# N60312: 1985 Boeing 737-3TO, registration cancelled 2006-04-03 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: April 3, 2006 - Exported to: Ireland - Status when cancelled: Triennial form not returned - Airframe: [Boeing 737-3TO](https://openairdocs.org/model/boeing-737-3to) (registry code 138447G) - Engine: [CFM International CFM56 series](https://openairdocs.org/engine/cfm-international-cfm56-series) (registry code 13802) - Serial number: 23363 - Year built: 1985 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: October 2, 1985 - Certificate issued: October 8, 1985 - Last registry action: July 15, 2003 - Mode S code: A7D4FA - Owner when cancelled: [Wilmington Trust Co Trustee](https://openairdocs.org/faa-owner/WILMINGTON%20TRUST%20CO%20TRUSTEE) - Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington) - Owner type: Corporation - Owner's area on the map: 39.7357° N, 75.5321° W: Placed by OpenAirDocs: center of Wilmington, DE, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N60312 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=60312 - Page: https://openairdocs.org/deregistered/N60312-2006-04-03 From the FAA registry file of November 4, 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 737-3TO: https://openairdocs.org/model/boeing-737-3to.md ## Service difficulty reports (68, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CALA0500318](https://openairdocs.org/sdr/CALA0500318), Sep 19, 2005: KEELBEAM. CORRODED. INSPECTION FOUND LEFT KEELBEAM LOWER SURFACE CORRODED AT STA 663.75 TO 727. REPAIRED KEEL BEAM LOWER CHORD IAW ECRA 5311-01238. - [SDR CALA0500317](https://openairdocs.org/sdr/CALA0500317), Sep 19, 2005: KEELBEAM. CORRODED. INSPECTION FOUND THE RIGHT KEEL BEAM CORRODED AT LOWER SURFACE BETWEEN STA 663.75 TO 696, S27R. REPAIRED IAW ECRA 5311-01239. - [SDR CALA0400643](https://openairdocs.org/sdr/CALA0400643), Sep 19, 2004: SOCKET. SHORTED. SMOKE BEGAN COMING FROM THE FLOURESCENT SIDEWALL LIGHTING AT ROWS 18-19 ABC WHILE EN ROUTE FROM TUS TO IAH. THE HALON FIRE EXTINGUISHER WAS USED, LIGHTS WERE TU - [SDR CALA0300460](https://openairdocs.org/sdr/CALA0300460), Aug 8, 2003: FIRE LOOP. DAMAGED. THE APU FIRE LIGHT ILLUMINATED DURING CLIMBOUT OF DEN. THE FIRE HANDLE WAS PULLED AND THE FIRE BOTTLE WAS DISCHARGED. THE LIGHT WENT OUT, BUT ILLUMINATED AGAIN - [SDR CALA0300387](https://openairdocs.org/sdr/CALA0300387), Jul 14, 2003: FRAME. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN RT MAIN FRAME ANGLE AT STA 616 FLOOR LINE. A STIFFENING ANGLE REPAIR WAS INSTALLED IAW ECRA 5311-01157. - [SDR CALA0300382](https://openairdocs.org/sdr/CALA0300382), Jul 12, 2003: SUPPORT ANGLE. GOUGED. INSPECTION FOUND LT MLG STAB LINK SUPPORT ANGLES GOUGED. THE ANGLES WERE REMOVED AND REPLACED IAW SRM 51-10-02. - [SDR CALA0300370](https://openairdocs.org/sdr/CALA0300370), Jul 8, 2003: FRAME. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN LT MAIN FRAME ANGLE AT STA 616 BELOW FLOOR LINE, WL 200. REPAIRED FRAME IAW ECRA 5311-01154. - [SDR CALA0300362](https://openairdocs.org/sdr/CALA0300362), Jul 3, 2003: STRINGER. GOUGED. INSPECTION FOUND A GOUGE IN STRINGER AT STA 1120, RT, IN APU COMPARTMENT. THE DAMAGED SECTION OF STRINGER WAS REMOVED AND A NEW SECTION OF STRINGER WAS INSTALLE - [SDR CALA0300361](https://openairdocs.org/sdr/CALA0300361), Jul 3, 2003: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED ON UPPER SURFACE AT STA 1006 BETWEEN RBL 24 AND RBL 32 AND RBL 27 INTERCOSTAL BS 1006-1016. A REPAIR WAS INSTALLED IAW SRM 5 - [SDR CALA0300357](https://openairdocs.org/sdr/CALA0300357), Jul 2, 2003: SEAT TRACK. CORRODED. INSPECTION FOUND THE LT I/B SEAT TRACK CORRODED BETWEEN BS 907 AND 947. A NEW SEAT TRACK SECTION WAS INSTALLED IAW SRM 53-00-52, FIGURE 204. - [SDR CALA0300354](https://openairdocs.org/sdr/CALA0300354), Jul 1, 2003: STRINGER. CORRODED. INSPECTION FOUND STRINGER 27L CORRODED AT STA 1006. THE STRINGER WAS REPAIRED IAW SRM 53-00-03, FIGURE 201. - [SDR CALA0300351](https://openairdocs.org/sdr/CALA0300351), Jul 1, 2003: ANGLE. CORRODED. INSPECTION FOUND L-1 DOOR JAMB ZEE ANGLE CORRODED FROM BS 306-344. THE ZEE ANGLE WAS REPLACED IAW SRM 51-40-02. - [SDR CALA0300350](https://openairdocs.org/sdr/CALA0300350), Jul 1, 2003: ANGLE. CORRODED. INSPECTION FOUND R-2 DOOR THRESHOLD Z-ANGLE CORRODED AT STA 937. THE ZEE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02. - [SDR CALA0300349](https://openairdocs.org/sdr/CALA0300349), Jul 1, 2003: STRINGER. CORRODED. INSPECTION FOUND STRINGER 26R CORRODED AT STA 1006-1016. THE STRINGER WAS REMOVED AND REPLACED IAW SRM 5-40-2. - [SDR CALA0300376](https://openairdocs.org/sdr/CALA0300376), Jun 30, 2003: FRAME. CRACKED. MAINTENANCE FOUND THE INNER CHORD ON THE LT FRAME AT STA 616 CRACKED. THE AREA WAS REPAIRED IAW ECRA 5311-01154. - [SDR CALA0300347](https://openairdocs.org/sdr/CALA0300347), Jun 30, 2003: CHANNEL. CORRODED. INSPECTION FOUND RT AFT LAV FORWARD WALL LOWER U-CHANNEL CORRODED AT STA 986.5 - 1006. THE U-CHANNEL WAS REPLACED IAW SRM 51-40-02. - [SDR CALA0300345](https://openairdocs.org/sdr/CALA0300345), Jun 30, 2003: WEB. CRACKED. INSPECTION FOUND BOTTOM SURFACE OF R-2 DOOR THRESHOLD WEB CORRODED AT STA 986.5 TO 990. THE LOWER SILL WEB WAS REMOVED AND REPLACED IAW SRM 51-40-02. - [SDR CALA0300343](https://openairdocs.org/sdr/CALA0300343), Jun 27, 2003: GALLEY TRACK. CORRODED. INSPECTION FOUND GALLEY TRACK CORRODED BETWEEN BS 328 AND 360 AT RBL 44. THE FLOOR TRACK WAS REMOVED AND REPLACED IAW SRM 51-10-2. - [SDR CALA0300342](https://openairdocs.org/sdr/CALA0300342), Jun 27, 2003: GALLEY TRACK. CORRODED. INSPECTION FOUND CORROSION ON GALLEY TRACK BETWEEN BS 277 AND 294, RBL 44. THE GALLEY TRACK WAS REMOVED AND REPLACED IAW SRM 51-10-2. - [SDR CALA0101040](https://openairdocs.org/sdr/CALA0101040), Dec 23, 2001: SKIN. CRACKED. INSPECTION FOUND A 3/8" CRACK IN FUSELAGE SKIN AT STA 373, S28, E&E EXHAUST BAY CUTOUT. REPAIRED IAW ECRA 5330-02894. - [SDR CALA0101035](https://openairdocs.org/sdr/CALA0101035), Dec 21, 2001: WEB. GOUGED. INSPECTION FOUND A GOUGE IN WEB ON R/H SIDE OF E&E DOOR JAMB STRUCTURE AT STA 338, RBL 15. A DOUBLER WAS INSTALLED IAW SRM 51-70-13. - [SDR CALA0101033](https://openairdocs.org/sdr/CALA0101033), Dec 18, 2001: WEB. CRACKED. INSPECTION FOUND A 1.25" AND 1" CRACK IN CENTER WEB OF FORWARD BULKHEAD AT STA 178, LBL 5.7, BETWEEN WL 195 AND 207. THE CENTER WEB WAS REPLACED IAW EA 5310-030 - [SDR CALA0101032](https://openairdocs.org/sdr/CALA0101032), Dec 18, 2001: KEELBEAM. CORRODED. INSPECTION FOUND LT WHEEL KEEL BEAM O/B LOWER CHORD CORRODED AT STA 715-724. THE KEEL BEAM WAS REPAIRED IAW ECRA 5310-03740. - [SDR CALA0101031](https://openairdocs.org/sdr/CALA0101031), Dec 17, 2001: SKIN. GOUGED. INSPECTION FOUND FUSELAGE SKIN GOUGED BELOW FORWARD END OF DORSAL FIN ON R/H SIDE AT STA 876-885, RBL 5, S1-S2R. THE GOUGED AREA WAS REMOVED AND A DOUBLER WAS I - [SDR CALA0101030](https://openairdocs.org/sdr/CALA0101030), Dec 14, 2001: TORQUE TUBE. CORRODED. INSPECTION FOUND R-2 DOOR FUSELAGE TORQUE TUBE CORRODED. THE TORQUE TUBE WAS REMOVED AND REPLACED IAW MM 52-41-41. - [SDR CALA9900818](https://openairdocs.org/sdr/CALA9900818), Jul 12, 1999: STIFFENER. CORRODED. INSPECTION FOUND CORROSION ON CENTERLINE DOUBLE STIFFENER JUST AFT OF BS 1016 AT BOTTOM OF APB FORWARD SIDE. A NEW CHANNEL SECTION AND DOUBLERS WERE INSTALLED I - [SDR CALA9900817](https://openairdocs.org/sdr/CALA9900817), Jul 12, 1999: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT STA 986.5. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED AND REPLACED IAW ECRA 5310-03851. - [SDR CALA9900816](https://openairdocs.org/sdr/CALA9900816), Jul 12, 1999: SKIN. CRACKED. INSPECTION FOUND A .375 INCH CRACK IN THE RT LOWER KEEL BEAM SKIN PANEL BETWEEN STA 660 AND 670. A REPAIR WAS INSTALLED IAW ECRA 5330-02844. - [SDR CALA9900814](https://openairdocs.org/sdr/CALA9900814), Jul 8, 1999: GUSSET. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN TORQUE BOX GUSSET AT STABILIZER CENTER SECTION, STA 1130. THE TORQUE BOX GUSSET WAS REMOVED AND REPLACED IAW SRM 51-10-2. - [SDR CALA9900763](https://openairdocs.org/sdr/CALA9900763), Jun 30, 1999: ANGLE. CORRODED. INSPECTION FOUND R-1 DOOR THRESHOLD FLOOR ATTACH ANGLE CORRODED. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-2. - [SDR CALA9900760](https://openairdocs.org/sdr/CALA9900760), Jun 30, 1999: SKIN. DELAMINATED. INSPECTION FOUND UPPER SURFACE OUTBOARD MID AREA OF LT AILERON DELAMINATED. THE AILERON WAS REPAIRED IAW ECRA 5761-01017. - [SDR CALA9900813](https://openairdocs.org/sdr/CALA9900813), Jun 29, 1999: TRACK. CORRODED. INSPECTION FOUND GALLEY TRACK CORRODED AT STA 290, RBL 45. THE TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-10-2. - [SDR CALA9900751](https://openairdocs.org/sdr/CALA9900751), Jun 29, 1999: ANGLE. CORRODED. INSPECTION FOUND L-2 PASSENGER DOOR THRESHOLD Z-ANGLE CORRODED FROM STA 914 TO 1006. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-2. - [SDR CALA9900750](https://openairdocs.org/sdr/CALA9900750), Jun 29, 1999: FLOORBEAM. CORRODED. INSPECTION FOUND CABIN FLOORBEAM CORRODED AT STA 328. THE UPPER SECTION OF FLOORBEAM WAS REMOVED AND REPLACED IAW SRM 53-10-51. - [SDR CALA9900746](https://openairdocs.org/sdr/CALA9900746), Jun 28, 1999: SEAT TRACK. CORRODED. INSPECTION FOUND LEFT O/B SEAT TRACK CORRODED AT STA 344 TO 362. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-10-2. - [SDR CALA9900745](https://openairdocs.org/sdr/CALA9900745), Jun 28, 1999: FLOORBEAM. CORRODED. INSPECTION FOUND LOWER SIDE OF FLOORBEAM CORRODED AT NUT PLATE, STA 294.5, LBL 48. THE CORRODED SECTION WAS REMOVED AND A NEW SECTION OF FLOORBEAM WAS INSTALLED - [SDR CALA9900743](https://openairdocs.org/sdr/CALA9900743), Jun 28, 1999: FLOORBEAM. CORRODED. INSPECTION FOUND TOP SIDE OF FLOORBEAM CORRODED AT STA 967, RBL 20 AND LBL 30. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED AND A REPAIR SECTION WAS INSTALLED - [SDR CALA9900742](https://openairdocs.org/sdr/CALA9900742), Jun 28, 1999: FLOORBEAM. CORRODED. INSPECTION FOUND CABIN FLOORBEAM CORRODED AT STA 312, LBL 17 TO RBL 38. INSTALLED REPAIR IAW SRM 53-00-51. - [SDR CALA9900731](https://openairdocs.org/sdr/CALA9900731), Jun 27, 1999: FRAME. CRACKED. INSPECTION FOUND A 4 INCH CRACK AT FASTENER HOLE OF FRAME AT STA 500, STRINGER 14R. THE CRACKED SECTION OF FRAME WAS CUT OUT. REPAIR DOUBLERS AND FILLER WERE IN - [SDR CALA9900729](https://openairdocs.org/sdr/CALA9900729), Jun 26, 1999: SUPPORT. CRACKED. INSPECTION FOUND A 3 INCH CRACK IN NR 1 ENGINE DIAGONAL FRAME SUPPORT AT NACELLE STA 315 ON RT SIDE. THE DIAGONAL FRAME SUPPORT WAS REPLACED IAW SRM 51-40-02. - [SDR CALA9900728](https://openairdocs.org/sdr/CALA9900728), Jun 26, 1999: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT STA 1006, LBL 30 TO RBL 11. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED, A REPAIR SECTION AND SPLICE WAS INSTALLED IAW - [SDR CALA9900727](https://openairdocs.org/sdr/CALA9900727), Jun 26, 1999: STRINGER. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN STRINGER 16L JUST AFT OF STA 500C. THE STRINGER WAS REPAIRED IAW SRM 53-00-03. - [SDR CALA9900768](https://openairdocs.org/sdr/CALA9900768), Jun 25, 1999: SKIN. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN FUSELAGE SKIN AT UPPER O/B CORNER OF L-1 WINDSHIELD. REPAIRED SKIN IAW ECRA 5330-02838. - [SDR CALA9900721](https://openairdocs.org/sdr/CALA9900721), Jun 25, 1999: FRAME. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN BELTFRAME AT STRINGER 16R AFT OF STA 500C. THE CRACKED SECTION OF FRAME WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 53-00- - [SDR CALA9900719](https://openairdocs.org/sdr/CALA9900719), Jun 24, 1999: FLOORBEAM. CORRODED. INSPECTION FOUND CABIN FLOORBEAM CORRODED AT STA 294, RBL 35. THE CORROSION WAS REMOVED AND A NEW SECTION OF FLOORBEAM WAS SPLICED IN IAW SRM 53-10-51, FIGURE 2 - [SDR CALA9900720](https://openairdocs.org/sdr/CALA9900720), Jun 23, 1999: STRINGER. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN STRINGER 4L AT STA 907. THE STRINGER WAS REMOVED AND REPLACED IAW SRM 51-10-2. - [SDR CALA9900716](https://openairdocs.org/sdr/CALA9900716), Jun 23, 1999: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT STA 1016. REPAIRED IAW ECRA 5310-03851. - [SDR CALA9900631](https://openairdocs.org/sdr/CALA9900631), Jun 3, 1999: TORSION LINK. BROKEN. ON LANDING ROLL AT APPROXIMATELY 70 KNOTS WITH NORMAL NOSE WHEEL TOUCHDOWN, A VIOLENT SHIMMY WAS FELT ON RUNWAY UNTIL AIRCRAFT MADE A COMPLETE AND SAFE STOP. TH - [SDR CALA9701251](https://openairdocs.org/sdr/CALA9701251), Aug 29, 1997: CIRCUIT CARD. INOPERATIVE. THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. THE GEAR LEVER WOULD NOT GO PAST THE OFF POSITION. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT IN - [SDR CALA9701090](https://openairdocs.org/sdr/CALA9701090), Jul 8, 1997: SKIN. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN LEFT ENGINE PYLON SKIN AT PANEL NR 5724. REPAIRED IAW ECRA 5430-01204. All 68: https://openairdocs.org/deregistered/N60312-2006-04-03/reports.md ## NTSB investigations (1) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB MIA95LA133](https://openairdocs.org/ntsb/MIA95LA133), May 19, 1995: Boeing 737-300 (N60312), Tallahassee, FL, no damage. Probable cause: THE FAILURE OF A PASSENGER TO COMPLY WITH FLIGHT CREW INSTRUCTIONS TO REMAIN SEATED WITH HER SEAT BELT FASTENED WHICH RESULTED IN HER BEING INJURED WHILE WALKING IN THE AISLE DURING A TURBULENCE… ## FAA accident and incident reports (4) 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 19990603026779I](https://openairdocs.org/incident/19990603026779I), Jun 3, 1999: Boeing 7373T0 (N60312), Indianapolis, IN. On 6/3/99 at 2007Z Continental F1682 enroute from hou to ind on runway 5R. On the rollout at 70KNTS the captain experienced severe vibration. The left bolt… - [Incident 19970530021049I](https://openairdocs.org/incident/19970530021049I), May 30, 1997: Boeing 7373T0 (N60312), Los Angeles, CA, Substantial damage. During pushback struck stabilizer of parked 757. Tug operator careless. Wing walkers not in place. Suspended. - [Accident 19950519013739A](https://openairdocs.org/incident/19950519013739A), May 19, 1995: Boeing 737300 (N60312), Tallahassee, FL. Encountered severe turbulence at FL290. Seat belt sign on. Passenger injured walking to lavatory. - [Incident 19870901055829I](https://openairdocs.org/incident/19870901055829I), Sep 1, 1987: Boeing 7373TO (N60312), Washington, DC. The fire warning activated on climbout. A safe return was made. Found a loose connector and chaffing in the loop. ## Other aircraft with N60312 - [Cancelled 2009-07-01](https://openairdocs.org/deregistered/N60312-2009-07-01): Hawker Beechcraft B200, S/N BB-2012, built 2009. Exported to Australia. Owner: [Wells Fargo Bank Northwest Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20BANK%20NORTHWEST%20NA%20TRUSTEE), [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City) --- 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.