# N357QS: 1967 Boeing 727-21, registration cancelled 2004-08-24 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: August 24, 2004 - Status when cancelled: Triennial form not returned - Airframe: [Boeing 727-21](https://openairdocs.org/model/boeing-727-21) (registry code 1384003) - Engine: [Pratt & Whitney JT8D-1](https://openairdocs.org/engine/pratt-whitney-jt8d-1) (registry code 52044) - Data sheets: [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs) - Serial number: 19259 - Year built: 1967 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: October 21, 1983 - Certificate issued: December 8, 1992 - Last registry action: March 19, 2002 - Mode S code: A4003D - Owner when cancelled: [Emery Worldwide Airlines Inc](https://openairdocs.org/faa-owner/EMERY%20WORLDWIDE%20AIRLINES%20INC) - Location: [Redwood City, CA](https://openairdocs.org/faa-place/CA/Redwood%20City) - Owner type: Corporation - Owner's area on the map: 37.5334° N, 122.2496° W: Placed by OpenAirDocs at the center of ZIP code 94065, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N357QS - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=357QS - Page: https://openairdocs.org/deregistered/N357QS-2004-08-24 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 (21) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR RYN2002F00004](https://openairdocs.org/sdr/RYN2002F00004), Aug 14, 2001: STRINGER. CORRODED. STRINGER EXFOLIATED BETWEEN BS 1148 TO BS 1166 BETWEEN STRINGER 3L AND 4L IN THE AFT CABIN CROWN AREA. ACCOMPLISHED FUSELAGE STRINGER REPAIR BS 1148 TO 1166 BET - [SDR 2002F00848](https://openairdocs.org/sdr/2002F00848), Aug 13, 2001: FITTING. CRACKED. FOUND CRACK AROUND C2 DOOR FORWARD UPPER HINGE ATTACH POINT AT BS 1070 STRINGER 20R AND 19R. ACCOMPLISHED C2 DOOR FORWARD FRAME REPAIR AT BS 1070 STRINGER 20R A - [SDR 2002F00841](https://openairdocs.org/sdr/2002F00841), Aug 6, 2001: STRINGER. DAMAGED. HOLE FOUND IN LOWER RADIUS AT BS 370 STRINGER 6R. ACCOMPLISHED FUSELAGE STRINGER REPAIR AT BS 370, STRINGER 6R IAW B727 SRM 53-10-2, FIGURE 2. (M) - [SDR 2002F00847](https://openairdocs.org/sdr/2002F00847), Aug 5, 2001: STRUCTURE. CORRODED. LEFT NOSE WHEEL WELL VERTICAL WEB EXFOLIATED AT INTERSECTION WITH UPPER NOSE CHORD AS VIEWED FROM DOG HOUSE AT BS 315 DUE TO CORROSION. ACCOMPLISHED NOSE WHEEL - [SDR 2002F00846](https://openairdocs.org/sdr/2002F00846), Aug 5, 2001: PRESSURE PANEL. CORRODED. NOSE WHEEL WELL SKIN CRACKED LEFT SIDE AT STATION 243.7. ACCOMPLISHED NOSE WHEEL WELL RIGHT SIDE SKIN REPAIR AT BS 243.7 IAW B727 SRM 51-40-2, FIGURE 1. (M) - [SDR 2002F00845](https://openairdocs.org/sdr/2002F00845), Aug 5, 2001: PRESSURE PANEL. CRACKED. NOSE WHEEL WELL RIGHT SIDE SKIN HAS A VERTICAL CRACK AT STATION 270. ACCOMPLISHED NOSE WHEEL WELL RIGHT SIDE SKIN REPAIR AT BS 270 IAW B727 SRM 51-40-2, FIGURE - [SDR 2002F00844](https://openairdocs.org/sdr/2002F00844), Aug 5, 2001: PRESSURE PANEL. CORRODED. DUE TO CORROSION, RIGHT NOSE WHEEL WELL VERTICAL WEB EXFOLIATED AT INTERSECTION WITH UPPER NOSE CHORD AS VIEWED FROM DOG HOUSE BS 315. ACCOMPLISHED RIGHT NOSE W - [SDR 2002F00843](https://openairdocs.org/sdr/2002F00843), Aug 5, 2001: FRAME. CORRODED. RIGHT NOSE WHEEL WELL, MID CHORD EXFOLIATED AT INTERSECTION OF RIGHT WEB AND FLOOR WEB AS VIEWED FROM DOG HOUSE. ACCOMPLISHED RIGHT NOSE WHEEL WELL MID CHORD RE - [SDR 2002F00842](https://openairdocs.org/sdr/2002F00842), Aug 5, 2001: SKIN. CORRODED. BULGING AND PILLOWING SKIN ON STRINGER 8L AT BS 1166 THROUGH BS 1183. ACCOMPLISHED FUSELAGE SKIN REPAIR FROM BS 1166 TO BS 1183 STRINGER 8L DUE TO CORROSION IAW - [SDR 2002F00840](https://openairdocs.org/sdr/2002F00840), Aug 5, 2001: SKIN. CORRODED. BULGING SKIN ALONG STRINGER 10L AT BS 920 THROUGH 1005 DUE TO CORROSION. ACCOMPLISHED FUSELAGE SKIN REPAIR FROM BS 920 TO BS 1005 AT STRIGNER 10L IAW B727 SRM 5 - [SDR RYN2002F00000](https://openairdocs.org/sdr/RYN2002F00000), Aug 5, 2001: SUPPORT. DAMAGED. AT MAIN CARGO DOOR FORWARD ACTUATOR, FORWARD AND AFT SUPPORT BLOCK ON DOOR STATION 540, 5 BOLTS HAVE OBLONGED/ELONGATED HOLES AND 1 LOOSE BOLT. ACCOMPLISHED MAI - [SDR 2001F00391](https://openairdocs.org/sdr/2001F00391), Aug 5, 2001: FRAME. CORRODED. RIGHT NOSE WHEEL WELL, MID CHORD EXFOLIATED AT INTERSECTION OF RIGHT WEB AND FLOOR WEB AS VIEWED FROM DOG HOUSE. ACCOMPLISHED RIGHT NOSE WHEEL WELL MID CHORD RE - [SDR RYN2002F00003](https://openairdocs.org/sdr/RYN2002F00003), Aug 5, 2001: SKIN. CORRODED. BULGING SKIN/DISHED FASTENER AT BS 1176 THRU BS 1183, STRINGER 20L THRU 21L UNDER AFT LAV SERVICE VALVE. ACCOMPLISHED FUSELAGE SKIN REPAIR FROM BS 1176 TO BS 11 - [SDR RYN2002F00002](https://openairdocs.org/sdr/RYN2002F00002), Aug 5, 2001: SKIN. DAMAGED. BULGING AND PILLOWING SKIN AT BS 1085 THRU BS 1110 ALONG FASTENER ROWS AT STRINGER 17R THRU 19R ON EXTERNAL FUSELAGE. ACCOMPLISHED FUSELAGE SKIN REPAIR FROM BS - [SDR RYN2002F00001](https://openairdocs.org/sdr/RYN2002F00001), Aug 5, 2001: SKIN. DAMAGED. BULGING/PILLOWING SKIN ALONG STRINGER 4L AT LAP JOINT BS 1130 THRU BS 1183. ACCOMPLISHED FUSELAGE SKIN REPAIR FROM BS 1130 TO BS 1183 STRINGER 4L DUE TO CORROSI - [SDR 2001F00201](https://openairdocs.org/sdr/2001F00201), Jul 14, 2001: FLAP. OUT OF ADJ. MODERATE VIBRATION DURING CLIMB-OUT, ABOVE 260 KNOTS. VIBRATION STOPPED WHEN APPLYING SPEED BRAKES. FUEL DUMPED. RETURNED TO AIRPORT WITH NO INCIDENT. ADJUSTED - [SDR 20010112SG042](https://openairdocs.org/sdr/20010112SG042), Dec 1, 2000: BULB. DAMAGED. FLT 736 - IAD - NR 1 SMOKE DETECTOR WILL NOT TEST. REMVOED AND REPLACED NR 1 SMOKE DETECTOR BULB. SYSTEM OPERATES NORMAL. (M) - [SDR 20010112SG064](https://openairdocs.org/sdr/20010112SG064), Nov 23, 2000: FIRE DETECTOR. MALFUNCTIONED. FLT 640 - GRR - LOWER CARGO COMPARTMENT FIRE DETECTOR HAS YELLOW MAINTENANCE LIGHT AND NO GREEN SYSTEM LIGHT. REMOVED AND REPLACED LOWER AFT CARGO FORWARD DETEC - [SDR 20000718AP003](https://openairdocs.org/sdr/20000718AP003), Apr 21, 2000: VALVE. BROKEN. FLT 649 - AIR RETURN TO OMA, ON CLIMB-OUT AT 1000 FEET AGL FLAPS 2 DEGREES WERE SELECTED AND A SPLIT FLAP CONDITION OCCURRED. SMOKE BEGAN TO FILL THE COCKPIT, A - [SDR 99ZZZM742](https://openairdocs.org/sdr/99ZZZM742), Aug 19, 1999: BULB. BURNED. FLT 701 - IND- NR 1 SMOKE DETECTOR WON'T SELF TEST. RELAMPED TEST BULBS. (M) - [SDR 96ZZZM1326](https://openairdocs.org/sdr/96ZZZM1326), Aug 22, 1996: DOOR. UNSECURED. UNABLE TO PRESSURIZE AIRCRAFT. AIRCRAFT MADE AN ATB INTO DAYTON. RESEATED E/E COMPARTMENT DOOR. ## 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 20000420020109I](https://openairdocs.org/incident/20000420020109I), Apr 20, 2000: Boeing 72721 (N357QS), Omaha, NE, Minor damage. (-23)On April 20, 2000, approximately 1738 CDT, Boeing 727-21, N357QS, departed Omaha epply airfield, Omaha, Nebraska, under ryan international flight 694. On… - [Incident 19950922033529I](https://openairdocs.org/incident/19950922033529I), Sep 22, 1995: Boeing 72721 (N357QS), Dayton, OH, Minor damage. After parking found NR1 slat failed retract. Found wing tip damaged. Wing tip hit runway landing. - [Incident 19840606029249I](https://openairdocs.org/incident/19840606029249I), Jun 6, 1984: Boeing 72721 (N357QS), Kansas City, MO. Smoke in cockpit. Turned off the radar. Smoke cleared. Replacing radar r/t unit. ## Other aircraft with N357QS - [Registered now](https://openairdocs.org/aircraft/N357QS): Cessna 680, S/N 680-0155, built 2007 --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.