# N432US: 1990 Boeing 737-4B7, registration cancelled 2015-09-04

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: September 4, 2015
- Status when cancelled: First renewal notice
- Airframe: [Boeing 737-4B7](https://openairdocs.org/model/boeing-737-4b7) (registry code 138449C)
- Engine: [CFM International CFM56 series](https://openairdocs.org/engine/cfm-international-cfm56-series) (registry code 13802)
- Serial number: 24554
- Year built: 1990
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: February 14, 1990
- Certificate issued: November 25, 2009
- Last registry action: January 4, 2013
- Mode S code: A52C5F
- Owner when cancelled: [Awas 24554 Trust](https://openairdocs.org/faa-owner/AWAS%2024554%20TRUST)
- Location: [New York, NY](https://openairdocs.org/faa-place/NY/New%20York)
- Owner type: Corporation
- Owner's area on the map: 40.7586° N, 73.9679° W: Placed by OpenAirDocs at the center of ZIP code 10022, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N432US
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=432US
- Page: https://openairdocs.org/deregistered/N432US-2015-09-04

From the FAA registry file of October 31, 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 737-4B7: https://openairdocs.org/model/boeing-737-4b7.md

## Service difficulty reports (266, newest 50)

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

- [SDR USAA2013030800008](https://openairdocs.org/sdr/USAA2013030800008), Mar 7, 2013: BATTERY PACK. DISCHARGED. MAINTENANCE REPORTED THE EMERGENCY LIGHTS FOR LEFT OVERWING AFT EXIT, CEILING EXIT RIGHT, AND EMERGENCY LIGHT IN BULLNOSE BETWEEN SEATS 9L AND 10L INOP. MAINTEN
- [SDR USAA2013011600006](https://openairdocs.org/sdr/USAA2013011600006), Jan 15, 2013: LENS. BROKEN. CREW REPORTED THE EMERGENCY EXIT LIGHT AT ROW 11C BROKEN. MAINTENANCE REPLACED EMERGENCY LIGHT LENS AT ROW 11C PER MPPM 54-01-10. AIRCRAFT OK FOR SERVICE.
- [SDR USAA2012122800015](https://openairdocs.org/sdr/USAA2012122800015), Dec 27, 2012: LENS. BROKEN. CREW REPORTED THE FLOOR EXIT LIGHTING LENSES AT ROWS 11 AND 12 WERE BROKEN OR MISSING. MAINTENANCE REPLACED LENSES FOR EMERGENCY LIGHTING AT ROWS 11 AND 12ABC P
- [SDR USAA2012121700019](https://openairdocs.org/sdr/USAA2012121700019), Dec 14, 2012: PANEL. DELAMINATED. PILOT REPORT - AREA OF DELAMINATION IN UPPER SURFACE OF NR 9 SPOILER PANEL APPROX 20.5 INCHES FROM INBOARD END & 3.5 INCHES UP FROM TRAILING EDGE. REPLACED NR 9
- [SDR USAA2012121700018](https://openairdocs.org/sdr/USAA2012121700018), Dec 14, 2012: PANEL. DELAMINATED. PILOT REPORT - AREA OF DELAMINATION ON UPPER SURFACE OF NR 9 SPOILER PANEL APPROX 8 INCHES FROM INBOARD END & 4 INCHES UP FROM TRAILING EDGE. REPLACED NR 9 SPOI
- [SDR USAA2012101000005](https://openairdocs.org/sdr/USAA2012101000005), Oct 9, 2012: SIGN. UNSECURE. CREW REPORTED THE OVERWING "EXIT" SIGN OVER ROW 12ABC LOOSE. MAINTENANCE SECURED "EXIT' SIGN AS REQUIRED. AIRCRAFT OK FOR SERVICE..
- [SDR USAA2012092400006](https://openairdocs.org/sdr/USAA2012092400006), Sep 23, 2012: SLIDE. LOW PRESSURE. Q6 CHECK - R1 DOOR ESCAPE SLIDE BOTTLE IS NOT IN THE GREEN BAND (BELOW BAND). REPLACED BOTTLE WITH NEW R-1 DOOR ESCAPE SLIDE ASSEMBLY IAW TASK CARD 03T10025002 
- [SDR USAA2012092400002](https://openairdocs.org/sdr/USAA2012092400002), Sep 23, 2012: LENS. MISSING. Q6 CHECK - OVERHEAD EXIT LIGHT AT OVERHEAD BIN 4 IS MISSING LENS. REPLACED OVERHEAD EXIT LIGHT AT BIN 4 IAW B737 AMM 33-51-11-002-004 AND 33-51-11-402-007.
- [SDR USAA2012092000002](https://openairdocs.org/sdr/USAA2012092000002), Sep 17, 2012: WIRE. BROKEN. Q6 CHECK - BROKEN WIRE ON BACK OF EXIT SIGN ABOVE R1 DOOR . REPAIRED WIRE ON BACK OF EXIT SIGN ABOVE R1 DOOR IAW BOEING COMMON SPWM 20-61-19 AND OPS CHECKED GOO
- [SDR USAA2012091900005](https://openairdocs.org/sdr/USAA2012091900005), Sep 17, 2012: SIGN. MISSING. Q6 CHECK - EMERGENCY EXIT SIGN MISSING ON LEFT SIDE WALL PANEL 10. INSTALLED EMERGENCY EXIT SIGN ON LEFT SIDEWALL PANEL 10 IAW B737 AMM 33-51-11-402-007.
- [SDR USAA2012092500020](https://openairdocs.org/sdr/USAA2012092500020), Sep 15, 2012: WEB. CRACKED. Q6 CHECK - CRACK ON RIGHT UPPER WEB IN APU COMPARTMENT AT BS 1122, RBL 12. REPAIRED RIGHT UPPER WEB AT BS 1122, RBL12 IAW B737 SRM 51-70-13-0G, FIG 1 DETAIL I.
- [SDR USAA2012092500018](https://openairdocs.org/sdr/USAA2012092500018), Sep 14, 2012: STIFFENER. CORRODED. Q6 CHECK - CORROSION ON VERTICAL STIFFENER IN APU COMPARTMENT AT BS 1122 BETWEEN S16R TO S18R. REPLACED VERTICAL STIFFENER AT BS 1122 BETWEEN S16R TO S18R IAW B
- [SDR USAA2012091800010](https://openairdocs.org/sdr/USAA2012091800010), Sep 14, 2012: SKIN. CRACKED. Q6 CHECK - CRACK IN FUSELAGE SKIN AT BS 944, S24R. REPAIRED FUSELAGE SKIN AT BS 944, S24R IAW B737 SRM 53-00-01-2R-31, FIG 201, DETAIL XIX.
- [SDR USAA2012100100009](https://openairdocs.org/sdr/USAA2012100100009), Sep 12, 2012: MOUNT FITTING. CORRODED. Q6 CHECK - EXFOLIATION CORROSION ON MOUNT FITTING AT BS 941, WL 208, LBL 51. REPLACED MOUNT FITTING AT BS 941, WL 208, LBL 51 IAW B737-400 AMM 20-50-11-912-002.
- [SDR USAA2012092800012](https://openairdocs.org/sdr/USAA2012092800012), Sep 6, 2012: STRINGER. CORRODED. C6 CHECK - LEVEL 2 EXFOLIATION CORROSION ON STRINGER AT BS 1112, S16R. REPLACED STRINGER AT BS 1112, S16R IAW B737 SRM 51-40-02-0G PAR 4 & 7, FIG 6 & 12.
- [SDR USAA2012091800006](https://openairdocs.org/sdr/USAA2012091800006), Sep 6, 2012: ANGLE. BROKEN. Q6 CHECK - BROKEN TAB ON ANGLE AT BS 807, S25R. REPLACED ANGLE AT BS 807, S25R IAW B737 SRM 51-40-02-0G FIG 8 & 12.
- [SDR USAA2012091800012](https://openairdocs.org/sdr/USAA2012091800012), Sep 2, 2012: STRAP. CRACKED. Q6 CHECK - CRACKED STRAP ON FUSELAGE FRAME AT BS 794, S27R. REPLACED STRAP ON FUSELAGE FRAME AT BS 794, S27R IAW B737 SRM 51-40-02-0G FIG 3 & 12.
- [SDR USAA2012092800011](https://openairdocs.org/sdr/USAA2012092800011), Aug 30, 2012: INTERCOSTAL. CORRODED. C6 CHECK - CORROSION ON INTERCOSTAL BETWEEN BS 927 TO BS 947, S26R. REPLACED INTERCOSTAL BETWEEN BS 927 TO BS 947, S26R IAW B737 SRM 51-40-02-0G, PAR 4E, FIG 8.
- [SDR USAA2012091800009](https://openairdocs.org/sdr/USAA2012091800009), Aug 28, 2012: SKIN. DELAMINATED. Q6 CHECK - DELAMINATION ON UPPER SURFACE OF LEFT OUTBOARD AFT FLAP BETWEEN WBL 230.68 TO WBL 235.68 APPROX 1 INCH FROM INBOARD EDGE & 5 INCHES FROM TRAILING EDG
- [SDR USAA2012091100008](https://openairdocs.org/sdr/USAA2012091100008), Aug 23, 2012: INTERCOSTAL. CRACKED. Q6 CHECK - CRACK ON INTERCOSTAL (BAFFLE) AT BS 500E, S26L. REPLACED INTERCOSTAL (BAFFLE) AT BS 500E, S26L IAW B737-400 SRM 51-40-02-0G FIGURES 8 AND 13.
- [SDR USAA2012091100012](https://openairdocs.org/sdr/USAA2012091100012), Aug 16, 2012: DOUBLER. CRACKED. Q6 CHECK - CRACK ON DOUBLER UNDER L1 DOOR STOP CUTOUT AT BS 303.9, BETWEEN S16L TO S17L. REPLACED DOUBLER UNDER L1 DOOR STOP CUTOUT AT BS 303.9, BETWEEN S16L TO
- [SDR USAA2012100100010](https://openairdocs.org/sdr/USAA2012100100010), Aug 15, 2012: SKIN. CRACKED. Q6 CHECK - CRACK ON FUSELAGE SKIN AT BS 727F MINUS 2 INCHES, S25L. REPAIRED FUSELAGE SKIN AT BS 727F MINUS 2 INCHES, S25L IAW EA 130947.
- [SDR USAA2012091100007](https://openairdocs.org/sdr/USAA2012091100007), Aug 15, 2012: WEB. CRACKED. Q6 CHECK - CRACK ON WEB BETWEEN BS 344 TO BS 340, RBL 60. REPAIRED WEB BETWEEN BS 344 TO BS 340, RBL 60 IAW B737-400 SRM 51-40-02-0G FIGURE 12.
- [SDR USAA2012091100006](https://openairdocs.org/sdr/USAA2012091100006), Aug 15, 2012: SKIN. CRACKED. Q6 CHECK - CRACK ON FUSELAGE SKIN AT BS 749, S22L. REPAIRED FUSELAGE SKIN AT BS 749, S22L IAW B737-400 SRM 53-00-01-2R-31, FIGURE 201, DETAIL VII.
- [SDR USAA2012091100003](https://openairdocs.org/sdr/USAA2012091100003), Aug 15, 2012: ATTACH ANGLE. CRACKED. Q6 CHECK - CRACKED ON ATTACH ANGLE AT BS 294.5, RBL 57. REPLACED ATTACH ANGLE AT BS 294.5, RBL 57 IAW B737-400 SRM 51-40-02-0G, PARAGRAPH 7D, FIGURE 12, DETAIL 
- [SDR USAA2012092500021](https://openairdocs.org/sdr/USAA2012092500021), Aug 14, 2012: DOOR FRAME. CORRODED. Q6 CHECK - LEVEL 2 EXFOLIATION CORROSION ON AFT CARGO DOOR CUTOUT SURROUND FRAME AT BS 794, RBL 9. REPLACED AFT CARGO DOOR CUTOUT SURROUND FRAME AT BS 794, RBL 
- [SDR USAA2012091100018](https://openairdocs.org/sdr/USAA2012091100018), Aug 14, 2012: SHEAR TIE. CORRODED. Q6 CHECK - EXFOLIATION CORROSION ON SHEAR TIE AT BS 745, S27R. REPAIRED SHEAR TIE AT BS 745, S27R IAW B737-400 SRM 53-00-07-2R-5 FIGURE 201, 51-40-02-0G FIGURE 
- [SDR USAA2012091100005](https://openairdocs.org/sdr/USAA2012091100005), Aug 14, 2012: STRINGER SPLICE. CORRODED. Q6 CHECK - EXFOLIATION CORROSION ON STRINGER SPLICE AT BS 912, S22R. REPLACED STRINGER SPLICE AT BS 912, S22R IAW B737-400 SRM 51-40-02-0G FIGURES 8 AND 12.
- [SDR USAA2012090700024](https://openairdocs.org/sdr/USAA2012090700024), Aug 14, 2012: STRINGER CLIP. CRACKED. Q6 CHECK - CRACK ON STRINGER CLIP AT BS 847, S4L. REPLACED STRINGER CLIP AT BS 847, S4L IAW B737 SRM 51-40-02-0G PAR 4 FIG 8 & PAR 7D FIG 12.
- [SDR USAA2012090700022](https://openairdocs.org/sdr/USAA2012090700022), Aug 14, 2012: SEAT TRACK. CRACKED. Q6 CHECK - CRACK ON SEAT TRACK AT BS 403, LBL 25. REPLACED SEAT TRACK AT BS 403, LBL 25 IAW B737 SRM 53-00-52-2R-1, FIG 201.
- [SDR USAA2012090700021](https://openairdocs.org/sdr/USAA2012090700021), Aug 14, 2012: SKIN. CRACKED. Q6 CHECK - CRACK ON FUSELAGE SKIN AT BS 893, S25R. REPAIRED FUSELAGE SKIN AT BS 893, S25R IAW B737 SRM 53-00-01-2R-31 PROC 5 FIG 201 DET 19.
- [SDR USAA2012090700020](https://openairdocs.org/sdr/USAA2012090700020), Aug 14, 2012: SKIN. CRACKED. Q6 CHECK - CRACK ON FUSELAGE SKIN AT BS 747.3, S24R. REPAIRED FUSELAGE SKIN AT BS 747.3, S24R IAW B737 SRM 53-00-52-2R-2, FIG 201.
- [SDR USAA2012090700015](https://openairdocs.org/sdr/USAA2012090700015), Aug 13, 2012: SHEAR WEB. CORRODED. Q6 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOOR SHEAR WEB AT BS 1030, WL 208 BETWEEN BL 0 TO LBL 2. REPLACED FLOOR SHEAR WEB AT BS 1030, WL 208 BETWEEN BL 0 T
- [SDR USAA2012091100002](https://openairdocs.org/sdr/USAA2012091100002), Aug 12, 2012: FITTING. CRACKED. Q6 CHECK - CRACKED CLIP IN FORWARD CARGO COMPARTMENT AT BS 500B, S26R. REPLACED CLIP AT BS 500B, S26R IAW B737-400 SRM 51-40-02-0G FIGURES 8 AND 12.
- [SDR USAA2012082200014](https://openairdocs.org/sdr/USAA2012082200014), Aug 12, 2012: STRINGER CLIP. CRACKED. Q6 CHECK - CRACK IN STRINGER CLIP AT BS 887, S4L. REPLACED STRINGER CLIP AT BS 887, S4L IAW B737 SRM 51-40-02-0G, PAR 4 & 7D, FIG 8 & 12.
- [SDR USAA2012092500017](https://openairdocs.org/sdr/USAA2012092500017), Aug 11, 2012: FITTING. CRACKED. Q6 CHECK - CRACK ON LEFT INBOARD GROUND SPOILER OUTBOARD FITTING AT WBL 174.50. REPLACED LEFT INBOARD GROUND SPOILER IAW B737 AMM 27-62-12-004-001 & 27-62-12-40
- [SDR USAA2012091800008](https://openairdocs.org/sdr/USAA2012091800008), Aug 11, 2012: SILL. CORRODED. Q6 CHECK - LEVEL 2 FILIFORM CORROSION ON SILL WEB AT BS 500+10 INCHES ABOVE, S19R. REPAIRED SILL WEB AT BS 500+10 INCHES ABOVE, S19R IAW B737 SRM 51-40-02-0G FI
- [SDR USAA2012100200006](https://openairdocs.org/sdr/USAA2012100200006), Aug 10, 2012: SKIN. DELAMINATED. Q6 CHECK - DELAMINATION ON LOWER TRAILING EDGE SURFACE OF RIGHT OUTBOARD FOREFLAP AT WS 141. REPLACED RIGHT OUTBOARD FOREFLAP AT WS 141 IAW JOB CARD 03C40727020
- [SDR USAA2012100100003](https://openairdocs.org/sdr/USAA2012100100003), Aug 10, 2012: ATTACH ANGLE. CORRODED. Q6 CHECK - FILIFORM CORROSION ON ATTACH ANGLE AT BS 500, BETWEEN S23L TO S24L. REPLACED ATTACH ANGLE AT BS 500, BETWEEN S23L TO S24L IAW B737-400 SRM 51-70-11-0
- [SDR USAA2012092800010](https://openairdocs.org/sdr/USAA2012092800010), Aug 10, 2012: FLOORBEAM. CRACKED. C6 CHECK - CRACK ON SEAT TRACK LONGITUDINAL FLOORBEAM UPPER CHORD AT BS 639, LBL 45. REPAIRED SEAT TRACK LONGITUDINAL FLOORBEAM UPPER CHORD AT BS 639, LBL 45 IA
- [SDR USAA2012092500015](https://openairdocs.org/sdr/USAA2012092500015), Aug 10, 2012: DOUBLER. CRACKED. Q6 CHECK - CRACK IN BONDED DOUBLER FOR OPENING OF ACCESS PANEL 5823R ON NR 2 PYLON AT NAC STA 236.75, WL 127.13. REPAIRED NR 2 PYLON AT NAC STA 236.75, WL 127.1
- [SDR USAA2012091800005](https://openairdocs.org/sdr/USAA2012091800005), Aug 10, 2012: DOUBLER. CRACKED. Q6 CHECK - CRACK ON NR 1 PYLON BONDED DOUBLER AT OPENING TO ACCESS PANEL 5723L AT NAC STA 236.75, WL 127.13. REPAIRED NR 1 PYLON BONDED DOUBLER AT OPENING TO AC
- [SDR USAA2012091100017](https://openairdocs.org/sdr/USAA2012091100017), Aug 10, 2012: SEAT TRACK. CRACKED. Q6 CHECK - CRACK ON SEAT TRACK AT BS 727B PLUS 2 INCHES, WL 208, RBL 24. REPLACED SEAT TRACK AT BS 727B PLUS 2 INCHES, WL 208, RBL 24 IAW B737-400 SRM 53-00-52-
- [SDR USAA2012091100015](https://openairdocs.org/sdr/USAA2012091100015), Aug 10, 2012: FLAP. DELAMINATED. Q6 CHECK - DELAMINATION ON TRAILING EDGE OF RIGHT OUTBOARD FLAP AT WBL 204.4. REPLACED RIGHT OUTBOARD FLAP IAW JOB CARD 03C40727020.
- [SDR USAA2012090700023](https://openairdocs.org/sdr/USAA2012090700023), Aug 10, 2012: SEAT TRACK. CRACKED. Q6 CHECK - CRACK ON SEAT TRACK BETWEEN BS 727B TO BS 727E+10 INCHES, RBL 45. REPLACED SEAT TRACK BETWEEN BS 727B TO BS 727E+10 INCHES, RBL 45 IAW B737 SRM 53-00
- [SDR USAA2012100100015](https://openairdocs.org/sdr/USAA2012100100015), Aug 9, 2012: INTERCOSTAL. CRACKED. Q6 CHECK - CRACK ON INTERCOSTAL AT BS 500B, S26R. REPLACED INTERCOSTAL AT BS 500B, S26R IAW B737-400 SRM 51-40-02-0G, FIGURES 8, 12.
- [SDR USAA2012091100014](https://openairdocs.org/sdr/USAA2012091100014), Aug 9, 2012: INTERCOSTAL. CRACKED. Q6 CHECK - CRACK ON INTERCOSTAL (BAFFLE) AT BS 500B, S26R. REPLACED INTERCOSTAL (BAFFLE) AT BS 500B, S26R IAW B737-400 SRM 51-40-02-0G FIGURES 8 AND 12.
- [SDR USAA2012100100004](https://openairdocs.org/sdr/USAA2012100100004), Aug 8, 2012: STRUCTURE. CORRODED. Q6 CHECK - EXFOLIATION CORROSION ON CHORD BETWEEN BS 251.6 TO BS 364, S17R. REPLACED CHORD BETWEEN BS 251.6 TO BS 364, S17R IAW B737-400 SRM 51-40-02-0G, FIGURE
- [SDR USAA2012092500023](https://openairdocs.org/sdr/USAA2012092500023), Aug 8, 2012: DOOR FRAME. CRACKED. Q6 CHECK - CRACK ON AFT CARGO DOOR CUTOUT SURROUND FRAME UPPER OUTBOARD DOOR STOP AT BS 847 BETWEEN S21R TO S22R. REPLACED AFT CARGO DOOR CUTOUT SURROUND FRAME 
- [SDR USAA2012091100013](https://openairdocs.org/sdr/USAA2012091100013), Aug 8, 2012: ATTACH ANGLE. CRACKED. Q6 CHECK - CRACK ON FORWARD CARGO ATTACH ANGLE AT BS 500E, S26L, BL 0. REPLACED ATTACH ANGLE AT BS 500E, S26L, BL 0 IAW B737-400 SRM 51-40-02-0G FIGURE 8.

All 266: https://openairdocs.org/deregistered/N432US-2015-09-04/reports.md

## FAA accident and incident reports (1)

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 19960629024849I](https://openairdocs.org/incident/19960629024849I), Jun 29, 1996: Boeing 7374B7 (N432US), Orlando, FL, Minor damage. Narrative: aircraft struck a deer at beginning of takeoff roll at approximately 30 knots. Returned to gate. Maintenance found nose gear landing light bracket…

## Other aircraft with N432US

- [Registered now](https://openairdocs.org/aircraft/N432US): DJI T40, S/N 1581F574B237600100F8

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