# N574US: 1987 Boeing 737-301, registration cancelled 2015-02-18

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: February 18, 2015
- Exported to: China
- Status when cancelled: Valid registration
- Airframe: [Boeing 737-301](https://openairdocs.org/model/boeing-737-301) (registry code 138447R)
- Engine: [CFM International CFM56 series](https://openairdocs.org/engine/cfm-international-cfm56-series) (registry code 13802)
- Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (OpenAirDocs)
- Serial number: 23739
- Year built: 1987
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 8, 1989
- Certificate issued: April 17, 2014
- Last registry action: April 17, 2014
- Mode S code: A75F18
- Owner when cancelled: [Bci 2005-3 LLC](https://openairdocs.org/faa-owner/BCI%202005-3%20LLC)
- Location: [Chicago, IL](https://openairdocs.org/faa-place/IL/Chicago)
- Owner type: Corporation
- Owner's area on the map: 41.8947° N, 87.6151° W: Placed by OpenAirDocs at the center of ZIP code 60611, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N574US
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=574US
- Page: https://openairdocs.org/deregistered/N574US-2015-02-18

From the FAA registry file of November 7, 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 737-301: https://openairdocs.org/model/boeing-737-301.md

## Service difficulty reports (166, newest 50)

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

- [SDR USAA2012120300004](https://openairdocs.org/sdr/USAA2012120300004), Dec 2, 2012: SKIN. CRACKED. C6 CHECK - FUSELAGE SKIN CRACKED AT BS 910, S23R. REPAIRED FUSELAGE SKIN BETWEEN BS 904 TO BS 949 FROM S19R TO S24R IAW EA 502588 REPAIR INSTRUCTIONS FROM STEPS
- [SDR USAA2012083100010](https://openairdocs.org/sdr/USAA2012083100010), Aug 30, 2012: SKIN. CRACKED. B CHECK - CRACK FUSELAGE SKIN AT BS 727E +7 INCHES, S24L. REPAIRED FUSELAGE SKIN AT BS 727E +7 INCHES, S24L IAW B737-300 SRM 53-00-01-2R-31.
- [SDR USAA2012083100009](https://openairdocs.org/sdr/USAA2012083100009), Aug 30, 2012: SKIN. CRACKED. B CHECK - CRACK FUSELAGE SKIN AT BS 727E +13 INCHES, S23L. REPAIRED FUSELAGE SKIN AT BS 727E +13 INCHES, S23L IAW B737-30 SRM 53-00-01, REPAIR 31.
- [SDR USAA2012083100008](https://openairdocs.org/sdr/USAA2012083100008), Aug 30, 2012: SKIN. CRACKED. B CHECK - CRACK FUSELAGE SKIN AT BS 727 +7 INCHES, S23L. REPAIRED FUSELAGE SKIN AT BS 727 +7 INCHES, S23L IAW B737-300 SRM 53-00-01-2R-31.
- [SDR USAA2012083100012](https://openairdocs.org/sdr/USAA2012083100012), Aug 29, 2012: SKIN. CRACKED. B-CHECK - CRACK IN FUSELAGE SKIN AT BS 727E+6 INCHES, S23L. REPAIRED FUSELAGE SKIN AT BS 727E+6 INCHES, S23L IAW SRM 53-00-01-2R REPAIR 31.
- [SDR USAA2012083100011](https://openairdocs.org/sdr/USAA2012083100011), Aug 29, 2012: SKIN. CRACKED. B-CHECK - CRACK IN FUSELAGE SKIN AT BS 727E+8 INCHES, S23R. REPAIRED FUSELAGE SKIN AT BS 727E+8 INCHES, S23R IAW SRM 53-00-01-2R REPAIR 31.
- [SDR USAA2012080700008](https://openairdocs.org/sdr/USAA2012080700008), Aug 7, 2012: WIRE. BROKEN. MAINTENANCE REPORTED THE EMERGENCY FLOOR LIGHT AT SEAT ROW 16ABC INOPERATIVE. MAINTENANCE REPAIRED WIRING IAW SWPM 20-10-13. CHECKS OK IAW AMM 33-51-12-700-802C
- [SDR USAA2012080600017](https://openairdocs.org/sdr/USAA2012080600017), Aug 4, 2012: FLASHLIGHT. INOPERATIVE. CREW REPORTED THE AFT FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT FLIGHT ATTENDANT FLASHLIGHT ASSEMBLY. OPS CHECKS GOOD.
- [SDR USAA2012061100016](https://openairdocs.org/sdr/USAA2012061100016), Jun 10, 2012: INDICATOR. FAULTY. ON APPROACH, CREW REPORTED THE FLAP INDICATOR SHOWED A 1/2 NEEDLE SPLIT BETWEEN 10 & 15. CREW ACCOMPLISHED GO-AROUND. FLAPS WERE NOT MOVEABLE UNTIL AFTER LANDIN
- [SDR USAA2012060800001](https://openairdocs.org/sdr/USAA2012060800001), Jun 8, 2012: SPAR. CRACKED. MLG FITTING REPLACEMENT VISIT - CRACK IN LEFT WING REAR SPAR UPPER SPAR CHORD AT RSS226. REPAIRED LEFT UPPER SPAR CHORD IAW EA 202579.
- [SDR USAA2012052100014](https://openairdocs.org/sdr/USAA2012052100014), May 15, 2012: SPAR. CRACKED. MLG FITTING REPLACEMENT VISIT - CRACK IN UPPER SPAR CHORD AT RSS222. REPAIRED RIGHT HAND UPPER SPAR CHORD IAW US AIRWAYS EA # 202560.
- [SDR USAA2012051700008](https://openairdocs.org/sdr/USAA2012051700008), May 14, 2012: SKIN. CRACKED. GEAR FITTINGS - CRACK IN SKIN LAP JOINT BETWEEN TWO RIVETS AT BS 747, S4L. REPAIRED SKIN LAP JOINT BETWEEN TWO RIVETS AT BS 747, S4L IAW B737-300 SRM 53-00-01-2
- [SDR USAA2012042300008](https://openairdocs.org/sdr/USAA2012042300008), Apr 22, 2012: SOCKET. FAULTY. MAINTENANCE REPORTED THE EMERGENCY EXTERIOR EGRESS LIGHT INOPERATIVE AT AFT RIGHT GALLEY SERVICE DOOR. MAINTENANCE REMOVED AND REPLACED THE REFLECTOR AND SOCKET
- [SDR USAA2012021000019](https://openairdocs.org/sdr/USAA2012021000019), Feb 9, 2012: HEATER. FAULTY. EN ROUTE FROM CLE TO CLT, AUTO MODE PRESSURIZATION SYSTEM FAILED AT FL180. IN DESCENT, SYSTEM CONVERTED TO STANDBY MODE. STANDBY MODE OPERATED NORMALLY. AT ALTI
- [SDR USAA2012020700017](https://openairdocs.org/sdr/USAA2012020700017), Feb 6, 2012: OUTFLOW VALVE. FAULTY. DURING LEVEL CRUISE AT FL250, CREW REPORTED THE CABIN ALTITUDE WARNING SOUNDED AND NOTICED CABIN PRESSURE APPROACHING 10K FEET. CREW COULD NOT CONTROL CABIN ALT
- [SDR USAA2011120500002](https://openairdocs.org/sdr/USAA2011120500002), Dec 3, 2011: DOOR. CRACKED. C5 CHECK - SEVERAL CRACKS RANGING FROM .125 INCHES TO .750 INCHES ON AFT CARGO DOOR AT BS 795 APPROX 22.5 INCHES FROM TOP INSIDE OF DOOR SKIN EDGE & 2.5 INCHES 
- [SDR USAA2011112200005](https://openairdocs.org/sdr/USAA2011112200005), Nov 21, 2011: FUSE. BLOWN. MAINTENANCE REPORTED THE LEFT FORWARD OVERWING ESCAPE LIGHT INOPERATIVE. MAINTENANCE FOUND A BLOWN FUSE AT POWER SUPPLY M1135. REPLACED FUSE AS REQUIRED. LIGHT 
- [SDR USAA2011110100003](https://openairdocs.org/sdr/USAA2011110100003), Oct 31, 2011: DOWNLOCK SENSOR. FAULTY. DURING CRUISE, EN ROUTE FROM BDL TO CLT, CREW REPORTED THE NOSE LANDING GEAR RED INDICATOR LIGHT ILLUMINATED. ON GEAR EXTENSION, ALL GEAR INDICATIONS WERE NORMA
- [SDR USAA2011092000005](https://openairdocs.org/sdr/USAA2011092000005), Sep 19, 2011: INDICATOR. FAULTY. ON APPROACH TO CLT, CREW REPORTED SELECTING FLAPS TO 25 AND A SPLIT FLAP INDICATION OCCURRED AS INNER NEEDLE WAS AT 15 DEGREES. CREW INITIATED A GO-AROUND AND P
- [SDR USAA2011080800005](https://openairdocs.org/sdr/USAA2011080800005), Aug 7, 2011: CONTROLLER. FAULTY. EN ROUTE FROM CLE TO CLT, DURING CRUISE, CREW REPORTED THE CABIN ALTITUDE WARNING HORN SOUNDED AND NOTED THAT THE CABIN ALTITUDE WAS CLIMBING. CAPTAIN ADVISED A
- [SDR USAA2011071500008](https://openairdocs.org/sdr/USAA2011071500008), Jul 14, 2011: LIGHT. DETACHED. CREW REPORTED THE EMERGENCY EXIT LIGHT AT SEAT 8C BECAME DETACHED. MAINTENANCE REPAIRED AS REQUIRED. AIRCRAFT OK FOR SERVICE.
- [SDR USAA2011071400004](https://openairdocs.org/sdr/USAA2011071400004), Jul 14, 2011: FLAP. SPLIT. ON APPROACH TO MIA, CREW REPORTED A SPLIT FLAP INDICATION AND ACCOMPLISHED A GO-AROUND. SELECTING FLAPS 25, RIGHT NEEDLE WAS AT 15 AND LEFT NEEDLE WAS AT 25. SE
- [SDR USAA2011062900006](https://openairdocs.org/sdr/USAA2011062900006), Jun 28, 2011: OUTFLOW VALVE. MALFUNCTIONED. FLT 1942 - CLT-BUF - CABIN PRESSURE - EN ROUTE FROM CLT TO BUF, AT FL370, CREW RECEIVED CABIN ALTITUDE WARNING HORN. CABIN INDICATED MORE THAN 9,000 FEET AND DI
- [SDR USAA2011061500001](https://openairdocs.org/sdr/USAA2011061500001), Jun 10, 2011: SKIN. CRACKED. CLT - RON - FUSELAGE SKIN CRACKED AT BS 870, S23R. REPAIRED FUSELAGE SKIN AT BS 870, S23R IAW B737 SRM 53-00-01 REPAIR 31.
- [SDR USAA20110525SB082](https://openairdocs.org/sdr/USAA20110525SB082), May 24, 2011: INDICATOR. FAULTY. CLE - DURING LANDING APPROACH, WHILE SELECTING FLAPS FROM 15 TO 25, THE RIGHT FLAP INDICATION STAYED AT 15 AND FLAPS STOPPED MOVING WITH A SPLIT OF ABOUT 4 DEGR
- [SDR USAA2011051691858](https://openairdocs.org/sdr/USAA2011051691858), May 13, 2011: BULKHEAD. CRACKED. PIT - FPBH INSPECTION - CRACK ON FORWARD PRESSURE BULKHEAD AT BS 178, WL 218, RBL 12.7. REPAIRED FORWARD PRESSURE BULKHEAD AT BS 178, WL 218, RBL 12.7 IAW B737 
- [SDR USAA2011051291838](https://openairdocs.org/sdr/USAA2011051291838), May 10, 2011: BULKHEAD. CRACKED. PIT - FORWARD PRESSURE BULKHEAD - 2 CRACKS IN VERTICAL WEB 3 INCHES AFT OF BS 178, WL 178, LBL 5.7. REPLACED VERTICAL WEB AT BS 178, WL 178, LBL 5.7 IAW B757 SR
- [SDR USAA2011051291839](https://openairdocs.org/sdr/USAA2011051291839), May 8, 2011: FRAME. CRACKED. PIT - FORWARD PRESSURE BULKHEAD - CRACK IN FUSELAGE FRAME AT BS 616, LBL 62. REPAIRED FUSELAGE FRAME AT BS 616, LBL62 IAW TYPICAL REPAIR TR737-5362-10-0023 & JO
- [SDR USAA2011051291843](https://openairdocs.org/sdr/USAA2011051291843), May 8, 2011: FITTING. CRACKED. PIT - FORWARD PRESSURE BULKHEAD - CRACK ON CLIP AT BS 639, RBL 45.5. REPLACED CLIP AT BS 639, RBL 45.5 IAW BOEING DRAWING J65-46540.
- [SDR USAA2011051291842](https://openairdocs.org/sdr/USAA2011051291842), May 8, 2011: FITTING. CRACKED. PIT - FORWARD PRESSURE BULKHEAD - NR 03-0553-8-0614-3 - CRACK ON CLIP AT BS639, LBL45.5. REPLACED CLIP AT BS639, LBL45.5 IAW BOEING DRAWING J65-46540.
- [SDR USAA2011051291841](https://openairdocs.org/sdr/USAA2011051291841), May 8, 2011: FLOORBEAM. CRACKED. FORWARD PRESSURE BULKHEAD - CRACK IN FLOORBEAM UPPER TEE AT BS 665, LBL 0.7.
- [SDR USAA20110224SB034](https://openairdocs.org/sdr/USAA20110224SB034), Feb 20, 2011: ENGINE. LEAKING. RDU - ON CLIMBOUT FROM CLT, EN ROUTE TO RDU, ALL THREE FLIGHT ATTENDANTS REPORTED A STRONG DIRTY FOOT, MUSTY, MOLDY SMELL FOR ABOUT FIVE MINUTES. SEVERAL PASSEN
- [SDR USAA20110104SB003](https://openairdocs.org/sdr/USAA20110104SB003), Jan 2, 2011: ACM. FAULTY. CLT - AT IDLE POWER, DESCENDING BELOW 10,000 FEET, CREW REPORTED A STRONG SMELL OF DIRTY SOCKS. MIGHT BE COMING FROM THE PACKS. AFTER ADDING POWER, SMELL DISSIP
- [SDR USAA20110104SB001](https://openairdocs.org/sdr/USAA20110104SB001), Jan 1, 2011: FILTER. DIRTY. CLT - DESCENDING THROUGH 9,000 FEET, CREW REPORTED AN UNUSUAL ODOR THAT CAME ON STRONGLY. SMELLED LIKE BURNT OIL. ODOR DISAPPEARED/DECREASED ON TAXI-IN. MAINTEN
- [SDR USAA20101223SB204](https://openairdocs.org/sdr/USAA20101223SB204), Dec 22, 2010: RECEIVER. FAILED. GSO - ON APPROACH TO CLT, AFDS SHOWS NO FLARE ARM AT 1,000 FEET. AUTO PILOT DISCONNECTS SHORTLY THEREAFTER. THE WEATHER IN CLT WAS BELOW MINIMUMS FOR THESE COND
- [SDR USAA2010110892542](https://openairdocs.org/sdr/USAA2010110892542), Nov 4, 2010: FLAP. DELAMINATED. CLT - C4 - MAJOR REPAIR - DELAMINATION ON BOTTOM SIDE OF RIGHT OUTBOARD FOREFLAP. REPLACED RIGHT OUTBOARD FOREFLAP IAW B737 AMM 27-51-37.
- [SDR USAA2010110892541](https://openairdocs.org/sdr/USAA2010110892541), Nov 4, 2010: SKIN. CRACKED. CLT - C4 - MAJOR REPAIR - CRACK ON NR 2 SPOILER LOWER SURFACE WHERE ACTUATOR ATTACHES. REPLACED NR 2 SPOILER IAW B737 AMM 27-61-11.
- [SDR USAA2010091692016](https://openairdocs.org/sdr/USAA2010091692016), Sep 16, 2010: SKIN. CRACKED. CLT - RON - MAJOR REPAIR - CRACK IN FUSELAGE SKIN AT BS747 + 6 INCHES, S21R. REPAIRED FUSELAGE SKIN AT BS 747 + 6 INCHES, S21R IAW EA 102194.
- [SDR USAA20100830SB138](https://openairdocs.org/sdr/USAA20100830SB138), Aug 29, 2010: POWER SUPPLY. INOPERATIVE. MCO - MAINTENANCE REPORTED THE SEAT LEVEL EMERGENCY LIGHTS AT SEAT ROWS 5 THROUGH 11 AND THE LEFT OVERWING EXIT SIGN INOPERATIVE. MAINTENANCE REMOVED AND REPLAC
- [SDR USAA2010082391745](https://openairdocs.org/sdr/USAA2010082391745), Aug 22, 2010: DOOR FRAME. CRACKED. PIT - CDFI - MAJOR REPAIR - FORWARD CARGO DOOR, FORWARD FRAME HAS .75 INCH CRACK AT BS 440, S24R, WL 160, RBL 35. REPAIRED FORWARD CARGO DOOR, FORWARD FRAME AT 
- [SDR USAA2010082391744](https://openairdocs.org/sdr/USAA2010082391744), Aug 22, 2010: DOOR FRAME. CRACKED. PIT - CDFI - MAJOR REPAIR - FORWARD CARGO DOOR AFT FRAME HAS .5 INCH CRACK AT BS 492.4, S24R, WL 160, RBL 30. REPAIRED FORWARD CARGO DOOR AFT FRAME AT BS 492.4,
- [SDR USAA2010081891701](https://openairdocs.org/sdr/USAA2010081891701), Aug 18, 2010: INTERCOSTAL. CRACKED. PIT - CDFI - MAJOR REPAIR - CRACK ON INTERCOSTAL AT BS 294.5, S12L. REPLACED INTERCOSTAL AT BS 294.5, S12L IAW B737 SRM 53-10-15.
- [SDR USAA2010081891707](https://openairdocs.org/sdr/USAA2010081891707), Aug 15, 2010: FITTING. CRACKED. PIT - CDFI - MAJOR REPAIR - CRACK ON CLIP AT BS 360, S11L. REPLACED CLIP AT BS 360, S11L IAW B737 SRM 53-10-15 & 51-40-02.
- [SDR USAA2010081891706](https://openairdocs.org/sdr/USAA2010081891706), Aug 15, 2010: FITTING. CRACKED. PIT - CDFI - MAJOR REPAIR - CRACK ON CLIP AT BS 360, S10L. REPLACED CLIP AT BS 360, S10L IAW B737 SRM 53-10-15 & 51-40-02.
- [SDR USAA2010081891704](https://openairdocs.org/sdr/USAA2010081891704), Aug 15, 2010: FITTING. CRACKED. PIT - CDFI - MAJOR REPAIR - CRACK ON CLIP AT BS 360, S9L. REPLACED CLIP AT BS 360, S9L IAW B737 SRM 53-10-15 & 51-40-02.
- [SDR USAA20100608SB096](https://openairdocs.org/sdr/USAA20100608SB096), Jun 6, 2010: BALLAST. FAULTY. CLT - FLIGHT ATTENDANT REPORTED AN ELECTRICAL ODOR IN THE CABIN. MAINTENANCE FOUND THE ODOR COMING FROM THE FORWARD ENTRY DOOR LIGHT BALLAST. REMOVED AND REPLAC
- [SDR USAA20100423SB057](https://openairdocs.org/sdr/USAA20100423SB057), Apr 22, 2010: CHARGER. INOPERATIVE. CLT - MAINTENANCE REPORTED THE EMERGENCY LIGHTING INOPERATIVE INSIDE THE CABIN AT SEAT ROWS 16 THROUGH 19 AND AFT RIGHT SERVICE DOOR. MAINTENANCE REMOVED AND RE
- [SDR USAA3009122193383](https://openairdocs.org/sdr/USAA3009122193383), Dec 20, 2009: FLAP SYSTEM. FALSE INDICATION. EMERGENCY LANDING- FLAP ASYMMETRY OCCURRED BETWEEN 10 AND 15 DEGREES WHEN FLAP 15 WAS SELECTED AN EMERGENCY WAS DECLARED AND EMERGENCY EQUIPMENT WAS DISPATCHED.
- [SDR USAA2009121693353](https://openairdocs.org/sdr/USAA2009121693353), Dec 11, 2009: STRINGER. CORRODED. CLT - C3 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON STRINGER AT BS 987, S27R. REPAIRED STRINGER AT BS 987, S27R IAW EA 101584.
- [SDR USAA2009121193327](https://openairdocs.org/sdr/USAA2009121193327), Dec 9, 2009: SKIN. CRACKED. CLT - C3 - MAJOR REPAIR - CRACK ON FUSELAGE SKIN AT AFT SERVICE DOOR UPPER HINGE CUTOUT. REPAIRED FUSELAGE SKIN AT AFT SERVICE DOOR UPPER HINGE CUTOUT IAW B737 

All 166: https://openairdocs.org/deregistered/N574US-2015-02-18/reports.md

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