# N169AW: 1986 Boeing 737-33A, registration cancelled 2002-05-31

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: May 31, 2002
- Exported to: Jordan
- Status when cancelled: Valid registration
- Airframe: [Boeing 737-33A](https://openairdocs.org/model/boeing-737-33a) (registry code 1384673)
- Engine: [Amateur-built UNKNOWN ENG](https://openairdocs.org/engine/amateur-built-unknown-eng) (registry code 99999)
- Serial number: 23630
- Year built: 1986
- Type of aircraft: Fixed wing multi engine
- Airworthiness: Standard, transport
- Airworthiness date: December 3, 1986
- Certificate issued: January 19, 2001
- Last registry action: February 1, 2001
- Mode S code: A11332
- 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/N169AW
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=169AW
- Page: https://openairdocs.org/deregistered/N169AW-2002-05-31

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 (62, newest 50)

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

- [SDR AWXA0001727](https://openairdocs.org/sdr/AWXA0001727), May 14, 2001: ACTUATOR. FAILED. PHX - AIR TURNBACK, AFTER TAKEOFF THE FLAPS WERE RETRACTED BUT L/E FLAPS TRANSIT LIGHT ON FORWARD PANEL AND NR 1 SLAT INDICATOR ON THE OVERHEAD PANEL REMAINED I
- [SDR AWXA0001691](https://openairdocs.org/sdr/AWXA0001691), May 1, 2001: FLOORBEAM. CORRODED. THREE SPOTS OF CORROSION ON UPPER FLANGE OF FLOORBEAM BS 294 RBL 28-31. REMOVED CORRODED SECTION; FORMED AND INSTALLED SECTION OF UPPER T-CHORD IAW B737 SRM 51-
- [SDR AWXA0001692](https://openairdocs.org/sdr/AWXA0001692), May 1, 2001: BULKHEAD. CRACKED. BS 178 BLKHD WEB RBL 5 WL 200 HAS A .60 INCH CRACK EMANATING FROM BENEATH THE STRAP. CUT OUT DAMAGED WEB AREA; LOCATED, DRILLED, INSTALLED REPAIR DOUBLER AND FI
- [SDR AWXA0001690](https://openairdocs.org/sdr/AWXA0001690), May 1, 2001: STRUCTURE. CRACKED. FS 837 AFT CARGO DOOR, CRACK AT LWR CROSS BEAM, LOWER TEE, VERT LEG, 3RD HI-LOK FROM END BEAM. REMOVED DAMAGED AREA, LOCATED, DRILLED AND INSTALLED REPAIR FILLE
- [SDR AWXA0001689](https://openairdocs.org/sdr/AWXA0001689), May 1, 2001: STIFFENER. CORRODED. FS 294 TEE CAP STIFFENER CORRODED RBL 28-43. REMOVED DAMAGED AREA, LOCATED, DRILLED AND INSTALLED NEW TEE CAP STIFFENER IAW B737-300 SRM 51-40-02 PG 1-10.
- [SDR AWXA0001688](https://openairdocs.org/sdr/AWXA0001688), May 1, 2001: WEB. CRACKED. FS 178 COCKPIT FLOOR WEB CRACKED AT RBL 23 WL 207. REMOVED DAMAGED AREA, LOCATED, DRILLED AND INSTALLED NEW WEB SECTION IAW B737-300 SRM 51-40-02 PG 1-6 & 51-10
- [SDR AWXA0001687](https://openairdocs.org/sdr/AWXA0001687), May 1, 2001: STIFFENER. CORRODED. FS 1153 TORQUE BOX LEFT LWR O/B EDGE OF STIFFENER. CUT OUT DAMAGED AREA, LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER IAW B737-300 SRM 51-70-13 FIG 1 PG 1.
- [SDR AWXA0001686](https://openairdocs.org/sdr/AWXA0001686), May 1, 2001: BULKHEAD. CRACKED. FS 178 BLKHD CRACKED 2 PLACES LBL 4 & 1.2, RBL 8 WL 187-188. CUT OUT DAMAGED AREA, LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER IAW B737-300 SRM 53-10-08 TR 53
- [SDR AWXA0001685](https://openairdocs.org/sdr/AWXA0001685), May 1, 2001: SKIN. CRACKED. AFT CARGO COMPT UPPER LINER SKIN CRACKED AT CENTER LIGHTENING HOLE. LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER IAW B737-300 SRM 51-40-02 PG 3.
- [SDR AWXA0001684](https://openairdocs.org/sdr/AWXA0001684), May 1, 2001: BULKHEAD. CRACKED. FS 178 BLKHD CRACK AT WL 202.5 RBL 4.8. CUT OUT DAMAGED AREA, LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER IAW B737-300 SRM 53-10-08 TR 53-15 PG 1-11.
- [SDR AWXA0001683](https://openairdocs.org/sdr/AWXA0001683), May 1, 2001: BULKHEAD. CRACKED. FS 178 BLKHD CRACKED AT WL 234.1 RBL 7.8-9.7. CUT OUT DAMAGED AREA, LOCATED, DRILLED, AND INSTALLED REPAIR DOUBLER IAW B737-300 SRM 53-10-08 PG 265-269.
- [SDR AWXA0001682](https://openairdocs.org/sdr/AWXA0001682), May 1, 2001: FRAME. CRACKED. FS 178 BLKHD CRACK AT WL 187-230 CENTER OF RADIUS. REMOVED, LOCATED, DRILLED AND INSTALLED NEW SIDE CHORD IAW B737-300 SRM 51-10-02 PG 15 & 51-40-02 PG 1, 10.
- [SDR AWXA0001681](https://openairdocs.org/sdr/AWXA0001681), May 1, 2001: SKIN. CORRODED. BLIND RIVET REPAIR FORWARD OF AFT PRESSURE BLKHD BS 1012 STR 23L WL 182. REMOVED DOUBLER REPAIR WITH BLIND FASTENERS; FORMED AND INSTALLED REPAIR DOUBLER IAW B7
- [SDR AWXA0001680](https://openairdocs.org/sdr/AWXA0001680), May 1, 2001: BULKHEAD. CRACKED. FS 178 BLKHD CRACK AT WL 202.4 LBL 4.5. CUT OUT DAMAGED AREA; LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER IAW B737-300 SRM 51-10-08 TR 53-15 PG 1-11.
- [SDR AWXA0001679](https://openairdocs.org/sdr/AWXA0001679), May 1, 2001: FLOORBEAM. CORRODED. CORROSION ON AFT CORNER OF TRACK SECTION AND UPPER FLANGE OF FLOORBEAM AT BS 294 RBL 12-14; CORROSION REMOVAL OUT OF LIMITS. REMOVED FLOORBEAM T-CAP SECTION; LO
- [SDR AWXA0001650](https://openairdocs.org/sdr/AWXA0001650), Apr 26, 2001: BULKHEAD. CRACKED. FS 178 BLKHD HAS 1 INCH CRACK AT WL 197-198 LBL 4.8. CUT OUT DAMAGED WEB; LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER AND FILLER IAW BOEING 737-300 SRM 53-10-
- [SDR AWXA0001654](https://openairdocs.org/sdr/AWXA0001654), Apr 26, 2001: BULKHEAD. CRACKED. FS 178.5 BLKHD CRACK AT WL 188 LBL 5.7. CUT OUT DAMAGED AREA; LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER IAW AWA ER 03-5313-01109-TB1.
- [SDR AWXA0001653](https://openairdocs.org/sdr/AWXA0001653), Apr 26, 2001: BULKHEAD. CRACKED. FS 178 BLKHD HAS 1 INCH CRACK AT WL 206 RBL .6-1.8. CUT OUT DAMAGED AREA; LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER IAW SRM 53-10-08 TR 53-15 PG 1-11.
- [SDR AWXA0001652](https://openairdocs.org/sdr/AWXA0001652), Apr 26, 2001: BULKHEAD. CRACKED. FS 178 BLKHD HAS 1.5 INCH CRACK AT WL 200.3 LBL 5. CUT OUT DAMAGD AREA; LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 53-10-08 TR 53-15 PG 1-
- [SDR AWXA0001651](https://openairdocs.org/sdr/AWXA0001651), Apr 26, 2001: WEB. PUNCTURED. PUNCTURE IN VERT WEB RBL 44 FS 311.CUT OUT DAMAGED AREA; LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER IAW SRM 51-70-11 PG 1 AND 51-20-01 PG 1 AND 51-40-02 PG 3
- [SDR AWXA0001649](https://openairdocs.org/sdr/AWXA0001649), Apr 26, 2001: BULKHEAD. CANNING. FS 178 OIL CANNING AT WL 188-207 LBL 5 TO RBL 5. LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER IAW B737-300 SRM 53-10-08 PG 1-11.
- [SDR AWXA0001644](https://openairdocs.org/sdr/AWXA0001644), Apr 24, 2001: BULKHEAD. CRACKED. HFEC INDICATES .5 INCH CRACK EMANATING FROM BENEATH STRAP IN WEB BS 178 BLKHD RBL 6.8 WL 212.5 CONFIRMED 10X VISUAL. CUT OUT DAMAGED WEB AREA; LOCATED, DRILLED 
- [SDR AWXA0001629](https://openairdocs.org/sdr/AWXA0001629), Apr 24, 2001: BULKHEAD. CRACKED. HFEC INDICATES CRACK AT FASTENER HOLE LBL 10 WL 234.1 BS 179 BLKHD WEB FORWARD SIDE. CUT OUT DAMAGED SKIN AREA; LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER AN
- [SDR AWXA0001628](https://openairdocs.org/sdr/AWXA0001628), Apr 24, 2001: PRESSURE PANEL. CRACKED. LEFT MLG W/W PRESSURE WEB CRACKED AT BS 663 APPROX BL 32. REMOVED UPPER ATTACH CHANNEL; TRIMMED OUT DAMAGED PORTION OF WEB; FABBED REPAIR -1 DOUBLER, -2 FILLER 
- [SDR AWXA0001168](https://openairdocs.org/sdr/AWXA0001168), Jan 2, 2001: WIRE. BROKEN. EMERGENCY ESCAPE PATH LIGHT AT SEAT 2B FAILED TO ILLUMINATE DURING TEST. FOUND BROKEN WIRE AT SEAT 2B; SPLICED THE WIRE AND LIGHT OPS CHECKED GOOD
- [SDR AWXA0000243](https://openairdocs.org/sdr/AWXA0000243), Apr 6, 2000: FRAME. CORRODED. C-CHECK, LEVEL 1 CORROSION AFT PRESS BULKHEAD CHORD AT RBL 2 IN BILGE AREA. REMOVED DAMAGED CHORD SEGMENT AND REPAIRED IAW ER 03-5312-00075-022 AND 737 SRM 53-8
- [SDR AWXA0000242](https://openairdocs.org/sdr/AWXA0000242), Apr 6, 2000: STIFFENER. CORRODED. C-CHECK, LEVEL 1 CORROSION FS 1016 AFT PRESS BULKHEAD BELOW FLOOR ON STIFFENER AT CENTERLINE RT SIDE. REMOVED DAMAGED AREA, FABRICATED STIFFENER AND FILLER FROM
- [SDR AWXA0000241](https://openairdocs.org/sdr/AWXA0000241), Apr 6, 2000: BULKHEAD. CORRODED. C-CHECK, LEVEL 1 CORROSION AFT PRESSURE BULKHEAD BELOW BL 0 TO RBL 3. REMOVED DAMAGED SECTION, FABRICATED REPAIR PARTS FROM 2024 T3 .032 IAW 737 SRM 53-80-08 FI
- [SDR AWXA0000240](https://openairdocs.org/sdr/AWXA0000240), Apr 5, 2000: SKIN. DELAMINATED. C-CHECK, LT WING I/B MID FLAP HAS AREA OF DELAMINATION 36 INCHES I/B FROM O/B END AND 2.5 INCHES UP FROM T/E UPPER AND LOWER SURFACE. REMOVED DELAMINATED SECTIO
- [SDR AWXA0000239](https://openairdocs.org/sdr/AWXA0000239), Apr 5, 2000: FLOORBEAM. CRACKED. C-CHECK, REPAIR DOUBLER ON AFT FACE OF FLOORBEAM AT BS 520 LBL 45.5 CRACKED IN RADIUS .5 INCH. REMOVED DAMAGED DOUBLER AND REPAIRED IAW AWA EO 53-14-12.
- [SDR AWXA0000238](https://openairdocs.org/sdr/AWXA0000238), Apr 5, 2000: FLOORBEAM. CORRODED. C-CHECK, FLOOR SUPPORT AT FS 950 LBL 50 - LBL 20 CORRODED AT FASTENER HOLES. REMOVED AND REPLACED DAMAGED PARTS IAW 737 SRM 51-40-02, FABRICATED SUPPORT FROM BA
- [SDR AWXA0000237](https://openairdocs.org/sdr/AWXA0000237), Apr 5, 2000: FLOORBEAM. CORRODED. C-CHECK, TOP SURFACE OF FLOOR SUPPORT BEAM FROM FS 1016 LBL 5 TO FS 986 LBL 20 HAS EXFOLIATED CORROSION. REMOVED AND REPLACED FLOOR SUPPORT IAW 737 SRM 51-40-02
- [SDR AWXA0000236](https://openairdocs.org/sdr/AWXA0000236), Apr 5, 2000: FLOORBEAM. CORRODED. C-CHECK, STA 1016 FLOORBEAM UPPER T FLANGE CORRODED AT LBL 5. CUT OUT DAMAGED AREA IAW 737 SRM 53-00-5, FABRICATED REPAIR SECTION FROM (BAC 1505-100617 7075T73)
- [SDR AWXA0000235](https://openairdocs.org/sdr/AWXA0000235), Apr 5, 2000: FLOORBEAM. CORRODED. C-CHECK, FS 967 RBL 44 UPPER T-CAP CORRODED. CUT OUT DAMAGED AREA 737 SRM 53-30-51, FABRICATED REPAIR PARTS IAW 737 SRM 53-30-51, INSTALLED PARTS IAW 737 SRM 53
- [SDR AWXA0000234](https://openairdocs.org/sdr/AWXA0000234), Apr 5, 2000: FLOORBEAM. CORRODED. C-CHECK, FLOORBEAM AT BS 967 RBL 6 CORRODED. CUT OUT DAMAGED AREA, FABRICATED REPLACEMENT PARTS IAW 737 SRM 53-00-51, TREATED AND PRIMED IAW 737 SRM 51-20-02, I
- [SDR AWXA0000233](https://openairdocs.org/sdr/AWXA0000233), Apr 5, 2000: FLOORBEAM. CORRODED. C-CHECK, FLOORBEAM FS 1006 CORRODED AT FASTENER HOLE RBL 12. REMOVED DAMAGED AREA IAW 737 SRM 53-00-51 FIG 202, FABRICATED REPAIR STRAP FROM .125 7075 T6, ALODI
- [SDR AWXA0000232](https://openairdocs.org/sdr/AWXA0000232), Apr 5, 2000: THRESHOLD. CORRODED. C-CHECK, L-2 DOOR MOP SILL ANGLE HAS EXFOLIATING INTERGRANULAR CORROSION AT DOOR THRESHOLD AREA. REMOVED AND REPLACED L-2 MOPSILL IAW 737 SRM 51-40-02 AND SRM 5
- [SDR AWXA0000231](https://openairdocs.org/sdr/AWXA0000231), Apr 5, 2000: SKIN. CRACKED. C-CHECK, L-1 DOOR LOWER HINGE CUTOUT IN FUSELAGE SKIN HAS VISUAL INDICATION OF CRACK. HFEC INSP IAW 737 NTM PT 6, STOP DRILLED .25 INCH CRACK IAW 737 SRM 53-10-
- [SDR AWXA0000230](https://openairdocs.org/sdr/AWXA0000230), Apr 5, 2000: FLOORBEAM. CORRODED. C-CHECK, FLOORBEAM AT 986.5 TOP T-ANGLE CORRODED FROM RBL 20 TO LBL 20 (PREVIOUS REPAIR). REMOVED DAMAGED SECTION IAW 737 SRM 53-00-51, FABRICATED PART AND INST
- [SDR AWXA9800187](https://openairdocs.org/sdr/AWXA9800187), Aug 5, 1998: FUSE. BLOWN. SEAT MOUNTED EMERGENCY EXIT LIGHTS INOP AT ROWS 19 THROUGH 23 LEFT. FOUND BLOWN FUSE ON BATTERY CHARGER. REPLACED FUSE, CORRECTED SHORTING CONDITION. OPS CK GOO
- [SDR AWXA9800137](https://openairdocs.org/sdr/AWXA9800137), May 28, 1998: INDICATOR. MALFUNCTIONED. FLAPS DID NOT DEPLOY WITH PRIMARY CONTROL, ALTERNATE OK. REMOVED AND REPLACED FLAP POSITION INDICATOR PER 27-58-41, OPS GOOD ON GROUND AT THIS TIME.
- [SDR AWXA9800030](https://openairdocs.org/sdr/AWXA9800030), Jan 6, 1998: SKIN. CRACKED. DURING SCHEDULED C-13 INSPECTION, FOUND CRACK ON EXTERNAL SKIN AT FWD GALLEY DOOR THRESHOLD AFT LOWER CORNER. SKIN CRACK IN EXTERNAL SKIN AT LOWER AFT CORNER OF
- [SDR AWXA9800029](https://openairdocs.org/sdr/AWXA9800029), Dec 23, 1997: STRINGER. CORRODED. DURING SCHEDULED C-13 INSPECTION, FOUND CORROSION ON STR 27 LT, BS 947 - 954. REPAIRED STRINGER 27 LT, BS 947-954 IAW, SRM 53-00-03 AND 51-40-2.
- [SDR AWXA9600741](https://openairdocs.org/sdr/AWXA9600741), Dec 12, 1996: WIRE. BROKEN. DURING ROUTINE MAINTENANCE CHECK, FOUND ROW 3 EMERGENCY LIGHT INOP. FOUND BROKEN WIRE. REPLACED SPLICE, OPS CHECK GOOD.
- [SDR AWXA9600753](https://openairdocs.org/sdr/AWXA9600753), Dec 9, 1996: SEAT TRACK. CORRODED. DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON SEAT TRACK AT STA 338, RBL 25, WL 208. INSTALLED NEW SEAT TRACK AT BS 338, RBL 25, WL 208 IN ACCORDANCE WIT
- [SDR AWXA9600756](https://openairdocs.org/sdr/AWXA9600756), Dec 5, 1996: CARRIAGE. CORRODED. DURING ROUTINE MAINTENANCE CHECK, FOUND R/W OUTBOARD MID FLAP INBOARD CARRIAGE SPINDAL CORRODED. REMOVED AND REPLACED R/W O/B MID FLAP I/B CARRIAGE PER MM 27-51
- [SDR AWXA9600754](https://openairdocs.org/sdr/AWXA9600754), Dec 4, 1996: SEAT TRACK. CORRODED. DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON SEAT TRACK AT STA 338, RBL 45, WL 208. INSTALLED NEW SEAT TRACK AT BS 338, RBL 45, WL 258 IN ACCORDANCE WIT
- [SDR AWXA9600757](https://openairdocs.org/sdr/AWXA9600757), Dec 3, 1996: FLOORBEAM. CORRODED. DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON FLOORBEAM UPPER CHORD AT BS 294.5, WL 208, RBL 14 TO LBL 2. REPAIRED FLOORBEAM UPPER CHORD IAW, SRM 53-10-5
- [SDR AWXA9600755](https://openairdocs.org/sdr/AWXA9600755), Dec 3, 1996: MOPSILL. CORRODED. DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON RT MOPSILL AT BS 284 TO 332, RBL 62, WL 208. REMOVED AND REPLACED MOPSILL AT BS 284 TO 332, WL 208, RBL 62,
- [SDR AWXA960491](https://openairdocs.org/sdr/AWXA960491), Jul 16, 1996: PIN. UNSEATED. PHX - FLT 2475 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHT 3-L INOPERATIVE. RESEATED PIN IN CONNECTOR UNDER SEAT 3A. OPERATONS CHECK GOOD. (X)

All 62: https://openairdocs.org/deregistered/N169AW-2002-05-31/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 19921018049759I](https://openairdocs.org/incident/19921018049759I), Oct 18, 1992: Boeing 73733A (N169AW), Boston, MA, Minor damage. Struck a fuel truck while parking at gate. Was under direction of lead marshaller. Truck inside safety circle.
- [Incident 19911215060019I](https://openairdocs.org/incident/19911215060019I), Dec 15, 1991: Boeing 73733A (N169AW), Santa Ana, CA. Due to cockpit TCAS noise crew missed ATC call for a turn. No loss of separation or terrain problem.

## Other aircraft with N169AW

- [Cancelled 2017-04-24](https://openairdocs.org/deregistered/N169AW-2017-04-24): Stuckman Larry EXEC 162F, S/N 6463, built 2008. Registration expired, pending cancellation. Owner: [Stuckman Larry N](https://openairdocs.org/faa-owner/STUCKMAN%20LARRY%20N), [Vincennes, IN](https://openairdocs.org/faa-place/IN/Vincennes)

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