# N417US: Boeing 737-401, registration cancelled 2015-09-22

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: September 22, 2015
- Exported to: Venezuela
- Status when cancelled: Registration pending
- Airframe: [Boeing 737-401](https://openairdocs.org/model/boeing-737-401) (registry code 138449B)
- 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: 23984
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: February 15, 1989
- Last registry action: August 21, 2015
- Mode S code: A4EFF4
- Location: [Miami, FL](https://openairdocs.org/faa-place/FL/Miami)
- Owner type: Individual
- Owner's area on the map: 25.8050° N, 80.3151° W: Placed by OpenAirDocs at the center of ZIP code 33122, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N417US
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=417US
- Page: https://openairdocs.org/deregistered/N417US-2015-09-22

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 737-401: https://openairdocs.org/model/boeing-737-401.md

## Service difficulty reports (224, newest 50)

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

- [SDR USAA2012010600025](https://openairdocs.org/sdr/USAA2012010600025), Jan 5, 2012: SEAL. OUT OF POSITION. CREW REPORTED THE RIGHT EMERGENCY EXIT WINDOW IS PARTALLY BLOCKED BY INSULATION. MAINTENANCE REPOSITIONED DUST SEAL AND RE-INSTALLED RIGHT EMERGENCY EXIT DOOR P
- [SDR USAA2012010400015](https://openairdocs.org/sdr/USAA2012010400015), Jan 2, 2012: ENGINE. VIBRATION. ON TAKEOFF THROUGH CLIMBOUT, CREW NOTICED A STRANGE SOUND. OUT OF APPROXIMATELY 10,000 MCL, VIBRATION INDICATOR ON NR 1 ENGINE CLIMBED STEADILY THROUGH 4.0 TO 5
- [SDR USAA2011121200002](https://openairdocs.org/sdr/USAA2011121200002), Dec 11, 2011: LENS. MISSING. CREW REPORTED THE EMERGENCY EXIT LENS MISSING AT AIRCRAFT LEFT, ROWS 11-12. MAINTENANCE REPLACED LEFT OVERWING EXIT DOOR EMERGENCY LIGHT LENS COVER. CHECKS OK P
- [SDR USAA2011103100003](https://openairdocs.org/sdr/USAA2011103100003), Oct 30, 2011: LENS. UNSECURE. CREW REPORTED THE OVERWING EXIT SIGN, AIRCRAFT LEFT, IS MISSING. MAINTENANCE SECURED THE LEFT OVERWING EXIT LENS. OK FOR SERVICE.
- [SDR USAA2011102100013](https://openairdocs.org/sdr/USAA2011102100013), Oct 21, 2011: SIGN. DETACHED. CREW REPORTED THE EXIT SIGN AT OVERWING EXIT NEEDS RE-ATTACHED. MAINTENANCE RE-ATTACHED EXIT SIGN AT OVERWING EXIT AS REQUIRED.
- [SDR USAA2011101400017](https://openairdocs.org/sdr/USAA2011101400017), Oct 13, 2011: SEAT TRACK. LACK OF LUBE. CAPTAIN'S SEAT IS DIFFICULT TO ADJUST FORE AND AFT. MAINTENANCE LUBED THE SEAT TRACKS. OPS CHECKS GOOD.
- [SDR USAA2011101000029](https://openairdocs.org/sdr/USAA2011101000029), Oct 9, 2011: MECHANISM. LACK OF LUBE. CAPTAIN'S SEAT WILL NOT STAY IN POSITION, SLIDES DURING TAKEOFF AND LANDING. MAINTENANCE LUBRICATED THE LOCKING MECHANISM. OPS CHECK GOOD.
- [SDR USAA2011091500001](https://openairdocs.org/sdr/USAA2011091500001), Sep 14, 2011: SIGN. DETACHED. CREW REPORTED THE EMERGENCY EXIT SIGN AT ROW 11/12, LEFT SIDE, KEEPS FALLING DOWN. MAINTENANCE REPAIRED EMERGENCY EXIT SIGN AS NEEDED. OPS CHECKS GOOD.
- [SDR USAA2011082900021](https://openairdocs.org/sdr/USAA2011082900021), Aug 20, 2011: STRAP. CORRODED. Q3 CHECK - LEVEL 2 EXFOLIATION CORROSION ON STRAP AT BS 795, S27R. REPAIRED STRAP AT BS 795, S27R IAW EA 103233.
- [SDR USAA2011082900007](https://openairdocs.org/sdr/USAA2011082900007), Aug 20, 2011: FLOORBEAM. CORRODED. Q3 CHECK - LEVEL 2 EXFOLIATION CORROSION ON AFT CARGO FLOORBEAM AT BS 773, LBL 3. REPLACED AFT CARGO FLOORBEAM AT BS 773, LBL 3 IAW EA 103286.
- [SDR USAA2011082900006](https://openairdocs.org/sdr/USAA2011082900006), Aug 20, 2011: FLOORBEAM. CORRODED. Q3 CHECK - LEVEL 2 EXFOLIATION CORROSION ON AFT CARGO FLOORBEAM AT BS 773, LBL 8. REPAIRED AFT CARGO FLOORBEAM AT BS 773, LBL 8 IAW EA 103286.
- [SDR USAA2011082900005](https://openairdocs.org/sdr/USAA2011082900005), Aug 20, 2011: FLOORBEAM. CORRODED. Q3 CHECK - LEVEL 2 EXFOLIATION CORROSION ON AFT CARGO FLOORBEAM AT BS 773, RBL 3. REPAIRED AFT CARGO FLOORBEAM AT BS 773, RBL 3 IAW EA 103286.
- [SDR USAA2011082600019](https://openairdocs.org/sdr/USAA2011082600019), Aug 20, 2011: FRAME. CORRODED. Q3 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FUSELAGE FRAME AT BS 747, LBL 8. REPAIRED FUSELAGE FRAME AT BS 747, LBL 8 IAW B737 SRM 53-00-07, REPAIR 4.
- [SDR USAA2011082600018](https://openairdocs.org/sdr/USAA2011082600018), Aug 20, 2011: FRAME. CORRODED. Q3 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FUSELAGE FRAME AT BS 747 BETWEEN S26L TO S27L. REPAIRED FUSELAGE FRAME AT BS 747 BETWEEN S26L TO S27L IAW B737 SRM 5
- [SDR USAA2011082600024](https://openairdocs.org/sdr/USAA2011082600024), Aug 19, 2011: FAILSAFE. GOUGED. Q3 CHECK - 4 WEAR MARKS ON FAIL SAFE CHORDS ON FUSELAGE FRAME AT BS 727A BETWEEN S20L TO S24L. REPAIRED FAIL SAFE CHORDS ON FUSELAGE FRAME AT BS 727A BETWEEN S2
- [SDR USAA2011082600023](https://openairdocs.org/sdr/USAA2011082600023), Aug 18, 2011: FAILSAFE. GOUGED. Q3 CHECK - 4 WEAR MARKS ON FAIL SAFE CHORDS ON FUSELAGE FRAME AT BS 727B AT S20L, S21L, S23L & S24L. REPAIRED FAIL SAFE CHORDS ON FUSELAGE FRAME AT BS 727B AT S
- [SDR USAA2011082600022](https://openairdocs.org/sdr/USAA2011082600022), Aug 18, 2011: FRAME. CORRODED. Q3 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FUSELAGE FRAME LOWER LEG AT BS 767 BETWEEN LBL 2 TO LBL 12. REPAIRED FUSELAGE FRAME LOWER LEG AT BS 767 BETWEEN LBL 
- [SDR USAA2011082900012](https://openairdocs.org/sdr/USAA2011082900012), Aug 17, 2011: SKIN. DAMAGED. Q3 CHECK - MISSING PLYS LOCATED AT RUDDER STATION 7.0, 1.5" X 2.5"; MISSING PLYS AT RUDDER STA 133.0, 1.5" X 0.75". REPLACED RUDDER IAW JOB CARD 03C70827007.
- [SDR USAA2011082600025](https://openairdocs.org/sdr/USAA2011082600025), Aug 16, 2011: FRAME. CORRODED. Q3 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FUSELAGE STUB FRAME AT BS 807 BETWEEN LBL 4 TO LBL 10. REPAIRED FUSELAGE STUB FRAME AT BS 807 BETWEEN LBL 4 TO LBL 1
- [SDR USAA2011081900027](https://openairdocs.org/sdr/USAA2011081900027), Aug 13, 2011: FRAME. CRACKED. Q3 CHECK - CRACK ON FUSELAGE FRAME AT BS 500C BETWEEN S20R TO S21R. REPAIRED FUSELAGE FRAME AT BS 500C BETWEEN S20R TO S21R IAW B737 SRM 53-00-07, REPAIR 13.
- [SDR USAA2011081900021](https://openairdocs.org/sdr/USAA2011081900021), Aug 12, 2011: FRAME. CORRODED. Q3 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FUSELAGE FRAME AT BS 787, LBL 8. REPAIRED FUSELAGE FRAME AT BS 787, LBL 8 IAW B737 SRM 53-00-07, REPAIR 3.
- [SDR USAA2011082900022](https://openairdocs.org/sdr/USAA2011082900022), Aug 11, 2011: ANGLE. CORRODED. Q3 CHECK - LEVEL 2 EXFOLIATION CORROSION ON TRANSITION ANGLE BETWEEN BS 767 TO BS 790, RBL 20. REPLACED TRANSITION ANGLE BETWEEN BS 767 TO BS 790, RBL 20 IAW B7
- [SDR USAA2011082900020](https://openairdocs.org/sdr/USAA2011082900020), Aug 11, 2011: SKIN. DELAMINATED. Q3 CHECK - DELAMINATION ON LEFT ELEVATOR TAB LOWER SKIN SURFACE AT NR 2 HINGE CUTOUT. REPLACED LEFT ELEVATOR TAB IAW JOB CARD 03C71127007.
- [SDR USAA2011082900013](https://openairdocs.org/sdr/USAA2011082900013), Aug 11, 2011: SKIN. DELAMINATED. Q3 CHECK - DELAMINATION ON RIGHT ELEVATOR TAB LOWER SKIN AT 2 HINGE CUTOUT. REPLACED RIGHT ELEVATOR TAB IAW JOB CARD 03C71227004.
- [SDR USAA2011082900008](https://openairdocs.org/sdr/USAA2011082900008), Aug 11, 2011: ATTACH ANGLE. CRACKED. Q3 CHECK - CRACK ON FLOORBEAM VERTICAL ATTACH ANGLE AT BS 328, RBL 32. REPLACED FLOORBEAM VERTICAL ATTACH ANGLE AT BS 328, RBL 32 IAW EA 103286.
- [SDR USAA2011081900034](https://openairdocs.org/sdr/USAA2011081900034), Aug 11, 2011: DOUBLER. CRACKED. Q3 CHECK - CRACK ON FUSELAGE FRAME WEB DOUBLER AT BS 303.9, S16L. REPAIRED FUSELAGE FRAME WEB DOUBLER AT BS 303.9, S16L IAW BOEING DRAWING 65-17684.
- [SDR USAA2011082600020](https://openairdocs.org/sdr/USAA2011082600020), Aug 10, 2011: BELTFRAME. CRACKED. Q3 CHECK - CRACK ON FUSELAGE FRAME AT BS 500D BETWEEN S20R TO S21R. REPAIRED FUSELAGE FRAME AT BS 500D BETWEEN S20R TO S21R IAW B737 SRM 53-00-07 REPAIR 13.
- [SDR USAA2011082900030](https://openairdocs.org/sdr/USAA2011082900030), Aug 5, 2011: BULKHEAD. CANNING. Q3 CHECK - OIL CANNING WAS FOUND AFTER REMOVING PREVIOUS REPAIR ON AFT PRESSURE BULKHEAD AT BS 1016 BETWEEN S9R TO S11R. REPAIRED AFT PRESSURE BULKHEAD WEB IAW 
- [SDR USAA2011082900023](https://openairdocs.org/sdr/USAA2011082900023), Aug 4, 2011: WEB. CORRODED. Q3 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON WEB BETWEEN BS767 TO BS787, S25R. REPLACED WEB BETWEEN BS 767 TO BS 787, S25R IAW B737 SRM 51-10-02.
- [SDR USAA2011082900010](https://openairdocs.org/sdr/USAA2011082900010), Aug 4, 2011: KEELBEAM. CORRODED. Q3 CHECK - CORROSION ON AFT FUSELAGE RIGHT KEEL BEAM CHORD BETWEEN BS727C + 11 INCHES TO BS 816, S27R. REPLACED AFT FUSELAGE RIGHT KEEL BEAM BETWEEN BS 727C + 1
- [SDR USAA2011081900028](https://openairdocs.org/sdr/USAA2011081900028), Aug 3, 2011: FRAME. CRACKED. Q3 CHECK - CRACK ON FUSELAGE FRAME AT BS 500F BETWEEN S20R TO S21R. REPAIRED FUSELAGE FRAME AT BS 500C BETWEEN S20R TO S21R IAW B737 SRM 53-00-07, REPAIR 13.
- [SDR USAA2011081900022](https://openairdocs.org/sdr/USAA2011081900022), Aug 3, 2011: FRAME. CRACKED. Q3 CHECK - CRACK ON FUSELAGE FRAME AT BS 500G, S13L. REPAIRED FUSELAGE FRAME AT BS500G, S13L IAW EA 103214.
- [SDR USAA2011082900017](https://openairdocs.org/sdr/USAA2011082900017), Aug 2, 2011: ATTACH ANGLE. CRACKED. Q3 CHECK - CRACK ON AFT END OF ATTACH ANGLE BETWEEN BS 303.9 & BS 294.5, S10L. REPLACED ATTACH ANGLE BETWEEN BS 303.9 & BS 294.5, S10L IAW B737 SRM 51-40-03.
- [SDR USAA2011082900024](https://openairdocs.org/sdr/USAA2011082900024), Aug 1, 2011: WEB. CRACKED. Q3 CHECK - CRACK IN FORWARD GALLEY DOOR LOWER WEB. REPLACED FORWARD GALLEY DOOR LOWER WEB IAW B737 SRM 51-40-02.
- [SDR USAA2011082900029](https://openairdocs.org/sdr/USAA2011082900029), Jul 31, 2011: PAN. CORRODED. Q3 CHECK - LEVEL 2 EXFOLIATION CORROSION ON AFT GALLEY FLOOR PAN BETWEEN BS 1016 +10 INCHES TO BS 1016 +16 INCHES & BETWEEN LBL 2 TO RBL 2. REPAIRED AFT GALLEY 
- [SDR USAA2011081900029](https://openairdocs.org/sdr/USAA2011081900029), Jul 31, 2011: FRAME. CRACKED. Q3 CHECK - CRACK ON FUSELAGE FRAME AT BS 500F JUST BELOW S13R. REPAIRED FUSELAGE FRAME AT BS 500F JUST BELOW S13R IAW TYPICAL REPAIR 737-5310-10-0327.
- [SDR USAA2011082900018](https://openairdocs.org/sdr/USAA2011082900018), Jul 30, 2011: ATTACH ANGLE. CRACKED. Q3 CHECK - CRACK ON AFT END OF ATTACH ANGLE BETWEEN BS 303.9 & BS 294.5, S13L. REPLACED ATTACH ANGLE BETWEEN BS 303.9 & BS 294.5, S13L IAW B737 SRM 51-40-02.
- [SDR USAA2011081900030](https://openairdocs.org/sdr/USAA2011081900030), Jul 30, 2011: FRAME. CRACKED. Q3 CHECK - CRACK ON FUSELAGE FRAME AT BS 520, 1 INCH BELOW S13R. REPAIRED FUSELAGE FRAME AT BS 520, 1 INCH BELOW S13R IAW TYPICAL REPAIR 737-5310-10-0327, TABLE
- [SDR USAA2011081900025](https://openairdocs.org/sdr/USAA2011081900025), Jul 30, 2011: FRAME. CRACKED. Q3 CHECK - CRACK ON FUSELAGE FRAME AT BS 500C BETWEEN S20L TO S21L. REPAIRED FUSELAGE FRAME AT BS 500C BETWEEN S20L TO S21L IAW B737 SRM 53-00-07, REPAIR 13.
- [SDR USAA2011081900024](https://openairdocs.org/sdr/USAA2011081900024), Jul 30, 2011: FRAME. CRACKED. Q3 CHECK - CRACK ON FUSELAGE FRAME AT BS 500E BETWEEN S20L TO S21L. REPAIRED FUSELAGE FRAME AT BS 500E BETWEEN S20L TO S21L IAW B737 SRM 53-00-07, REP 13.
- [SDR USAA2011081900023](https://openairdocs.org/sdr/USAA2011081900023), Jul 30, 2011: FRAME. CRACKED. Q3 CHECK - CRACK ON FUSELAGE FRAME AT BS 500B BETWEEN S20R TO S21R. REPAIRED FUSELAGE FRAME AT BS 500B BETWEEN S20R TO S21R IAW B737 SRM 53-00-07, REP 13.
- [SDR USAA2011082200025](https://openairdocs.org/sdr/USAA2011082200025), Jul 29, 2011: FRAME. CRACKED. Q3 CHECK - CRACK ON FUSELAGE FRAME AT BS 500B BETWEEN S20L TO S21L. REPAIRED FUSELAGE FRAME IAW B737 SRM 53-00-07, REPAIR 13.
- [SDR USAA2011081900033](https://openairdocs.org/sdr/USAA2011081900033), Jul 29, 2011: ANGLE. CRACKED. Q3 CHECK - CRACK ON FUSELAGE FRAME REINFORCEMENT ANGLE AT BS 500B BETWEEN S20L TO S21L. REPAIRED FUSELAGE FRAME REINFORCEMENT ANGLE IAW B737 SRM 53-00-07, REPAI
- [SDR USAA2011081900031](https://openairdocs.org/sdr/USAA2011081900031), Jul 29, 2011: FRAME. CRACKED. Q3 CHECK - CRACK ON FUSELAGE FRAME AT BS 500E, S13R. REPAIRED FUSELAGE FRAME AT BS 500E, S13R IAW TYPICAL REPAIR 737-5310-10-0327.
- [SDR USAA2011082900025](https://openairdocs.org/sdr/USAA2011082900025), Jul 27, 2011: WEB. CRACKED. Q3 CHECK - CRACK IN INTERCOSTAL WEB AT BS 294.5, S12R. REPLACED INTERCOSTAL WEB AT BS 294.5, S12R IAW B737 SRM 51-40-02.
- [SDR USAA2011081900032](https://openairdocs.org/sdr/USAA2011081900032), Jul 27, 2011: SKIN. CRACKED. Q3 CHECK - CRACK ON RIGHT PYLON UPPER SKIN PANEL CUTOUT 5827R BETWEEN NAC STA210 TO NAC STA220. REPAIRED RIGHT PYLON UPPER SKIN PANEL CUTOUT 5827R IAW TYPICAL R
- [SDR USAA2011081900026](https://openairdocs.org/sdr/USAA2011081900026), Jul 27, 2011: FRAME. CRACKED. Q3 CHECK - CRACK ON FUSELAGE FRAME AT BS 480 BETWEEN S8R TO S9R. REPAIRED FUSELAGE FRAME AT BS 480 BETWEEN S8R TO S9R IAW EA 103207.
- [SDR USAA2011082900026](https://openairdocs.org/sdr/USAA2011082900026), Jul 25, 2011: ANGLE. CORRODED. Q3 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON Z-ANGLE BETWEEN B887 TO BS1016, S17L. REPLACED Z-ANGLE BETWEEN BS 887 TO BS 1016, S17L IAW B737 SRM 51-40-02, 51-4
- [SDR USAA2011081900035](https://openairdocs.org/sdr/USAA2011081900035), Jul 23, 2011: SKIN. CRACKED. Q3 CHECK - CRACKS ON FUSELAGE SKIN AT MAIN ENTRY DOOR UPPER HINGE CUTOUTS AT BS303.9 BETWEEN S10L TO S13L. REPAIRED FUSELAGE FUSELAGE SKIN AT MAIN ENTRY DOOR UP
- [SDR USAA2011082900027](https://openairdocs.org/sdr/USAA2011082900027), Jul 20, 2011: STRAP. CRACKED. Q3 CHECK - CRACK ON H-STRAP AT BS 303.9, S13L. REPLACED H-STRAP AT BS303.9, S13L IAW B737 SRM 53-10-15 & BOEING DRAWING 65-17684 FRAME NR 1.

All 224: https://openairdocs.org/deregistered/N417US-2015-09-22/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 20070122000619I](https://openairdocs.org/incident/20070122000619I), Jan 22, 2007: Boeing 737401 (N417US), Miami, FL, Minor damage. (-23) On January 22, 2007 us airways flight #1898, while on pushback at Miami International Airport struck a catering truck. The aircraft was struck at…
- [Incident 19981219043379I](https://openairdocs.org/incident/19981219043379I), Dec 19, 1998: Boeing 737400 (N417US), Albuquerque, NM. (-5) U s air F165 diverted to abq due to fuel imbalance on aircraft. Cross feed valve/actuator failed causing imbalance. Fuel was redistributed on ground at…
- [Incident 19940930037159I](https://openairdocs.org/incident/19940930037159I), Sep 30, 1994: Boeing 737401 (N417US), Kansas City, MO. Split trailing edge flap condition and lockup. Zero flap landing mci. Broke circuit breaker by crew seat back.

## Other aircraft with N417US

- [Registered now](https://openairdocs.org/aircraft/N417US): Bell 407, S/N 53580, built 2003

---
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.