# N208AU: Boeing 737-222, registration cancelled 2000-07-20 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: July 20, 2000 - Exported to: Peru - Status when cancelled: Triennial form not returned - Airframe: [Boeing 737-222](https://openairdocs.org/model/boeing-737-222) (registry code 1384473) - Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (OpenAirDocs) - Serial number: 19547 - Type of aircraft: Fixed wing multi engine - Certificate issued: May 14, 1997 - Last registry action: May 16, 2000 - Mode S code: A1AFCE - Owner when cancelled: [First Security Bank Na Owner Trustee](https://openairdocs.org/faa-owner/FIRST%20SECURITY%20BANK%20NA%20OWNER%20TRUSTEE) - Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City) - Owner type: Corporation - Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N208AU - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=208AU - Page: https://openairdocs.org/deregistered/N208AU-2000-07-20 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 737-222: https://openairdocs.org/model/boeing-737-222.md ## Service difficulty reports (98, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR P2EA99348](https://openairdocs.org/sdr/P2EA99348), Dec 3, 1999: SKIN. DELAMINATED. SJO - LEFT WING OUTBOARD FLIPPER FLAPPER DELAMINATED. DEFECT SIZE, LENGTH 9 INCH, WIDTH 7.25 INCH. REPAIRED FLIPPER FLAPPER PER COOPESA EO COO-CMP-3-57-711-99, - [SDR P2EA99344](https://openairdocs.org/sdr/P2EA99344), Dec 3, 1999: FRAME. CRACKED. SJO - C-CHECK, FRAME CRACKED AT BS 967, BETWEEN STRINGER 20/21LT. DEFECT SIZE, LENGTH 3.5 INCH, WIDTH .16 INCH, DEPTH .63 INCH. REPAIRED FUSELAGE SECTION AT BS - [SDR P2EA99337](https://openairdocs.org/sdr/P2EA99337), Dec 1, 1999: SEAT TRACK. CORRODED. SJO - C-CHECK, SEAT TRACK CORRODED FROM BS 360 TO BS 380, LBL 35 INCHES. DEFECT SIZE, LENGTH 8 INCHES, WIDTH 2.25 INCHES, DEPTH .200 INCHES. REPAIRED SEAT TRACK - [SDR P2EA99356](https://openairdocs.org/sdr/P2EA99356), Nov 30, 1999: SKIN. DISBONDED. SJO - DURING C-CHECK, RIGHT AILERON INBOARD TRAILING EDGE DISBONDED AT REAR SPAR AREA. REPAIRED RIGHT AILERON PER SRM 51-40-6, PAR 5. (M) - [SDR P2EA99347](https://openairdocs.org/sdr/P2EA99347), Nov 30, 1999: FRAME. CRACKED. SJO - FORWARD CARGO DOOR FRAME CRACKED AT AFT FRAME, DEFECT SIZE, LENGTH .750 INCH. REPAIRED FORWARD CARGO DOOR BETWEEN BEAM NR 1 AND BEAM NR 3 PER SRM 51-40-3 - [SDR P2EA99346](https://openairdocs.org/sdr/P2EA99346), Nov 30, 1999: RIB. CRACKED. SJO - SLAT TRACK RIB CRACKED AT RIGHT WING FRONT SPAR SS356. DEFECT SIZE, LENGTH 1.5 INCH, WIDTH .32 INCH. REPLACED RIB AT SS 356 OUTBOARD TRACK PER SRM 51-30-2 - [SDR P2EA99338](https://openairdocs.org/sdr/P2EA99338), Nov 30, 1999: FLOORBEAM. CORRODED. SJO - C-CHECK, FLOORBEAM UPPER CHORD CORRODED AT BS 344, WL 208, BETWEEN LBL 32 AND BL 0. DEFECT SIZE, LENGTH 15 INCHES, WIDTH 1.5 INCH, DEPTH .050 INCH. REPAIR - [SDR P2EA99334](https://openairdocs.org/sdr/P2EA99334), Nov 30, 1999: INTERCOSTAL. CRACKED. SJO - FORWARD SERVICE DOOR INTERCOSTAL CRACKED AT BEAM 3. ANGLE REPLACED PER SRM 51-10-1 PAGE 5, 51-30-2 PAGE 8. (M) - [SDR P2EA99341](https://openairdocs.org/sdr/P2EA99341), Nov 29, 1999: SKIN. CRACKED. SJO - C-CHECK, FUSELAGE SKIN CRACK FROM BS 764 TO BS 767 BETWEEN STRINGER 18 AND 19 LEFT. DEFECT SIZE, LENGTH 3 INCH, WIDTH .032 INCH, DEPTH .028 INCH. REPAIRED - [SDR P2EA99339](https://openairdocs.org/sdr/P2EA99339), Nov 29, 1999: SKIN. SCRATCHED. SJO - C-CHECK, E/E DOOR WITH DEEP SCRATCHES AND MISSING MATERIAL. DEFECT SIZE, LENGTH 1.125 INCH, WIDTH .250 INCH, DEPTH .040 INCH. REPLACED DOOR SKIN PER SRM 5 - [SDR P2EA99309](https://openairdocs.org/sdr/P2EA99309), Oct 31, 1999: DETENT ARM. OUT OF ADJUST. MDW - FLT 277 - FLAPS 1 THROUGH 25 SELECTED, NR 6 LEADING EDGE SLAT EXTENDS CROOKED. FLAPS 30 THROUGH 40 SELECTED, NR 6 LEADING EDGE SLAT GOES TO FULL EXTEND. A - [SDR P2EA99216](https://openairdocs.org/sdr/P2EA99216), Jun 29, 1999: MECHANISM. OUT OF ADJUST. MDW - FLT 586 - NR 6 LEADING EDGE SLAT WOULD NOT EXTEND IN FLIGHT UNTIL FLAPS 30 POSITION WAS SELECTED. ADJUSTED TENSION ON NR 6 SLAT DETENT ARMS PER MM 27-81-0 - [SDR P2EA99199](https://openairdocs.org/sdr/P2EA99199), Jun 1, 1999: CONNECTOR. LOOSE. DEN - FLT 305 - EMERGENCY DECLARED (APU PREVIOUSLY DEFERRED) LANDING UNEVENTFUL AT SCHEDULED DESTINATION. LEFT ENGINE DRIVEN GENERATOR DROPPED OFF LINE IN FLIGH - [SDR P2EA99127](https://openairdocs.org/sdr/P2EA99127), Mar 13, 1999: KEEL BEAM. CORRODED. SJO - DURING Q-CHECK, A SECTION OF THE KEEL BEAM AT BS 630, RBL 5 WAS FOUND WITH CORROSION. THE AREA WAS REPAIRED AS PER COOPESA EO C00-3-53-176-99 AND BOEING F - [SDR P2EA99091](https://openairdocs.org/sdr/P2EA99091), Mar 1, 1999: BOLT. WORN. SJO - DURING Q-CHECK, THE NR 2 ENGINE, AFT MOUNT ATTACH BOLT, WAS FOUND WITH WEAR. NR 2 ENGINE AFT MOUNT ATTACH BOLT REPLACED IAW MM 71-21-11. (M) - [SDR P2EA99083](https://openairdocs.org/sdr/P2EA99083), Feb 26, 1999: SKIN. DAMAGED. SJO - DURING Q-CHECK, A SKIN REPAIR AT BS 500A, STRINGER 26R, WAS REMOVED FOR INVESTIGATION. AREA WAS CLEANED, INSPECTED AND REPAIRED AS PER SRM 53-30-3, FIGURE - [SDR P2EA99101](https://openairdocs.org/sdr/P2EA99101), Feb 25, 1999: PANEL. DELAMINATED. SJO - DURING Q-CHECK, THE RIGHT WING FIXED TRAILING EDGE PANEL, P/N 65-70947-24 WAS FOUND DELAMINATED. THE PANEL WAS REPAIRED IW EO NR COO-CMP-3-57-159-99. (M) - [SDR P2EA99100](https://openairdocs.org/sdr/P2EA99100), Feb 25, 1999: SKIN. DELAMINATED. SJO - DURING Q-CHECK, THE LEFT WING NR 2 TRAILING EDGE SLAT WAS FOUND WITH DELAMINATION. THE SLAT WAS REPAIRED IAW EO NR COO-CMP-3-57-149-99. (M) - [SDR P2EA99111](https://openairdocs.org/sdr/P2EA99111), Feb 24, 1999: SKIN. DELAMINATED. SJO - DURIGN Q-CHECK RIGHT AILERON WAS FOUND WITH DELAMINATION. AILERON WAS REPAIRED AS PER COOPESA NR COO-CMP-3-57-151-99. (M) - [SDR P2EA99097](https://openairdocs.org/sdr/P2EA99097), Feb 24, 1999: SKIN. DELAMINATED. SJO - DURING Q-CHECK, FLIGHT SPOILER NR 3 WAS FOUND WITH DELAMINATION. FLIGHT SPOILER REPAIRED AS PER COOPESA EO NR COO-CMP-3-57-150-00. (M) - [SDR P2EA99092](https://openairdocs.org/sdr/P2EA99092), Feb 24, 1999: BOLTS. WORN. SJO - DURING Q-CHECK, NR 2 ENGINE, FORWARD MOUNT THRUST LINKS ATTACH BOLTS FOUND WITH WEAR. REPLACED ATTACH BOLTS AS PER MM 71-20-11. (M) - [SDR P2EA99089](https://openairdocs.org/sdr/P2EA99089), Feb 24, 1999: BOLT. WORN. SJO - DURING Q-CHECK, ENGINE NR 1 FORWARD MOUNT THRUST LINK ATTACH BOLTS FOUND WITH WEAR. BOLTS REPLACED AS PER MM 71-20-11. (M) - [SDR P2EA99118](https://openairdocs.org/sdr/P2EA99118), Feb 23, 1999: MECHANISM. CORRODED. SJO - DURING Q-CHECK, THE R2 DOOR HANDLE MECHANISM HOUSING WAS FOUND WITH CORROSION AT THE LOWER TORQUE TUBE POSITION. REWORKED BEARING BORE AND MOUNTING HOLES - [SDR P2EA99117](https://openairdocs.org/sdr/P2EA99117), Feb 23, 1999: BEARING. CORRODED. SJO - DURING Q-CHECK, THE R1 DOOR WAS FOUND WITH CORROSION ON THE UPPER TORQUE TUBE BEARING POSITION. THE BEARING BORE AND MOUNTING HOLES WERE REWORKED AS PER O - [SDR P2EA99106](https://openairdocs.org/sdr/P2EA99106), Feb 23, 1999: SKIN. DELAMINATED. SJO - DURING Q-CHECK, DELAMINATION WAS FOUND ON THE LEFT AILERON. THE AILERON WAS REPAIRED PER COOPESA EO COO-CMP-3-57-127-99. (M) - [SDR P2EA99084](https://openairdocs.org/sdr/P2EA99084), Feb 23, 1999: BULKHEAD CHORD. CRACKED. SJO - DURING Q-CHECK, A CRACK WAS FOUND ON THE BS 178 PRESSURE BULKHEAD, FORWARD SIDE, LOWER HORIZONTAL CHORD. CRACK WAS REPAIRED IAW SRM 51-40-4 FIGURE 1. (M) - [SDR P2EA99126](https://openairdocs.org/sdr/P2EA99126), Feb 22, 1999: SUPPORT. WORN. SJO - DURING Q-CHECK, THE NR 1 ENGINE THRUST REVERSER, RIGHT ACTUATOR SUPPORT WAS WORN TO LIMITS. THE ACTUATOR SUPPORT WAS REPLACED IAW SRM 51-10-1. (M) - [SDR P2EA99107](https://openairdocs.org/sdr/P2EA99107), Feb 22, 1999: SKIN. CRACKED. SJO - DURING Q-CHECK, LFEC DETECTED A CRACK IN A FASTENER HOLE AT BS 492.4, BETWEEN STRINGERS 23 AND 24 RIGHT. THE AREA WAS REPAIRED AS PER COOPESA EO NR COO-2- - [SDR P2EA99125](https://openairdocs.org/sdr/P2EA99125), Feb 21, 1999: FIREWALL. WORN. SJO - DURING Q-CHECK, THE NR 2 ENGINE PYLON FORWARD FIREWALL WAS FOUND WORN. THE FIREWALL PANEL WAS REPAIRED AS PER COOPESA EO NR 3-54-189-99 AND BOEING FAX COO - [SDR P2EA99124](https://openairdocs.org/sdr/P2EA99124), Feb 21, 1999: INTERCOSTAL. CORRODED. SJO - DURING Q-CHECK, A STIFFENER AND INTERCOSTAL IN THE E/E COMPARTMENT BETWEEN BS 294.5 AND BS 312 AT STRINGER WERE FOUND WITH CORROSION. THE INTERCOSTAL AND - [SDR P2EA99099](https://openairdocs.org/sdr/P2EA99099), Feb 21, 1999: BULKHEAD WEB. CRACKED. SJO - DURING Q-CHECK, A CRACK WAS FOUND ON THE WEB OF THE PRESSURE BULKHEAD AT BS 294.5 BETWEEN STRINGER 27 AND 28 RT IN THE E/E COMPARTMENT. WEB SECTION WAS RE - [SDR P2EA99085](https://openairdocs.org/sdr/P2EA99085), Feb 21, 1999: RIB. CRACKED. SJO - DURING Q-CHECK, A RIB WAS FOUND CRACKED IN THE RIGHT WING INTERNAL AREA AT WS 505 UPPER FLANGE. THE CRACK WAS REPAIRED IAW SRM 57-10-7 FIG 1. (M) - [SDR P2EA99123](https://openairdocs.org/sdr/P2EA99123), Feb 20, 1999: FRAME. CRACKED. SJO - DURING Q-CHECK, THE BS 685 RIGHT FRAME FITTING WAS FOUND CRACKED. THE CRACK WAS REPAIRED AS PER BOEING FAX NR COO-SJO-99-0388RR AND COOPESA EO NR COO-3-53 - [SDR P2EA99119](https://openairdocs.org/sdr/P2EA99119), Feb 20, 1999: SKIN. CRACKED. SJO - DURING Q-CHECK, THE L1 DOOR CUT OUT LOWER AFT CORNER OUTER SKIN WAS FOUND CRACKED. THE SKIN WAS REPAIRED FROM BS 322 TO 355 IAW SB 53-1083 REV 3, PART IV - [SDR P2EA99098](https://openairdocs.org/sdr/P2EA99098), Feb 20, 1999: FLOORBEAM. CRACKED. SJO - DURING Q-CHECK, THE UPPER FLANGE OF THE FLOORBEAM AT BS 668.75, LBL 25 WAS FOUND CRACKED. REPAIRED FLOORBEAM AS PER COOPESA EO NR COO-3-53-154-99 AND BOEI - [SDR P2EA99122](https://openairdocs.org/sdr/P2EA99122), Feb 19, 1999: SKIN. CORRODED. SJO - DURING Q-CHECK, THE RIGHT WING OUTBOARD MID-FLAP SKIN AT WS 497 WAS BULGED. REPAIRED SKIN AS PER BOEING FAX COO-SJO-99-0330RR. (M) - [SDR P2EA99116](https://openairdocs.org/sdr/P2EA99116), Feb 19, 1999: MECHANISM. CORRODED. SJO - DURING Q-CHECK, THE L2 DOOR HANDLE MECHANISM HOUSING HAD CORROSION AT LOWER TORQUE TUBE BEARING HOLE. THE HOLE AND BUSHING WERE REWORKED IAW OHM 52-16-03. - [SDR P2EA99115](https://openairdocs.org/sdr/P2EA99115), Feb 19, 1999: SKIN. CRACKED. SJO - DURING Q-CHECK, A CRACK WAS FOUND AT THE LEFT WING, INBOARD MID FLAP LE SKIN AT INBOARD TRACK CUTOUT. THE CRACK WAS REPAIRED IAW BOEING FAX COO-SJO-99-027 - [SDR P2EA99114](https://openairdocs.org/sdr/P2EA99114), Feb 19, 1999: SKIN. CRACKED. SJO - DURING Q-CHECK, A CRACK WAS FOUND AT THE LEFT WING, OUTBOARD MIDFLAP LE SKIN AT OUTBOARD TRACK CUTOUT. THE CRACK WAS REPAIRED IAW BOEING FAX NR COO-SJO-99 - [SDR P2EA99105](https://openairdocs.org/sdr/P2EA99105), Feb 19, 1999: SKIN. WORN. SJO - DURING Q-CHECK, THE SKIN ON THE LEADING EDGE OF THE RIGHT WING OUTBOARD FOREFLAP WAS FOUND WITH WEAR. THE SKIN WAS REPAIRED FROM WSL 498 TO 505 AS PER SRM - [SDR P2EA99104](https://openairdocs.org/sdr/P2EA99104), Feb 19, 1999: RIB. CRACKED. SJO - DURING Q-CHECK, LEFT WING OUTBOARD MID FLAP INTERNAL LE RIB AT WBL 298 WAS FOUND CRACKED. RIB REPLACED AS PER SRM 51-10-1 PAGE 5. (M) - [SDR P2EA99103](https://openairdocs.org/sdr/P2EA99103), Feb 19, 1999: RIB. CRACKED. SJO - DURING Q-CHECK, THE LEFT INBOARD MID FLAP STRUCTURE, FOREFLAP CENTER TRACK SUPPORT FITTING RIB (INBOARD) WAS CRACKED AT TWO PLACES. RIB REPLACED AS PER SR - [SDR P2EA99093](https://openairdocs.org/sdr/P2EA99093), Feb 19, 1999: STRINGER. CORRODED. SJO - DURING Q-CHECK, A REPAIR LOCATED AT BS 767, STRINGER 9L WAS REMOVED FOR INVESTIGATION. AREA WAS CLEANED, INSPECTED AND REPAIRED AS PER SRM 53-30-3 FIG 6. - [SDR P2EA99080](https://openairdocs.org/sdr/P2EA99080), Feb 19, 1999: SKIN. DAMAGED. SJO - DURING Q-CHECK, AN EXISTING SKIN REPAIR LOCATED AT BS 727A, STRINGER 8R, WAS REMOVED FOR INVESTIGATION. AREA WAS CLEANED, INSPECTED AND A PERMANENT REPAIR - [SDR P2EA99895](https://openairdocs.org/sdr/P2EA99895), Feb 18, 1999: CARGO TRACK. CORRODED. SJO - DURING Q-CHECK, THE FORWARD CARGO COMPARTMENT CARGO TRACK AT BS 468, RBL 14, WAS FOUND WITH CORROSION. THE TRACK WAS REPAIRED AS PER SRM 53-10-5 FIG 5. (M - [SDR P2EA99121](https://openairdocs.org/sdr/P2EA99121), Feb 18, 1999: SPLICE. CRACKED. SJO - DURING Q-CHECK, THE STRINGER SPLICE AT BS 359, STRINGER 14L WAS FOUND CRACKED. THE STRINGER SPLICE WAS REPLACED AS PER SRM 51-10-1 PAGE 5. (M) - [SDR P2EA99112](https://openairdocs.org/sdr/P2EA99112), Feb 18, 1999: STRINGER. CORRODED. SJO - DURING Q-CHECK, TO VERIFY SRM COMPLIANCE, A REPAIR AT BS 1016 STRINGER 18L WAS REMOVED FOR INVESTIGATION. THE AREA WAS CLEANED, INSPECTED, AND REPAIRED AS - [SDR P2EA99110](https://openairdocs.org/sdr/P2EA99110), Feb 18, 1999: WEB. CRACKED. SJO - DURING Q-CHECK, A CRACK WAS FOUND ON THE NLG WHEEL WELL UPPER WEB AT BS 278, RBL 10. THE UPPER WEB WAS REPAIRED IAW COOPESA EO NR COO-SJO-99-0267. (M) - [SDR P2EA99109](https://openairdocs.org/sdr/P2EA99109), Feb 18, 1999: SKIN. CRACKED. SJO - DURING Q-CHECK, A CRACK WAS FOUND ON THE RIGHT WING INBOARD MIDFLAP, LE SKIN AT WBL 87.75. CRACK REPAIRED IAW BOEING FAX COO-SJO-99-0280. (M) - [SDR P2EA99102](https://openairdocs.org/sdr/P2EA99102), Feb 18, 1999: RIB. CRACKED. SJO - DURING Q-CHECK, RIGHT WING, UPPER CHANNEL OF THE LE RIB AT WS 213 WAS FOUND CRACKED. THE CHANNEL WAS REPLACED IAW SRM 51-10-1 PAGE 5. (M) All 98: https://openairdocs.org/deregistered/N208AU-2000-07-20/reports.md ## NTSB investigations (1) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB CHI99LA145](https://openairdocs.org/ntsb/CHI99LA145), May 6, 1999: Boeing 737-222 (N208AU), Chicago, IL, no damage. Probable cause: the flight attendants did not follow the cockpit crews instructions to be seated because of expected turbulence. A factor associated with the accident was the turbulence encountered. ## FAA accident and incident reports (5) 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. - [Accident 19990505041889A](https://openairdocs.org/incident/19990505041889A), May 5, 1999: Boeing 737222 (N208AU), Chicago, IL. (.4)Flight 432 encountered about 30 seconds of moderate turbulence while deviating around weather cells during a descent from 17,000 feet mean sea level (MSL).… - [Incident 19980525036029I](https://openairdocs.org/incident/19980525036029I), May 25, 1998: Boeing 737200 (N208AU), Chicago, IL, Substantial damage. (-5) As take off roll was initiated, a shimmy developed and the captain aborted the takeoff and exited the runway. Aircraft sustained major damage to upper and… - [Incident 19970407008549I](https://openairdocs.org/incident/19970407008549I), Apr 7, 1997: Boeing 737222 (N208AU), Kansas City, MO. Narrative: on 04/07/97, vanguard flight 123 was inbound to mci, when the crew declared an emergency due to fumes in the cockpit. Maintenance inspected the left… - [Incident 19900905046089I](https://openairdocs.org/incident/19900905046089I), Sep 5, 1990: Boeing 737222 (N208AU), Syracuse, NY. High oil temperature on NR2 engine. Shut engine down. Heat valve was stuck open. - [Incident 19900511024329I](https://openairdocs.org/incident/19900511024329I), May 11, 1990: Boeing 737222 (N208AU), Lexington, KY. Passenger complained of breathing problem. Administered oxygen and diverted for emergency landing. ## Other aircraft with N208AU - [Cancelled 2015-10-14](https://openairdocs.org/deregistered/N208AU-2015-10-14): Liberty Aerospace XL-2, S/N 0114, built 2008. Owner: [Averett University Of Danville Va](https://openairdocs.org/faa-owner/AVERETT%20UNIVERSITY%20OF%20DANVILLE%20VA), [Danville, VA](https://openairdocs.org/faa-place/VA/Danville) --- 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.