# N174AW: 1987 Boeing 737-33A, registration cancelled 2006-07-31

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: July 31, 2006
- 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: 23633
- Year built: 1987
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 27, 1987
- Certificate issued: November 24, 2004
- Last registry action: November 24, 2004
- Mode S code: A1281E
- Owner when cancelled: [Rpk Capital I LLC](https://openairdocs.org/faa-owner/RPK%20CAPITAL%20I%20LLC)
- Location: [Chicago, IL](https://openairdocs.org/faa-place/IL/Chicago)
- Owner type: Corporation
- Owner's area on the map: 41.9022° N, 87.6833° W: Placed by OpenAirDocs at the center of ZIP code 60622, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N174AW
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=174AW
- Page: https://openairdocs.org/deregistered/N174AW-2006-07-31

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 (173, newest 50)

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

- [SDR AWXA200600406](https://openairdocs.org/sdr/AWXA200600406), Mar 1, 2006: SLIDE. UNKNOWN. PHX - EES - DURING SCHEDULED DEPLOYMENT OF THE R-1 DOOR, THE SLIDE ENDED UP NOT BEING PERPENDICULAR TO THE AIRCRAFT, THE SLIDE CAME OUT TWISTED. MAINTENANCE REM
- [SDR AWXA200600206](https://openairdocs.org/sdr/AWXA200600206), Feb 5, 2006: PROXIMITY SENSOR. FAULTY. PHX - AIR TURN BACK - FLT 504 - CREW REPORTED THAT AFTER T/O HAD NORMAL GEAR RETRACTION, PASSING THROUGH 10000 FEET GOT A RED NOSE GEAR INDICATION. CREW LOWERED
- [SDR AWXA200600008](https://openairdocs.org/sdr/AWXA200600008), Jan 2, 2006: TERMINAL BLOCK. LOOSE. LAS - AIR TURN BACK - FLT 421 - AFTER CLIMB-OUT, CREW REPORTED THAT THE NR 2 ENG OVERHEATED WITH AN EGT INDICATION OF 1130 DEG C FOR 2 TO 3 SECONDS WITH ASSOCIA
- [SDR AWXA200501610](https://openairdocs.org/sdr/AWXA200501610), Dec 27, 2005: WINDSHIELD. CRACKED. DURING CRUISE, DEPARTED FROM DFW EN ROUTE TO LAS, AT FL 340 CREW REPORTED CAPT OUTER WINDSHIELD CRACKED. CREW DIVERTED & LANDED WITHOUT FURTHER INCIDENT. MX R &
- [SDR AWXA200501261](https://openairdocs.org/sdr/AWXA200501261), Oct 20, 2005: SKIN. DAMAGED. PHX - MAJOR REPAIR - DURING OVERNIGHT INSPECTION DISCOVERED 3.5 INCH CRACK IN FUSELAGE LOCATED AT STA 927 AND STR 25R. MAINTENANCE REMOVED DAMAGED SKIN IAW BOEI
- [SDR AWXA200500756](https://openairdocs.org/sdr/AWXA200500756), Jun 24, 2005: CONNECTOR. DIRTY. ON LANDING, FLAPS AT ZERO, HOT LANDING. LANDED WITHOUT FURTHER INCIDENT. CREW REPORTED FLAP PROBLEM TO TOWER PRIOR TO LANDING. CREW REQUESTED PRIORITY LANDING D
- [SDR AWXA200500535](https://openairdocs.org/sdr/AWXA200500535), May 3, 2005: BATTERY. DISCHARGED. MCI - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE AFT CABIN EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT CABIN EMERGENCY FL
- [SDR AWXA200500482](https://openairdocs.org/sdr/AWXA200500482), Apr 16, 2005: BRACKET. CRACKED. MCN - MAJOR REPAIR - DURING C-19 CHECK 2 INCH CRACK WAS FOUND AT FASTENER HOLE AND A 1 INCH CRACK WAS FOUND IN INBOARD FLANGE RADIUS OF GUSSET BRACKET AT FR 335
- [SDR AWXA200500489](https://openairdocs.org/sdr/AWXA200500489), Apr 15, 2005: CLIP. CRACKED. MCN - MAJOR REPAIR - DURING C-19 CHECK A .5625 INCH CRACK WAS FOUND ON FRAME ATTACH CLIP AT BS 827 BETWEEN STR 25 RT AND STR 26 RT. MAINTENANCE REMOVED CRACKED 
- [SDR AWXA200500492](https://openairdocs.org/sdr/AWXA200500492), Apr 4, 2005: FRAME. CRACKED. MCN - MAJOR REPAIR - DURING C-19 CHECK A .375 INCH CRACK WAS FOUND IN FORWARD EDGE OF AFT CARGO DOOR AT FASTENER HOLES FOR PULLEY BRACKET BS 801. MAINTENANCE CU
- [SDR AWXA200500488](https://openairdocs.org/sdr/AWXA200500488), Apr 4, 2005: SKIN. DELAMINATED. MCN - MAJOR REPAIR - DURING C-19 CHECK FOUND THE UPPER SURFACE OF THE NR 3 SLAT T/E WEDGE ASSEMBLY DELAMINATED AT SLAT STA 54 LT. MAINTENANCE CUT OUT DELAMINATE
- [SDR AWXA200500487](https://openairdocs.org/sdr/AWXA200500487), Apr 4, 2005: SKIN. DELAMINATED. MCN - MAJOR REPAIR - DURING C-19 CHECK FOUND THE UPPER SURFACE OF THE NR 3 SLAT T/E WEDGE ASSEMBLY DELAMINATED AT SLAT STA 84 LT. MAINTENANCE CUT OUT DELAMINATE
- [SDR AWXA200500486](https://openairdocs.org/sdr/AWXA200500486), Apr 4, 2005: SKIN. DELAMINATED. MCN - MAJOR REPAIR - DURING C-19 CHECK FOUND THE RIGHT TOP AFT SECTION OF RUDDER DELAMINATED AT RUDDER STA 238. MAINTENANCE REMOVED DELAMINATED SECTION OF RT TO
- [SDR AWXA200500464](https://openairdocs.org/sdr/AWXA200500464), Apr 4, 2005: SKIN. DELAMINATED. MCN - MAJOR REPAIR - DURING C-19 CHECK THE NR 2 SLAT WEDGE WAS FOUND DELAMINATED ON THE UPPER & LOWER SURFACE AT OUTBOARD END BETWEEN SLAT STA 250.9 AND SLAT ST
- [SDR AWXA200500463](https://openairdocs.org/sdr/AWXA200500463), Apr 4, 2005: SKIN. DELAMINATED. MCN - MAJOR REPAIR - DURING C-19 CHECK THE NR 1 SLAT WEDGE WAS FOUND DELAMINATED ON THE UPPER & LOWER SURFACE AT SLAT STA 348 LT. MAINTENANCE REMOVED DAMAGE IN 
- [SDR AWXA200500462](https://openairdocs.org/sdr/AWXA200500462), Apr 4, 2005: SKIN. DELAMINATED. MCN - MAJOR REPAIR - DURING C-19 CHECK THE NR 4 SLAT WEDGE WAS DELAMINATED AT THE BOTTOM OUTBOARD END BETWEEN SLAT STA 120-124 RT. MAINTENANCE REMOVED DAMAGE IN
- [SDR AWXA200500490](https://openairdocs.org/sdr/AWXA200500490), Apr 2, 2005: SKIN. CHAFED. MCN - MAJOR REPAIR - DURING C-19 CHECK THE LEFT INBOARD MID-FLAP LOWER SKIN WAS FOUND CHAFED AT WS 100. MAINTENANCE BLENDED OUT DAMAGE ON LEFT INBOARD MID-FLAP 
- [SDR AWXA200500493](https://openairdocs.org/sdr/AWXA200500493), Apr 1, 2005: SKIN. CHAFED. MCN - MAJOR REPAIR - DURING C-19 CHECK FOUND THE LOWER CENTER SECTION SKIN OF THE LEFT OUTBOARD FORE-FLAP CHAFED AT WBL 298. MAINTENANCE CUT OUT CHAFED SKIN ON 
- [SDR AWXA200500491](https://openairdocs.org/sdr/AWXA200500491), Apr 1, 2005: SKIN. DELAMINATED. MCN - MAJOR REPAIR - DURING C-19 CHECK THE LT OUTBOARD FORE-FLAP WAS FOUND DELAMINATED AT THE UPPER AFT OUTBOARD CORNER. MAINTENANCE CUT OUT DAMAGE ON LT OUTBOA
- [SDR AWXA200500471](https://openairdocs.org/sdr/AWXA200500471), Apr 1, 2005: DOOR FRAME. CRACKED. DURING C-19 CHECK A .3125 INCH CRACK WAS FOUND ON R-1 DOOR AFT FRAME AT 3RD DOOR STOP CUTOUT FROM BOTTOM BS 329, STR 12 RT. MAINTENANCE TRIMMED OUT DAMAGE R-1 D
- [SDR AWXA200500470](https://openairdocs.org/sdr/AWXA200500470), Apr 1, 2005: DOOR FRAME. CRACKED. DURING C-19 CHECK A .375 INCH CRACK WAS FOUND ON R-1 DOOR AFT FRAME AT 4TH DOOR STOP FROM BOTTOM BS 344, STR 13 RT. MAINTENANCE TRIMMED OUT DAMAGE R-1 DOOR AFT 
- [SDR AWXA200500378](https://openairdocs.org/sdr/AWXA200500378), Mar 30, 2005: WIRE. BROKEN. PHX - EEL - DURING 4-DAY CHECK, FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 14 LT INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE AT PIN FOR CONNECTOR, RETER
- [SDR AWXA200500361](https://openairdocs.org/sdr/AWXA200500361), Mar 24, 2005: SWITCH. SHORTED. PHX - ABORTED TAKEOFF - FLT 0506 - ON TAKEOFF AT PHX EN ROUTE TO YVR UPON ADVANCING THROTTLES AND BRAKE RELEASE THE TAKEOFF CONFIGURATION WARNING HORN SOUNDED, 
- [SDR AWXA200500363](https://openairdocs.org/sdr/AWXA200500363), Mar 2, 2005: CIRCUIT BREAKER. DEFECTIVE. LAS - ABORTED TAKEOFF - FLT 0399 - ON TAKEOFF AT LAS EN ROUTE FOR DFW THE TAKEOFF CONFIGURATION WARNING HORN SOUNDED COUNTINUOUSLY, RETURNED TO GATE. MAINTENANC
- [SDR AWXA200401358](https://openairdocs.org/sdr/AWXA200401358), Dec 6, 2004: LIGHT. INOPERATIVE. DFW - EEL - DURING A-01 CHECK FUNCTIONAL TEST OF EMERGENCY LIGHT SYSTEM, FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 18 LT WAS INOPERATIVE. REMOVED AND RE
- [SDR AWXA200400850](https://openairdocs.org/sdr/AWXA200400850), Aug 4, 2004: WIRE. LOOSE. DURING 4-DAY CHECK THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 23 LT WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED A LOOSE WIRE AT SPLICE SEAT ROW 23 LT, OPERATIO
- [SDR AWXA200400812](https://openairdocs.org/sdr/AWXA200400812), Jul 25, 2004: WIRE. BROKEN. PHX - EEL - DURING 4-DAY CHECK EMERGENCY ESCAPE PATH LIGHT WAS FOUND INOPERATIVE AT SEAT ROW 16 LT. MAINTENANCE REPAIRED A BROKEN WIRE FOR EMERGENCY ESCAPE PATH
- [SDR AWXA200400535](https://openairdocs.org/sdr/AWXA200400535), May 18, 2004: LIGHT. INOPERATIVE. DEN - EEL - DURING 8-DAY CHECK FOUND THE EMERGENCY EXIT LIGHT JUST FORWARD OF THE L-2 DOOR IN THE LT AFT GALLEY INOPERATIVE. MAINTENANCE REMOVED AND REPLACED TH
- [SDR AWXA200400260](https://openairdocs.org/sdr/AWXA200400260), Mar 10, 2004: WIRE. BROKEN. PHX - EEL - DURING 4-DAY CHECK FOUND EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 15 LT INOPERATIVE. MAINTENANCE REPAIRED A BROKEN SPLICE ON EMERGENCY ESCAPE PATH LI
- [SDR AWXA200400198](https://openairdocs.org/sdr/AWXA200400198), Feb 15, 2004: CONNECTOR. LOOSE. PHX - EMERGENCY LANDING - FLT 0769 - ON APPROACH INTO PHX EN ROUTE FROM MZT TRAILING EDGE FLAPS WENT ASYMMETRIC BETWEEN FLAP POSITION 1 & 2. ABORTED APPROACH AN
- [SDR AWXA200400169](https://openairdocs.org/sdr/AWXA200400169), Feb 10, 2004: BATTERY. DISCHARGED. LAS - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED CABIN EMERGENCY FLASHLIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY FLASHLIGHT BATTERIES, OPERAT
- [SDR AWXA200400144](https://openairdocs.org/sdr/AWXA200400144), Feb 4, 2004: WIRE. BROKEN. PHX - EEL - FLIGHT CREW REPORTED ELECTRICAL WIRE FOR EMERGENCY LIGHTING BROKEN IN AFT GALLEY AT LT TRASH BIN COMPARTMENT. MAINTENANCE REPAIRED BROKEN WIRE FOR E
- [SDR AWXA200400137](https://openairdocs.org/sdr/AWXA200400137), Jan 30, 2004: SKIN. CRACKED. PHX - MAJOR REPAIR - DURING 8-DAY CHECK A 3 INCH CRACK WAS FOUND IN FUSELAGE SKIN JUST AFT OF WING TO BODY FAIRING BETWEEN BS 727D AND 727 E, AT STR 23 LT. MAIN
- [SDR AWXA200400043](https://openairdocs.org/sdr/AWXA200400043), Jan 7, 2004: SUPPORT. CORRODED. MCN - MAJOR REPAIR - DURING C-18 CHECK INTERGRANULAR CORROSION WAS FOUND ON LT INBOARD MIDFLAP, INBOARD SPINDLE, OUTER BEARING SUPPORT. MAINTENANCE REMOVED AND 
- [SDR AWXA200400042](https://openairdocs.org/sdr/AWXA200400042), Jan 7, 2004: SUPPORT. CORRODED. MCN - MAJOR REPAIR - DURING C-18 CHECK INTERGRANULAR CORROSION WAS FOUND ON RT INBOARD FLAP, INBOARD SPINDLE, OUTER BEARING SUPPORT. MAINTENANCE REMOVED AND REP
- [SDR AWXA200400023](https://openairdocs.org/sdr/AWXA200400023), Jan 4, 2004: SPAR. DELAMINATED. MCN - MINOR REPAIR - DURING C-18 CHECK THE RT AILERON FORWARD SPAR LOWER FLANGE WAS FOUND DELAMINATED AT ACCESS PANEL ATTACHMENT WS 430. MAINTENANCE TRIMMED OUT
- [SDR AWXA200400008](https://openairdocs.org/sdr/AWXA200400008), Dec 21, 2003: ANGLE. CRACKED. MCN - MINOR REPAIR - DURING C-18 CHECK A .5 INCH CRACK WAS FOUND ON LT AIR CONDITIONING BAY FORWARD OUTBOARD DUCT SUPPORT (TEE ANGLE) BS 530, LBL 58, WL 156. MA
- [SDR AWXA200400009](https://openairdocs.org/sdr/AWXA200400009), Dec 19, 2003: CLIP. CRACKED. MCN - MINOR REPAIR - DURING C-18 CHECK A .5 INCH CRACK WAS FOUND ON LT AIR CONDITIONING BAY FORWARD DUCT SUPPORT CLIP AT BS 530, LBL 56, WL 158. MAINTENANCE REM
- [SDR AWXA200301540](https://openairdocs.org/sdr/AWXA200301540), Dec 9, 2003: BRACKET. CRACKED. DURING C-18 CHECK A .375 INCH CRACK WAS FOUND IN BRACKET FOR JUNCTION BOX J10 AT BS 380. MAINTENANCE REMOVED BRACKET FOR JUNCTION BOX J10 AT BS 380; FABRICATED 
- [SDR AWXA200301605](https://openairdocs.org/sdr/AWXA200301605), Dec 8, 2003: FLOORBEAM. CRACKED. MCN - MAJOR REPAIR - DURING C-18 CHECK A 1 INCH CRACK WAS FOUND AT RT CENTER FLOORBEAM T-CAP ANGLE BS 540, BL-0. MAINTENANCE REMOVED CRACKED T-CAP ANGLE AT BS 5
- [SDR AWXA200301598](https://openairdocs.org/sdr/AWXA200301598), Dec 8, 2003: FLOORBEAM. DEBONDED. MCN - MAJOR REPAIR - DURING C-18 CHECK THE CENTER LT FLOORBEAM T-CAP ANGLE WAS DISBONDED AT BS 540, LBL 22. MAINTENANCE REMOVED CRACKED T-CAP ANGLE AT BS 540, L
- [SDR AWXA200301579](https://openairdocs.org/sdr/AWXA200301579), Dec 8, 2003: INTERCOSTAL. CRACKED. MCN - MAJOR REPAIR - DURING C-18 CHECK A .25 INCH CRACK WAS FOUND ON L-1 DOOR FORWARD INTERCOSTAL AT BS 294.5, STR 12 LT. MAINTENANCE REMOVED CRACKED INTERCOSTA
- [SDR AWXA200301595](https://openairdocs.org/sdr/AWXA200301595), Dec 6, 2003: STRINGER. CRACKED. MCN - MAJOR REPAIR - DURING C-18 CHECK A 1 INCH CRACK WAS FOUND ON STRINGER 16 LT AT LIGHT ASSEMBLY BS 500C. MAINTENANCE TRIMMED OUT CRACK ON STRINGER 16 LT AT 
- [SDR AWXA200301586](https://openairdocs.org/sdr/AWXA200301586), Dec 6, 2003: STRINGER. CRACKED. MCN - MAJOR REPAIR - DURING C-18 CHECK A .2500 INCH CRACK WAS FOUND ON STRINGER 16 RT AT LIGHT ASSEMBLY BS 500C. MAINTENANCE REMOVED DAMAGE FROM END OF STRINGER
- [SDR AWXA200301542](https://openairdocs.org/sdr/AWXA200301542), Dec 6, 2003: STRINGER CLIP. CRACKED. DURING C-18 CHECK A .25 INCH CRACK WAS FOUND IN STRINGER CLIP BS 520, STR 14 LT. MAINTENANCE REMOVED CRACKED STRINGER CLIP AT BS 520, STR 14 LT; RECEIVED A NEW 
- [SDR AWXA200400058](https://openairdocs.org/sdr/AWXA200400058), Dec 5, 2003: WEDGE. DELAMINATED. MCN - MAJOR REPAIR - DURING C-18 CHECK FOUND THE NR 3 SLAT OUTBOARD END UPPER WEDGE SKIN DELAMINATED. MAINTENANCE CUT OUT DELAMINATED AREA NR 3 SLAT OUTBOARD EN
- [SDR AWXA200400004](https://openairdocs.org/sdr/AWXA200400004), Dec 5, 2003: FLOORBEAM. CORRODED. MCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOORBEAM AT FASTENER HOLE BS 344, RBL 7. MAINTENANCE REMOVED DAMAGED SECTION OF FLOOR
- [SDR AWXA200301592](https://openairdocs.org/sdr/AWXA200301592), Dec 5, 2003: SKIN. DELAMINATED. DURING C-18 CHECK THE NR 1 SLAT TRAILING EDGE WEDGE UPPER SKIN WAS FOUND DELAMINATED AT OUTBOARD MAIN TRACK. MAINTENANCE REMOVED DAMAGED NR 1 SLAT TRAILING EDGE
- [SDR AWXA200301591](https://openairdocs.org/sdr/AWXA200301591), Dec 5, 2003: SKIN. DELAMINATED. DURING C-18 CHECK THE NR 1 SLAT TRAILING EDGE UPPER SKIN WAS FOUND DELAMINATED AT OUTBOARD AUXILIARY TRACK. MAINTENANCE REMOVED DAMAGED NR 1 SLAT TRAILING EDGE 
- [SDR AWXA200301589](https://openairdocs.org/sdr/AWXA200301589), Dec 5, 2003: WEDGE. DELAMINATED. DURING C-18 CHECK THE NR 5 SLAT OB END UPPER WEDGE TRAILING EDGE SKIN WAS FOUND DELAMINATED AROUND PREVIOUS REPAIR. MAINTENANCE REMOVED PREVIOUS REPAIR AND DELA

All 173: https://openairdocs.org/deregistered/N174AW-2006-07-31/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 19970107011209I](https://openairdocs.org/incident/19970107011209I), Jan 7, 1997: Boeing 73733A (N174AW), Salt Lake City, UT, Minor damage. Narrative: a/c returned to slc with smoke in the cockpit. It was later learned that there was no smoke in the cockpit, but just the smell of a bird that the…
- [Incident 19891108057609I](https://openairdocs.org/incident/19891108057609I), Nov 8, 1989: Boeing 73733A (N174AW), Burbank, CA. Smoke from right gear after landing. Deplaned on ramp. Found leaking brake line.

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