# N118RW: 1983 Boeing 737-2Y5, registration cancelled 2004-05-11 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: May 11, 2004 - Exported to: Honduras - Status when cancelled: Valid registration - Airframe: [Boeing 737-2Y5](https://openairdocs.org/model/boeing-737-2y5) (registry code 1384554) - Engine: [Pratt & Whitney JT8D-15](https://openairdocs.org/engine/pratt-whitney-jt8d-15) (registry code 52051) - Data sheets: [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs) - Serial number: 23040 - Year built: 1983 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: February 21, 1998 - Certificate issued: November 20, 2003 - Last registry action: November 20, 2003 - Mode S code: A04B77 - Owner when cancelled: [Wells Fargo Bank Northwest Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20BANK%20NORTHWEST%20NA%20TRUSTEE) - Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City) - Owner type: Corporation - Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N118RW - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=118RW - Page: https://openairdocs.org/deregistered/N118RW-2004-05-11 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 737-2Y5: https://openairdocs.org/model/boeing-737-2y5.md ## Service difficulty reports (103, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR FL3A200200389](https://openairdocs.org/sdr/FL3A200200389), Nov 16, 2002: CHECK VALVE. INOPERATIVE. DURING CLIMB OUT, THE FLIGHT CREW NOTED AN ILLUMINATED WING/BODY OVERHEAT LIGHT WHICH WOULD NOT EXTINGUISH WHEN QUICK REFERENCE HANDBOOK ITEMS WERE ACCOMPLISHED - [SDR F3LA200200385](https://openairdocs.org/sdr/F3LA200200385), Nov 6, 2002: HYDRAULIC LINE. DAMAGED. DURING FLIGHT, A SYSTEM HYDRAULIC QUANTITY DROPPED TO ZERO FOLLOWED BY THE FAILURE OF THE NUMBER 2 ENGINE, ENGINE DRIVEN HYDRAULIC PUMP. A SYSTEM PRESSURE REMIA - [SDR F3LA200200265](https://openairdocs.org/sdr/F3LA200200265), Sep 25, 2002: A/C PACK. MALFUNCTIONED. AIR TURN BACK. FLIGHT CREW REPORTED SMOKE IN CABIN, LT WING/BODY OVERHEAT ILLUMINATED AND RT PACK TRIPPED OFF. DECLARED AN EMERGENCY AND RETURNED TO DEN. AIRCRA - [SDR F3LA200200258](https://openairdocs.org/sdr/F3LA200200258), Sep 10, 2002: ODOR. DETECTED. AIR TURNBACK. FLIGHT CREW REPORTED FWD LAVATORY SMOKE ALARM ACTIVATED WHILE CLIMBING THROUGH 8000 FT. PASSENGERS IN ROW 2 NOTED DISTINCT SMELL/ODOR OR SMOKE (OV - [SDR F3LA200200201](https://openairdocs.org/sdr/F3LA200200201), Jul 26, 2002: OVERHEAT LOOP. OUT OF POSITION. DURING CLIMBOUT, THE FLIGHT CREW DISCOVERED A WIND/BODY OVERHEAT LIGHT ON. QRH ITEMS ACCOMPLISHED AND LIGHT EXTINGUISHED. AIR TURNBACK ACCOMPLISHED. UPON INSPEC - [SDR F3LA200200152](https://openairdocs.org/sdr/F3LA200200152), May 21, 2002: FIRE DETECTOR. FALSE ACTIVATION. UPON ARRIVAL AT GATE, FLIGHT CREW REPORTED THE FIRE BELL SOUNDED AND THE NR 1 ENGINE FIRE HANDLE WAS ILLUMINATED. PULLED NR 1 FIRE HANDLE AND DISCHARGED THE LEF - [SDR F3LA200200103](https://openairdocs.org/sdr/F3LA200200103), Feb 28, 2002: COWLING. CRACKED. DURING C-3 CHECK, INSPECTION REPORTED CRACK ON AFT LOWER CORNER OF NR 2 ENGINE OUTBOARD FIXED COWL NEXT TO FIRE SEAL. FABRICATED AND INSTALLED REPAIR PER SRM 51 - [SDR F3LA200200102](https://openairdocs.org/sdr/F3LA200200102), Feb 28, 2002: WEB. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED AFT LAVATORY FLOOR WEB CORRODED, STA 1016, AT DRAIN TO LBL 30. - [SDR F3LA200200101](https://openairdocs.org/sdr/F3LA200200101), Feb 28, 2002: ATTACH ANGLE. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON SIDEWALL PANEL ATTACH ANGLE AT STA 727, LBL 21 TO LBL 25. - [SDR F3LA200200100](https://openairdocs.org/sdr/F3LA200200100), Feb 28, 2002: ATTACH ANGLE. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON SIDEWALL ATTACH ANGLE AT STA 947.5, STR 21R TO 24R. FABRICATED AND INSTALLED REPLACEMENT ANGLE PER BOEING DRA - [SDR F3LA200200098](https://openairdocs.org/sdr/F3LA200200098), Feb 28, 2002: CLIP. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON CLIP AT FWD FRAME, STA 360. FABRICATED AND INSTALLED CHANNEL TIE PER SRM 51-20-01 AND 51-30-2. - [SDR F3LA200200097](https://openairdocs.org/sdr/F3LA200200097), Feb 28, 2002: WEB. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED VERTICAL WEB CORRODED FROM STA 352 TO STA 360. FABRICATED AND INSTALLED REPLACEMENT WEB PER SRM 51-20-01 AND 51-30-2. - [SDR F3LA200200096](https://openairdocs.org/sdr/F3LA200200096), Feb 28, 2002: STIFFENER. CRACKED. DURING C-3 CHECK, INSPECTION REPORTED STIFFENER ANGLE CRACKED AT STA 298 - STA 304. FABRICATED AND INSTALLED REPLACEMENT CLIP PER SRM 51-10-2 AND 51-30-2. - [SDR F3LA200200095](https://openairdocs.org/sdr/F3LA200200095), Feb 28, 2002: THRESHOLD. CRACKED. DURING C-3 CHECK, INSPECTION REPORTED CRACK IN RADIUS UPPER SURFACE 28 INCHES FWD OF AFT EDGE OF WEB THRESHOLD C-2 DOOR AT STR 25-R, STA 794-847. REMOVED DAMAGE - [SDR F3LA200200094](https://openairdocs.org/sdr/F3LA200200094), Feb 28, 2002: PANEL. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED CORROSION AT SCREW HOLES ON TRANSITION PANEL AT STA 500-520. FABRICATED AND INSTALLED REPLACEMENT TRANSITION PANEL PER SRM - [SDR F3LA200200093](https://openairdocs.org/sdr/F3LA200200093), Feb 28, 2002: WEB. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON WEB AT STA 797 BETWEEN STR 22-R AND 24-R. REPLACED WEB PER SRM 51-30-2 AND 51-10-1. - [SDR F3LA200200092](https://openairdocs.org/sdr/F3LA200200092), Feb 27, 2002: SKIN. CRACKED. DURING C-3 CHECK, INSPECTION REPORTED L2 DOOR CUTOUT CRACKED AT FWD LOWER CORNER OUTER SKIN APPROXIMATELY 1 INCH FROM RIVET TO DOOR CORNER. REPAIRED DAMAGE PER - [SDR F3LA200200091](https://openairdocs.org/sdr/F3LA200200091), Feb 27, 2002: SKIN PANEL. DAMAGED. DURING C-3 CHECK, INSPECTION REPORTED MISSED DRILLED RIVET HOLE IN FWD LT. CORNER OF AFT E&E DOOR CUTOUT AT STA. 326. FABRICATED DOUBLER, TRIPLER AND FILLER PER - [SDR F3LA200200090](https://openairdocs.org/sdr/F3LA200200090), Feb 27, 2002: COWLING. DAMAGED. DURING C-3 CHECK, INSPECTION REPORTED NR 1 ENGINE LT OUTBOARD COWL TOP EDGE DAMAGED BETWEEN SECOND AND LAST HINGE. REMOVED DAMAGE PER SRM 51-40-3. FABRICATED AN - [SDR F3LA200200089](https://openairdocs.org/sdr/F3LA200200089), Feb 27, 2002: MOUNT BRACKET. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED LT WING REAR SPAR MOUNT TEE FOR NR 4 SPOILER OUTBOARD ACTUATOR MOUNT BRACKET CORRODED. REPLACED BRACKET AND BUSHING PER SR - [SDR F3LA200200088](https://openairdocs.org/sdr/F3LA200200088), Feb 27, 2002: BEAM. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED BEAM IN FWD BULKHEAD, AFT CARGO COMPARTMENT, CORRODED AT NUT PLATE ATTACHMENT POINT FOR LOWER DUCT SHROUD BRACKETS AT LBL - [SDR F3LA200200087](https://openairdocs.org/sdr/F3LA200200087), Feb 27, 2002: ANGLE. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON AFT CARGO COMPARTMENT PANEL ATTACH ANGLE AT STA. 727, RBL 21 TO RBL 25. FABRICATED AND INSTALLED REPLACEMENT - [SDR F3LA200200079](https://openairdocs.org/sdr/F3LA200200079), Feb 24, 2002: BELTFRAME. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON BELT FRAME AT STA 827, RBL 10. REMOVED DAMAGE, FABRICATED AND INSTALLED PER SRM 53-10-4. - [SDR F3LA200200078](https://openairdocs.org/sdr/F3LA200200078), Feb 24, 2002: FRAME. CRACKED. DURING C-3 CHECK, INSPECTION REPORTED FRAME AT STA 82.7, RBL 10, CRACKED AT SHEAR TIE ATTACH FASTENERS IN AFT CARGO COMPARTMENT. REMOVED DAMAGE, FABRICATED AND - [SDR F3LA200200076](https://openairdocs.org/sdr/F3LA200200076), Feb 23, 2002: STIFFENER. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED CORROSION IN NUT PLATE HOLE AT STA 727, RBL 12, VERTICAL STIFFENER. CUT OUT DAMAGED AREA, FABRICATED REPLACEMENT PARTS AND - [SDR F3LA200200075](https://openairdocs.org/sdr/F3LA200200075), Feb 23, 2002: FLOORBEAM. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED FLOORBEAM AT STA 967 CORRODED. FABRICATED AND INSTALLED REPLACEMENT FLOORBEAM CAP PER SRM 51-30-2. - [SDR F3LA200200074](https://openairdocs.org/sdr/F3LA200200074), Feb 23, 2002: FLOOR PANEL. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED CORROSION AROUND EDGES OF AFT FLOOR PANEL IN FWD CARGO COMPARTMENT. REMOVED CORROSION AROUND EDGES OF AFT FLOOR PANEL PER - [SDR F3LA200200073](https://openairdocs.org/sdr/F3LA200200073), Feb 23, 2002: STRAP. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED AFT LAVATORY FLOOR WEB STRAP CORRODED AT STA 1006 TO STA 1016. FABRICATED AND INSTALLED REPLACEMENT WEB STRAP PER SRM 51-3 - [SDR F3LA200200071](https://openairdocs.org/sdr/F3LA200200071), Feb 23, 2002: FLOOR SUPPORT. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED FLOOR SUPPORT AT STA 957, LBL 16 TO LBL 42, CORRODED. FABRICATED AND INSTALLED REPLACEMENT FLOOR SUPPORT PER SRM 53-10-2 A - [SDR F3LA200200072](https://openairdocs.org/sdr/F3LA200200072), Feb 23, 2002: FRAME. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON CHORD AT STA 352, STR 28L. REPLACED DAMAGED CHORD PER SRM 51-10-2 AND SRM 51-30-2. - [SDR F3LA200200070](https://openairdocs.org/sdr/F3LA200200070), Feb 23, 2002: PANEL. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON CLOSING PANEL AROUND NUT PLATES AT STA 789, RBL 39 TO RBL 46. REPLACED CLOSING PANEL PER SRM 51-10-1. - [SDR F3LA200200069](https://openairdocs.org/sdr/F3LA200200069), Feb 23, 2002: PANEL. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON CLOSING PANEL AROUND NUT PLATE AT STA 789, RBL 27 TO RBL 34. REPLACED CLOSING PANEL PER SRM 51-10-1. - [SDR F3LA200200068](https://openairdocs.org/sdr/F3LA200200068), Feb 23, 2002: FLOORBEAM. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED TOP SURFACE OF FLOORBEAM AT STA 986 CORRODED. REPLACED FLOORBEAM CAP PER SRM 53-10-9. - [SDR F3LA200200067](https://openairdocs.org/sdr/F3LA200200067), Feb 23, 2002: INTERCOSTAL. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED INTERCOSTAL AT STA 986 TO STA 1006, RBL 3, CORRODED. FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL PER SRM 51-30-2 AND - [SDR F3LA200200066](https://openairdocs.org/sdr/F3LA200200066), Feb 23, 2002: WEB. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED WEB AT STA 996 TO STA 1016, RBL 40, NEXT TO R2 DOOR CORRODED. FABRICATED AND INSTALLED REPLACEMENT WEB PER SRM 51-30-2. - [SDR F3LA200200065](https://openairdocs.org/sdr/F3LA200200065), Feb 23, 2002: STRAP. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED STRAP ALONG THE BOTTOM OF PRODUCTION BREAK AT STA 1016, STR 23-L TO 23-R CORRODED. REPLACED STRAP PER SRM 51-30-2 AND BOEI - [SDR F3LA200200064](https://openairdocs.org/sdr/F3LA200200064), Feb 23, 2002: SKIN. CRACKED. DURING C-3 CHECK, INSPECTION REPORTED FUSELAGE SKIN RUBBED BY BELT 2 INCHES BELOW L-1 DOOR TOP SPIGOT (INTERIOR). PERFORMED EDDY CURRENT INSPECTION OF L-1 DOOR - [SDR F3LA200200063](https://openairdocs.org/sdr/F3LA200200063), Feb 22, 2002: FLOORBEAM. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED FLOORBEAM AT STA 986 CORRODED AT BOTTOM SURFACE AT FASTENERS THROUGH FLOORBOARDS. ALSO SHOWS EVIDENCE OF CORROSION ON TOP - [SDR F3LA200200062](https://openairdocs.org/sdr/F3LA200200062), Feb 22, 2002: INTERCOSTAL. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON INTERCOSTAL AT STA 847, BL 16-R. FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL PER BOEING DRAWING 65-47957 - [SDR F3LA200200061](https://openairdocs.org/sdr/F3LA200200061), Feb 22, 2002: INTERCOSTAL. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED INTERCOSTAL AT STA 794, STR 27-R CORRODED. FABRICATED AND REPLACED INTERCOSTAL PER SRM 51-30-2 AND 51-20-1. - [SDR F3LA200200060](https://openairdocs.org/sdr/F3LA200200060), Feb 22, 2002: INTERCOSTAL. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED FLOOR INTERCOSTAL IN AFT GALLEY ENTRY CORRODED STA 957, BL 16L TO BL 42L. FABRICATED AND INSTALLED REPLACEMENT FLOOR SUPPO - [SDR F3LA200200058](https://openairdocs.org/sdr/F3LA200200058), Feb 21, 2002: INTERCOSTAL. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED FLOORBEAM INTERCOSTAL CORRODED FROM STA 1006 TO STA 1016, BL 0. FABRICATED AND REPLACED INTERCOSTAL PER SRM 53-10-2 AND 51 - [SDR F3LA200200057](https://openairdocs.org/sdr/F3LA200200057), Feb 21, 2002: FLOORBEAM. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED AFT LAVATORY TRANSVERSE BEAM CORRODED AT STA 1006 TO STA 1016, LBL 6. REPLACED TRANSVERSE FRAME PER SRM 51-30-2. - [SDR F3LA200200056](https://openairdocs.org/sdr/F3LA200200056), Feb 21, 2002: DOOR FRAME. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FWD DOOR FRAME AT STA 803, STR 24-R, CRACKED AND CORRODED. REPLACED AFT CARGO COMPARTMENT DOOR FRAME - [SDR F3LA200200055](https://openairdocs.org/sdr/F3LA200200055), Feb 21, 2002: GUSSET. WORN. DURING C-3 CHECK, INSPECTION REPORTED NR 1 ENGINE RT EXHAUST COWL INSIDE FLANGE ON BOTTOM OF THIRD RIB FROM FRONT WORN. REMOVED DAMAGED GUSSET FROM NR 1 ENGINE - [SDR F3LA00200054](https://openairdocs.org/sdr/F3LA00200054), Feb 21, 2002: FLOORBEAM. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED AFT LAVATORY TRANSVERSE FLOORBEAM CORRODED AT STA 986 TO STA 1006, LBL 10. REPLACED DAMAGED TRANSVERSE FRAME TOP CAP PER S - [SDR F3LA200200053](https://openairdocs.org/sdr/F3LA200200053), Feb 21, 2002: WEB. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED WEB AT STA 1016, STR 20-L, BEHIND L-2 DOOR. FABRICATED AND INSTALLED REPLACEMENT WEB PER SRM 51-30-2 AND BOEING DRAWING 65 - [SDR F3LA200200052](https://openairdocs.org/sdr/F3LA200200052), Feb 21, 2002: FLOORBEAM. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED AFT FLOORBEAM AT STA 967 CORRODED ON TOP SURFACE. FABRICATED AND REPLACED FLOORBEAM CAP PER SRM 51-30-2. - [SDR F3LA200200051](https://openairdocs.org/sdr/F3LA200200051), Feb 21, 2002: SUPPORT. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED AFT LAVATORY SUPPORT PARTITION FRAME CORRODED AT STA 998, 14 LBL. FABRICATED AND INSTALLED REPLACEMENT FRAME SUPPORT PER S - [SDR F3LA200200050](https://openairdocs.org/sdr/F3LA200200050), Feb 21, 2002: SKIN. CORRODED. DURING C-3 CHECK, INSPECTION REPORTED CORROSION ON AFT CARGO COMPARTMENT DOOR CUTOUT, LOWER FWD CORNER, AT STA 790. REPAIRED DAMAGED SECTION PER SRM 53-30-3. All 103: https://openairdocs.org/deregistered/N118RW-2004-05-11/reports.md ## Other aircraft with N118RW - [Registered now](https://openairdocs.org/aircraft/N118RW): Cessna 560, S/N 560-0389 --- 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.