N435FE

Part: JACKSCREW — FAILED (LE SLATS) · airframe 42,570 hrs · 20,612 cycles

DURING DESCENT AT MEM TO 36R, SLATS WOULD NOT EXTEND AT 210 KTS. EXECUTED QRH PROCEDURES, DECLARED EMERGENCY AND REMAINDER OF APPROACH AND LANDING NORMAL. CREW LEFT SLAT/FLAP HANDLE IN 30/40 POSITION TO ASSIST MX PROCEDURES. REMOVED REPLACED RIGHT WING NR 3 SLAT JACKSCREW IAW MM 27-84-22.ALSO REPLACED NR 5 SLAT JACKSCREW IAW MM 27-84-23.ALL RIG AND OPS CHECKS GOOD. VERIFIED ALL REMAINING SLAT JACKSCREW RIGS ON RIGHT WING ARE GOOD.

Part: PANEL — CORRODED (RT ELEVATOR) · airframe 41,585 hrs · 19,942 cycles

RT ELEVATOR, L/E PANEL 345DT, OTBD LANDING HAS 1 EA CORRODED FASTNER HOLE, 2EA MISDRILLED HOLES, AND CORROSION ON THE WEB ATTACHMENT STRAP. REMOVED LEVEL 1 CORROSION AT RT ELEVATOR L/E PANEL FASTNER HOLE AND WEB ATTACHMENT STRAP IAW SRM 51-74-10, PAGE 204. FOUND FASTNER HOLE TO BE OUT OF LIMITS IAW SRM 51-40-44, WEB ATTACHMENT STRAP WAS OUT OF LIMITS SRM 55-20-00. REMOVED 1 EA STRAP AND 1 EA PROFILE IAW SRM 51-40-21. FABBED FILLER AND REPAIR ANGLES FOR RT ELEVATOR SPAR IAW EA 6-5520-145657, PT 1. INSTALLED ANGLES AND TOP COATED IAW THE EA 6-5520-145657 PT1 AND SRM 51-75-10, PAGE 206.

Part: SKIN — GOUGED (RT WING) · airframe 41,585 hrs · 19,942 cycles

RT WING FIX L/E IS GOUGED APPROX 6" LONG BETWEEN SLAT TRACK 5 AND 6, FROM CONTACT WITH NR 2 SLAT LOWER SKIN FASTENERS. SMOOTHED AND BLENDED AREA IAW SRM 51-75-10 AT RT WING FIX L/E SLAT TRACK 5 AND 6. NDT FOR CRACK AND LIMITS, NO LIMIT REMAINING THICKNESS. CUTOUT DAMAGE AREA FOR REPAIR IAW SRM 57041-12PB201, FIG 204. FORMED AND FAB NEW SKIN SECTION, FABRICATED 2EA BUTT STRAPS AND 2EA REINFORCING STRAPS,IAW SRM57-41-12 FIG 204, DRILLED AND INSTALLED REPAIR PARTS IAW SRM 57-41-12. REPROTECTED AREA IAW SRM 51-75-10.

Part: SKIN — GOUGED (HORIZONTAL STAB) · airframe 41,585 hrs · 19,942 cycles

RT HORIZONTAL STAB L/E PANEL 341AB, EXTERNAL SKIN SCRATCHED AND GOUGED, ENTIRE LENGTH OF INBD EDGE. BLENDED OUT AREAS (4EA) ON RT HORIZONTAL STAB L/E PANEL 341AB EXTERNAL SKIN IAW SRM 51-73-10; CHECKED LIMITS FOUND AREAS (3EA) WITHIN LIMITS, 1 AREA OUT OF LIMITS IAW SRM 55-10-00, ALODINED AREAS 1, 2, & 3 IAW SRM 51-21-10, CHECKED NDT IAW NTM NO CRACK INDICATION AFTER BLENDED; AREA NR4 CUTOUT DAMAGE AREA, FABRICATE, TREATED, PRIMER AND INSTALLED FILLER AND DOUBLER REPAIR IAW SRM 55-12-12 AND EA 6-5510-145649.

Part: ATTACH FITTING — CORRODED (ZONE 500) · airframe 41,585 hrs · 19,942 cycles

LT WING RIB 5 FWD LUG BORE DIAMETER HAS CORROSION THAT HAS EXCEEDED MAX ALLOWABLE REWORK DIMENSIONS "4.8405 IN". REMOVED LEVEL 1 CORROSION FROM LT WING RIB 5 BY OVERSIZING THE BORE AND SPOT FACING THE AFT LUG FACE, NDT INSPECTED (NIL FINDING) INCLUDED ACID ETCH, FINISHING CUTS WERE PERFORMED AND THE SURFACE PROTECTION WAS RESTORED. NEW OVERSIZED BUSHES WERE MFG AND INSTALLED ALL IAW DWG R572-49121 REV D, WITHOUT DEVIATION. FINAL BORE DIAMETER 4.920" AND LUG THICKNESS 2.235". COMPLIED WITH EO 6-5750-145650 PT 1, WINGS - AD 2008-17-0.

Part: ADAPTER — CRACKED (ZONE 200) · airframe 41,585 hrs · 19,942 cycles

CLEVIS ADAPTER AT FR 46 BETWEEN SEAT TRACKS 2R & 3R IS CRACKED APPROX.2" LONG AT FWD & AFT FLANGE. R & R CLEVIS ADAPTER AT FR 46, BETWEEN TRACKS 2R AND 3R IAW SRM 51-72-10, PG. 1-3.

Part: CHANNEL — BENT (ZONE 300) · airframe 41,585 hrs · 19,942 cycles

INNER FUSELAGE "U" CHANNEL IS BENT STR 33L BETWEEN FR 83 TO FR 84. R & R CHANNEL AT STR 33L BETWEEN FR 83 TO FR 84 IAW SRM 51-40-21. PARAGRAPH 7.

Part: INTERCOSTAL — BENT (FUSELAGE) · airframe 41,585 hrs · 19,942 cycles

INTERCOSTAL AND UPPER ANGLE ARE BENT STR 33R. INNER FUSELAGE BETWEEN FRAME 85 AND FRAME 86. REMOVED AND FAB AND INSTALLED INTERCOSTAL ANGLE ON FR 85 TO 86 RT STRINGER 33R, REF SRM 51-40-21, PG7 REPROTECTED AREA IAW SRM 51-75-10.

Part: FRAME — CORRODED (ZONE 100) · airframe 41,585 hrs · 19,942 cycles

AFT CARGO DOOR AFT EDGE SEAL LANDING STRIP GOUGED AT MULTIPLE PLACES ON FUSELAGE CUTOUT FR 63A R & R 3EA AFT CARGO DOOR AFT EDGE SEAL LANDINGS IAW SRM 51-72-10. UPON FURTHER EVALUATION, FOUND CORROSION AT FR 63A, STR 28R TO 29R, REMOVED CORROSION IAW SRM 51-74-10, AREAS 1 AND 2 FOUND TO BE OUT OF LIMITS IAW DWG A53973557. CUT OUT DAMAGE FROM AREAS 1 AND 2. REMOVED SUPPORT ANGLES, MILLED FRAME, FABRICATED REPAIR ANGLE, FILLER AND 2EA T-SECTIONS IAW SRM 53-17-13, FIG 203. INSTALLED REPAIR ANGLE, FILLER, 2EA T-SECTIONS, AND SUPPORT ANGLES IAW SRM 53-17-13, FIG. 203. REPROTECTED AREAS IAW SRM 51-72-10.

Part: PANEL — CRACKED (HORIZONTAL STAB) · airframe 41,585 hrs · 19,942 cycles

RT HORIZ L/E PANEL 341AB, INTERNAL STIFFENER CRACKED AT AFT END, FROM FASTENER TO EDGE OF PART, .3125" LONG, UPPER AFT CORNER OF PANEL. REMOVED FASTENERS HORZ L/E PANEL 341AB STOP-DRILLED CRACK ON INTERNAL STIFFENER, NDT FOR CRACKS. NO CRACKS WERE FOUND, FABRICATED, DRILLED AND INSTALLED 2 EA DOUBLERS IAW SRM 55-12-19FIG201. REPROTECTED AREA IAW SRM 51-75-10.

Part: SKIN — GOUGED (FUSELAGE) · airframe 41,585 hrs · 19,942 cycles

UPPER AFT AREA OF AFT CARGO DOOR CUTOUT, EXT SURFACE, HAS MULTIPLE SCRATCHES EXTENDING 10" AFT OF CUTOUT (FR63) BETWEEN STRINGERS 27R & 28R. SMOOTHED AND BLENDED 10" SQ IN AFT CARGO DOOR CUTOUT EXT SURFACE FR63, STR 27 & 28 IAW SRM 51-73-10. MAP AREA FOR NDT REMAINING THICKNESS . FOUND WITHIN ALLOWABLE L/E LIMIT .079 MATL LOSS .012 AND .009. R & R 3 EA HILOKS IAW SRM 53-17-12, FIG 103, PG 119-120. REPROTECTED AREA IAW A51-75-10. ORG THICKNESS .236 & .158, FIG 2, PAGE 11, REMAIN THICKNESS .224 & .149.

Part: TRAY — CORRODED (PDU) · airframe 41,585 hrs · 19,942 cycles

AFT CARGO COMPARTMENT LT FWD PDU TRAY FLANGE IS BENT BETWEEN FR55 AND 56 AND NR 2L AND NR 3L TRACK ROLLERS. R & R PDU TRAY IAW SRM 51-40-21, DUE TO CORROSION FOUND OUT OF LIMITS IAW SRM 51-74-10 CORRODED AREA MEASURES 6.00L X 5.00 W X .012. MATERIAL LOSS=.019 REMAINING MATERIAL .020 COMPLIED WITH ELECTRICAL BONDING CHECK-RESISTANCE WITHIN LIMITS IAW AMM 20-28-11-00. PDU OPS CHECK GOOD.

Part: HINGE — CRACKED (ACCESS DOOR) · airframe 41,585 hrs · 19,942 cycles

BOTTOM EXT FUSE EXT ELECTRICAL POWER PLUG ACCESS DOOR INNER DOUBLER CRACKED .2" IN LENGTH. REMOVED ELECTRICAL POWER PLUG ACCESS DOOR, R & R DAMAGED INNER DOUBLER, AND RE-INSTALLED ELECTRICAL POWER PLUG ACCESS DOOR IAW SRM 51-40-21, PARA 5 AND 6.

Part: ACCESS DOOR — CRACKED (APU) · airframe 41,585 hrs · 19,942 cycles

APU RT ACCESS DOOR 316AR AFT MATING FLANGE ON TAILCONE ASSY DEFORMED BELOW LATCH RECEPTACLE, MEASURED 4 IN LENGTH. REMOVED MATING FLANGE IAW SRM 51-40-21. INSTALLED NEW MATING FLANGE IAW SRM 51-40-21 AT AFT APU DOORS AFT MATING FLANGE.

Part: ACCESS PANEL — CRACKED (ZONE 600) · airframe 41,585 hrs · 19,942 cycles

RT WING L/E ACCESS PANEL NR 624EB CUT OUT LANDING IS CRACKED APPROX 1" LONG. R & R CUT OUT LANDING FOR ACCESS PANEL 624EB IAW SRM 51-40-01, PAR 6 & 7 AND SRM 51-40-44 PG1-16, SRM 51-40-21 PARA 6&7. APPLIED ALODINE, PRIMED AND PAINTED IAW SRM 51-75-10.

Part: RETAINER — CRACKED (NR 1 SPOILER) · airframe 41,585 hrs · 19,942 cycles

RT WING NR1 SPOILER T/E RETAINER STRAP IS CRACKED APPROX 1" LONG INBD END. R & R RETAINER STRIP IAW CMM 57-71-11.

Part: ADAPTER — CRACKED (ZONE 200) · airframe 41,585 hrs · 19,942 cycles

CLEVIS ADAPTER AT FR 45 BETWEEN SEAT TRACK 2 & 3 RT IS CRACKED APPROX 1" LONG AT FWD FLANGE. R & R CLEVIS ADAPTER IN MDCC AT FR 45 BETWEEN SEAT TRACKS NR 2 AND NR 3 RT IAW SRM51-40-21. FLOORBOARD LOCATED AND DRILLED IAW SRM 51-40-44. HOLES TREATED AND PROTECTED IAW SRM 51-24-10.

Part: SUPPORT BRACKET — CRACKED (THRUST REVERSER) · airframe 41,585 hrs · 19,942 cycles

NR1 ENGINE THRUST REVERSER TRANSLATING COWL UPPER GUIDE SUPPORT SLIDER BRACKET CRACKED. REMOVED NR 1 ENG O/B TRANSLATING SLEEVE IAW A310-200 AMM 78-32-11-04. REMOVED CRACKED UPPER COWL GUIDE SUPPORT BRACKET IAW SRM 54-40-21 AND SRM 54-04-01 PG.11. FABRICATED NEW BRACKET IAW A310-200 SRM 51-28-10, GMM 7-0-100, SRM 51-25-00. REPROTECTED NEW BRACKET ON ENG O/B T/R TRANSLATING COWL SLEEVE IAW ROHR SRM 54-04-07. REINSTALLED NR 1 O/B T/R SLEEVE REF TO A310-200 AMM 78-32-11-4. RIG AND OPS CHECKGOOD REF TO AMM 78-32-00-5.

Part: INTERCOSTAL — BENT · airframe 41,585 hrs · 19,942 cycles

INNER FUSELAGE INTERCOSTAL IS BENT STR 33L BETWEEN FR85 TO FR84. REMOVED INTERCOSTAL STR 33L BETWEEN FR85 TO FR84 IAW SRM51-40-21, PARA 6, B/S FABRICATED STIFFENER AND WEB IAW DWG A53986749.LOCATED AND DRILLED AND INSTALLED STIFFENER AND WEB ,FR85 TO FR84, STR 33L. REPROTECTED AREA IAW SRM 51-75-10. INSTALLATION SRM 51-40-21, PARA 6 & 7.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 41,585 hrs · 19,942 cycles

RT SIDE STRINGER 9R BETWEEN FR 98 TO 100 HAS 2 PIECES BROKEN OFF. R & R STRINGER 9R FROM FR 95 TO 102 IAW SRM 51-72-10, PARA 5A & 6A. FABRICATED NEW STRINGER IAW DWG 19A53989507. REPROTECTED IAW SRM 51-21-10, 51-23-10, & 51-75-10.

Part: INTERCOSTAL — BENT (ZONE 100) · airframe 41,585 hrs · 19,942 cycles

INTERCOSTAL IS BENT STR 35R INNER FUSELAGE BETWEEN FR86 TO FR87. REMOVED DAMAGED INTERCOSTAL, REPLACED WITH NEW INTERCOSTAL AND STRIP AT STR 35R BETWEEN FR 86 AND FR87 IAW SRM51-75-10 AND SRM51-21-10.

Part: STRUCTURE — GOUGED (NR 7 SPOILER) · airframe 41,585 hrs · 19,942 cycles

RT WING SPOILER NR 7 LOWER T/E IS GOUGED APPROX .500" WIDE. R & R T/E OF RT WING NR 7 SPOILER IAW SRM 51-72-10.

Part: MOUNT BRACKET — CRACKED (PYLON) · airframe 41,585 hrs · 19,942 cycles

AFT UPPER PYLON RIB 21, 3 INCH CRACK AT WING TO PYLON MOUNT BRACKET. R & R TEE PICK-UP ANGLE IAW SRM 51-72-10, PGS 1-3 AND SRM 51-40-21, PGS 31-36.

Part: ACCESS PANEL — CRACKED (LT WING) · airframe 41,585 hrs · 19,942 cycles

LT EXTERNAL PACK AREA INBD LANDING FOR PANEL 143FL HAS .250. CRACK REMOVED LANDING FOR PANEL 143FL, INSTALLED NUTPLATES ON NEW LANDING IAW SRM 51-40-21. INSTALLED NEW LANDING ON LT EXTERNAL PACK AREA FOR PANEL 143FL IAW SRM 51-40-21.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 41,585 hrs · 19,942 cycles

FLOOR TRACK L3 HAS DAMAGED RECEPTICLES LOCATED BETWEEN FLOORBEAM 61 AND 60. REMOVED DAMAGED SECTION FROM BETWEEN FRAMES 58 AND FRAMES 62 AND INSTALLED SPLICE REPAIR IAW SRM 53-10-16, FIG 208 SHEET 1. RESTORED PROTECTIVE COATINGS IAW SRM 51-75-10 AND 51-21-10.

Part: INTERCOSTAL — BENT (FUSELAGE) · airframe 41,585 hrs · 19,942 cycles

INTERCOSTAL IS BENT STR 33R INNER FUSELAGE BETWEEN FR'S 86 AND 87 FABRICATED. REPLACEMENT INTERCOSTAL, LOCATED, DRILLED, INSTALLED AND REPROTECTED IAW SRM 51-40-44, DWG A539-86751 AND 51-42-11, PG 7-22 AND 51-75-10.

Part: FRAME — CORRODED (BULKHEAD) · corrosion level 2 · airframe 41,585 hrs · 19,942 cycles

AFT PRESSURE BULKHEAD LWR FWD SIDE CIRCUMFERENCE STRAP CORRODED 2 INCHES LENGTH X 3 INCHES WIDTH BETWEEN STGR 44L AND 46L. REMOVED AND REAPPLIED SEALANT ON AFT PRESS BULKHEAD FWD SIDE IAW SRM 51-74-10 PB 201, R & R ANGLE ANGLE SUPPORT IAW SRM 51-40-21; FABRICATED ANGLE IAW DWG 5381823 AND SRM 51-21-10 & 51-23-10, APPLIED CPC ON AREA IAW IAW AMM 51-22-00-00.

Part: SEAL — WORN (NACELLE) · airframe 41,585 hrs · 19,942 cycles

PANEL 475CL FWD FINGER SEAL IS WORN APPROX 20 PERCENT ACROSS THE RT SIDE. REMOVED SEAL , FABRICATED NEW SEAL IAW SRM 51-40-44. INSTALLED NEW SEAL IAW SRM 51-40-21.

Part: BRACKET — BENT (ZONE 200) · airframe 41,585 hrs · 19,942 cycles

FR 33, STGR 15L, 2 EA ISOLATOR BRACKET BENT. REMOVED 2 EA BRACKETS IAW SRM 51-40-21. FABBED 2 EA BRACKETS IAW DWG A53771078. ALODINED BRACKETS IAW SRM 51-21-10. PRIMED AND TOPCOATED IAW SRM 51-21-10, PARTMARKED IAW GMM 7-0-1001. INSTALLED 2 EA BRAKETS IAW SRM 51-40-210, PARA 6.

Part: ROLLER TRAY — CORRODED (ZONE 100) · airframe 41,585 hrs · 19,942 cycles

INSIDE AFT CARGO COMPT AT THE BOTTOM SURFACE OF 2R ROLLER TRACK, CORROSION 2.5" X 3" AT 10" FWD OF FR62. AFTER REMOVAL OF BALL MATS FOUND 1EA AREA ON ROLLER TRAY TO BE LEVEL 1, OUT OF LIMITS IAW SRM 53-10-15, FIG 102, BEYOND REPAIR, R & R ROLLER TRAY IAW AT FR 58- FR63 2R IAW SRM 51-72-10.

Part: ADAPTER — CRACKED (ZONE 200) · airframe 41,585 hrs · 19,942 cycles

CLS ADAPTER AT FS 42 BETWEEN SEAT TRACK 2R AND 3R IS CRACKED APPROX 1.5" LONG AT FWD FLANGE. R & R CLS ADAPTER AT FR42 BETWEEN SEAT TRACKS 2 AND 3RT IAW SRM 51-40-21.

Part: STRINGER SPLICE — CORRODED (ZONE 100) · airframe 41,585 hrs · 19,942 cycles

STRINGER 26R SPLICE AT FRAME 54 HAS A 1 SQ IN AREA OF CORROSION, AFT SIDE OF FRAME. REMOVED CORROSION AT SPLICE PLATE AND FOUND LEVEL 1 CORROSION TO BE OUT OF LIMITS IAW SRM 51-73-10. R & R SPLICE IAW SRM 51-72-10.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 41,585 hrs · 19,942 cycles

CLS ADAPTER AT FS 43 BETWEEN SEAT TRACKS 2R & 3R IS CRACKED APPROX 1 INCH LONG AT FWD FLANGE. R & R CLS ADAPTER AT FR 43 BETWEEN SEAT TRACK 2 & 3 IAW SRM 51-40-21.

Part: BRACKET — CRACKED (ZONE 200) · airframe 41,585 hrs · 19,942 cycles

FR26, STR 15 LT ISOLATOR BRACKET BROKEN IAW AMM 25-50-00-06. R & R ISOLATOR BRACKET AT FR 26 STR 15 LT IAW SRM 51-72-10 & 51-40-21, PARA 6.

Part: RIB — CRACKED (LT PYLON) · airframe 41,585 hrs · 19,942 cycles

LT PYLON AT RIB 22 UPPER AFT SIDE HAS A 2 IN LONG CRACK. R & R TEE PICKUP ON LT NR1 PYLON AT RIB 22 IAW SRM 51-72-10.

Part: STRAP — CORRODED (RUDDER) · airframe 41,585 hrs · 19,942 cycles

RUDDER L/E ATTACH LANDING, RT SIDE INTERNAL STRAP CORRODED 2SQ IN, 8" ABOVE NR4 HINGE FITTING. REMOVED NUT PLATE STRAP IAW SRM 51-72-10: FABRICATED PLATE IAW DWG A554-71556, ALODINED NUT PLATE STRAP IAW SRM 51-21-10 PAR.6, PRIMED IAW A310-200 SRM 51-75-10 PG 205, APPLIED TOP COAT IAW SRM 51-72-10 PAR 6. INSTALLED NUT PLATE STRAP IAW SRM 51-72-10, PAR 6.

Part: STRAP — CORRODED (RUDDER) · airframe 41,585 hrs · 19,942 cycles

RUDDER L/E ATTACH LANDING , RT SIDE , INTERNAL STRAP CORRODED, 2SQ IN , 6 INCHES ABOVE NR1 HINGE FITTING. REMOVED NUT PLATE STRAP IAW SRM 51-72-10, PAR 5, FABRICATED NUT PLATE STRAP IAW DWG A554-71556, ALODINED IAW SRM 51-21-10 PG 6. PRIMED IAW SRM 51-75-10, PG 203. APPLIED TOP COAT IAW SRM 51-72-10, PAR 6. INSTALLED NUT PLATE STRAP IAW SRM 51-72-10, PAR 6.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 41,585 hrs · 19,942 cycles

AVIONICS COMPT FLOOR PANEL 121JF HAS 1 EA CORNER BROKEN AND 1 EA CORNER PLIES WORN THRU. FABRICATED REPLACEMENT FLOOR PANEL 121JF IAW DWG SRZ-25-005, REV J.

Part: FLOOR PANEL — CONTAMINATED (ZONE 200) · airframe 41,585 hrs · 19,942 cycles

FLOOR PANEL 147BF IS OIL SOAKED. FABRICATED REPLACEMENT PANEL 147BF IAW DWG SRZ-25-005, REV J.

Part: FLOOR PANEL — CRACKED (ZONE 100) · airframe 41,585 hrs · 19,942 cycles

FLOOR PANEL 252GF HAS 1EA 12" CRACK FABRICATED REPLACEMENT FLOOR PANEL 262GF IAW DWG SR2 25-005, REV J.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 41,585 hrs · 19,942 cycles

FLOOR PANEL 251WH HAS 12 IN CRACK FABRICATED REPLACEMENT PANEL 251WH IAW DWG SRZ-25-005, REV J.

Part: FLOORBOARD — DAMAGED (ZONE 100) · airframe 41,585 hrs · 19,942 cycles

AFT CARGO FLOORBOARD 152EF MISSING EDGE FILLER DEFCT MEASURES 2 SQ INCHES. FABRICATED REPLACEMENT FLOORBOARD 152EF IAW DWG SR2 25-005, REV J.

Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 41,585 hrs · 19,942 cycles

FLOORBOARD 251GF HAS PUNCTURE. FABRICATED REPLACEMENT FLOORBOARD 251GF IAW DWG SRZ-25-005, REV J.

Part: SPAR — CORRODED (ZONE 300) · airframe 41,585 hrs · 19,942 cycles

LEFT HORIZONTAL STAB UPPER REAR SPAR TOP FLANGE BOTTOM SIDE CORRODED AT 4EA NUTPLATE HOLES LOCATED 6 TO 18 INCHES OTBD OF FUSELAGE BETWEEN RIBS 3 AND 5 MEASURED 8 SQ INCHES. REMOVED CORROSION IAW A SRM 51-74-10, FOUND TO BE OUT OF LIMITS IAW SRM 55-10-00 CONFIG 1, FIG 101 SH 2 PG 103. REPAIRED SPAR IAW SRM 55-11-21 FIG 211 PG 265/266 AND FIG 217 PG 299 - 306.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 41,585 hrs · 19,942 cycles

FWD CARGO MAIN DECK FLOORBEAM AT FRAME 34 CRACKED AT STIFFENER, BETWEEN SEAT TRACKS 2 & 3 RT SIDE. CUTOUT DAMAGE AT FLOORBEAM IN FWD CARGO COMPARTMENT SUPPORT FR 34 RT SIDE IAW SRM 53-10-15. NDT IAW NTM 51-10-08 SHOW NO CRACK INDICATION AFTER CUTOUT OF DAMAGE. FABRICATED 1EA SPLICE IAW SRM 53-10-15. LOCATED AND DRILLED OUT NEW PART IAW SRM 51-40-44. ALODINED PART AND AREA REPAIR IAW SRM 51-21-10. PRIMED PART AND AREA REPAIR IAW SRM 51-23-10.

Part: CLEVIS — CRACKED (SEAT TRACK) · airframe 41,585 hrs · 19,942 cycles

MDCC AT FS 54.1 AT SEAT TRACK 3RT CLEVIS ADAPTER MOUNT FITTING CRACK APPROX 2" LONG. R & R CLEVIS IN MDCC AT FR 54.1 ON RT NR 3 TRACK IAW SRM 51-72-10 PARA 5A & 6A. LOCATED, DRILLED & DEBURRED NEW CLEVIS IAW SRM 51-40-44, PG 16.

Part: SKIN — CRACKED (APU DOOR) · airframe 41,585 hrs · 19,942 cycles

APU EXHAUST DOOR 317AL RT LOWER LATCH CUTOUT SKIN HAS A .10 INCH CRACK. ROUTED OUT CRACK, NDT FOUND NO CRACKS, REPROTECTED AREA IAW SRM 52-41-18, PAGE 203 AND SRM 51-75-10. FABRICATED DOUBLER, DRILLED AND INSTALLED IAW SRM 52-41-18, FIG 201, PAGES 207-208.

Part: CLEVIS — BENT (SEAT TRACK) · airframe 41,585 hrs · 19,942 cycles

MDCC AT FS 54.1 BETWEEN SEAT TRACKS 2 & 3 RT CLEVIS ADAPTER FWD FLANGE IS BENT IN 2 EA PLACES. R & R ADAPTER AT FR 54.1 MDCC BETWEEN TRACKS 2 & 3 ON RT SIDE IAW SRM 51-72-10 PARA 5A & 6A . LOCATED, DRILLED & DEBURRED NEW ADAPTER IAW SRM 51-40-44, PG 1-16.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 41,585 hrs · 19,942 cycles

FLOOR PANEL 241 MK HAS 2EA AREAS CRUSHED TOTAL 32 SQ" INCHES, IN ZONE 240. FABBED REPLACEMENT FLOOR PANEL 241 MK USING DWG SRZ 25-005, REV J.

Part: FLOOR PANEL — CRACKED (ZONE 100) · airframe 41,585 hrs · 19,942 cycles

FLOOR PANEL 147 AF HAS A 1" INCH CRACK AND IS OIL SOAKED. FABRICATED REPLACEMENT FLOOR PANEL 147 AF USING DWG SRZ 25-005, REV J.

Part: SUPPORT — CRACKED (ZONE 100) · airframe 41,585 hrs · 19,942 cycles

FWD CARGO COMPARTMENT CENTER CARGO CONTAINER GUIDE AT FR36 BETWEEN 1L AND 1R LOADING TRACK SUPPORT STRUCTURE HAS CRACK THAT MEASURE .5"(L) .03"(W) . R & R CRACKED LOADING SUPPORT TRACK PLATE IAW SRM 51-40-21, PARAGRAPH 5, PG 7. R & R YZ LATCHES IAW CMM 25-51-57-040-001-A01 & CMM25-51-57-440-001-A01.

Part: SUPPORT ANGLE — CHAFED (ZONE 100) · airframe 41,585 hrs · 19,942 cycles

FORWARD CARGO COMPARTMENT LT SIDE BETWEEN NR2 AND NR3 LOADING TRACKS AT FR 25 HAS A SUPPORT ANGLE WITH CHATTER MARKS DAMAGE. R & R FILLER IN FWD CARGO PIT ON LT SIDE, BETWEEN TRACKS 2 & 3 AT FR 25 IAW SRM 51-40-21, PARA 6 & 51-72-10 PARA 5A & 6A. FABRICATED NEW FILLER IAW SAMPLE, REF GMM 7-0-1001 FROM 2024-T3 CLAD .125. REPROTECTED FILLER IAW SRM 51-75-10, PG 204.

Part: SUPPORT — DAMAGED (CARGO BAY) · airframe 41,585 hrs · 19,942 cycles

FORWARD CARGO COMPARTMENT RT SIDE AT FR 21 & FR 22 CARGO DOOR INTERNAL STRUCTURE PANEL SUPPORT HAS 2EA DAMAGE NUTPLATE HOLES. REMOVED AND REPLACED INTERNAL STRUCTURAL PANEL ON UPPER FORWARD CARGO DOOR FRAME CUTOUT AREA BETWEEN FR 21 AND FR 22 IAW SRM 51-72-10 PAGES 1 THRU 3. PERFORMED OPS CHECK ON DOOR IAW AMM 52-31-11-06 AND FOUND IT TO BE SATISFACTORY.

Part: SIDEWALL PANEL — DAMAGED (ZONE 100) · airframe 41,585 hrs · 19,942 cycles

SIDEWALL PANEL 152DW HAS 5 EA FASTENER HOLES DAMAGED AND 25 SQ IN, OF SKIN MISSING. FABRICATED REPLACEMENT PANEL 152 DW IAW AIM 2001, REV D.

Part: FLOOR PANEL — CRACKED · airframe 41,585 hrs · 19,942 cycles

FLOOR PANEL 231QH HAS 1 EA 10 IN CRACK FABRICATED NEW FLOOR PANEL 231QH IAW DWG SRZ 25-5-005, REV J.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 41,585 hrs · 19,942 cycles

FLOOR PANEL 252GF HAS 1 EA, 12 INCH CRACK.

Part: PANEL — DAMAGED (ZONE 100) · airframe 41,585 hrs · 19,942 cycles

CEILING PANEL 152BC HAS 20 SQ IN OD DELAMINATION. FABRICATED REPLACEMENT PANEL 152BL IAW MCG AIM 2001, REV D.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 41,585 hrs · 19,942 cycles

FLOOR PANEL 242LK IS CRACKED IN HALF. FABRICATED NEW PANEL 242LK IAW DWG SRZ 25-5-005, REV J.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 41,585 hrs · 19,942 cycles

FLOOR PANEL 252UH HAS 1 EA, 14 IN. CRACK. FABRICATED NEW PANEL 252UH IAW DWG SRZ 25-5-005, REV J.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 41,585 hrs · 19,942 cycles

FLOOR PANEL 242AJ HAS A CRACK ACROSS PANEL. FABRICATED REPLACEMENT PANEL 242AJ IAW DWG SR2 25-005 REV J.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 41,585 hrs · 19,942 cycles

FLOOR PANEL 242ZJ HAS 7 EA CRUSHED AREAS. FABRICATED REPLACEMENT PANEL 242ZJ IAW DWG SR2 25-005 REV J.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 41,585 hrs · 19,942 cycles

FLOOR PANEL 252BF HAS 1 EA, 10 IN CRACK, FABRICATED NEW PANEL 252BF IAW DWG SRZ 25-5-005, REV J.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 41,585 hrs · 19,942 cycles

FLOOR PANEL 241WH HAS 1 EA, 10 INCH CRACK. FABRICATED REPLACEMENT FLOOR PANEL 241WH, IAW DWG SRZ 25-005, REV J.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 41,585 hrs · 19,942 cycles

FLOOR PANEL 242UJ HAS 3 EA AREAS CRUSHED, 42 SQ INCHES TOTAL. FABRICATED REPLACEMENT PANEL 242 UJ, REFERENCE DWG SRZ 25-005 REV J.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 41,585 hrs · 19,942 cycles

FLOOR PANEL 232XH HAS 3 EA CRUNCHED AREAS, 24 SQ IN TOTAL.

Part: PANEL — DAMAGED (ZONE 100) · airframe 41,585 hrs · 19,942 cycles

SIDEWALL PANEL 151GW HAS 25 SQ IN OF UPPER SKIN MISSING. FABRICATED REPLACEMENT PANEL 151GW IAW MCG AIM 2001 REV D.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 41,585 hrs · 19,942 cycles

FLOOR PANEL 252PH HAS 2 EA. 12 IN. CRACKS FABRICATED NEW FLOOR PANEL 252PH IAW DWG SRZ 25-5-005 REV J.

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 41,585 hrs · 19,942 cycles

OFF ACFT PART--FWD CARGO FLOOR PANEL 131YF HAS 14 SQ IN EDGE DAMAGE AND 6 IN CRACK, FABRICATED NEW PANEL 131YF IAW DWG SRZ 25-5-005 REV J.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 41,585 hrs · 19,942 cycles

OFF ACFT PART--FLOOR PANEL 242EK HAS 6 EA CRUSHED AREAS FABRICATED NEW PANEL 242EK IAW DWG SRZ-25-005, REV J.

Part: PANEL — DAMAGED (ZONE 100) · airframe 41,585 hrs · 19,942 cycles

CEILING PANEL 152AC HAS 20 SQ IN OF SKIN MISSING. FABRICATED REPLACEMENT CEILING PANEL 152AC IAW AIM 2001 REV D

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 41,585 hrs · 19,942 cycles

FLOOR PANEL 242QJ HAS 3 EA, 8 INCH CRACKS. FABRICATED FLOOR PANEL 242QJ IAW DWG SRZ -25 -005, REV J.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 41,585 hrs · 19,942 cycles

FLOOR PANEL 232LT HAS 2 EA. 10 IN CRACKS FABRICATED NEW FLOOR PANEL 232LH IAW DWG SRZ 25-5-005, REV J.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 41,585 hrs · 19,942 cycles

FLOOR PANEL 251RH HAS 1EA, 10 INCH CRACK. FABRICATED REPLACEMENT PANEL 251RH IAW DWG SRZ-25-005, REV J AND IDENTIFIED REPLACEMENT PANEL IAW GMM 7-0-1001.

Part: RESERVOIR — LEAKING (HYD SYSTEM) · airframe 41,493 hrs · 19,879 cycles

BLUE HYD LEAK, AFTER SECURING PUMP LEAK STOPPED. REMOVED AND INSP BLUE HYD SYS MANIFOLD PRESS SW AND REINSTALLED WITH NEW PACKING REF MM 29-12-12-04. AS PRECAUTION. NEEDS LEAK CK. FOUND BLUE SYS RESERVIOR LEAKING, NEEDS RESERVIOR. R & R BLUE HUD SYS RESERVIOR IAW AMM 29-12-46, LEAK AND OPS CHECKED SYS WITH BLUE ELECTRIC PUMPS AND RAN NR 1 ENGINE IAW JRH, OPERATED ALL FLIGHT CONTROLS TO BLEED BLUE SYS. BLUE SYS LEAK AND OPS CHECKED GOOD.

Part: SLAT SYSTEM — MALFUNCTIONED · airframe 41,036 hrs · 19,594 cycles

ON APPROACH SPEED 230KTS, SLAT SYS 1 & 2 FAULT WHEN SLATS EXTENDED. MOMENTARY WENT OUT. UNTIL FLAP 15 SELECTED, THEN CAME BACK ON. PERFORMED GO-AROUND THEN PERFORMED CYCLE. SLATS EXTENDED OK WITHOUT FAULT. FOUND SFCC1 AND SFCC2 WITH THE SAME 4 FAULT BALLS DISPLAYED WHICH INDICATES A SLAT JAM CONDITION. NO 90 DAY HISTORY. BOTH SFCC SHOWED 4 FAULT BALLS FOR SLATS RESET FAULT BALLS AND RESET MTP UPSTAIRS RAN ENGINES AND OPERATED SLAT/FLAPS NUMEROUS TIMES NO FAULTS NOTED ALSO NO HISTORY IN 99 DAYS OPS CHECK GOOD AT THIS TIME REF TSM 27-80-00 AND 27-80-00-03-0. TSI IN WORK CHECKING SYS/COMPONENT LUBS IAW TSM.

Part: RIB — CORRODED (ZONE 600) · corrosion level 2 · airframe 40,597 hrs · 19,307 cycles

FOUND CORROSION DURING A RIB 5 MOD INSP ON RT SIDE MLG SUPPORT RIB AFT PINTLE BEARING FWD LUG BORE AND FACES. THIS CORROSION WAS REMOVED BY OVERSIZING THE BORE AND SPOTFACING THE LUG FACES, NDT INSP (NO FINDINGS), AND INSTALLING OVERSIZE BUSHES IAW REPAIR INSTRUCTIONS AND OPERATOR'S DAMAGE REPORTS. ALL WORK WAS PERFORMED AT CWF UNDER WO 00048771. DOCUMENTED ON NON-ROUTINE NR N00006 AND EA 6-5710-141580, THIS IS A MAJOR REPAIR IAW GMM 6-2-100.

Part: RIB — DENTED (LT ELEVATOR) · airframe 39,347 hrs · 18,487 cycles

LT ELEVATOR INBD UPPER SURFACE T/E RIB NR 1 HAS DENT MEASURES .50 INCH BY .50 IN BY .012 INCH DEEP. DENT REPAIRED AT LT ELEVATOR UPPER SURFACE RIB NR 1 WITH WET OVERLAY REPAIR IAW A310 SRM 55-21-11, FIG 204.

Part: SKIN — DENTED (ZONE 100) · airframe 39,347 hrs · 18,487 cycles

LT EXTERIOR FUSELAGE BETWEEN FRAMES 76 AND 77, STRINGERS 25 LT AND 26LT IS A DENT APPROX 1 INCH WIDE BY 1 INCH LONG BY 0.040 INCH DEEP. CUT OUT DAMAGED AREA AND INSTALLED EXTERNAL PERMANENT SKIN REPAIR BETWEEN FR 76 AND FR 77, STRINGERS 25 LT AND 26 LT IAW SRM 53-10-12, FIG 225, SHEET 1. THIS REPAIR REQUIRES INSPECTION AT INTERVALS AS DEFINED PER SRI 53-10-12-2-005-00.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 39,347 hrs · 18,487 cycles

MAIN DECK CARGO COMPARTMENT NR 3 RT SEAT TRACK HAS 2 ELONGATED SCALLOPS AT FR 54.2 AND 6 INCHES AFT OF FR 54.2. REMOVED DAMAGED SECTION OF TRACK AND INSTALLED NEW SEAT TRACK AT TRACK NR 3 RT BETWEEN FR 54.2 AND FR 58 IAW A310-200 SRM 51-72-10.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 39,347 hrs · 18,487 cycles

MAIN DECK CARGO COMPARTMENT SEAT TRACK NR 3RT BETWEEN FR 16 AND FR 17 HAS 15 SQ INCH OF CORROSION REMOVED LEVEL 1 CORROSION. REMOVED AND REPLACED SEAT TRACK SECTION NR 3RT BETWEEN FR15 AND FR18 IAW A310-200 SRM 51-72-10.

Part: FLOORBEAM — DAMAGED (ZONE 200) · airframe 39,347 hrs · 18,487 cycles

6 HOLES AT AFT END OF TEE FITTING AT FR 15 ARE ELONGATED. REMOVED DAMAGED TEE FITTING AND INSTALLED FLOOR STRUCTURE TEE SPLICING REPAIR AT FR 15 AND SEAT TRACK NR 3RT IAW SRM 53-12-15, FIG 207.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 39,347 hrs · 18,487 cycles

MAIN DECK CARGO COMPARTMENT SEAT TRACK NR 2 LT, 12 INCHES AFT OF FR 17 HAS 10 SQ IN OF CORROSION. REMOVED LEVEL 1 CORROSION. REMOVED DAMAGED SEAT TRACK AND INSTALLED NEW TRACK AT TRACK NR 2 LT BETWEEN FR 14 AND FR 17 IAW A310-200 SRM 51-72-10.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 39,347 hrs · 18,487 cycles

MAIN DECK CARGO COMPARTMENT NR 5RT SEAT TRACK HAS 2 ELONGATED SCALLOPS, AFT OF FR 54.2 CUT OUT DAMAGED SEAT TRACK SECTION AND INSTALLED SEAT TRACK CUTOUT REPAIR AT TRACK NR 5 RT BETWEEN FR 54.2 AND FR 59 IAW SRM 53-10-16, FIG 201.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 39,347 hrs · 18,487 cycles

FWD CARGO COMPARTMENT UPPER END OF UPPER FLOOR SUPPORT BEAM FWD SIDE AT FR 37 BETWEEN SEAT TRACKS 4L AND 5L CRACKED .200 LONG. REMOVED CRACK AND REPAIRED FLOOR SUPPORT BEAM AT FR 37 BETWEEN SEAT TRACKS 4L AND 5L IAW SRM 53-10-15 FIG 203.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 39,347 hrs · 18,487 cycles

MDCC SEAT TRACK 2R FROM FRAME 16 TO FRAME 18 CORRODED APROX 50 INCHES IN LENGTH. AFTER EVALUATION OF TRACK, IS CORRODED (LEVEL I) BEYOND ECONOMICAL REPAIR. REMOVED AND REPLACED SEAT TRACK 2R AT FRAME 16 IAW A310-200 SRM 51-72-10.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 39,347 hrs · 18,487 cycles

FWD CARGO COMPARTMENT UPPER END OF FLOOR SUPPORT BEAM AT FR 37 BETWEEN SEAT TRACKS 2R AND 3R CRACKED .200 LONG. REMOVED CRACK ON FLOOR SUPPORT BEAM AT FR 37 BETWEEN S/T 2R AND 3R IAW SRM 51-73-10 AND SRM 53-10-15. INSTALLED REPAIR CHANNEL IAW SRM 53-10-15 FIG 203. APPLIED PROTECTIVE COATING IAW SRM 51-75-10.

Part: SEAT TRACK — DAMAGED (ZONE 600) · airframe 39,347 hrs · 18,487 cycles

MDCC ZONE 252 SEAT TRACK 5R BETWEEN FR 60 TO 61 HAS A 2 INCH AREA OF BROKEN SCALLOPS. REPAIRED SEAT TRACK IAW A310-200 SRM 53-10-16.

Part: ROD — BENT (L1 DOOR) · airframe 39,165 hrs · 18,360 cycles

CLIMBING PAST FL 280, ECAM CAUTIONED LT CABIN DOOR WAS OPENED. PRESSURIZATION WAS CLIMBING AT NORMAL 500 FPM WITH DIFFERENTIAL AT 8.0 AND CABIN ALTITUDE AT 5000 FT. COMPLIED WITH ECAM AND CHECKED DOOR VISUALLY, IT INDICATED THAT THE DOOR WAS OPENED. RETURNED TO KIND. ON DESCENT PAST 13000 FT, LIGHT WENT OUT & ECAM CLEARED. FOUND UPPER LINKAGE ROD BENT. PERFORMED INSPECTION AFTER ABNORMAL CREW DOOR MOVEMENT, PRECAUTIONARY, PER AMM 05-51-29-0. R&R UPPER LINKAGE ROD IAW MM 52-11-12-4. REPLACED ALL DOOR PANELS. L1 ENTRY DOOR WARNING SYSTEM OP CHECKED NORMAL IAW MM 52-41-00-5.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 38,972 hrs · 18,224 cycles

ON CLIMB-OUT, L INR PUMPS HOWEVER, LFT INR ISOLATION VALVE WAS AMBER, NO FUEL WAS BEING BURNED. GRAVITY FED FUEL MANUALLY TO BALANCE. LANDED W/ 28.8 ON LT AND 24.8 ON RT. LANDED OVER MAX LANDING WT. 200 FPM DESCENT ON LANDING. LANDING WT 276.1 AND MAX LANDING WT LIMIT 267.9. T/S AUTO FUEL FEED SYS PER REVISED/AMM 28-21-00-5, NO DEFECTS, REMOVED AND REPLACED RELAYS 139QA, 136QA, 89QA, 140QA, 131QA, 133QA, CONFIRMED WIRING CONFIG, OPS CHECK NORMAL. R & R RT NR 2 FUEL PUMP PRESS SW TANK ISO VLV TEST/AMM 28-22-00-5. R & R 73QU, 140QA RELAY, 154VD. R & R SDAC AND LEFT INNER ISOL VLV, NO FAULTS. ALL TESTS PASSED, RETURNED A/C TO SERVICE. NO PART CONFIRMED DEFECTIVE.

Part: CONTROL UNIT — MALFUNCTIONED (ZONE 100) · airframe 38,025 hrs · 17,684 cycles

AFTER T/O, NR 5 SPOILER FAULTED W/ RT WING NR 5 SPOILER INDICATING UP. RAN QRH PROCEDURE NO RELIEF. RTB IND. REMOVED AND REPLACED NR 1 AND 2 EFCU'S IAW A310-200 MM 27-61-34-4. OPS CK GOOD PERFORMED GROUND SPOLIER, OPS TEST IAW 27-61-00-5 SUPPLIED FROM AIRBUS WEB SITE. VISUAL INSPECTION OF NR 1 AND 5 RT SPOILERS SHOW NO DEFECTS.

Part: CONTROL UNIT — FAILED (NR 5 SPOILER) · airframe 38,017 hrs · 17,678 cycles

AFTER T/O, NR 5 SPOILER FAULTED W/RT WING NR 5 SPOILER INDICATING UP. RAN QRH PROCEDURE NO RELIEF. REMOVED AND REPLACED NR 1 AND 2 EFCU'S IAW A310-200 MM 27-61-34-4. OPS CK GOOD, PERFORMED GROUND SPOILER OPS TEST IAW 27-61-00-5. SUPPLIED FROM AIRBUS WEB SITE. VISUAL INSPECTION OF NR 1 AND 5 RT SPOILERS SHOW NO DEFECTS.

Part: SKIN — DENTED (CARGO DOOR) · airframe 37,422 hrs · 17,362 cycles

AFT BULK CARGO DOOR HAS TWO DENTS EXTERNAL SKIN, FOUND UPPER DENT TO BE WITHIN LIMIT AND LOWER DENT FOUND TO BE OUT OF LIMIT. FOUND TO BE CRACKED ON LOWER DENT. REPAIRED CRACKED IAW SRM 52-30-00 FIG 207.

Part: PROXIMITY SENSOR — MALFUNCTIONED (MLG) · airframe 35,045 hrs · 16,074 cycles

NR 1 AUTOPILOT, FLIGHT DIRECTOR AND PITCH TRIM INOP. REMOVED AND REPLACED FCC NR 1 IAW A310 MM 22-18-34-4. AFS LAND TEST WILL NOT PASS, FAILS TEST AT DIFFERENT PHASES. AUTO PILOTS ENGAGE INTERMEDIATELY. AUTO THROTTLE WOULD DISENGAGE AT RANDOM. PITCH TRIM AND YAW DAMP ALSO ENGAGE INTERMEDIATELY. AUTOPILOT TRANSFERRED TO WRI 22-10-0479. PITCH TRIM TRANSFERRED TO WRI 22-23-0477. FLT DIRECTOR TRANSFERRED TO WRI 34-62-0475. REMOVED AND REPLACED PROX DETECTION SYSTEM MM 32-31-71-4.