# N10251: Boeing 737-291, registration cancelled 1999-04-17 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: April 17, 1999 - Status when cancelled: Valid registration - Airframe: [Boeing 737-291](https://openairdocs.org/model/boeing-737-291) (registry code 138448W) - Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (OpenAirDocs) - Serial number: 20361 - Type of aircraft: Fixed wing multi engine - Last registry action: April 17, 1999 - Mode S code: A00F43 - Owner when cancelled: [Rfc 737/23 Inc](https://openairdocs.org/faa-owner/RFC%20737%2F23%20INC) - Location: [Cheyenne, WY](https://openairdocs.org/faa-place/WY/Cheyenne) - Owner type: Corporation - Owner's area on the map: 41.1001° N, 104.9249° W: Placed by OpenAirDocs at the center of ZIP code 82001, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N10251 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=10251 - Page: https://openairdocs.org/deregistered/N10251-1999-04-17 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 737-291: https://openairdocs.org/model/boeing-737-291.md ## Service difficulty reports (59, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CALA9801570](https://openairdocs.org/sdr/CALA9801570), Aug 27, 1998: POWER SUPPLY. INOPERATIVE. INSPECTION FOUND SECTION OF EMERGENCY FLOOR PATH LIGHTING IN AFT CABIN INOPERATIVE. MAINTENANCE FOUND THE M913 POWER SUPPLY AT STA 776 AT FAULT. THE M913 POWER - [SDR CALA9800999](https://openairdocs.org/sdr/CALA9800999), Jun 9, 1998: FRAME. CRACKED. INSPECTION FOUND A 3 INCH CRACK AT FORWARD LOWER CORNER OF DOOR FRAME JUST BELOW OPEN LATCH ASSEMBLY OF FORWARD CARGO DOOR. THE AREA WAS REPAIRED IAW SRM 51-10- - [SDR CALA9800919](https://openairdocs.org/sdr/CALA9800919), May 29, 1998: FIRE DETECTOR. INOPERATIVE. THE APU FIRE WARNING LIGHT AND BELL ACTIVATED, WITH APU OFF, WHILE EN ROUTE. THE APU FIRE BOTTLE WAS DISCHARGED, BUT THE LIGHT AND BELL CONTINUED TO ACTIVATE IN - [SDR CALA9800876](https://openairdocs.org/sdr/CALA9800876), May 17, 1998: SKIN. DENTED. INSPECTION FOUND FUSELAGE SKIN DENTED AT FS 294.5, STRINGER 14. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3. - [SDR CALA9800888](https://openairdocs.org/sdr/CALA9800888), May 16, 1998: BEAM. CRACKED. INSPECTION FOUND TRANSVERSE BEAM CRACKED IN RADIUS FORWARD AND AFT IN THREE EACH PLACES AT STA 675, RBL 24, WBL 208. THE CRACKS WERE APPROXIMATELY 1 INCH LONG. - [SDR CALA9800887](https://openairdocs.org/sdr/CALA9800887), May 16, 1998: FRAME. CRACKED. INSPECTION FOUND A 1.5 CRACK IN RADIUS OF FRAME AT STA 675, RBL 24, WBL 208 AND A 1.5 CRACK IN FRAME AT STA 675, LBL 24, WBL 208. REPAIRS WERE PERFORMED IAW SA0 - [SDR CALA9800875](https://openairdocs.org/sdr/CALA9800875), May 16, 1998: TEAR STRAP. CORRODED. INSPECTION FOUND FRAME TO SKIN TEAR STRAP CORRODED AT BS 360, STRINGER 29R. REPAIRED IAW SRM 53-30-3. - [SDR CALA9800874](https://openairdocs.org/sdr/CALA9800874), May 16, 1998: WEB. CRACKED. INSPECTION FOUND A .25 INCH CRACK IN FORWARD CARGO COMPARTMENT DOOR CUTOUT AFT FRAME AFT FACE OF WEB AT BS 492.4, STRINGER 25R. A REPAIR WAS FABRICATED AND INST - [SDR CALA9800873](https://openairdocs.org/sdr/CALA9800873), May 16, 1998: SPLICE. CRACKED. INSPECTION FOUND A 1 CRACK IN LT WING LANDING GEAR BEAM AFT SPLICE PLATE AT FS 727. THE SPLICE PLATE WAS REPAIRED IAW DRAWING NR 65C292288. - [SDR CALA9800855](https://openairdocs.org/sdr/CALA9800855), May 14, 1998: THRESHOLD. CRACKED. AFT PIT THRESHOLD AFT CORNER CRACKED (3.5). REMOVED AFT PIT THRESHOLD CORNER AND INSTALLED A NEW CORNER PER SRM 51-30-2. - [SDR CALA9800826](https://openairdocs.org/sdr/CALA9800826), May 11, 1998: SKIN. DENTED. FUSELAGE SKIN DENTED STA 259 BETWEEN STR 23R AND 24R. FABRICATED, PRIMED, SEALED, AND INSTALLED DOUBLER PER SRM 53-30-3, 51-10-2 AND 51-20-4. - [SDR CALA9800827](https://openairdocs.org/sdr/CALA9800827), May 10, 1998: FLOOR PANEL. CRACKED. FLOOR PANEL FWD PIT FS 380 TO 420 HAS TEARS. FABRICATED FWD PIT PANEL PER ECRA 2550-01046. - [SDR CALA9800817](https://openairdocs.org/sdr/CALA9800817), May 7, 1998: SKIN. DENTED. FUSELAGE SKIN HAS A DENT AT STA 905 STR 22R. REMOVED DAMAGED AREA, FABRICATED REPAIR. TREATED, PRIMED AND INSTALLED PER SRM 53-30-1, 53-30-3, 51-20-2, AND MM 51 - [SDR CALA980800](https://openairdocs.org/sdr/CALA980800), May 6, 1998: DOUBLER. CHAFED. NUMBER ONE ENGINE O/B COWLING NUMBER SIX RIB CHAFED AT DOUBLER REPAIR. REMOVED DOUBLER AND FILLER MATERIAL. FABRICATED, TREATED, PRIMED, AND INSTALLED NEW DOUBL - [SDR CALA9800801](https://openairdocs.org/sdr/CALA9800801), May 6, 1998: ANGLE. CRACKED. CABIN FLOORBEAM ATTACH ANGLE CRACKED STA 520 BL 0.0. REMOVED CRACKED ATTACH ANGLE. FABRICATED, TREATED, PRIMED AND INSTALLED NEW ANGLE PER SRM 51-40-3, 51-10-2 - [SDR CALA9800799](https://openairdocs.org/sdr/CALA9800799), May 6, 1998: SKIN. CRACKED. FORWARD CARGO DOOR INNER SKIN CRACKED (1/2). FABRICATED, ALODINED, PRIMED AND INSTALLED REPAIR PER SRM 51-40-2, 51-10-2, 51-30-2 AND MM 51-20-0. - [SDR CALA9800790](https://openairdocs.org/sdr/CALA9800790), May 6, 1998: SKIN. DENTED. LOWER RIGHT SIDE AFT FUSELAGE AT BS 787 STR R26 DENTED FORWARD OF AFT CARGO DOOR CUTOUT. REMOVED DAMAGED AREA. INSTALLED REPAIR PER SRM 53-30-1, 51-00-00, 53-30 - [SDR CALA9700384](https://openairdocs.org/sdr/CALA9700384), Mar 7, 1997: BULKHEAD. CRACKED. INSPECTION FOUND A SIX INCH CRACK IN BULKHEAD AT STA 178, WL 208, RBL 18. ALSO, A SIX INCH CRACK WAS FOUND IN BULKHEAD AT STA 178, WL 208, LBL 16. THE CRACKED A - [SDR CALA9700383](https://openairdocs.org/sdr/CALA9700383), Mar 7, 1997: SKIN. PUNCTURED. THE FUSELAGE SKIN WAS PUNCTURED APPROXIMATELY FIVE FEET AFT OF L-1 DOOR SILL. THE PUNCTURED AREA OF SKIN AND DOUBLER WERE CUT OUT IAW SRM 53-30-3. A REPAIR DOUB - [SDR CALA9700382](https://openairdocs.org/sdr/CALA9700382), Mar 7, 1997: ANGLE. CORRODED. INSPECTION FOUND FLOOR ATTACH ANGLE CORRODED FROM BS 290 TO 360, LBL 65. REMOVED CHORD AND INSTALLED NEW CHORD IAW SRM 51-30-2. A DOUBLER AND FILLER FLOOR WEB W - [SDR CALA9700381](https://openairdocs.org/sdr/CALA9700381), Mar 7, 1997: SPLICE. CRACKED. INSPECTION FOUND A 3 INCH CRACK IN STRINGER 27R SPLICE AT STA 420. THE CRACKED SPLICE WAS REMOVED, A NEW SPLICE WAS FABRICATED AND INSTALLED IAW BOEING DRAWING - [SDR CALA9700380](https://openairdocs.org/sdr/CALA9700380), Mar 7, 1997: WEB. CORRODED. INSPECTION FOUND AFT LT WEB CORRODED IN AN AREA APPROXIMATELY 20 BY 8.5 AT STA 1016. THE CORRODED WEB WAS REMOVED, A NEW WEB WAS FABRICATED AND INSTALLED IAW SR - [SDR CALA9700379](https://openairdocs.org/sdr/CALA9700379), Mar 7, 1997: FLOORBEAM. CORRODED. INSPECTION FOUND RT FLOORBEAM CORRODED AT STA 1016. THE CORRODED AREA OF FLOORBEAM CAP WAS CUT OUT, A NEW CAP WAS FABRICATED AND INSTALLED IAW SRM 53-10-9 AND 5 - [SDR CALA9700378](https://openairdocs.org/sdr/CALA9700378), Mar 7, 1997: WEB. CORRODED. INSPECTION FOUND RT OUTBOARD WEB AT STA 996 TO 1016 CORRODED AND DELAMINATED APPROXIMATELY 10 BY 1.5 IN AREA. THE WEB AND TWO FLOOR SUPPORTS WERE REMOVED, A NEW - [SDR CALA9700377](https://openairdocs.org/sdr/CALA9700377), Mar 7, 1997: CHANNEL. CORRODED. INSPECTION FOUND RT AFT COAT CLOSET FORWARD BULKHEAD FLOOR CHANNEL CORRODED ON TOP AND BOTTOM. THE CHANNEL WAS REMOVED AND A REPLACEMENT CHANNEL WAS FABRICATED - [SDR CALA9700376](https://openairdocs.org/sdr/CALA9700376), Mar 7, 1997: SKIN. CRACKED. INSPECTION FOUND .125 INCH CRACKS AT EIGHT FASTENER HOLES IN RT SECTION 41 SKIN PANEL. THE SKIN PANEL WAS REMOVED AND THE AREA WAS CLEANED IAW SRM 51-30-2 AND 5 - [SDR CALA9700375](https://openairdocs.org/sdr/CALA9700375), Mar 7, 1997: SKIN. DENTED. INSPECTION FOUND SKIN DENTED AND BUCKLED AT FORWARD CARGO DOOR. THE SKIN WAS REMOVED AND NEW SKIN WAS FABRICATED IAW BOEING DRAWING 65-46921. THE SKIN WAS INSTA - [SDR CALA9700374](https://openairdocs.org/sdr/CALA9700374), Mar 7, 1997: INTERCOSTAL. CRACKED. INSPECTION FOUND A .75 INCH CRACK IN INTERCOSTAL AT BS 420 TO 440, STRINGER 26L. THE INTERCOSTAL WAS REMOVED AND A NEW INTERCOSTAL WAS FABRICATED AND INSTALLED - [SDR CALA9700373](https://openairdocs.org/sdr/CALA9700373), Mar 7, 1997: SUPPORT BEAM. CORRODED. INSPECTION FOUND CORROSION ON TOP CAP OF LT DIAGONAL SUPPORT BEAM AT STA 996 TO 1006. THE SUPPORT BEAM WAS REMOVED AND A NEW SUPPORT BEAM WAS FABRICATED AND INS - [SDR CALA9700372](https://openairdocs.org/sdr/CALA9700372), Mar 7, 1997: STRINGER. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN STRINGER 26L AT STA 420. THE CRACKED AREA OF STRINGER WAS CUT OUT IAW SRM 53-10-3. A NEW STRINGER SECTION, SPLICES, AND FILLE - [SDR CALA9700371](https://openairdocs.org/sdr/CALA9700371), Mar 7, 1997: ANGLE. CRACKED. INSPECTION FOUND A 1.5 INCH CRACK IN LT HORIZONTAL STABILIZER ATTACH ANGLE AT STA 142 CENTER SPAR LEADING EDGE. THE CRACK WAS STOP DRILLED IAW SRM 55-10-4. REPA - [SDR CALA9700370](https://openairdocs.org/sdr/CALA9700370), Mar 7, 1997: ANGLE. CRACKED. A 1 INCH CRACK WAS FOUND BETWEEN FASTENER HOLES IN RT MLG WHEEL WELL UPPER FORWARD ATTACH ANGLE AT STA 664, STATION 18A SHEAR BEAM. THE ANGLE WAS REMOVED AND A - [SDR CALA9700369](https://openairdocs.org/sdr/CALA9700369), Mar 7, 1997: PAN. CORRODED. INSPECTION FOUND AFT LAV SERVICE CENTER PAN STRUCTURE CORRODED AT STA 1006. CHANNELS WERE FABRICATED IAW BOEING DRAWING 69-36677 AND A NEW LAV PAN STRUCTURE WAS - [SDR CALA9700368](https://openairdocs.org/sdr/CALA9700368), Mar 7, 1997: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED FROM STA 1006 TO 1016, BBL 0. A NEW FLOORBEAM WAS FABRICATED AND INSTALLED IAW BOEING DRAWING 65-46812 AND SRM 51-30-2. - [SDR CALA9700367](https://openairdocs.org/sdr/CALA9700367), Mar 7, 1997: WEB. CORRODED. INSPECTION FOUND CORROSION IN AFT RT WEB AT STA 1016 TO 1022. A NEW WEB WAS FABRICATED AND INSTALLED IAW SRM 51-30-5 AND 51-30-2. - [SDR CALA9700366](https://openairdocs.org/sdr/CALA9700366), Mar 7, 1997: SUPPORT. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN RT WING FLAP WELL UPPER TRAILING EDGE PANEL SUPPORT JUST AFT OF AFT SPAR AT STA RSS 446.94. THE T-CHANNEL WAS REMOVED AND A N - [SDR CALA9700295](https://openairdocs.org/sdr/CALA9700295), Feb 25, 1997: SKIN. CRACKED. INSPECTION FOUND CRACKS AT EIGHT FASTENERS IN RT SECTION 41 SKIN PANEL. THE CRACKS WERE APPROXIMATELY .5 INCH LONG. THE SKIN PANEL WAS REMOVED AND A NEW PANEL W - [SDR CALA9601922](https://openairdocs.org/sdr/CALA9601922), Dec 31, 1996: SEAL. LEAKING. THE NR 1 ENGINE WAS SHUTDOWN DUE TO LOSS OF OIL WHILE EN ROUTE. THE AIRCRAFT LANDED AT EWR WITHOUT INCIDENT. MAINTENANCE FOUND OIL LEAKING FROM NR 1 ENGINE NR 6 - [SDR CALA9600649](https://openairdocs.org/sdr/CALA9600649), May 28, 1996: SENSOR. OUT OF ADJUST. THE LANDING GEAR HANDLE WOULD NOT MOVE PAST THE OFF POSITION AFTER TAKEOFF. THE LANDING GEAR REMAINED DOWN WITH THREE GREEN LIGHTS AT ALL TIMES. THE AIRCRAFT WA - [SDR CAL960602](https://openairdocs.org/sdr/CAL960602), May 2, 1996: BATTERY PACK. DISCHARGED. GSO - THE AFT RT SERVICE DOOR SLIDE LIGHT HAD NO VOLTAGE AT TEST JACK WITH LANYARD PULLED. THE DOOR SLIDE LIGHT BATTERY PACK WAS REMOVED AND REPLACED IAW MM 33- - [SDR CAL960601](https://openairdocs.org/sdr/CAL960601), May 2, 1996: BATTERY PACK. DISCHARGED. GSO - THE FORWARD RT SERVICE DOOR SLIDE LIGHT HAD NO VOTLAGE AT TEST JACK WITH LANYARD PULLED. THE DOOR SLIDE LIGHT BATTERY PACK WAS REMOVED AND REPLACED IAW MM - [SDR CAL960600](https://openairdocs.org/sdr/CAL960600), May 2, 1996: BATTERY PACK. DISCHARGED. GSO - THE AFT LT ENTRY DOOR SLIDE LIGHT HAD NO VOLTAGE AT TEST JACK WITH LANYARD PULLED AND LIGHTS ON. THE DOOR SLIDE LIGHT BATTERY PACK WAS REMOVED AND REPLACE - [SDR CAL960597](https://openairdocs.org/sdr/CAL960597), Apr 30, 1996: SKIN. CORRODED. GSO - INSPECTION FOUND LT AFT CORNER OF NOSE WHEELWELL CUT-OUT EXTERNAL SKIN CORRODED AT STA 294.5. THE CORRODED AREA OF SKIN AND BEAR STRAP WERE CUT OUT. STRAP - [SDR CAL960596](https://openairdocs.org/sdr/CAL960596), Apr 30, 1996: PANEL. CRACKED. GSO - INSPECTION FOUND A 1.5 INCH CRACK IN FORWARD OUTBOARD CORNER OF LT WING UPPER TRAILING EDGE PANEL FORWARD OF NR 4 SPOILER. THE PANEL WAS REMOVED AND A NEW - [SDR CAL960599](https://openairdocs.org/sdr/CAL960599), Apr 29, 1996: DOOR FRAME. CRACKED. GSO - INSPECTION FOUND A 3 INCH CRACK IN AFT CARGO COMPARTMENT DOOR CUTOUT FORWARD FRAME. THE FRAME SECTION WAS REMOVED AND REPLACED IAW EA 5310-02555. (M) - [SDR CAL960598](https://openairdocs.org/sdr/CAL960598), Apr 28, 1996: ANGLES. CRACKED. GSO - INSPECTION FOUND FOUR EACH ATTACH ANGLES CRACKED AT LT MLG STR 18A SHEAR BEAM. THE CRACKS MEASURED FROM 2 TO 5 INCHES IN LENGTH. THE ANGLES WERE REMOVED A - [SDR CAL950212](https://openairdocs.org/sdr/CAL950212), Mar 15, 1995: DOOR. CRACKED. GSO - INSPECTION FOUND A 1.2 INCH CRACK IN AFT CARGO DOOR ON THE INSIDE RIGHT CORNER UNDER DOUBLER. THE CRACK WAS REPAIRED BY FABRICATING AND INSTALLING DOUBLER - [SDR CAL950211](https://openairdocs.org/sdr/CAL950211), Mar 15, 1995: SLAT. CRACKED. GSO - INSPECTION FOUND A 1.1 INCH CRACK IN THE NR 2 SLAT INBOARD AUXILIARY TRACK CUT-OUT. THE CRACKED AREA WAS REMOVED IAW SRM 57-30-4 AND REPAIR FILLER AND DOU - [SDR CAL950210](https://openairdocs.org/sdr/CAL950210), Mar 15, 1995: LE RIB. CRACKED. GSO - INSPECTION FOUND A 1.2 INCH CRACK IN RT WING LEADING EDGE RIB, JUST OUTBOARD OF NR 5 SLAT ACTUATOR. THE CRACKED SECTION WAS REMOVED IAW SRM 51-30-2 AND A - [SDR CAL950209](https://openairdocs.org/sdr/CAL950209), Mar 15, 1995: FRAME. CRACKED. GSO - INSPECTION FOUND A .75 INCH CRACK IN FRAME AT BS 500B, STR 22L. THE CRACKED FRAME WAS REMOVED AND REPLACED WITH REPAIR KIT IAW BOEING DRAWING 65C25113. (X All 59: https://openairdocs.org/deregistered/N10251-1999-04-17/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 19980729038009I](https://openairdocs.org/incident/19980729038009I), Jul 29, 1998: Boeing 737291 (N10251), Newark, NJ. (-5)All exits on right side. Taxi out, parked on bravo shut down #1, ramp control said saw smoke and go to ground freq. Told ground to roll CFR, brief f/a to… - [Incident 19910511032009I](https://openairdocs.org/incident/19910511032009I), May 11, 1991: Boeing 737291 (N10251), Minot, ND, Minor damage. Aircraft received several bird strikes on takeoff. Returned and landed safely. ## Other aircraft with N10251 - [Registered now](https://openairdocs.org/aircraft/N10251): Flagg Larry D LARRYS MIXTURE, S/N 1, built 2001 - [Cancelled (date not recorded)](https://openairdocs.org/deregistered/N10251-undated): Grumman G-164, S/N 51 --- 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.