N595AG

Cancelled 2012

Deregistered aircraft · Boeing 737-4S3 · CFM International CFM56-3C series

Cancelled
May 25, 2012
Exported to
France
Status when cancelled
Valid registration
Serial number
25595
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
April 14, 2011
Certificate issued
April 26, 2012
Last registry action
April 30, 2012
Mode S code
A7B001
Owner when cancelled
Aviation Capital Group Corp
Owner type
Corporation

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.

Service difficulty reports · 8

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

SDR FOTR2020815451Skin · crackedLT SIDE OF FUSELAGE HAS A CRACK IN THE SKIN AT BS 727F+10. CUT OUT DAMAGED AREA 3.75" X .5" IAW SKETCH CGP-CGP-10-0070. FABRICATED REPAIR TRIPLER FROM 2024T3 .050 PO 90010715, DIM 16.5" X 11.5" IAW SKETCH CGP-CGP-10-0070 AND FILLER FROM 2024T3 .071 PO 9001Mar 31, 2011 · N595AG · Boeing 7374S3 · Fuselage Main, Plate/SkinSDR FOTR2020815494Frame · crackedFWD CARGO COMPARTMENT, BS 500G FRAME HAS CRACK INDICATION BETWEEN STRINGERS 20R AND 21R AT 1.04 IN POWER FEEDER WIRE PENETRATION HOLE. CUT OUT CRACK AT WIRE PENETRATION HOLE .250 IAW SRM 53-00-07, FIG 202. FABRICATED REPAIR ANGLES FROM .050 7075-O PO 9001187Mar 31, 2011 · N595AG · Boeing 7374S3 · Fuselage Main, FrameSDR FOTR2020815495Frame · crackedFWD CARGO COMPARTMENT, BS 520 FRAME HAS CRACK INDICATION BETWEEN STR 20R AND 21R AT 1.04 INCH WIRE PENETRATION HOLE. CUT OUT CRACK AT WIRE PENETRATION HOLE .250 IAW SRM 53-00-07, FIG 202. FABRICATED REPAIR ANGLES FROM 7075-0 .050 PO 9001187, DIM 3" X 11" ANDMar 31, 2011 · N595AG · Boeing 7374S3 · Fuselage Main, FrameSDR FOTR2020815653Cusp Web · corrodedMAIN CABIN RT SIDE, STR 17 CUSP WEB UPPER SURFACE HAS AREAS OF CORROSION BETWEEN BS 787 AND BS 807. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-00-04 AND 53-60-13 FIG 101. FABRICATED NEW WEB FROM 7075T6 .040 PO 90010492 DIM 12" X 7" IAW SRM 53-60-13Mar 31, 2011 · N595AG · Boeing 7374S3 · Fuselage Miscellaneous StructureSDR FOTR2020815666Cusp Web · corrodedRT MAIN CABIN STRINGER 17 RT, CUSP WEB UPPER SURFACE HAS AREAS OF CORROSION BETWEEN BS 727D AND BS 727E. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-00-04. FABRICATED NEW WEB FROM 7075T6 .032 PO 9009201 DIM 20.6250" X 7.0312" IAW SRM 53-60-13 FIG 1 Mar 31, 2011 · N595AG · Boeing 7374S3 · Fuselage Miscellaneous StructureSDR FOTR2020815677Frame · crackedCABIN INTERIOR FRAME CRACKED AT BS 500E, STR 10L. CUTOUT DAMAGED AREA 2" X 1" IAW SRM 53-00-07. FABRICATED Z FRAME REPAIR CHANNELS FROM 7075-0 .050 DIM 3.5" X 15" PO 90010501 IAW SRM 53-00-07. HEAT TREATED MATERIAL TO 7075T6 IAW FAS REPORT 2-37153-801, REV Mar 31, 2011 · N595AG · Boeing 7374S3 · Fuselage Main, FrameSDR FOTR2020815678Shear Tie · crackedFRAME SHEAR TIE IS CRACKED AT BS 500F STRINGER 10L. CUTOUT DAMAGED AREA DIM 5.3750" X .3750" IAW SRM 53-00-07. FABRICATED SHEAR TIE REPAIR FROM 7075-0 .050 PO 90010501 DIM 6.7500" X 4.5" IAW SRM 53-00-07. HEAT TREATED MATERIAL TO 7075T6 IAW FAS REPORT 2-371Mar 31, 2011 · N595AG · Boeing 7374S3 · Fuselage Internal Mounting StructureSDR FOTR2020815697Shear Tie · crackedMAIN CABIN HAS CRACKED SHEAR TIE AT BS 500E, STRINGER 10L. CUTOUT DAMAGED AREA DIM 6" X 1" IAW SRM 53-00-07, REPAIR 7, FIG 201. FABRICATED SHEAR TIE REPAIR FROM PN 7075-0 .050 PO 90010501, DIM 9.5" X 6.75" IAW SRM 53-00-07. HEAT TREATED MATERIAL TO 7075T6 Mar 31, 2011 · N595AG · Boeing 7374S3 · Fuselage Internal Mounting Structure

Other aircraft with N595AG · 1

The FAA can assign a mark to another aircraft once a registration is cancelled. N595AG is registered now to the first aircraft listed.