N708AS

Part: FITTING — CORRODED (TE FLAP TORQ TUB) · corrosion level 2 · airframe 52,991 hrs · 29,926 cycles

AFTER REMOVAL OF INBD FOREFLAP INBD TORQUE TUBE, FOUND ATTACH FITTING FOR TORQUE TUBE CORRODED. ACFT GROUNDED. REMOVED AND REPLACED THE FITTING IAW AMM 20-50-11-912-602 PG 6.

Part: FITTING — CORRODED (FLAP TORQ TUBE) · corrosion level 2 · airframe 52,991 hrs · 29,926 cycles

AFTER REMOVAL OF OTBD FOREFLAP OTBD TORQUE TUBE, FOUND ATTACH FITTING FOR TORQUE TUBE CORRODED. ACFT GROUNDED. REMOVED & REPLACED THE FITTING IAW AMM 20-80-11-912-002, PG 6.

Part: FRAME — CRACKED (BS 827) · airframe 52,991 hrs · 29,926 cycles

PAX CABIN FRAME CRACKED BS 827 BETWEEN STRINGERS 8 AND 9R. ACFT GROUNDED. REPAIRED THE FRAME IAW T/C AD20062609-400-53-107 REV 00.

Part: FLOOR SUPPORT — CORRODED (BS 952) · corrosion level 2 · airframe 52,991 hrs · 29,926 cycles

FLOOR SUPPORT RBL 22 CORRODED AT BS 952. ACFT GROUNDED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-60-51-01-1, REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02-0G-0.

Part: FLOORBEAM — CRACKED (BS 538) · airframe 52,991 hrs · 29,926 cycles

CABIN FLOORBEAM CRACKED AT BS 538 LBL 1 - 22. ACFT GROUNDED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-05-0G-0.

Part: FLOOR SUPPORT — CORRODED (BS 947-967) · corrosion level 2 · airframe 52,991 hrs · 29,926 cycles

FLOOR SUPPORT LBL 42 BS 947 TO 967 CORRODED MULTIPLE AREAS. ACFT GROUNDED. REMOVED AND REPLACED DAMAGED FLOOR SUPPORT IAW SRM 51-40-02-0G-0.

Part: FLOOR SUPPORT — CORRODED (BS 947-967) · corrosion level 2 · airframe 52,991 hrs · 29,926 cycles

FLOOR SUPPORT LBL 22 CORRODED AT BS 952. ACFT GROUNDED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02-0G-0W.

Part: SKIN — CHAFED (LT WING) · airframe 52,991 hrs · 29,926 cycles

LT WING I/B EXHAUST GATE O/B UPPER CORNER SKIN IS CHAFED. GROUNDED - YES. REMOVED DAMAGE FROM UPPER SKIN REMAINING MAT. FOUND TO BE .0605, RESTORED FINISH IAW SRM 57-53-01-0G-0. REQUIRES A DETAILED VISUAL INSPECTION OF AREA AT EVERY 3000 FLT CYCLES OR EVERY 12 MOS, WHICHEVER COMES FIRST.

Part: TRANSITION PANEL — CRACKED (BS 727E-727F) · airframe 52,991 hrs · 29,926 cycles

AFT CARGO RIGHT TRANSITION IS CRACKED AT BS 727F. ACFT GROUNDED. REMOVED CRACKED TRANSITION PANEL AND REPLACED WITH NEW IAW SRM 51 40 02 0G 0.

Part: CARGO TRACK — CRACKED (BS 747) · airframe 52,991 hrs · 29,926 cycles

AFT CARGO RT CARGO TRACK IS CRACKED IN RADIUS OF VERTICAL LEG AT BS 747. ACFT GROUNDEDS. REPAIRED THE CARGO TRACK IAW SRM 53-00-53-2R-2 AND EA 400-53EA-18029.

Part: FLOORBEAM — CORRODED (BS 312) · corrosion level 2 · airframe 52,991 hrs · 29,926 cycles

FLOORBEAM BS 312 HAS SPOT OF CORROSION AT LBL 14. ACFT GROUNDED. REPAIRED DMGE TO FLOOR BEAM UPPER CHORD IAW SRM 53-10-51-2R-5.

Part: CARGO TRACK — CRACKED (BS 727C) · airframe 52,991 hrs · 29,926 cycles

AFT CARGO BAY RT CARGO TRACK IS CRACKED IN THE RADIUS OF VERTICAL LEG AT BS 727C. ACFT GROUNDED. REPAIRED THE CARGO TRACK IAW SRM 53-00-53-2R-2.

Part: ARM — OUT OF ADJUST (L1 DOOR) · airframe 52,609 hrs · 29,647 cycles

L1 DOOR WILL NOT CLOSE. THERE WERE NO PRESSURIZATION ISSUES ON PREVIOUS FLIGHT SEGMENT. ACFT GROUNDED. ADJUSTED L1 DOOR GUIDE ARM, IAW AMM 52-11-00-705. ACCOMPLISHED L1 DOOR OPS TEST, IAW AMM 52-11-00-755. OPS CHECKED GOOD. ACFT OK FOR SERVICE.

Part: LATCH — GOUGED (CARGO DOOR HANDL) · airframe 51,992 hrs · 29,207 cycles

AFT CARGO DOOR HANDLE RECESS IS GOUGED FROM MISSING HANDLE BUMPER. ACFT GROUNDED. REMOVED RIVETS FROM HOUSING, REF SRM 51-40-02. ALL HOLES PREVIOUSLY OVERSIZED TO NR 6 RIVETS EXCEPT 1 WHICH IS OVERSIZED TO .238. REMOVED AFT CARGO DOOR HANDLE, REF AMM 52-31-14-004-035, REPLACED ROD END ON ACTUATOR ON INTERIOR SIDE OF HANDLE. REPLACED DOOR HANDLE HOUSING H414.55 IAW SRM 51-40-02 AND REPAIRED FASTENER OVERSIZED HOLES IAW EA 400-52EA-17139. INSTALLED AFT CARGO DOOR HANDLE, SAFETIED AND ADJUSTED, REF AMM 52-31-14-004-054 AND 52-31-00-404-022, PRESSURIZED ACFT NO DEFECTS NOTED.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 51,760 hrs · 29,064 cycles

PROMPTLY AFTER LEVEL OFF AT FL 310 HEARD CABIN ALTITUDE WARNING HORN ACCOMPANIED BY VISUAL CABIN RED ANNUNCIATER LIGHT PERFORMED QRH CHECKLIST PROCEDURES & EXECUTED EMERGENCY DECENT TO 10000'. CABIN STABILIZED IN STANDBY MODE AT 10000 REMAINED OF FLIGHT. ACFT GROUNDED. PERFORMED OPS TEST, PRESSURIZATION CONTROL SYS IAW AMM 21-31-00, OPS CHECKS GOOD, NO FAULTS FOUND. R & R AUTO CABIN PRESSURE CONTROLLER FOR CONVENIENCE, PRECAUTION. PERFORMED OPS TEST, PRESSURIZATION CONTROL SYS AFTER INSTALLING NEW AUTO PRESSURE CONTROLLER, NO FAULTS FOUND, REF AMM 21-31-00. PERFORMED AIRPLANE SINGLE PACK OPERATION, CONFIDENCE CHECK IAW AMM 21-00-05, NO FAULTS FOUND, ALL TESTS PASS.

Part: LAMP — FAILED (EMERGENCY LIGHT) · airframe 50,501 hrs · 28,281 cycles

EMERGENCY LIGHT EXIT LOCATOR SIGNS AT LT FORWARD, LT AFT, AND RT AFT OVERWING EXITS HAVE MULTIPLE LAMPS INOPERATIVE. ACFT GROUNDED. RELAMPED AND TESTED IAW MM 33-51-81-962-011. OPS NORMAL.

Part: FLOOR SUPPORT — BENT (BS 727A-727B) · airframe 50,255 hrs · 28,126 cycles

AFT CARGO COMPARTMENT, LT FLOOR SUPPORT INTERCOSTAL BS 727A-727B IS BENT. ACFT GROUNDED. R & R FLOOR SUPPORT INTERCOSTAL AT BS 727A-727B IAW SRM 51-10-02, PARA NR 8 SRM 51-40-05 , DWG 69-16500 REV:D AND REAPPLIED CIC IAW AMM 51-21-91.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 50,255 hrs · 28,126 cycles

LEFT HORIZONTAL STABILIZER AT STABILIZER 129.5 RIB, STIFFENER CRACKED. ACFT GROUNDED. R & R STIFFENER IAW SRM 51-10-02, PARA 8 AND 51-40-02, AND DWG 65-47508, REV C.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 50,255 hrs · 28,126 cycles

LEFT HORIZONTAL STABILIZER AT STAB STA 129.5 RIB, STIFFENER, PN 65-47508-50 IS CRACKED. ACFT GROUNDED. R & R STIFFENER IAW SRM 51-10-02, PARA 8 AND 51-40-02, AND BAC DWG 65-47508, REV C.

Part: FRAME — DAMAGED (BS 727F) · airframe 50,255 hrs · 28,126 cycles

FUSELAGE FRAME 727F HAS AN ENLONGATED HOLE AT LT LOWER Z-ANGLE ATTACHMENT. ACFT GROUNDED. REPAIRED FRAME IAW EA 400-53EA-15684, REV NEW, STA 727F.

Part: FRAME — DAMAGED (BS 727D) · airframe 50,255 hrs · 28,126 cycles

FUSELAGE FRAME BS 727D HAS AN ENLONGATED HOLE AT LT LOWER Z ANGLE ATTACHMENT. ACFT GROUNDED. REPAIRED IAW EA 400-53EA-15683, REV NEW.

Part: WEB — CORRODED (BS 805-847) · corrosion level 2 · airframe 50,255 hrs · 28,126 cycles

AFT CARGO DOOR SILL WEB IS CORRODED. ACFT GROUNDED. REMOVED CORRODED ORIG .045", REMAIN .040" LOSS OF .005", FOUND OUT OF LIMITS IAW SRM 53-60-16, NEW WEB IAW DWG 65-479.57 AND DWG A530001818L. DRILLED AND INSTALLED 2 EA DOUBLERS IAW DWG A5330001818L.

Part: STRIP — CORRODED (BS 727F) · corrosion level 2 · airframe 50,255 hrs · 28,126 cycles

AFT CARGO COMPARTMENT, RT CAPSTRIP NR 3, FWD OF DOORWAY IS CORRODED. ACFT GROUNDED. REMOVED CORROSION MEASURED THICKNESS OF METAL USING TOOL T82254 CAL DATE 11/25/2015, ORIGINAL THICKNESS .063", REMOVED .024" REMAINING THICKNESS .039" FOUND TO BE OUT OF ALLOWABLE LIMITS, NEW PART ORDER 65-4931.-25, PO 844404.1, LOCATED AND DRILLED HOLES IN NEW PART IAW DWG 65C32630, REV B 65C32631, REV A, CAP STRIP WILL BE REINSTALLED ON CUSTOMER CARD G542070. ALLOWABLE LIMITS IAW SRM 53-60-53.

Part: STRIP — CORRODED (BS 847-948) · corrosion level 2 · airframe 50,255 hrs · 28,126 cycles

AFT CARGO COMPARTMENT, RT CAP STRIP NR 4, AFT OF DOORWAY IS CORRODED. ACFT GROUNDED. REMOVED CORROSION, MEASURED THICKNESS OF METAL, ORIGINAL THICKNESS -.063. REMOVED -.012 REMAINING THICKNESS .051 FOUND TO BE OUT OF LIMITS IAW SRM 53-60-53, MAT ID 2024-T3, PO 837825.1 IAW DWG 65C32630, REV: B, FABRICATED NEW CAP STRIP IAW DWG 65C32630, REV: B, ALODINED AND PRIMED IAW SRM 51-20-01, PAINTED IAW AMM 51-21-73.

Part: FLOOR SUPPORT — CORRODED (BS 727-760) · corrosion level 2 · airframe 50,255 hrs · 28,126 cycles

AFT CARGO BAY LT FLOOR SUPPORT ANGLE IS CORRODED APPROXIMATELY BS 727+4 TO BS 760. ACFT GROUNDED. REMOVED CORROSION AND FOUND BEYOND ALLOWABLE LIMITS IAW SRM 53-60-53-1A-1, ORIGINAL MATERIAL THICKNESS WAS 0.040 IN REMAINING THICKNESS 0.000 IN ACCOMPLISHED SPLICE REPAIR TO LT FLOOR SUPPORT ZEE ANGLE IAW SRM 53-60-53-2R-4 .

Part: SUPPORT — CORRODED (BS 727-727D) · corrosion level 2 · airframe 50,255 hrs · 28,126 cycles

AFT CARGO SIDEWALL CAPSTRIP IS CORRODED RT NR 1. ACFT GROUNDED. REMOVED CORROSION MEASURED THICKNESS OF METAL, ORIGINAL THICKESS .063, REMOVED .013, REMAINING THICKNESS .050 FOUND TO BE PAST 10 PERCENT ALLOWABLE LIMITS IAW SRM 53-60-53. REPLACED IAW SRM 51-10-02, PARA 8. LOCATED AND DRILLED HOLES IAW DWG 65C32630, REV B & 6532631, REV A.

Part: FRAME — CRACKED (BS 520) · airframe 50,255 hrs · 28,126 cycles

CRACK INDICATIONS FOUND BS 520 ABOVE S-21L IN .500" HOLE, MARKED AT 7 & 9 O'CLOCK POSITION IN FWD PIT. ACFT GROUNDED. REPAIRED FRAME IAW EA 400-53EA-15603.

Part: SUPPORT — CORRODED (BS 860) · corrosion level 2 · airframe 50,255 hrs · 28,126 cycles

AFT CARGO SIDEWALL CAPSTRIP SPLICE IS CORRODED. ACFT GROUNDED. REMOVED CORROSION. MEASURED THICKNESS OF METAL, ORIGINAL THICKNESS .063. REMOVED .037, REMAINING THICKNESS .026. FOUND TO BE PAST 10 PERCENT ALLOWABLE LIMITS IAW SRM 53-60-53. REPLACED IAW SRM 51-10-02, PARA 8. LOCATED AND DRILLED HOLES IAW DWG 65C32630, REV B AND 65C32631, REV A.

Part: SUPPORT — CORRODED (BS 727F) · corrosion level 2 · airframe 50,255 hrs · 28,126 cycles

AFT CARGO SIDEWALL CAPSTRIP SPLICE IS CORRODED. ACFT GROUNDED. REMOVED CORROSION MEASURED THICKNESS OF METAL, ORIGINAL THICKNESS 0.63, REMOVED .012, REMAINING THICKNESS .051 FOUND TO BE PAST 10 PERCENT ALLOWABLE LIMITS IAW SRM 53-60-53. REPLACED IAW SRM 51-10-02, PARA 8 LOCATED AND DRILLED HOLES IAW DWG 65C32630, REV B AND DWG 65C32631, REV A.

Part: SUPPORT — CORRODED (BS 727-727D) · corrosion level 2 · airframe 50,255 hrs · 28,126 cycles

AFT CARGO SIDEWALL CAPSTRIP IS CORROSION LT NR 1. ACFT GROUNDED. REMOVED CORROSION MEASURED THICKNESS OF METAL. ORIGINAL THICKNESS .063, REMOVED .022, REMAINING THICKNESS .041 FOUND TO BE PAST 10 PERCENT ALLOWABLE LIMITS IAW SRM 53-60-53. REPLACED IAW SRM 51-10-02, PARA 8. LOCATED AND DRILLED HOLES IAW DWG 65C32630, REV B & 65C32630, REV B 65C32631, REV A.

Part: STRIP — CORRODED (BS 727D-727F) · corrosion level 2 · airframe 50,255 hrs · 28,126 cycles

PARTS RACK, AFT CARGO FLOOR/SIDEWALL CAPSTRIP IS CORRODED. LT NR 2. ACFT GROUNDED. REMOVED CORROSION, MEASURED THICKNESS OF METAL. ORIGINAL THICKNESS .063, REMOVED .020 REMAINING THICKNESS .049 FOUND TO BE OUT OF LIMITS IAW SRM 53-60-53 MATERIAL ID 2024-T3 PO 837825.1 IAW BAC DWG 65C326030, REV B, FABRICATED NEW CAP STRIP IAW DWG 65C32630, REV B, ALODINED & PRIMED IAW SRM 51-20-01 PAINTED IAW AMM 51-21-73, REMOVED DOT B986.

Part: SUPPORT — CORRODED (BS 727D) · corrosion level 2 · airframe 50,255 hrs · 28,126 cycles

AFT CARGO SIDEWALL CAPSTRIP SPLICE IS CORRODED. ACFT GROUNDED. REMOVED CORROSION MEASURED THICKNESS OF METAL, ORIGINAL THICKNESS .063, REMOVED .031, REMAINING THICKNESS .032 FOUND TO BE PAST 10 PERCENT ALLOWABLE LIMITS IAW SRM 53-60-53. REPLACED IAW SRM 53-60-53. REPLACED IAW SRM 51-10-02, PARA 8 LOCATED AND DRILLED HOLES IAW DWG 6532630, REV B AND 6532631 REV A.

Part: SUPPORT — CORRODED (BS 727F-772) · corrosion level 2 · airframe 50,255 hrs · 28,126 cycles

AFT CARGO SIDEWALL CAPSTRIP IS CORRODED. ACFT GROUNDED. REMOVED CORROISON. MEASURED THICKNESS OF METAL, ORIGINAL THICKNESS .063, REMOVED .024. REMAINING THICKNESS .039. FOUND TO BE PAST 10 PERCENT ALLOWABLE LIMITS IAW SRM 53-60-53. REPLACED IAW SRM 51-10-02, PARA 8. LOCATED AND DRILLED HOLES IAW DWG 65C32630, REV B & 65C32631, REV A.

Part: FRAME — CRACKED (BS 500B) · airframe 50,255 hrs · 28,126 cycles

RIGHT BS 500B, .500" WIRE PENETRATION HOLE, ABOVE S-21R HAS CRACK INDICATION DUE TO NOISE. IN FWD PIT, MARKED. ACFT GROUNDED. CLEANED HOLE RT BS 500B, 500" WIRE PREPERATION, HOLE ABOVE S-21R IAW NDT MANUAL PART 6, 51-00-00 PROCEDURE 1, PARA 4, CRACK INDICATION STILL NOTED, ACCOMPLISHED REPAIR TO FRAME AT BS 500B, S20R TO S21R IAW EA 400-53EA-15608, REV NEW.

Part: STRIP — CORRODED (BS 727F-794) · corrosion level 2 · airframe 50,255 hrs · 28,126 cycles

PARTS RACK, AFT CARGO FLOOR/SIDEWALL CAPSTRIP IS CORRODED, RT NR 3. ACFT GROUNDED. REMOVED CORROSION FROM PANEL, ORIGINAL THICKNESS .063. REMAINING THICKNESS .039 FOUND TO BE OUT OF LIMITS WITH MINIMUM THICKNESS REMAINING OF .057 IAW SRM 53-60-53, 10 PERCENT. REMOVED -.024 TOOL, T8225Y, CAL 11-25-15 MATERIAL ID T2024T3, PO 837825.1 IAW DWG 65C32630, REV B, FABRICATED NEW CAP STRIP IAW BAC DWG 65C32650, REV B ALODINED AND PRIMED IAW SRM 51-20-01, PAINTED IAW AMM 51-21-73, REMOVED DOT B9960.

Part: SUPPORT — CORRODED (BS 772-860) · corrosion level 2 · airframe 50,255 hrs · 28,126 cycles

AFT CARGO SIDEWALL CAPSTRIP IS CORRODED LT NR 4. ACFT GROUNDED. REMOVED CORROSION, MEASURED THICKNESS OF METAL, ORIGINAL THICKNESS .063 REMOVED .018. REMAINING THICKNESS .045 FOUND TO BE PAST 10 PERCENT ALLOWABLE LIMITS IAW SRM 53-60-53. REPLACED IAW SRM 51-10-02, PARA 8. LOCATED & DRILLED HOLES IAW DWG 65C32631, REV A.

Part: SUPPORT — CORRODED (BS 859-949) · corrosion level 2 · airframe 50,255 hrs · 28,126 cycles

AFT CARGO SIDEWALL CAPSTRIP IS CORRODED. ACFT GROUNDED. REMOVED CORROISON. MEASURED THICKNESS OF METAL. ORIGINAL THICKNESS .063, REMOVED .031. REMAINING THICKNESS .032, FOUND TO BE PAST 10 PERCENT ALLOWABLE LIMITS IAW SRM 53-60-53. REPLACED IAW SRM 51-10-02, PARA 8. LOCATED AND DRILLED HOLES IAW BODING DWG 65C32630, REV B 65C32631, REV A.

Part: SUPPORT — CORRODED (BS 772) · corrosion level 2 · airframe 50,255 hrs · 28,126 cycles

AFT CARGO SIDEWALL CAPSTRIP SPLICE IS CORRODED. ACFT GROUNDED. REMOVED CORROSION. MEASURED THICKNESS OF METAL. ORIGINAL THICKNESS .063, REMOVED .011. REMAINING THICKNESS .052 FOUND TO BE PAST 10 PERCENT, ALLOWABLE LIMITS IAW SRM 53-60-53. REPLACED IAW SRM 51-10-02, PARA 8. LOCATED AND DRILLED HOLES IAW DWG 65C32630, REV B & DWG 65C32631, REV A.

Part: STOP FITTING — GOUGED (BS 440) · airframe 50,255 hrs · 28,126 cycles

FORWARD CARGO DOOR, FWD DOOR FRAME, UPPER DOOR STOP PIN FITTING GOUGED DEEP. APPROXIMATELY S-20R, MARKED IN RED, DOT ATTACHED. ACFT GROUNDED. R & R CARGO DOOR FWD DOOR FRAME UPPER STOP PIN FITTING IAW SRM 51-10-02, PARA 8 AND 51-40-02, DWG 65-46921, REV K REMOVED & REINSTALLED FWD CARGO DOOR IAW AMM 52-31-00, REMOVED DOT.

Part: DOOR FRAME — GOUGED (BS 799) · airframe 50,255 hrs · 28,126 cycles

AFT CARGO DOOR, FWD DOOR FRAME, 2ND FROM UPPER DOOR STOP PIN FITTING GOUGED. APPROXIMATELY S-21R MARKED IN RED. DOT ATTACHED. ACT GROUNDED. R & R AFT CARGO DOOR FWD FRAME 2ND FROM UPPER STOP FITTING, BEAM B IAW SRM 51-40-02 AND 51-10-02, PARA 8, AND DWG 65-47952, REV C. REMOVED AND REINSTALLED AND ADJUSTED AFT CARGO DOOR, CLEARANCE AND FLUSHNESS CHECK GOOD IAW AMM 52-31-00. REMOVED, REINSTALLED, AND ADJUSTED AFT CARGO DOOR BALANCE MECHANISM IAW AMM 52-31-12. REMOVED DOT B883, GOUGE FOUND BEYOND ALLOWABLE LIMITS IAW SRM 52-30-02-1A-2, REMOVED 0.070 IN, MAX ALLOWABLE IS 0.020 IN).

Part: FRAME — CRACKED (BS 500G) · airframe 50,255 hrs · 28,126 cycles

BS 500G, LT FRAME IN FWD CARGO BAY, A .500 INCH HOLE HAS CRACK INDICATION NOTED IN FRAME AT 10 O'CLOCK POSITION. REF OPS 7318, FIG 11, CIRCLE NOTE 1, STR 20L-STR 21L. ACFT GROUNDED. REPAIR FUSELAGE FRAME AT BS 500G LT SIDE S-20L TO S-21L IAW SRM 53-00-07-2R-B.

Part: FRAME — CRACKED (BS 500B) · airframe 50,255 hrs · 28,126 cycles

BS 500B, LT FRAME IN FWD PIT, .500" HOLE HAS CRACK INDICATION NOTED IN FRAME AT 1 O'CLOCK POSITION, REF OPS 7318, FIG 11, CIRCLE NOTE 1, STR 20L-STR 21L. ACFT GROUNDED. REPAIRED FUSELAGE FRAME AT BS 500B, S-20L TO S-21L IAW SRM 53-00-07-2R-B.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 50,255 hrs · 28,126 cycles

CRACK INDICATION ON LT HORIZONTAL STABILIZER LOWER SKIN, APPROXIMATELY STABILIZER BS 123, APPROXIMATELY 1" IN LENGTH, MARKED IN RED. ACFT GROUNDED. REPAIRED LT HORIZONTAL STABILIZER LOWER SKIN IAW EA 400-55EA-15572, REV NEW AND REO-G19081, REV A.

Part: ATTACH BRACKET — GOUGED (BS 440) · airframe 50,255 hrs · 28,126 cycles

FWD CARGO DOORWAY FWD FRAME INTERNAL ATTACH BRACKET GOUGED, STREAMER ATTACHED, STR 24R. ACFT GROUNDED. R & R FWD CARGO DOORWAY, FW FRAME BACKUP FITTING IAW SRM 51-10-02, PARA 8 AND 51-40-02 AND BAC DWG 65-20722, REV B, REMOVED DOT N258 .

Part: FRAME — CRACKED (BS 500F) · airframe 50,255 hrs · 28,126 cycles

BS 500F STRINGERS 20 - 21L FRAME IN FWD CARGO BAY, A .500 HOLE HAS CRACK INDICATION NOTED IN FRAME AT 5 O'CLOCK POSITION. ACFT GROUNDED. REPAIRED THE FRAME IAW SRM 53-00-07-2R-13.

Part: FRAME — CRACKED (BS 500D) · airframe 50,255 hrs · 28,126 cycles

BS 500D LT FRAME IN FWD PIT, .500" HOLE HAS CRACK INDICATION NOTED IN FRAME AT 1 O'CLOCK POSITION, REF OPS 7318, FIG 11, CIRCLE NOTE 1, STR 20L-STR 21L. ACFT GROUNDED. ACCOMPLISHED REPAIR BS 500D LT FRAME AT .500 HOLE AT STR 20L-STR 21L IAW SRM 53-00-07-2R-13.

Part: FRAME — CRACKED (BS 500F) · airframe 50,255 hrs · 28,126 cycles

BS 500F RT FRAME IN FWD PIT, .500" HOLE HAS CRACK INDICATION NOTED IN FRAME AT 6 O'CLOCK POSITION, REF OPS 7318, FIG 11, CIRCLE NOTE 1, STR 20L-STR 21L. ACFT GROUNDED. REPAIRED FUSELAGE FRAME AT BS 500F, S-20R-S-21R IAW EA 400-53EA-15605, REV: NEW.

Part: HINGE — CRACKED (R1 DOOR) · airframe 50,255 hrs · 28,126 cycles

FORWARD SERVICE DOOR, LOWER HINGE HAS ONE FASTENER HOLE WITH A CRACK INDICATION. UNABLE TO DETERMINE LAYER. INDICATION POSITIONED AT 11 O'CLOCK IN HOLE, MARKED. ACFT GROUNDED. ACCOMPLISHED REPAIR TO FUSELAGE SKIN AND BEAR STRAP COMMON TO FORWARD GALLEY, R1, DOOR LOWER HINGE CUTOUT IAW EA 400-53EA-15655, REV NEW.

Part: FITTING — CRACKED (HORIZONTAL STAB) · airframe 50,255 hrs · 28,126 cycles

CRACK INDICATION ON LT UPPER, OTBD HORIZONTAL STABILIZER THRUST BEAM CORNER FITTING, APPROX 2" IN LENGTH. ACFT GROUNDED. ACCOMPLISHED REPLACEMENT OF LT SIDE HORIZONTAL STABILIZER THRUST BEAM CORNER FITTINGS IAW EA 400-55EA-15573, REV A.

Part: FLOORBEAM — CORRODED (BS 727F) · corrosion level 2 · airframe 50,255 hrs · 28,126 cycles

AFT CARGO FLOOR PANEL SPLICE TEE AT BS 727F+5 IS CORRODED/EXFOLIATED, PARTS RACK. ACFT GROUNDED. REMOVED CORROSION IAW SRM 53-60-53-1A-1, DETAIL IV SECTION B-13. ORIGINAL THICKNESS 0.070, REMOVED 0.015, REMAINING THICKNESS 0.055, FOUND TO BE OUT OF LIMITS IAW SRM 53-60-53-1A-1, TOOL, T8225P, REPLACED SPLICE TEE IAW IAW SRM 51-10-02 PARA AND IAW BAC DWG 65C82630, REV: B, LOCATED AND DRILLED AND INSTALLED NUT PLATES TO NEW SPLICE IAW BAC DWG 65C32630, REV: B REMOVED DOT B632. REMOVED DISCREPENT SPLICE AND INSTALLED NEW SPLICE IAW SRM 51-40-02. .

Part: CARGO TRACK — CORRODED (BS 757-877) · corrosion level 2 · airframe 50,255 hrs · 28,126 cycles

AFT CARGO COMPARTMENT, DOORWAY FLOOR SUPPORT TRACK IS CORRODED/EXFOLIATED. ACFT GROUNDED. REMOVED CORROSION AND FOUND BEYOND ALLOWABLE LIMITS IAW SRM 53-60-53-1A-1. ORIGINAL MATERIAL THICKNESS WAS 0.090", REMOVED 0.052", REMAINING THICKNESS WAS 0.038". ACCOMPLISHED PARTIAL TRACK REPLACEMENT IAW SRM 53-00-53-2R-2 FROM APPROXIMATELY BS 757-STA 877, RBL 13.8.

Part: BEAR STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,255 hrs · 28,126 cycles

AFT CARGO DOOR CUTOUT, AFT SIDE, SKIN BEARSTRAP DOUBLER IS CORRODED. ACFT GROUNDED. REMOVED CORROSION MATERIAL, REMOVED .030" FOUND TO BE OUT LIMITS IAW SRM 53-00-01. REMOVED DOOR THRESHOLD WEB, AFT EDGE COVER STRAP, CORNER EDGE COVER STRAP AND LOWER SILL OTBD CHORD TO FOM REPAIR IAW SRM 51-40-02. REPAIRED IAW SRM 53-00-01-2R-32. REINSTALLED DOOR THRESHOLD WEB AFT EDGE STRAP, CORNER EDGE STRAP AND LOWER SILL OTBD CHORD IAW SRM 51-40-02. THIS IS A CATEGORY B REPAIR REINSPECT IAW SB737-53A1228, INSPECTION THRESHOLD 50,000 FLIGHT CYCLES, REPEAT INSPECTION 8,000 FLIGHT CYCLES, REMOVED DOT B626 .

Part: FLOORBEAM — CORRODED (BS 772) · corrosion level 2 · airframe 50,255 hrs · 28,126 cycles

AFT CARGO COMPARTMENT, FLOOR PANEL SPLICE TEE AT BS 772 IS CORRODED/EXFOLIATED, PARTS RACK. ACFT GROUNDED. REMOVED CORROSION IAW SRM 53-60-53-1A-1, DETAIL V SECTION B-B. ORIGINAL THICKNESS 0.070, REMOVED 0.014, REMAINING THICKNESS 0.056, FOUND TO BE OUT OF LIMITS IAW SRM 53-60-53-1A-1, TOOL T8225P. REPLACED SPLICE TEE IAW IAW SRM 51-10-02, PARA 8 AND IAW DWG 65C32630, REV: B. LOCATED AND DRILLED AND INSTALLED NUT PLATES IAW DWG 65C32630, REV: B. R & R TEE IAW SRM 51-10-02, PARA 8 AND 51-40-02. REMOVED DOT B628. .

Part: CHANNEL — CORRODED (BS 767-794) · corrosion level 2 · airframe 50,255 hrs · 28,126 cycles

AFT CARGO COMPARTMENT, DOOR SURROUND SHIELD IS CORRODED. ACFT GROUNDED. R & R DOOR SURROUND SHIELD IAW SRM 51-40-02 AND DWG 65-47957 CORROSION, REMOVED AND FOUND BEYOND ALLOWABLE LIMITS IAW SRM 53-60-15-1A-1. ORIGINAL THICKNESS WAS .050 IN REMOVED 0.0006 IN, 0.044 IN THICKNESS REMAINING BEYOND ALLOWABLE 10 PERCENT THICKNESS MAX.

Part: CIRCUIT BREAKER — TRIPPED (EMERGENCY LIGHTS) · airframe 49,981 hrs · 27,946 cycles

EMERGENCY LIGHTS STAY ON IN ARMED POSITION. ACFT GROUNDED. FOUND EMERGENCY LIGHTS CIRCUIT BREAKER OUT RESET IAW MM 20-01, OPS CHECKED GOOD IAW MM 33-51-02.

Part: GUIDE ARM — OUT OF ADJUST (R2 DOOR HANDLE) · airframe 48,659 hrs · 27,126 cycles

F/A UNABLE TO CLOSE DOOR. HANDLE SEEMS TO BE JAMMED. ACFT GROUNDED. ADJUSTED GUIDE ARM, R2 DOOR IAW AMM 52-13-31-404-004, DOOR OPS CKS GOOD.

Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 47,331 hrs · 26,321 cycles

DENT FOUND ON RT HORIZONTAL STABILIZER L/E AT HSS 88. ACFT GROUNDED. REPAIRED IAW SRM 55-10-01-2R-2.

Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 47,331 hrs · 26,321 cycles

FOUND A DENT ON THE RT STABILIZER L/E AT APPROXIMATELY L/E HSS 164. ACFT GROUNDED. REPAIRED IAW SRM 53-10-01-2R-2.

Part: SUPPORT ANGLE — CRACKED (HEAT EXCHANGER) · airframe 47,129 hrs · 26,196 cycles

AFTER REMOVAL OF THE LT HEAT EXCHANGER FOUND THE SUPPORT ANGLE FOR THE LT RAM AIR DUCT CRACKED. ACFT GROUNDED. R & R SUPPORT ANGLE IAW SRM 51-40-02-0G-0, LK CK GOOD. ACCOMPLISHED ON NAAS W/O 11446M797- NR8-2-53.

Part: DOUBLER — CORRODED (BS 1112) · corrosion level 2 · airframe 47,129 hrs · 26,196 cycles

APU TORQUE BOX INLET CUTOUT AT APPROX BS 1112 IB FWD DOUBLER IS CORRODED AND CHAFED. ACFT GROUNDED. REMOVED, FABRICATED, INSTALLED FILLER IAW SRM 51-40-02-0G-0 AND SRM 51-40-05-0G-0.

Part: ANGLE — CRACKED (BS 348) · airframe 47,129 hrs · 26,196 cycles

ANGLE AT BS 348, S14L IS BENT WITH ELONGATED, DAMAGED HOLES. ACFT GROUNDED. REMOVED, LUBRICATED NEW AND INSTALLED NEW ANGLE IAW SRM 51-40-02-0G-0 AND SRM 51-40-05-0G-0.

Part: ANGLE — CRACKED (BS 348) · airframe 47,129 hrs · 26,196 cycles

ANGLE ON LOWER SURFACE OF STRINGER 15L CRACKED AT BS 348. ACFT GROUNDED. REMOVED, FABRICATED NEW AND INSTALLED NEW ANGLE IAW SRM 51-40-02-0G-0 AND SRM 51-40-05-0G-0.

Part: SKIN — DELAMINATED (NR 2 SLAT) · airframe 47,129 hrs · 26,196 cycles

LT WING NR 2 SLAT PANEL OTBD UPPER CORNER IS DELAMINATED. ACFT GROUNDED. REPAIRED LT WING NR 2 SLAT PANEL OTBD UPPER CORNER IAW SRM 51-70-10-2R-4, REPAIR 4.

Part: SKIN — DELAMINATED (NR 2 SLAT) · airframe 47,129 hrs · 26,196 cycles

LEFT WING NR 2 SLAT PANEL INBD UPPER CORNER IS DELAMINATED. ACFT GROUNDED. REPAIRED LT WING NR 2 SLAT PANEL INBD UPPER CORNER IAW SRM 51-70-10-2R-4, REPAIR 4.

Part: SCREW — MISSING (L2 DOOR LINER) · airframe 47,054 hrs · 26,160 cycles

F/A REPORTS L2 DOOR DIFFICULT TO OPEN. MADE LOUD POPPING SOUND. FOUND INNER GRAY RUBBER DOOR SEAL LOOSE & SCREWS MISSING. FOUND 2 SHEET METAL SCREWS ON AFT LT GALLEY FLOOR. ACFT GROUNDED. VISUALLY INSPECTED DOOR FOUND 6 MISSING FASTENERS FOR THE DOOR LINER. REPLACED 4 EA AND SECURED. OPS CK DOOR CK OK. REF AMM 52-13-00-705-003. DEF MAINTENANCE MISSING FASTENERS AT AFT UPPER CORNER. LINER SECURED. INSTALLED 2 EA DOOR LINER SEAL STUDS ON UPPER AFT CORNER OF L2 DOOR IAW MM 25-21-25. INT CLEARED, SEAM C.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 44,407 hrs · 24,564 cycles

EMERGENCY LIGHT COVER IS BROKEN IN ROW 17A. ACFT GROUNDED. REINSTALLED COVER- OPS CHECKED GOOD.

Part: ROLLER — LOOSE (R2 WINDOW) · airframe 44,090 hrs · 24,353 cycles

F/O SIDE WINDOW WILL NOT OPEN. REMOVED R2 SLIDING WINDOW AND FOUND LOWER FORWARD ROLLER TO BE LOOSE. RESECURED LOWER FORWARD ROLLER AND REINSTALLED WINDOW REF AMM 56-12-11. WINDOW OPS NORMAL.

Part: WEDGE — DENTED (LT WING TE FLAP) · airframe 43,600 hrs · 24,081 cycles

LT WING INBD MIDFLAP T/E WEDGE IS DENIED ON INBD END LWR SURFACE REPAIRED DENT LT WING INBD MIDFLAP T/E WEDGE INBD END LWR SURFACE IAW SRM 51-70-10, REPAIR 4.

Part: SKIN — CHAFED (BS 1138-1156) · airframe 43,600 hrs · 24,081 cycles

LT HORIZONTAL SKIN BELOW LOWER AFT SLIDER SEAL IS CHAFED AND KNIFE EDGED. ACFT GROUNDED. DAMAGE AREA FOUND TO BE OUT OF LIMITS, REMOVED SKIN AND FABRICATED NEW SKIN, INSTALLED IAW SRM 53 00 01 AD2, SRM 51 40 05, SRM 51 40 02.

Part: FLOOR PANEL — GOUGED (AFT CARGO) · airframe 43,600 hrs · 24,081 cycles

AFT CARGO NR 2 FLOOR PANEL IS GOUGED DEEPER THAN 50 ON UPPER SURFACE. FABRICATED FLOOR PANEL IAW SRM 51-40-05, FIG 2.

Part: SPAR — CHAFED (LT WING TE FLAP) · airframe 43,600 hrs · 24,081 cycles

LT WING INBD MIDFLAP EDGE FWD SPAR ANGLE UNDER THE OTBD ROD ARM IS CHAFED. ACFT GROUNDED. REPAIRED LT INBD MID FLAP T/E WEDGE BEAM IAW ASA EA 400-57EA-09685.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 43,600 hrs · 24,081 cycles

LT WING OTBD FOREFLAP L/E IS CHAFED. REPLACED LT WING OTBD FOREFLAP INBD L/E SECTION IAW SRMS 51-30-01 AND AMM 20-50-11-912-002. FOREFLAP TO MID FLAP GAPS FOUND TO BE ACCEPTABLE AS IS IAW EA 400 27, EA 09690.

Part: SKIN — GOUGED (NR 9 SPOILER) · airframe 43,600 hrs · 24,081 cycles

RT WING NR 9 SPOILER HAS A SMALL GOUGE ON LOWER SURFACE. ACFT GROUNDED. REPAIRED RT WING NR 9 SPOILER LOWER SURFACE GOUGE IAW SRM 51-70-10, REPAIR 4.

Part: SKIN — DENTED (NR 8 SPOILER) · airframe 43,600 hrs · 24,081 cycles

RT WING NR 8 SPOILER HAS SEVERAL DENTS ON LWR SURFACE INBD END. ACFT GROUNDED. REPAIRED RT WING NR 8 SPOILER DENTS ON LWR SURFACE INBD END IAW SRM 51-70-10, REPAIR 4

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 43,600 hrs · 24,081 cycles

LT WING INBD MIDFLAP T/E WEDGE IS DENTED ON LOWER SURFACE AT THE CENTER OF THE WEDGE. ACFT GROUNDED. REPAIRED LT WING INBD MIDFLAP T/E WEDGE ON LOWER SURFACE AT THE CENTER OF WEDGE IAW SRM 51-70-10, REPAIR 4.

Part: WEDGE — DELAMINATED (NR 2 SLAT) · airframe 43,600 hrs · 24,081 cycles

LT WING NR 2 SLAT OTBD T/E WEDGE IS DELAMINATED ON THE LOWER SURFACE. REPAIRED LT WING NR 2 SLAT OTBD T/E EDGE ON LOWER SURFACE IAW SRM 51-70-10, REPAIR 4.

Part: FLOOR PANEL — PUNCTURED (727F-772) · airframe 43,600 hrs · 24,081 cycles

AFT CARGO FLOOR PANEL NR 1535 SKIN HAS AN APPROX 1.4 HOLE PUNCH THROUGH. REMOVED, FABRICATED AND INSTALLED NEW FLOOR PANEL.

Part: ARM — LOOSE (L1 DOOR GUIDE) · airframe 42,972 hrs · 23,703 cycles

L1 DOOR DIFFICULT TO CLOSE. FOUND JAM NOT LOOSE ON GUIDE ARM ADJUSTMENT MECHANISM. ADJUSTED GUIDE ARM REF AMM 52-11-00. DOOR OPERATES NORMALLY. SECURED JAMB NUT.

Part: COVER — OUT OF POSITION (CABIN) · airframe 40,968 hrs · 22,513 cycles

EMERGENCY LIGHT COVER FELL OFF AFT LEFT GALLEY. REPLACED L325 ASSY REF WDM 33 29 01, OPS NORMAL.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 40,196 hrs · 22,089 cycles

FORWARD OF R1 DOOR ANGLE CRACKED ON UPPER SURFACE OF THIRD WEB BELOW THE UPPER DOOR HINGE. REPLACED ANGLE IAW B737 400 SRM 51 40 02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,196 hrs · 22,080 cycles

FRAME 400 IS CRACKED BELOW STR 8L. REPAIRED IAW EA AD20062609 400 53 124 REV A.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,196 hrs · 22,080 cycles

FRAME 400 IS CRACKED BELOW STR 8R. REPAIRED IAW EA AD20062609 400 53 124 REV A.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,196 hrs · 22,080 cycles

THE 827 FRAME IS CRACKED BELOW STR 8L. REPAIRED IAW EA AD20062609 400 53 124 REV A.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,196 hrs · 22,080 cycles

THE 787 FRAME CRACKED BELOW STR 8L. REPAIRED IAW EA AD20062609 400 53 124 REV A.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,196 hrs · 22,080 cycles

THE 907 FRAME IS CRACKED BELOW STR 8C. REPAIRED IAW EA AD20062609 400 53 124 REV A.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,196 hrs · 22,080 cycles

FRAME 440 IS CRACKED BELOW STR 8L. REPAIRED IAW EA AD20062609 400 53 124 REV A.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,196 hrs · 22,080 cycles

FRAME 380 IS CRACKED BELOW STR 8R. REPAIRED IAW EA AD20062609 400 53 124 REV A.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,196 hrs · 22,080 cycles

FRAME 480 CRACKED BELOW STR 8R. REPAIRED IAW EA AD20062609 400 53 124 REV A.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,196 hrs · 22,080 cycles

THE 787 FRAME IS CRACKED BELOW STR 8R. REPAIRED IAW EA AD20062609 400 53 124 REV A.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,196 hrs · 22,080 cycles

FRAME 440 IS CRACKED BELOW STR 8R. REPAIRED IAW EA AD20062609 400 53 124 REV A.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,196 hrs · 22,080 cycles

THE 907 FRAME IS CRACKED BELOW STR 8R. REPAIRED IAW EA AD20062609 400 53 124 REV A.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,196 hrs · 22,080 cycles

FRAME 480 IS CRACKED BELOW STR 8L. REPAIRED IAW AD 20062609 400 53 124 REV A.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,196 hrs · 22,080 cycles

THE 867 FRAME CRACKED BELOW STR 8R. REPAIRED IAW EA AD20062609 400 53 124 REV A.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,196 hrs · 22,080 cycles

727F FRAME IS CRACKED BELOW STR 8R. REPAIRED IAW EA AD20062609 400 53 124 REV A.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,196 hrs · 22,080 cycles

THE 747 FRAME IS CRACKED BELOW STR 8L. REPAIRED IAW EA AD20062609 400 53 124 REV A.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,196 hrs · 22,080 cycles

THE 867 FRAME CRACKED BELOW STR 8L. REPAIRED IAW EA AD20062609 400 53 124 REV A.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,196 hrs · 22,080 cycles

PASSENGER CABIN AFT WET AREA L 2 INNER CHORD (NOP SILL) CORRODED FROM STA 947 TO 986. REMOVED CORROSION MATERIAL LOSS FOUND TO BE OUT OF LIMITS. REPLACED INNER CHORD AND REINSTALLED ATTACHING PARTS IAW B737 400 SRM 53 60 15, 51 40 05 & 51 40 02.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,196 hrs · 22,080 cycles

PASSENGER CABIN AFT WET AREA R 2 INNERCHORD (MOP SILL) CORRODED FROM 947 996. REPLACED CORROSION MATERIAL LOSS FOUND TO BE OUT OF LIMITS. REPLACED INNERCHORD AND REINSTALLED ATTACHING PARTS IAW BA737 400 SRM 53 60 15, 51 40 05 & 51 40 02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,196 hrs · 22,080 cycles

FS 360 FRAME CRACKED BELOW STR 8. REPAIRED IAW ASA EA AD20062609 400 53 124.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 40,196 hrs · 22,080 cycles

FORWARD OF R1 DOOR ANGLE CRACKED ON UPPER SURFACE OF WEB ABOVE UPPER DOOR HINGE. REPLACED ANGLE IAW B737 400 SRM 51 40 02.

Part: SKIN — CHAFED (LE SLAT) · airframe 40,196 hrs · 22,080 cycles

RT WING NR 4 SLAT CHAFE AT LOWER SURFACE AFT END IN NUMBEROUS PLACES. REPAIRED CHAFE DAMAGE IAW B737 400 SRM 51 70 10 REPAIR 4 PAGE 201.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 40,196 hrs · 22,080 cycles

RT WING NR 5 SLAT UPPER COMPSITE SURFACE DELAMINATED AT O/B CORNER. REPAIRED THE DAMAGED AREA OF THE NR 5 SLAT UPPER SURFACE O/B CORNER IAW B737 400 SRM 51 70 10 REPAIR 4.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 40,196 hrs · 22,080 cycles

RT WING NR 4 SLAT UPPER COMPOSITE SURFACE DELAMINATED AT I/B CORNER. REPAIRED DELAMINATION DAMAGE IAW B737 400 SRM 51 70 10 REPAIR 4 PAGE 201.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 40,196 hrs · 22,080 cycles

RT WING NR 6 UPPER COMPSITE SURFACE DELAMINATED AT I/B CORNER. REPAIRED THE DAMAGED AREA OF THE NR 6 SLAT UPPER SURFACE I/B CORNER IAW B737 400 SRM 51-70-10 REPAIR 4.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,196 hrs · 22,080 cycles

STRINGER CLIP CRACKED AT STA 380 BELOW STR 8R. REPLACED THE STRINGER CLIP IAW B737 400 SRM 51 40 02.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,196 hrs · 22,080 cycles

PAX CABIN STRINGER CLIP CRACKED AT STA 663.75 STR 10L. REPLACED THE STRINGER CLIP IAW B737 400 SRM 51 40 02.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 40,196 hrs · 22,080 cycles

FORWARD OF R/1 DOOR ANGLE CRACKED ON UPPER SURFACE OF SECOND WEB BELOW THE UPPER DOOR HINGE. REPLACED ANGLE IAW B737 400 SRM 51 40 02.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 40,196 hrs · 22,080 cycles

RT WING NR 5 SLAT UPPER COMPOSITE SURFACE DELAMINATED AT I/B CORNER. REPAIRED THE DAMAGED AREA OF THE RT WING NR 5 SLAT UPPER SURFACE I/B CORNER IAW B737 400 SRM 51-70-10 REPAIR 4.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 40,196 hrs · 22,080 cycles

FORWARD OF R1 DOOR ANGLE CRACKED ON LOWER SURFACE OF WEB BELOW THE UPPER DOOR HINGE. REPLACED ANGLE IAW B737 400 SRM 51 40 02.

Part: STRUCTURE — CRACKED (LT WING) · airframe 40,196 hrs · 22,080 cycles

LT WING STA WBL 135.5 RIB LOWER CHORD CRACKED BETWEEN WING STR 23. REMOVED CRACKED PORTION OF CHORD. REPAIRED CHORD IAW EA 400 57EA 06417.

Part: ENGINE — BIRD INGESTION (NR 1) · airframe 37,204 hrs · 20,448 cycles

HIGH SPEED RTO (110 KNTS) BIRD INGESTION IN NR 1 ENGINE, NO ENGINE FIRE. NORMAL TAXI TO GATE WITH /C VIBRATION. FLAPS 15 NO BLEEDS 22K MAX POWER TAKEOFF TOW 131.7 NR 1 ENGINE REPLACED ON L/P 6738792. ADDITIONAL DAMAGE AND INSPECTIONS DUE TO BIRD STRIKE DOCUMENTED ON L/PS 6738784 6738785 6738786 6738787 6738788 673889 673890 AND 673891.

Part: SKIN — PUNCTURED (SPOILER) · airframe 36,675 hrs · 20,136 cycles

NR 4 SPOILER UPPER SKIN HAS LARGE PUNCTURE. REPAIRED NR 4 SPOILER UPPER SKIN.

Part: SKIN — DENTED (SPOILER) · airframe 36,675 hrs · 20,136 cycles

NR 3 SPOILER IS DENTED WITH UNPAINTED REPAIR ON SURFACE. REPAIRED NR 3 SPOILER.

Part: SKIN — BULGED (SPOILER) · airframe 36,675 hrs · 20,136 cycles

NR 0 SPOILER HAS BULGE 10" FROM LOWER SURFACE SEAL. REPAIRED NR 0 SPOILER.

Part: SKIN — BULGED (SPOILER) · airframe 36,675 hrs · 20,136 cycles

NR 1 SPOILER HAS A BULGE ON LOWER SURFACE SEAL FASTENER TO LONG. REPAIRED THE DAMAGED AREA OF THE NR 1 SPOILER.

Part: SKIN — DELAMINATED (SPOILER) · airframe 36,675 hrs · 20,136 cycles

NR 8 SPOILER HAS A BULGE ON LOWER SURFACE SEAL FASTENER. REPAIRED DELAMINATION.

Part: ACCESS PANEL — GOUGED (VERTICAL STAB) · airframe 36,675 hrs · 20,136 cycles

VERTICAL STAB ACCESS PANEL 9503 IS GOUGED ON THE EDGES. FABRICATED AND INSTALLED NEW PANEL.

Part: SKIN — DENTED (FUSELAGE) · airframe 33,707 hrs · 18,226 cycles

FUSELAGE HAS NUMEROUS PROTRUDING DENTS AFT AND BELOW RADOME. REPAIRED SKIN DENTS.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 33,450 hrs · 18,080 cycles

NR 7 FLAP TRACK AFT MOUNT SURFACE CORRODED. R&R FLAP TRACK.

Part: STRIP — CORRODED (AFT CARGO BAY) · airframe 33,450 hrs · 18,080 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CAPSTRIP CORRODED FWD OF CARGO DOOR. REMOVED FABRICATED NEW CAPSTRIP AND INSTALLED.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 33,451 hrs · 18,080 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CAPSTRIP CORRODED AFT OF CARGO DOOR. R&R CAPSTRIP PER SRM 51-40-02.

Part: FITTING — GOUGED (CARGO DOOR) · airframe 33,450 hrs · 18,080 cycles

FWD CARGO DOOR FWD LWR PIN FITTING GOUGED. R&R FITTING.

Part: STRIP — CORRODED (CARGO BAY) · airframe 33,450 hrs · 18,080 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CAPSTRIP CORRODED AFT OF CARGO DOOR. REMOVED FABRICATED NEW STRIP AND INSTALLED.

Part: PANEL — DAMAGED (RT WING) · airframe 33,450 hrs · 18,080 cycles

RW IB UPPER NO STEP PANEL AFT FASTENER HOLE IS ELONGATED. R&R RW IB UPPER NO STEP PANEL ANGLE.

Part: STRIP — CORRODED (CARGO BAY) · airframe 33,450 hrs · 18,080 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CAPSTRIP CORRODED FWD OF CARGO DOOR. REMOVED FABRICATED NEW STRIP AND INSTALLED.

Part: SPAR — DELAMINATED (RUDDER) · airframe 33,450 hrs · 18,080 cycles

RUDDER LE SPAR DELAMINATED. REPAIRED RUDDER LE SPAR.

Part: HINGE FITTING — CRACKED (L1 DOOR) · airframe 33,450 hrs · 18,080 cycles

L1 DOOR UPPER HINGE CUTOUT FASTENER HOLE HAS CRACK INDICATION IN THE FITTING AT BS 304 WL 259. R&R L1 DOOR UPPER HINGE FITTING AT BS 304 WL 259.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 33,450 hrs · 18,080 cycles

INTERCOSTAL CRACKED. R&R INTERCOSTAL.

Part: CARGO TRACK — CORRODED (BS 747-867) · corrosion level 2 · airframe 26,739 hrs · 14,329 cycles

AFT CARGO PIT FLOOR SUPPORT TIE DOWN TRACK CORRODED. REPLACED AFT CARGO FLOOR SUPPORT TIE DOWN TRACK IAW SRM 53-00-53 FIG 201.

Part: SILL — CORRODED (BS 960-986) · corrosion level 2 · airframe 26,739 hrs · 14,329 cycles

L2 DOOR ENTRANCE CORROSION FOUND AT LWR SILL CHORD. REPLACED CHORD IAW SRM 51-40-02 AND 51-40-05.

Part: SILL — CORRODED (BS 860-1006) · corrosion level 2 · airframe 26,739 hrs · 14,329 cycles

AFT GALLEY SERVICE DOOR SILL HAS AREA OF CORROSION. REPLACED AFT GALLEY SERVICE DOOR SILL IAW SRM 51-40-02.

Part: FLOOR SUPPORT — NICKED (BS 777-807) · airframe 26,739 hrs · 14,329 cycles

AFT CARGO COMPARTMENT FLOOR SUPPORT NICKED IN 3 EACH PLACES. FLOOR SUPPORT REPAIRED IAW SRM 53-00-53 FIG 201.

Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 26,739 hrs · 14,329 cycles

RIGHT HORIZONTAL STAB L/E SKIN DENTED O/B OF EMPENAGE. REPAIRED DENT PER SRM 55-10-01 FIG 101.

Part: CARGO TRACK — CORRODED (BS 945) · corrosion level 2 · airframe 26,739 hrs · 14,329 cycles

AFT CARGO PIT RIGHT T/E TIE DOWN TRACK CORROSION FOUND AROUND NUT PLATE HOLES. REPLACED TIE DOWN TRACK IAW SRM 53-00-53 FIG 201.

Part: SILL — CORRODED (BS 960-986) · corrosion level 2 · airframe 26,739 hrs · 14,329 cycles

AFT SERVICE DOOR LWR SILL CHORD HAS AREA OF CORROSION. REPLACED SILL PER SRM 51-40-02 AND 51-40-05.

Part: CARGO TRACK — CORRODED (BS 747-867) · corrosion level 2 · airframe 26,739 hrs · 14,329 cycles

AFT CARGO COMPARTMENT FLOOR SUPPORT TIE DOWN CORRODED. REPLACED CORRODED TIE DOWN IAW SRM 51-40-02 AND 51-40-05.

Part: SKIN — DENTED (NR 5 SPOILER) · airframe 26,739 hrs · 14,329 cycles

TWO EACH DENTS ON NR 5 SPOILER LWR SURFACE. NR 5 SPOILER LWR SURFACE DENTS REPAIRED IAW SRM 51-70-10 REPAIR 2 PARAGRAPH 4.

Part: STRINGER CLIP — CRACKED (BS 706 S12R) · airframe 26,739 hrs · 14,329 cycles

TIE CLIP CRACKED. REPLACED TIE CLIP IAW SRM 51-40-05 AND 51-40-02.

Part: FLOOR SUPPORT — CRACKED (BS 777-807) · airframe 26,739 hrs · 14,329 cycles

AFT CARGO COMPARTMENT FLOOR SUPPORT NICKED IN 3 EACH PLACES. AFT CARGO COMPARTMENT FLOORBEAM REPAIRED IAW SRM 53-00-53 FIG 201.

Part: SKIN — DENTED (NR 5 SPOILER) · airframe 26,739 hrs · 14,329 cycles

TWO EACH DENTS ON NR 5 SPOILER LWR SURFACE. NR 5 SPOILER LWR SURFACE REPAIRED IAW SRM 51-70-10 REPAIR 2 PARAGRAPH 4.

Part: SILL — CORRODED (BS 860-1006) · corrosion level 2 · airframe 26,739 hrs · 14,329 cycles

AFT GALLEY SERVICE DOOR SILL (R2) HAS AREAS OF CORROSION. AFT GALLEY SERVICE DOOR SILL (R2) REPLACED IAW SRM 51-40-02.

Part: STRINGER CLIP — CRACKED (BS 706) · airframe 26,739 hrs · 14,329 cycles

FOUND TIE CLIP CRACKED. REPLACED TIE CLIP PER SRM 51 40 02 AND 51 40 05.

Part: SILL — CORRODED (BS 960-986) · corrosion level 2 · airframe 26,739 hrs · 14,329 cycles

L2 DOOR ENTRANCE CORROSION FOUND ATY LWR SILL CHORD. L2 DOOR ENTRANCE SILL CHORD REPLACED WITH NEW PART IAW SRM 51 40 02 AND 51 40 05.

Part: SKIN — DENTED (FS 998-999)

OKC - FUSELAGE SKIN IS DENTED AT BS 999 BETWEEN STRINGER 13R-14R. A=1.8 INCH, Y=0.067 INCH, A/Y = 26.9. LOWER EDGE OF DENT PERIPHERY IS 1.2 INCH FROM SKIN LAP JOINT UPPER FASTENER ROW. CUTOUT DAMAGED AREA OF SKIN. FABRICATED AND INSTALLED A STRUCTURAL FILLER, EXTERNAL DOUBLER AND EXTERNAL TRIPLER IAW ASA EA 5330-02010. (M)

Part: SKIN — GOUGED (RT AILERON)

OKC - RIGHT AILERON TRAILING EDGE LOWER SURFACE GOUGED EDGE ADJACENT TO THE THIRD TAB HINGE FROM THE INBOARD EDGE. REMOVED DAMGAED AREA OF PLIES, PREPARED AND APPLIED REPAIR PLIES IAW B737-400 SRM 57-60-01 FIGURE 201 AND 51-70-05 PARAGRAPH 3. WEIGHT AND BALANCE ACCOMPLISHED ON MIG-5 4911163. (M)

Part: SKIN — GOUGED (AFT CARGO DOOR) · airframe 19,725 hrs · 10,596 cycles

OKC - AFT CARGO DOOR HAS A DENT WITH A GOUGE. REMOVED DAMAGE IN SIX LOCATIONS, HFEC FOR CRACKS, NONE FOUND, INSURANCE CUT ALL CUTOUTS, FABRICATED AND INSTALLED REPAIR FILLERS.

Part: SKIN — PUNCTURED (LT IB FORE FLAP) · airframe 19,725 hrs · 10,596 cycles

OKC - FOUND HOLE IN THE LOWER SURFACE OF THE LT IB FORE FLAP, 3 INCH FROM THE T/E, 17 INCHES FROM THE IB EDGE. REMOVED DAMAGED AREAS, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER.

Part: SKIN — DAMAGED (NR 4 SPOILER) · airframe 19,725 hrs · 10,596 cycles

OKC - FOUND HOLE IN THE NR 4 SPOILER 12 INCHES FORWARD OF THE T/E, 19 INCHES OB OF IB EDGE ON THE LOWER SURFACE. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER.

Part: FRAME — CRACKED (FUSELAGE)

SEA - DURING L4 WINDOW REPLACEMENT, FOUND FRAME AT FUSELAGE STATION 219.5, LEFT BUTTOCK LINE 16 CRACKED. REPAIRED FRAME PER EA. (M)

Part: WIRE — DISCONNECTED (ROWS 13-15)

PDX - DURING MAINTENANCE CHECK,THE EMERGENCY EXIT TRACK LIGHTS AT ROWS 13-15 WERE FOUND INOPERATIVE. RE-CONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (X)