# N129NA: Boeing 727-2J7, registration cancelled 2000-11-03

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: November 3, 2000
- Exported to: Brazil
- Status when cancelled: Valid registration
- Airframe: [Boeing 727-2J7](https://openairdocs.org/model/boeing-727-2j7) (registry code 138400E)
- Serial number: 20880
- Type of aircraft: Fixed wing multi engine
- Certificate issued: August 23, 2000
- Last registry action: August 23, 2000
- Mode S code: A0764E
- 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/N129NA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=129NA
- Page: https://openairdocs.org/deregistered/N129NA-2000-11-03

From the FAA registry file of October 28, 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 727-2J7: https://openairdocs.org/model/boeing-727-2j7.md

## Service difficulty reports (16)

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

- [SDR 97ZZZX1467](https://openairdocs.org/sdr/97ZZZX1467), Oct 8, 1996: FLOOR BEAM. CORRODED. DURING C-10 INSPECTION, CORROSION WAS NOTED ON LOWER FLOOR BEAM CHORD AT FS 1166 AT BL ZERO.
- [SDR 97ZZZX1466](https://openairdocs.org/sdr/97ZZZX1466), Oct 8, 1996: SKIN. CORRODED. DURING C-10 INSPECTION, CORROSION WAS NOTED ON SKIN PANEL AT FS 340 BETWEEN S22F AND S23R.
- [SDR 97ZZZX1461](https://openairdocs.org/sdr/97ZZZX1461), Oct 8, 1996: CHANNEL. CRACKED. DURING C-10 INSPECTION, A CRACK WAS NOTED IN THE NOSE GEAR LOCK ACTUATOR CHANNEL.
- [SDR 97ZZZX1458](https://openairdocs.org/sdr/97ZZZX1458), Oct 6, 1996: STRINGER. CORRODED. DURING C-10 INSPECTION, CORROSION WAS NOTED ON STR 26L AT FS 328 UNDER FLOOR WEB.
- [SDR 97ZZZX1465](https://openairdocs.org/sdr/97ZZZX1465), Oct 4, 1996: SKIN. DENTED. DURING C-10 INSPECTION, A DENT WAS NOTED ON FUSELAGE EXTERNAL AT STA 1090 AT S18L AND S19L.
- [SDR 97ZZZX1464](https://openairdocs.org/sdr/97ZZZX1464), Oct 4, 1996: WEB. CRACKED. DURING C-10 INSPECTION, A 3.50 INCH CRACK WAS NOTED IN FS 870 WEB, FORWARD SIDE OF LT MAIN WHEELWELL. REF: C53-100-01.
- [SDR 97ZZZX1463](https://openairdocs.org/sdr/97ZZZX1463), Oct 4, 1996: ANGLE. CRACKED. DURING C-10 INSPECTION, A CRACK WAS NOTED IN ANGLE BELOW AFT AIRSTAIR ACTUATOR SUPPORT FITTING AT FS 1273. REF: C53-137-01.
- [SDR 97ZZZX1462](https://openairdocs.org/sdr/97ZZZX1462), Oct 4, 1996: SKIN. DAMAGED. DURING C-10 INSPECTION, 6 EACH FASTENER HOLES FOUND KNIFE-EDGED THROUGH SKIN AT LAP SEAM, STA 344, S23R. REF: C53-100-01.
- [SDR 97ZZZX1460](https://openairdocs.org/sdr/97ZZZX1460), Oct 4, 1996: T CHORD. CORRODED. DURING C-10 INSPECTION, CORROSION WAS NOTED ON LOWER T-CHORD, FLOOR BEAM STA 1070 AT LBL 30.
- [SDR 97ZZZX1459](https://openairdocs.org/sdr/97ZZZX1459), Oct 4, 1996: SEAT TRACK. CORRODED. DURING C-10 INSPECTION, CORROSION WAS NOTED ON CABIN SEAT TRACK FROM STA 1030 TO STA 1110 AT LBL 40.
- [SDR 97ZZZX1457](https://openairdocs.org/sdr/97ZZZX1457), Oct 4, 1996: WEB. CORODED. DURING C-10 INSPECTION, CORROSION WAS NOTED AT L-2 DOOR FRAME CUT-OUT, LOWER AFT SIDE, STA 1070 AT S17L.
- [SDR 97ZZZX1456](https://openairdocs.org/sdr/97ZZZX1456), Oct 4, 1996: STRINGER. CORRODED. DURING C-10 INSPECTION, CORROSION WAS NOTED ON S23R AT STA 340.
- [SDR 97ZZZX1455](https://openairdocs.org/sdr/97ZZZX1455), Oct 4, 1996: SKIN. CORRODED. DURING C-10 INSPECTION, CORROSION WAS NOTED IN EXTERNAL SKIN AT FS 344 AT S24L.
- [SDR 96ZZZX3519](https://openairdocs.org/sdr/96ZZZX3519), Jun 1, 1996: FITTING. CORRODED. DURING C-CHECK INSPECTION, NOTED THE FORWARD TIE-DOWN MOUNT FITTING HAD INTERGRANULAR CORROSION AT STA 560, AT S26R.
- [SDR 96ZZZX3518](https://openairdocs.org/sdr/96ZZZX3518), Jun 1, 1996: FITTING. CORRODED. DURING C-CHECK INSPECTION, NOTED THE SECOND FROM FRONT TIE-DOWN MOUNT FITTING HAD INTERGRANULAR CORROSION AT STA 570 AND STA S26R.
- [SDR 96ZZZX3517](https://openairdocs.org/sdr/96ZZZX3517), Jun 1, 1996: WEB. CORRODED. DURING C-CHECK INSPECTION, INTERGRANULAR CORROSION WAS NOTED ON FORWARD BAG PIT LOWER SILL CUT-OUT WEB. FROM STA 560 TO STA 620, LOCATED AT S26R.

## 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 19800107012269I](https://openairdocs.org/incident/19800107012269I), Jan 7, 1980: Boeing 7272J7 (N129NA), Los Angeles, CA. Passengers baggage contained fireworks which ignited and smouldered. Emergency declared. No fire.

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