# N372PA: 1987 Boeing 737-306, registration cancelled 2006-12-06 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: December 6, 2006 - Exported to: Bermuda - Status when cancelled: Valid registration - Airframe: [Boeing 737-306](https://openairdocs.org/model/boeing-737-306) (registry code 13844BG) - 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: 23546 - Year built: 1987 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: November 29, 2001 - Certificate issued: November 1, 2006 - Last registry action: November 13, 2006 - Mode S code: A43C7F - Owner when cancelled: [Wells Fargo Bank Northwest Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20BANK%20NORTHWEST%20NA%20TRUSTEE) - Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City) - Owner type: Corporation - Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N372PA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=372PA - Page: https://openairdocs.org/deregistered/N372PA-2006-12-06 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 737-306: https://openairdocs.org/model/boeing-737-306.md ## Service difficulty reports (84, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR PIDA06027](https://openairdocs.org/sdr/PIDA06027), Feb 24, 2006: WINDOW POST. CRACKED. LEFT SIDE COCKPIT WINDOW POST CRACKED AT THE UPPER OUTBOARD CORNER. REPAIRED PER SRM 53-10-01 FIGURE 201 DETAIL II. - [SDR PIDA06025](https://openairdocs.org/sdr/PIDA06025), Feb 24, 2006: STRUCTURE. CRACKED. LEFT ENGINE PYLON PANEL 5724 LT HAS A SMALL CRACK AT THE EDGE OF THE CUTOUT. REPAIRED CRACK IN THE UPPER FORWARD CORNER OF THE CUTOUT PER BOEING SB 737-54-1032. - [SDR PIDA06024](https://openairdocs.org/sdr/PIDA06024), Feb 20, 2006: STRUCTURE. CRACKED. NR 2 PYLON OUTBOARD MID ACCESS CUTOUT FOR PANEL 5824R IS CRACKED AT THE UPPER FORWARD AND LOWER AFT CORNERS. REPAIRED PER BOEING SB 737-54-1032. - [SDR PIDA06023](https://openairdocs.org/sdr/PIDA06023), Feb 17, 2006: FAIRING. CRACKED. FAIRING ON TOP OF LEFT WING AT NR 3 FLAP TRACK HAS A CRACK AT THE FORWARD EDGE. REPLACED FAIRING PER SRM 51-00-05 AND 51-40-02. - [SDR PIDA20050063](https://openairdocs.org/sdr/PIDA20050063), Aug 9, 2005: LAMP. INOPERATIVE. L1 DOOR EMERGENCY LIGHT ON EXTERIOR OF FUSELAGE INOP. RELAMPED L1 DOOR EXTERIOR LIGHT PER MM 33-50. OPS CHECKS GOOD. - [SDR 372PA0080](https://openairdocs.org/sdr/372PA0080), Mar 24, 2005: LIGHT. INOPERATIVE. RIGHT BULL NOSE EMERGENCY LIGHT (OVERHEAD BAGGAGE BIN) INOP. REPLACED EXIT LIGHT, OPS CHECKS GOOD. - [SDR 372PA0079](https://openairdocs.org/sdr/372PA0079), Nov 9, 2004: BULB. INOPERATIVE. L2 DOOR EMERGENCY LIGHT INOP AND LENS CRACKED. REPLACED BULB AND LENS. OPS CHECKS NORMAL. - [SDR 372PA0055](https://openairdocs.org/sdr/372PA0055), Sep 9, 2004: FLOORBEAM. CORRODED. AFT CABIN FLOORBEAM AT BS 947 HAS CORROSION AROUND NUT PLATE HOLES FROM LBL 46 TO RBL 46. REPLACED T-CAP PER SRM 53-00-51 AND SRM 53-60-51. - [SDR 372PA0052](https://openairdocs.org/sdr/372PA0052), Sep 9, 2004: PAN. CORRODED. AFT LAV SERVICE PANEL PAN HAS CORROSION AROUND DUMP SHOOT CONNECTION. REPLACED CORRODED CHANNELS P/N 69-36677-1 AND 69-36677-2 PER SRM 51-40-02 AND DRAWING 65-4 - [SDR 372PA0078](https://openairdocs.org/sdr/372PA0078), Sep 9, 2004: FRAME. CRACKED. FRAME CRACKED IN RADIUS AT BS 480 AT STR 25 LT. REPAIRED PER SRM 51-70-11. - [SDR 372PA0077](https://openairdocs.org/sdr/372PA0077), Sep 9, 2004: FRAME. CRACKED. FRAME CRACKED IN RADIUS AT BS 460 AT STR 25 LT. REPAIRED PER SRM 51-70-11. - [SDR 372PA0076](https://openairdocs.org/sdr/372PA0076), Sep 9, 2004: ANGLE. CRACKED. DRAG ANGLE CRACKED ABOVE RIGHT RAM AIR INLET. REPLACED ANGLE PER EA 53-235. - [SDR 372PA0074](https://openairdocs.org/sdr/372PA0074), Sep 9, 2004: FRAME. CRACKED. AFT CARGO AFT FRAME AT BS 847 AT STR 23 RT DOOR STOP ATTACH FITTING CRACKED. REPLACED FITTING PER SRM 51-10-2. - [SDR 372PA0073](https://openairdocs.org/sdr/372PA0073), Sep 9, 2004: INTERCOSTAL. CORRODED. INTERCOSTAL FROM BS 328 TO BS 344 AT RBL 12 HAS CORROSION. REPLACED INTERCOSTAL PER SRM 51-10-2. - [SDR 372PA0072](https://openairdocs.org/sdr/372PA0072), Sep 9, 2004: STRAP. CRACKED. STRAP ON LOWER SURFACE OF FLOORBEAMS CRACKED AT BS 312 AND BS 344 AT BL 0. REPLACED STRAP IAW SRM 51-10-2. - [SDR 372PA0071](https://openairdocs.org/sdr/372PA0071), Sep 9, 2004: STRAP. CRACKED. STRAP CRACKED ON LOWER SURFACE OF FLOORBEAMS AT BS 312 AND BS 344 AT RBL 32. REPLACED STRAP IAW SRM 51-10-2. - [SDR 372PA0070](https://openairdocs.org/sdr/372PA0070), Sep 9, 2004: ATTACH ANGLE. CRACKED. INTERCOSTAL ATTACH ANGLE CRACKED AFT SIDE OF BS 344 FLOORBEAM AT LBL 12. REPLACED ANGLE PER SRM 53-10-51, SRM 51-20-01 AND SRM 51-40-00. - [SDR 372PA0069](https://openairdocs.org/sdr/372PA0069), Sep 9, 2004: FLOORBEAM. CORRODED. SEVERAL AREAS OF CORROSION ON UPPER SURFACE OF FLOORBEAM AT BS 344. REPLACED SECTION OF (T) CAP IAW SRM 53-10-51. - [SDR 372PA0068](https://openairdocs.org/sdr/372PA0068), Sep 9, 2004: FLOORBEAM. CORRODED. UPPER SURFACE OF FLOORBEAM AT BS 312 HAS SEVERAL AREAS OF CORROSION. REPLACED SECTION OF T-CAP PER SRM 53-10-51. - [SDR 372PA0067](https://openairdocs.org/sdr/372PA0067), Sep 9, 2004: FLOORBEAM. CORRODED. UPPER SURFACE OF FLOORBEAM AT BS 294 HAS SEVERAL AREAS OF CORROSION. REPLACED T-CAP PER SRM 53-10-51 AND SRM 51-10-2. - [SDR 372PA0066](https://openairdocs.org/sdr/372PA0066), Sep 9, 2004: WEB. CORRODED. CLOSE OUT WEB ON FWD FRAME AT BS 794 HAS CORROSION FROM STR 25 RT TO STR 23 RT. REPLACED WEB PER SRM 53-60-15 AND SRM 51-70-13. - [SDR 372PA0065](https://openairdocs.org/sdr/372PA0065), Sep 9, 2004: SEAT TRACK. CORRODED. SEAT TRACK AT RBL 45 CORRODED IN NUMEROUS PLACES FROM BS 328 TO BS 480. REPLACED SEAT TRACK PER SRM 51-10-02, SRM 53-00-52, AND DWG 65-46814. - [SDR 372PA0064](https://openairdocs.org/sdr/372PA0064), Sep 9, 2004: SUPPORT ANGLE. CRACKED. AFT CARGO BIN BS 767 AT STR 19 LT UPPER SIDE WALL PANEL SUPPORT ANGLE CRACKED. REPLACED ANGLE PER SRM 51-10-02. - [SDR 372PA0063](https://openairdocs.org/sdr/372PA0063), Sep 9, 2004: WEB. CRACKED. FWD CARGO BIN WEB FROM BS 460 TO BS 480 AT STR 25 LT CRACKED. REPLACED INTERCOSTAL WEB PER SRM 51-10-02 AND SRM 51-20-01. - [SDR 372PA0062](https://openairdocs.org/sdr/372PA0062), Sep 9, 2004: FAILSAFE. CORRODED. FAILSAFE LINK BETWEEN BS 967 AND BS 986.5 AT LBL 46 CORRODED. REPLACED FAILSAFE LINK PER SRM 51-10-2. - [SDR 372PA0061](https://openairdocs.org/sdr/372PA0061), Sep 9, 2004: STRINGER. CORRODED. LOWER LOBE STR 26 RT CORRODED FROM BS 1006 TO BS 1016. REPLACED SECTION OF STRINGER PER DRAWING 65-45776-8 AND SRM 51-10-2. - [SDR 372PA0060](https://openairdocs.org/sdr/372PA0060), Sep 9, 2004: STRAP. CORRODED. FLOORBEAM STRAP AT BS 1016 HAS CORROSION AROUND NUT PLATE HOLES FROM RBL 7 TO LBL 7. REPLACED STRAP PER SRM 51-10-2 AND SRM 51-40-0. - [SDR 372PA0059](https://openairdocs.org/sdr/372PA0059), Sep 9, 2004: GALLEY TRACK. CORRODED. GALLEY SUPPORT AT BS 1016 HAS CORROSION AROUND NUT PLATE HOLES AT BL 0. REPLACED GALLEY SUPPORT PER SRM 51-10-2 AND SRM 51-40-00. - [SDR 372PA0058](https://openairdocs.org/sdr/372PA0058), Sep 9, 2004: FLOORBEAM. CORRODED. AFT CABIN FLOORBEAM AT BS 986.5 HAS CORROSION AROUND NUT PLATE HOLES FROM LBL 45 TO RBL 45. REPLACED T-CAP PER EA 53-234. - [SDR 372PA0057](https://openairdocs.org/sdr/372PA0057), Sep 9, 2004: INTERCOSTAL. CORRODED. INTERCOSTAL HAS CORROSION, AFT CABIN BS 967 TO BS 986.5 AT RBL 18. REPLACED INTERCOSTAL PER SRM 51-10-01. - [SDR 372PA0056](https://openairdocs.org/sdr/372PA0056), Sep 9, 2004: INTERCOSTAL. CORRODED. INTERCOSTAL HAS CORROSION, AFT CABIN FROM BS 967 TO BS 986.5 AT LBL18. REPLACED INTERCOSTAL PER SRM 51-10-01. - [SDR 372PA0054](https://openairdocs.org/sdr/372PA0054), Sep 9, 2004: ATTACH ANGLE. CRACKED. SIDEWALL ATTACH ANGLE CRACKED AT BS 767 LBL 54. REPLACED ANGLE PER SRM 51-10-02. - [SDR 372PA0053](https://openairdocs.org/sdr/372PA0053), Sep 9, 2004: SKIN. DAMAGED. OUTFLOW VALVE CUTOUT DOUBLER AT BS 986 BETWEEN STR 23 RT AND STR 24 RT HAS CORROSION. REPLACED DOUBLER PER SRM 51-20-01. - [SDR 372PA0051](https://openairdocs.org/sdr/372PA0051), Sep 9, 2004: ACOUSTIC LINER. CRACKED. NR 1 ENGINE FWD ACOUSTICAL PANEL AT 6 O'CLOCK POSITION CRACKED. REPLACED PANEL PER MM 72-33-02. - [SDR 372PA0050](https://openairdocs.org/sdr/372PA0050), Sep 9, 2004: SEAT TRACK. DAMAGED. SEAT TRACK DAMAGED AT BS 470 AT RBL 24. REPLACED DAMAGED SECTION OF SEAT TRACK PER SRM 53-00-52. - [SDR 372PA0049](https://openairdocs.org/sdr/372PA0049), Sep 9, 2004: ANGLE. CRACKED. ANGLE CRACKED ON I/B SIDE OF LEFT PYLON AT THE I/B CUTOUT FOR THE MID FLAP TORQUE TUBE. REPLACED ANGLE PER SRM 51-10-02. - [SDR 372PA0048](https://openairdocs.org/sdr/372PA0048), Jul 19, 2004: SWITCH. OUT OF ADJUST. LEADING EDGE FLAPS TRANSIT LIGHT AND CONFIGURATION HORN ON DURING TAKEOFF, BELOW 80 KTS. REJECTED TAKEOFF. CHECKED FLAP INDICATION SYSTEM AND ADJUSTED NR 1 LEAD - [SDR 372PA0047](https://openairdocs.org/sdr/372PA0047), Jul 16, 2004: COMPUTER. FAILED. FIRST OFFICER'S FLIGHT DIRECTOR INOPERATIVE AND SPEED TRIM FAIL AND MACH TRIM LIGHTS ILLUMINATED ON RECALL DURING LANDING CHECKS (SINGLE CHANNEL FAILURE). REPLA - [SDR 372PA0046](https://openairdocs.org/sdr/372PA0046), Jul 6, 2004: BATTERY PACK. INOPERATIVE. RIGHT OVERWING EMERGENCY EXIT INTERIOR LIGHT INOP. REPLACED RIGHT OVERWING EMERGENCY EXIT INTERIOR LIGHT BATTERY PACK. OPS CHECK GOOD PER MM 33-50-00. - [SDR 372PA0045](https://openairdocs.org/sdr/372PA0045), Jun 5, 2004: COMPUTER. MALFUNCTIONED. AUTO THROTTLE DISENGAGES IN LEVEL FLIGHT. WILL NOT RE-ENGAGE. REPLACED AUTO THROTTLE COMPUTER. OPS CHECK AND BITE TEST OK. REF ATA 22-30. - [SDR 372PA0044](https://openairdocs.org/sdr/372PA0044), Apr 7, 2004: ACTUATOR. SHORTED. DFCS HISTORY SHOWS AUTO-PILOT TRIM SERVO HAS NO RESPONSE. AUTO-PILOT COLUMN SWITCHING MODULE CHECKS OK PER MM 27-41-00. FOUND OPEN IN AUTO-PILOT STABILIZER TRIM - [SDR 372PA0043](https://openairdocs.org/sdr/372PA0043), Mar 21, 2004: COMPUTER. MALFUNCTIONED. AUTO THROTTLE WILL NOT ARM. RELEASED ON MEL 22-4. 03/23/2004: REPLACED AUTO THROTTLE COMPUTER PER MM 22-31-10. BITE CHECKS GOOD. - [SDR 372PA0041](https://openairdocs.org/sdr/372PA0041), Feb 16, 2004: LIGHT. INOPERATIVE. AFT SECTION OF EMERGENCY FLOOR PATH LIGHTING INOP. DRIED MOISTURE FROM FLOOR PATH LIGHTING AND OPS CHECKED OK. - [SDR 372PA0042](https://openairdocs.org/sdr/372PA0042), Feb 12, 2004: LIGHT. CONTAMINATED. FWD SECTION OF EMERGENCY FLOOR PATH LIGHTING INOPERATIVE. CLEANED AND DRIED WATER FROM TRACK AND CONTACTS. OPS CHECKS NORMAL. - [SDR 372PA0040](https://openairdocs.org/sdr/372PA0040), Jan 10, 2004: COMPUTER. MALFUNCTIONED. AUTOTHROTTLE DISCONNECTED ON TAKEOFF AND INITIAL CLIMB THROUGH 16,000. PLACED ON MEL 22-4. REPLACED AUTOTHROTTLE COMPUTER PER MM 22-31-10. OPS CHECKS NORMAL. - [SDR 372PA0039](https://openairdocs.org/sdr/372PA0039), Jan 6, 2004: SYNCRONIZER. OUT OF ADJUST. AUTO THROTTLES DISENGAGED ON TAKE OFF ROLL. ADJUSTED PLA SYNCHRO. OPS NORMAL IAW MM 22-31-00. - [SDR 372PA0038](https://openairdocs.org/sdr/372PA0038), Oct 24, 2003: CONNECTOR. DIRTY. AUTO PILOT B WILL NOT ENGAGE AND AUTO PILOT A IS INTERMITTENT. REMOVED DIRT FROM AUTO PILOT A AND AUTO PILOT B CONNECTORS. A AND B SYSTEMS TEST OK IAW MM 22-10- - [SDR 372PA0037](https://openairdocs.org/sdr/372PA0037), Oct 23, 2003: POWER UNIT. INOPERATIVE. RIGHT OVERWING EXIT LOWER LUMINESCENT EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT POWER UNIT PER MM 33-51-51. OPS CHECKS NORMAL. - [SDR 372PA0036](https://openairdocs.org/sdr/372PA0036), Oct 22, 2003: POWER SUPPLY. INOPERATIVE. RIGHT OVERWING EMERGENCY EXIT LIGHT INOP. REPLACED POWER SUPPLY/BATTERY CHARGER PER MM 33-51-51. OPS CHECKS OK. - [SDR 372PA0075](https://openairdocs.org/sdr/372PA0075), Sep 9, 2003: ANGLE. CRACKED. DRAG ANGLE CRACKED ABOVE LEFT RAM AIR INLET. REPLACED ANGLE PER EA 53-235. All 84: https://openairdocs.org/deregistered/N372PA-2006-12-06/reports.md ## Other aircraft with N372PA - [Cancelled 2024-12-28](https://openairdocs.org/deregistered/N372PA-2024-12-28): Helicopteres Guimbal CABRI G2, S/N 1150, built 2016. Sale reported, canceled. Owner: [Mcminnville, OR](https://openairdocs.org/faa-place/OR/Mcminnville) - [Cancelled 1997-04-10](https://openairdocs.org/deregistered/N372PA-1997-04-10): Boeing 727-295, S/N 20249. Triennial form not returned. Owner: [First Security Bank Na Trustee](https://openairdocs.org/faa-owner/FIRST%20SECURITY%20BANK%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.