PWS Addendum 1 Description of Services to Accept and Regenerate 15 T-38 Aircraft.docx

T-38 CAM PWS Addendum #1 Description of Services to Accept and Regenerate 7 T-38A Aircraft

* For proposal purposes the government projects 7 each aircraft requiring regeneration effort at the Holloman CRF for FY 12

1. Once the aircraft are delivered to the Holloman CRF the contractor shall take appropriate acceptance actions as outlined in TO 00-20-1.

2. The aircraft will be placed in an approved depot status until they are regenerated.

3. T-38 CAM Service Summary Metrics will not apply to ROK regeneration aircraft until they become mission capable.

4. Each aircraft will require regeneration actions as identified in the attached OO-ALC Memorandum “Requirements to Regenerate Korean T-38s to Flight Worthy Status” dated 6 Apr 2010 (Attachment #1) and the Excel spreadsheet titled “Korean Aircraft TCTO and TCI Requirements.”

5. All aircraft are required TCTO 838, 839, 842, and 843 in addition to those listed in Excel spreadsheet titled “Korean Aircraft TCTO and TCI Requirements” attachment #2. The approximate required man-hours are included within each applicable TCTO.

6. All aircraft will require the Dual Radio Modification attached as Attachment #3

7. Each aircraft shall be evaluated for corrosion control (top coat, strip, paint, markings, etc) and completed in accordance with the appropriate technical data.

8. The government’s expected aircraft production (aircraft ready for assignment and delivery) is 2 aircraft every NLT every 70 calendar days. The contractor will not be held accountable for delays outside their control such as parts availability, aircraft grounding conditions, severe weather, etc.

9. We (GOV and contractor) will jointly evaluate actions to transfer aircraft between Holloman, Beale and Tyndall to account for aircraft phase time distribution management.

10. The government expects the Aircraft Phase Inspection process on all other fleet aircraft to continue as prescribed within the PWS

T38 Dual Radio Mod Specs.pdf image1.emf

Korean Aircraft Regeneration Requirements.docx

DEPARTMENT OF THE AIR FORCE

HEADQUARTERS OGDEN AIR LOGISTICS CENTER (AFMC)

HILL AIR FORCE BASE, UTAH

April 6, 2010

Memorandum For: Todd Call

506 ACSS/GFLB (Bldg 1254)

Hill AFB, UT

From: 558 ACSG/EN

6057 Box Elder Lane (Bldg. 1285)

Hill AFB, UT 84056-5811

Subject: Requirements to Regenerate Korean T-38s to Flight Worthy Status

1. The Korean Air Force recently returned 15 leased T-38A aircraft to the USAF. These aircraft were loaded on sea vessel without adequate preparation thus exposing the aircraft to seawater and potential corrosion. Once delivered to the United States the aircraft were loaded on flatbed trucks and driven the AMARG where they were parked without any additional actions to preserve the aircraft. ACC requested the System Program Office (SPO) identify the requirements to regenerate these aircraft to flight worthy status.

2. 558th Engineering evaluated history of the aircraft and regeneration requirements for the Korean T-38 aircraft to return to a flight worthy status. Due to the unknown flight loads on the aircraft during Korean AF activity and the unknown status of periodic maintenance, a conservative approach is recommended to ensure Operation Safety Suitability and Effectiveness (OSS&E).

3. The following actions shall be accomplished to return all Korean T-38s to flight worthy status:

a. Comply with “removal from Storage” requirements as outlined in T.O. 1T-38A-17

b. Comply with the following inspections

i. 225 Hourly Post Flight Inspection (HPO); T.O. 1T-38A-6WC-1

ii. 450 Hour Periodic (Minor PE); T.O. 1T-38A-6WC-3

iii. 900 Hour Periodic (1st Major); T.O. 1T-38A-6WC-3

iv. 1800 Hour Periodic (2nd Major); T.O. 1T-38A-6WC-3

v. Aircraft Structural Integrity Inspections as outlined in 1T-38A-6 Paragraph 22-55 (complete all requirements regardless of time since last inspection)

c. Review Aircraft records

i. Accomplish any time change requirements not documented in aircraft forms; 1T-38A-6 Chapter 3 (see attached excel file for requirements)

ii. Clear all red X and red slash

d. Unless previously complied with as indicated by aircraft records, accomplish all TCTOs as noted in attached excel file. Of the 57 required TCTOs several may not be required depending on the final desired configuration, for example; the AUP mod (TCTO 1T-38-800), PMP mod (TCTO 1T-38-792), etc.

4. Engineering recommends the aircraft that have been out of service the longest be the first to accomplish the inspections. After 6 aircraft have been regenerated the SPO will review discrepancies noted on the first 6 aircraft and will consider waiving some of the requirements of this document.

5. Per Mil-Std-882D, the risk of not accomplishing the above requirements results in a Hazard Risk Index of an 8. After accomplishment of the requirements above the HRI is a 12.

6. Our point of contact is Eric Flygare, 558 ACSG/ENB, DSN 775-6225, (801) 775-6225.

//Signed//

Grant D. Herring

Chief, Engineering Division

558 ACSG/EN

image1.emf image2.emf

Korean Aircraft TCTO and TCI Requirements.xlsx TCTOs

TCTO Number TCTO Title Pub Date Safety Required Notes Checked Hours REQD Additional parts required Defer to owning base? 62-3615 62-3691 62-3702 62-3706 62-3722 63-8131 63-8133 63-8154 63-8163 63-8218 63-8229 64-13176 66-8404 67-14828 67-14923

SY07-957964 INTERIM INTERCOM FOR DGS-2 06/Mar/1995 N N 1

1T-38-749 REPL WINDSHIELD ASSY 01/Apr/1995 Y Y If not incorporated, aircraft will be limited during low level operations Y-Eric 27.5 Y c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI

1T-38-750 INSP OF AILERON GUIDE CLAMPS 10/Apr/1995 N N Required Y-Eric 3

1T-38-748 INSTALL OF ILS PROTECTION BRACKET 01/May/1995 N Y Only applicable for aircraft equipped with AN/ARN 147 instrument landing system Y-Eric 1.3 Y

SY07-957963 TGIF II UPGRADES FOR DGS2 10/May/1995 N N 5

1T-38-751 INSP OF LWR WING SKIN AILERON ACCESS PAN 28/Sep/1995 Y Y Applicable to AT-38B and IFF aircraft Y-Eric 10 Y

1T-38-733 MOD OF BULKHEAD STATION 325 15/Jan/1996 Y N 900 Hr inspection of bulkhead required if TCTO not complied with Y-Gary 7 c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI

1T-38-753 INSTALL OF SEALED LEAD ACID BATTERY 01/Feb/1996 N N Only applicable to AETC Aircraft Y-Eric 8

1T-38-748C 1 TIME INSTALL OF ILS PROTECTIVE BRACKET 01/Apr/1996 N Y Only applicable for aircraft equipped with AN/ARN 147 instrument landing system Y-Eric 1.3 Y

1T-38A-989 INSP OF AILERON ACCESS SKIN LAND, 15/Jun/1996 N N This is now accomplished per -6 requirements Y-Gary 10

1T-38-755 TORQUE OF LOWER LONGERON ATTACH BOLTS 31/Jul/1996 N Y Required Y-Gary 6 N

1T-38-754 INSP LOWER LONGERON ATCH BOLT F.S. 284 31/Jul/1996 N Y Required Y-Gary 15 N c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI

1T-38-654F ILS REPLACEMENT IN T-38 AIRCRAFT 01/Sep/1996 N N This is a 1990 TCTO to install the AN/ARN 147 ILS Y-Eric 13 c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI

1T-38-756 INST SEALED BATTERY SLAB 15/Sep/1996 N N Only applicable to AETC Aircraft Y-Eric 14

1T-38-757 REPL HORIZ TAIL OPER MECH CABLES 15/Sep/1996 N N This is now accomplished at every 1800 hr Phase Y-Eric 15

1T-38-759 INSP ELEC JUMPERS LF & RT FUSE REC ST252 15/Dec/1996 N Y Applicable to all rewired A/C Michael 1.5 Y

1T-38-745 REMOVAL OF APX-64(V) RECEIVER 15/Dec/1996 N Y Required. Note: 113589 I/W RT727AAPX64V Michael 2

1T-38-752 COLD WORK 228 FASTENER HOLE LOWER WING 15/Jan/1997 N Y Or all holes inspected and new dta funded to derive alternate inspection intervals Y-Gary 576 N c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI

1T-38-758 REMOVAL OF MXU-553 FLT. LDS DATA RECORD 15/Feb/1997 N Y Most likely not installed but it should be checked. Y-Eric 3.75 Y

1T-38-761 INSP OF CLEAR,DOOR #1 & ATTITUDE CONT AS 01/Jun/1997 N Y Required Y-Eric 1 Y

1T-38-762 RETORGUE AFT ARCH NUTS STD WDSHD ASSY 15/Jul/1997 N Y Only applicable if bird resistant windshield is installed (TCTO 1T-38-749) Y-Eric 2 Y c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI

1T-38-753D INST OF A SEALED LEAD ACID BATTERY 31/Aug/1997 N N Only applicable to AETC Aircraft Y-Eric 22

1T-38-756C INSTALL OF SEALED LEAD ACID BATTERY (SLB 31/Aug/1997 N N Only applicable to AETC Aircraft Y-Eric 23

1T-38-763 I.D.WEAPON SYS SUPPORT POD P/N 3-10259-1 31/Mar/1998 N N Not applicable to Korean Aircraft (AETC only) Y-Eric 24

1T-38-764 INSTALL SWAMPING RESISTOR IN INTERCOM 15/Oct/1998 N Y Required Michael 12

1T-38-765 INSP REAR CANOPY AIRSPD IND PNEU HOSES 16/Oct/1998 Y Y Required Y-Eric 4.5 Y c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI

1T-38-766 REPLACE CONNECTING KINKS (ROD ASSY) 15/Feb/1999 Y Y Required Y-Eric 7 N

1T-38-769 INSPT. OPERATIONAL FORMATION LIGHTS 31/May/1999 N Y Required Y-Eric 4 Y c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI

1T-38-767 RPL GEARBOX 3-51100-1 W/ 14-51100-501 31/May/1999 N Y Required Y-Eric 12 Y 1/1/97

1T-38-771 INSPECTION OF RUDDERS P/N 2-34001-5 14/Jun/1999 Y Y Required Y-Gary 6 Y

1T-38-753E SLAB BATTERY HQ AETC T/AT-38A/B ACFT 01/Jul/1999 N N Only applicable to AETC Aircraft Y-Eric 31

1T-38-760 "D"PANEL & AILERON ACCESS DR SCREW HOLES 30/Sep/1999 N Y Required Y-Gary 260 N c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI c/w LSI

1T-38-772 RPL. GASKET 2/54324-5 W/ 2-54324-7/ -9 01/Dec/1999 N Y Required, replaces defective gaskets Y-Eric 13 N

1T-38-768 INSP WING RIB ASSY P/N 2-23221-19/-20 05/Jan/2000 N N Radiographic Inspection required every 900 hours Y-Gary 34 c/w LSI

1T-38-770 RPT.ACFT MOD/SPT POD ASSY.P/N 3-0259-1 15/Jan/2000 N N Not applicable to Korean Aircraft (follow up to 1T-38-763) Y-Eric 35

1T-38-776 REMOVE LFT. & RT. A/C GEN. TERM. COVERS 31/Jan/2000 N Y Required Y-Eric 1.25 Y

1T-38-777 INSP & REM.HORZ.SERV CTRN ROD 3-73461-1 29/Feb/2000 N N This will essentially be accomplished during replacement of rod ends during 1800 Y-Eric 37

1T-38-775 INSP./INST. THROTTLE GATE P/N 8443244-10 29/Feb/2000 N Y Required Y-Eric 7.5 Y

1T-38-779 INSP. RUDDER FORCE SPRING P/N 2-73336-1 17/Apr/2000 Y N RFP spring is replaced as part of the 900 hr phase which is reqd as part of Regen Y-Eric 39

1T-38-781 INSPEC L/RH MLG STRUT AXEL FOR CRACKS 28/Jun/2000 Y N Accomplished during 900 hr Periodic, Which is Reqd for regen Y-Eric 40 8/14/00

1T-38-800 MOD. T-38A/B TO T-38C CONFIGURATION 01/Dec/2000 N N This is the AUP mod and will not be required per ACCs request Y-Eric 41

1T-38-782 INSPECTION OF NLG STRUT P/N 7227219-10 18/Dec/2000 N Y Required Y-Eric 0.5 N

1T-38-783 INSPECT/REPLACE HOR STAB ACT VALVE ROD E 27/Dec/2000 Y N The rod end is replaced as part of the 1800 hr phase, Reqd for regen Y-Eric 43 1/8/01

12R5-5ARN147-501 AN/ARN-147 FM INTERFERENCE IMMUNE CAPAB 05/Jan/2001 N Y Only applicable for aircraft equipped with AN/ARN 147 instrument landing system Y-Eric 3 Y

1T-38-784 INSP/REPL HOR STAB ACT HORN TAPER PINS 24/Jan/2001 Y Y Required Y-Gary 1.5 Y

1T-38-786 INSPECT VERT STAB LWR ATTACH BOLT/NUT 12/Mar/2001 Y N Required, also done every 1800 periodic Y-Gary 3/30/01

1T-38-787 INSP/REPL L/H R/H MLG DEFECT GY TIRES 15/Mar/2001 Y Y The subject tires have been purged from supply but this should be accomplished. Y-Eric 0.2 Y 3/29/01

1T-38-788 INSP/REPL L/H R/H MLG DEFECT TIRES 15/Mar/2001 Y N This insects for defective tires in base supply Y-Eric 48 3/30/01

4W1-7-573 INSP&REMOVE T-38 MAIN WHEEL TIE BOLT 04/Apr/2001 N Y Bolt inspection is reqd during every tire removal: TCTO not required if tires are R2 Y-Eric 5 Y

4W1-7-573C INSP&REMOVE OF T-38 MAIN WHEEL TIE BOLTS 11/Apr/2001 N Y Bolt inspection is reqd during every tire removal: TCTO not required if tires are R2 Y-Eric 5 Y

1T-38-789 REPL HORIZ STAB ACT SERVO VALVE ROD END 04/May/2001 N N The rod end is replaced as part of the 1800 hr phase Y-Eric 51

1T-38-642 INSP-RIB WING STA125 24/May/2001 Y N Radiographic Inspection required every 900 hours Y-Gary 52

1T-38-790 FRONT & REAR COCKPIT FLASHLIGHTS INSP 16/Jul/2001 Y Y Required Y-Eric 1 Y

1T-38-632 INSP/REPL OF NOSEWHEEL STEER HYD HO 24/Aug/2001 N Y Required Y-Eric 3 N

1T-38-791 INSP#6 DORSAL COVER PN2-1186-1/3-11861-1 01/Oct/2001 N N Not Required Y-Gary 55

1T-38-793 REPLACEMENT OF RUDDER FORCE PROD SPRING 13/Mar/2002 Y N RFP spring is replaced as part of the 900 hr phase which is reqd as part of Regen Y-Eric 56

1T-38-795 INSP/REPL NLG DRAG BRACE STUD SHLD BOLT 28/May/2002 Y N R2 during 1800 Phase, Reqd during regen Y-Eric 57

1T-38-796 REP NLG STRUT DRG BRACE SHD BOLT 9756C94 24/Jul/2002 Y N R2 during 1800 Phase, Reqd during regen Y-Eric 58

1T-38-792 PMP TCTO EJECTORS, INLET DUCT,& ENGINES 31/Aug/2002 N N Korean Jets are not and will not be PMP Y-Eric 59

1T-38-793D REPL OF RUDDER PRODUCER SPRING 13/Mar/2003 Y N RFP spring is replaced as part of the 900 hr phase which is reqd as part of Regen Y-Eric 60

13A5-45-507 T38 INITIATOR POST CORR FOR INIT.FITTING 14/May/2003 N Y Required Y-Eric 5

1T-38-801 REM/INSTL OF SEAT ASSY ICW 13A5-45-507 12/Jun/2003 Y Y Required Y-Eric 5 Y

1T-38-802 INSP/INSTALL OF REAR CANOPY EXTERNAL DOW 22/Oct/2003 N Y Required Y-Eric 5 Y

1T-38-805 REM & REPL OF CKU-7A ROCKET CATAPULT 10/Feb/2004 N Y Required Y-Eric 6.5 N 7/31/07

1T-38-806 INSP OF RC LIQUID OXY IND WIRING SEC/CHA 26/Apr/2004 Y Y Required Y-Eric 0.5 Y

1T-38-804 MOD OF L&R HYD RES PANEL FOR T5 AMP DOOR 06/May/2004 N Y Required Y-Eric 28 Y

1T-38-807 INSPEC & REPAIR OF LOWER WING SKIN & 62% 27/Sep/2004 N N Inspection required for IFF (Cat 3) usage at 450 hour periodic Y-Gary 35 11/11/04

1T-38-808 INSP OF LH/LH MLG PISTON 26/Jan/2005 N N Accomplished during 900 hr Periodic, Which is Reqd for regen Y-Eric 68 7/26/06

1T-38-808C INSP OF LH/RH MLG PISTON 09/Feb/2005 N N Accomplished during 900 hr Periodic, Which is Reqd for regen Y-Eric 69

1T-38-809 INSP OF DORSAL LONGERON, P/N 3-11413-1/2 02/Jun/2005 Y Y Required Y-Gary 8.2 N

1T-38-803 PANEL FASTENER CHANGEOVER 24/Aug/2005 N Y ????? Couldn't locate this TCTO in WSMT ????

1T-38-811 ONE TIME INSP SEAT RAFTS 27/Feb/2006 Y Y Required Y-Eric 3.75 Y

1T-38-812 REP GEARBOX INTRSHAFT ASSY 19E83-2-ACL53 10/May/2006 N Y Required Y-Eric 0.25 Y 4/29/08

1T-38-810 REPL OF GEARBOX 501 W 503 SGAGE 30/May/2006 N Y Required Y-Eric 3 Y

1T-38-813 INSP CONT STICKS FOR SCREW LOCKING INSER 21/Aug/2006 N Y Required Y-Eric 3.2 N 1/17/08

1T-38-814 INSP FUEL CARD FOR DODAAC FP2403 19/Sep/2006 N Y Required Y-Eric 0.5 Y

1T-38-815 INSP OF FWD ENGINE MOUNT BOLTS 03/Oct/2006 N Y Required Y-Eric 1 N 8/18/09

1T-38-817 INSPEC T-38 WINDSCREEN AFT BOLT HOLES 10/May/2007 N Y This only applies to a/c modified by TCTO 1T-38-749 Y-Eric 6.25 Y c/w

1T-38-819 REPLCE GEARBOX OIL FILL SIGHT GAUGE CAP 12/Jul/2007 N Y Required Y-Eric 1 Y

1T-38-820 INSP PRIMARY FLT CONTROLS NON COATED CBL 11/Oct/2007 N Y Required Y-Eric 1 N 4/23/08

1T-38-818 INST CANOPY SEAL FITTING A EXTENSION TUB 29/Oct/2007 N Y Required Y-Eric 4.5 Y 10/17/08

1T-38-821 ONE-TIME INSP ALL T38 A/C LT/RT AILERON 02/May/2008 Y N Replacement of the lever is required at 900 hr, which is required for regen Y-Eric 82 5/7/08

13A5-45-508 REPLACE T-38 SEAT TIME DELAY INITIATOR 01/Aug/2008 Y Y Required Y-Eric 4 N 8/18/08

1T-38-824 INSP OF SINGLE MOTION EJECTION SEAT 01/Aug/2008 Y Y Required Y-Eric 6 N 8/18/08

1T-38-825 REPLACE ALL T38 LT/RT AILERON ACT SERVO 01/Aug/2008 Y N Replacement of the lever is required at 900 hr, which is required for regen Y-Eric 85 11/25/08

1T-38-827 INSP HORIZONTAL STABILIZER CONTROL RODS 05/Dec/2008 Y Y This should be accomplished in conjunction with 1T-38-766 above Y-Eric 5 N 2/9/09

13A5-45-509 REMOVAL/REPLACE OF SEAT 1.0 TCI 15/Jan/2009 Y Y Required Y-Eric 4 N

1T-38-828 REMOVE & REPLACE TIME DELAY INITIATORS 15/Jan/2009 N Y Required Y-Eric 6 N

1T-38-829 INSPECTION OF MLG SIDEBRACE TRUNNION 12/Feb/2009 Y N Accomplished during 900 hr Periodic, Which is Reqd for regen Y-Eric 89

1T-38-792D INSTALL EXHAUST EJECTOR ASSY 19/Feb/2009 N N Korean Jets are not and will not be PMP Y-Eric 90

1T-38-823 R2 RUDDER FORCE PRODUCER SPRING 04/May/2009 N Y Required Y-Eric 14 Y

1T-38-831 INSPECTION OF RUDDER SPF ATTACH POINTS 13/Jul/2009 Y Y Required Y-Eric 1.5 N 8/5/09

1T-38-832 NDI OF LOWER WING FASTNER HOLES 15/Sep/2009 N N Only specific aircraft applicable to this inspection at this time Y-Gary 93

1T-38-833 INSPECTION OF 15% WING TO FUSELAGE BOLT 14/Dec/2009 Y Y Required Y-Gary 1.5 N

1T-38-837 INSPECTION OF STEEL DORSAL LONGERON Y Y Required Y-Gary 8.5 N

N= 38 Time required for TCTO 241.95 241.95 246.45 241.95 241.95 237.95 237.95 241.95 237.95 241.95 241.95 242.45 237.95 190.55 237.95

Y= 57 Time required -6 inspections 471.15 471.15 471.15 471.15 471.15 471.15 471.15 471.15 471.15 471.15 471.15 471.15 471.15 464.65 471.15

Total time required 713.1 713.1 717.6 713.1 713.1 709.1 709.1 713.1 709.1 713.1 713.1 713.6 709.1 655.2 709.1

Dash 6 inspections

T.O. Required Inspection Hrs Reqd 62-3615 62-3691 62-3702 62-3706 62-3722 63-8131 63-8133 63-8154 63-8163 63-8218 63-8229 64-13176 66-8404 67-14828 67-14923

-6WC-1/-3 225 Hourly Post Flight Inspection (HPO) "7.5"

450 Hour Periodic (Minor PE) "79.9" 7/10/09

900 Hour Periodic (1st Major) "169.5" 2/15/08

1800 Hour Periodic (2nd Major) 230.15

-6 insp

23 Wing lower skin fastener holes 140-161, 206….. (Ultrasonic) 7.5

24 Wing lower skin fastener holes 116-139, 196-….. (Ultrasonic) 4

25 Wing lower skin fastener holes 1-29, 162-…(Ultrasonic) 4

26 Wing lower skin fastener holes 723-727, 735-….. (Ultrasonic) 4

27 Wing lower skin fastener holes 290-295, 470-….. (Ultrasonic) 4

28 Wing lower skin fastener holes 451-455, 496-….. (Ultrasonic) 4

29 Wing lower skin aft edge, land and radius W.S. 26.6-60 and 60-64.8 (visual and eddy) 2

30 Wing root radius at W.S. 25.1 (eddy current) 16

31 Wing lower wing skin land W.S. 77, 44 and 66% spar (Eddy Current) 4

32 Wing fwd land between WS 72.25 and 76.7 (eddy current 1

33 Wing lower milled pockets at WS 78 between 39 and 44% spar (ultrasonic) 3

34 Wing lower skin screw holes and aileron access doors between 76 an 101 on 44% (eddy current) 2

35 Wing lower skin critical fastener holes 728 to 734 (Ultrasonic Roto-scan) 2

36 Wing spars and ribs (radiograph) 2

37 Wing 66% between 101 and 76 (eddy current) 1

38 Thin skin wing only, Fasteners at 44 and 39% spar (ultrasonic) 0.5

39 Thin skin wing only, Wing root radius WS 25.88 (eddy current) 0.5

40 Thin skin wing only, Wing lower skin WS 26.6 - 64-8 (eddy current) 0.5

41 Wing attach trunnions (ultrasonic and Eddy current) 6

42 Wing attach bushings flanges 15 and 44% (dimensional check) 120

43 Not required (required when bushings are removed) 2

44 Wing attach bolts (mag particle) 3

45 Cockpit longeron FS 146 (prior to TCTO 717) (eddy and penetrant) 0.5 N/A

46 Cockpit longeron FS 146 (after TCTO 717) (eddy and penetrant) 0.5

47 Cockpit longeron hook slots (except cat 5) (eddy current) 0.5

48 Cockpit longeron hook slots FS 267 (cat 5 only) (Eddy current) 0.5

49 Cockpit longeron hook slots FS 267 (eddy current) 4 N/A

50 Outboard engine mounts (mag particle) 4

51 Inboard engine mounts (Mag particle) 4

52 V-tip antenna (eddy current) 2

53 Vertical stab radius (ultrsonic/borescope) 0.5

54 H-stab torque tube fillet (visual) 4

55 Upper longeron canted FS 264 (eddy Current) 0.5

56 Upper longeron splice FS 284 bolt installed (ultrasonic) 0.5

57 Upper longeron splice FS 284 bolt uninstalled (ultrasonic) 0.5

58 Upper longeron splice bolt 0.5

59 Steel dorsal longeron (eddy current) 7

60 Steel dorsal longeron hi-Loc holes at 400.02 (eddy current) 0.5

61 Steel dorsal longeron rivets FS 351.25, 367, and 380 (fluorescent Pen) 8

62 Steel dorsal longeron rivets FS 405.05 (eddy current) 1

63 Steel dorsal longeron upper edge (eddy current) 6

64 Steel dorsal longeron vertical fastener holes (eddy current) 1

65 Aluminum dorsal longeron nut plates FS 317-393 and 400-424 (eddy current) 0.5 N/A

66 Aluminum dorsal longeron holes FS 329 (eddy current) 0.5 N/A

67 Aluminum dorsal longeron holes FS 337. 351, 364. 378, 389 (eddy current) 0.5 N/A

68 Aluminum dorsal longeron nutplate holes (eddy current) 0.5 N/A hours required for -6 and -6WC inspections 471.15 471.15 471.15 471.15 471.15 471.15 471.15 471.15 471.15 471.15 471.15 471.15 471.15 464.65 471.15

Time Change Items

TCTO # P/N Nomenclature Qty Cost each Qty Available NSN Alt NSN

N/A 8140601-03 BOLT, Shoulder (Replaces 3-20001-1) 2 $42.30 0 5306 009626779

N/A 3-11787-3 BUSHING, Front Spar Attach Fitting Sleeve 2 $19.26 221 3120 009538403

N/A NAS577-7A NUT, Self-locking, Barrel 2 $26.92 Not in E-Mall 5310 008097632

N/A 2-13300-35 PANEL ASSY, Instructor’s Canopy 1 $15,018.40 111 1560 008634491

N/A 2-13201-49 PANEL ASSY, Student’s Canopy 1 $18,040.68 28 1560 009961399

N/A GID 21-288-503 CHUTE, DROGUE 2 $704.68 252 1670 010402569

N/A GID 53-686-311 SLEEVE, DEPLOYMENT 2 $162.15 698 1670 010405864

N/A GID 51-474-505 HARNESS, DROGUE CHUTE 2 $132.54 1357 1670 010345836

N/A 9155455-10 MAIN LANDING GEAR SIDEBRACE TRUNNION 2 $2,974.49 Not in E-Mall 1620 013511053

N/A 2-43169-5 AILERON SERVO VALVE CONTROL LEVER 1 $338.46 / $559.65 2 / 155

Denver.Miller: Denver.Miller:

Alternate NSN (p/n 2-43169-9) qty 155, $559.65 ea 1680 007677698 1680 015639065

2-43169-6 AILERON SERVO VALVE CONTROL LEVER 1 $283.86 / $1349.07 12 / 171

Denver.Miller: Denver.Miller:

Alternate NSN (p/n 2-43169-10) qty 171, $1349.07 ea

Denver.Miller: Denver.Miller:

Alternate NSN (p/n 2-43169-9) qty 155, $559.65 ea 1680 007677699 1680 015639064

N/A NAS464P6LA21 BOLT, HORIZONTAL STABILIZER SUPPORT 2 $8.38 19 5306 008386705

N/A 5045T88P01 DISK, Stage 2 2 2840 011873181

N/A 5126T33P02 DISK, Stage 3 2 2840 014888016

N/A 5018T16P01 DISK, Stage 4 2 2840 008676279

N/A 5013T79P01 DISK, Stage 5 2 2840 010682042

N/A 5013T80P01 DISK, Stage 6 2 2840 010682043

N/A 5013T82P01 DISK, Stage 7 2 2840 010682044

N/A 5013T83P01 DISK, Stage 8 2 2840 010682045

N/A 37D401302P103 SPACER, Stage 2 2 2840 010682048

N/A 37D401303P104 SPACER, Stage 3 2 2840 010682049

N/A 5013T88P01 SPACER, Stage 4 2 2840 010682046

N/A 5013T89P01 SPACER, Stage 5 2 2840 010665225

N/A 37D401306P105 SPACER, Stage 6 2 2840 010682050

N/A 37D401307P103A SPACER, Stage 7 2

N/A 6052T63P01 BLADE, COMPRESSOR, STAGE 1 62 2840 012441412

N/A 5004T73P02 SHAFT, Compressor Drive 2

N/A 4010T01P02 SEAL, Labyrinth, Stage 8 2 2840 001189651

N/A SHAFT AND SEAL, COMPRESSOR INCL DISK, STAGE 1 2

N/A 6013T62G18 SHELL, Outer 2 2840 012289195

N/A 5020T27G10 SHELL, Inner 2 2840 015400872

N/A 6028T44P01 WHEEL, Turbine Rotor, Stage 1 2

N/A 37D401014P101 RING, TORQUE, TURBINE 2 2840 007041301

N/A 4036T24P01 WHEEL, Turbine Rotor, Stage 2 2 $27,914.15 2840 010048911 2840 004877917

N/A D8565/11-1 AIRCRAFT BATTERY (SLAB) 1 $649.06 380 6140 012866294

N/A 66WAZ300-5 PUMP, Hydraulic 2 $6,215.30 Not in E-Mall 4320 000867167

N/A 106788S103 ACTUATOR ASSY, FUEL SHUTOFF VALVE 2 $7,998.39 Not in E-Mall 4810 009318957

N/A 1000-54 ROTARY ACTUATOR 2 $2,399.00 Not in E-Mall 1377 010497586

N/A M9 CATAPULT (M9) 0 N/A THIS A/C

N/A CKU-7A/A CATAPULT (CKU-7/A) 2 $15,000.00 Not in E-Mall 1377 015124035

N/A M26 INITIATOR (M26) 0 N/A THIS A/C

N/A M27 INITIATOR (M27) 4 $291.25 Not in E-Mall 1377 008451059

N/A M31 INITIATOR (M31) 1 $1,373.62 Not in E-Mall 1377 007563499

N/A M32A1 INITIATOR (M32A1) 0 N/A THIS A/C

N/A M120 INITIATOR (M120) 0 N/A THIS A/C

N/A PART NO. 10520619 INITIATOR (M-53) 2 $124.03 Not in E-Mall 1377 007319272

N/A 1007-4 INITIATOR (PART NO. 1007-4) 4 $461.15 Not in E-Mall 1377 010477458

N/A 1010-4 INITIATOR (PART NO. 1010-4) 2 $573.71 Not in E-Mall 1377 011376039

N/A 1139-5 INITIATOR (PART NO. 1139-5) 4 $519.83 Not in E-Mall 1377 011376040

N/A PART NOS. 0113226-3 AND -23 0 N/A THIS A/C

N/A M25A1 THRUSTER (M25A1) 2 $1,197.00 Not in E-Mall 1377 005543103

N/A PART NO. 1018-500 GUN, DROGUE 2 $779.29 Not in E-Mall 1377 010156422

TCTO parts required

TCTO # P/N NSN Nomenclature Qty required Cost each Quantity available

1T-38-748 N/A

1T-38-751 N/A

1T-38-748C N/A

1T-38-755 N/A

1T-38-759 N/A

1T-38-745 113589-11 Receiver-transmitter 1 unavailable

1T-38-758 N/A

1T-38-761 NONE

1T-38-764 RCR20G750JS

M27500-22SD1T23

M22759/34-22-9

MIL-S-8516

323986

RCR20G4R7JS

M22759/34-22-0

SN60WRAP3

SP0450-94-M-FA58

RCR20G103JS

RCR20G183JS RESISTOR

WIRE

WIRE

SEALING COMPOUND

TERMINAL, LUG

RESISTOR

WIRE

SOLDER

INSULATION SLEEVE

RESISTOR

RESISTOR 4

120 INCHES

8 INCHES

1 KIT

24 INCHES

1 SPOOL

1 FOOT

2 $.84

$.20 FOOT

$.08 FOOT

$59.02 $.17 $.84

$.18 FOOT

$10.96

$.11 FOOT

$3.50 $.08 2905 98561 785727

GSA

DOD

51136 11093

1T-38-766 2-73030-13

MS24665-69

MS17826-3

AN960D10L CONNECTING LINK

COTTER PIN

NUT

WASHER 2

2 $164.14 EA

$6.30 HD

$.88

$1.44 HD 1660

48238

1T-38-769 NONE

1T-38-767 NONE

1T-38-771

1T-38-772 NONE

1T-38-776 NA NA NA NA NA NA

1T-38-775 Local Manufacture Drawing #8443244 Throttle Gate 1 NA NA

1T-38-782 7227219-10 00-299-0278 NLG Strut Assembly 1 UNK

12R5-5ARN147-501 COULD NOT LOCATE

1T-38-784 14-32207-1 01-034-7580 Pin 1 $40.11 0

14-32207-3 01-165-2010 Pin 1 $38.07 81

14-32207-5 01-287-2486 Pin 1 $49.35 255

14-32207-7 01-287-2487 Pin 1 $250.98 2

14-34204-1 01-034-1000 Washer 1 $1.90 662

NAS1291C8M 00-458-2115 Nut 1 $6.71 1326

1T-38-786 AN960D916L XXXXXXX Washer AR UNK

MS21245L9 00-449-2380 Nut 1 $4.76 2687

1T-38-787 QTR #461B-3484-TL 01-042-2783 MLG TIRE (20X4.4/14PR) AR $539.89 0

4W1-7-573 COULD NOT LOCATE

4W1-7-573C COULD NOT LOCATE

1T-38-790 A6900C1495 00-825-1714 Light Assembly, Trim Panel AR $193.31 42

A5395C1 00-729-9396 Lighg Assembly, Glare Shield AR $86.32 84

1T-38-632 2-43803-27 00-943-2341 NWS Hydraulic Hose 2 $62.65 15

13A5-45-507 COULD NOT LOCATE

1T-38-801 NA NA NA NA NA NA

Local Manufacture Figure 1 Indicator Tab 1

1T-38-802 MS20426AD-5-X XXXXXXX Rivit AR UNK

1T-38-805 512-174-0110 01-512-4035 Catapult, Aircraft 1 UNK

MS28775-011 01-035-0988 Packing AR $0.07 3984

MS28778-4 00-805-2966 Packing AR $0.13 120283

1T-38-806 NA NA NA NA NA NA

1T-38-804 NAS601-6P 00-841-2944 Screw, Machine 4 $5.33 779

MS21076-06 00-764-6597 Nut Plate, Self-Locking 4 $1.76 5559

MS20426AD3 00-117-6947 Rivit (length to be determined) 8 $14.49 2400

MS20426AD4 00-1176951 Rivit (length to be determined) 14 $14.02 3466

NAS1097AD5 00-068-8262 Rivit (length to be determined) AR $0.27 1366

NAS1097AD3 01-495-2872 Rivit (length to be determined) AR UNK

1T-38-807 NAS1670-08DL4 01-291-0184 Rivit, Blind AR $1.53 13635

NAS1670-08DL5 01-290-3803 Rivit, Blind AR $1.48 8244

NAS1670-08DL6 01-291-2267 Rivit, Blind AR $2.02 4451

NAS1670-08DL7 01-291-9487 Rivit, Blind AR $2.74 431

NAS1670-08DL8 01-291-2263 Rivit, Blind AR $4.38 2388

NAS1670-3DL7 01-291-2264 Rivit, Blind AR $2.13 5308

1T-38-809 NAS1068RA3 01-081-0145 Nutplate AR $0.31 4805

NAS1623-4 00-058-2575 Screw AR $6.66 4117

NAS1623-2 00-935-3025 Screw AR $12.69 0

MS20426AD4 00-117-6951 Rivit AR $14.02 3466

1T-38-803 CA17078-1HS 01-188-1800 Stud, Live lock Fastener AR $45.44 2173

CA17078-2HS 01-188-1799 Stud, Live lock Fastener AR $37.62 7243

CA17078-3HS 01-193-7003 Stud, Live lock Fastener AR $53.55 2079

CA1753 01-163-3138 Ring,Retainer AR $0.73 31825

CA17027 01-191-3290 Receptacle, Live lock AR $27.27 7966

MS20426AD3 00-117-6939 Rivit AR $17.17 3218

MS20605FL3W4 01-466-5591 Rivit, Blind AR $1.36 7935

1T-38-811 NO PARTS REQUIRED

1T-38-812 19E83-2ACL53 1560-00-989-6805 SHAFT ASSEMBLY, INTERCONNECTING 1 $2,775.77 250

1T-38-810 14-622-505 6680-01-530-8433 INDICATOR, SIGHT, LIQUID 1 $126.76 1700

1T-38-813 MS21209F4-20 5325-00-721-7498 INSERT, SCREW THREAD AS REQ $0.22 6014

MS21209F45-20 5325-00-582-7256 INSERT, SCREW THREAD AS REQ $0.24 14688

1T-38-814 NO PARTS REQUIRED

1T-38-815 NAS6604-6 5306-01-106-5220 BOLT, SHEAR AS REQ $14.65 HD 1463

NAS1304-6 5306-00-722-1788 BOLT, SHEAR AS REQ $25.38 HD 0

1T-38-817 CONSUMABLES ONLY REQ

1T-38-819 14-622-9 6685-01-530-2752 VENTED CAP ASSEMBLY AS REQ $34.75 416

MIL-DTL-83420L 1640-01-196-3398 ROPE, WIRE AS REQ $0.21 FT 5485

MS51844-21 4030-01-257-7788 SWAGING SLEEVE, WIRE ROPE AS REQ $0.10 5853

1T-38-820 NO PARTS REQUIRED

1T-38-818 AMS-WW-T-700/4 4710-00-541-4932 TUBING, METALLIC 1 FT. $1.30 FT 3032

AN818-4D 4730-00-287-0289 NUT, TUBE COUPLING 2 $0.46 11965

AS5176-04 4730-00-278-0678 SLEEVE, FLARED, TUBE FITTING 2 $1.47 8897

AN815-4D 4730-00-834-9560 NIPPLE, BOSS 1 $1.89 7735

MS21919WDG4 5340-00-291-5323 CLAMP, LOOP AS REQ $32.20 HD 11

NAS6603-1 5306-01-136-3540 BOLT 1 $6.66 261

MS21042-3 5310-00-807-1467 NUT, SELF-LOCKING, EXTENDED WASHER 1 $28.20 HD 6

AN960D10L 5310-00-167-0752 WASHER, FLAT 2 $1.44 HD 5500

NAS1100-06-( ) SCREW AS REQ

13A5-45-508 NO DATA AVAILABLE

1T-38-824 NO PARTS REQUIRED

1T-38-827 2-73030-13/-21 3040-01-415-4493 CONNECTING LINK, RIGID 2 $164.14 1660

MS17826-3 5310-00-066-4289 NUT, SELF-LOCKING SLOTTED, HEXAGON 2 $0.88 45542

MS24665-132 5315-00-839-2325 PIN, COTTER 1 $0.58 HD 14424

MS24665-69 5315-00-828-8190 PIN, COTTER 1 $6.30 HD 1742

AN960D10L 5310-00-167-0752 WASHER, FLAT 1 $1.44 HD 5500

AN960D10 5310-00-851-0913 WASHER, FLAT 1 $1.41 HD 27876

13A5-45-509 NO DATA AVAILABLE

1T-38-828 NO PARTS REQUIRED

1T-38-823 200530548-01 5360-01-540-3581 SPRING, HELICAL, EXTENSION 1 $29.40 1

MS24665-134 5315-00-839-5820 PIN, COTTER 1 $1.41 HD 7106

MS17826-3 5310-00-066-4289 NUT, SELF-LOCKING, SLOTTED HEXAGON 1 $0.88 45542

1T-38-831 NO PARTS REQUIRED

1T-38-833 NO PARTS REQUIRED

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