# N16301: 1985 Boeing 737-3TO, registration cancelled 2013-03-21

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: March 21, 2013
- Status when cancelled: Third renewal notice
- 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: 23352
- Year built: 1985
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 17, 1985
- Certificate issued: April 7, 2006
- Last registry action: April 21, 2009
- Mode S code: A0FF45
- Owner when cancelled: [Continental Airlines Inc](https://openairdocs.org/faa-owner/CONTINENTAL%20AIRLINES%20INC)
- Location: [Houston, TX](https://openairdocs.org/faa-place/TX/Houston)
- Owner type: Corporation
- Owner's area on the map: 29.7568° N, 95.3657° W: Placed by OpenAirDocs at the center of ZIP code 77002, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N16301
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=16301
- Page: https://openairdocs.org/deregistered/N16301-2013-03-21

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 737-3TO: https://openairdocs.org/model/boeing-737-3to.md

## Service difficulty reports (89, newest 50)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR CALA0800546](https://openairdocs.org/sdr/CALA0800546), Jun 5, 2008: MEGAPHONE. DEFECTIVE. A/C MEGAPHONE MISSING VOLUME KNOB AND LOW IN VOLUME. REPLACED MEGAPHONE, OPS CHECK GOOD.
- [SDR CALA0800139](https://openairdocs.org/sdr/CALA0800139), Feb 14, 2008: SKIN. CRACKED. STA 747 ABOVE STRINGER 24 FOUND 1.8" LONG CRACK WHILE PERFORMING C-SCAN INSPECTION. REPAIRED FUSELAGE PER SRM 53-00-01 REPAIR 31 DETAIL X.
- [SDR CALA0700702](https://openairdocs.org/sdr/CALA0700702), Nov 27, 2007: SKIN. CRACKED. FUSE SKIN CRACK INDICATION RT SIDE 39 INCHES AFT OF AFT BIN DOOR FRAME & 30 INCHES ABOVE LAP SEAM. COMPLETED SKIN REPAIR 31 PER SRM 53-00-01 AND REPAIR DEVIATIO
- [SDR CALA0700699](https://openairdocs.org/sdr/CALA0700699), Nov 25, 2007: SKIN. CRACKED. CRACK IN FUSELAGE SKIN 10 INCHES ABOVE LAP JOINT AND 11 INCHES AFT OF AFT UPPER BODY FAIRING RIGHT SIDE AT STATION 727A AND STRINGER S-19R. REPAIRED FUSELAGE SK
- [SDR CALA0700564](https://openairdocs.org/sdr/CALA0700564), Oct 4, 2007: REFLECTOR. CONTAMINATED. THE L-1 DOOR EXTERIOR EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. THE EMERGENCY LIGHT REFLECTOR ASSEMBLY WAS REMOVED AND REPLACED IAW MM 33-51-02 AND 33-51-11.
- [SDR CALA0700443](https://openairdocs.org/sdr/CALA0700443), Aug 18, 2007: FRAME. CORRODED. INSPECTION FOUND FORWARD CORROSION AT ACCESS DOOR AFT FRAME IN BULKHEAD CHORD, BS 227.8 BETWEEN LBL 5.7 AND RBL 5.7. REPAIRED IAW ECRA 5311-01353.
- [SDR CALA0700115](https://openairdocs.org/sdr/CALA0700115), Mar 2, 2007: DRAG ANGLE. CRACKED. LEFT UPPER WING TO BODY DRAG ANGLE CRACKED FWD OF A/C DOOR 3302L. REPAIRED IAW ECRA 5311-01300.
- [SDR CALA0700114](https://openairdocs.org/sdr/CALA0700114), Mar 2, 2007: FRAME. CRACKED. LEFT MAIN FRAME CRACKED AT STA 639. REPAIRED IAW ECRA 5311-01299.
- [SDR CALA0700113](https://openairdocs.org/sdr/CALA0700113), Mar 2, 2007: WEB. CRACKED. CRACKED AT WEB STA 639 ABOVE FLOOR LINE. REPAIRED IAW ECRA 5311-01299.
- [SDR CALA0700116](https://openairdocs.org/sdr/CALA0700116), Mar 1, 2007: FITTING. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN UPPER RADIUS OF FITTING AFT OF FRAME JUST BELOW STRINGER 17L AND CREASE BEAM AT STA 616. A NEW FITTING WAS INSTALLED IAW SRM
- [SDR CALA0700103](https://openairdocs.org/sdr/CALA0700103), Mar 1, 2007: BEAM. CRACKED. CRACKED L1 DOOR AFT SIDE OF THE THIRD FROM BOTTOM DOOR STOP CUTOUT. REPAIRED IAW ECRA 5210-01919.
- [SDR CALA0700102](https://openairdocs.org/sdr/CALA0700102), Feb 28, 2007: SKIN. CRACKED. A 2 INCH CRACK IN R1 DOOR AT THE LOWER BOTTOM CORNER. REPAIRED IAW ECRA 5331-01291.
- [SDR CALA0700101](https://openairdocs.org/sdr/CALA0700101), Feb 28, 2007: SKIN. CRACKED. A 3 INCH CRACK LOWER AFT FUSELAGE STA 727D AND 727E. REPAIRED IAW ECRA5331-01292.
- [SDR CALA0700100](https://openairdocs.org/sdr/CALA0700100), Feb 27, 2007: FRAME. CRACKED. AFT CARGO COMPARTMENT CRACKED ON FWD BULKHEAD FRAME. INSTALLED STIFFENER IAW SRM 51-10-02, 51-30-01, AND 51-40-02.
- [SDR CALA0700096](https://openairdocs.org/sdr/CALA0700096), Feb 25, 2007: FRAME. CORRODED. AFT CARGO FLOOR FRAME AT STA 747 IS CORRODED FROM STR 26L TO 26R. REPAIRED IAW SRM 53-00-07 DETAIL 2, 51-40-02 & 51-10-02.
- [SDR CALA0700094](https://openairdocs.org/sdr/CALA0700094), Feb 24, 2007: KEELBEAM. DAMAGED. LOWER FUSE SKIN BULGED BETWEEN RIVETS ALONG STRINGER 28R STA 500C TO 500D. REPAIRED KEEL BEAM IAW SRM 53-60-12.
- [SDR CALA0700093](https://openairdocs.org/sdr/CALA0700093), Feb 24, 2007: KEELBEAM. CORRODED. AFT CARGO COMPARTMENT CORRODED AT KEEL BEAM STA 727, LBL 6. REPAIRED IAW ECRA 5311-01293 AND 5311-01296.
- [SDR CALA0700092](https://openairdocs.org/sdr/CALA0700092), Feb 23, 2007: PAN. CRACKED. C2 DOOR FWD SIDE PAN CRACKED AT SPLICE POINT. INSTALLED NEW PAN IAW SRM 52-30-02.
- [SDR CALA0700091](https://openairdocs.org/sdr/CALA0700091), Feb 23, 2007: PAN. CRACKED. UPPER FWD PAN CRACKED AT FWD SPLICE. INSTALLED SERVICEABLE PAN.
- [SDR CALA0700089](https://openairdocs.org/sdr/CALA0700089), Feb 23, 2007: BULKHEAD. CORRODED. FWD APB LOWER CENTER SECTION WEB CORRODED. REPAIRED IAW ECRA 5311-01298.
- [SDR CALA0700088](https://openairdocs.org/sdr/CALA0700088), Feb 23, 2007: STRUCTURE. BULGED. FWD BAG BIN BULGED ALONG S28L FROM STA 500D 6 INCHES. REPAIRED IAW SRM 53-30-12.
- [SDR CALA0700090](https://openairdocs.org/sdr/CALA0700090), Feb 22, 2007: SUPPORT ANGLE. CRACKED. SUPPORT ANGLE CRACKED AT 360 AND STRINGER S11L. REPAIRED IAW ECRA 5311-01297.
- [SDR CALA0700083](https://openairdocs.org/sdr/CALA0700083), Feb 22, 2007: FRAME. CORRODED. INSPECTION FOUND AFT CARGO COMPARTMENT FLOOR FRAME CORRODED AT STA 847 BETWEEN STRINGERS 27L AND 27R, LBL 8 TO RBL 8. THE CORRODED SECTION OF FLOOR FRAME WAS RE
- [SDR CALA0700082](https://openairdocs.org/sdr/CALA0700082), Feb 21, 2007: STRINGER. CORRODED. INSPECTION FOUND LIGHT SURFACE CORROSION DOWN CENTER OF STRINGER 26L IN FORWARD BAGGAGE BIN AT STA 500D-520. THE STRINGER WAS REPAIRED IAW SRM 53-00-03.
- [SDR CALA0700081](https://openairdocs.org/sdr/CALA0700081), Feb 20, 2007: SKIN. CRACKED. INSPECTION FOUND A 0.75 INCH CRACK IN FUSELAGE SKIN AT R-2 DOOR FORWARD LOWER RADIUS, STA 947.5, S14R. A DOUBLER WAS INSTALLED IAW SRM 53-60-01, FIGURE 201.
- [SDR CALA0700075](https://openairdocs.org/sdr/CALA0700075), Feb 20, 2007: FRAME. CORRODED. INSPECTION FOUND AFT CARGO COMPARTMENT FRAME CORRODED AT CENTER FLOOR AREA, STA 867, S28L TO S28R. THE CORRODED SECTION OF FRAME WAS TRIMMED OUT AND A REPAIR DO
- [SDR CALA0700067](https://openairdocs.org/sdr/CALA0700067), Feb 15, 2007: STIFFENER. CORRODED. INSPECTION FOUND TWO CHANNEL STIFFENERS CORRODED ON FORWARD FACE OF APB LOWER SECTION. THE STIFFENERS WERE REMOVED AND NEW SECTIONS WERE SPLICED IN IAW BOEING D
- [SDR CALA0700066](https://openairdocs.org/sdr/CALA0700066), Feb 15, 2007: STRINGER. CORRODED. INSPECTION FOUND CENTER OF STRINGER 27L CORRODED AROUND NUT PLATE IN FORWARD BAGGAGE BIN AT STA 500D. THE STRINGER WAS REPAIRED IAW SRM 53-00-03.
- [SDR CALA0700062](https://openairdocs.org/sdr/CALA0700062), Feb 11, 2007: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT STA 947, RBL 6 TO LBL 6. A FLOORBEAM REPAIR WAS INSTALLED IAW SRM 53-00-51, FIGURE 201.
- [SDR CALA0700061](https://openairdocs.org/sdr/CALA0700061), Feb 11, 2007: FRAME. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN RT MAIN FRAME AT STA 616 BELOW FLOOR LINE. THE CRACKED AREA OF FRAME WAS REMOVED AND A REPAIR ANGLE WAS INSTALLED IAW ECRA 53
- [SDR CALA0700060](https://openairdocs.org/sdr/CALA0700060), Feb 10, 2007: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT NUT PLATES ON TOP AND BOTTOM, STA 1016, LBL 6 TO LBL 34. THE FLOORBEAM CHORD WAS REMOVED AND REPLACED IAW ECRA 5310-03851
- [SDR CALA0700059](https://openairdocs.org/sdr/CALA0700059), Feb 9, 2007: FRAME. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN LT FRAME AT STA 616, S17L TO S18L BELOW FLOOR LINE. THE CRACKED AREA OF FRAME WAS REMOVED AND A REPAIR ANGLE AND FILLER WAS I
- [SDR CALA0700054](https://openairdocs.org/sdr/CALA0700054), Feb 6, 2007: FRAME. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN FRAME AT STA 597, S13L. THE FRAME WAS REPAIRED IAW SRM 53-00-07, PAGE 203, FIGURE 201.
- [SDR CALA0600511](https://openairdocs.org/sdr/CALA0600511), Dec 11, 2006: SKIN. CRACKED. INSPECTION FOUND A 1.5 INCH CRACK IN FUSELAGE SKIN AT STA 727A-727B, S22R TO S25R. REPAIRED IAW ECRA 5331-01283.
- [SDR CALA0600225](https://openairdocs.org/sdr/CALA0600225), Jun 26, 2006: FRAME. CORRODED. INSPECTION FOUND AFT CARGO DOOR FORWARD FRAME CORRODED. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-80-02.
- [SDR CALA0500132](https://openairdocs.org/sdr/CALA0500132), Apr 18, 2005: PANEL. CRACKED. FUSELAGE SKIN CRACKED AT STA 727D, STRINGER 23R. REPLACED PANEL PER ECRA 5331-01178A.
- [SDR CALA0500076](https://openairdocs.org/sdr/CALA0500076), Mar 11, 2005: SKIN. CRACKED. INSPECTION FOUND A 1.7 INCH CRACK IN FUSELAGE SKIN THREE INCHES AFT OF STA 727D JUST BELOW S23R ON BONDED DOUBLER LINE. THE CRACKED AREA WAS REMOVED AND A REPAI
- [SDR CALA0500066](https://openairdocs.org/sdr/CALA0500066), Mar 4, 2005: STIFFENER. CRACKED. INSPECTION FOUND 8 INCH CRACK IN STIFFENER FOR NR 3 VHF ANTENNA BETWEEN STA 727D AND 727E. A NEW STIFFENER WAS INSTALLED IAW SRM 51-40-2.
- [SDR CALA0300165](https://openairdocs.org/sdr/CALA0300165), Apr 1, 2003: SKIN. CRACKED. INSPECTION FOUND A 0.4 INCH CRACK IN SKIN AT UPPER FORWARD CORNER OF PILOT'S WINDOW CD POST AT BS 205, WL 238. REPAIRED IAW SRM 53-10-01, FIGURE 210.
- [SDR CALA0300164](https://openairdocs.org/sdr/CALA0300164), Apr 1, 2003: FLOORBEAM. CORRODED. INSPECTION FOUND TOP SURFACE OF TOP CAP OF LATERAL FLOORBEAM AT STA 1016 CORRODED AT LT SIDE AREA UNDER LAV TANK. REPAIRED IAW ECRA 5310-03851.
- [SDR CALA0300163](https://openairdocs.org/sdr/CALA0300163), Apr 1, 2003: SKIN. DENTED. INSPECTION FOUND R-2 DOOR EXTERNAL SKIN DENTED AT FORWARD LOWER CORNER. REPAIRED IAW SRM 52-00-01.
- [SDR CALA0300162](https://openairdocs.org/sdr/CALA0300162), Apr 1, 2003: BULKHEAD. CRACKED. INSPECTION FOUND TWO 0.1 INCH CRACKS AT RIVET HOLES IN AFT PRESSURE BULKHEAD BETWEEN S6L AND S7L AT BS 1016. REPAIRED IAW SRM 53-80-08, FIGURE 202 AND 207.
- [SDR CALA0300161](https://openairdocs.org/sdr/CALA0300161), Apr 1, 2003: STRINGER. CORRODED. INSPECTION FOUND AFT CARGO COMPARTMENT STRINGER 26R CORRODED AT BS 1010. REPAIRED IAW SRM 51-40-02 AND B737-300 AMM 20-50-11.
- [SDR CALA0300157](https://openairdocs.org/sdr/CALA0300157), Mar 31, 2003: FRAME. CORRODED. INSPECTION FOUND AFT CARGO COMPARTMENT LOWER LOBE INTERIOR FRAME CORRODED AT BS 847 BETWEEN S28L AND S28R. REPAIRED IAW SRM 53-00-07, FIGURE 208.
- [SDR CALA0300156](https://openairdocs.org/sdr/CALA0300156), Mar 31, 2003: FLOORBEAM. CORRODED. INSPECTION FOUND CABIN FLOORBEAM CORRODED AT BS 312 AND 320, R-1 DOOR THRESHOLD. REPAIRED WITH REPLACEMENT PART IAW SRM 51-40-02.
- [SDR CALA0300155](https://openairdocs.org/sdr/CALA0300155), Mar 31, 2003: SKIN. TORN. INSPECTION FOUND FORWARD CARGO DOOR SKIN CUTOUT TORN AT BS 440, S24R. THE SKIN WAS REPAIRED IAW ECRA 5330-03222.
- [SDR CALA0300154](https://openairdocs.org/sdr/CALA0300154), Mar 28, 2003: SKIN. GOUGED. INSPECTION FOUND LT HORIZONTAL STABILIZER LEADING EDGE SKIN GOUGED AT STA 176.50. REPAIRED IAW ECRA 5515-01008.
- [SDR CALA0300153](https://openairdocs.org/sdr/CALA0300153), Mar 28, 2003: SKIN. DENTED. INSPECTION FOUND VERTICAL STABILIZER LEADING EDGE SKIN DENTED AT L/E STA 132.92 + 6 AND AT 226.54 + 1.3. THE DENTED AREAS WERE REPAIRED IAW SRM 55-30-01, FIGURE
- [SDR CALA0300152](https://openairdocs.org/sdr/CALA0300152), Mar 28, 2003: STRINGER. PUNCTURED. INSPECTION FOUND STRINGER 24R PUNCTURED AT BS 363. REPAIRED IAW SRM 53-00-03, FIGURE 201.
- [SDR CALA0300151](https://openairdocs.org/sdr/CALA0300151), Mar 28, 2003: STRINGER. CORRODED. INSPECTION FOUND STRINGER 25R CORRODED AT BS 364 AND S24R WAS CORRODED AT BS 360. REPAIRED IAW SRM 53-00-03, FIGURE 201.

All 89: https://openairdocs.org/deregistered/N16301-2013-03-21/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 19860521029219I](https://openairdocs.org/incident/19860521029219I), May 21, 1986: Boeing 7373TO (N16301), Salt Lake City, UT. Fire in tail pipe after balked start. Passenger jumped from galley door during jetway evacuation. Replaced igniter.

## Other aircraft with N16301

- [Cancelled 1948-08-04](https://openairdocs.org/deregistered/N16301-1948-08-04): Piper J-2, S/N 534. Owner: [Schwuchow Raymond](https://openairdocs.org/faa-owner/SCHWUCHOW%20RAYMOND), [Chicago, IL](https://openairdocs.org/faa-place/IL/Chicago)

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