# N511PE: 1973 Boeing 727-232, registration cancelled 2017-05-31

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: May 31, 2017
- Status when cancelled: Registration expired, pending cancellation
- Airframe: [Boeing 727-232](https://openairdocs.org/model/boeing-727-232) (registry code 1384082)
- Engine: [Pratt & Whitney JT8D-9 series](https://openairdocs.org/engine/pratt-whitney-jt8d-9-series) (registry code 52048)
- Data sheets: [TCDS A3WE](https://openairdocs.org/tcds/A3WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs)
- Serial number: 20634
- Year built: 1973
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard
- Certificate issued: July 3, 2007
- Last registry action: July 9, 2010
- Mode S code: A66670
- Owner when cancelled: [U Boats Parts Inc](https://openairdocs.org/faa-owner/U%20BOATS%20PARTS%20INC)
- Location: [Miami, FL](https://openairdocs.org/faa-place/FL/Miami)
- Owner type: Corporation
- Owner's area on the map: 25.6682° N, 80.2970° W: Placed by OpenAirDocs at the center of ZIP code 33156, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N511PE
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=511PE
- Page: https://openairdocs.org/deregistered/N511PE-2017-05-31

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 (101, newest 50)

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

- [SDR C7WA200500125](https://openairdocs.org/sdr/C7WA200500125), Dec 21, 2005: INDICATOR. INTERMITTENT. AIR RETURN. IB FLAP STUCK AT 15 DEGREES, AFTER TAKEOFF. REMOVED AND REPLACED FLAP POSITION INDICATOR IAW MM. FLAP SYS OPERATIONAL CHECKS GOOD. (K)
- [SDR C7W2006F00000](https://openairdocs.org/sdr/C7W2006F00000), Dec 21, 2005: INDICATOR. INTERMITTENT. AIR RETURN. IB FLAP STUCK AT 15 DEGREES AFTER TAKEOFF. REMOVED AND REPLACED FLAP POSITION INDICATOR IAW MM. FLAP SYS OPERATIONAL CHECKS GOOD.
- [SDR C7WA200400074](https://openairdocs.org/sdr/C7WA200400074), Jan 11, 2005: ENGINE. DAMAGED. NR 3 THROTTLE VIBRATION FELT INFLIGHT ALL OTHER ENGINE INSTRUMENT AND INDICATIONS NORMAL, REF LOGPAGE NR 21307. C1, C2, AND C3 DAMAGE FOUND, NR 3 ENGINE REPLACE
- [SDR C7WA200400032](https://openairdocs.org/sdr/C7WA200400032), Jun 9, 2004: SKIN. DENTED. FOUND LEFT FUSELAGE SKIN DENTED FS 380 STRINGER 26 RT. INSTALLED EXTERNAL SKIN REPAIR IAW 727 SRM 57-30-3 FIGURE 3. (M)
- [SDR C7WA200400019](https://openairdocs.org/sdr/C7WA200400019), Jun 9, 2004: SKIN. CORRODED. FOUND WING CENTER SECTION UPPER SKIN CORRODED RBL 50 BETWEEN STATION 848 AND 870. INSTALLED INTERNAL SKIN REPAIR IAW 727 SRM 57-30-3 FIGURE 3. (M)
- [SDR C7WA200400020](https://openairdocs.org/sdr/C7WA200400020), Jun 9, 2004: SKIN. CORRODED. FOUND WING CENTER SECTION UPPER SKIN CORRODED LBL 50 BETWEEN STATION 848 AND 870. INSTALLED INTERNAL SKIN REPAIR IAW 727 SRM 57-30-3 FIGURE 3. (M)
- [SDR C7WA200400017](https://openairdocs.org/sdr/C7WA200400017), Jun 9, 2004: HINGE. CRACKED. FOUND MAIN CARGO DOOR UPPER AFT HINGE SECITON CRACKED. REMOVED AND REPLACED UPPER AFT HINGE SECTION PER AEI SERVICE BULLETIN AE01-01 AND AE MM CHAPTER 52 PAGE 1
- [SDR C7WA200400018](https://openairdocs.org/sdr/C7WA200400018), Jun 9, 2004: STRINGER. CORRODED. FOUND STRINGER 28 RIGHT STATION 1050 EVIDENCE OF CORROSION. INSTALLED EXTERNAL SKIN REPAIR IAW 727 SRM 53-30-3 FIGURE 3. (M)
- [SDR C7WA200400021](https://openairdocs.org/sdr/C7WA200400021), Jun 9, 2004: FRAME. CORRODED. FOUND AFT CARGO COMPARTMENT FUSELAGE FRAME CORRODED STAITON 1148 STRINGER 25 RIGHT. INSTALLED INTERNAL FRAME REPAIR IAW 727 SRM 51-20-1 AND 51-30-2. (M)
- [SDR C7WA200400022](https://openairdocs.org/sdr/C7WA200400022), Jun 9, 2004: STRINGER. CORRODED. FOUND AFT CARGO COMPARTMENT STRINGER 27 RIGHT STATION 950E HAS LIGHT CORROSION. INSTALLED STRINGER REPAIR IAW 727 SRM 51-40-4 FIGURE 3. (M)
- [SDR C7WA200400023](https://openairdocs.org/sdr/C7WA200400023), Jun 9, 2004: STRINGER. CORRODED. FOUND FORWARD CARGO COMPARTMENT STRINGER 27 RIGHT STATION 720E CORRODED. INSTALLED STRINGER REPAIR IAW 727 SRM 51-10-3 FIGURE 1. (M)
- [SDR C7WA200400024](https://openairdocs.org/sdr/C7WA200400024), Jun 9, 2004: STRINGER. CORRODED. FOUND FORWARD CARGO COMPARTMENT STRINGER 27 RIGHT STATION 700 CORRODED. INSTALLED STRINGER REPAIR IAW 727 SRM 51-10-3 FIGURE. (M)
- [SDR C7WA200400025](https://openairdocs.org/sdr/C7WA200400025), Jun 9, 2004: STRINGER. CORRODED. FOUND E/E COMPARTMENT STRINGER 28 LEFT STATION 720C CORRODED. INSTALLED STRINGER REPAIR IAW 727 SRM 51-10-4 FIGURE 13. (M)
- [SDR C7WA200400026](https://openairdocs.org/sdr/C7WA200400026), Jun 9, 2004: STRINGER. CORRODED. FOUND E/E COMPARTMENT STRINGER 27 LEFT STATION 450 CORRODED. INSTALLED STRINGER REPAIR IAW 727 SRM 51-10-3 FIGURE 1. (M)
- [SDR C7WA200400027](https://openairdocs.org/sdr/C7WA200400027), Jun 9, 2004: STRINGER. CORRODED. FOUND E/E COMPARTMENT STRINGER 20 RIGHT STATION 460 CORRODED. INSTALLED STRINGER REPAIR IAW 727 SRM 51-10-3 FIGURE 1. (M)
- [SDR C7WA200400028](https://openairdocs.org/sdr/C7WA200400028), Jun 9, 2004: SKIN. CORRODED. FOUND WING CENTER SECTION UPPER SKIN CORRODED FS 825.95 RBL 50. INSTALLED REPAIR IAW 727 SRM 57-30-3 FIGURE 3. (M)
- [SDR C7WA200400029](https://openairdocs.org/sdr/C7WA200400029), Jun 9, 2004: STRINGER. CORRODED. FOUND E/E COMPARTMENT STRINGER 28 RIGHT STATION 480 CORRODED. INSTALLED STRINGER REPAIR IAW 727 SRM 51-10-3 FIGURE 1. (M)
- [SDR C7WA200400030](https://openairdocs.org/sdr/C7WA200400030), Jun 9, 2004: FRAME. CORRODED. FOUND FUSELAGE FRAME UPPER CHORD CORRODED BS 950E AT STRINGER 27 RT. INSTALLED FRAME REPAIR IAW 727 SRM 53-10-4 FIGURE 2. (M)
- [SDR C7WA200400031](https://openairdocs.org/sdr/C7WA200400031), Jun 9, 2004: STRINGER. CORRODED. E/E COMPARTMENT STRINGER 26 RIGHT STATION 480 CORRODED. INSTALLED STRINGER REPAIR IAW 727 SRM 51-10-3 FIGURE 1. (M)
- [SDR C7WA200200034](https://openairdocs.org/sdr/C7WA200200034), Oct 22, 2002: OIL COOLER. FAULTY. AFTER TAEKOFF, NR 1 ENGINE OIL TEMPERATURE WENT INTO YELLOW ARC (APPROX 126) AND STAYED THERE. HIGH OIL TEMP ABNORMAL CHECKLIST ACCOMPLISHED. AFTER 15 MINUTES O
- [SDR C7WA200200033](https://openairdocs.org/sdr/C7WA200200033), Oct 22, 2002: GROUND WIRE. LOOSE. CLIMBING THROUGH FL195 FOR FL280 CABIN ALTITUDE WARNING HORN SOUNDED. CABIN ALTITUDE WAS AT 10.5. EMERGENCY DESCENT INITIATED AS PRESSURE COULD NOT BE MAINTAINE
- [SDR C7WA200200032](https://openairdocs.org/sdr/C7WA200200032), Oct 19, 2002: POSITION SWITCH. FAILED. FLT 41 - DURING TAKEOFF AT 80 KNOTS, THE FORWARD LEADING EDGE INTRANSIT LIGHT ILLUMINATED. TAKEOFF WAS ABORTED. REMOVED AND REPLACED NR 8 LEADING EDGE SLAT POSI
- [SDR COOSDR020218](https://openairdocs.org/sdr/COOSDR020218), Aug 1, 2002: SKIN. DELAMINATED. NOSE LANDING GEAR LEFT AFT DOOR DELAMINATED SKIN.
- [SDR COOSDR020217](https://openairdocs.org/sdr/COOSDR020217), Aug 1, 2002: SKIN. DELAMINATED. LEFT WING OUTBOARD AILERON TRAILING EDGE DELAMINATED.
- [SDR COOSDR020216](https://openairdocs.org/sdr/COOSDR020216), Aug 1, 2002: BULKHEAD. CRACKED. AFT CARGO COMPARTMENT PRESSURE BULKHEAD, CRACKED.
- [SDR COOSDR020221](https://openairdocs.org/sdr/COOSDR020221), Aug 1, 2002: FLAP TRACK. BROKEN. RT WING, INBOARD FLAP, NR 5 MOVABLE FAIRING INBOARD FAIRING TRACK, BROKEN.
- [SDR C7WA200200005](https://openairdocs.org/sdr/C7WA200200005), Jul 13, 2002: SKIN. DENTED. DURING C-CHECK INSPECTION, FOUND EXTERIOR FUSELAGE BS 310 BETWEEN STRINGER 23R AND 24R SKIN WITH DENT OUT OF LIMITS. REPAIRED FUSELAGE SKIN SECTION FROM BS 312.
- [SDR C7WA200200004](https://openairdocs.org/sdr/C7WA200200004), Jul 13, 2002: SKIN. DENTED. DURING C-CHECK INSPECTION, FOUND EXTERIOR FUSELAGE BS 40 BETWEEN STRINGER 19R AND 20R SKIN WITH DENT OUT OF LIMITS. INSTALLED REPAIR IAW SRM 53-30-3 FIG 13. (M)
- [SDR C7WA200200027](https://openairdocs.org/sdr/C7WA200200027), Jul 13, 2002: SKIN PANEL. DELAMINATED. DURING C-CHECK INSPECTION, FOUND LT WING OUTBOARD AILERON TRAILING EDGE PANEL DELAMINATED. REPAIRED LEFT WING OUTBOARD AILERON IAW COOPESA EO COO0CMP-2-57-366-0
- [SDR C7WA200200026](https://openairdocs.org/sdr/C7WA200200026), Jul 13, 2002: SKIN. DELAMINATED. DURING C-CHECK INSPECTION AT , FOUND NLG LEFT AFT DOOR DELAMINATED. REPAIRED DELAMINATION IAW COOPESA EO COO-CMP-2-52-369-02 WITH DER APPROVAL. (M)
- [SDR C7WA200200025](https://openairdocs.org/sdr/C7WA200200025), Jul 13, 2002: SKIN. CRACKED. DURING C-CHECK INSPECTION, FOUND EXTERIOR FUSELAGE SKIN CRACK AT BS 196.5 WL 217. REPAIRED FUSELAGE SKIN FROM BS 191.5 TO BS 203.0 BETWEEN WL 212.5 AND WL 222.5
- [SDR C7WA200200024](https://openairdocs.org/sdr/C7WA200200024), Jul 13, 2002: SKIN. CRACKED. DURING C-CHECK INSPECTION, FOUND EXTERNAL FUSELAGE SKIN CRACK AT BS 203.8 BETWEEN RIGHT WL 219 AND WL 220. REPAIRED FUSELAGE SKIN FROM BS 191.0 TO BS 209.0 BETW
- [SDR C7WA200200022](https://openairdocs.org/sdr/C7WA200200022), Jul 13, 2002: SKIN. CRACKED. DURING C-CHECK INSPECTION, FOUND FORWARD ENTRY DOOR OUTER SKIN UPPER HINGE AREA CRACKED. REPAIRED FORWARD ENTRY DOOR SKIN FROM BS 325 TO BS 316 UPPER HINGE CUTO
- [SDR C7WA200200023](https://openairdocs.org/sdr/C7WA200200023), Jul 13, 2002: SKIN. CORRODED. DURING C-CHECK INSPECTION, FOUND EXT FUSELAGE SKIN BULGED AT BS 950F PLUS 10.0 AT STRINGER 4R. REPAIRED FUSELAGE SKIN LEVEL 2 CORROSION FROM BS 950F PLUS 8.00 T
- [SDR C7WA200200021](https://openairdocs.org/sdr/C7WA200200021), Jul 13, 2002: SKIN. DENTED. DURING C-CHECK INSPECTION, FOUND FUSELAGE SKIN DENT AT BS 360 BETWEEN STRINGER 16L AND 17L. REPAIRED FUSELAGE SKIN FROM BS 360 TO BS 371.50 BETWEEN STRINGER 16L
- [SDR C7WA200200020](https://openairdocs.org/sdr/C7WA200200020), Jul 13, 2002: SKIN. DENTED. DURING C-CHECK INSPECTION, FOUND DENT AT BS 421 BETWEEN STRINGER 16R AND 17R. REPAIRED FUSELAGE SKIN FROM BS 416.25 TO BS 428 BETWEEN STRINGER 16R AND STRINGER 
- [SDR C7WA200200019](https://openairdocs.org/sdr/C7WA200200019), Jul 13, 2002: BULKHEAD. CRACKED. DURING C-CHECK INSPECTION, FOUND FUSELAGE BS 178 BULKHEAD WITH CRACK BETWEEN LBL 4.00 AND LBL 10.00 BETWEEN WL 232.T AND WL 238.5. REPAIRED CRACKED WEB IAW SRM 
- [SDR C7WA200200018](https://openairdocs.org/sdr/C7WA200200018), Jul 13, 2002: STRINGER. CORRODED. DURING C-CHECK INSPECTION, FOUND LEVEL 2 CORROSION ON FS STRINGER 26L BETWEEN BS 480 AND BS 720D. REPAIRED FUSELAGE STRINGER 26L FROM BS 480 TO BS 680 IAW SRM 5
- [SDR C7WA200200017](https://openairdocs.org/sdr/C7WA200200017), Jul 13, 2002: STRINGER. CORRODED. DURING C-CHECK INSPECTION, FOUND LEVEL 2 CORROSION ON STRINGER 25R BETWEEN BS 720F AND BS 740. REPAIRED FUSELAGE STRINGER 25R FROM BS 720D PLUS 5.00 TO BS 740 I
- [SDR C7WA200200016](https://openairdocs.org/sdr/C7WA200200016), Jul 13, 2002: STRINGER. CORRODED. DURING C-CHECK INSPECTION, FOUND LEVEL 2 CORROSION ON STRINGER 22R BETWEEN BS 720 AND BS 740. REPAIRED FUSELAGE STRINGER 22R BETWEEN BS 720E PLUS 1.50 TO BS 740
- [SDR C7WA200200015](https://openairdocs.org/sdr/C7WA200200015), Jul 13, 2002: STRINGER. CORRODED. DURING C-CHECK INSPECTION AT COOPESA-SJO, FOUND LEVEL 2 CORROSION ON STRINGER 21R BETWEEN BS 720F AND BS 740. REPAIRED FUSELAGE STRINGER 21R BETWEEN BS 720E PLU
- [SDR C7WA200200014](https://openairdocs.org/sdr/C7WA200200014), Jul 13, 2002: STRINGER. CORRODED. DURING C-CHECK INSPECTION, FOUND LEVEL 2 CORROSION ON FUSELAGE STRINGER 25L BETWEEN BS 720F AND BS 740. REPAIRED FUSELAGE STRINGER 25L BETWEEN BS 720E PLUS 5.00
- [SDR C7WA200200013](https://openairdocs.org/sdr/C7WA200200013), Jul 13, 2002: STRINGER. CORRODED. DURING C-CHECK INSPECTION, FOUND LEVEL 2 CORROSION ON STRINGER 22L BETWEEN BS 720F AND BS 740. REPAIRED FUSELAGE STRINGER 22L FROM BS 720E PLUS 4.00 TO BS 740 I
- [SDR C7WA200200012](https://openairdocs.org/sdr/C7WA200200012), Jul 13, 2002: STRINGER. CORRODED. DURING C-CHECK INSPECTION, FOUND LEVEL 2 CORROSION STRINGER 21L BETWEEN BS 720 AND 740. REPAIRED FUSELAGE STRINGER 21L FROM BS 720E PLUS 3 TO BS 740 IAW SRM 53-
- [SDR C7WA200200011](https://openairdocs.org/sdr/C7WA200200011), Jul 13, 2002: STRINGER. CORRODED. DURING C-CHECK INSPECTION, FOUND LEVEL 2 CORROSION ON STRINGER 29R FROM BS 480 TO BS 540. REPLACED STRINGER 29R SECTION BETWEEN BS 480 AND BS 545 IAW SRM 51-30-
- [SDR C7WA200200010](https://openairdocs.org/sdr/C7WA200200010), Jul 13, 2002: FRAME. CORRODED. DURING C-CHECK INSPECTION, FOUND FUSELAGE FRAME AT BS 1110 WITH LEVEL 2 CORROSION AND HOLE DAMAGED IN UPPER SECTION BETWEEN STRINGER 27L AND STRINGER 29L. REPAI
- [SDR C7WA200200006](https://openairdocs.org/sdr/C7WA200200006), Jul 13, 2002: SKIN. CANNING. DURING C-CHECK INSPECTION, FOUND EXTERIOR FUSELAGE SKIN BS 469 TO 458 BETWEEN STRINGER 21R AND 23R OIL CANNED. REPAIRED WITH DOUBLER AND FILLER IAW SRM 53-30-4 
- [SDR C7WA200200009](https://openairdocs.org/sdr/C7WA200200009), Jul 13, 2002: BULKHEAD. CRACKED. DURING C-CHECK INSPECTION, FOUND AFT AFT PRESSURE BULKHEAD BS 1183 WITH 1.5 INCH CRACK AT WL 188.31 LBL 13. REPAIRED BS 1183 WEB WITH DOUBLERS LBL 9.5 TO LBL 22
- [SDR C7WA200200008](https://openairdocs.org/sdr/C7WA200200008), Jul 13, 2002: SKIN. CORRODED. DURING C-CHECK INSPECTION, FOUND EXTERIOR FUSELAGE SKIN BULGED FROM BS 344 TO BS 360 BETWEEN STRINGER 19R AND 24R. REPAIRED FUSELAGE SKIN FROM BS 337.5 TO BS 36
- [SDR C7WA200200007](https://openairdocs.org/sdr/C7WA200200007), Jul 13, 2002: STRINGER. CORRODED. DURING C-CHECK INSPECTION, FOUND EXT FUSELAGE BETWEEN BS 440 AND BS 450 AT STRINGER 23R SKIN BULGED. REPAIRED STRINGER 23R FROM BS 440 TO BS 473 DUE TO LEVEL 2 

All 101: https://openairdocs.org/deregistered/N511PE-2017-05-31/reports.md

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