# N214UP: 1986 Boeing 727-2A1, registration cancelled 2003-05-06

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: May 6, 2003
- Exported to: Brazil
- Status when cancelled: Valid registration
- Airframe: [Boeing 727-2A1](https://openairdocs.org/model/boeing-727-2a1) (registry code 138407F)
- Engine: [Amateur-built UNKNOWN ENG](https://openairdocs.org/engine/amateur-built-unknown-eng) (registry code 99999)
- Serial number: 21342
- Year built: 1986
- Type of aircraft: Fixed wing multi engine
- Airworthiness: Provisional
- Airworthiness date: January 10, 1986
- Certificate issued: March 17, 2003
- Last registry action: March 17, 2003
- Mode S code: A1CA2E
- Owner when cancelled: [Second Platinum Aircraft Acquisition Inc](https://openairdocs.org/faa-owner/SECOND%20PLATINUM%20AIRCRAFT%20ACQUISITION%20INC)
- Location: [Miami Springs, FL](https://openairdocs.org/faa-place/FL/Miami%20Springs)
- Owner type: Corporation
- Owner's area on the map: 25.8166° N, 80.3105° W: Placed by OpenAirDocs at the center of ZIP code 33166, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N214UP
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=214UP
- Page: https://openairdocs.org/deregistered/N214UP-2003-05-06

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 727-2A1: https://openairdocs.org/model/boeing-727-2a1.md

## Service difficulty reports (91, newest 50)

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

- [SDR UPS01237375](https://openairdocs.org/sdr/UPS01237375), Dec 20, 2001: BATTERY. DISCHARGED. INSPECTION TYPE:PFLT CREW ENTRANCE EMERGENCY EXIT LIGHT DOES NOT TEST. REPLACED BATTERIES, OPS CHECKED GOOD.
- [SDR UPS01237193](https://openairdocs.org/sdr/UPS01237193), Oct 30, 2001: BULKHEAD. CORRODED. INSPECTION TYPE:IN FWD SIDE OF BS 1342 NR 2 ENGINE BULKHEAD IS CORRODED AT APPROX LBL TO LBL 40 AS VIEWED LOOKING AFT STANDING ON AIRSTAIRS JUST O/B OF NR 2 ENG
- [SDR UPS01236767](https://openairdocs.org/sdr/UPS01236767), Sep 5, 2001: WINDOW. CRACKED. INSPECTION TYPE:PFLT CAPTAIN'S L1 WINDOW INNER PANE CRACKED AND ARCHING. REPLACED L1 WINDOW PER MM 56-11-11.
- [SDR UPS01236152](https://openairdocs.org/sdr/UPS01236152), Jun 19, 2001: BATTERY. DISCHARGED. INSPECTION TYPE:N/A EMERGENCY LIGHT FAILED TEST. REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES.
- [SDR UPS01235403](https://openairdocs.org/sdr/UPS01235403), Mar 23, 2001: TERMINAL. DAMAGED. AMBER MAIN CARGO DOOR LIGHT ILLUMINATED IN FLIGHT. FOLLOWED PROCEDURES PER AOM CH 2. DIVERTED FLIGHT TO FWA. DEFERED PER MEL 52-4 AND COMPLIED WITH DMP VERIFYIN
- [SDR UPS01235239](https://openairdocs.org/sdr/UPS01235239), Feb 15, 2001: SKIN. CRACKED. INSPECTION TYPE:C, LEFT WING I/B AFT FLAP LOWER SURFACE L/E CRACKED AT O/B CENTER ECCENTRIC ROLLER FITTING CUTOUT. REPAIRED PER SRM 57-50-4.
- [SDR UPS01235023](https://openairdocs.org/sdr/UPS01235023), Jan 10, 2001: STRINGER. CORRODED. INSPECTION TYPE:C CORROSION (C53-100-01.00-04) UNDER STRINGER 29L BETWEEN BS 1166- BS 1183 AND T-CLIP AT 1183. REMOVED CORROSION ON STRINGER 29L IN AN AREA OF 1
- [SDR UPS01235022](https://openairdocs.org/sdr/UPS01235022), Jan 7, 2001: SHEAR TIE. CORRODED. INSPECTION TYPE:C CORROSION (C53-113-01.00-01) ON FRAME SHEAR TIE, BS 600 BETWEEN STR 28R AND STR 28L. FABRICATED REPAIR PARTS AND INSTALLED PER SRM 53-10-4, 51
- [SDR UPS99230991](https://openairdocs.org/sdr/UPS99230991), Oct 26, 1999: BATTERY PACK. DISCHARGED. INSPECTION TYPE:N/A, ENTRY DOOR EMERGENCY LIGHT INOP. REPLACED BATTERIES, OPS CHECK GOOD.
- [SDR UPS99230990](https://openairdocs.org/sdr/UPS99230990), Oct 26, 1999: BATTERY PACK. DISCHARGED. INSPECTION TYPE:N/A, COCKPIT EMERGENCY LIGHT INOP. REPLACED BATTERIES, OPS CHECK GOOD.
- [SDR UPS99230241](https://openairdocs.org/sdr/UPS99230241), Jul 28, 1999: SKIN. CORRODED. INSPECTION TYPE:C WHILE WORKING CARD 973519, FOUND CORROSION ON INNER SKIN AT BS 1005, RBL 7, WL 148. REMOVED CORRODED SECTION OF SKIN AT BS 1005, RBL 7, WL 148
- [SDR UPS99230239](https://openairdocs.org/sdr/UPS99230239), Jul 28, 1999: KEEL BEAM. CORRODED. INSPECTION TYPE:C CORROSION (C53-113-01.06-02) BS 982 RT KEEL BEAM. REMOVED CORRODED KEEL BEAM SEGMENT AND REPLACED WITH NEW SEGMENT IAW ER 99-5790.
- [SDR UPS99230240](https://openairdocs.org/sdr/UPS99230240), Jul 27, 1999: STRINGER. CORRODED. INSPECTION TYPE:C WHILE WORKING CUST CARD NR 973522 FOUND CORROSION ON STR 20R STA 1153. REMOVED CORRODED STRINGER BS 1153 AND REPLACED WITH NEW STRINGER IAW SR
- [SDR UPS99230238](https://openairdocs.org/sdr/UPS99230238), Jul 26, 1999: CLIP. CORRODED. INSPECTION TYPE:C CORROSION ON SHEAR TIE T-CLIP AT BS 990, RBL 8, WL 148 BETWEEN STR 29-29 R (WHILE WORKING CARD 973519). REMOVED CORRODED T-CLIP AND REPLACED W
- [SDR UPS99230172](https://openairdocs.org/sdr/UPS99230172), Jul 25, 1999: SHEAR TIE. CORRODED. INSPECTION TYPE:C WHILE WORKING 973519, FOUND CORROSION ON SHEAR TIE AT BS 970 RBL 8, WL 148 BETWEEN STRINGER 28, 29R. REPAIRED SHEAR TIE AT BS 970 RBL 8 WL 148
- [SDR UPS99230171](https://openairdocs.org/sdr/UPS99230171), Jul 23, 1999: SHEAR TIE. CORRODED. INSPECTION TYPE:C CORROSION ON FRAME SHEAR TIE BS 990, RBL 4, WL 148 BETWEEN STR 29-30R. REMOVED DAMAGE SHEAR TIE AND REPAIRED IAW SRM 53-10-04 FIG 15.
- [SDR UPS99230170](https://openairdocs.org/sdr/UPS99230170), Jul 23, 1999: SEAT TRACK. CORRODED. INSPECTION TYPE:C CORROSION ON SEAT TRACK UPPER SURFACE O/B SIDE BS 950, LBL 45. REMOVED AND REPLACED SEAT TRACK FROM BS 870 TO BS 960.
- [SDR UPS99230156](https://openairdocs.org/sdr/UPS99230156), Jul 23, 1999: CREASE BEAM. CRACKED. INSPECTION TYPE:C, LEFT I/B CREASE BEAM IS CUT AT BS 116, WL 209, LBL 64. FOUND CREASE BEAM TO BE CRACKED AT BS 1166, WL 209, LBL 64 FOUND TO BE OUT OF LIMITS. 
- [SDR UPS99230157](https://openairdocs.org/sdr/UPS99230157), Jul 22, 1999: SPLICE. CORRODED. INSPECTION TYPE:C, WHILE WORKING CARD 973519, FOUND CORROSION AND GOUGE ON STRINGER SPLICE BS 1000, STR 29R, RBL 6, WL 148. REMOVED AND REPLACED STR SPLICE BS 1
- [SDR UPS99230178](https://openairdocs.org/sdr/UPS99230178), Jul 12, 1999: CREASE BEAM. CORRODED. INSPECTION TYPE:C CORROSION ON CREASE BEAM I/B BS 1166, WL 209 RBL 64. CORROSION OUT OF LIMITS REPAIR WILL BE ACCOMPLISHED ON NRC 973389 DO TO OTHER DEFECTS REP
- [SDR UPS99230177](https://openairdocs.org/sdr/UPS99230177), Jul 12, 1999: CREASE BEAM. CORRODED. INSPECTION TYPE:C CORROSION ON I/B CREASE BEAM BS 1170 WL 208 LBL 64. CORROSION OUT OF LIMITS REPAIRS WILL BE ACCOMPLISHED ON NRC 973397, WHICH ENCOMPASS THIS A
- [SDR UPS99230112](https://openairdocs.org/sdr/UPS99230112), Jul 6, 1999: FRAME. CRACKED. INSPECTION TYPE:C, CRACKS NOTED IN BS 1183, LBL 18 DOOR FRAME. ONE CRACK AT NR 7L DOOR STOP CUTOUT AND THE OTHER CRACK AT 2 FWD OF NR 7L DOOR STOP CUTOUT. ACCES
- [SDR UPS99229972](https://openairdocs.org/sdr/UPS99229972), Jun 25, 1999: WINDOW. SHATTERED. INSPECTION TYPE:N/A, AIRCRAFT DIVERTED INTO TUL DUE TO L-2 WINDOW SHATTERED IN FLIGHT. *S/D* REMOVED AND REPLACED L-2 WINDOW WITH NEW PER MM 56-12-11 (P/N 5-717
- [SDR UPS98225724](https://openairdocs.org/sdr/UPS98225724), Feb 5, 1998: SKIN. CORRODED. INSPECTION TYPE:SI CORROSION (C53-224-01.00-02) ON INTERIOR OF SKIN AROUND PERIMETER OF SIDELIGHT BETWEEN BS 720B PLUS 5 AND 720C LBL 73 WL 218-228 BETWEEN STR 
- [SDR UPS98225711](https://openairdocs.org/sdr/UPS98225711), Feb 2, 1998: RIB. CORRODED. INSPECTION TYPE-SI, FRETTING CORROSION ON VERTICAL STAB L/E FAIRING RIB, FWD LIP AT FIN STA 55.9. RECEIVED NEW TEE-EXTRUDED RIB AND INSTALLED WEB TO NEW RIB PER
- [SDR UPS98225664](https://openairdocs.org/sdr/UPS98225664), Jan 27, 1998: BOTTLE PIN. CORRODED. INSPECTION TYPE-SI, R/W REAR BOTTLE PIN IS CORRODED. ALSO, FWD AND AFT BUSHINGS ARE MISSING SECTION OF MICARTA INNER SLEEVE CORROSION (C53-100-05.00-04). REMOVE
- [SDR UPS98225663](https://openairdocs.org/sdr/UPS98225663), Jan 27, 1998: REAR SPAR. CRACKED. INSPECTION TYPE-SI, L/W STRINGER 2ND FROM REAR SPAR ON UPPER SKIN AT WING STATION 686.5 IS CRACKED AT STRINGER 5 TO 10. REPAIRED L/W STRINGER 2ND FROM REAR SPAR
- [SDR UPS98225709](https://openairdocs.org/sdr/UPS98225709), Jan 22, 1998: SUPPORT. CORRODED. INSPECTION TYPE-SI, NR 7 FLAP TRACK FWD ATTACH FITTING IS CORRODED AT AFT BOLT HOLES FLAP TRACK FWD ATTACH POINT BUSHING HAS MIGRATED. ALSO, FWD HARDWARE REQUIR
- [SDR UPS98225710](https://openairdocs.org/sdr/UPS98225710), Jan 18, 1998: SUPPORT. CORRODED. INSPECTION TYPE-SI, NR 4 FLAP TRACK FWD ATTACH FITTING IS CORRODED AT FLAP TRACK FWD ATTACH LUG I/B SIDE. REMOVED AND REPLACED NR 4 FLAP TRACK FWD FITTING IAW M
- [SDR UPS98225496](https://openairdocs.org/sdr/UPS98225496), Jan 16, 1998: SILL. CRACKED. INSPECTION TYPE-SI, MOPSILL CRACKED LBL 54 STA 294 TO 304 WL 208. REPLACED MOPSILL AT LBL 54 STA 294 TO 304 WL 208 IAW SRM 51-30-2.
- [SDR UPS98225497](https://openairdocs.org/sdr/UPS98225497), Jan 15, 1998: BEAM. CORRODED. INSPECTION TYPE-SI, CORROSION (C53-224-01.05-02) ON LONGITUDINAL BEAM ST 760 TO 848 LBL 45 WL 208. CORROSION REWORK OUT OF LIMITS IAW SRM 53-10-1. REPLACED LONG
- [SDR UPS98225495](https://openairdocs.org/sdr/UPS98225495), Jan 14, 1998: STRINGER. CRACKED. INSPECTION TYPE-SI, DISCOVERED END OF STR 15L TO BE CRACKED AT BS 720+5. AREA OF DAMAGE REMOVED AND STRINGER END REPAIRED PER SRM 53-10-3 AND SRM 51-30-2.
- [SDR UPS98225478](https://openairdocs.org/sdr/UPS98225478), Jan 14, 1998: SKIN. CORRODED. INSPECTION TYPE-SI, WHILE CLOSING FLOOR ON CARD 656802 FOUND CORROSION ON SKIN AT BS 1090 AT STR 28R. REMOVED CORROSION IAW SRM 51-10-6 REWORK OUT OF LIMITS IAW
- [SDR UPS98225477](https://openairdocs.org/sdr/UPS98225477), Jan 14, 1998: CHORD. CORRODED. INSPECTION TYPE-SI, CORROSION (C53-224-01.05-03) ON NUT PLATE AND FLOORBEAM AT STA 1166, LBL 10, WL 208. REMOVED CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-
- [SDR UPS98225473](https://openairdocs.org/sdr/UPS98225473), Jan 14, 1998: ANGLE. CORRODED. INSPECTION TYPE-SI, CORROSION (C53-224-01.05-01) AT MOP SILL AT BOTTOM OF RT ENTRY DOOR BS 380 TO 410 RBL 63 WL 208 TOP AND BOTTOM SURFACES. REMOVED CORROSION F
- [SDR UPS98225472](https://openairdocs.org/sdr/UPS98225472), Jan 13, 1998: SEAT TRACK. CORRODED. INSPECTION TYPE-SI, CORROSION (4-25-02) ON SEAT TRACK FLANGE BETWEEN BS 720D TO 720F LBL 25. CORROSION REWORK OUT OF LIMITS IAW SRM 53-10-1. REMOVED AND REPLACE
- [SDR UPS98225470](https://openairdocs.org/sdr/UPS98225470), Jan 13, 1998: FRAME. CRACKED. INSPECTION TYPE-SI, CRACK INDICATION NOTED AT FASTENER HOLE IN FRAME AT BS 783.95 APPROX WL 207 APPROX LBL 65. REPAIRED CRACK IN FRAME STA 783.95 LBL 65 WL 207 
- [SDR UPS98225469](https://openairdocs.org/sdr/UPS98225469), Jan 13, 1998: SEAT TRACK. CORRODED. INSPECTION TYPE-SI, CORROSION (4-25-02) AND MECHANICAL DAMAGE ON SEAT TRACK WELL AND TOOTH BETWEEN BS 980 TO 1010 LBL 25. CORROSION REWORK OUT OF LIMTS IAW SRM 
- [SDR UPS98225468](https://openairdocs.org/sdr/UPS98225468), Jan 13, 1998: FLOORBEAM. CORRODED. INSPECTION TYPE-SI, CORROSION (C53-224-01.05-02) ON TOP OF FLOORBEAM 950 RBL 25 TO 65. CORROSION REWORK OUT OF LIMITS IAW SRM 53-10-1. REPAIRED 950 FLOORBEAM RB
- [SDR UPS98225467](https://openairdocs.org/sdr/UPS98225467), Jan 12, 1998: LUG. CORRODED. INSPECTION TYPE-SI, NR 4 K-FLAP HAS CORROSION ON O/B UPPER LUG WHERE BONDING JUMPER ATTACHES. REMOVED AND REPLACED NR 4 K-FLAP IAW OHM 57-51-21 AND MM 27-81-01.
- [SDR UPS98225466](https://openairdocs.org/sdr/UPS98225466), Jan 12, 1998: FLOORBEAM. CORRODED. INSPECTION TYPE-SI, CORROSION AT BS 380 RBL 45 TO 63 WL 208 ON UPPER SURFACE OF FLOORBEAM AND BOTTOM SURFACE AT FASTENER HOLES (C53-224-01.05-01). CORROSION REM
- [SDR UPS98225465](https://openairdocs.org/sdr/UPS98225465), Jan 12, 1998: SEAT TRACK. CORRODED. INSPECTION TYPE-SI, CORROSION (4-25-02) ON SEAT TRACK AT BS 720C TO BS 745 RBL 25, WL 208. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED
- [SDR UPS98225464](https://openairdocs.org/sdr/UPS98225464), Jan 12, 1998: SEAT TRACK. CORRODED. INSPECTION TYPE-SI, CORROSION (2-224-01) GOUGES AND BARE METAL ON SEAT TRACK AT BS 520 BS 610, LBL 60, WL 208. REMOVED CORROSION FOUND TO BE OUT OF LIMITS PER S
- [SDR UPS98225463](https://openairdocs.org/sdr/UPS98225463), Jan 12, 1998: LINK. CORRODED. INSPECTION TYPE-SI, CORROSION (C53-224-01.00-02) ON EXPANSION LINK AT BS 740 TO 755 LBL 45. REMOVED CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED
- [SDR UPS98225404](https://openairdocs.org/sdr/UPS98225404), Jan 9, 1998: FRAME. CORRODED. INSPECTION TYPE-SI, CORROSION ON FRAME BS 720D STR 10 TO 13 RT. REMOVED DAMAGED AREA AND INSTALLED REPAIR DOUBLER IAW SRM 51-40-3.
- [SDR UPS98225403](https://openairdocs.org/sdr/UPS98225403), Jan 9, 1998: FLOORBEAM. CORRODED. INSPECTION TYPE-SI, CORROSION AFT CARGO BAY ON FLOORBEAM, FWD LOWER FLANGE UNDER NUT PLATES BS 1070, BL 0 TO LBL 10 WL 200. REMOVED DAMAGED SECTION AND REPAIRED
- [SDR UPS98225462](https://openairdocs.org/sdr/UPS98225462), Jan 8, 1998: FLOORBEAM. CORRODED. INSPECTION TYPE-SI, CORROSION (C53-224-01.05-01) AT BS 480 LBL 45 RBL 63 WL 208 ON UPPER SURFACE OF FLOORBEAM AS MARKED. CORROSION FOUND OUT OF LIMITS PER SRM 5
- [SDR UPS98225461](https://openairdocs.org/sdr/UPS98225461), Jan 8, 1998: FLOORBEAM. CORRODED. INSPECTION TYPE-SI, CORROSION (C53-224-01.05-01) ON TOP CHORD OF FLOORBEAM AT BS 620 RBL 10 WL 208. CORROSION ON CHORD FOUND TO BE OUT OF LIMITS. FABRICATED REP
- [SDR UPS98225460](https://openairdocs.org/sdr/UPS98225460), Jan 8, 1998: SEAT TRACK. DENTED. INSPECTION TYPE-SI, CORROSION (4-25-02) ON SEAT TRACK AT BS 484 TO BS 570 BL 0 WL 208. CORROSION ON SEAT TRACK WAS FOUND TO BE WITHIN LIMITS AFTER CLEAN UP. HOW
- [SDR UPS98225397](https://openairdocs.org/sdr/UPS98225397), Jan 8, 1998: FLOORBEAM. CORRODED. INSPECTION TYPE-SI, CORROSION AFT CARGO BAY ON FLOORBEAM, FWD LOWER FLANGE AT NUT PLATE BS 950F, LBL 12, WL 200. REMOVED DAMAGED SECTION AND INSTALLED DOUBLER A

All 91: https://openairdocs.org/deregistered/N214UP-2003-05-06/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 19881017059019I](https://openairdocs.org/incident/19881017059019I), Oct 17, 1988: Boeing 727200 (N214UP), Omaha, NE. Took off and returned twice. Smoke in cockpit due to bad seal between cooling fand duct. Anti ice overheat light.

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