# N356QS: 1967 Boeing 727-21, registration cancelled 2014-12-02

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: December 2, 2014
- Status when cancelled: Registration expired, pending cancellation
- Airframe: [Boeing 727-21](https://openairdocs.org/model/boeing-727-21) (registry code 1384003)
- Engine: [Pratt & Whitney JT8D series](https://openairdocs.org/engine/pratt-whitney-jt8d-series) (registry code 52053)
- Serial number: 19258
- Year built: 1967
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: November 8, 1983
- Certificate issued: February 13, 2006
- Last registry action: February 17, 2009
- Mode S code: A3FC86
- Owner when cancelled: [International Asset Group Ltd](https://openairdocs.org/faa-owner/INTERNATIONAL%20ASSET%20GROUP%20LTD)
- Location: [St Simons Island, GA](https://openairdocs.org/faa-place/GA/St%20Simons%20Island)
- Owner type: Corporation
- Owner's area on the map: 31.2572° N, 81.3420° W: Placed by OpenAirDocs at the center of ZIP code 31522, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N356QS
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=356QS
- Page: https://openairdocs.org/deregistered/N356QS-2014-12-02

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 727-21: https://openairdocs.org/model/boeing-727-21.md

## Service difficulty reports (74, newest 50)

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

- [SDR RYN2004F00026](https://openairdocs.org/sdr/RYN2004F00026), Aug 7, 2003: ACTUATOR. SPLIT. AFTER TAKEOFF, NOSE LANDING GEAR WOULD NOT RETRACT. GREEN LIGHT ON, RED L DOOR LIGHT OUT, AND HYDRAULIC PRESSURE NORMAL. AIRCRAFT CONTINUED AND LANDED WITHOUT I
- [SDR 2003F00247](https://openairdocs.org/sdr/2003F00247), Oct 29, 2002: LINE. CRACKED. ON DESCENT INTO RDU, SYSTEM PRESSURE WAS LOST ON 'A' SYSTEM HYDRAULICS. EMERGENCY WAS DECLARED AND EMERGENCY CHECKLIST WAS COMPLIED WITH. AIRCRAFT LANDED WITHOU
- [SDR LCQ05](https://openairdocs.org/sdr/LCQ05), Jan 5, 2002: WEDGE. DAMAGED. RIGHT WING OUTBOARD FWD FLAP T/E WEDGE COMPOSITE HAS DELAMINATION AND 17 FT 2 INCHES OF THE SECTION OF WEDGE MISSING AND 42 INCHES OF HONEYCOMB REMAINING.
- [SDR 2002F00116](https://openairdocs.org/sdr/2002F00116), Jan 4, 2002: WEDGE. DAMAGED. FOUND RIGHT WING OUTBOARD FORWARD FLAP TRAILING EDGE WEDGE COMPOSITE HAS DELAMINATION AND APPROXIMATELY 75 PERCENT OF THE SECTION OF WEDGE IS MISSING. (M)
- [SDR 2001F00464](https://openairdocs.org/sdr/2001F00464), Sep 11, 2001: SKIN. DAMAGED. RIGHT HORIZONTAL STABILIZER UPPER SURFACE SKIN DAMAGED AT INBOARD END AFT OF LEADING EDGE SKIN. (M)
- [SDR 2001F00428](https://openairdocs.org/sdr/2001F00428), Sep 9, 2001: DOOR FRAME. CRACKED. MAIN CARGO DOOR CUTOUT, FORWARD FRAME SKIN HAS A CRACK APPROXIMATELY AT BS 502 ABOVE STRINGER 14L. (M)
- [SDR 2001F00465](https://openairdocs.org/sdr/2001F00465), Aug 25, 2001: RUB STRIP. BULGED. VERTICAL STABILIZER UPPER FORWARD RUB STRIPS, FOR HORIZONTAL STABILIZER PATH, HAS BULGED AREAS ON BOTH RIGHT AND LEFT SIDES. (M)
- [SDR 2002F00861](https://openairdocs.org/sdr/2002F00861), Aug 22, 2001: ATTACH FITTING. CRACKED. WING CENTER SECTION INTERIOR REAR SPAR UPPER CHORD ATTACH CLIP, SMALL ANGLE, CRACKED AT BS 870 AND BBL 0. (M)
- [SDR 2002F00688](https://openairdocs.org/sdr/2002F00688), Aug 22, 2001: FRAME. CORRODED. FOUND STATION 351 HAS CORROSION AT LOWER FLANGE, LOWER SURFACE, INBOARD OF STRINGER 26L. (M)
- [SDR 2002F00687](https://openairdocs.org/sdr/2002F00687), Aug 22, 2001: STRUCTURE. CORRODED. FOUND FS 344 HAS CORROSION ON LOWER FLANGE, LOWER SURFACE, INBOARD OF STRINGER 26L. (M)
- [SDR 2002F00686](https://openairdocs.org/sdr/2002F00686), Aug 22, 2001: FRAME. CORRODED. FOUND STATION 351 HAS CORROSION AT LOWER FLANGE, LOWER SURFACE, INBOARD OF STRINGER 26L. (M)
- [SDR 2002F00685](https://openairdocs.org/sdr/2002F00685), Aug 22, 2001: FRAME. CORRODED. FOUND CORROSION AT STATION 351 AFT SIDE UNDER FRAME CHORD 6 INCHES INBOARD OF STRINGER 26L. (M)
- [SDR 2001F00463](https://openairdocs.org/sdr/2001F00463), Aug 22, 2001: DOUBLER. CRACKED. CABIN FUSELAGE STATION BS 480 STRINGER 17L LOWER FLOORBEAM ANGLE STRAP REPAIR CRACKED. (M)
- [SDR 2001F00462](https://openairdocs.org/sdr/2001F00462), Aug 22, 2001: FRAME. CORRODED. FUSELAGE STATION 351 FRAME LOWER FLANGE INBOARD OF STRINGER 26R HAS CORROSION. (M)
- [SDR 2001F00409](https://openairdocs.org/sdr/2001F00409), Aug 22, 2001: CLIP. CRACKED. WING CENTER SECTION INTERIOR REAR SPAR UPPER CHORD ATTACH CLIP (SMALL ANGLE) CRACKED AT BS 870 AND BBL 0. REMOVED AND REPLACED ATTACH CLIP IN WING CENTER SECTIO
- [SDR 2002F00717](https://openairdocs.org/sdr/2002F00717), Aug 21, 2001: STRINGER. CRACKED. FOUND LOWER CARGO COMPARTMENT BETWEEN BS 680 AND BS 700 STRINGER 20L SHOWS CRACK TO CENTER. ALSO, BS 700 FRAME TIED TO FUSELAGE IS CRACKED FROM TOP FASTENER. (M
- [SDR 2002F00707](https://openairdocs.org/sdr/2002F00707), Aug 21, 2001: PRESSURE PANEL. CORRODED. FOUND NOSE WHEEL WELL STATION 312 TO STATION 285 LEFT VERTICAL WEB LOWER EDGE HAS CORROSION ON OUTBOARD SIDE. (M)
- [SDR 2001F00461](https://openairdocs.org/sdr/2001F00461), Aug 21, 2001: FITTING. CORRODED. NOSE LANDING GEAR DRAG SUPPORT FITTING HAS CORROSION ON LOWER SURFACE. (M)
- [SDR 2001F00429](https://openairdocs.org/sdr/2001F00429), Aug 21, 2001: STRINGER. CRACKED. LOWER FORWARD CARGO COMPARTMENT BETWEEN BS 680 AND BS 700 STRINGER 20L SHOWS CRACK TO CENTER. ALSO, BS 700 FRAME TIED TO FUSELAGE IS CRACKED FROM TOP FASTENER. 
- [SDR 2002F00709](https://openairdocs.org/sdr/2002F00709), Aug 20, 2001: FRAME. CRACKED. FOUND FRAME LOWER FLANGE CRACKED AT STATION 320 BELOW STRINGER 26R. (M)
- [SDR 2002F00708](https://openairdocs.org/sdr/2002F00708), Aug 20, 2001: FRAME. CORRODED. FOUND FRAME LOWER FLANGE HAS CORROSION AT STATION 312 BELOW STRINGER 26R. (M)
- [SDR 2002F00691](https://openairdocs.org/sdr/2002F00691), Aug 20, 2001: PRESSURE PANEL. CORRODED. NOSE WHEEL WELL STATION 285 TO STATION 312 RIGHT VERTICAL WEB LOWER EDGE HAS CORROSION ON OUTBOARD SIDE. (M)
- [SDR 2002F00690](https://openairdocs.org/sdr/2002F00690), Aug 20, 2001: PRESSURE PANEL. CORRODED. NOSE LANDING GEAR WHEEL WELL STATION 328 TO STATION 351 RIGHT VERTICAL WEB HAS CORROSION ON INBOARD SIDE LOWER EDGE. (M)
- [SDR 2002F00689](https://openairdocs.org/sdr/2002F00689), Aug 20, 2001: PRESSURE PANEL. CORRODED. NOSE LANDING GEAR WHEEL WELL STATION 328 TO 351 LEFT VERTICAL WEB HAS CORROSION ON INBOARD SIDE LOWER EDGE. (M)
- [SDR 2002F00697](https://openairdocs.org/sdr/2002F00697), Aug 17, 2001: FLOOR SUPPORT. CORRODED. FOUND CORRODED COCKPIT FLOOR SUPPORT ANGLE AT BS 295 RBL 10 INCHES. (M)
- [SDR 2002F00696](https://openairdocs.org/sdr/2002F00696), Aug 17, 2001: FLOOR PANEL. CORRODED. FOUND CORROSION ON COCKPIT FLOOR SUPPORT PANEL FROM BS 259.5 TO BS 282.5 AT LBL 8. (M)
- [SDR 2002F00695](https://openairdocs.org/sdr/2002F00695), Aug 17, 2001: FLOOR PANEL. CORRODED. FOUND CORROSION ON COCKPIT FLOOR SUPPORT PANEL BS 259.5 FROM RBL 0 TO 12 AND FROM LBL 0 TO LBL 32. (M)
- [SDR 2002F00694](https://openairdocs.org/sdr/2002F00694), Aug 17, 2001: FLOOR PANEL. CORRODED. FOUND CORROSION ON UNDERSIDE OF COCKPIT FLOOR PANEL NR 2301. (M)
- [SDR 2002F00693](https://openairdocs.org/sdr/2002F00693), Aug 17, 2001: FLOOR PANEL. CORRODED. FOUND CORROSION ON COCKPIT FLOOR PANEL 2303, UNDER FACE. (M)
- [SDR 2002F00692](https://openairdocs.org/sdr/2002F00692), Aug 17, 2001: FLOOR PANEL. CORRODED. FOUND CORROSION ON UNDERSIDE OF COCKPIT FLOOR PANEL NR 2306. (M)
- [SDR 2001F00411](https://openairdocs.org/sdr/2001F00411), Aug 17, 2001: FLOOR SUPPORT. CORRODED. FOUND CORROSION ON COCKPIT FLOOR SUPPORT PANEL FROM BS 259.5 TO BS 282.5 AT LBL 8 INCHES. REMOVED FLOOR SUPPORT SECTION BETWEEN BS 259.5 TO 282.5. INSTALLED NEW
- [SDR 2001F00410](https://openairdocs.org/sdr/2001F00410), Aug 17, 2001: FLOOR SUPPORT. CORRODED. CORRODED COCKPIT FLOOR SUPPORT ANGLE AT BS 295 RBL 10 INCHES. REMOVED CORRODED FLOOR SUPPORT AT BS 295 RBL 10 INCHES IAW B727 SRM 51-30-2. REMOVED CORROSION AND
- [SDR 2002F00716](https://openairdocs.org/sdr/2002F00716), Aug 16, 2001: INTERCOSTAL. CORRODED. FOUND CORROSION ON INTERCOSTAL BETWEEN BS 970 AND BS 990 AT LBL 16. (M)
- [SDR 2002F00713](https://openairdocs.org/sdr/2002F00713), Aug 16, 2001: FRAME. CRACKED. FOUND FUSELAGE LOWER FORWARD CARGO, BS 700 STATION 20L, AT FRAME TO SKIN WEB, HAS A CRACK AT RIVET. (M)
- [SDR 2001F00430](https://openairdocs.org/sdr/2001F00430), Aug 16, 2001: FRAME. CRACKED. FUSELAGE LOWER FORWARD CARGO, BS 700 STATION 20L, AT FRAME TO SKIN WEB, HAS A CRACK AT RIVET. CUT OUT DAMAGE AREA AND INSTALLED FRAME REPAIR AT BS 700 STATION 2
- [SDR 2002F00710](https://openairdocs.org/sdr/2002F00710), Aug 9, 2001: DOUBLER. CRACKED. FOUND MAIN CARGO DOOR CUTOUT EXTERNAL DOUBLER CRACKED AND BULGED AT STATION 17L BS 560. (M)
- [SDR 2002F00712](https://openairdocs.org/sdr/2002F00712), Aug 7, 2001: SILL. CRACKED. FOUND LOWER FORWARD CARGO COMPARTMENT BS 680 LOWER SILL BEAM AT SPLICE, BOTTOM ROUTED OUT, ELONGATED AND CRACKED. ALSO, MISSING RIVET INTERIOR TO FUSELAGE SKIN.
- [SDR 2002F00711](https://openairdocs.org/sdr/2002F00711), Aug 7, 2001: SILL. CRACKED. FOUND CABIN FUSELAGE STATION BS 480 STRINGER 17L LOWER SILL BEAM TIED FRAME TO FUSELAGE, FORWARD AND AFT, ARE CRACKED. (M)
- [SDR 2002F00715](https://openairdocs.org/sdr/2002F00715), Aug 2, 2001: DOUBLER. BULGED. FOUND FUSELAGE EXTERIOR SKIN DOUBLER HAS BULGE AT STRINGER 10L BS 470, JUST FORWARD OF MAIN CARGO DOOR. (M)
- [SDR 2002F00714](https://openairdocs.org/sdr/2002F00714), Aug 2, 2001: FRAME. CRACKED. FOUND MAIN CABIN FUSELAGE FRAME CRACKED AND AFT SIDE ATTACH ANGLE CRACKED AT STATION 480 JUST BELOW STRINGER 17L. (M)
- [SDR 2002F00699](https://openairdocs.org/sdr/2002F00699), Aug 2, 2001: SCREW. MISSING. FOUND MAIN CABIN FLOOR SEAT TRACK, JUST AT MAIN CARGO DOOR FRAME, HAS LOOSE AND MISSING SCREWS, LBL 64 BETWEEN BS 540 TO BS 660. (M)
- [SDR 2002F00698](https://openairdocs.org/sdr/2002F00698), Aug 2, 2001: SEAT TRACK. DAMAGED. FOUND MAIN CABIN FLOOR SEAT TRACK DAMAGED AT BS 640, RBL 24. (M)
- [SDR 2001F00431](https://openairdocs.org/sdr/2001F00431), Aug 2, 2001: SEAT TRACK. DAMAGED. MAIN CABIN FLOOR SEAT TRACK DAMAGED AT BS 640, RBL 24. REMOVED AND REPLACED SECTION OF SEAT TRACK IN MAIN CABIN FROM BS 600 TO BS 740 RBL 24 IAW B727 SRM 53-10-
- [SDR 2002F00702](https://openairdocs.org/sdr/2002F00702), Jul 31, 2001: PANEL. CORRODED. FOUND CORROSION ON 2ND OBSERVER SEAT SUPPORT PANEL AFT AND FORWARD EDGE. (M)
- [SDR 2002F00701](https://openairdocs.org/sdr/2002F00701), Jul 31, 2001: FLOOR PANEL. CORRODED. FOUND CORROSION ON COCKPIT FLOOR SUPPORT PANEL BETWEEN BS 289.5 AND BS 312 AT RBL 12. (M)
- [SDR 2002F00700](https://openairdocs.org/sdr/2002F00700), Jul 31, 2001: FLOOR PANEL. CORRODED. FOUND CORROSION ON COCKPIT FLOOR SUPPORT PANELS FROM BS 257.5 TO BS 312, AT LBL 13. (M)
- [SDR 2001F00412](https://openairdocs.org/sdr/2001F00412), Jul 31, 2001: FLOOR SUPPORT. CORRODED. FOUND CORROSION ON COCKPIT FLOOR SUPPORT PANELS FROM BS 257.5 TO BS 312 AT LBL 13 INCHES. REMOVED CORROSION BETWEEN STATION 259.5-278 AND STATION 294-312 IAW B7
- [SDR 2002F00720](https://openairdocs.org/sdr/2002F00720), Jul 27, 2001: SKIN. BULGED. FOUND EXTERNAL LEFT FUSELAGE LAP SEAM STATION 400 TO 420, STRINGER 26L HAS A BULGE. (M)
- [SDR 2002F00719](https://openairdocs.org/sdr/2002F00719), Jul 27, 2001: SKIN. CRACKED. FOUND LOWER AFT CARGO COMPARTMENT DOOR SKIN HAS A CRACK CLOSE TO REAR LOWER EDGE. (M)
- [SDR 2002F00718](https://openairdocs.org/sdr/2002F00718), Jul 27, 2001: PANEL. CRACKED. FOUND LOWER AFT CARGO COMPARTMENT DOOR INNER BOTTOM BAFFLE PANEL HAS A BEND AT CORNERS WITH TWO CRACKS, ONE OVER PREVIOUS REPAIR. (M)

All 74: https://openairdocs.org/deregistered/N356QS-2014-12-02/reports.md

## FAA accident and incident reports (3)

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 20000112000069I](https://openairdocs.org/incident/20000112000069I), Jan 12, 2000: Boeing 72721 (N356QS), Charlotte, NC, Minor damage. (-23) N536QS operated by ryan intl landed at the Charlotte/Douglas intl airport on 01/12/2000 at approximately 0530 LCL. The aircraft was being taxied by the…
- [Incident 19971112041589I](https://openairdocs.org/incident/19971112041589I), Nov 12, 1997: Boeing 72721 (N356QS), Omaha, NE. Narrative: N356QS,B-727-21, being operated as ryan flight 524 from dayton, Ohio to Omaha, Nebraska experienced a loss of b system hydraulic fluid.…
- [Incident 19940118004159I](https://openairdocs.org/incident/19940118004159I), Jan 18, 1994: Boeing 72721 (N356QS), Nashville, TN. Narrative: on 1/18/94, ryan 205, a B-727-21, N356QS, departed Nashville, TN (bna), for dayton, OH. After takeoff, ryan 205 reported that he had a vibration in…

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