HA200296016](https://openairdocs.org/sdr/C1HA200296016), Nov 9, 2002: LIGHT. INOPERATIVE. EMERGENCY EXIT SIGN RT OF AFT AIRSTAIR EXIT 1 BULB OUT. RELAMPED 1 BULB EMERGENCY EXIT SIGN RIGHT OF AFT AIRSTAIR EXIT.
- [SDR C1HA200296015](https://openairdocs.org/sdr/C1HA200296015), Jun 8, 2002: COMPRESSOR. STALLED. ON TAKEOFF IN LAS HAD COMPRESSOR STALL, PULLED OFF RUNWAY CALLED MX CONTROL. RAN UP ENGINE, ALL ENGINE PARAMETERS NORMAL. INSPECTED ALL ENGINES AND NO DEFECTS F
- [SDR C1HA200296014](https://openairdocs.org/sdr/C1HA200296014), May 10, 2002: POWER SUPPLY. INOPERATIVE. LH aft exterior emergency light inoperative. Removed and replaced power supply IAW MM. Operationally checks good.
- [SDR C1HA200296013](https://openairdocs.org/sdr/C1HA200296013), Apr 11, 2002: TRANSMITTER. FAILED. ONE TAKEOFF ROLL, NR 2 EPR GAUGE INOPERATIVE. ABORTED TAKEOFF. TROUBLESHOT SYSTEM AND REMOVED AND REPLACED NR 2 EPR TRANSMITTER. ENGINE RUN UP TO MAX. TRIM AND 

All 82: https://openairdocs.org/deregistered/N696CA-2018-01-23/reports.md

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