N933FR

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 33,944 hrs · 16,750 cycles

OPERATIONAL TEST OF EMERGENCY LIGHTS FAILED DURING HEAVY SERVICE CHECK. R & R EPSU BATTERY PACK 10WL IAW AMM 33-51-00-920-050-A.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 33,944 hrs · 16,750 cycles

OPERATIONAL TEST OF EMERGENCY LIGHTS FAILED DURING HEAVY SERVICE CHECK. R & R EPSU BATTERY PACK L1WL IAW AMM 33-51-00-920-050-A.

Part: BATTERY — DISCHARGED (CABIN) · airframe 32,814 hrs · 16,196 cycles

EMERGENCY LIGHTS FAILED EMERGENCY LIGHT TEST. EPSU BATTERY EMERGENCY RT FAULT & 12WL, EMERGENCY EXIT RT BATTERY NEEDS REPLACED. R & R EPSU BATTERY EMERGENCY EXIT RT IAW AMM 33-51-38 PB 401, OPERATIONS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 31,364 hrs · 15,405 cycles

EPSU BATTERY 13WL FAILED TEST ON HEAVY SERVICE CHECK. R & R BATTERY ASSEMBLY. OPS CHECK GOOD. REF AMM 33-51-39-000-005A AND AMM 33-51-39-400-005A.

Part: SERVO — FAULTED (NLG STEERING) · airframe 28,790 hrs · 14,088 cycles

IN CRUISE, RECEIVED WHEEL NOSE LANDING WHEEL STEERING FAULT. REPLACED NOSE WHEEL STEERING SERVO CONTROL REF AMM 32-5 1-5 1-ODO-OO1 -A, 32-5 1-51 ·400-00 I-A, TEST OK. NO LEAKS NOTED.

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 21,689 hrs · 10,561 cycles

REF NON=ROUTINE N0691, FWD CARGO FLOOR PANEL 131AF BROKEN COTR APPROX 2.0 IN X 2.5 IN. ACFT IS IN C-CHECK. REPAIR DAMAGE AREA ON PANEL 131AF USING RESIN AND GLASS CLOTH PATCH METHOD IAW SRM 53-02-00, PARA 8B.

Part: PLATE — CORRODED (ZONE 100) · airframe 21,689 hrs · 10,561 cycles

REF NON-ROUTINECARD N0392, AFT CABIN RT SHEAR PLATE BETWEEN FRAMES 69 AND 70, HAS CORROSION THAT IS OUT OF LIMITS. R & R SHEAR PLATE AT AFT CABIN RT SIDE BETWEEN FRAMES 69 AND 70 IAW SRM 51-42-11 AND EO AO-53E0-31434.

Part: SILL — CORRODED (ZONE 200) · airframe 21,689 hrs · 10,561 cycles

MAIN CABIN FLOOR STRUCTURE LONGERON AT OTBD POSITION FRAME 66 HAS A 1 SQ IN ARE OF CORROSION REF NON-ROUTINE N0451. CUT OUT CORROSION AT NUTPLATE HOLE IAW SRM 53-42-14 PRINCIPLE 6 FABRICATED REPAIR ANGLES IAW SRM 53-42-14 PRINCIPLE 6 TREATED PRIMED AND TOP COOFED REPAIR PARTS IAW SRM 53-42-14 PRINCIPLE 6 INSTALLED REPAIR ANGLES AND FILLER IAW 53-42-14 PRINCIPLE 6.

Part: CONTROL CABLE — OUT OF LIMITS (RUDDER) · airframe 21,689 hrs · 10,561 cycles

REF AEROFRAME NON-ROUTINE N0491 RUDDER CABLE TENSION ON TESSION REGULATOR IS OUT OF LIMITS. R & R RUDDER TENSION REGULATOR IAW AMM 27-21-48, PAGE 401. OPS CHECK RUDDER IAW AMM 27-24-00-710-001. OPS CHECKS GOOD.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 21,689 hrs · 10,561 cycles

REF HEAVY MX NON ROUTINE N0604. MAIN CABIN FLOOR PANEL 261 PF HAS COMPOSITE DAMAGE. REPAIRED 9 EACH AREAS OF SKIN DAMAGE ON FLOOR PANEL 261PF USING RESIN AND GLASS CLOTH IAW SRM 53-02-00, PARAGRAPH 8.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 21,689 hrs · 10,561 cycles

REF HEAVY MX NON ROUTINE N0561. RT CABIN FLOOR AT FRAME 69 TO FRAME 70 SUPPORT EXTRUSION BELOW SHEAR PLATE IS CORRODED. R & R SUPPORT IAW SRM 51-72-11.

Part: LIGHT — NO TEST (ESCAPE SLIDE) · airframe 17,060 hrs · 8,330 cycles

DURING HEAVY CHECK, INSPECTION NOTED THE L2 DOOR EMERGENCY LIGHT FAILED TO TEST. MAINTENANCE REMOVED AND INSTALLED A NEW SLIDE, REFERENCE AMM 25-62-44 PB 401.

Part: STRUT — DAMAGED (NLG) · airframe 16,648 hrs · 8,138 cycles

REFERENCE NON-ROUTINE C057865. DURING C3 C-CHECK, INSP NOTED THE LT NLG AFT GROMMET WORN .005 DEEP, .690 VERTICAL, .520 WIDE, 21 INCHES UP FROM THE BOTTOM OF THE BARREL. MX PERFORMED MAJOR REPAIR, BLENDED DAMAGE, PERFORMED FLAP-PEEN, NDT AND PAINTED IAW EA A9-32R-30965 REVISION A.

Part: ATTACH FITTING — CRACKED (NLG WW) · airframe 16,648 hrs · 8,138 cycles

REFERENCE NON-ROUTINE C057626. DURING C3 C-CHECK, MAINTENANCE COMPLIED WITH A MAJOR REPAIR OF THE LT NLG ACTUATOR ATTACH FITTING THAT WAS FOUND CRACKED WHILE PERFORMING EO A0-53EO-2073. REPAIR PERFORMED IAW EA A9-53R-12014 REVISION A, STEPS 1-16.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 16,648 hrs · 8,138 cycles

REFERENCE NON ROUTINE C058373. DURING C3 C-CHECK, INSPECTION CORROSION ON FLOOR PANEL 262FF. MAINTENANCE REMOVED AND REPLACED FLOOR PANEL WITH NEW, REFERENCE WORK CARD C534103-01 AND AMM 53-42-12-400-002.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 16,648 hrs · 8,138 cycles

REFERENCE NON-ROUTINE C058372. DURING C3 C-CHECK, INSPECTION NOTED CORROSION ON FLOOR PANEL 261FF. MAINTENANCE REMOVED AND REPLACED FLOOR PANEL WITH NEW, REFERENCE WORK CARD C534103-01 AND AMM 53-42-12-400-002.

Part: BARREL — DAMAGED (ZONE 700) · airframe 16,648 hrs · 8,138 cycles

REFERENCE NON-ROUTINE C057860. DURING C3 C-CHECK, INSP NOTED THE RT NLG AFT GROMMET WORN ON CORNER WEB .002 DEEP, .550 VERTICAL, .500 WIDE, 21.375 INCHES UP FROM THE BOTTOM OF THE BARREL AT INTERSECTION OF LOWER WEB TO BARREL. MX PERFORMED MAJOR REPAIR, BLENDED DAMAGE, PERFORMED FLAP-PEEN, NDT AND PAINTED IAW EA A9-32R-30965 REVISION A.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 16,648 hrs · 8,138 cycles

REFERENCE NON ROUTINE C057992. DURING C3 C-CHECK, INSPECTION NOTED CORROSION ON VARIOUS NUT CLIP FASTENER HOLES ON FLOORBEAM Y1292 BETWEEN FRAME 66 AND FRAME 68. MAINTENANCE REMOVED AND REPLACED FLOORBEAM WITH NEW PER SRM 51-42-11.

Part: ROLLER — BROKEN (DOOR HANDLE) · airframe 12,204 hrs · 5,934 cycles

MAINTENANCE REPORTED BROKEN ROLLER BEARING ON L2 SERVICE DOOR OUTER HANDLE/LATCH. REMOVED AND REPLACED CRANK ON THE OUTER CONTROL HANDLE IAW AMM 52-13-21-400-001. OPS CHECK NORMAL.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 10,752 hrs · 5,226 cycles

DURING C-2 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FLOOR PANEL 151VE DAMAGED. REPAIRED FLOOR PANEL 151VE IAW SRM 53-02-00.

Part: PANEL — DAMAGED (FUSELAGE) · airframe 10,752 hrs · 5,226 cycles

DURING C-2 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT TRANSITION PANELS 151BE, 151UG, 161BF, AND 161CF DAMAGED. REPAIRED TRANSITION PANELS IAW SRM 53-02-00, FIG 204.

Part: PANEL — DAMAGED (FUSELAGE) · airframe 10,752 hrs · 5,226 cycles

DURING C-2 CHECK, INSPECTION REPORTED FWD CARGO COMPARTMENT TRANSITION PANEL 131CF DAMAGED. REPAIRED ONE SKIN PENETRATION IAW SRM 53-02-00, PAGE 204, 205, PARA 2-E, FIG. 201, AND AMM 25-00-00-370-001.