N799AS

Part: STRAP — CRACKED (BS 312-344) · airframe 53,874 hrs · 30,556 cycles

FLOORBEAM STABILIZING STRAP AT RBL 31.6 CRACKED IN ELECTRONIC EQUIPMENT BAY. ACFT GROUNDED. R & R FLOORBEAM STABILIZING STRAP IAW SRM 51-40-02-0G-0, SHEET 3.

Part: STRAP — CRACKED (BS 328 FLOORBEAM) · airframe 53,874 hrs · 30,556 cycles

FLOORBEAM STABILIZING STRAP AT RBL 50.5 CRACKED IN ELECTRONIC EQUIPMENT BAY. ACFT GROUNDED. REPAIRED CRACKED FLOORBEAM STABILIZING STRAP IAW SRM 53-10-51-2R-4.

Part: STRAP — CRACKED (BS 312-344) · airframe 53,874 hrs · 30,556 cycles

FLOORBEAM STABILIZING STRAP AT LBL 11 CRACKED IN ELECTRONIC EQUIPMENT BAY. ACFT GROUNDED. R & R FLOORBEAM STABILIZING STRAP IAW SRM 51-40-02-0G-0.

Part: SNUBBER — FAILED (L2 DOOR) · airframe 51,578 hrs · 29,083 cycles

CSA REPORTED L-2 DOOR HARD TO CLOSE. ACFT GROUNDED. OPENED DOOR, FOUND TO DOOR TO BIND WHEN APPROXIMATELY 45 DEG TO FUSELAGE. WHILE CLOSING L-2 DOOR FOUND SNUBBER ATTACH POINT ON FUSELAGE SIDE MOVING. REMOVED AND INSTALLED A NEW AFT ENTRY DOOR (L-2) SNUBBER REF AMM 52-13-71-004-020 AND AMM 53-13-71-404-022. OPS CK GOOD, NO BINDING NOTED.

Part: SKIN — CRACKED (L2 DOOR) · airframe 50,620 hrs · 28,531 cycles

L2 DOOR SKIN IS CRACKED AT FWD LOWER CORNER. ACFT GROUNDED. REPAIRED L2 DOOR SKIN AT FWD LOWER CORNER IAW SRM 53-00-01-2R-32, DETAIL IV, CATEGORY B REPAIR FOR THRESHOLD, INTERVAL AND INSPECTION METHODS, SRM 53-00-01-2R-32, FIG 201.

Part: INTERCOSTAL — CORRODED (BS 847-867) · corrosion level 2 · airframe 50,620 hrs · 28,531 cycles

FOUND INTERCOSTAL BS 847-867 STRINGERS 25-26R TO HAVE LARGE AREAS OF CORROSION. ACFT GROUNDED. REMOVED DAMAGE FOUND TO BE OUT OF LIMITS FABRICATED NEW INTERCOSTAL IAW SRM 51-40-05-0G-0.

Part: FITTING — CORRODED (STRINGER 22L) · corrosion level 2 · airframe 50,620 hrs · 28,531 cycles

BS 1016, S22L END FITTING IS EXFOLIATED. ACFT GROUNDED. R & R STRINGER END FITTING IAW AMM 20-50-11-912-002 AND SRM 51-40-02-0.

Part: CARGO TRACK — CORRODED (BS 771) · corrosion level 2 · airframe 50,620 hrs · 28,531 cycles

CARGO TRACK RBL 13.8 IS CORRODED AT BS 771. ACFT GROUNDED. REPAIRED IAW SRM 53-00-53-2R-2.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,620 hrs · 28,531 cycles

APU INLET CUTOUT AFT STIFFENER CORRODED. ACFT GROUNDED. R & R STIFFENER IAW SRM 51-40-02-0G-0.

Part: FLOOR SUPPORT — CORRODED (BS 771) · corrosion level 2 · airframe 50,620 hrs · 28,531 cycles

AFT CARGO BAY FLOOR SUPPORT RBL 3, BS 771 HAS CORROSION AT JOGGLE LOCATION. ACFT GROUNDED. REPAIRED IAW EA 400, 53EA 13287.

Part: STRINGER — CORRODED (BS 1125) · corrosion level 2 · airframe 50,620 hrs · 28,531 cycles

APU COMPARTMENT LOWER STRINGER, AFT OF APU INLET CORRODED ON I/B END. ACFT GROUNDED. REMOVED AND REPLACED LOWER STRINGER IAW SRM 51-40-02-0G.

Part: STRINGER — CRACKED (APU BAY) · airframe 50,620 hrs · 28,531 cycles

APU BAY STRINGER AT LOWER END OF THE APU INLET FOURTH FASTENER HOLE AFT HAS A SMALL CRACK ON THE INNER SURFACE. ACFT GROUNDED. R & R STRINGER IAW SRM 01-40-02-0G-0.

Part: FLOOR SUPPORT — CORRODED (BS 771) · corrosion level 2 · airframe 50,620 hrs · 28,531 cycles

AFT CARGO BAY FLOOR SUPPORT LBL 8.1, BS 771 HAS CORRODED AT JOGGLE LOCATION. ACFT GROUNDED, REPAIRED THE FLOOR SUPPORT IAW EA 400, 53EA 13290.

Part: FLOOR SUPPORT — CORRODED (BS 771) · corrosion level 2 · airframe 50,620 hrs · 28,531 cycles

AFT CARGO FLOOR SUPPORT LBL 3, BS 771 HAS CORROSION AT JOGGLE LOCATION. ACFT GROUNDED. REPAIRED THE FLOOR SUPPORT IAW EA 400, 53 EA 13278.

Part: ANGLE — CRACKED (R1 DOOR WAY) · airframe 50,620 hrs · 28,531 cycles

LEFT ANGLE FWD OF R1 DOOR BETWEEN 10R-11R IS CRACKED. ACFT GROUNDED. REMOVED LEFT ANGLE IAW SRM 51-40-02-0G-0.

Part: FLOOR SUPPORT — CORRODED (BS 771) · corrosion level 2 · airframe 50,620 hrs · 28,531 cycles

AFT CARGO BAY FLOOR SUPPORT, RBL 8.1, BS 771 CORRODED AT JOGGLE LOCATION. ACFT GROUNDED. REPAIRED THE FLOOR SUPPORT IAW EA 400-53EA 13289.

Part: STIFFENER — CORRODED (APU INLET) · corrosion level 2 · airframe 50,620 hrs · 28,531 cycles

APU INLET CUTOUT FWD STIFFENER CORRODED ON INNER SURFACE. ACFT GROUNDED. R & R APU INLET CUTOUT FWD STIFFENER IAW SRM 51-40-02-0G-0.

Part: FLOORBEAM — CORRODED (BS 947) · corrosion level 2 · airframe 50,620 hrs · 28,531 cycles

FLOORBEAM BS 947 CORRODED ON TOP CAP AT LBL 4. ACFT GROUNDED. REMOVED DAMAGE AND FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 51-10-02-0G-0 AND 53-00-51-2R-3 REPAIR 3.

Part: ATTACH ANGLE — CRACKED (BS 348) · airframe 50,620 hrs · 28,531 cycles

INTERCOSTAL ATTACH ANGLE IS CRACKED AT STA 348.2, STR 15L. ACFT GROUNDED. R & R INTERCOSTAL ATTACH ANGLE CLIP AT STA 348.2, STR 15L IAW SRM 51-40-02-0G-0.

Part: CARGO TRACK — CORRODED (BS 727F) · corrosion level 2 · airframe 50,620 hrs · 28,531 cycles

AFT CARGO TRACK AT LBL 17.2, BS 727F IS CORRODED AT LUG. ACFT GROUNDED. R & R AFT CARGO TRACK BS 727F -815 IAW SRM 53-00-53-2R-2.

Part: FLOORBEAM — CORRODED (BS 986) · corrosion level 2 · airframe 50,620 hrs · 28,531 cycles

FLOORBEAM BS 986 HAS MULTIPLE AREAS OF CORROSION ALONG UPPER TEE CAP. ACFT GROUNDED. CORROSION REMOVAL FOUND TO BE OUT OF LIMITS, REPAIRED FLOORBEAM UPPER CAP IAW EA 40053EA13376.

Part: CHANNEL — CORRODED (BS 988) · corrosion level 2 · airframe 50,620 hrs · 28,531 cycles

AFT WASTE WATER DRAIN MAST SUPPORT CHANNEL IS CORRODED BS 988. ACFT GROUNDED. R & R AFT DRAIN MAST SUPPORT CHANNEL IAW EA 400 53EA 13300.

Part: STRUCTURE — CHAFED (TE FLAP) · airframe 50,620 hrs · 28,531 cycles

AFT OF FIXED FAIRING BETWEEN INBD AND OTBD FLAP CHAFED IN THE INBD. ACFT GROUNDED. BLENDED AREA FOUND TO BE OUT OF LIMITS ACCOMPLISHED REPAIR IAW EA 57EA 13370 TO NR 3 IF O/T FAIRING.

Part: CARGO TRACK — CORRODED (BS 944) · corrosion level 2 · airframe 50,620 hrs · 28,531 cycles

CARGO TRACK AT LBL 17.2, BS 944 HAS SEVERAL AREAS OF CORROSION. ACFT GROUNDED. REPAIRED THE CARGO TRACK IAW SRM 53-00-53-2R-2.

Part: ANGLE — CORRODED (BS 290-360) · corrosion level 2 · airframe 50,620 hrs · 28,531 cycles

L1 LOWER SILL INNER ANGLE IS CORRODED. ACFT GROUNDED. R & R MOPSILL IAW SRM 51-40-05-0G- 0, W 2.0", O .090", R .045, L 6.0", D .045".

Part: SUPPORT ANGLE — CORRODED (BS 312-344) · corrosion level 2 · airframe 50,620 hrs · 28,531 cycles

L1 LOWER DOOR SILL INNER THRESHOLD SUPPORT ANGLE IS CORRODED. ACFT GROUNDED. R & R SUPPORT ANGLE IAW SRM 51-40-02-0G-0.

Part: SUPPORT ANGLE — CORRODED (BS 294-328) · corrosion level 2 · airframe 50,620 hrs · 28,531 cycles

R1 LOWER SILL INBD THRESHOLD SUPPORT ANGLE IS CORRODED. ACFT GROUNDED. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. INSTALLED NEW ANGLE IAW SRM 51-40-04-0G-0, W 1.0, O .090, R .078, L 1.0, D .012.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 50,620 hrs · 28,531 cycles

MID FLAP ON LT WING INBD PHNOLIC STRIP TORN, METAL SKIN CHAFED. ACFT GROUNDED. REPLACED 3 RUBSTRIPS AND REPAIRED MIDFLAP LT WING OTBD FLAP SLIP IAW SRM 51-70-10-2R-4 TYPE EA 57-50-01185, REV C.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 50,620 hrs · 28,531 cycles

RIGHT INBD MIDFLAP CHAFED ON INBD UPPER EDGE. ACFT GROUNDED. DAMAGE FOUND TO BE OUT OF LIMITS, R & R RT INBD MID FLAP UPPER AFT SKIN PANEL IAW SRM 51-40-02-0G-0.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 49,124 hrs · 27,659 cycles

F/A REPORTS LENS FELL OUT OF FWD EXIT SIGN. ACFT GROUNDED. REPLACED/REINSTALLED NEW EXIT SIGN, FWD POSITION.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 48,654 hrs · 27,353 cycles

AFT LT WINDOW EXIT SIGN MISSING COVER. ACFT GROUNDED. INSTALLED NEW EXIT COVER AT LT AFT EMERGENCY EXIT. CHECKS SECURE, OK FOR SERVICE.

Part: EXHAUST GATE — WORN (RT WING) · airframe 48,359 hrs · 27,184 cycles

RT WING INBD EXHAUST GATE WORN. ACFT GROUNDED. REMOVED DAMAGE AND FOUND OUT OF LIMITS IAW SRM 57-53-01-1A-A. R & R RT WING INBD EXHAUST GATE PANEL ASSY IAW AMM 27-51-05.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 47,164 hrs · 26,455 cycles

LEFT WING OTBD FORE FLAP L/E IS CHAFED AT INBD END REMOVED, FABRICATED AND INSTALLED NEW L/E SKIN SECTION IAW SRM 57-53-01, 51-40-05 AND 51-40-02.

Part: STRUCTURE — CORRODED (BS 695-663) · airframe 47,164 hrs · 26,455 cycles

LEFT WHEEL WELL MANIFOLD ASSY LOWER CHORD HAS BARE METAL AND SURFACE CORROSION. ACFT GROUNDED. REMOVED CORROSIONS CHECK OUT OF LIMITS IAW SRM 53-60-71. REMOVED, FABRICATED FWD AND LWR CENTER, LOCATED AND DRILLED, TREATED PRIMED TOP COATED AND INSTALLED NEW FWD AND CENTER LWR CHORD IAW SRM 51-40-02.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 47,164 hrs · 26,455 cycles

RT WHEEL WELL MANIFOLD ASSY LOWER CHORD SPLICE PLATE AT 400 POSITION CORRODED. REMOVED CORROSION, CHECKED OUT OF LIMITS IAW SRM 53-60-71, R & R SPLICE ANGLE IAW SRM 51-40-02.

Part: WEB — DAMAGED (LT MLG WW) · airframe 47,164 hrs · 26,455 cycles

LT MLG WHEEL WELL MAINFOLD WEB HAS DAMAGED HOLES. ACFT GROUNDED. REMOVED OLD WEB SECTION. FABRICATED AND INSTALLED NEW WEB SECTION IAW EA 400-53EA-10334.

Part: STRUCTURE — GOUGED (RT MLG WW) · airframe 47,163 hrs · 26,455 cycles

RT MLG WW FORWARD LOWER STRUCTURE HAS A DEEP GOUGE. ACFT GROUNDED. REMOVED GOUGE, CHECK OUT OF LIMITS IAW SRM 53-60-71. R & R FORWARD LOWER STRUCTURE IAW SRM 51-40-02.

Part: STRUCTURE — DAMAGED (BS 663.75-727) · airframe 47,164 hrs · 26,455 cycles

LT WHEEL WELL MANIFOLD UPPER CHORD HAS ELONGATED HOLE AT 500 POSITION. REMOVED OLD CHORD LOCATED AND DRILLED AND INSTALLED NEW CHORD IAW SRM 51 40 02.

Part: STRUCTURE — CORRODED (RT MLG WW) · airframe 47,164 hrs · 26,455 cycles

RT WHEEL WELL MANIFOLD ASSY UPPER CHORD HAS SURFACE CORROSIONS AND BARE METAL. REMOVED RT WHEEL WELL UPPER CHORD, FABRICATED NEW CHORD IAW SRM 51-40-05. TREATED, PRIMED AND TOPCOATED IAW SRM 20-41-02 AND INSTALLED IAW SRM 51-40-02.

Part: STRUCTURE — CORRODED (RT MLG WW) · airframe 47,164 hrs · 26,455 cycles

RT WHEEL WELL MANIFOLD ASSY LOWER CHORD HAS BARE METAL AND SURFACE CORRODED SEVERAL AREAS. ACFT GROUNDED. REMOVED CORROSION ON CENTER LWR CHORD FOUND WITHIN LIMITS IAW SRM 53-60-71. REMOVED CORROSION ON AFT CHORD LWR CHECK TO BE OUT OF LIMITS IAW SRM 53-60-71. R & R AFT LOWER CHORD IAW SRM 51-40-02.

Part: FLOOR SUPPORT — DAMAGED (BS 727E-727D) · airframe 47,164 hrs · 26,455 cycles

AFTER REMOVAL OF NR 2 FLOOR PANEL IN AFT PIT, FOUND THE FLOOR SUPPORT, STA 727E, LBL 8 HAS EDGE DAMAGE. ACFT GROUNDED. REPAIRED FLOOR SUPPORT AT STA 727E LBL8 IAW SRM 53 00 53, FIG 201.

Part: FLOOR SUPPORT — DAMAGED (BS 727D-727F) · airframe 47,164 hrs · 26,455 cycles

AFTER REMOVAL OF NR 2 FLOOR PANEL IN AFT CARGO, FOUND THE FLOOR SUPPORT BS 727E, LBL 13 HAS EXTRA HOLES. ACFT GROUNDED. REPAIRED AFT CARGO FLOOR SUPPORT AT BS 727E, LBL 13 IAW SRM 53-00-53-2R-1 AND EA 400-53EA-10321.

Part: SKIN — GOUGED · airframe 47,164 hrs · 26,455 cycles

BS 1022, ABOVE 19L SKIN HAS A SMALL GOUGE. ACFT GROUNDED. REPAIRED SKIN IAW EA 400-53EA-10338.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 47,164 hrs · 26,455 cycles

RT WING INBD FOREFLAP INBD UPPER SURFACE SKIN IS CHAFED. ACFT GROUNDED. REPAIRED CHAFE ON RT WING INBD FOREFLAP, INBD UPPER SURFACE IAW SRM 51-70-10-2R0, REPAIR 4, PARA 20., PG 48.

Part: TRANSITION PANEL — CORRODED (BS 727C-767) · airframe 47,164 hrs · 26,455 cycles

AFTER REMOVAL OF AFT PIT RT SIDEWALL FOUND RT TRANSITION PANEL TO BE CORRODED. ACFT GROUNDED. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-60-53-1A1, FIG 101. REPAIRED TRANSITION PANEL IAW SRM 53-60-53-2R5, W2, O .040, R 0, L 50, D .040.

Part: TRANSITION PANEL — CORRODED (BS 727D-747) · corrosion level 2 · airframe 47,164 hrs · 26,455 cycles

FOUND AFT CARGO LT TRANSITION PANEL TO BE CORRODED. ACFT GROUNDED. REMOVED, FABRICATED AND INSTALLED NEW IAW SRM 53-60-53-2R4.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 47,164 hrs · 26,455 cycles

LEFT WING INBD MIDFLAP UPPER SURFACE IS CHAFED ON INBD END. ACFT GROUNDED. UPON FURTHER INVESTIGATION FOUND CHAFED AREAS TO BE KNIFE EDGE AND OUT OF LIMITS. REMOVED AND FABRICATED AND INSTALLED REPAIR IAW SRM 57-53-01-2R3, FIG 201.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 47,164 hrs · 26,455 cycles

LEFT WING INBD T/E FOREFLAP IS CHAFED ON UPPER SURFACE INBD END. ACFT GROUNDED. REMOVED LT INBD FOREFLAP IAW AMM 27-51-07-004 -001, PG 1, STEPS 2, C4-2.C6B. REPAIRED SURFACE IAW SRM 51-70-10-2R0 REPAIR 4. INSTALLED IAW AMM 27-51-07-404 010, STEPS 3 D 1-10.

Part: SKIN — DENTED (BS 807) · airframe 47,164 hrs · 26,455 cycles

LEFT FUSELAGE BS 807 S21L SKIN DENTED. FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 53-00-01-212-35.

Part: SKIN — SCRATCHED · airframe 47,164 hrs · 26,455 cycles

SCRATCHES ON SKIN BELOW NR 5 EYEBROW WINDOW. REPAIRED SCRATCHES ON SKIN BELOW NR 5 EYEBROW WINDOW IAW ASA EA NR 400, 53EA 10352.

Part: SUPPORT ANGLE — CRACKED (RT WING TE FLAP) · airframe 47,164 hrs · 26,455 cycles

RT UPPER FIXED T/E PANEL INBD OF INBD FLAP HAS SUPPORT ANGLE CRACKED. ACFT GROUNDED. REPAIRED SUPPORT ANGLE IAW EA 5720-01149 REV B, DATE ISSUED 10, APR 08.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 47,164 hrs · 26,455 cycles

LEFT WING OTBD FLAP FOREFLAP OTBD EDGE IS DENTED. ACFT GROUNDED. REPAIRED DENT DAMAGE ON L/W OTBD FOREFLAP ON OTBD EDGE IAW SRM 51-70-10 REPAIR 4, PAR 3, PG 1 PAINT T/U ON SN 5405313, WO 1009728-7400-0021 AP-16 NR 29347, AP-17 ITEM 26.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 63,614 hrs · 40,242 cycles

RT OTBD FORE FLAP OTBD L/E CHAFED. ACFT GROUNDED. R & R WITH NEW DOUBLER IAW SRM 57-53-01-2R-1.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 46,265 hrs · 25,889 cycles

EMERGENCY LIGHT FLOOD LIGHT ON FUSELAGE ADJACENT TO RT AFT OVERWING EXIT HAS ONE LAMP INOPERATIVE. LAMPED AND TESTED IAW MM 33-51-22-962-001. OPS NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 46,265 hrs · 25,889 cycles

EMERGENCY LIGHT RT AFT OVERWING FLOOD LIGHT ON FUSELAGE IS INOP. LAMPED AND TESTED IAW MM 33-51-22-962-001. OPS NORMAL.

Part: COVER — DISLODGED (EMERGENCY LIGHT) · airframe 45,885 hrs · 25,667 cycles

SEAT 17F EMERGENCY LIGHT COVER FELL OFF. REINSTALLED COVER AS REQUIRED.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 60,953 hrs · 33,389 cycles

EXIT SIGN COVER BY L1 MISSING. ACFT GROUNDED. REINSTALLED EXIT SIGN COVER.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 43,940 hrs · 24,493 cycles

RT OUTBOARD AFT FLAP HAS DELAM AT T/E. REPAIRED RT OUTBOARD AFT FLAP T/E IAW B737 400 SRM 51 70 10 REPAIR 4.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 43,940 hrs · 24,493 cycles

RT WING 4 L/E SLAT INBD AFT CORNER UPPER SURFACE HAD DELAMINATION. REPAIRED RT NR 4 L/E SLAT INBD AFT CORNER IAW B737 400 SRM 51 70 10 REP 14.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 43,940 hrs · 24,493 cycles

RIGHT NR 5 L/E SLAT INBD UPPER SURFACE DELAMINATED. REPAIRED RT NR 5 SLAT INBD UPPER SURFACE IAW B737 400 SRM 51 70 10.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 56,850 hrs · 31,990 cycles

FORWARD CARGO SHEAR TIE AT STA 500B BETWEEN STR 28L AND 27L CORRODED. REMOVED CORROSION OUT OF LIMITS. FABRICATED TREATED APPLIED FINISH AND INSTALLED REPAIR PART IAW B737 400 SRM 53 00 07.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,850 hrs · 31,990 cycles

FORWARD CARGO SHEAR TIE AT STA 500A BETWEEN STR 27R AND 28R CORRODED. BLENDED CORROSION OUT OF LIMITS. FABRICATED TREATED APPLIED FINISH AND INSTALLED REPAIR PART IAW B737 400 SRM 53 00 07.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 56,850 hrs · 31,990 cycles

FORWARD CARGO SHEAR TIE AT STA 500 BETWEEN STR 28L AND 28R CORRODED. REMOVED CORROSION OUT OF LIMITS. FABRICATED TREATED APPLIED FINISH AND INSTALLED REPAIR PARTS IAW B737 400 SRM 53 00 07.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 42,418 hrs · 23,621 cycles

EMERGENCY LIGHT EXIT LOCATOR SIGNS AT L1 DOOR RIGHT FORWARD OVERWING EXIT AND RIGHT AFT OVERWING EXIT EACH HAVE MULTIPLE LAMPS INOP. RELAMPED EMERGENCY LIGHT EXIT IDENTIFIERS AT L1 DOOR RT FWD AND RT AFT OVERWING EXITS AND TESTED PER MM 33 51 81 962 011, OPS NORMAL.

Part: SKIN — DENTED (FUSELAGE) · airframe 40,400 hrs · 22,359 cycles

DENT IN SKIN AT BS 1018 AND STR 22 WITHIN 3 INCHES OF BUTT SPLICE. REPAIRED DENTED SKIN IAW EA 14220 AND ASA EA 400 53EA 04351 REV 11/28/10.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,332 hrs · 20,553 cycles

CABIN FRAME CRACKED AT STA 867 BETWEEN STR 8R AND 9R IS CRACKED. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS, INSTALLED PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,332 hrs · 20,553 cycles

CABIN FRAME CRACKED AT STA 380 BETWEEN STR 8R AND 9R IS CRACKED. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS, INSTALLED PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,332 hrs · 20,553 cycles

CABIN FRAME CRACKED AT STA 827 BETWEEN STR 8R AND 9R IS CRACKED. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS, INSTALLED PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,332 hrs · 20,553 cycles

CABIN FRAME CRACKED AT STA 787 BETWEEN STR 8L AND 9L. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS, INSTALLED PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,332 hrs · 20,553 cycles

CABIN FRAME CRACKED AT STA 787 BETWEEN STR 8L AND 9L. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS, INSTALLED PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,332 hrs · 20,553 cycles

CABIN FRAME CRACKED AT STA 827 BETWEEN STR 8L AND 9L. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS, INSTALLED PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,332 hrs · 20,553 cycles

CABIN FRAME CRACKED AT STA 867 BETWEEN STR 8L AND 9L IS CRACKED. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS, INSTALLED PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,332 hrs · 20,553 cycles

CABIN FRAME CRACKED AT STA 907 BETWEEN STR 8R AND 9R. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS, INSTALLED PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,332 hrs · 20,553 cycles

FRAME CRACKED AT STA 360 BETWEEN STR 8L AND 9L. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS, INSTALLED PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,332 hrs · 20,553 cycles

CABIN FRAME CRACKED AT STA 907 BETWEEN STR 8L AND 9L. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS, INSTALLED PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,332 hrs · 20,553 cycles

CABIN FLOORBEAM STA 986.5 HAS AREAS OF CORROSION RBL 60 TO LBL 60. REPAIRED FLOORBEAM IAW EA.

Part: RIB — CRACKED (LT WING) · airframe 37,332 hrs · 20,553 cycles

LEFT WING INSIDE FUEL TANK ON RIB LOWER CHORD AT WBL 135.5 BETWEEN STRINGERS 2 & 3 IS CRACKED. REPAIRED RIGHT WING LOWER CHORD IAW EA.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 37,332 hrs · 20,553 cycles

CREASE IN FUSELAGE SKIN STA 807 827 STR 26R. REPAIRED DENT BY INSTALLING DOUBLER TRIPLER AND FILLER.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,332 hrs · 20,553 cycles

R1 DOOR MOP SILL CORRODED. REPAIRED R1 DOOR MOP SILL IAW EA.

Part: RIB — CRACKED (RT WING) · airframe 37,332 hrs · 20,553 cycles

RIGHT WING INSIDE FUEL TANK ON RIB LOWER CHORD AT WBL 135.5 BETWEEN STRINGERS 2 & 3 IS CRACKED. REPAIRED RIGHT WING LOWER CHORD IAW EA.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 37,332 hrs · 20,553 cycles

AFT PIT CARGO DOOR CUTOUT FWD REVEAL UNDERLYING INTERCOSTAL CORRODED STA 787 794 STRINGER 25R. FABBED INTERCOSTAL.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,332 hrs · 20,553 cycles

Z-CHANNEL AT STA 990 LBL 33 LBL 45 IS CORRODED. REMOVED DAMAGED CHANNEL, FABBED REPLACEMENT PART AND INSTALLED REPLACEMENT PARTS.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 37,332 hrs · 20,553 cycles

INTERCOSTAL BETWEEN STA 328 TO 340 AT LBL 44 IS CRACKED. REMOVED DAMAGED AREA, FABBED REPAIR PARTS AND INSTALLED REPAIR.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 37,332 hrs · 20,553 cycles

INTERCOSTAL BETWEEN STA 312 328 AT LBL 44 IS CRACKED. REMOVED DAMAGED AREA, FABBED REPAIR PARTS AND INSTALLED REPAIR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,332 hrs · 20,553 cycles

FLOORBEAM AT STA 986 AND LBL 20 CORRODED. REPAIRED FLOORBEAM IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 37,332 hrs · 20,553 cycles

FOUND CORROSION ON FLOOR STRUCTURE SUPPORT. REMOVED AND REPLACED FLOOR STRUCTURE SUPPORT.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,332 hrs · 20,553 cycles

CABIN FLOORBEAM AT STA 312 AND RBL 8 CORRODED. REPAIRED FLOORBEAM IAW SRM.

Part: FITTING — CORRODED (FUSELAGE) · airframe 37,332 hrs · 20,553 cycles

UPON REMOVAL OF STIFFENER FOUND CLIP CORRODED AT BS 797 STR 27R. REMOVED DAMAGED CLIP FABBED PART AND INSTALLED PART.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,332 hrs · 20,553 cycles

FRAME AT BS 807 STR 25L IN AFT PIT IS CORRODED. REMOVED DAMAGED AREA, FABBED REPAIR PARTS AND INSTALLED REPAIR.

Part: DOUBLER — DEBONDED (SPOILER) · airframe 37,332 hrs · 20,553 cycles

NR 3 SPOILER LOWER INBOARD END REPAIR DOUBLER DISBONDED AT TRAILING EDGE AT RADIUS AT FWD END I/B CORNER. REMOVED PREVIOUS REPAIR, SPOILER TO BE NON-REPAIRABLE, REPLACED SPOILER WITH SERVICEABLE PART.

Part: SKIN — DENTED (FUSELAGE) · airframe 37,332 hrs · 20,553 cycles

RT EXTERNAL FUSELAGE SKIN DENTED AT STA 309 BETWEEN STR 23R 24R. REMOVED DAMAGED AREA, FABBED FILLER AND DOUBLER AND INSTALLED REPAIR.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,332 hrs · 20,553 cycles

AFT PIT STIFFENER ANGLE ON 797 STUB FRAME CORRODED 25R 27R. REMOVED ANGLE, FABBED REPLACEMENT PART AND INSTALLED PARTS.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 37,332 hrs · 20,553 cycles

AFT PIT INTERCOSTAL UPPER FLANGE CORRODED STA 767 STR 252R. REMOVED INTERCOSTAL, FABBED REPLACEMENT PART AND INSTALLED.

Part: STRAP — CORRODED (FUSELAGE) · airframe 37,332 hrs · 20,553 cycles

AFT PIT STRAP CORRODED 757 847 ABOVE STR 25R. REMOVED STRAP, FABBED REPLACEMENT PART AND INSTALLED.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,332 hrs · 20,553 cycles

AFT PIT STIFFENER ANGLE ON 797 STUB FRAME CORRODED STR 25R 27R. REMOVED ANGLE, FABBED REPLACEMENT PART AND INSTALLED.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,332 hrs · 20,553 cycles

L2 DOOR MOPSILL IS CORRODED. REMOVED CORRODED MOPSILL AT L2 DOOR AND INSTALLED A NEW MOPSILL.

Part: TRANS PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,332 hrs · 20,553 cycles

LEFT TRANSITION PANEL AT STA 947.5 ABOVE STR 25L IS CORRODED. REMOVED DAMAGED AREA, FABBED REPLACEMENT PART AND INSTALLED REPAIR.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,332 hrs · 20,553 cycles

FRAME CRACKED AT STA 727D BETWEEN STR 8R AND 9R. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS, INSTALLED PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,332 hrs · 20,553 cycles

FRAME CRACKED AT STA 480 BETWEEN STR 8R AND 9R. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS, INSTALLED PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,332 hrs · 20,553 cycles

FRAME AT STA 400 BETWEEN STR 8R AND STR 9R IS CRACKED. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS, INSTALLED PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,332 hrs · 20,553 cycles

CABIN FRAME CRACKED AT STA 400 BETWEEN STR 8L AND 9L IS CRACKED. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS, INSTALLED PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,332 hrs · 20,553 cycles

FRAME CRACKED AT STA 747 BETWEEN STR 8R AND 9R. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS, INSTALLED PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,332 hrs · 20,553 cycles

FRAME CRACKED AT STA 440 BETWEEN STR 8L AND 9L. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS, INSTALLED PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,332 hrs · 20,553 cycles

FRAME CRACKED AT STA 727F BETWEEN STR 8L AND 9L. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS, INSTALLED PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,332 hrs · 20,553 cycles

FRAME CRACKED AT STA 747 BETWEEN STR 8L AND 9L. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS, INSTALLED PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,332 hrs · 20,553 cycles

CABIN FRAME CRACKED AT STA 827 BETWEEN STR 8L AND 9L. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS, INSTALLED PER EA.

Part: SKIN — DENTED (SPOILER) · airframe 37,332 hrs · 20,553 cycles

NR 8 SPOILER HAS 2 EACH DENTS ON LOWER SURFACE .013 X.5 AND .004 X.3. REMOVED DAMAGED AREA, FABRICATED DOUBLER BONDED REPAIR.

Part: SKIN — DENTED (SPOILER) · airframe 37,332 hrs · 20,553 cycles

NR 3 SPOILER LOWER SURFACE HAS 5 DENTS JUST AFT OF OUTBOARD END. REMOVED DAMAGED AREA, FABRICATED REPAIR PART, BONDED REPAIR.

Part: SKIN — DENTED (SPOILER) · airframe 37,332 hrs · 20,553 cycles

NR 6 SPOILER HAS 2 DENTS ON LOWER SURFACE OUTBOARD END. REMOVED DAMAGED AREA, FABRICATED FILLER AND DOUBLER BONDED REPAIR.

Part: SKIN — DAMAGED (ELEVATOR TAB) · airframe 37,332 hrs · 20,553 cycles

LEFT ELEVATOR TAB I/B HINGE CUTOUT FIBER IS DAMAGED. PREPPED AND REPAIRED DAMAGE ON LEFT ELEVATOR HINGE TAB.

Part: INDICATOR — MALFUNCTIONED (TE FLAPS) · airframe 34,808 hrs · 19,036 cycles

ON APPROACH WHEN CONFIGURING WITH FLAP 1 AT YAK FLAP INDICATOR STAYED UP AND LED "LED FLAP EXT" LIGHT WAS GREEN. ACFT DIVERTED TO ANC PER MX AND DISPATCH. AT ANC SAME CONDITION ALTERNATE FLAP OPERATION DID NOT WORK. LANDED WITH ZERO T/E FLAPS. FOUND T/E POSITION C/B OUT. RESET C/B PER RESET PROCEDURE. L/E & T/E FLAP OPERATION AND INDICATION OPS CKS NORMAL. SUSPECT DURING F/O'S SHOULDER HARNESS RELEASE BELT CLIP TRIPPED C/B.

Part: SKIN — CRACKED (KRUEGER FLAP) · airframe 34,063 hrs · 18,628 cycles

RT WING NR 3 K FLAP LEADING EDGE GOUGED ON EXTERIOR 5.5 INCHES FROM LEADING EDGE AND 13.2 INCHES FROM IB END VERIFIED CRACK IN GOUGE STOP DRILLED CRACK. FABRICATED AND INSTALLED DOUBLER IAW B737 400 SRM 57 43 02 FIG 201 REPAIR 2.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 34,063 hrs · 18,628 cycles

LT WING UPPER OTBD FORE FLAP DENT WITH DELAMINATION ON UPPER SURFACE 63 INCHES FROM INBD SIDE. PREPARED DAMAGED AREA FABRICATED DOUBLER AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 2.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 34,063 hrs · 18,628 cycles

LEFT WING INBOARD AFT FLAP OUTBOARD LOWER CORNER DELAMINATED. REMOVED DAMAGED AREA. PREPARED FABRICATED FILLER SKIN DOUBLER AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 4.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 34,063 hrs · 18,628 cycles

LT WING INBOARD FORE FLAP UPPER SURFACE HAS 4 EACH DENTS 15 INCHES FROM O BEND PREPARED DAMAGED AREA. FABRICATED DOUBLER AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 2.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 34,063 hrs · 18,628 cycles

LEFT WING OUTBOARD AFT FLAP LOWER SURFACE HAS 2 EACH DENTS 20 INCHES FROM INBOARD END AND 6 INCHES FROM TRAILING END PREPARED DAMAGED AREA. FABRICATED DOUBLER AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 2.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 34,063 hrs · 18,628 cycles

LT WING INBD FORE FLAP LOWER SURFACE HAS NUMEROUS SMALL DENTS BETWEEN 1ST AND 2ND TRACK. PREPARED DAMAGED AREA FABRICATED DOUBLER AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 2.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 34,063 hrs · 18,628 cycles

RIGHT INBOARD FORE FLAP LOWER SURFACE 3 EACH SMALL PUNCTURES AT CENTER TRACK AREA PREPARED DAMAGED AREA. FABRICATED FILLER AND REPAIR DOUBLER AND BONDED IAW B737 400 SRM 51 70 10 REPAIR NR 2.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 34,063 hrs · 18,628 cycles

LT WING INBD FORE FLAP HAS 8 EA SMALL DENTS ON LOWER SURFACE NEAR 2ND TRACK OTBD. PREPARED DAMAGED AREA FABRICATED DOUBLER AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 2.

Part: WEDGE — CHAFED (NR 4 SLAT) · airframe 34,063 hrs · 18,628 cycles

RIGHT WING NR 4 SLAT TRAILING EDGE WEDGE LOWER SURFACE CHAFED THROUGH IN TWO PLACES ON AFT EDGE ONE EACH AT INBOARD AREA AND 1 EACH AT ACTUATOR AREA. PREPARED DAMAGED AREA. FABRICATED FILLERS AND DOUBLERS AND BONDED IAW B737 400 SRM 51 70 10 REPAIR NR 4.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 34,063 hrs · 18,628 cycles

LEFT WING INBOARD MID FLAP UPPER SKIN CHAFED AT INBOARD END CUT OUT DAMAGED AREA. FABRICATED REPAIR PARTS AND INSTALLED IAW B737 400 SRM 57 53 01 FIG 201 REPAIR 3.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 34,063 hrs · 18,628 cycles

LEFT OUTBOARD AFT FLAP LOWER SURFACE CHAFED 58 INCHES FROM OUTBOARD END PREPARED DAMAGED AREA. FABRICATED DOUBLER AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 2.

Part: SKIN — DAMAGED (RT WING TE FLAP) · airframe 34,063 hrs · 18,628 cycles

RIGHT OUTBOARD AFT FLAP UPPER SURFACE TRAILING EDGE DAMAGED 47.5 INCHES FROM OUTBOARD END PREPARED DAMAGED AREA. FABRICATED FILLER AND DOUBLER IAW B737 400 SRM 51 70 10 REPAIR 2.

Part: SKIN — DENTED (NR 4 SPOILER LT) · airframe 34,063 hrs · 18,628 cycles

LT WING NR 4 SPOILER LOWER SURFACE HAS 8 EACH SMALL DENTS AT INBOARD END. PREPARED DAMAGED AREA, FABRICATED DOUBLER FILLER AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 4.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 34,063 hrs · 18,628 cycles

RIGHT OUTBOARD AFT FLAP FORE FLAP OUTBOARD LEADING EDGE CHAFED PREPARED DAMAGED AREA BY BLENDING. FABRICATED REPAIR DOUBLER AND INSTALLED IAW B737 400 SRM 57 53 01 FIG 201 REPAIR 1.

Part: SKIN — DENTED (NR 1 SPOILER LT) · airframe 34,063 hrs · 18,628 cycles

LT WING NR 1 SPOILER UPPER SURFACE DENTED 12 INCHES FROM T/E AND 10 INCHES FROM OUTBOARD END. PREPARED DAMAGED AREA, FABRICATED DOUBLER AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 2.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 34,063 hrs · 18,628 cycles

LEFT WING OUTBOARD AFT FLAP DENTED ON LOWER SURFACE 46 INCHES FROM OUTBOARD END AND 4 INCHES FROM TRAILING EDGE. PREPARED DAMAGED AREA FABRICATED DOUBLER AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 2.

Part: SKIN — DENTED (NR 4 SPOILER LT) · airframe 34,063 hrs · 18,628 cycles

LT WING NR 4 SPOILER LOWER SURFACE ABOVE INBD ACTUATOR HAS 8 EACH SMALL DENTS NEAR TRAILING EDGE. PREPARED DAMAGED AREA, FABRICATED DOUBLER FILLER AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 4.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 34,063 hrs · 18,628 cycles

LEFT WING OUTBOARD AFT FLAP HAS 3 EACH DENTS ON LOWER SURFACE 9 INCHES FROM INBOARD END AND 4 INCHES FROM TRAILING EDGE. PREPARED DAMAGED AREA FABRICATED DOUBLER AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 2.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 34,063 hrs · 18,628 cycles

RIGHT WING INBOARD MID FLAP UPPER SKIN CHAFED AT INBOARD END WITH A DENT CUT OUT DAMAGED AREA. FABRICATED REPAIR PARTS AND INSTALLED IAW B737 400 SRM 57 53 01 FIG 201 SHEET 2 OF 3 REPAIR 2.

Part: ATTACH FITTING — CRACKED (O2 MASKS) · airframe 30,281 hrs · 16,571 cycles

DURING C-CHECK MAINTENANCE FOUND RELEASE CBL LANYARD ATTACH EYELET ON SEVERAL O2 MASK ASSYS CRACKED/BROKEN, WHICH IN THE EVENT OF CABIN DEPRESSURIZATION AND MASK DEPLOYMENT WOULD PREVENT THE O2 GENERATOR RELEASE PIN FROM BEING PULLED. INSPECTION CARRIED OUT ON ALL PSU O2 MASK ASSYS. ALL O2 MASK ASSYS IDENTIFIED AS UNSERVICEABLE WERE REPLACED WITH SERVICEABLE ASSYS.

Part: FRAME — DENTED (BS 767 S25R) · airframe 26,477 hrs · 14,533 cycles

FOUND FRAME AT BSTA 767 STR 25R IS DENTED. DENTED FRAME REPAIRED PER SRM 53 00 07 FIG 201.

Part: SUPPORT — CHAFED (RT OB TE FLAP) · airframe 26,477 hrs · 14,533 cycles

RT OB FLAP I B ROLLER SUPPORT CHAFING. RT OB FLAP IB ROLLER SUPPORT REPLACED WITH NEW ONE IAW SRM 51 40 02 PARA 7A.

Part: FRAME — DENTED (BS 727G S25R) · airframe 26,477 hrs · 14,533 cycles

FOUND FRAME AT BS 727G STR 25R IS DENTED. REPAIRED PER SRM 51 70 11 FIG 1.

Part: SUPPORT — CHAFED (FLAP ROLLER) · airframe 26,477 hrs · 14,533 cycles

RT OUTBD FLAP INBD ROLLER SUPPORT CHAFING. RT OUTBD FLAP INBD ROLLER SUPPORT REPLACED WITH NEW PART PER SRM 51 40 02 PARA A7A.

Part: SKIN — WORN (BS 860-875) · airframe 26,477 hrs · 14,533 cycles

FUSELAGE SKIN WORN AT BS 860-875 AT DORSAL FIN RT SEAL CONTACT AREA. REPAIRED PER EM 5520 01068.

Part: DUCT — CORRODED (TOILET DRAIN) · corrosion level 2 · airframe 26,477 hrs · 14,533 cycles

FUSELAGE LWR LOBE INTERIOR RT SIDE TOILET DRAIN DUCT OUTLET DOUBLER CORRODED. PAN ASSY REPLACED PER SRM 51 40 02.

Part: FRAME — DENTED (BS 907) · airframe 26,477 hrs · 14,533 cycles

DENT IN FRAME. DENT REPAIRED IAW SRM 5 00 07 FIG 201 REPAIR 1 AND ERO 5523.

Part: FAILSAFE — CORRODED (BS 795) · airframe 26,477 hrs · 14,533 cycles

FAILSAFE AT BS 795.5 AND STR 26R HAS CORROSION. FAILSAFE REPLACED IAW SRM 51 30 01 AND 51 40 02.

Part: SKIN — DENTED (BS 1040) · airframe 26,477 hrs · 14,533 cycles

FOUND FUSELAGE SKIN AT BSTA 1040 TO 6" AFT BL 0 LWR FUSELAGE AT AFT PRESURE BULKHEAD DENTED. DENT REPAIRED IAW SRM 53 80 01 FIG 201 REPAIR 3.

Part: SKIN — LIGHTNING STRIKE (BS 360) · airframe 26,477 hrs · 14,533 cycles

YXX- LIGHTING STRIKE AT BS 360, STR 22R. LIGHTING STRIKE REPAIRED IAW B737-400 SRM 53-00-01 FIG 201 REPAIR 19.

Part: SKIN — LIGHTNING STRIKE (BS 227) · airframe 26,477 hrs · 14,533 cycles

YXX- LIGHTNING STRIKE AT BSTA 227, BETWEEN STR 22R AND 23R. LIGHTNING STRIKE REPAIRED IAW B737-400 SRM 53-00-01 FIG 201, REPAIR 19.

Part: SKIN — LIGHTNING STRIKE (BS 340) · airframe 26,477 hrs · 14,533 cycles

YXX- LIGHTING STRIKE FOUND AT BSTA 340 BETWEEN STR 21 AND 22 RT. LIGHTING STRIKE REPAIRED IAW B737-400 SRM 53-00-01, FIG 201.

Part: SKIN — LIGHTNING STRIKE (BS 400) · airframe 26,477 hrs · 14,533 cycles

YXX- LIGHTING STRIKE AT BS 40O BETWEEN STR 20 AND 21R. LIGHTING STRIKE AT BS 400, BETWEEN STR 20 AND 21 RT REPAIRED IAW B737-400 SRM 53-00-01 FIG 201.

Part: SKIN — LIGHTNING STRIKE (BS 385) · airframe 26,477 hrs · 14,533 cycles

LIGHTING STRIKE AT BSTA 385 BETWEEN STR 21 AND 22 R/H. LIGHTING STRIKE REPAIRED AT BSTA 385 BETWEEN STR 21 AND 22 RT REPAIRED IAW B737-400 SRM 53-00-01 FIG 201.

Part: SKIN — LIGHTNING STRIKE (BS 385) · airframe 26,477 hrs · 14,533 cycles

YXX- LIGHTING STRIKE AT BS 385, BETWEEN STR 21 AND 22 RT. LIGHTING STRIKE AT BS 385 BETWEEN STR 21 AND 22 RT REPAIRED PER B737-400 SRM 53-00-01.

Part: SKIN — LIGHTNING STRIKE (BS 296) · airframe 26,477 hrs · 14,533 cycles

YXX- LIGHTNING STRIKE FOUND AT BSTA 296 AND STR 22R. LIGHTNING STRIKE REPAIRED IAW B737-400 SRM 53-00-01 FIG 201.

Part: SKIN — LIGHTNING STRIKE (FUSELAGE) · airframe 26,477 hrs · 14,533 cycles

LIGHTING STRIKE AT BSTA 320 BETWEEN STRINGER 21R AND 22R. LIGHTING STRIKE REPAIRED IAW SRM 53-00-01, FIG 201, REPAIR 19.

Part: SKIN — LIGHTNING STRIKE (BS 274) · airframe 26,477 hrs · 14,533 cycles

YXX- LIGHTING STRIKE FOUND AT BSTA 274 AND STR 22RT. LIGHTING STRIKE REPAIRED IAW B737-400 SRM 53-00-01 FIG 201.

Part: SKIN — LIGHTNING STRIKE (BS 440) · airframe 26,477 hrs · 14,533 cycles

YXX- LIGHTNING STRIKE AT BS 440 BETWEEN STR 19 AND 20 RT. LIGHTING STRIKE REPAIRED IAW B737-400 SRM 53-00-01 FIG 201.

Part: SILL — CORRODED (FUSELAGE)

YXX - FOUND L2 DOOR ENTRY AREA SILL PLATE CORRODED BEYOND LIMITS. REPLACED WITH FABRICATED PART, BOEING P/N 65-125 NOT PROCURABLE IAW B737-400 SRM 51-30-01. (M)

Part: SILL — CORRODED (FUSELAGE)

YXX - FOUND R2 DOOR ENTRY SILL PLATE CORRODED. REPLACED IAW B737-400 SRM 51-40-02 FIG 3 PARAGRAPH 7D. (M)

Part: SKIN — TORN (FUSELAGE)

ANC - REFUEL TRUCK HIT RT SIDE OF AIRCRAFT. PERFORMED A SRM REPAIR IAW DETAIL 12 AND EA CARGO HOLD. (K)

Part: STOP FITTING — CRACKED (R1 DOOR) · airframe 24,297 hrs · 13,295 cycles

R-1 DOOR STOP FITTING CRACKED. REMOVED AND REPLACED DOOR. (K)

Part: SKIN — DENTED (FUSELAGE)

SEA - FOUND DENT AT BS 787 STRINGER 27L TO 27R. DENT IS OUT OF LIMITS IAW WITH THE 737 SRM 53-00-01 FIG 101. DENT IS COMMON TO A STRINGER A=4, Y=.126, A/Y=31.75. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR FILLER AND DOUBLER IAW ASA EA 5330-01929 AND AAR EA 10927. (M)

Part: SKIN — DENTED (SPOILER)

SEA - DENT ON BOTTOM OF INBOARD SPOILER ON AFT EDGE AFT OF INBOARD ACTUATOR A=.250, Y=.027, A/Y=9.25. OUT OF LIMITS PER B737 SRM 57-50-01. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR FILLER AND DOUBLER IAW B737 SRM 51-70-10 REPAIR 21. (M)

Part: PAD — DISLODGED (L2 DOOR)

SEA - DURNG A ROUTINE FLIGHT ATTENDANT TRAINING CAMP, THE L2 DOOR SLIDE FAILED TO COMPLETELY INFLATE. UPON INVESTIGATION IW WAS NOTED THAT THE AIRCRAFT DOOR PAD WAS TAPED TO THE SIDE OF THE AIRCRAFT, THE TAPE ITSELF WAS OF POOR QUALITY AND INSUFFICIENT SIZE TO HOLD THE PAD IN PLACE. THIS ALLOWED THE PAD TO BE SUCKED INTO THE ASPIRATOR, BLOCKING THE AIR FROM ENTERING THE SLIDE. USE BAG PIT TAPE WHICH IS WIDER AND MORE ADHESIVE TO ATTACH PAD TO AIRCRAFT. (M)

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT)

PDX - DURING MAINTENANCE CHECK, FOUND FORWARD EMERGENCY FLOOR TRACK LIGHT INOPERATIVE. RECONNECTED WIRE. LIGHT THEN OPERATED NORMALLY. (M)

Part: LIGHT — INOPERATIVE (AFT CABIN)

SEA - DURING LINE CHECK, FOUND EMERGENCY TRACK LIGHT IN AFT CABIN INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMBLY OPERATIONAL CHECK GOOD. (M)

Part: SKIN — GOUGED (FUSELAGE)

PAE - DURING C-CHECK, FOUND EXTERNAL SKIN GOUGED AT BS 494 AND STRINGER 21-22. REPAIRED IAW EA. (M)

Part: WIRE — DISCONNECTED (ROWS 14 - 15)

SEA - PRIOR TO FLIGHT 496, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 14 AND 15 WERE FOUND TO BE INOPERATIVE. RECONNECTED LOOSE WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: BOTTLE — LEAKING (ESCAPE SLIDE)

PDX - DURING MAINTENANCE CHECK, THE R2 DOOR EVAC SLIDE GAUGE WAS FOUND TO BE IN THE RED. REPLACED THE R2 DOOR EVAC SLIDE. AIR CRUISERS INSPECTED THE BOTTLE AND FOUND IT TO BE LEAKING FROM THE GAUGE ADAPTER O-RING. REPAIRED BY AIR CRUISERS, REFILLED, LEAK CHECK GOOD. (M)

Part: SEAL — OUT OF POSITION (R1 DOOR)

SNA - FLT 413, PRIOR TO FLIGHT, THE R1 DOOR WAS FOUND TO BE BINDING AND WAS DIFFICULT TO CLOSE. CONTRACT MAINTENANCE INSPECTED AND FOUND THAT THE DOOR SEAL HAD COME OUT OF TRACK. REINSTALLED DOOR SEAL INTO TRACK AND DOOR OPERATED NORMALLY. (M)

Part: SLIDE — PRESSURE LOW (L2 DOOR)

PAE - DURING MAINTENANCE CHECK, THE L2 DOOR EVACUATION SLIDE BOTTLE PRESSURE WAS FOUND TO BE LOW. REPLACED EVACUATION SLIDE AND ROUTED TO ASA SLIDE SHOP WHERE THE BOTTLE WAS REPLACED. (M)

Part: SNAP-RING — DETACHED (L1 DOOR)

JNU - UPON ARRIVAL OF FLIGHT 62, THE L1 DOOR WOULD NOT OPEN. INSPECTED DOOR AND FOUND THE SNAP-RING DETACHED ON THE UPPER HINGE DOOR RELEASE MECHANISM. REINSTALLED SNAP-RING AND DOOR OPERATED NORMAL. (M)

Part: LIGHT — INOPERATIVE (CABIN)

PDX - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROWS 14-18. RECONNECTED LIGHTS/WIRING AND LIGHTS OPERATED NORMALLY. (X)