# N951WP: 1985 Boeing 737-3B7, registration cancelled 2005-10-12 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: October 12, 2005 - Exported to: Thailand - Status when cancelled: Valid registration - Airframe: [Boeing 737-3B7](https://openairdocs.org/model/boeing-737-3b7) (registry code 138447F) - Engine: [CFM International CFM56 series](https://openairdocs.org/engine/cfm-international-cfm56-series) (registry code 13802) - Serial number: 22951 - Year built: 1985 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: November 27, 1985 - Certificate issued: August 12, 2004 - Last registry action: August 12, 2004 - Mode S code: AD3A60 - Owner when cancelled: [Afs Investments Xxvii LLC](https://openairdocs.org/faa-owner/AFS%20INVESTMENTS%20XXVII%20LLC) - Location: [Stamford, CT](https://openairdocs.org/faa-place/CT/Stamford) - Owner type: Corporation - Owner's area on the map: 41.0534° N, 73.5387° W: Placed by OpenAirDocs: center of Stamford, CT, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N951WP - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=951WP - Page: https://openairdocs.org/deregistered/N951WP-2005-10-12 From the FAA registry file of November 5, 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 737-3B7: https://openairdocs.org/model/boeing-737-3b7.md ## Service difficulty reports (67, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DL733040691](https://openairdocs.org/sdr/DL733040691), Jul 25, 2004: WIRE. SHORTED. ON DESCENT, CREW SAW SPARK AND HEARD POP COMING FROM THE WHISKEY COMPASS. COPILOT EXTENDING COMPASS AND RECEIVED SMALL SHOCK. NO FURTHER ARCING AND NO DEFECTS W - [SDR DL733030933](https://openairdocs.org/sdr/DL733030933), Oct 18, 2003: ACM. FAILED. ON CLIMBOUT FROM SLC UNABLE TO MAINTAIN PRESSURIZATION ON ONE PACK - LT PACK ON MCO FOR LOW FLOW - HISTORY ITEM. REPLACED LT ACM AND ACM DISCHARGE TEMP SW, RAN - [SDR DL733030553](https://openairdocs.org/sdr/DL733030553), Jun 17, 2003: COFFEEMAKER. LEAKING. ELEC ODOR COMING FROM FWD GALLEY COFFEEMAKER UNIT WAS TURNED OFF AND CB'S OPENED ODOR WENT AWAY. REMOVED COFFEEMAKER FOR INSPECTION FOUND WATER LEAK AT WATER SU - [SDR DL733030519](https://openairdocs.org/sdr/DL733030519), Jun 5, 2003: SKIN. CRACKED. THE FUSELAGE SKIN WAS FOUND WITH A 3 INCH CRACK AT FS 727D JUST ABOVE STRINGER 23R RUNNING ALONG THE BONDED DOUBLER EDGE. THE CRACK WAS REMOVED WITH A 4 X 1 INC - [SDR DL733030275](https://openairdocs.org/sdr/DL733030275), Mar 24, 2003: LIGHT. DAMAGED. FOUND CABIN EMERGENCY EXIT LIGHT INOP AT SEAT 24DEF. REPLACED WIRE CONNECTORS AT LIGHT ASSY. OPS CHECKS NORMAL. - [SDR DL733030266](https://openairdocs.org/sdr/DL733030266), Mar 22, 2003: PROXIMITY SENSOR. MALFUNCTIONED. NR 2 T/R LIGHT ILLUMINATED CLIMBING THROUGH 12,000 FT. RETURN TO SLC QRH PROCEDURES COMPLIED WITH. REVERSER LIGHT ON OVERHEAD PANEL. ATB. CLEANED SIX PROXIMITY - [SDR DL733030030](https://openairdocs.org/sdr/DL733030030), Jan 6, 2003: ROD BOLT. MISSING. L1 DOOR WOULD NOT OPEN FROM EITHER INSIDE OR OUTSIDE. FOUND LOWER LATCH AND GATE CONTROL ROD BOLT MISSING. INSTALLED CONTROL ROD BOLT. RE- INSTALLED TRIM AND SL - [SDR DL733021199](https://openairdocs.org/sdr/DL733021199), Oct 14, 2002: SPAR. CRACKED. INSPECTION OF THE MLG BEAM ATTACH FITTINGS AND REAR SPAR ON THE LT WING REVEALED 6 HOLES COMMON TO THE FITTINGS AND SPAR WITH CRACK INDICATIONS. ADDITIONAL HOLE - [SDR DL733020193](https://openairdocs.org/sdr/DL733020193), Feb 15, 2002: FAN. MALFUNCTIONED. WHILE SITTING AT GATE NOTICED SMOKE/SMELL IN AFT CABIN. GROUND PERSONNEL STATED SMOKE CAME FROM EQUIP COOLING FAN EXHAUST. MTC INSPECTED ALL AREAS WHERE EQUIP C - [SDR DL733010396](https://openairdocs.org/sdr/DL733010396), Mar 11, 2001: SENSOR. FAILED. IR - AIRCRAFT WOULD NOT PRESSURIZE AFTER TAKEOFF. CABIN CLIMBED AT 1500-2000 FPM. OUTFLOW VLV SHOWED FULL CLOSED AND STBY MODE NO CHANGE. CABIN PRESSURE STABILI - [SDR DL733002318](https://openairdocs.org/sdr/DL733002318), Nov 28, 2000: SKIN. CRACKED. FUSELAGE / SKIN / AFT GALLEY DOOR CUTOUT / LWR HINGE CUTOUT:CRACK REPAIR. THE LOWER HINGE CUTOUT OF THE AFT GALLEY DOOR OPENING SURROUND SKIN WAS FOUND WITH A T - [SDR DL733002037](https://openairdocs.org/sdr/DL733002037), Oct 16, 2000: FITTING. CRACKED. INSPECTION OF THE RT WING MLG BEAM OUTBOARD ATTACH FITTING REVEALED A CRACK EMANATING FROM A FASTENER HOLE COMMON TO THE REAR SPAR UPPER CHORD. INSPECTION OF TH - [SDR DL733002036](https://openairdocs.org/sdr/DL733002036), Oct 16, 2000: FITTING. CRACKED. THE MLG BEAM OUTBOARD AFT ATTACH FITTING WAS FOUND WITH A TYPICAL CRACK EMANATING FROM AN ATTACHMENT HOLE COMMON TO THE REAR SPAR UPPER CHORD. BOLT HOLE HFEC IN - [SDR DL733001255](https://openairdocs.org/sdr/DL733001255), Jul 3, 2000: SLIDE. DISLODGED. 1R DOOR ESCAPE SLIDE ON FLOOR. SLIDE PARTILLY DEPLOYED UPON REMOVAL. RPLD DOOR SLIDE. - [SDR DL733000854](https://openairdocs.org/sdr/DL733000854), Apr 28, 2000: ENGINE. OVERTEMP. JUST AFTER ROTATION, NR 1 EGT 970 DEG WITH WARNING HORN FOR APPROX 10 SECONDS. REPLACED NR 1 ENG PER ROUTINE CARD DECK. - [SDR DL733982622](https://openairdocs.org/sdr/DL733982622), Dec 24, 1998: ANTI ICE VALVE. FAILED. RIGHT ENGINE ANTI-ICE FAILED CLOSED POSITION. AIR TURN BACK. REPLACED ANTI-ICE VALVE. - [SDR DL733981597](https://openairdocs.org/sdr/DL733981597), Aug 3, 1998: SKIN. CRACKED. R1 DOOR CUTOUT SKIN CRACKED AT AFT LWR CORNER. INSTALLED REPAIR PER SRM 53-10-01 FIG 202. - [SDR DL733981588](https://openairdocs.org/sdr/DL733981588), Aug 1, 1998: SKIN. GOUGED. REPAIRED GOUGE ON FUSELAGE SKIN AT STA 400 BELOW STRINGER 19 LEFT PER SRM 53-00-01 FIG 210. - [SDR W8PA980021](https://openairdocs.org/sdr/W8PA980021), Jan 21, 1998: LAMP. FAILED. DEN - AFT CABIN OVERHEAD EMERGENCY EXIT LIGHT IS INOP. REPLACED LAMP, OPS CHECK GOOD. - [SDR W8PA980026](https://openairdocs.org/sdr/W8PA980026), Jan 19, 1998: CONNECTOR. DISCONNECTED. DEN - EMERGENCY TRACK LIGHT INOP AT ROW 15. RECONNECTED EMERGENCY LIGHT. OPS CHECK GOOD. - [SDR W8PA980004](https://openairdocs.org/sdr/W8PA980004), Jan 7, 1998: REFLECTOR. INOPERATIVE. DEN- R2 DOOR EXTERIOR EMERGENCY LIGHT IS INOP. REPLACED R2 DOOR EMERGENCY LIGHT REFLECTOR ASSY, OPS CHECK GOOD. - [SDR W8PA980005](https://openairdocs.org/sdr/W8PA980005), Jan 6, 1998: BULB. FAILED. DEN- OVERHEAD EMERGENCY LIGHT AT ROW 23 IS INOP. REPLACED BULB, OPS CHECK GOOD. - [SDR W8PA971549](https://openairdocs.org/sdr/W8PA971549), Dec 21, 1997: BULB. FAILED. DEN- THRESHOLD LIGHT AT L1 DOOR IS INOP. REPLACED BULB, OPS CHECK GOOD. - [SDR W8PA971502](https://openairdocs.org/sdr/W8PA971502), Oct 24, 1997: BULB. FAILED. DEN- EMERGENCY LIGHT AT ROW 18 IS INOP. RELAMPED EMERGENCY LIGHT AT ROW 18, OPS CHECK NORMAL. - [SDR W8PA971430](https://openairdocs.org/sdr/W8PA971430), Sep 12, 1997: WIRE. FAILED. AFTER TAXI FROM HANGAR TO THE GATE, THE APU TEMP GAUGE BACKROUND LIGHT WAS FLICKERING AND THERE WAS THE SMELL OF SMOKE IN THE COCKPIT. FOUND SEVERAL WIRES CHAFE - [SDR W8PA971347](https://openairdocs.org/sdr/W8PA971347), Jul 23, 1997: BULB. FAILED. BULLNOSE EMERGENCY EXIT LIGHT AT ROW 23 IS INOPERABLE. RELAMPED AS REQUIRED. OPS CHECK GOOD. (X) - [SDR W8PA971166](https://openairdocs.org/sdr/W8PA971166), Jun 20, 1997: LIGHT. LOOSE. AISLE TRACK LIGHT CAME LOOSE FROM FLOOR ON RIGHT SIDE OF AIRCRAFT. RESECURED TRACK LIGHTING. (X) - [SDR W8PA971163](https://openairdocs.org/sdr/W8PA971163), Jun 11, 1997: CYLINDER. CORRODED. RIGHT MLG OUTER CYLINDER TRUNNION LUG CORRODED AND CHROME PLATING CHIPPING AWAY ON THE FWD TRUNNION LUGS. REPLACED THE RT MLG OUTER CYLINDER. (M) - [SDR W8PA971165](https://openairdocs.org/sdr/W8PA971165), Jun 10, 1997: SKIN. DELAMINATED. LEFT INBOARD FORE FLAP HAS A SMALL DISBOND ON LOWER SKIN IN CENTER OF FLAP. REMOVED DAMAGED AREA, FABRICATED REPAIR AND INSTALLED PER SRM 51-70-10. (M) - [SDR W8PA971156](https://openairdocs.org/sdr/W8PA971156), Jun 4, 1997: SUPPORT. CORRODED. CORROSION ON STATION 986-1006, WL 208, LBL 38, AND STATION 1006-1016, LBL 38, WL 208 IN ANGLES. ORIGINAL THICKNESS 1. REMOVED CORRODED PARTS, INSTALLED NEW PART - [SDR W8PA971161](https://openairdocs.org/sdr/W8PA971161), May 29, 1997: FLOORBEAM. CRACKED. FOUND CRACK THROUGH NUT PLATE HOLES ON FLOORBEAM BS 947, LBL 60, WL 208. REPAIRED FLOORBEAM PER SRM 53-60-51, 51-20-01, AND MM 51-21-21. (M) - [SDR W8PA970679](https://openairdocs.org/sdr/W8PA970679), May 26, 1997: SUPPORT. CORRODED. CORROSION ON FLOOR SUPPORT BS 312 - BS 328, RBL 11, WL 208. ORIGINAL THICKNESS .080 INCH. FOUND TO BE OUT OF LIMITS PER SRM 53-10-51. REMOVED AND REPLACED STIFF - [SDR W8PA970678](https://openairdocs.org/sdr/W8PA970678), May 26, 1997: FLOOR SUPPORT. CORRODED. CORROSION ON FLOOR SUPPORT BS 328 - BS 344, RBL 11, WL 208. ORIGINAL THICKNESS .080 INCH. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED FLO - [SDR W8PA970733](https://openairdocs.org/sdr/W8PA970733), May 24, 1997: 'A' FRAME. CRACKED. NR 7 FLAP TRACK CANOE FAIRING A-FRAME IS CRACKED. REMOVED AND REPLACED CRACKED 'A' FRAME PER SRM 51-10-02. (M) - [SDR W8PA971164](https://openairdocs.org/sdr/W8PA971164), May 22, 1997: SKIN. DELAMINATED. DISBOND. REMOVED DAMAGED SKIN AND REPAIRED PER SRM 51-70-00, STEP 4. (M) - [SDR W8PA971155](https://openairdocs.org/sdr/W8PA971155), May 22, 1997: GROMMETS. WORN. WORN GROMMETS ON FLOORBEAM. REPLACED GROMMETS PER MM 20-10-41. (M) - [SDR W8PA971153](https://openairdocs.org/sdr/W8PA971153), May 22, 1997: SUPPORT. DOUBLE HOLE. DOUBLE HOLE ON FLOOR SUPPORT BS 340. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-40-02. (M) - [SDR W8PA971152](https://openairdocs.org/sdr/W8PA971152), May 22, 1997: SUPPORT. MISDRILLED. DOUBLE HOLE ON FLOOR SUPPORT. REPAIRED PER EWO 97-0537. (M) - [SDR W8PA971142](https://openairdocs.org/sdr/W8PA971142), May 22, 1997: MOPSILL. CORRODED. CORROSION ON AFT SERVICE DOOR MOPSILL BS 954-993, WL 208, RBL 53. ORIGINAL .071, REMOVED CORROSION FOUND TO BE OUT OF LIMITS PR 53-60-15. REMOVED AND REPLACED M - [SDR W8PA970720](https://openairdocs.org/sdr/W8PA970720), May 22, 1997: SEAT TRACK. DAMAGED. MECHANICAL DAMAGE ON SEAT TRACK. REPAIRED PER SRM 53-00-52. (M) - [SDR W8PA970709](https://openairdocs.org/sdr/W8PA970709), May 22, 1997: SEAT TRACK. DAMAGED. MECHANICAL DAMAGE ON SEAT TRACK. BLENDED DAMAGE, FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED SEAT TRACK PER SRM 53-00-52, 51-40-02, 51-20-01. (M) - [SDR W8PA970700](https://openairdocs.org/sdr/W8PA970700), May 22, 1997: SEAT TRACK. DAMAGED. MECHANICAL DAMAGE ON SEAT TRACK, MARKED BETWEEN BS 540 AND BS 727 + 7 INCHES, RBL 45, WL 208. REMOVED AND REPLACED SEAT TRACK FROM BS 540 TO BS 727 + 7 INCHES, - [SDR W8PA970688](https://openairdocs.org/sdr/W8PA970688), May 22, 1997: SEAT TRACK. DAMAGED. MECHANICAL DAMAGE ON SEAT TRACK AT BS 328 - BS 480, RBL 24, WL 208. REPAIRED PER SRM 53-00-52. (X) - [SDR W8PA970676](https://openairdocs.org/sdr/W8PA970676), May 22, 1997: SEAT TRACK. DAMAGED. MECHANICAL DAMAGE ON SEAT TRACK. ORIGINAL THICKNESS .160 INCH. REMOVED AND REPLACED SEAT TRACK PER SRM 53-00-52. (X) - [SDR W8PA970628](https://openairdocs.org/sdr/W8PA970628), May 22, 1997: FRAME. GOUGED. GOUGES IN FRAME AT FASTENER HOLE BS 400, RBL 57, WL 175. REPAIRED PER SRM 51-70-11. (X) - [SDR W8PA970613](https://openairdocs.org/sdr/W8PA970613), May 22, 1997: FRAME. CRACKED. CRACK IN FRAME INNER CHORD BS 616, RBL 665, WL 201. CRACK WAS REPAIRED PER SB 737-53-1182. (X) - [SDR W8PA970604](https://openairdocs.org/sdr/W8PA970604), May 22, 1997: FLOOR BEAM. CORRODED. CORROSION ON FLOOR BEAM BS 328, LBL 50 - RBL 47, WL 208. ORIGINAL THICKNESS .080 INCH. FOUND BS 328, LBL 49 - LBL 51, WL 208 TO BE OUT OF LIMITS. REMOVED AND RE - [SDR W8PA970602](https://openairdocs.org/sdr/W8PA970602), May 22, 1997: WEB. CRACKED. CRACKED WEB AT BS 1016, LBL 38, WL 208. REMOVED DAMAGED WEB, FABRICATED NEW PART, AND INSTALLED PER SRM'S 51-40-02-BS, 51-20-01, AND 51-30-01, AND MM 51-21-99. - [SDR W8PA970600](https://openairdocs.org/sdr/W8PA970600), May 22, 1997: WEB. CRACKED. CRACKED WEB ANGLE BS 927 - BS 947, BL ZERO, WL 208. FABRICATED, ALODINED AND PRIMED, INSTALLED REPAIR PARTS. (X) - [SDR W8PA970598](https://openairdocs.org/sdr/W8PA970598), May 22, 1997: FLOOR BEAM. CORRODED. CORROSION ON FLOOR BEAM STA 967, RBL 18, LBL 43, WL 208. ORIGINAL THICKNESS .125 INCH. REMOVED DAMAGED PARTS, FABRICATED NEW PARTS, INSTALLED PER SRM 53-00-51. All 67: https://openairdocs.org/deregistered/N951WP-2005-10-12/reports.md --- 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.