# N12327: 1986 Boeing 737-3TO, registration cancelled 2012-02-07 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: February 7, 2012 - Status when cancelled: Sale reported - 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: 23457 - Year built: 1986 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: June 12, 1986 - Last registry action: December 20, 2010 - Mode S code: A06195 - Location: [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis) - Owner type: Individual - Owner's area on the map: 35.0351° N, 89.9272° W: Placed by OpenAirDocs at the center of ZIP code 38118, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N12327 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=12327 - Page: https://openairdocs.org/deregistered/N12327-2012-02-07 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 737-3TO: https://openairdocs.org/model/boeing-737-3to.md ## Service difficulty reports (72, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CALA0700611](https://openairdocs.org/sdr/CALA0700611), Oct 25, 2007: SKIN. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN FUSELAGE SKIN AT STA 727E + 3, S23L. REPAIRED IAW SRM 53-00-01, REPAIR 31, FIGURE 201, PROCEDURE 5. - [SDR CALA0700610](https://openairdocs.org/sdr/CALA0700610), Oct 25, 2007: SKIN. CRACKED. INSPECTION FOUND A .75 INCH CRACK IN FUSELAGE SKIN THREE INCHES AFT OF OF STA 727E AND JUST BELOW STRINGER 23R. REPAIRED IAW ECRA 5331-01359. - [SDR CALA0700609](https://openairdocs.org/sdr/CALA0700609), Oct 25, 2007: SKIN. CRACKED. INSPECTION FOUND A 3 INCH CRACK IN FUSELAGE SKIN AT STA 727D, S23R BELOW EMERGENCY LIGHT. REPAIRED IAW ECRA 5331-01359. - [SDR CALA0700007](https://openairdocs.org/sdr/CALA0700007), Jan 4, 2007: STRINGER. CORRODED. INSPECTION FOUND STRINGER 27L CORRODED IN FORWARD BAGGAGE BIN AT STA 500A+10 TO 500C. THE CORRODED STRINGER SECTION WAS REMOVED AND A NEW SECTION WAS INSTALLED - [SDR CALA0700006](https://openairdocs.org/sdr/CALA0700006), Jan 4, 2007: KEELBEAM. CORRODED. INSPECTION FOUND FUSELAGE SKIN BULGING AT S28L BETWEEN STA 500C AND 500D, 6 INCHES LEFT OF AIRCRAFT CENTERLINE. REPLACED FORWARD SECTION OF LT KEEL BEAM IAW SRM - [SDR CALA0700002](https://openairdocs.org/sdr/CALA0700002), Jan 3, 2007: ANGLE. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN ANGLE AT R-1 DOOR TORQUE BOX UPPER FORWARD ATTACH HOLES, NEAREST TORQUE TUBE. THE ANGLE WAS REPLACED IAW SRM 51-10-02. - [SDR CALA0600548](https://openairdocs.org/sdr/CALA0600548), Dec 31, 2006: DOOR FRAME. CRACKED. INSPECTION FOUND A 1.5 INCH CRACK AT LOWER STOP PAD BRACKET OF FORWARD CARGO DOOR CUTOUT AFT FRAME, STA 493. THE FRAME WAS REPLACED IAW SRM 51-40-02 AND BOEING - [SDR CALA0500082](https://openairdocs.org/sdr/CALA0500082), Mar 17, 2005: ACTUATOR. INOPERATIVE. CREW REPORTED THAT THE NOSE LANDING GEAR REQUIRED A MANUAL EXTENSION ON APPROACH TO DTW. EXTENSIVE TROUBLESHOOTING WAS PERFORMED. MAINTENANCE FOUND THAT THE NLG - [SDR CALA0500058](https://openairdocs.org/sdr/CALA0500058), Feb 23, 2005: ACTUATOR. MALFUNCTIONED. THE NOSE GEAR UNSAFE LIGHT ILLUMINATED WHEN GEAR WAS EXTENDED ON APPROACH TO EWR. THE GEAR WAS CYCLED DURING A GO-AROUND AND THREE GREEN SAFE GEAR LIGHTS ILLUMI - [SDR CALA0400739](https://openairdocs.org/sdr/CALA0400739), Dec 7, 2004: ACTUATOR. INOPERATIVE. THE RED NOSE GEAR UNSAFE LIGHT ILLUMINATED AND THE NOSE GEAR WOULD NOT EXTEND WHEN GEAR HANDLE WAS LOWERED ON APPROACH TO IAH. THE GEAR WAS CYCLED DURING A GO-A - [SDR CALA0400688](https://openairdocs.org/sdr/CALA0400688), Oct 28, 2004: SKIN. CRACKED. INSPECTION FOUND A .25 INCH CRACK IN NR 3 SLAT SKIN BELOW ACTUATOR. A DOUBLER WAS INSTALLED ON LOWER SKIN IAW SRM 57-43-01. - [SDR CALA0400687](https://openairdocs.org/sdr/CALA0400687), Oct 24, 2004: FLOORBEAM. CORRODED. INSPECTION FOUND UPPER FLANGE OF FLOORBEAM CORRODED AT STA 328, LBL 6 TO RBL 6. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED AND REPLACED IAW SRM 53-10-51. - [SDR CALA0400686](https://openairdocs.org/sdr/CALA0400686), Oct 23, 2004: FLOORBEAM. CORRODED. INSPECTION FOUND UPPER FLANGE OF FLOORBEAM CORRODED AT STA 344, RBL 45 TO LBL 12. THE CORRODED AREA OF FLOORBEAM UPPER CHORD WAS REMOVED AND A NEW UPPER CHORD A - [SDR CALA0400684](https://openairdocs.org/sdr/CALA0400684), Oct 22, 2004: FLOORBEAM. CORRODED. INSPECTION FOUND THE UPPER FLANGE OF FLOORBEAM CORRODED AT NUT PLATE HOLE, STA 312, RBL 8. A FLOORBEAM REPAIR WAS INSTALLED IAW SRM 53-10-51. - [SDR CALA0400680](https://openairdocs.org/sdr/CALA0400680), Oct 19, 2004: FLOORBOARD. CORRODED. INSPECTION FOUND UPPER AFT FLANGE OF CABIN FLOORBOARD CORRODED AT NUT PLATE HOLE, STA 360, RBL 2. THE CORROSION WAS REMOVED AND A REPAIR STRAP WAS INSTALLED IAW - [SDR CALA0400580](https://openairdocs.org/sdr/CALA0400580), Jul 19, 2004: VALVE. INOPERATIVE. THE NOSE GEAR DID NOT EXTEND ON FIRST ATTEMPT ON APPROACH INTO IAH. A MANUAL EXTENSION WAS PERFORMED AND THE NOSE GEAR SHOWED DOWN AND LOCKED. THE AIRCRAFT LAND - [SDR CALA0400569](https://openairdocs.org/sdr/CALA0400569), Jul 8, 2004: ACTUATOR. INOPERATIVE. THE NOSE LANDING GEAR DID NOT EXTEND ON FIRST ATTEMPT ON APPROACH INTO IAH. THE RED UNSAFE LIGHT WAS ILLUMINATED. THE GEAR WAS CYCLED AND THE NLG EXTENDED NORMA - [SDR CALA0400555](https://openairdocs.org/sdr/CALA0400555), Jun 28, 2004: ACTUATOR. INOPERATIVE. THE NOSE GEAR DID NOT EXTEND INITIALLY WHEN THE GEAR WAS SELECTED DOWN ON APPROACH INTO IAH. THE GEAR WAS CYCLED RESULTING IN NORMAL EXTENSION AND INDICATIONS. - [SDR CALA0400220](https://openairdocs.org/sdr/CALA0400220), Mar 6, 2004: ENGINE. MALFUNCTIONED. THE NR 1 ENGINE EXPERIENCED A POWER LOSS AT CRUISE WHILE EN ROUTE FROM MCO TO CLE. THE AIRCRAFT WAS DIVERTED TO ATL WHERE IT LANDED WITHOUT INCIDENT. THE NR 1 E - [SDR CALA0300120](https://openairdocs.org/sdr/CALA0300120), Mar 19, 2003: SKIN. CRACKED. INSPECTION FOUND A 5" CRACK IN SKIN AT AFT CARGO DOOR INSIDE INSPECTION HOLE ABOVE HANDLE BOX. A DOUBLER WAS INSTALLED IAW ECRA 5232-01024. - [SDR CALA0200588](https://openairdocs.org/sdr/CALA0200588), Dec 16, 2002: SKIN. CRACKED. INSPECTION FOUND A 2.25" CRACK IN L/H FUSELAGE SKIN ABOUT TWO FEET AFT OF EMERGENCY LIGHT, AFT OF LEFT WHEEL WELL, STA 727E, S24L. REPAIRED IAW ECRA 5330-03188. - [SDR CALA0200506](https://openairdocs.org/sdr/CALA0200506), Oct 25, 2002: BALLAST. SMOKE IN AFT LAVATORY. LEFT AFT LAVATORY MIRROR CIRCUIT BREAKER OUT. FOUND BREAKER FOR LIGHTS POPPED. BALLAST BURNT. REMOVED AND REPLACED BALLAST. - [SDR CALA0001968](https://openairdocs.org/sdr/CALA0001968), Dec 20, 2000: SKIN. CRACKED. INSPECTION FOUND C-1 DOOR INNER SKIN CRACKED AROUND LIGHTENING HOLES. THE CRACKS WERE 1/2 TO 1 INCH LONG. THE SKIN WAS REPAIRED BY INSTALLING DOUBLERS IAW ECRA - [SDR CALA0001967](https://openairdocs.org/sdr/CALA0001967), Dec 20, 2000: SKIN. DENTED. INSPECTION FOUND C-1 DOOR SKIN DENTED. THE DOOR SKIN WAS REMOVED AND REPLACED IAW OHM 52-36-02 AND DRAWING 65-46921. - [SDR CALA0001966](https://openairdocs.org/sdr/CALA0001966), Dec 20, 2000: PAN. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN C-1 DOOR LOWER FORWARD DOOR PAN. THE LOWER FORWARD DOOR PAN WAS REMOVED AND REPLACED IAW OHM 52-36 AND DRAWING 65-46821. - [SDR CALA0001938](https://openairdocs.org/sdr/CALA0001938), Dec 17, 2000: SKIN. CRACKED. INSPECTION FOUND A 1/4 INCH CRACK IN NR 2 OB PYLON SKIN AFT OF UPPER T/R ABOVE PANEL 5824R. A DOUBLER AND FREEZE PLUGS WERE INSTALLED IAW SRM 5450-01330 AND ECR - [SDR CALA0001911](https://openairdocs.org/sdr/CALA0001911), Dec 13, 2000: CARGO TRACK. CORRODED. INSPECTION FOUND TIE DOWN RAIL CORRODED AT STA 500D-520 BETWEEN STRINGER 26L AND 27L. THE CORRODED SECTION OF TIE DOWN RAIL WAS REMOVED AND REPLACED IAW SRM 53- - [SDR CALA0001910](https://openairdocs.org/sdr/CALA0001910), Dec 13, 2000: PANEL. CORRODED. INSPECTION FOUND TRANSITION PANELS CORRODED AT STA 420, S26R, STA 492-520, S26L, STA 380-492, S26L, AND STA 500C +18R. THE PANELS WERE REMOVED AND REPLACED IAW - [SDR CALA0001906](https://openairdocs.org/sdr/CALA0001906), Dec 13, 2000: WEB. CRACKED. INSPECTION FOUND A 5" CRACK IN WEB AT STA 500C, LONGERON 26L IN FORWARD CARGO AREA. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-10-02. - [SDR CALA0001905](https://openairdocs.org/sdr/CALA0001905), Dec 13, 2000: WEB. CRACKED. INSPECTION FOUND A 12 INCH CRACK IN WEB AT LT SIDE OF FORWARD CARO AREA BETWEEN STA 500A AND 500B, STRINGER 25L. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-10- - [SDR CALA0001899](https://openairdocs.org/sdr/CALA0001899), Dec 12, 2000: PANEL. CORRODED. INSPECTION FOUND L/H TRANSITION PANEL CORRODED AROUND NUTPLATE HOLES AT STA 877-947. A NEW TRANSITION PANEL WAS INSTALLED IAW SRM 51-10-2. - [SDR CALA0001879](https://openairdocs.org/sdr/CALA0001879), Dec 11, 2000: SKIN. CRACKED. INSPECTION FOUND A 3 INCH CRACK IN KEEL BEAM LOWER SKIN AT STA 706, LBL 6, WL 148.5. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-60-12, FIGURE 202, SHEET 3. - [SDR CALA0001875](https://openairdocs.org/sdr/CALA0001875), Dec 9, 2000: SKIN. DENTED. INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 338-353 BETWEEN STRINGERS 19R AND 20R. THE DENTED AREA WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 53-00-01, FIG - [SDR CALA0001874](https://openairdocs.org/sdr/CALA0001874), Dec 8, 2000: STRINGER. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN STRINGER 14L AT BS 360. THE STRINGER WAS REPLACED IAW SRM 51-10-02. - [SDR CALA0001865](https://openairdocs.org/sdr/CALA0001865), Dec 5, 2000: SUPPORT. CORRODED. INSPECTION FOUND LT DIAGONAL SUPPORT CORRODED AT STA 986-1016. A NEW DIAGONAL SUPPORT WAS INSTALLED IAW SRM 51-10-02. - [SDR CALA0001861](https://openairdocs.org/sdr/CALA0001861), Dec 4, 2000: INTERCOSTAL. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN INTERCOSTAL AFT OF BS 302 AT STRINGER 4L. A NEW STRAP AND INTERCOSTAL WAS INSTALLED IAW SRM 51-10-2. - [SDR CALA0001860](https://openairdocs.org/sdr/CALA0001860), Dec 4, 2000: FLOOR SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 986.5-1006, RBL 42. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-10-02. - [SDR CALA0001859](https://openairdocs.org/sdr/CALA0001859), Dec 4, 2000: SKIN. DENTED. INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 388, S16L. A SKIN REPAIR WAS INSTALLED IAW SRM 53-00-01, FIGURE 201 AND 51-40-03, PARAGRAPH 4D. - [SDR CALA0001858](https://openairdocs.org/sdr/CALA0001858), Dec 4, 2000: ANGLE. CORRODED. INSPECTION FOUND RT Z-ANGLE CORRODED BETWEEN STA 947 AND 998. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-02 AND 51-40-02. - [SDR CALA0001857](https://openairdocs.org/sdr/CALA0001857), Dec 4, 2000: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM UPPER CHORD CORRODED AROUND FASTENERS AT STA 1016, RBL 5 TO RBL 6. A FLOORBEAM UPPER CHORD REPLACEMENT SECTION WAS INSTALLED IAW ECRA - [SDR CALA0001856](https://openairdocs.org/sdr/CALA0001856), Dec 4, 2000: WEB. CORRODED. INSPECTION FOUND WEB CORRODED BETWEEN STA 1006 AND 1016, RBL 32. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-10-02. - [SDR CALA0001854](https://openairdocs.org/sdr/CALA0001854), Dec 3, 2000: SPINDLE. CORRODED. INSPECTION FOUND RT WING O/B MID NR 7 AND NR 8 FLAP MAIN CARRIAGE SPINDLES CORRODED. THE NR 7 AND NR 8 FLAP MAIN CARRIAGES WERE REMOVED AND REPLACED IAW MM 27-5 - [SDR CALA0001853](https://openairdocs.org/sdr/CALA0001853), Dec 2, 2000: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT STA 1006, LBL 6 TO LBL 27. THE CORROSION WAS REMOVED AND A REPAIR STRAP WAS INSTALLED IAW SRM 53-00-51, FIGURE 203. - [SDR CALA0001849](https://openairdocs.org/sdr/CALA0001849), Dec 1, 2000: SPLICE. CRACKED. INSPECTION FOUND 1.25" CRACK IN STRINGER SPLICE AT BS 907, S4R. THE STRINGER SPLICE WAS REMOVED AND REPLACED IAW SRM 51-10-2. - [SDR CALA0001843](https://openairdocs.org/sdr/CALA0001843), Dec 1, 2000: SEAT TRACK. CORRODED. INSPECTION FOUND SEAT TRACK CORRODED AT STA 924-933, LBL 46. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-00-52, FIGURE 204, SHEETS 1-4. - [SDR CALA9601902](https://openairdocs.org/sdr/CALA9601902), Dec 23, 1996: SKIN. CRACKED. INSPECTION FOUND A .5 INCH CRACK AT RIVET IN LOWER SKIN OF NR 6 SLAT AT ACTUATOR. THE SKIN WAS REPAIRED IAW ECRA 5750-01159. - [SDR CALA9601918](https://openairdocs.org/sdr/CALA9601918), Dec 19, 1996: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT STA 986, R-2 DOOR TO L-2 DOOR. A FLOORBEAM UPPER CHORD REPAIR WAS INSTALLED IAW ECRA 5310-03385. - [SDR CALA9601903](https://openairdocs.org/sdr/CALA9601903), Dec 12, 1996: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT STA 947, RBL 5 AND LBL 5. A REPAIR WAS INSTALLED IAW SRM 53-50-01. - [SDR CALA9601921](https://openairdocs.org/sdr/CALA9601921), Dec 11, 1996: SUPPORT. CORRODED. INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT STA 951, 12 INCHES RIGHT OF CENTER AND CABIN FLOOR SUPPORT CORRODED AT STA 951, 20 INCHES FROM RIGHT SIDEWALL. - [SDR CALA9601920](https://openairdocs.org/sdr/CALA9601920), Dec 11, 1996: SUPPORT. CORRODED. INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED FROM STA 947.5 TO 967, 18 INCHES RIGHT OF CENTER AND CABIN FLOOR SUPPORT CORRODED FROM 967 TO 986.5, 18 INCHES LEF All 72: https://openairdocs.org/deregistered/N12327-2012-02-07/reports.md ## FAA accident and incident reports (1) 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 19901025052839I](https://openairdocs.org/incident/19901025052839I), Oct 25, 1990: Boeing 7373T0 (N12327), Orlando, FL, Minor damage. Lost right main outboard wheel assembly on takeoff. Diverted to Orlando. Wrong inboard bearing installed. ## Other aircraft with N12327 - [Registered now](https://openairdocs.org/aircraft/N12327): Yuneec H520, S/N YU20310019B11A01 - [Cancelled (date not recorded)](https://openairdocs.org/deregistered/N12327-undated): Cessna 172M, S/N 17261930. Owner: [Cessna Aircraft Corp](https://openairdocs.org/faa-owner/CESSNA%20AIRCRAFT%20CORP), [Wichita, KS](https://openairdocs.org/faa-place/KS/Wichita) --- 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.