N906FD

Part: HANDLE — FAILED (BRAKE) · airframe 535 hrs · 23,313 cycles

PARKING BRAKE HANDLE SPINS. SECURED PARING BRAKE HANDLE IAW MM 32-44-01-4.

Part: BOTTLE — LEAKING (L1 DOOR) · airframe 533 hrs · 23,162 cycles

L1 DOOR, EMERGENCY POWER RESERVOIR BOTTLE PRESSURE READS ZERO PSI. R & R THE EMERGENCY POWER RESERVOIR IAW MM 52-11-30-4.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 533 hrs · 23,160 cycles

ON BLOCK IN L1 DOOR DID NOT GET DISARMED PROPERLY & SLIDE DETACHED FROM DOOR & FELL ONTO CREW STAIRS PLATFORM. SLIDE DID NOT INFLATE. INSTALLED L1 DOOR SLIDE ASSEMBLY IAW MM 25-66-01-4. CHECKED OPERATION OF GIRT BAR, ARMING & DISARMING SEVERAL TIMES. OPERATIONS CHECKED NORMAL. ACFT OK FOR SERVICE.

Part: BEARING — FAILED (ENTRY DOOR) · airframe 53,042 hrs · 22,943 cycles

ON LT FWD ENTRY DOOR FOUND UPPER ROLLER BEARING ON DOOR THAT SETS THE DOOR INDICATION SWITCH BROKEN. R & R LT FWD ENTRY DOOR UPPER AFT ROLLER BEARING THAT CONTACTS SWITCH IAW MM 20-11-00-2. DOOR & INDICATION OPERATIONS CHECKED GOOD. ACFT OK FOR SERVICE.

Part: SKIN — DENTED (FUSELAGE) · airframe 53,040 hrs · 22,941 cycles

LOWER FUSELAGE HAS A DENTED AREA BS 664 BETWEEN STRINGERS 25L & 26L. COMPLIED WITH EA F-5330-TO311447 PART 1. COMPLIED WITH HFEC & DVI INSPECTIONS NO DEFECTS NOTED. INSTALLED DENT DOT AT DENT LOCATION IAW GMM 6-3-101.

Part: FLOORBEAM — CORRODED (BS 1200) · corrosion level 2 · airframe 53,037 hrs · 22,939 cycles

MAIN CABIN BS 1200 BETWEEN BL 0 - LBL 24 FLOORBEAM CORRODED. REMOVED CORROSION FROM FLOORBEAM IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51 AD1. CUT OUT DAMAGED SECTION AND FABRICATED REPAIR ANGLES IAW SRM 53-00-51 REPAIR 3 & ER 2-37153-801A REV A. INSTALLED REPAIR TO FLOORBEAM IAW SRM 53-00-51 REPAIR 3.

Part: LANYARD — LOOSE (GIRT BAR) · airframe 52,337 hrs · 22,398 cycles

LEFT FWD ENTRY DOOR WILL NOT ARM AFTER CLOSED. FOUND LANYARD LOOSE TO GIRT BAR. REPOSITIONED LANYARD, CLOSED DOOR AND ARMED. OPS CHECKED GOOD IAW MM REF 25-66-10-2. OK TO CONTINUE.

Part: SKIN — DENTED (BS 663) · airframe 52,191 hrs · 22,308 cycles

DENT ON LOWER FUSELAGE SKIN, BS 663 BETWEEN S28-29R. CUT OUT DAMAGED AREA, FABRICATED REPAIR DOUBLER AND INSTALLED REPAIR IAW EA F-5330-T0302229 & SRM 51-40-02, 51-20-01 & 51-40-05.

Part: PLATE — CORRODED (BS 1680) · corrosion level 2 · airframe 52,191 hrs · 22,308 cycles

MAIN CABIN DECK PLATE AT BS 1680, LBL 12 HAS CORROSION. CUT OUT DAMAGED AREA, FABRICATED REPAIR DOUBLER & FILLER AND INSTALLED REPAIR IAW SRM 51-10-02, 53-60-51 REPAIR 2, 51-40-02, & 51-20-01.

Part: FLOORBEAM — CORRODED (BS 1680) · corrosion level 2 · airframe 52,191 hrs · 22,308 cycles

MAIN CABIN FLOORBEAM AT BS 1680, LBL 12 HAS CORROSION. CUT OUT DAMAGE, FABRICATED REPAIR AND INSTALLED IAW SRM 51-40-02, 53-60-51 REPAIR 3 FIG 201 AND 51-10-02.

Part: GIRT BAR — OBSTRUCTED (DOOR SLIDE) · airframe 51,659 hrs · 21,948 cycles

LEFT CREW ENTRY DOOR WILL NOT ARM, DOOR CLOSES. INSPECTED DOOR SLIDE IAW AMM 25-66-01-6, FOUND DIRT AND DEBRIS IN GIRT BAR TRACK. CLEANED TRACK, OPS CHECKED GOOD, ACFT OK FOR SERVICED.

Part: LAMP — INOPERATIVE (L1 DOOR SLIDE) · airframe 51,461 hrs · 21,832 cycles

L1 "SLIDE ARMED" LIGHT FOUND BURNED OUT DURING POST FLIGHT. LAMPED L1 "SLIDE ARMED" LIGHT IAW SMP CHECKED L1 DOOR ARM/DISARM OPERATION REF: AMM 52-11-00-6. OPS CHECKS GOOD. FINAL CLOSED.

Part: GIRT BAR — LACK OF LUBE (L1 DOOR) · airframe 51,066 hrs · 21,537 cycles

THE L1 DOOR IS DIFFICULT TO CLOSE AND DIFFICULT TO ARM. CLEANED DEBRIS FROM DOOR FRAME AND LUBRICATED GIRT BAR REF MM 12-21-18-3. OK TO CONTINUE. FINAL CLOSED.

Part: COVER — OUT OF ADJUST (L1 DOOR SLIDE) · airframe 50,979 hrs · 21,490 cycles

L1 DOOR WOULD NOT ARM. ADJUSTED L1 DOOR SLIDE COVER AND DOOR ARMS AS REQUIRED, IAW AMM 25-66-02-4. ACFT OK TO CONTINUE.

Part: FRAME — DENTED (BS 1500) · airframe 50,174 hrs · 21,057 cycles

FOUND FRAME UPPER FLANGE DENTED, BS 1500. FRAME REPAIRED IAW SRM 53-00-07, REPAIR 5 AND EA F-5310-153443 AND F-5310-153444.

Part: SKIN — TORN (PAX DOOR) · airframe 50,174 hrs · 21,057 cycles

R4 DOOR INTERNAL SKIN TORN AT LOWER AFT END AT APPROX BS 1672 AND WL. 213. CUT OUT DAMAGED AREA, FABRICATED DOUBLER AND INSTALLED DOUBLER IAW EA F-5210-152439.

Part: FRAME — DAMAGED (BS 1520 S26-27R) · airframe 50,174 hrs · 21,057 cycles

UPON REMOVAL OF RT TRANSITION PANEL, FOUND (2)EA ELONGATED FASTENER HOLES, BS 1520 FRAME UPPER FLANGE, S26-27R. CUT OUT DAMAGED AREA IAW SRM 51-10-02 AND 53-00-07 FIG 201 REPAIR 5. FABRICATED REPAIR IAW SRM 53-00-07 FIG 201 REPAIR 5 AND 51-40-5. INSTALLED REPAIR IAW SRM 51-40-2 AND 53-00-07 FIG 201 REPAIR 5, REV 103 AND EA F-5310-152444.

Part: FRAME — DENTED (BS 1500 S26-27R) · airframe 50,174 hrs · 21,057 cycles

UPON REMOVAL OF RT TRANSITION PANEL, FOUND FRAME UPPER FLANGE DENTED, BS 1500 BETWEEN STRINGER 27R TO 26R. CUT OUT DAMAGED AREA IAW SRM 51-10-2 AND 53-00-07 FIG 201 REPAIR 5. FABRICATED REPAIR IAW SRM 53-00-07 FIG 201 REPAIR 5, AND 51-40-5. INSTALLED REPAIR IAW SRM 51-40-02 AND 53-00-07 FIG 201 REPAIR 5, REV 103, AND EA F-5310-153443.

Part: SENSOR — FAILED (R1 DOOR SLIDE) · airframe 50,053 hrs · 20,990 cycles

R1 ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHT INOPERATIVE. FOUND FWD GIRT BAR SENSOR AT FAULT (S10216). R & R R1 ESCAPE SLIDE GIRT BAR FORWARD SENSOR AND ACTUATOR IAW MM 25-66-11-2, OPS TESTED SERVICABLE.

Part: SLIDE — DISLODGED (R1 DOOR) · airframe 50,053 hrs · 20,990 cycles

R1 DOOR EMERGENCY ESCAPE SLIDE FELL OUT OF DOOR WHILE DOOR WAS STILL ARMED. OCCURED PRIOR TO ACFT STAIR REMOVAL. R & R R1 DOOR SLIDE IAW MM 25-66-00-2-0, CHECKED SERVICEABLE.

Part: BATTERY PACK — MISINSTALLED (EMERGENCY LIGHTS) · airframe 49,189 hrs · 20,466 cycles

DOOR EMERGENCY LIGHT INOP INTERIOR. RELEASED FOR SERVICE IAW MEL: 33-51-01-01, CATEGORY: D EXPIRATION: 01JAN11 "MEL 33-51-01-01: INTERIOR EMERGENCY LIGHTS - INOP." FOUND BATTERY PACK NOT FULLY INSTALLED. SECURED BATTERY AND SYS OPS GOOD IAW MM 33-51-01.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 49,191 hrs · 20,467 cycles

R1 DOOR EXTERIOR EMERGENCY LIGHT INOP. RELAMPED R1 DOOR EMERGENCY LIGHT, OPS CHECKED GOOD, REF MM 33-51-06-2.

Part: RETAINER — CORRODED (APU INTAKE DOOR) · corrosion level 2 · airframe 46,574 hrs · 19,051 cycles

CORROSION ON NUT PLATE RETAINER OF APU INTAKE DOOR CUT-OUT BESIDE STA 1787.45 UPPER RT BULKHEAD. REMOVED AND REPLACED FWD SKIN STRAP, AFT SKIN DOUBLER, BOTTOM ANGLE SUPPORT IAW SRM 51-40-02 AND MFG BLUEPRINT 148N3138 THIS IS CLASSIFIED AS MAJOR REPAIR, NO FOLLOW-UP TRACKING REQUIRED .

Part: RETAINER — CORRODED (FUSELAGE) · airframe 46,574 hrs · 19,051 cycles

CORROSION ON NUT PLATE RETAINER OF APU INTAKE DOOR CUT-OUT BESIDES STA 1787.45 UPPER RT BULKHEAD. REMOVED AND REPLACED FWD SKIN STRAP, AFT SKIN DOUBLER, BOTTOM ANGLE SUPPORT IAW SRM 51-40-02 AND BLUEPRINT 148N3138. THIS IS CLASIFIED MAJOR REPAIR NO FOLLOW-UP TRACKING REQUIRED .

Part: SKIN — DELAMINATED (BS 1941 S5\R) · airframe 46,574 hrs · 19,051 cycles

APU COMPT RT SIDEWALL HAS 10 INCH BY 12 INCH DELAMINATION. REMOVED AND INSTALLED SERVICABLE APU COMPT SKIN IAW SRM 51-40-02,STA 1941. MAJOR REPAIR.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 46,574 hrs · 19,051 cycles

UPON REMOVAL OF SEAT TRACK AT LBL 24, BS 540-640, MAIN CABIN, IT WAS DISCOVERED THAT THERE WERE SEVERAL EXISTING ELONGATED FASTENER HOLES. TWO EACH AT BS 540-620 AND ONE EACH ON THE FOWARD SIDE OF BS 640. REPAIRED SEAT TRACK PER MAE EA 757-5335-16-F0975, REV -, DATED 06/02/2008, ON MAE NON- ROUTINE NR 68500220001. FEDEX NON-ROUTINE N01155 DOCUMENTS ACCOMPLISHMENT OF THIS REPAIR PER ABOVE NOTED MAE REFERENCES.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 46,574 hrs · 19,051 cycles

UPON REMOVAL OF SEAT TRACK AT LBL 24, BS 540-640, MAIN CABIN, IT WAS DISCOVERED THAT THERE WERE SEVERAL EXISTING ELONGATED FASTENER HOLES. TWO EACH AT BS 540-620 AND ONE EACH ON THE FOWARD SIDE OF BS 640. REPAIRED SEAT TRACK PER MAE EA 757-5335-16-F0975, REV -, DATED 06/02/2008, ON MAE NON- ROUTINE # 68500220001. FEDEX NON-ROUTINE N01155 DOCUMENTS ACCOMPLISHMENT OF THIS REPAIR PER ABOVE NOTED MAE REFERENCES.

Part: SEAT TRACK — CORRODED (BS 440-680) · corrosion level 2 · airframe 46,574 hrs · 19,051 cycles

SEAT TRACK LBL 45 STA 440-680 CORRODED AND SCALLOPS DAMAGED IN NUMEROUS LOCATIONS. FABRICATED SEAT TRACK FROM STA 440 TO 680 LBL 45.5 IAW MAE TRAV NR T8/739184 AND IAW SRM 53-00-52, INSTALLED SEAT TRACK IAW SRM 51-40-02, MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 440-680) · airframe 46,574 hrs · 19,051 cycles

SEAT TRACK LBL 45 STA 440-680 CORRODED AND SCALLOPS DAMAGED IN NUMEROUS LOCATIONS. FABRICATED SEAT TRACK FROM STA 440 TO 680 LBL 45.5 PER MAE TRAV NR T8/739184 AND IAW SRM 53-00-52. INSTALLED SEAT TRACK IAW SRM 51-40-02, MAYOR REPAIR.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 46,574 hrs · 19,051 cycles

MAIN CARGO DECK SEAT TRACK STA 1540-1640 LBL 24 CORRODED REMOVED SEAT TRACK IAW SRM 51-41-02. RECEIVED AND FABRICATED NEW SEAT TRACK ON MAE TRAV NR T8/746699, MAT ID BAC1520-792, 7178T6511 IAW SRM 53-00-52 FIG 201, BATCH NR 00013400254 AND LOCATED, TRIMMED, AND DRILLED IAW SRM 51-41-02. TREATED AND PRIMED IAW SRM 51-21-00 AND INSTALLED NEW SEAT TRACK IAW SRM 51-41-02.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,574 hrs · 19,051 cycles

MAIN CARGO DECK SEAT TRACK STA 1540-1640 LBL 24 CORRODED REMOVED SEAT TRACK IAW SRM 51-41-02. RECEIVED AND FABRICATED NEW SET TRACK ON M.A.E TRAV NR T8/746699, MAT ID BAC1520-792, 7178T6511 IAW SRM 53-00-52 FIG. 201, BATCH NR 00013400254 AND LOCATED, TRIMED, AND DRILLED IAW SRM 51-41-02 ,TREATED AND PRIMED IAW SRM 51-21-00 AND INSTALLED NEW SEAT TRACK IAW SRM 51-41-02.

Part: FLOORBEAM — CORRODED (BS 1640) · airframe 46,574 hrs · 19,051 cycles

CABIN FLOORBEAM, HAS CORROSION, BS 1640, LBL 6 - RBL 6. COMPLIED WITH EA F-5310-110867, REV -, DATED 05/20/2008. EA CLASSIFIED REPAIR AS A MAJOR REPAIR.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 46,574 hrs · 19,051 cycles

BS 440-640, LBL 24, SEAT TRACK HAS DOUBLE DRILLED HOLES AND GOUGES AROUND CLIPNUT HOLES. REMOVED DAMAGE SEAT TRACK IAW SRM 51-40-02. ALL DAMAGE TO SEAT TRACK IS OUT OF LIMITS PER SRM 53-00-52. FABRICATED A NEW SEAT TRACK, ON TRAVELER NR T8/741233, AND INSTALLED IAW SRM 51-40-02 AND 53-00-52. ALSO FABRICATED 2 ANGLES, 1 PLATE AS PART OF REPAIR FOR SEAT TRACK. THIS IS A CATEGORY "A" MAJOR REPAIR WITH NO FOLLOW UP TRACKING.

Part: FRAME — DENTED (ZONE 100) · airframe 46,574 hrs · 19,051 cycles

AFT CARGO COMPARTMENT, LT SIDE, STA 1340, S026L, FRAME IS DENTED. REPAIRED DENTED FRAME BY INSTALLING A FABRICATED DOUBLER REPAIR, ON MAE TRAVELER NR T8/741854, IAW SRM 53-00-07, REPAIR NR 5. THIS REPAIR IS CLASSIFIED AS A CATAGORY "A" MAJOR REPAIR.

Part: FRAME — DENTED (ZONE 100) · airframe 46,574 hrs · 19,051 cycles

AFT CARGO COMPARTMENT LT STA 1460 S-26L, FRAME IS DENTED. CUT OUT DAMAGED AREA IAW SRM 53-00-01, FIG 201. NDT, HFEC IAW NTM 51-00-00, FIG 6, OF CUT OUT AREA. FABRICATED SPLICE ANGLE IAW SRM 53-00-07, MAT. 7075T6, .071 INCH C, BATCH NR 532681, PO NR MST 0023621 ON MAE TRAVELER NR T8/743564. COLD WORKED HOLES IAW SRM 51-40-00 AND 53-00-07. INSTALLED ALL REPAIRS PARTS IAW SRM 51-40-02 AND 53-00-07. THIS REPAIR IS CLASSIFIED AS A CATEGORY "B" MAJOR REPAIR. INITIAL INSP OF REPAIR AT 37,500 FC AND REPEAT INSP. THEREAFTER AT 12,000 FC.

Part: SKIN — CORRODED (NR 2 STRUT) · airframe 46,574 hrs · 19,051 cycles

STRUT NR 2 INBD SIDE OF SKIN AT APPROX PPS 200.50 HAS EXFLOIATED CORROSION (APPEARS TO BE TRAVELING UNDER FRAME/CORD ALSO). REMOVED SKIN IAW SRM 51-40-02. REMOVED CORROSION AT STA 157, ORIGINAL MATERIAL THICKNESS .090", REMAINING THICKNESS .062", OUT OF LIMITS IAW SRM 54-50-01. REMOVED AND RE-INSTALLED INBD SUPPORT FITTING AND PLATE, 3EA ACCESS DOORS, 2EA BULB SEALS, HEAT SHIELD, AND INBD FAIRING IAW ARM 51-40-02 TO FACILITATE SKIN REMOVAL & INSTALLATION, INSTALLED REPAIR SKIN IAW DWG 311N5002 AND SRM 51-40-02. THIS IS A MAJOR REPAIR CATAGORY A NO FOLLOW UP TRACKING REQUIRED.

Part: SKIN — CORRODED (NR 2 STRUT) · airframe 46,574 hrs · 19,051 cycles

STRUT NR 2 INBOARD SIDE OF SKIN AT APPROX PPS 200.50 HAS EXFOLIATED CORROSION (APPEARS TO BE TRAVELING UNDER FRAME/CORD ALSO). REMOVED SKIN IAW SRM 51-40-02. REMOVED CORROSION AT STA 157, ORIGINAL MATERIAL THICKNESS .090 INCH, REMAINING THICKNESS .062 INCH, OUT OF LIMITS PER SRM 54-50-01. REMOVED AND RE-INSTALLED I/B SUPPORT FITTING AND PLATE, 3 ACCESS DOORS, 2 BULB SEALS, HEAT SHIELD, AND I/B FAIRING IAW ARM 51-40-02 TO FACILITATE SKIN REMOVAL AND INSTALLATION. INSTALLED REPAIR SKIN IAW DWG 311N5002 AND SRM 51-40-02. THIS IS A MAJOR REPAIR CATEGORY A, NO FOLLOW UP TRACKING REQUIRED.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,574 hrs · 19,051 cycles

BS 1440, STRINGER 28R, AFT CARGO DOOR LOWER SILL AREA, IS CORRODED. REMOVED CORROSION IAW SRM 53-00-03, FIG 1, DETAIL 3. CORROSION REMOVAK WAS 100% THROUGH MATERIAL. REMOVED AND REPLACED STRINGER 28R, FROM BS 1380 - 1457 IAW SRM 53-00-03 AND 51-40-02. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR, CATEGORY A.

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 46,574 hrs · 19,051 cycles

STA 440-640 RBL 24 SEAT TRACK HAS HOLE AND GOUGES AROUND CLIPNUTS HOLE. REMOVED DAMAGED SEAT TRACK IAW SRM 51-40-02. FABRICATED NEW SEAT TRACK ON MAE TRAVELER T8/741234 MAT BAC1520-792-7178-T6511. INSTALLED NEW SEAT TRACK AND SPLICE REPAIR ON STA 440-530 IAW SRM 53-00-52, 51-40-02. MAJOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 780-879) · corrosion level 2 · airframe 46,574 hrs · 19,051 cycles

FOUND SEAT TRACK HAS CORROSION STA 780-879 LBL 45. REMOVED SEAT TRACK, FAB`D NEW FROM MAT BAC1520-792, AND INSTALLED SEAT TRACK STA 780-879 LBL 45 IAW SRM 51-40-02.

Part: SEAT TRACK — CORRODED (BS 377-440) · corrosion level 3 · airframe 46,574 hrs · 19,051 cycles

FOUND STA 377-440 LBL 45 SEAT TRACK HAS CORROSION. REMOVED SEAT TRACK, FAB`D FROM MAT BAC1520-792, IAW SRM 51-10-02. TREATED AND PRIMED AND INSTALLED NEW SEAT TRACK STA 377-440, LBL 45 IAW SRM 51-40-02.

Part: SEAT TRACK — CORRODED (BS 780-879) · corrosion level 2 · airframe 46,574 hrs · 19,051 cycles

FOUND SEAT TRACK STA 780-879 RBL 45 HAS CORROSION. REMOVED SEAT TRACK, FAB`D NEW FROM MAT BAC1520-792 IAW SRM 51-10-02. INSTALLED SEAT TRACK STA 780-879 RBL 45, IAW SRM 51-40-02.

Part: SEAT TRACK — CORRODED (BS 780-879) · airframe 46,574 hrs · 19,051 cycles

FOUND SEAT TRACK HAS CORROSION STA 780-879, LBL 24. REMOVED SEAT TRACK, FAB`D NEW FROM MAT BAC1520-792 IAW SRM 53-00-52. INSTALLED SEAT TRACK STA 780-879, LBL 24, IAW SRM 51-40-02. MINOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 780-879) · corrosion level 2 · airframe 46,574 hrs · 19,051 cycles

FOUND SEAT TRACK STA 780-879 RBL 24 HAS CORROSION. REMOVED SEAT TRACK, FAB`D NEW FROM MAT BAC1520-792 IAW SRM 53-00-52. INSTALLED SEAT TRACK STA 780-879, RBL 24 IAW SRM 51-40-05.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 46,574 hrs · 19,051 cycles

FLOORBEAM HAS CORROSION BS 1300, RBL 28, BELOW UPPER T-CAP FWD SIDE, AT FLOOR PANEL HOLE. REMOVED CORROSION ON FLOORBEAM IAW SRM 51-00-51. AFTER CORROSION REMOVAL FOUND FLOORBEAM TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL 3. REWORK DIMENSIONS ARE AS FOLLOWS: L=1.0", W=2.0", D=.035". FABRICATED REPAIR ANGLES PER MAE TRAVELER NR T8/734293 AND T8/734294. FABRICATED REPAIR STRAPS IAW SRM 53-00-51. FABRICATED REPAIR TEE SECTION IAW SRM 53-00-51. LOCATED AND DRILLED ALL REPAIR PARTS AND TREATED/PRIMED IAW SRM 53-00-51. INSTALLED ALL REPAIR PARTS IAW SRM 53-00-51. THIS REPAIR IS A CATEGORY "A" REPAIR AND MAJOR. NO FOLLOW UP TRACKING IS REQUIRED.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,574 hrs · 19,051 cycles

MCD FLOOR SUPPORT HAS CORROSION, STA 1660-1681, RBL1, WL 208. REMOVED CORROSION, L= 2", W= .75", D= .010", ORIGINAL MATERIAL THICKNESS .050" FOUND TO BE OUT OF SRM 53-00-51, FIG 101, DETAIL III LIMITS. REMOVED FLOOR SUPPORT CHANNEL IAW SRM 51-40-02. FABRICATED REPLACEMENT CHANNEL ON MAE TRAVELER NR T8/732409, FROM 7075-0 .050B, HEAT TREATED TO T6. INSTALLED REPLACEMENT CHANNEL IAW SRM 51-40-02. THIS IS A CATEGORY "A", MINOR REPAIR WITH NO RECURRING INSPECTIONS.

Part: STIFFENER — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,574 hrs · 19,051 cycles

RIGHT MLG WHEEL WELL, STIFFENER FOR FAIRING STRUCTURE BETWEEN STA 1128-1146, RBL 75 IS CORRODED. AFTER CORROSION REMOVAL FOUND STIFFENER TO BE OUT OF SRM 53-00-71, FIG 101, DETAIL VII LIMITS. ORIGINAL MATERIAL THICKNESS .050", AFTER CORROSION REMOVAL .036 INCH. REMOVED STIFFENER IAW SRM 51-40-02. FABRICATED REPLACEMENT STIFFENER ON MAE TRAVELER NR T8/729363 FROM 7075 - O .050", HEAT TREATED TO T6 IAW SRM 53-40-71. INSTALLED REPLACEMENT STIFFENER IAW SRM 51-40-05 AND 51-40-02.