# N948WP: 1985 Boeing 737-301, registration cancelled 2005-12-16 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: December 16, 2005 - Exported to: Thailand - Status when cancelled: Valid registration - Airframe: [Boeing 737-301](https://openairdocs.org/model/boeing-737-301) (registry code 138447R) - Engine: [CFM International CFM56 series](https://openairdocs.org/engine/cfm-international-cfm56-series) (registry code 13802) - Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (OpenAirDocs) - Serial number: 23259 - Year built: 1985 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: July 15, 1985 - Certificate issued: August 11, 2004 - Last registry action: August 11, 2004 - Mode S code: AD2CE2 - 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/N948WP - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=948WP - Page: https://openairdocs.org/deregistered/N948WP-2005-12-16 From the FAA registry file of October 31, 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 737-301: https://openairdocs.org/model/boeing-737-301.md ## Service difficulty reports (70, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DL733040998](https://openairdocs.org/sdr/DL733040998), Oct 28, 2004: CONTROLLER. MALFUNCTIONED. AT 26K ALT CABIN BEGAN TO RISE RAPIDLY, EMERGENCY DESCENT WAS INITIATED. THE CABIN REACHED 15K, MASKS DROPPED. PERFORMED ALL REQUIRED TESTS, NO TROUBLE FOUND. - [SDR DL733031048](https://openairdocs.org/sdr/DL733031048), Nov 24, 2003: OVEN. FAILED. ON TAKEOFF, SMOKE FROM FWD GALLEY OVEN. REPLACED SAME. - [SDR DL733030901](https://openairdocs.org/sdr/DL733030901), Oct 5, 2003: INDICATOR. MALFUNCTIONED. CAPTS VSI STARTED SPARKING WHEN AT THE GATE IN SLC BRIEF ELECTRICAL FIRE FOLLOWED BY SMOKE IN COCKPIT. C PERFORMED EXTERNAL LEAK CHECK OF AREA ABOVE CAPT'S INST - [SDR DL733030548](https://openairdocs.org/sdr/DL733030548), Jun 13, 2003: VALVE. MALFUNCTIONED. AT 33000 FT WARNING HORN SOUNDED AND COCKPIT LOST PRESURIZATION. CABIN ALT CLIMBED TO 12500 AND AUTO FAIL LIGHT ILLUMINATED ON CABIN PRESSURIZATION CONTROLLER. - [SDR DL733021152](https://openairdocs.org/sdr/DL733021152), Sep 30, 2002: OVEN. MALFUNCTIONED. FLT ATTENDANT REPORTED SMOKE/ELECTRICAL SMELL COMING FROM F/C GALLEY OVEN AND CONTROL PANEL. FIRE EXTINGUISHER USED. NO FIRE NOTICED. GALLEY POWER SECURED. ELEC - [SDR DL733020486](https://openairdocs.org/sdr/DL733020486), Apr 27, 2002: LIGHT. DAMAGED. L2 DOOR EMERGENCY EXIT IDENT NEAR FLOOR DAMAGED. REPLACED BASE, OP CKS GOOD. - [SDR DL733011038](https://openairdocs.org/sdr/DL733011038), Jun 21, 2001: SKIN. PUNCTURED. FUSELAGE / SKIN / FS 277-295 / STRG. 19R-20R : GROUND DAMAGE CUTOUT REPAIR THE FUSELAGE SKIN BETWEEN FS 277 & 295 AT STRINGERS 19R & 20R WAS STRUCK BY GROUND EQ - [SDR DL733010905](https://openairdocs.org/sdr/DL733010905), Jun 1, 2001: BULKHEAD. CRACKED. INSPECTION OF THE FS 178 BULKHEAD WEB REVEALED A CRACK IN A TOOLING HOLE AT WL 234 AND LBL 12. A SECOND CRACK WAS FOUND AT A FASTENER HOLE AT WL 233 AND LBL 12. - [SDR DL733010328](https://openairdocs.org/sdr/DL733010328), Feb 24, 2001: OVEN. MALFUNCTIONED. FWD OVEN HAD AN ELECTRICAL /BURNT SMELL. GALLEY PWR WAS REMOVED, CONDITION IMPROVED. REPLACED FWD GALLEY OVEN AND BOTH CONTROLLERS. OVEN DPN 255701023, S/N 98-1 - [SDR DL733001751](https://openairdocs.org/sdr/DL733001751), Sep 10, 2000: OVEN. ODOR. A/C DIVERTED TO CYS AFTER EXPERIENCING FUMES IN THE CABIN. REPLACED F/C OVEN. - [SDR DL733000907](https://openairdocs.org/sdr/DL733000907), May 5, 2000: OUTFLOW VALVE. INOPERATIVE. CABIN HORN SOUNDED AT 10,000 FT AND CABIN DID NOT PRESSURIZE WORKING OFF A SINGLE PACK OPERATION. REPLACED AFT OUTFLOW VALVE, PRESSURIZED A/C TO 7.0 WITH NO PRO - [SDR DL733000356](https://openairdocs.org/sdr/DL733000356), Feb 22, 2000: CONTROLLER. INOPERATIVE. AIRCRAFT WOULD NOT PRESSURIZE IN AUTO OR STANDBY, CONTROL POSSIBLE IN MANUAL A/C. REPLACED PRESSURE CONTROLLER PER MM. OPS CHECKED OK. RAN ENGINES TO PRESSURIZE - [SDR DL733992709](https://openairdocs.org/sdr/DL733992709), Dec 10, 1999: SLIDE. DEPLOYED. WHILE REPOSITIONING A/C TO GATE FOR FIRST FLIGHT DEPARTURE, R1 SLIDE WAS INADVERTENTLY DEPLOYED DUE TO GIRT BAR APPARENTLY SHIFTED AND WHEN OPS ATTEMPTED TO BOA - [SDR DL733992563](https://openairdocs.org/sdr/DL733992563), Nov 21, 1999: CONTROLLER. MALFUNCTIONED. PRESSURIZATION LOST AFTER T/O FROM COS. UNABLE TO REGAIN PRESSURATION ANY CONFIGURATION. CHECKED ALL DOORS, RAN ENGS AND PACKS ON GROUND. ACFT PRESSURIZATION NO - [SDR DL733992230](https://openairdocs.org/sdr/DL733992230), Oct 6, 1999: SKIN. GOUGED. FUSELAGE SKIN FS 807-907, STRINGER 25L-27R, SKIN GOUGE REPAIR. THE FUSELAGE SKIN WAS BADLY SCRATCHED AND GOUGED FROM FS 807 TO FS 907 BETWEEN STRINGERS 25L AND - [SDR DL733991393](https://openairdocs.org/sdr/DL733991393), Jun 18, 1999: BEARING. FAILED. AILERONS BINDING WITH FLAPS AT 5 DEG DURING CONTROL CHECK. FOUND AILERON CENTERING CAM BEARING FROZEN. REPLACED BEARING AND SYS OPS NORMAL. - [SDR W8PA980032](https://openairdocs.org/sdr/W8PA980032), Jan 22, 1998: ANGLE. WORN. PAE- LT VERTICAL STABILIZER TO BODY CLOSURE ANGLE IS CHAFED AND WORN THROUGH ON AFT END. REMOVED ANGLE, INSTALLED NEW ANGLE. - [SDR W8PA980031](https://openairdocs.org/sdr/W8PA980031), Jan 22, 1998: SUPPORT. CORRODED. PAE- FWD CARGO BAY, CORROSION ON FLR TO SIDEWALL SUPPORT, BS 500C-500C+3, LBL 25. REMOVED CORROSION, REMOVED AND REPAIRED. FLOOR SUPPORT, OUT OF LIMITS. - [SDR W8PA980030](https://openairdocs.org/sdr/W8PA980030), Jan 22, 1998: FITTING. GOUGED. PAE- FWD ENTRY DOOR UPPER AND LOWER FWD CATCH ROLLER FITTINGS GOUGED. BLENDED UPPER FWD LATCH, PLACED LOWER FITTING. OUT OF LIMITS. - [SDR W8PA980029](https://openairdocs.org/sdr/W8PA980029), Jan 22, 1998: ANGLE. CRACKED. PAE- E AND E BAY RACK SUPPORT CRACKED. REMOVED CRACKED ANGLE, FABRICATED NEW SUPPORT ANGLE AND INSTALLED. - [SDR W8PA971329](https://openairdocs.org/sdr/W8PA971329), Jul 18, 1997: BULB. FAILED. LEFT OVERWING EMERGENCY EXIT LIGHTIS INOPEIS INOPERABLE. RELAMPED EXIT LIGHT, OPS CHECK GOOD. (X) - [SDR W8PA970533](https://openairdocs.org/sdr/W8PA970533), May 18, 1997: LENS. LOOSE. RIGHT HAND FUSELAGE EMERGENCY LIGHT JUST AFT OF WHEELWELL HAS LOOSE LENS. REMOVED AND REPLACED EMERGENCY LIGHT LENS. (X) - [SDR W8PA970116](https://openairdocs.org/sdr/W8PA970116), Mar 22, 1997: FAIRING. BROKEN. AFTER DEPARTING EWR RIGHT MAIN LANDING GEAR WOULD NOT FULLY RETRACT, GEAR OPERATED NORMALLY IN DOWN POSITION. AFTER LANDING IN IND FOUND RIGHT INBOARD FLAP TRAC - [SDR W8PA970110](https://openairdocs.org/sdr/W8PA970110), Mar 16, 1997: HYD PUMP. LEAKING. AIRCRAFT HAD A LOSS OF B-SYSTEM HYDRAULIC FLUID. REPLACED B-SYSTEM ELECTRIC HYDRAULIC PUMP ASSY. (M) - [SDR W8PA970077](https://openairdocs.org/sdr/W8PA970077), Mar 6, 1997: DOUBLER. CORRODED. DURING C-CHECK, FOUND CIRCULAR DOUBLER AT AFT CARGO BAY LIGHT SWITCH IS CORRODED AROUND NUTPLATES. FORWARD SIDE OF BS 794, FRAME RBL 33, WL 162. REMOVED CORROSI - [SDR W8PA970102](https://openairdocs.org/sdr/W8PA970102), Feb 25, 1997: FLOORBEAM. CORRODED. DURING C-CHECK, FOUND CORROSION ON UPPER CHORD OF FLOORBEAM AT BS 312, RBL 34.5, WL 208. BLENDED CORROSION. FOUND PART OUT OF LIMITS, FABRICATED AND INSTALLED R - [SDR W8PA970101](https://openairdocs.org/sdr/W8PA970101), Feb 25, 1997: INTERCOSTAL. CRACKED. DURING C-CHECK, INTERCOSTAL CRACKED AT BS 279, RBL 56, WL 231. REMOVED CRACKED INTERCOSTAL, FABRICATED AND INSTALLED NEW INTERCOSTAL. (M) - [SDR W8PA970100](https://openairdocs.org/sdr/W8PA970100), Feb 25, 1997: RIB. CRACKED. DURING C-CHECK, LEFT INBOARD FLAP UPPER FIXED PANEL APPROXIMATELY, WBL 85, OUTBOARD SUPPORT RIB IS CRACKED. REMOVED CRACKED RIB AND INSTALLED NEW RIB. (M) - [SDR W8PA970099](https://openairdocs.org/sdr/W8PA970099), Feb 25, 1997: FLOORBEAM. CORRODED. DURING C-CHECK, FOUND CORROSION ON UPPER CHORD OF FLOORBEAM AT BS 294, LBL 20, WL 208. REMOVED CORROSION, REPAIRED UPPER CHORD OF FLOORBEAM AT BS 294, LBL 20, W - [SDR W8PA970098](https://openairdocs.org/sdr/W8PA970098), Feb 25, 1997: ANGLE. CORRODED. DURING C-CHECK, FOUND CORROSION ON NUTPLATES OF FSD MOP SILL L-ANGLE SUPPORT FROM BS 305-323. REMOVED CORROSION, PART OUT OF LIMITS, REMOVED L-ANGLE SUPPORT AND - [SDR W8PA970097](https://openairdocs.org/sdr/W8PA970097), Feb 25, 1997: INTERCOSTAL. CORRODED. DURING C-CHECK, FOUND CORROSION BS 996-1006, LBL 10 - 13, WL 208 (INTERCOSTAL). REMOVED CORRODED INTERCOSTAL AND INSTALLED NEW INTERCOSTAL. (M) - [SDR W8PA970096](https://openairdocs.org/sdr/W8PA970096), Feb 25, 1997: FITTING. CORRODED. DURING C-CHECK, FOUND CORROSION ON FORWARD ENTRY DOOR GIRT BAR FITTING MOUNTS. REMOVED CORROSION, FOUND PARTS OUT OF LIMITS, INSTALLED NEW FITTING MOUNTS IAW SR - [SDR W8PA970095](https://openairdocs.org/sdr/W8PA970095), Feb 25, 1997: STIFFENER. CORRODED. DURING C-CHECK, FOUND CORROSION ON STIFFENER AT LBL 16.5, BS 314, 320, 325, WL 208. REMOVED CORROSION, FOUND PARTS OUT OF LIMITS, REMOVED CORRODED PARTS AND INS - [SDR W8PA970094](https://openairdocs.org/sdr/W8PA970094), Feb 25, 1997: FLOORBEAM. CORRODED. DURING C-CHECK, FOUND CORROSION ON UPPER CHORD OF FLOORBEAM AT BS 947, RBL 6, WL 208. BLENDED OUT CORROSION, FOUND TO BE OUT OF LIMITS PER SRM 53-10-51. FABRICA - [SDR W8PA970093](https://openairdocs.org/sdr/W8PA970093), Feb 25, 1997: ANGLE. CRACKED. DURING C-CHECK, INTERCOSTAL TO SKIN TIE ANGLE IS CRACKED AT STATION 290, WL 241, BETWEEN STRINGER 13 AND 14 RIGHT. REMOVED AND REPLACED ANGLE. (M) - [SDR W8PA970092](https://openairdocs.org/sdr/W8PA970092), Feb 25, 1997: FLOORBEAM. CORRODED. DURING C-CHECK, FOUND CORROSION BS 1006, LBL 36-RBL 36, WL 208, AROUND FLOOR BOARD ATTACH HOLES. REMOVED OUT OF LIMITS AREA AT BS 1006, LBL 29, WL 208. REPAIRED - [SDR W8PA970091](https://openairdocs.org/sdr/W8PA970091), Feb 25, 1997: CHANNEL. CORRODED. DURING C-CHECK, FOUND CORROSION ON INTERCOSTAL AT RBL 11.5, BS 347, WL 208. REMOVED CORROSION FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED INTERCOSTAL. (M) - [SDR W8PA970090](https://openairdocs.org/sdr/W8PA970090), Feb 25, 1997: FLOOR SUPPORT. CORRODED. DURING C-CHECK, FOUND CORROSION ON INTERCOSTAL AT RBL 45, BS 953, AND BS 957.5, WL 208. REMOVED CORROSION FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED INTERC - [SDR W8PA970089](https://openairdocs.org/sdr/W8PA970089), Feb 25, 1997: HAT CHANNEL. CORRODED. DURING C-CHECK, FOUND CORROSION ON CORNER OF HAT CHANNEL AND SUPPORT BRACKET BS 307, LBL 11, WL 208. REMOVED CORROSION FOUND TO BE OUT OF LIMITS. FABRICATED AND - [SDR W8PA970088](https://openairdocs.org/sdr/W8PA970088), Feb 25, 1997: FLOORBEAM. CORRODED. DURING C-CHECK, FOUND CORROSION BS 967, FOUND ON UPPER CHORD OF THE FLOORBEAM AT BS 344, RBL 8.5, WL 208. CORROSION FOUND TO BE OUT OF LIMITS. FABRICATED AND IN - [SDR W8PA970087](https://openairdocs.org/sdr/W8PA970087), Feb 25, 1997: SUPPORT. CORRODED. DURING C-CHECK, FOUND CORROSION BS 967, LBL 53 - RBL 53, WL 208, (AROUND FLOOR BOARD ATTACH HOLES). CORROSION FOUND TO BE OUT LIMITS. REPAIRED UPPER CHORD. (M) - [SDR W8PA970086](https://openairdocs.org/sdr/W8PA970086), Feb 25, 1997: FORMER. CRACKED. DURING C-CHECK, FORMED SECTION CRACKED AT BS 295, RBL 54, WL 209. REMOVED AND REPAIRED CRACKED AREA. (M) - [SDR W8PA970085](https://openairdocs.org/sdr/W8PA970085), Feb 25, 1997: INTERCOSTAL. CORRODED. DURING C-CHECK, INTERCOSTAL CRACKED AT AFT CARGO DOOR UPLATCH ATTACH BS 787-807, RBL 16.5, WL 203. REPLACED INTERCOSTAL WITH NEW PART. (M) - [SDR W8PA970084](https://openairdocs.org/sdr/W8PA970084), Feb 25, 1997: FLOORBEAM. CORRODED. DURING C-CHECK, FOUND CORROSION ON UPPER CHORD OF FLOORBEAM AT BS 328, LBL 28.5, WL 208. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS, REMOVED DAMAGED AREA, FAB - [SDR W8PA970083](https://openairdocs.org/sdr/W8PA970083), Feb 25, 1997: HAT CHANNEL. CORRODED. DURING C-CHECK, FOUND CORROSION BS 996, LBL 22-34, WL 208, (HAT CHANNEL FORWARD FLANGE). REMOVED CORROSION, FOUND TO BE OUT OF LIMITS, FABRICATED AND INSTALLED - [SDR W8PA970082](https://openairdocs.org/sdr/W8PA970082), Feb 25, 1997: HAT CHANNEL. CORRODED. DURING C-CHECK, FOUND CORROSION BS 996, RBL 5-49, WL 208-209. (HAT CHANNEL AND GALLEY ATTACH ANGLE). REMOVED CORROSION, FOUND TO BE OUT OF LIMITS, FABRICATED AN - [SDR W8PA970081](https://openairdocs.org/sdr/W8PA970081), Feb 25, 1997: FLOORBEAM. CORRODED. DURING C-CHECK, FOUND CORROSION FOUND ON UPPER CHORD OF FLOORBEAM AT BS 294, LBL 20 WL 208. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALL - [SDR W8PA970080](https://openairdocs.org/sdr/W8PA970080), Feb 25, 1997: ANGLE. CORRODED. DURING C-CHECK, CORROSION BS 1012-1030, LBL 6 - 1030, LBL 6 - RBL 15, WL 208-209, (FLOOR WEB ATTACH STRAPS AND GALLEY ATTACH ANGLES). REMOVED CORROSION, FROM GA - [SDR W8PA970079](https://openairdocs.org/sdr/W8PA970079), Feb 25, 1997: INTERCOSTAL. CORRODED. DURING C-CHECK, FOUND CORROSION BS 108, LBL 8, WL 208 (INTERCOSTAL). REMOVED CORROSION, FOUND TO BE OUT OF LIMITS, REMOVED DAMAGED INTERCOSTAL, INSTALLED NEW IN - [SDR W8PA970078](https://openairdocs.org/sdr/W8PA970078), Feb 25, 1997: INTERCOSTAL. CORRODED. DURING C-CHECK, FOUND CORROSION BS 988, RBL 17, WL 208, INTERCOSTAL FLOOR ATTACH HOLE. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS, REMOVED DAMAGED INTERCOSTAL All 70: https://openairdocs.org/deregistered/N948WP-2005-12-16/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 20020930025319I](https://openairdocs.org/incident/20020930025319I), Sep 30, 2002: Boeing 737301 (N948WP), Texico, TX, Minor damage. (-23) On 09/30/2002, 17:25 CDT delta flight 1628, a Boeing B737 was enroute from dfw to ontario, CA. Flight was over Texico, new Mexico at time of incident.… - [Incident 19970322012739I](https://openairdocs.org/incident/19970322012739I), Mar 22, 1997: Boeing 737300 (N948WP), Indianapolis, IN. Narrative: crew diverted into Indianapolis from planned flight neward to Colorado springs for unsafe gear indication. Contract maintenance from usair did… --- 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.