N914FR

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 30,009 hrs · 14,354 cycles

C-CHECK: NON ROUTINE NR 36931; CABIN FR66 Y-1292 FWD OF SPLICE FLOOR SUPPORT HAS CORROSION. REPLACED FWD FLOOR SUPPORT IN MAIN CABIN AT FR66 Y-1292 IAW SRM 51-42-11 PARA 5, PARA 6A.(3), PARA 7.A.(6)(7).

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 30,009 hrs · 14,354 cycles

NON-ROUTINE 36905; CABIN FR68 Y-1292 AFT OF SPLICE FLOOR SUPPORT HAS CORROSION. REPLACED AFT FLOOR SUPPORT IN MAIN CABIN AT FR68 Y-1292 IAW SRM 51-42-11 PARA 5, PARA 6.A.(3), PARA 7 A.(6)(7).

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 30,009 hrs · 14,354 cycles

C-CHECK: NON ROUTINE NR 36907; CABIN FR66, Y-1292 AFT OF SPLICE FLOOR SUPPORT HAS CORROSION. REPLACED AFT FLOOR SUPPORT IAW SRM 51-42-11, PARA 5, PARA 6.A.(3) AND PARA 7A.(6)(7).

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 30,009 hrs · 14,354 cycles

C-CHECK: NON ROUTINE 36929; CABIN FRAME 68 Y-765, FLOOR SUPPORT HAS SURFACE CORROSION. R & R FLOOR IAW SRM 51-42-11, PARA 5 AND 6.B, PARA 7.B, SRM 51-44-11, PARA 2.A. AND B.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 30,009 hrs · 14,354 cycles

C-CHECK: NON ROUTINE 36906; CABIN FR68 - FR66 Y-1292 FLOOR SUPPORT HAS CORROSION IN NUMEROUS AREAS. REPLACED FLOOR SUPPORT, MAIN CABIN AT FR68 - FR66 Y-1292 IAW SRM 51-42-11, PARA 5, PARA 6.A.(3), PARA 7.A(6)(7).

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,009 hrs · 14,354 cycles

C-CHECK: NON ROUTINE NR 36902; FRAME 70 RT INTERNAL SHEAR PLATE HAS CORROSION. R & R SHEAR PLATE IAW SRM 51-42-11, FIG 8, 51-44-11 PARA 6A (1), 7A(1) AND PARA 7, FIG 12, 51-21-11 PARA 4 (A)-(D), 51-75-12 AND 51-23-11.

Part: SILL — CORRODED (ZONE 200) · corrosion level 2 · airframe 30,009 hrs · 14,354 cycles

NON ROUTINE NR 36903; CABIN FR68 AT RT AT DOOR SILL BEAM HAS CORROSION. REPAIRED SILL BEAM IAW SRM 53-41-14. REPAIR PRINCIPLE K.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 30,009 hrs · 14,354 cycles

C-CHECK: NON ROUTINE NR 36889; CABIN FR68-FR66, Y1292 FWD OF SPLICE FLOOR SUPPORT HAS CORROSION. REPLACED FWD FLOOR SUPPORT IN MAIN CABIN AT FR68-FR666, Y1292 IAW SRM 51-42-11, PARA 5, PARA 6.A.(3), PARA 7. A.(6)(7).

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 30,009 hrs · 14,354 cycles

C-CHECK: NON ROTINE 36933; CABIN FR66, Y-765 FWD OF SPLICE, FLOOR SUPPORT HAS CORROSION AT FLOOR PANEL. REPLACED CABIN FLOOR SUPPORT FR66, Y-765 IAW SRM 51-42-11 PARA 5, PARA 6.D, PARA 5.A. AND B.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 30,009 hrs · 14,354 cycles

C-CHECK: NON ROUTINE NR 36890; CABIN FR68 AT L2 DOOR OTBD FLOOR SUPPORT HAS CORROSION. REPAIRED SILL BEAM IAW SRM 53-41-14, FIG 201, REPAIR PRINCIPLE K.

Part: SKIN — DENTED (ZONE 100) · airframe 30,009 hrs · 14,354 cycles

C-CHECK: NON ROUTINE NR 36804; FUSELAGE UNDER FWD CARGO DOOR FRAME 26, BETWEEN STR 43 RT AND 43 LT HAS A DENT. REPAIR SKIN DENT REF SRM 53-21-11, PARA 5.K, FIG 214 REPAIR CATEGORY B.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 30,009 hrs · 14,354 cycles

C-CHECK: NON ROUTINE NR 36930; CABIN FR66, Y-765 FWD OF SPLICE HAS CORROSION AT FLOOR PANEL ON FLOOR SUPPORT. REPLACED CABIN FLOOR SUPPORT FR66, Y-765 IAW A319 SRM 51-42-11, PARA 5 AND 6.D AND PARA 5A. AND B.

Part: PROFILE — CORRODED (ZONE 100) · airframe 24,572 hrs · 11,785 cycles

DURING C5 C-CHECK, INSPECTION NOTED THAT THE PROFILE AT FRAME 28 IN THE FORWARD CARGO PIT HAD CORRODED FLOOR PANEL ATTACH HOLES. MAINTENANCE REMOVED AND REPLACED THE PROFILE IAW SRM 51-72-11 AND 51-42-11.

Part: PROFILE — CORRODED (ZONE 100) · airframe 24,572 hrs · 11,785 cycles

DURING C5 C-CHECK, INSPECTION NOTED THE PROFILE AT FRAME 34 IN THE FORWARD CARGO PIT HAD CORRODED FLOOR PANEL ATTACH HOLES. MAINTENANCE REMOVED AND REPLACED THE PROFILE IAW SRM 51-72-11 AND 51-42-11.

Part: PROFILE — CORRODED (ZONE 100) · airframe 24,572 hrs · 11,785 cycles

DURING C5 C-CHECK, INSPECTION NOTED THAT THE PROFILE LOCATED BETWEEN FRAME 24.5 AND FRAME 28, HAD CORROSION AROUND THE FLOOR PANEL ATTACH HOLES. MAINTENANCE REMOVED AND REPLACED THE PROFILE IAW SRM 51-72-11.

Part: PROFILE — CORRODED (ZONE 100) · airframe 24,572 hrs · 11,785 cycles

DURING C5 C-CHECK, INSPECTION NOTED THE PROFILE LOCATED BETWEEN THE FORWARD AND AFT FLOOR PANELS AT FRAME 28 HAD CORRODED ATTACH HOLES. MAINTENANCE REMOVED AND REPLACED THE PROFILE IAW SRM 51-72-11.

Part: ROLL PIN — SHEARED (EMERGENCY EXIT) · airframe 24,572 hrs · 11,785 cycles

DURING DEN C5 C-CHECK, INSPECTION NOTED THAT THE LT EMERGENCY EXIT DOOR LOCKING PIN WILL NOT LOCK IN THE ARMED POSITION. MAINTENANCE REMOVED AND REPLACED THE ROLL PIN THAT HOLDS THE LOCKING PIN IN PLACE PER AMM 52-21-11-400-003.

Part: CONTROL CABLE — LACK OF LUBE (EMERGENCY EXIT) · airframe 24,572 hrs · 11,785 cycles

DURING C5 C-CHECK, INSPECTION NOTED THAT THE RT OVERWING EXIT FLEX CONTROL CABLE FOR THE INFLATION RESERVOIR FAILED THE FUNCTIONAL TEST. MAINTENANCE LUBRICATED THE OVERWING EXIT CONTROL CABLE IAW AMM 52-21-00-720-001 AND AMM 25-62-00-640-001.

Part: PROFILE — CORRODED (ZONE 100) · airframe 24,572 hrs · 11,785 cycles

DURING DEN C5 C-CHECK, INSPECTION NOTED CORROSION BETWEEN FRAME 28 AND FRAME 30 ON THE AFT RIGHT HAND FLOOR PROFILE ATTACH HOLES. MAINTENANCE REMOVED AND REPLACED THE PROFILE IAW SRM 51-42-11 AND 51-72-11 PARAGRAPH 6.

Part: PLATE — CORRODED (FUELAGE) · corrosion level 2 · airframe 19,583 hrs · 9,232 cycles

DURING C4 S1 C CHECK INSPECTION NOTED MAIN DECK WEB AT FRAME 70 RBL 52 WAS CORRODED. MAINTENANCE REMOVED AND REPLACED MAIN DECK WEB AT FRAME 70 RBL 52 IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-72-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FITTING — FAILED (PAX DOOR) · airframe 19,583 hrs · 9,232 cycles

DURING C4 S1 C CHECK INSPECTION REPORTED THE FORWARD ENTRY DOOR FAILED RIG CHECK AT TORSION BAR BELL CRANK AND REDUCER SHAFT BELLCRANK. MAINTENANCE REMOVED AND REPLACED LEFT FITTING FOR RIG PIN AND ADJUSTED DOOR RODS IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 52-11-21-400-001 AND CHECKED RIG PINS IN ACCORDANCE WITH THE REQUIREMENTS OF WORK CARD C528002-2 STEP 4B. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FITTING — FAILED (PAX DOOR) · airframe 19,583 hrs · 9,232 cycles

DURING C4 S1 C CHECK INSPECTION NOTED THE FORWARD ENTRY DOOR FAILED RIG CHECK AT THE TORSION BAR BELL CRANK AND REDUCER SHAFT. MAINTENANCE REMOVED AND REPLACED THE LEFT FITTING FOR RIG PIN AND ADJUSTED DOOR RODS IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 52-11-400-001. MAINTENANCE CHECKED THE RIG PINS IN ACCORDANCE WITH THE REQUIREMENTS OF WORK CARD C528002-2 STEP 4B. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOOR PANEL — PUNCTURED (FUSELAGE) · airframe 19,583 hrs · 9,232 cycles

DURING C4 S1 C CHECK INSPECTION NOTED PANEL 251RF HAS TWO PUNCTURES. MAINTENANCE CLEANED AREA OF DAMAGE, PREPPED AND APPLIED REPAIR IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 53-02-00. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOOR PANEL — CORRODED (CABIN) · corrosion level 2 · airframe 19,583 hrs · 9,232 cycles

DURING C4 S1 C CHECK INSPECTION REPORTED CORROSION ON MAIN CABIN R1 DOOR ENTRY FLOOR PANEL LOWER SURFACE AND AT VARIOUS FASTENER HOLES. MAINTENANCE REMOVED AND REPLACED R1 DOOR ENTRY PANEL 222FF. INSTALLATION WILL BE ACCOMPLISHED ON WORK CARD CP753-12.

Part: STRAP — CORRODED (FUSELAGE) · airframe 19,583 hrs · 9,232 cycles

DURING C4 S1 C CHECK INSPECTION REPORTED SURFACE CORROSION ON AFT CARGO BAY FLOOR STRAP FROM FLOOR STRAP 2350-2030 STRINGER 38 LEFT. MAINTENANCE FABRICATED NEW STRAP OUT OF 2024-T3 .040 IN ACCORDANCE WITH THE REQUIREMENTS OF AIRBUS A319 DRAWING D53470477. PART WAS TREATED, PRIMED AND PAINTED IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-21-11 AND SRM 51-42-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: WIRE HARNESS — MISSING (EMERGENCY LIGHT) · airframe 19,583 hrs · 9,232 cycles

DURING C4 S1 C CHECK INSPECTION REPORTED EMERGENCY LIGHT CONNECTOR MISSING MATE LOCK CAP SEAT ROW 1 HARNESS 350WLI. MAINTENANCE REPLACED CONNECTOR HARNESS, HARNESS TO BE INSTALLED ON AIRCRAFT IN CONJUNCTION WITH INSTALLATION OF CARPET, SEATS IN ACCORDANCE WITH WORK CARD CP725-1 ITEM 9601 STEP 4 D 2.

Part: FLOOR PANEL — DAMAGED (221DF) · airframe 19,583 hrs · 9,231 cycles

DURING C4 S1 C CHECK, INSPECTION REPORTED DELAMINATION, AT THE EDGES, AND A LARGE GOUGE, IN FLOOR PANEL 221DF. MAINTENANCE REPAIRED THE FLOOR PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 51-77-12. UPON COMPLETION OF THE REPAIR, THE PANEL WAS INSPECTED AND FOUND ACCEPTABLE.

Part: PANEL — DAMAGED (CARGO BAY) · airframe 19,583 hrs · 9,232 cycles

DURING C4 S1 C CHECK INSPECTION REPORTED PANEL 151TG AFT CARGO SLANT PANEL HAS HOLE. MAINTENANCE FABRICATED DOUBLER AND APPLIED REPAIR IN ACCORDANCE WITH SRM 53-02-00 AND AMM 25-00-00. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOOR PANEL — DAMAGED (221EF) · airframe 19,583 hrs · 9,231 cycles

DURING C4 S1 C CHECK, INSPECTION REPORTED FLOOR PANEL 221EF HAD PUNCTURE DAMAGE. MAINTENANCE REPAIRED THE PUNCTURE IN THE PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-12-00. UPON COMPLETION OF THE REPAIR, THE PANEL WAS INSPECTED AND FOUND ACCEPTABLE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,583 hrs · 9,231 cycles

DURING C4 S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND ON SEAT TRACK Y-1292, AT FUSELAGE STATION 810, ON THE RIGHT SIDE, EXTENDING FORWARD TOWARD FRAME 20. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 51-72-11, PAGES 1 AND 2. UPON COMPLETION OF THE INSTALLATION, IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: STRAP — CORRODED (CARGO FLOOR) · corrosion level 2 · airframe 19,583 hrs · 9,232 cycles

DURING C4 S1 CHECK INSPECTION REPORTED SURFACE CORROSION ON CARGO BAY FLOOR STRAP 2403 TO 2456 STRINGER 38R. MAINTENANCE REMOVED AND REPLACED FLOOR STRAP IN ACCORDANCE WITH SRM 51-72-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,583 hrs · 9,232 cycles

DURING C4 S1 C CHECK INSPECTION REPORTED SURFACE CORROSION ON AFT CARGO BAY FLOOR FRAME STRAP UPPER SURFACE AT FLOOR STRAP 2243 FRAME 56. MAINTENANCE REMOVED AND REPLACED FLOOR STRAP IN ACCORDANCE WITH SRM 51-72-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: STRAP — CORRODED · corrosion level 2 · airframe 19,583 hrs · 9,232 cycles

DURING C4 S1 C CHECK INSPECTION REPORTED SURFACE CORROSION ON AFT CARGO BAY FLOOR STRAP FROM FLOOR STRAP 2216 TO 2030 STRINGER 38 RIGHT. MAINTENANCE REMOVED AND REPLACED DAMAGED FLOOR STRAP IN ACCORDANCE WITH SRM 53-41-14 FIGURE 2 AND SRM 51-42-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: STRAP — CORRODED · corrosion level 2 · airframe 19,583 hrs · 9,232 cycles

DURING C4 S1 C CHECK INSPECTION REPORTED CORROSION ON AFT CARGO BAY FLOOR FRAME STRAP UPPER SURFACE FLOOR STRAP 2350 FRAME 58. MAINTENANCE REMOVED AND REPLACED FLOOR STRAP 2350 AT FRAME 58 IN ACCORDANCE WITH SRM 51-72-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,583 hrs · 9,231 cycles

DURING C4 S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND UNDER THE WEB AT FRAME 70 AND RIGHT BUTT LINE 52. MAINTENANCE REMOVED AND REPLACED THE WEB AT FRAME 70 IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 51-72-11. UPON COMPLETION OF THE INSTALLATION, THE NEW WEB WAS INSPECTED AND FOUND ACCEPTABLE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,583 hrs · 9,231 cycles

DURING C4 S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND ON SEAT TRACK Y-1292, AT FUSELAGE STATION 810, ON THE RIGHT SIDE, EXTENDING FORWARD TOWARD FRAME 20. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 51-72-11, PAGES 1 AND 2. UPON COMPLETION OF THE INSTALLATION, IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: SEAT TRACK — CORRODED · corrosion level 2 · airframe 19,583 hrs · 9,232 cycles

DURING C4 S1 C CHECK INSPECTION REPORTED DEEP CORROSION CABIN FLOOR STRUCTURE SEAT TRACK AT FRAME 21, Y1292 FLOOR STRAP 810. MAINTENANCE REMOVED AND REPLACED NEW SEAT TRACK AND ONE SPLICE IN ACCORDANCE WITH SRM 51-72-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOOR PANEL — DAMAGED (222EF) · airframe 19,583 hrs · 9,231 cycles

DURING C4 S1 C CHECK, INSPECTION REPORTED FLOOR PANEL 222EF HAD PUNCTURE DAMAGE. MAINTENANCE REPAIRED THE PUNCTURE IN THE FLOOR PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-12-00. UPON COMPLETION OF THE REPAIR, THE PANEL WAS INSPECTED AND FOUND ACCEPTABLE.

Part: FLOOR PANEL — CORRODED (261PF) · corrosion level 2 · airframe 19,583 hrs · 9,231 cycles

DURING C4 S1 C CHECK, INSPECTION REPORTED CORROSION AND DAMAGE WAS FOUND ON FLOOR PANEL 261PF, UNDER THE RIGHT CORNER OF THE AFT GALLEY. MAINTENANCE REPAIRED THE CORROSION AND DAMAGE IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-12-00. UPON COMPLETION OF THE REPAIRS, THE PANEL WAS INSPECTED AND FOUND ACCEPTABLE.

Part: COVER — BROKEN (EMERGENCY LIGHTS) · airframe 19,583 hrs · 9,231 cycles

DURING C4 S1 C CHECK, INSPECTION REPORTED A CRACK WAS FOUND IN THE EMERGENCY EXIT LIGHT LENS COVER LOCATED ON THE AFT SIDE OF THE FORWARD RIGHT DOOR FRAME. MAINTENANCE REMOVED AND REPLACED THE LENS COVER IN ACCORDANCE WITH AMM 33-51-13 PB 400-001. THE LIGHT WAS TESTED IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 33-51-13-400-001 AND OPERATIONALLY TESTED OKAY.

Part: LAMP — DEFECTIVE (EMERGENCY LIGHTS) · airframe 19,583 hrs · 9,231 cycles

DURING C4 S1 C CHECK, INSPECTION REPORTED THE EMERGENCY EXIT LIGHT, ABOVE THE L1 DOOR ENTRANCE, FLICKERED. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 33-21-11-020-50 AND AMM 33-21-11-42-050. THE LAMP WAS OPERATIONALLY TESTED IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 32-21-11-710-050 AND TESTED OKAY.

Part: SUPPORT BEAM — CORRODED (FRAME 67-69) · corrosion level 2 · airframe 11,580 hrs · 5,320 cycles

DURING REMOVAL OF FLOOR PANEL 262EF FOR DISCREPANCY REGARDING AFT LAVATORIES, MAINTENANCE REPORTED CORROSION ON AFT GALLEY FLOOR SUPPORT BEAM BETWEEN FRAME 67-69 Y-765. REPLACED FLOOR SUPPORT BEAM IAW SRM 53-00-14 AND 53-41-14.

Part: ATTACH FITTING — CORRODED (LAVATORY) · corrosion level 2 · airframe 11,580 hrs · 5,320 cycles

DURING REMOVAL OF FLOOR PANEL 262EF FOR DISCREPANCY REGARDING AFT LAVATORIES, MAINTENANCE REPORTED L-2 DOORWAY FLOOR PANEL AFT ATTACH PLATE CORRODED. FABRICATED NEW ATTACH PLATE PER AIRBUS DRAWING 10D53670099. TREATED, INSTALLED AND INSTALLED ATTACH PLATE PER SRM 51-42-11, 51-72-11, AND 51-23-00.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,580 hrs · 5,320 cycles

DURING REMOVAL OF FLOOR PANEL 262EF FOR DISCREPANCY REGARDING AFT LAVATORIES, MAINTENANCE REPORTED AFT GALLEY FLOOR SUPPORT BEAM AT R-2 DOOR CORRODED ON TOP OF FLANGE. REPLACED SUPPORT BEAM IAW SRM 53-00-14, 53-41-14 AND AIRBUS DRAWING 18D53472815.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,580 hrs · 5,320 cycles

DURING REMOVAL OF FLOOR PANEL 262EF FOR DISCREPANCY REGARDING AFT LAVATORIES, MAINTENANCE REPORTED CORROSION ON AFT GALLEY CONNECTING PLATE MOUNT HOLES FOR FLOOR PANEL. REPLACED CONNECTING PLATE IAW AMM 53-42-12-400-002.