# N165AW: 1986 Boeing 737-33A, registration cancelled 2002-05-20

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: May 20, 2002
- Exported to: Spain
- Status when cancelled: Valid registration
- Airframe: [Boeing 737-33A](https://openairdocs.org/model/boeing-737-33a) (registry code 1384673)
- Engine: [CFM International CFM56 series](https://openairdocs.org/engine/cfm-international-cfm56-series) (registry code 13802)
- Serial number: 23626
- Year built: 1986
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 3, 1986
- Certificate issued: January 24, 2001
- Last registry action: April 12, 2002
- Mode S code: A10456
- Owner when cancelled: [Awms I](https://openairdocs.org/faa-owner/AWMS%20I)
- 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/N165AW
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=165AW
- Page: https://openairdocs.org/deregistered/N165AW-2002-05-20

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 737-33A: https://openairdocs.org/model/boeing-737-33a.md

## Service difficulty reports (75, newest 50)

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

- [SDR M522001F00000](https://openairdocs.org/sdr/M522001F00000), Aug 26, 2001: PRESSURE PANEL. CRACKED. LEFT HAND W/W FUS STATION 664.0 PRESSURE WEB CRACKED IN 1 LOCATIONS LBL 34.
- [SDR AWXA0002004](https://openairdocs.org/sdr/AWXA0002004), Jul 20, 2001: INDICATOR. FAILED. PHX -AIR TURNBACK- FLT 173- AFTER TAKEOFF FROM PHX THE NR 1 ENGINE EGT INDICATOR WENT TO ZERO AND THE AIRCRAFT RETURNED TO PHX. THE AIRCRAFT LANDED OVERWEIGHT A
- [SDR AWXA0001887](https://openairdocs.org/sdr/AWXA0001887), May 30, 2001: NUT. LOOSE. IAH-AIR TURNBACK- INFLIGHT SHUTDOWN - FLT 831- DURING CLIMB THE NR 1 ENGINE EGT INDICATOR RED LIGHT ILLUMINATED. THE DIGITAL AND ANALOG EGT INDICATIONS SHOWED E
- [SDR AWXA0001483](https://openairdocs.org/sdr/AWXA0001483), Mar 12, 2001: FIRE LOOP. OUT OF POSITION. PHX - AIR TURNBACK - 3/5/01 - ON CLIMBOUT AT FL270 W/ FULL POWER, THE RT WING BODY OVERHEAT LIGHT ILLUMINATED; W/ THE ISOLATION VALVE CLOSED AND RIGHT BLEED OFF
- [SDR AWXA0001149](https://openairdocs.org/sdr/AWXA0001149), Dec 29, 2000: SKIN. CRACKED. LIGHT AFT OF RT AFT WING-BODY FAIRING HAS TEMP REPAIR DOUBLER BS 727D STR 23R. REMOVED TEMP DOUBLER, FABED REPAIR PARTS AND INSTALLED IAW ER 03-5361-00347-001 A
- [SDR AWXA0001148](https://openairdocs.org/sdr/AWXA0001148), Dec 29, 2000: BRACKET. BROKEN. RT A/C EXHAUST LOUVER MOUNT BRACKETS BROKEN. REMOVED, FABED REPLACEMENT BRACKET, INSTALLED IAW SRM 51-40-02 AND SRM 51-30-01
- [SDR AWXA0001147](https://openairdocs.org/sdr/AWXA0001147), Dec 29, 2000: FLOORBEAM. CORRODED. FS 312 RBL 6 - RBL 12 FLOOR BEAM UPPER CHORD CORRODED OUT OF LIMITS. CUT OUT DAMAGED CHORD LBL 6 - RBL 26 AND REPAIRED IAW SRM 53-10-51 FIG 205
- [SDR AWXA0001146](https://openairdocs.org/sdr/AWXA0001146), Dec 29, 2000: BRACKET. BROKEN. LT A/C EXHAUST LOWER MOUNT BRACKETS BROKEN. REMOVED, FABED REPLACEMENT BRACKET, INSTALLED IAW SRM 51-40-02 AND SRM 51-30-01
- [SDR AWXA0001145](https://openairdocs.org/sdr/AWXA0001145), Dec 29, 2000: SKIN. CRACKED. LT PYLON SKIN CRACKED AT ACCESS PANEL 5727L. STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER IAW SRM 54-50-01, S/B 737-54-1035
- [SDR AWXA0001144](https://openairdocs.org/sdr/AWXA0001144), Dec 29, 2000: SKIN. CORRODED. LIGHT SURFACE CORROSION ON LT WING LOWER SKIN AT ACCESS PANEL 7212 FLANGE. REMOVED CORROSION W/I LIMITS IAW SRM 57-20-01 FIG 205; SHOT PEENED IAW 51-20-06 FIG 1
- [SDR AWXA0001143](https://openairdocs.org/sdr/AWXA0001143), Dec 29, 2000: SKIN. CRACKED. LT O/B WING AFT FLAP L/E DEEP CHAFE WITH CRACK AT O/B ROLLERS. REMOVED DAMAGE, FABED AND INSTALLED REPAIR PARTS SKIN & SPLICE IAW SRM 57-53-01 FIG 204.
- [SDR AWXA0001135](https://openairdocs.org/sdr/AWXA0001135), Dec 21, 2000: STIFFENER. CRACKED. NR 6 FLAP TRACK FAIRING STIFFENER AND DOUBLER CRACKED. REMOVED RT. WING I/B FLAP ASSY BOTTOM I/B STIFFENER AND DOUBLER IAW SRM 51-40-02; INSTALLED NEW STIFFENER
- [SDR AWXA0001134](https://openairdocs.org/sdr/AWXA0001134), Dec 21, 2000: SKIN. CRACKED. LEFT I/B AFT FLAP LEADING EDGE CRACKED AT 3RD HINGE OBD. REMOVED LEADING EDGE IAW SRM 51-40-02; CUTOUT DAMAGED PORTION IAW 57-53-01; FABED SKIN REPAIR AND SPLIC
- [SDR AWXA0001133](https://openairdocs.org/sdr/AWXA0001133), Dec 21, 2000: SKIN. BROKEN. FLANGE ON A/C GROUND CONNECT BROKEN (INNER FLANGE INNER DOUBLER) ON FUSELAGE SKIN AT DOOR LANDING RING. CUT OUT DAMAGED FLANGE; HFEC SHOWS NO CRACKS; FABED REPA
- [SDR AWXA0001132](https://openairdocs.org/sdr/AWXA0001132), Dec 21, 2000: SKIN. CORRODED. LIGHT SURFACE CORROSION ON LT WING LOWER SKIN AT ACCESS PANEL 7211 FLANGE. REMOVED CORROSION W/I LIMITS IAW SRM 57-20-01 FIG 205; SHOT PEENED IAW 51-20-06 FIG 1
- [SDR AWXA0001131](https://openairdocs.org/sdr/AWXA0001131), Dec 21, 2000: BULKHEAD. CRACKED. ULTRASONIC INSP. DETECTED CRACK APPROX. 4.0 INCHES LONG AT FWD PRESSURE BULKHEAD AT STA 178 WL 213 BETWEEN LBL 5 & LBL 17 ON WEB BEHIND HORIZ ANGLE STIFFENER. R
- [SDR AWXA0001130](https://openairdocs.org/sdr/AWXA0001130), Dec 21, 2000: FRAME. CRACKED. CABIN RT I/B FWD OVERWING EXIT FRAME SUPPORT CRACKED AT BOTTOM FASTENER HOLE AREA BS 616 BELOW CABIN FLOOR PANEL STR 17R. REMOVED FASTENERS AND COLLARS IAW ER 0
- [SDR AWXA0001129](https://openairdocs.org/sdr/AWXA0001129), Dec 21, 2000: STRAP. CRACKED. FS 178 WL 187 BL 0 STRAP CRACKED. REMOVED STRAP; FABED REPAIR STRAP AND DOUBLER IAW SRM 51-70-13 FIG 1
- [SDR AWXA0001128](https://openairdocs.org/sdr/AWXA0001128), Dec 21, 2000: SEAT TRACK. CORRODED. CABIN SEAT TRACK RBL 24 I/B FLANGE HAS BARE METAL ON UNDERSIDE AT EACH FLOOR BOARD FASTENER HOLE - SOME WITH LIGHT SURFACE CORROSION - FROM BS 540 - 727. REMOVE
- [SDR AWXA0001127](https://openairdocs.org/sdr/AWXA0001127), Dec 21, 2000: CHANNEL. CORRODED. CORROSION ON RT AFT LAV WALL LOWER SUPPORT CHANNEL STA 993 FROM RBL 23 - RBL 44 WAS FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED HAT SECTION IAW SRM 51-40-02; FAB
- [SDR AWXA0001126](https://openairdocs.org/sdr/AWXA0001126), Dec 21, 2000: WEB. CRACKED. FLOOR WEB CRACKED FS 180 WL 207 LBL 26 (1.0L). REMOVED DAMAGED WEB; FABED NEW WEB; INSTALLED WEB IAW SRM 51-40-02 DWG 65-45833
- [SDR AWXA0001124](https://openairdocs.org/sdr/AWXA0001124), Dec 20, 2000: SKIN. CRACKED. NR 1 SLAT HAS CRACKS IN AFT ROW OF RIVETS LWR SURFACE, INBD OF ACTUATOR. REMOVED DAMAGED AREA; FABED AND INSTALLED REPAIR PARTS, FILLER AND SPLICE PLATE IAW SRM
- [SDR AWXA0001123](https://openairdocs.org/sdr/AWXA0001123), Dec 20, 2000: SKIN. SCRATCHED. FUSE SKIN FROM STA 1060-1070 L14L HAS DEEP SCRATCH UNDER W OF TAIL NUMBER; FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED SKIN; NDT NO CRACKS NOTED; FABED REPAIR PL
- [SDR AWXA0001122](https://openairdocs.org/sdr/AWXA0001122), Dec 20, 2000: WEB. CRACKED. FLOOR WEB CRACKED FS 180 WL 207 RBL 26 (1.0L). REMOVED DMGD WEB IAW SRM 51-40-02; FABED REPLACEMENT WEB IAW DWG 65-45833; INSTALLED IAW 51-40-02
- [SDR AWXA0001121](https://openairdocs.org/sdr/AWXA0001121), Dec 20, 2000: FRAME. CRACKED. SIDE CHORD CRACKED FS 178 WL 207 LBL 26 (1.6L) AND WL 195 LBL 24 (1.3L). CUTOUT CRACKED SECTION OF CHORD WL 212-175 IAW ER 03-5310-00339-JS3; NDT NO CRACKS NOTE
- [SDR AWXA0001120](https://openairdocs.org/sdr/AWXA0001120), Dec 20, 2000: WEB. CRACKED. CENTER WEB CRACKED FS 178 WL 187 LBL 0.7 AND RBL 0.7. REMOVED DAMAGED AREA; FABED AND INSTALLED REPAIR PARTS IAW SRM 53-10-08 FIG 203
- [SDR AWXA0001119](https://openairdocs.org/sdr/AWXA0001119), Dec 20, 2000: WEB. CRACKED. CENTER WEB CRACKED FS 178 RBL 5.0 WL 198 (1.3L) AND WL 202 (0.9L). REMOVED DAMAGE; FABED AND INSTALLED REPAIR PARTS IAW SRM 53-10-08 FIG 209
- [SDR AWXA0001115](https://openairdocs.org/sdr/AWXA0001115), Dec 18, 2000: FRAME. GOUGED. RT MLG WHEEL WELL, AFT CUTOUT VERTICAL ANGLE BRACKET GOUGED (LOCATED ADJACENT TO GROUNDING STUD). REMOVED RT HYD PANEL COVER MAIN LANDING GEAR RIGHT SIDE IAW SR
- [SDR AWXA0001114](https://openairdocs.org/sdr/AWXA0001114), Dec 18, 2000: STIFFENER. CRACKED. LT WING LWBL 184 TE AT NR 3 FLAP TRACK FAIRING INBOARD FORMER/STIFFENER CRACKED. REMOVED AND REPLACED STIFFENER IAW SRM 51-40-02
- [SDR AWXA0001113](https://openairdocs.org/sdr/AWXA0001113), Dec 18, 2000: BULKHEAD. CRACKED. CENTER WEB CRACKED FS 178 LBL 5.0 WL 198 & 202. REMOVED DAMAGE, FABED AND INSTALLED REPAIR PARTS IAW SRM 53-10-18 FIG 209
- [SDR AWXA0001112](https://openairdocs.org/sdr/AWXA0001112), Dec 18, 2000: INTERCOSTAL. CRACKED. INTERCOSTAL CRACKED THRU FS 178 WL 195 RBL 24. REMOVED INTERCOSTAL IAW SRM 51-40-02; CUTOUT DAMAGE IAW 53-10-08 FIG 202; HFEC INSPEC IAW B737 NTM PT.6 51-00-00 
- [SDR AWXA0001111](https://openairdocs.org/sdr/AWXA0001111), Dec 18, 2000: INTERCOSTAL. CRACKED. INTERCOSTAL CRACKED THRU FS 178 WL 195 LBL 24. REMOVED INTERCOSTAL IAW SRM 51-40-02; CUTOUT DMG IAW 53-10-08 FIG 202; HFEC INSPEC IAW B737 NTM PT.6 51-00-00 FIG
- [SDR AWXA0001049](https://openairdocs.org/sdr/AWXA0001049), Dec 12, 2000: SKIN. SCRATCHED. FUSELAGE SKIN STA 1060-1070 L14L HAS DEEP SCRATCH UNDER W OF TAIL NUMBER - FOUND OUT OF LIMITS. REMOVED DAMAGED SKIN, NDT NO CRACKS NOTED; FABED REPAIR PLATE, I
- [SDR AWXA0001048](https://openairdocs.org/sdr/AWXA0001048), Dec 12, 2000: BULKHEAD. CRACKED. CENTER WEB CRACKED FS 178 WL 187 LBL 0.7 (1.9) AND RBL 0.7 (1.5L). REMOVED DAMAGED AREA, FABED AND INSTALLED REPAIR PARTS IAW SRM 53-10-08 FIG 203
- [SDR AWXA0001047](https://openairdocs.org/sdr/AWXA0001047), Dec 12, 2000: BULKHEAD. CRACKED. CENTER WEB CRACKED FS 178 RBL 5.0 WL 198 (1.3L) AND WL 202 (0.9L). REMOVED DAMAGE, FABED AND INSTALLED REPAIR PARTS IAW SRM 53-10-08 FIG 209
- [SDR AWXA0001046](https://openairdocs.org/sdr/AWXA0001046), Dec 12, 2000: BULKHEAD. CRACKED. CENTER WEB CRACKED FS 178 LBL 5.0 WL 198 & 202. REMOVED DAMAGE, FABED AND INSTALLED PARTS IAW SRM 53-10-08 FIG 209
- [SDR AWXA0001050](https://openairdocs.org/sdr/AWXA0001050), Dec 12, 2000: FRAME. CRACKED. CABIN RT I/B FWD OVERWING EXIT FRAME SUPPORT CRACKED AT BOTTOM FASTENER HOLE AREA STA 616 STR 17R BELOW CABIN FLOOR PANEL. REMOVED FASTENERS AND COLLARS, CUT OU
- [SDR AWXA0000881](https://openairdocs.org/sdr/AWXA0000881), Nov 15, 2000: ADC. FAILED. INBOUND TO ONT FAILURE FLAGS DISPLAYED ON CAPTAINS AIRSPEED IND, VMO POINTER, MACH ASI, ALTIMETER, VSI FAIL AND SPEED TAPE FAIL ON CAPT''S HORIZON GPWS ALSO FAI
- [SDR AWXA0000492](https://openairdocs.org/sdr/AWXA0000492), Jul 20, 2000: BLOWER. FAILED. ON DESCENT TO LGB, ACRID SMELL NOTED BY ALL CREW MEMBERS. MEL ISSUED. REMOVED AND REPLACED E & E BLOWER (NML POSITION) AND FLOW SENSOR, OPS CHECK NORMAL. NO HIS
- [SDR AWXA9900448](https://openairdocs.org/sdr/AWXA9900448), Dec 3, 1999: TIE CLIP. CRACKED. STRINGER CLIP CRACKED STR 15L STA 1040. REMOVED DAMAGED PART PER SRM 51-40-02, FABRICATED REPLACEMENT PART FROM 7075T6 .032 QQA 250/134 R682523 IAW SRM 51-30-01
- [SDR AWXA9900447](https://openairdocs.org/sdr/AWXA9900447), Dec 3, 1999: TIE CLIP. CRACKED. REMOVED DAMAGED PART PER 737-300 SRM 51-40-02, FABRICATED REPLACEMENT PART FROM 7075T6 - .032 QQA250/13 R682523 IAW SRM 51-30-01 TREATED AND PRIMED PART IAW SRM
- [SDR AWXA9900446](https://openairdocs.org/sdr/AWXA9900446), Dec 3, 1999: SKIN. CRACKED. L-1 DOOR JAMB AFT LWR CORNER HAS 1 CRACK .25 LONG COMING OUT OF FASTENER .125 INCH ON EACH SIDE OF FASTENER. REPAIRED L-1 DOOR JAMB AFT LWR CORNER FUSELAGE SKIN
- [SDR AWXA9900445](https://openairdocs.org/sdr/AWXA9900445), Dec 3, 1999: SKIN. CRACKED. R-1 DOOR JAMB AFT LWR CORNER HAS 3 CRACKS, ALL START FROM EDGE TWO 1/4 CRACKS STOP AT FASTENERS ONE EXTENDS PAST FASTENER. CUT OUT DAMAGED AREA, ACCOMPLISHED HF
- [SDR AWXA9900441](https://openairdocs.org/sdr/AWXA9900441), Dec 2, 1999: SKIN. CRACKED. CRACK IN FUSELAGE SKIN AT THE UPPER CORNER OF L-2 DOOR HINGE CUTOUT. DAMAGED MATERIAL REMOVED, FABRICATED REPAIR DOUBLER OF 301 1/2 HARD 2660361 AND FILLER 2024
- [SDR AWXA9900442](https://openairdocs.org/sdr/AWXA9900442), Dec 1, 1999: FRAME. CRACKED. UPPER PART OF FRAME 500 HAD A CRACK APPROXIMATELY 1.5 INCH LONG AT BL 0 IN THE FWD CARGO COMPARTMENT. STOP DRILLED CRACK, FABRICATED A REPAIR DOUBLER PER 737 SR
- [SDR AWXA9800196](https://openairdocs.org/sdr/AWXA9800196), Aug 20, 1998: CHARGER. INOPERATIVE. EMERGENCY EXIT LIGHTS FROM ROW 19 TO 23 ON PAX SEATS INOP. REPLACED AFT BATTERY CHARGER, CHECK OK.
- [SDR AWXA9700552](https://openairdocs.org/sdr/AWXA9700552), Sep 4, 1997: SKIN. DENTED. DURING ROUTINE MAINTENANCE CHECK, FOUND DENT AT BS 405 ABOVE STR 16L. REMOVED DAMAGED SKIN, FABRICATED AND INSTALLED REPAIR PARTS PER SRM 53-00-01.
- [SDR AWXA9700551](https://openairdocs.org/sdr/AWXA9700551), Sep 4, 1997: STRINGER. CORRODED. DURING ROUTINE MAINTENANCE CHECK, FOUND FUSELAGE STRINGER 16 RT AT WING SCANNING LIGHT CUTOUT TO BE CRACKED AT STA 500C + 4 AND 500C + 16. REPAIRED DAMAGED STRI
- [SDR AWXA9700550](https://openairdocs.org/sdr/AWXA9700550), Sep 3, 1997: TRACK. CORRODED. DURING ROUTINE MAINTENANCE CHECK, FOUND LEFT WING, OUTBOARD FOREFLAP, OUTBOARD TRACK HAS CORRODED HOLES. REMOVED AND REPLACED OUTBOARD TRACK OHM 20-50-01.
- [SDR AWXA9700549](https://openairdocs.org/sdr/AWXA9700549), Sep 2, 1997: CARRIAGE. CORRODED. DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON NR 7 MAIN CARRIAGE SPINDLE. REMOVED AND REPLACED NR 7 CARRIAGE PER MM 27-51-44.

All 75: https://openairdocs.org/deregistered/N165AW-2002-05-20/reports.md

## FAA accident and incident reports (2)

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 19961026038119I](https://openairdocs.org/incident/19961026038119I), Oct 26, 1996: Boeing 737300 (N165AW), Kansas City, MO. Narrative: on 10/26/96, america west flight 2404 was en route phx to stl, when there was an electrical power loss on the right half of the console. The crew…
- [Incident 19890614039869I](https://openairdocs.org/incident/19890614039869I), Jun 14, 1989: Boeing 73733A (N165AW), Des Moines, IA. Nose gear unsafe light on. Made missed approach. Gear appeared down. Landed without incident.

## Other aircraft with N165AW

- [Cancelled 2015-05-20](https://openairdocs.org/deregistered/N165AW-2015-05-20): Waggonner Jack H EXCALIBUR, S/N 001, built 2010. Registration pending, canceled. Owner: [Kimberly, ID](https://openairdocs.org/faa-place/ID/Kimberly)

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