# N697CA: 1983 Boeing 727-270, registration cancelled 2013-07-18

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: July 18, 2013
- Status when cancelled: Registration expired, pending cancellation
- Airframe: [Boeing 727-270](https://openairdocs.org/model/boeing-727-270) (registry code 138408P)
- Data sheets: [TCDS A3WE](https://openairdocs.org/tcds/A3WE) (OpenAirDocs)
- Serial number: 23052
- Year built: 1983
- Type of aircraft: Fixed wing multi engine
- Certificate issued: September 12, 2008
- Last registry action: May 18, 2010
- Mode S code: A944EA
- 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/N697CA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=697CA
- Page: https://openairdocs.org/deregistered/N697CA-2013-07-18

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 727-270: https://openairdocs.org/model/boeing-727-270.md

## Service difficulty reports (112, newest 50)

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

- [SDR C1HA200797003](https://openairdocs.org/sdr/C1HA200797003), Jul 10, 2007: INDICATOR. MALFUNCTIONED. DURING CLIMB-OUT CAPTAINS AIRSPEED INDICATOR .95 ON CAPTAINS SIDE/COPILOTS MACH INDICATOR .76 MACH AIRSPEED CLACKER SOUNDED UNCONTROLLABLE COMPLIED WITH COM 2.3
- [SDR C1HA200797002](https://openairdocs.org/sdr/C1HA200797002), Jul 8, 2007: INDICATOR. INACCURATE. ON CLIMB-OUT, CAPTAIN'S AIRSPEED INDICATOR INDICATED ERRONEOUS AIRSPEED AND MACH. COMPLIED WITH COM 2.31.8.9.10.11.12 "FLIGHT WITH UNRELIABLE AIRSPEED/MACH" IVS
- [SDR C1HA200697021](https://openairdocs.org/sdr/C1HA200697021), Nov 25, 2006: SWITCH. FAILED. AFTER TAKEOFF DURING FLAP RETRACTION STEADY HORN SOUNDED WITH NORMAL FLAP AND GEAR INDICATIONS. PULLED CB TO SILENCE HORN. RESET CB DURING CRUISE. DURING FLAP E
- [SDR C1HA200697018](https://openairdocs.org/sdr/C1HA200697018), Sep 25, 2006: FLOORBEAM. CORRODED. CORROSION AT FLOORBEAM 360 RBL 5. REMOVED FABRICATED NEW BACL 505-100617 AND INSTALLED AT LBL 8- RBL 14 IAW SRM 53-10-8 FIG 3 AND 51-30-2.
- [SDR C1HA200697009](https://openairdocs.org/sdr/C1HA200697009), Sep 25, 2006: FLOORBEAM. CORRODED. CORROSION ON CABIN FLOOR BEAM BS 440 LBL 45 TO RBL 24. REPAIRED FLOORBEAM AT BS 440 IAW SRM 53-10-8 FIG 3.
- [SDR C1HA200697017](https://openairdocs.org/sdr/C1HA200697017), Sep 25, 2006: FLOORBEAM. CORRODED. CORROSION OF FLOORBEAM BS 1110 LBL 65 TO RBL 65. REPAIRED DAMAGED AREA ON FLOORBEAM BS 1110 FROM LBL 66 TO RBL 15 IAW SRM 53-10-2 AND 53-10-8.
- [SDR C1HA200697015](https://openairdocs.org/sdr/C1HA200697015), Sep 25, 2006: BULKHEAD. CORRODED. AFT SIDE OF COCKPIT BULKHEAD CORRODED BS 303 LBL 15-45. REMOVED AND REPLACED LOWER WEB SECTION OF AFT SIDE OF COCKPIT BULKHEAD IAW SRM 53-10-2 AND 51-20-4.
- [SDR C1HA200697002](https://openairdocs.org/sdr/C1HA200697002), Sep 25, 2006: FRAME. CRACKED. BS 1303 FRAME FIN WL (O) HAS WEB CRACK LT SIDE BOTTOM. STOP DRILLED CRACK AT FIN WL (0) IAW EO CA0909-06 REV N/C. VERIFIED CRACK STOPPED IAW NDTM PT 6 51-00-00 
- [SDR CIHA200697003](https://openairdocs.org/sdr/CIHA200697003), Sep 25, 2006: FRAME. CRACKED. BS 1303 FRAME FIN WL (6) HAS WEB CRACKED LT SIDE +6 INCHES FROM BOTTOM. STOP DRILLED CRACK AT WL 6 IAW EO CA 0909-06 REV N/C. VERIFIED CRACK STOPPED IAW NDTM PT
- [SDR C1HA200697014](https://openairdocs.org/sdr/C1HA200697014), Sep 25, 2006: FLOORBEAM. CORRODED. CORROSION ON CABIN FLOORBEAM BS 340 LBL 65 - RBL 65 UPPER AND LOWER SURFACE. REPAIRED CORRODED AREA AT BS 340 FROM BL 0 TO RBL 28 IAW B727 SRM 53-10-2 AND 53-10
- [SDR C1HA200697006](https://openairdocs.org/sdr/C1HA200697006), Sep 25, 2006: SEAT TRACK. CORRODED. PASSENGER CABIN SEAT TRACK CORRODED 1110 - 1145 LBL 24. REMOVED AND REPLACED SEAT TRACK FROM BS 990 - 1145 LBL 45 IAW B727 SRM 53-10-5 FIG 7 AND 51-30-2 FIG 1 &
- [SDR C1HA200697011](https://openairdocs.org/sdr/C1HA200697011), Sep 25, 2006: SUPPORT. CORRODED. CORROSSION ON FWD LAV AFT WALL SUPPORT BS 340 RBL 10-55. FABRICATED AND INSTALLED NEW WALL SUPPORT IAW B727 SRM 53-10-2 FIG 7 AND 51-30-2 FIG 1.
- [SDR C1HA200697010](https://openairdocs.org/sdr/C1HA200697010), Sep 25, 2006: FLOORBEAM. CORRODED. CORROSION ON FLOORBEAM (CABIN) BS 400 LBL 45- RBL 24 (UPPER T-SECTION). REMOVED UPPER T-SECTION OF FLOORBEAM FROM LBL 14 - RBL 17 IAW B727 SRM 53-10-8 FIG 3. FA
- [SDR C1HA200697016](https://openairdocs.org/sdr/C1HA200697016), Sep 25, 2006: SEAT TRACK. CORRODED. SURFACE CORROSION ON SEAT TRACK RBL 45 BS 990-1130. REMOVED AND REPLACED SECTION OF SEAT TRACK FOUND WITH CORROSION OUT OF LIMITS AT BS 970-1080 RBL 45 IAW B727
- [SDR C1HA200697013](https://openairdocs.org/sdr/C1HA200697013), Sep 25, 2006: SUPPORT. CORRODED. CORROSION IN CABIN AT FWD LAV WALL SUPPORT BS 303-340 RBL 20. FABRICATED AND INSTALLED NEW WALL SUPPORT IAW B727 SRM 53-10-2 FIG 7 AND 51-30-2 FIG 1.
- [SDR C1HA200697012](https://openairdocs.org/sdr/C1HA200697012), Sep 25, 2006: SEAT TRACK. CORRODED. FOUND CORROSION ON SEAT TRACK BS 340-480 RBL 24. REPLACED SEAT TRACK AT BS 340-480 RBL 24 AS PER B727 SRM 51-30-2, B727 SRM 53-10-2 FIG 7.
- [SDR C1HA200697020](https://openairdocs.org/sdr/C1HA200697020), Sep 25, 2006: BEAM. CORRODED. NOSE SECTION, WALKWAY BEAM LEFTSIDE INTERNAL CHANNEL ANGLE HAS CORROSION BS 304, FROM LEFT TRUNNION ACCESS WINDOW. INSTALLED REPAIR AS REQUIRED IAW EO CA 0910-0
- [SDR C1HA200697005](https://openairdocs.org/sdr/C1HA200697005), Sep 25, 2006: SHEAR TIE. CORRODED. VERT STAB NR 3 TENSION TIE MOUNT HOLE PITTED. REAMED HOLE TO REMOVE PITTING IAW B727 CHAMPION AIR M/M 55-30-61 FIG 604 AND INSTALLED A FASTENER HOLE REPAIR IAW 
- [SDR C1HA200697008](https://openairdocs.org/sdr/C1HA200697008), Sep 25, 2006: FLOORBEAM. CORRODED. FOUND FLOORBEAM CORRODED BS 460 RBL 24-65. REPAIRED FLOORBEAM BS 460 FROM RBL 33 TO RBL 36 IAW B727 SRM 53-10-2 AND 53-10-8.
- [SDR C1HA200697007](https://openairdocs.org/sdr/C1HA200697007), Sep 25, 2006: SEAT TRACK. CORRODED. FOUND PASSENGER CABIN SEAT TRACK CORRODED 1110-1145 LBL-55. REMOVED CORRODED SEAT TRACK FROM FS 1110-1145 LBL 55 IAW B727 SRM 51-30-2. FAB NEW SEAT TRACK (5'10"
- [SDR C1HA200697019](https://openairdocs.org/sdr/C1HA200697019), Sep 25, 2006: SEAT TRACK. CORRODED. FOUND SEAT TRACK AT STA 950F RBL 45 HAS CORROSION. REPAIRED SEAT TRACK AS REQUIRED IAW B727 SRM 53-10-5 FIG 7.
- [SDR C1HA200697004](https://openairdocs.org/sdr/C1HA200697004), Sep 25, 2006: TENSION TIE. CORRODED. VERT STAB TENSION TIE AFT END CORRODED. REMOVED AND REPLACED VERT STAB TENSION TIE IAW B727 MM 55-10-01 AND MM 55-30-51.
- [SDR C1HA200697001](https://openairdocs.org/sdr/C1HA200697001), Jun 14, 2006: INDICATOR. STICKING. ON FINAL APPROACH NOTICED A SPLIT FLAP INDICATION, WENT AROUND PERFORMED COM PROCEDURES 2.27.28 AND 2.274. FLAPS OPERATED NORMALLY WITH THE ALTERNATE SYSTEM. CO
- [SDR C1HA200597002](https://openairdocs.org/sdr/C1HA200597002), Aug 14, 2005: TRANSMISSION. INOPERATIVE. AFTER LANDING FLAP INDICATOR FLAPS STUCK ON 8 DEG (INBOARD) C/B`S CLOSED. PERFORMED ADJUSTMENT, FOUND SHEERED PIN ON OUTPUT DRIVE GEAR OF NR 5 FLAP TRANSMISSION
- [SDR 1HA200597001](https://openairdocs.org/sdr/1HA200597001), Jan 28, 2005: POSITION SWITCH. OUT OF ADJUST. L/E FLAPS [AMBER] LIGHT REMAINED ILLUMINATED UPON CLIMB AT/FLAP RETRACTION. NR 5 L/E FLAP ALSO ILLUMINATED ON F/E'S AUX PANEL. ADJUSTED NR 5 L/E FLAP POSITION S
- [SDR C1HA200497015](https://openairdocs.org/sdr/C1HA200497015), Sep 25, 2004: SKIN. CRACKED. NR 4 SLAT EXTERNAL SKIN IS CRACKED 2 (EA) PLACES AT AERODYNAMIC FENCE MOUNTING AREA, (MARKED). REPAIRED 2 (EA) CRACKS IN NR 4 SLAT EXTERNAL SKIN IAW B727 SRM 57
- [SDR C1HA200497016](https://openairdocs.org/sdr/C1HA200497016), Sep 25, 2004: SKIN. CRACKED. NR 4 SLAT EXTERNAL SKIN IS CRACKED 2 PLACES AT AERODYNAMIC FENCE MOUNTING AREA (MARKED). REPAIRED 2 CRACKS IN NR 4 SLAT EXTERNAL SKIN IAW B727 SRM 57-50-3 FIG 1
- [SDR C1HA200497010](https://openairdocs.org/sdr/C1HA200497010), Sep 20, 2004: RIB. CRACKED. NR 3 SLAT O/B CAP END SKIN IS CRACKED. CRACK=8 INCHES. REPLACED RIB.
- [SDR C1HA200497014](https://openairdocs.org/sdr/C1HA200497014), Sep 13, 2004: SKIN. CRACKED. NR 4 SLAT LEADING EDGE LOWER SKIN IS CRACKED AT AERODYNAMIC FENCE AFT LOWER MOUNT AREA (MARKED). REPAIRED PER SRM.
- [SDR C1HA200497011](https://openairdocs.org/sdr/C1HA200497011), Sep 13, 2004: FLOORBEAM. CORRODED. FLOORBEAM STA 1230 LBL 15 - RBL 24 IS CORRODED AROUND FASTENER HOLES. REPAIRED FLOORBEAM LBL 15 TO RBL 24.
- [SDR C1HA200497007](https://openairdocs.org/sdr/C1HA200497007), Sep 13, 2004: FLOORBEAM. CORRODED. FLOORBEAM STA 1230 LBL 15 - RBL 24 IS CORRODED AROUND FASTENER HOLES. REPAIRED FLOORBEAM LBL 15 TO RBL 24.
- [SDR C1HA200497002](https://openairdocs.org/sdr/C1HA200497002), Sep 13, 2004: RIB. GOUGED. NR 4 SLAT O/B SIDE CHAFED & GOUGED. REPLACED RIB.
- [SDR C1HA200497012](https://openairdocs.org/sdr/C1HA200497012), Sep 12, 2004: SPAR. CRACKED. NR 3 SLAT FWD SPAR CRACKED AT SLAT STA 177 FWD OF ACTUATOR CONNECTION. INSTALLED REPAIR DOUBLERS.
- [SDR C1HA200497006](https://openairdocs.org/sdr/C1HA200497006), Sep 12, 2004: RIB. CRACKED. NR 3 SLAT LEADING EDGE INTERNAL RIB IS CRACKED FWD OF ACTUATOR PISTON ROB END MOUNTING NUT (MARKED) WS 519. CRACK = 1 INCH. REPLACED RIB.
- [SDR C1HA200497005](https://openairdocs.org/sdr/C1HA200497005), Sep 12, 2004: RIB. CRACKED. NR 3 SLAT LEADING EDGE INTERNAL RIB IS CRACKED IMMEDIATE I/B OF ACTUATOR PISTON ROD END AT WS 515 (MARKED). REPAIRED RIB.
- [SDR C1HA200497004](https://openairdocs.org/sdr/C1HA200497004), Sep 12, 2004: RIB. CRACKED. NR 4 SLAT LEADING EDGE INTERNAL RIB IS CRACKED FWD OF SLAT ACTUATOR PISTON ROD END MOUNTING BOLT WS 410. CRACK = 0.500. REPLACED RIB.
- [SDR C1HA200497003](https://openairdocs.org/sdr/C1HA200497003), Sep 12, 2004: RIB. CRACKED. NR 4 SLAT LEADING EDGE INTERNAL RIB IS CRACKED IMMEDIATE I/B OF SLAT ACTUATOR PISTON ROD END WS 408 (MARKED) CRACK = 0.490. REPLACED RIB.
- [SDR C1HA200497009](https://openairdocs.org/sdr/C1HA200497009), Sep 11, 2004: RIB. CRACKED. RT WING NR 7 SLAT ACTUATOR ROD END ATTACH POINT AREA, INTERNAL RIBS CRACKED AT 2 EA PLACES ON THE RT AND 1 EA ON THE LEFT AS MARKED. REPLACED RIB.
- [SDR C1HA200497008](https://openairdocs.org/sdr/C1HA200497008), Sep 11, 2004: RIB. CRACKED. RT WING NR 5 SLAT ACTUATOR ROD END ATTACH POINT AREA, INTERNAL RIBS CRACKED AT 2 EA PLACES ON THE RT AND 2 EA ON THE LEFT AS MARKED (5 EA CRACKS TOTAL 1 EA PREV
- [SDR C1HA200497013](https://openairdocs.org/sdr/C1HA200497013), Sep 8, 2004: SKIN. CORRODED. WING CENTER BOX LWR SKIN EXFOLIATED AT S-4C LBL 24 STA 825.95. INSTALLED REPAIR DOUBLER.
- [SDR C1HA200497001](https://openairdocs.org/sdr/C1HA200497001), Jun 10, 2004: STRIKER. OUT OF ADJUST. AFT AIRSTAIR AMBER LIGHT CAME ON IN FLIGHT. RAN COM 2.25.2. RETURNED TO LAS. DAYLIGHT WAS VISABLE FROM INSIDE THE AIRCRAFT. INSPECTED & RESCHEDULED PER MEL 52-6
- [SDR C1HA20039701](https://openairdocs.org/sdr/C1HA20039701), Nov 12, 2003: CHARGER. FAILED. EMERGENCY LIGHTS OUT BETWEEN ROW 11 TO ROW 20. REMOVED & REPLACED BATTERY CHARGER PER M/M 33-50-01. OPS CHECK GOOD. P/N 11-0049
- [SDR C1HA200397016](https://openairdocs.org/sdr/C1HA200397016), Oct 21, 2003: BATTERY. INOPERATIVE. AFT AIRSTAIR OVERHEAD EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERIES, OPS CHECK NORMAL IAW MM 33-50-61.
- [SDR C1HA200397015](https://openairdocs.org/sdr/C1HA200397015), Oct 19, 2003: BATTERY PACK. INOPERATIVE. RIGHT FWD EXTERIOR WING LIGHT INOP. REMOVED & REPLACED BATTERY PACK AT STA 835. REF M/M CH 33-50-23, OPS OK.
- [SDR C1HA200397014](https://openairdocs.org/sdr/C1HA200397014), Oct 19, 2003: POWER SUPPLY. INOPERATIVE. FOUND EMERGENCY EXIT LIGHT (FLOOR TRACK) INOP FROM ROWS 12 TO 20. REMOVED & REPLACED POWER SUPPLY AT STATION 440. REF MM CH 33-50-23, OPS OK.
- [SDR C1HA200397013](https://openairdocs.org/sdr/C1HA200397013), Oct 13, 2003: BATTERY PACK. INOPERATIVE. MID CABIN FLOOR EMERGENCY PATH LIGHTING INOP. REMOVED AND REPLACED FORWARD FLOOR POWER SUPPLY AND BATTERY PACK IAW 727 MM 33-50-23. FLOOR EMERGENCY PATH LIGHTIN
- [SDR C1HA200397012](https://openairdocs.org/sdr/C1HA200397012), Jun 6, 2003: HYDRAULIC SYSTEM. LEAKING. AFTER 1 HR IN FLIGHT SYSTEM A-HYDRAULIC QUANTITY STARTED TO DECREASE, QUANTITY FELL TO 2.3 GALLONS.
- [SDR CH1A200397011](https://openairdocs.org/sdr/CH1A200397011), Apr 18, 2003: FLAP TRACK. CORRODED. NR 7 FLAP TRACK CENTER FAIRING AFT FITTING HAS SOME CORROSION.
- [SDR C1HA200397008](https://openairdocs.org/sdr/C1HA200397008), Feb 22, 2003: BATTERY. CORRODED. AFT AIRSTAIR EMERGENCY AREA LIGHT IS INOPERATIVE. CLEANED/REMOVED CORROSION FROM BATTERY CONTACTS & OPS CHECK WAS GOOD. REF: 727 MM 33-50-01.
- [SDR C1HA200397007](https://openairdocs.org/sdr/C1HA200397007), Feb 22, 2003: CONNECTOR. LOOSE. RT STA 940 EXTERIOR EMERGENCY LIGHT IS INOPERATIVE. SECURED LOOSE CONNECTOR AT BATTERY PACK IAW 727 MM 33-50-22. OPS CHECK WAS GOOD.

All 112: https://openairdocs.org/deregistered/N697CA-2013-07-18/reports.md

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20061110023159I](https://openairdocs.org/incident/20061110023159I), Nov 10, 2006: Boeing 727270 (N697CA), Huntington, WV. (-23) On November 10, 2006, at 1115E, grand holdings inc. (champion air) flight #621, a B727, was started on the ramp when airport operations personnel…

## Other aircraft with N697CA

- [Registered now](https://openairdocs.org/aircraft/N697CA): Piper PA-28-181, S/N 2881133, built 2019

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