# N14788: Boeing 727-232, registration cancelled 2000-08-29

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: August 29, 2000
- Status when cancelled: Triennial form undeliverable
- Airframe: [Boeing 727-232](https://openairdocs.org/model/boeing-727-232) (registry code 1384082)
- Data sheets: [TCDS A3WE](https://openairdocs.org/tcds/A3WE) (OpenAirDocs)
- Serial number: 20642
- Type of aircraft: Fixed wing multi engine
- Certificate issued: January 4, 1990
- Last registry action: July 10, 2000
- Mode S code: A0C042
- Owner when cancelled: [Security Pacific Equipment Leasing](https://openairdocs.org/faa-owner/SECURITY%20PACIFIC%20EQUIPMENT%20LEASING)
- 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/N14788
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=14788
- Page: https://openairdocs.org/deregistered/N14788-2000-08-29

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 (200, newest 50)

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

- [SDR CALA9901504](https://openairdocs.org/sdr/CALA9901504), Nov 16, 1999: BATTERY. DISCHARGED. INSPECTION FOUND THE RT CENTER OVERWING EMERGENCY LIGHT INOPERATIVE. THE BATTERY PACK WAS REMOVED, CHARGED, AND REINSTALLED. OPERATION CHECKED GOOD IAW MM 33-50
- [SDR CALA9901503](https://openairdocs.org/sdr/CALA9901503), Nov 16, 1999: BATTERY. DISCHARGED. INSPECTION FOUND R-2 DOOR EXIT IDENTIFIER INOPERATIVE. THE BATTERY PACK WAS REMOVED, CHARGED AND REINSTALLED. OPERATION CHECKED GOOD IAW MM 33-50-22, PAGE 401.
- [SDR CALA9901502](https://openairdocs.org/sdr/CALA9901502), Nov 16, 1999: BATTERIES. DISCHARGED. INSPECTION FOUND SELF CONTAINED FIXED EMERGENCY LIGHT INOPERATIVE IN FORWARD CABIN. THE LIGHT ASSEMBLY WAS REMOVED, THE BATTERIES WERE REPLACED, AND THE LIGHT W
- [SDR CALA9901500](https://openairdocs.org/sdr/CALA9901500), Nov 15, 1999: SKIN. DELAMINATED. INSPECTION FOUND THE NR 8 SPOILER DELAMINATED. THE NR 8 SPOILER WAS REPLACED IAW MM 27-62-1.
- [SDR CALA9900463](https://openairdocs.org/sdr/CALA9900463), May 1, 1999: POWER SUPPLY. INOPERABLE. IAH - TWO OVERWING EMERGENCY LIGHTS AND ONE EMERGENCY LIGHT AFT OF FLAPS LEFT SIDE OF FUSELAGE INOPERABLE. FOUND M654, M954, AND M955 POWER SUPPLIES BAD. REPLAC
- [SDR CALA9900198](https://openairdocs.org/sdr/CALA9900198), Feb 28, 1999: WIRE. BROKEN. INSPECTION FOUND THE LAST FIVE AISLE PATH LIGHTS WOULD NOT ILLUMINATE. MAINTENANCE FOUND A BROKEN WIRE AT AFT BATTERY PACK. THE WIRE WAS REPAIRED AND OPERATION 
- [SDR CALA9801921](https://openairdocs.org/sdr/CALA9801921), Oct 7, 1998: CONNECTOR. SHORTED. INSPECTION FOUND LT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE FOUND THE CANNON PLUG SHORTED AT POWER SUPPLY. THE PLUG WAS REPLACED AND EXIT LIGHT O
- [SDR CALA9801900](https://openairdocs.org/sdr/CALA9801900), Oct 1, 1998: WEB. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN RT MLG FLYING DOOR WEB FORWARD OF AFT HINGE FITTING. THE HINGE WEB WAS REMOVED IAW SRM 51-30-2. A NEW HINGE WEB WAS INSTALLED
- [SDR CALA9801852](https://openairdocs.org/sdr/CALA9801852), Sep 22, 1998: FITTING. CORRODED. INSPECTION FOUND RT WING NR 6 FLAP TRACK FORWARD ATTACH FITTING CORRODED. THE FLAP TRACK FITTING WAS REMOVED AND REPLACED IAW SRM 51-30-2.
- [SDR CALA9801851](https://openairdocs.org/sdr/CALA9801851), Sep 22, 1998: SKIN. LIGHTNING STRIKE. INSPECTION FOUND LIGHTNING STRIKE DAMAGE TO STATIC PORT SKIN ON RT FUSELAGE FORWARD OF FORWARD PIT DOOR AT STA 500. THE DAMAGE WAS REPAIRED IAW SRM 53-30-03.
- [SDR CALA9801847](https://openairdocs.org/sdr/CALA9801847), Sep 21, 1998: FLOORBEAM. CORRODED. INSPECTION FOUND UPPER SURFACE OF FLOORBEAM CORRODED AT BS 1166, RBL 50 TO RBL 66. THE CORROSION WAS REMOVED AND A REPAIR STRAP WAS INSTALLED IAW SRM 51-30-5, 5
- [SDR CALA9801835](https://openairdocs.org/sdr/CALA9801835), Sep 21, 1998: ANGLE. CORRODED. INSPECTION FOUND NOSE RADOME AREA LOWER L-ANGLE CORRODED AT FS 178, LBL 6 TO RBL 6. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-40-3, 51-30-2
- [SDR CALA9801834](https://openairdocs.org/sdr/CALA9801834), Sep 20, 1998: SPLICE. CORRODED. INSPECTION FOUND LT FORWARD CARGO BUTT SPLICE NR 6 AND BUTT SPLICE AT BS 720 TO 730 CORRODED. NEW BUTT SPLICES WERE INSTALLED IAW SRM 51-20-1, FIGURE 7, 51-10-2
- [SDR CALA9801833](https://openairdocs.org/sdr/CALA9801833), Sep 20, 1998: SEAT TRACK. CORRODED. INSPECTION FOUND RT SEAT TRACK CORRODED AT STA 1132-113 TO , RBL 48. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-10-5, FIGURE 7, 51-3
- [SDR CALA9801832](https://openairdocs.org/sdr/CALA9801832), Sep 20, 1998: ANGLE. CORRODED. INSPECTION FOUND ANGLE CORRODED BELOW FORWARD FLIGHT ATTENDANT'S SEAT AT STA 303.9 FROM LBL 12 TO LBL 50. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IA
- [SDR CALA9801830](https://openairdocs.org/sdr/CALA9801830), Sep 19, 1998: RIB. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN RT WING NR 5 SLAT INBOARD AND OUTBOARD RIBS AT ACTUATOR ROD END ATTACH POINT. BOTH THE INBOARD AND OUTBOARD RIBS WERE REMOVE
- [SDR CALA9801829](https://openairdocs.org/sdr/CALA9801829), Sep 19, 1998: FLOOR. CORRODED. INSPECTION FOUND COCKPIT LT SIDE FLOOR PANEL CORRODED. A NEW FLOOR PANEL WAS INSTALLED IAW SRM ECRA 5320-01448.
- [SDR CALA9801827](https://openairdocs.org/sdr/CALA9801827), Sep 19, 1998: FRAME. CRACKED. INSPECTION FOUND C-3 CARGO DOOR CUTOUT FORWARD FRAME LOWER CORNER CRACKED OUT OF BOTTOM STOP FITTING UPPER INBOARD BOLT HOLE AND LOWER PART OF FRAME WAS CORRODE
- [SDR CALA9801826](https://openairdocs.org/sdr/CALA9801826), Sep 19, 1998: FITTING. CORRODED. INSPECTION FOUND TOP OF VERTICAL STABILIZER LT HORIZONTAL HINGE ATTACH FITTINGS CORRODED. THE FITTINGS WERE REMOVED AND REPLACED IAW SRM 51-30-2, 51-30-4, AND E
- [SDR CALA9801825](https://openairdocs.org/sdr/CALA9801825), Sep 19, 1998: STRINGER. CRACKED. INSPECTION FOUND A 4 INCH CRACK IN STRINGER 14L AT STA 900. THE CRACKED SECTION OF STRINGER WAS REPLACED IAW SRM 51-30-2.
- [SDR CALA9801824](https://openairdocs.org/sdr/CALA9801824), Sep 19, 1998: WEB. CORRODED. INSPECTION FOUND RT AFT LAV FLOOR WEB CORRODED VANITY PLUMBING FITTING. THE FLOOR WEB WAS REMOVED, A NEW LAV FLOOR WEB, DOUBLER, AND FILLER WERE INSTALLED IAW S
- [SDR CALA9801823](https://openairdocs.org/sdr/CALA9801823), Sep 18, 1998: PRESS PANEL. CRACKED. INSPECTION FOUND A .1875 INCH CRACK IN NLG RT SIDE PRESSURE PANEL OUT OF FASTENER HOLE AT BS 271, WL 185. THE EXISTING DOUBLER WAS REMOVED IAW SRM 51-30-2. THE 
- [SDR CALA9801822](https://openairdocs.org/sdr/CALA9801822), Sep 18, 1998: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT STA 1130, RBL 26 TO RBL 34 AND LBL 62. THE FLOORBEAM AREAS WERE REPAIRED IAW ECRA 5321-01028 AND ECRA 5321-01027.
- [SDR CALA9801821](https://openairdocs.org/sdr/CALA9801821), Sep 18, 1998: FRAME. CORRODED. INSPECTION FOUND SIDE WALL SUPPORT FRAME CORRODED AT STA 720D ABOVE STRINGER 26R. THE CORRODED SECTION OF SUPPORT FRAME WAS REMOVED. A REPAIR ANGLE AND DOUBLER 
- [SDR CALA9801820](https://openairdocs.org/sdr/CALA9801820), Sep 18, 1998: CHANNEL. CRACKED. INSPECTION FOUND C-1 CARGO DOOR UNDER LOWER LIGHT HAD A PIECE OF PAN CRACKED OUT. THE PAN CHANNEL WAS REMOVED, A REPAIR WAS INSTALLED IAW SRM 52-30-1, 51-10-2, 
- [SDR CALA9801819](https://openairdocs.org/sdr/CALA9801819), Sep 18, 1998: ANGLE. CRACKED. INSPECTION FOUND 8 INCH CRACK IN L-ANGLE AT STA 1166, STRINGER 26L TO 26R. THE ANGLE WAS REMOVED, A REPAIR ANGLE, NUT PLATES, AND RADIUS BLOCK WERE INSTALLED IA
- [SDR CALA9801818](https://openairdocs.org/sdr/CALA9801818), Sep 18, 1998: PANEL. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN PANEL NR 3338. THE CRACKED AREA WAS CUT OUT, A WEB AND DOUBLER REPAIR WAS INSTALLED IAW SRM 51-20-1, 51-30-2, 51-10-2 AND MM
- [SDR CALA9801817](https://openairdocs.org/sdr/CALA9801817), Sep 18, 1998: CHORD. CORRODED. INSPECTION FOUND LT UPPER CHORD CORRODED INSIDE NOSE WHEEL WELL AT STA 292, LBL 20. THE CHORD WAS REMOVED AND A NEW CHORD WAS INSTALLED IAW SRM 51-30-2.
- [SDR CALA9801811](https://openairdocs.org/sdr/CALA9801811), Sep 17, 1998: STIFFENER. CORRODED. INSPECTION FOUND VERTICAL STIFFENER CORRODED AT RT FUSELAGE STA 340. A NEW STIFFENER WAS INSTALLED IAW ECRA 5300-01196 AND SRM 51-30-2.
- [SDR CALA9801810](https://openairdocs.org/sdr/CALA9801810), Sep 17, 1998: STRINGER. CORRODED. INSPECTION FOUND STRINGER 25R CORRODED AT STA 1140 TO 1183. THE STRINGER WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 53-10-3.
- [SDR CALA9801798](https://openairdocs.org/sdr/CALA9801798), Sep 16, 1998: ANGLE. CORRODED. INSPECTION FOUND LT WING NR 3 SPOILER L-ANGLE CORRODED AT INBOARD SIDE OF TRANSMISSION, WS 491. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-1
- [SDR CALA9801797](https://openairdocs.org/sdr/CALA9801797), Sep 16, 1998: MECHANISM. OUT OF ADJUST. THE LT FORWARD OVERWING EMERGENCY EXIT DOOR FAILED PULL CHECK. THE PULL FORCE ON THE DOOR WAS ADJUSTED TO SPECIFICATION IAW MM 52-21-0.
- [SDR CALA9801796](https://openairdocs.org/sdr/CALA9801796), Sep 16, 1998: SKIN. CORRODED. INSPECTION FOUND CORROSION IN FUSELAGE SKIN UNDER RIVET HEAD AT BS 560 TO 580, STRINGER 5R. THE CORRODED AREA OF SKIN WAS CUT OUT AND A DOUBLER STRAP REPAIR WAS
- [SDR CALA9801777](https://openairdocs.org/sdr/CALA9801777), Sep 15, 1998: CHORD. CORRODED. INSPECTION FOUND SHEAR TIE T-CHORD CORRODED AT STA 351.5, BL 0, WL 148.5. THE T-CHORD WAS REMOVED AND A NEW T-CHORD WAS INSTALLED IAW SRM 51-10-02.
- [SDR CALA9801776](https://openairdocs.org/sdr/CALA9801776), Sep 15, 1998: STRINGER. CORRODED. INSPECTION FOUND STRINGER 23R CORRODED AT LOWER NOSE WHEEL WELL RT LAP SEAM STA 294.5. A STRINGER REPAIR WAS INSTALLED IAW SRM 53-10-3, FIGURE 1.
- [SDR CALA9801775](https://openairdocs.org/sdr/CALA9801775), Sep 15, 1998: SKIN. IMPACTED. INSPECTION FOUND LIGHTNING STRIKE DAMAGE TO C-1 DOOR SKIN. DOUBLER WAS INSTALLED IAW SRM 52-00-3, FIGURE 4 AND ECRA 5232-01004.
- [SDR CALA9801774](https://openairdocs.org/sdr/CALA9801774), Sep 15, 1998: SKIN. DAMAGED. INSPECTION FOUND LIGHTNING STRIKE DAMAGE ON FUSELAGE SKIN AT STA 448 TO 451, STRINGER 25R, AND AT STA 380, STRINGER 23R. DOUBLERS WERE INSTALLED IAW SRM 53-30-3
- [SDR CALA9801773](https://openairdocs.org/sdr/CALA9801773), Sep 15, 1998: SEAT TRACK. CORRODED. INSPECTION FOUND LT SEAT TRACK CORRODED AT STA 1136, LBL 46. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-10-2, 51-10-2, 51-30-2, AND MM 51-20-12.
- [SDR CALA9801772](https://openairdocs.org/sdr/CALA9801772), Sep 15, 1998: CHANNEL. CRACKED. INSPECTION FOUND A 1.75 INCH CRACK IN NR 3 ENGINE PYLON UPPER FIXED COWL FORWARD END U-CHANNEL. THE CHANNEL WAS REMOVED AND A NEW CHANNEL WAS INSTALLED IAW SRM 
- [SDR CALA9801771](https://openairdocs.org/sdr/CALA9801771), Sep 15, 1998: STRAP. CORRODED. INSPECTION FOUND AFT CARGO PIT LT LOWER SIDE WALL PANEL STRAP CORRODED AT STA 1050. A NEW STRAP WAS INSTALLED IAW SRM 51-10-6.
- [SDR CALA9801770](https://openairdocs.org/sdr/CALA9801770), Sep 15, 1998: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT STA 344, RBL 65 TO LBL 65. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 51-30-2, 53-1
- [SDR CALA9801756](https://openairdocs.org/sdr/CALA9801756), Sep 14, 1998: PANEL. CORRODED. INSPECTION FOUND LT TRANSITION PANEL CORRODED IN FORWARD CARGO PIT AT FS 660 TO 720D. THE PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED IAW SRM 51-30-2, 51-10
- [SDR CALA9801755](https://openairdocs.org/sdr/CALA9801755), Sep 14, 1998: PANEL. CORRODED. INSPECTION FOUND FLOOR TRANSITION PANEL CORRODED AT BS 720A-720D, STRINGER 26R. THE PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED IAW SRM 51-30-2, 51-10-2, AN
- [SDR CALA9801754](https://openairdocs.org/sdr/CALA9801754), Sep 14, 1998: PANEL. CORRODED. INSPECTION FOUND RT TRANSITION PANEL CORRODED AROUND NUT PLATES IN FORWARD CARGO COMPARTMENT AT STA 620-720D. THE PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLE
- [SDR CALA9801753](https://openairdocs.org/sdr/CALA9801753), Sep 14, 1998: FLOOR PAN. CORRODED. INSPECTION FOUND CABIN INTERIOR CENTER AISLE FLOOR PAN CORRODED AT BS 1173, RBL 22. THE FLOOR PAN WAS REMOVED AND A NEW FLOOR PAN WAS INSTALLED IAW SRM 51-30-2,
- [SDR CALA9801730](https://openairdocs.org/sdr/CALA9801730), Sep 13, 1998: INTERCOSTAL. CORRODED. INSPECTION FOUND INTERCOSTAL CORRODED AT FS 303.9, LBL 0 TO 12. THE INTERCOSTAL WAS REMOVED AND A NEW INTERCOSTAL WAS INSTALLED IAW SRM 51-30-2.
- [SDR CALA9801729](https://openairdocs.org/sdr/CALA9801729), Sep 13, 1998: PANEL. CORRODED. INSPECTION FOUND FORWARD CARGO PIT LT TRANSITION PANEL CORRODED FROM STA 530-550. THE PANEL WAS REMOVED AND REPLACED IAW SRM 51-30-2, 51-10-2, AND MM 51-20-12.
- [SDR CALA9801728](https://openairdocs.org/sdr/CALA9801728), Sep 13, 1998: BRACKET. CRACKED. INSPECTION FOUND A 2 INCH AND 1.5 INCH CRACK IN CABIN FLOOR SUPPORT BRACKET AT STA 303.9, LBL 12. THE FLOOR SUPPORT BRACKET WAS REMOVED AND NEW BRACKET WAS INST
- [SDR CALA9801727](https://openairdocs.org/sdr/CALA9801727), Sep 13, 1998: FRAME. CORRODED. INSPECTION FOUND CORROSION AT HOLE OF LT UPPER DOOR FRAME STA 1183, WL 273, LBL 19.22. REPAIRED IAW ECRA 5310-03765.
- [SDR CALA9801726](https://openairdocs.org/sdr/CALA9801726), Sep 13, 1998: SUBFLOOR. CORRODED. INSPECTION FOUND FORWARD LAV SUBFLOOR CORRODED AT STA 340, RBL 42-60. THE LAV SUBFLOOR WAS REMOVED AND REPLACED IAW SRM 51-20-1.

All 200: https://openairdocs.org/deregistered/N14788-2000-08-29/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 19990903027259I](https://openairdocs.org/incident/19990903027259I), Sep 3, 1999: Boeing 727232 (N14788), El Paso, TX. (-23) During cruise no. 3 engine start vlv lt illuminated intermittently. Shut down no. 3 engine and diverted to elp. No other info available at this time.

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