# N339LF: Boeing 737-4Q8, registration cancelled 2014-03-24 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: March 24, 2014 - Exported to: Brazil - Status when cancelled: Valid registration - Airframe: [Boeing 737-4Q8](https://openairdocs.org/model/boeing-737-4q8) (registry code 138447Q) - Serial number: 25375 - Type of aircraft: Fixed wing multi engine - Certificate issued: August 1, 2013 - Last registry action: August 1, 2013 - Mode S code: A3B83E - Owner when cancelled: [Global Air Fleet LLC](https://openairdocs.org/faa-owner/GLOBAL%20AIR%20FLEET%20LLC) - Location: [Dansbury, CT](https://openairdocs.org/faa-place/CT/Dansbury) - Owner type: Corporation - Owner's area on the map: 41.3778° N, 73.4575° W: Placed by OpenAirDocs at the center of ZIP code 06810, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N339LF - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=339LF - Page: https://openairdocs.org/deregistered/N339LF-2014-03-24 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 737-4Q8: https://openairdocs.org/model/boeing-737-4q8.md ## Service difficulty reports (22) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR EE4Y2013120300141](https://openairdocs.org/sdr/EE4Y2013120300141), Dec 3, 2013: SKIN. DEBONDED. LEFT WING OTBD AFT FLAP LOWER SKIN DISBONDED. THE DAMAGED SECTION WAS REPAIRED IAW EO COO-CMP-3-57-172-13. - [SDR EE4Y2013120200139](https://openairdocs.org/sdr/EE4Y2013120200139), Dec 2, 2013: SKIN. DENTED. LEFT WING SPOILER, UPPER SKIN DENTED. THE UPPER SKIN WAS REPLACED. - [SDR EE4Y2013120500145](https://openairdocs.org/sdr/EE4Y2013120500145), Nov 22, 2013: SKIN. DENTED. LEFT WING, MID FLAP, L/E DENTED WBL 117. REPAIRED. - [SDR EE4Y2013111500135](https://openairdocs.org/sdr/EE4Y2013111500135), Nov 15, 2013: FRAME. CORRODED. LOWER FUSELAGE, FWD CARGO COMPARTMENT BS 500G FRAME SECTION WITH CORROSION BETWEEN S25R AND 25L. SECTION FRAME WAS REPAIRED AS STATED IN NON ROUTINE ITEM A1B127 - [SDR EE4Y2013111100132](https://openairdocs.org/sdr/EE4Y2013111100132), Nov 3, 2013: KEELBEAM. CORRODED. LOWER FUSELAGE, KEEL BEAM LOWER FLANGE CORRODED AT BS 562, LBL 6.3, WL 150. REPAIRED IAW EO COO-3-53-163-13. - [SDR EE4Y2013093000129](https://openairdocs.org/sdr/EE4Y2013093000129), Oct 30, 2013: FRAME. CORRODED. LOWER FUSELAGE, AFT CARGO BAY BS 727D FRAME S25-26R INBD FLANGE CORRODED. FRAME REPAIRED IAW A1B2171-242. - [SDR EE4Y2013103000126](https://openairdocs.org/sdr/EE4Y2013103000126), Oct 30, 2013: PANEL. CORRODED. LOWER FUSELAGE KEEL BEAM AREA FROM BS 608 - 628 BTW LBL 6.5 AND RBL 6.5 LOWER PANEL WITH CORROSION. PANEL REPLACED WITH NEW . - [SDR EE4Y2013103000127](https://openairdocs.org/sdr/EE4Y2013103000127), Oct 30, 2013: FRAME. CORRODED. LOWER FUSELAGE AFT CARGO BAY BS 727D BETWEEN S25-26L FRAME INBD SECTION CORRODED. FRAME REPARED IAW SRM 53-00-07, REPAIR 14. - [SDR EE4Y2013103000128](https://openairdocs.org/sdr/EE4Y2013103000128), Oct 30, 2013: FRAME. CORRODED. LOWER FUSELAGE AFT CARGO BAY BS 727E BETWEEN S25-26L FRAME SECTION CORRODED. FRAME WAS REPAIRED IAW SRM 53-0007, REPAIR 14. - [SDR EE4Y2013120300140](https://openairdocs.org/sdr/EE4Y2013120300140), Oct 25, 2013: BULKHEAD WEB. CORRODED. LOWER FUSELAGE AFT SECTION BS 1016 BETWEEN LBL 13 - 16 BULKHEAD WEB CORRODED. THE BULKHEAD WEB WAS REPAIRED IAW EO COO-3-53-177-13. - [SDR EE4Y201310230123](https://openairdocs.org/sdr/EE4Y201310230123), Oct 23, 2013: CARGO TRACK. CORRODED. LOWER FUSELAGE AFT CARGO BAY CARGO TRACK CORRODED AT RBL 13.80 BETWEEN BS 727+4 AND 947.5. CARGO TRACK REPLACED. - [SDR EE4Y201310230122](https://openairdocs.org/sdr/EE4Y201310230122), Oct 23, 2013: CARGO TRACK. CORRODED. LOWER FUSELAGE AFT CARGO BAY CARGO TRACK CORRODED AT LBL 17.20 BETWEEN BS 727+4.5 AND 947.5, CARGO TRACK REPLACED. - [SDR EE4Y2013093000106](https://openairdocs.org/sdr/EE4Y2013093000106), Sep 30, 2013: STRINGER CLIP. CORRODED. UPPER FUSELAGE, MAIN CABIN, BS 887, STRINGER CLIP 3L CORRODED. STRINGER CLIP REPLACED. - [SDR EE4Y2013093000105](https://openairdocs.org/sdr/EE4Y2013093000105), Sep 30, 2013: FLOOR SUPPORT. CORRODED. UPPER FUSELAGE AFT SECTION FROM BS 967 - 986.5 AT LBL 16 AND RBL 16, WL 208 FLOOR SUPPORT TEE WITH CORROSION. THE FLOOR SUPPORT WAS REPLACED, SEE NON ROUTINE IT - [SDR EE4Y2013093000104](https://openairdocs.org/sdr/EE4Y2013093000104), Sep 30, 2013: FLOOR SUPPORT. CORRODED. UPPER FUSELAGE AFT SECTION, BS 943.5 AT LBL 15, WL 208, FLOOR SUPPORT TEE WITH CORROSION. THE FLOOR SUPPORT WAS REPLACED, SEE NON ROUTINE ITEM A1B215 2-44 FOR D - [SDR EE4Y2013093000103](https://openairdocs.org/sdr/EE4Y2013093000103), Sep 30, 2013: FLOOR SUPPORT. CORRODED. UPPER FUSELAGE AFT SECTION BS 957 AT LBL 50, WL 208, FLOOR SUPPORT STRAP WITH CORROSION. THE STRAP WAS REPLACED. - [SDR EE4Y2013093000101](https://openairdocs.org/sdr/EE4Y2013093000101), Sep 30, 2013: FLOOR SUPPORT. CORRODED. UPPER FUSELAGE AFT SECTION BS 964 AT LBL 16, WL 208 FLOOR SUPPORT WITH CORROSION. FLOOR SUPPORT WAS REPLACED AS STATED IN NON ROUTINE, ITEM A1B215 2-42. - [SDR EE4Y2013093000102](https://openairdocs.org/sdr/EE4Y2013093000102), Sep 3, 2013: FLOOR SUPPORT. CORRODED. UPPER FUSELAGE AFT SECTION BS 951 AT RBL 50, WBL 208, FLOOR SUPPORT STRAP CORRODED. THE DAMAGED PART WAS REPLACED IAW SRM 51-10-02, PARA 8. UNDER NON-ROUTINE IT - [SDR EE4Y2013093000100](https://openairdocs.org/sdr/EE4Y2013093000100), Sep 3, 2013: FLOOR SUPPORT. CORRODED. UPPER FUSELAGE AFT SECTION BS 950 AT LBL 25, WBL 208, FLOOR SUPPORT COORRODED. THE DAMAGED PART WAS REPLACED IAW SRM 51-10-02, PARAGRAPH 8. UNDER NON-ROUTINE IT - [SDR EE4Y2013093000099](https://openairdocs.org/sdr/EE4Y2013093000099), Sep 2, 2013: FLOOR SUPPORT. CORRODED. UPPER FUSELAGE FWD ENTRY AREA FROM BS 294.5 TO 312, RBL 10, WL 208, FLOOR SUPPORT CORRODED. THE DAMAGED PART WAS REPLACED IAW SRM 51-10-02, PAR 8. UNDER NON ROU - [SDR EE4Y2013093000096](https://openairdocs.org/sdr/EE4Y2013093000096), Sep 2, 2013: FLOORBEAM. CORRODED. BS 360 BETWEEN RBL 12 - 48, WL 208 FLOORBEAM UPPER FLANGE CORRODED. CORROSION REMOVED IAW SRM 51-10-02 PARAGRAPH 14A AND REPAIRED IAW EA PD37-53-1855. - [SDR EE4Y2013093000095](https://openairdocs.org/sdr/EE4Y2013093000095), Aug 30, 2013: FLOORBEAM. CORRODED. UPPER FUSELAGE AFT SECTION BS 986.5 BETWEEN RBL 51 AND LBL 45 FLOORBEAM UPPER FLANGE CORRODED. CORROSION REMOVED IAW SRM 51-10-02, PARAGRAPH 14A AND REWORKED AR ## Other aircraft with N339LF - [Registered now](https://openairdocs.org/aircraft/N339LF): Pipistrel D O O ALPHA TRAINER, S/N AT162A0039 - [Cancelled 2008-01-30](https://openairdocs.org/deregistered/N339LF-2008-01-30): Boeing 737-3Q8, S/N 26288. Exported to China. Owner: [Castle 2003-2e LLC](https://openairdocs.org/faa-owner/CASTLE%202003-2E%20LLC), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington) --- 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.